N464UP

Part: STRAP — CORRODED (ZONE 200) · airframe 34,953 hrs · 21,431 cycles

UPON REMOVAL OF FWD UPPER AND LOWER NUT PLATE STRAPS APU INLET FOUND AFT INNER AND OUTER NUTPLATE STRAPS CORRODED ATA 53-80. FABRICATED REPAIR STRAP -2 AND REPAIR FILLER-4 TREATED AND PRIMED REF. B 757-200 SRM 53-80-15-2R-1 REPAIR 1 REQUEST OK TO INSTALL.

Part: FRAME — DENTED (ZONE 100) · airframe 34,953 hrs · 21,431 cycles

WORKING FRAME REPAIR BS 600 T3F18E006XCWS FOUND DENT ON FRAME BS 580. INSTALLED REPAIR PARTS 3EA (FRAME FILLER, FILLER ANGLE & REPAIR ANGLE), ONE CLIP AT FRAME BS 580 RT STGR 16, 1 EA WEB CLIP AND 1 EA FILLER AT RT FRAME BS 580 STR 17 IAW B757-200PF SRM 53-30-07-2R-1 REP. 1 DETAIL VI PAR.4 STEP R & S. & SRM 51-40-02-0G-0. ACCOMPLISHED FRAME DENT DAMAGE REPAIR AT BS 580 BETWEEN S16R TO S17R PER VT SAA E.A 757-5300-1-B0531 STEP 2 REV P2 AND RESTORED ACCESS PER VT SAA E.A 757-5300-1-B0531 STEP 4 REV P1 REQUIREMENTS. ACCOMPLISHED REPAIR PER EO-94321-REQ1 AND EA 757-5300-01-B0531 IR IN CONJUNCTION WITH SRM 53-30-07-2R-1 REPAIR 1.

Part: FRAME — DENTED (NOT REPORTED) · airframe 34,953 hrs · 21,431 cycles

WORKING FRAME STA. 520 T3F18E006XCUX FOUND DENT ON FRAME STA. 540 ATA 53-10. INSTALLED 3 EA REPAIR PARTS (FRAME FILLER, FILLER ANGLE AND REPAIR ANGLE), 1 EA CLIP AT FRAME STA 540 RH STGR 16, 1 EA WEB CLIP P/N 143N5269-2 AND 1 EA FILLER P/N: 143N5520-14 AT R/H FRAME STA 540 STR 17 IAW B757-200PF SRM 53-30-07-2R-1 REP. 1 DETAIL VI PAR.4 STEP R AND S. AND SRM 51-40-02-0G-0. ACCOMPLISHED REPAIR PER EO-94314-REQ1 AND EA 757-5300-01-B0530 IR IN CONJUNCTION WITH SRM 757-200 PF SRM 53-30-07-2R-1 REPAIR 1.

Part: FRAME — DENTED (ZONE100) · airframe 34,953 hrs · 21,431 cycles

UPON REMOVAL OF ISOLATOR STA. 520 LWR. DATO PANEL T3F18E006W14Y FOUND DENT ON FRAME. INSTALLED REPAIR PARTS 3EA (FRAME FILLER, FILLER ANGLE AND REPAIR ANGLE) AND 1 EA CLIP AT FRAME STA 520 RH STGR 16 IAW B757-200PF SRM 53-30-07-2R-1 REP. 1 DETAIL VI PAR.4 STEP R AND S. AND SRM 51-40-02-0G-0.

Part: FRAME — DENTED (ZONE 100) · airframe 34,953 hrs · 21,431 cycles

UPON REMOVAL OF ISOLATOR STA.600 R/H LWR. DATO PANEL T3F18E006W161 FOUND DENT ON FRAME ATA 53-10. INSTALLED REPAIR PARTS 3EA (FRAME FILLER, FILLER ANGLE AND REPAIR ANGLE), 1 EA CLIP AT FRAME STA 600 RH STGR 16, 1 EA WEB CLIP P/N 143N5269-1 AND 1 EA FILLER P/N: 143N5520-14 AT R/H FRAME STA 600 STR 17 IAW B757-200PF SRM 53-30-07-2R-1 REP. 1 DETAIL VI PAR.4 STEP R AND S. AND SRM 51-40-02-0G-0. ACCOMPLISHED REPAIR PER EO-94318-REQ1 AND EA 757-5300-01-B0529 IR IN CONJUNCTION WITH 757-200PF SRM 53-30-07-2R-1 REPAIR 1.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 34,953 hrs · 21,431 cycles

APU INLET INTERNAL ACCESED FROM 311 SHOWS SIGNS OF ADVANCED CORROSION AND DELAMINATION AROUND NUTPLATES AND AREA WHERE DUCT ATTACHES TO FUSLAGE ON ALL SIDE. REMOVED UPPER AND LOWER NUT PLATE SUPPORT ANGLE AT APU INLET INTERNAL IAW SRM 51-40-02-G-0. FABBRICATED REPLACEMENT ANGLES IAW BOEING DWG. # 148N3152. R & R SUPPORT ANGLE AND STRAP IAW DWG 148N3152, 148N3141, AND 148N3138 IAW SRM.

Part: ANGLE — CORRODED (ZONE 100) · airframe 34,953 hrs · 21,431 cycles

STR / AFT CARGO COMPARTMENT ANGLE UNDER R/H TRANSITION PANEL IS CORRODED BETWEEN STA 1440 AND STA 1460, RBL 25. 031-013. ATA-53-00.REMOVED CORRODED ANGLE FROM LOWER SIDE OF R/H TRANSITION PANEL STA 1440 TO STA 1460 TO F.O.M.IAW B757-200PF SRM 51-40-02-OG-0.REMOVED CORROSION AT ANGLE AND FOUND TO BE OUT OF LIMITS IAW B757-200PF SRM 53-00-53-1A-1 (100% MATERIAL LOSS).FABRICATED CHORD PN 146N5215-1SAAU FOR AFT CARGO RH TRANS PNL, IAW DWG 146N5215.INSTALLED FABRICATED CHORD PN 146N5215-1SAAU AND R/H SIDE TRANSITION PANEL AT AFT CARGO STA 1440 TO STA 1500 IAW B757-200PF SRM 51-40-02-0G-0

Part: ANGLE — CORRODED (ZONE 100) · airframe 34,953 hrs · 21,431 cycles

STR / AFT CARGO COMPARTMENT FRAME STA 1440 LOWER FLANGE HAS CORROSION BETWEEN STGR 27RH AND STGR 28RH. 031-015. ATA-53-00.REMOVED CORRODED ANGLE AT AFT CARGO COMPARTMENT FRAME STA 1440 BETWEEN STGR 27RH AND STGR 28R REF B 757 SRM 51-40-02-OG-O.CLEANED AREA ON LWR CORNER ITERCOASTAL NO CRROSION FOUND ONLY DRIED SEALANT REF. B757 -200 AMM 51-31-01-392-081.LOCATED AND DRILLED 1EA CLIP P/N: 146N8515U1, BATCH:0004406597,AT AFT CARGO COMP, STA-1440 BETWEEN STR-27RH AND 28RH,IAW B757-200 SRM 51-40-05-0G-0.INSTALLED NEW ANGLE (CLIP) P/N: 146N8515U1, BATCH:0004406597 AND 1EA SUPPORT FITTING ASSY AT CARGO COMP STA 1440 BETWEEN STR 27 RH AND 28RH. IAW B757-200 PF SRM 51-40-02-0G-0

Part: DOOR LATCH — BROKEN (ESCAPE ROPE) · airframe 34,831 hrs · 21,365 cycles

CAPTAIN SIDE ESCAPE ROPE DOOR ASSY LATCH BROKEN REMOVED AND REPLACED CAPTAIN SIDE ESCAPE ROPE DOOR ASSY AS REQUIRED.

