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Engine P/N Serial # ID # Cycles Operating Hours Overhaul Install Date

#1 CFM56-7B27/B3 893772 AXC772 3670 4608.0 9-Mar-06 1-Mar-07

#2 CFM56-7B27/B3 892796 AXC796 3670 4608.0 9-Mar-06 1-Mar-07

APU P/N S/N Cycles Hours

3800702-1 00000P7101 392.9 4454

Landing Gear S/N Hours

RT 161A1100-40 03884Y1908 2461.7

LT 161A1100-39 03883Y1908 2461.7

N 162A1100-9 01061Y1908 2461.7

#1 CFM56-7B27/B3 892998 AXC998 3716 3885.0 9-Mar-06 5-Jul-07

#2 CFM56-7B27/B3 892999 AXC999 3716 3885.0 9-Mar-06 5-Jul-07

3800702-1 00000P5769 333.2 12567.5

RT 161A1100-40 04094Y2008 2269.7

LT 161A1100-39 04093Y2008 2269.7

N 162A1100-9 01166Y2008 2269.7

#1 CFM56-7B27/B3 894376 QXC476 3384 4011.7 9-Mar-06 25-Apr-07

#2 CFM56-7B27/B3 894377 QXC377 3384 4011.7 9-Mar-06 25-Apr-07

3800702-1 00000P7347 391.2 4043.5

RT 161A1100-40 04370Y2141 2432.1

LT 161A1100-39 04369Y2141 2432.1

N 162A1100-9 01302Y2141 2432.1

#1 CFM56-7B27/B3 805640 AXX640 1306 1139.2 30-Nov-10 20-Nov-11

#2 CFM56-7B27/B3 804652 AXX652 1306 1139.2 29-Nov-10 20-Nov-11

3800702-1 00000P8812 158.4 1181.3

RT 161A1100-40 072B0Y3512 1119.8

LT 161A1100-39 07279y3512 1119.8

N 162A1100-9 02739Y3512 1119.8

09-0540

05-0730

05-0932

05-4613

Scott AFB C-40C Component Information

PAGE OF1 PAGES3

20121024

DATE

AIRCRAFT/MISSILE CONDITION DATA

DynCorp ASD/MDS 1280 Arnold Avenue Andrews AFB, MD

BOCK, JASON J., 89 MXG/CD

1. USING ACTIVITY ADDRESS MAINTENANCE OFFICER

TYPE/PRINT NAME

SIGNATURE

PART

A LTC

GRADE

DSN 858-2442

PHONE

BOCK.JASON.J.1136962520

C-32A

2. MDS

98-0001

3. SERIAL NUMBER 4. SUB SERIAL NO.

2013-03-15

5. SCHEDULED 7. HRS/MONTHS SINCE LAST PDM 8. HRS/MONTHS SINCE NEW

HQ AMC/A4MK

401 Scott Dr.

Scott AFB, IL 62225-5001

1. USING ACTIVITY ADDRESS

B

George Azimi

GS-12

DSN 334-7118

AZIMI.GEORGE.M.1180884510, george.azimi@us.af.mil

DATE PDM ACTIVITY ACCCEPTED ADDITIONAL WORK

AFTO FORM 103, 20070917 PREVIOUS EDITION IS OBSOLETE

DATE COPY OF COMPLETED FORM TO MAJCOMDATE COPY OF COMPLETED FROM TO USING ACTIVITY

INSTRUCTIONS: SEE T.O. 00-25-4

20121026

SYSTEM PROGRAM MANAGER

Richard Holden

MSgt

DSN 779-2729

HOLDEN.RICHARD.J.1087307677, richard.holden@us.af.mil

20121025

MAJCOM OPR

AFLCMC/WLVVC

3001 Staff Drive Tinker AFB, OK 73145-3020

SPM ADDRESS

C

1. Accomplish 85A Checks and 7C Check

2. AD 2010-15-01 (757-03-0019 R1, R2) Repetitive Inspections For Damage Of The Electrical Terminal at the Left and Right Fightdeck Window 1 and Corrective Actions – Perform Revision 2, Terminating Action (LH Window only)

3. 757-24-0132 - ELECTRICAL POWER - Batteries - Change to the Battery Charger System Wiring for Extended Flight on Limited Standby Power

4. 757-27A0152 R1, IN01 - FLIGHT CONTROLS - Spoiler, Drag Devices and Variable Aerodynamic Fairings - New Spoiler Control Module Relay Installation **Boeing recommends incorporating R2.**

5. 757-28A0081 R1, R2, IN02 - FUEL - Engine Fuel Feed System - Center Fuel Tank Fuel Boost Pumps - Automatic Shut Off System Installation **Concurrent Requirements: Ref:#15 757-28A0105 R3**

6. 757-28-0112 R1 IN01 - FUEL - Fuel Quantity Indicating System (FQIS) - Out-Of-Tank Lightning Shield Bond Path Resistance Inspection and Repair

LIST THOSE DEFECTS WHICH ARE KNOWN OR THOUGHT TO BE BEYOND USING ACTIVITY CAPABILITY BUT NOT IN THE DEPOT WORK PACKAGE

LIST THE TASKS FROM PART B WHICH ARE APPROVED BY THE SPM

CONTINUATION PAGE

PAGE PAGESOF2 3

///////////////////////////////////////////////////////////////////////////// CONTINUED/////////////////////////////////////////////////////////////////////////////

7. 757-32-0177 IN01 - LANDING GEAR - Wheels and Brakes - Main Gear Anti-Skid System Electrical Flex Conduits and Bracket Replacement

8. 757-49-0022 - AIRBORNE AUXILIARY POWER - APU Surge Bleed System - Change to the Environmental Control System Signal Interface with the Auxiliary Power Unit

9. 757-78-0049 R1 - EXHAUST - Thrust Reverser System - Replacement of Anti-Rotation Clips with Bolts and Lock Wire on the Blocker Doors of the Thrust Reverser

10. 757-SL-21-063 - 757 ORIFICE AND RESTRICTOR PLATE LOCATIONS FOR OVERHEAD DISTRIBUTION NOZZLE AND

SIDEWALL OUTLETS

11. 757-53A0093 - FUSELAGE - Section 46 - Structure - Doorway Number 4 - Aft Frame Body Station 1681.8 Left and Right Side - Doorstop to Intercostal Tee Clips - Inspection and Replacement

12. 757-28-0095 R1- FUEL - Engine Fuel Feed System - Fuel Boost Pump Wire Changes

13. 757-57A0064 R1 - WINGS - Center and Outer Wing - Fastener Sealing and Wire Bundle Support Inspection and Modification

14. 757-28A0085 R3 - FUEL - Indicating - Hot Short Protector Installation for FQIS Fuel Densitometer

15. 757-28A0105 R3 - FUEL - Engine Fuel Feed System - Center Fuel Tank, Fuel Pumps - Power Failed ON Protection System (Un-commanded Pump ON) - Relays Installation **Concurrent Requirements: SB 757-28A0081 (R2 completed, inspect wire route per R3)**

16. AD2011-01-15 Crown Skin Panel – Station 297 to Station 439, Chem-Milled Step Above Stringer 4 Left and Stringer 4 Right Lap Joint - Inspection

17. AD2012-02-17 Cracks found in the front spar lower chord at the fastener locations common to the side link support fitting at wing station (WS) 292

18. SIL-03-02 Availability of Inconel 625 Bleed Air Leak Detection Elements

19. Inspection of Main Deck Accessible Floorboards (Pending SL and TCTO) **C32A-SL-187 Fuselage– Cabin Floor Panel Detailed Inspection**

20. 757-28A0131 Fuel- Engine Fuel feed System-Engine Fuel Suction Feed Operational Test

21. 757-34-0487 Navigation- Ground Proximity Warning System- Enhanced Ground Proximity Warning System Altitude Callouts Change

////////////////////////////////////////////////////// OTHER ACTIVITIES/////////////////////////////////////////////////////////////////////////////////////////// Permanent Repair – Dent in Fuselage Skin At STA 438 Between S-18L and S-19L (SR 1-1973250461)

FLIGHT DECK

Laminate on aft walls have several gouges Stainless steel strip behind right jump seat is scratched + gouged

FORWARD GALLEY

Feature strips above 1L + 1R needs adjusting and glue Laminate on left side of forward countertop has a dent Several scratches on laminate around potable water gauge Stainless steel strip above door 119 requires replacement Emergency assist bottle access door has several gouges Seal above microwave loose and discolored Laminate in between curtain + flight deck door requires replacement

FORWARD LAVATORY

Heater access door has gouges (recover)

DSO/CSO

Seal around DSO station “yellowed” and loose

MID GALLEY

Stains on the laminate by air stair lock access door Seals around both entry doors dirty and gouged Laminate on left sidewall by air stairs is gouged 3 rectangular panels above 2R door requires paint Vertical wall seal between flight attendant seats requires paint Touch-up door 2L & 2R door jams (may be accomplished during paint effort)

HALLWAY

2nd + 5th windows scratched

CONFERENCE ROOM

Gouge in aft right most sidewall panel (currently touched-up, replace in refurbishment)

AIRCRAFT

AIRCRAFT/MISSILE CONDITION DATA (CONTINUATION)

