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1 OF 2 150526 WRO F381 PIC0092015
WORK REQUEST ORDER
PICTON II LTD
VP-BBJ 16737-72U I SN 29273 I YG006
NC I E2T I E2C I APUT I APUC
I
TO: FROM (CAM):
Seyidi Ersevik Steve Wilson
COMPANY: DATED:
hit Aviation Geneva 76.05.7014
FAX NUMBER: QUOTATION REFERENCE:
NJA
EMAIL ADDRESS: WORK REQUEST ORDER NUMBER:
P1C0092015
W/O ENTRY
ITEM DESCRIPTION
SIGNATURE
1. Comply with 1A/2A CAMP WO attached - -VP-BB) 2A Check 2015".
Comply with Due Maintenance CAMP WO attached - "VP-BB) Due MX Jun 2015".
2. Compliance with AD 2012.24.08 / SB 737-30A1063 R2
NOTE: KITS provided as ordered with Jet Aviation.
AMOC Letters to be referred if SB 737.30A1063 is not possible to install as is.
(AMOC letters:
I. GAMOC_1305-13-254
2. GAMOC_1305.14-66
3. SB-737-30A1063-02-AMOC-01 = 36 Months
3. Compliance with Task 28-AWL-05 and any other A/R applicable task after AD 2012-24.08 C/W.
4. Compliance with AD 2010-24-11 / SB 737.57A1279 consumables to be ordered ASAP.
NOTE: A/R Tasks (MPD) to be verified N/A before access closure.
S. Compliance with AD 2012-25-05 N/A by PN installed. Please check aircraft and record in WO
accordingly.
6. Compliance with SB 737-28A1206 R3. Revision 2 previously C/W.
7.
THANK YOU
EXPECTED ARRIVAL: 15.06.2015
REQUESTED AVAILABILITY: 26.06.2015
CONTINUED AIRWORTHINESS MANAGEMENT (on behalf of PICTON II Ltd)
Qjet Aero I Switzerland I [email protected] I Tel: +41 76 510 2654
EFTA_R1_02140495
EFTA02714500
150526 WRO F381 PIC0092015
WORK REQUEST ORDER
INSTRUCTIONS RELEVANT - CERTIFICATE OF RELEASE TO SERVICE (CRS)
1. After entry of Work Request Items into MRO system, Planning or Technical
Support shall sign in the allocated space. Signature indicates that request(s)
have been transferred to the actual project.
2. Item numbers showing "*" have been amended/added after original order
was issued.
3. Certificate of Release to Service (CRS) shall refer Work Request Order
Number and encompass all requested items unless otherwise specified or
communicated.
4. Work Order entries (items) shall detail maintenance reference/specific
chapters in all cases. Generic references and vague statements will not be
accepted. AMM revision status shall also be indicated.
5. CRS shall comprise Flight Log Entry/Stamp/Signature and printed Certificate
for Aircraft/Engine/APU Logbook(s).
INSTRUCTIONS RELEVANT - CONTINUED AIRWORTHINESS MANAGEMENT
1. Before aircraft departure CRS, WO and Flight Log Entry shall be scanned and
sent to the Continued Airworthiness Manager (CAM) for review.
2. After project closing, all CAMP Cards including CRS shall be scanned and sent
to CAMP SYSTEMS for update within 5 working days.
3. Original Work Package documents shall be handed to the Operator or CAM as
arranged.
Note: There is no requirement for originals/copies of procedures used during
maintenance to be provided.
CONTINUED AIRWORTHINESS MANAGEMENT (on behalf of PICTON II Ltd)
Qjet Aero I Switzerland I [email protected] I Tel: +41 76 510 2654
EFTA_R1_02140498
EFTA02714501
CAMP
A^....P•••••••••••ey
Work Order Contents Report
SERIAL : 29273 (YG006) REGNO : VP-BBJ MODEL NAME : BBJ 737-700IGW/-800/-900ER WORK ORDER A: VP-BB.1 2A CHECK 2015
DATE IN : UTC:15-Jun-2015 12:00 AM DATE OUT : UTC:26-Jun-2015 12:00 AM ICAO : SERVICE CENTER : JET AVIATION (GENEVE) S.A.
SORT ITEM NO DESCRIPTION STATUS
COMPLIANCE NEXT DUE TIME
REMAINING
1.0 050020 A-2 CHECK OPEN
1.1 352003 VISUAL INSPECTION OXYGEN SYS. BOX(S) OPEN
1.2 352004 VISUAL INSPECTION OXYGEN SYS MASK(S) OPEN
1.3 21-88)-01 INSPECT AND CLEAN OR REPLACE THE LEFT HAND NC COALESCER BAG OPEN
1.4 21-88)-02 INSPECT AND CLEAN OR REPLACE THE RIGHT HAND NC COALESCER BAG OPEN
1.5 33-090-00 GENERAL VISUAL INSPECTION OF THE TRANSPARENT FAIRING LENS LOCATED ON THE FORWARD LEADING OPEN
EDGE OF THE WINGLET, LEFT AND RIGHT
1.6 25-020-00 DETAIL INSPECTION OF PIE CAPTAIN, FIRST OFFICER, FIRST OBSERVER AND SECOND OBSERVER (IF OPEN
INSTALLED) SEAT HARNESSES, CROTCH STRAPS, AND SHOULDER BELTS (AS APPLICABLE) FOR WEAR,
CONDITION AND SECURITY.
1.7 28-20-01 PATS OPERATIONAL CHECK OF THE AUXILIARY FUEL CONTROL UNIT OPEN
1.8 23-110-00 (FAR 91.207) INSPECT (FIXED) EMERGENCY LOCATOR TRANSMITTER TAW FAR 91.207(D) OPEN
1.9 54.090-01 FUNCTIONALLY CHECK THE LEFT ENGINE FORWARD STRUT AND AFT STRUT MIRING DRAINS. OPEN
1.10 54-090-02 FUNCTIONALLY CHECK THE RIGHT ENGINE FORWARD STRUT AND AFT STRUT MIRING DRAINS. OPEN
1.11 385015 CLEAN AFT GALLEY SINK DRAIN FILTER OPEN
1.12 21-140-01 CHECK THE LEFT WATER SEPARATOR INDICATION DISK (WITH THE AIR CONDITIONING SYSTEM OPERATING) OPEN
1.13 21.140.02 CHECK THE RIGHT WATER SEPARATOR INDICATION DISK (WITH THE AIRCONDITIONING SYSTEM OPERATING) OPEN
1.14 23-040-00 OPERATIONAL CHECK OF THE VOICE RECORDER AND RECORDER INDEPENDENT POWER OPEN
SUPPLY (RIPS) (IF INSTALLED).
