N782SP

Part: SKIN — CORRODED (RT WING) · corrosion level 3 · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016331, RT WING OTBD LE, OTBD SECTION HAS INTERGRANULAR CORROSION AROUND FASTENERS ON UPPER SKIN, BETWEEN XFS710.000 - 747.500. ITEM REPAIRED ON EA 008-5710-38-5863.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016060, LT WING UPPER SURFACE HAS INTERGRANULAR CORROSION AROUND A FASTENER AT XW 761 & STRINGER 2. ITEM REPAIRED IAW EA 008-5710-38-A5879.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

RT WING SKIN CTR LE HOIST POINT AT XFS 385.250 HAS INTERGRANULAR CORROSION. REPAIRED ON EA 008-5730-38-A5966.

Part: SKIN — DAMAGED (LT WING) · airframe 95,432 hrs · 23,967 cycles

AFTER REMOVAL OF LT OTBD LE STUB WING, FOUND SKIN UPPER ATTACH SCREW HOLE COUNTERSINK DAMAGED. REPAIRED IAW EA 008-5730-38-A5967.

Part: SKIN — CORRODED (LT WING) · corrosion level 3 · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016593, LT WING CTR LE UPPER SKIN HAS INTERGRANULAR CORROSION AROUND FASTENERS AT XFS 347.750. ITEM REPAIRED IAW EA 008-5730-38-A6009.

Part: SKIN — CORRODED (RT WING) · corrosion level 3 · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016797, RT WING CTR LE UPPER SKIN, TE HAS INTERGRANULAR CORROSION AROUND FASTENERS AT XOLD16.225 & XFS 429. REPAIR ACCOMPLISHED IAW EA 008-5730-38-A5993.

Part: SKIN — CRACKED (LT WING) · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A019317, LT WING INBD LE, OTBD SECTION UPPER SKIN HAS SEVERAL CRACKS AT XILD 42. ITEM REPAIRED IAW EA 008-5730-38-A6019.

Part: SKIN — CORRODED (LT WING) · corrosion level 3 · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016224, LT WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN CTR & AFT SPAR & XRS 393 - 428. ITEM REPAIRED IAW EA 008-5710-38-A5885.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016333, RT WING OTBD LE, OTBD SECTION HAS INTERGRANULAR CORROSION AROUND FASTENERS ON UPPER SKIN BETWEEN XFS 778.750 - XW 761.695. ITEM REPAIRED ON EA 008-5710-38-A5863.

Part: SKIN — CORRODED (LT HORIZ STAB) · airframe 95,432 hrs · 23,967 cycles

LEFT HORIZ STAB INBD LE UPPER SURFACE HAS CORROSION AT OTBD HOIST ATTACH POINT. ITEM REPAIRED IAW EA 008-5530-38-A5938.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A017180, COCKPIT SUBFLOOR IS EXFOLIATED THROUGH SKIN AT STATION 133 RT CUSP AREA. REPAIR ACCOMPLISHED ON EA 008-5310-38-A5956.

Part: SKIN — CORRODED (TAILCONE) · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016101, TAIL CONE SKIN CORRODED AT LOWER TAIL LIGHT ASSEMBLY. ITEM REPAIRED IAW EA 008-5330-38A5869.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A017940, AFTER REMOVING RT CABIN WINDOW AT STATION 1410, FOUND CORROSION ON WINDOW FRAME & INSIDE FASTENER HOLES. ITEM REPAIRED ON EA 008-5320-38-A5955.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016084, EXTERIOR FUSELAGE HAS CORROSION ON SKIN AT WINDOW REPAIR DOUBLER, STATION 1340. REPAIR WAS ACCOMPLISHED ON EA 008-5320-38-A5955.

Part: SKIN — CORRODED (RT WING) · corrosion level 3 · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016795, RT WING CTR LE UPPER SKIN, TE HAS INTERGRANULAR CORROSION AROUND FASTENER AT XFS 385.250. ITEM REPAIRED ON EA 008-5730-38-A5993.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016226, LT WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN STRINGER 4 & CTR SPAR & XRS 358-393. ITEM REPAIRED IAW EA 008-5710-38-A5882.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

RIGHT WING, INBD LE, OTBD SECTION LOWER SKIN HAS INTERGRANULAR CORROSION AT XS 250.089. REPAIR ACTION ACCOMPLISHED IAW EA 008-5710-38-A6018.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

EXTERIOR FUSELAGE DOUBLER HAS CORROSION AT RT AFT DRAIN MAST, STATION 1552 32-015.

Part: SKIN — CORRODED (LT WING) · airframe 95,432 hrs · 23,967 cycles

LEFT WING LOWER SURFACE HAS CORROSION AT STRINGER 53 & INBD OF PYLON, 28-023.

Part: STRINGER — CORRODED (LT WING) · airframe 95,432 hrs · 23,967 cycles

EXFOLIATED LOWER FWD STRINGER INBD END, INSIDE FUEL ACCESS PANEL 514D.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

REFERENCE A017940, AFTER REMOVING RT CABIN WINDOW AT FS 1410, FOUND CORROSION ON WINDOW FRAME & INSIDE FASTENER. REPAIR ACCOMPLISHED IAW EA 008-5320-38-A5955.

Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

AFTER REMOVAL OF AFT RT LAVATORY DUMP PAN & FASTENERS. MAIN CABIN FLOORBEAM FOUND EXFOLIATED.