AFTO FORM 103, 20070917

PAGE PAGESOF3 3

////////////////////////////////////////////////////// OTHER ACTIVITIES CONTINUED///////////////////////////////////////////////////////////////////////

AFT LAVATORY’S

Replace seals above right and left lavatory (loose & discolored)

AFT PASSENGER AREA

Laminate under coffee maker is stained Replace reveal shade of forward left window (dented + gouged)

AFT GALLEY

Replace wall closeout seal (yellowed + stained)

THROUGHOUT AIRCRAFT

Replace all foam fillers Repair/Replace all plastic trim fillers Replace carpet Replace any yellowed light lenses Replace any damaged seat track covers Clean all Tambour door tracks (binding) Recover/repair any damaged ceiling panels Replace all seals around all entry doors Replace any damaged feature strips between sidewalls Replace/repair any damaged wall coverings

///////////////////////////////////////////////////////////781K ITEMS////////////////////////////////////////////////////////////////////////////////////////////////// 082680110 FWD Cargo Comp Barrier Floor Mount LH Aft side B/N/P 100210057 Corrosion on Cabinet Structure Beneath FWD Galley Sink

20121126

ISENHOUR, WALTER, 89 MXG/CC

A Col

ISENHOUR.WALTER.L.1083007962

C-32A

98-0002

2013-04-24

CIV

DSN 884-7118

AZIMI.GEORGE.M.1180884510, george.azimi@us.af.mil

20121211

HOLDEN.RICHARD.J.1087307677, richard.holden@us.af.mil

20121210

OC-ALC/GKSVD

1. Accomplish 7C Check and #84 A Check requirements

2. Re-inspect and re-evaluate the corrosion in the G4B galley adjacent to galley pan

3. Re-inspect and re-evaluate the corrosion in the G1A galley adjacent to galley pan

4. AD 2010-15-01 (757-30-0019 R2) Repetitive Inspections For Damage Of The Electrical Terminal At The Left And Right Flightdeck Window 1 And Corrective Actions (Perform Revision 2, Terminating Action, Rt window PCW)

5. AD 2012-02-17 (757-57-0065 R1) Cracks Found In The Front Spar Lower Chord At The Fastener Locations Common To The Side Link Support Fitting At Wing Station (WS) 292 - Inspection

6. 757-24-0123 Change to the Battery Charger System Wiring for Extended Flight on Limited Standby Power

7. 757-27A0152 R1, R2 IN01 New Spoiler Control Module Relay Installation

8. 757-28A0131 Engine Fuel Suction Feed Operational Test

9. 757-28A0081 R2, IN01 Center Fuel Tank Fuel Boost Pumps – Automatic Shut Off System Installation (Perform Revision 2)

LIST THOSE DEFECTS WHICH ARE KNOWN OR THOUGHT TO BE BEYOND USING ACTIVITY CAPABILITY BUT NOT IN THE DEPOT WORK PACKAGE

10. 757-28-0112 R2 IN01 Fuel Quantity Indicating System (FQIS) – Out-Of-Tank Lightning Shield Bond Path Resistance Inspection and Repair

11. 757-32-0177 IN01 Main Gear Anti-Skid System Electrical Flex Conduits And Bracket Replacement

12. 757-49-0022 APU Surge Bleed System - Change to the Environmental Control System Signal Interface with the Auxiliary Power Unit

13. 757-78-0049 R1 Thrust Reverser System - Replacement of Anti-Rotation Clips with Bolts and Lock Wire on the Blocker Doors of the Thrust Reverser

14. 757-SL-21-063 757 Orifice and Restrictor Plate Locations for Overhead Distribution Nozzle and Sidewall Outlets

15. DELETED (PCW)

16. 757-28-0095 R3 Fuel Boost Pump Wire Changes

17. AD 2011-01-15 (SB 757-53-0097) Crown Skin Panel - Station 297 to Station 439, Chem-Milled Step Above Stringer 4 Left and Stringer 4 Right Lap Joint - Inspection

18. DELETED (duplicate item)

19. 757-28A0105 R3 Power failed ON protection system relay installation (verify colors)

20. 757-54-0033 R1 Nacells/Pylons - Fan Cowl Support Beam - Fireseal Replacement (If engine removed)

21. C32A-SL-187 Fuselage - Cabin Floor Panel Detailed Inspection

//////////////////////////////////////////////////////////////AIRCRAFT CHANGES/////////////////////////////////////////////////////////////////////////////////// AC1309-Legacy GWOT Comm Upgrade (OCO) BC1260 - C-32A DMS Changes (8-Wire Ethernet Cable, Reference Wire Kit 728-11366) ///////////////////////////////////////////////////////OTHER ACTIVITIES///////////////////////////////////////////////////////////////////////////////////////////// Weigh Acft Interior Refresh Items (TBD)

122055289 CARPET AREA IN FRONT OF PRINTER IS STAINED (CARPET CHANGE)

122390027 FL-12239-0001 #1 GALLEY STOWAGE UNIT TAMBOUR DOOR IS DE-LAMINATED (R.H.FWD) 121300041 FL-12130-0004 FWD CLOSET AFT OF FWD GALLEY BOTTOM LATCH ON CARGO NET BROKEN 122625315 STAIN ON FLOOR FWD OF FLIGHT ATTENDANT SEAT NEXT TO 2L (Replace Gerflor doors 1, 2 and 3)

/////////////////////////////////////////////////////////////////////////781K Items/////////////////////////////////////////////////////////////////////////////////////// 121460038 FL-12146-0002 RH ENG CORE COWL CENTER BOLT INBOARD SIDE NEEDS REPLACEMENT (POH)

122010022 PLENUM FOR DOOR #4 AVIONICS EQUIP CLOSET (FWD OF DSO STATION) IS NOT FLUSH WITH CLOSET

DOOR WHEN CLOSED, CAUSING RECIR FAN FAULTS. (HOLD FOR RESEARCH).

122640164 FL12264-0014 E/E DOOR LADDER TEFLON FWD WORN. NOTE: IF FWD LOCK LATCH IS NOT LOCKED, BOTH LADDER OPERATING SWITCHES MAY NOT WORK, DUE TO UPPER MICROSWITCH NOT MAKING CONTACT.

20131114 1 2

89 MXG

1280 Arnold Ave

LAWRENCE HAVIRD

C-32A 99-0003 NP903

2014-03-17

HQ AMC/A4MK, 401 SCOTT DR, SCORR AFB, IL 62225-5001

Accomplish 7C Check and 84 A Check 105886, 757-27A0152, New Spoiler Control Module Relay Installation 105892, 757-57-0065, Front Wing Spar Lower Chord at WS 292 Pylon Side link Fitting – Inspection 105910, 757-28A0081 R1, R2, Center Fuel Tank Fuel Boost Pumps - Automatic Shut Off System Installation 105927, 757-28A0081 R1 IN02 Center Fuel Tank Fuel Boost Pumps Automatic Shut Off System Installation 105935, 757-27A0152 R1 (see 105886) New Spoiler Control Module Relay Installation 107290 AD 2011-01-15 (757-053-0097 R1 ) Fuselage - Skin - Crown Skin Panel - Station 297 to Station 439, Chem-Milled Step Above Stringer 4 Left and Stringer 4 Right Lap Joint – Inspection per Option B

RICKY R.BROWN

3001 STAFF DRIVE, TINKER AFB, OK 73145-3020

PAGE OF PAGESAIRCRAFT/MISSILE CONDITION DATA

MAINTENANCE OFFICER

NAME

A

2. MDS 3. SERIAL NUMBER 4. SUB SERIAL NO.

5. SCHEDULED INPUT DATE 7. HRS/MONTHS SINCE LAST PDM 8. HRS/MONTHS SINCE NEW

MAJCOM OPR ADDRESS

LIST THOSE DEFECTS WHICH ARE KNOWN OR THOUGHT TO BE BEYOND USING ACTIVITY CAPABILITY BUT NOT IN THE DEPOT WORK SPEC

DATE/SIGN WHEN PDM ACTIVITY ACCEPTED ADDITIONAL WORK

DATE COPY OF COMPLETED FORM TO MAJCOM

DATE COPY OF COMPLETED FORM TO USING ACTIVITY

AFTO FORM 103, 20130620 PREVIOUS EDITION IS OBSOLETE

0-6/Col

E-9/CMSGT

DSN 779-2133

SIGNATURE DATE

GS12

405-736-4970

HAVIRD.LAWRENCE.B.1050071843

BROWN.RICKY.R.1116289152, ricky.brown@us.af.mil 20131115

AZIMI.GEORGE.M.1180884510 20131120

Click to sign

2 2

C-32A 99-0003 NP903

110363, 757-78-0049 R1, Replacement of Anti-Rotation Clips with Bolts and Lock wire on Blocker Doors 0110376, 757-24-0132 R1 , Change to battery charger wiring for extended flight on limited standby power 0115374, 757-28A0081 R2, Center Fuel Tank Boost Pump Auto Shutoff System Installation 0115375, 757-57A0062 R1, Relocation of Rib Air Dam from WS 388 to WS 357 0115549, 757-49-0022, Change to ECS wiring signal interface 0115548, 757-28A0105 R3, CTR Fuel Tank Pump Relay Inst Power Failed on Protection for Group 2, Configuration 3 aircraft (Reference AMOC Letter Number 757-28A0105-AMOC-02) 0115056, 757-SL-21-063, Orifice and restrictor Plate for Overhead Distro Nozzle and Sidewall Outlets 0133085, 1C-32A-WA-1-535, AD 2012-02-17, (757-57-0065 R1) Cracks Found In the Front Spar Lower Chord at the Fastener Locations Common to the Side Link Support Fitting At Wing Station (WS) 292 133076, 1C-23A-WA-1-533, 757-28A0131, Engine Fuel Suction Feed Operational Test 103377, 1C-32A-WA-1-538, 757-27A0152 R2, New Spoiler Control Module Relay Installation for Group 2, Configuration 1 aircraft 0103389, 1C-32A-WA-1-545 , C32A-SL-188-A, Bleed Air Leak Detection System-Sensing Elements-Removal and Replacement of Inconel Sensors (Terminating Action-Part 2) 0109599, 1C-32A-WA-1-552 757-53-0094 R1, Number 1 Left Passenger Door Cutout -Upper Forward Corner - Skin and Bear Strap Preventive Modification 0103382, 1C-32A-WA-1-542, C32A-SL-187, Fuselage - Cabin Floor Panel Detailed Inspection 0103408, 1C-32A-WA-1-549, 757-24-0137 R0 and R1, STBY Power Failure Detection Circuit Change