Part: LATCH — BROKEN (ESCAPE ROPE) · airframe 34,838 hrs · 21,369 cycles

CAPTAIN SIDE ESCAPE ROPE DOOR ASSY LATCH BROKEN REMOVED AND REPLACED CAPTAIN SIDE ESCAPE ROPE DOOR ASSY AS REQUIRED.

Part: STRINGER — CRACKED (HORIZONTAL STAB) · airframe 33,043 hrs · 20,333 cycles

*MAJOR REPAIR* FAULT: LT HORIZONTAL STABILIZER STRINGER HAS EVIDENCE OF A HORIZONTAL CRACK BETWEEN RIB 15 AND RIB 14 ON STRINGER #1. JOB WAS ACCOMPLISHED IAW UPS EO 87660-REQ1 AND VTMAE 757-5510-27-A3293 REV -.

Part: DOUBLER — CORRODED (UNKNOWN) · airframe 33,042 hrs · 20,332 cycles

FAULT- #1 ENGINE PYLON OUTBD SKIN, INNER SURFACE FWD OF VENT PANEL OPENING HAS EXFOLATION CORROSION. DOT 8-001. CERTIFIED ALL ACTION STEPS ON THIS NON-ROUTINE CARD WERE ACCOMPLISHED AND COMPLETED. INSPECTION COMPLETE

Part: PYLON — DAMAGED (UNKNOWN) · airframe 33,042 hrs · 20,332 cycles

FAULT- #2 ENGINE PYLON OUTBD SKIN, INNER SURFACE HAS EXFOLATION CORROSION. DOT 8-005 AND IN RED. REVIEWED

Part: FRAME — DAMAGED (BS 1560) · airframe 33,042 hrs · 20,332 cycles

FAULT: AFT CARGO PIT - STA 1560 RH SIDE FRAME HAS AN EXISTING REPAIR INBOARD OF STR 26R - NEED ALTERNATIVE METHOD OF INSPECTION PER UPS EO-73926-JIC002 REVIEWED

Part: PYLON — DAMAGED (UNKNOWN) · airframe 33,042 hrs · 20,332 cycles

FAULT: #2 ENG I/B FWD PYLON SKIN WITH CORROSION AT OUTSIDE SKIN. DOT 07308-001 VERIFIED JOB COMPLETE AND ACCOMPLISHED IAW UPS EO-87576-REQ1 AND VT MAE 757-5450-27-A3280 REV-

Part: BLOWER — FAILED (EVAS) · airframe 30,904 hrs · 19,010 cycles

INSPECTION TYPE:N/ART EVAS FAILED BLOWER MOTOR TESTREPLACED RT EVAS IAW 25-69-00 ESR: IPC 25-60-00-090A 002

Part: FLOORBEAM — CORRODED (BS 1600) · airframe 30,902 hrs · 19,008 cycles

INSPECTION TYPE:SEG4MAIN DECK FLOOR BEAM STA 1600 BETWEEN KBK 24.75 AND 45.50 HAS SEVERAL CORROSION.REPAIRED PER EO B757-5310-81449-A. RCD 217045 AND VT MAE EA 757-5360-A2675.

Part: FLOORBEAM — CORRODED (BS 1200 RBL24-25) · airframe 30,902 hrs · 19,008 cycles

INSPECTION TYPE:SEG4CORROSION ON MAIN CARGO FLOOR SUPPORT BEAM STA 1200 BETWEEN RBL 45.5 AND RBL 24.75REPAIRED IAW EO B757-5310-81278-A AND VT MAE EA 757-5360-27-A2661 REV-

Part: FRAME — DENTED (BS 413) · airframe 30,902 hrs · 19,008 cycles

INSPECTION TYPE:SEG4AT APPR. BSTA 413 AND STR 23L THERE IS A PROTRUDING DENT FROM INSIDE THE MAIN E/EREPAIRED IAW SRM 53-00-01-2R-29

Part: PANEL — BROKEN (ESCAPE ROPE) · airframe 30,802 hrs · 18,948 cycles

EMERGENCY ESCAPE ROPE PANEL BROKEN ON FIRST OFFICER SIDE. ACCOMPLISHED DETAILED INSPECTION PER E.O B757-2510-80884-A, REMOVED THE DOOR ASSY & DISBONDED DOOR CATCH GRABBERS. ACCOMPLISHED A DETAILED INSPECTION AT & AROUND EMERGENCY ESCAPE ROPE INSTALLATION TO VERIFY THAT THE ROPE IS NOT DMGD. ENSURED THE EMERG ESC ROPE IS INSTD. REBONDED THE CATCH ASSEMBLIES TO THE FO'S EMERGENCY ESCAPE ROPE DOOR ASSY IN REF TO B757 SRM 51-30-10. OPS CHECK GOOD.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 30,441 hrs · 18,727 cycles

INSPECTION TYPE:NA**DIVERSION-NO EMERG DECLD-NO EMERG EQUIP USED-LANDED W/OUT INCIDENT-AC TAKEN OOS** RCVD L HYD SYS PRESS MSG AFTER T/O. THE LH HYD RESERVOIR LESS THAN 1.7 PSI DURING LT & RT OPERATION.PERFORMED VISUAL INSPECTION AND FOUND FLEXIBLE HOSE BLOWN AT MAIN WHEEL WELL AREA, REMOVED AND REPLACED AS PER AMM 20-401-20-10-10, LEAK CK ACCOMPLISHED AND NO LEAKS NOTED.

Part: WEB — GOUGED (BS 560) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE: SEG3, METAL FLOOR IN FRONT OF MAIN CARGO AT BS 560 GOUGED. REPAIRED THE DAMAGE IAW SRM 53-30-15-2R-4.

