N785FD

Part: SKIN — GROUND DAMAGE (ZONE 200) · airframe 76,591 hrs · 30,511 cycles

DURING TOWING OF THE AIRCRAFT INTO THE HANGAR 8.2, TAIL LH SIDE OF FUSELAGE STA 1768.80 TO STA 1787.45 STRINGER 20L MADE CONTACT WITH THE TAIL STAND. ACCMPLISHED REPAIR IAW EA 757-5380-16-A3665 SECTION 48 - FUSELAGE STA 1768 TO STA 1787.5 S-19L TO S-20L LAP SPLICE - DENT AND GOUGE AND FED EX EA F-5330- T0380366: FUSELAGE - PLATES AND SKIN - TAIL SKIN AT STA 1768.8 AND S19L / 20L DAMAGE WHILE TOWING INTO HANGAR. MAJOR REPAIR

Part: COLLAR — SHEARED (UNKNOWN) · airframe 76,128 hrs · 30,184 cycles

GUST LOCK BROKEN ON R1 ENTRY DOOR. VERIFIED HOLD-OPEN COLLAR NEEDS REPLACED BUT NIS AT GSO. R1 ENTRY OPEN & CLOSED SEVERAL TIMES REF FDX RELEASED FOR SERVICE PER MEL : 52-11-01-A. REMOVED AND REPLACED R1 DOOR GUST LOCK REF B757 AMM 52-11-08-4. OP CHECK GOOD, NO FURTHER DEFECTS NOTED.

Part: ADAPTER — LOOSE (N/A) · airframe 76,122 hrs · 30,177 cycles

PDIS 785 27-10 7609 16NOV23 IND FACT U IN THE FLARE BELOW APPROXIMATELY 50 IT TOOK SIGNIFICANTLY MORE EFFORT THAN NORMAL TO MOVE THE CONTROL WHEEL LEFT OR RIGHT. THE RESISTANCE INCREASES SIGNIFICANTLY AFTER A SHORT AMOUNT OF CONTROL WHEEL TRAVEL. IT S AS IF SOMETHING IS RESTRICTING OR BLOCKING FREE MOVEMENT OF THE CONTROL WHEEL. PREFLIGHT AND POSTFLIGHT MOVEMENT OF CONTROL WHEEL WAS NORMAL. AMM: 71-11-02-4 REMOVED CAPTAINS LATERAL CONTROL WHEEL AND FOUND THE HARDWARE FOR ADAPTER, REF IPC 27-11-02-01 ITEM 200, NOT SECURE AND ALLOWING PLAY. SECURED HARDWARE TO THE ADAPTER AND REINSTALLED THE LATERAL CONTROL WHEEL WITH NO PLAY NOTED REF AMM 27-11-02-4. ALL OP'S NORMAL.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 75,605 hrs · 29,815 cycles

ONE EMERGENCY LIGHT WILL NOT ILLUMINATE EXTERIOR OF L1 DOOR. DUE TO EXTENDED LAYOVER BATTERIES NEEDED TO BE CHARGED FOR OPS CHECK. PERFORMED ADJUSTMENT/TEST PER B757 AMM 33-51-00-5 WITH NO DEFECTS NOTED. AC OK FOR SERVICE.

Part: SENSOR — FAILED (SLATS) · airframe 75,431 hrs · 29,679 cycles

LE SLAT ASYM MESSAGE ON DEPARTURE BETWEEN FLAPS 1 AND UP. RAN QRH AND COMPLIED WITH CHECKLIST. DECLARED EMERGENCY AND RETURNED TO MCI. REST OF FLIGHT WAS UNEVENTFUL. EMERGENCY DECLARED AMM: 27-81-41-4 REMOVED AND REPLACED LOSS SENSING SWITCH FOR THE INBOARD LE SLATS. OPS CHECK GOOD.

