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26-00.fm THREE ENGINE FERRY FLIGHT TABLE OF CONTENTS Page 1 26.00 F F26 A340 26.00 26.01 - INTRODUCTION 26.02 - TRAINING FOOTPRINT 26.03 - TRAINING SYLLABI FERRY N -1 FFS syllabus ....................................................... Page 1 FLIGHT CREW TRAINING PROGRAM Issue 00 FEB 2005

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Page 1: THREE ENGINE FERRY FLIGHT 26.00 Page 1 A340 F F26 TABLE …elearning.onurair.com.tr/webcmi/data/Airbus/A300_310/XAY09301/A34… · 26-00.fm three engine ferry flight table of contents

26-00.fm

THREE ENGINE FERRY FLIGHT

TABLE OF CONTENTS

Page 126.00F F26A340

26.00

26.01 - INTRODUCTION

26.02 - TRAINING FOOTPRINT

26.03 - TRAINING SYLLABI

FERRY N -1 FFS syllabus .......................................................Page 1

FLIGHT CREW TRAINING PROGRAM Issue 00 FEB 2005

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26-00.fm

Page 2THREE ENGINE FERRY FLIGHT

TABLE OF CONTENTS

26.00F F26A340

26.00

PAGE LEFT INTENTIONALLY BLANK

FLIGHT CREW TRAINING PROGRAM Issue 00 FEB 2005

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26-01.fm

THREE ENGINE FERRY FLIGHT

INTRODUCTION

Page 126.01F F26A340

26.01INTRODUCTION

This course provides the training required to ensure a safe preparation and management of a 3 engine ferry flight for flight crew members currently rated and experienced on A340.

The flight crew member must be qualified, current, experienced on A340 and specifically desig-nated to carry out 3 engine ferry flights. The Captain shall be qualified Instructor.

Before carrying out a 3 engine ferry flight, the designated flight crew member shall follow theapproved A340 "3 Engine Ferry Flight" course if they have not completed this course in the pre-ceding 30 days.

IMPORTANT NOTICE :

It is the Airline responsibility to obtain operational clearance for

3 Engine Ferry Flights from its own Authorities.

FLIGHT CREW TRAINING PROGRAM Issue 00 FEB 2005

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26-01.fm

Page 2THREE ENGINE FERRY FLIGHT

INTRODUCTION

26.01F F26A340

26.01

01 - TRAINING OBJECTIVE

• To ensure the safe preparation and management of a 3 engine ferry flight

02 - SCHEDULE

Briefing duration : 2.00 hours

03 - EQUIPMENT

DOC references : • FCOM 2.04.40 (Special Operations)• FCOM 3.02.10 (2 Engine Inoperative Operations)

04 - INSTRUCTOR'S ACTION

Briefing of the following key point :

A. MAIN

• Runway alignment prior to take-off• Thrust setting procedures• Sidestick position during take-off roll• Rejected take-off• Following β target• ECAM messages• Inoperative systems• Importance of calls out

B. SECONDARY

• Use of MMEL / MEL• Knowledge of performance calculations• Knowledge of limitations• Weather limitations• 3 engine cruise and fuel planning

THREE ENGINE FERRY FLIGHT BRIEFING

FLIGHT CREW TRAINING PROGRAM Issue 00 FEB 2005

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26-01.fm

THREE ENGINE FERRY FLIGHT

INTRODUCTION

Page 326.01F F26A340

26.01

05 - TRAINEES' ACTIONS

FCOM 2.04.40 gives details of the procedures and limitations required for the operation of a 3 engine ferry flight.

The crew to perform the flight should be trained in all the procedures and techniques associ-ated with the 3 engine ferry flight. Airbus recommends that the crew should practice the tech-niques in the simulator prior to carrying out the flight. This may be required by the regulatory Authorities or the Airline.

Certain technical conditions must be fulfilled, especially the condition of the failed engine i. e. whether it should be windmilling or locked. Additional limitations are placed on the duration of the flight depending on this condition. Further, some systems must be fully operational for the proposed flight. Other systems must be specially configured for the flight. Reference must be made to the MMEL.

