emirates daily chk b777 rev.99 (qaf0336).pdf

BOEING 777 (PASSENGER) DAILY CHECK

AIRCRAFT REGN: DATE: STN: FLT: PAGE No 1 of 12

NOTE: DAILY CHECK TO BE ACCOMPLISHED EVERY 24 HOURS (NOT TO EXCEED 48 HOURS).

ITEM WORK TO BE CARRIED OUT MECH *CERT

BEWARE OF HUMAN INDUCED ERRORS. REPORT AND DISCUSS ANY UNCERTAINTIES OF COMPLETING THIS TASK WITH YOUR SUPERVISOR.

*CERTIFIED IAW

GCAA REQUIREMENTS

REF EPM 07-01

QA/F/0336 REV.99 AMP REV. 50

NOTE: It is recommended that the C/Bs C26639 FIRE EXT CGO BTTL 2A, 2B, 2C (L7) and, if applicable, C26601 FIRE EXT CGO BTL 2D, 2E, 2F (L12) on the P310 panel be temporarily opened while the airplane is being powered on after an airplane has been powered down for any extended duration (for longer than 24 hours). The circuit breakers should be restored after full airplane power is applied. Failure to do so may result in an inadvertent discharging of Cargo Fire Extinguisher Squib bottles.

1 ARRIVAL ITEMS

1A Check ramp area clear of debris.

1B Install wheel chocks.

1C Place the towing lever in the “TOW POSITION” and install lock pin for pushback or towing.

1D Install nose and main landing gear safety pins.

1E

Check both engine oil levels at sight glass after a minimum of 10 minutes of engine shut-down (not to exceed 30 minutes for Trent engines and 60 minutes for GE engines). Service as required to full using MOBIL JET II oil and record uplift(s) in the aircraft Technical Log. (i.a.w. AMM 12-13-01-600-801 & AMM12-13-01-130-803-002).

LH

Ensure Oil Servicing Caps are securely fastened. (LH and RH Engine) ( Ref: AMP 79-015-00 / AMP 79-395-00)

RH

1F

If the aircraft electrical network is not energized perform a safety check to ensure proper position of controls, and switches before energizing the network. Energize the aircraft electrical network. (Ref. FCOM )

1G

Review aircraft Technical Log and Cabin Log books. Action as necessary.

1H Check SMI-CRS for Out of Phase inspection requirements. Action as necessary.

1I

AT DXB ONLY Ensure a minimum of twenty five TLP and CLP sector record pages, minimum of five each ADD, CDD and BDD numbered pages and one unused Notice to Crew Sheet are available before departure. (Ref: EPM Volume VI Procedures 08-04 and 08-06)

1J AT DXB ONLY B777-200/-300 ONLY: Remove the optical disk from the Quick Access Recorder (QAR) and install a new optical disk i.a.w. AMM 31-35-02-000-802 & 31-35-02-400-802.






*CERTIFIED IAW

GCAA REQUIREMENTS

REF EPM 07-01


1K

AT DXB ONLY B777-200LR/300ER ONLY: Remove PCMCIA card from PQAR and install a blank PCMCIA card i.a.w B777 AMM 31-35-02-000-804 and 31-35-02-400-804. Record aircraft registration, date and time on both the removed and installed cards. Route the removed PCMCIA card to Flight Operations for readout.

(Ref: ETS Recommendation dated 2 7th Mar 2005)

1L

For flights arriving into and departing from any station reported to encounter volcanic ash: Carry out external visual inspection to determine if the aircraft has flown through volcanic ash - refer to TN 05-004 latest revision, Paragraph (B)2,for guidance. If there is evidence of volcanic ash exposure, contact MCC for further action. (Ref: Email from VP-ETS dated 12 May 2010)

2 FORWARD FUSELAGE

2A Carry out General Visual Inspection of Forward Fuselage Exterior from the ground for obvious damage, leakage, obstruction, security and condition i.a.w. AMM 05-41-00-210-801, including:

Service panels, doors and Hatches

Entry doors.

