N976FD

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,050 hrs · 24,588 cycles

MDIS 976 33-50 4847 30MAY19 MCI FACT U THE RIGHT EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED THE RIGHT BATTERY PACK PER MM 33-51-07-2. OPS GOOD.

Part: O-RING — CUT (AILERON ACTUATOR) · airframe 64,047 hrs · 24,585 cycles

"C HYD QTY" DURING FLIGHT. HAPPENED IN CRUISE AT FL340. FLUCTUATED DOWN TO .08 DURING DESCEN. PARKED AT GATE WITH .26 UPON FURTHER TROUBLESHOOTING, FOUND O-RING CUT UNDER AILERON ACTUATOR CHECK VALVE ACCESS PLUG. REMOVED RT I/B ACTUATOR TO FOM REF. 27-11-20-2. REPLACED O-RING AND SAFETIED ACCESS PLUG. INSTALLED RT I/B AILERON ACTUATOR UP TO STEP H. (1) (A) REF. 27-11-20-2.

Part: TARGET — FAILED (L1 DOOR) · airframe 63,111 hrs · 23,960 cycles

L1 DOOR ARM SLIDE LIGHT DOES NOT ILLUMINATE WHEN ARMED. REMOVED AND REPLACED L1 DOOR GIRT BAR FWD PROX SWITCH TARGET REF MM 52-11-25-5 OP`S CHECKS GOOD. SWITCH TARGET INSTALLED REF MM 20-11-00-2.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 62,969 hrs · 23,857 cycles

FLIGHT DECK DOME/EMERGENCY LIGHT WILL NOT ILLUMINATE DURING TEST. RELAMPED REF MM 33-51-09-3. OPS CHECK NORMAL. A/C OK FOR SERVICE.

Part: SUPPORT BRACKET — CRACKED (RADOME) · airframe 62,915 hrs · 23,823 cycles

RADOME HOLD OPEN ROD STOWAGE SUPPORT BRACKET IS DAMAGED AND BENT. EVALUATED DAMAGED SUPPORT BRACKET ON RADOME HOLD OPEN ROD STOWAGE AREA, FOUND A CRACKED BRACKET. FOUND TO BE OUT LIMITS IAW SRM 53-10-08-1A, FIG 101, NOTE A, DETAIL XIII. REMOVED, FABRICATED AND INSTALLED A NEW SUPPORT BRACKET IAW DWG 141N7835, REV - AND F.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 62,915 hrs · 23,823 cycles

TWO DENTS AT THE LEFT HORIZONTAL STABILIZER UPPER SKIN. L/E HSS 100 AND 13 INCHES FROM L/E. PERFORMED REPAIR IAW SRM 51-70-10-2R, FIG 201.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,915 hrs · 23,823 cycles

CRACK STA 580 FLOORBEAM END FITTING APPROX LBL 45. COMPLIED WITH EA F-5310-T0338373 P1. FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,148 hrs · 22,603 cycles

REWORK OF SNRM N00079 WO 65679. MAIN CABIN COURIER SEAT TRACK LT, SEAT TRACK CORRODED LBL 6.8. REWORK DUE TO NO SDR, REPAIR CLASSIFICATION INCORRECT & INSPECTION BUYBACK AS NON RII. SDR ISSUED 16-0603, REPAIR CLASSIFIED AS MAJOR & RII IAW GMM 11-0-2700.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,148 hrs · 22,603 cycles

REWORK OF SNRM N00080 W/O 65679. MAIN CABIN COURIER SEAT TRACK CORRODED, RBL 13.95". REWORK DUE TO NO SDR ISSUED. NO REPAIR CLASSIFICATION SELECTED, BLOCK 17, SDR ISSUED, NR 16-0604. REPAIR CLASSIFIED AS MAJOR IAW GMM 11-0-2700.