The RTOW performance determination differs form that normally applied for public transport operations. Careful reading of the section of FCOM 2.04.40 relating to performance is manda-tory.

The 3 engine ferry flight take-off, en route net flight path, go around and landing performance must be determined by using the Performance Engineering Program/OCTOPUS by selecting 3 ENGINE FERRY FLIGHT CASE.

The take-off case computed by OCTOPUS is the most conservative, i. e. dispatch with an outer engine unserviceable, failure of the other outer engine at take-off and no landing gear retraction. However the en route net ceiling for 2 engines inoperative are given for landing gear retracted only.

Take-off is permitted with CONF 3 ONLY (A340-600)Dispatch form contaminated runways is not permitted. Flight into known icing is not approved. Maximum crosswind for take-off is 10 KT. French DGAC is recommending :

• a runway width of at least 45 meters,• for take-off 1500 ft ceiling and 1 NM of visibility,• for landing 600 ft ceiling and 2 NM of visibility

When lining up on the runway, the airplane should be positioned 5 meters from the centreline, on the side with 2 operating engines. On the take-off roll some ECAM cautions may appear. A knowledge of which to expect will enable rapid determination of unusual or unexpected mes-sages.

The procedures for thrust setting during the take-off roll differ slightly depending on whether an outer or inner engine is inoperative. The different procedures are detailed in FCOM 2.04.40.

THREE ENGINE FERRY FLIGHT BRIEFING (CONT’D)

FLIGHT CREW TRAINING PROGRAM Issue 03 MAY 2007

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26-01.fm

Page 4THREE ENGINE FERRY FLIGHT

INTRODUCTION

26.01F F26A340

26.01

05 - TRAINEES' ACTIONS (END)

While target speeds are given for when to advance the 3rd thrust lever, the actual technique is straightforward : advance the symmetrical engines to TOGA, advance the other engine to 50%, then coordinate increase in thrust from the 3rd engine, with the use of full rudder to maintain runway centreline and achieve 70% N1 at 100 KT. As speed increases the rudder will become more effective, allowing more thrust to be applied on the 3rd engine.

If a second engine failure occurs before 100 KT, the thrust levers are not aligned and therefore the pilots hands are not in the correct position to close ALL the thrust levers at once. Failure to close all the thrust levers after a second engine failure will result in directional control difficul-ties. It is important not to delay any actions in the case of a 2nd engine failure during the take-off roll.

Full rudder deflection may be needed early in the take-off roll particularly in crosswind condi-tions. It is important that half nose down deflection is held on the sidestick until jut before VR. As VR for the 3 engine ferry case is much higher than the normal 4 engine VR, if the sidestick was not held forward then the nose would lift before VR.

After lift off follow the β target. Accelerate if the β target cannot be centered with full rudder deflection. With a 2nd engine failure, acceleration will be required until β target is centered, at the expense of rate of climb.

Note : For T/O procedure A340-600 refer to FCOM 2.04.40 p.4

06 - COMPLETION STANDARDS

• Knowledge of required procedures• Knowledge of risks linked to a 2nd engine failure during take-off• Knowledge of limitations• Safe determination of fuel planning

07 - COMMON ERRORS

• Not accelerating to center β target following 2nd engine failure

THREE ENGINE FERRY FLIGHT BRIEFING (END)

