N966FD

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 76,239 hrs · 30,012 cycles

CAPTAINS NO. 1 WINDSHIELD HAS SMALL AREA OF ARCING . REPLACED CAPTAINS FWD WINDSHIELD REF AMM 56-11-01-4 UP THRU STEP 3.E.(21).(C).

Part: WINDOW — BURNED (L1) · airframe 76,239 hrs · 30,011 cycles

IN CRUISE, CAPTAIN FWD WINDSHIELD ARCING AND BURN MARKS. WINDOW HEAT EICAS MESSAGE. COMPLIED WITH QRH AND NO FURTHER ISSUES. ***EMERGENCY DECLARED*** DAMAGE TO OUTER PANE ONLY EA AND MEL APPLIED FOR FLIGHT TO IND FOR L1 WINDOW REPLACEMENT

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 75,842 hrs · 29,708 cycles

RH AFT FLAP IN INBD UPPER TRAILING EDGE DISBONDED REPAIRED TRAILING EDGE FLAP AS REQUIRED PER 757 SRM 57-53-01-2R (REPAIR 1, FIG 201, SHEET 5)AND SRM 51-70-05.

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 75,842 hrs · 29,708 cycles

LH AFT FLAP IN INBD UPPER TRAILING EDGE DISBONDED REPAIRED TRAILING EDGE FLAP AS REQUIRED PER 757 SRM 57-53-01-2R (REPAIR 1, FIG 201, SHEET 5)AND SRM 51-70-05.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 75,837 hrs · 29,702 cycles

TAXING IN AFTER LANDING, WHILE MAKING THE LEFT TURN FROM TAXIWAY C ONTO C8, THE TILLER LOST RESPONSIVENESS FOLLOWED BY A MASTER CAUTION ALERT AND L HYD SYS PRESS EICAS MESSAGE. VERIFIED ZERO HYD QUANTITY AND PRESSURE. COORDINATED A MX TOW IN WITH COMPANY AND GROUND. REMOVED AND REPLACED HYDRAULIC FLEXIBLE LINES AT ELBOW BACE4BN0404T IAW AMM 20-10-10-4. REPLENISHED LEFT HYDRAULIC SYSTEM IAW AMM 12-12-01. PERFORMED LEAK AND OPS CHECK IAW AMM 32-32-00-5. OPS CHECK GOOD, NO LEAKS OR DEFECTS NOTED. CYCLED LEFT ELECTRIC HYDRAULIC MOTOR IAW AMM 29-11-00-5, OPS CHECK GOOD, NO DEFECTS NOTED. PERFORMED #1 ENGINE IDLE RUN IAW AMM 71-00-00-2. OPS CHECK GOOD, NO DEFECTS NOTED. REINSPECTED LEFT HYDRAULIC SYSTEM DPI'S IAW AMM 29-11-00-6, NO DEFECTS NOTED. SERVICED LEFT HYDRAULIC SYSTEM TO FULL AFTER OPS CHECKS IAW AMM 12-12-01. A/C OK FOR SERVICE.

Part: GIRT BAR — FAULTED · airframe 75,611 hrs · 29,559 cycles

ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS - INOP. VISUALLY VERIFIED ENGAGED PRIOR TO EACH DEPARTURE.

Part: SLIDE — OUT OF ALIGNMENT (R1 DOOR) · airframe 75,611 hrs · 29,559 cycles

MDIS 966 52-10 7355 09JUN22 PAE OPEN U R1 DOOR SLIDE WILL NOT ENGAGE MEL 09JUN22 02:32 PAE U RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 12JUN22 "MEL 52-11-01-A: _R1____ (IDENTIFY L1 OR R1 DOOR OR SLIDE) - ___INOP______ (IDENTIFY INOP OR MISSING)." INSTALLED PLACARD VERIFIED DOOR SECURE. A/C OKAY FOR SERVICE FACT 10JUN22 19:12 MEM FOUND R1 DOOR ESCAPE SLIDE PARTIALLY UNSTOWED. REMOVED AND REPLACED R1 DOOR SLIDE IAW B757MM 25-66-01-4. PERFORMED OPS CHECK OF GIRT BAR MECHANISM IAW B757MM 52-11-25-5. ALL TEST PASSED. A/C OK FOR SERVICE.PART - SLIDE/RAFT EVAC SYSTEM MANF - SAFETECH P/N - D30654-122 SER NO. - 1856

Part: BOTTLE — EMPTY (DOOR SLIDE) · airframe 74,936 hrs · 29,045 cycles

DUE TO PARTCIAL DEPLOY OF R/H MAIN DOOR SLIDE FOUND EMERGENCY BOTTLE IN CEILING (L/H BOTTLE) FOR R/H MAIN DOOR , DEPLETED. REMOVED AND REPLACED R/H EMERGENCY POWER CYLINDER REF AMM: 52-11-30-4 OP'S CHECK GOOD. REF WRITE NUMBER : 52-10/ 6560 FOR ORIGINAL DOOR W/U.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 74,866 hrs · 28,992 cycles

