unclassified n hhhmehmhh hhhhhhhmmmmmhh … · i hhhhhhhhhhhhh. llyel%' avradcom ",- 4/...
TRANSCRIPT
L AD-AI05 516 GENERAL ELECTRIC CO BIN4ANTON N Y AIRC RAFT EUPETDVF9IELECTRONIC MASTER MONITOR AND ADVISORY DISPLAY SYSTEM. OPERATIO--ETCCU)OCT 80 OAAKSO-79..C-0270
UNCLASSIFIED ACS-,2-21? USAAVRAOCMTR79-070-2 N-3 MENOhhhMlEhhhMEhmhh
hhhhhhhmMMMmhhI hhhhhhhhhhhhh
LLYEL%'AVRADCOM ",- 4/
Technical Report - 79-0270-2
0 1 ELECTRONIC MASTER MONITOR AND ADVISORY DISPLAY SYSTEM,OPERATIONAL FUNCTIONS REPORT
GENERAL ELECTRIC COMPANYI AIRCRAFT EQUIPMENT DIVISION 2-
BINGHAMTON, NY 13902
I OCTOBER 1980SECOND INTERIM REPORT FOR PERIOD COVERING JUN 79- OCT 80
I DTICDISTRIBUTION STATEMENT ELECTEfApproved Ior public release:isribtion unliit. O CT 7 19 81 ;
PREPARED FOR: B
I AVIONICS R&D ACTIVITY
.8Research and Development Technical Report
6L- Aviation Research and Development Command
• -6 .q' ,.* t
UNCLASSIFIEDSECURITY CL SFICATION OF THIS PAGE (Whoe Date ffntor.41
1 7 REPORT DCUMENTATION PAG~E READ DiSTRUCTIONSII MNI ~BEFORE COMPLETIG FORM
1. REPRTUMR"F2 GOT ACCESSION No. 3. RECIPIENT SATAL0G NUMBER
TITLE (ad &ua) *-- 5. TYPE OF REPORT &PERIOD COVERED
Electronic Master Monitor and Advisory Dipa R&D June 79 - Oct 805System, Operational F'unctions Reporh ______________
9 . PERFORMING ORGANIZATION NAME AND ADDRESS 10. P GRA EMET. PROJECT, TASK
General Electric Co. L 20AH8T3121Aircraft Equipment Division F ,12620-A8 0-23Binghamnton. NY__13902 _____________
1t. CONTROLLING OFFICE NAME AND ADDRESS 12. EPRDATE
Avionics R&D Activity j Oct 80jCommunications, Sensors, Instrumentation Div. 19NUBR5 FPAE
14 .W.'w. .~ ADOVWS"ffOftrnfte~Mb~f~ Office) 15. SECURITY CLS &%~epm,-
-77 UNCL ~;?9
I~t~ns~lwwTow 4?TUUUN*E .DECLASSIFICATION DWNGRADING
Approved for public release, distribution unlimited.
17. DISTR1SUTION STATEMENT (of the abstract entered In Block 2,If different f,.., Report)
IS. SUPPLEMENTARY NOTES
It. KEY WOROS (Con*Im. on reverse side it necesaran id datlf by block rnibwr)
Aircraft, Subsystems, Advisory displays,
This includes ray data, discrete and sumary status information related tothe engine, transmission, rotor, fuel, hydraulic and electrical subsystems.This report describes the results of work done under Task I of contract No.DAAK 80-79-C-0270, to establish basic system operating requirements for an
4 Electronic Master Monitor and Advisory Display System (DIMADS). This system
WO I =M7W3 mmna w @ ta $11 isSO6LETR UNCLASSIFIEDS9CUSIT CLASUFICATIOW OF TWOS PA1111 (Mbut Data So
S1CURITY CLASSIFICATION OF THIS PAGE(Wlmm Date Entered,
lock 20, cont'd
is being developed for use on U.S. Army helicopters to reduce crew workloadby assuming responsibility for tasks associated with subsystem status monitor-ing. EMMADS will integrate all instrumentation normally dedicated to sub-system status monitoring (eog. all pressures, temperatures, etc.) plus caution/warning/advisory indicators, into a computer controlled, solid state system.It will detect, analyze and provide emergency checklists for any faults thatit is programmed to monitor for in these subsystems. This report representsa tieing together of Tasks I & II to provide a baseline for defining therequirements of the feasibility demonstration hardware. In Task 1, helicoptersrepresenting all operational helicopter categories (cargo, utility, scout, andattack) were identified and a signal analysis was done on each. While theEMMADS functions described in this report are applicable to all helicoptercategories studied under Tasks I & II, specific examples used herein are allrelated to the CH-47C helicopter, since this aircraft had been selected asthe basis for the EMMADS feasibiltty model.
SECURITY CLASSIPICATION OF THIS PA*K(tfmea Da*a Zate'me
TABLE OF CONTENTS
Section Page
GLOSSARY OF ABBREVIATIONS ........................ iii
1.0 SCOPE ............................................ 1
2.0 APPLICABLE DOCUMENTS ............................. 3
3.0 EMMADS CHARACTERISTICS ........................... 4
3.1 System Overview ............................. 4
3.2 System Functions ............................ 4
3.2.1 Primary Functions .................... 7
3.2.1.1 Display Areas ............... 7
3.2.1.2 Fault Detection ............. 9
3.2.1.3 Fault/Parameter Display ...... 11
3.2.1.4 Multilegend Display
Switch (MLDS) Operation ...... 25
3.2.1.5 Emergency Action Check-
Lists ....................... 31
3.2.2 System Secondary Functions ........ 38
3.2.2.1 Routine Checklists ...... 38
3.2.2.2 Performance Calculations. 46
3.2.2.3 Maintenance Data Summary. 46
APPENDIX
1 Subsystem Parameter Data Lists ................. 48
2 Fault/Parameter Matrix ....................... 170
3 Fault/Advisory List ............................ 177
4 Routine Checklists ............................. 178
mn - , i
m • '.* - -
LIST OF ILLUSTRATIONS
Figure Page
1 EMMADS Block Diagram ........................... 5
2 Display Unit Areas .............................. 8
3 Sample Display Format - No Faults ............... 19
4 Sample Display Format - Fault Detected ......... 20
5 Sample Display Format - Warning Acknowledged
Checklist Displayed ......................... 226 Sample Display Format - Fault Acknowledged,
Checklist Displayed ......................... 237 MLDS Functions - Subsystem Information Level 27
8 MLDS Operation - Format Level Selection ........ 28
9 ALDS Operation - Routine Checklists Level ...... 29
10 Normal Operational State Sequence .............. 40
1i Sample Display Format - Full Page Checklist .... 43
LIST OF TABLES
Table Page
1 Fault Prioritization for the CH-47C Helicopter . 13
2 Switch Legend Descriptions ..................... 33
3 CH-47C Emergency Action Checklists .............. 364 CH-47C Routine Checklists and
Modification Parameters ...................... 39
ii
GLOSSARY OF ABBREVIATIONS
AC - Alternating Current
ACK - Acknowledge
Aft Vert Thrust - Aft Vertical Thrust Bearing
Brng
AGB - Accessory Gear Box
APU - Auxiliary Power Unit
aux - auxiliary
bst - boost0C - degrees Celsius
Cond lever - Condition lever
CRSE - cruise
CTRL (or CTL) - Control
DC - Direct Current
ELEC - Electrical
EMMADS - Electronic Master Monitor and Advisory
Display System
ENG - Engine
exh - exhaust
ext - external
fwd - forward
gen - generator
HIT - Health Indicator Test
hyd (or HYDR) - hydraulic
lndg - landing
MISC - Miscellaneous Accession For
MLDS - Multilegend Display Switch NTIS GRA&I
DTIC TAB 5
N1 - engine gas producer speed Unannclfced 0
N2 - engine power turbine speednorm - normal -..--OVSP - Overspeed --Distribution/ . .
Avniltbillty Codes
Avail nnd/orDist : pnclal
- : ' ' ' "" ' I _ I I I IA ,
GLOSSARY OF ABBREVIATIONS (CONT)
pos - position
press (or prs) - pressure
proc - procedure
PTIT - Power Turbine Inlet Temperature (same as TGT)
qty - quantity
ref - reference
rel - release
rt - right
RTU - Remote Transmission Units
rpm - revolutions per minute
SAS (or Stab Aug) - Stability Augmentation System
STAT - Status
sw - switch
TBD - To Be Determined
TBS - To Be Specified
temp - temperature
TGT - Turbine Gas Temperature (same as PTIT)
X-feed - cross feed
X-tie - cross tie
XMSN - transmission
iv
__ii I I7r~ IIIII --
1.0 SCOPE
This report describes the results of work done under Task I of
contract No. DAAK 80-79-C-0270, to establish basic system
operating requirements for an Electronic Master Monitor and
Advisory Display System (EMMADS). This system is being developed
for use on U.S. Army helicopters to reduce crew workload by
assuming responsibility for tasks associated with subsystem
status monitoring. EMMADS will integrate all instrumentation
normally dedicated to subsystem status monitoring (e.g. all
pressures, temperatures, etc.) plus caution/warning/advisory
indicators, into a computer controlled, solid state system. It
will detect, analyze and provide emergency checklists for any
faults that it is programmed to monitor for in these subsystems.
While this report is being identified with Task I elements of the
contract, it in fact also represents a tieing together of Tasks I
& II to provide a baseline for defining the requirements of the
feasibility demonstration hardware of Task IV. In Task I,
helicopters representing all operational helicopter categories
(cargo, utility, scout and attack) were identified and a signal
analysis was done on each. The results of the analyses for these
aircraft (CH-47C, UH-60A, OH-58C and YAH-64 respectively) are in
the form of Subsystem Parameter Data Lists, shown in Appendix 1.
Under Task II, surveys of pilots were made to determine when and
how information should be displayed (see EMMADS Human Engineering
Summary Report). Coupling all of the above information together
with a thorough understanding of flight operations, the Systems
Engineering task of developing and implementing a coherent EMMADS
operating philosophy was accomplished. This resulted in a system
design based on the following underlying principles:
a) The aircrew should be managers of the aircraft and as
such must have information required for operation of
the aircraft in minimum time and in the simplest pos-
sible form.1
I m . __ i i
b) The pilot in any flight situation must be able to fly
the aircraft, i.e., he must retain or regain control of
the aircraft. Any system that relates to this function
(such as EMMADS) must enhance this capability and
absolutely cannot interfere with it.
c) During fault display operations, interactive manual
inputs to EMMADS by the aircrew should be kept to a
minimum.
These principles then form the core of the EMMADS operating
philosophy. In this report, each element of the system's
operation is presented and justified in terms of this philosophy.
While the EMMADS functions described in this report are
applicable to all helicopter categories studied under Tasks I &
II, specific examples used herein are all related to the CH-47C
helicopter, since this aircraft had been selected as the basis
for the EMMADS feasibility model.
2
2.0 APPLICABLE DOCUMENTS
Electronic Master Monitor and Advisory Display System: Human
Factors Engineering Summary Report (ACS 12,385), R. McLane,
Reliability and Human Factors Engineering, GE, Pittsfield, MA,
Aug. 1980.
Subsystem Parameter Data Lists for CH-47C, UH-60A, OH-58C &
YAH-64 (ACS 11,995) Appendix 1, General Electric Co., Binghamton,
NY.
Technical Proposal for the Electronic Master Monitor and Advisory
Display System - Part 1 (ACS 11,773-1), February 1979, General
Electric Aircraft Equipment Division, Binghamton, NY.
TM 55-1520-227-10-2, Operator's Manual, Army Model CH-47C
Helicopter, 23 August 1978.
Advanced Subsystem Status Monitor, Final Report, Contract
DAAK51-78-C-0023, Sikorsky Aircraft, Div. of United Technologies
Corp.
3
3
3.0 EMMADS CHARACTERISTICS
3.1 System Overview
The block diagram shown in Figure 1 illustrates the basic EMMADS
architecture as installed on an aircraft. The system utilizes a
dual 1553B digital bus for data transmission. RTU's provide the
interface required to digitally encode and place on the bus the
aircraft sensor signals described in Appendix 1. Two digital
display processors perform the monitoring and fault detection
functions described in this report. They also determine the
current formats to be displayed on the electroluminesrent flat
panels. Note that a separate processor is to be made usabltu at
each crew station. A set of multilegend display switches (HLDS)
associated with each display unit, provide the pilot with displa
control during all system operations. A keyboard is provided for
data inputs to the system also. Provision for expanding system
capabilities to include audio warning is also shown.
3.2 System Functions
The EMMADS operational functions requirements are described in
this report according to the system's primary and secondary
functions.
The primary functions of an EMMADS are:
a) Provide a continuous display of Rotor RPM, Torque,
Flight Time Remaining (based on continuously monitored
fuel consumption) and, when applicable, a countdown of
remaining allowable time for operation of parameters
within time limited ranges. It shall also display
non-flight parameters to aircrew members upon request.
b) Monitor aircraft subsystem parameters for possible
4
*
z 0L0K 00CLc
z Ln
LL >
Cn -U-
-u -t -~~ -- 9
> > Ce
Figue 1.EMMAS Blck Dagra
U cm tU < :5 5ZA 0 C
faults. This monitoring activity includes:
1) Correlation of current parameter status (value)
with a particular limit or set of limits, the
vatues of which may be functionally dependent Dn
other parameter values. A parameter value that
approaches, meets or exceeds an associated limit
requires that the aircrew be notified.
2) Co:- elation of the time rate of change of a
pa.- neter value with a maximum allowable rate of
ch;,r4e based on manufacturer/procurement
sp, Lfications or some experimentally established
bab.;-line. A rate of change that exceeds this
maN mum value requires notification of the
air rew.
c) Detect ...nposite faults resulting from multiple
parametei excursions. Provide an unambiguous
notification of the fault nature to the aircrew.
d) Display Aults to the crew utilizing a flexible
prioriti ation system and provide a means of rapidlV
communic. ing to EMMADS the pilot's observation of each
fault.
e) Display recommended fault correction actions (emergency
checklists) in response to aircrew requests.
The secondary functions of EMMADS include:
a) The ability to display routine, interactive type check-
lists such as the Before Starting Engines, Starting
Engines, Engine Ground Operation, Before Taxi, Taxiing
Check, Before Tahcnff, Cruise Check, Before Landing,
After Landing and Engive Shutdown Checklists.6
II L r-I'
b) Calculations to predict aircraft performance
characteristics.
c) Recording the occurrence of any faults, as required for
post-flight maintenance analysis.
3.2.1 Primary Functions
3.2.1.1 Display Areas
The EMMADS display is broken into three areas to facilitate
efficient information transfer to the pilot. These are shoun in
Figure 2. (Note: In this and all other figures showing display
formats, boxes are drawn around alphanumeric characters and may
also be shown, empty, in other areas of the display. These are
not part of the format, but are used to indicate the amount of
space reserved for these characters.) The Dedicated Status Area
is utilized for information requiring continuous display. This
includes rotor rpm, torque and remaining flight time (in
minutes). Other items shown in this area are connected with
fault detection aspects of EMMADS. Once activated, they remain
in this area, continuous displayed, until deactivated by other
fault logic. Their operation is further described in Section
3.2.1.3. The Warning Message Area is reserved for displaying up
to six messages of eight characters each, under conditions
described in 3.2.1.3. The Subsystem Data Area is utilized for
displaying parameters in the engine, fuel, transmission,
electrical, hydraulic and miscellaneous subsystems, as well as
emergency action checklists. (The engine subsystem is shown as
an example in Figure 2.) The dotted lines shown with the bar
(thermometer type) scales and pointer scales indicate these
symbols can oversize to indicate a fault with that parameter.
Oversized, hollow indicators are used to depict rate (trend) type
faults, while oversized, filled-in symbols indicate a limit type
fault. Special symbols for chips (*) and other discrete type
7
TOROUE 01 * 2)SUBSYSTEM NAMES (FAULT CUESI ROTOR RPM
xs~II
A
Dedicated Status Area
Warning Message Area
Subsystem Data Area
IMI
Cjj 4i J,
TOROUE (1 2)REMAINING
T CUES) ROTOR RPM FLIGHT
TIME
L E Q' 24 58 -u'TIMEDYDR ,PARAMETER
LIMIT
IC 6 -J*-\ CLOCKPARAMETERLABEL
A
7777 I I l: I 1 7T ]T I=) i lLI:
r1 )L II1J ": Figure 2. Display Unit Areas
8i
.- I I I I I IF 1 .I
faults are also used (e.g. QTY indicates low engine oil quantity
and CTL indicates that an Ni control loop is energized). These
and other faults are described in Sections 3.2.1.2 and 3.2.1.3.
3.2.1.2 Fault Detection
The primary functions of fault detection and fault/ parameter
display are to be performed on a continuous basis, i.e. they Are
accomplished independent of flight phase. The primary functions
must be considered as preemptive of any secondary function.
Sufficient time must be allocated to sample all parameters,
update those currently being displayed, compute rates of change
and compare these and current values to maximum rates of change
or value limits, respectively, determine what faults exist, if
any, and display them according to their priority. Adequate
additional time per cycle should be available for secondary
functions.
The test for fault conditions may be linked to flight phase. For
example, in order to distinguish between an engine low side beep
trim failure and a pilot commanded reduction to ground idle
power, the EMMADS must be able to sense the position of the
engine condition lever. While a commanded power reduction is
normally a no-fault condition, during airborne operations the
placement of an engine condition lever in a ground or idle
position should be indicated to the pilot. It could be considered
as a fault or as an advisory, but, in any event, it is a
condition which warrants an information display to the pilot and
constitutes a link with flight phase. The flight phase is useful
in determining the operating mode for the measurement of
parameter conditions, as part of the EMMADS primary function.
Under various operating modes, parameter values (conditions) may
or may not be abnormal, as shown in Appendix 1, Subsystem
Parameter Data Lists.
9
I -" --- ' 1I II II l I I I II. II . ..-
|I
T iere are two fault types which are handled by the EMMADS; single
param(ter faults and multiple parameter faults. A single
parameter fault is detected by examining the characteristics of
an individual parameter (signal) for:
U. An out of tolerance value, or
b. An out of tolerance rate of change (unfavorable trend).
A multiple parameter fault is one inferred by correlating the
values of various related parameters. For example, to properly
identify an engine failur, gas producer speed, turbine gas
temperature, torque and engine oil prtssure need to be compared.
Parameter attributes, (values or rate. of change) used by EMMADS
as standards of comparison to detect * ither of these fault types,
are set by the operating mode mentioned previously. The operating
mode may be determined by some unrela~ed parameter or parameter
group (e.g. when gross weight sets th3 normal rotor rpm limits).
Due to the large variations in the size and configuration of
helicopters studied, the classification of faults and the relat&J
operating modes is aircraft specific. An example of a fault set,
the Fault/Parameter Matrix for the CH-47C, is shown in Appendix
2. This matrix relates each fault to a set of parameters which
either belong to a specific aircraft subsystem or are used to
relate to a particular operating mode. For single parameter
faults in this case, the Subsystem Parameter Data List, CH-47C,
Appendix 1 illustrates the relationship between operating modes
and various parameter conditions. The conditions on that list not
classified as "normal" constitute fault conditions. For multiple
parameter faults the operating modes and conditions are obtained
from Chapter 9 of the Aircraft Operator's Manual.
10
3.2.1.3 Fault/Parameter Display
When a fault is detected, the pilot must be made aware of it. The
system must allow the pilot to control what is on the display. At
the same time he must be given information about new faults as
they occur. A priority system must be established to allow the
EMMADS to differentiate between faults of higher and lower
relative importance.
In establishing such a fault priority structure, it is important
to understand the information requirements when a fault occurs
during a specific flight situation. The first task of the pilot
when a fault occurs is to regain/maintaLin aircraft control. The
second task is to take whatever action is necessary/possible to
correct the condition. In no case should the accomplishment of 61
the second task interfere with the first task. These fundamental
considerations dictate that faults be divided into three majorcategories:
a) Warnings - those faults whicti, if not immediately acted
upon by the crew, will most likely seriously compromise
the pilot's ability to control the aircraft and
therefore could result in personal injury or loss of
life.
b) Cautions/Precautions - those faults which do not
immediately jeopardize the safety of the crew or the
ability to control the aircraft but which may result inequipment damage if not attended to. In addition, such
faults, if allowed to continue without corrective
action being taken, may precipitate one or more
Warnings.
c) Advisories - these are conditions (actually parameter
states) the pilot should be made aware of. The
11r
determination of whether or not these states are faults
is left to the pilot, since the determination of the
normal conditions depends on pilot judgement (e.g.
Cargo Hook Open, Parking Brake ON, etc.)
Given the faults to be detected (such as those shown in the
Fault/Parameter Matrix of Appendix 2) the first step in
prioritization is simply to designate which faults fall into the
Warning category. Then, by designating the conditions which are
Advisories, the remaining fault conditions fall automatically
into the Caution/Precaution category.
Such a fault partitioning scheme as applied to the CH-47C is
shown in Table 1. Placing faults into the Warning category was
based on the following considerations:
a) A total loss of hydraulic pressure in the flight
control systems makes it impossible to move the flight
controls.
b) Rotor rpm is directly related to aircraft lift, so loss
of rotor rpm requires rapid pilot response.
c) In a dual engine aircraft, given a choice of responding
to a loss of engine speed control versus an engine
failure, the pilot should first attend to the engine
that is still operating.
d) Faults in any subsystem which can rapidly precipitate
loss of flight controls, loss of lift or loss of engine
power are candidates for inclusion in the Warnings cate-
gory. Each must be considered on an individual basis.
In assigning the specific numeric priorities contained in Table 1,
the following additional considerations were taken into account:
12
.. _ _________... .... . .. .. :f. ' .
TITABLE 1. FAULT PRIORITIZATION FOR THE CH-47C HELICOPTER
SubsystemFault Displayed Priority
WARNINGS
Quill Shaft Failure Hydraulic 1'
Rotor RPM Limit (continuous display) Engine 2No. 1 Engine Beep Trim Engine 3High Side Failure
No 2. Engine Beep Trim Engine 3High Side Failure
No. 1 Engine N2 Sensing Failure Engine 3
No. 2 Engine N2 Sensing Failure Engine 3No. 1 Engine Beep Trim Engine 4Low Side Failure
No. 2 Engine Beep Trim Engine 4Low Side Failure
No. 1 & 2 Engines Failed Engine 4
No. 1 Engine Failed Engine 5No. 2 Engine Failed Engine 5
No. 1 Flight Control Hydraulic Press Hydraulic 6Low/Rate
No. 2 Flight Control Hydraulic Press Hydraulic 6
Low/Rate
Eng. 1 & 2 Fuel Boost Press Limit Fuel 7(PA >6000')
Eng. 1 Fuel Boost Press Limit Fuel 8(PA >6000')
Eng. 2 Fuel Boost Press Limit Fuel 8(PA >6000')
No. 1 and 2 SAS OFF Miscellaneous 9
CAUTIONS/PRECAUTIONS
Eng. 1 PTIT Limit/Rate (starting only) Engine 10Eng. 2 PTIT Limit/Rate (starting only) Engine 10Eng. 1 Torque Limit (continuous display) Engine 10Eng. 2 Torque Limit (continuous display) Engine 10Eng. 1 N1 Limit Engine 10
Eng. 2 Ni Limit Engine 10Eng. 1 Oil Press Limit/Rate Engine 10Eng. 2 Oil Press Limit/Rate Engine 10Eng. 1 Oil Temp Limit/Rate Engine 10Eng. 2 Oil Temp Limit/Rate Engine 10Eng. 1 Chip Detected Engine 10Eng. 2 Chip Detected Engine 10
13
TABLE 1.FLIGHT PRIORITIZATION FOR THE CH-47C HELICOPTER (cont'd)
SubsystemFault Displayed Priority
CAUTIONS/PRECAUTION (cont'd)
Eng. 1 Oil Level Limit Engine 10Eng. 2 Oil Level Limit Engine 10Eng. 1 N1 Control Loop Energized Engine 1)Eng. 2 Ni Control Loop Energized Engine 10
Fuel Qty-Left, Fwd Limit/Rate Fuel itFuel Qty-Left, Main Limit/Rate Fuel 11Fuel Qty-Left, Aft Limit/Rate Fuel 11Fuel Qty-Right, Fwd Limit/Rate Fuel 11Fuel Qty-Right, Main Limit/Rate Fuel IFuel Qty-Right, Aft Limit/Rate Fuel 11Eng. 1 Fuel Boost Press Limit Fuel it
(PA <6000')Eng. 2 Fuel Boost Press Limit Fuel ii
(PA <6000')Fuel Boost Press, Left, Fwd Limit Fuel 11Fuel Boost Press, Left, Aft Limit Fuel iiFuel Boost Press, Right,Fwd Limit Fuel itFuel Boost Press, Right,Aft Limit Fuel 11Eng. 1 Fuel Flow High Fuel 11Eng. 2 Fuel Flow High Fuel 11
Eng. 1 Xmsn Oil Press Limit/Rate Powertrain 12)Eng. 2 Xmsn Oil Press Limit/Rate Powertrain 12Combining Xmsn Oil Press Limit/Rate Powertrain 12Fwd Xmsn Oil Press Limit/Rate Powertrain 12Aft Xmsn Oil Press Limit/Rate Powertrain 12Eng. 1 Xmsn Oil Temp Limit/Rate Powertrain 12Eng. 2 Xmsn Oil Temp Limit/Rate Powertrain 12Combining Xmsn Oil Temp Limit/Rate Powertrain 12Fwd Xmsn Oil Temp Limit/Rate Powertrain 12Aft Xmsn Oil Temp Limit/Rate Powertrain 12Combining Xmsn Chip Detected Powertrain 12Fwd Xmsn Chip Detected Powertrain 12Aft Xmsn Chip Detected Powertrain 12Aft Thrust Bearing Chip Detected Powertrain 12
No. 1 Generator Load Limit Electrical 13No. 2 Generator Load Limit Electrical 13No. 1 & 2 Generators Failed Electrical 13No. I Rectifier Load Limit Electrical 13No. 2 Rectifier Load Limit Electrical 13No. 1 & 2 Rectifiers Failed Electrical 13AC Bus X-Tie Failure Electrical 13DC Bus X-Tie Failure Electrical 13
14
TABLE 1FAULT PRIORITIZATION FOR THE CH-47C HELICOPTER (Cont'd)
SubsystemFault Displayed Priority
CAUTIONS/PRECAUTIONS (Cont'd)
No. 1 Flight Control Hydraulic Hydraulic 14Press High
No. 2 Flight Control Hydraulic Hydraulic 14Press High
Utility Hydraulic Press Limit/Rate Hydraulic 14Utility Hydraulic Temp Limit Hydraulic 14APU Accumulator Press Limit Hydraulic 14
No. I SAS OFF Miscellaneous 15No. 2 SAS OFF Miscellaneous 15Fwd Cyclic Trim Actuator Position Limit Miscellaneous 15Aft Cyclic Trim Actuator Position Limit Miscellaneous 15Right Aft Landing Gear Phase Limit Miscellaneous 15Heater Output Temperature Limit Miscellaneous 15
ADVISORIES
AC External Power Connected Electrical 16DC External Power Connected Electrical 16Parking Brake On/Off Miscellaneous 16Cargo Hook Open/Closed Miscellaneous 16APU On/Off Miscellaneous 16
1
15
a) If similar faults can occur in more than one area of
the same subsystem, then there is no difference in
their priority unless all such faults occur in com-
bination (e.g., a flameout in one engine is just as
serious as a flameout in the other engine, but a flam-
eout in both engines is more serious).
b) Faults that are mutually exclusive can be assigned the
same level of priority. For example, a given engine
cannot simultaneously experience a beep trim high side
and low side failure.
c) In assigning general priorities within the Caution/
Precaution category, it is more reasonable to assign
priorities based on the subsystems wherein the faults
reside, as opposed to assigning priorities on an indi-
vidual basis (except in the case of those faults in the
"Miscellaneous" subsystem).