Part: FITTING — CORRODED (LT NACELLE) · corrosion level 2 · airframe 75,424 hrs · 29,672 cycles

LT WING PYLON DRAG LINK FITTING HAS CORROSION IN 5EA HOLES IN FITTING LAYER ONLY. HOLE NUMBERS 1,3,8,10, AND 15. COMPLIED WITH EA F-5730-T0370901 PT1 WINGS - PLATES AND SKIN AT PYLON DRAG FITTING, CORROSION FINDINGS. THIS EA DEVIATES FROM EO F-5730-E0340076. MAJOR REPAIR.

Part: ATTACH FITTING — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 75,424 hrs · 29,672 cycles

#2 ENGINE PYLON DRAG LINK ATTACHMENT FITTING HAS 8 HOLES WITH CORROSION. HOLES 2,3,5,7,10,14. AND 15 IN FITTING LAYER. HOLE 8 HAS CORROSION IN SKIN LAYER. COMPLIED WITH EA F-5730-T03700894 PT1 R/H WING UPPER SKIN AT DRAG FITTING CORROSION FINDINGS. THIS EA DEVIATES FROM EO F-5730-E0340076. MAJOR REPAIR

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 75,424 hrs · 29,672 cycles

MAIN DECK FLOOR FS1681. FS 1681 FLOOR BEAM UPPER CHORD, UPPER SECTION EXFILIATED BETWEEN WEB AND FLOOR BEAM APPROX LBL12. REPAIRED MAIN DECK FLORO FS 1681 FLOOR BEAM UPPER CHORD, UPPER SECTION FROM LBL 3 TO LBL 20 IAW SRM 53-60-51-2R. CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-51-1A PARA B DETAIL III. MAJOR REPAIR

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 75,424 hrs · 29,672 cycles

VIEW FROM FWD CARGO COMPT. MAIN CARGO FLOOR BEAM AT BS 580 LBL 45 HAS CRACK. REPAIRED FLOOR BEAM AT STA 580 LBL 45 IAW EA TF-5310-T0370825 PT1. FUSELAGE - MAINFRAME- FLOOR BEAM AT STA 580 AND LBL 45 CRACKED - REPAIR PER DRAWING SR57-53- 004. MAJOR REPAIR

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 75,424 hrs · 29,672 cycles

ZONE 220 FLOOR BOARD 221AF IS DELAMINATED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T22/1638355 IAW DWG SRZ- 25- 005 REVISION R. MAJOR REPAIR

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 75,424 hrs · 29,672 cycles

ZONE 220 FLOOR BOARD 222AF IS DELIAMINATED FABRICATED ZONE 220 FLOOR BOARD 222AF ON VT MAE TRAVELER T22/1638359 IAW DWG SRZ- 25- 005 REV R. MAJOR REPAIR

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 75,424 hrs · 29,672 cycles

ZONE 220 FLOOR BOARD 221MBF IS DELAMINATED FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELER T22/1638356 IAW DWG SRZ-25-005 REV R. MAJOR REPAIR

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 75,424 hrs · 29,672 cycles

ZONE 20 FLOOR BOARD 222MAF IS DELAMINATED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T22/1638358 IAW DWG SRZ- 25-005 REV R. MAJOR REPAIR

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 75,330 hrs · 29,597 cycles

DOOR WAS DISARMED AND NEW CALLOUT WAS MADE BUT SLIDE FELL OUT OF DOOR. SLIDE DID NOT DEPLOY. REMOVED AND INSTALLED NEDW R-1 DOOR SLIDE RFEF B757 AMM 25-66-01-4 GIRT BAR OPERATES NORMALLY PLACARED REMOVED PER SDR SLIDE ASSY MANUFATURE P/N D31038-201FX S/N 0977

Part: GUST LOCK — DAMAGED (L1 DOOR) · airframe 75,154 hrs · 29,475 cycles

L1 DOOR GUST LOCK FOUND BROKEN ON POST FLIGHT. (REMOVED BROKEN COLLAR) INSTALLED NEW GUST LOCK TO L1 DOOR REFERENCE TO AMM 52-11-08-8. DOOR OPS CHECK GOOD TO AMM 52-11-08-8.