DOT(137-05) LH WING I/B MAIN FLAP UPPER SURFACE HAS SEVERAL HAIL DAMAGED. REPAIRED L/H WING I/B MAIN FLAP UPPER SURFACE IAW SRM 57-53-01-1A AND 51-70-07, MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 74,866 hrs · 28,992 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL 231MGF IS DELAMINATED AND DAMAGED. FABRICATED FLOOR PANEL 231MGF ON VT MAE TRAVELER T21/1551858 IAW DWG SRZ-25-005 REV R. MAJOR REPAIR

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 74,866 hrs · 28,992 cycles

LH MAIN CARGO COMPT FLOOR PANEL 231MCF IS DELAMINATED AND DAMAGED. FABRICATED FLOOR PANEL 231MCF ON VT MAE TRAVELER T21/1551856 IAW DWG SRZ-25-005 REV R. MAJOR REPAIR

Part: DRAG FITTING — CRACKED (NR 1 NACELLE) · airframe 74,866 hrs · 28,992 cycles

#1 PYLON INBD DRAG FITTING HAS A CRACK INDICATION AT #3 HOLE. ACCOMPLISHED EA #F-5740-T0361812, TITLE: WINGS-ATTACH FITTINGS-DRAG FITTING #3 CRACKED HOLE-FEDEX EO F-5730-E0340076 PART 1 REV B- BOEING SB757-57A0073 STEPS 1 AND 2, MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (LAVATORY) · airframe 74,866 hrs · 28,992 cycles

LAVATORY FLOOR PANEL 221BF DELAMINATED. FABRICATED FLOOR PANEL 221BF ON VTMAE TRAVELER #T21/1550763 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 74,866 hrs · 28,992 cycles

COURIER FLOOR PANEL 222MAF DELAMINATED. FABRICATED ZONE 220 COURIER FLOOR PANEL 222MAF ON VTMAE TRAVELER # T21/1550761 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 74,866 hrs · 28,992 cycles

COURIER FLOOR PANEL 221MBF DELAMINATED. FABRICATED ZONE 220 COURIER FLOOR PANEL 221MBF ON VTMAE TRAVELER #T21/1550764 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 74,866 hrs · 28,992 cycles

MAIN CARGO COMPT FLOOR PANEL 231MSF HAS A DAMAGED AREA LOCATED AT FWD LH EDGE . FABRICATED FLOOR PANEL 231 MSF ON TRAVELER T21/1551857 IAW SRZ-25-005 REVISION R MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (MAIN CARGO DECK) · airframe 74,866 hrs · 28,992 cycles

MCD FLOORBOARD PNL 232 MTF HAS DAMAGE. FABRICATED MCD FLOORBOARD 232 MTF ON TRAVELER # T21/1551859 IAW DWG SRZ-25-005 REVESION R MAJOR REPAIR

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,246 hrs · 27,868 cycles

STA 580 FLOORBEAM CRACKED - LBL45 , UPPER CORD AFT FLANGE. COMPLIED WITH EA F- 5310 - T0346588 P1 TITLE : FUSELAGE MAINFRAME STA.580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,246 hrs · 27,868 cycles

CORROSION ON SEAT TRACK FLANGE STA 1640 RBL 45.5 MAIN CARGO CABIN. REMOVED CORROSION AT SEAT TRACK FLANGE STA 1640 RBL 45.5, IAW SRM 51-10-02-OG EVALUATED AREA DAMAGE, ORIGINAL MAT. 0.070", REMAINING MAT. 0.035",MAT LOSS 0.035" FOUND TO BE OUT LIMITS IAW SRM 53-00-52-1A FIG 101 DETAIL VII. REMOVED DAMAGED SECTION, LOCATED DRILLED,TRIMMED AND INSTALLED NEW SECTION SEAT TRACK AT STA 1540 TO STA B1640 RBL 45.5 IAW B DWG 146N5128 REV - ,REV A AND SRM 51-40-02-OG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,246 hrs · 27,868 cycles

CORROSION FOUND ON FLOOR SHEAR WEB MAIN CARGO CABIN STA 1688 LBL 57. REMOVED CORROSION AT FLOOR SHEAR WEB STA 1688 LBL 57 IAW SRM 51-10-02-OG ORIGINAL MAT. 0.071", MATERIAL REMAINING 0.058", MATERIAL LOSS 0.013", EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A, DETAIL III, FIG 101, FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW SRM 53-60-51-2R, REP 2 ALT I FIG 201 APPLIED TOP COATED PARTS AND AREA IAW AMM 51-21-15-7.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,246 hrs · 27,868 cycles

CORROSION FOUND ON SHEAR WEB MAIN CARGO CABIN STA 1701 LBL 55.0. REMOVED CORROSION AT SHEAR WEB STA 1701 LBL 55.00 IAW SRM 51-10-02-OG ORIGINAL MAT. 0.071",MATERIAL REMAINING 0.038",MATERIAL LOSS 0.033",EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A,DETAIL III ,FIG 101,FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW SRM 53-60-51-2R,REP 2 ALT I FIG 201 APPLIED TOP COATED PARTS AND AREA IAW AMM 51-21-15-7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,246 hrs · 27,868 cycles

CORROSION FOUND STA 1681 RBL 13 FLOORBEAM UNDER LIP OF THE TOP "T" CAP. COMPLIED WITH EA F-5310-T0346723 P1. TITLE: FUSELAGE-MAINFRAME - CORROSION ON STA 1681 FLOORBEAM UPPER CHORD, REINFORCING REPAIR, BL 0 TO RBL 45.7.