This last point may not seem realistic until one one realizes
that all of the immediate action (Warning category) faults are
removed first and the remaining faults (Not Advisories) all
require a pilot reaction of about the same level of urgency.
Given that the pilot is going to acknowledge all faults in a
reasonably short time and that he will be alerted when any fault
occurs, the prioritization according to subsystem importance is
the simplest and most logical procedure to follow.
Highest on the list of Cautions/Precautions should be the Engine
subsystem since the engines provide the power to stay aloft. This
is followed by the Fuel subsystem because it directly affects the
ability of the engines to continue operating. Next comes the
Powertrain subsystem (minus the continuously displayed rotor rpm)
since it is probable that there will be a larger time span within
which to react to a fault in this subsystem as opposed to faults
16
_._----- .
in the two subsystems just listed. (For example, transmissions
have been designed to run as long as 30 minutes with no oil in
the sump.) Following this would be the Electrical and Hydraulic
subsystems, respectively. (Keep in mind that major flight control
hydraulic faults are already included in the Warning category.)
Finally, all remaining faults are prioritized according to
estimated relative urgency in the Miscellaneous subsystem. At
this time, no further prioritization has been deemed necessary.
It is possible that future considerations may indicate that s;ome
faults in one subsystem should really have the same priority as
faults in another subsystem, insofar as the urgency of the
desired crew reaction is concerned. Determinations of this type
can be made only after a prototype system has been used to gather
specific aircrew recommendations under suitable test conditions.
The final subcategory, which has not yet been addressed, is that
of Advisories. When an advisory level condition occurs, it is
generally a state change of a discrete sensor. It has the lowest
display priority. Hence advisory state changes will be displayed
only if no faults take display priority. In the case of the
CH-47C used as an example in Table 1, there are five advisory
conditions currently identified: AC External Power, DC External
Power, Parking Brake Status, Cargo Hook Status and APU On/Off
Status.
Given the preceeding discussion as background, the system opera-
tion with regards to fault detection and display may now be dis-
cussed. As previously described, with no faults active, the
display is clear except for Rotor rpm, Torque and Remaining
Flight Time, as shown in Figure 3. If a fault is detected, the
following events take place:
17
_ , !
a) The aircraft Master Caution light is illuminated by the
EMMAADS computer.
b) EMMADS determines the highest priority fault using the
priority structure of Table 1 and displays the raw data
of the subsystem related to that fault in the Subsystem
Data Area. Figure 4 shows an example of this for the
case of a failure of the number 2 engine. Note that the
out of tolerance parameters are indicated by the use of
oversized symbology. The fact that the symbols are
filled in indicates that an operational limit has been
exceeded. Note also that if other faults existed in the
same subsystem, they would likewise appear even though
they might be of lower priority than the fault which
brought about the display of that subsystem. The
symbols are flashing because they are part of a fault
which is not yet acknowledged. Also, the subsystem
name "ENG" in the upper left of the Dedicated Status
Area is flashing because there is an unacknowledged
fault in that subsystem. Note that the MLDS previously
labeled "ENG DATA" now reads "ENG ACK" and the right
most switch now reads "WARN ACK".
When a Warning is detected, an appropriate message is
displayed in the Warning Message Area. (In the case of
the example in Figure 4, the engine failure results in
the message ENG 2 OUT being displayed.) A box around
the message(s) indicates the highest priority
warning(s) displayed. These highest priority warning
messages are located in the top row of the Warning
Message Area. The messages have positional
significance: left and right of center if they pertain
to engine or system numbers 1 & 2 respectively or
centered when no such symmetry considerations exist
(e.g., rotor rpm).
18
'_ _" _ _• _t i-i-i
240 158
68 69
Ht
ENG FUEL XMSN ELEC HYDR MISC CHCKDATA DATA DATA DATA DATA DATA LSTS
Figure 3. Sample Display Format - No Faults
19
I,
ENG 240 158
b66
100100 6835ENG~~JE G FUL XMN EEC IHYA MSC WR
ACK DATA DATA DATA j DATA DATA ACI(
Figure 4. Sample Display Format - Fault Detected
20
c) The pilot must manually acknowledge that he has
reviewed the faults in the displayed subsystem, using a
cyclic mounted acknowledge switch or the MLDS labeled
"ENG ACK" or "WARN ACK" as described in Section3.2.1.4. Actuation of either of these switches
acknowledges the highest priority Warning and results
in the appropriate emergency procedures checklist being
placed on the display together with or instead of thesubsystem data. Figure 5 illustrates this transition
for the example started in Figures 2 and 3. This first
actuation of the acknowledge switch also extinguishes
the Master Caution Light.
d) The pilot notifies EMMADS of checklist completion using
the acknowledge function. In the example used in Figure5, no other faults existed and the failed engine
checklist has been acknowledged so the display formatwould change to that shown in Figure 6. Note that the
word ENG is now steadily illuminated in the upper left
hand corner, indicating that the engine fault, althoughacknowledged, still exists.
An important distinction should be made regarding
acknowledgement of Warnings versus other faults. The
acknowledge (ACK) switch on the flight control willacknowledge Warnings separately. Once all Warnings are
acknowledged, all remaining faults are acknowledged by
subsystem. Thus, an engine display with two or more"non-Warning" type faults will be cleared by actuating
the ACK switch once. This allows the pilot to rapidlyreview all faults while keeping his hands on the flight
controls.
21
t - .. . .. . .. ... -' - . .... . . . .. . .. . . . ~ -; . .. . 1 - I - . . . .. . . .. . ' . . . .
ENG 240 158
68 0
N1 , IGT
COLL-ADJ NRENG1 BP-INCEXT"LD-RELLNDG-BEGINCNDLV2-STP 4FIRE HNDL-2 100.8 50.8XFEED-OPEN 680 3 5 0
ENG FUEL XMSN ELEC HYR M ISC C CKACK DATA DATA DATA DATA DATA LSTS
Figure 5. Sample Display Format - Warning Acknowledged,
Checklist Displayed
22
240 158ENG= 6I
68 0
ENG FUEL XMSN ELEC HYDR MISC CHCK
DATA DATA DATA DATA DATA DATA LSTS
Figure 6. Sample Display Format - Fault Acknowledged,Checklist Completed
23
;i
The previous example did not address the question of what happens
when a fault of lower priority is displaced by a high priority
fault. This can occur in two ways: the lower priority fault
occurs first and then the high priority fault masks it or the low
priority fault occurs while the pilot is still dealing with the
high priority fault. In either case, the name of the subsystem
in which the low priority fault resides will appear, flashing, in
the top left of the Dedicated Status Area, to indicate that an
active fault(s), not yet acknowledged, exists in that subsystem.
Another element of the fault display not yet discussed has to do
with the amount of time remaining when a parameter is operating
in a time limited range. This information also appears in the
Dedicated Status Area, as a Timed Parameter Limit Clock located
under the Remaining Flight Time indicator. The logic governing
the use of this Timed Parameter Limit Clock dictates that it's
display requires a priority system different from that employed
for fault display. From both an operational and a human factors
standpoint, the major considerations in establishing such a
priority system are:
a) The pilot is capable of taking action on only one
countdown at a time, and
b) The pilot will concentrate on the countdown with the
least time to go.
Based on this, it is logical to display only one countdown at a
time; the one with the least time remaining. However, there may
be some parameters with timed operating ranges the pilot can
control directly and others he cannot. In this case, the display
priority for remaining time is in two major divisions, with
actively controlled parameters having priority over those that
are not. Within each of these two categories, the least time
remaining criteria applies for display priority.
24
As an example of the total amount of information which must be
processed for this mode the parameters on the CH-47C that have
timed operating limits include Rotor RPM, Torque, PTIT and Engine
Gearbox Oil Temperature. (See Subsystem TParameter Data List,
CH-4C, Appendix 1.) Thus, the first three are placed in the
higher (actively controlled) display category, and their
countdowns have priority over that of the Engine Gearbox Oil
Temperature.
3.2.1.4 Multilegend Display Switch (MLDS) Operation
The aircrew has the capability of selecting raw data for display,
by subsystem, using a series of MLDS's located adjacent to the
display panel. Several factors governing their operation should
be noted:
a) Whenever the format on the EMMADS display is not one
seen under "normal" operating conditions (i.e., only
the Dedicated Status Area appears) the right most
switch marked "STAT ONLY" is available to allow the
pilot to return the display back to the Dedicated
Status Area only.
b) This same switch is used to modify the operating mode
of all the other switches, by changing their legends
simultaneously. This results in three major levels of
switch operation: Data/Emergency Procedures, Routine
Checklists and Performance Calculations.
c) Switch actuation will change the display only if there
is no conflict with the fault detection and display
algorithms, which have priority.
There are two modes of operation possible for the MLDS's Manual
Display Command operations and Fault Related Operations.
25
-k. %
3.2.1.4.1 MLDS Operations - Manual Display Command
Under normal conditions, with no faults displayed, the sevenMLDS's immediately below the display bear the legends shown in of
Figure 7a. Actuation of any one of the first six switches places
the data for the selected subsystem on the EMMADS display and
changes the legend of the depressed switch and the right-most
switch as shown in the figure. The set of MLDS legends in Figure
7a then represents the system being in the Subsystem Information
Level. The result of depressing a switch with a "PROC" label is
that the subsystem data is replaced by the first page of the
highest priority emergency procedures checklist applicable to
that subsystem. Successive actuations of that switch will result
in the sequential display of all such checklists remaining.
Depressing the "PROC" switch one more time when the last
checklist is on the screen clears the display except for the
Dedicated Status Area and returns all switch legends to the
original set shown in Figure 7a. For Figures, 7b-7g, depressing
any switch other than the one with the "PROC" or the "STAT ONLY"
legends will have no effect.
The legends may be changed simultaneously to the Routine
Checklist Level by depressing the "CHCK LSTS" switch, as shown in
Figure 8. This also clears the display except for the Dedicated
Status Area. The six left-most switches now provide for selectionof various routine checklists, to be displayed in the combined
Warning Message and Subsystem Data Areas. As shown in Figure 9,
depressing any of the first six switches changes the legend of
that switch and the right-most switch, as well as presenting the
first page of that checklist on the display. For example, in
Figure 9c, the Normal Starting Engines checklist is selected
("NORM STRT" depressed). Depressing that same switch again (now
labeled "MTF STRT" in the example shown) calls up a different
checklist for display and would change that switch legend back to
the previous one ("NORM STRT"). All of the first six switches
26
III~~. IIIT
A 240 158
68 6 9
B
2240 158
6868 69
FWDPRS TMP NI% TGT CYC TRM ACT 040
___________________________________AFT
ENG FUEL XMN ELEC HYDR MISC STAT SAS # 1 ONDATA DATA DATA DATA DATA DATA LSTS PARK BRAKE ON
85 85 1008i100 8100100 68068024 15
ENG FUEL XMSNT ELECI HYDR MISC STAT E;z, FULXtE EEPPOC DATA DATAIDATA DATA, DTA0NY 6 8 69DATA DATA DATA DATA 0A
BOOST TOTAL BOOST
FI 70O F72# 556# ON
N ON
ON 1703# 16 80 # ON
ON 02# 5 2 1W# ON 240 158
X . E E 6 8 6 9c I 25*/HR1 2 2 7 ' /HR.
ENG IFUEL IXM6SN ELEC I YDR MISC ISTATDATA PROC DATA DATA DATA DATA ONLY PRS TMP
ENG IFUEL XI4N ELEC HYDM MISC STATDATA DATA PROC DATA DATA DATA ONLY
Figure 7
A. Display Unit and M LOS in normal operationss mode
9 lINo Faults - Subsystem information Level Selected),
8 E ngine Subsystem Date Selected
C. Fuel Subsystem Date Selected
D. Trasnarnivsfon Subsystem Data Selected
240 1 58 E. Electrical Subsystem Data Selected
12, fF. Hydraulic Subsystem Data Selected6 8 6 9 G. Miscellaneous Subsystemn Dastal Sodecte
CY TRM ACT 04M 160_AFT
*S TTSAS # 1 ON #2 ONDATA LSTS PARK BRAKE ON
240 158
68 69ENG FULXSNEE YDA MISC STATDATA DATA DATA DATA DATA PROC ONLY
SI'S1 SYS2
FLT CTRL PRS 2600\7 3100
2 58 AU ACCUY PRS 3000205
UTL TYAFNIO
2 1 ~1 0 158
MIC TT N FUEL XMSN ELEC HYD MISC STAT
~DATA DATA DATA IO DATA PO DATA ONLY
Fiue7oLSFncinp usse Infra io Level
27 OD F ILXTE07
2 40 1 58
t 240
68 6 9
IA
EMER NORM TIO CR SE ILNDG SHSTRT STRT CHCK CHCK CHCK DC
I _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ I
A Subsystem Inflormation Level
Note that only Dedicated Status Areainformation ison the fliiroy linrl(
2 40 1 58 8 Routine Checklist Levil
\ 112-Iflj(Note that only Dedicated Status Area
68 69 information ison the Display UnitlI
C. Performance Calculation Level
(Note that only Dedicated Status Area
information is on the Display Unetli
0, The "STAT ONLY" legend appears Onthe last switch whenever any of the
indicated switches are depressed. Theinformation on the Display Unit andthe other switch legends are discussed
in the text.
v!H NORM T 0 CR SE LNDG SHUT PERF
ST P STR T CHCK CHCK CHCK DOWN CALC 240 158
68 6 9
C
Figure 8. MLDS Operation-Format Level Selection
28
A
68 6 9
EMEA NOAM TiO CASE LNDG SHUT STT NE -AEKSTA~~STT STT CHCK CHCK CHCI( DOWN ONY XF0VLvLS- ES
F I IRE 6JUJA REPST
MASTE(R CAUTL_ - - TE ST
rATPUO OIJL J MT TEST
[TNA -APU-*1 S +4: 1VSI A SE Tf
I IGIEINFTi&1 C T R L S W S ON
I j~T PEWIE:. IS N
F FT CTRIS I- - PO SCHECTKU TT1
EMER MTF TO" CASE L-NOGSHT TASTAT STAT CHCK CHCK ClICKDON NL
EMER NORM MTF CASE LNDG SHUT STATSTAT STAT T/b CHCK CHCI( DOWNI ONLY
A Display Unit and MULS after selection of
t8 Routine Checkrlists level [See Figure 2-6b)
B5 Emergency Start Checklist selected (FinalFormat T BS)
C Normal Start Cfhecklist selected (FinnalFormnat TOS -Sample Format showen,wi~th several iteins already completed)
0 Before Take Of f Checkinst selected(Finnal Format 185)
E Cruise Checklist selected (Finaf FormatTBS)
F. Before Landing Checklist selected (Final
Format TBS)
Gi. Engine Shutdown Checklist selected
R RInal Format TBS)
F ME R INORMI TO CASE ILNOG M ISTAT
JH [STRT CHCI( CHCI( ClICK STOP ONLY
EMER NORM TO CASE MITF SU STAT
STAT STAT CICK ClC LNOG DOWN ONLY
T N TNL EMERI NORM T/O IMT F ILNDG SHUT STAT
fN[N SCTAT ISTAT IClICK ICASE IClICK DOWN ONLY
Figure 9. MLDS Operation -
Routine Checklists Level
29
(except "EMER STRT") operate in a similar manner, as shown.
Depressing the switch labeled "PERF CALC" changes the switch
legends as shown in Figure 8c while simultaneously clearing the
display, except for the Dedicated Status Area. This figure shows
that depressing the 7 "LMTS SUMM" switch changes the legend of
that switch only. This is true of all the other switches as well,
with no change in the legends of the first six switches. The
"LMTS SUMM" switch displays the Limits Summary data which is used
for post-flight maintenance playback of faults. Other switches
select various performance calculations for display (see Section
3.2.2.2)
The only function not yet described i'- that of the "STAT ONLY"
switch. Figure 8d shows that no mattey what legends appear on the
first six switches, depressing the "SIAT ONLY" switch always
returns the switch legends to those of the Subsystem Information
Level and clears the display except fcr the Dedicated Status
Area.
3.2.1.4.2 MLDS Operations - Fault Related
In the case where a fault is being displayed, the switch normally
associated with the displayed subsystem has it's legend changed
to "XXXX ACK", where "XXXX" represents the subsystem name. This
switch function now exactly duplicates that of the ACK switch on
the flight control. The switch legends revert back to those of
Figure 7a when all faults/emergency procedure checklists are
acknowledged. If Warning Messages are displayed, the legend of
the right-most switch will also be changed to "WARN ACK". The
pilot has the option of using this switch to simultaneously
acknowledge all Warnings, as opposed t3 acknowledging each one
separately. This would also bypass the automatic display of each
emergency procedures checklist associated with those Warnings.
These checklists would then be selectable later using the "XXXX
30j
Ai
PROC" switches. Once the "WARN ACK" switch is depressed, its
legend reverts to "ClICK LSTS".
The switches described above are the only ones actually changed
when faults are being displayed. All others retain their original
legends but will do nothing if depressed.
A description of the switch legends is included in Table 2.
3.2.1.5 Emergency Action Checklists
The display of emergency action checklists is accomplished
through two mechanisms:
a) Checklists associated with Warning type faults are auto-
matically displayed after an acknowledge switch other
than "WARN ACK" is actuated,
b) All ch-cklists may be accessed using the relegendable
switches marked "PROC" as described in Section 3.2.1.4.
After the acknowledgement of an individual Warning, the
associated emergency action checklist is displayed, utilizing
formats (TBS) supplied by Human Factors Engineering. The
checklists are manually acknowledged and are completed item by
item in the same manner as the routine interactive checklists
discussed later in Section 3.2.2.1. Upon completion of a
checklist, the subsystem for the next highest priority Warning
appears. The Warning Message is boxed in (see Figure 3) and it's
checklist may then be displayed in a like manner. If there are no
more Warnings, the subsystem with the next highest priority
fault(s) is displayed. To access emergency checklists in a given
subsystem, depressing the "PROC" switch (after all faults have
been acknowledged) changes the "PROC" to "ACK" and causes EMMADS
to display the checklist for the highest priority, active fault
31
TABLE 2. SWITCH LEGEND DESCRIPTIONS
Leend Description
(XXXX) DATA Raw sensor data is displayed for the subsystemsdesignated by "XXXX" - i.e., the Engine, Fuel,Transmission, Electrical, Hydraulic and Miscel-laneous subsytems. (Formats other than EngineSubsystem TBS)
CHCK LSTS Checklists switch legends will be selected
(XXXX) PROC Emergency procedures (checklists) are displayedfor the subsystems designated by "XXXX" (asdescribed above for DATA legends. Formats TBS)
STAT ONLY Display cleared except for the Dedicated StatusArea (see Figure 8).
EMER STRT Emergency Start checklist will be displayed. (TBS)
NORM STRT Normal Start checklist will be displayed. (seeAppendix 4)
T/O CHCK Before Takeoff checklist will be displayed. (seeAppendix 4)
CRSE CHCK Cruise checklist will be displayed. (seeAppendix 4)
LNDG CHCK Before Landing checklist will be displayed. (seeAppendix 4)
SHUT DOWN Engine Shutdown checklist will be displayed. (seeAppendix 4)
PERF CALC Performance Calculation switch legends will beselected.
MTF (XXXX) Maintenance Test Flight versions of the checklistsdesignated by "XXXX" will be selected(provisional).
HIT CHCK (Engine) Health Indicator Test calculation will bedisplayed. (see Section 3.2.2.2)
HVR PWR Power Required to Hover (IGE and OGE) calculationwill be displayed. (see Section 3.2.2.2)
MAX PWR Maximum Available Power calcuation will bedisplayed. (see Section 3.2.2.2)
32
TABLE 2. SWITCH LEGEND DESCRIPTIONS (CONT)
Legend Description
WT & BAL Weight and Balance Calculation will be displayed.(see Section 3.2.2.2)
SYST TEST System Self Test will be initiated and displayed(previsional).
LMTS SUMM Limits Summary will be displayed (maintenance datasummarized - post-flight operation. See Section3.2.2.3.)
(XXXX) ACK Duplicates acknowledge switch function for faultsin subsystem described by "XXXX". The "XXXX"portion of the legend also reflects the subsystembeing displayed (with unacknowledgedfaults/emergency procedures checklists).
WARN ACK Simultaneously acknowledges all currently activeWarnings.
3
33
in that subsystem, provided the checklist has not been completed
since fault detection. If there are none, the switch retains it's
"PROC" legend and allows a review of all checklists for that
subsystem, as previously described in Section 3.2.1.4.1. Upon
completion of one checklist, the next highest priority one is
automatically displayed. If no more exist, the display is cleared
and the switch iegend returns to "DATA" as shown in Figure 8a.
An emergency checklist for a Warning may not be removed from the
display unless:
a) The checklist is acknowledged as complete by using the
ACK switch on "XXXX ACK" MLDS.
b) A higher priority fault is detected.
c) The fault related to the checklist is cleared.
A complete list of the emergency procedures checklists associated
with the CH-47C is shown in Table 3. Before any such checklists
are incorporated into EMMADS, they must be rewritten observing
the following criteria:
a) Checklists consisting of so called "immediate action"
items will be displayed with the idea that they will be
used by the pilot, after he has already completed the
items, to verify completion. This is because the
required speed of reaction does not allow time to "read
and respond" to such items, as the aircraft operator's
manuals currently indicate.
b) Other checklists (or portions thereof) that have no
immediate action items but which provide for natural
follow on responses to them will be appended to those
immediate action items (e.g., Engine Cleanup and
Restart combined with Engine Failure checklist).
34
~1
c) Where applicable, these checklists will be displayed
along with any raw data necessary for checklist accom-
plishment (e.g., Engine Restart shown with N1 and TGT).
Formats are TBS pending final results of a human
factors study.
A suitably rewritten version of the checklists in Table 3 is TBS.
It
d
35
& * ,~ ** -NNW
TABLE 3. CH-47C EMERGENCY ACTION CHECKLISTS
RelatedChecklist Fault(s)*
I. Failure of Two Engines - 61Low Altitude/Low Airspeed
2. Failure of Two Engines - 61Cruise
3. Failure of One Engine 60Low Altitude/low Airspeed
4. Failure of One Engine - 60Cruise
5. Engine Restart During Flight 60, 61
6. Engine Cleanup Procedure 60, 61
7. Normal Engine Beep Trim System 62, 63Failure - High Side
8. N2 Governor Failure 64, 65
9. Normal Engine Beep Trim System 66, 67Failure - Low Side
10. Engine Shutdown - Complete 71Electrical Failure
11. Engine Residual Fire During 3, 4 (Rate Trigger)
Starting and Shutdown
12. Engine Fire - Ground 3, 4 (Rate Triger)
13. Single Fuel Pump Failure 25, 25, 27, 28
14. Fuel Cell Overpressure 17, 19, 20, 22, 68, 69
15. Fuel Pump System Failure 23, 24
16. Fuel Low and One or Both 17-22, 26, 28Aft Pumps Inoperative
17. Failure of Both Generators 71
18. Failure of Both Transformer 72Rectifiers
36
TABLE 3. CH-47C EMERGENCY ACTION CHECKLISTS (Cont'd)
RelatedChecklist Fault~s)*
19. Failure of One Flight Control 44,45Hydraulic System
20. Failure of Both Flight Control 70Hydraulic Systems
21. Longitudinal Cyclic Trim Failure 53, 54
22. Single SAS Failure 55, 56
23. Dual SAS Failure 73
373
ii
i
ChSels Apenix2ltFul/Avior)Ls
19. ailre f On FlghtContol 374
3.2.2 System Secondary Functions
3.2.2.1 Routine Checklists
The EMMADS secondary functions are related to the flight phases.
It is convenient to define the time span from system power-up to
power-down as a flight. Each flight, in turn, may be divided into
a number of sorties where a sortie begins with a take-off (from
the ground or from hover to forward flight) and ends with a
landing (to a hover or to the ground). The EMMADS may then be
envisioned as normally cycling through various states based on
the stage of flight. The current operational state is described
by the particular routine checklist which the system is currently
running or last finished running. The checklists applicable to
the CH-47C are shown in Table 4, including a set of operating
conditions (called modification parameters) that modify the
indicated checklists. The flight state numbers shown next to each
checklist are used in Figure 10 to indicate how the EMMADS would
progress from state to state in any flight. It should be noted
that it would be quite natural to regroup these checklists into
the categories illustrated in Figure 9.
In Figure 10, a method of communicating flight state changes to
EMMADS is shown. Differentiation is made between two methods of
progression from one state to the next. The sequential state
change paths could be brought about through the use of the ACK
switch. As EMMADS moves to a new flight state, the associated
routine checklist could be displayed. After the last item in a
given checklist is completed, (provided there are no faults
requiring acknowledgement) actuation of the ACK switch would
enable the next checklist in the sequence shown.