Communication/Navigation Antennas

Windows

Fwd outflow valve door.

Ports, vents, and drains.

Radome: Latches positively locked, paint not deteriorated.

Positive Press. Relief Valve: closed (bright coloured edge on valve not visible).

Crew oxygen cylinder overboard discharge indicator: green disc in place.

Pitot – Static ports, TAT and Ice Detector probes and AOA sensors: covers installed as required. Check and ensure that the Pitot Static Ports, TAT and Ice Detectors Probes and AOA Sensors are free of any obstruction/foreign object and that they are clean, including their surrounding areas.

Exterior lights: cleanliness.

Landscape camera window: clean with window cleaning agent.

Panels and fairing for missing fasteners

Check General Cleanliness ensuring No Dirty surfaces with grease, oil, or any unacceptable un-clean condition. If found dirty arrange to clean or raise DD for cleaning at the earliest opportunity.

(Ref: AMP 53-802-00)






*CERTIFIED IAW

GCAA REQUIREMENTS

REF EPM 07-01


3 NOSE LANDING GEAR

3A Carry out general visual inspection of Nose Landing Gear from the ground for obvious damage, leakage, obstruction, security and condition, including:

Doors and wheel well area (as far as visible from ground with doors closed).

Hydraulic lines and fittings.

Gear assembly: structural damage, evidence of leakage, all placards including red tyre servicing instructions/placards for legibility.

Shock strut: correct extension, cleanliness. Wipe down exposed chrome with a clean cloth that is soaked in MIL-H-5606 fluid (Aeroshell fluid 4 or 41).

Wheels: Corrosion, cracks, flaked or blistered paint, rim damage, loose/ damaged /or missing tie bolts & tie bolt nuts; ensure the hubcaps are not loose.(i.a.w. AMM 32-45-03-700-801)

Tires: Wear and damage. Check pressure, using a TPG, preferably when tires are cool; inflate as necessary with NITROGEN to the correct pressure i.a.w. AMM 12-15-03-610-801.

a. i.a.w. AMM 12-15-03-780-802 (To check tire pressures prior to a two hour cool down of the tires).

b. i.a.w. AMM 12-15-03-780-801 (To check tire pressures when the tires are cool after a minimum of two hours).

c. i.a.w. AMM 32-45-04-700-801 (Tires inspection for wear & damage)

(Ref: AMP 29-115-00, 32-010-00, 32-190-00, 32-200-00, 32-215-00-00-E)

4 LOWER CENTER FUSELAGE

4A Carry out General Visual Inspection of Lower Centre Fuselage Exterior from the ground for obvious damage, leakage, obstruction, security and condition i.a.w. AMM 05-41-00-210-801, including:

Service panels, doors and Hatches.

Ram air inlet and exhaust doors.

ADP exhaust.

Navigation/Communication Antennas.


Ram Air Turbine (RAT) doors: properly closed.

Panels and Belly fairing for missing fasteners

Check General Cleanliness ensuring No Dirty surfaces with grease, oil, or any unacceptable un-clean condition. If found dirty arrange to clean or raise DD for cleaning at the earliest opportunity

(Ref: AMP 53-802-00)






*CERTIFIED IAW

GCAA REQUIREMENTS

REF EPM 07-01


5 RIGHT / LEFT WING LEADING EDGE

5A Carry out General Visual Inspection of Lower Wing Leading Edge and associated devices from the ground for obvious damage, leakage, obstruction, security and condition, including:

Krueger flap and slats.


Landing lights and Runway Turn-off lights: cleanliness.

Panels for missing screws


6 LEFT / RIGHT POWER PLANT AND NACELLE STRUT

6A Carry out general visual inspection of power plant and nacelle strut from the ground for obvious damage, leakage, obstruction, security and condition (with cowls closed) including:

Inlet cowl inner surface and sensors

Thrust reversers

Fan blades and spinner

Latches: security

Cowlings

Ports, vents, and drains

Access doors and pressure relief doors

Turbine exhaust

Pylon and associated panels for missing screws

(Ref: AMP 71-830-00 / AMP 71-844-00)

LH

RH

6B Inspect (General Visual) the Integrated Drive Generator (IDG) oil filter element bypass condition: Ensure the differential pressure indicator (red button) is not extended. (i.a.w. AMM. 12-22-07-200-802).