Part: SKIN — CORRODED (LT HORIZ STAB) · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016309, LT HORIZONTAL STABILIZER INBD LE, UPPER SURFACE HAS CORROSION AT INBD HOIST ATTACH POINT. ITEM REPAIRED IAW EA 008-5530-38-A5929.

Part: PANEL — CORRODED (LT AILERON) · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016695, LT WING INBD AILERON CTR & OTBD BALANCE PANELS HAVE RUST CORROSION. REPAIR ACCOMPLISHED IAW EA 008-5751-38-A5958.

Part: DOOR SEAL — TORN (ZONE 200) · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016448 & A023498 INGRESS & EGRESS DOOR FROM FLIGHT DECK TO UPPER CARGO COMPARTMENT, MAIN CARGO DECK, HAS TORN & COMPRESSED FIRE SUPPRESSION SEALS. THIS ITEM WAS REPAIRED IAW EA AQ56-25-101.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016097, EXTERIOR FUSELAGE, AFT RT LAVATORY SERVICE PANEL, CUT OUT HAS CORROSION INSIDE. REPAIR ACCOMPLISHED IAW EA 008-5330-38-A6035.

Part: PANEL — CORRODED (RT AILERON) · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016937, RT INBD AILERON BALANCE PANEL HAS CORROSION. REPAIR ACCOMPLISHED IAW EA 008-5751-38-A5959.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016313, LT WING INBD STUB WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN XILD 42 - XW 257 AT FWD SPAR ATTACHMENT.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A017102, AFT ACCESSORY COMPARTMENT, FS 1530, LONGERON 28L - 28R, AFT FACING SURFACES CORRODED.

Part: SKIN — CORRODED (LT WING) · airframe 95,432 hrs · 23,967 cycles

REFERENCE NRC A016056, LT WING LOWER SURFACE HAS CORROSION OTBD SIDE OF NR 1 PYLON AT STRINGER 52 28-034.

Part: SKIN — CORRODED (LT WING) · airframe 95,432 hrs · 23,967 cycles

LT WING UPPER SURFACE HAS INTERGRANULAR CORROSION AROUND A FASTENER AT XRS763 & STRINGER 2 28-039.

Part: SKIN — CORRODED (LT WING) · airframe 95,432 hrs · 23,967 cycles

LT WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN STRINGER 9 & FWD SPAR, BETWEEN XRS 255 - 289.28-063.

Part: CAP — CORRODED (LT WING) · airframe 95,432 hrs · 23,967 cycles

LT WING INBD LE FUEL TANK UPPER TE TEE CAP HAS INTERGRANULAR CORROSION. BETWEEN XFS 30.000 - 57.000.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK LUGS DAMAGED 2 PLACES STATION 834, LBL 24.

Part: RIVET — CRACKED (TE FLAP) · airframe 95,432 hrs · 23,967 cycles

LT INBD FLAP UPPER SURFACE INBD RUB PLATE HAS POPPED & CRACKED RIVETS 28-010.

Part: FINGER DOUBLER — BROKEN (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

COCKPIT SUBFLOOR RT SIDE CUSP AREA STATION 148, FINGER DOUBLER HAS MANY BROKEN OFF FASTENERS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION AT SPLICE SAT 590, LBL 24.32-156.

Part: SKIN — CORRODED (LT HORIZ STAB) · airframe 95,432 hrs · 23,967 cycles

LEFT HORIZONTAL STAB TIP HAS CORROSION ON SKIN AT STATIC WICK BASES.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

FOUND FITTING THAT ATTACHES FRAME TO FLOORBEAM AT STATION 1480 RT SIDE WITH INTERGRANULAR CORROSION. REMOVED FITTING. FABRICATED & INSTALLED NEW FITTING IAW EA 008-5310-38-A6040.

Part: SEAT TRACK — CORRODED (BS 990) · airframe 95,432 hrs · 23,967 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION AT SPLICE, BS 990, LBL 24, 32-151.

Part: BULKHEAD WEB — CRACKED (ZONE 100) · airframe 95,432 hrs · 23,967 cycles

CRACK FOUND AT LT INBD SIDE OF AFT PRESSURE BULKHEAD BETWEEN LONGHORN 10 AND 11 APPROXIMATELY 2.25" IN LENGTH. VERIFIED BY FPI AND HFEDC INSPECTION.

Part: FRAME — CORRODED (BS 1060) · airframe 95,432 hrs · 23,967 cycles

FRAME BS 1060, UPPER CAP CORRODED INCLUDING EXFOLIATION AT SEVERAL PLACES FROM S34L TO S31R.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

LT WING CTR UE UPPER SKIN HAS INTERGRANULAR CORROSION AROUND FASTENER AT XFS 261.500.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

LEFT WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN CTR SPAR & STRINGER 11 & XRS 204 & 238.052.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

AFTER REMOVAL OF LOWER IFF ANTENNA, FOUND CORROSION, JUST AFT OF NLG INTERNAL STRUCTURE AROUND ANTENNA CUT OUT. GAINED ACCESS TO AREA & FOUND LONGERON 36L WITH ELONGATED HOLES. REMOVED LONGERON 36L. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER, REPLACEMENT ANTENNA PAN FITTING & REPLACEMENT LONGERON IAW SRM.

Part: STRINGER — CORRODED (LT WING) · airframe 95,432 hrs · 23,967 cycles

UPON OK TO CLOSE, FOUND EXFOLIATED LOWER FWD STRINGER INSIDE FUEL ACCESS PANEL 514D, INBOARD END. REMOVED STRINGER 59. FABRICATED STRINGER 59 REPAIR SPLICE FITTING. INSTALLED IAW SRM & EA 008-5710-38-A6042.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

FOUND LONGERON 23L, EXFOLIATED IN 2 PLACES. REMOVED SECTION, FABRICATED NEW & INSTALLED IAW SRM.

