N965FD

Part: AUTOTHROTTLE SYS — INOPERATIVE · airframe 45,737 hrs · 18,508 cycles

AUTO THROTTLES WOULD NOT ENGAGE DURING TAKEOFF ROLL. ABORTED TAKEOFF AT VERY SLOW AIRSPEED LESS THEN 30 KNOTS. MEL 28JUN22 04:58 JFK U RELEASED FOR SERVICE PER MEL : 22-30-01 CATEGORY : C EXPIRATION : 08JUL22 "MEL 22-30-01: THRUST MANAGEMENT SYSTEM/AUTOTHROTTLE SYSTEM - INOP." C/7322664 FACT 30JUN22 15:26 ORD REVERSED FROM MEL PROCEDURES. ACCOMPLISHED BITE CHECK REF 757 FIM 22-02 FAULT TREE 801. FOUND CSEU POWER SUPPLY MODULES M536 1L/M538 1R AND M539 2R FAULTING MODULE. RESET SUCCESSFULLY. ALSO FOUND STAB TRIM & ELEV ASYM LIMIT MODULE M524 LEFT AND M525 RIGHT FAULTING AIR-GROUND RELAY. RESET MODULES SUCCESSFULLY. ACCOMPLISHED MCDP GROUND TEST 30 AND TEST 40 (AUTOLAND) REF 757 AMM 22-00-02-2, ALL TESTS PASSED, NO 30 DAY HISTORY. O.K. FOR SERVICE.

Part: MODULE — FAILED (RUDDER) · airframe 45,635 hrs · 18,431 cycles

RUDDER RATIO EICAS MESSAGE AFTER TAKEOFF. QRH CHECKLIST ACCOMPLISHED. NOTIFIED GOC. NO ADVERSE HANDLING CHARACTERISTICS NOTED IN FLIGHT OR ON LANDING. EMERGENCY DECLARED. SHGN 29APR22 17:31 OAK FOLLOWING 757 FIM 27-21 FAULT TREE 809. AT STEP 21 FOUND HYD PRESS SWITCH S27 WITH DISCOLORATION AT PIN 3. REMOVED AND REPLACED SWITCH S27 PRECAUTIONARY REF AMM 29-11-17-4. LEAK AND OPS NORMAL. RUDDER SYS TEST NORMAL REF AMM 27-21-00-5. STILL T/S RUDDER RATIO SYS. SHGN 29APR22 18:02 OAK REF TSI 27-21/7703 AND 27-21/7702. ALL TEST AND BITE CHECKS PASS NORMAL. CAN NOT DUPLICATE PROBLEM. REMOVED AND REPLACED LEFT RUDDER RATIO CHANGER MODULE REF MM 27-09-00-2 AND PERFORMED ADJUSTMENT AND TEST REF MM 27-21-00-5. ALL TEST PASSED. REF TSI 27-21/7702 SUGGEST CHANGING RIGHT RUDDER RATIOCHANGER MODULE AS WELL. ONLY 1 IN STOCK OAK. PLACED ANOTHER AOG. REMOVED AND REPLACED RIGHT RUDDER RATIO CHANGER MODULE REF MM 27-09-00-2 AND PERFORMED ADJUSTMENT AND TEST REF MM 27-21-00-5. ALL TEST PASSED. ACFT OK TO CONT SERVICE.

Part: FLOORBOARD — BROKEN (ZONE 200) · airframe 44,807 hrs · 17,819 cycles

ZONE 250 FLOOR BOARD 251MWF IS BROKEN. FABRICATED ZONE 250 FLOOR BOARD 251MWF ON VT MAE TRAVELER # T21/1540891 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR.