The specifically directed state change paths indicate that the
crew must make some other input to the system to produce the
38
TABLE 4. CH-47C ROUTINE CHECKLISTS AND MODIFICATION PARAMETERS
Routine Checklists
State Checklist Title1 Before Starting Engines2 Starting Engines
3 Engine Ground Operation4 Before Taxi5 Taxiing Check6 Before Takeoff (to a hover)*7 Hover Check8 Before Takeoff (to forward flight)*9 Cruise Check10 Before Landing11 After Landing
12 Engine Shutdown
* (These checklists are identical in TM 55-1520-237-10-2. Theyare listed separately here in order to differentiate betweentwo distinct flight modes.)
Modification Parameters
Parameter Affected Checklist(s)
1. Through-Flight Operation Before Starting Engineswith crew change Starting Engines
Engine Ground Operation
2. External Cargo Before TaxiOperation Before Takeoff (8)
CruiseBefore Landing
3. Night Flight Operation Starting EnginesEngine Ground OperationHover Check
4. Instrument Flight Starting Engines A
Operation Engine Ground Operation 4Hover Check
5. Water Operation Before TaxiBefore Landing
6. Cold Weather Operation Starting Engines
7. Hot Weather Operation Engine Shutdown
8. Maintenance Test Flight All (except Before Takeoff andOperation Before landing)
39
Power-Up(APU Started)
1
2
3
4
5
6
7
8
9
10
Power-Down
no Sequential State Change Path
---- ~Specifically Directed State Change Path
Figure 10. Normal Operational State Sequence
40
indicated state change. This would accomplished by using one of
the MLDS's described in Section 3.2.4.1.
The sequential state change operating scheme would make it easy
for the pilot (without removing his hands from the flight
controls) to display and accomplish those checklist items most
often used in helicopter operations; Before Takeoff and Before
Landing. This is a particularly useful feature for both
operational and training type missions, where multiple takeoffs
and landings are the rule.
Given this operating scheme it is advantageous at this point to
consider a representative scenario for the EMMADS operation in
order to highlight other features of the routine checklists. When
the system powers up it will begin to sample parameter data and
display any detected faults. If the EMMADS is powered up before
engine start, many subsystems will have erroneous "fault"
conditions associated with them. A method for disabling fault
displays must be provided, so that as each subsystem powers up tonormal operation, the associated fault conditions can be enabled
for display. A convenient method for doing this is through the
routine checklists such as STARTING ENGINES and ENGINE GROUND
OPERATION. (Note: It is assumed that the APU must be running or
that external power is connected before EMMADS is powered up. In
the former case, provision would have to be made for bypassing
the first part of the STARTING ENGINES checklist which deals with
APU starting.) The sample scenario is shown below:
a) The system powers up and enables all Advisory condi-
tions for display. In addition, faults 11-22, 40-43,
47, 48, 57 and 58 are all enabled (see Appendix 3). The
display at this point only contains data in the
Dedicated Status Area unless any of the enabled faults
are detected, in which case the display reflects the
highest priority faults, as described in Section
41
ifi
3.2.1.3. During power up and initialization, the
switch legends should be those shown in Figure Ba. If
no faults are detected, the legends will remain in that
state. If any faults are detected the relegendable
switches will have their legends changed as described
in Section 3.2.1.4.2.
b) Once all faults are acknowledged the pilot may either
select the Dedicated Status Area, specific subsystem
data or initiate the STARTING ENGINES checklist by
depressing the appropriate MLDS under the display.
c) If the checklist option is elected, this essentially
places the system in State 1 of the secondary functions
mode, as shown in Figure 10. Although the final check-
list formats are TBS (based on the final results of
human factors testing), a sample format is illustrated
in Figure 11. This shows the essential elements of an
EMMADS managed checklist, which are:
(1) An indication by the system of what the current
checklist item is,
(2) A description of the actionis) to be taken by the
crew for each item plus the required response, and
(3) An acknowledgement by the system that an item is
complete.
In this example the system identifies the current item
by boxing the procedure description and the response.The pilot accomplishes the item and indicates
completion by using the ACK switch. (Note that Figure
11 is the only exception to the rule that the Dedicated
Status Area is always displayed. Once an engine is
42
t.________________IIIII_____________I_______
TE TJ SIT] -CHECK I-I--dT
E7T ' MRE2U -- P T
AP TU OI PRS LT-T
-[ L~~ ~~ .-j JEST I
IAPU ST 1 S1 1 F____
7VfjTPWRU - I SC !N E 18T
F1 F [LfTI CT TIR LTB]-- -T7 6 1S1 CIHIE"IC K
Figure 11. Sample Display Format -Full Page Checklist
43
started the display area available for the checklist
would no longer include the Dedicated Status Area.) of
When the item is sensed as completed, the response
message is changed to a .... or other suitable
indication of completion and the next item is boxed.
The response section contains a command word or a
switch legend which changes during some sequenced
operation, thereby modifying the action to be taken
during the course of accomplishing that item. The pilot
follows these instructed changes as they appear. The
sequence of item completion may loop back to a
previously accomplished item, changing the desired
response for that item and boxing the procedure
description and new response until completion is sensed
by the system.
The checklists are indexed by having the current
checklist item (boxed procedure description) move down
from the top until it is in the middle of the screen.
From this point on the checklist items are scrolled
from bottom to top so that the current item always
maintains the same relative screen position. When the
last item in a checklist is completed, the next
actuation of the ACK switch clears the display but the
system remains in the state associated with that
checklist (see Figure 10 and Table 4).
d) If at any time an enabled fault is detected, that fault
must be displayed in accordance with the procedures pre-
viously outlined. If a fault occurs while running a
routine checklist, the checklist is replaced on the
display until the fault is cleared and/or acknowledged.
If there is an emergency procedures checklist that
automatically follows on the acknowledgement of a
44
Warning then this checklist must be completed, as
described in Section 3.2.1.5.
e) If no checklist is being run and no faults are pending,
actuation of the ACK switch or an appropriate MLDS
causes a sequencing within the secondary functions mode
to the next appropriate state (see Figure 10) and
displays the routine checklist associated with that
state.
f) After the last approach is made and the aircraft is on
the ground, the crew must manually select the AFTER
LANDING CHECKLIST using the appropriate relegendable
switch. Progression to the ENGINE SHUTDOWN CHECKLIST
may then be accomplished using the ACK switch. As each
system is shut down the faults normally associated with
that shutdown are detected and displayed, thus allowing
a post flight check of their operation. Acknowledgement
of these faults clears them from the display and
returns the display to the checklist at the appropriate
point.
An example of the form that routine CH-47C checklists might take
when rewritten for incorporation in an EMMADS is shown in
Appendix 4. The section under the heading "EMMADS Actions"
describes what the EMMADS does during each item and is not part
of the displayed information. These checklists do not include any
Maintenance Test Flight (MTF) checklists or the Emergency Start
(EMER STRT) checklist listed in Table 2. These switch legends
were provided to indicate such checklists as growth items for
further development, since it is recognized that EMMADS must be
compatible with maintenance test flight activities and also
should enhance the pilot's ability to rapidly start the aircraft
and evacuate it from a hazardous area (presumably under combat
conditions). The checklists in Appendix 4 refer to the list of
45
faults in Appendix 3 by number, as regards the enabling of
various fault conditions. For operations such as engine start
where the pilot must normally cross correlate certain parameters
(including time) with certain operations, EMMADS performs these
functions for the pilot. For example, EMMADS correlates N1
acceleration with time during engine start and triggers a fault
indication for N1 if ground idle speed is not attained 45 seconds
into the start.
3.2.2.2 Performance Calculations
(TBS)
3.2.2.3 Maintenance Data Summary
(TBS)
46
Subsystem Parameter Data Lists
for the
CH-47C, UH-60A, OH-58C and YAH-64
47
______________________________m________ 9
APPENDIX I
SUBSYSTEM PARAMETER DATA LIST
FOR THE
CH-47C
48
0 aC
S I-.o
wU , m~ R c-.
0 ow r- 0
LUc) s-U L-0 c..U)0
o o o o-
o m
w C o 0 M m)
o o .2 m -? 0 D-
cm~ Co .D 0 co c. CI C 0
Q C L. I- 4J 0i Lmw cm > 0 0 a, > ull a, m 0M
w -j c^L L s
m SQ
o 4)
I--ccz
CJ
2U
L9)9
I In
e~~e Ln IA Ne
C I t
I
C) iL ICc QC 0 0. QI
0 o r E 3 5o o i 0c o I
I m 0 1 C L GD -C . C Gcc 4.1 ID -~ 5 z 4. C 4.
I- 0 o- 0 Uj 0
C. m. o I mC o I
I2 - 0; 0- cG t-M 0 m m m Ol
:z- D :-
1-0z z14 xD0
wI. 2 D Ln c
In a,, n40 c44 L
c)C o c? al-C) cDDaD
84 8
ac m
In
c)w0
a 0
c5 C02I
LacL ~G
U-V
u) Q a GE
c i0_j
S.cD 1 O N
w _j t
50
0 c3
(7) CD
coo-
wM IL/C c?
L. oL LL 0) o-~~~CM~~c C CMAcM- M OuLA cl~ cI Ix CLI
0- MI C ICL.Cca lrL. cLu- 1c l;
La-.' 0. . 00 0.0u-i.', 0.00. 0.00. .0.00
I- C Cf LA M C LA M L CM M L
* I II I
-o CM CMoIC MC M
a- -
G o-a 2 ; n 5.I- 0 M - o u -;;'
C, c4."1&
0.l &.MCwoo& o
CDS
.
*- a) ,a & ,
- 0 -I z
4j I- wL
(A2.- 3E C) ' ' .w a)1 - 0 0 'V .C. mV C .
a, L' =V2-a L 2d231 0 CO) (A -u -'
(DID .C a 0' -(2(0 a'V m.a-' OC
C, ~ - ~ 0- L. Z '
1; C.C3 L! LU (
5 w Q 22 . .C L C('0 Q. O 0'v > (A .10 .- 0 o w0 c2L w 0w
-0.0.- (0 0- L MVC' m C ; C .0'VLO" MG- 0 0. 0 ~ ~ 2 '
Oo- mL.' aO 0V 41. uA .Ca, 00 w. 0. V2 a,-- 3: J-- 20 E-
a,0 0 Q(~.( CZ V . ;:O (A0- *.)- (A:; *'V .. a,-
m4 -M-0 m2 2 1 0' -'0~0 ' .0.0.L 2 2.- 2 C 0, 0.20 C222 ~ ~ ~ ~ ~ ( CV 2 -. OO '..- X -.
w..C 0) w ~ C aL0 0'2.' 0 C- 0
>A 4)>2- (Aa'C m'0 '0 0 u cL a ' 2- 0 C -'0 L- -o m-
E ot* cmV"<' CI 0 .2 0'
0( m~ 1- 0 u- '.
.Ea, , '.' V '4 7.. c L 0.0 L L *-mco 2( L. a .' a.. ~ a 1
<-( .- = 41C2 m((> 'V x0 15 -.5 '( 0
w0 CL2. 00.'. . 0- 0>0 .-- C M0 a 2a'N C
01- IC a-C) 2.-A2 ) 3 0- =Wo2V ON a3 0 m-L.0 d C, ~0 u
2.-SI-a~~~t >. 4)>U .3 0 ~ C 0 .0.) ..- LC2. -' 'V . 3; C0.A C' .42 -'VC 3Lt- 0 L5 Cw'V='
> 0 m L ' a)' . .C c' m C
w2 0 (''U .5 1C: (L) ., 2 'V 0 C~ 2.'l'o 0 .M 02 M 4).C-C L -, 2 0 a.. c .01
eV L. .- C 00 0 tm4 Z) 0cV U . ' * (a, IC 'U0. -41VU 0 u. wA.
~~~~~~CL 0V25' ( a- U-9-( d V.)0 L IL,.- 0- 2 . C C .a 'V 0 2 - C
r- 0 ' ' =0 -1 -x 0 2 2 (A 300-aLOr .- JV , . e-C.-0 o.C- L .s 0
C ~~ ~ 1 (A22 0( L-0 0 - C 0 'V0C . 0 .r-o 05 C.! 20 -*) (AA V 0 LL- 2 'E (.
C 4.- CC 'V LI 0 ' 0) U. C
w C ..Cu 0
E' 0 '-C.-'0 * A 0520 0 00 'VCm1 ,' U >C 2 WIOC 2 r-. tm *-'
.C'V. 2 m 0 .0 U U -0 wI w. 3: 0- 20 OC0-~~ L- 'a1 20L5 a c -a
- -C " 1-'VI- ! 4 .C40 u 20 (m 0. (0 .0 +L'V05 (L. 20. (a- r '. L. > cm 2 2
oO 'V. c (O C 3, a4 C>. o o2U.0+ L cV CT- C". C1 C
Va. 0 2CU O. i*2 ' . . ..L'V.- <.52 U. C!. d' g L- (At2-'VU 02 'V 1-2 0
a0 (0. 4 ( a-. .. O.i --. 0 0 2 C
u W w 1.A C5 0. C V .' .2 5 0062- -' . UOU ' C~' a) 2W 2W .. V '
E.+ 0 o C 0 .- a .5I a) c .0 aCOW 03 a. m Q4 I-9 C0 . F -C ''Vc -V0 = x50'.. :.0 : -U
01.AC 1- 412.2 ,-~ X 02 9
COU Uol O.1m I-I a2.- L-5'4 2a a ~ *~
M5 LL N. L0 ',aIOr 0'V- 0- ua' N 2 CL _.u -~l. 23 2 -. .0+ 0 +. 1- 061
v- 17;' >,l 0r-4 02 0.-0 00 W 0 Uj &c4, eI- >20 N.WL 0+0 0 -..- 0 5 0 1* ~ ~ ~ ~ ~ ~ ~ . a,- 20U. WV00 .+ . L 4
'4-0' 1-~. 0VV. i
200.4 C L. OW-< I'm 01 *4 U - 2- W5 -4c I LI,-1 W 0 U S -- I-U
+5 4404 M05( om, mC W CL.- 45.-. 0 - 1
'V 'V +5 X 2- 'V
w . 1 -2 -L.' 9U =- do2 1*O a0U.- 00- OwP o.. 4 m4. L. v 04,
W U- OIL 0( +C L- 2 L C 06 L ~ C 0 S.w
41 1 -- M IV- 6. 'V A -. I4 4' U) % 0, u ~L. 4U N 06 m) ID 0
I--
0 1 C
43 ~4 _ __ _ ___ ____ ___ ____ ___ ____ ___ ____ ___ _____C--1 CLC l xr
nl C4 0c l f f
'o .c Sn
C-)( 3,.
(' (4KCNIx Z' Z' N
L~0f O00. f .
m: u
C) C:.O~A) S~
C-1-
W) C) a)
cc0
Z.-- -0 4- 43
C9
Cr 0 0v0. 4j. I c- 4
41.C-
w 0 -j 0l4' 0
0~~~U w' N
Li I I &A V4
01 00'
31- 06__ _ _ N
so U. A V C
'/553
0) 0L- 0 -m)
.4)Q 00 .0
Z ~ ~ ~ ~ l 4-.4) 4. V .40-- 4) 04-4)4
0m L 4 '. c'- 0 0
.4 u.) 4 ' ~ -
4,,~3 a)) O. a4O-)44 L0 0 , 4'4
300
E uC 4 c
04 0)cl>a C40z
S.- )' J--- 0m 0.))4
u4A.4 00 -44
3t 04 4-44- M. .4)-.-. AL4)~~ 0- 0) 4)44)
- 0 C~
- Wc -0 4 3.
X044 414) . 4)0
C0) cu 4 c) )4L 0
Cj 0.
L 0 - aj '0-) C
.4)4) 0.
4)4 CL 404
C3LC C 4 )-4
'0 44 'C, 0 4 )
C)~ 110 00 30 C .C
V.O L- LA M 1 0
*.-4). ) 4)4 .40 ) V0 1-.0 . 4)34
'0, L41 04) M7 L..- L .4 .4 x4 .- 4,
E)4 4, !4
oo w 0. 4 A O
'04)4)4o 4'4 00 4..C.0 0,.4 w- L 44
4)_ C, . 0 0..-
C m 044) .) 44 M'
4 ) 41 C.- 400IM) 0 4)3 0 4.- I404
V0 c 0 C -- A 0 400%) 0- oo C 0
m3 '4M- L- C! E 4 A!406 4 c ) 4)444 0. 4
944 CL 0 CL 0
4) ~ ~ 4 4)- 04)0 )S 0! 44~ .4)401
4) 0 L 40 4.0)
COLL4)I. 0 w 40> 04- 04' - - AO 40 . A4>L a.0 'Col. 40 v0- 14)4)4) ( aIW IN- 5'- LLA *. -)42-
4)9 I 9.-a) AA 404
101C* I
00 1I
73 .
*l r17 0;L Li-oIA ~-. I
Nj 43
5I o- -soN
E-I m . E. 0. E.
o ~ = ; L 0 =3 i
o E~
in u C C . i E-4x n w 4 43 E 4 * x .- x n i .
(o 0 43 3 L 33 ~ i 3
I ~ ~ ~ ~ ~ L ko lo %Di -. 3 .C ~ 4 *
0 I 0 In - l 0 1 lo cin - Iml I 0 ;
m Le) Io m IQ '-I
m -o 63 a) 43 c30 4 . 33 43 ' 3 4E ~ ~ ~ s 0&33 ' 4I - .3
) c.5 i( mE XE a i( C, C
0.jIn -! '- Z A z E z L r
le IAzKc18
0~~~ ~~ N AIA C33 -
<A 3 0 3cc cl C
0 N N('4 N NN 41
UW LL3> '0 I
w0 OE If 43.V)
v) (
L. N-. 03)DA
I. La I
a. I. Y
.j3LI 0 3j of 1 1. 8 o
3. L55
.,~~ 00"
Lx-r')7oc ,-
a , m'---C' Cl
z oj m maQjJ ~ U
xI c o '.
o- T'
c:, u a
-20
n -
I- U4 . .:'
.
1.3 c3
S at-
a U
cn5u
on o t- L
C- 0)0a, 400 003,0.) 00
00 W - - 0 - 0
o) t.)0 t- 0 0 )
.0) w~0 .- 00 -- 0 .0 . td), Xt u) o- ci. t- *o -
.c0) m. 0 o
0)L OX u- c - )0
aO.t L 0 )L 4 4) 0
0) ~ ~ ~ ~ a oto)0)) * ) -
d 4) 44 w) . 400 4- 0)0 0-r- ).- w0) r- o) C
-'- UI I) dc) C. 0)Q.0 l
o- c) 0-4 44 0)
t-~~~ L44 M-)> 0)
0. 4--. 03. 4) a'=0>o f E0 U -- 0 .0)
- 4 o 44- a, 0) 0)
00)m -a >.'-0) m))- .- 0)2
0)~~ 0.- 0) 0) I- 00 ) 00.0)0)).-- )0 -- 0)_j
4444 ~ ~ ~ ~ ~ o 0 u.) . ) .0 0
L. 0. 0,
I) C) o- -0)
V .- 0) :on L Q
)00) t)40 0)0) 00w
0 =- 0 L: o ) 0. Q 0 .0 00 40
o'-4) 4 0 4 44)44 ) 0) '
.- tL. s- EU- -0 0 U) ut0) C
0) 0.0) 0. 'r 44 40 4 D0 .'0N
- I-0 E) 4- 0- m- cm3 V 0)'0400 -- m40 a 00 0 ) 4
o))0 z 0 0))4 0)' -f u )0 a-
0-'0) -.. *10 'top0 0) 00 m)0
0)0)0 -. 0). aQ0) 0 a0)-0 . 0 ) --. E o- m.0 0 4 U
o- 44.. 0. (a-0 0) 0/00 0)c)0 0) 0)-0 o n0)7 U 04 .
0) 0) 0" 0) c 00 In W ccm G4-a 443 4v 0 0 U m 0 N
m &A LAt n 'A L0 1.- 'A )0)
000. 3 .. >,) )0- 4 0) E
0)00 on )440 0) ). ~ .57
0) 0) 0) ) 0.00 U 0->,m444
. 0 C)4
O f C )
Tw 04 0
a a
ex 0, 04 00
E 4 .-. CsJ0
CD C
In C D C C 4 C ) 0 CD aC: C) (U -d
CII
u -A El 0
4J
0
C) ~ C 4, 'A4 0~~~C C'8) 0 a 4 0 )
0, V
cc CL L4,LI
m,
05)
u4)
0 4
(0 0>
L)4)
0
0
3 a
EA 40j
t! (n cu
"0
4..- ' ru
go, al
6A 0
d 'a ?(A
o o *-4
0 0
.0.;
7 - 04 0 i & ^A C
(A4)C4
4-' 59
U-,: C:, C,~888 8
a~ 0 m - 1
.- a,
C. 0 -- .CL L c
Q.i Q. -x -Lm , aLcc
8-8 8 Ai 8 A 1.4 8t.. A 80
aa
C8 ) o m8 c m
> o -
gu 'o m. r . 0m- 3C Oo C . C 4o
Q, LA. . 0l L. (
t. .- 8 %- o v.8 0otoc . L'3 L) o-I- .0( - o 4
a~~ , -; w 948 84 .)I 4 0
8- L- 4) 0 ) 0a)00-m:) o n8 LAmmwa r )a oo )
'o c, OLA . Lc I- o. c1
c8 0 c8 LA 4 -
-~Q - ,A al 8 . O .in~~~~ s8) . 0. 48 a)%- 88 L
-~~~ ~~~~ m o8..- w1Eu r L-.8L 08 03C.7)0 81 8)884AA'88) 0 4 I) 4 8 ~ 8.3 .
-~o - u00 .- ~ > 00Z 0. 0'C- .i-.4 *8~ 8'.0 0 .. 0 .. A ZL0U
u LA.8.8 C5 W-84 .8 *8 8.88 840- ~ 08- ..-.
O8La8)4 848 C 0C8 0(8)0 8 . 0
le 6- m , o IL
8-)~~v M.)C C 42- S 3v a L8A.) 4888-cc 4
'-c 90 -a0 _j01
A60
o co
c) c. a, ___ Lo
W,
-C .0LO- 0 . C
ec . eVo' .0 .
<J s Cl0
I- Co)0 >, > oc
c I Im M CS en enj a)n n
caIN L' L-'J - IN
o- w=>,=
0 I-
0? L -
- 0 c
- L 44
o 8- 00805 W-I0.O~C
m~~~ C- . c
0.6C,
0 wi Lj =
05- cc' 4,m
n
2- AL mn in0 -s . L ,v
I.- &- nG -
u, % L- "5-) - 0. -. 0 0. -00 . -. -0a.U IU 1ur .NA
-1wL Li -- inn LLrnn LLr~ LLrr Lrr
o~~~ o -
co t a
oo s4 0 o L.L
0 -l
-O r 4- IN 11
L. %-I
*.- O,- 0 vI ancDkoO.La, v, CVIOLML M 00.C I-I GG
w~ co m L.- Lj amI1 m
Ig 01 '1 130 5,
CL 31 x00 31- 10L C.3~ GI4Lo) 15.-. 05,C> 3) I,5CI 5£ D00
LI D :..0 . E---, u 6u c.'-- .1s-~3I- 15 I-~'0 %D L..- E LIJ .=5 L 8
.2", K -6cL4
co 31 .cN44j -l 0+j uco6
00)
0 C: z(4
"4. 0,C hc.C
In; ((4 -l
UicD9-ia g.
c( 0(3
M .0 4, 0.1
014NJ- L a,
(I C)I .) -o xcc. Dc oM m .
o n- u 0)0! j) i jo o
ad o.W> o,0 i ca.,-io .o
O 0....0(L o &- s m L. Ln... 0
DE 4L- GO0 4L (u a() W'V
o1. L. L x )nm)a)TUa i a ) c> UI JL Lm s-ir s".0 - L- .. L. cL-.'.OVn 'am(0 .mv)uL -c
zv
In]n
(4-- , -in M"
0.1
ix =. I ..a cL 1. 0L Muca) W:I 4AO &'(O 1n,( 1,(
ii- . -a. v-o wa. a0 m. - ec -awI- 0. c L. . l - - o.. - -04I - a o o0 .
urn-ur ur -ur *.m Go *.-uw- o4 wLL LL14n LLrr LL)rr 1. tL( rnn LLr>Uo cai C) 'D don
.4 *~63
-a -a
.8~y 1f .8 IL
u 0% 1~(1) ap .
aO ~ ~ c 0.)0 .0000
0 , M~ u C% C'% = =
c -o 4- a.
10 Lo I I
Ou L ;3 o w o 4-o
02t0 IIJfO0-44 51 00L U - 0 ~ V 4 . -11
r jia.0 oG c oc
e1 L L.N-ca&L.%1!
'0~~L b-J'I IJL
cz ~L) .4~~ 05
uUl. x1 1-~I -1 0
64
7--~I -a _- 1o ) c mc; c
m) - -) __________ _0
a-6 cl aLO nCL
I7 c4 t Lr cItL
c3 e a L a) a. a> at ) a a m t a a D
('4~o. ('4 tO c' ('t) (4 'I I I I I I I
zo
u aL a~ mt
o 4 ) CJ u 41 u.-
4-~ m a.) a 4 _ a.I CC.o
a CIca u w
< ,>C -:;CCU
-;; -
cD u
cc 04 -r c
t. cof . L. c I.! a .
F- uu L Qe-u
m 4) .- .La. -a - .41 n - un u
U I. .- Z 11 c ' IOU
tj ~ ~ C a. L.wL.M c 111c.1, 4c x 0 tU e IIz4 - T 4
65
a-a'? C() Ln )
Q..) £0 C
cO*
I~ I i0 4) ~ 0. co s-
('41' d) o x o u a)C4)i'.mI~1 I I
K~~ ~ ~ ~- _______2__ ____D__ o___z_
Q.I a 4* c* LLD Q. Q. tI,, E i n >
0~~4)- .i i £0v. ,0 .06 4*:i L. mt M*i u, (u 4'1 GI
~cx =~C.
Ei c"'J ". I4 W-
I. L
LL w cowcccn -e co v*0 Ln I c
ol 0, 4i - c*0'. w(f co 2
Zj - . . -I L. wo I. -65 w0 112U-4. u4 - .. - 0a4 - ..
