European Air Transport Leipzig
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1 European Air Transport Leipzig B PCF Familiarization Information Source: Precision Conversions LLC Vision Safe Corporation Innovative Solutions & Support Rolls Royce PLC Pratt & Whitney Name HR Training of the presenter Anrca International LLC Aviation Partners Boeing AIM Aviation Inc. Telair SLC Rockwell Collins 1 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
2 CONTENTS 0. Airplane Changes Overview 1. ATA 21 Air Conditioning 2. ATA 25 Flight Deck Wall 3. ATA 25 Cargo Barrier 4. ATA 25 Lavatory 5. ATA 25 Galley 6. ATA 25 Cargo Compartment 7. ATA 25 Cargo Handling System 9. ATA 27 Flight Controls 10. ATA 28 Fuel 11. ATA 31 Indication and Recording systems 12. ATA 38 Water and Waste 13. ATA 52 Doors 14. ATA 56 Windows 15. ATA 57 Wings 16. ATA 70 Engines 8. ATA 26 Fire Protection 2 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
3 0) AIRPLANE CHANGE OVERVIEW EMERGENCY VISION ASSURANCE SYSTEM NEW LAVATORY INSTALLED RIGHT DOOR DELETED 9G RIGID CARGO BARRIER ADDED PASSENGER DOORS DEACTIVATED WINGLETS (COMING WITH A/C #3) OVERWING EMERGENCY EXITS DEACTIVATED (IF INSTALLED) PASSENGER WINDOWS PLUGGED PASSENGER DOORS DELETED INTIGRATED STANDBY UNIT FLAT PANEL DISPLAY SYSTEM MAIN DECK CARGO DOOR ADDED NEW CREW ENTRY DOOR FLIGHT DECK DOOR AND PORTION OF WALL REMOVED FRAMES MODIFIED FOR CARGO CLEARANCE ANCRA CARGO LOADING SYSTEM 3 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
4 0) AIRPLANE CHANGE OVERVIEW Boeing PCF Manual Supplements Various B PCF Precision PtoF Supplements PC Supplemental Maintenance Manual Rev. M: PC Supplemental Maintenance Manual TR40 Rev. 40: PC Supplemental Illustrated Parts Catalog Rev. M: PC Supplemental Illustrated Parts Catalog TR 33 Rev. 33: PC Supplemental Structural Repair Manual Rev. 16: PC Supplemental Structural Repair Manual TR 20 Rev. 20: Various MSN Aviation Partners Boeing Blended Winglet Program Aircraft Maintenance Manual Part I Rev. H: Oct 2010 Aircraft Maintenance Manual Part II Rev. H: Oct 2010 Supplement Structural Repair Manual Rev. July 2012 Supplement to Non Destructive Test Manual Rev. C: Nov 2012 Supplement to Fault Isolation Manual Rev. B: Oct 2008 Supplement Aircraft Illustrated Parts Catalog Rev. N: Sep 2011 Supplement Wiring Diagram Manual Rev. E: Mar 2014 Fuel Quantity Measuring Stick Data Stick 4 & 5 (KG&KG) Rev. IR: Fuel Quantity Measuring Stick Data Stick 2 & 3 (KG&KG Rev. IR: Aviation Partners Winglets related CMM s Stand 01. October HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
5 0) AIRPLANE CHANGE OVERVIEW Boeing PCF Manual Supplements B PCF Rockwell Collins VHF Transceiver Wiring Diagram Rev. G: B PCF ARCAS Maintenance Manual Supplement TBA TBA TBA B PCF B757 Cargo Floor Modification Aircraft Manual Supplement MMS/ Rev. 1: B PCF AIM Aviation INC. Lavatory AIM Maintenance Manual AA Rev. 3: AIM Illustrated Parts Catalog AA Rev. 3: AIM Lavatory related CMM s B PCF Sliding Carpet FWD Cargo Compartment Telair SLC Manual B FWD Rev. 15: B PCF Sliding Carpet AFT Cargo Compartment Telair SLC Manual B FWD Rev. 16: B PCF ANCRA Cargo Loading System ANCRA B Cargo Handling System Part I Rev. 1: ANCRA B Cargo Handling System Part I Rev. 1: Stand 01. October HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
6 0) AIRPLANE CHANGE OVERVIEW Boeing PCF Manual Supplements B PCF Installation of Emergency Vision Assurance (EVAS) Precision Engineering Authorisation EA Rev. IR: TBA TDG Universal Fault Interrupter UFI TDG , AMM Supplement Rev. H: TDG , Illustrated Hardware Diagram Rev. A: TDG , Troubleshooting + Fault Isolation Rev. A: TDG , WDM Supplement Rev. D: B PCF WQAR Installed on B757 Series Aircrafts TBA TBA B PCF Flat Panel Display System AMM Flat Panel Display System Rev. IR: B PCF Integrated Standby Unit Operation and Installation Manual for ISU Rev. 11: B PCF Portable Electronic Flight Bag (EFB) Mounting and Power Supply System TBA TBA TBA TBA B PCF Lightweight Window Plug Installation Lightweight Window Plug Installation LAP2006 Rev. B: Stand 01. October HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