1.15 27-102-00 LUBRICATE STABILIZER TRIM ACTUATOR AND ACTUATOR GIMBAL PINS AND BALLNUT OPEN
1.16 27-170-01 LUBRICATE LEFT WING TRAILING EDGE FLAP ACTUATION MECHANISM OPEN
1.17 27-170-02 WBRICATE RIGHT WING TRAILING EDGE FLAP ACTUATION MECHANISM OPEN
L18 32-010-01 CLEAN LEFT MAIN LANDING GEAR ASSEMBLY SHOCK STRUT OPEN
1.19 32-010-02 CLEAN RIGHT MAIN LANDING GEAR ASSEMBLY SHOCK STRUT OPEN
1.20 32-020-01 SERVICE LEFT MAIN LANDING GEAR ASSEMBLY SHOCK STRUT OPEN
1.21 32-020-02 SERVICE RIGHT MAIN LANDING GEAR ASSEMBLY SHOCK STRUT OPEN
1.22 32-030-01 LUBRICATE LEFT MAIN LANDING GEAR ASSEMBLY OPEN
1.23 32-030-02 WBRICATE RIGHT MAIN LANDING GEAR ASSEMBLY OPEN
1.24 32-060-00 CLEAN NOSE LANDING GEAR SHOCK STRUT OPEN
1.25 32-070-00 SERVICE NOSE LANDING GEAR SHOCK STRUT OPEN
1.26 32-080-00 LUBRICATE NOSE LANDING GEAR ASSEMBLY OPEN
1.27 32-270-01 VISUAL CHECK LEFT BRAKE WEAR PINS FOR MINIMUM EXTENSION OPEN
1.28 32-270-02 VISUAL CHECK RIGHT BRAKE WEAR PINS FOR MINIMUM EXTENSION OPEN
1.29 32-800-00 EXTERNAL ZONAL INSPECTION (GV) NOSE LANDING GEAR AND LANDING GEAR DOORS (FROM GROUND) OPEN
PERFORM AN EXTERNAL ZONAL INSPECTION (GV) Of THE NOSE LANDING GEAR AND LANDING GEAR DOORS.
INSPECTION IS ACCOMPLISHED FROM THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. (EZAP)
1.30 32.804.01 EXTERNAL ZONAL INSPECTION (GV) LEFT MAIN LANDING GEAR AND LANDING GEAR DOORS (FROM GROUND) OPEN
PERFORM AN EXTERNAL ZONAL INSPECTION (GV) OF THE LEFT MAIN LANDING GEAR AND LANDING GEAR
DOORS. INSPECTION IS
ACCOMPLISHED FROM THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS
1.31 32.808.02 EXTERNAL ZONAL INSPECTION (GV) RIGHT MAIN LANDING GEAR AND LANDING GEAR DOORS (FROM GROUND) OPEN
PERFORM AN EXTERNAL ZONAL INSPECTION (GV) OF THE RIGHT MAIN LANDING GEAR AND LANDING GEAR
DOORS. INSPECTION IS
ACCOMPLISHED FROM THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS
26-MAY-2015 © CAMP SYSTEMS I of 3
EFTA_R1_02140497
EFTA02714502
CAMP
A^....P•••••••••••ey
Work Order Contents Report
SERIAL : 29273 (YG006) REGNO : VP-BB) MODEL NAME : 68) 737.700IGW/-800/-900ER WORK ORDER At: VP-B8) 2A CHECK 2015
DATE IN : UTC:15-Jun-2015 12:00 AM DATE OUT : UTC:26-Jun-2015 12:00 AM ICAO : SERVICE CENTER : JET AVIATION (GENEVE) S.A.
SORT ITEM NO DESCRIPTION STATUS
COMPLIANCE NEXT DUE TIME
REMAINING
1.32 33-010-00 OPERATIONAL CHECK EMERGENCY LIGHTS OPEN
1.33 53-800-00 EXTERNAL ZONAL INSPECTION (GV) OF THE LOWER FUSELAGE. THE NOSE LANDING GEAR WHEEL WELL AND OPEN
MAIN LANDING GEAR WHEEL WELL ARE ALSO INCLUDED. INSPECTION IS ACCOMPLISHED FROM THE GROUND,
WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRED (EZAP)
1.34 53.81200 INTERNAL ZONAL INSPECTION (GV) FORWARD CARGO COMPARTMENT - SECTION 43, STATION 396 TO OPEN
FORWARD CARGO COMPARTMENT AFT BULKHEAD
1.35 53-830-00 INTERNAL ZONAL INSPECTION (GV) AFT CARGO COMPARTMENT - SECTION 46 AND 47 (PART), STATION 727 OPEN
TO STATION 947.5
1.36 53.84400 EXTERNAL ZONAL INSPECTION (GV) OF THE WING TO BODY FAIRING. INSPECTION IS ACCOMPLISHED FROM OPEN
THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRE
1.37 53-894-00 EXTERNAL ZONAL INSPECTION (GV) OF 711E FUSELAGE. INSPECTION IS ACCOMPLISHED FROM THE GROUND, OPEN
WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRED
1.38 55-800-00 EXTERNAL ZONAL INSPECTION (GV) VERTICAL FIN AND HORIZONTAL STABILIZER. INSPECTION IS OPEN
ACCOMPLISHED FROM THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS
PANELS REQUIRED
1.39 57.802-01 EXTERNAL ZONAL INSPECTION (GV) LEFT WING INSPECTION IS ACCOMPLISHED FROM THE GROUND, WITHOUT OPEN
THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRED.
1.40 57-872-02 EXTERNAL ZONAL INSPECTION (GV) RIGHT WING INSPECTION IS ACCOMPLISHED FROM THE GROUND, OPEN
WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRED.
1.41 70-803-01 EXTERNAL ZONAL INSPECTION (GV) NO. 1 ENGINE STRUT FAIRINGS. INSPECTION IS ACCOMPLISHED FROM OPEN
THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. NO
ADDITIONAL ACCESS PANELS REQUIRED.
1.42 70-810-02 EXTERNAL ZONAL INSPECTION (GV) NO. 2 ENGINE STRUT FAIRINGS INSPECTION IS ACCOMPLISHED FROM OPEN
THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. NO
ADDITIONAL ACCESS PANELS REQUIRED
1.43 52-150-00 LUBRICATE AIRSTAIR DOOR SYSTEM (INCLUDES TWO ROLLERS, CARRIAGE DRIVE BEARING, DRIVE NUT IN OPEN
JACK SCREW, LOCK PIN GREASE FITTING AND FOUR BEARINGS IN THE CARRIAGE ROLLERS).