FLIGHT CREW TRAINING PROGRAM MAY 2007Issue 03

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26-02.fm

THREE ENGINE FERRY FLIGHT

TRAINING FOOTPRINT

Page 126.02F F26A340

26.02TRAINING FOOTPRINT

TRAINING DAILY FOOTPRINT

.DAY 1

FFS briefing 2:00FFS 3:00

FLIGHT CREW TRAINING PROGRAM Issue 00 FEB 2005

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26-02.fm

Page 2THREE ENGINE FERRY FLIGHT

TRAINING FOOTPRINT

26.02F F26A340

26.02

PAGE LEFT INTENTIONALLY BLANK

FLIGHT CREW TRAINING PROGRAM Issue 00 FEB 2005

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FFS.fm

STANDARD COURSE

GROUND PHASE

Page 126.03A340 F F2S

26.03 TRAINING SYLLABI

TAKE-OFF DATA

INIT PAGE ATIS

CO RTE FROM TO TRIP DIST RWY....................................... 14 R / 32 L

LFBO/LFBO LOCAL WIND ..................................... Vari-able

ALTN/CO RTE CRZ WIND VISI ........................................ 10 km

CEILING................................. 3000 ft

FLT NBR ALTN TEMP ..................................... 14°C

[Airline ID] 402 LFBP DEW POINT...........................

LAT LONG ALTN DIST QNH....................................... 1010 hPa/29.83 inHg

4338.1N 00122.1E 105 QFE........................................ 992 hPa/29.29 inHg

COST INDEX FLT to ALTN RWY COND ...........................

90 FL 150 Observations.......................... :

CRZ FL/TEMP TROPO

2000 ft / 10°C 36 090

26 .03MALFUNC

REF- FERRY N -1 FFS -

1 - TRANSIT COCKPIT PREPARATION2 - BEFORE START3 - ENGINE START (MANUAL)4 - AFTER START PROCEDURE5 - TAXI6 - BEFORE TAKE-OFF7 - TAKE-OFF WIND CALM - INBD INOP

INIT T/O

8 - TAKE-OFF - WIND CALM OUTBD INOP9 - CLIMB - STUDY OF N -2 ENG FLIGHT

10 - VISUAL PATTERN11 - LANDING

INIT T/O

ERRY N

FLIGHT CREW TRAINING PROGRAM Issue 00 FEB 2005

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FFS.fm

Page 2 F F2626.03THREE ENGINE FERRY FLIGHT

TRAINING SYLLABIA340

12 - TAKE-OFF - CROSSWIND 10 KT - INBD INOP

INIT T/O

13 - TAKE-OFF - CROSSWIND 10 KT - OUTBD INOP *

INIT T/O

14 - TAKE-OFF - CROSSWIND 10 KT - OUTBD INOP - ENG FAILURE *15 - VISUAL PATTERN16 - GO AROUND17 - VISUAL PATTERN18 - LANDING

INIT T/O CROSSWIND 10 KT

19 - TAKE-OFF (OUTBD INOP) - ENG FAILURE AT V1 -10 KT - RTO *

INIT T/O

20 - TAKE-OFF (OUTBD INOP) - ENG FAILURE AT 100 KT - RTO *

INIT T/O

21 - TAKE-OFF (INBD INOP) - ENG FAILURE AT V1 -10 KT - RTO *

INIT T/O

22 - TAKE-OFF (INBD INOP) - ENG FAILURE AT 90 KT - RTO *

INIT T/O

23 - TAKE-OFF - VISUAL PATTERN - LANDING24 - AFTER LANDING25 - PARKING

* ITEMS TO BE REPEATED AS NECESSARY UNTIL PROFICIENCY

26.03MALFUNC

REF- FERRY N -1 FFS -

FLIGHT CREW TRAINING PROGRAM Issue 00 FEB 2005

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FFS.fm

Page 3 F F2626.03THREE ENGINE FERRY FLIGHT

TRAINING SYLLABIA340

26.03

A340313 - JAA CFM56-5C4 engines TOULOUSE - BLAGNAC TLS - LFBOElevation 487 FT TORA 3500 M