_j .. I
II < .11 a. *44 3 o*
£0u - %44~ a. _j
cL o. s4 a. w.JI.--0tI
n ._j_ _ _ ___ ___ __ _L'___
_I
- 66 -
10 1U., In C
w ,~ In Lcr Ino
N ~ ~. -
0- W.0N
CL r0 c 0 CD
In -co m~4 G-2 0 > 04-10
8o E1 -8 ML - L.
0 U.I, > ~I.
CD 4)4 n o
Nd tom a -m< L1 - C
CU.,
Q- In
U CL CD
-) '. U L I.-n I. -u
LaL
~40--- Jj
I-. It. V~ I- Vbe~ V l0. 0 ,~IV~I .L
CLu , 4 55 =_
67
u, C'J I,1 o IC DML
0 *o cl M
Ic c,0. -. s~o C CL M J M ~ -ML00,0C\ C4 Le;
41 a, EIL >
- 1 M--
* L) l
E ID
I.In
C. Q. 40 cc~ Lr jc 1ca0 o0
0 0
I-~~I !-- 'E__ _ t 00 L.__ __ __
*6 u L) L) L
o C L.L LUL C
.- c~I. z..- aC I. L
-p - 0 n
wU U. XU C~l O L I-U aZ ~-ZL 9L, L ~ a~
2tc
u. o. 'I
0.Lj 0.0.- , Q.. D. -a a, . -.a 0.0c,
-C0M
c)m m ~ 00 #A
oo D.- D> - L.0cn 'U =~1 - r- 43''
a) o rVo1 0 V o I- 0u u C
hfV L s.. U VI41 0.14 0-4
0 E! cc ~ W I 0.L.L0 cV 0 4uL) 4 vL
4- co
C>
<I
L t. U 1L cL 06. 13 IL
U) 0. - 0 -I. - 0. - 0. .c*
- c-r .,ki *n rn
-- o cL L).' OI.6Lov
.flvI L.) -a ; .L- S
U-V wr~ Vs. wx L., c-. Xkv'usGo w M 40=
4.-~~ 1.-_ n__ _ _ _ _ _ _ u____ __ _ _ _ C_____ PooOl I"_o______"_ A
69
I1 0 1c c
Q. I -a 1..-' ) if I ' 0 M. C, CI - .- cx 0 C
C, 'n ffl a;n
0 -A. S- LA. coA 0 m. IM C. L.' V.L 0.) a
L 0 0 .=3 4- v a u.0 & 00. 0.I 0.0
0. UI wL
cI U . * a ME
cog In U~~ 0) 4- - I
'1
05 CL10 to -I 5)o, 0.03 )CL 41' c-- > CL'0 L-*Q )
L.C- In 5)L. L.0 L)S co U. Cc U n ccoOS5)5 Lf50) . &-4 J.flI- .. 15 L.A 15 - 3~-I'.- 05) E~~L, 0
5) " S. m 000a 'm I.-
)L, 00 =v M j-3 C
.z~
I;I I 4J 5) - C5
Il 4 L IT 1 L.
w) CE ua: a. I-L- t )- L).M
U7
0D
0
a,
C)) A
~L ~ a aLA a
c) AS IC
t Io
w a) W
La L. u
o o E 4 o~ 14) o-S I-Ea -
Lvcm. ~ 4- - '- 4.L a, 11 c-4U 4)LA T;~. W rL A a.(L
m U o U m Lc aV>
u- L. no 4)0 >0J. (J a Le,,~ .-
5--3
c)
LAe
I- -4 %
co w4o
cc _ _ _ _ ___.
5a)
o ~ o 41 -11 42 104 -. as41-~0 L.-. .1vUc
-L 0 0
Go Lo m) !tiH6
IM ___%________EIfMu_%A___ I
I C)
4)) E
'C~L in~i . f 'u~.
4) I'.- g
C'.' ca.f o cr oa c- U.C ) '. C'.'EE
I~ ao a t a aa a) 8 a
o 4) co cc o lo wc m o 4, ;:
ca a L
ca u c
tE
. LO 4-, 3
V L L.o o ) Wj
_j a> 'S Q.-M.C"o m (D~'C ) 41~ wU'I wU-. 9C cm.. &-
cc ex.ii USW u cSW a) C w .mv%-c oEC ucec U cc 3cC a-A Oa 'SEC
U U) WU ~ miO UI.'CXWUe7C
W -a W .- WLW -WL~CWW )LCT
w N%tA NL
a) -o W U.W. ;%-l
cD w~( w0.0"I.
z3 ~ ~ ~ ~ o ( ) oMft4, > N
L. u L.__
mw - -o A.. E w -- .
M )clc . o 4. OGJ -. c0Ia
4) x mwVI
a_ _ __ __ LAO Cn2
-. l~ 41- 4 .J.J a- a - ,
U.)~~ ~ 2: gO.- w : ~ 4 ~ .44-u..0. 5,3. mc MA" wo ~ . L.- wx 0 0 D 4o- mw oW= m
z(AZOZZU
cc 1
Z a
In
106
I* I. U
LIlu21;c 0 4* a
* 41.. 4j40 .
4.0fl36. ___
o oD
Un
0. D 0, - cx -' a-.
m c.o
m 8a ~aI I H
L
o 4, o Ko t
.I OCLj "I u
OE~ c . ~ UL
A-.- 3 o - o rLII 4, c
.r *4-t.
cC - caC-
L t 1. L.L
0Jj L _ r_ a o 0. C)'
ra - . ;-:.-'A ..- Ql. a. _j. >.- t. 'A
L uoa lo. WIj. o .(17 1;I ItI
it 111 uL.E uj cc o.. L> - z0 J
< 4-3 ag tAi cL c) ~ ) O L
.~ i-.~ 30 E0 01 .01~01 0 01' 0 r .WIJJ01 I- I 74I
0lI
(7
GIla G.4 Ln In
I 'c. l .COOULa.lf m.0 ~ cl a0 0.
UJ al O.O 0.. 0.O 0.. 0. 0.LInmQ" 6&I
w ~~~~~N RZ LQ % L c 4c l J
0
u 4)
014 .) .;^. m) a) MI V M @m
v v Wl lU 06.u0
0 .4 - Ln 0
C,.
WlM-
le-I
4j
I-~~ ~ ~ ~ , - Lf)___ _______
Cl. co I- &- c c
LI 0 -j m.-0. U
01 -j 5 ,.. - -i(a!.G t. 'L LLC o:
U LI~LI -.U.o
31-1 -v dll 0,
~ I- 0.~IS 75
0( IC
I 0-.- I 5O. lo 0 UC
u l al ana-
a n" o en e 0 of o' m- uf wfD &- 05.0 w50 NI. 50
*~ E e I S I I
00co-) op o I = o -1c3c , -1& omc
rz 90~e *-LcLL 4 ma, -, E.
C4J cx &5(5 w44 E,1
5
wma
u0 ca L. -Qccc -I-~~L L.)5 5 5
II _j vi c aDne0.4 cc u .. 0 -- a.
014= 1L -3, uL1 a L-L L
L C c L L j me. u
-~4 C-33 I-so 501h 0.0 O 1
Inl a3 .. jI m40 =It -c 4'L m l
76
I.--a
o )c z 's D or w
Nc In Inj Ln Do Ln wn 8
La.- .... * , L'Ln Da0 L k -o cLc ~ 0 06N 66 alt NLc
1a I cn.4 -1 cy- I ll I
C> llN e-.N l r
L - oNN L N- N N N - NI I : -;; 0 I I I
0 L(D o
u m0oc l
0 "o @1 -o Ix -
oL I , V 2 I4 L I I 5
" w u'u w 41. V'L I. a, 41 mo
in 4- 0441 G.,
cmL~l 4 0 -j4 .6 .1 _j4
w.- .- " WfM>L.=4 *u m~ W lo 4 I*La 11 c L O- UD CC -l w01 . 1
Id
IL n in ca% C e
Q6 06 __ _ __ _ __ _ __ _ __ _
cL4 L4 CL. 4J cL
LLL 4, v) "m I-Li 1- -1.-i' fmU, _mU-
0 L _O . Cii 4J
W .0.D c .
_____ ____77
4y,
C)
-0 LA
4OC -a6
cl.j~ I-.I* S IS S
elj ca .7 eJ3SL3 . 'U
aa a. m a. a a3.33 In. a. a.a.. a a a..n a. a
< L. I SS I
cL
La .3 ~ 4 *ULa
0C'J, 0C, 0 loo cla j3 :3 -o o. o
oa .co -9 .- VI4.co
'A- I-0
41 U, 9L
C)
%-- $
v a. tr o a. -u Girn ggn5 ch. -m a.x a. -o o.-. a.cc~
u L. L u co.. L.. r M a. am-~~~~~~ 6.. co . ~ *un un*-r
u. I -- U N jtj (
n~~ La3.-- 0
.0~ a.- 21 w ia.u .5
78d
w Iu C5 1oc 1zi c'4I
m cl -o z~,,
a. c
('sa4 ) U, -Lit u. Ct ~ o 4n(4t - CJI'
oif Z. cL ! IOoi 4) C\Lv o Io L o
g- CL o 41N ; U-a )) 0>0o ) I t It)-
L- awcx a - ju S o oKN
0 )
c> I- l . . - Z-
co C, ___:_ _______Q5m C- 0 V) -x O .4J
-. ~ ~~ ~~ Ot'U 0 f Ot )
oL vO 4 t C* Ocm) aa E cltO: a Q.q~ CU 4
4) ~ ~ ~ ~ ~ ~ L -c4) ck I ) U tC ~ U ~ '
w am . oot
6. cc
a~~~I - L1i 6
4.Im- a ) q 0 w L
-~--c
L 0 c : '0 C
00 aC - LC
0 CD 4) CX U u)
0"- S 4 C, -a) 41 04 U
C fV---L S- 0~ 1C 4, -i 5UCC4L~ LU '4 41 '-. m4 f )
5,54)0 -k .r 0. OC SI. 0 m 5V.- 0.s d) Cw 41 0 L C
a) 'oa) u) - . -- )V, .
004z >1- 0 ' 04 ex wS 44) ->,* 4'.- L C C *39 . 4
LS S-.-. 'aC ai4 C) , 'a - 0 0 34 S.>
SUU cu 0) w)U . E s 0 4 1 L
0>O v W C-' .C m -0 4) C C S 4
w.O <54. co 5 S 0) m mC'-4
w - >o. ;6 -V -.1 zA . 4 V 1 0UUO O)00 C SA 40 C
0 104 >,,S - UU C Z.- CCC S -0
555410)L 0'L) V. a) U 3tU 00 'V05-C U Q. mC3 C XU ) C 4.
v6SrJi 00.) C,- m. TI 4).' 0t z) 0>40 1)4 >0 0 V1 S..0 - C
C 0 U '- U' - .05 0.4 . ~ S.c3) M ) US. V- S- CC 4 5 ) 02--
02) 0 L . V) 4)) . 4) SCL .M 4) 'D00- 0> S .. C )' o *t 0 wU
a)-c) c00 Ca) U C" >L VS U'c .
C'thUS o4)a.-a) 0U 0c V X -- 4 m. 0 CC - 4o.). 0)0 .Cs.. U CDS X S.L.- -"
C 41- UC. at m'4 L. 41 '40 @ h 55
L, .r (UCS S.- m ) a -0 .21 &.- 0 (5 41 C 0 4) *0 ua)C) a 0 L 0 w 0- 0 CV. 0- C = V 0.o
S. 10 UVC 040 -- 4 0 0.C a-' .)- 041mS. *V CO 0al@ CL = 41 U U .
C40.AU LO LSC = -2 U' CDL C U* U )0th 4)14 S..S 0) 01 cU U 0 S. 0.I U m S'
UCOLA> ~ ~ ~ ~ ~ ~ C 4) 0CO' C5 . 40 04 4
S .0. 5 - 5 4 4 ) 0 4 C C ) V 0 ' - S 0 U A 00 I '
>U4 I-E S C4. 4 LA' 0 CS. S. -m.0 CU4o>4.a L w C7..CU .04 4 U4) 4)4 a, 3- 4)' 41S 0.
CVC a) VC2 U S.o .004.1 - 4- -U 04S. 1C04 0-s-A S. a) V'- Sc 1. 1 . V 0
cC 0 0) C 0.0o >44 a 0 US 0.S 4) UU w do V LA
VCS E U U 0. -- m. . 44U 0 S - 4 0 U
4) a, .0. S L.V Ua) V cu-' fn.4* SL4) C x 0 c . 4 4 . 1 04
'- ~ U0a a) 0. U 0 4 0 S . V U )LnU )
Ua 0.) 0S. w -s. VS SC t US. Vw 0S -' w1 0 41 * A -
4 U04 04 S. CD Um m0 4)U M1 U1 %- 4-)' U4 0 -
0) 0 1 UC, 4)- 41 UU 0 C) 0 S. S. 0 L. CS.LAOS'.'055'v 4)D 32 V& C 0 4-S. C: 41 m >4"C1
.0 0f oC C CXOc0 4) S.A U CmCUC C - . )
04 V4U a) =1 00. -05. 4C a) CU 0 U U >4 1 U'
Va)0a,4 'U0C I )S u - S.V S. 4 L) .
- ~ 3= S.1L4- S. So .02 4 > C41)o S.n -0 a, 0 1. . 1 0
~0 m'-C-5. 0 t O U0-4 OND.. U S 1 L 0. m4 m m) (D U C
004410 fC 0 C, -) S. 41 44 ) 4 - 0 'aC 0 .'.' 4) 0n LV5t 4 S S C C 34 C 4 C
w) 0 Cw4) uCO m. '.- 0 C LA 0 40 .4 )a,- -C C 0 Vc .C c40 = ' 41 0 '-0 >4 U m4 U
o4 S -- ) Ca) O U3 S. . vS .D 41 u m
S-L V V m 1 cS a) C wU. '- a) S. r). 4 '. .
0 -0 s S 0 0 0 . mO
U0 Ua .A- =-. U U- U' CD 0 0 4)4 U 4) U 4) L- V0W LCC M- U Z' C3 tU CUL L 4) 4)C V U ,
U'.-0thUI w0- 41-h 0 '. >0 01 S 4 1 M ) 4114 0 C O
S.441)U c -t a) a) o) M1 CS. 1 $04 - -L 0- M1 c
Cm 1 SU U C L U .0 0 W.~ W 4, 0 LA) t.4> 41 m1 41 .2
CS w)1. E .. C 0- C :0.V 0 -S UC (N04 . . . 4-
0C0CLS 0- I-A osC w- 9X CL. C0 S. U s014Lk, O CO 44) LA CL 00 '4 US m1 S. S.0010 4 C
U" ,.0 ) 4 CC L LA , -0 '- 41 04 C' - 41-- ~I s-AO u1 41J C- 01 ( 3 1 C 0 - @ - 4 4 4 L G 0 U
UM th' U'' US V0 m -S '.w 0X 'A* ~ A 0 1N E S 0 .- U LtS. S.'. U4) 4) U U ; 30 0. C. .014 1 4 - 0
41 W z)14 .0 4U0 4-) 4 41~ u15. f41 U 4 4 4 . 10
0" S .t a,0h) S. 0 - U 0m u .. o .W4. 0 0 4 L. U3 0 ~ 4 L A 2 S. LA U0C i S. OU 44) 4 A 414 'I, LA. C,; 4) C U(I U 41S..1-
LA ZU 1 v 41- %U cA w44- mC 4) c- 0 aU a'. '4 c
UCw-00 .4 0 0. 'A 04S OSA 04 0> k1'. C S. v0 Ln Ci C41 .
(C4 .IL S. C4
LASJ.UO L U L*-'1 AV th SC . 1 4 44- 4..' 10
'C C' - 0e
'D 00 U.'a-
a): CC aC-lc a)C M L L
C; A) At
CD Vu~ u .O. O
D-0
Cl'" 0 0 . 0 L. a o .
r 0
I-~. N- cu' N e
0. 0nn o COL an =2 0at -N C . C D N 4,
<- ^ &'- - .-Q3 )-ca 2! 0* 4- ) 7;0 CD . -
CD .) U ( L - cu.cx d) a). 0)0 'I0j aE 0. o 0 L' I. = C.
*- , 011 a, 0 )
I. Iz C3 I
CI- CD 0 wL,0.~~~ 0 0
L.0
I.--I.
L.q) 0 30 IWDI-~- ~.S.LJr u wc-4u 81
('J.. C'J
0.0.0 ~ ~ 000 .
0 - ,1 l -
- CL..-C 14C
0- CL
C m
A I I
CL c
C' 41 .'.-0
t! 0 085
075 .- 0 !
10
zt WL - (8 O m- -
U.u 3tL8
c. S-
LD
CD
., co Os L
cc ) CI Co. 3 0o 0a,, 0.
0- *.. 4.o 0
882
C1*
11(0 '4- 0cu .0 w 3: a) x 0
C0 0.0) 0V U.>,
0) .- ~V 4- . ,
Qj 00. E~.- mf 03 0 0
41 )
01t .71 X4 Cz
CL.- -1 L4 w-
C) LO 0
o ~ ~ 4 W, . 01 ,*
0- =0 0 o3 ) C) C z Cm 0
C T I- w0 0 4 4
0 LI Cj L = -4- L
-u D 00 w W 4-'C m --0I
0. 0' 00 0 4(Vo - -0 'r0 0-
a,- wo tm- =4 C, 0)4
0' 05 .0 C 'Ac Cj >OW=1
0 0 4 -z .J [:. ( C
(4 a.. a) C
0x Ct w~ 0.
0, -10 0. O t.. .0 .'0
0,04-ol 0- 4- 00 ( 00- 0,0
0~~~ x4 , (-1 01 0 0
CD(1 -C i -~ N 4) t 0M 044
0 010 m E E0.t-- L
0 0- C 0 4, w0d,- 00 j
QO. LA 0.. 0) c c 0 . C L -0)a). CO 0 C .0 3.'.'C -; C
00 L2 a,.( "0-0 O~.- ~0' 'AW C, 4 0 0 0 w
40-0. 4x- C0 50 15Z1010~~~~ 0.s-AL .1 0
Lu - 0M .- 0K. - = t (440) 0
0 'A 6.. om W - C (4 U0 u
30 0 - .10~ mw0 m3 ('(
S00 CW 01)-0 . . C 0C' .4 -
1040 g- -0.> 7 .- 4
010 Al >C 0 10-'-u0k- t.L- VO- (4 S..- CC-M'0
M~~ m o~ a' V-0 3t~- 'a - -
v ' IA a)0 03 u- 1fl *.- UL ..4 C 0) >0- C
L) A0 0 w'0' I;;-- 'CO4) kuC .000..- (410 k 4)0 01'-..4k..4r r00 c). 0 4 4
>,.0.4 - 1 0 w' O-1 0m Itti . . CI
w :30 W-0 ' CM0 00( (1k -
C1 g4 0. 04l 0 .- (4b .U- 0L ' 00'L. 05 ol. wk 0( - C75k~. 4.4-k 0 (4 640 . OQ~
44~~~ ! s .0 Q.-0 c.0 -AC w ~ 0 5(!2 4
L. C4-5 wu7 8 .'' *-) 44 5
COa 100 O O- ' 'A0044.' O~ - 0- V 0C. 0-0 00
10 .05 545059- z A k4A.0 104 41o -. C0. - COc 0 A L. 044-.- v 004.V
OAL ' ' 0a L. .. 00 0 4) 094 000=
83
4-...- -- ~0' -,,i.4(4
ti .
ly- t,
c C34- 0)
Cl. w m
ix~~ ~ ~ C) m04M0
0 1 C00 C . C 0 0
6- ,m 0W it m,
-, C- E.- cc-
m 063 I InC C3, w mC 0
w 41-'LA
1=
6/64
17
_ --
O ,. C 4 0 '0) 0 -
C C 3..- . -...
.0 0 53 0
0 0 0 0 4
Z
004 g 0. 1 a
S a II0
fN f .,0- 4
_ . . .. ..,.. .'
woCO .,
3.- 0,.
.. . 000.4 ,, 0.,_'
004) .04) 0C0 C 04)085
ELECTRONIC MASTER MONITOR AND ADVISORY DISPLAY SYSTEM. OPERATIO--ETC(U)OCT 80 OAAKO-79-C-027O
UNCLASSIFIED ACS-12-217 USAAVRADCON-TR-79O27O-2 NL2I3flflffffllfEIIIIIIIIIIIIlIIIIIIIIIIIIIlmmmoaammmomI uumuuuuuuuuum
SUBSYSTEM PARAMETER DATA LIST
FOR THE
UH-60A
-8,
41
LCIACA c AX
en 0 0Ucm
In.
*j ADl M4 CL 6- 06. I aNL& 06 mD,
WIm I- C4 M1
oL cc F ~ 0.~0.
0 -!!01C3 0:O LA5 c c
AL- 5~I .0 0 G A To ..~6 2. 0 C 4. 4AAS
GA 5 n n 0C0 5 GAC0 0A 41
Go- 0 1 c 4. ru 0m 0U. 41 .
0 C .0 r5A A A .
, 3c 15 0 m s
"MA~ m. C? Cco
A 1 0 .1 A c
0~~~ ~ L.W.LJf L..JUf
C C 4 -J
Ln 0co % CD0 u 0I . T20Z- L
CD, S~U o N . I'
A. -C 2V 0
0 0 0
A. GACD
AU4 c 4.1 Ch . JS.A.
I 6 41 u.. L
64 4A C3 ILa
m. LD. L.a
A a
U Sf
87
oo Ox; '
'A to Mo
tnea -a 'n (31 onf"a'~~r 33nO (n m 1 0
L)0 *-, *3~ tI .8.l In~~c~a CA*3 -j -- ' moo..3 6-06 "c mc Mko M L
cc31 6x cL cL ~ 4 C..(J3"M CL M "; m
ITS c; 'A a;~ t A c; A A"acl 31 c 0- . - O f .. I0
c- 0 o a1
- C t-m c2 C I .3 I o*6o o 013 oc m u
-~~~ 0 .- 3I m N-
o> o -a oU -- 3B~ z4r3oX X X .
W3 4) hl In'.3 ' ~ 3 ~ A C 3 0
o w 01tCw*, 3 4
0.~L (D .5 It-m 543 ) In
I I .~
0j Mn to 1 4fl 0o 1ILt 40 -in - 3 - - 0 0 0
6 6 1 - 6 C' 6 333 333343 -0So ~ ~ ~ ~ ~ ~~d v 3 3
- -- -t.1
-~ A'&A6-0 34 01.-
CC) - -
4-- L'Sbc L
__0 LO -
M o ~ ~ * 10 1 -cI -a 04cj. oc C.
m " I .J -. - : ac
w0 - 410
o ' en 0).. 0; o l 4c-. 4ccC 1 A. A4 cUAc 1c
m. 410a) M u .. )~1O
CC 0
Q..
m o)
Q) 4- -
M C
cla -- .*)
4A .1c
-1 4-L.I a .
US I oALI4
a C
0) 0
L N4
C) r- t
a,--
La a CL- ~ : -a.. o 0 c) o-I
Sc4S >aI0.La a-_________ ~ ~ ~ l a,___ _______
a Im,-1 -c
I 4
i L if 0. 0~- 4
c IIT i 'Vl
C ..-0f 0L'~ CL m'
r-* 3 '
4' an.! - 0, if i-i ; A'LC~~ UilfU' 4' 'a 4
I ) 4j 4 , Cif ~~~ ~ L *0o4 0 -
CL. *a' *.00
Or- zf0 I.
'a f CL 4
3ci 4J D
o- if Oz4 if f.
44' 'oi I- MC C O O-L I mc p f- 4 ' 4 ' i ' - ' - . f0
C f .4. f
cn i 4. r4' -. 40' U UC A
CLC
m 0. 0 ~ ~ ~ I C.n 0 ( J C ' f .4 C 4
'It C~ 00
'0 0= C0 L t Z-i
l- oCi Z. 4' if u.o LII 0,z t 5C 4- C i if 0 0 ~ 4
if C! .f U . ifinif I- 1 0 4-ifIL c. 4f . fO 4C aiff1
U 48 O C u'f 4
2. ~ 10~.C4m Z ,- 4 ' C-f0 4 4 C .4.0 (A &f s. - uC 4 i i n i f
Go CL S. 0.C -CL2i
4 ' 0 w' ' 0 '
0 Cu
inC4 '0C f *. '00 63C~ Cm C4i
2 ~ ~ ' ~ 4 ~ 09 0
co C; C
ac -.
ID a a Z- -6 1~ ' m
Nu cA I~ NI~s c0j Ne I ..ol
Uj u,4 C4 4.- fnU1
6 lIn 0 L L 6-C-cn
o L m45 - MI
cl .n A As C;
z L 41 IU>
4-. . 1
0j c
L4 L JcUL
41 *E :! :
-~~~~o 0 4.U- 0 5.0 00- - CL . -' r- r
-~~~I u 415 c4~U s 0 C0
I-.- Sl S1 0 cO c
O~~ N -, o L . 0 0Ln c
(D..0.0 5 9 40D -D____~% L445Ul.4. 04.40 040
045 F 2L
4/4 0 _ _ _ _ _)_ __ _
4/S a
C
04 00!L !
c 41 =NjvwL
_j0 j
I...4O K- , US .L. . O,_t U, 4.6 Uj
-j IN g -J 3 Go
60.UU 6>. NL j
-j st
91
CLLk M4 .C CL
M.04-14 11 4
4' ~ ~~~ L0- . 4-. 1 4). .
IA C- 41 IC a, O4.C0 -4 41. X. 4-x0
44lo. 4 0 - C
C'4-4141~~ 411'4 0I
0.
x 0 r CL . . 0 '.C41 f 141- 44
0.41 1 z 41C1 '
IA 41 0. 0. -1 . 4
L 0. .- C. - L)'44
4 41 el '4 )410 C 0 m '4
Z0 - C0.4. 41 .. C.v 3: 001 - 00 0. V
0~0(; u0 - -1
0 C,0; cO 0,. .0 UI) 0. C 4
uL - ' f .0 44.. 0'
V ,C4. 444) 4 a 1(414 0
44.C,.1 .V 0 S '4
44u444-; ' 44 It4 a O 4L )
0. A 5 l- . 1U 041 4- '40 '4 w.4 4 4) M4,'010W C12 c 30 4,
.~.CCU 01404 nJ 0.4 W'4403 41 M0 .0 >2 '4
04'~ 0 M0
4444 C il(am C C. *0 L 0 01 o
CE L 41-. 00 - 0
O0 4 0 .- ' 4 4 0 34 4,U1.1 C4'4 C ~lu
4--. ' -2 - 444 C101 4
00'.-a 0 3 41 IM . '4
41,00 .3441 4 > 1441 C
to '4 M 4 4 0) > . C
C o 0,t.- CMIa 14 .