Part: DECK PLATE — CORRODED (BS 1716) · corrosion level 2 · airframe 73,246 hrs · 27,868 cycles

CORROSION ON EXISTING REPAIR FLOOR WEB MAIN CABIN STA 1716 FROM RBL 45 TO BLO. COMPLIED WITH EA F-5310-T0346613 P1.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 73,246 hrs · 27,868 cycles

CORROSION T CAP FLOOR BEAM MAIN CABIN STA 1681 RBL 32.0 COMPLIED WITH FEDEX EA # F-5310-T0346723 P1.

Part: SHEAR WEB — CORRODED (BS 1681) · corrosion level 2 · airframe 73,246 hrs · 27,868 cycles

CORROSION SHEAR WEB AFT WEB AREA STA 1681 RBL 32. REMOVED CORROSION ON SHEAR WEB IAW SRM 51-10-02-0G. EVALUATED DAMAGED AREA, FOUND TO BE OUT LIMITS IAW SRM 53-00 00-51-1A,FIG 101, DETAIL III. CUT OUT DAMAGED AREA, FABRICATED, LOCATED, DRILLED, AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-60-51-2R, FIG 201, DETAIL I, REPAIR 2, ALT II.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,837 hrs · 27,594 cycles

COCKPIT CEILING EMERGENCY LIGHT WILL NOT TEST. RELAMPED AND OPS CHECK NORMAL REF MM 33-51-09-3. A/C OK FOR SERVICE.

Part: BUSHING — BENT (GIRT BAR) · airframe 72,579 hrs · 27,422 cycles

L1 DOOR DIFFICULT TO DISARM. L1 DOOR WILL NOT OPEN. APEARS THAT GIRT BAR HAS DROPPED FROM BOTTOM OF DOOR AND WAS JAMMED ALONG THE FLOOR. REPLACED THE L1 DOOR GIRT BAR FORWARD MECHANISM SPRING, BUSHINGS AND BOLT. OPS CHECKED GOOD IAW AMM 52-11-25-5.

Part: SENSOR — OUT OF ADJUST (L1 DOOR) · airframe 71,696 hrs · 26,798 cycles

LEFT FWD ENTRY DOOR WHEN OPEN, DOES NOT SHOW OPEN ON THE OVERHEAD PANEL OR EICAS SCREEN. CLEANED AND ADJUSTED THE L1 ENTRY DOOR SENSOR IAW AMM 52-71-00-5. OPS CHECKED GOOD.

Part: LINER — OUT OF ADJUST (L1 DOOR) · airframe 71,401 hrs · 26,590 cycles

L1 ENTRY DOOR ARMING LEVER INDICATOR DOES NOT FULLY RETRACT WHEN DOOR IS DISARMED. ADJUSTED L1 DOOR LINING IAW MM 52-11-02-4 . OPS CHECKED GOOD.

Part: LEVER — MALFUNCTIONED (L1 DOOR) · airframe 71,231 hrs · 26,467 cycles

L1 DOOR ARMED INDICATOR HANDLE DOES NOT RECEDE FLUSH WITH DOOR PANEL IN THE DISARM POSITION. ACCOMPLISHED AN OPS CHECK OF THE L1 DOOR, DOOR ARMED INDICATOR WILL RETURN TO FLUSH. UNABLE TO DUPLICATE IAW AMM 52-11-00-0.

Part: LANYARD — TANGLED (EVAC SLIDE) · airframe 70,648 hrs · 26,034 cycles

ON BLOCK IN, FIRST OFFICER WAS UNABLE TO CONFIRM RT ENTRY DOOR DISARMED. WHEN HANDLE IN ARMED POSITION THE ARMED LIGHT DOES NOT COME ON. WHEN HANDLE MOVED TO DISARM POSITION, TAB MOVES IN BUT HANDLE DOES NOT MOVE ALL THE WAY TO DISARM. VISUALLY INSPECTED R1 DOOR EVAC SLIDE GIRT BAR & FOUND FWD SLIDER BAR HAD LANYARD & D RING TANGLED, PREVENTING PROPER ENGAGEMENT OF FWD GIRT BAR SLIDER. STOWED LANYARD & D RING BACK IN VELCRO POUCH SECTION OF SLIDE & OPERATIONS CHECKED NORMAL IAW AMM 25-66-10-2. OK TO CONTINUE.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 700 hrs · 25,609 cycles