Part: SKIN — DAMAGED (BS 600-620) · airframe 59,546 hrs · 21,536 cycles

FUSELAGE EXTERIOR SKIN HAD NUMEROUS NICKS & SCRATCHES BETWEEN STRINGERS 26L & 26R AT BS 600 - 620. BLENDED AND FOUND OUT OF LMITS IAW SRM 53-00-01 FIG.101 DETAIL II, REV.110. REPAIRED IAW EA 757-5331-08-08-E2502 REV-. REPAIR IS MAJOR.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 59,546 hrs · 21,536 cycles

AFT CARGO DOOR INNER SKIN, REPAIR DOUBLER GOUGED 14 INCHES FROM FWD EDGE & 12 INCHES FROM LOWER EDGE. REPAIRED IAW EA F-5230-T0305332 P1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DAMAGED (BS 460-480) · airframe 59,546 hrs · 21,536 cycles

FUSELAGE SKIN HAS NUMEROUS NICKS & SCRATCHES BETWEEN STRINGER 26L & STRINGER 26R AT BS 460 - 480. REMOVED IAW SRM 51-10-02 REV 110. BLENDED AREA, EVALUATED & FOUND OUT OF LIMIT IAW SRM 53-00-01 FIG 101 DET II REV 110. ACCOMPLISHED EA F-5330 T0 304978, PART 1, STEP 1.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

RT CREASE BEAM BS 1240 - 1260, WL 208.8 CORRODED. DWG 146N5590 SHT 1 REV F. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (AFT CARGO DOOR) · airframe 59,546 hrs · 21,536 cycles

AFT CARGO DOOR INNER SKIN, CORRODED .4 INCHES FROM FWD EDGE & 24 INCHES FROM LOWER EDGE. REPAIRED IAW EA F-5230-T0305332 P. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

FLOORBEAM, TOP TEE, BS 365, LBL 10 TO RT SIDE FRAME JOINT, WL 208.8 CORRODED. REPAIRED IAW EA 757-5315-08-E2471 REV A. REPAIR CLASSIFIED AS MAJOR.

Part: BULKHEAD — CHAFED (NR 1 NACELLE) · airframe 59,546 hrs · 21,536 cycles

NR 1 PYLON AFT BULKHEAD AFT SURFACE FOUND CHAFED LBL 1.75, WL 137.75. REPAIRED IAW EA F-5450-T0304928. REPAIR CLASSIFIED AS MINOR

Part: STRINGER — CORRODED (BS 1520) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

AFT CARGO BAY LT SIDE FRAME BS 1520, STRINGER 30 HAS CORROSION. REPAIRED IAW EA F-5310-T0305386 PART 1. REPAIR IS MAJOR.

Part: DOOR FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

AFT CARGO DOOR CUT OUT FWD FRAME BS 1380, FRAME HAS CORROSION ON AFT WEB BETWEEN STRINGER 23 & 24R. REPAIRED IAW EA F-5310-T0305241 P1. REPAIR CLASSIFIED AS MAJOR.

Part: PANEL — CORRODED (CENTER FUEL CELL) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

BS 1030 - 1040, LBL 60 FUEL TANK UPPER PANEL FOUND CORRODED. REPAIRED IAW E.A. F-5730-T0305134 PART 1. REPAIR IS MAJOR.

Part: SKIN — DAMAGED (BS 1681-1701) · airframe 59,546 hrs · 21,536 cycles

FUSELAGE SKIN, NICKED & SCRATCHED BETWEEN STRINGERS 12-13R BS 1681.8 - 1701. FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 110 AND REPAIRED IAW EA F-5330-T0305366 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

AFT CARGO COMPARTMENT RT SIDE STATION 1402 SPLICE STRAP & ATTACHING RIVETS HAS CORROSION BETWEEN STRINGER 28R & STRINGER 29R.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

AFT CARGO COMPARTMENT LT STATION 1402, SPLICE STRAP HAS CORROSION BETWEEN STRINGER 28L & STRINGER 29L.