J51* .!e14 V1 '4 ~ 0 0 .do '~ 4 0- 0. 0. 00. *0
.04 44 C'C
440' 0.. Z.C 0 4 1 0 4
41414' .0'61.- , 4 2 0 0 4,Mt.C4 J-f * - 41 " 0 ) "4 1
'441 411 =t! :5c 1 0- 0
O-104 34C- '4 '4 c44 -441 4
O~a'41"0'to Q'- ". 0. 04141~W 4-4 UC'40- -. 0- 0a L.
a, 40 1 13. 2n 2 A- 0 4
4.044 A -U U '4 '4 --- 44 1 0 41 00 * 0 0 4, .04* .
c 41) 0 IS =4 Vz 4, d,
44'4 440 00 a"- 4
U 4. 0 fA 44 w0 CL
041 000-41 4J 34J to 0M0
0 11 44 041 &A 3 4'4'44-14 41 t1 04 005
34 0 , I4 44, 1-41 1
'4415 A.0 A02 0.A0u1'. IA VI4 Vt
9. 2 4
I~~~I "I14 3 3 V .
%'J c'J
'U lC m m lo
w~~ 'n ex - xQ
L- 7
10 c 'o C% C 'co0
LAd%0 c u vgII
~ - 0 0 u%0. m0 :3IVc'g c.1 4)U z )0 2 I
c r_ o c I a)
I VI
- , 4) a, 0 . 1
di di dl.~d. 4JO0
= i C 0 c v di E'0 -0 d) X0.4CD *. 'o a) (U- 4)0 C% L M M
0.. C: 04 L- C .* .
0- 1 p "- a 2 C- I
w I>, Lc I. I4A 0 U 0 %d n
EC Cor d 0 %io- I-o 0l~C >-
L.Ja- b4. VA 0j v i-.. - i~ '
0 di *. - GJ'di.4~Iw
3-o C, 0l di U '44i:iIU . U U '
9z 1 K.- I. J K K )L 0 . )
I-j
ix c3
o -
It Ij S -moc t
K L.C *'~W0 LOCie di
_j1 0 _j_ _
93-
0~
V) -0 -a
(00 0041*0. -a4 00
0 c -000 In 0(.6i bO.4 IL0 C I
InD 0 r
en Sl en
2: 0. C CL. 0 " 0 c'
:3
c41
, 41 C D -r c- ..
o ~ m % ~ 0 w 1414
0.. C .S!0- c * C L
- C 0 CL
LiL
Id C, C& E8.
0 2 0 0
01 0z CD
5- 4: 5 x x W
do (M 02: 0 m a; - !- U-V
o~ ((4 U1 L041
- 594
CO 0,
IAc O c o
w~ 2!
L i (
XLJa D J
c0.
Li
C-
9- C_j _j
c 0 cotG L
40
ass tccJ t
C-5
4L1o
0) 4J C M 40 4
1.1) LO 414 1
L_ .C .4i 41
0 v c 2...W0 0 t" w 1fl.
V4. d. L 41 .*4v (" c Z> W.41id
~ ~C0 . 1 41 1 4.4.1 .2 0 4 -'04-
t.04 4j 4 410 414 .Ck.r
41 2C. M41 -41 Wvi -y02 k~ 0'- .- i4) U
0~~s. -..C.W n i0C t1 C ; =tg- L i 4
0041 CL-0
x t -* .C4 -11 .g 9 E 0..T
m 4114 i 4 0 0 -
72 0* 0 .- * 0 4.0 01 0.CL M 0
un t ! 4 1i" 1 41 N41.J.
ci V 1 0 41 2
.0W '4- U *- 41-
w~ LN o34 4.4 4ZM .1
ov W..o .0 ( . C41 co,'A - - C 041 41NvW I 'A 4'" C 4
_%i4 CW-.*4vi u
,1 2 L g1- L.v 30 2n-
4 1 O W .- d 0 t- C . - ..cN a >411-.r m41 .141- *x.0 g,~
0 QJ 4.4. C. ~+j~ 412 . - m
41 a 1 404U
fj '4.1 0 c r- Cvi 310. NA >1 o1i ~ ~ 1 1 4C 4
41.. . - . .. .u 41I 41 1 4.--
41 ~ ~ ~ ~ ~ Z -- 4C ). ~ 05!- 441 UV m -k4, 0 04 0 1C
c2
I g 0 4 1 a 4 1F a*.-) 7
in Ov C C.n
4m cm41. J OUo 0 4 01i 4
0.1- Le;i .4
U 0 1 .) 141C~~9Vv
en 0U, -a all -a 7n
z- a ls -l I .4I --1- MM 0%
m a-.- H a l . .Q- ow anl M n4 M'Sa M a5. 0k M ancja
Z5.4~~ In.C I ELL -a a*J. M 0. a .Ix .U .aC'l 'UIl cL'. aa a 'aD.a
L~a. I SS I ~ '0Qaa '.J0. c; a.0 5.444 0 a.0I. 50. a SJ0.0.c M4A.' A.0 C;0 In, 00 c;00L A c; A A 00AUA.j 0. j -04 0j 0.
4- Go. 0. . 0. .. *0.0 .
c- a-- r_ M
.c 4 1 - - 4 -4
U 4- U U 4-ILI,
C. a)1L. 0 D( Ds
I- s- s-.50
I-L
0 -1 5,5_j
o~V o o44
"o 0C an 0 0n an .C2. 4w - 0pLO
**p -a '5l E- ft E-.454'A ft
.2 M . 0 . No a. 0l -. o. Pe
5. C . 5. 5.97
d) GD ' oC
GDO0- 4)D
ZD .c 0 m aD * U U G
L 0. LcGGD . D
M D L- -uQ
C 0 0 G
0. 04..D a
GD 3C 00 0
0D cO 0 c ~Q. C ~
- ) 0GD 3 LA4A
GD-G 01 C C,
c m 06O D
0~ m ' m GD 0. .
CL 00 * G.
L c > Q.
U 0 L c;3LOD.
0 s WD. .C GD L 0 0 ..
D *0~ 1 41 0 'A 041
a OL C 0.- " C 06
L .0 0 wD.
**fo 3 D DD0 C 0
~.Gw wD - 0 .c
GD 0 GD 7- 0,, -- G
vD L 00 0 0.3
0 U !
06 84
-4 4ML
- 43 - - m~
W LC n cIc -1 c; c I 1 mccKil n n l mn 1- .
aj cl. i ~o Mn '.aCk L L a. M- cx c L ~ ,Mlcr-~O n. - . 0
OI a- I -nj
Lac~ CI I-. M-j I I a. I
0 - 0.4 0 w-0-
- - a a-, - a a t, oa t
a 'A _S '0 In 41 "0 a a o
c, 43 43 a, o)4f"a r L (ua4 z- -a
I/o 4. 3--4 34
'A G)= 0 U D
La LA o 4La 'a It Oo E a
a.- c uu ofu Mo c m4 nww wwM* L c. iL
>- 014 00 01 L5 0' 0 0oma
ccI -- - c - ~cL o a) a3 I w34
innic5 LI
- j =a.- 4- :a 2-,. -- - 43 .
4j0 0 -p
inI -A4 t nI.- w A
r - i a
1- 4A LZV4
41 43 30
meow
ul coa~
0mo enm 0mm mn In, mmmu.A I MQN;N .N -.6N C'.J 06 C. C'JCQL ,J
.5, *Ss C%5 CL 06I II II ISc .0 .MM 6C-Lcw
* 2C
cLC6 C36
' .0 A ~ 1- -CL
SOS. (uas
I-~~a *'.UI ;c M w445Oi c 4u. -- ~ rn L41 410 E~i. 0. mo .. 0E .tr~C * -t
.CW. oC. L.*-'s = m a OES T:4
o*m . 0 - -> ,-19a'
0 ~ ~ l 0.o mo-L co oW > - "I) C aI..___~~ ~ 2!:-a.~ .4. c, COv ~O Q..W 8l.a)~ .
M-Cc,I->v fi , xL
0L
amocwL -^-cr-
b45
0'f CI Ina.a.a
*0 -JS. I.4 L
4. 13 00 N
U 2 8- 72 USo m
w041 MN S. .ILI ~ ~ B ' V, s.6 c o s~ ~ I ~ ~ 41 . ~ f000 00
-ct- 0.
0* 4Z i ~ u & ,
100
4,
o cco
00) 0 I I
aa CL Il.C
4)0 tf c: 4-0 A AO
Li) ) C n4 ,c n
0~4 54-)aj C. c w MZ w .1i 2-: aE4 0 a . -i f- am
;:: I M.azC >
> a S-a* - - >.-'0o
.- W -L- co Q - .- 4) rz-0C
Ca C
M' > EEL'M W rIn >4 L. 1- 0 .[-CDMt L 0 C ) cC 0 . '-- O -co-.~ .r or- W tot
O~~ M a- 1-E LL - *eiL.~ t
C) > OC
CL - -Z AC- L4. in4~.aL- z
0
(n Go
I- a-4 c a
m .u
40 'a Lzj0, 4 0 ICL ay- C L -LU " W 14J 4 Ad A 0
Z101
C, CL- -.
ON 0 -
4- R~ .e
9-)0 9 0(9 co > =o r i
r.~ cc .V CU
aM. a
m m 0. 4
CLt't' u mc' > c 4(C - - mc 0 0
C)
C)
a- CL
acxc
%- co0 ~ ~ .(JOo 0*4 oL o
A' LInj . u 0. v~ am .C I W to >9 EoLL. U .- 91( UW i 8- In L. VA. 0 . w L. cc
0~e'j ~ 0>9L)u n*. - L( W ~ .L. n
00 L.
0 4')
in I.-n
inn
.11 L. 10 InLtn 1 cmW L L' LVLO
102 .rm S .- m r
0 C)
Ca -- -___-4 a C1 -a l
0J O. c -a
L-~r 0 I 0g 0.l 4-l s-. . ,L$ 0N >O - a c$.rC. o((4 C3 0 ,.
0.m 0
C)e
2!
-C rn Ini
I- - L . -
oo 41coC
Cl CJ C.C-
MU -nN.0w C I
4,I J. C 0
- w IS 41 06 w4 4w.' -a
InL .- 0610 =0 ;do 60 c'4 I ~ 1I ~ .10 ;cw
C2 c= C4! CCCC=C 05603
103
IC'. CL Q.0 .,L
.9c.
em4 N 'NIf .....
m >,aOC6c
1-' ~ ~ e .30-I C CJf> -,, . mf uf rC
Z r
m 0 !4
uC 4- c 4-
2E-
V) LLn
nocn a N LL II L flU C fL
CL
41 I. L
V Iv- e. 4.- a.. g
U1 -
In i-I- 104
.0
0*0
o
L-tf Caao-
~ n u a mL- cu. 0'
u,:-=o 0n 9034 Mc
m0 ~0.l
c) o-M0ERt
0. u m u L'. u 93.
,j14, 1 o W - >1jwuj u
9L a- vaca0~U0 co'.
oz
L-C o 0..6-0 -&V -C Il-ULun f0 n.4
JL c LO.. C) w .40 a;* V , .0
3 3 3105
r-0 CD -a
a, cD In
Li 'co QL
ce C l
oit a).42
o a. -z- -o7
I-. 04 In w.- a)G , = ,C 12
-z on > 40 Ino 0 u o
a D 0 . a>'
V o-.c 4 a4
00 0 c0
C L a)L. 4-C
SUE~-m ~a 3K
0 ' 0 .07)~~ ~~6 I8Zi 0~ UO .
0 0 0. D.i~. IIuCC ~ 0 *I~U In
txL~0L ) fWCO L 00 ~ .4
o
o M41
LLv Go Li. !i
& -___ Ij c r L
xLi
to i * &I.- _j; c,0LI~~~ I. lo.UWU L L
U I
cL 3tzJ," 3
~ 08. . 101
0 C
C-aC '. C7 o0V, o -
N.~ IJ* n I
a NJ CI 0 nc CJ C L
c3 , c-a A~ An
~ 0.j cC0.0.
; 455 - > C
oo loC)CC)' C N
C> E= - T IS 155 5
oL , Ec 1 ) m 4
o4, oco o 4
I-m 4 a . 1 L
0. L- _____ o__
mL mI .12.
~~r 47-L a1 cm 0. Ln'Jo Mn~o, Lno> w ;
cc U
c -cL L u&. c. a m., cc
4, r,-I. CL c o- u, -4 0ZA 01,3 ,-
a L. 2
v;4 S ;" "
-A. 1S)O (.4 Uc w .-r 'woda 4A_ A -KC
107-
L..J~C.. 0 * -**ac~ - .d x
0.n0
3 L- 00W.
II 4u z o> * -MCD > 00 01 % )
ic c'J
Co oL C= t0-, 01w
0.M a'' 0 > C M.,00~ ~ CI.. cm 0 W 0 =D M I~' - 011 /
I- I 0>, -O J J O U.,a- Mw O.*~e~-. o4m 0 0.
Ur V) In m U-,-U 0V ~ .
x C1IT 0U U04 r- 0. 0 C
2: -k 1
cr /~fl IO.fl 0
CL
. L. L6" V 0- .- V 0
n- 2 : 0. j .L
A a Li I.-, I-
L. 0 1E 6 UL. 0. W z I-!
t 1-LL W
j- Aniiii-j i I; 0.0,108
40
-a p I4' -a0 .0.
zn Ij T~jw ~'D 00 1.- 10 "410
C,- *L a*- C.J C1
, 0. 0. 0. 0. ,0...cl 0. *0. 0 '
C, A- A c A CJ An A-) -
0~CD
u. 0: 1) U md F- 0- 0L 1- co cmL ~
O RMC-l-- - ) di4 cc "0 - coI M=~C X4m 40> C) ap '.t U)
'0., 4040 0 . 0 CO ' m " CL) o0OJ 4 ~ - 2) z ? E c - wE
In L0 E X I ,S-. M> ul W aE 0 I
II 4)4 - LIL-C 0 CL 40 0 x1~ *0V (/I
CL =UUf 4 0
CD z
Ile
W
T L. L
.~ C;
4, - LLLu (A . 3
I- Sj- w4. SC.Id Z...- Lj AA 6-
ew - 1 I W0 - 40
109
it
co - en
000 .00 C; mON *o
010~e aae aa aN-N
ac al m ~ - a az a - ~ a - -
D a)e o en ca e on-3 N, NJ- N -N - J N
-a Wc
a ) m
r=~.- m wca..j
co a co mI-
0 cm 1)1~IeJ~ 0
InU0
r -: to M to
0~ to
ca Li W - N 6"s
e e o- 4L-- ~-I0.LI c, U I- It *1
UI - 9 s
.5 . .....
Cii
C)zo~
Of -C'
o n Oem
CD 000
I'l %.0 ICLmo
-0L In u c
:1 0 ; .,0" 6wA C
0m cc 0 v Ix ___ ___ __
w I1.- -. cn aI w0 7
zz
LI g vvzm -
m Uw I. I.o 1%0 U jZ kC --
ado==
(0 E c
0 m V)0cc 0
a, 0r CNa a M w(.4( 0 = )Z 0
aa a
I , . -Lo -s--0s-&
C3Z
IE 4t1 4Ic i .'- C
-o U > Lc
I. 0L
o, -1. .'' A E. Aa
14;9 u L .'I ,. -- %4.0 1(4A' S4. t'L. >--
tC, , f . oC
112I
D2' ,
C,, l 14
.- , 04 t,
S_ L. 04 aE
a - c oo . - c ) 0 c2' CL'. oo5
-0404 z> E L E c C 1 l
C0LMCJ 0.CI
E U m44 0) LW4 EC 4)-) &- 0.EELm m 41L C '
0 L .EEO L, US .44U '0 -2ML. S- S.. 2> -- 4 .(L 0). = E L)E u 0, L ) ! O
- L. L CC .C be~) S~000I-~ US -cc .1' 42 CLE c US0 U ~.
(D~~4 L)a-m 1CD >'~ O ~ ~ E- C ~ L ) .
=> W .4 W U
a0) * Z0- U DULoc -a w4> S-> S. S0>. I r e 0 ~ 24
I~~ 4) S ) 4 >
L.m LV. .
0 CL54 4k>L 4kL co~+
E5 w a- 0?'z V0L"0 4004 50 a 4
02
41a L.a L2 t L L
t- -C a a ujj a a soc
LI - rn *- U r11U
0 ~
'-I~k CDJ mcoi CA 1 tO
clen*.AI t~cCL
~t\J ~ I NNUfltfl m
a~~~4 .1e~tfe e
o- cme N e
fm en en o en
a
L I- _ _ L_ _
4e.- co 4- co elU
ve GA W-G TA .-o ~ ~ L In v-~r ..o ot
-D -a A-ovI
1:1 ..
- ~ a 0 Got co( oADctWcc- o
cI-, IL I- t;
v. cL.- u -co . L4L. en a en0oN0o
I ur I.- L3 F. -r - nI. ur
4. w It__ _ __ _ _j_ _ _ _ __ _ _ _
< cL. I-) )- c --j _j
v, fin.
44, 4. L. L. U N n Im. 3. IvL. 2 Z.J a.-a. 0 J-ctJOA
114
C, 0
oo LP.
C)0) >U
E C3 14 14
CD 00 Lfl 00 t, 0 '
zcsaE C%:U
&.-U UCLO,3
LaI
I.- 3 C 0 0
0- Z0.Z.00 W 73- CX CL3,CLC
Cc CL C L. 4,04J0
C Z01C .
0 0ILu1* , 26Ltx-C
+,3 'a 40 10 L.33 )
00 9 ; L O -j ne -1 O0.. -1 C C 3 _j L 03
Lw C,)Il- C - - ~ D - ~ ,->
- >3300 0 0 0115
L2
all~
La L
CaD
.sJ mC,~) t
a-CD L~
0- 'LI - 0cl =
o '
CSI
m I- COr cp a
T _j 04y i 0
a D _ _ _ _ _ _ _ _ _ _ _ _
Oo La E 6 104-9 La Va L. Uw t i .
eg ~ wa .- - C VI 1 TjCDW,- 0,4 1. LAL 0 C4 CLa?_ &e. ,I 0.. c-lo
Z 3. = :La0 1
~lie
-a C
C',o
4, .4C MC
u Cc1 7 1
e',,00
(U ia.- 0.0 0.-
C>-
- CDC,- ~ - 'II i :3L3 Lo L.
IIn
CL 0On CL~f 0m* 'C" Lco C.L ccl CL 4jc
0m 0 c 3
4n~ 9L ' .:w
I. L L L. CA
LLL 1. $.--A
U~~ -it_ _L I 4AzO A- C Wa 0.1C C La
~ ~ ~ .c 117
o' - C:; OI
0 105 T- C~0C4
* -O . t-I 0 a 1
LW 4L C~ 0 05 w 0- 41 m u 0Q.0. C, wL L 414 w 4) 4 1 -0
.42 .C .0.4 .0- 0 = -. 4= w ,'a 0 m 4- 1d1 c1-1 0 > 1 410n1 u C . 0
~~~~~ §.. 21 41 0 0 1 w0 1(. C
r- cl t0 4 co-
OIA 414 %-n0 InC
*0 ~ ~ *CI a, 0. L 41- 0.0.- 0 c 1'I
1 W0 0 u- .D m4 , ~ 1 u. C L
a LI 41 0-O 4 1 ~ 4~-
t '.0. . 0 4 ) - r -0 I.
4'1 Ml .- 0 mn 0 C.C 01
ac.- I41 L. U 14 0 V 40 1.I.
-U *..6- L. Ifl L. 400 - 4 1 4
0 "a 'A 04 0 u nn -- L O 0. 1- m G
2411 * .'~ - *- U Ig at
.C...4 410 L 41 0- *.E 0 01 0= C5 410 01 ~ L.
c.0) )dc c 0 N
-~~~ co .0 I1.C L 0.. .0D 0.0 41V 'll0 01IL 4
~4.. . ~ 40 41 C 0~ .r0 0 . w CL
4-~~4 00 3= 3-1.fI-f.0 In- *0 L C-0 Wn L 4,(rW 14 -4 4
41 41 0. 41 4n. 0W 1C OcII
Wn 0. In 41 x10
CLC w1L 041 41- " 4) m1- 4
o~~~ :3 ,: g,1*- 54
1- .mU Il/14Z41 OO I
1 0 w 4 1. 0 0n.. d) 000 W42-. 0. m4C ,0 41
1-- LII )0 E
C41 .C- -- 4101.0L4
0L1ac.w 00 .w CL m%1 a1- CL40 U4410 O.C a).. 0 - .l40
r- M1. o0 .- 41 m C v1 O 41 C
41 La- t' m14 cc C1. ZL r - C
LOU 0 S *0 -c.CZ LI 411 L . L) 0CI 4jC U K
a11 V 0 I u .C. :..0 0 o. p w .e 'L41
41 fl- 0u, 0 U 1 -'I*. 0: 41, c. l I.- 0.c c u ~ O
w L.0 c AIV L .u A am .c 0 L w1 al ~ 4.C 1 00 A
41004 = M1- 0J -U 4.4 J L-~ O=. 04c
LL c 4. mC 0w t . 0.0 .In- 00 L 44 In 4: 414C 0 4 I 1041 4
In %nC W11. 41 41 C 140m41 ~ ~ ~ ~ ~ -S414 11; IL0 t2c- K t
go 4)4 C -4 C4) 3. 41W m 2. 0 & 4,C
41 Z 0 A 0 C1 4, w --. 00
5.L14 00 W4 12 8414141004 414. 95 1 C
41 -C- 0. 0 I0O~ do 0 6 c0L 0 0-4. 0- 41 0 41 C33L= co A E
L- V1K 41 U.. 01 9L K 1 4- -iw0 0D41 1- 41 U0 A40
AI CG In L. -0 4--I ~~I414 Ew40
.. L = 4. 4
I CL uZr)L I1 16 .10i
~1 0-.'
(Ii 44 mm ODC ,N4 . C:
m- @1 8 4 -*mD.
@L meo .- -
zC. a)N (v N4 4)N n) 0 0LueS -C-. I - -- I CC N 1C CN -. S C..~-. en ~ 0, C)C0~0N en~oC JN en CN*
Lee~ e ~ * f N4 el o'cc - m4* m m4 4 . 4 .. N 4)0 .W4- 0..-0.r00 00 .- 00~~ 0.0 . C0N 40
w . . *- . . *.. . . * . . 04 *.!?- NC .. C..C C J~fl . ) ~ N
cC C)C C C4.x4 C ) D C ) 0 C~ C ) 0 C)C)D -cL- .N -J.N . N 4- C J --
mcm 41 Qm- C~ -. c
(3.4 = .)4
u 0 o COEC4,0 aC.c.- D Is t- OC vvlL
a.CC) CAD =0CU-LC
2 o M.CUCC 4-
CU
U3 L. L. -. -. C.Lu CC 4.4 Id
ex'C' 0.
4. W0. I
0
'a $-
4. 410 C L. .- w Oog. E. w 0! o 0 - 0-o
I.- -C e 1
3. J004" 41MI Ca: C. _j_j . p to I .
z* It- I0
-a .41 4 ,o U
M CLD .4nRLa M4CI'osoC, a~ Qc..
csj C 0L% 5( 1 s
"3A A A5- C;A A c.- A A-.~~csJcl c-.l- C145 5 Il 4"3sf)~~~C 0.-CI-I o N
=3 so u.~r- u'~ (j-s fsr.4
. 0. 0 0
I 43 . 03 0
I- dl !I-*
40 u1 4- a). a-0. 0 0.
0A iv In. 43 4343C C~~ C 0 . .0
41 0. C1 CC c4
2. 0. 1--t >3 4 M 43
Cj a CL
~~~-s C
I a 43434 0 CU'
Cj Lic i gi _3 C
I _ ___V__I
ICA I c 4 -
UO~ ~~ 00f' - ~ 45.. 0. m3 4 L.L . C
o~ EC. C I3r -0U4- 4-- #3. 3AA M. -4 ;3 0! aI-.. 0..- 0..* 'A 'A 0 0 -CIJ) 0N43 04 let
. 4 4300
O "3 AU )%I120
0p4) 0 41 w. uL
* ~ ~ ~ ~ M 4 01 I 4So L0 , 410. 0D 41, (5
M0 0 .4 L 0 m c a -W C..1 00 I
o1. 0 41 , 014 L. CIDI
4w 001.-1, (D C 40 .1- ?' 4 J1 - I-41 C C14 44 4 .. .c0 .0 U . m1
a) ' C41C a, C3 m1 0 20 0
-u c'.10 caA -r-... m4 1- pI. 0 4404
.OOIA1-)IA 41u M-- C 4 0 * > 4~.4101-14.~~~~~ w'0- 0 0 1 0 .c4
mI U 01 1 4 1 -I
411IA 441 - 0 I 4 4 4 ) caM4- .M1 04 O: C m
m1C'L0 VA IT 1-0 E L 1 4 40)s- I *. U 4101C *. 0 (v m-
- 11 - .c ca. 1-.w44,1. nAJ 0- m ' 1.- =1 (D Ix
44 D., c c ca % = 0 4)1 Cm-C m 41 44C 4J L .. 4 I
0.- 4444 1- C 1.C C>(.04&14 11 caI00 0
4100 ,; 44 .4- .- 1o~
4110 .C1 41 0 'V 0' 0m0 0 .0 4 .0 V444 s- 1 A
o04 a 0 44 C 14 L 4 1 I .-W.! 1-4U4 0 m 04Iu c. 41 .0; 0
4404.-> In. mA x-4. =- E- 4m1440.- V c10 1 4 QA . 10 . '-0.