NOTE: If fan cowls are closed this check may be performed using EICAS (electrical system Maintenance Page – ATA 24) for an IDG BLOCKED filter indication; however if fan cowls are open pop-out R/H indicators must be physically checked.

(Ref: AMP 24-080-00)

LH

RH






*CERTIFIED IAW

GCAA REQUIREMENTS

REF EPM 07-01


6C Check VSCF Backup Generator oil level and service as required to full using MOBIL JET II i.a.w. AMM 12-13-07-200-801. (Ref: AMP 24-030-00)

Note 1: This is an AMP Task with an interval of 100 FH. For ease of control it has been aligned with Daily Checks performed on specific days of the week.

Note 2: In the event the Daily is due but not performed on the specified days (Daily 24 Hrs not to exceed 48hrs) then perform the task on the following day.

Note 3: Annotate N/A on those days when this task is not performed.

Task to be performed on the highlighted days of the week only:

L/H Engine

R/H Engine

Days of the Week

SUN MON TUE WED THU FRI SAT

Days of the Week

SUN MON TUE WED THU FRI SAT

LH

RH

7 RIGHT / LEFT WING TIP AND TRAILING EDGE

7A Carry out General Visual Inspection of Wing Tip and Trailing Edge and associated devices from the ground for obvious damage, leakage, obstruction, security and condition, including:

Position and Anti collision lights: cleanliness.

Control surfaces, flaps and flap track fairings.

Static Dischargers: damage, missing.

Lower wing surface: evidence of fuel leakage.

Panels for missing screws

Wing To Fuselage Section


7B Carry out operational check of Navigation (Position) lights i.a.w. AMM 33-43-00-710-801.






*CERTIFIED IAW

GCAA REQUIREMENTS

REF EPM 07-01


8 RIGHT / LEFT MAIN LANDING GEAR

8A1

Carry out General Visual Inspection of Main Landing Gear from the ground for obvious Damage, Leakage, Obstruction, Security and Condition, including:

Doors and wheel well areas (as far as visible from ground with doors closed).

Hydraulic lines and fittings.

Gear assembly: structural damage, evidence of leakage, all placards including red tyre servicing instructions/placards for legibility.

Shock strut: normal extension, cleanliness. Wipe down exposed chrome with a clean cloth that is soaked in MIL-H-5606 fluid (Aeroshell fluid 4 or 41).

Wheels: Corrosion, cracks, flaked or blistered paint, heat shield damage, overheat damage, rim damage, debris guard damage, loose / damaged / or missing tie bolts & tie bolt nuts. (i.a.w. AMM 32-45-03-700-801)

Tires: Wear and damage. Check pressure, using a TPG, preferably when tires are cool; inflate as necessary with NITROGEN to the correct pressure i.a.w. 12-15-03-610-801.

a. i.a.w. AMM 12-15-03-780-802 (To check tire pressures prior to a two hour cool down of the tires).

b. i.a.w. AMM 12-15-03-780-801 (To check tire pressures when the tires are cool after a minimum of two hours).

c. i.a.w. AMM 32-45-04-700-801 (Tires inspection for wear & damage).

(Ref: AMP 29-115-00, 32-010-00, 32-190-00, 32-200-00, 32-215-00-00-E)

8A2

Carry out General Visual Inspection of Brake units for damage, evidence of leakage (with braking pressure applied). i.a.w. AMM 32-45-07-700-802. (Ref: AMP 32-215-00E)

8A3

Carry out General Visual Inspection of Brake Units for Condition and Wear (with Braking Pressure applied) i.a.w AMM 32-45-07-700-801. Replace brake If wear pin indicator is at 01mm and less or if the end of wear indicator pin is level with, or below the face of a guide. (REF: TN32- 043) (Ref: AMP 32-210-00)

8B For INBD AND OUTBD AFT BRAKE ROD, installed on both LH and RH MLG:

− Carry out GVI on the AFT BRAKE ROD spherical bearing outer race (made of Stainless Steel) for any defects, missing, and/or migration condition. In case of findings, replace the affected AFT BRAKE ROD ASSY before further flight.