7 1) ATA 21 AIR CONDITIONING Sidewall air distribution system deleted Main overhead distribution duct modified Two of four rise ducts deleted Relocation of flight deck air distribution riser Right recirculation system deactivated Portion of lavatory/galley vent system deleted Mix manifold retained Shut-off system added 7 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
8 UP 1) ATA 21 AIR CONDITIONING Riser Ducts DELETED RIGHT RISER DUCT FWD ZONE DUCT: (RELOCATED FROM DELETED LEFT RISER DUCT) 1) AIR TEMPERATURE SENSOR 2) TEMPERATURE BULB 3) OVERHEAT SWITCH FWD ZONE RIGHT RISER DUCT AFT ZONE LEFT RISER DUCT AFT ZONE DUCT CAPPED PASSENGER SIDEWALL AIR OUTLETS 1) AIR TEMPERATURE SENSOR 2) TEMPERATURE BULB 3) OVERHEAT SWITCH DELETED LEFT RISER DUCT 8 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
9 1) ATA 21 AIR CONDITIONING Flight deck air distribution riser between BS 297 and BS 310 relocated to accommodate new crew entry door. S 3L SUPPORT BRACKET REDUCER OEM DUCT P 11 PANEL VIEW LOOKING OUTBOARD FWD FLEX HOSE (3 DIA) SLEEVE STA DOOR JAMB, FWD OEM DUCT 9 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
10 1) ATA 21 AIR CONDITIONING Overhead duct 10 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
11 1) ATA 21 AIR CONDITIONING 11 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
12 1) ATA 21 AIR CONDITIONING Riser Shutoff Valves 12 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
13 1) ATA 21 AIR CONDITIONING Air Distribution Schematic FLGHT DECK LAV MAIN DECK MAIN DECK TO FLIGHT DECK CONDITION AIR DISTRIBUTION AIR CONDITIONING MIX BAY RISER SHUTOFF VALVES FWD LOWER DECK CARGO TRIM AIR MODULATING VALVES TRIM AIR PRESS REGULATING VALVE FROM L PACK MIX MANIFOLD ALTERNATE AIR SHUTOFF VALVE ALTERNATE MAIN E/E EQUIPMENT COOLING FROM R PACK AFT LOWER DECK CARGO ZONE TRIM AIR FROM L RECIRC SYS CONDITIONED AIR COLD AIR AIR GROUND CONNECTOR HOT AIR ADDED FOR B PCF CARGO CONVERSION Alternate Air shutoff valve (electrically actuated butterfly valve): System is added to include an alternate source of air in the event of main cargo compartment fire. 13 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
14 1) ATA 21 AIR CONDITIONING Relocated from the stowage bins (BS 517) to the ceiling panels (BS 505): Relocated from BS 1177 to BS 1170: ZONE TEMP SENSOR MODULE FAN SENSOR MODULE FAN ZONE TEMP SENSOR ZONE TEMP SENSOR ZONE TEMP BULB (REF) ZONE TEMP BULB (REF) CABIN AIR CABIN AIR 14 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
15 1) ATA 21 AIR CONDITIONING Equipment Cooling Simplified Flow Diagram FLGHT DECK MAIN PANELS OVERHEAD PANELS FWD LAV FWD MAIN DECK PURGE LINE AFT MAIN DECK CENTER AISLE STAND EQUIP COOLING AUXILIARY FAN FWD EQUIP COOLING SUPPLY SMOKE SENSORS 1 AND 2 WEATHER RADAR FWD EQPT SUPPLY LOW FLOW SENSOR FROM MIX MANIFOLD (ALTERNATE AIR) EQUIPMENT COOLING FANS CLEAN AIR PURGE LINE E/E EQPT RACK FWD EQPT EXHAUST LOW FLOW SENSOR E/E EQUIPMENT RACK E/E COMPARTMENT RECIRCULATION FAN EQPT COOLING SMOKE SENSOR OVERBOARD EXHAUST VALVE TO MIX MANIFOLD A/C MIX BAY AFT EQPT VENT FANS OUTFLOW VALVE MODIFIED FOR B PCF CARGO CONVERSION Overboard exhaust valve controls have been modified to command the valve to open when suppressing a main cargo compartment fire. 15 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
16 OUTBD STA 860 STA 839 STA 820 1) ATA 21 AIR CONDITIONING Flow Control Valve 2x FLEX HOSE SHUTOFF VALVE FWD MIX MANIFOLD OEM FLOOR BEAM CLAMP The pack flow control system has been modified to prevent the flow control and shutoff valves from switching to high flow mode, when on a/c pack is shut off during main cargo compartment fire suppression. 16 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