UPON REMOVAL OF PROTECTIVE COVERING ON THE RCB SHEAR PLATE BETWEEN BS 400 - 440, RBL 24.75 - 45.50 FOUND CORROSION. COMPLIED WITH EA F-5310-T0317046 REV.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 700 hrs · 25,609 cycles

UPON REMOVAL OF PROTECTIVE COVERING ON THE RCB SHEAR PLATE BETWEEN BS 400 - 440, LBL 45.50 - 24.75 FOUND CORROSION. COMPLIED WITH EA F-5310-T0317067 REV A.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 700 hrs · 25,609 cycles

UPON REMOVAL OF PROTECTIVE COVERING ON THE RCB SHEAR PLATE BETWEEN BS 400 - 440, BL 0 TO RBL 24.75 FOUND CORROSION. COMPLIED WITH EA F-5310-T0316995 REV.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 700 hrs · 25,609 cycles

UPON REMOVAL OF PROTECTIVE COVERING ON THE RCB SHEAR PLATE BETWEEN BS 400 - 440, LBL 24.75 TO BL 0 FOUND CORROSION. COMPLIED WITH EA F-5310-T0317018 REV.

Part: LIGHT — DAMAGED (CABIN) · airframe 69,623 hrs · 25,279 cycles

EMERGENCY LIGHT, UNARMED LIGHT, INOPERATIVE. WHILE LAMPING THE LIGHT CAPSULE FELL APART. REQUIRES LIGHT ASSEMBLY. PANEL ASSEMBLY REQUIRED. R & R EMER LIGHTS, UNARMED, LIGHT ASSEMBLY IAW SMP. TESTED GOOD IAW MM 33-51-00-5.

Part: SKIN — DENTED (TE FLAP) · airframe 69,419 hrs · 25,121 cycles

LEFT INBD AFT FLAP OTBD UPPER SURFACE HAS HAIL DAMAGE. SANDED, CLEANED & PREPPED AREA AT LT INBD AFT FLAP OTBD UPPER SURFACE. APPLIED REPAIR TO FLAP IAW SRM 57-53-01, 51-70-17 & TOP COAT IAW MM 51-20-01 IAW EA F-57-50-T0308504.

Part: SKIN — DENTED (TE FLAP) · airframe 69,419 hrs · 25,121 cycles

RIGHT OTBD AFT FLAP UPPER TE INBD SIDE HAS HAIL DAMAGE. SANDED, CLEANED & PREPARED AREA IAW SRM 57-53-01 FIG 201, 51-70-17 PARA 4 C. APPLIED REPAIR TO FLAP RT OTBD UPPER TE INBD SIDE OF AFT FLAP IAW SRM 57-53-01, 51-70-17 & TOP COAT IAW AMM 51-00-01.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 69,012 hrs · 24,833 cycles

L1 WINDOW OUTER LAYER CRACKED AT FLT LV 400 -60C, AFTER 2.5 HRS OF FLIGHT. INSTALLED NEW L-1 WINDOW, FIRST TORQUE COMPLETED AT 2119Z. R & R L1 WINDSHIELD IAW AMM 56-11-01-4.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 68,743 hrs · 24,621 cycles

LOST LEFT HYD QTY AND LEFT HYD SYS PRESSURE AFTER POWER UP FOR TAKEOFF. RUDDER RATIO ON EICAS AND POWER TRANSFER UNIT ON STATUS CAME UP AS WELL. NO NOSE WHEEL STEERING AVAILABLE AFTER PTU AUTOMATICALLY CAME ON. APPEARS LOST ALL FLUID IN LEFT HYD. INSTALLED STEERING FLEX LINES ON NOSE GEAR TO BULKHEAD FITTING IAW AMM 20-10-10-4. RAN LT ENGINE REF JRH AND CYCLED ALL FLIGHT CONTROLS AND NOSE WHEEL STEERING. NO LEAKS NOTED. OK FOR SERVICE.

Part: SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 68,646 hrs · 24,559 cycles

LT FWD ENTRY DOOR LIGHT & EICAS MESSAGE COMES ON INFLIGHT. LT FWD ENTRY DOOR WARNING SENSOR SYS ADJUSTMENT CARRIED OUT IAW AMM 52-71-00, REV 106 FOUND GOOD. TESTING OF DOOR WARNING SYS FOR NR 1 PASSENGER DOOR FOUND GOOD IAW AMM 52-71-00, REV 106.

Part: SPAR — CORRODED (ZONE 600) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

IAW EO F-2822-7-5009 PART 3, STEP B1. C (PAGE 16 OF 33). CORROSION AT RT AFT WING SPAR SURFACE. REMOVED AND SPAR WEB THICKNESS FOUND LESS THAN THE MINIMUM. IAW EO F-2822-7-5009, PART 3, STEP B1. C (PAGE 16 OF 33). CORROSION AT RT AFT WING SPAR SURFACE REMOVED AND SPAR WEB THICKNESS FOUND LESS THAN THE MINIMUM. CORROSION REPAIRED IAW EA F-5710-162930, PART 1. MAJOR REPAIR.