Part: STRUCTURE — CORRODED (THRESHOLD) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE: SEG3, CREW ENTRY DOOR LOWER THRESHOLD FLOOR STRUCTURE CORRODED. REWORKED IAW AE 757-5311-27-A2362 REV -, AND EO B757-5310-73382-A.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 231XHF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 232XJF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 232XGF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 121XAF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N4000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 231XBF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 231XFF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 231XJF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 232XBF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 222XCF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 221XAF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH #3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 232XEF REQUIRES FAB. FABRICATED NEW FLOOR PANEL 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 221XXCF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 231XCF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 231XAF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N4000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 231XEF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N4000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 232XFF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 221XBF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 222XBF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N4000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 231XDF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 211XAF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 232XCF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 232XHF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 232XDF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 222XAF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N4000ISS-G BATCH#3489641 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 231XGF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG3 FLOOR PANEL 232XAF REQUIRES FAB. FABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH#3489461 PER SREO B757-5320-9692-K.

Part: PANEL — DELAMINATED (RT HORIZ STAB) · airframe 28,173 hrs · 17,402 cycles

INSPECTION TYPE:SEG31 DENT FOUND ON RT HORIZONTAL STAB UPR FWD TQ BOX PANEL MARKED IN RED FOUND TO BE DELAMINATED. REPAIRED DAMAGED AREA IAW SRM 51-70-10-2R AND SRM 55-10-01-1A-1 FIGURE 101 NOTE I 250.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 28,009 hrs · 17,309 cycles

INSPECTION TYPE:N/AEMER. LTS. "UNARMED" ANNUNCIATOR REQUIRES RELAMP.RELAMPED EMRE. LTS."UNARMED" ANNUNCIATOR, OPS CHRCK GOOD REF TC 0101, PG 9.

Part: SKIN — DENTED (TE FLAP) · airframe 26,966 hrs · 16,706 cycles

RT IB MAIN FLAP UPPER SKIN HAS DENT WITH DELAM 20.5" FROM OB EDGE AND 24.75" FROM T/E. REPAIRED PER EO B757-5750-68417-B.

Part: SKIN — DENTED (TE FLAP) · airframe 26,966 hrs · 16,706 cycles

3 DENTS ON MAIN I/B FLAP UPPER RT SIDE UPPER SKIN. REPAIRED PER EO B757-5750-68417-B.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 25,795 hrs · 15,971 cycles

INSPECTION TYPE: C, MAIN DECK FLOOR PANEL 231XFF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO 757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 25,795 hrs · 15,971 cycles

INSPECTION TYPE:C, MAIN DECK FLOOR PANEL 231XJF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO 757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 25,795 hrs · 15,971 cycles

INSPECTION TYPE: SEG2, MAIN DECK FLOOR PANEL 241XHF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO 757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 25,795 hrs · 15,971 cycles

INSPECTION TYPE: SEG2, MAIN DECK FLOOR PANEL 242XDF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO 757-5320-9692-K.

Part: HANDLE — BINDING (COCKPIT WINDOW) · airframe 25,739 hrs · 15,939 cycles

CAPTAIN'S WINDOW HANDLE VERY HARD TO ROTATE AFT. REPLACED THE NR 2 LT WINDOW ASSY IAW MM 56-11-02.

Part: SKIN — DAMAGED (BS 580) · airframe 25,650 hrs · 15,886 cycles

FUSELAGE SKIN PUNCTURED AT BS 580 BETWEEN STRINGERS 21 - 22L. REPAIRED IAW EO B757-5310-64052-A.

Part: STRINGER — DAMAGED (BS 570-590) · airframe 25,650 hrs · 15,886 cycles

FUSELAGE STRINGERS 21 & 22L DAMAGED BETWEEN BS 570 - 590. REPAIRED IAW EO B757-5310-64052-A.

Part: WEDGE — PUNCTURED (NR 2 SLAT) · airframe 24,055 hrs · 14,880 cycles

INSPECTION TYPE:C-9L/W WING NR 2 L/E SLAT INBD T/E WEDGE DENTED, PUNCTURED ON LOWER SURFACE. REPAIRED WITH METAL HOT BOND IAW SRM 51-70-10 AND REO-G19023, REV A.

Part: DEFLECTOR — BROKEN (THRUST REVERSER) · airframe 24,055 hrs · 14,880 cycles

INSPECTION TYPE:C-9, DURING LEAK CHECK OF THE NR 1 ENGINE THRUST REVERSER, FOUND DEFLECTOR RING ASSEMBLY TO BE BROKEN AT THE 1 O'CLOCK POSITION OF THE OTBD T/R. R & R DEFLECTOR RING IAW AMM 78-31-28-004-001-R00.

Part: WEDGE — DELAMINATED (NR 2 SLAT) · airframe 24,055 hrs · 14,880 cycles

INSPECTION TYPE:C-9, LT WING SLAT NR 2 SLAT OTBD SIDE UPPER T/E WEDGE DELAMINATED. REPAIRED WITH METAL HOT BOND REPAIR IAW SRM 51-70-10 AND REO-G19016, REV B.

Part: FRAME — CORRODED (BS 1992) · airframe 24,055 hrs · 14,880 cycles

INSPECTION TYPE:C9, S1 APU TAILCONE ATTACH FRAME AT BS 1992.8 IS CORRODED. REPLACED FRAME ASSY PN 148N1606-7.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 24,055 hrs · 14,880 cycles

INSPECTION TYPE:C9, LEFT INBD FLAP UPPER SURFACE IS DENTED, CREASED. REPAIRED WITH METAL HOT BOND REPAIR IAW SRM 57-53-01, REPAIR 1 AND 51-70-10, REPAIR 2.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 24,055 hrs · 14,880 cycles

INSPECTION TYPE: C9, LEFT INBD FLAP UPPER SURFACE IS DENTED, CREASED. REPAIRED WITH HOT METAL BOND REPAIR IAW SRM 57-53-01, REPAIR 1 AND 51-70-10, REPAIR 2.

Part: SKIN — CORRODED (BS 1992) · airframe 24,055 hrs · 14,880 cycles

INSPECTION TYPE: C-9, EMPENNAGE APU EXHAUST TAIL CONE EXTERIOR HAS CORROSION AT BS 1992.8 AND 0630 POSITION, LBL6. REPAIRED PANEL WITH METAL HOT BOND REPAIR IAW REO-G19014 AND SRM 51-70-10.

Part: FLOORBOARD — CRUSHED (MAIN CARGO) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, MAIN CARGO COMPARTMENT FLOORBOARD 231XTF IS CRUSHED AT CORNER. FABRICATED NEW FLOORBOARD IAW SREO B757-5320-9692H.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOOR PANEL XHF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692H.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOOR PANEL 231XUF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692H.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8 MAIN CABIN FLOORBOARD 242XGF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692H.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C8 MAIN CABIN FLOORBAORD 241XJF HAS DAMAGE. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692H.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,755 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOORBOARD 241XGF IS DAMAGED. FABRICATED NEW FLOORBOARD IAW SREO B757-5320-9692H.