JCN 130520162, #1 ENG PYLON ACCESS PANEL FWD HINGE LOOSE

JCN 130450132, FUEL LK FROM LT MAIN TANK AROUND #2 FIXED FAIRING AND FLAP TRACK FWD MOUNT (classified as a seep IAW 28-11-00-206-001 Fig 602) /////////////////////////////////////////////////////////////////////Other Activities///////////////////////////////////////////////////////////////////////////////////// Weigh Acft Interior Refresh Items (TBD) Replace Carpet throughout Acft Re-inspect and re-evaluate the corrosion in the G4B galley adjacent to galley pan Re-inspect and re-evaluate the corrosion in the G1A galley adjacent to galley pan

PAGE OF PAGESAIRCRAFT/MISSILE CONDITION DATA CONTINUED

LIST THOSE DEFECTS WHICH ARE KNOWN OR THOUGHT TO BE BEYOND USING ACTIVITY CAPABILITY BUT NOT IN THE DEPOT WORK SPEC

PART B CONTINUATION

AFTO FORM 103, 20130620

PART C CONTINUATION

20120426

ISENHOUR, WALTER, 89 MXG/CC

A Col

ISENHOUR.WALTER.L.1083007962, walter.isenhour@us.af.mil

C-40B

01-0040

2012-08-27

Angela Burris

DSN 336-7167

CLICK HERE TO SIGN

CLICK HERE TO SIGN

1. Accomplish 4C Check, #51 and #52 A-Check items

2. Engine Inlet Acoustic Panel(s) Replacement Re-evaluation (781K Item)

3. AD 2005-24-03 R1 (737-57-1275 R3), To Prevent Inadequate Fastener Clamp-up, Which Could Result in Cracking of the Fastener Holes

4. 737-21A1139 R1, Air Conditioning-Distribution-Overhead Distribution Duct-Installations and Tapes or the Overhead Ducts and Plenums

5. 737-21-1177, Air Conditioning - Pressurization Control System - Change of the Power Source to the Pressurization System Circuit Breaker

6. 737-24-1176 R3, Re-Pin Wires at Two Wing-To-Strut Electrical Connectors at Each Engine Strut Bracket

7. 737-27A1299 IN01& IN02, Elevator Tab Control Mechanism Detailed Inspection and Bearing Retainer Installation

8. 737-28-1172 R1, Alignment Of Center Tank Boost Pump Inlets and Fuel Pump Alignment Bracketry

LIST THOSE DEFECTS WHICH ARE KNOWN OR THOUGHT TO BE BEYOND USING ACTIVITY CAPABILITY BUT NOT IN THE DEPOT WORK PACKAGE

9. 737-30-1056 R3, Gray Water Composite Drain Mast Bonding Jumper Installation (Part 4 only )

10. 737-32-1448 IN01, Main Landing Gear - Forward and Aft Trunnion Pin Assemblies Inspection and Change (Gear Overhaul)

11. 737-32-1369 R4, Main Landing Gear Extension and Retraction - Retract Actuator Cylinder Assembly Modification Or Replacement (Gear Overhaul)

12. 737-33-1130 R1 IN01,IN02,IN03,IN04, Passenger Compartment Lights-Replace the 115 VAC ATM Connectors

13. 737-36-1021, R1, R2, Change to the Aircraft Condition Monitoring System to Give More Inputs to the Digital Flight Data Acquisition Unit for Easier Environmental Control System Troubleshooting

14. 737-53-1276 IN01 IN02, Forward and Aft Cargo Compartment - Corrosion Prevention Modification

15. 737-53-1277 R1, IN02, Nose Wheel Well Retract Actuator Support Fitting Inspection and Modification

16. 737-53-1282 R1 IN03, Nose Wheel Upper Drag Brace and Trunnion Bushing Replacement (Gear Overhaul)

17. 737-53-1294, Lower Bulkhead Chords at Body Station 540 - Skin Inspection, Chord Splice Installation and Skin Repair

18. 737-53-1296, Passenger Cabin Floors - Station 727B Splice Strap Installation 19, 737-53-1298, Dorsal Fin Seal Retainer And Fuselage Skin Station 847 To 1007 (Insp)

20. 737-57-1268 R1 IN01, Lower Wing Skin Panels - Installation of the Rub Strips

21. 737-57-1284 IN01 IN02, Inspection, Repair / Modification - Wing Buttock Line 147 to Wing Buttock Line 201

22. 737-57-1288 R1 IN01 IN02, Number 3 and Number 6 Tailcone Assemblies - Inspection and Repair

23. 737-57-1293, R1 IN02, IN03, Leading Edge and Leading Edge Devices - Fuel Drain Path Modification

24. 737-57-1310, IN01, IN02 Forward Trunnion Support Fitting - Fuse Pin Bores - Inspection For Corrosion (Gear Overhaul)

25. 737-71-1608, Inspection and Repair of the Engine Build Up Brackets To Prevent Damage to the Engine Fan Case

26. 737-71-1682, Power Plant - B1 Flange Inspection

27. DELETED

28. 737-78-1077, Installation Of Lightning Strike Protection On The Thrust Reverser

29. 737-78-1079 R2, (Concurrent with 737-78-1085), Reverser Inner Wall Inspection, Repair, and Cooling Hole Modification

30. 737-78-1085, Change to the Insulation Blankets on the Thrust Reversers

31. 737-78-1086, Inspection of the Fire Seal and Installation of a New Fire Seal Bracket on the Thrust Reverser

32. 737-SL-28-060-B, Short Screws Installed on Engine Fuel Shutoff Valves, Crossfeed Valve and Defuel Valve

33. 737-SL-28-062-B, Possible miss-location of fuel tank vent tube climb port

34. 737-SL-32-168, Potentially Incorrect Main Landing Gear Axle Installation (Gear Overhaul)

35. 737-57-1309, Front Spar Shear Pin Inspection, Repair and Preventitive Maintenance

36. 737-SL-32-169, Potentially Incorrect Main Landing Gear Lower Torsion Link Installation (Gear Overhaul)

37. 737-SL-33-053-C, Anti-Collision Light Power Supply & Bracket - Faying Seal Application

38. 737-SL-53-064, Missing Fasteners Common To BS 360 Shear Tie Between Stringer 14R and Stringer 15R

39. 737-SL-53-079, Bolts Installed With Gaps, Missing Washers, And Incorrect Nuts At BS 727 At S-19R And S-19L

40. 737-SL-53-080, Possible Damaged Hi-Loks In Main Entry Door Upper Sill At BS303.90

41. 737-SL-53-083-A, Possible Gap Common To The Body Station 203 Waterline 234 Inner Chord Splice Structure

42. 737-SL-57-093, Spar Corrosion Common To Main Fuel Tank Boost Pump Bonding Jumpers

43. 05027-B, Installation of Trim Cover on Affected Seats

44. CFMI 72-825, On Wing Inspection of Pre-CFM56-7B S/B 72-0811 Actuation Compressor Stator Inlet Guide Vane Ring Assemblies

45. 737-53-1303, #3 Window Frame Inspection and Freeze Plug

46. 737-26-1131 R1, Duct Leak Overheat Support Installation

47. DELETED

48. 737-55-1090, Stab Rear Spar Termination Fitting Inspection

49. 737-SL-53-093, Lwr Airstair Sill Gapping on Acft With and Without Airstairs

50. DELETED

51. 737-21-1174, Replacement of Pack Link Arm

52. 737-27-1290 R2, Flap Limit Switch And Flap Landing Warning Switch Replacement

53. DELETED / DEFERRED

54. DELETED / DEFERRED

55. DELETED / DEFERRED

56. DELETED / DEFERRED

57. BBJ-25-34, Removal Of Cargo Compartment Lower Bilge Insulation Blankets

58. 737-78-1083, Inspection and Change to or Replacement of the Thrust Reverser Actuator Attach Fitting And Actuator Rod Ends

59. DELETED / DEFERRED (on hold)

60. DELETED / DEFERRED

SERVICE ACTIONS CONT.