NOTE: The Spherical bearing is the one installed on the AFT BRAKE ROD to the AFT Brake Unit attachment. Ref Tech Notice 32-027 for further details.

(Ref: ETS Recommendation dated 7th Feb 2008 / Tech Notice 32-027)






*CERTIFIED IAW

GCAA REQUIREMENTS

REF EPM 07-01


8C Perform DVI on the MLG (LH & RH) J501 and J503 Electrical Junction Boxes Truck Mounting for damage and abnormalities. Pay particular attention to migrated parts and/or broken clamps throughout the circumference.

In case of findings, corrective action should be carried out i.a.w the applicable AMM.

Raise Tech Log entry following accomplishment of DVI.

(Ref: TN32-033)

9 AFT FUSELAGE

9A Carry out General Visual Inspection of Aft Fuselage Exterior from the ground for obvious damage, leakage, obstruction, security and condition i.a.w. AMM 05-41-00-210-801, including:

Service Panels, Doors and Hatches.

Navigation/Communication Antennas.

Entry doors.

Aft outflow valve door.

Exterior lights: cleanliness.


Tail Strike assembly.

Panels and fairing for missing fasteners


(Ref: AMP 53-802-00)

10 EMPENNAGE

10A Carry out General Visual Inspection of Empennage Exterior from the ground for obvious damage, leakage, obstruction, security and condition, including:

Horizontal stabilizer.

Vertical stabilizer.

Elevators.

Rudders.

Static Dischargers: damage, missing.







*CERTIFIED IAW

GCAA REQUIREMENTS

REF EPM 07-01


11 APU AREA

11A Carry out general visual inspection of APU area from ground for obvious damage, leakage, obstruction, security and condition, including:


Doors: closed and secured.

Exhaust.

12 CARGO COMPARTMENT CHECKS

12A Carry out general visual inspection of fwd, aft, and bulk cargo compartments, with doors fully open, for condition, including:

Ceilings, side walls and floor panels: damage, cleanliness, missing screws and no evidence of fluid spillage.

Fire Extinguishing Nozzles: for damage. NOTE: Make sure ALL fire extinguishing nozzles qty 8, for 777-200/-200LR and qty 10, for 777-300/-300ER are clear of any obstructions or adhesive tapes.

Cargo Smoke Detector Sampling Ports: for damage.

NOTE: Make sure ALL sampling ports are clear of any obstructions or adhesive tapes.

Cargo nets and restraints: damage.

Cargo door cut outs and seals: damage and security.

(Ref: AMP 53-816-00 / AMP 53-846-00 / AMP 53-848-00) (ARN 03884)

13 WATER DRAINAGE FROM FUEL TANKS

13A - Drain water from all fuel tanks at sump drain valves as per AMM 12-11-02-680-801; After drainage ensure drain valves are properly seated and not leaking.

Note: Task to be performed if aircraft ground time exceeds 3.5 hours.

- Make a Technical Log Book entry that water drainage has been performed and record amount of water found in each tank.

(Ref: AMP 28-400-00E)

14 FLIGHT DECK CHECKS

14A Review Maintenance Memo’s and action as necessary.

14B Check cleanliness and general condition of flight deck.

14C Check windows for damage, condition and cleanliness.

14D Check hydraulic fluid level using EICAS Status Display. Service as required with SKYDROL LD4 and record uplift(s) in aircraft Technical Log Book. (i.a.w. AMM 12-12-01-610-801)

(Ref: AMP 29-005-00)






*CERTIFIED IAW

GCAA REQUIREMENTS

REF EPM 07-01


14E Check Crew Oxygen System for correct pressure using EICAS Status Display i.a.w. 35-00-00-210-801. Ensure oxygen pressure above minimum (1500 psi at 21°C (70°F)).