Isa temp 14 C TODA 3560 M

rwy slope 0.09% ASDA 3560 M

14R 6 obstacles

22.0.2 29-SEP-03

AA313C02 V 9 QNH 1013.25 HPA

Air cond. Off

Anti-icing Off

Ferry flight 1OUTER LKD

Dry check

for training only

DRY TOGA

OAT C

CONF 2TAILWIND

-10 KTTAILWIND

-5 KTWIND0 KT

HEADWIND10 KT

HEADWIND20 KT

-1 155.2 3/3

157/63/74

165.3 3/3

159/63/74

177.1 3/3

160/63/73

179.2 3/3

163/63/73

179.2 8/8

163/63/73

9 150.2 3/3

157/63/74

159.9 3/3

158/63/74

170.9 3/3

159/63/73

179.0 3/3

160/63/73

179.2 8/8

163/63/73

19 145.3 3/3

156/63/74

154.8 3/3

158/63/74

165.0 3/3

159/63/73

172.8 3/3

160/63/73

178.8 3/3

161/63/73

29 140.7 3/3

155/63/74

149.9 3/3

157/63/74

159.6 3/3

159/63/73

166.8 3/3

159/63/73

171.6 3/3

161/63/73

31 137.2 3/3

155/63/74

146.1 3/3

157/63/74

155.6 3/3

159/63/73

162.6 3/3

160/63/73

168.6 3/3

161/63/73

33 .......................

.......................

141.9 3/3

157/63/73

151.3 3/3

159/63/73

158.0 3/3

160/63/73

165.3 3/3

160/63/72

35 .......................

.......................

137.8 3/3

157/63/73

146.9 3/3

159/63/73

153.3 3/3

160/63/72

160.4 3/3

160/63/72

37 .......................

.......................

134.1 3/3

157/63/73

142.8 3/3

159/63/72

149.1 3/3

160/63/72

155.9 3/3

160/63/72

39 .......................

.......................

.......................

.......................

138.5 3/3

159/63/72

144.5 3/3

160/63/72

151.2 3/3

160/63/72

41 .......................

.......................

.......................

.......................

134.4 3/3

159/63/72

140.1 3/3

159/63/72

146.5 3/3

160/63/72

43 .......................

.......................

.......................

.......................

.......................

.......................

135.5 3/3

159/63/71

141.5 3/3

160/63/71

45 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

136.4 3/3

160/63/71

47 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

131.3 3/3

160/63/71

49 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

51 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

53 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

54 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................LABEL FOR INFLUENCE

DW (1000 KG) DTFLEX

DV1-DVR-DV2 (KT)

(TVMC OAT C) DW (1000 KG) DTFLEX

DV1-DVR-DV2 (KT)

MTOW(1000 KG) codes

V1/VR/V2 (kt)

VMC

LIMITATION

Tref (OAT) = 29 C

Tmax(OAT) = 54 C

Min acc height 636 FT

Maxacc height 2547 FT

Min QNH alt 1123 FT

Max QNH alt 3034 FT

LIMITATION CODES:

1=1st segment 2=2nd segment 3=runway length 4=obstacles

5=tire speed 6=brake energy 7=max weight 8=final take-off 9=VMU

Min V1/VR/V2 = ***/163/171

CHECK VMU LIMITATION

Correct. V1/VR/V2 = 0.2 KT/1000 KG

FLIGHT CREW TRAINING PROGRAM Issue 00 FEB 2005FEB 2005

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FFS.fm

Page 4 F F2626.03THREE ENGINE FERRY FLIGHT

TRAINING SYLLABIA340

26.03

A340313 - JAA CFM56-5C4 engines TOULOUSE - BLAGNAC TLS - LFBOElevation 497 FT TORA 3500 M