Part: FLOOR PANEL — SHEARED (ZONE 200) · airframe 44,807 hrs · 17,819 cycles

ZONE 250 FLOOR BOARD 251MVF IS BROKEN. FABRICATED ZONE 250 FLOOR BOARD 251MVF ON VT MAE TRAVELER # T21/1540720 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 44,807 hrs · 17,819 cycles

AFT MAIN CABIN R/H FLOOR PANEL STA 1640 TO 1660 HAS BLUE WATER STAIN. PANEL 252MVF FABRICATED AFT MAIN CABIN R/H FLOOR PANEL 252MVF STA 1640 TO 1660 ON VT MAE TRAVELER # T21/1540623 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 44,807 hrs · 17,819 cycles

LAVATORY FLOOR PANEL 221BF DELAMINATED. FABRICATED LAVATORY FLOOR PANEL 221BF ON VTMAE TRAVELER # T21/1540096 IAW DWG SRZ-25-005 REV "R". CAT "A" MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 44,807 hrs · 17,819 cycles

AFT MAIN CABIN FLOOR PANEL STA 1540 TO STA 1640 HAS A BLUE WATER STAIN. PANEL 252MNF. FABRICATED ZONE 250 FLOOR BOARD 252MNF ON VT MAE TRAVELER # T21/1541444 IAW DWG SRZ-25-005 REVISION R. MAJOR REPA

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 44,807 hrs · 17,819 cycles

ZONE 250 FLOOR BOARD 252MVF HAS BLUE STAIN. FABRICATED ZONE 250 FLOOR BOARD 252MVF ON VT/MAE TRAVELER # T21/1540717 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 44,807 hrs · 17,819 cycles

COURIER FLOOR PANEL 222MF DELAMINATED. FABRICATED COURIER FLOOR PANEL 222MAF ON VTMAE TRAVELER # T21/1540228 IAW FEDEX DWG SRZ-25-005. CAT 'A' MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (COURIER AREA) · airframe 44,807 hrs · 17,819 cycles

COURIER 221MBF FLOOR PANEL DELMINATED. FABRICATED COURIER 221MBF FLOOR PNEL ON VTMAE TRAVELEL # T21/1540114 IAW FEDEX DWG SRZ-25-005. CAT A MAJOR REPAIR

Part: FRAME — DAMAGED (BS 1060) · airframe 44,807 hrs · 17,819 cycles

MAIN CABIN AT STA. 1060 FR. REPAIR BTW STR 3R AND 9R REQUIRES OUTER AND INNER CHORDS TO BE FABRICATED. INNER CHORD FABRICATED ON VTMAE TRAVELER T21/1539829, OUTER CHORD FABRICATED ON VTMAE TRAVELER T21/1539836 IAW WORK CARD E.A. T F-5310-T0345523 B P2 STEP 4. PART MARKED PER GMM 07-0-1001. CAT 'B' MAJOR REPAIR

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 44,807 hrs · 17,819 cycles

COURIR FLOOR PANEL 222AF DELAMINATED. FABRICATED COURIER FLOOR PANEL 222F ON VTMAE TRAVELER # T21/1540217 IAW FEDEX DWG SRZ-25-005 REV R. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (COURIER AREA) · airframe 44,807 hrs · 17,819 cycles

COURIER 221AF FLOOR PANEL DELAMINATED. FABRICATED COURIER 221AF FLOOR PANEL ON VTMAE TRAVELER # T21/1540104 IAW FEDEX DWG SRZ-25-005 REV R. CAT A MAJOR REPAIR.

Part: SLIDING WINDOW — OUT OF ADJUST (CAPTAIN'S) · airframe 44,571 hrs · 17,650 cycles

CAPTAIN SIDE WINDOW VERY DIFFICULT TO CLOSE. FOUND LATCH HANDLE DIFFICULT TO ROTATE AFT TO OPEN WINDOW. PERFORMED ADJUSTMENT TO LOWER LINK ARM, REF 757 AMM SUBTASK 56-11-02-825-013. OPERATIONS CHECKS GOOD. A/C OK TO CONTINUE FOR SERVICE.

Part: LINK ASSY — OUT OF ADJUST (L2 WINDOW) · airframe 44,342 hrs · 17,495 cycles

CAPTAIN`S EMERGENCY ESCAPE WINDOW DOES NOT FUNCTION CORRECTLY. MUST TURN WINDOW CRANK IN ORDER TO UNLOCK WINDOW HANDLE. ADJUSTED THE L2 WINDOW LINK ARM IAW AMM 56-11-02-5, UP TO STEPS (5)I(2). CONTINUE WITH L2 WINDOW LINING INSTALLATION PER (5)F. INSTALLED WINDOW TRIM IAW AMM 56-11-02-5. OPS CHECKED GOOD. AC OK FOR SERVICE.