Part: FLOORBOARD — DAMAGED (MAIN CARGO) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, MAIN CARGO FLOORBOARD 252XUF HAS DAMAGE. FABRICATED NEW FLOORBOARD IAW SREO B757-5320-9692H.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C8, MAIN CABIN FLOOR PANEL 241XCF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C8, MAIN CABIN FLOOR PANEL 231XSF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692H.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOOR PANEL 231XVF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692H.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOORBOARD 241XMF HAS DAMAGE. FABRICATED NEW FLOORBOARD IAW SREO B757-5320-9692H.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOOR PANEL 212XAF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692H.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,755 cycles

INSPECTION TYPE:C-8 MAIN CABIN FLOORBOARD 232XVF IS DAMAGED. FABRICATED NEW FLOORBOARD IAW SREO B757-5320-9692H.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOOR PANEL 232XVF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692H.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C8, MAIN CABIN FLOOR PANEL 242XFF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SERO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOOR PANEL IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8 MAIN CABIN FLOOR PANEL 232XWF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692H

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,755 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOORBOARD 252XSF IS DAMAGED. FABRICATED NEW FLOORBOARD IAW SREO B757-5320-9692H.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOORBOARD 251XQF HAS DAMAGE. FABRICATED NEW FLOORBOARD IAW SREO B757-5320-9692H.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOOR PANEL 232XYF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692H.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOORBOARD 252XTF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692H.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C8 MAIN CABIN FLOOR PANEL 211XAF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692H.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, MAIN CABIN FLOOR PANEL 242XJF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692H.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C8, MAIN CABIN FLOOR PANEL 232XUF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8 MAIN CABIN FLOOR PANEL 231XKF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692H.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C8, MAIN CABIN FLOORBOARD 251XPF HAS DAMAGE. FABRICATED NEW FLOORBOARD IAW SREO B757-5320-9692H.

Part: FRAME — DENTED (BS 1560) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, BULK CARGO COMPARTMENT FRAME DENTED AT BS 1560, STR 26-27R. REPAIRED DENTED FRAME IAW SRM 53-60-07-2R-1 AND 53-00-07-2R-5, DETAIL I.

Part: FRAME — DENTED (BS 1460) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, AFT CARGO LT SIDE FRAME DENTED BS 1460 STR 25L. REPAIRED DENTED FRAME IAW SRM 53-00-07-2R-5, FIG 201, DETAIL III.

Part: FRAME — DENTED (BS 1580) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C8, AFT CARGO LT SIDE FRAME DENTED BS 1580 S25-26L. REPAIRED DENTED FRAME IAW SRM 53-60-07-2R AND 53-00-07-2R- 5, DETAIL III.

Part: FRAME — DENTED (BS 1540) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, BULK CARGO COMPARTMENT, FRAME DENTED BS 1540, STRINGERS 23-24R. REPAIRED DENTED FRAME IAW SRM 53-00-07-2R-5, FIG 201, DETAIL III.

Part: ATTACH ANGLE — CORRODED (AFT CARGO) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, AFT CARGO LT SIDE LOWER WEB ATTACH ANGLE BELOW TRANSITION PANEL IS CORRODED. FABRICATED A NEW ATTACH ANGLE IAW DWG 146N5434-15.

Part: FRAME — DENTED (BS 1500) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C8, BULK CARGO COMPARTMENT FRAME DENTED BS 1500, STR 26R. REPAIRED FRAME IAW PF SRM 53-60-07-2R-1 AND 53-00-07-2R-5, DETAIL I.

Part: FRAME — DENTED (BS 1480) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, AFT CARGO LT SIDE FRAME DENTED BS 1480, STR 26L. REPAIRED DENTED FRAME IAW SRM 53-00-07-2R-5, FIGURE 201, DETAIL I.

Part: FLOOR SPLICE — CORRODED (AFT CARGO) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8 AFT PIT FLOOR SPLICE PLATE CORRODED AT NUMEROUS SPOTS. FABRICATED A NEW FLOOR SPLICE PLATE IAW DRAWING 453N1611-35

Part: ATTACH ANGLE — CORRODED (BS1490 S27L) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C8 AFT CARGO LT SIDE LOWER WEB ATTACH ANGLE BELOW TRANSITION PANEL CORRODED BS 1490 S27L. REMOVED, FABRICATED & INSTALLED NEW ANGLE IAW DWG.

Part: FRAME — DENTED (BS 1600) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, AFT CARGO LT SIDE FRAME DENTED BS 1600, STR. 25L. REPAIRED DENTED UPPER FLANGE OF FRAME IAW SRM 53-00-07-2R-5, FIG 201, DETAIL III.

Part: SEAT TRACK — CORRODED (BS 1040-1070) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C8, MAIN CABIN UNDER FLOOR, SEAT TRACK CORRODED AT RADIUS AND FASTENER HOLES BS 1040-BS 1070, LBL 65. R & R SEAT TRACK IAW SRM 51-40-02.

Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C8, MAIN CABIN FLOOR PANEL 251XLF INSERT MISSING AND BOARD BROKEN. FABRICATED NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: SKIN — DENTED (FWD CARGO DOOR) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:C-8, FORWARD LOWER CARGO DOOR, EXTERNAL SKIN, BELOW EXTERNAL LATCH HANDLE DENTED. REPAIRED DENTED AREA IAW EO 5230-51355-A AND SRM 52-30-01-2R-4, FIG 201, DETAIL I.

Part: SKIN — PUNCTURED (HORIZONTAL STAB) · airframe 22,160 hrs · 13,775 cycles

INSPECTION TYPE:SPV, LT HORIZONTAL STAB UPPER SKIN PUNTURE. FABRICATED AND INSTALLED RERPAIR ON LT HORIZONTAL STAB UPPER SKIN IAW REO -G16288, REV A AND EO B757-5510-51326A.

Part: SKIN — DENTED (NR 5 SLAT)

NR 5 LT SLAT DENTED. REPAIRED IAW EO B757-5750-50300-A.

Part: SKIN — DENTED (NR 2 SLAT)

LT WING NR 2 L/E SLAT HAS DENT ON UPPER SURFACE T/E WEDGE. REPAIRED REF EO B757-5750-50297A.

Part: SKIN — DAMAGED (NR 3 SLAT)

UPPER SURFACE OF NR 3 LT SLAT HAS 1 INCH DENT WITH DELAMINATED DAMAGE. REPAIRED REF EO B757-5057-50303-A.

Part: DENTED (NR 1 SLAT)

NR 1 SLAT DENTED. REPAIRED IAW EO B757-5750-50298-A.

Part: SLAT — DAMAGED (LT WING)

LT WING NR 1 SLAT DAMAGED. REPAIRED IAW EO B757-5750-49186.