1.44 26-450-00 INSPECT (DETAILED) THE PORTABLE HALON FIRE EXTINGUISHERS FOR PROPER PRESSURE (IF GAUGE OPEN
INSTALLED), WEIGHT AND CONDITION.
1.45 050010 A- I CHECK OPEN
1.46 257001 GENERAL VISUAL INSPECTION HEADLINER CEILING PANELS OPEN
1.47 257002 GENERAL VISUAL INSPECTION INTERIOR BULKHEADS OPEN
1.48 257003 GENERAL VISUAL INSPECTION COMPARTMENT DOORS OPEN
1.49 257004 GENERAL VISUAL INSPECTION SEATS ANDTABLES OPEN
1.50 257005 GENERAL VISUAL INSPECTION CLOSET AND CABINETS OPEN
1.51 257006 GENERAL VISUAL INSPECTION CLOSET AND CABINET DOORS OPEN
1.52 257007 GENERAL VISUAL INSPECTION BED AND DIVANS OPEN
1.53 257011 CHECK SAFETY BELTS OPEN
1.54 352002 GENERAL VISUAL INSPECTION CHEMICAL 02 MASK OPEN
1.55 381120 CHECK WATER/WASTE DRAIN LINES OPEN
1.56 385010 CLEAN WATER/WASTE INSIDE FILTER OPEN
1.57 57-950-01 EXTERNAL ZONAL INSPECTION OF THE LEFT WINGLET OPEN
1.58 57-952-01 INTERNAL ZONAL INSPECTION LEFT WINGLET OPEN
1.59 57-960-02 EXTERNAL ZONAL INSPECTION OF THE RIGHT WINGLET OPEN
26-MAY-2015 © CAMP SYSTEMS 2 of 3
EFTA_R1_02140498
EFTA02714503
CAMP
A^....P•••••••••••ey
Work Order Contents Report
SERIAL : 29273 (YG006) REGNO : VP-BB) MODEL NAME : 88) 737.700IGW/-800/-900ER WORK ORDER At: VP-88) 2A CHECK 2015
DATE IN : UTC:15-Jun-2015 12:00 AM DATE OUT : UTC:26-Jun-2015 12:00 AM ICAO : SERVICE CENTER : JET AVIATION (GENEVE) S.A.
SORT ITEM NO DESCRIPTION STATUS
COMPLIANCE NEXT DUE TIME
REMAINING
1.60 57-962-02 INTERNAL ZONAL INSPECTION OF THE RIGHT WINGLET OPEN
1.61 33-055-00 FUNCTIONAL CHECK THE EMERGENCY LIGHTING BATTERY PACKS FOR CAPACITY (15 MIN. MINIMUM) AND ONE OPEN
COMPLETE DEEP CYCLE.
1.62 72-020-01 DETAILED INSPECTION OF LEFT ENGINE INLET AND FAN BLADES. OPEN
1.63 72-020-02 DETAILED INSPECTION OF RIGHT ENGINE INLET AND FAN BLADES OPEN
Prepared By: Date:
Approved By: Date:
26-MAY-2015 © CAMP SYSTEMS 3 of 3
EFTA_R1_02140499
EFTA02714504
CAMP
A^....P••••••••••ey
Work Order Contents Report
SERIAL : 29273 (YG006) REGNO : VP-BEJ MODEL NAME : BB) 737.700IGW/-8001.900ER WORK ORDER At: VP-B8) DUE MX )UN. 2015
DATE IN : UTC:15-Jun-2015 12:00 AM DATE OUT : UTC:26-Jun-2015 12:00 AM ICAO : SERVICE CENTER : JET AVIATION (GENEVE) S.A.
SORT ITEM NO DESCRIPTION STATUS
COMPLIANCE NEXT DUE TIME
REMAINING
1.0 737-28A1206 R3 FUEL - DISTRIBUTION - CENTER FUEL TANK BOOST PUMP AUTO SHUTOFF AND MASTER CAUTION LOGIC OPEN
CHANGE, SERVICE BULLETIN
2.0 252501 VISUALLY CHECK FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE BOTTLE FOR PROPER OPEN
PRESSURE
3.0 252502 VISUALLY CHECK FORWARD SERVICE DOOR EMERGENCY ESCAPE SLIDE PRESSURE BOTTLE FOR PROPER OPEN
PRESSURE
4.0 252503 VISUALLY CHECK AFT ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE BOTTLE FOR PROPER PRESSURE OPEN
5.0 252504 VISUALLY CHECK AFT SERVICE DOOR EMERGENCY ESCAPE SLIDE PRESSURE BOTTLE FOR PROPER PRESSURE OPEN
6.0 FM 2005-18-23 CORROSION PROTECTION OF THE ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELL OPEN
7.0 FM 2006-21-01 PART 1 FLIGHT CONTROLS AILERON AND AILERON TRIM CONTROL SYSTEM MEASURE THE FREEPLAY OF BOTH OPEN
AILERON CONTROL BALANCE TABS
8.0 FM 2006-21-01 PART 2 FLIGHT CONTROLS - AILERON AND AILERON TRIM CONTROL SYSTEM - REPETATIVE LUBRICATION OPEN
9.0 FM 2011.27-03 PAM (6)(1)(1)(1) DETAILED INSPECTION TO PREVENT AN UNDETECTED FAILURE OF THE PRIMARY LOAD PATH FOR THE OPEN
BALLSCREW IN THE DRIVE MECHANISM OF THE HSTA AND SUBSEQUENT WEAR AND FAILURE OF THE
SECONDARY LOAD PATH IN ACCORDANCE WITH SERVICE BUITIN 737-27A1277 R2
10.0 29-230-03 OPERATIONAL CHECK STANDBY RUDDER SYSTEM TO INCLUDE OBSERVING LOW PRESSURE LIGHT OPEN
ILLUMINATION AND THEN EXTINGUISHING.