Part: SKIN — DENTED (CARGO DOOR) · airframe 68,641 hrs · 24,554 cycles

CARGO DOOR OUTER SKIN AFT LOWER CORNER DENTED. REPAIRED IAW EA F-5230-166052 PART 1. MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

FUSELAGE EXTERIOR SKIN DENTED AT BS 1717.5 AND 0.5 INCHES BELOW S14L. REPAIRED IAW EA F-5330-162939 PART 1. MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 100) · airframe 68,641 hrs · 24,554 cycles

FUSELAGE EXTERIOR SKIN HAS A PROTRUDING DENT AT BS 746 THREE INCHES ABOVE S25R. REPAIRED IAW SRM 53-00-01, FIG.201, REPAIR 16, REV.108. CAT B, MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

AFTER PAINTING OBSERVED FUSELAGE EXTERIOR SKIN HAS A DENT AT BS 1695 AND 1 INCH ABOVE S15L. REPAIRED IAW EA F-5330-162939 PART 1. MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

FUSELAGE EXTERIOR SKIN DENTED BS 1698 AND 1 INCH BELOW S15L. REPAIRED IAW EA F-5330-162939 PART 1. MAJOR REPAIR.

Part: STRINGER — CORRODED (ZONE 100) · airframe 68,641 hrs · 24,554 cycles

AREA AFT OF AFT CARGO BS 1681-1701, S22R HAS CORROSION ON UPPER FLANGE. REPAIR CARRIED OUT ON CORRODED PART OF STRINGER S-22R AT STA 1681-STA 1701, IAW SRM 53-00-03 FIG.201 DETAIL I REPAIR 2 REV.108. REPAIR IS MAJOR.

Part: SHEAR TIE — DAMAGED (BS 1701) · airframe 68,641 hrs · 24,554 cycles

FOUND 0.200 GAP IN BETWEEN SKIN AND SHEAR TIE AT BS 1701 BETWEEN STRINGER 15 - 16 LEFT, ONLY ALLOWED FOR UP TO 0.040 MAXIMUM GAP. REMOVED AND REPLACED WITH NEW SHEAR TIE FABRICATED AS PER DWG 140N2002 SHT.4 REV.B AND INSTALLED AS PER DWG 146N1026 SHT.2 REV.D. MAJOR REPAIR.

Part: SKIN — DENTED (BS 1700) · airframe 68,641 hrs · 24,554 cycles

FUSELAGE EXTERIOR SKIN HAS A DENT AT BS 1700 AND 1 INCH ABOVE S15L. REPAIRED IAW EA F-5330-162939 PART 1. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

MAIIN DECK STA 365 FLOORBEAM UPPER TEE CORRODED AT RBL 4- 43.5. REMOVED AND REPLACED IAW EA 757-5315-08-E2035 REV.A.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

MAIN DECK BS 418 FLOORBEAM UPPER TEE FOUND ELONGATED HOLE AT LBL 34.5.

Part: FLOORBEAM — CORRODED (BS 377.7) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

MAIN DECK BS 377.7 FLOORBEAM UPPER TEE CORRODED AT RBL 6. REMOVED AND REPLACED IAW EA 757-5315-08-E2050 REV.

Part: FRAME — CORRODED (BS 1560) · airframe 68,641 hrs · 24,554 cycles

AFT CARGO RT SIDE FRAME, BS 1560 HAS CORROSION ON UPPER SURFACE OF LOWER WEB FLANGE BETWEEN STR 26R AND 25R. REPAIR CARRIED OUT IAW EA F-5310-155981. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

MAIN DECK BS 365 FLOORBEAM UPPER TEE CORRODED RBL 45. REMOVED AND REPLACED IAW EA 757-5315-08-E2035 REV.A.

Part: SKIN — DENTED (ZONE 100) · airframe 68,641 hrs · 24,554 cycles

FUSELAGE EXTERIOR SKIN HAS A DENT AT BS 743 AND 3 INCHES ABOVE S25R. REPAIRED IAW SRM 53-00-01 FIG.201, REPAIR 16, REV.108. REPAIR IS CAT B, MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

MAIN DECK BS 1320 FLOORBEAM UPPER ANGLE CORRODED AT FASTENER HOLES BETWEEN LBL 45 - 62. REPAIRED IAW EA 757-5365-08-E2130, REV.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

FLOORBEAM BS 365 RBL 24 CORRODED. REMOVED AND REPLACED IAW EA 5315-08-E2035 REV.A.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

MAIN DECK BS 1640 FLOORBEAM UPPER TEE UPPER SURFACE FOUND CORRODED AT RBL 56. R & R IAW EA 757-5365-08-E1970 REV.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 68,641 hrs · 24,554 cycles

FUSELAGE EXTERIOR SKIN LT SIDE THERE IS A SCRATCH AT STRINGER 14 L BETWEEN BS 1384 -1388. REPAIRED IAW EA F-5310-155980. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

CABIN STA 377 LBL 24 TO LBL 45 HAS CORROSION FLOORBEAM. REPAIRED IAW EA 757-5315-08-E2050 .