61. 737-27-1291, Leading Edge Slats – Titanium Proximity Sensor Provisional Installation

62. 737-32-1422 R1, Control System Aft Control Quadrant Clearance Measurement and Replacement

63. DELETED

64. DELETED

65. 737-56-1025, Flight Deck Number 2 Window Pane - Replacement

66. DELETED

67. DELETED DUPLICATE

68. DELETED

69. CFMI 72-728 R2, Fuel Nozzle Induced Stages 1, 2, And 3 LPT Nozzle Distress

70. CFMI 72-454R1, R2 Improvement of the Fan and Booster Vane Assy to Prevent the Corrosion in Field Only

71. AD 2009-01-02, (737-25-1544 R1)Attachment Holes of the Support Bracket of the Air Conditioning Outlet Extrusion

72. 737-53-1244 R5, Station 520 to 540 Pivot Link Assembly Repair/Replace

73. 737-SL-32-176 Potentially Incorrect MLG Upper Torsion Link Pin Installation (concurrent with gear change)

74. 737-SL-32-131-B Main landing gear retract actuator – Loose locknut & broken safety wire

75. 737-28A1206 FUEL - Distribution - Center Fuel Tank Boost Pump Auto Shutoff and Master Caution Logic Change - No cost to restore wiring

76. 737-28A1248 FUEL - Engine Fuel Feed System - Center Fuel Tank, Fuel Pumps - Power Failed ON Protection System (Un -commanded Pump ON) - Relays Installation

77. 737-32-1443 LANDING GEAR - Extension and Retraction - Manual Extension Control Mechanism Access Door Switch Replacement

78. 737-30A1063 Ice and Rain Protection- Pitot and Static- Air Data Probe Anti-Icing System- Air Data Probe Heat Automation Installation

79. 737-25-1602 Automatic Overwing Exit Door Surround Structure –Change Upper and Lower door Sill

80. Perform Gear Exchange ///////////////////////////////////////////////////////////////////////////781K Items//////////////////////////////////////////////////////////////////////////////////////

1. A120470082 When adjusting the rudder pedals to full forward position, ensure to turn hand crank back one-half turn to prevent binding

20130917 1 4

201AS

1234 Menoher Dr.

Joint Base Andrews, MD 20762

Michael E. Teigen, DCANG

C-40C 02-0201 N/A

2014-03-10 1069.3 7889.9

NGB/A4MY

3500 Fetchet Avenue, Andrews AFB, MD 20762-5157

1. 737-26-1131 R1 IN01 Fire Protection - Duct Leak Overheat Detector Support Installation

- Work concurrently with C40C-SL-069-A

2. 737-27-1290 R4 1C-40-WA-1-517D: Flap Limit Switch and Flap Landing Warning Switch Replacement

3. 737-27-1291 R1 IN04 Leading Edge Slats Titanium Proximity Sensor Provisional Installation

4. 737-28A1206 R2 IN05 Center Fuel Tank Boost Pump Auto Shutoff and Master Caution Logic Change

5. 737-28-1209 R1 0103396 1C-40-WA-1-539: Wing Center Tank Wire Bundles Installation Change

6. 737-28A1248 R2 Center Fuel Tank, Fuel Pumps - Power Failed ON Protection (Un-commanded Pump ON) **************************************CONTINUED ON PAGE 2 ***************************************

Michael Schaefferkoetter

AFLCMC/WLVVC

3001 Staff Dr., Tinker AFB, OK 73145

All the actions identified on this document have been coordinated with the unit and the MAJCOM and are approved for work.

PAGE OF PAGESAIRCRAFT/MISSILE CONDITION DATA

MAINTENANCE OFFICER

A

5. SCHEDULED INPUT DATE 7. HRS/MONTHS SINCE LAST PDM 8. HRS/MONTHS SINCE NEW

MAJCOM OPR ADDRESS

LIST THOSE DEFECTS WHICH ARE KNOWN OR THOUGHT TO BE BEYOND USING ACTIVITY CAPABILITY BUT NOT IN THE DEPOT WORK SPEC

DATE/SIGN WHEN PDM ACTIVITY ACCEPTED ADDITIONAL WORK

DATE COPY OF COMPLETED FORM TO MAJCOM

DATE COPY OF COMPLETED FORM TO USING ACTIVITY

AFTO FORM 103, 20130620 PREVIOUS EDITION IS OBSOLETE

Lt. Col

240-857-6935

CTR

240-612-8491

Marcia Babin

GS12

405.736.4973

TEIGEN.MICHAEL.ERIK.1128020566

SCHAEFFERKOETTER.MICHAEL.LOUIS.1143254689 20131021

BABIN.MARCIA.L.1256605038, marcia.babin@us.af.mil 20131021

Click to sign

2 4

7. 737-32-1393 Main Gear Doors - Walking Beam and Retract Actuator Clevis Bushing Replacement

8. 737-32-1422 Control System Aft Control Quadrant Clearance Measurement and Replacement

9. 737-32-1443 IN01 0133054 1C-40-WA-1-515: Manual Extension Control Mechanism Access Door Switch Replace.

10. 737-33-1146 R1 0133065 1C-40-WA-1-520: Lightning Protection of the Tail Strobe Light system wiring

11. 737-36-1021 R2 0115364 Change the Aircraft Condition Monitoring System to Give More Inputs DFDAU & EECS

12. 737-52-1169 Inboard Main Landing Gear - Inspection and Repair

13. 737-53-1244 R5 0193816 Station 520 To 540 - Pivot Link Assembly Repair/Replace

14. 737-53-1294 0119295 Body Station 540 - Skin Inspection, Chord Splice Installation and Skin Repair

15. 737-53-1296 0110364 Station 727B Splice Strap Installation

16. 737-53-1298 Dorsal Fin Seal Retainer and Fuselage Skin Station 847 to 1007 – Inspection

17. 737-53-1307 0133095 1C-40-WA-1-531C: Panel 194E & Panel 193D - Inspect & Rework

18. 737-54-1049 0103401 1C-40-WA-1-541: Strut Seal Plane Access Panels Leak Inspection

19. 737-71-1682 R2 0219558 2J-F56-WA-1-504: B1 Flange Inspection

20. 737-78-1083 R1 0110371 Inspect and Change or Replace of the TR Actuator Attach Fitting and Actuator Rod Ends

21. 737-78-1085 R1: 0103386 1C-40-WA-1-535: Change to the Insulation Blankets on the Thrust Reversers

22. 737-78-1086 R1 0110369 Inspect. of the Fire Seal and Installation of a New Fire Seal Bracket on the Thrust Reverser

23. 737-SL-27-234 R1 0103400 Flap Position Switch Corosion Protection

24. 737-SL-32-168 Potentially Incorrect Main Landing Gear Axle Installation

25. 737-SL-32-169 Potentially Incorrect Main Landing Gear Lower Torsion Link Installation

26. 737-SL-33-053-C Anti-Collision Light Power Supply & Bracket – Faying Seal Application

27. 737-SL-53-083-B Possible Gap Common To The Body Station 203 Waterline 234 Inner Chord Splice

28. 737-SL-53-088 Possible Missing Stiffener in Transverse Floor Beam at BS 344, RBL 54.

29. 737-SL-53-093 0119301 Lower Airstair Sill Installation Gapping on Aircraft with airstairs and without Airstairs

30. 737-SL-57-102 0103407 1C-40-WA-1-544: MLG Forward Trunnion Fitting Bearing Retaining Nut Inspection

31. AD 2012-23-08, 737-54-1043 R2 IN05: 0133074 1C-40-WA-1-525C: Aft Fairing Drain Tube Assembly Replacement

**************************************CONTINUED ON PAGE 3***************************************

LIST THOSE DEFECTS WHICH ARE KNOWN OR THOUGHT TO BE BEYOND USING ACTIVITY CAPABILITY BUT NOT IN THE DEPOT WORK SPEC

3 4

32. AD 2012-24-08, 737-30A1063 R1 IN01 0133052 1C-40-WA-1-513C: Air Data Probe Heat Automation Installation

- Work concurrrently with BAE 233A3201-30-02 R1

33. AD 2013-06-05, 737-27-1300 IN01 0103373 1C-40-WA-1-534: Elevator Tab - Aft Attach Lug Modification

34. AD 2013-15-16, 737-52A1167 Inboard Main Landing Gear Door Hinge Fitting inspection and Replacement

35. BAE 233A3201-30-02 R1 Window and pitot Heat Module

- Work concurrently with AD 2012-24-08, 737-30A1063 R1 IN01

36. C40C-SL-069-A 0133099 1C-40C-WA-1-509:Remove Inconel 600 sensors and replace with Inconel 625 Sensors

- Work concurrently with 737-26-1131 R1 IN01: Duct Leak Overheat Detector Support Installation

37. CFMI 72-893 New Bolt-Washer Assembly to Improve the Flange Attachment

38. FCF required for AD 2013-06-05, 737-27-1300 IN01 0103373 1C-40-WA-1-534

39. Perform Engine Wash on engine serial numbers 876358 and 876360

40. Comply with 6C - Check

41. Comply with 71A - Check

**********************************ADDITIONAL REQUIREMENTS**************************************

ADDITIONAL REQUIREMENTS:

1. Replace DV area partition upper connection rails (stations 611 left and right)

2. Replace Passenger Cabin carpet throughout aircraft

3. Replace Flight Deck carpet

4. Replace DV Lav Flooring

5. Replace baseboard carpet

6. Replace DV partition wall covering worn where passengers rest their feet on the wall

- FS 380 left, FS 400 right, FS 611 left and right

7. Replace seat track covers

9. Replace DV lounge lampshade

**************************************CONTINUED ON PAGE 4***************************************

LIST THOSE DEFECTS WHICH ARE KNOWN OR THOUGHT TO BE BEYOND USING ACTIVITY CAPABILITY BUT NOT IN THE DEPOT WORK SPEC

4 4

ADDITIONAL REQUIREMENTS CONTINUED:

10. Repair or replace Upper trim in FWD and AFT galley

- FS 344 to FS 380 & FS 947 to FS 1016

11. Replace overhead bin foam dividers

- 19 each between each overhead bin set

12. Replace or paint Emergency Escape Slide Covers (4each)

13. Leather Institute seat refurbishment

14. Replace Divan covering with approved leather

15. Repair delamination on Aft Lav rear wall

- FS 947

16. Repaint Flight Attendant Call Panel

- FS 947

LIST THOSE DEFECTS WHICH ARE KNOWN OR THOUGHT TO BE BEYOND USING ACTIVITY CAPABILITY BUT NOT IN THE DEPOT WORK SPEC

G081L9035-01 SIGNIFICANT HISTORICAL DATA 29APR14/1419 ZULU

AUTOMATED AFTO FORM 95

MDS S/N 00CF893772 CEI A00001L ACC DATE 25FEB07 LOC VDYD

LAST OVHL 09MAR06 MANF P/N CFM56-7B27/B3 MANF

NOMENCLATURE ENGINE, CFM56-7B CUR TIME 4608.0 CYC/LAND 3670

STATUS: INSTALLED ON NHA CEI: MA0001L S/N: 0005000730 POS: 1 DATE 01 MAR 07

NHA HRS: 4608.0 NHA CYC/LANDINGS: 3670

DATE REMARKS PERF ORG

23FEB07 26 FEB 2007 ENGINE 893772 ARIVED AT THIS STATION FROM BOEING 932 MXG

ON AIRCRAFT 05000730 INSTALLED IN THE #1 POSITION

TOTAL TIME: 37.5 TOTAL CYCLES 23

932 MXG/MX00E SCOTT AFB, IL 62225 (TSGT M. O'MALLEY)

01MAR07 ENGINE/ITEM INSTALLED ON AIRCRAFT 05000730, POSITION NR 1 , VDYD

AIRCRAFT TIME AT INSTALLATION 00037.5,

ENG/ITEM TT: 00037.5 TSOH 37.5 CSOH 23 TCYCS 23

A/C FULL STOP 000013 A/C TOTAL LAND 000023

02MAR07 SERIAL NUMBER A00001L0000893772 CHANGED TO A00001L00CF893772 SN CHNG

19JUN07 NUMBER SB107492361856 DATA CODE L932707 RELEASE DATE 06238 VDYD

RECISION DATE 08238 COMPLIANCE DATE 07170 CODE LETTER L

STATUS CODE 01 HOW MAL 801,ACCOMPLISHED BY ,CORRECTIVE

ACTION-REMOVED BAR PART # 107492-5 S/N 9506, INST

*TCTO DESCRIPTION (-) PNEUMATIC BLEED AIR REGULATOR REWORK C

ANGE P/N 107492-5 TO P/N 107492-6. (#1 ENGINE)

OTI CW SB107492361856 WB/NA PRIME

20NOV08 NUMBER CFMI 73-139 DATA CODE 0199993 RELEASE DATE 08218 VDYD

RECISION DATE 10218 COMPLIANCE DATE 08325 CODE LETTER L

STATUS CODE 01 HOW MAL 801,ACCOMPLISHED BY 00281,CORRECTIVE

ACTION-UPDATED SOFTWARE

*TCTO DESCRIPTION (/) ENGINE FUEL CONTROL ECU 73-21-60 NEW S

FTWARE 7.B.S

10FEB09 NUMBER 737-SL-36-016 DATA CODE 0111860 RELEASE DATE 08345 VDYD

RECISION DATE 09345 COMPLIANCE DATE 09041 CODE LETTER L

ACTION-C/W S/B 737-SL-36-016

*TCTO DESCRIPTION (/) PERFORM HIGH STAGE REGULATOR MODIFICAT

ON ON #2 ENGINE IAW SERVICE LETTER 737-SL-36-01

WB/NA PRIME SHOP A1ASP

10FEB09 NUMBER CFMI 72-705 DATA CODE 0111867 RELEASE DATE 08342 VDYD

RECISION DATE 09342 COMPLIANCE DATE 09041 CODE LETTER L

ACTION-CFMI SERVICE BULLETIN 72-705 C/W

*TCTO DESCRIPTION (/) PERFORM HPTACC MANIFOLD ASSEMBLY BOLT

NSTALLATION ON #2 ENG IAW SERVICE BULLET

N CFMI 72-705 WB/NA PRIME SHOP A1A

09MAR09 NUMBER 737-SL-36-017 DATA CODE 0199992 RELEASE DATE 08218 VDYD

RECISION DATE 10218 COMPLIANCE DATE 09068 CODE LETTER L

STATUS CODE 01 HOW MAL 801,ACCOMPLISHED BY 00190,CORRECTIVE

ACTION-SERVICE LETTER C/W ON #1 ENG, SEE JCN 2559

*TCTO DESCRIPTION (/) HIGH STAGE BLEED AIR VALVE

27APR09 ON THIS DATE THE FORWARD SPINNER CONE WAS REPLACED WITH AN 932 MXS

OVERHAULED (NEWLY PAINTED). REASON FOR REPLACEMENT WAS DUE

TO EXCESSIVE PAINT PEELING. NEW S/N INSTALLED DD242131-1

04AUG09 NUMBER CFMI 80-010 R2 DATA CODE 0111894 RELEASE DATE 09142 VDYD

RECISION DATE 10142 COMPLIANCE DATE 09216 CODE LETTER L

STATUS CODE 01 HOW MAL 801,ACCOMPLISHED BY 03297,CORRECTIVE

ACTION-#1 ENG STARTER CFMI TCTO C/W

*TCTO DESCRIPTION (/) #1 ENG - PACKINGS FOR HTS OILS AND NEW

MAGNETIC DRAIN PLUG ASSY

CW TCTO CFMI 80-010 R2 WB/NA PRIME

11SEP09 ON THIS DATE A SEMI-ANNUAL REVIEW WAS CONDUCTED OF ESN VDYD

893772 ENGINE RECORDS BY J. MATTINGLY 00281.

13DEC09 NUMBER CFMI 72-649 DATA CODE L932902 RELEASE DATE 08345 VDYD

RECISION DATE 10345COMPLIANCE DATE 09347 CODE LETTER

CORRECTIVE-ACTION NOT REQ PER REVISION 2

*TCTO DESCRIPTION ENGINE FAN AND BOOSTER FAN BLADE SHIM ASSE

13DEC09 PER CFMI 72-649 R2 THIS SERVICE BULLETIN DOES NOT APPLY TO VDYD

THE C-40C. THIS SB IS APPLICABLE TO ENGINES WITH

REWORKED FAN DISK PN/S 340-000-471-0, 340-000-472-0,

340-000-473-0, OR 340-000-474-0 INITIALLY INTRODUCED BY

CFMI SB 72-0342. ALL ENGINES INSTALLED ON C-40C HAVE FAN

DISK P/N'S 340-000-410-0 OR 340-000-420-0 FAN DISKS

INSTALLED.