Isa temp 14 C TODA 3590 M

rwy slope -0.09% ASDA 3590 M

32L 2 obstacles

22.0.2 04-JUL-03

AA313C02 V 9 QNH 1013.25 HPA

Air cond. Off

Anti-icing Off

Ferry flight 1OUTER LKD

Dry check

for training only

DRY TOGA

OAT C

CONF 2TAILWIND

-10 KTTAILWIND

-5 KTWIND0 KT

HEADWIND10 KT

HEADWIND20 KT

-1 155.3 3/3

158/63/74

165.5 3/3

159/63/74

177.3 3/4

160/63/73

179.2 3/8

163/63/74

179.2 8/8

163/63/73

9 150.1 3/3

157/63/74

160.1 3/3

159/63/74

171.1 3/3

160/63/74

179.1 3/3

161/63/73

179.1 8/8

163/63/73

19 145.2 3/3

156/63/74

154.9 3/3

158/63/74

165.2 3/3

159/63/74

173.0 3/3

160/63/73

178.8 3/8

162/63/73

29 140.7 3/3

156/63/74

149.9 3/3

158/63/74

159.8 3/3

159/63/74

167.0 3/3

160/63/73

171.5 3/3

162/63/73

31 137.2 3/3

156/63/74

146.0 3/3

158/63/74

155.8 3/3

159/63/73

162.7 3/3

160/63/73

168.6 3/3

161/63/73

33 .......................

.......................

141.9 3/3

158/63/73

151.4 3/3

159/63/73

158.1 3/3

160/63/73

165.5 3/3

161/63/73

35 .......................

.......................

137.8 3/3

157/63/73

147.1 3/3

159/63/73

153.5 3/3

160/63/73

160.6 3/3

161/63/72

37 .......................

.......................

.......................

.......................

142.9 3/3

159/63/73

149.2 3/3

160/63/72

156.0 3/3

161/63/72

39 .......................

.......................

.......................

.......................

138.6 3/3

159/63/72

144.7 3/3

160/63/72

151.3 3/4

161/63/72

41 .......................

.......................

.......................

.......................

134.4 3/3

159/63/72

140.2 3/3

160/63/72

146.6 3/4

161/63/72

43 .......................

.......................

.......................

.......................

.......................

.......................

135.6 3/3

160/63/72

141.3 3/4

161/63/71

45 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

135.5 3/4

161/63/71

47 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

49 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

51 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

53 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

54 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................LABEL FOR INFLUENCE

DW (1000 KG) DTFLEX

DV1-DVR-DV2 (KT)

(TVMC OAT C) DW (1000 KG) DTFLEX

DV1-DVR-DV2 (KT)

MTOW(1000 KG) codes

V1/VR/V2 (kt)

VMC

LIMITATION

Tref (OAT) = 29 C

Tmax(OAT) = 54 C

Min acc height 412 FT

Maxacc height 2525 FT

Min QNH alt 909 FT

Max QNH alt 3022 FT

LIMITATION CODES:

1=1st segment 2=2nd segment 3=runway length 4=obstacles

5=tire speed 6=brake energy 7=max weight 8=final take-off 9=VMU

Min V1/VR/V2 = ***/163/171

CHECK VMU LIMITATION

Correct. V1/VR/V2 = 0.2 KT/1000 KG

FLIGHT CREW TRAINING PROGRAM Issue 00 FEB 2005FLIGHT CREW TRAINING PROGRAM Issue 00 FEB 2005Issue 00FLIGHT CREW TRAINING PROGRAM FEB 2005

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FFS.fm

STANDARD COURSE

GROUND PHASE

Page 526.03A340 F F2S

Issue 03FLIGHT CREW TRAINING PROGRAM

26.03

A340642 - JAA RR TRENT 556 engines TOULOUSE - BLAGNAC TLS - LFBOElevation 487 FT TORA 3500 M