Part: LONGERON FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

LONGERON 26 LT, STATION 1530, EXFOLIATED AT BARREL NUT HOLD END FITTING.

Part: LONGERON FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

LONGERON 28 LT, STATION 1530, END FITTING EXFOLIATED AT BARREL NUT HOLE. REMOVED, FABRICATED NEW & INSTALLED IAW SRM.

Part: LONGERON FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

LONGERON 26 RT, END FITTING EXFOLIATED INSIDE OF BARREL NUT HOLE STATION 1530. REMOVED END FITTING, FABRICATED NEW END FITTING & INSTALLED IAW SRM.

Part: LONGERON FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

LONGERON 24 LT, END FITTING EXFOLIATED AT BARREL NUT HOLE, STATION 1530. REMOVED END FITTING, FABRICATED NEW END FITTING & INSTALLED IAW SRM.

Part: LONGERON FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

LONGERON 30L AT STATION 1530, END FITTING EXFOLIATED AT BARREL NUT HOLE. REMOVED END FITTING, FABRICATED NEW FITTING & INSTALLED IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

RIGHT END FITTING, FABRICATED NEW END FITTING & INSTALLED IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

WHILE WORKING NR A016127, FOUND LONGERON 36 AT STATION 612 - 712 WITH EXFOLIATION. REMOVED LONGERON 36, 2 EACH EXTRUSION. FABRICATED NEW LONGERON 36 & INSTALLED IAW 008-5310-38-A6024.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

FOUND SUBFLOOR WEB EXFOLIATED AT LOWER SURFACE OF WEB, BS 1480, L21R. REMOVED SUBFLOOR WEB, FABRICATED NEW SUBFLOOR WEB & INSTALLED IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

FOUND LT SUBFLOOR CRACKED, BELOW AFT LT ENTRY DOOR, STATION 1480 - 1520. GAINED ACCESS TO AREA. REMOVED WEB, FABRICATED INTERCOSTAL & INSTALLED IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

FOUND SKIN SPLICE STRAP EXFOLIATED FROM STATION 1530 - 1606, LONGERON 28L. REMOVED STRAP, FABRICATED NEW STRAP & INSTALLED IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

SKIN SPLICE STRAP FOUND EXFOLIATED FROM STATION 1530 - 1606, LONGERON 28R. REMOVED STRAP, FABRICATED NEW STRAP & INSTALLED IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

EXISTING REPAIR ON LONGERON SECTION 32 RT AFT OF STATION 1530, HAS CORROSION & DAMAGED FASTENER HOLES. REMOVED REPAIRED SECTION. FABRICATED NEW REPAIR & INSTALLED IAW SRM.

Part: SKIN — GOUGED (RT WING) · airframe 95,432 hrs · 23,967 cycles

AFTER REMOVAL OF RT WING UPPER PANEL, ABOVE AILERON BAY FOUND GOUGE MARKS ON UPPER SKIN. CUT OUT DAMAGED AREA. HFEC SURFACE INSPECTION, NO CRACKS NOTED. FABRICATED REPLACEMENT DOUBLER & FILLER IAW EA 008-5730-38-A6021 & INSTALLED.

Part: WEB — CRACKED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

FOUND CRACKED WEB, BETWEEN STATION 1520 - 1540, RBL 24, MAIN CABIN. REMOVED WEB, FABRICATED NEW WEB & INSTALLED IAW SRM.

Part: SKIN — CORRODED (LT WING) · airframe 95,432 hrs · 23,967 cycles

LEFT WING LOWER SURFACE HAS INTERGRANULER CORROSION AROUND FASTENERS AT XW 761. REMOVED FASTENERS & REMOVED CORROSION. UT INSPECTION. OPEN HOLE INSPECTION, BLEND OUT OF LIMITS. FABRICATED REPAIR DOUBLER & FILLER. INSTALLED IAW EA 008-5730-38-A6020.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

MAIN CABIN LT OTBD SEAT TRACK, LOWER REPAIR STRAP IS EXFOLIATED AT LOWER SURFACE IN AFT ACCESSORY COMPARTMENT, STATION 1420. REMOVED CORROSION, OUT OF LIMITS. FABRICATED SPLICE PLATE & INSTALLED IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

MAIN CABIN SEAT TRACK IS CORRODED AT LOWER FLANGE, STATION 1480, BL0. CORROSION IS OUT OF LIMITS. CUT OUT DAMAGED SECTION. FABRICATED REPLACEMENT SEAT TRACK & INSTALLED IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

AFTER REMOVAL OF AFT RT DUMP PAN FOUND FUSELAGE FLOOR FRAME EXFOLIATED AT STATION 1500, LONGERON 23R - 24R. PERFORMED BLEND, BLEND OUT OF LIMITS. FABRICATED REPAIR ANGLE & FILLER. INSTALLED IAW EA 008-5310-38-A6007.

Part: DOUBLER — CORRODED (LT WING) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

WHILE WORKING NR A016589, FOUND INTERNAL PRODUCTION DOUBLER EXFOLIATED, LT WING LE STATION XFS 304.000. REMOVED DOUBLER & REMOVED SURFACE CORROSION. FABRICATED & INSTALLED REPLACEMENT DOUBLER IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

FOUND CORROSION ON SKIN LT WW, STATION 980, BETWEEN STRINGERS 25 - 30. GAINED ACCESS, CUT OUT DAMAGED LONGERON. FABRICATED LONGERON & INSTALLED IAW SRM.