11.0 24-120-00 (001.1) RESTORE MAIN BATTERY OPEN
12.0 24-120-00(002.1) RESTORE AUXILIARY BATTERY OPEN
13.0 254206 LAERDAL HEARTSTART FR DEFIBRILLATOR PADS OPEN
14.0 081001 WEIGHT CHECK OF AIRCRAFT OPEN
15.0 252901 CAPTAIN LIFE JACKET OPEN
16.0 252902 FIRST OFFICER LIFE JACKET OPEN
17.0 252903 FIRST OBSERVER LIFE JACKET OPEN
18.0 252904 NO. 1 FORWARD FLIGHT ATTENDANT LIFE JACKET OPEN
19.0 252905 NO. 2 FORWARD FLIGHT ATTENDANT LIFE JACKET OPEN
20.0 252906 NO. 1 AFT FLIGHT ATTENDANT UFE JACKET OPEN
21.0 252907 NO. 2 AFT FLIGHT ATTENDANT LIFE JACKET OPEN
22.0 252909 SECOND OBSERVER LIFE JACKET OPEN
23.0 256323 (001.1) OPERATIONAL CHECK OF THE NO. 1 FORWARD EMERGENCY FLASHUGHT OPEN
24.0 256323 (002,1) OPERATIONAL CHECK OF THE NO. 2 FORWARD EMERGENCY FLASHUGHT OPEN
25.0 256323 (003.1) OPERATIONAL CHECK OF THE NO. 1 COCKPIT FLASHLIGHT OPEN
26.0 256323 (004.1) OPERATIONAL CHECK OF THE NO. 2 COCKPIT FLASHUGHT OPEN
27.0 256323 (005.1) OPERATIONAL CHECK OF THE NO. 1 AFT EMERGENCY FLASHUGHT OPEN
28.0 256325 (003.1) OPERATIONAL CHECK OF THE CARGO NET OPEN
29.0 347105 (1) BIANNUAL CHECK EGPWS TERRAIN DATABASE VERSION STATUS OPEN
30.0 33.06600 RESTORE EMERGENCY LIGHTING BATTERY PACK (TWO OR MORE COMPLETE DEEP CYCLES) BATTERY CAPACITY OPEN
TO REQUIRED STANDARD
31.0 25-310-00 (002.1) RESTORE NO. 2 LIFE RAFT PRESSURE BOTTLE OPEN
32.0 25-420-03 (001.1) RESTORE FORWARD FIRST AID KIT OPEN
33.0 25-420-00 (002.1) RESTORE AFT FIRST AID KIT OPEN
34.0 25-430-00 (001.1) RESTORE MEDAIRE - BLUE FIRST AID MEDICAL KIT OPEN
26-MAY-2015 © CAMP SYSTEMS 1 of 2
EFTA_R1_02140500
EFTA02714505
CAMP
A^....P••••der...4 .•
Work Order Contents Report
SERIAL : 29273 (YG006) REGNO : VP-BB) MODEL NAME : 88) 737.700IGW/-800/-900ER WORK ORDER At: VP-B8.1 DUE MX )UN. 2015
DATE IN : UTC:15-Jun-2015 12:00 AM DATE OUT : UTC:26-Jun-2015 12:00 AM ICAO : SERVICE CENTER : JET AVIATION (GENEVE) S.A.
SORT ITEM NO DESCRIPTION STATUS
COMPLIANCE NEXT DUE TIME
REMAINING
35.0 38-040-00 RESTORE WASTE DRAIN BALL VALVE THE WASTE DRAIN BALL-VALVE BY REPLACING SEALS (2) (OFF OPEN
AIRCRAFT)
36.0 FM 2015-04-02 NO. 1ENGINE - ENGINE FUEL AND CONTROL - MODIFY THE ENGINE BY REMOVING FULL AUTHORITY DIGITAL OPEN
ENGINE CONTROL (FADEC) SOFTWARE, VERSION 7.B.V4 OR EARUER, INSTALLED IN THE ELECTRONIC ENGINE
CONTROL (EEC)
37.0 FM 2015-04-02 NO. 2 ENGINE - ENGINE FUEL AND CONTROL - MODIFY THE ENGINE BY REMOVING FULL AUTHORITY DIGITAL OPEN
ENGINE CONTROL (FADEC) SOFTWARE, VERSION 7.B.V4 OR EARLIER, INSTALLED IN THE ELECTRONIC ENGINE
CONTROL (EEC)
38.0 25-300-00 (002.1) INSPECT AFT LIFE RAFT OPEN
39.0 25-300-00 (003.1) INSPECT NO. 3 LIFE RAFT OPEN
40.0 26-330-00 (002.1) REPLACE (LIID2) CARGO FIRE EXTINGUISHER BOTTLE AFT SQUIB OPEN
41.0 25-60-00 GENERAL VISUAL INSPECTION OF ALL COCKPIT / CABIN EMERGENCY EQUIPMENT OPEN
42.0 28-054-00 OPERATIONAL CHECK (BITE) THE FUEL PUMP GFI RELAY OPEN
43.0 28-056-00 FUNCTIONALLY CHECK THE CENTER TANK FUEL BOOST PUMP POWER FAILED ON PROTECTION SYSTEM OPEN
44.0 28-115-00 FUNCTIONALLY CHECK THE CENTER TANK BOOST PUMP AUTO SHUTOFF SYSTEM OPEN
45.0 28-AWL-19 REVIEW CENTER TANK FUEL BOOST PUMP AUTOMATIC SHUTOFF SYSTEM OPEN
46.0 28-AWL-20 REVIEW OVER-CURRENT AND ARCING PROTECTION ELECTRICAL DESIGN FEATURES OPERATION - BOOST PUMP OPEN
GROUND FAULT INTERRUPTER (CFI)
47.0 28-AWL-23 FUNCTIONALLY TEST CENTER TANK FUEL BOOST PUMP POWER FAILED ON PROTECTION SYSTEM. OPEN
48.0 737015 (I) ANNUAL CHECK OF EEC# I & EEC#2 SOFTWARE ENGINE FUEL AND CONTROL ECU SOFTWARE STATUS OPEN
49.0 FM 2011.27-03 PAM (G)(1XI)(2) LUBRICATE TO PREVENT AN UNDETECTED FAILURE OF THE PRIMARY LOAD PATH FOR THE 8A11FrREW IN THE OPEN
DRIVE MECHANISM OF THE HSTA AND SUBSEQUENT WEAR AND FAILURE OF THE SECONDARY LOAD PATH IN
ACCORDANCE SERVICE BULLETIN 737-27A1277 R2
50.0 347101 UPDATE NAV DATABASE OPEN
Prepared By: Date:
Approved By: Date:
26-MAY-2015 © CAMP SYSTEMS 2 of 2
EFTA_R1_02140501
EFTA02714506
WORK REQUEST ORDER
PICTON II LTD
VP-BBJ 16737-72U I SN 29273 I YG006
NC I E2T I E2C I APUT I APUC
I
TO: FROM (CAM):
Seyidi Ersevik Steve Wilson
COMPANY: DATED:
hit Aviation Geneva 76.05.7014
FAX NUMBER: QUOTATION REFERENCE:
NJA
EMAIL ADDRESS: WORK REQUEST ORDER NUMBER:
P1C0092015
W/O ENTRY
ITEM DESCRIPTION
SIGNATURE
1. Comply with 1A/2A CAMP WO attached - -VP-BB) 2A Check 2015".
Comply with Due Maintenance CAMP WO attached - "VP-BB) Due MX Jun 2015".