Isa temp 14 C TODA 3560 M

rwy slope 0.09% ASDA 3560 M

14R 6 obstacles

24.0.0U 16-NOV-06

AA642A05 V20 QNH 1013.24 HPA

Air cond. Off

Anti-icing Off

Ferry flight 1OUTER WML for training only

DRY TOGA

OAT C

CONF 3TAILWIND

-10 KTTAILWIND

-5 KTWIND0 KT

HEADWIND10 KT

HEADWIND20 KT

-1 266.0 3/3

162/63/82

278.1 8/8

164/64/82

278.1 8/8

164/64/82

278.1 8/8

165/65/83

278.1 8/8

165/65/83

9 258.6 3/3

161/63/82

275.2 3/3

163/63/81

278.3 8/8

165/65/82

278.3 8/8

164/64/82

278.3 8/8

165/65/82

19 251.4 3/3

160/63/82

267.3 3/3

162/63/82

278.4 3/8

164/65/82

278.4 8/8

164/64/82

278.4 8/8

165/65/82

29 244.5 3/3

160/63/82

259.9 3/3

161/63/82

264.9 8/8

163/63/81

264.9 8/8

163/63/81

264.9 8/8

163/63/81

33 235.0 3/3

159/63/81

249.7 3/3

161/63/81

250.8 8/8

163/63/81

250.7 8/8

163/63/81

250.7 8/8

163/63/81

37 225.1 3/3

159/63/81

236.5 3/8

162/63/80

236.5 8/8

164/64/80

236.5 8/8

163/63/80

236.5 8/8

163/63/80

41 215.3 3/3

158/63/80

223.4 3/8

162/63/80

223.4 8/8

163/63/80

223.4 8/8

163/63/80

223.4 8/8

163/63/80

45 205.3 3/3

158/63/79

211.6 3/8

162/63/79

211.6 8/8

163/63/79

211.6 8/8

163/63/79

211.6 8/8

163/63/79

49 195.0 3/3

158/63/78

199.6 3/8

162/63/78

199.6 8/8

163/63/78

199.6 8/8

163/63/78

199.6 8/8

163/63/78

53 184.5 3/3

157/63/78

187.7 3/8

162/63/77

187.7 8/8

163/63/77

187.7 8/8

163/63/77

187.7 8/8

163/63/77

57 174.0 3/3

156/63/77

184.3 3/3

159/63/76

184.5 3/8

163/63/76

184.5 8/8

163/63/76

184.5 8/8

163/63/76

61 .......................

.......................

173.1 3/3

158/63/76

183.8 3/3

160/63/75

184.5 3/8

163/63/75

184.4 8/8

163/63/75

65 .......................

.......................

.......................

.......................

171.8 3/3

159/63/75

178.8 3/3

161/63/74

184.4 3/8

162/63/74

69 .......................

.......................

.......................

.......................

.......................

.......................

166.4 3/3

160/63/74

173.1 3/3

161/63/73

73 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

74 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................LABEL FOR INFLUENCE

DW (1000 KG) DTFLEX

DV1-DVR-DV2 (KT)

MTOW(1000 KG) codes

V1/VR/V2 (kt)

VMC

LIMITATION

Tref (OAT) = 29 C

Tmax(OAT) = 54 C

Min acc height 614 FT

Maxacc height 3479 FT

Min QNH alt 1101 FT

Max QNH alt 3966 FT

LIMITATION CODES:

1=1st segment 2=2nd segment 3=runway length 4=obstacles

5=tire speed 6=brake energy 7=max weight 8=final take-off 9=VMU

Min V1/VR/V2 = ***/164/172

CHECK VMU LIMITATION

Correct. V1/VR/V2 = 0.2 KT/1000 KG

MAY 2007

-600

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FFS.fm

Page 6STANDARD COURSE

GROUND PHASE

26.03A340 F F2S

26.03

A340642 - JAA RR TRENT 556 engines TOULOUSE - BLAGNAC TLS - LFBOElevation 497 FT TORA 3500 M