Part: HINGE FITTING — CORRODED (CARGO DOOR) · airframe 95,432 hrs · 23,967 cycles

MAIN CARGO DOOR ACTUATOR HINGE FITTING, PN 5777788-1, CORRODED. REMOVED HINGE FITTING, REMOVED CORROSION, FABRICATED 4 EACH BUSHINGS & INSTALLED IAW EA 008-5310-38-A6014.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

RIGHT FWD FUSELAGE AT AFT PRIMARY HEAT EXCHANGER, FUSELAGE FRAME AT STATION 148, LONGERON 23R HAS HEAVY CORROSION. REMOVED FRAME, FABRICATED NEW FRAME & INSTALLED IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

CRACK FOUND AT RT OTBD SIDE OF AFT PRESS BULKHEAD WEB, BETWEEN LONGERON 10 & 11. APPROX 2 INCHES IN LENGTH. CUT OUT DAMAGED AREA. HFEC SURFACE INSPECTION. FABRICATED REPAIR DOUBLER & FILLER. INSTALLED REPAIR DOUBLER & FILLER IAW SRM.

Part: SEAT TRACK — CORRODED (BS 1420) · airframe 95,432 hrs · 23,967 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION BS 1420, LBL 59. REPLACED SEAT TRACK.

Part: TAB — CRACKED (RT ELEVATOR) · airframe 95,432 hrs · 23,967 cycles

ON OK TO INSTALL LE PANELS ON RT ELEVATOR GEAR TAB, FOUND SMALL ROUND ACCESS HOLE BENT & CRACKED. NDT VERIFIED 2 EACH CRACKS. BLENDED CRACKED AREAS. HFEC SURFACE INSPECTION PERFORMED. ACCOMPLISHED REPAIR TO RT ELEVATOR GEAR TAB ACCESS HOLE IAW EA 008-5510-38-A6034.

Part: SKIN — CORRODED (RT WING) · airframe 95,432 hrs · 23,967 cycles

RT WING CENTER L/E UPPER CENTER SLOT PANEL HAS INTERGRANULER CORROSION.

Part: BULKHEAD WEB — CORRODED (RT MLG WW) · airframe 95,432 hrs · 23,967 cycles

AFTER REMOVAL OF LONGERON 24R, FOUND CORROSION ON AFT WALL RT WW AT STATION 980, LONGERON 24R. CORROSION OUT OF LIMITS. REMOVED DAMAGED AREA FROM STATION 980 BULKHEAD SKIN. FABRICATED WEB SKIN & SPLICE. INSTALLED IAW EA 008-5310-38-A5925.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

FOUND CORROSION ON COPILOT FLOOR WEB. REMOVED WEB, FABRICATED NEW WEB & INSTALLED WEB IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

AFTER REMOVAL OF LONGERON 24R, FOUND BRACKET CRACKED AT STATION 940. FABRICATED ANGLE FLAP SUPPORT BRACKET LOCATED AT STATION 940, LONGERON 24R. REQUIRE MATERIAL SUBSTITUTION AS 7075-T651 CLAD PLATE IS NOT AVAILABLE TO PURCHASE. ACCOMPLISHED REPAIR TO LONGERON 24R, BRACKET STATION 940 IAW EA 008-5300-38-A6023.

Part: SKIN — DELAMINATED (ELEVATOR TAB) · airframe 95,432 hrs · 23,967 cycles

FOUND LT ELEVATOR CONTROL TAB UPPER SURFACE DELAMINATED IN SEVERAL AREAS. CUT OUT DAMAGE, FABRICATED FILLERS & DOUBLERS. BONDED FILLERS & DOUBLERS IAW SRM. TO BE BALANCED ON NR A020022.

Part: SKIN — DELAMINATED (ELEVATOR TAB) · airframe 95,432 hrs · 23,967 cycles

FOUND RT ELEVATOR CONTROL TAB UPPER SURFACE DELAMINATED IN SEVERAL AREAS. CUT OUT DELAMINATED AREAS, FABRICATED FILLERS & DOUBLERS, BONDED FILLERS & DOUBLER IAW SRM.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 95,432 hrs · 23,967 cycles

AFTER REMOVAL OF MAIN CARGO DOOR, FWD UPPER HINGE FITTING, FOUND CORROSION ON OUTER SKIN INTERNAL SURFACE. BLENDED AREA, BLEND OUT OF LIMITS, CUT OUT DAMAGED AREA. HFEC SURFACE & OPEN HOLE INSPECTION. ACCOMPLISHED REPAIR IAW EA 008-5230-38-A6016.