NOTE: At outstations, if pressure is below 1500 psi, refer to FCOM to determine that quantity is sufficient for the scheduled flight.

(Ref: AMP 35-400-00)

14F - Check complement of spare bulbs in flight deck container, replenish as required.

- Check for presence of CB Collar PN 10164-3 qty 4 in spare bulb container, replenish as required.

- Check for presence of Fuse PN B215-06 qty 4 in spare bulb container, replenish as required.

(Ref: Line Maintenance recommendation E-mail dated 31Jul2012)

14G Check emergency equipment for presence and proper stowage, including fire extinguishers for seal and correct pressure. Ref. Emergency Equipment Check List (Form QA/F/0127 for -200, QA/F/0113 for -300, QA/F/0349 for -300ER and QA/F/0597 for -200LR aircraft).

(Ref: AMP 25-005-00E)

14H Operationally check FIRE WARNING SYSTEM (Use the Fire/ OVHT Test switch) i.a.w. AMM 31-51-00-710-801.

(Ref: AMP 31-100-00)

14I Perform operational check of Flight Deck Access System (if installed) as follows: With electrical power established and the flight deck door open.

Position Chime Module switch to NORM (guard closed).

Position Door Lock Control selector to AUTO.

Enter keypad access code.

Verify the door chime sounds and the AUTO UNLK light illuminates.

Position Door Lock Control selector to DENY.

Verify AUTO UNLK light extinguishes.

Position Door Lock Control selector to “UNLKD” and release.

Position Chime Module switch to OFF (guard extended).

Verify LOCK FAIL light illuminates.

Position Chime Module switch to NORM (guard closed). (AMM 52-51-00-710-802).

(Ref: ETS Recommendation dated 17th Dec 2002, 9th Feb 2003 and 20th Jul 2003)

14J Applicable to Trent 800 engine only Check that the Nut Assembly (P/N AS15825 Qty 2) and Union (P/N AS 27467 Qty 1) required to deactivate the FMU, are present in the passenger restraint kit stowage compartment (Ref T/N 73-007). Replace missing items or raise an ADD.






*CERTIFIED IAW

GCAA REQUIREMENTS

REF EPM 07-01


14K Ensure the availability of EAI Deactivation tool kit P/N K28703 in the First Officer stowage closet (Upper flight manual stowage compartment).

(Ref: ETS Recommendation dated 1st Aug 2007)

14L Perform operational check of Actuator Control Electronics (ACE) monitoring functions of Flight Controls System using ACE self-test. (i.a.w. AMM 27-02-02-400-801)

(Ref: AMP 27-160-00 associated 27-CMR-02)

Note 1: This is an AMP Task with an interval of 250 FH. For ease of control it has been aligned with Daily Checks performed on a specific date of each month.

Note 2: In the event the Daily is due but not performed on the specified date (24 Hrs not to exceed 48hrs) then perform the task on the following day.

Note 3: Annotate N/A on those days when this task is not performed.

200 / 200ER / 300

Days of the Month

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15

16 17 18 19 20 21 22 23 24 25 26 27 28 29 30

300ER / 200LR

Days of the Month

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15

16 17 18 19 20 21 22 23 24 25 26 27 28 29 30

15 PASSENGER CABIN CHECKS

15A Check passenger cabin for general condition and cleanliness.

15B Check galleys and lavatories for general condition, odour, cleanliness, evidence of water leakage and condition of floor covering. Check lavatory flush for efficient operation.

15C Extend platen and lower shroud of Trash Compactor. Ensure proper cleaning of upper surface of platen and shroud has been carried out by cleaning contractors.

15D Carry out detailed visual inspection of lavatory waste compartment doors and flaps for proper installation, operation, and sealing. Also, Check that placarded ashtrays are installed and “ No Smoking”, “ No Cigarette Disposal” placards are installed and legible i.a.w. AMM 25-41-08-200-801.