17 2) ATA 25 FLIGHT DECK WALL Coming with A/C #4: Bin and stowage for trolleys in front of the partition liner. 17 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
18 2) ATA 25 FLIGHT DECK WALL The passenger configuration flight deck wall and the flight deck door will be removed. The existing crew and observer seats in the flight compartment will be retained. Observer Seat in front of the partition liner is not installed. ELT will be installed below the emergency torch. 18 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
19 3)ATA 25 CARGO BARRIER To protect the crew if there is an emergency landing, a rigid 9g cargo barrier will be installed. 19 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
20 3)ATA 25 CARGO BARRIER The rigid cargo barrier will have a sliding doorway for entry into the main deck cargo compartment. 20 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
21 4) ATA 25 LAVATORY The lavatory is installed on the RH side. Re-circulating External servicing Potable Water Dispenser (coming with A/C #4) Lavatory with Potable Water Dispenser 21 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
22 4) ATA 25 LAVATORY The lavatory will retain external servicing capabilities on right hand side of the aircraft. Lavatory Service Panel (Relocated RHS) 22 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
23 5) ATA 25 GALLEY Crew Galley A crew galley will be added in the flight compartment, aft and outboard of the copilot. Hot/cold liquid container Flight compartment, aft and outboard of copilot 23 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
24 6) ATA 25 CARGO COMPARTMENT A Class E cargo compartment will be installed in the airplane main cabin area. 9g cargo barrier acts as smoke barrier Accessible in flight Ceiling raised for 82 inch ULDs Transverse pallet capability Floor panels sealed and non-slip Cargo handling system for 15 ULDS 24 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
25 6) ATA 25 CARGO COMPARTMENT Cargo Compartment (FLA) 25 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
26 7) ATA 25 CARGO HANDLING SYSTEM Cargo Handling System An STC-approved cargo handling system will be installed in the main deck cargo compartment to load/unload and restrain ULDs. The Cargo Handling System is manually operated 26 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
27 7) ATA 25 CARGO HANDLING SYSTEM Cargo handling system Basic CHS accepts ULD arrangements given below (refer to ANCRA CMM) 15 ULDs 88 x 125 inches (223.5 x cm) or 13 ULDs 96 x 125 inches (243.8 x cm) 27 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
28 7) ATA 25 CARGO HANDLING SYSTEM Cargo handling system Option 1 CHS accepts ULD arrangements give below (refer to ANCRA CMM) 15 ULDs 88 x 125 inches (223.5 x cm) or 13 ULDs 88 x 108 inches (223.5 x cm) 28 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
29 7) ATA 25 CARGO HANDLING SYSTEM Increased Height Rails 29 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
30 7) ATA 25 CARGO HANDLING SYSTEM Aft Back Stop Door Sill Protector 30 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
31 7) ATA 25 CARGO HANDLING SYSTEM Crosstrack (Part Number: 83760) Position 15 Container Guide 31 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
32 7) ATA 25 CARGO HANDLING SYSTEM Crosstrack (Part Number: ) Roller Rail (Part Number: 81384) 32 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
33 8) ATA 26 FIRE PROTECTION A smoke detection system that meets the one-minute detection requirements will be installed to monitor the main deck. The system will alert the flight crew on the flight deck by both aural and visual alerts. This system will provide detection and alerting only; no fire-extinguishing agents will be provided for main deck fire suppression. CARGOBARRIER LAVATORY A CREW CREW ENTRY ENTRY DOOR MAIN DECK MAIN CARGO DECK DOOR BS ( DOOR 317.5) CARGO BS ( 550) DOOR BS BS 550 DOOR #2 #2 DDOOR #3 DOOR #3 INOPERATIVE INOPERATIVE INOPERATIVE INOPERATIVE BS 710 BS 1335 BS ( 710) BS ( 1335) A SLIDINGDOOR DOOR Smoke Detector 33 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