Part: DOUBLER — CRACKED (RT WING) · airframe 95,432 hrs · 23,967 cycles

WHILE WORKING NR A016629 ON RT WING UPPER SURFACE FOUND AN EXISTING REPAIR DOUBLER WITH MULTIPLE CORROSION AREAS STATION XRS 74.8 FROM FWD SPAR TO CTR SPAR. UT INSPECTION PERFORMED. REMOVED EXISTING REPAIR DOUBLER & REMOVED CORROSION. DP INSPECTION PERFORMED. BLEND WITHIN LIMITS. PERFORMED HFEC OPEN HOLE INSPECTION. FOUND 2 EACH CRACKS. REMOVED CRACKS IAW SRM. ACCOMPLISHED REPAIR IAW EA 008-5730-38-A612.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

AFTER REMOVING LT CABIN WINDOW AT STATION 1290, FOUND CORROSION ON WINDOW FRAME. REMOVED CORROSION. FABRICATED WINDOW REPAIR DOUBLER & INSTALLED IAW EA 008-5320-38-A5955.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

AFTER REMOVING RT SIDE CABIN WINDOW AT STATION 1250, FOUND CORROSION ON WINDOW FRAME. REMOVED 2 EA OLD REPAIR DOUBLERS. REMOVED CORROSION. PERFORMED HFEC OPEN HOLE INSPECTION. FABRICATED NEW DOUBLER & INSTALLED IAW EA 008-5320-38-A5955.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

FUSELAGE EXTERIOR, AFTER REMOVAL OF LOWER STRESS PANELS, CTR SECTION KEEL BEAM HAS CORROSION, GAINED ACCESS. REMOVED KEEL BEAM SECTION. FABRICATED NEW KEEL BEAM SECTION & INSTALLED IAW EA 008-5302-38-A5957.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

AFTER REMOVAL OF LT NOSE TUNNEL INSULATION BLANKETS FOUND COCKPIT SUBFLOOR HEAVILY CORRODED AT STATION 173 - 188. CUT OUT CORROSION FROM COCKPIT SUBFLOOR PANEL & FLOORBEAM. ACCOMPLISHED REPAIR IAW 008-5310-38-A5962.

Part: SKIN — CRACKED (LT WING) · airframe 95,432 hrs · 23,967 cycles

LT WING CENTER L/E LOWER SKIN IS CRACKED AT 2 FASTENERS AT XOLDI 6.225.

Part: TRUNNION — CORRODED (NLG) · airframe 95,432 hrs · 23,967 cycles

NLG REMOVED, FOUND RT TRUNNION PIVOT BORE WITH PITTING IN SEVERAL AREAS. REPAIRED NLG TRUNNION PIVOT BORE IAW EA 008-5310-38-A5945.

Part: SKIN — CORRODED (RT WING) · airframe 95,432 hrs · 23,969 cycles

RT WING OTBD L/E INBD SECTION LOWER SKIN HAS INTERGRANULER CORROSION AROUND FASTENERS.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

AFTER REMOVAL OF RT WING LONGERON 24 BARREL NUT & BOLT. FOUND LONGERON 24 CRACKED IN 2 PLACES IN BOLT HOLE AT RT WW STATION 857. ACCOMPLISHED REPAIR TO RT LONGERON 24 IAW EA 008-5300-38-A5915.

Part: SKIN — NICKED (RT WING) · airframe 95,432 hrs · 23,967 cycles

RT OTBD LE STUB WING, UPPER SKIN HAS SEVERAL NICKS & SCRATCHES. BLENDED, BLEND OUT OF LIMITS. ACCOMPLISHED REPAIR IAW EA 008-5730-38-A5982.

Part: SKIN — CORRODED (BS 1600) · airframe 95,432 hrs · 23,967 cycles

EXTERNAL FUSELAGE SKIN HAS POCKET OF CORROSION AT BS 1600, LONGERON 32L.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

AFT CABIN SEAT TRACK FS 1520 - 1547, RBL 24 IS CORRODED. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK & INSTALLED IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

AFT CABIN SEAT TRACK BL 0, FS 1520 - 1547 IS CORRODED. GAINED ACCESS & REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK & INSTALLED IAW SRM.

Part: CONTROL COLUMN — CORRODED (COCKPIT) · airframe 95,432 hrs · 23,967 cycles

CAPTAINS CONTROL COLUMN, LOWER END IS CORRODED. GAINED ACCESS. REPLACED CAPTAINS CONTROL COLUMN PN 5614272-501.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

AFT CABIN FLOOR SUPPORT EXTRUSION FS 1589, LBL 35 TO RBL 35, HAS BARE METAL, PREVIOUS REWORKED AREAS & CORROSION. REMOVED FLOOR SUPPORT ASSEMBLY, FABRICATED NEW FLOOR SUPPORT & INSTALLED IAW SRM.

Part: FINGER DOUBLER — DAMAGED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

COCKPIT SUBFLOOR RT CUSP AREA, STATION 148, FINGER DOUBLER HAS MANY BROKEN OFF FASTENERS. REMOVED DOUBLER FITTING & ATTACHMENT. FABRICATED TWO EACH FINGER DOUBLERS & INSTALLED IAW SRM.

Part: CONTROL COLUMN — CORRODED (COCKPIT) · airframe 95,432 hrs · 23,967 cycles

COPILOT'S CONTROL COLUMN IS EXFOLIATED THROUGHOUT. GAINED ACCESS TO CONTROL COLUMN. REPLACED COPILOT'S CONTROL COLUMN IAW AMM.

Part: FITTING — CORRODED (FS 1530) · airframe 95,432 hrs · 23,967 cycles

AFT ACCESSORY COMPARTMENT S36 END FITTING AFT AFT SIDE OF FRAME FS 1530 IS CORRODED.

Part: STRINGER FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

AFT ACCESSORY COMPARTMENT, STRINGER 28R, END FITTING AT AFT SIDE OF FRAME, FS 1530 IS CORRODED. REMOVED FITTING, FABRICATED NEW FITTING & INSTALLED FITTING IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

AFT ACCESSORY COMPARTMENT, FS 1586, CANTED FRAME IS CORRODED STRINGER 30L - 30R. REMOVED DAMAGED SECTION, FABRICATED NEW SECTION FRAME & INSTALLED IAW SRM.