2. Compliance with AD 2012.24.08 / SB 737-30A1063 R2
NOTE: KITS provided as ordered with Jet Aviation.
AMOC Letters to be referred if SB 737.30A1063 is not possible to install as is.
(AMOC letters:
I. GAMOC_1305-13-254
2. GAMOC_1305.14-66
3. SB-737-30A1063-02-AMOC-01 = 36 Months
3. Compliance with Task 28-AWL-05 and any other A/R applicable task after AD 2012-24.08 C/W.
4. Compliance with AD 2010-24-11 / SB 737.57A1279 consumables to be ordered ASAP.
NOTE: A/R Tasks (MPD) to be verified N/A before access closure.
S. Compliance with AD 2012-25-05 N/A by PN installed. Please check aircraft and record in WO
accordingly.
6. Compliance with SB 737-28A1206 R3. Revision 2 previously C/W.
7.
THANK YOU
EXPECTED ARRIVAL: 15.06.2015
REQUESTED AVAILABILITY: 26.06.2015
CONTINUED AIRWORTHINESS MANAGEMENT (on behalf of PICTON II Ltd)
Qjet Aero I Switzerland I [email protected] I Tel: +41 76 510 2654
EFTA_R1_02140495
EFTA02714500
150526 WRO F381 PIC0092015
WORK REQUEST ORDER
INSTRUCTIONS RELEVANT - CERTIFICATE OF RELEASE TO SERVICE (CRS)
1. After entry of Work Request Items into MRO system, Planning or Technical
Support shall sign in the allocated space. Signature indicates that request(s)
have been transferred to the actual project.
2. Item numbers showing "*" have been amended/added after original order
was issued.
3. Certificate of Release to Service (CRS) shall refer Work Request Order
Number and encompass all requested items unless otherwise specified or
communicated.
4. Work Order entries (items) shall detail maintenance reference/specific
chapters in all cases. Generic references and vague statements will not be
accepted. AMM revision status shall also be indicated.
5. CRS shall comprise Flight Log Entry/Stamp/Signature and printed Certificate
for Aircraft/Engine/APU Logbook(s).
INSTRUCTIONS RELEVANT - CONTINUED AIRWORTHINESS MANAGEMENT
1. Before aircraft departure CRS, WO and Flight Log Entry shall be scanned and
sent to the Continued Airworthiness Manager (CAM) for review.
2. After project closing, all CAMP Cards including CRS shall be scanned and sent
to CAMP SYSTEMS for update within 5 working days.
3. Original Work Package documents shall be handed to the Operator or CAM as
arranged.
Note: There is no requirement for originals/copies of procedures used during
maintenance to be provided.
CONTINUED AIRWORTHINESS MANAGEMENT (on behalf of PICTON II Ltd)
Qjet Aero I Switzerland I [email protected] I Tel: +41 76 510 2654
EFTA_R1_02140498
EFTA02714501
CAMP
A^....P•••••••••••ey
Work Order Contents Report
SERIAL : 29273 (YG006) REGNO : VP-BBJ MODEL NAME : BBJ 737-700IGW/-800/-900ER WORK ORDER A: VP-BB.1 2A CHECK 2015
DATE IN : UTC:15-Jun-2015 12:00 AM DATE OUT : UTC:26-Jun-2015 12:00 AM ICAO : SERVICE CENTER : JET AVIATION (GENEVE) S.A.
SORT ITEM NO DESCRIPTION STATUS
COMPLIANCE NEXT DUE TIME
REMAINING
1.0 050020 A-2 CHECK OPEN
1.1 352003 VISUAL INSPECTION OXYGEN SYS. BOX(S) OPEN
1.2 352004 VISUAL INSPECTION OXYGEN SYS MASK(S) OPEN
1.3 21-88)-01 INSPECT AND CLEAN OR REPLACE THE LEFT HAND NC COALESCER BAG OPEN
1.4 21-88)-02 INSPECT AND CLEAN OR REPLACE THE RIGHT HAND NC COALESCER BAG OPEN
1.5 33-090-00 GENERAL VISUAL INSPECTION OF THE TRANSPARENT FAIRING LENS LOCATED ON THE FORWARD LEADING OPEN
EDGE OF THE WINGLET, LEFT AND RIGHT
1.6 25-020-00 DETAIL INSPECTION OF PIE CAPTAIN, FIRST OFFICER, FIRST OBSERVER AND SECOND OBSERVER (IF OPEN
INSTALLED) SEAT HARNESSES, CROTCH STRAPS, AND SHOULDER BELTS (AS APPLICABLE) FOR WEAR,
CONDITION AND SECURITY.
1.7 28-20-01 PATS OPERATIONAL CHECK OF THE AUXILIARY FUEL CONTROL UNIT OPEN
1.8 23-110-00 (FAR 91.207) INSPECT (FIXED) EMERGENCY LOCATOR TRANSMITTER TAW FAR 91.207(D) OPEN
1.9 54.090-01 FUNCTIONALLY CHECK THE LEFT ENGINE FORWARD STRUT AND AFT STRUT MIRING DRAINS. OPEN
1.10 54-090-02 FUNCTIONALLY CHECK THE RIGHT ENGINE FORWARD STRUT AND AFT STRUT MIRING DRAINS. OPEN
1.11 385015 CLEAN AFT GALLEY SINK DRAIN FILTER OPEN
1.12 21-140-01 CHECK THE LEFT WATER SEPARATOR INDICATION DISK (WITH THE AIR CONDITIONING SYSTEM OPERATING) OPEN
1.13 21.140.02 CHECK THE RIGHT WATER SEPARATOR INDICATION DISK (WITH THE AIRCONDITIONING SYSTEM OPERATING) OPEN
1.14 23-040-00 OPERATIONAL CHECK OF THE VOICE RECORDER AND RECORDER INDEPENDENT POWER OPEN
SUPPLY (RIPS) (IF INSTALLED).