Part: SLAT — DAMAGED (LT WING)

LT WING NR 4 SLAT DAMAGED. REPAIRED IAW EO B757-5750-48195-A.

Part: ADC — INOPERATIVE (COCKPIT)

ON TAKE OFF ROLL, APPROX 100 KIAS F/O AIRSPEED INDICATOR NEEDLE WENT 0, CONTINUED T/O. ONCE AIRBORNE EICAS CAUTION IAS DISAGREE. RUDDER RATIO AND MACH/SPD TRIM. COMPLETED QRH PROCEDURE F/O IAS INDICATION RETURNED TO NORMAL AFTER SELECTING ALTN AIR DATA. DIVERTED, TROUBLESHOT IAW FIM 34-12-00-815-808, FIG 107 AND 34-12-00-815-813, FIG 109. FOUND FAULT BALL ON RT ADC AND WOULD NOT TEST FROM P61 PANEL.

Part: FLOORBOARD — DETERIORATED (MAIN CARGO)

MAIN CARGO FLOORBOARD ASSY, 144N5361-22, DETERIORATED ALONG EDGE OF PANEL. MULTIPLE CHECKS TOTAL MORE THAN 2" OVER LIMITS IAW SRM 53-00-50-1 A, NOTE B. IDENTIFIED AS A MAJOR REPAIR. REMOVED PANEL AND TRANSFERED TO NR 47572 1.

Part: FLOORBOARD — DETERIORATED (MAIN CARGO)

MAIN CARGO FLOORBOARD ASSY 144N5361-22 DETERIORATED ALONG EDGE OF PANEL. MULTIPLE CRACKS TOTALING MORE THAN 2" OVER LIMIT IAW SRM 53-0 0-50-1A. IDENTIFIED AS A MAJOR REPAIR. REMOVED FLOORBOARD AND TRANSFERED TO NR 47572 0.

Part: FLOORBOARD — DETERIORATED (FUSELAGE)

MAIN CARGO FLOORBOARD ASSY, 144N5361-11, DETERIORATED ALONG EDGE OF PANEL. MULTIPLE CRACKS TOTALING MORE THAN 2" OVER LIMIT IAW SRM 53- 00-50-1A, NOTE B. IDENTIFIED AS A MAJOR REPAIR. REMOVED FLOORBOARD AND TRANSFERRED TO NR 4757 19.

Part: FLOOR SKIN — CORRODED (BS 277) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, REPAIRED COCKPIT LWR FLOOR WEB CORROSION IAW ENGINEERING AT BS 277, LBL 7, WL 200. REPAIRED COCKPIT FLOOR WEB IAW ATS ER 11-04147.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, WHILE ACCESSING FOR CUSTOMER CARD NR 945357, FOUND THE F/O'S FWD INBD AND AFT INBD SEAT TRACKS CORRODED. R & R THE F/O FWD INBD AND AFT INBD SEAT TRACKS IAW MM 25-1101-2.

Part: WEB — CORRODED (BS 1680) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, FOUND CORROSION ON THE AFT DECK PLATE AT BS 1680, BETWEEN RBL 27-54, WL 208. REPAIRED IAW ATS ER 11-04044.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, ACB FLOOR PANEL NR 4 HAS CORROSION ON UPPER SURFACE 25. FABRICATED NEW FLOOR PANEL IAW SRM 53-60-53-1A1, 51-40-05-0G, SRM 53-60-53-0I-2, 51-20-01-0G.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, WHILE ACCESSING FOR CUSTOMER CARD NR 945360, FOUND THE CAPT SEAT TRACKS (4EA) CORRODED. R & R THE 4EA CAPT SEAT TRACKS IAW MM 25-11-01-2.

Part: SKIN — DELAMINATED (LT WING) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, LT WING FIXED L/E UPPER SURFACE IS DELAMINATED AT WS 314. REPAIRED FIXED L/E UPPER SURFACE IAW SRM 57-41-01-0I, SRM 57-41-01-1A 1, SRM 57-41-01-2R-1, SRM 51-70-08, SRM 51-7017 ER 11-04065.

Part: ANGLE — CRACKED (BS 1064) · airframe 20,376 hrs · 12,706 cycles

INSP TYPE:C3, RT MAIN WHEEL WELL CUTOUT L-ANGLE IS CRACKED AT FWD OTBD CUTOUT BS 1064, RBL 60. R & R CRACKED LT ANGLE IAW SRM 51-40-020.

Part: STRAP — CORRODED (VERTICAL STAB) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, VERTICAL STABILIZER TIP-STRAP ON TOP OF STAB TIP HAS SURFACE CORROSION. REMOVED, FABRICATED AND INSTALLED VERTICAL STAB TIP STRAP IAW SRM 51-30-01, 55-30-30-01.

Part: SUPPORT — CORRODED (BS 645-764) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, FWD CARGO BAY, CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE BS 645-764, RBL 22. REPLACED THE SIDEWALL SUPPORT PLATE ASSY FROM BS 645-765, RBL 22 IAW DWG 143N5320, SRM 51-40-02-0G, SRM 51-40-05-0G, SRM 51-40-08-0G.

Part: FLOOR SUPPORT — CRACKED (BS 1470) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, ACB FLOOR SUPPORT IS CRACKED AT STA 1470, RBL 16.10. REPLACED THE AFT CARGO BAY FLOOR SUPPORT IAW DWG 146N5390, SRM 51-40-02-0G, AND SRM 51-40-05-0G.

Part: SIDEWALL PANEL — CORRODED (CARGO BAY) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT HAS AREAS OF CORROSION FROM STA 1466 TO 1530. REPLACED SIDEWALL PANEL ASSY IAW DWG 146N5390, SRM 51-40-02-0G, SRM 51-40-05-0G, AND SRM 51-40-08-0G.

Part: SKIN — CORRODED (RT ELEVATOR) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, CORROSION RT ELEVATOR UPPER SURFACE OTBD END T/E ON BONDED DOUBLER. R & R BONDED DOUBLER (CONDUCTIVE FRAME) IAW SRM 55-20-01-1A1 SRM 51-40-02-0G, AMM 51-21-10-7, DWG 183N2003.

Part: SUPPORT — CORRODED (BS 505-645) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, FWD CARGO BAY, CORROSION ON FLOOR TO SIDEWALL PLATE BS 520-645, LBL 22. REPLACE THE FWD CARGO BAY SIDEWALL SUPPORT PLATE FROM BS 505-645, LBL 22 IAW DWG 143N5320, SRM 51-40-02-0G, SRM 51-40-05-0G, AND SRM 51-40-08-0G.

Part: SKIN — CORRODED (RT ELELVATOR) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, CORROSION ND SHEAR FASTENERS ON RT ELEVATOR UPPER SURFACE OTBD END T/E ON SPLICE DOUBLER. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SPLICE STRAP IAW DWG 183N2007 AND SRM 51-40-02.