34 8) ATA 26 FIRE PROTECTION The Cargo Fire Maintenance Units (CFMU) are installed in the E/E bay CFMUs monitor main cargo smoke detectors CFMUs connected to CFFU in flight compartment 34 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
35 8) ATA 26 FIRE PROTECTION The flight deck unit will not only provide smoke detection system status. As a part of the Class E firefighting procedures, the flight crew will shut off the airflow to the cargo compartment by pushing a switch on this panel. Annunciator lights will indicate if the shutoff valves are open or closed. 35 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
36 8) ATA 26 EVAS EVAS (Emergency Vision Assurance System) For Major Inflight Cockpit Smoke events EVAS RIGHT INSTALLATION ZONE EVAS LEFT INSTALLATION ZONE 36 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
37 8) ATA 26 EVAS 37 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
38 8) ATA 26 EVAS The deployment location is critical to the operation and functionality of EVAS 38 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
39 9) ATA 27 FLIGHT CONTROLS The captain s elevator control cable system will be modified to allow for increased main cargo compartment ceiling height. Two sets of aft pulleys will be modified to allow for ceiling and cargo clearance. 39 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
40 9) ATA 27 FLIGHT CONTROLS Pre-mod Pulleys Post-mod Pulleys 40 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
41 10) ATA 28 FUEL Universal Fault Interrupter (UFI), designed to protect center tank fuel override pumps from: 1. Electrical faults (line-to-ground, line-toline,open phases, out-of-range conditions) 2. Extended operation with uncovered inlet 3. Un-commanded operation (via control of redundant control relays) The UFI device detects the following electrical and operational fault conditions: Low Fuel Auto-Shutoff Relay Failure Undercurrent Differential Current Over Current 41 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
42 10) ATA 28 FUEL 42 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
43 11) ATA 31 INDICATION/RECORDING SYSTEMS Cargo fire flight deck unit Aural warning panel Crew warning control panel 43 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
44 11) ATA 31 INDICATION/RECORDING SYSTEMS MAIN FIRE VALVE CLOSED FWD VALVE CLOSED AFT FAULT T E S T MAIN CARGO FIRE AIRFLOW VALVES CLOSE CARGO Aural Warning Panel Cargo fire flight deck unit 44 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
45 11) ATA 31 INDICATION/RECORDING SYSTEMS Crew warning control panel (Post-mod) Crew warning control panel (Pre-mod) 45 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
46 11) ATA 31 INDICATION/RECORDING SYSTEMS The flight data recorder has been relocated Moved from the aft passenger cabin ceiling Installed below the main cargo compartment floor, aft of the lower aft bulk cargo compartment; Access is through the aft lower cargo compartment Maintenance Practices Maintenance procedures have not changed See OEM Maintenance Manual MAIN DECK FLOOR SECTION 46 STA 1640 E6 RACK AFT, LOWER CARGO STA 1200 CARGO DOOR VOICE AND FLIGHT DATA RECORDER RACK 46 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
47 11) ATA 31 COCKPIT FLAT PANEL DISPLAY The B757 PCF is equipped with an Innovative Solutions & Support Flat Panel Display System. The FPDS consists of: Primary Flight Displays (PFD) Navigation Displays (ND) 47 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
48 11) ATA 31 COCKPIT FLAT PANEL DISPLAY Navigation Display and Primary Flight Display 48 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