Part: FLOOR SUPPORT — DAMAGED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

MAIN DECK FLOOR SUPPORT HAS AN ELONGATED HOLE THROUGH FLOORBEAM AT BS 1640 JUST INBD OF RT DOOR SILL. REPAIRED IAW EA 757-5365-08-E1990.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

MAIN DECK BS 1640 FLOORBEAM UPPER TEE MISDRILLED LBL 19. REPAIRED IAW EA 757-5365-08-E1970 REV.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

MAIN DECK BS 1640 FLOORBEAM UPPER TEE SURFACE FOUND CORRODED FROM LBL 7 TO RBL 7. REPAIRED IAW EA 757-5365-08-E1970 REV.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

MAIN DECK BS 1320 FLOORBEAM UPPER ANGLE CORRODED AT RBL 21. REPAIRED IAW EA 757-5365-08-E2130 REV. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

STA 365 RBL 6 FLOORBEAM HAS CORROSION. REMOVED AND REPLACED IAW EA 757- 5315-08-E2035 REV.A

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

RIGHT CREASE BEAM SCRIBE LINED BETWEEN BS 1320 AND 1340. REMOVED AND REPLACED IAW DWG 148N8322 SHT.1 REV.F. DUE TO CORROSION (REF. SNRM N01735). REPAIR IS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

BS 1320 TO 1340 LBL 64 CORROSION AROUND FASTENER HOLES IN CREASE BEAM. REMOVED AND REPLACED CREASE BEAM FABRICATED AS PER DWG 146N8326 SHT.1 REV.C AND INSTALLED IAW DWG 146N8322 SHT.1. REV.F. REPAIR IS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

RIGHT CREASE BEAM CORRODED BETWEEN BS 1340 AND 1360. REMOVED AND REPLACED IAW DWG 146N8322 SHT.1. REV.F. REPAIR IS MAJOR.

Part: CREASE BEAM — CORRODED (BS 1241.5) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

MAIN DECK LT CREASE BEAM CORRODED AT BS 1241.5. REPAIRED IAW EA F-5360-155977. MAJOR REPAIR.

Part: SPAR — CORRODED (LT WING TE FLAP) · airframe 68,641 hrs · 24,554 cycles

LEFT WING OTBD T/E MAIN FLAP FRONT SPAR LOWER ANGLE UPPER SURFACE FOUND CORRODED AT TRACE AF BS 489 AFTER CLEANING. REPAIRED IAW EA F-5750-162936. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 940-1040) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

MAIN DECK CREASE BEAM INNER ANGLE, FOUND A NUMBER OF FASTENER HOLES CORRODED FROM BS 940 TO 1040. REMOVED AND REPLACED WITH NEW INNER ANGLE FABRICATED AS PER DWG 144N5152 SHT.1 REV.- AND INSTALLED IAW DWG 144N5140 SHT.1 REV.C. MAJOR REPAIR.

Part: WEB — CORRODED (L3 DOOR FRAME) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

CABIN- L3 DOOR SURROUND STRUCTURE FOUND MINOR SURFACE CORROSION AT UPPER SILL, BS 1318, S10L. WEB REMOVED AND REPLACED WITH NEW WEB FABRICATED AND INSTALLED IAW DWG 146N8321 STH.1 REV.E. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

RT CREASE BEAM LOWER SURFACE CORRODED AT BS 1300 - 1320. REMOVED AND REPLACED WITH NEW CREASE BEAM WEB FABRICATED AND INSTALLED IAW DWG 146N8322 SHT.1 REV.F. REPAIR IS MAJOR.

Part: WEB — CORRODED (L4 DOOR FRAME) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

MAIN DECK-L4 DOOR SURROUND INTERCOSTAL WEB FOUND CORRODED AT BS 1635, S11-12L. REMOVED AND REPLACED WITH NEW WEB FABRICATED AND INSTALLED IAW DWG 146N8733 SHT.1. REV.E. MAJOR REPAIR.

Part: WEB — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

MAIN DECK-R4 DOOR SURROUND INTERCOSTAL WEB FOUND CORRODED AT BS 1635, S11-12R. REMOVED AND REPLACED WITH NEW WEB FABRICATED AND INSTALLED IAW DWG 146N8733 SHT.1 REV.E. MAJOR REPAIR.

Part: RIB — CORRODED (ZONE 500) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

LEFT WS 670.27 T/E RIB FOUND CORRODED AT CONNECTION POINT TO INBD BONDING JUMPER. REPAIRED IAW EA F-5740-162932 PART 1. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 1340) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

MAIN DECK RT BS 1340 CREASE BEAM INNER CHORD CORRODED. R & R WITH NEW CREASE BEAM IAW DWG 146N8322 SHT 1, REV F, REPAIR IS MAJOR.

