1) Section 41 – FWD Bulkhead
Section 48 – AFT Bulkhead 2) E5 – Aft the FWD Cargo Dorr
E6 – Aft of the AFT Cargo Door
E7 – Aft part of the cabin Area

3) Card file P84 – RHS
Card file P85 – LHS

4) 640 AB

6 – RHS Wing
A – Inboard
B – Bottom

542 AT 5 – LHS Wing
T – Top 5) Towing airplane – From Nose or Main landing gear

6) Plump port – RHS Lever

7) ESDS – Electrostatic discharge sensitive, Electricity change box, must wear a wrist strap, Special conductive covers, pullout car

8) Service interphone - 3 groups

9) Cockpit to Ground – P40

Maintenance Documents 10) AIMS - Airplane information management system
P1 301-to-309 = Servicing 401-to-499 = Removal & Installation

11) ATA – Servicing chapters (12)

12) DDG – Dispatch Deviations Guide

i) Section 2 – MMEL

ii) Section 3 – CDL

13) Failure
Fault Code = 8 Digits
Maintenance Message = 7 Digits 14) Wing to Body Fairing with composite panels are with honeycomb structure.

15) ELMS = 7 Panels
P100, P200 = LH, RH Power Panel Controller Respectively *P200 Heavy Loads
P320 = Ground Handling TR Unit 16) How are batteries (Main APU) charged? – Charged from Ground Sevice Bus 17) E-10 Rack = APU battery & Charger 18) IDG (integrated drive generator) to LRUS (Line replaceable units) = i) two filters ii) Remote Oil Sensors 19) IDG Servicing when i) Service Indication ii) Underfill/Overfill You must do a IDG Shutdown + 10mins 20) Location of Backup Generator Supplement cooling fan : MEC RHS 21) Number of Permanent Backup Generators : (3) 22) Treat as Emergency Power Source = Main battery & R.A.T 23) Rack located = Aft right main landing gear wheel well. 24) GH Bus Pri Ext Power – TopPriority APU – 2nd Sec Ext Power – 3rd 25) No of Transformers = (4) 26) Inside P85 cardfiles signal gateway = (2) each in each card file. 27) How many 629 buses = [7] Arinc i) 4 System bases & ii) 3 flight control buses 28) ACMS (airplane condition monitoring system) location = Only left aims cabinet 29) Quick Access Recorder (QAR) Which component records? = computer memory card international association (PCMCIA) flash memory card.

30) Where is the Flight Data recorder Located : E7

31) AIMS cabinet process parameters in : Both Left & Right

32) When does the recorder start? : First Engine starts

33) Indication 6 – i) Where do we get supply signal for PDS = CPM GG ii) Where are Coax couplers = LHS & RHS

34) AIMS cabinet located at : E2 Right, E3 Left

35) Warning Systems : Left WS (Captain), Right WS ( 1st Officer)

36) Where is stick located : Below the cockpit on the FWD eqpt centre.

37) How to adjust brightness control - Remote light sesnors outboard = Left & Right

38) Read Camera Display? How many displays? (2) inboards & lower centres

39) Red Messages, Amber Messages, Memo Message : Least Priority

40) Scroll pases : flipped out cancel recall to amber warnings.

41) CCD : Cursor control Device has no. of hotspots : (4)

42) Taxi Camera Kill Switch = E56 located behind the main wing wheel LHS

43) Control Maintenance = Ground test menu = Line maintenance :

Ground test enable switch located at : E61 Maintenance Panel

44) Central Maintenance record : 15 Flight Fail & 100 Flight Takeoffs

45) Technicians access : (3)

46) Electronic Flight Deck – Document Uploads : P18 Panel located at LH Elect cross to RH

47) EFB displays location = P13 & P14

48) Static probes – 8 ADMS – 4 Pitot ADMS = located MEC

Static Probes located = FWD cargo compartment ceiling

49) Where is ISFD located = Centre MMR
50) ISFD test length = 110 Seconds
51) Info Adeleu – How many gyros – 6 laser gyros, 6 accelerometers , 4 lasers, 4 accelerometers
52) Switch on/off Adeleu? I) Adeleu switch ii) Ground speed below 20 knots switch off
53) Pitot Takes heatier levels : i) Low Level – on ground ii) High Level – in flight
54) How many Radar Altanater Antennas = (16) Located bottom of FWD Fuselage & 2500, left PSD If left fails then – Centre- Then Right
55) LCR located – LHS RCR Located – RHS
56) T-eas When indication – Resolution Advisory.
57) Mode 5 – Glidescope, Mode 6 : Radio Callout.
58) Location of VOR : Right top of vertical stabilizer
59) Test of wheiver Marker Beacon – Which VOR receiver = Left VOR Receiver
60) Radio auto/manual to : ADF doesn’t have auto timing
61) What caution for weather Radar – No person < 15feet
62) Which page do you find flight data : Ident page
63) Testing of emergency Lighting duration – 1min
64) E.A.T frequency : 121.5 / Normal, 293 /Communication, 406/data
65) Operating Servors Operation : Connected to flight interphone
66) Cockpit to call ground : Ground Horn comes on
67) How long does flight recorder : 120mins /2hr
68) Light systems Emergency Systems lights comes on the : Overhead panel Door 1 Left
69) VHF – (3) – Left, Right, Centre : Any of them for radio training
70) Location of VHF : Bottom
71) HFT (High Frequency Trans) located = Half Cargo E6 rack
72) Precaution for HF? : People around <transmitter Antenna 6ft
73) Satelite communications used for : Voice & data
74) Location of SAT camm : Cabin E11 Rack
75) Cabin function light/seatbelts/functions can be done by : CSSP/CSAP software loading & test
76) Distribute info to cabin zones : (4)