Part: SLIDING WINDOW — MALFUNCTIONED (L2) · airframe 44,341 hrs · 17,494 cycles

CAPTAIN`S EMERGENCY ESCAPE WINDOW DOES NOT FUNCTION CORRECTLY. MUST TURN WINDOW CRANK IN ORDER TO UNLOCK WINDOW HANDLE. ADJUSTED THE L2 WINDOW LINK ARM IAW AMM 56-11-02-5 UP TO STEPS (5) I (2). CONTINUE WITH L2 WINDOW LINING INSTALLATION PER (5) F. INSTALLED WINDOW TRIM IAW AMM 56-11-02-5. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: OXYGEN MASK — DAMAGED (NR 1) · airframe 43,770 hrs · 17,148 cycles

MDIS 965 35-20 5884 12DEC19 MEM FACT U FOUND #1 OXYGEN MASK STORAGE BOX IN THE PASSANGER COURIER AREA BUSTED. ALL OXYGEN LEAKED OUT OF THE TOP OF THE BOX. R/I 12DEC19 10:24 MEM U REASON CODE : FAILED OPS CK. & REPLACED WITH SERVICABLE UNIT OFF MPN: MF20-108 POS: 3JP SRL: 79508 TAG NBR: 792G87 ON MPN: MF20-108 CPN: 3510596 SRL: SE09844 TAG NBR: G58259 REMOVED AND REPLACED BOTH OXYGEN STORAGE BOX AND OXYGEN MASK. OPS CHECK AND LEAK CHECK GOOD. AMM 35-11-51-4-99. FACT 12DEC19 10:54 MEM U VERIFIED BOTH FWD AND AFT HIGH PRESSURE OXYGEN CYLINDERS ARE SAFETIED OPEN REF AMM 35-11-30 & 35-11-32. SEE WRI 35-01 5882 FOR P/N AND S/N VERIFICATION OF BOTH O2 CYLINDERS AFTER REPLACEMENT.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,172 hrs · 16,727 cycles

CORROSION SHEAR WEB AREA MAIN CABIN STA 1683 RBL 45. REMOVED CORROSION AND EVALUATED DAMAGED AREA ON MAIN DECK PLATE STA 1683, RBL 45 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101, DET III. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER AT STA 1681 TO 1688, RBL 50 IAW SRM 53-60-51-2R, FIG 201, DET I, REPAIR 2, ALT II.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,172 hrs · 16,727 cycles

CORROSION SHEAR WEB AFT WEB AREA MAIN CABIN FLOOR STA 1691 RBL 34.0 REMOVED CORROSION AND EVALUATED DAMAGED AREA ON MAIN DECK PLATE STA 1691, RBL 34 AND STA 1683, RBL 25 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101, DET III. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND REPAIR FILLER AND SHIM AT STA 1681 TO 1693, RBL 22 TO RBL 39 IAW SRM 53-60-51-2R, FIG 201, DET I, REPAIR 2, ALT II.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,172 hrs · 16,727 cycles

CORROSION SHEAR WEB AFT WET AREA MAIN CABIN FLOOR STA 1691 RBL 10.0 REMOVED CORROSION ON MAIN DECK PLATE STA 1691, RBL 10 IAW SRM 51-10-02-OG. EVALUATED DAMAGED AREA, ORIG MAT = .071", REM MAT = .055",MAT LOSS = .016" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101, DET III. FABRICATED AND INSTALLED REPAIR DOUBLER AND SHIM AT STA 1690 TO 1697, RBL 9 TO RBL 15 IAW SRM 53-60-51-2R, FIG 201, DET I , REPAIR 2, ALT I.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,172 hrs · 16,727 cycles