Part: FITTING — CORRODED (FS 1530) · airframe 95,432 hrs · 23,967 cycles

NR A017106, AFT ACCESSORY COMPARTMENT S34R END FITTING AT AFT SIDE OF FRAME FS 1530 IS CORRODED.

Part: FITTING — CORRODED (FS 1530) · airframe 95,432 hrs · 23,967 cycles

AFT ACCESSORY COMPARTMENT S32L END FITTING AT AFT SIDE OF FRAME FS 1530 IS CORRODED.

Part: FITTING — CORRODED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

AFT ACCESSORY COMPARTMENT, STRINGER 30R, END FITTING AT AFT SIDE OF FRAME FS 1530 IS CORRODED. INSTALLED REPLACEMENT FITTING IAW SRM.

Part: FITTING — CORRODED (FS 1530) · airframe 95,432 hrs · 23,967 cycles

NR A017107, AFT ACCESSORY COMPARTMENT S32R END FITTING AT AFT SIDE OF FRAME FS 1530 IS CORRODED.

Part: FITTING — CORRODED (FS 1530) · airframe 95,432 hrs · 23,967 cycles

AFT ACCESSORY COMPARTMENT S34L END FITTING AT AFT SIDE OF FRAME FS 1530 IS CORRODED.

Part: PANEL — CORRODED (RT AILERON) · airframe 95,432 hrs · 23,967 cycles

RT INBD, CTR INBD BALANCE PANEL, HAS RUST CORROSION ON LOWER SURFACE. REPAIRED IAW EA 008-5751-38-A5959.

Part: SEAT TRACK — CORRODED (BS 1300) · airframe 95,432 hrs · 23,967 cycles

NR A016891, MAIN DECK CARGO COMPARTMENT HAS SEAT TRACK CORROSION AT SPLICE. BS 1300, RBL 49. 32-164. REPLACED SEAT TRACK.

Part: PANEL — CORRODED (RT AILERON) · airframe 95,432 hrs · 23,967 cycles

RT INBD AILERON, INBD BALANCE PANEL HAS CORROSION. REMOVED CORROSION. REPAIRED IAW EA 008-5751-38-A5959.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

RIGHT WING, LOWER SKIN HAS CORROSION AROUND FASTENERS AT STRINGER 58 & FWD SPAR & XRS 763. PERFORMED UT INSPECTION. REMOVED FASTENERS & REMOVED CORROSION. PERFORMED OPEN HOLE HFEC, BLEND OUT OF LIMITS. FABRICATED REPAIR DOUBLER & INSTALLED IAW EA 008-5730-38-A6028.

Part: MOUNT FITTING — GOUGED (RT AILERON) · airframe 95,432 hrs · 23,967 cycles

RT WING AILERON BAY CONTROL QUADRANT, ACTUATOR MOUNT FITTING IS GOUGED IN MULTIPLE AREAS. ACCOMPLISHED REPAIR IAW EA 008-5740-38-A6027.

Part: PANEL — CORRODED (RT AILERON) · airframe 95,432 hrs · 23,967 cycles

RT INBD AILERON, CTR INBD BALANCE PANEL HAS CORROSION. REPAIRED IAW EA 008-5751-38-A5959.

Part: PANEL — CORRODED (RT AILERON) · airframe 95,432 hrs · 23,967 cycles

RT INBD AILERON, CTR OTBD BALANCE PANEL HAS CORROSION. REPAIRED IAW EA 008-5751-38-A5959.

Part: PANEL — CORRODED (RT AILERON) · airframe 95,432 hrs · 23,967 cycles

RT INBD AILERON, OTBD BALANCE PANEL HAS CORROSION. REPAIRED IAW EA 008-5751-38-A5959.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

RIGHT WING LOWER SKIN HAS CORROSION AROUND FASTENERS AT STRINGER 57 & FWD SPAR & XRS 795. REMOVED CORROSION, PERFORMED UT, REMOVED FASTENERS, PERFORMED HFEC OPEN HOLE INSPECTION, NO CRACKS. CHECKED MATERIAL THICKNESS, OUT OF LIMITS. FABRICATED REPAIR DOUBLER & INSTALLED IAW EA 008-5730-38-A6022.

Part: SKIN — GOUGED (BS 960) · airframe 95,432 hrs · 23,967 cycles

LT EXTERIOR FUSELAGE SKIN IS GOUGED AT FS 960, APPROXIMATELY LONGERON 25L.

Part: SPAR — DAMAGED (RT WING) · airframe 95,432 hrs · 23,967 cycles

RT WING FWD SPAR UPPER FLANGE HAS A DAMAGED FASTENER HOLE AT APPROX XFS 188.750. GAINED ACCESS. REAMED HOLE TO ROUND. PERFORMED HFEC SURFACE & OPEN HOLE INSPECTION. INSTALLED 2 EACH FREEZE PLUGS IAW EA 008-5720-38-A6015.

Part: SKIN — CORRODED (RT WING) · airframe 95,432 hrs · 23,967 cycles

RT WING INBD LE FUEL TANK, AFT SKIN IS CHAFED AT XFS 26.250. BLENDED AREAS, BLEND IS OUT OF LIMITS. GAINED ACCESS. PERFORMED OPEN HOLE INSPECTION, NO CRACKS. FABRICATED REPAIR DOUBLER & INSTALLED IAW EA 008-5730-38-A6013.