1' 00 41 1 14 4 1 - 44 0, 0 -I. m
41 1,- CD. - I OC - 1 0 41 .a)-~ m 0 01 41 -1,.4' 3 0
0. CC 0) C M14 0 411-41-...4-0 4-A U) 410 C
L 4,4 .- .- I IA 04 4 .. a1 w41 L, I .- > 4A ='V1 .41 11 .
w 1-.44 L4 L..- C = .A 0 $- m10 IA CA In 1- ' 4 1 4 .I A .I
0. u C'I M4C 0 44O IA u 4 u IL .E4) -0.4 4 .0 Q1 - 01 I-x aA t
41.4. I-w 0' V.I 44- 0' (n -41 0C' >, >1 W0 54 4-4 1- C S -
o4-'l44 c4 00. 0 - 0 V 1 z CM1.0r
(1 040 L 1 0I- 4 (4 >, CIc 140,I 4 0._ cm 1 C 4' M- =, 0 4 4
4'1-41 0C. 0 ~ L. - - 0
c 0. 44 44 01.4 V I174
0.IA4441 m V) 0c C C 0 CL E. 1. 0a, 7141 .,m 410 - 0 .- 44
r 111, ..-- M 0 A a) .0 -1 41
.15 .. CV ,4~e *0 4 C.?4 1 Z AWA4'O >,-Z w' 1 1 /1 I .0- 0 C .a m. n ~
- I 3 C - >417 CL mA 1- ,- 0 4 1 C . 0 4
1 04 0 -- =I .. -0, ! ' . V .- 0 .1'
ITL 1440 . 4 4 =4 0. C ^ 41 MC 0 CI/CI WI CL 4' C44.- cc I
41u 1 I C .- 4 0. 1- 0
414-0.4 4U MC .~-40 40 0 O 0 >- (1-.0IA41-.,- C ~ 44 = 4 41 = I00 C 1
L-0 4 . 0- 0V '-. C41 0,W * . ,C L.I .0.41I0 U41 44U1- 4 .-. -'00 c. 1. 0'4
0) .01W 1 C.9 014 414 L C uI -' 14
0= 0 041 S4.1,0 .. 0 414 W, 041aCLI CIO04 ON mL- 444 'A LC m 41 '. M..
10 '410~A 4.- 4C .0.4 0 A . *- C C1'011-, -4'o u. m0 (1 41 U 14-.aa IAU 4 1J 0 t! 4414.
_~~> 08M0W C0C OO C 41 41_ r1'40 * 44 .- 4
W.4CO WU .44 014 C6- 4410 .0 41 41'A u 4A 1 41 04 .4 oA U 014 c4 C 41 41
C 0 - 4. 40 Z 40. 01U' =4.C C- CZ' ~ 119 ~ 4I ' 4 44 41 * & 0 341 0044
C.4' 1. 0 U0 0 4-IACOC41 1-41 41- Z 0 04-4-
1-... .0. 410 10 I 410 4j c-4 0 01*.
L.4 *r- 44.. c ; - 414
Cw C0 0. 0.AIO 4 ~ -44 4 414 44 .0 C 4 1 1 1 - 41 - 1-41
w0,. 41 -. -4 IA1 41 &4 C 0 41C1-1 IA. 00 4.0 4 ... 0 1 * I 4O0 CL L ,ui " A .
44-.414 .4) 44 4111
1-) 44C3 0121
OD 00 ~Z
z "' . m-~
OL Ct - CJ CL 06 C' LCu L 0. at
041 (11 CME C.3
00
0 MID
a) m. C)t. R"91w 4- . cm
-C CM1
Cl 2C 0 C)4
0.- Im 0 0m :0zI e2-- m
g .0 J3XL w C 1L
c55L)L
I- 41
*a: T 'A0
ix 1. . 0S
0 '500 Vt0t Vt L .
C 0 CI A ~ '. -t'C 0*
0L 4 n 1
122o
0) (v =
0o 4) E)4)
Z) 4) 00 (
:3 4.- >~ )c4.4 4)4)4.4 .0 --
4) E.-' ) >44 c
L-~ 00.co . -4 0 ., c
4. = 0 .0m4c
. u<-4t , - )
444*-. > 4 .4a0- ., m . 0 .'c 4- L
'4o
o a4 . . C vr. L C
a . 0 00 E
c>..4 ~ ~ a c) U ) 4
4) 0) 4
444 00) 0)--
0 u4 44)) 4
C 04 re4o
'ao 04)4 0
.0.0 0 4 a... 4)- fc
I4)-..;
4-0 C '0.4) L, 1j
S.03 4 4)4 0 )c
0, L) -0 'a~ 0 ()U
0u 0 - 4444) - 4 4
0C 0 .- 0 714
-Z 4 ) .04444 0 - o
UCL m) -) v0 - 4) u. 0 4
4)44. 0) '0> =020L 4- L 4.. -0) C
4)4-x co4 (4.
0-.. 0 4j 4 )0 ~.-4CU40. fn ow 04( an
64- 0 .0- CL 0---. D440 - - 4-41 - 4)4).
*-I U4 '4L 00T 0.0
.0 )4 4 0 - L- )
444A 0
A)4.4 4)44 c E 44)4. 0C 4-
4) 0 409 &1, 0''00
Vol) t.oGo 0 4.0--0 MI I0 -r- 9
44-)4 44. LI 4 00 a
4--4- .4) Q.44 44441234
SUBSYSTEM P'ARAMETER DATA LIST
FOR THE
OH-58C7
124
Q)
- 00
U,~~C U' ,N N I
14 If "aI
a0- a a ,~ U -4.02)4.
a M
o a,,a
m 4- m
o ~ N,
o- o -N N
- E4,x L xso aQ) o 0 E
o~~L c)N4 - ~ 0
c: 10coC 0 - ~ ~ C 0
CI a0> I) lo w ~ aI .1
w a u?~:I !I'a~~- Cm 1,00. 0 1 9 06 G).
w c o- m ,I-! im C
v) ) a)~ C
aaa~u -. - - -
a 4)3 ) 43 ,4) --le o )90 a o-c 0).-04 .- ) . CD41C
- I--~ #0I #
X I.
0 4)
j c - a- w . I u .-4
C La 120
I I- I~o0 Oo--
w ,C, i 0 I I
am cU, %I,)l
UJc Il l a-I a- CM4 I mN I'I
0.~~4 0. I01
o r ne znoee
C. c w coIIo 41 C. 0 41 E m
o .c) u . - I .. D en 2 . c , I L .J 6 .c . .-
u. I u L u 'a 0 u 0 L C I L
- 0 0 . U 0 en .GJ~ 2 .2 0 0T;0E z;1 z .5 >. U c L0 ~ . U U
24 C C : x 2! C 2 Z- 2 C: at 2: Co
0. "m 0l 20 w 2D o 0 2D 0- o C,0 O 2 0 2 .
m - - - - - - -m - - - - - - - -
C) 0o en0 N 0 0 0
cc) c0 CC en 0?) 2 NJ 0 U, men - 2 0Cn) I,<- o) en co n
Cx - 'G
Cc-a 01
o u;C4' uJiJ L~U1 U'
I _j
en-cj 0)0 U,-ne 00N-))OLu-~-
0.~~~ 00 -fl00~L en0 U
en,-.12-
* ,0 -I I l 8 m
'n C',L
I) I
w--0
a,,)~~ ~~ * u) U
-~~~ M). Go) 'a- d U)-C
cm S - I
C') ~ 4 C~' I' 0 C'
c- a-C c) -- Frd t!-a- d
0 ,.
414
ca CLC
aa - c
0 4 0 1 ' 4-U a.
L4 - c c 443 u11 0)a w.-. wav
a~al~a ,127
I~4 Q
WE CO 0 4
0.. 0 4.J) CL M
0VIL04 0 0 n
EC. 0 z .4 44
'VVLO C 3 C-ff m 4 4'
V'V 0 0
0, D .C 0. 'V-
u ' CD *m "aM4
0) 0. 0
.4. a- 3tn Ev 0 >,
CC>,. 4- 4-
c C" 0 CC 0-7' ._ m
0 k3 4 .L. 41 rn4A 4C 04
w 44 L I- S41
-. 0 0 Cn'- *Ln, 4 .)V I 4.
'V c C 0 Z 0 - 0
>.4 0 -
OD O 44' 4)3:4
eU 4 L un -C - 4
cu40 C 4)-4 V .C-00 qm= .0 'V )n .
"a ,0 .- :
. .C a4,40.a ,cd) ~ ~ o-4 V C U 1
0 a* ;9 44 1..M -2 IC) 44 ' V 4 - m 044 4
.0 u .1 - a u4 =4M
M.. Z 0 . m c 1 Z :2 0LU. m0. 31 6'0 0' - 0)0) CU C C c'. CU .. 4 'C4 I... r. c4 2 -- 0 a %
V L... 4- cm VO.- cL43. Q. c 0 o :3 C4-)
o ~ ~ ~ ~ C 443 44 . E On .
C j mn V .0 L, .
4-~~ 2. '
M4 4-EM .'.4 A4-I 44 C
o 0 - a ,4 .- it
C) 0-' M U-A I
c 0c v 0)-0- 44 C 4. L . %A 0 .0 04 . . 0 m A 44 0.
44 r-U C 'V UC. CL C = 0CWV -) W' 4 Up #a IV a,0
V) V.0 'V 4 44 44 .0 -In 34
ft.- .cm U; %Z a;4 .0:
.0- -I- C .- I~n 4~U128
aa
I) 0N %0 c a
fl~c 1N r
c,; M. cL - M
u cU , n i -~ el
~~~L 0 .e U, C 7
4) 0 4)4 4)
o o
>1 *. C C
*u u
mm 0 m c
:5 .
8Clo0 0 ). 4). 40
9x1 E (2)10 1(O
0) 0 E
c, 0) co 0 5
o~l o , CUU
I-I8
u LL) _j0:
I- jI- - co _jLa
12, 'A 4) E w
2) -s wOCZcaC
-A Jac,-I
_j 9L wdL Q0.L~.4
- I.- .. 129
LCU
W C4:4 4 W .C 4
L. ~ C -
0) X: ~OLC'(' ) C U
f40 , 4 ') L 4-
4)- 0
M.; U . C CU u- C
0)) 0
.- X r_ L
O,-4)--4) 0.)4.440
m 1A-- -0 0 .4-', C o 040 t -Lo
.20 - UC 444)0 Mr
3'M 4 4-L 0) z -
-0 0 V)0L ) 4
4,~ ~ ~ m -L .0 eL tou L o .n
0C4. 20 ' cla )O 00 4
-0 4- m C 0 -
04 4), C- - C- 4
4)~4 0
LU0 P0 > ~C 0 Q- CL -
t) C) 4 41 4J 0 0
Z04---m c 04 ) 44
L4r.4. 0 0 .L
A- O.04 .-- 4 .00lb4.~ >0=~0--4 04-.
4--,-4 0.0 C
V)4 0 m *t
r 4)4 L - 44-l 0009-- 4, - 0L
w ~ 4) 0 al 44 .0
to 0'0) >-, .00 E -
IL. CL4))-0)4 CC
.0 1.-. 44.-. 4>,> ~ L.4 44)
.. 0.C04)0 4- .130
___ m
en~c *j -- I 0.
CNF--a csJU,
NC. .1u j a. ac. c -.1 a. co c-, mm -woc.ua~a
cc 2- a.OI * au *cm In * I
o o o n cEe on e
5~ 1
D o s0 1 c 41 41
C~c c c c c
-u V1 4C V. 1
m L lo -a Lm ma
a.~~1 0x 10)I 4
0 -U,~~ 0n A ~4
'm ma
V))
I- al IT t- 1 11C114 c l
c-
0 ___ _____ ___;
Uucp
0 0 41 4
ix 41 1n 0
L9I
La I. mo m NOW G
C, c,
ummxz - a, c : , 0
0 C
0 04:t
C ~ Q L C U
4- 0 4-4 40 4-c) - - ) M I )
0 4-
04-U -C 04Z-' -C). 0) C 1-u V,> > C d
4 ) dl4
C 4L
4) 1 )
4) WL 4 >) ) ~
0 0 C U) )/). CC
4) A C
O~' L - 4
.C 0).4~~~ L4 AC 4 '0
o, . m
4)C:~ L-).0 4 u)U
ot0 t 0 .C ) 0. C U
44 4' - O 4 .m CI). r_ C, 4 Q)C C Z 0
C L.0 ) 0) ) ) 4) O L ) C I 0 4
0L01- 4c 4 L 14- +1)4 0j
0 'o 94 0 0 c 2 U
C) 0- , 1 - GO- 0 * '
L. 4 6 -- 40 L I0 0.
~~4: 4L -L4U)).
.0 .C'0 40,.%) v~ C44 Z, = '.) .
0 4) 0 '! w L -.4 3U 04 A CU)z. 0
- -~~~- C 44 4 4
- ~ ~ ~ I132
I I.1* * i-x., 0 -,no
~A
C) 4
cL.
Ln flUcc,
Lm U
I.o (., 7j
im a L('m 0
S CA
* 133
c0
m 40
'0
u
0 m3
C4m
Ca
C~i
413
--Aom
c-l433 CJ )
L~ 0 03/
a", 3/) c: a 30. cjr
el .t ,) 0)1
w Oc' I mIc\3(JO UC40- *LA cL Q!. Ln M)
LJU) 1 I 3011 O
LO 0.3( M. Q .) . M~a: I I *: I
A A c Z: 'n 0D:E1- I- 1343) -l I.-3
cz
x W3
u U
co 43
0j 00
cc ~ ~ ~ I CmL 1v ," -
Lla -6 A s*- CC..-
E 44-l:UC
4j- .C IW4) .3 Lc w
41 4.V3.
I.- cc 1.C O.~
-- 4-S 1.,3) 6.21 0@3
lo 4- 0 j U3@@ -j I.- u
011_0.L 0Cn~f0U
fin2C
IL 3 . C3 u3.3 a
swomo M-0 PON3 33
lo -a
x ~ ccJ m c'JtDc
U, .y. 1 1 -'M m -t2a -
L~Cn
Coe~ 0 s >s , 0=
41.~o -acoc L
V . a, 0. w 0.5 L.** L. c.U 4- 0U 4
5L 0 55 5g4 4A 55M
0rLm e
E
az -- uj .U r atjc
GJ to w 5- G-,~ to 0 41 c~t 0 uG
a. L 4J1 M W m u
-0C.J.-ItM- _j (A
t)w .,o . ..- o E t=D U OL 2 SL
L.~o U, ~ j
.3 Wo 41S 0In E ITT ,
o L,,. L,
I-L.C
0 C5~ ~ T
4-S ac I., ot I
0 L LI- oe LI. I ,
U 5L5 -*13.
) I ~ C,C, C5. .5 14D "5 lf . 1 1 1 5
Co. -W (, 4Co- "-4 ICIcoIli -I C
4IJIn CW C '1 C .C.J-) ('
* p 0eC.4 ClI Oi C,11 OiCLC l Oil 0,1CL. .40L . .04 .- 4L4 I- O~ C-4LI
Ln.a 40.CLL . .
m.l mt m.1 3E C.11 X: M.1 CD Y.u m ut:! .)11u ( tUeJU C'l 14el
-(. -. ~ll .1l. -- e l .- 1 ~l C4(4 ~ l
a.oeo ~ C.. cocC 10 0c
II. 0i.
o cc cc co 4,a
In ~ 9 L. VI 411 r- - 8
414 C Co Gle j 0ll 41.-. 41.1 tol L.(1~~~~ 4-I. C~.t E- CC EA .C 44- w ~ 4-
.C0LC 5. 40 L. 4 10 C LO41 00 1,
".0 -l 0. w a-lI.U 04D4
CD41
41 IAm~ IA
CL4 00- >- 41.0
O-- I- F5 2c- -
u14 4
IA
LI. 9 A
137
CD -o7 C, 'a
M -01 CIO CID C", - 8 )
a, II.~' 0 rC', 03 11. 0I C-4 I
3c1IC. CJ1 .I LeI U. C. , i. 3(vLC Cs.U* CLu a. CM.n -0.a
.,n Ln U, . 0n . 0-
(' 14 l' 11Il (M-ClC.
r I
ILI 41 w ILE s-44
t m1 4'm 0' cm; 1j0 044 &-L L1 r %-.l.-0. :.- 4 4)1, ; w :-. 23..41 04-.lf 0...
OD .0 0 DC o0-
CE .- ZC 41 C 11400.1 04, E>> u
0~v. 41w uc
CL -C c
'VL. x0 L mu0 w O.U, l/14.OL OL41 __ _
CD
A co
00
0~ 0.
3--
1.1 L. L
'AA
u0 0 '.. F41j3.--~o _______.______
138
a ;-
u, C) U C'z U , (%4 'n
*~ 0 *
C,' C, CS.40('- a
c-iCO 00 14 1 S S'a-- 0 w- 0 - 0'LC)* ('.02 9 ('4 WI (n
e'~c X: Ac mmmtO c.0. .%L
0 o C(', OD 00 E ('a 0 c u10i
a,. 4I r= L. (-u I
I--
0 L
W.)
- LU
IC) C 3
(41 L.)1#T
'CL
co 4
CL 4
4n 5- atWin I 11 c .gl .
I -If -0 % lu
W.6 = a. .6uc DC. - -1 0 -1 0:-6 0 j 44 .6N 9umC
13
01z z-
C, -U-
WL OI C:> I
mm.
z E
> 0
ca
m 14 0 w014)
C, m . .1 .CL.) 411
- >-)~ ~ 4
OL~~~~i2 4j 11 I~l
Inj (%.C InC .0' In
410I w,~ lI
LiL
U,140
01 .4
0 0 0: 041~' 4 - W4) 01#
0 .- r' .-D
CL 00a ,1 L
d 1 W V.C IL L 0-
uI40 L-0 1 4L
o > w) uC c-o 0 L 40
01 LW m) )0
01 4m.' 041 C,u0 .C = I-4 m.-
41 .0 41 0.0S - 1.C 1441. L 14
a E 4) 04
CL 0 L L 1
4) 41 m1 V10
, L C 01 41
00 0
L- C QC 41 I 14V w 9- $- w m 4 4
414 m 4)4 4
4* 0 m1
LI-
31 * 01 40 4)0c1 4) r 4) rL 414
41 0 C0-S L -LL.
l .L C,- 4 )E1 4)01 . o -
0L X
.N a, 720 - -C) 0.
41 4* 0.41 41 M -4
31 .6- 4) j 1( 4) a14 LC 4 .0 00A 4*
41 C 0 4* 41
4 41 0 in 004fa 01 0 00EC*V L 0 .44. = I 4141O 0
01 ~ ~ ~ c 4n4 3(4041 w0 4 0. 41 W.
V 41 CL U -01 L 40 0.1
41 ~ ? .0 4* 1',;1 1' 4
&I LI V . L 441 4 1..41c
41001a) c41~ r41
41 1 wL. 0 1 j 41 0.
41 0 0 11 4C-
0~ ~~~ 41 4 01 LL
-. ~ C f" -4 1u0
410 . 141
z a
-a 4-'a
LAVDC cs
Li a, 0.I
CC r*
w - = 4
o 44 d 43.
o- - M 4 4
4) 4
C 0-
39 L.
4D D ) 4c - )
C C
tIlS I
14
0
'o4
.0 0
a x
W- C5 m
0, 2
41ca~
0. 4
o
0.0
C r
06
CA 0
cz
4' 143
SUBSYSTEM PARAMETER DATA LIST
FOR THE
YAH-64
1441
iCl4n
8 Ic,
-e .8
I *l I L
wimm~f~d 0 D04~e en m I44- cL *%C~f I U,.O fLNI in.A
r- - .r0 oc1
0 .6 0 6 CL 06F 2oL o 41a 0 41
=1 o C C
C 1 W 1 0 C 41 0
cI E a No c ~ a I N
Iv, 0 40 - 4uCZ 4:' = IV 80I0. W1 IA L41 w1 4
CD, a; m_ 'z
N; -w - N
cm w-, CC CL) 41CC 41CC I,!a0 o La,~i 0.JC __w__CI __c
ina)0C I0~ 1nN.iO 41 (
41 . 41 4n . .
C.'
4J L U 4I. I. LI 0. u1 0. E nLI
_LL -E z ~ i14L
m31- La .. 8
. -I . - S.1 L C ~ a c
414
_ _ _ _I_ _ _ _ _ _ _ _ _ _ _ _ _F_
w P- --- A.
-4 z 7 1- a
cmf ;ul 'A. %L s n
4. Liv) Ox
0~ tt7 0. 0~
(D CD aO
olo a.-
4I o c M
o) Cn C C C4,D
I ~ 0 u,0 E 4 0 4
I ap U U) U"
5- 0 8~ 0 '
J, 0I. -j3 nr- 0I.._j' e
cc 0 = 0 0Li 4j .i
c vl-.3 I C La to I.
-0 ~UI. 4 L 4C A) 4' 414,4
o~c 0U o*11 Z; a' I
4,~
1c; -
.JL. 06 CL 06
:3 o- 0 c C
U)0 cm0 0O !) u u ~ U
I. 'LO.-'F -
'a U) cO o 'a o0. -. .0.-I0 0 0-
4, 'A Cl CA - 4 4
0 U041 3 C ,
00cmC 4* 3 -0 *-'
c4 ~LU U .- ' U) 0~ - -'
w. C & 34'4-
v U) A Iwo luC I
Aco05 G., Um 4 - L
C C L 4
in z. ) _j) 0 0 - cD U)w~ _
I _j pc I I U)
L) -5
if- U 00A1ou
LU i'U o-, wIC0. C"QJ
1474
11*oo CYN
w_ _ _L_ -W - - 1. C
C -CA-L 91 *a
a c- lc-.lc
u0.
ccm
*4 -- -
o3 fi oN N
I "r o c
'A 5I1 r5.
0.0 .00 . .0 . .
41i A-4,4
4A)
cc ;Z .- L
z- L i2r
A. w & w o . w , C - I...-" Q
o 0 005..0... 148
0 C .m0 C- 06 a,.? . c01 C
*~S1 43 ft1 0 u
o n U0 . InW 4- -
L n C4. In- 'V 4 '.L.4 3
a~~~~~~31 4 .:- .- *-4 V .3 8 43 3 43-~ ow E .43 - w =.~ V.3C
Cuo .443 V -4 VE "a43 0.
C C> 3.-4 -43' 1 4 2 0 - -0
0I- + ~ C.. =-l I-4 V- 4..- 0 m.~ 43 0040 2 C
03 43 A4 . - - '.-) E 0
EC 01 .+) a,3 >1 V C M41 G X
43 CO 0343 43 IM 4 0 4 0.I 03 *n..-4u0 E
.4 c. 0 m 4-C 04c0 c-4 ' ~
0> a;- 431 C 3 csj.. E1. 434 OC V V r,=. L.4 0i 3 \3 3434'a4r_ 0
1-0cm 043m L3 m-.. 1"00102 4 9
. 43 433 0 ..
43 ... 3 -0 4 0-.- 0n. 4 4E0 4(v4 03 43 w.4 0- 3 .4 C C, 300
4- 4-1 3 321 03 0. 03. 00 04A
C L 43 un m.4. In04w - 41 3- 33.0.4-~ U3 C, M.94 In M3.34 n3
o 3 c4 4C 0 >I0 0 0. o -4I2
m 00. V.3 .LIC 43 C - In 0 .4 4.) U3 42.
o 0 Ca 04w a. 0 C 'D43 W .CLV 33> %0 ."a0'
a-3 V.-. 9 40 m,34 c.1 =4 C .43. 434I In4
w0e :C33 ll.n . I 3 0.1.- .0 3-
C ~-1-) -.44 C3 In WLn W334 ->.> - 4 ' .4 0 4. cm 3 & CD 4. MC * -
Go. 43, =414 00.4 4. . - .- m 0 m 0
33 43 ... ' v3 1 V.00 z, IV-u 44343 j 430 w 4.424 03.0 1- *0 = 3.3
ch w3 1-43C4 M CC nC1 33 1
4.0 m 01 L, n C3O 044 n 0 34000 43 a) .- 42 In V)3 4-00143
1.- 0- 01 u- 04 43 w L.0Va In 0- CL= 0- M 30
* 0 m34 0 w44 43.'.L I 1
C44~u 4 43VC .43 0 L. 4334 a-~0- 43 .- "a *. .0 10.0 03 cE 4mc.- 00
c 0 W4 V.m 4V. W3n m~ 1- 'A41-n4.3 3c4 430 C. 0. 00 w 43 44 - 4
s-0 Lnu 4) 0 a m44 3 01 -. .43 - .- V m1
m44 w- . In3 -
0 CWn~ 6.. C 4-3 43 31 In .JX 0
00.4In4 -In3m
0-I .44 v344 u1C40304 03 031 241 m = =
343 03 -. 43 431-CC -0 0 4.w 4'44
1-43 3~. C 43 -7 N 400 0' o 1-.- . 4. 333I. 4
C.) 'A 4. '0 4o 0043 In C 3 .0). 0-44-1 r > 033 -4 .. 4 43 3 n 1 1-.4 .00
, .!!3 0m . V c~44 0-4I 3 1 4.1-3 0 =433 433.
'V CL .44 43V A .10 4 In 033 0 42,-3- 4- 2 43 1- 43434 .4 -343 C 3 14 3 . 1- 4
4!4 "4 1-. _03~4 43 In4 43 -3 I3 01
0. 33 4 V= * c I. Z1- v ~ ~ f~-
0 -.0, 00. 4331 4034 COD Vmn- 3 0JV- 43 00j 30 4314. 1n 43 43. 43 434 3vt!4 -V- -c 0u a00 .4 04 I4;A3~e
Lm 433- -a.4.
1 4 VO % C.
& 3cI z 3 0 - -n.U-- Mn 4l1-
c 0.0. fn w -
-,0 3 4344 ICU,433. 4I2 j 3 3WCV .3 .I ~ * O
4.3 - 0 4.1--4. -
0.~~g a.9k A'.v: In In M_ c; 0.C . 43
o~~r . -- = %40-
CD C . q In 4 .- IY
U ..- ..-3~ In 14.3jI~
&- 0 >1.1 0
41L-04 0 m.
L~n~ V
C m 4)1 C 10
0.
0 0 m c01 41 "a
~~Vm C44 41 . 0 0CC. 000 0. X: .. C4
M1- =. L .CV11.L144IJ1 Dn4
I'a 0 0 0 L a1CC IV> CWC4 Q 0 41 .1 c
j. L 0. 1 C >,0,~4
x114 4 3 - 41
04I ~ 04. W 4-L -
41 *,- t-l 0m4 0 ..C V n
u~C~4 c 1 S.-4 s1 . -L
a,~ a,141. n 1 4- 0. * 1I
> 14 u O C C C- 41 41 0..
cm441. 14, C a1 41.