TSGT JASON JONES, SCOTT AFB IL, DSN 576-9566

23JAN10 NUMBER CFMI 73-157 DATA CODE 0120216 RELEASE DATE 09244 VDYD

RECISION DATE 10202 COMPLIANCE DATE 10023 CODE LETTER L

STATUS CODE 01 HOW MAL 801,ACCOMPLISHED BY 43001,CORRECTIVE

ACTION-TCTO C/W

*TCTO DESCRIPTION (/) #1 ENGINE AND FUEL CONTROL - ECU - NEW

SOFTWARE VERSION 7.B.U1

CW TCTO CFMI 73-157 WB/NA PRIME

09MAR10 ON THIS DATE A SEMI-ANNUAL RECORDS REVIEW WAS PERFORMED ON VDYD

ESN 893772. REVIEW PERFORMED BY EMP# 42999

16MAR10 NUMBER 737-SL-71-062 DATA CODE 0120238 RELEASE DATE 10010 VDYD

RECISION DATE 11010 COMPLIANCE DATE 10075 CODE LETTER L

STATUS CODE 01 HOW MAL 801,ACCOMPLISHED BY 43002,CORRECTIVE

ACTION-R2 BRACKET IAW 737-SL-71-062

*TCTO DESCRIPTION (X) (#1 ENG) ENGINE-MOUNTED FAN COWL RADIA

SUPPORT BRACKET IMP

CW TCTO 737-SL-71-062 WB/NA PRIME

31MAR10 NUMBER 737-78-1076 DATA CODE 0111883 RELEASE DATE 09120 VDYD

RECISION DATE 10120 COMPLIANCE DATE 10090 CODE LETTER L

ACTION-TCTO 737-78-1076 C/W

*TCTO DESCRIPTION (/) #1 ENGINE THRUST REVERSER SYSTEM CASCA

E ASSEMBLY REPLACEMENT

CW TCTO 737-78-1076 WB/NA PRIME

31MAR10 NUMBER 737-29-1111 DATA CODE 0120232 RELEASE DATE 09335 VDYD

RECISION DATE 10335 COMPLIANCE DATE 10090 CODE LETTER L

STATUS CODE 01 HOW MAL 801,ACCOMPLISHED BY 42998,CORRECTIVE

ACTION-TCTO 737-29-1111 C/W

*TCTO DESCRIPTION (/) (#1 ENG) SUPPORT BRACKET CHANGE FOR TH

HYDRAULIC PRESSURE HOSE CW TCTO 737-29-1111 WB/NA

PRIME SHOP A1ASP

01APR10 NUMBER 737-36-1019 R1 DATA CODE 0120229 RELEASE DATE 09335 VDYD

RECISION DATE 10335 COMPLIANCE DATE 10091 CODE LETTER L

ACTION-TCTO 737-36-1019 IN 01 WB/NA C/W

*TCTO DESCRIPTION (/) (#1 ENG) CLAMP INSTALL ON ENGINE SENSE

TUBES FOR PNEUMATIC SYSTEM FLEX LINES CW TCTO 737-36-1019 I

01 WB/NA PRIME SHOPA1ASP

30OCT10 ANNUAL RECORD REVIEW WAS PERFORMED ON THIS DATE BY J. VDYD

MATTINGLY EMP #42999

09MAY11 NUMBER CFMI 72-678 DATA CODE 0111878 RELEASE DATE 09062 VDYD

RECISION DATE 11273 COMPLIANCE DATE 11129 CODE LETTER L

ACTION-TCTO CFMI 72-678 C/W

*TCTO DESCRIPTION (/) FAN AND BOOSTER ASSY - INTRODUCTION OF

A NEW AXIAL STOP PIN

CW TCTO CFMI 72-678 WB/NA PRIME

28OCT11 ON THIS DATE AN ANNUAL RECORDS REVIEW WAS PERFORMED BY VDYD

J. MATTINGLY EMP #42999

23APR12 NUMBER 1C-40B/C-509 DATA CODE 0110379 RELEASE DATE 11291 VDYD

RECISION DATE 12130 COMPLIANCE DATE 12114 CODE LETTER L

STATUS CODE 01 HOW MAL 801,ACCOMPLISHED BY 42996,CORRECTIVE

ACTION-R2 #1 PRSOV

*TCTO DESCRIPTION (X) 737-SL-36-019 REMOVAL AND REPLACEMENT

F PRSOV VALVE VALVE REMOVED

CW TCTO 1C-40B/C-509 WB/NA PRIME SH

07SEP12 NUMBER 2J-F56-WA-1-502 DATA CODE 0219555 RELEASE DATE 12178 VDYD

RECISION DATE 13176 COMPLIANCE DATE 12251 CODE LETTER L

ACTION-2J-F56-WA-1-502 C/W

*TCTO DESCRIPTION (/) (CFMI 72-876) ENG-COMBUSTION ASMBLY-IN

P FUEL NOZZLE CW TCTO 2J-F56-WA-1-502

03OCT12 NUMBER 2J-F56-WA-1-501 DATA CODE 0219554 RELEASE DATE 12178 VDYD

RECISION DATE 13176 COMPLIANCE DATE 12277 CODE LETTER L

ACTION-TCTO 2J-F56-WA-1-501 C/W

*TCTO DESCRIPTION (/) (CFMI 73-178) ENG FUEL & CNTRL-ECU-NEW

S/W VER 7.B.V2 CW TCTO 2J-F56-WA-1-501

20OCT12 ON THIS DATE AN ANNUAL RECORDS REVIEW WAS PERFORMED BY J. MA VDYD

TTINGLY EMPLOYEE #42999

27NOV12 NUMBER CFMI 72-825 DATA CODE 0219549 RELEASE DATE 11293 VDYD

RECISION DATE 14293 COMPLIANCE DATE 12332 CODE LETTER L

STATUS CODE 01 HOW MAL 801,ACCOMPLISHED BY 42948,CORRECTIVE

ACTION-VERIFIED AND ACCOMPLISHED NCR 34 AT DELTAL

*TCTO DESCRIPTION (/) COMPRESSOR FRONT STATOR ASSY - ON WING

INSPECTION OF PRE CFM56-7B S/B 72-0811

CW TCTO CFMI 72-825 WB/NA PRIME

20DEC12 NUMBER CFMI 72-586 R1 DATA CODE 0111891 RELEASE DATE 09142 VDYD

RECISION DATE 16061 COMPLIANCE DATE 12355 CODE LETTER L

ACTION-C/W DURING C-CHECK

*TCTO DESCRIPTION (/) INTRODUCTION OF A NEW FAN BLADE PLATFO

M WITH A NEW ELASTOMER SEAL

CW TCTO CFMI 72-586 R1 WB/NA PRIME

29APR13 NUMBER 2J-F56-WA-1-503 DATA CODE 0219557 RELEASE DATE 13094 VDYD

RECISION DATE 14094 COMPLIANCE DATE 13119 CODE LETTER L

ACTION-TCTO 503 C/W NO FURTHER ACTION NESSASARY

*TCTO DESCRIPTION (-) CFM56-7B SB 73-190

REPLACEMENT OF THE FUEL DIFF PRESSURE SWIT

H CW TCTO 2J-F56-WA-1-503 WB/NA PRIME

16JAN14 16 JAN 2014 ENGINE FAN BLADE SHIMS REPLACED WITH 932 MXS

P/N 340-252-307-0 POST SERVICE BULLETIN: 72-0649 , 72-0649R1

72-0777

AT ENGINE HRS 04327.9 , CYC 3488

**END OF MESSAGE 9035**

G081L9035-01 SIGNIFICANT HISTORICAL DATA 29APR14/1426 ZULU

MDS S/N 00CF892796 CEI A00001L ACC DATE 25FEB07 LOC VDYD

STATUS: INSTALLED ON NHA CEI: MA0001L S/N: 0005000730 POS: 2 DATE 01 MAR 07

23FEB07 26 FEB 2007 ENGINE 892796 ARIVED AT THIS STATION FROM BOEING 932 MXG

ON AIRCRAFT 05000730 INSTALLED IN THE #2 POSITION

01MAR07 ENGINE/ITEM REMOVED FROM AIRCRAFT 05000730, POSITION NR 1 , VDYD

A/C TIME AT INSTALLATION 00037.5 A/C TIME AT REMOVAL 00037.5

ENG/ITEM TT: 00037.5 TSOH 37.5 CSOH TCYCS 23

REMOVAL REASON: 799-NO DEFECT

01MAR07 ENGINE/ITEM INSTALLED ON AIRCRAFT 05000730, POSITION NR 2 , VDYD

02MAR07 SERIAL NUMBER A00001L0000892796 CHANGED TO A00001L00CF892796 SN CHNG

02MAR07 THE 3 ABOVE ENTRIES ON ESN 00CF892796 DATED 1 MAR 07 ARE VDYD

ERRORS RELATED TO ATTEMPTS TO LOAD THE NEW ENGINES INTO

G081. ENGINE WAS NOT REMOVED FROM THE AIRFRAME AT ANY TIME

ON THOSE DATES.

30JUL07 NUMBER SB107492361856 DATA CODE L932707 RELEASE DATE 06238 VDYD

RECISION DATE 08238 COMPLIANCE DATE 07211 CODE LETTER L

STATUS CODE 01 HOW MAL 801,ACCOMPLISHED BY 00083,CORRECTIVE

ACTION-R2 BLEED AIR REGULATOR

ANGE P/N 107492-5 TO P/N 107492-6. (#2 ENGINE)

06AUG08 ON THIS DATE DISCOVED MINOR NICK ON #8 1ST STAGE FAN BLADE. 932MXS

NICK IS LOCATED ON LEADING EDGE OF BLADE WITH A DEPTH OF

.005 IN. LIMIT IS .040IN. NO REPAIR IS REQUIRED IAW AMM

II 72-21-02-200-801-F00 PARA G STEP 2.