Part: BULKHEAD — GOUGED (APU BAY) · airframe 59,546 hrs · 21,536 cycles

APU COMPARTMENT RT SIDE HAS A GOUGE AT BS 1885, WL 203, RBL 7 INCHES. REPAIRED IAW SRM 53-80-08, FIG 201 REPAIR 2 REV 110.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

CORROSION AT THE FLOORBEAM TOP TEE BS 345, RBL 53 TO RT SIDE DOOR FRAME JOINT WL 208.8. REPAIRED IAW EA F-5310-T0304808 PART 1. MAJOR REPAIR.

Part: WEB — CRACKED (NR 1 NACELLE) · airframe 59,546 hrs · 21,536 cycles

NR 1 PYLON, FOUND CRACKED ON LOWER STEEL WEB DURING NDT CHECK. WEB REPLACED IAW DWG 311N5042 SHT 2 REV H. REPAIR CLASSIFIED AS MAJOR.

Part: WEB — CORRODED (ZONE 400) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

NR 1 PYLON INBD SIDE WEB CUTOUT FOR PANEL 433LR UPPER & LOWER AFT EDGE INNER SURFACE FOUND CORRODED. WEB REMOVED AND REPLACED IAW DWG 311N5002 SHT.14 REV.E. MAJOR REPAIR.

Part: WEB — CORRODED (ZONE 400) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

NR 1 PYLON INBD SIDE WEB INNER SURFACE FOUND CORRODED AT PSTA 144.4 - 153.9. REMOVED AND REPLACED IAW DWG 311N5002 SHT.14 REV.E. MAJOR REPAIR.

Part: WEB — CORRODED (ZONE 400) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

PYLON NR 1, PYLON OTBD SIDE WEB INNER SURFACE FOUND CORROSION AT PSTA 144.4 - 153.9. REPAIRED PER EA F-5450-T0304976. REPAIR CLASSIFIED AS MINOR

Part: WEB — CORRODED (ZONE 400) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

PYLON NR 2, PYLON INBD SIDE WEB INNER SURFACE FOUND CORRODEDAT PSTA 144.4 - 174.3. REPAIRED IAW EA F-5450-T0304977 PART 1. REPAIR IS MINOR.

Part: WEB — CRACKED (NR 1 NACELLE) · airframe 59,546 hrs · 21,536 cycles

NR 1 PYLON AFT UPPER WEB, PP STATION 174.75, PP RBL 3.0, FOUND CRACKED FROM FASTENER HOLE TO WEB EDGE, AFTER FASTENER & SEALANT REMOVAL. REPAIRED IAW EA F-5450-T0305059B. REPAIR CLASSIFIED AS MAJOR

Part: PAN — CHAFED (L2 DOOR) · airframe 59,546 hrs · 21,536 cycles

L2 DOOR EXTERNAL HANDLE PAN FOUND CHAFED. REPAIRED IAW D EA F-5210-T0305204. REPAIR CLASSIFIED AS MINOR.

Part: WEB — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

NR 1 PYLON INBD SIDE WEB INNER SURFACE FOUND CORRODED AT PSTA 153.9 - 174.30. WEB REMOVED AND REPLACED IAW DWG 311N5002 SHT.14 REV.E WITH E.A. F-5450-T0304661 PART 1. REPAIR IS MAJOR.

Part: WEB — CORRODED (BS 740-760) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

BS 740 - 760, R2 DOOR LOWER SILL WEB FOUND CORRODED AT UPPER & LOWER SURFACES. REMOVED AND REPLACED WEB IAW DWG 143N8322 SHT.1 REV.K. REPAIR IS MAJOR.

Part: FRAME — GOUGED (BS 1280) · airframe 59,546 hrs · 21,536 cycles

BS 1280, STRINGER 10R FRAME INNER FLANGE FOUND GOUGED. REPAIRED IAW SRM 53-00-07 REPAIR 3 REV 110 REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — SCRATCHED (FUSELAGE) · airframe 59,546 hrs · 21,536 cycles

EXISTING REPAIR FINDINGS. CABIN RT SIDE EXISTING REPAIR FRAME HAS SCRATCHES AT 1280, STRINGER 10R - 13R. DAMAGED FRAME SECTION CUT & REMOVED FROM APPROXIMATELY STR 9R TO 14R STA 1280. NEW FRAME REPAIR CARRIED OUT AS PER SRM 53-00-07 REPPAIR 3 FIG 201 REV 110. REPAIR CLASSIFIED AS MAJOR