1.15 27-102-00 LUBRICATE STABILIZER TRIM ACTUATOR AND ACTUATOR GIMBAL PINS AND BALLNUT OPEN
1.16 27-170-01 LUBRICATE LEFT WING TRAILING EDGE FLAP ACTUATION MECHANISM OPEN
1.17 27-170-02 WBRICATE RIGHT WING TRAILING EDGE FLAP ACTUATION MECHANISM OPEN
L18 32-010-01 CLEAN LEFT MAIN LANDING GEAR ASSEMBLY SHOCK STRUT OPEN
1.19 32-010-02 CLEAN RIGHT MAIN LANDING GEAR ASSEMBLY SHOCK STRUT OPEN
1.20 32-020-01 SERVICE LEFT MAIN LANDING GEAR ASSEMBLY SHOCK STRUT OPEN
1.21 32-020-02 SERVICE RIGHT MAIN LANDING GEAR ASSEMBLY SHOCK STRUT OPEN
1.22 32-030-01 LUBRICATE LEFT MAIN LANDING GEAR ASSEMBLY OPEN
1.23 32-030-02 WBRICATE RIGHT MAIN LANDING GEAR ASSEMBLY OPEN
1.24 32-060-00 CLEAN NOSE LANDING GEAR SHOCK STRUT OPEN
1.25 32-070-00 SERVICE NOSE LANDING GEAR SHOCK STRUT OPEN
1.26 32-080-00 LUBRICATE NOSE LANDING GEAR ASSEMBLY OPEN
1.27 32-270-01 VISUAL CHECK LEFT BRAKE WEAR PINS FOR MINIMUM EXTENSION OPEN
1.28 32-270-02 VISUAL CHECK RIGHT BRAKE WEAR PINS FOR MINIMUM EXTENSION OPEN
1.29 32-800-00 EXTERNAL ZONAL INSPECTION (GV) NOSE LANDING GEAR AND LANDING GEAR DOORS (FROM GROUND) OPEN
PERFORM AN EXTERNAL ZONAL INSPECTION (GV) Of THE NOSE LANDING GEAR AND LANDING GEAR DOORS.
INSPECTION IS ACCOMPLISHED FROM THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. (EZAP)
1.30 32.804.01 EXTERNAL ZONAL INSPECTION (GV) LEFT MAIN LANDING GEAR AND LANDING GEAR DOORS (FROM GROUND) OPEN
PERFORM AN EXTERNAL ZONAL INSPECTION (GV) OF THE LEFT MAIN LANDING GEAR AND LANDING GEAR
DOORS. INSPECTION IS
ACCOMPLISHED FROM THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS
1.31 32.808.02 EXTERNAL ZONAL INSPECTION (GV) RIGHT MAIN LANDING GEAR AND LANDING GEAR DOORS (FROM GROUND) OPEN
PERFORM AN EXTERNAL ZONAL INSPECTION (GV) OF THE RIGHT MAIN LANDING GEAR AND LANDING GEAR
DOORS. INSPECTION IS
ACCOMPLISHED FROM THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS
26-MAY-2015 © CAMP SYSTEMS I of 3
EFTA_R1_02140497
EFTA02714502
CAMP
A^....P•••••••••••ey
Work Order Contents Report
SERIAL : 29273 (YG006) REGNO : VP-BB) MODEL NAME : 68) 737.700IGW/-800/-900ER WORK ORDER At: VP-B8) 2A CHECK 2015
DATE IN : UTC:15-Jun-2015 12:00 AM DATE OUT : UTC:26-Jun-2015 12:00 AM ICAO : SERVICE CENTER : JET AVIATION (GENEVE) S.A.
SORT ITEM NO DESCRIPTION STATUS
COMPLIANCE NEXT DUE TIME
REMAINING
1.32 33-010-00 OPERATIONAL CHECK EMERGENCY LIGHTS OPEN
1.33 53-800-00 EXTERNAL ZONAL INSPECTION (GV) OF THE LOWER FUSELAGE. THE NOSE LANDING GEAR WHEEL WELL AND OPEN
MAIN LANDING GEAR WHEEL WELL ARE ALSO INCLUDED. INSPECTION IS ACCOMPLISHED FROM THE GROUND,
WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRED (EZAP)
1.34 53.81200 INTERNAL ZONAL INSPECTION (GV) FORWARD CARGO COMPARTMENT - SECTION 43, STATION 396 TO OPEN
FORWARD CARGO COMPARTMENT AFT BULKHEAD
1.35 53-830-00 INTERNAL ZONAL INSPECTION (GV) AFT CARGO COMPARTMENT - SECTION 46 AND 47 (PART), STATION 727 OPEN
TO STATION 947.5
1.36 53.84400 EXTERNAL ZONAL INSPECTION (GV) OF THE WING TO BODY FAIRING. INSPECTION IS ACCOMPLISHED FROM OPEN
THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRE
1.37 53-894-00 EXTERNAL ZONAL INSPECTION (GV) OF 711E FUSELAGE. INSPECTION IS ACCOMPLISHED FROM THE GROUND, OPEN
WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRED
1.38 55-800-00 EXTERNAL ZONAL INSPECTION (GV) VERTICAL FIN AND HORIZONTAL STABILIZER. INSPECTION IS OPEN
ACCOMPLISHED FROM THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS
PANELS REQUIRED
1.39 57.802-01 EXTERNAL ZONAL INSPECTION (GV) LEFT WING INSPECTION IS ACCOMPLISHED FROM THE GROUND, WITHOUT OPEN
THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRED.
1.40 57-872-02 EXTERNAL ZONAL INSPECTION (GV) RIGHT WING INSPECTION IS ACCOMPLISHED FROM THE GROUND, OPEN
WITHOUT THE USE OF STANDS OR LADDERS. NO ADDITIONAL ACCESS PANELS REQUIRED.
1.41 70-803-01 EXTERNAL ZONAL INSPECTION (GV) NO. 1 ENGINE STRUT FAIRINGS. INSPECTION IS ACCOMPLISHED FROM OPEN
THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. NO
ADDITIONAL ACCESS PANELS REQUIRED.