STATUS CODE 01 HOW MAL 801,ACCOMPLISHED BY 00464,CORRECTIVE

ACTION-C/W S/L 737-SL-36-016

ON ON #1 ENGINE IAW SERVICE LETTER 737-SL-36-016

ACTION-C/W S/B CFMI 72-705

NSTALLATION ON #1 ENG IAW SERVICE BULLETIN CFMI 72-70

ACTION-SERVICE LETTER C/W ON #2 ENG, SEE JCN 2559

03AUG09 NUMBER CFMI 80-010 R2 DATA CODE 0111894 RELEASE DATE 09142 VDYD

RECISION DATE 10142 COMPLIANCE DATE 09215 CODE LETTER L

ACTION-C/W TCTO

*TCTO DESCRIPTION (/) #2 ENG - PACKINGS FOR HTS OILS AND NEW

892796 ENGINE RECORDS BY J. MATTINGLY 00281.

STATUS CODE 01 HOW MAL 801,ACCOMPLISHED BY 43000,CORRECTIVE

*TCTO DESCRIPTION (/) #2 ENGINE AND FUEL CONTROL - ECU - NEW

CW TCTO CFMI 73-157 WB/NA PRIME S

ESN 892796. REVIEW PERFORMED BY EMP# 42999

ACTION-TCTO COMPLIED WITH IAW 737-SL-71-062

*TCTO DESCRIPTION (-) (#2 ENG) ENGINE-MOUNTED FAN COWL RADIA

01APR10 NUMBER 737-78-1076 DATA CODE 0111883 RELEASE DATE 09120 VDYD

RECISION DATE 10120 COMPLIANCE DATE 10091 CODE LETTER L

ACTION-T/R CASCADE ASSEMBLY REPLACEMENT C/W IAW T

*TCTO DESCRIPTION (X) #2 ENGINE THRUST REVERSER SYSTEM CASCA

02APR10 NUMBER 737-29-1111 DATA CODE 0120232 RELEASE DATE 09335 VDYD

RECISION DATE 10335 COMPLIANCE DATE 10092 CODE LETTER L

STATUS CODE 01 HOW MAL 801,ACCOMPLISHED BY 42999,CORRECTIVE

*TCTO DESCRIPTION (/) (#2 ENG) SUPPORT BRACKET CHANGE FOR TH

02APR10 NUMBER 737-36-1019 R1 DATA CODE 0120229 RELEASE DATE 09335 VDYD

ACTION-TCTO 737-56-10119 C/W CLAMPS INSTALLED

*TCTO DESCRIPTION (/) (#2 ENG) CLAMP INSTALL ON ENGINE SENSE

17OCT10 DUE TO BLEND REPAIR ON 1ST STAGE FAN BLADES #'S 1,16, 9, VDYD

AND 19 THE FOLLOWING MUST BE ACCOMPLISHED AT FIRST

OPPORTUNITY IAW AMM II SUBTASK 72-21-02-280-001

AT THE FIRST OPPORTUNITY AND IF THE FAN BLADE IS REMOVED

FROM THE ROTOR OS WHEN THE ENGINE IS REMOVED FROM THE

AIRCRAFT, DO THESE STEPS

(A) MEASURE THE MOMENT WEIGHT OF THE BLADES

(B) MAKE A RECORD OF THE NEW MOMENT WEIGHT OF THE BLADE

(C) IF THE MOMENT WEIGHT CHANGES MORE THAN 79 GRAM-INCHES

(200 G-CM), CORRECT THE BALANCE OF THE FAN BLADE ROTOR.

17OCT10 ON THIS DATE ESN 892796 1ST STAGE FAN BLADES #'S 1, 16, 9, VDYD

AND 19 WERE REPAIRED AFTER FOD INCIDENT. BLADE #1 DAMAGE IN

AREA "C" DEPTH BEFORE BLENDING WAS .038" AND DEPTH AFTER

BLENDING WAS .050". BLADE #16 DAMAGE IN AREA "C" DEPTH

BEFORE BLENDING WAS .045" AND DEPTH AFTER BLENDING WAS

.051". BLADE #9 IN AREA "E" DEPTH PRIOR TO BLENDING WAS

.052" AND DEPTH AFTER BLENDING WAS .070". BLADE #19 IN

AREA "C" DEPTH PRIOR TO BLENDING .050" AND DEPTH AFTER

BLENDING .065". BLADE #2 WAS DAMAGE OUT OF LIMITS WITH A

.008" NICK IN THE CRITICAL ROOT AREA "J"AND WAS REPLACED.

BLADE #14 WAS ALSO REPLACED AS PART OF THE SET. BLADES

BLENDS WERE PERFOMED BY EMP #42998 AND INSPECTED BY EMP

#42999. A FLUORESCENT PENETRANT INSPECTION WAS PERFOMED ON

ALL BLENDED BLADES AND NO CRACKS OR FURTHER DAMAGE

WAS INDICATED.

17OCT10 ON THIS DATE A BORESCOPE INSPECTION WAS PERFORMED AFTER A VDYD

FOD INCIDENT ON ESN 892796. A 4 INCH X 1/8TH INCH METAL ROD

WAS DISCOVERED BETWEEN THE 1ST STAGE FAN BLADES AND THE

OULET GUIDE VANES. NO DAMAGE PAST THE 1ST STAGE FAN WAS

NOTED ON THE BORESCOPE INSPECTION. THE INSPECTION WAS

PERFORMED BY EMP#42998. ENG TT: 2639.7 CSN:2171. SEVERAL

FIRST STAGE FAN BLADES WERE DAMAGED AND THE FAN CASE

ABRAIDABLE SHROUD WAS DAMAGED AROUND A 360 DEGREE

CIRCUMFERENTIAL AREA. THE DAMAGE HAS A CONTINUE IN

SERVICE LIMIT OF 50 CYCLES OR 125 HOURS. DAMAGE IS DUE

REPAIR BY 2764.7 TSN OR 2221 CSN.

05NOV10 ON THIS DATE ALL 1ST STAGE FAN BLADES WERE REMOVED FOR THE VDYD

ABRAIDABLE SHROUD REPAIR. THE SHROUD WAS REPAIRED IAW THE

AIRCRAFT MAINTENANCE MANUAL AND THERE ARE NO FURTHER

SERVICE RESTRICTIONS PLACED ON THE ENGINE. UPON INSPECTING

THE REMOVED FAN BLADES A WEAR MARK WAS DISCOVERED ON BLADE

#12. THE DAMAGE WAS LOCATED IN THE DOVETAIL AREA OF THE

BLADE MEASURED AT .004". THE BLADE PAIR #'S 12 AND 24 WERE

REPLACED. ALL BLADES WERE INSPECTED, RE-LUBED AND

INSTALLED. A VIBE SURVEY WAS PERFORMED IAW TASK 71-00-00-70

0-814-F00 AND INDICATIONS WERE WITHIN LIMITS. ALL BLADE

P/N'S, S/N'S AND MOMENT WEIGHTS ARE RECORDED AND ON FILE

WITH THE ENGINES RECORDS.

08NOV10 NUMBER CFMI 72-678 DATA CODE 0111878 RELEASE DATE 09062 VDYD

RECISION DATE 11273 COMPLIANCE DATE 10312 CODE LETTER L

ACTION-CFMI 72-678 C/W #2 ENGINE

*TCTO DESCRIPTION (/) FAN AND BOOSTER ASSY - INTRODUCTION OF

A NEW AXIAL STOP PIN

CW TCTO CFMI 72-678 WB/NA PRIME

05AUG11 ON THIS DATE PERFOMED A FAN TRIM BALANCE DUE TO CREW VDYD

REPORTS OF MINOR VIBRATION FELT IN FLIGHT DECK. 4 EA

SPIINER WEIGHTS WERE REPLACED IN THE FOLLOWING LOCATIONS.

POSITION #18 P09 WAS REMOVED AND P14 INSTALLED. POSITION 26

P14 WAS REMOVED AND P13 INSTALLED. POSITION 29 P09 WAS

REMOVED AND P14 WAS INSTALLED. POSITION 35 P14 WAS REMOVED

AND P13 WAS INSTALLED. MAP OF ALL WEIGHTS CURRENTLY

INSTALLED IN CONTAINED IN THE ENGINE RECORDS. A VIBE

SURVEY WAS PERFORMED AND FLIGHT DECK VIBE INDICATIONS WAS

BELOW 1.0 AT ALL POWER SETTINGS. SURVEY DATA IS FILED WITH

ENGINE RECORDS.