Part: SUPPORT — CORRODED (CARGO BAY) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT HAS AREAS OF CORROSION FROM STA 1640 TO 1530. REPLACED IAW DWG 146N5390, SRM 51-40-02-0G, SRM 51-40-05-0G, SRM 51-40-08-0G.

Part: TIE DOWN — DAMAGED (BS 820) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, FWD CARGO BAY, CARGO TIE DOWN FITTING LUG DAMAGED, BS 820, LBL 22. R & R CARGO TIE DOWN FITTING LUG IAW SRM 51-40-02-0G, SRM 51-40-05 AND DWG 143N1020.

Part: FRAME — DENTED (BS 1260) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, DENT ON INNER FLANGE OF ACB FRAME BS 1260, RBL 28, WL 157. REPAIRED FRAME IAW ATS ER 11-04002.

Part: SUPPORT — CORRODED (BS 765-845) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, FWD CARGO BAY, CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE BS 765-845, RBL 22. REPLACED THE FWD CARGO BAY SUPPORT PLATE ASSY IAW DWG 143N5320, SRM 51-40-02-0G, SRM 51-40-05-0G, AND SRM 51-40-08-0G.

Part: SUPPORT — CORRODED (BS 645-765) · airframe 20,376 hrs · 12,706 cycles

FWD CARGO BAY, CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE BS 645-765, LBL 22. REPLACE THE FWD CARGO BAY SIDEWALL SUPPORT PLATE FROM BS 645-765, LBL 22 IAW DWG 143N5320, SRM 51-40-02-0G, SRM 51-40-05-0G AND SRM 51-40-08-0G.

Part: SKIN — CORRODED (RT ELEVATOR) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, CORROSION ON RT ELEVATOR LOWER SURFACE OTBD END T/E OTBD SIDE OF SPLICE DOUBLER ON TIP FITTING REPAIR, REPLACE IAW ER 11-04100, DWG 183N2902.

Part: SEAT TRACK — CORRODED (BS 1680) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, MCB FLOOR SEAT TRACK HAS AREA OF CORROSION AT RBL 45, STA 1680, WL 208. REPLACED SEAT TRACK IAW SRM 51-40-02.

Part: WEDGE — DENTED (NR 6 SLAT) · airframe 20,376 hrs · 12,706 cycles

INSP TYPE:C3, DENT IN NR 6 SLAT LOWER T/E WEDGE 26" FROM INBD END 3" FROM T/E. REPAIRED DENTED T/E WEDGE IAW SRM 57-43-02-0I-1, SRM 57-43-02-1A-1 SRM 57-43-02-1, SRM 57-70-10, ER 11-03991.

Part: ATTACH BRACKET — CORRODED (BS 680) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, CORROSION ON ATTACH BRACKET FOR CREASE BEAM FWD SIDE OF BS 680 FLOORBEAM RBL 64, WL 201. REPLACED BRACKET (FITTING) IAW SRM 51-40-02-0G, SRM 53-30-13-0I 1, SR, 51-10-02-0G, AMM 51-31-01-2, DWG 143N5275, SRM 51-40-05-0G, AMM 51-21-10-7

Part: SUPPORT BRACKET — BROKEN (BS 520) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, FWD CARGO BAY CEILING SUPPORT BRACKET BROKEN BS 520, BL 0, WL 199. REPLACED BRACKET (CHANNEL) IAW SRM 51-40-02-0G, DWG PL 453N1858, SRM 51-30-01-0G, SRM 51-40-05-0G, SRM 51-20-04-0G.

Part: SEAT TRACK — CORRODED (BS 1680) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, MCB FLOOR SEAT TRACK HAS AREA OF CORROSION AT RBL 45, STA 1680, WL 208. R & R THE SECTION OF SEAT TRACK FROM BS1540-1680, RBL45, WL208 DWG 146N5220, 146N5217, SRM 51-40-02-0G, SRM 51-40-05-0G, SRM 51-40-08-0G.

Part: BRACKET — WORN (BS 1787.45) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, APU PNEUMATIC DUCT BRACKETS HAVE EXCESSIVE PLAY AT STA 1787.45. REMOVED, FABRICATED AND INSTALLED NEW PNEUMATIC DUCT BRACKETS IAW SRM 51-10-02-0G, SRM 51-40-02-0G DWG 212N3007.

Part: SKIN — DENTED (BS 688-694) · airframe 20,376 hrs · 12,706 cycles

INSPECTION TYPE:C3, PROTRUDING DENT IN FUSELAGE SKIN BS 688-694 JUST BELOW S25R. REPAIRED IAW SRM 53-00-01-2R-2.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR BOARD.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

FLOOR PANEL DAMAGED, FABRICATED NEW PANEL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: SEAT TRACK — DAMAGED (BS 440)

SEAT TRACK DAMAGED, STA 440. REPAIRED IAW EO B757-5310-41062-A.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK)

MAIN CARGO DECK FLOOR PANEL POSTION 2, 6TH FROM THE LT HAS DAMAGED BEYOND LIMITS IAW SRM B757-5300-501A1. REMOVED PANEL AND TRANSFERRED TO NRC 452049. OK TO INSTALL FLOOR PANEL. INSTALLED REPLACEMENT FLOOR PANEL IAW 53-01-01-4.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK)

MAIN CARGO DECK PANEL POSITION 1, SECOND FROM THE LT HAS DAMAGE BEYOND LIMITS IAW SRM 53-00-50-1A1. MAJOR REPAIR - PANEL REMOVED AND TRANSFERRED TO NRC 452046. RII OK TO INSTALL FLOOR PANEL. INSTALLED FABRICATED REPLACEMENT PANEL IAW AMM 53-01-01-4.

Part: SEAT TRACK — CORRODED (CABIN)

WHEN INSPECTED AREA PRIOR TO FLOORBOARD INSTALLATION FOUND CORROSION DAMAGE TO SEAT TRACK AT A/C STATION 44/ RT BUTTOCK LINE 45.50. AREA OF CORROSION IS ON THE RT SIDE OF SEAT TRACK. REMOVED CORROSION IAW ENGINEERING REQUEST. AFTER CORROSION WAS REMOVED, DAMAGED AREA IS .32 INCH LONG, .26 WIDE, .065 DEEP AT THE DEEPEST POINT, .675 OF AN INCH TO THE CLOSEST HOLE. ACCOMPLISHED EO B757-5310-40637. PERMANENT REPAIR WITHIN 60 DAYS.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK)

MAIN CARGO DECK FLOOR PANEL POSITION 2 SECOND FROM LT HAD DAMAGE BEYOND LIMITS IAW SRM 53-00-501A1. FABRICATED REPLACEMENT PANEL BY CUTTING OUT A NEW PANEL FROM A402H AND MAKING INSERT LOCATION USING EXISTING PANEL AS A TEMPLATE. DRILLED AND AND CLEANED HOLES OF DEBRIS. INSTALLED INSERTS USING 420 A/B EPI BOND.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