&1L-C ~~ 41 V u V 1 4
a ,l uL =- 4 1 u . 1
0 '-1 GJ W n C1 In4mL >-M04 OC 0 .C 4.0
0 . -4 4 1 , C O *.- 41 0. z . 0 .
(L' w 4' L4'.4 041L~ C -- 0 4 1 = 1 UC)1 4 '0 1 1 In L 1 In 4
C, 10Cn InU' .1 .0 0E 0a, L. i cm c (4 VL V 104
a14 C ;r. 4-..C ;o . .; 41 CI.C.,4 IOC=I .0 - 0 a)..
CO C, 1 Q w1 C C CL -I 0. .D0
a,41 L u ', .. a) c 1 1
In 3 0.- InI -- .r ~ 0 ~ 4 .
4141 L> 1- 1 II 1 - 4.'I C4 V
C ~ ~ l Mn 04 41' In c-l .. 1 I
'-> ~ 0. L.1 n 41 A
OL 4 u I .: 0 0 C .. .. .4£,41 I:f -n 0, -:0 0 41
..- C 1-O 1 . C . 0 4- 0
0L 0n 4 'a n 0 VO I i 4C1~ 0.L L. u 0 C4 0 . 41 L1 C 1(CL11. . L- 'a4 0.m L. -
41InCL-.-40I CC- 0. 0 41 41 0 r_~41l1.1101..-( c.£ 4 414' ~ . I. L cm1 4.1 C
014 0.0 0 C L Lo -0 4 4 014Il.04. m1 40-.' u' 4. .10 C W' W
V 1 O n O 014 4. 41 In 41C 00 0 uM0. L. V v..
*-, : 05 c 41 0i 0 0 I4 1 -0 C1' 4 .c1 In .04 cm~ 0 -0 0.41" =
V41304 C-0 351 4
w1 420 L
LI4 v£. 04'I &8£4m. 416 *V u'. s 3
S .,4'4 M OD ZC 41 cm 3. 41
Cn L.-. *;; 1 C -1 .o 41 C- OS 0 1 4- a. 44 V ol-
C~~~ 414 E0. . U-
L.- 0MC .4 LA E L'C IV C 4- -0 0
* ~ ~ ~ ~ 0 gr -K u.114 8-O0 I . U I .1 n
.0 5-. I
150
_ _ _ _ _ _ _ _ F
ar :E -
.4W -m co.6 ~1c -. .6 -1-- A
caL '- sw - CC [; OD
L~~~2 c L);"- a-- .- c-
s 0) 1W) d)d, EU ~
4, o~ o 41c. -0-0 c.-
o
LA. G) 4-4- >) -
z 0 1- 0!-C O C C, d) C)4
C) CUE C'aU
- 0lo I
0 C)C)fl S .L~~~i3 -G ..CC)C '0
-D w al4~ 4
0. - -w
D C)cL
< 4- 4- C, v) 4-
Q- o 0s- 0.ac
0~~o o Z1 1 + )-~- -,t 0 v Il "1 11 4. 461 4o
* , I C
_ _ _ 0 _ _ _ ' '~_ _ _ _ __;
If. 0 41 vi
0 1 _______in__
4A _ji wJ o!U1 - 6 X()Xt jm
c) U) U
g- t- 0.
4A La0
06 06. C)4L6 a
0 ' 0 ~ U 1(1
;vP' i
cl Q.C
-CL
c* .-0 -z i c - I
-J u
~ZC) Oc
exL -c u.
di Qn- mn
0.- 0.0 0. u
CL
C>W
a, 0
Ci
LaL
L..J 44. .
L. at- ar dL w .9 -
I.- 0152
C C
C 0.
z 4 C IV4
u 'A~W1
GA =.4i 0
00
*~4 0 -4.
0, P, N 0 . 0 L 01 UQ. 0 . - 4- -.U 0~
.C 44 ~ 4U C in. Cac L C . 0
L ft3 0 CL Uc11.- 0 .0 Cj L.-0 W 4.#
LV 01 r .6 ., - g-
0. 4. 0
k4-
- a' O U eO c. 4..
do X, CO CC fu"0In' - 0 U CX
U, .0 . 1 04 01
0 U, 3V 3.U
44. A4, 044-U, 4 C-S4
4.' 0 ~ 0 OLI U,4 00~ 04 UEw ;
41 IV~U 01 0U
0. C 0. 0
44 C 0 01 - 11 04. 40
C=. S U,3 UIL c 44
0! M- -4 011 I 4.-
%- 4-- 010Z4Go L. 610 O
L.~ 441 L 4
U 00 0
-a. - V 04. "04 S- 0 444 C -- C
*PM L J .0 0
elm,0 U 0 - 0, M34- - L4- 4.0.
S - - '0 ~ I- U 0 U2.2 '0 F4 MU 5 1 ' 4- 0.=
4.j L U . ~ 40 U ~ Cul 4
41U !~ .. " 415. .
t -2 0. * o
0 0 1 0 i' 1 'E U4. I ,L - U, C
440. U4 U3,051 9" t
v vv :5 U
- ~ ~ v F4 I.~ z ~ 1 ED -.jZ
£4 -%, 01 4
A- 420 js.D .CEI*>
r %* - - -
'a 0 ~ 04
in .6
24 - -a-' C-4r
w - c~j4cl cN c-
ul Ni.J Z L3c8I*.i
ix-.- in L--00 4,'
ino~~~ c~*~0OLfl C % -.
o o
x xI-
41 0' o
2 co
C C
4j4~ ~ - ~ - iw N14
LIL
rI.- 0S£ ua
. = ..
_j 00x. 4
0mw _j
U, -,
9L)
c -A
1154
0*
w a; Cc 10.
Cie
U. C - 'CI
LoJ 00L.JCL .0L- k
CL- O
ww
CL 'o
0 C)
C7S.
P. 4 i a n . n 41'A4 0 4 j 4 0 4 0
I- -
31
_ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 0G9V. 'A
La t
0a 01 L
ol z- - L's
0- 06- a-
- CCc
-. - LD
L.) <
o 0 0 o
0. o
'a LW
oc 0 o - .aC 0 L O00 4V 1 0 4
LD
0 ~. j _ _ _ _ _ _ wo t
L) U .
LL bL L2cc
p~L 00 4- m---_
u1 0 _4- .
20 34l .
V 0 C .x1 r3 0 .o 1 Go'C. -. 4 C 10 4
43 -0 00 I .0 C -n 4-C
C .4- Go if 85 O= w3-C
-, m4 .0 0L1- MU 4-C 40.1 0 1~ C- 11 03 0
Ch-
Q. 0 4)
12 toC 43 0. 01 c. 0M l o
4-~~ ~ o-0 * CL.4 3Z . 4-u 3 4I O 4 i r_ 4 0,0.414 O .w . 01 ali C 00 0.4 Q. 0~~.1 G14 434) 0 - 4 0 4 L4-2L. Vn 0) w4.1. 0 V. 4) L.
41 Q . 0.1414 41 .- 410410~ ~~~ 0 43 . . 343 4 L 3 3 -4 -/
T~ 4)(4- 00 433t43 0. 0. 4- u 0. - 4 . .0 4-r0 0 3 . £I 0 . V U-
43M . 0- 4-.1 4-. 0 4-0 -i C43 V-1 4343 Q -. 31 3 ~ .
- ~ 1 4-. 0Vo - . 0 L4443~~~~~Q 43 544 IC 0 £eJ -41 -0
.- 0 V 414 1 . 43I. -0 U41. 2 1, . - 43 0Q. '0 43 10 43 - 44
OUw n di V c- 04)- u. 4m 0. 0 0 m
42 LM V . 4 - 9 4A (A.4 3 * .L.1 C41. 213 Ell 4- 41 1 C
'0 3 40.6 V J CLC 43t
fiI 43. =. C - I- Q m-~ C 43U,-4314 4 u .- C 04 0.4CM 314. 4-4- V0 IV 43;2 43 0 14 041
.43 V-I1 or *m L4O 01 -0 0n CL
0A c.- 4 04 . 010 0 t! 04. C 04
43.- 43 0 S3 C0 4- ,.~4-. %..44 4- 4.L.I4
0 3 -4334 3 0 j-C, C. 0.0 004-. IMO N- 40 DQ~ CL. . 0 Z; -r- =1 w4 cmC- 41 4 0 . z. '71 4-111 I 04~In 4.1 4.1 0* - -C4-4 0 10 1- 0 41.Cl3 4. 43 0 3 .0 01 3 .01 4 * 4
. V V- Li do1 .61 .i .f U t 0.1 4- 1 b0m1A4Lt.(-0 -C0L-- c1 w-. C. N1.-g
.- 0c 0 lC 43 -L 0 -C .3 00 40 - m43.-- :T- -V .0 .0 1 4C 4af -4 c a02 0oa0 41 =3 8 =- 4
03 KC 0 1 .2 4= E~ L -a- 4- L-
00 41 .443 .1 £ . L.a u*. IL - 4.4R 13'- ~ 4100 4.4J 0 fin t Q. 4 m 4- 3 ~ ! 4-.I .o - *-,- 0'- 0 43 0.0 1 .41 0-5L = =4 £ It pa 01 N CL 0
3. 43 43 43 43 40L. . 0
V 1-B - 4- W-. &4- V'2 .0441 - 3 0£4433. .. 1- 06' 4. 0. 91Z 431, 4.043411 N3 11. --34. 34,434 in1 C4w 71 5cf.
; C1 M C
44 -. - 1I - a) 0 0 0 W CO 43
CD4 4 4.1 1 o Ol0- - 0. ~ 4C~~~~~~: 414 14- 4 31 . 4
*4 .- . 4 CC" 06~. 4 40 . 4
Is-
41 uI * IaI 1
157j
-. ON mv13
0 CI
- -L41L
-9 An o_ _ _ _ _ _ _ _ _ _ _ _
4,tu
ca U
z n 9
ad 3-
- z .L=Dc.0
me4
42 L
-I m -lo loCC
ch p4 .u -j
45v c
tms P2. is a. mU3
158
-V Lw--
- .44 1
-~ I- CNU.LIJ 4.1 -
La -- CD~a- js C,
0.~0
0 In
L gU6, u
ocwe CD *
0. 4.4
I I C 0Iii' mccc
a
I3 u13~ 9.
159~
cICr
MO 0
.- c
0 L.
S. j )
.3 0 >
U 1 0
0 ' cl E= 41
0 0-w
Z-m
13. ~ ~ L 043 4'.0 SC 0 C .
4, 134 UI4
CL-;; 0**.38 4. .(
4.4 4m . U% 4'1 -
~~~ -r m ,44
-m 4- U U0 3
c . 5' 4 '- L 4
L. cnf Z ~ U '
I W, 4* a, 4' 0
cU 01~ 24,04,,
V; U I, Z u 0 0.
m, A
-0 -- o -Z 4333
u. -M v 4
- ': 0
.9=u C V4
IL CCLL 160
05 0 O.
z z w
w3 C3-e
P.- li Lnc 0 c
C OS %o4
0; 00 0.3
In =1 I,0. CA3, '. CZ,
C3 4
CLC
z010
I-I
CL
5 o 0
06 4. c
71 41=4 S 0o -.<~~~~s a S .u t4
m L. Ln0 04-
C3~
IV ci OE 0 aL) C 2 0 0I V=O -m
0 C 0 CM 181
0)0
c" -a-
cc C "
U.L.J~~~~ -1 -*0C- n0
4, C D co 0
= C4 00 0
CL V) I I:
CL L L
41 cu414.0 0
C,
- 04 4
z l
4A 0 0
Lm
4, CL u a
CaCA
LO CC f - V, 0.'N0 > Gi (M fta LC41~ n0106> -
m C, 0 L n L.(-) 4 . t
162- c
44.CA
0 w
o o 41o
0 *-o CL mO
w 4 4C 4-
o41C 4
Va 3 ~ C .
in u
.0 CA01I- 0J0
c V 410
m cn V0 c~ -
- 0 W j0. 4) c
L. m .m ~ 4) do
o cr. 'a. C 0 c .1
4) lo.- 4 4J*.. .
CA U - 10 -2 rL
o - ' CU 0
4- 4-4 m. WEVL CL = b 0L
C 'A 4- .3 00
0. 0 C 4)E in
4- CL WW E 1
+j CL0 0 4 -
0 2 OF E VC .41
o 'A0OW4
ON O
V. 0E =1 '
~~~E- CA n. 4
~ Oijin 1'3
10 m
z
.M 6).0en-
'- - Z;
0 o0'
LU 4Z U~ u
- r)- L~~*. 'IUflN~~e c~s~ ~
N~N 00
'A r 4- L.L )
(~~4 MA- '0.Oc~ 0. a)0 0. 0. " 0. 0
41 6) L- 4)m C) .- 0 A 4 C- - CD
cz C4 C C4
a. Q.
a. m r-3 CI3
InLU
LU) - c C. c-c..
0.01
'A I..) z.U;.6 0 (- 0 0.~IC L ~ * -( L L
2. 6) LU M 4
o u u 0.4o0 GJ . C 6
-2 N . ' I C,; C) S.
16
0c OD **
'A ,- - %a
C= 01 In0;
t, 0)
L~LJnco CO cc
C, --- : Cl0 C L C1 CLV
a, a, Q, 0. C. 0.-,
0 0 430
(-*0 U W 4-x. )2
0 a 043 00.
CDC
00 t40
I I(.
X,.a
0Lr L. w3
93 .*c0CL 014 0
0. 0 000 o
34-3 to
ZZ 44 43.ZC 403 3
%J --c _3 U - a .1-
v OP
S Z. .S 3
U. L.
a 4c- a.. ", l U___ ___
I.. 6
0 OC.f
z- -a OD -a-
-- a
LU~ w 0 -o
C, m,
00
di d)* CCL
F.o 0 0CL 04 0. 04
.43 0
L. 0 0
-' m i 4- . .
0L L 04 0diU-ccI.-~~~ CL 000 C
tn0
z U4-
V,wd
4. 4UC1 41 44
00
Ci CL-LcR
_jC u. 4 .4.
wl. 6. A.
udi uU. I
Li . 41
166
44 Iwo . 4
GD 1
Ln .1C
V)ol 4-2 D
do Co wOGCJ
CGD 4-
C m4
ms u'G 4 - 4
o' 06 GD o- D D G
V U0 006C. G
.0 4-' 4 t, o'' ~ '
.0 40 c~ d) >GD GC U 0W G
-U GD ~ Q 4-C
V - . 41- *o GD ' o
d~ U' 2. DG 3420 42 V aC ~ ~ ~ ~ ~ d u'' a. .,'-
o c. GD u. o-.4 w
GD a' ci s-' ;D4 C O
1; GD aD 0 .0'c-
31, 3(' g G
o,: mI %-+I- GD 'S'- -a
uc c 0d- 0
2C el *w 4,0D
U'G 44 3G4D o'- a' U.
*Z U' c- le 4-G 4) ..0- V0.. do 00 -L -am0 'C D G
04o m 0v Cc CU0-D
.43d 42 44
1 4 ,C 4-4 -V 2. 4- =DGw
o =- a).G 4- 4 4D 1 C aa 4 ' GD UGD C G--9 F- U' U'4
U'41 D0 w- U -GDD01 G
- V.S U 5; 0A - GDa a0 4 a.
e-' 4 m ~ 'A Go 4-' oD N -' G
4-~~ r WC * G ~ - o 4 G.C1 -'A GDG 44. 4' L 5 . o6 G
GDC U'2 Vc Lo -n - C G
Ri - 4 U"o I0 U' % " I
GD! -n4- U4204. U' GD4. G
1-~~~ ~~ 1- 5 'UtD - . 40 0 a
U'U CVC- wo L t
_404 4A AD4A
44GD~~~~~~~ GDA~-~* U 0 - 4 D G
0.01-- U 0 E 44 24 GD44 7
_ -I0 0 0V>
z - -
- 0,
WZLA
.<.
0~ a
2w, L, --
S 0, ,i
C LC0
C5
o o
La L
L-00
0 .* ' W A. L
1-0.0 0 168
"4 4) 0
o~. 41 u ~ '
VC o 4.400 0 CD
o W3~ 0... 3
.1 u 0 a =" 40 )..-m43 0 Q .
.C4 om. a3 cc3 V 1. .
.C C 0'
m 3 0
L- s3 - uA C >*4m~ c 0. w-. m 4 a
43~~ co - ~(D 043 '4 D' 'a44M. u0C . '- ~ . L0 0. 00 0 CCo
4-)4- 431 a)04- o'0 0 fl.C .C O , 'o
o. CL00 o.. oA. *.- L-D
's- X 4 1 C-C' 1-. M. 4'0 ' *j 040
4-) E 3 . . 443> > o~~4 4
o3 '0 o. Co-D M.- v4
00 ~ ~ ~ ( 010, C .A .4300.
U. .C (u 044,4 c -4o 4 iI- y, 4 1
4)43 ~ c 1. . *- >' . 034-434 ) 01
43 '> V
r~ c3 0L- o. 4
0o- m C- 00
Z ~ ~ ~ u '0-o A 03C
4-'30 a-4 .4 . . C.
0D Go 1 434D *
IA*u IA '0 .. n s-
o43. o ~ 0.L IJ 4 .1 00
w I 4-01 * 44
430 414 '0 4-43
to a) . C- I l4
X 434 '0u43 9a. 4 L'( .4
4-A~ 0 N O 4
0 Orn '0 &n
1694- .
APPENDIX 2
FAULT/PARAMETER MA RIX
170
oL
1OJ4UOD .Id z I I*O
'ISIN AObI lanld Z U x
qSIH AOld l1fld I U
eanssaidisAo 1103 04land U;Ufl IqSTII
ainssaidjOAo 1103 xland uTvN '1191
- uz.jL deee Z U
w~j, deeg I SUB
Cd EN z BuzS
'a ~ ~ Z w.1d SUB
r TVA OPTS qSII
4 Iflowd PT Ou x x x x
Q~ xjpuaddv a9g)ma.pe,4vopuxes -nduj w0wt 000I qmV0Wt 00 0 _4O a q C) V t- 0 I, 4C V00r O-OM- a
2uTj~nbeV jlnud(~mmmm
.10uvJvd OBIuSUto
(010JOS~a-a 'SolvuV-y)AITITqvlTvAv ~ ~ ~ ~lVUuTg/jOsues
'I 00 C C CC ,
z04 z 00 00 aa. ado Uo It4- 0 - goM00-E.0
4~.~ lii %~- .It" 0 tso oa 00Cw 4 00 4 mm .aU 4 k %wCO00 -C 4 0 0 6 46.2..j g o o aIL s a)ss1 E
to E.400000 JOO 44j 4~Ja .' .I P5I.4 O CP X 4 3 -D. :0 4 4. 4 1--[-.4 aCO0?00 ) 4 oUW U U W W M M O 0 0w o g .aM IOU 0: C9 a'aI4 I .
TITA PANtOJIUOD J.Ia z v I *ON
q3TH AOTA lendA I S
Oaflsas9djBaO 1103
aiflssaOJAO 1183
iedl OPTS A01
w1jjL deg Z 1US
* -- wjj deefi I SUN
tiuj 9UTSUOS
(0 z BU
43 - W~jL doaq Z BS
.0
CO4newl Zl BUI 'SI
WTJ ee U
*0 _______I___
E-~W~g U43xpadyaS
E-
(Oja 08qW1- Isluvv OnUNo
AI-lqlTA(1V~uBeddy 005)
u 4
4j0W~~ BISU, d 0S.0
At0qW~~ 44 4444C
CS t; WS d444.-.44 C .4 14 4.4+) .
-000x009
000&( 4j 4'. 4 f'S chC 4C4 m.0 t e.
cq 0 $ 4 454 10 V) toJ~~ £01
172
lITA PAH
IOJIU03 lidU z I I *ON
qOlH &Old lOa I j
9jnlssBjdjoAO 1193
Ionad UTN '4;01
- wl.j, doag Z u
flUA OPTS 401O xx x
T1vA SuTSUOS
co IT'd sulsuas
0.
tTTVdOPTSqD3TH x x4 x xxWT.zjL deg Z Sua
IivJdOPTS OTH >4 xx xwTij deeg I Sua
*0
C iflwewl d Bu >4 x
CC
E-(Z x~puaddy oaS) c, mI Il ~ -
c ujtnbsH sjInvd c) V - I C13 to~f to:4 JOlOU1vJUA GChTS -4C 03' C)V
0. C')oL C4 'n 0 c'
* (e00nociolo-C-. C.O.C-) .C.444 c C4C OnoC.. edAj
JOSuOS/IvuUS
pojinbll .osueS &O x xx
d 'A
0 0 0 to u k0 0 02a~- -4) 0444J 4 0 0 w0 4 4At k
M .4 4 J Jd 0d J J 40 d -, 0 0 CO04 d .'44 - 0 U) 404J4J4M 00 4'0 444 4A 0 0) 0 o4j+
0, c a Sb-4 0 0 .4 49 WAS. v 00 f .r o0 0. 0 0
4. 0 1- 4 4 0: 0. V 0 )U 0 44U ElNk.Nw 0 0 8 E .U 3 ^;
0a ~ 0 ,0 .4 M,44101. $. 4 JW*OO0m 004 bO k 14 b41 . 4. 4J 1 04.I 4 k.-
+A4 4+ 10 0 4*-4 $4 4-4 4-0 -M f k I UQA 00.2c 9 boI l4) 0U44US0 01 u. 0' 4
"t M002, V+ i14 00 axMA0 04 0.4 J k0
13 02.' 0 soa- to-to 60 0 0 4, b 60
ca . w -OM 0 1 C4 :.'qCC9 0
173
r..
r. _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ __a
TTva aTI-X sng 3VE
od I ON
0. 90:1WJquag z I T ON
x lU STV s s z I *ON
,4 .4- -1CtC Ct Ct C cnC 1C C ~. 4(.4-.4 44. 4 4 4 . . . 4CSC ' C C
JOZBUUJvd Iwm$9A9qnS
0 0
to00 v 4
S. k 404 0 E.0.
0-1 0-u,~ %41 4- )4 . 40. a: oo 0 04J00U 0'154 14 -aV4 0, 4
.3 3 od C9 . 0 0 o -
k .4a 1a4 4r 4 *ga 4
Ja . 4 .74J . 54'S=.. 11 tk0 ,44"*Q.4 4 0 P 1.0%>.PJ.30 ) 0) A 4. 04.a4
00E. 0000UU84 4Ji 4J 40--k .s p 00000OO74.4.4vc 0.0.0 m 3. 0 030to
ow 004~. 4 ) no .. 44 .r0b b 0 4Jb t.0 4.
174
4)4
4. ~ IT 4 i a Ti-X Ong OUmCx
E- m _____________1_1_ON
c4 l9J~ e SV Z I T ON 0
0. JOBTUOU O V I O4no
-4 ~ qV T A -C- n4 nITUST/i~ses .94 .49.4
0.0
0.0S41
00 O.00
w to0. kk 04 4J0 0
jU k0004"
4A 44 U S
~ ~ ~ ~ ~ . Mq M-.- O*G on I~S~
175
+ 41
4)
"Io
c:3
0
- En-0
co :3 0
blO 0
0 0-o
-z 0~
0 0
A II'A 0 V 41
E- 4)ojsu- V21uvv c4.L0
0. 4.4 0 4r
as=0
V0 e :200
41 In4.' 4) R.
o0
4) 0 4) o . W4) 0 0 a a a 0 .4(D 0) 4- 4. 4-. 0 0 :. 4 tob 0 4 -V
0 44 n 4J ti k54~ It d.4 ( S. W 0 44 W
4.4 4 It4'C O~ 00 0i24C4OJO, 44 41 >~ od ."
. o Go a4,4 W 0 0 044 I 41C4 .- - 41 0 V 0 .3 *0 0)
0 0 0 0 001.0 b 01. a) cq C4
V 0 4-UU 0 0 aI aL- 0C. C .3 00 Ml .4.4 0 M 4 -44414 S. 4 O 0-4 Q -
0 .. $ 04, 1-. 1F 4- 4 s--. 00 4 . ,I .- WV- '4 4 . It InS 14''4 4. C V 0 E. . $4 4 4 4 . 1, 14 V .0 040. 4 4 0 +P d. 0. 1.- -4 -c A ok V .00 Q4 .1 q1 fl 0attO ' p... 00 0 bo.
4 0 I4 rl to 4
I aOOMU4.'4.' 0 WO0 01 p 0a1 0 -,f0.-. 4U 41 It 4
0 b 1 4 4 Q- N4 4"UV I It 4 L) -'a04)
a~~~ , -- a 0 04nn.. . .4 N 410.
to WM M ~ O 041 -1OFM~ 4.41 0V 0 W bb 0 4.' 0 (D..... 4cq1 4 .41 Maa 0 -. ~a ... Ue p..a0 4 6a a 0414, 0.-
0 Wmsmo X GV0Wb o 0 4 D4
14 If0 14~-~b - 14 c4 4 *4 Q4 4lGo 401
176
4.. 41 41-4 --
W 0 40 : 44 041
w0 0 0 415.. .. 1. -4 a
4J *--4 4 cc .4 4 N-4. )0V. 4 0:I ...L A d.d 1010 4)04) 4) > th .4
0 d 308.4 0 4 0 0 V.0 1 .- -0 0 , 0t) V44l. 0 o 9. 0 d d A.0.0.5.. -
1. V 0 .4 88 d = 4 s. A A -4D 4 4 0 4>I 0. E 0 .4 .3J 4 4J 0 be4 . , w' .4 4 W S.k t -4 V. 0
CI 0000JJ2.4'. u 01 bih dbp 4 -A -41 CUl. 0. 4,) 4.#M'r4 .4
0. ... d 0k b4 0 Cd ~ 4 4 d ~-4 W4
4 1. 10..~2.- a - 4 -- 00 0 0 e E- t' 4 00e4J ad .3 5.5. a -444- 0 1 4 )04 4)5408544 0CC ,I4I 4 0..4 es93 d Id J 1. OV U 0 :1 149 -S.0. a-I0 CCr-Ir-4C.00M.0 1. 40
0 0$. C)0 00 "0.4O Ow..