CORROSION SHEAR WEB AFT AREA MAIN CABIN FLOOR STA 1703 RBL 45. REMOVED CORROSION ON MAIN DECK PLATE STA 1703, RBL 45 IAW SRM 51-10-02-OG, EVALUATED DAMAGE AREA, ORIG. MAT =.071", REM. MAT = .048", MAT LOSS = .023" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101, DET III, FABRICATED & INSTALLED REPAIR DOUBLER AND SHIM AT STA 1697 TO 1711, RBL 41 TO RBL 48 IAW SRM 53-60-51-2R, FIG 201, DET I, REPAIR 2, ALT I.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,172 hrs · 16,727 cycles

CABIN STA 365 .25 BETWEEN RBL 45.50 - 64.20 FLOORBEAM T CHORD CORRODED. EVALUATED PREVIOUS REPAIR ON STA 365,RBL 45.5 TO RBL 64.20 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101, DET. III, REMOVED PREVIOUS REPAIR AND ADDITIONAL. CUT OUT UPPER FLOORBEAM, FABRICATED AND INSTALLED T-CHORD SECTION ON STA 365.25 LBL32 TO RBL 65 IAW SRM 53-00-51-2R, FIG 201 DET II REPAIR 8.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 43,172 hrs · 16,727 cycles

MAIN CABIN STUB FLOORBEAM IS CRACKED AT STA 580 LBL 45. COMPLIED WITH EA F-5310-T0345550 P1 TITLE: FUSELAGE - MAINFRAME - STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR AT LBL 45.

Part: EVAS UNIT — FAILED (COCKPIT) · airframe 42,883 hrs · 16,533 cycles

REFER TO WRI 25-60 4953 E.O. # F-2560-E0323178 REV NO. E PS P2. CAPTIAN AND F/O EVAS BASE SERVICE DUE DATE DECEMBER 2018. REASON CODE : REMOVAL FROM A/C ONLY **NO INSTALLATION** OFF MPN: 107STC-265 CPN: 2525341 POS: LH SRL: 018AA12P TAG NBR: 563F86 REASON CODE : REMOVAL FROM A/C ONLY **NO INSTALLATION** OFF MPN: 107STC-266 CPN: 2525342 POS: RH SRL: 034AA12P TAG NBR: G75065 MEL 05NOV18 03:10 SHV U RELEASED FOR SERVICE PER MEL : 25-60-01 CATEGORY : D EXPIRATION : 05MAR19 "MEL 25-60-01: (IDENTIFY CAPT AND/OR F/O)____CAPT AND F/O______EMERGENCY VISION ASSURANCE SYSTEM (EVAS) - (IDENTIFY INOP OR MISSING)_____MISSING_____." ON MPN: 107STC-265 CPN: 2525341 POS: LH SRL: 026AA12P TAG NBR: 0733F7 ON MPN: 107STC-266 CPN: 2525342 POS: RH SRL: 0031Y05P TAG NBR: E65016 INSTALLED LEFT AND RIGHT EMERGENCY VISION ASSURANCE SYSTEM. OP CK NORMAL. REF B757-200 MM 25-62-00-4

Part: FUSE — MALFUNCTIONED (NR 1 BRAKE) · airframe 42,648 hrs · 16,382 cycles

WHILE REPLACING NR 1 TIRE FOUND NR 1 BRAKE NOT WORKING WITH APPLICATION OF BRAKE. RESET NR 1 BRAKE ANTISKID MODULE HYDRAULIC FUSE AND BLEED NR 1 BRAKE CK FOR LEAKS NON FOUND. NR 1 BRAKE OPS CK GOOD

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,902 hrs · 15,876 cycles

ON PREFLIGHT ALL LEFT EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-07-2. ALL LIGHTS OPS CHECKED GOOD.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 41,881 hrs · 15,863 cycles

L1 DOOR SLIDE PARTIAL DEPLOY AFTER RAMP PULLED DOOR OPEN. F/O SAID DOOR WAS DISARMED. REMOVED AND REPLACED L1 DOOR POWER ASSIST BOTTLE IAW AMM 52-11-30-4-0. REMOVED AND REPLACED L1 ESCAPE SLIDE PER MM 25-66-01-4-0. OPERATIONAL CHECKS NORMAL. OK FOR SERVICE.