49 11) ATA 31 COCKPIT FLAT PANEL DISPLAY FPDS Component Locations DCP DCP E2 - RACK 49 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
50 11) ATA 31 COCKPIT FLAT PANEL DISPLAY FPDS Component Locations 50 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
51 11) ATA 31 COCKPIT FLAT PANEL DISPLAY ISU Connector location Integrated Standby Unit (ISU) 51 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
52 11) ATA 31 FMCS B757/767 PEGASUS 2009 Flight Management Computer System is installed in the B757 PCF Control Display Unit 52 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
53 12) ATA 38 WATER AND WASTE The water/waste systems will be modified to accommodate deletion of existing lavatories and galleys and installation of a new lavatory. Modification will include the following: Retain forward and aft drain masts Delete existing lavatory and galley waste systems Install waste system for new lavatory. Delete existing water supply Deactivate internal plumbing components of unused service panels and seal penetrations Install main deck floor drain 53 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
54 12) ATA 38 WATER AND WASTE Aft Cabin Waste Water Drain Aft Cabin Waste Water Drain 54 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
55 12) ATA 38 WATER AND WASTE The existing fresh water storage and delivery system components will be removed. A potable water system for the lavatory will be added. The potable water tank will be filled from an exterior service panel and drained through the sink faucet. Potable Water Service Panel 55 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
56 13) ATA 52 DOORS CREW ENTRY DOOR Crew Entry Door STA FWD EDGE OF DOOR SKIN STA AFT EDGE OF DOOR SKIN 56 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
57 13) ATA 52 DOORS CREW ENTRY DOOR Only one crew entry door. Opens inward to fully open position Moves under its own weight Stops against the cargo barrier Weighs approximately 75 lbs 57 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
58 13) ATA 52 DOORS CREW ENTRY DOOR NO 6 DOOR STOP P-SEAL SEAL RETAINER DOOR SEAL INTERIOR LINER SUPPORT UPPER CONTROL ROD NO 1 DOOR STOP NO 1 DOOR STOP UPPER LATCH ROD INNER HANDLE NO 1 LATCH CAM NO 3 LATCH CAM NO 1 LATCH CAM INNER HANDLE IN OPEN POSITION NO 3 DOOR STOP SWING ASSY LOWER CONTROL ROD NO 2 LATCH CAM NO 3 LATCH CAM NO 4 LATCH CAM NO 5 DOOR STOP INTERIOR LINER NO 10 DOOR STOP SCREWS NO 10 DOOR STOP INTERIOR LINER SUPPORT 58 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
59 13) ATA 52 DOORS CREW ENTRY DOOR Swing Hinge REMOVE THE 2 BOLTS SECURING THE AFT HINGE TO THE SWING HINGE ASSEMBLY. THE SWEING HINGE SHALL REMAIN ATTACHED TO THE DOOR FRAME HINGE. NOTE: SPACERS SUPPORT THE DOOR ON THE AFT HINGE FRAME ASSEMBLY, THESE WILL FALL OUT ONCE THE SECUREING BOLT IS REMOVED. 59 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
60 13) ATA 52 DOORS CREW ENTRY DOOR CREW ENTRY DOOR FRAME NO 1 LATCH CAM FWD JAMB FRAME LATCH ROLLER 60 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
61 13) ATA 52 DOORS Door 2 - Deactivation No. 1 entry door, right, deleted 61 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
62 13)ATA 52 DOORS L-4 & R-4 DOOR No. 4 entry doors deleted 62 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
63 13) ATA 52 DOORS MAIN DECK CARGO DOOR The Main Cargo Door is controlled from a door control panel located on the partition forward and adjacent to the L1 crew entry door. Mounted to the back of the first observer seat MAIN CARGO DOOR CONTROL PANEL 63 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
64 13) ATA 52 DOORS MAIN DECK CARGO DOOR Main deck cargo door Hydraulic system completely independent of the existing airplane hydraulic systems Main Cargo Door is located on the left hand side of the airplane at BS and extends to BS Main deck cargo door 64 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