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 59,546 hrs · 21,536 cycles

CABIN STATION 1320 RBL 24.75 SEAT TRACK OTBD FLANGE CHAFE MARKS. SEAT TRACK FROM STA 1320 TO STA 1350, RBL 24.75, REPAIRED IAW SRM 53-00-52 REPAIR 1, OPTION 1, FIG 201, REV 110. REPAIR IS MAJOR.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

CABIN STATION 1360 - STATION 1380 R3 DOOR LOWER SILL WEB BOTH SURFACE CORROSION. CORROSION EXCEEDED LIMIT, DOOR SILL WEB. REMOVED & REPLACED WITH FABRICATED WEB AS PER SRM 51-40-02 REV 110 & BOEING DWG 146N8322 SHT 2 REV D. DOOR LOWER SILL WEB FABRICATED AS PER BOEING DWG 146N8322 SHT 2 REV D REPAIR CLASSIFIED AS MAJOR

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

EXISTING REPAIR FINDINGS, CABIN. EXISTING REPAIR HAS CORROSION & BLEND AT THE FLOORBEAM TOP CHORD STATION 377, LBL 8.7 TO LT SIDE FRAME JOINT, WL 208.8 SNRM 00961. FLOORBEAM REMOVED AS PER SRM 51-40-02 REV 110. NEW FLOORBEAM FABRICATED AS PER BOEING DWG 141N5123 SHT 1 REV A & INSTALLED AS PER BOEING DRAWING 141N5113 SHT 1 REV F. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 59,546 hrs · 21,536 cycles

CABIN STATION 560 - 620, RBL 24.75 SEAT TRACK INBD FLANGE FOUND CHAFFED. CHAFE EXCEEDED LIMIT AS PER SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 REV 110. SEAT TRACK REPAIR CARRIED OUT AT STA 570-620 RBL 24.75 AS PER SRM 53-00-52 REAIR 1 OPTION 1 FIGURE 201 REV 110. REPAIR IS MAJOR

Part: FRAME — GOUGED (FUSELAGE) · airframe 59,546 hrs · 21,536 cycles

CABIN STATION 1681, STRINGER 5L, FRAME INNER FLANGE FOUND GOUGE MARK. COMPLIED WITH EA F-5310-T0305360 PART 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: STRINGER — DENTED (FUSELAGE) · airframe 59,546 hrs · 21,536 cycles

MAIN EE COMPARTMENT STATION 470 STRINGER 23R, FOUND DENT. DENT REPAIRED AS PER SRM 53-00-03 FIG 201, REPAIR 2, REV 110. REPAIR IS MAJOR.

Part: WEB — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

PYLON NR 1 INBD SIDE WEB SKIN INNER SURFACE FOUND CORROSION AT PP STATION 187 AFTER SKIN OPEN UP. CORRODED PYLON SIDE WEB SKIN REMOVED AND REPLACED IAW DWG 311N5002 SHT 14 REV E WITH EA F-5450-T0304661 PART 1. REPAIR IS MAJOR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 59,546 hrs · 21,536 cycles

CABIN STATION 540 - 560 RT CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-10-02 REV110. MATERIAL THICKNESS REMOVED 0.015" FOUND EXCEED LIMIT AS PER SRM 53-30-13 ALLOWABLE DAMAGE 1 FIG 101 REV110. COMPLIED WITH EA F-5310-T0305240 A PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