Part: SLIDE — PARTIAL DEPLOY (R1 DOOR) · airframe 41,827 hrs · 15,818 cycles

R1 DOOR SLIDE BOTTLE DEPLOYED SLIDE PARTIALLY DEPLOYED SLIDE REINSTALLED PER AMM25-66-01-4 AND OPERATES MANUALLY BUT NOT WITH DOOR. DOOR ASSIST BOTTLE NEEDS SERVICING OR REPLACED REMOVED AND REPLACED R1 DOOR EMERGENCY POWER RESERVOIR IAW AMM 52-11-30-4. THIS CLEARS MEL.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 41,611 hrs · 15,644 cycles

AFTER UPSIZE OF FASTENER HOLE TO REMOVE ELONGATION, FOUND EDGE MARGIN LESS THAN 2D- AFT LOWER CARGO STA 1300 FRAME, STR 20L- 21L , UPPER SHEAR TIE ATTACHMENT FASTENER HOLE. COMPLIED WITH EA F-5310-T0332083 P1, FUSELAGE-MAINFRAME-STA 1300 FRAME SHORT EDGE DISTANCE COMMON TO SHEAR TIE NEAR STRINGER S-20L.

Part: SKIN — CRACKED (TE FLAP FAIRING) · airframe 41,611 hrs · 15,644 cycles

LT WING IB SIDE OF NR 2 FLAP CANOE FAIRING AFT FLAP LWR SKIN CRACKED COMPLIED WITH EA F - 5750 - T0331961 A P1. WING - FLIGHT SURFACES - LT OUTBOARD AFT FLAP LOWER SURFACE SKIN REPAIRS - RSC TRACKING.

Part: SKIN — DENTED (TE FLAP) · airframe 41,611 hrs · 15,644 cycles

LT WING IB LWR FLAP IB SIDE OF NR 1 CANOE FAIRING HAS 2 EA DENTS. COMPLIED WITH EA F-5750-T0331961 A P1. LT OUTBOARD AFT FLAP LOWER SURFACE SKIN REPAIRS.

Part: BULKHEAD — CRACKED (NR 2 PYLON) · airframe 41,611 hrs · 15,644 cycles

NR 2 PYLON AFT BULKHEAD LOWER O/B SECTION AFT I/B HOLE HAS A CRACK INDICATION IN THE ALUMINUM BULKHEAD ONLY. COMPLIED WITH EA F-5450-T0331906 P1, DEVIATION TO EO F-5450-7-5006 DUE TO CRACK INDICATION IN BULKHEAD AT BRACE FITTING MOUNT HOLE ON NR 2.

Part: SKIN — DENTED (TE FLAP) · airframe 41,611 hrs · 15,644 cycles

LT WING OB AFT FLAP OB END LWR SKIN HAS 1 EA DENT. COMPLIED WITH EA F-5750-T0331961 A P1. AFT FLAP LOWER SURFACE SKIN REPAIRS

Part: STRINGER — DENTED (FUSELAGE) · airframe 41,611 hrs · 15,644 cycles

COMPLY WITH EA T F-5321-T0330028 PT 2. ACCOMPLISH PERMANENT REPAIR OF AFT CARGO STRINGER STA 1365 LBL 10.65. ACCOMPLISHED PERMANENT REPAIR.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,611 hrs · 15,644 cycles

AFT PIT SHEAR TIE STA 1300 STR 20L - 21L IS CRACKED. SHEAR TIE REMOVED & REPLACED PER DWG 140N2002 REV D & H.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,338 hrs · 15,458 cycles

SERVICE CHECK, R1 DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED THE BULB IAW AMM 33-51-06-2-1, OPS NORMAL. OK FOR SERVICE.