(AD 74-08-09, UK CAA CAP 747 GR No. 20) - ( Ref: AMP 25-070-00 )

15E For each waste bin location check temperature decals for colour (White/Grey dots indicate serviceable extinguisher, black dots indicate extinguisher has been fired and requires weight check to confirm status or replacement). Note: View decals in chute through the waste flap. Examine the fusible tips, replace bottle and temperature indicator if fusible tips found melted.






*CERTIFIED IAW

GCAA REQUIREMENTS

REF EPM 07-01


15F Check wing upper surface and control surfaces, through cabin windows, for general condition and evidence of fluid leakage.

15G Check emergency equipment for presence and proper stowage, including fire extinguishers for seal / correct pressure and portable oxygen cylinders for correct pressure (nominal pressure is 1800 psi at 21°C (70°F)).Ref. Safety Equipment Check (Form QA/F/0127 for -200, QA/F/0113 for -300, QA/F/0349 for -300ER and QA/F/0597 for -200LR aircraft).

(Ref: AMP 25-005-00E)

15H Check EPAS Battery for correct charge at each Passenger door position i.a.w. AMM 52-12-20-200-805 (300 and 300ER) and AMM 52-11-20-710-801 (200, 200ER and 200LR).

(Ref: AMP 52-090-00 / AMP 52-090-01)

15I Check operation of First Class and Business Class seat footrests, paying particular attention to the roller position within the tracks underneath the footrest as well as the correct operation of the arm fitted control switch.

15J Ensure Seat-to-Seat cabling is not exposed and cable raceway covers are correctly installed.

15K - Switch ‘on’ the Emergency Escape Path Marking System lights.

- Check and ensure that all Emergency Escape Path Marking lights are operational in all affected areas.

- Switch ‘off’ the Emergency Escape Path Marking System lights.

(Ref: ETS Recommendation dated 16th Mar 2005)

15L 1. Inspect all Protective Breathing Equipment (PBE) for presence (in the cockpit, cabin

and crew rest compartments, as applicable), integrity of vacuum sealing/packing;

expiry date and any obvious damage/abnormalities (Refer to TN 35-013). Refer to the

Emergency and Loose Equipment Checklist for PBE locations (Form QA/F/0127 for -

200, QA/F/0113 for -300, QA/F/0349 for -300ER and QA/F/0597 for -200LR aircraft).

2. In case of findings, replace the PBE.

3. Raise a Technical Log entry stating: INSPECTION OF PBEs CARRIED OUT IN

ACCORDANCE WITH UAE GCAA DG DIRECTIVE 09-2014 AND TN 35-013.

NOTE:

a. This task is ONLY applicable to airplanes fitted with PBE P/N: 119003-11

(pre-mod of EO MMB777-35-0001).

b. This task is NOT applicable to airplanes fitted with PBE P/N: MR10022N

(post-mod of EO MMB777-35-0001).






*CERTIFIED IAW

GCAA REQUIREMENTS

REF EPM 07-01


16 INFLIGHT ENTERTAINMENT (IFE) SYSTEM CHECKS

16A Select Camera Channels at any one seat and ensure that camera pictures are available.

16B Check quality of Video and Audio at any one last seat in each EADB/ADB zone.

17 WATER / WASTE SERVICING

17A Ensure toilets are serviced i.a.w. AMM 12-17-01 Empty waste tanks, Flush waste tanks. Add pre-charge to waste tank.

18 FINAL ITEMS

18A Carry out a Check to ensure that all tools and equipment used have been removed from aircraft and are accounted for.

18B Ensure all cabin doors, cargo compartment doors and service panels are properly closed and secured.

Pay particular attention to the Potable Water Service Door(s) and Waste Service Door and ensure these are properly closed and latched.

18C Ensure all protective covers and blanks are installed (as required).

18D De-energize the aircraft electrical network (if required).

18E Ensure aircraft Daily Check is endorsed in the aircraft Technical Log Book.

emirates daily chk b777 rev.99 (qaf0336).pdf

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