Part: STRINGER SPLICE — CORRODED (BS 660) · airframe 68,641 hrs · 24,554 cycles

FWD CARGO BAY RT SIDE STRINGER 28R HAS CORROSION INSIDE SPLICE JOINT AT BS 660. R & R WITH NEW SPLICE JOINT FABRICATED IAW DWG 143N3800 SHT.1 REV C AND INSTALLED IAW SERM 51-40-02 REV 108. REPAIR IS MAJOR.

Part: CREASE BEAM — CORRODED (BS 1320-1340) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

CABIN BS 1320 TO 1340, LBL 64 TO LBL 70 HAS CORROSION UNDERSIDE OF CREASE BEAM WEB. REMOVED AND REPLACED WITH NEW CREASE BEAM WEB FABRICATED AND INSTALLED IAW DWG 146N8322 SHT.1. REV.F. REPAIR IS MAJOR.

Part: SKIN — DENTED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

AFT FUSELAGE EXTERIOR SKIN AT BS 1848 STR 2-3L DENTED. REPAIRED IAW SRM 53-00-01 FIG. 201 REPAIR 16 REV.108. REPAIR IS CAT.B, MAJOR.

Part: SPLICE PLATE — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

NR 1 NACELLE STRUT PYLON STRUCTURE UPPER WEB INBD SPLICE PLATE AT PP 170.0, FOUND WITH CORROSION. REMOVED AND REPLACED IAW DWG 311N5040 REV.N. REPAIR IS MAJOR.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

LEFT, AFTER REMOVAL OF OVERWING FILL PORT ADAPTER, FOUND UPPER SKIN CORRODED AT MATING SURFACE TO OVERWING FILL PORT ADAPTER. REPAIRED IAW EA F-5710-155960. MAJOR REPAIR.

Part: FRAME — CORRODED (ZONE 100) · airframe 68,641 hrs · 24,554 cycles

AFT CARGO BAY LEFT SIDE FRAME BS 1360 HAS CORROSION ON FRAME UPPER FLANGE BETWEEN STR 25 AND 26L. REPAIRED FRAME FROM S16-25L IAW EA F-5310-163861, PART 1. REPAIR IS CAT B, MAJOR.

Part: SEAT TRACK — CORRODED (BS 365-386) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

MAIN DECK RBL 24 SEAT TRACK SUPPORT FLANGE FOUND CORRODED AT BS 365.25-386. R & R WITH NEW SEAT TRACK SUPPORT IAW DWG 141N5130, SHT 2, REV.E. REPAIR IS MAJOR.

Part: SEAT TRACK — CORRODED (BS 366) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

MAIN DECK RBL 45 SEAT TRACK SUPPORT FLANGE FOUND CORRODED AT BS 366. CORRODED SEAT TRACK REMOVED AND REPLACED WITH NEW SEAT TRACK IAW DWG 141N5130 SHT.2. REV.E. REPAIR IS MAJOR.

Part: SKIN — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

NR 1 NAC STRUT PYLON STRUCTURE INBD SKIN AT PP STA 185.0 FOUND WITH BULGING. SKIN REMOVED AND REPLACED IAW DWG 311N5002 SHT.14 REV.E, WITH ALTERNATE SKIN IAW REF EA F-5410-155964. MAJORREPAIR.

Part: SKIN — CORRODED (NR 4 SLAT) · airframe 68,641 hrs · 24,554 cycles

LEFT WING NR 4 L/E SLAT NOSE SKIN UPPER SURFACE FOUND CORRODED ADJACENT TO INBD MAIN TRACK FITTING. REPAIRED NR 4 L/E SLAT NOSE SKIN UPPER SURFACE IAW E/A F-5750-162925 PART 1. MAJOR REPAIR.

Part: SKIN — SCRATCHED (NR 4 SLAT) · airframe 68,641 hrs · 24,554 cycles

LEFT WING NR 4 SLAT NOSE SKIN MINOR SCRATCH. FOUND JUST INBD OF OTBD MAIN TRACK. REPAIRED IAW EA F-5750-162921, PART 1. MAJOR REPAIR

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 68,641 hrs · 24,554 cycles

SKIN AT BS 1550 BETWEEN STR 28 - 29 MISREPAIRED. REPAIRED IAW SRM 51-40-02, REV 108 AND SRM 53-00-01, FIG 201, REV 108, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

MAIN DECK RBL 45, SEAT TRACK FLANGE CORRODED AT BS 441. REPAIRED IAW EA 757-8365-08-E2100, REV. MAJOR

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

MAIN DECK LBL 45 SEAT TRACK FLANGE FOUND CORRODED AT BS 377.7. R & R WITH NEW SEAT TRACK FABRICATED IAW DWG 141N5131 SHT 1, REV A AND INSTALLED IAW DWG 141N5130, SHT 1, REV F. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

MAIN DECK LT CREASE BEAM WEB FOUND CORRODED BETWEEN BS 1080 AND 1100. R & R IAW DWG 144N5210, SHT 1, REV - AND INSTALLED IAW DWG 144N5200 SHT 1, REV B. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