Part: CYLINDER — FAILED (DOOR) · airframe 40,925 hrs · 15,171 cycles

EMERGENCY POWER RESERVOIR READS 0. REF WRI 25-60 2895. REMOVED EMER POWER SPRING CYLINDER & INSTALLED REPAIRED CYLINDER IAW MM 52-11-33-4.

Part: SLIDE — DETACHED (DOOR) · airframe 40,918 hrs · 15,166 cycles

RIGHT DOOR SLIDE DETACHED WHEN CREW ENTRANCE DOOR OPENED, DUE TO LATE DG FREIGHT BEING DELIVERED. R1 DOOR SLIDE INOPERATIVE OR MISSING. NO JUMP SEATERS OR ACM'S ARE TO OCCUPY COURIER AREA IN FLIGHT. R & R RT ESCAPE SLIDE IAW AMM 25-66-01-4.

Part: SKIN — DENTED (BS 1618) · airframe 400 hrs · 14,546 cycles

SKIN DENTED AT BS 1618 BETWEEN STRINGERS 17L & 18L. FOUND TO BE OUT OF LIMITS. REPAIRED AREA IAW EA F-5330-T0315612 REV PS P1. CUTOUT, FABRICATED, AND INSTALLED A REPAIR DOUBLER.

Part: SKIN — DENTED (BS 1590) · airframe 400 hrs · 14,546 cycles

FUSELAGE SKIN HAS A DENT AT BS 1590 BETWEEN STRINGERS 17 & 18R. FOUND OUT OF LIMITS. CUTOUT, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW EA F-5330-T0315616 REV PS P1 & SRM 53-00-01.

Part: SKIN — DENTED (BS 650) · airframe 400 hrs · 14,546 cycles

FUSELAGE SKIN HAS A DENTED AREA AT BS 650 BETWEEN STRINGERS 26L & 27L. FOUND TO BE OUT OF LIMITS. REPAIRED AREA IAW EA F-5330-T0315599 REV PS P1.

Part: LAMP — INOPERATIVE (R1 DOOR SLIDE) · airframe 38,578 hrs · 13,460 cycles

R1 DOOR EMERGENCY "SLIDE" LIGHT INOPERATIVE. REPLACED LAMP IAW SMP, OPS CHECKED GOOD.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 38,569 hrs · 13,443 cycles

RT WING UPPER SKIN, WS 435 ALONG THE FWD EDGE CORRODED. REPAIRED IAW EA F-5710-165127. CORROSION DETERMINED TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 101, SHT 4, PAGE 104 DET A. THIS REPAIR IS CLASSIFIED AS A CATAGORY A MAJOR REPAIR.

Part: SKIN — GOUGED (BS 675) · airframe 38,569 hrs · 13,443 cycles

LEFT FUSELAGE SKIN, INTERNAL BS 675 S11-12L, GOUGED. REPAIRED IAW EA 757-5311-16-F4085, REV. CLASSIFIED AS MAJOR REPAIR.

Part: FRAME — CHAFED (BS 239) · airframe 38,569 hrs · 13,443 cycles

FWD LOWER FUSELAGE AT E/E COMPARTMENT, ALONG STA 239, BETWEEN RBL 11 THRU RBL 23 CIRCUMFERENTIAL FRAME UPPER FLANGE HAS CHAFED AND SOME RIVETS NEED PAINT . BLENDED DAMAGED AREA SMOOTH IAW SRM 51-10-02, ORIGINAL FRAME FLANGE THICKNESS .045", AFTER REWORK .025", REMOVED .020", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, SHEET 3, DETAIL 1. REMOVED DAMAGED FRAME IAW SRM 51-40-02 . RECEIVED NEW FRAME ON TRAVELER T12/973422 , LOCATED AND DRILLED NEW FRAME IAW SRM 51-40-05, INSTALLED NEW FRAME IAW SRM 51-40-02 AND DWG 141N1205 , PAINTED AREA IAW AMM 51-21-10-7. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 1060 S4R) · corrosion level 2 · airframe 38,569 hrs · 13,443 cycles

CABIN FRAME FWD SIDE, BS 1060, S4R, CORRODED . REMOVED CORROSION, FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG.101. REMOVED FRAME STA 1060, STR 4R TO 9R. FABRICATED FRAME SECTION AND REPAIR SPLICES IAW SRM 53-00-07, REPAIR NR 3 OF STAM TRAVELERS T12/975725, T12/975726, T12/975727. INSTALLED REPAIR FRAME AND SPLICES STA 1060, STR 4R TO 9R IAW SRM 53-00-07. REPAIR 3. CATEGORY "B" MAJOR REPAIR.