Part: BULB — FAILED (ZONE 800) · airframe 75,006 hrs · 29,383 cycles

MDIS 785 33-50 6302 04MAR22 EWR FACT U ON SERVICE CHECK FOUND LH EMERGENCY SLIDE LIGHT INOP. FACT 04MAR22 18:42 EWR U RELAMPED LH EMERGENCY SLIDE LIGHT AS PER 757 AMM 33-51-06-2-1. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: DOOR — GOUGED (N/A) · airframe 74,974 hrs · 29,362 cycles

MAIN CARGO DOOR IS GOUGED AND DENTED ON SKIN AT STA 599 REPAIRED REF 757 SRM 52-30-01-2R REPAIR 4 AND EA F-5230-T0367049

Part: CYLINDER — DISCHARGED (R1 EMER OPEN) · airframe 73,926 hrs · 28,624 cycles

R1 DOOR EMERGENCY POWER RESERVOIR CYLINDER DISCHARGED. REMOVED AND REPLACED EMERGENCY POWER RESERVOIR, REF B757 AMM 52-11-32-4.

Part: CASCADE — DAMAGED (THRUST REVERSER) · airframe 72,839 hrs · 27,870 cycles

DURING POST STORM WALKAROUND FOUND RT ENGINE RT T/R HALF AT 2 O'CLOCK POSITION L.E. DAMAGE APPX 16 INCHES X 9 INCHES.

Part: VANE — DAMAGED (THRUST REVERSER) · airframe 72,839 hrs · 27,870 cycles

DURING POST STORM WALKAROUND FOUND RT ENGINE RT THRUST REVERSER HALF AT 2 O'CLOCK POSITION L.E. DAMAGE APPX 16 INCHES X 9 INCHES. TEMP REPAIR PER EA F-7830-T0348334. COMPLIED WITH EA F-7830-T0348334 PT 1 INSTALLED RT ENGINE O/B SLEEVE IAW AMM 78-31-07-4, OPS CHECKED GOOD.

Part: FRAME — PUNCTURED (BS 231) · airframe 70,440 hrs · 26,256 cycles

FRAME AT BS 231, BL 0 IS PUNCTURED. REPAIRED IAW EA F-5310-T0328373 P1.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 70,207 hrs · 26,086 cycles

THREE TIMES DURING FLIGHT WE SMELLED AN ACRID ELEC BURNING SMELL. NO SMOKE NOTED & UNABLE TO ISOLATE. FIRST OFFICER ALWAYS SMELLED IT FIRST. ALWAYS WENT AWAY IN 1 MIN. NO SMELL IN COURIER AREA. IAW FIM 21-00 PROC 4, SINCE FAULT CAN'T BE DUPLICATED & ALL ELEC PANELS HAVE BEEN INSPECTED, IN PREVIOUS UPDATED, SUSPECT LT RECIRC FAN MAY HAVE BEEN OVERHEATING. R & R LT RECIRC FAN PRECAUTIONARY IAW AMM 21-25-01-4. OPERATIONS CHECKED GOOD, NO FUMES OR DEFECTS NOTED. FAN OFF PN 645705-3, SN 45-211, FAN ON PN 645705-3 & SN 102-86.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 697 hrs · 25,703 cycles

R1 DOOR EXTERNAL SLIDE LIGHT INOPERATIVE. R & R R1 DOOR SLIDE LIGHT ASSEMBLY IAW MM 33-51-06-2-1. OPERATIONS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 692 hrs · 25,375 cycles

DURING SERVICE CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE, REPLACED THE LAMP. ALL OPS CHECKED NORMAL IAW AMM 33-51-06-2-1.