1.42 70-810-02 EXTERNAL ZONAL INSPECTION (GV) NO. 2 ENGINE STRUT FAIRINGS INSPECTION IS ACCOMPLISHED FROM OPEN
THE GROUND, WITHOUT THE USE OF STANDS OR LADDERS. NO
ADDITIONAL ACCESS PANELS REQUIRED
1.43 52-150-00 LUBRICATE AIRSTAIR DOOR SYSTEM (INCLUDES TWO ROLLERS, CARRIAGE DRIVE BEARING, DRIVE NUT IN OPEN
JACK SCREW, LOCK PIN GREASE FITTING AND FOUR BEARINGS IN THE CARRIAGE ROLLERS).
1.44 26-450-00 INSPECT (DETAILED) THE PORTABLE HALON FIRE EXTINGUISHERS FOR PROPER PRESSURE (IF GAUGE OPEN
INSTALLED), WEIGHT AND CONDITION.
1.45 050010 A- I CHECK OPEN
1.46 257001 GENERAL VISUAL INSPECTION HEADLINER CEILING PANELS OPEN
1.47 257002 GENERAL VISUAL INSPECTION INTERIOR BULKHEADS OPEN
1.48 257003 GENERAL VISUAL INSPECTION COMPARTMENT DOORS OPEN
1.49 257004 GENERAL VISUAL INSPECTION SEATS ANDTABLES OPEN
1.50 257005 GENERAL VISUAL INSPECTION CLOSET AND CABINETS OPEN
1.51 257006 GENERAL VISUAL INSPECTION CLOSET AND CABINET DOORS OPEN
1.52 257007 GENERAL VISUAL INSPECTION BED AND DIVANS OPEN
1.53 257011 CHECK SAFETY BELTS OPEN
1.54 352002 GENERAL VISUAL INSPECTION CHEMICAL 02 MASK OPEN
1.55 381120 CHECK WATER/WASTE DRAIN LINES OPEN
1.56 385010 CLEAN WATER/WASTE INSIDE FILTER OPEN
1.57 57-950-01 EXTERNAL ZONAL INSPECTION OF THE LEFT WINGLET OPEN
1.58 57-952-01 INTERNAL ZONAL INSPECTION LEFT WINGLET OPEN
1.59 57-960-02 EXTERNAL ZONAL INSPECTION OF THE RIGHT WINGLET OPEN
26-MAY-2015 © CAMP SYSTEMS 2 of 3
EFTA_R1_02140498
EFTA02714503
CAMP
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Work Order Contents Report
SERIAL : 29273 (YG006) REGNO : VP-BB) MODEL NAME : 88) 737.700IGW/-800/-900ER WORK ORDER At: VP-88) 2A CHECK 2015
DATE IN : UTC:15-Jun-2015 12:00 AM DATE OUT : UTC:26-Jun-2015 12:00 AM ICAO : SERVICE CENTER : JET AVIATION (GENEVE) S.A.
SORT ITEM NO DESCRIPTION STATUS
COMPLIANCE NEXT DUE TIME
REMAINING
1.60 57-962-02 INTERNAL ZONAL INSPECTION OF THE RIGHT WINGLET OPEN
1.61 33-055-00 FUNCTIONAL CHECK THE EMERGENCY LIGHTING BATTERY PACKS FOR CAPACITY (15 MIN. MINIMUM) AND ONE OPEN
COMPLETE DEEP CYCLE.
1.62 72-020-01 DETAILED INSPECTION OF LEFT ENGINE INLET AND FAN BLADES. OPEN
1.63 72-020-02 DETAILED INSPECTION OF RIGHT ENGINE INLET AND FAN BLADES OPEN
Prepared By: Date:
Approved By: Date:
26-MAY-2015 © CAMP SYSTEMS 3 of 3
EFTA_R1_02140499
EFTA02714504
CAMP
A^....P••••••••••ey
Work Order Contents Report
SERIAL : 29273 (YG006) REGNO : VP-BEJ MODEL NAME : BB) 737.700IGW/-8001.900ER WORK ORDER At: VP-B8) DUE MX )UN. 2015
DATE IN : UTC:15-Jun-2015 12:00 AM DATE OUT : UTC:26-Jun-2015 12:00 AM ICAO : SERVICE CENTER : JET AVIATION (GENEVE) S.A.
SORT ITEM NO DESCRIPTION STATUS
COMPLIANCE NEXT DUE TIME
REMAINING
1.0 737-28A1206 R3 FUEL - DISTRIBUTION - CENTER FUEL TANK BOOST PUMP AUTO SHUTOFF AND MASTER CAUTION LOGIC OPEN
CHANGE, SERVICE BULLETIN
2.0 252501 VISUALLY CHECK FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE BOTTLE FOR PROPER OPEN
PRESSURE
3.0 252502 VISUALLY CHECK FORWARD SERVICE DOOR EMERGENCY ESCAPE SLIDE PRESSURE BOTTLE FOR PROPER OPEN
PRESSURE
4.0 252503 VISUALLY CHECK AFT ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE BOTTLE FOR PROPER PRESSURE OPEN
5.0 252504 VISUALLY CHECK AFT SERVICE DOOR EMERGENCY ESCAPE SLIDE PRESSURE BOTTLE FOR PROPER PRESSURE OPEN
6.0 FM 2005-18-23 CORROSION PROTECTION OF THE ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELL OPEN
7.0 FM 2006-21-01 PART 1 FLIGHT CONTROLS AILERON AND AILERON TRIM CONTROL SYSTEM MEASURE THE FREEPLAY OF BOTH OPEN
AILERON CONTROL BALANCE TABS
8.0 FM 2006-21-01 PART 2 FLIGHT CONTROLS - AILERON AND AILERON TRIM CONTROL SYSTEM - REPETATIVE LUBRICATION OPEN
9.0 FM 2011.27-03 PAM (6)(1)(1)(1) DETAILED INSPECTION TO PREVENT AN UNDETECTED FAILURE OF THE PRIMARY LOAD PATH FOR THE OPEN
BALLSCREW IN THE DRIVE MECHANISM OF THE HSTA AND SUBSEQUENT WEAR AND FAILURE OF THE
SECONDARY LOAD PATH IN ACCORDANCE WITH SERVICE BUITIN 737-27A1277 R2
10.0 29-230-03 OPERATIONAL CHECK STANDBY RUDDER SYSTEM TO INCLUDE OBSERVING LOW PRESSURE LIGHT OPEN
ILLUMINATION AND THEN EXTINGUISHING.