Part: FAIRING — GOUGED (LT NACELLE) · airframe 38,569 hrs · 13,443 cycles

NR 2 SAILBOAT FAIRING AFT LT SIDE OF LOWER PAN GOUGED, PP STA 243.52.

Part: FAIRING — GOUGED (NR 1 NACELLE) · airframe 38,569 hrs · 13,443 cycles

LT PYLON AFT SAILBOAT FAIRING BOTTOM AREA AT PP STA 243 HAS 2 GOUGES. REPAIRED IAW EA F-5450-163993. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 38,569 hrs · 13,443 cycles

SEAT TRACK BS 1540 -600, LBL 24, CORRODED AND GOUGED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. REMOVED SEAT TRACK IAW SRM 51-40-02, LOCATED AND DRILLED NEW SEAT TRACK IAW DWG 146N5137-2. INSTALLED NEW SEAT TRACK IAW DWG 146N5120 & SRM 51-40-02.

Part: FRAME — CRACKED (BS 640) · airframe 38,569 hrs · 13,443 cycles

FWD PIT, BS 640 FRAME WEB, S22-23R, CRACKED. FOUND OUT OF LIMITS IAW NDTM PT 6, 51-00-19 . REMOVED FRAME IAW SRM 51-40-02 . FABRICATED IAW DRAWING 143N1024. INSTALLED FRAME IAW 51-40-02 & DRAWING 143N1011. MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (BS 700) · airframe 38,569 hrs · 13,443 cycles

FLOORBEAM UPPER TEE AT BS 700 HAS SEVERAL AREAS WITH NICKS, SCRATCHES, AND CORROSION AROUND NUTPLATE HOLES. R & R FLOORBEAM TEE IAW SRM 51-40-02 AND DWG 143N5014. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (BS 1660) · corrosion level 2 · airframe 38,569 hrs · 13,443 cycles

MAIN CABIN FLOORBEAM UPPER TEE AT BS 1660, LBL 58 TO RBL 58 HAS CORROSION AROUND FASTENER HOLES OF UPPER AND LOWER SURFACES. REMOVED CORROSION AT FLOORBEAM & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III . REMOVED FLOORBEAM IAW SRM 51-40-02. FABRICATED NEW FLOORBEAM IAW DWG 146N5110-9 . INSTALLED NEW FLOORBEAM IAW DWG 146N5500. MAJOR REPAIR.

Part: DECK PLATE — CORRODED (BS 1681-1720) · airframe 38,569 hrs · 13,443 cycles

MAIN DECK AFT DECK PLATE FROM BS 1681 TO 1720, LBL 52 TO RBL 52 HAS SEVERAL CORRODED SPOTS ESPECIALLY ON FWD AND AFT EDGES. R & R DECK PLATE IAW SRM 51-40-02 & DWG 146N5300, SHT 208. MAJOR REPAIR.

Part: SKIN — CORRODED (NR 1 NACELLE) · airframe 38,569 hrs · 13,443 cycles

NR 1 PYLON RT AFT SKIN INTERNAL SURFACE PP STA 153 TO 174 HAS SIGNS OF CORROSION BETWEEN THE SKIN AND LOWER CHORD. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DET III, PYLON. RT AFT INTERNAL STRUT FAIRING SKIN CORROSION REPAIR, REPAIRED IAW EA F-5450-163992. MAJOR REPAIR.