Part: DOUBLER — SCRATCHED (FUSELAGE) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE EXTERIOR SKIN, WHILE PERFORMING EA F-5330-T0308700PT1 FOUND DOUBLER HAS SCRATCHES AT STATION 1350 STRINGER 1 - 2R. SCRATCH ON DOUBLER CLEARED & TREATED IAW SRM 51-10-02 REV 112 & SRM 51-20-01 REV 112. FOUND NO SIGNIFICANT MATERIAL LOST. PART 1 OF EA F-5330-T0308700A TITLE FUSELAGE PLATES & SKIN FUSELAGE SKIN REPAIR BETWEEN BS 1340 - 1360 & STRINGER 1 - 2R SKY RADIO ANTENNA REMOVAL SA5831NM COMPLIED REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DENTED (BS 1701-1720) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE SKIN HAS A DENT BS 1701 - 1720 STRINGER 28 - 30R. REPAIRED IAW EA F5330-T0310832. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 68,836 hrs · 25,096 cycles

BS 377.7 LBL 55 - 60 FLOORBEAM UPPER TEE FOUND CORROED ON LOWER SURFACE. FLOORBEAM TEE REMOVED AND REPLACED IAW DWG 141N5113 SHT 1 REV F. DWG 141N5123 SHT 1 REV A AND EA F-5310-T0311051 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 1701-1720) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE SKIN HAD NUMEROUS NICKS & SCRATCHES BETWEEN STRINGER 26L & 26R BETWEEN BS 1701 - 1720. DAMAGE REMOVED AND TREATED IAW SRM 51-10-02 REV 112. FOUND ONE SPOT OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE 1 REV 112, REPAIRED OUT OF LIMITS SPOT IAW SRM 53-00-01 REPAIR 6 REV 113 . REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — DAMAGED (BS 1622) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1622 STRINGER 27 - 28L. THE DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00-01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE 1 REV 112. PART 1. REPAIRED IAW EA F-5330-T0312331. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 1627) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 1627 STRINGER 27 - 28L. DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00-01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 11 DETAIL II ALLOWABLE DAMAGE 1 REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0312331. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 1571) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1571 STRINGERS 27 - 28L. DAMAGE BLENDED AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWANCE DAMAGE 1 REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0311361. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 1576) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1576 STRINGER 27 - 28L. BLENDED THE DAMAGE AND FOUND OUT OF LIMITS IAW SRM 53- 00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE 1 REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0311361. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 1653) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 1653 STRINGER 28 - 29L. DAMAGE REMOVED IAW SRM 53-00- 01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE I REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0312332. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 1654) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1654 STRINGER 28 - 29L. THE DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00-01 REPAIR 6 AND SRM 51-20-01 REV 112, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE I REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0312331. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 1630) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 1630 STRINGER 27 - 28L. DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00- 01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE I REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0312331. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 1581) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1581 STRINGER 27 - 28L. DAMAGE BLENDED AND FOUND OUT OF LIMITS IAW SRM 53- 00-01 FIG 101 DETAIL II ALLOWANCE DAMAGE 1 REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0311361. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME SPLICE — GOUGED (BS 1520) · airframe 68,836 hrs · 25,096 cycles

AFT CARGO BAY BS 1520 STRINGER 24 - 25R, FRAME SPLICE FOUND DAMAGED. REMOVED AND REPLACED IAW SNRM N04012. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 1420-1423) · airframe 68,836 hrs · 25,096 cycles

MULTIPLE TOOL DAMAGE ON THE INTERIOR SKIN AT BS 1420 - 1423, STRINGER 25L - 26L. REPAIRED IAW EA F-5330-T0311215 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — GOUGED (BS 1360) · airframe 68,836 hrs · 25,096 cycles

AFT CARGO BAY FRAME BS 1360 STRINGER 23 - 24L OUTER FLANGE GOUGED. REPAIRED IAW EA F5310-T0311806 P1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 68,836 hrs · 25,096 cycles

THERE IS A CRACK AT FWD CARGO DOOR EXTERIOR SKIN AT LOWER AFT CORNER BS 600 - 620 STRINGER 25 - 26R. REPAIRED IAW EA F-5230-T0311723. REPAIR CLASSIFED AS MAJOR.