MAIN DECK LT CREASE BEAM WEB CORRODED BETWEEN BS 1120 AND 1140. CORROSION REMOVED IAW SRM 51-10-02 REV 107. FOUND EXCEED 10 PERCENT LIMIT IAW SRM 53-40-13 ALLOWABLE DAMAGE 1, FIG 101, REV 108. CREASE BEAM WEB REMOVED IAW SRM 51-40-02, REV 108. NEW CREASE BEAM WEB FABRICATED IAW DWG 144N5210 SHT 1, REV --. NEW CREASE BEAM WEB INSTALLED IAW DWG 144N5200, SHT 2, REV B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

MAIN DECK LT CREASE BEAM WEB CORRODED BETWEEN BS 1100 AND 1120. R & R IAW DWG 144N5210 SHT 1, REV AND INSTALLED IAW DWG 144N5200, SHT 1, REV B. MAJOR REPAIR.

Part: DOUBLER — CORRODED (CREASE BEAM) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

MAIN DECK LT CREASE BEAM WEB DOUBLER CORODED BETWEEN BS 1060 AND 1080. CORRODED DOUBLER REMOVED AN REPLACED WITH NEW DOUBLER FABRICATED AS PER DWG 144N5211 REV.A AND INSTALLED IAW DWG 144N5200 SHT.1 REV.B. REPAIR IS MAJOR.

Part: DOUBLER — CORRODED (CREASE BEAM) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

MAIN DECK RT CREASE BEAM WEB DOUBLER CORRODED AT STA 312, RBL 64. CORRODED DOUBLER REMOVED. NEW DOUBLER FABRICATED AND INSTALLED IAW DWG 141N8422 SHT. 1 REV. R. REPAIR IS MAJOR.

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

MAIN DECK L1 DOOR SURROUND INTERCOSTAL WEB LOWER SURFACE CORRODED AT STA 315 TO STA 317, STR-16L. R & R WITH NEW WEB FABRICATED IAW DWG 141N8341, REV C AND INSTALLED IAW DWG 141N8341 SHT 6, REV C REPAIR IS MAJOR.

Part: SHEAR WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

CABIN FLOOR SHEAR WEB BS 1680-1685 , LBL 13.5 -25.5 DOUBLER FOUND SURFACE CORROSION. R & R IAW EA F-5310-162922, PART 1. MAJOR REPAIR.

Part: SHEAR WEB — DAMAGED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

MAIN DECK CABIN FLOOR SHEAR WEB FOUND CHIPPED AT BS 1700, RBL5. REPAIRED IAW SRM 53-60-51, FIG 201, ALTERNATE II, REPAIR 2, REV 108. REPAIR IS MAJOR.

Part: DECK PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

DECK PLATE AT BS 1680-1690 FROM LBL10-LBL 21.5 FOUND CORRODED. REPAIRED IAW EA F-5310-162922, PART 1. REPAIR IS MAJOR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

MAIN DECK SEAT TRACK CORRODED AT BS1640, RBL45. REPAIRED IAW SRM 53-00-52, FIG.201, REPAIR 1, OPTION 1, REV.108. MAJOR REPAIR.

Part: SKIN — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

NR 1 PYLON NAC STRUT STRUCTURE INBD ACCESS HOLE CUT-OUT INNER EDGES SKIN FOR PANEL NR 433LR AT PPSTA.181.0 FOUND WITH CORROSION. CORRODED SKIN PANEL R & R IAW DWG 311N5002, SHT 14, REV E WITH ALTERNATE SKIN IAW EA F-5410-155964. REPAIR IS MAJOR.

Part: DECK PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,641 hrs · 24,554 cycles

CORROSION FOUND ON DECK PLATE AT BS 1680-1690, RBL 10 TO LBL 10. REPAIRED IAW EA F-5310-162922, PART 1.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

MAIN DECK RBL24, SEAT TRACK END FLANGE FOUND CHAFING AT BS 1640. REPAIRED IAW SRM 53-00-52 FIG 201, REPAIR 1, OPTION1, REV 108. REPAIR IS MAJOR.

Part: SHEAR WEB — CORRODED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

MAIN DECK CABIN FLOOR SHEAR WEB BS 1717-1722, LBL 3-16 DOUBLER FOUND MINOR SURFACE CORROSION. DOUBLER REPLACED IAW EA 757-5365-08-E2004, REV A. MAJOR.

Part: SHEAR WEB — CORRODED (ZONE 200) · airframe 68,641 hrs · 24,554 cycles

MAIN DECK CABIN FLOOR SHEAR WEB STA 1680-1685, LBL3-RBL5 DOUBLER FOUND MINOR SURFACE CORROSION. R & R IAW EA F-5310-162922, PART 1. MAJOR REPAIR.

Part: SKIN — BULGED (NR 2 NACELLE) · airframe 68,641 hrs · 24,554 cycles

NR 2 NACELLE STRUT PYLON STRUCTURE INBD SKIN AT PPSTA 185.0 FOUND BULGING. REPAIRED IAW EA F-5450-16290, PART 1. AD 2004-12-07, EO F-5450-7-5003, SB 757-54-0035 R4. MAJOR REPAIR.