REF BILL OF WORK TS2930 MAIN CARGO DECK FLOOR PANEL, PN 143N5457-93, PI POSITION 2 FIRST FROM THE LT HAS DAMAGE BEYOND LIMITS IAW SRM B757-5 3-00-50-1A1. MFG FLOOR PANEL IAW EO B757-5320-9692 AND INSTALLED FLOOR PANEL IAW AMM 53-01-01-04.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK)

MAIN CARGO DECK FLOOR PANEL, POSITION 2, SECOND FROM LT HAD DAMAGE BEYOND LIMITS IAW SRM 53-00-501A1. FABRICATED REPLACEMENT PANEL BY CUTTING OUT A NEW PANEL FROM A402H AND MAKING INSERT LOCATION USING EXISTING PANEL AS A TEMPLATE. DRILLED AND AND CLEANED HOLES OF DEBRIS. INSTALLED INSERTS USING 420 A/B EPIBOND.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

REF BILL OF WORK TS2930 MAIN CARGO DECK FLOOR PANEL, PN 143N5457-3, POS 2 SECOND FROM THE LT HAS DAMAGE BEYOND LIMITS IAW SRM B757- 53-00-50-1A1. MFG NEW FLOOR PANEL IAW EO B757 5320-9692 AND INSTALLED FLOOR PANELIAW AMM B757-53-01-01-04.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

REF BILL OF WORK TS2930 MAIN CARGO DECK FLOOR PANEL PN 1141N5410-16, POSITION 1 SECOND FROM THE LT, DAMAGED BEYOND LIMITS IAW SRM B757-53- 00-50-1A1. MFG NEW FLOOR PANEL IAW EO B757-5320-9692 AND INSTALLED IAW AMM 53-01-01-04.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

REF BILL OF WORK TS2930 MAIN CARGO DECK FLOOR PANEL, PN 143N5457-85, PO POSTION 2 6TH FROM THE LT HAS DAMAGE BEYOND LIMITS IAW SRM B757-53-0 0-50-1A1, MFG NEW PANEL IAW EO B757-5320-9692 AND INSTALLED FLOOR PANEL IAW AMM 53-01-01-04.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT)

INSPECTION TYPE:N/A ATB - DURING GEAR RETRACTION EICAS MESSAGE "GEAR DISAGREE" ALONG WITH CAUTION LIGHTS AND AMBER GEAR LIGHTS ILLUMINATED. COMPLIED WITH FIM 32-30-00 FIG 114A. NO DISAGREE MESSAGE. GEAR WARNING NOW NORMAL. REF BLOCK 21.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 WHILE WORKING CUSTOMER CARD 817194 FOUND NR 6 SLAT UPPER SURFACE T/E WEDGE TO HAVE DELAMINATED AREA 9 - 28 INCHES FROM I/B END 8 INCHES FROM T/E. REPAIRED PER SRM 51-70-10, REPAIR 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND CORROSION ON SURFACE OF SEAT TRACK AT STA 1169 TO STA 1186 RBL 60. REMOVED AND REPLACED SEAT TRACK FROM STA 1080 TO STA 1186 IAW SRM 51-40-02-0G.

Part: CLOSEOUT PANEL — CORRODED (LE SLAT) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 NR 2 SLAT LOWER CLOSE OUT PANEL T/E FACE SKIN CORRODED SEVERAL LOCATIONS. REMOVED AND REPLACED IAW AMM 27-81-02-4.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 AFT CARGO BAY STATION 1640, AFT BULKHEAD SUPPORT ANGLE IS CRACKED, (LT SIDE FLOOR TO LOWER SIDEWALL TRANSITION ANGLE). REMOVED & REPLACED PER SRM.

Part: FRAME — GOUGED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 AFT CARGO BAY, GOUGE IN FRAME BS 1240 3 INCHES UP FROM STR 26L. REPAIRED PER UPS EO NR B757-5310-34776A AND ATS ER NR 09-4264.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND CORROSION ON SURFACE OF SEAT TRACK AT STA 990 TO 1040 RBL 60. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02, 51-40-05, 51-40-08 & 51-20-01-0G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND NUMEROUS CORROSION ON FLOOR SUPPORT AT STA 1055 RBL 1- RBL 24 WL 208. REMOVED AND REPLACED FLOOR SUPPORT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND CORROSION ON SURFACE OF SEAT TRACK AT STA 1100 TO 1105 RBL 47. REMOVED AND REPLACED SEAT TRACK BS 1075 TO BS 1180 RBL 45 PER SRM 51-40-02-0G, SRM 51-40-05, SRM 51-40-08, SRM 51-20-01-0G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND CORROSION ON SURFACE OF SEAT TRACK AT STA 1196 RBL 47. REPAIRED SEAT TRACK PER ATS ER NR 09-4263 AND EO NR B757-5310-34757-A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND NUMEROUS CORROSION ON FLOOR SUPPORT AT STA 1055 RBL 26-45 WL 208. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02.

Part: BEAM — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND CORROSION ON UPPER SURFACE OF LONGITUDINAL BEAM AT STA 1033 LBL 1. REPAIRED PER ATS ENGINEERING 09-4252 DATED 8/26/09.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 CORROSION ON UPPER SURFACE OF FLOORBEAM AT STA 1200 AT LBL 60 TO RBL 44. REPAIRED PER UPS EO B757-5310-34779-A AND ATS ER NR 09-4259.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND CORROSION ON SURFACE OF SEAT TRACK AT STA 1197 RBL 60. REPAIRED PER UPS EO NR B757-5310-34780-A AND ATS ER 09-4249.

Part: BEAM — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND CORROSION ON UPPER SURFACE OF LONGITUDINAL BEAM AT STA 1012 TO 1017 LBL 47. REPAIRED PER UPS EO NR B757-5310-34770-A AND ATS ER NR 09-4265.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND NUMEROUS CORROSION ON UPPER SURFACE OF FLOOR SUPPORT AT STA 1055 LBL 26 TO LBL 44. FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND NUMEROUS CORROSION ON FLOOR SUPPORT AT STA 1055 RBL 47 TO RBL 60. REMOVED CORRODED FLOOR SUPPORT, FABRICATED, INSTALLED NEW FLOOR SUPPORT PER SRM 51-40-02, 51-40-05, 51-40-08, MM 51-21-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND CORROSION ON SEAT TRACK SUPPORT AT STA 1046 RBL 1. REPAIRED PER ATS ENGINEERING ER-09-4257 DATED 8/21/09.