Part: SKIN — CRACKED (L4 DOOR) · airframe 68,836 hrs · 25,096 cycles

L4 DOOR INTERNAL HANDLE BOX CUT OUT AFT EDGE INNER SKIN FOUND CRACKED AT EDGE. REPAIRD IAW EA F-5210-T0311310 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,836 hrs · 25,096 cycles

AFT CARGO COMPARTMENT STATION 1380 BL0 - RBL 15 FRAME FLANGE HAS CORROSION. COMPLIED AS PER EA F-5310 - T0311624 PT 1. TITLE : FUSELAGE - MAINFRAME - REPAIR FOR OUT OF LIMIT BLEND OUT CORROSION AT FREE FLANGE OF STA 1380 146N1028-88 BOTTOM FRAME AND 146N8511-2 INNER CHORD. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,836 hrs · 25,096 cycles

AFT CARGO COMPARTMENT STATION 1380 RBL 10 FRAME UPPER CHORD FOUND CORROSION DURING REMOVING CORROSION AT FRAME FLANGE IAW SNRM N03563. COMPLIED AS PER EA F-5310-T0311624 P1 TITLE: FUSELAGE - MAINFRAME - REPAIR FOR OUT OF LIMIT BLEND OUT CORROSION AT FREE FLANGE OF STA 1380 146N1028-88 BOTTOM FRAME AND 146N8511-2 INNER CHROD. REPAIR CLASSIFIED AS MAJOR

Part: SKIN — GOUGED (FUSELAGE) · airframe 68,836 hrs · 25,096 cycles

EXISTING REPAIR FINDING FUSELAGE THERE IS GOUGE ON THE INTERIOR SURFACE OF THE DOUBLER OF THE EXISTING REPAIR AT STATION 1350 STRINGER 29L - 28R. REMOVED BY HAND CLEAN & TREATED PER SRM 51-10-01 REV 112 AND SRM 51-20-01 REV 112. NEW REPAIR CARRIED OUT PER FEDEX EA F-5330-T0312050 PT1, TITLE: FUSELAGE - PLATES AND SKINS - EXTERNAL DOUBLER REPAIR @ BS - 1350 & STR 29L - 28R - REPAIR. REPAIR CLASSIFIED AS MAJOR

Part: SKIN — GOUGED (BS 1701-1720) · airframe 68,836 hrs · 25,096 cycles

GOUGES ON EXTERIOR SURFACE OF THE REPAIR DOUBLER BS 1701 - 1720 STRINGERS 28 - 30R. REPAIRED IAW EA F-5330-T0310832. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — GOUGED (BS 1420) · airframe 68,836 hrs · 25,096 cycles

AFT CARGO BAY BS 1420 STRINGERS 28 - 29R FRAME UPPER FLANGE GOUGED. LENDED AND FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL III ALLOWANCE DAMAGE I REV 112. REPAIRED IAW EA F-5310-T0311467 PT1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CRACKED (R4 DOOR) · airframe 68,836 hrs · 25,096 cycles

R4 DOOR INNER SKIN LIGHTNING HOLE FOUND CRACK & CHAFED AT EDGE. REPAIRED.

Part: FRAME — DENTED (BS 680) · airframe 68,836 hrs · 25,096 cycles

FORWARD CARGO BAY BS 680 STRINGER 26 - 27L FRAME UPPER FLANGE DENTED. REPAIRED IAW EA F-5310-T0311435 P1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 669) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE SKIN HAS A LIGHTNING STRIKE AT BS 669 STRINGER 24 - 25L. REPAIRED IAW SRM 53-00-01 REPAIR 6 REV 112 AND FOUND OUT OF SRM 53-00-01 ALLOWABLE DAMAGE 1 REV 112 LIMITS. PART 1 OF EA F-5330-T0311464 REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 660-680) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE EXTERIOR SKIN THERE IS A LIGHTNING STRIKE AT BS 660 - 680 STRINGER 9- 10L. REPAIRED IAW EA F-5330-T0311888 PART 1. REPAIR CLASSIFIED MAJOR AS PER FEDEX GMM 6-2-100.