1. E0 E. 4' 0.0.C=C010 0 -4-4.... 0d5 Wu ~ ~ ~ ~ 0 V04'V40 I4004 ) C h.A c o G
41 -4~ 4'4 Ok 0 Id Mwe 0 C 4) -Ad C4 ,) 5.C4 X. 51. 04;1
-4.~ 0414. 0 00 4)-C.C4.C 4..-4444C00 M.io d0 4-4 4J c c CO 4 (aw 4.4
,4 ~ ~ ~ ~ a d d a 0 ~ 0 0 a 04.4- C0- 4,44444 A 0
041. C3 0 %3 amaOC C3 a).. 000 C t L) 0C'
0
- 0 0
> 0 00 0 0
S 0 0V0 : 0 4.'
04 00 00 0l
0.4 4 0 1 ,0 4
0 -- ) 4) 0)4 0 08d (64 0 ~~0 4 0 aJ 4 0 c 44
-4-4 4-4 9 04 40g O .4 04
4)4J H 0 qa4 66.' 4 A. 0 d s d4 0.4414 a4% 4a% 14 f44 4 A 4 00-. .05. 4J4 T Ct
144W 4 . .5 . g a to0 04'.~' a C014 . . 3 . -4..8 .4 1 a" 8 4J 4d
d .4.4 V84. 4 - f 8- 4-4 0 -
4- 4AV1 J. R 9 k-
0~45 4J 4 440 V 4 "t 0 .401 4100
545. 000 . 0 .0s4.14. lk* 1U4 - 4 v4 04ww( r - 44 300. a
0 4 4; -; 4 a 4 14ba o 0,-0 otEa uO a 4). 04,4,4qW0 -1J V 4J4J44J 5 ng 54454 S..~04
4 0I C44 40,l .444 0 01 1 I 4wCa0 03 Q4 04 . CC-09 9 A.44 .0 I0 m 0 A .0 W M 0
-P4 8 88 U8 8 0, a . 4 x~~ A . L
MI .4 V 4 . .44 CdCC5C .4A 0 0.t.0 %b.0%00 000a005 Jz Z 0 00 000 U 4A0 + 4 00 O C. k N .1 ,17S1F
- k S E.- 4 (7 -U - cy --c r 0. i. 9 9
APPENDIX4
ROUTINE CHECKLISTS
178
0 (3 02 4 0 )0 00 0) >
4,>, 0' >
44- 4 4,
E 9 s. C -0 4 d~ 02.4) c4.j CA. 0~ 0) 41 od 40 n A44-
4. m .- 4a d22. Cd- 0 4
02 0 ' 0 a Cd a,0J400 .. 4 r. C V * . 0 ... 0J0
V0 0 Id.V4. 4 :0. 02 0. or- r. s d
0 Q) . -k at k a) v V -W -a1.. > 01 0 0* 4- 00 r. ad 0 a00-4 RO 0~ W 4 44 'S 002
E2' -4 0) 0 '4 0 m 0 0
(D 0001 2 > 4j -4 : M2 cO ~-
41C I. u4Jc 40 a)
d 0m (4 w 136 ad C oOU MOO) .-44 d r as b
c2 D0 0 o 1 uV 0 0 3r - 0 Wa- 3d 0 I04
u4040o 2 02 02 02 02 02 C 0 -4 000 a 4) -4 .-4 c.- v4 o- .. 0 r
4 44 4) .4
-4 ., ul " 0 c O R, -A 4.4. s -04 0) 00 0 0 'A 0t C o 0 at.-
0.02 0 m 0 n 0d 0 0.3 0 0 0 02
0 ~ W a) ( M .40 +44-
r. U- -A C) -, :5 co C) Z4 0 U4 D) v i. .004 4 4 4 4 0 0 41 4-
a)- ) 0m )3 0 0 00,44 00. 41-40
U(D -J0. 0- W 1.0-)a 0 )a 0 c :
_4 0 c: a- V020ma-c4S . 4 , 0u. CO r_) 0)p )c( - 1 4
4.' 0 ) >O > .0 >- >O >O o u' 0 0 W0. 0.o 0.1 0 0- 0 0 0 4.0004)'.0. I-E- 14 +- *)z
4) 4) -=0 4 0 d 0 CO m 0d W c0 >. c:..(D0 W -(a ta m- 0 W 0 1 4 .4JN W m
CO Cdo )V 1 - 02'X80 ad 4 D:o 0 1 0 0 0 0C ) 4 00
42 4) ~ 0 Q)Q Ac A 4 & )0c ad ) 01< 0 d 5-. as 0. .1) MO 4), -) . d0 4 ) a 00 0
0 3t0
W 00 - m . o a-
411 0. - 9 0 )Q04 4 0. . . . . 0 0 14 1 CO. 14 02
1791
a (n
04.)4 4 .'
0p
0~ 4..'1
V 04. 00 4J24-'u0 o a)
.' 4 .v Wa 4 Cf 0 r.
4. 40~@0 . 00ow 43 4. as~ > 0-D-0 4 V.'C 2 (D4 0
41 41 l W 0 0
@0 M 4Ud 0 14 4* a 1.o r. i
40 .7 x ) 0 a- S.f
0 0 -@C 0 0J3 0.0 -0 -a1
4-' U ed~ W 0 -.a.-2 C
4 0 MO) ->4'
on c.o. 0'(2. W>. 5 0 0@3aO 0. 00C
0 -f 0 Cn 41 r, dLo dAd 4 3ata c 3 'o.- o-
a0 wU it ).- ap -1 0
)0 Ad 04. '. 0 c0 E- 0
41 14 4 ro. 0 -' a
4J U 00~ ~~
-4 0 4IO !to d) 020
0 ~ 4 0 di M 04'4
a a d a: (a =. 0
a 0a
U: U U U U U 0) U U04c 4 44 > 4 0 1 4
0 0 4 0 0) 0- 40 41 4 0 4
M0o-0 o 0 r 0 (Ab
U) 2 -) 02 >- 4) 4J 94 > v z 0 e. z 0 034
0 d0 ) 04JW 0 4 W2 0 0 S.w 0:.d 020 z 1 . 0 - 4 0A4 Q -
d l . 0t 0d2' -,4 Cd -'.L ~' 4J ON to 9)r 4
44 02 a 01d 0t. oo (a 0. 02) Q wr 4
:, 40000)0 ck4w
0) 1- 44. t) 00 1- 1-* JO CI I
54~- to. W .2 0.9- - 1 4 4f0 4'4 COC013 co 0. 06 0,'4(
4) 0) 4) 0) 0. 1-0 aZ
000 -0 V -0101-(.2 0 40. 4) 4)
180
:1 C -4 (Dd cd c 1. ' 0 z :a..C+) -~44 + t.) 9341d .06c (0 . Idd 4.4 . c'5 (aWz4l x ~ a44. , 44 bC4.4 U.0 - 4) 4 .0 0 O44 dE C~- CsU) a) .4 i .41 .00 Cdz 0 ~.40,f 4) d C 4 4444) ) a Cdd ::)
4) r. d C.4 .D0 a 0 R4 Id> M r.CO~l.0. D 1W0-c Qmr. t 4) 0 ' w. c v.-
( -40( ~0 ~-4 sW 0 .4 cs a) .4> 'd 0 Q) 41 W CVa))4 a) .. a d- c 4 o0. .c 0 4) a)..4 (D )05C.40 4 50 > W4)b ' -- o. 4..a)C..)a)Q) . 41 a 440.Z() Q . ) 0 4 ZO 44 0-4) d 0.
:3 - l) .0 c~0. 45W4) V 0 '.) 4-s~ (d04.4C a 4) n 4 .9 4) k' 0. z .0 a 4 C.
.. > 000 0 a F I 1'0 d.) 0 0~ 4) c d)0O.o-d 0 4-'a 0754a= 41' 4: ).54 cd .- 340-w) 2 . 0O-. O d d *a UC4 w C)-d O w c O mfn R Ca 0co 4o 0. 4. f C c..- 00 00 z.-
,a 1 ) 4) U . 4. C4 0) w QL 0(.(. -0.4 LO4) 4)L 54 0 4- 410 S.U CZ;) E- OdC3 U 0-:3dd) a ) -C0, -4) ~ ~ ~ ( :3 -4.. 41 W d OW = 0o 0C..-
> r. = -2. 4)O 00 C40 U~ 4. 44) 0 r.0O70t-4 4) r ) 06.-C 0 dUO.C 44Cdo 0 4 4 4 1 .C 0 2W) 4-O 4) W4a 4-ia) M0.d+ d C4 ( 0 r CZ 4 .. 4 C E W t) 40 u 4v a) (A>I4. )w 4- - tQ r 3 Aa 40 Id -4 r- >.c ' -0o 0 d a) Z)CWm "4 4) . 0 - .0 .V_ id (0 -4 C) r.~ to 1. 43Z.O IM Q) 4'40'.0 0 4 )0 0 W 4 5.4 W 4-4
4C r.-44.4~~~~ 4) a 4 3. 0 0a4 5 f. ~ V 4 .0 5 1 )V w to 04 E4 4.Z(0 a) *~~4 0 4) 04) 0 Im d) (D c '4
d)(4 ) C .- 4l) +045-4 111.41 ECEO
0 d ?k :3 d C13 Ua ) CO9 .4) .0 0 ) Q) '0 0-0 - E-a.44? 4 "0 k41 0 dk a)& O4)d )SVC ,.4 4.4 0 4.4 If4 a:lC to-A -.4 ) 0 0 W4)~tV d4)0 . 'I 0 :3 bd E.Cc' 4 0U0 U W4J d4') C
40(s A 4)) ..4Mc40W ))Ca) 4)w4 sO d 4W 0 to.0 '-04)I- ..U 4).d -4 c C,) C Wc ) -"4z U) Z b 41 u
4 .0 E a)t) 00 0 C w W. 0 04 1 )0 V-4 d (D 540 5. 44. ) 4) c 4) d 0U. (4) =4 060.* 54 C 0C4 w a) a S.lz 0.0 E .. a) 0, S.).)2aC. 02)-4 Og -)44 . 4) 0 0
d+ 41 ( 544) a O c c" 0 d) -) 5440E0 w is00 > 41-41 C -4 dW A.4. 020- 041 .4) Q C- 0. 0CC.). 40 VOlo) >8. 4) W W 44'b44 *W~)) ) - O -A .C W4)0 , Z 54.0(D0
) JC 0 e4 .4 0''-.- 0.~ 0. .4 4))444C0 c-4 AV-e d (4) 0 . r_ 4' > d) ) > 44 . 4) -A * d a) c- a) nOa)..C4).4 r (Aoo Q 0 4*C 14 4. 44M
01U 0 N54 ) 4)700 4) 0 1 Dr 4~4 ) Q4 W -
C o c a 4440 d. ( . C ' 054-1 u a44 .4 o0 >. S4 V'C44).0 ) ) a454. 4 0 0O WZ''V) 04- 00.. kO 0C)c'44 .dC 0.s f0 a.j 0 C11 0 0 (0 U . , I0d0 w L 00 0.C 5 ". (.0 w- V 4 4 D..
4J Id V4 M d 0.0
w ~C,4 00 F'5. 0.0(.w4) 0V44~ LO4 w4)z .+jZd. 4) 4 4 in IV40.. c) a-, w 0 c~) 4) a) a 4 od'c d .V 4 m ) 4 .0 d ' U5 l-.4 4 vc 1. 4 4 04 0 'd M Z- (4).4 cz 0 =1 u 0 0 4 -* CO.. 0 WV . *.C. E-.U
zO 5- ' ) () 0 44- (4)- 010)4 0C 0)a 0.- C 00)C4O 4)4 S- o )c-~~ .. s 00 4) .4 j~)00 020 . 5 a 0 H4 1 r-.0.(). 4 )
5- 5- S. r t - W 4
u c ~ ~ ~ (40 (4) U)0C 1 ) )40 CI D1 D7V d d0. 4 . to , 4) oU aw eCCb )-)c bC3 zWw d
U).
00.
z 0. 93 z Cd.4 04 0 0 00
0 4 m 0 )
4)E.4 .4 4C
on 4)
0 ) 0 0 0 (
Cdl IN2-~ UU~d&n
118
AD-AI05 516 GENERAL ELECTRIC Co BINGHAMTON N T AIRCRAFT EQUIPMENT DIV F/S 173ELECTRONI C MASTER 040NITOR AND ADVISORY DISPLAY SYSTEM. OPERA? IO--ETC IU)OCT 80 0AA060-79-C 0270
r UNCLASSIFIED ACS-12-217 USAAVRADCON-TR-Tq-0270-2 NL*mmm.umri'Stttttttttttt-C
-44 0
bo =I0 4j 1C., d 0
*.-V 4 4 4>. -
~0 04)0.. 4), )
.0 V.C V4 to 44) w) f 4aM Is 0.4-, "*~ 0ar.a
4 4J a 4) V0 a $.w 4VA .. ~0 4 0d1 40 dwc 4-L 410 V N
C.) C' ~ -4- O- d -A0 V -0a aZ a..=.).0
$4 41 .2. 4J0 0 .'0 4' q : ) 4) :,0 4)00 41 t
. c 4 .a Od0. Wa Cl .C. *4v;0 0 0 0 4-.C vd *4l Ad It0 14 O
0 aa V a ). 0 4 ) 0.4) 241 C 4J -. ) 4 0)U) - >4 a4 +') V4. 0'S0 d I f0l 41 41 C o A.0 5 s06o
.4 .4-44)fl 4) )' -. jU 1 4)0 n ' C)L .4 444 -4J4' 0 ' 1- 1
E o: C).m T- ... r- C -4' 0-~ a &.
4) a a a O4) 4) 4) I)0 - ...0 0 0 04 .W. - 1 I- Ad O) ~ 41 M
0) 44 44 4 )0 4) d 4 -4 m .U (7-0LO0 0 0 O 4 4 10b Sd 14 V4 .414
w 4 eq S'. .0 4 ".0 0-( C 4 >0- 41V )C C'C
4 Cd 0104) 00 w 54- H,41 Cd :3
'a 93 a to -0 r04.'-S 0.42 .0--4 C )4 ) 4) (.4. -. 4 CZ~> 4 0 00- 0 - 0 LO (D m ;) -4) 0,-4 0C -4 V -4C.
4dt 0 04. 0 4J a$ jj bb 44)1-4)4 I4) .w- co 0 4 >- 0.0 .40 s 54 4.' 0 0 0
64 w l0ZM.01 0 0 O4)dV 0 $2-40 .- 4 4 $)x a). qq 4) .-4 N O(2 aw.3C 4) 4) N 4) .4 4.1)2. >, a.. c0 (4
0.5 .0 04 0. 4)9: 0 (a 4)M 4j ca +;CJ) C40.A. 0 14+- 42e 1 >44 COV
.40 ki) 41"5- A
bb' 0 . 0 0 4 4 4 '
1a, 0 3 40) 0 5-. N o
'. o C o d4 14 U) 0 v
41.
'4 to G'o
0182
4--
.4 0 s
00
0 0: "-44 U W CL~ 0. b .44 J3 .4 do o 11 A. -, or
&40 0 0CL 4-
0 4 4-4 .s . * 0 >. 0$4 0-' .40 -4 9. >
44O) 04.0 .0.4 0 s 0 1V0 4-4 0 4 .-4 0-
a0 (a-4 4)0 t. a -4U
41 .~4 40 0 0 .4. a~ 4. w* d) A cu 03 C) 0 0 4 " S. 4)
02 00 afl4 4.- -4 m A* aJ -4 -4 C
4) 41 A 4).'- . C 4 0 4.4 -. fl .4 A,b cc 4)-41 4a a d 0 . 4 00 ) Co 4Go V. : 0 Id ) -4o 0 0 04. c co
-0 4) 0o I 0 001d4 00 0 a 414.4a S. V4 %4 .0 .04 4' > 0d
"-A 4) u'C 93 .00 0. -4 1O4 .4' .0 D. 4 lot 1 0 bb 3 aA 00 4--
4 0 4. 0.0 46. 1 0) 4) 4 0>b, 0D 040 40 a > X ~N
Co 0 4 as0 0~0 00 0 0 0
W 1444 Ln0. Cd )0C ' - 4 4 00
41 0 0' .4 a 0 4 -0 1 J41 4 10 N -1 0 0u _; a 0 C-4 4J 04 bo0 .4 0 4-' 44 be4 bl c
.W C6 t'v. 0 0+ D0d4' . V ) 0 ) a n c4 iGo 2. N - 0 0 0 0 c .41 0
4- 4 .4 100 0-4S0 0 C9 0 .. 4. -4
Ad0 0 0 0 11.0 tlo41 .0 *- 00i A 0 1 . a 4. z 0
ad0 ) - 4 .40. 0 C-04 N 4 -0 a 14 A - K 0 0 r.'4 'A 4 *- A 4 d 4l 0 0 4 a
V CL 0 0. 24) -A1 m.00 00 O) 0 00 -Co 1 41 Co 0 0 044 0 44 1ag a 4' *. 0'
I.0 0 -0 4- . -40. m~ ..I 0 41 .Co C) 0 '4 '-1 0 .14ON . O
4o- M4 .0 %4 004 04.4 .0 N . 0 .~0 0. C) 0 014 04.4 0 . ) . 0 0 4 041 0 -443 0 0 0 ) 14 V 4C .4 A -to W4 'A 0- 4.' a
02 0) to v 04 3 C) o CO *0 r. E1.3.4 Z 00c -1 G-C 1 .0. 00 0 N 0
00o- 1 140 0.4 0 0), 04 0E- a C4 OOb d 00 WV 00 0a 93 (A 0 2 (n 0 Go
t (D0 .. 0 04O 00 . 0 0 0 0 lo 0 wo
oa .0"oCoto
0 0 0 0 00z Z4.4 0 0 0 0 00
1.40016a a
02~~ 02 (ii t2- 12
-4 v C m vi 103
pc r. ts Go I--
- 30
00 -
.0 W- C 004)0 0' o
0). 00
d0~d
0-'.4 0,4 C) C)
0 W 00)0 ) -40 a ~
rD.4 0 0
WOC .) d0> (L~ 14 -4
0 0 0 4
-4. 06
-4 0 (AId '
'd t 0 .0 44
0 0 ) -H d>.a S.O in IV4'
W ~ -40 >Go0
0 0.4* w U$. CO 0 0 1
S00. 0 4) 1
0a Ia.M- 1 4 0E- c . 4 ) 0 -f.
to w C Q 2 41 4)0 0 x
=N x. WP m - 0
4J ~ 0. V00 0 0
4- .0 003 '0CO4 4 o0UC 04)1 C3 *4 0 -4 C
CD.- d 0.2 0+0 -440
-' a0.
0.2, CO ~ 0.-. C.4
004.4104
4-4%4 .. %
41z 0
4-'0o
00.~ d C) 07
w to ~ 0d 0. 40
0 Ow v. -4
o S.> 4. k4 0 lei)*0~0.
S.D 0: kc4J 0 v
0 oil
S4. 4 4. r.4 -4
at . 0 44 0000 4 V
0 aO)V ) 0 .c -
xo 00V0.0 0 0 1- 4 -
t ~ ) Id 0 04 L
0 0 to 0 %5
t- . a D 40 4 . 4 " 4. 4 .
a i 4
A .. 4 04 0
#A 0 d 050 a2 4&-V0
.404 0 0 0 0)
040 A 0 0 0 364421 A .2'4 0 w 0 M 96
.4.
04 ae
16
4J.d
0 It
42 06 MOJ.
2! 0 A~0
0 6 .4 0 0
.- 0 a .0 La
54 a.. d .0 0 -4
0 0.* .4 %804 . dO0 0 00 Ad
.00001 : ou.04 0 00 0504.0 -4u80
-M .4 2.A d or"0- 10 to 4A V
0.44 0Go 00 aO '. 4, -
0-. r-4 d 0 qA
. 0. 0.V4 .40-rto V 44 d.80A 4V 00 A d 4 0 -4.10 +.0'
A U.4 4 : 8.0 d ~ 0044
0 5.0 %4''0 5 40Ad %4 8.4 '00.
41 Aj 5.
00-4 1 -~ ."
ol 0.4 .. a
.4 4' (A0
0 a 14 e
V4 .4g4 00 . .4 00 v' E1.0 0 0 In 5.02 00 N. > 5.' O0V
ta 0 Q~ 0005I I a (A 004 4 00 55
u0 c N4'
5 4 Ou08 4
+-. * 85 -4 0 4 *4-
02 d4'0.w5- 4 020 023 02 4404 0
00
d 40 00 02 4 02O 0 d
0 V 1-
0
0.0 0 8lee
0 S. "4094 0.4
d 40 4,14r4 0 v 4,C6 00 0 0
V. 0
'0 0) d dr
Rw SO 1w m 0;
0 4'
00 1 o0 055no
*9 4,0 4 t 4,d 04'k4'
U2 04 01 0 -444,
M 1 4, 0 S0C2 0 4' 0 1 0 * 4041 0 4S 01
0 .02A4 05: kked S144l
C) ~ ~ 4 WO 0 -5
0 v1 a02 0 9 4-4
0 4, ISC)
0.44, 44 4
.. )S 4) U 4 40 441 055 0) 4-0. o'40 140
V4 14 126 0 4 to .
L) t0445Co.4
4t I 00 AdOc"n 2 4W. 0144
0 d0
4 4
.4 '0
I m0
0
137
V 4 o
0 0 041 0
u 40 93
0 0.
u4 4
a .00o d 0
0 4. 4
41.>
0 0 ao 3 d a
04 0 04 0
.a d C)
4)) A 0
0 & a0 $4
.~0 a (DGo CD 4
0 0 l wa 44 W U.00
Cd 0 It (ALO M 0 0 00
00 :3 a a 93 V04 0 54 1
00
In. 0 a 2
0 Im~ 0 0
41
02p
o
ILI'
00 z- 0 4U .. paM 0
U 0 4M4 (204 0-.4 w 09
4)t -. .4',., 0 d :tal be 00 cq4 0 4..I.0 0 0 o4'4 kO0ti
cd 9. -4W Aw 0 S4 0 40.W-4 40+
5.. in k~~ Ij 93 a A 4 0I
to . .4. 4 0 C3 t- 4 4) 04J0 .0. ao p .(A.4 41'
04 40 $4 0 .4 104,01,-4 4 m4) toi 0 4..
a~~4 0 AtIE-O~0U,.24 .00,25. 4 U 4Q 4 4, Cl $. s V~
U C k4, 500 0 048 o.- 04,4 4, *
5. 4 %4. 4,4 0d 4 - 44, 0 0.6 .00.5- -0.,44c .4 ti0.- OU44''00 .0 -M4 4, 0 0 .s
- 4 W w0
4 *-4 4 4. 4 44 05.>4 4, 4. 44, 041 004 0 4. r- *4 0 4
4) X b AS..4 04J b 4Z )( 4,4- 14
Da,'4.' 040.0 4 C k-50 " MO 0 4 .C:5 4, 4-5 S .. = o )01 41 V0 0.t 4,Go 0
4' 50 .0 0 V4 4 0-4 0 ( 4. co
4, .44, 4W000.00 ; 55l .04) 4,4 0 5.. 0 b '0 A+ -. ~ 0a C 4A2 k5. 02 V 'A2 "4 . d
04>, 0 $4 .44' .0 4) 03 'A 0 4
0e 4, $4 44 204 * .4,4 to CDU
020 .02 4,~ 5 5- 4 4 a. 0a ' 0 54 4
02 0 0 0 0 0 ) ; 4'.S4 >,0 . 0 4, 0.- 4 4, 44A,
024' .0 Ul 4 , t, 4 , 4 4-~ 4 , 4, 4 4)- ... 4Go~- 00 4, 6 400 > >.e. 4 0 4 4'0.b 4,,W.-M > wa
(.) F.' 0 03 Eu 045 uu-4&l. 4, W-i~0U432U 02 0;2 a0.4 22 A20.'I 2 0.40 - I 1O
-W . -s.. 0 2 02 02 0 0 02 t" ' 0.k i200
4, 41 4, 4, 0, 4, 4I 4, 4 A>, 'U U U' ' A, V -, J 0 S
4'0 C34,Go4,4,4, 414z 4, 4
932 - 4 ,*4 -4 .0 41
0l 40
00
0 r
4 .00 0 0 0 i 0 0
4.' id A-4 -4 0 : i (
L) H tlala
03~~~
0 >
.-a C1 0i
4, 'r , Ia.. 4. 0ta v4 all, ae ba-od 1.0 C- ..4)*.( a1 9
ad (4j) (4 - m-4) 01 04 0 4) S. 4.O -A
at ;.. C2) C.t w..4 04 0 t) .0 0 a ( t-
£4 4) o 4 S. w.014 4 ) d 'CD A 00 06 "M u 4V 4j V
0 00 (1. 4 0 V w4 > mv 4.1 0 'a: w 4 v 4
w :, 0 ( a C 0 4) 1 -0 %4) p4... 0. 'w 'a
'S V mI 04 . It 4)
4 . C O ($ .4 . >. L L
a eq 4. .43 412 U. 4.C M
u0.0 4 V. 41 4- 1
a a O4) -d 48 C1 . $1.d - :
4). )) 10 v 4. 4) 4 (_9 4.1 4.4 -,.4 4 t4 41 c
('a 0 02( N V C.4 ) £4 Z(4W 4 (4 0 f00 0 4
4. W'4 4- 4 v0))1 . Ow
.) do 3 4).4 0 4) w) " a. 4. cc
o ~.4 r44) 4.w 4. ) 03 (4. 0
C. 14 0 a - o 4.. 4. N - 4.41 4. 4. a.4-.4. . 4 4.) id4..4 .
+P 04 4)9 r.4 A-4 4) 0C-2 -4 41 f-8 0
4o t.Q CO ( 4 v a 0
.0 4.. a 4) 44 t .4r. at d.0).a2 -4 4 . as0 0- 4. ) 4)
N,14w -4 V.44
1.
W W ) $4OD C 4 C;04 44) d) Vat t)
(J2 -34 0 14 .4 W -4 0 4J-' 4) 0W. cq 4)4 4. 0.
E) - 4) 05 :04 4)o-+ 1
4. ~ ~ + !J: 4. . 4) 4.5 M. 09(4 . 4.
(.34 4) 010 1A 44 IA 0). 4 4)(.d( d d4a a4 (4 4) a.)) 2 4
00 z .0040 d) .w1.. &a P. 0.- 4) cc 14)02
0 -o he bb 3a
u It.
£44,
4.40 go £1Z o0w 0 00 .4 9( 0
Go 4
0 4.
Go
0 0 4
m VC4 C
~ 3 0NOW44 C
I ATE
LMED