Isa temp 14 C TODA 3590 M

rwy slope -0.09% ASDA 3590 M

32L 2 obstacles

24.0.0U 16-NOV-06

AA642A05 V20 QNH 1013.24 HPA

Air cond. Off

Anti-icing Off

Ferry flight 1OUTER WML for training only

DRY TOGA

OAT C

CONF 3TAILWIND

-10 KTTAILWIND

-5 KTWIND0 KT

HEADWIND10 KT

HEADWIND20 KT

-1 268.1 3/3

162/63/82

278.0 8/8

164/64/82

278.0 8/8

164/64/82

278.0 8/8

165/65/83

278.0 8/8

165/65/83

9 260.6 3/3

162/63/82

277.6 3/3

163/63/81

278.2 8/8

164/64/82

278.2 8/8

164/65/82

278.2 8/8

165/65/82

19 253.3 3/3

161/63/82

269.4 3/3

163/63/82

278.3 8/8

164/64/82

278.3 8/8

164/64/82

278.3 8/8

165/65/82

29 246.3 3/3

160/63/82

261.9 3/3

162/63/82

264.8 8/8

163/63/82

264.8 8/8

163/63/82

264.8 8/8

163/63/82

33 236.6 3/3

160/63/82

250.6 3/3

162/63/81

250.6 8/8

163/63/81

250.6 8/8

163/63/81

250.6 8/8

163/63/81

37 226.7 3/3

159/63/81

236.4 3/8

163/63/81

236.4 8/8

163/63/81

236.4 8/8

163/63/81

236.4 8/8

163/63/81

41 216.9 3/3

159/63/80

223.3 3/8

163/63/80

223.3 8/8

163/63/80

223.3 8/8

163/63/80

223.3 8/8

163/63/80

45 206.7 3/3

159/63/79

211.5 3/8

163/63/79

211.5 8/8

164/64/79

211.5 8/8

163/63/79

211.5 8/8

163/63/79

49 196.3 3/3

158/63/79

199.6 3/8

163/63/78

199.5 8/8

163/63/78

199.5 8/8

163/63/78

199.5 8/8

163/63/78

53 185.8 3/3

158/63/78

187.6 3/8

163/63/78

187.6 8/8

163/63/78

187.6 8/8

163/63/78

187.6 8/8

163/63/78

57 175.3 3/3

157/63/77

184.5 3/8

160/63/77

184.5 8/8

163/63/77

184.5 8/8

163/63/77

184.5 8/8

163/63/77

61 .......................

.......................

174.4 3/3

159/63/76

184.4 3/3

161/63/76

184.4 8/8

163/63/76

184.4 8/8

163/63/76

65 .......................

.......................

.......................

.......................

173.1 3/3

160/63/75

179.6 3/4

161/63/75

184.3 3/8

163/63/74

69 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

171.0 3/4

163/63/74

73 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

74 .......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................

.......................LABEL FOR INFLUENCE

DW (1000 KG) DTFLEX

DV1-DVR-DV2 (KT)

MTOW(1000 KG) codes

V1/VR/V2 (kt)

VMC

LIMITATION

Tref (OAT) = 29 C

Tmax(OAT) = 54 C

Min acc height 413 FT

Maxacc height 3460 FT

Min QNH alt 910 FT

Max QNH alt 3957 FT

LIMITATION CODES:

1=1st segment 2=2nd segment 3=runway length 4=obstacles

5=tire speed 6=brake energy 7=max weight 8=final take-off 9=VMU

Min V1/VR/V2 = ***/164/172

CHECK VMU LIMITATION

Correct. V1/VR/V2 = 0.2 KT/1000 KG

Issue 03FLIGHT CREW TRAINING PROGRAM MAY 2007

-600

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FFSgd.fm

STANDARD COURSE

GROUND PHASE

Page 6A26.03A340 F F2S

26.03

01 - SESSION OBJECTIVE

• To practice required special operational procedures and skills.• To make the trainee proficient in handling the aircraft during a 3 engine take-off with or

without a second engine failure.• To review 2 engine approach, go around and landing.

02 - BRIEFING TOPICS

A. REVIEW

NIL

B. INTRODUCE

Refer to "3 Engine Ferry Flight" briefing note.

03 - SESSION PROFICIENCY CRITERIA

• Proficiency to conduct a 3 engine ferry flight.

04 - SESSION GUIDE

7, 8,12,13:Study of thrust setting technique

14 : Inner engine failure after take-off.

19 : Loss of 2nd engine same wing.

23 : Use max crosswind 10 KT and after CG 35%.

FERRY N -1 FFS SESSION GUIDE

FLIGHT CREW TRAINING PROGRAM Issue 00 FEB 2005

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FFSgd.fm

Page 6BSTANDARD COURSE

GROUND PHASE

26.03A340 F F2S

26.03

PAGE LEFT INTENTIONALLY BLANK

FLIGHT CREW TRAINING PROGRAM Issue 00 FEB 2005