Part: FRAME — CHAFED (BS 1480) · airframe 68,836 hrs · 25,096 cycles

AFT CARGO BAY BS 1480 STRINGER 29R FRAME UPPER FLANGE CHAFED. REPAIRED IAW EA F-5310-T0311313 REV A P1. REPAIR MLASSIFIED AS MAJOR.

Part: FRAME — CORRODED (BS 1460) · corrosion level 2 · airframe 68,836 hrs · 25,096 cycles

AFT CARGO BAY BS 1460 STRINGER 26R FRAME UPPER FLANGE HAS CORROSION. CORROSION REMOVED AND TREATED IAW SRM 51-10-02 REV 112 AND 51-20-01 REV 112. FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG. 101 ALLOWABLE DAMAGE 2 REV 112. REPAIRED IAW EA F-5310-T0311233 PT1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 68,836 hrs · 25,096 cycles

LEFT WING, AFTER FILL PORT REMOVAL, UPPER SKIN UPPER SURFACE FOUND CORRODED AT OVERWING FILL PORT ADAPTER MATING AREA. CORROSION REMOVED AND TREATED PER SRM 51-20-01 AND 51-10-02 REV 112. REPAIR WAS CARRIED OUT IAW EA F-5730-T0310960 PT1 . REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 68,836 hrs · 25,096 cycles

RIGHT WING OTBD TE MAIN FLAP NOSE SKIN FOUND CHAFED STATION 494. REPAIRED IAW EA F-5750-T0311846 P1. REPAIR CLASSIFIED AS MINOR.

Part: SKIN — DAMAGED (BS 1568) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 1568 STRINGER 27L - 28L. BLENDED AND FOUND OUT OF SRM 53-00-01 FIG 101 DETAIL II REV 112 LIMIT. NEW REPAIR CARRIED OUT PER PART 1 OF EA F-5330-T0311361. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — CHAFED (BS 1640) · airframe 68,836 hrs · 25,096 cycles

BS 1640 STRINGER 5 - 6R FRAME INNER FLANGE FOUND CHAFED. REPAIRED IAW EA F-5310-T0312191 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE EXTERIOR SKIN THERE IS A LIGHTNING STRIKE AT STATION 1156 STRINGER 1 - 2R. LIGHTNING STRIKE REMOVED, FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 112 & REPAIR CARRIED OUT AS PER 53-00-01 FIG 201 REPAIR 16 REV 112. THIS IS A CAT B REPAIR WITH THRESHOLD 29000 F/C FROM TIME OF REPAIR REQUIRE LFEC REPEAT INSPECTION INTERVAL AT 3000 F/C. REPAIR CLASSIFIED AS MAJOR

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE EXTERIOR SKIN THERE IS A LIGHTNING STRIKE AT STATION 1218 STRINGER 1 - 2 R. LIGHTING STRIKE REPAIR CARRIED OUT AS PER EA F-5330-TO311504 PART 1, TITLE: FUSELAGE - PLATES & SKINS - (02 EA) LIGHTNING STRIKE DAMAGE AT BS 1220, BETWEEN STRINGER S1-S2R. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE EXTERIOR SKIN THERE IS A LIGHTNING STRIKE AT STATION 1222 STRINGER 6L - 7L. REPAIR CARRIED OUT AS PER EA F-5330-T0311570 PART 1, TITLE: AD 2008-06-14-FUSELAGE-PLATES & SKINS - REPAIR FOR LIGHTNING STRIKE DAMAGE AT STA 1222 STR 6L TO STR 7L. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,836 hrs · 25,096 cycles