CABIN STATION 365 RBL 45.5 SEAT TRACK CROWN SUPPORT FOUND CORROSION. CABIN STA 365 RBL 45.5 SEAT TRACK CROWN SUPPORT CORROSION REMOVED AS PER SRM 51-10-02 REV 110. REWORKED AREA EVALUATED, MATERIAL THICKNESS REMOVED 0.024" FOUND EXCEED 10% LIMIT AS PER SRM 53-00-52 ALLOWANCE DAMAGE 1 FIG 101 REV 110. SEAT TRACK CROWN SUPPORT REMOVED FROM STA 377.7 - 418 RBL 45.5 AS PER SRM 51-40-02 REV 110. NEW SEAT TRACK CROWN SUPPORT INSTALLED AS PER BOEING DRAWING 141N5130 SHT 6 REV A REPAIR CLASSIFIED AS MAJOR

Part: SHEAR TIE — DENTED (R3 DOOR) · airframe 59,546 hrs · 21,536 cycles

CABIN R3 DOOR BETWEEN AFT NR 3 STOP & FWD NR 3 STOP, FWD CLIP DENT. FWD CLIP REMOVED & REPLACED WITH FABRICATED CLIP (SHEAR TIE) AS PER SRM 51-40-02 REV 110 & BOEING DWG 146N6313 SHT 2 REV K CLIP (SHEAR TIE) FABRICATED AS PER BOEING DWG 146N6346 SHT 1 REV. REPAIR CLASSIFIED AS MAJOR

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,546 hrs · 21,536 cycles

CABIN STATION 1140 RT CREASE BEAM INNER CHORD SPLICE FITTING CRACKED. CRACKED SPLICE FITTING ON STA 1140 RT CREASE BEAM INNER CHORD REMOVED AND REPLACED AS PER DWG 144N5200 SHT 1 REV B. REPAIR IS MAJOR.

Part: SHEAR TIE — DENTED (R3 DOOR) · airframe 59,546 hrs · 21,536 cycles

CABIN R3 DOOR BETWEEN AFT NR 3 STOP & FWD NR 3 STOP, AFT CLIP DENT. AFT CLIP REMOVED & REPLACED WITH FABRICATED CLIP (SHEAR TIE) AS PER SRM 51-40-02 REV 110 & BOEING DWG 146N6313 SHT 2 REV K CLIP (SHEAR TIE) FABRICATED AS PER BOEING DWG 146N6346 SHT 1 REV - REPAIR CLASSIFIED AS MAJOR

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

CABIN STATION 310.5 RBL 2 - RBL 4 FLOOR BEAM UPPER CHORD FOUND CORROSION. CORROSION AT STA 310.5 RBL 2- RBL 4 FLOOR BEAM UPPER CHORD REMOVED AS PER SRM 51- 10-02 REV 110. MATERIAL REMOVED 0.009' FOUND WITHIN 10% LIMIT AS PER SRM 53-00-51 ALLOWABLE DAMAGE 1, FIG 101, REV 110.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

CABIN STATION 720 LBL 46 - LBL 64 FLOOR BEAM UPPER FLANGE FOUND CORROSION. REPAIR CARRIED OUT. REFER TO DRC 0047, STAE EA 757-5335-08-E2459 REV - WITH 8110-3 DATED JAN 16 2014 FOR WORK DETAIL. REPAIR CLASSIFIED AS MINOR

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 59,546 hrs · 21,536 cycles

CABIN STATION 560 LBL 7 - RBL 10 FLOOR BEAM UPPER FLANGE FOUND CHAFFED. REPAIR CARRIED OUT. REFER TO DRC 0046, STAE EA 757-5335-08-E2458 REV - WITH 8110-3 DATED JAN 16 2014 FOR WORK DETAIL. REPAIR CLASSIFIED AS MINOR

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

CABIN STATION 345 BL0 - LBL 24 FLOOR BEAM UPPER FLANGE FOUND CORROSION. CORROSION REPAIR CARRIED OUT. REFER TO DRC 0044, STAE EA 757-5315-08-E2452 REV - WITH 8110-3 DATED JAN 16 2014 FOR WORK DETAIL. REPAIR CLASSIFIED AS MINOR

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 59,546 hrs · 21,536 cycles

CABIN STATION 440 RBL 2 FLOOR BEAM UPPER FLANGE FOUND CHAFFED. REPAIR CARRIED OUT. REFER TO DRC 0045, STAE EA 757-5335-08-E2457 REV A WITH 8110-3 DATED JAN 16 2014 FOR WORK DETAIL. REPAIR CLASSIFIED MINOR PER GMM 6-2-100