23APR12 NUMBER 1C-40B/C-509 DATA CODE 0110379 RELEASE DATE 11291 VDYD

RECISION DATE 12130 COMPLIANCE DATE 12114 CODE LETTER L

STATUS CODE 01 HOW MAL 801,ACCOMPLISHED BY 54559,CORRECTIVE

ACTION-R2 #2 ENG PRSOV

*TCTO DESCRIPTION (X) 737-SL-36-019 REMOVAL AND REPLACEMENT

F PRSOV VALVE VALVE REMOVED

CW TCTO 1C-40B/C-509

07SEP12 NUMBER 2J-F56-WA-1-502 DATA CODE 0219555 RELEASE DATE 12178 VDYD

RECISION DATE 13176 COMPLIANCE DATE 12251 CODE LETTER L

ACTION-TCTO 2J-F56-WA-1-502 C/W

*TCTO DESCRIPTION (/) (CFMI 72-876) ENG-COMBUSTION ASMBLY-IN

P FUEL NOZZLE CW TCTO 2J-F56-WA-1-502

03OCT12 NUMBER 2J-F56-WA-1-501 DATA CODE 0219554 RELEASE DATE 12178 VDYD

RECISION DATE 13176 COMPLIANCE DATE 12277 CODE LETTER L

ACTION-TCTO 2J-F56-WA-1-501 C/W

*TCTO DESCRIPTION (/) (CFMI 73-178) ENG FUEL & CNTRL-ECU-NEW

S/W VER 7.B.V2 CW TCTO 2J-F56-WA-1-501

27NOV12 NUMBER CFMI 72-825 DATA CODE 0219549 RELEASE DATE 11293 VDYD

RECISION DATE 14293 COMPLIANCE DATE 12332 CODE LETTER L

ACTION-VERIFIED AND ACCOMPLISHED NCR 34 AT DELTA

*TCTO DESCRIPTION (/) COMPRESSOR FRONT STATOR ASSY - ON WING

INSPECTION OF PRE CFM56-7B S/B 72-0811

CW TCTO CFMI 72-825 WB/NA PRIME

29APR13 NUMBER 2J-F56-WA-1-503 DATA CODE 0219557 RELEASE DATE 13094 VDYD

RECISION DATE 14094 COMPLIANCE DATE 13119 CODE LETTER L

ACTION-TCTO C/W PN: QA07995 INSTALLED NO FURTHER

*TCTO DESCRIPTION (-) CFM56-7B SB 73-190

REPLACEMENT OF THE FUEL DIFF PRESSURE SWIT

H CW TCTO 2J-F56-WA-1-503 WB/NA PRIME

15OCT13 24 EA FAN BLADES REMOVED INSPECTED LUBED AND REINSTALLED. 932AMXS

TSN: 4312.2 CSN: 3449

24 EA. PART # 340-252-307-0 SHIMS INSTALLED.

24 EA. PART # 340-001-816-0 PLATFORMS INSTALLED.

MICHAEL O'MALLEY 43002

16OCT13 NUMBER CFMI 72-586 R1 DATA CODE 0111891 RELEASE DATE 09142 VDYD

RECISION DATE 16061 COMPLIANCE DATE 13289 CODE LETTER L

ACTION-PLATFORMS REPLACED AS REQUIRED SEE JCN 289

*TCTO DESCRIPTION (/) INTRODUCTION OF A NEW FAN BLADE PLATFO

M WITH A NEW ELASTOMER SEAL

CW TCTO CFMI 72-586 R1 WB/NA PRIME

APU

G081L9035-01 SIGNIFICANT HISTORICAL DATA 29APR14/1428 ZULU

MDS S/N 00000P7101 CEI MC0020L ACC DATE 25FEB07 LOC VDYD

LAST OVHL 02MAR06 MANF P/N 3800702-1 MANF

NOMENCLATURE AUXILIARY POWER UNIT CUR TIME 4454.0 TOT CYC 392.9

STATUS: INSTALLED ON NHA CEI: MA0001L S/N: 0005000730 POS: 2 DATE 21 SEP 07

23FEB07 ON FEB 2007 APU P7101 ARIVED AT THIS STATION FROM BOEING 932 MXG

ON AIRCRAFT 05000730 TOTAL TIME: 100.8 TOTAL CYCLES 123

932 MXG/MXOOE, SCOTT AFB, IL 62225 (TSGT M. O'MALLEY)

02MAR07 ENGINE/ITEM INSTALLED ON AIRCRAFT 05000730, POSITION NR 1 , VDYD

AIRCRAFT TIME AT INSTALLATION 00041.1,

ENG/ITEM TT: 00109.3 TSOH 109.3 CSOH TCYCS

A/C FULL STOP 000014 A/C TOTAL LAND 000024

17MAY07 ENGINE/ITEM REMOVED FROM AIRCRAFT 05000730, POSITION NR 1 , VDYD

A/C TIME AT INSTALLATION 00041.1 A/C TIME AT REMOVAL 00259.0

ENG/ITEM TT: 00320.6 TSOH 368.7 APU TOTAL CYCLES 26.8

REMOVAL REASON: 916-JOINT OIL ANALYSIS PROGRAM (JOAP) REMOV

AL A/C FULL STOP 000079 A/C TOTAL LAND 000270

21SEP07 ENGINE/ITEM INSTALLED ON AIRCRAFT 05000730, POSITION NR 1 , VDYD

AIRCRAFT TIME AT INSTALLATION 00521.0,

ENG/ITEM TT: 00369.3 TSOH 369.3 CSOH TCYCS 291

A/C FULL STOP 000155 A/C TOTAL LAND 000507

21SEP07 ON THIS DATE AN ACCEPTANCE INSPECTION WAS PERFORMED ON APU VDYD

S/N P7101 PRIOR TO INSTALLATION INTO ACFT 05000730. NO

DEFECTS WERE NOTED. INSPECTION WAS PERFORMED BY EMPLOYEE #

00281. TT: 369.3 TSOH:369.3 TCYC 291. APU WAS RECIEVED

FROM OVERHAUL BY HONEYWELL REPAIR STATION # ZN3R030M.

REPAIR ORDER # 2007-774414-001

21MAY09 NUMBER 2118966-49-4210 DATA CODE 0111884 RELEASE DATE 09120 VDYD

RECISION DATE 10120 COMPLIANCE DATE 09141 CODE LETTER L

STATUS CODE 01 HOW MAL 801,ACCOMPLISHED BY 00784,CORRECTIVE

ACTION-APU ECU CONTROLLER MODIFICATION C/W

*TCTO DESCRIPTION (/) APU CONTROLLER ECU MODIFICATION

11SEP09 ON THIS DATE A SEMI-ANNUAL REVIEW OF APU S/N P7101 WAS VDYD

COMPLETED BY J. MATTINGLY 00281

22SEP09 NUMBER 2118966-49-4209 DATA CODE 0111861 RELEASE DATE 08345 VDYD

RECISION DATE 09345 COMPLIANCE DATE 09265 CODE LETTER L

ACTION-TCTO 2118966-49-4209 C/W

*TCTO DESCRIPTION (/) AIRBORNE AUXILIARY POWER UNIT CONTROLL

R SOFTWARE CHANGE

CW TCTO 2118966-49-4209 WB/NA PRIME

APU S/N P7101. REVIEW PERFORMED BY EMP# 42999

17MAR10 NUMBER D200907000007 DATA CODE 0120243 RELEASE DATE 10050 VDYD

RECISION DATE 11050 COMPLIANCE DATE 10076 CODE LETTER L

ACTION-APU FUEL MANIFOLD HAS BEEN INSPECTED, NO D

*TCTO DESCRIPTION (-) APU FUEL MANIFOLD INSPECTION FOR CHAFI

G

CW TCTO D200907000007 WB/NA PRIME

RIGHT MLG

G081L9035-01 SIGNIFICANT HISTORICAL DATA 29APR14/1431 ZULU

MDS S/N 03884Y1908 CEI MC0002L ACC DATE 23FEB07 LOC VDYD

LAST OVHL MANF P/N 161A1100-40 MANF

NOMENCLATURE MAIN LANDING GEAR CUR TIME 2461.7 CYC/LAND

STATUS: INSTALLED ON NHA CEI: MA0001L S/N: 0005000730 POS: DATE 23 FEB 07

23FEB07 ITEM INSTALLED ON AIRCRAFT 05000730 AIRCRAFT TIME AT

INSTALLATION 00000.0 ITEM TT: 00000.0 LANDINGS 0

23FEB07 ITEM REMOVED FROM AIRCRAFT 05000730 AIRCRAFT TIME AT VDYD

INSTALLATION 02144.0 AIRCRAFT TIME AT REMOVAL 02144.0

ITEM TT: 00000.0 LANDINGS 1729 REMOVAL REASON:799-NO DEFEC

T

04NOV09 DURING THE C-CHECK IN ATLANTA, SERVICE BULLETIN 737-32-1402 BOEING

WAS ACCOMPLISHED. THE TERMINATING ACTION FOR THIS SERVICE

BULLETIN IS TO REMOVE AND REPLACE THE FORWARD TRUNNION PIN.

THE MLG WAS REMOVED AND REINSTALLED TO ACCOMPLISH THIS

SERVICE BULLETIN. REFER TO DELTA JOB # 64126, BARCODE

NUMBER P7XCNR, CARD NUMBER 22.

932ND MXOOS, TSGT JASON JONES, DSN 576-9566

LEFT MLG

G081L9035-01 SIGNIFICANT HISTORICAL DATA 29APR14/1432 ZULU

MDS S/N 03883Y1908 CEI MC0002L ACC DATE 23FEB07 LOC VDYD

LAST OVHL MANF P/N 161A1100-39 MANF

NOMENCLATURE MAIN LANDING GEAR CUR TIME 2461.7 CYC/LAND

23FEB07 ITEM REMOVED FROM AIRCRAFT 05000730 AIRCRAFT TIME AT VDYD

INSTALLATION 02144.0 AIRCRAFT TIME AT REMOVAL 02144.0

ITEM TT: 00000.0 LANDINGS 1729 REMOVAL REASON:799-NO DEFEC

T

04NOV09 DURING THE C-CHECK IN ATLANTA, SERVICE BULLETIN 737-32-1402 BOEING

WAS ACCOMPLISHED. THE TERMINATING ACTION FOR THIS SERVICE

BULLETIN IS TO REMOVE AND REPLACE THE FORWARD TRUNNION PIN.

THE MLG WAS REMOVED AND REINSTALLED TO ACCOMPLISH THIS

SERVICE BULLETIN. REFER TO DELTA JOB # 64126, BARCODE

NUMBER P7XCNQ, CARD NUMBER 21.

932ND MXOOS, TSGT JASON JONES, DSN 576-9566

NLG

G081L9035-01 SIGNIFICANT HISTORICAL DATA 29APR14/1433 ZULU

MDS S/N 01061Y1908 CEI MC0001L ACC DATE 23FEB07 LOC VDYD

LAST OVHL MANF P/N 162A1100-9 MANF

NOMENCLATURE NOSE LANDING GEAR CUR TIME 2461.7 CYC/LAND

08NOV10 ON THIS DATE THE NLG STRUT…