Part: ACCESS PANEL — CHAFED (NR 2 PYLON) · airframe 95,432 hrs · 23,967 cycles

NR 2 PYLON PANEL 293B IS CHAFED. BLENDED DAMAGED AREA, GAINED ACCESS. PERFORMED UT INSPECTION. ACCOMPLISHED REPAIR IAW EA 008-5430-38-A6001.

Part: SKIN — CORRODED (RT WING) · airframe 95,432 hrs · 23,967 cycles

RT WING CTR LE UPPER SKIN HAS INTERGRANULER CORROSION AROUND FASTENER AT XFS 341.500. PERFORMED UT INSPECTION, CORROSION MARKED AS DETECTED, GAINED ACCESS. REMOVED CORROSION, BLEND OUT OF LIMITS. ACCOMPLISHED REPAIR IAW EA 008-5730-38-A5987.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

RIGHT WING CTR LE LOWER SKIN HAS CORROSION AROUND INBD FUELING GND POINT. PERFORMED UT INSPECTION. REMOVED CORROSION. HFEC SURFACE INSPECTION PERFORMED. BLEND OUT OF LIMITS. REPAIRED IAW EA 008-5730-38-A5992.

Part: ACCESS PANEL — DAMAGED (NR 4 PYLON) · airframe 95,432 hrs · 23,967 cycles

NR 4 PYLON ACCESS PANEL 492A, HAS 2 EACH SCREW HOLES ELONGATED. FOUND HOLES WORN & COUNTERSINK DAMAGED. FABRICATED REPAIR DOUBLER & FILLER . INSTALLED IAW EA 008-5430-38-A6032.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

LEFT WING INBD LE, OTBD SECTION LOWER AFT SKIN HAS INTERGRANULER CORROSION AT XFS 245. PERFORMED UT INSPECTION, REMOVED FASTENERS. REMOVED CORROSION & BLENDED AREA IS OUT OF LIMITS. HFEC SURFACE INSPECTION. FABRICATED EXTERNAL SPLICE REPAIR DOUBLER & INSTALLED IAW EA 008-5730-38-A6017.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

STATION 1606, LONGERON 3L & 3R, CHORD ANGLE CRACKED IN RADIUS AT STATION 1606. VIEWED THRU NR 60 ACCESS DOOR. HFEC VERIFIED 2 EACH CRACKS. FABRICATED 3 EACH ANGLES & FILLERS. INSTALLED IAW EA 008-5310-38-A5980.

Part: SKIN — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

RIGHT HORIZONTAL STABILIZER UPPER SKIN HAS POCKETS OF CORROSION, BETWEEN STATION XFS-47 & 65, INCLUDING AREA UNDER UPPER SLIDING FAIRING, FROM LE TO CLOSING SPAR. REMOVED CORROSION & PERFORMED UT. ACCOMPLISHED REPAIR IAW EA 008-5510-38-A6038.

Part: AILERON — GOUGED (LT WING) · airframe 95,432 hrs · 23,967 cycles

LT WING INBD AILERON IS CHAFED & GOUGED JUST AFT OF CTR OTBD BALANCE PANEL, GAINED ACCESS & BLENDED. BLEND IS OUT OF LIMITS. OPEN HOLE HFEC INSPECTION PERFORMED, NO CRACKS. FABRICATED SHIM & EXTERNAL SPLICE DOUBLER & INSTALLED IAW EA 008-5720-38-5989.

Part: SKIN — CORRODED (LT HORIZ STAB) · airframe 95,432 hrs · 23,967 cycles

LT HORIZONTAL STABILIZER UPPER SKIN HAS POCKETS OF CORROSION, BETWEEN STATION XFS 47 & 65, INCLUDING AREA UNDER UPPER SLIDING FAIRING, FROM LE TO CLOSING SPAR. ACCOMPLISHED REPAIR TO LT HORIZONTAL STABILIZER UPPER SURFACE, XFS 47 - 65 IAW EA 008-5510-38-A6037.

Part: SKIN — CORRODED (LT WING TE FLAP) · airframe 95,432 hrs · 23,967 cycles

LEFT WING INBD FLAP UPPER SURFACE INBD RUB PLATE HAS POPPED AND CRACKED RIVETS. FOUND EXFOLIATED SKIN UNDER PLATE.

Part: SKIN — CRACKED (RT WING) · airframe 95,432 hrs · 23,967 cycles

RT WING UPPER SURFACE, FROM XW 240 - XW 467, HAS SURFACE CORROSION IN MULTIPLE AREAS. PERFORMED UT INSPECTION, CORROSION DETECTED. GAINED ACCESS, BLENDED. DPI PERFORMED & HFEC OPEN HOLE PERFORMED. ALL BLENDED AREAS ARE WITHIN LIMITS. SEVERAL FASTENER HOLES HAVE CRACKS DETECTED. REAMED HOLES, HFEC REAMED HOLES, NO CRACKS NOTED. TREATED, PRIMED & FABRICATED REPAIR DOUBLER, TRIPLER & FILLERS. INSTALLED IAW EA 008-5710-38-A6026.

Part: SKIN — CORRODED (RT WING) · airframe 95,432 hrs · 23,967 cycles

RT WING UPPER SURFACE FROM XW 468 TO WING TIP, HAS SURFACE CORROSION FORMING IN MULTIPLE AREAS. PERFORMED UT INSPECTION & CORROSION DETECTED. PERFORMED BLEND OUT. PERFORMED NDT, DP & HFEC OPEN HOLE INSPECTIONS. BLEND OUT OF LIMITS. FABRICATED REPAIR DOUBLER & INSTALLED IAW EA 008-5730-38-A6030.