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

CABIN STATION 740 LBL 46 - LBL 64 FLOOR BEAM UPPER FLANGE FOUND CORROSION. REPAIR CARRIED OUT. REFER TO DRC 0048, STAE EA 757-5335-08-E2461 REV - WITH 8110-3 DATED JAN 16 2014 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

CABIN STATION 1000 - STATION 1040 RT CREASE BEAM INNER CHORD CORROSION. CORROSION REPAIR CARRIED OUT ON RT CREASE BEAM INNER CHORD FROM STA 1010 TO STA 1040, RBL 64, IAW DWG LOR5L53017 REPAIR 2 REV A AND DWG 144N5140 SHT 2 REV C. REPAIR IS MAJOR.

Part: FAILSAFE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

CABIN STATION 1160 STRINGER 16L - 17L, FRAME OUTER CHORD CORROSION. CABIN STA 1160 STR 16L - 17L FROM OUTER CHORD (FAIL SAFE CHORD) CORROSION REMOVED AS PER SRM 51-10-02 REV 110 FOUND EXCEED LIMIT PER SRM 53-00-07 ALLOWANCE DAMAGE 2 FIG 101 REV 110. FAIL SAFE CHORD REMOVED AS PER SRM 51-40-02 REV 110 & REPLACED WITH FABRICATED CHORD PER BOEING DWG 144N1112 SHT 3 REV F. FAIL SAFE CHORD FABRFICATED PER FABRICATED PER BOEING DRAWING 144N1050 SHT 2 REV - REPAIR CLASSIFIED AS MAJOR

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

MAIN EE COMPARTMENT STATION 482 RBL 1, FUSELAGE SKIN INNER SURFACE FOUND CORROSION. SURFACE CORROSION REMOVED AS PER SRM 51- 10-02 REV 110. FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DET II REV 110. ACCOMPLISHED E.A.# F-5330-T0304978, PART 1 STEP 2 TITLE : FUSELAGE - PLATES AND SKIN - SCRATCH, NICK AND CORROSION ON FUSELAGE SKIN PANEL, STA 460 - STA 500, S26R - S28R. REPAIR CLASSIFIED AS MAJOR.

Part: ANGLE — CORRODED (DOOR SILL) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

BS 1380, R3 DOOR LOWER SILL INNER ANGLE FOUND CORRODED. REMOVED ANGLE IAW SRM 51-40-02 REV.110 AND REPLACED ANGLE IAW DWG 146N8322 SHT.1 REV.F. MAJOR REPAIR.

Part: FRAME — CHAFED (BS 377.7) · airframe 59,546 hrs · 21,536 cycles

BS 377.7, S6R FRAME INBD FLANGE FOUND CHAFED. REPAIRED IAW EA 757-5312-08-E2453 REV. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (BS 600-620) · corrosion level 2 · airframe 59,546 hrs · 21,536 cycles

BS 600 -620 RT CREASEBEAM WEB FOUND CORRODED. REMOVED IAW SRM 51-40-02 REV 110 & REPLACED WITH FABRICATED CREASE BEAM WEB IAW DWG 143N5520, SHT 3, REV B.

Part: BUSHING — MIGRATED (NR 2 NACELLE) · airframe 59,546 hrs · 21,536 cycles

NR 2 PYLON LOWER SPAR FITTING BUSHING MIGRATED. REPAIRED PER SRM 54-50-90 REV 110 REPAIR 5. REPAIR CLASSIFIED AS MAJOR

Part: BUSHING — MIGRATED (NR 1 NACELLE) · airframe 59,546 hrs · 21,536 cycles

NR 1 PYLON LOWER SPAR FITTING BUSHING MIGRATED. REPAIRED IAW SRM 54-50-90 REPAIR 5, FIG 201, PROCEDURE III, REV.110. MAJOR REPAIR.