Part: SKIN — CORRODED (NR 1 NACELLE) · airframe 38,569 hrs · 13,443 cycles

NR 1 PYLON RT FWD SKIN INTERNAL SURFACE AT 433GR DOOR CUT-OUT LOWER SIDE HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, FIG 101 DET III. R & R NR 1 PYLON RT FWD SKIN, IAW DWG 311N5002, SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 1540-1600) · airframe 38,569 hrs · 13,443 cycles

SEAT TRACK BS 1540-1600 LBL 45 CORRODED AND GOUGED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. FABRICATED NEW SEAT TRACK IAW DWG 1465137-2. INSTALLED SEAT TRACK IAW SRM 51-40-02 AND DWG 146N1520. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 38,569 hrs · 13,443 cycles

BS 365, BL 0 - RBL 62, FLOORBEAM UPPER TEE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 DETAIL II & IV FIG 101. REMOVED AND REPAIRED UPPER CHORD AT STA 365 LBL 15.5 TO RBL 70 IAW SRM 53-00-51 FIG201, REPAIR 3. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 38,569 hrs · 13,443 cycles

CABIN BS 345, RBL 18-LBL 30 FLOORBEAM UPPER STRUCTURE CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, SH NR 4, DET III . REPAIRED FLOORBEAM IAW SRM 53-00-51, FIG 201, DETAIL I, SH 4, REPAIR 3, MAJOR REPAIR .

Part: SKIN — CORRODED (RT WING) · airframe 38,569 hrs · 13,443 cycles

RIGHT WING UPPER SKIN L/E, BBL 70.50 TO WS 806.50 CORROSION BLEEDING INTO SEALANT GAP AND ARROUND FASTENERS. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 101, DETAIL A. REPAIRED WING, RT OUTER WING UPPER SKIN AT WS 435 ALONG THE FWD EDG IAW EA F-5710-165127 & WING RT OUTER WING UPPER INTERSPAR SKIN CORROSION IAW EA NR F-5710- 165119. MAJOR REPAIR.

Part: SKIN — CORRODED (FUEL TANK) · airframe 38,569 hrs · 13,443 cycles

CABIN CENTER FUEL TANK UPPER SKIN BS 1040 RBL 24 TO RBL 45, CORRODED. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 57-10-01, PG 102, FIG 101, NOTE A. REPAIRED IAW EA F-5730-165074. MAJOR REPAIR.

Part: SKIN — CORRODED (LT WING) · airframe 38,569 hrs · 13,443 cycles

LT WING UPPER SKIN L/E WS 369.50 CORROSION BLEEDING INTO SEALANT GAP AND AROUND FASTENERS. REPAIRED WINGS PLATES AND SKIN IAW EA F-5730-163713. MAJOR REPAIR.

Part: FUEL CELL — CORRODED (CENTER) · airframe 38,569 hrs · 13,443 cycles

CABIN CENTER FUEL TANK UPPER SKIN STA 1020-1040 RBL 45 TO RBL 62, CORRODED. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 57-10-01, PG 102, FIG 101, NOTE A. REPAIRED IAW EA F-5730-165074. MAJOR REPAIR.

Part: FRAME — DENTED (BS 1460) · airframe 38,569 hrs · 13,443 cycles

AFT CARGO BAY FRAME BS 1460 S23-24L UPPER FLANGE DENTED. R & R FRAME IAW SRM 51-40-02, FABRICATED NEW FRAME, LOCATED AND DRILLED IAW SRM 51-40-02 AND INSTALLED IAW SRM 51-40-02 AND DWG 146N1014. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 38,569 hrs · 13,443 cycles

CABIN BS 324 RBL 40-62 FLOORBEAM UPPER TEE CORRODED. REMOVED CORROSION IAW SRM 51-10-02, FOUND TEE TO BE OUT OT LIMITS IAW SRM 53-10-08, FIG 101, DETAIL XI. R & R TEE IAW SRM 51-40-02, MAJOR REPAIR.

Part: FUEL TANK — LEAKING (CENTER) · airframe 38,566 hrs · 13,442 cycles

STRONG ODOR OF FUEL IN CABIN. SUSPECT CENTER TANK LEAK. TROUBLESHOOT AND REPAIRED INBD CENTER TANK FUEL LEAK ALL WORK ACCOMPLISHED.