65 13) ATA 52 DOORS MAIN DECK CARGO DOOR The MCD Hydraulic System is: Electrically powered Independent of the airplane main systems Manual Operation: Hydraulic hand pump in forward baggage compartment, on the right sidewall just aft of the cargo pit door. Two hydraulic actuators, at the forward and aft edge of the door, will raise and lower the door. 65 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
66 13) ATA 52 DOORS MAIN DECK CARGO DOOR MCD Hydraulic Pump and Reservoir Forward Hold, RHS, Aft of door Pump Handle for Manual Operation 66 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
67 13) ATA 52 DOORS MAIN DECK CARGO DOOR Main Cargo Door Vents 67 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
68 13) ATA 52 DOORS MAIN DECK CARGO DOOR Door Latch and Lock System: Latched by means of eight hydraulically operated over-center hooktype latches A single hydraulic cylinder actuates the latching mechanism Locking is provided by eight pins Gang bar will not translate to the unlocked position as long as the vent doors are in the closed position The vent door cannot be closed until the latches are locked 68 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
69 13) ATA 52 DOORS MAIN DECK CARGO DOOR Main Cargo Door Locking Mechanism 69 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
70 13) ATA 52 DOORS MAIN DECK CARGO DOOR PIN, LOCK Main Cargo Door Locking Mechanism 70 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
71 13) ATA 52 DOORS MAIN DECK CARGO DOOR Main Cargo Door Locking Mechanism GANG BAR 71 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
72 13) ATA 52 DOORS MAIN DECK CARGO DOOR Main Cargo Door Main Cargo Door Latch 72 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
73 13) ATA 52 DOORS MAIN DECK CARGO DOOR Door Sill Protector (retracted) Door Sill Protector (extended) 73 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
74 13) ATA 52 DOORS MAIN DECK CARGO DOOR An Aural Warning Panel is installed in the overhead P5 panel, it provides aural warning to the flight crew in the event Main Cargo Door is in unsafe condition. 74 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
75 14) ATA 56 WINDOWS No. 2 RHS window modified for external opening LATCH STUD PIN LINK ASSEMBLY LOWER SILL NO 2 RHS WINDOW OUTER RELEASE HANDLE BOLT NO 2 RHS WINDOW OPEN BOEING HANDLE GEAR HOUSING BOEING INNER HANDLE SUPPORT STRUCTURE AIRFRAME STRUCTURE ROD GEAR GEAR BOX ASSEMBLY INNER MECHANISM BOLTS Inner Handle 75 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
76 14) ATA 56 WINDOWS No. 2 RHS Window Handle Modification MAIN EXTERIOR HANDLE SHOWN PULLED OUT AND BROKEN OPEN SHAFT RELEASE HANDLE NO 2 RHS WINDOW OML SKIN 76 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
77 13) ATA 56 WINDOWS Passenger windows plugged with STC approved window plugs. 77 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
78 15) ATA 57 WINGS Coming with A/C #3 some of the B757 PCF will have Aviation Partners Boeing winglets installed. Warning: The span of the aircraft with winglets installed will increase about 3m! 78 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
79 15) ATA 57 WINGS 757 APB Winglet Equipment like Anti collision lights, Strobe lights and the Rear position light will be figured out in the associated Aviation Partners Winglets related CMMs not in the AMM. 79 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
80 16) ATA 70 ENGINES B757 PCF with German Registration will be powered by PW2000 engines B757 PCF with British Registration will be powered by RR RB engines 80 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
81 Thank you for your Attention! Name of the presenter 81 HR Training B PCF Familiarization Information Leipzig Rev.: 01 October 2015
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