11.0 24-120-00 (001.1) RESTORE MAIN BATTERY OPEN
12.0 24-120-00(002.1) RESTORE AUXILIARY BATTERY OPEN
13.0 254206 LAERDAL HEARTSTART FR DEFIBRILLATOR PADS OPEN
14.0 081001 WEIGHT CHECK OF AIRCRAFT OPEN
15.0 252901 CAPTAIN LIFE JACKET OPEN
16.0 252902 FIRST OFFICER LIFE JACKET OPEN
17.0 252903 FIRST OBSERVER LIFE JACKET OPEN
18.0 252904 NO. 1 FORWARD FLIGHT ATTENDANT LIFE JACKET OPEN
19.0 252905 NO. 2 FORWARD FLIGHT ATTENDANT LIFE JACKET OPEN
20.0 252906 NO. 1 AFT FLIGHT ATTENDANT UFE JACKET OPEN
21.0 252907 NO. 2 AFT FLIGHT ATTENDANT LIFE JACKET OPEN
22.0 252909 SECOND OBSERVER LIFE JACKET OPEN
23.0 256323 (001.1) OPERATIONAL CHECK OF THE NO. 1 FORWARD EMERGENCY FLASHUGHT OPEN
24.0 256323 (002,1) OPERATIONAL CHECK OF THE NO. 2 FORWARD EMERGENCY FLASHUGHT OPEN
25.0 256323 (003.1) OPERATIONAL CHECK OF THE NO. 1 COCKPIT FLASHLIGHT OPEN
26.0 256323 (004.1) OPERATIONAL CHECK OF THE NO. 2 COCKPIT FLASHUGHT OPEN
27.0 256323 (005.1) OPERATIONAL CHECK OF THE NO. 1 AFT EMERGENCY FLASHUGHT OPEN
28.0 256325 (003.1) OPERATIONAL CHECK OF THE CARGO NET OPEN
29.0 347105 (1) BIANNUAL CHECK EGPWS TERRAIN DATABASE VERSION STATUS OPEN
30.0 33.06600 RESTORE EMERGENCY LIGHTING BATTERY PACK (TWO OR MORE COMPLETE DEEP CYCLES) BATTERY CAPACITY OPEN
TO REQUIRED STANDARD
31.0 25-310-00 (002.1) RESTORE NO. 2 LIFE RAFT PRESSURE BOTTLE OPEN
32.0 25-420-03 (001.1) RESTORE FORWARD FIRST AID KIT OPEN
33.0 25-420-00 (002.1) RESTORE AFT FIRST AID KIT OPEN
34.0 25-430-00 (001.1) RESTORE MEDAIRE - BLUE FIRST AID MEDICAL KIT OPEN
26-MAY-2015 © CAMP SYSTEMS 1 of 2
EFTA_R1_02140500
EFTA02714505
CAMP
A^....P••••der...4 .•
Work Order Contents Report
SERIAL : 29273 (YG006) REGNO : VP-BB) MODEL NAME : 88) 737.700IGW/-800/-900ER WORK ORDER At: VP-B8.1 DUE MX )UN. 2015
DATE IN : UTC:15-Jun-2015 12:00 AM DATE OUT : UTC:26-Jun-2015 12:00 AM ICAO : SERVICE CENTER : JET AVIATION (GENEVE) S.A.
SORT ITEM NO DESCRIPTION STATUS
COMPLIANCE NEXT DUE TIME
REMAINING
35.0 38-040-00 RESTORE WASTE DRAIN BALL VALVE THE WASTE DRAIN BALL-VALVE BY REPLACING SEALS (2) (OFF OPEN
AIRCRAFT)
36.0 FM 2015-04-02 NO. 1ENGINE - ENGINE FUEL AND CONTROL - MODIFY THE ENGINE BY REMOVING FULL AUTHORITY DIGITAL OPEN
ENGINE CONTROL (FADEC) SOFTWARE, VERSION 7.B.V4 OR EARUER, INSTALLED IN THE ELECTRONIC ENGINE
CONTROL (EEC)
37.0 FM 2015-04-02 NO. 2 ENGINE - ENGINE FUEL AND CONTROL - MODIFY THE ENGINE BY REMOVING FULL AUTHORITY DIGITAL OPEN
ENGINE CONTROL (FADEC) SOFTWARE, VERSION 7.B.V4 OR EARLIER, INSTALLED IN THE ELECTRONIC ENGINE
CONTROL (EEC)
38.0 25-300-00 (002.1) INSPECT AFT LIFE RAFT OPEN
39.0 25-300-00 (003.1) INSPECT NO. 3 LIFE RAFT OPEN
40.0 26-330-00 (002.1) REPLACE (LIID2) CARGO FIRE EXTINGUISHER BOTTLE AFT SQUIB OPEN
41.0 25-60-00 GENERAL VISUAL INSPECTION OF ALL COCKPIT / CABIN EMERGENCY EQUIPMENT OPEN
42.0 28-054-00 OPERATIONAL CHECK (BITE) THE FUEL PUMP GFI RELAY OPEN
43.0 28-056-00 FUNCTIONALLY CHECK THE CENTER TANK FUEL BOOST PUMP POWER FAILED ON PROTECTION SYSTEM OPEN
44.0 28-115-00 FUNCTIONALLY CHECK THE CENTER TANK BOOST PUMP AUTO SHUTOFF SYSTEM OPEN
45.0 28-AWL-19 REVIEW CENTER TANK FUEL BOOST PUMP AUTOMATIC SHUTOFF SYSTEM OPEN
46.0 28-AWL-20 REVIEW OVER-CURRENT AND ARCING PROTECTION ELECTRICAL DESIGN FEATURES OPERATION - BOOST PUMP OPEN
GROUND FAULT INTERRUPTER (CFI)
47.0 28-AWL-23 FUNCTIONALLY TEST CENTER TANK FUEL BOOST PUMP POWER FAILED ON PROTECTION SYSTEM. OPEN
48.0 737015 (I) ANNUAL CHECK OF EEC# I & EEC#2 SOFTWARE ENGINE FUEL AND CONTROL ECU SOFTWARE STATUS OPEN
49.0 FM 2011.27-03 PAM (G)(1XI)(2) LUBRICATE TO PREVENT AN UNDETECTED FAILURE OF THE PRIMARY LOAD PATH FOR THE 8A11FrREW IN THE OPEN
DRIVE MECHANISM OF THE HSTA AND SUBSEQUENT WEAR AND FAILURE OF THE SECONDARY LOAD PATH IN
ACCORDANCE SERVICE BULLETIN 737-27A1277 R2
50.0 347101 UPDATE NAV DATABASE OPEN
Prepared By: Date:
Approved By: Date:
26-MAY-2015 © CAMP SYSTEMS 2 of 2
EFTA_R1_02140501
EFTA02714506