Part: DOUBLER — GOUGED (CARGO DOOR) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 MAIN CARGO DOOR HAS 3 (SCREW START) GOUGES AT STA 614, WL 215. DOUBLER WAS REPLACED PER SRM 51-40-02 AND DWG 69-24182.

Part: BEAM — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND CORROSION ON UPPER SURFACE OF LONGITUDINAL BEAM AT STA 1050.5 LBL 24. LONGITUDINAL BEAM REPLACED IAW SRM 51-40-02.

Part: SKIN — CHAFED (LE SLAT) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 LEFT WING NR 3 SLAT LWR T/W WEDGE SKIN IS CHAFED, ABOVE INBOARD MAIN TRACK. MARKED WITH TAPE REPAIRED IAW SRM 51-70-10 2R.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND NUMEROUS CORROSION ON UPPER SURFACE OF FLOOR SUPPORT AT STA 1055 LBL 0 TO LBL 24. FLOOR SUPPORT WAS REPLACED PER SRM 51-40-02-0G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 CORROSION ON SEAT TRACK, BS 1166 TO 1180, LBL 60, WL 208. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK PER SRM 51-40-02.

Part: BEAM — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND CORROSION ON UPPER SURFACE OF LONGITUDINAL BEAM AT STA 1046. REPAIRED PER ATS ENGINEERING REPAIR 09-4258 DATED 8/25/09.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND CORROSION ON UPPER SURFACE OF SEAT TRACK AT STA 1104 TO 1136 LBL 24. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK PER SRM 51-40-02, 51-40-05, 51-40-08, 51-24-04.

Part: DOUBLER — GOUGED (CARGO DOOR) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 MAIN CARGO DOOR HAS 3 (SCREW START) GOUGES AT STA 487, WL 215. DOUBLER WAS REPLACED PER SRM 51-40-02 AND DWG 65-25327.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND NUMEROUS CORROSION ON FLOOR SUPPORT AT STA 1016 RBL 26 TO RBL 45. REMOVED CORRODED FLOOR SUPPORT, FABRICATED, INSTALLED NEW FLOOR SUPPORT PER SRM 51-40-02, 51-40-05, 51-40-08, 51-21-10.

Part: FITTING — GOUGED (TE FLAP) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 LT WING I/B FLAP O/B FLAP TRACK FWD FITTING I/B SIDE IS GOUGED 3 EA LOCATION. FITTING WAS REPAIRED PER ATS ENGINEERING 09-4267, DATED 27AUG09.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND CORROSION ON UPPER SURFACE OF FLOORBEAM AT STA 1100 AT LBL 60 TO RBL 60. REPAIRED BS 1100 FLOORBEAM PER UPS EO B757-5310-34763-A AND ATS ER NR 09-4275.

Part: BEAM — CORRODED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 FOUND CORROSION ON LONGITUDINAL BEAM STA 1027 TO 1033 LBL 43. REPAIRED PER ATS ER 09-4265 AND UPS EO NR B757-5310-34770-A.

Part: SKIN — GOUGED (TE FLAP) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 PREVIOUS REPAIR ON RT WING O/B MAIN FLAP UPPER I/B SKIN PANEL WBL 361.0 - 374.0 GOUGED IN TWO PLACES (W4-01). REPAIRED PER ATS ENGINEERING REPAIR 09-4250 DATED 27AUG09.

Part: FASTENER — DAMAGED (VERTICAL STAB) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:C2 LIGHTNING STRIKE ON FASTENER ON LT SIDE VERTICAL STAB 6 INCHES AFT OF L/E WL 575. REPAIRED PER ATS ER 09-4262 DATED 26AUG09 AND UPS EO B757-5530-34728-A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,262 hrs · 11,400 cycles

INSPECTION TYPE:1C9 FUSELAGE BS 670 BETWEEN STR 6 & 7, 2 EA LIGHTNING STRIKES RT SIDE. REPAIRED 2EA LIGHTNING STRIKES IAW SRM 53-00-01-1A1 FIG 101 DETAIL II, SRM 53-30-101-021 FIG 101 DETAIL 11 AND SRM 53-00-01-2R6 STEPS 2-3A.

Part: STRUCTURE — DENTED (CARGO DOOR)

DENT ON NR 1 CARGO DOOR - REPAIR REF. EO B757-5230-3260 WILL REQUIRE REPETITIVE LFEC INSP PER EO EO.

Part: SKIN — DELAMINATED (AFT FLAP)

TOP SKIN INBD EDGE AFT INBD FLAP DELAM, REPAIRED IAW EO B757-5750-31869-A.

Part: FLAP — DAMAGED (LT WING)

INSPECTION TYPE:N/A LEFT I/B AFT T/E FLAP DAMAGED ON I/B SIDE DURING EXTENSION OF FLAPS. REMOVED AND REPLACED LT I/B FLAP.

Part: SMOKE DETECTOR — INTERMITTENT (COCKPIT)

ATB DUE TO CAPT AND F/O ADI SCREENS BLANKING THEN LOSING COLOR. GOT A FLT DK EQUIP SMOKE AND RECIRC FAN EICAS MSG. THEN RECEIVED A EQUIP OVHT EICAS MSG. SELECTING "ALTN" ON THE EQUIP COOLING SWITCH RESTORED SCREENS T NORMAL. REF L/P 927415 NR 1 REPEAT ITEM. CONFIRMED FAULT TO BE NR 2 FLT DECK SMOKE DETECTOR AND REPLACED SAME PER 21-58-19-2.

Part: UNKNOWN — SMOKE (COCKPIT)

DECLARED AN EMERGENCY DUE TO CREW REPORTING SMOKE IN THE COCKPIT. [SUP 05-14-07] ACCOMPLISHED AMM 05-51-14-2 HIGH ENERGY STOP INSP. FOUND NO FAULTS ON TIRES CONDITION AND BRAKE OPERATION. REF LOG PAGE 587368 ITEM 3. OPERATED APU & ENGINES FOR EVIDENCE OF OIL IN BLEED SYST. NO FAULTS FOUND.RAN L&R PACKS NO EVIDENCE OF SMOKE SMELL.INSP WINDOW HEAT TERM NO EVIDENCE OF SHORTS.INSP CARGO COMPTS & E&E OK FOR SERVICE. SUSPECT SMOKE FROM FLORIDA GROUND FIRES

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE)

RT PACK TRIPPED OFF AND LEFT PACK FAILED TO RESPOND IN FLIGHT. TESTED BOTH PACKS IAW MM 21-31-00-5. RERACK OF CABIN PRESSURE CONTROLLERS TEST PACK TEMP CONTROL IAW 21-51-00-5 AND 21-51-14-5 PLACARD INSTALLED.

Part: PBE — INOPERATIVE (COCKPIT)

A/C PBE UNIT VACUUM LOST. REMOVED AND REPLACED A/C PBE UNIT.