Part: SKIN — CORRODED (RT WING) · airframe 95,432 hrs · 23,967 cycles

RT WING UPPER SURFACE, FROM XW 69 - XW 240, HAS SURFACE CORROSION FORMING IN MULTIPLE AREAS. UT INSPECTION PERFORMED, PERFORMED OPEN HOLE INSPECTION. BLEND OUT OF LIMITS. FABRICATED REPAIR DOUBLER & INSTALLED IAW EA 008-5730-38-A6029.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

SURFACE CORROSION ON LOWER SURFACE OF MIDDLE INTERCOSTAL INSIDE STRUCTURAL BOX AT AFT OTBD CORNER OF LT MLW WW. GAINED ACCESS, FOUND 4 EA INTERCOSTALS CORRODED. REMOVED CORROSION & BLEND IS OUT OF LIMITS. FABRICATED REPLACEMENT INTERCOSTALS & INSTALLED IAW SRM.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 95,432 hrs · 23,969 cycles

LEFT HORIZONTAL STABILIZER INBD L/E UPPER SURFACE HAS CORROSION AT INBD SCREW HOLE. REMOVED CORROSION IAW SRM. FABRICATED FILLER AND DOUBLER AND INSTALLED IAW SRM 55-2-1.

Part: SKIN — CORRODED (LT WING) · airframe 95,432 hrs · 23,967 cycles

LEFT WING UPPER SKIN HAS CORROSION AROUND FASTENERS AND VORTEX GENERATORS AT CENTER SPAR BETWEEN XW 408 AND XW 485.28-49.

Part: STRIKER — WORN (NLG WW) · airframe 95,432 hrs · 23,967 cycles

RT NOSE TUNNEL ACCESS DOOR 91D, CUT OUT HAS 3 BROKEN & WORN STRIKER PLATES. REMOVED 3 EACH STRIKER PLATES. FABRICATED 3 EACH STRIKER PLATES & INSTALLED IAW EA 008-5310-38-A6031.

Part: DOOR — CORRODED (LE SLOT) · airframe 95,432 hrs · 23,967 cycles

LEFT WING OTBD SLOT DOOR CTR PANEL HAS EXFOLIATION CORROSION. FABRICATED REPLACEMENT DOOR IAW DWG. INSTALLED DOOR IAW SRM.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 95,432 hrs · 23,967 cycles

LEFT WING OTBD LE, OTBD SECTION HAS INTERGRANULER CORROSION AROUND FASTENERS ON UPPER SKIN, BETWEEN XFS 841.250 - 860.000.. BLENDED DAMAGED AREA. BLEND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, FILLER & INSTALLED IAW SRM.

Part: ACCESS PANEL — CORRODED (LE SLOT) · airframe 95,432 hrs · 23,967 cycles

LT WING OTBD SLOT DOOR, UPPER INBD PANEL HAS EXFOLIATION CORROSION. UT INSPECTION CONFIRM CORROSION, GAINED ACCESS. FABRICATED REPLACEMENT PANEL & INSTALLED IAW SRM.

Part: SKIN — CORRODED (LT WING) · airframe 95,432 hrs · 23,967 cycles

LT WING UPPER SKIN HAS CORROSION AT AFT SPAR, BETWEEN XRS139 - 172. PERFORMED BLEND OUT. PERFORMED UT INSPECTION. POSSIBLE CORROSION EXIST UNDERNEATH STRAP, FAIRING. REMOVED STRAP & ADDITIONAL CORROSION. BLENDED AREAS OUT OF LIMITS. FABRICATED FILLER & REPAIRED DOUBLER IAW EA 008-5730-38-A5922.

Part: SKIN — CORRODED (LT WING) · airframe 95,432 hrs · 23,967 cycles

LT WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN CTR SPAR, STRINGER 14 & XRS 172 - 204. PERFORMED UT INSPECTION. GAINED ACCESS & BLENDED. BLEND OUT OF LIMITS. ACCOMPLISHED EA 008-5710-38-A5990.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

EXTERIOR FUSELAGE AFT LT LAVATORY, SERVICE PANEL CUT OUT WORN & GOUGED AT LATCH CONTACT POINTS. FOUND GOUGE TO BE OUT OF LIMITS & FOUND CRACK ON FRAME. REPAIRED IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 95,432 hrs · 23,967 cycles

EXTERIOR FUSELAGE, CORROSION ON LOWER SKIN, BETWEEN STRESS PANELS, STATION 680, LONGERON 36. REMOVED CORROSION. PERFORMED UT INSPECTION. BLEND OUT OF LIMITS. UPON GAINING ACCESS, FOUND CORROSION ON INNER SKIN & SURROUND STRUCTURE, BETWEEN STATION 683 - 718, LONGERON 36. GAINED ACCESS. FABRICATED NEW SKIN PANEL, 4 EACH REPAIR DOUBLERS & 4 EACH FINGER DOUBLERS & INSTALLED IAW EA 008-5300-38-A5865.

Part: GOUGED (ZONE 500) · airframe 95,432 hrs · 23,967 cycles

LEFT WING, OTBD FLAP UPPER SURFACE, INBD OF STATION 219, FLAP TRACK IS CHAFED & GOUGED. BLENDED OUT DAMAGED AREA, MATERIAL LOSS OUT OF LIMITS. FABRICATED REPAIR DOUBLER & INSTALLED IAW 008-5700-38-A5864.