FUSELAGE EXTERIOR SKIN THERE IS A LIGHTNING STRIKE AT STATION 1218 STRINGER 1 - 2R. LIGHTNING STRIKE REPAIR CARRIED OUT AS PER EA F-5330-T0311504 PART 1, TITLE: FUSELAGE - PLATES & SKINS - (02 EA.) LIGHTNING STRIKE DAMAGE AT BS 1220 BETWEEN STRINGER S1-2R. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,836 hrs · 25,096 cycles

EXISTING DENT FUSELAGE THERE IS A DENT AT STATION 1540 - 1560 STRINGER 17R - 18R. EXISTING DENT ON FUSELAGE SKIN AT STA 1540 - 1560 STR 17R - 18R FOUND OUT OF SRM LIMITS PER SRM 53-00-01 FIG 101. DETAIL II ALLOWANCE DAMAGE I REV 112. REPAIR CARRIED OUT PER SRM 53-00-01 FIG 201 REPAIR 16 REV 112. THIS REPAIR IS A CAT B REPAIR, THREHOLD 16000 F.C FROM THE TIME OF REPAIR & REPEAT INSPECTION LFEC AT INTERVAL 3000 FC REPAIR CLASSIFIED AS MAJOR

Part: DOOR FRAME — CHAFED (FUSELAGE) · airframe 68,836 hrs · 25,096 cycles

CABIN STATION 685 STRINGER 8L TO 9L L2 DOOR CUT OUT FWD FRAME FOUND CHAFED AT INNER SURFACE.

Part: FRAME — SCRATCHED (FUSELAGE) · airframe 68,836 hrs · 25,096 cycles

EXISTING REPAIR FINDINGS AFT CARGO THERE ARE SCRATCHES ON THE EXISTING REPAIR FRAME DOUBLER AT STATION 1340 STRINGER 26R - 27R. EXISTING REPAIR AT AFT CARGO FRAME STA 1340 STR 26R - 27R. REMOVED & NEW REPAIR CARRIED OUT PER EA F-5310-T0310693 PT 1. TITLE: FUSELAGE - MAINFRAME - EXISTING REPAIR, FUSELAGE FRAME INBD CHORD REPAIR, STA 1340, S25R - S27R. REPAIR CLASSIFIED AS MAJOR

Part: ATTACH FITTING — DAMAGED (NR 1 PYLON) · airframe 68,836 hrs · 25,096 cycles

NUMBER 1 PYLON AFT ENG MOUNT BULKHEAD FITTING FWD & AFT SHEAR PIN BUSHING HOLES FOUND OUT OF DWG TOLERANCE. ACCOMPLISHED EA F-5450-T0310618 P1. TITLE NACELLES / PYLON - PYLONS STRUCTURES - SB - 757-71-0093 - OVERSIZED MOUNT HOLES ON NR 1 & NR 2 STRUT AFT ENGINE MOUNT BULKHEAD FITTING. REPAIR CLASIFIED AS MAJOR.

Part: FITTING — DAMAGED (NR 2 PYLON) · airframe 68,836 hrs · 25,096 cycles

NR 2 PYLON AFT ENG MOUNT BULKHEAD FITTING FWD SHEAR PIN BUSHING HOLE FOUND OUT OF DWG TOLERANCE. ACCOMPLISHED EA F-5450-T0310618 P1. TITLE NACELLES / PYLON - PYLONS STRUCTURES - SB - 757-71-0093 - OVERSIZED MOUNT HOLES ON NR 1 & NR 2 STRUT AFT ENGINE MOUNT BULKHEAD FITTING. REPAIR CLASIFIED AS MAJOR.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 68,836 hrs · 25,096 cycles

EXISTING REPAIR FINDING FUSELAGE THERE ARE TOOL MARKS ON STRINGER 29R. EXISTING REPAIR AT STATION 1701 - 1720 STRINGER 28R - 30. STRINGER REPAIR CARRIED OUT IAW PART 1 OF EA F-5310-T0310856. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 68,836 hrs · 25,096 cycles

CABIN STATION 1276 - 1290 LBL 24.75 SEAT TRACK CROWN FOUND CHAFED. CHAFE MARK REMOVED PER SRM 51-10-02 REV 112. CLEANED UP DEPTH OF 0.040" FOUND OUT OF LIMITS 0.020" PER SRM 53-00-52, ALLOWABLE DAMAGE 1 FIG 101 REV 112. REMOVED AND REPLACED BY NEW FABRICATED SEAT TRACK PER BOEING DRAWING 146N5120 SHT 28 REV A & SHT 28 REV-. NEW SEAT TRACK FABRICATED AS PER BOEING DRAWING 146N5133 SHT 2 REV-. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,836 hrs · 25,096 cycles

CABIN STATION 680 - 700 RBL 24.75 SEAT TRACK INNER FLANGE FOUND CORROSION. EVALUATED & FOUND MORE THAN 50% MATERIAL LOST. R & R BY NEW FABRICATED SEAT TRACK SUPPORT IAW DWG 143N5080 SHEET 24 REV C. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 68,836 hrs · 25,096 cycles

CABIN STATION 1210 - 1230 LBL 24.75 SEAT TRACK CROWN FOUND CHAFED. CHAFFED MARK REMOVED AS PER SRM 51-10-02 REV 112. CLEAN UP TO DEPTH OF 0.026" FOUND EXCEED CROWN LIMIT OF 0.020" AS PER SRM 53-00-52. ALLOWANCE DAMAGE 1 FIG 101 REV 112. SEAT TRACK ST STA 1180 - 1320 LBL 24.75 REMOVED AND REPLACED BY NEW FABRICATED SEAT TRACK AS PER DWG 146N5120 SHT 28 REV A & SHT 29 . REV NEW SEAT TRACK FABRICATED AS PER DWG 146N5133 SHT 2 REV - REPAIR CLASSIFIED AS MAJOR

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 68,836 hrs · 25,096 cycles

CABIN STATION 1030 - 1050 LBL 24.75 SEAT TRACK CROWN FOUND CHAFED. CHAFFED MARK REMOVED AS PER SRM 51-10-02 REV 112. CLEANED UP DEPTH OF 0.030" FOUND EXCEED CROWN LIMIT 0.020" AS PER SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 REV 112. SEAT TRACK CROWN SECTION BETWEEN STA 1030 TO STA 1070 LBL 24.75 REMOVED AND REPLACED BY SEAT TRACK CROWN. REPAIR AS PER SRM 53-00-52 FIG 201 REPAIR 4 REV 113. REPAIR CLASSIFIED AS MAJOR.

Part: BUSHING — MIGRATED (NR 1 PYLON) · airframe 68,836 hrs · 25,096 cycles

NR 1 PYLON NAC STRUT UPPER SPAR FITTING OUTBD LUG BUSHINGS MIGRATED. NR 1 PYLON NAC STRUT UPPER SPAR FITTING OUTBOARD LUG HOLE REPAIR & BUSHING REPLACEMENT CARRIED OUT AS PER SRM 54-51-90 REPAIR 3 FIG 201 REV 112. REPAIR CLASSIFIED AS MAJOR

Part: BUSHING — MIGRATED (NR 2 PYLON) · airframe 68,836 hrs · 25,096 cycles

PYLON NR 2 PYLON NAC STRUT UPPER SPAR FITTING OTBD LUG BUSHING MIGRATED.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 68,836 hrs · 25,096 cycles

CABIN STATION 1585 RBL 24.75 SEAT TRACK OTBD FLANGE FOUND ONE EACH ELONGATED HOLE. R & R BY NEW FABRICATED SEAT TRACK IAW DWG 146N5120 SHT 30 REV. NEW SEAT TRACK FABRICATED IAW DWG 146N5137 SHT 2 REV. REPAIR CLASSIFIED AS MAJOR.