N452UP

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 41,781 hrs · 23,746 cycles

STR ATA 53-00 WHILE WORKING LINE# 816 T3F18E006KWYG AT THE APU AERA DOOR HOUSING TOP OF HORZ. STAB CENTER SECTION FOUND CORROSION AT ANGLE UNDER NUTPLATES. INSTALLED FORWARD STRAP P/N 148N3138-20SAAU AND LOWER ANGLE SUPPORT P/N 148N3152-1SAAU FOR APU INLET FWD DOOR HOUSING REF. B-757 SRM 51-40-02-0G-0. REVIEWED

Part: ANGLE — CORRODED (ZONE 100) · airframe 41,781 hrs · 23,746 cycles

CORROSION FOUND ON SUPPORT ANGLE FOR AFT CARGO AFT WALL R/H UPPER ANGLE RBL APPROX. 20" .ATA 53 SKILL STR. INSTALLED PANEL 161AZ HINGE AT AFT CARGO COMPT AFT CENTER WALL (BULKHEAD) IAW 757-200PF SRM 51-40-02-0G-0 AND 51-40-04-0G-0.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 41,781 hrs · 23,746 cycles

CORROSION FOUND ON SUPPORT ANGLE FOR AFT CARGO AFT WALL R/H UPPER ANGLE RBL APPROX. 20" .ATA 53 SKILL STR VERIFIED STEP 25

Part: SKIN — CORRODED (ZONE 100) · airframe 41,305 hrs · 23,478 cycles

EVIDENCE OF CORROSION ON FUSELAGE SKIN, CENTER LINE JUST AFT OF APU COMPARTMENT DOORS. INSTALLED SKIN PANEL IAW SRM 51-40-02. FILLET SEAL AND LEVELING COMPOUND COMPLETED. TOP COAT APPLIED AS REQUIRED REF SRM 51-00-00 AND AMM 51-21-00

Part: SKIN — CORRODED (ZONE 100) · airframe 41,305 hrs · 23,478 cycles

EVIDENCE OF CORROSION ABOVE APU RT COMPARTMENT DOOR, FWD HINGE. EO-92119-REQ1 IS COMPLIED WITH.

Part: SLIDING WINDOW — OUT OF ADJUST (NR 2) · airframe 40,929 hrs · 23,241 cycles

FO'S NR 2 SLIDING WINDOW OPERATING MECHANISM OUT OF ADJUSTMENT. ADJUSTED FO'S NR 2 SLIDING WINDOW OPERATING MECHANISM IAW MM 56-11-02. OPS CHECKED GOOD.

Part: SLIDING WINDOW — OUT OF ADJUST (NR 2) · airframe 40,929 hrs · 23,241 cycles

CAPTAIN'S NR 2 SLIDING WINDOW OPERATING MECHANISM OUT OF ADJUSTMENT. ADJUSTED CAPTAIN'S NR 2 SLIDING WINDOW OPERATING MECHANISM IAW MM 56-11-02. OPS CHECKED GOOD.

Part: SLIDING WINDOW — OUT OF ADJUST (R2) · airframe 40,926 hrs · 23,239 cycles

CAPTAIN'S #2 SLIDING WINDOW OPERATING MECHANISM OUT OF ADJUSTMENT READJUSTED CAPTAIN'S #2 SLIDING WINDOW OPERATING MECHANISM IAW 757 MM 56-11-02 OPS CHECK GOOD. OPEN

Part: SLIDING WINDOW — OUT OF ADJUST (NR 2) · airframe 40,926 hrs · 23,239 cycles

FO'S #2 SLIDING WINDOW OPERATING MECHANISM OUT OF ADJUSTMENT READJUSTED FO'S #2 SLIDING WINDOW OPERATING MECHANISM IAW 757 MM 56-11-02 OPS CHECK GOOD.

Part: ACTUATOR — FAILED (SLAT SYS) · airframe 40,782 hrs · 23,165 cycles

ATB, LE SLAT DISAGREE AFTER TAKEOFF RESULTED IN ATB INSTALLED #4 OUTBOARD ROTARY SLAT ACTUATOR REF MM 27-81-18-424-019 UP TO AND INCLUDING STEP E.(5)(L). CONTINUED INSTALLATION FROM STEP E.(5)(L). FOR #4 SLAT O/B ROTARY ACTUATOR. ADJUSTMENT AND OPS CK GOOD IAW AMM 27-81-18-424-019. C/W RII REQUIREMENTS PER GMM 04-02.

Part: STRINGER — CORRODED (BS 1455) · airframe 40,708 hrs · 23,122 cycles

CORROSION FOUND AT AFT PIT FUSELAGE AREA APPROX STA 1455 COMPLETED ALL STEPS OF EO-89792-REQ1 AS REQUIRED . THIS IS A PERMANENT REPAIR

Part: NOT REPORTED — CORRODED (BS 1455) · airframe 40,700 hrs · 23,118 cycles

*SDR FILED OPEN* CORROSION FOUND AT AFT PIT FUSELAGE AREA APPROX STA 1455

Part: FLOOR PANEL — CORRODED (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

*MAJOR REPAIR* FAULT-GIVING OK TO CLOSE FLOOR PANEL MAIN CARGO COMPARTMENT, FOUND (01 EA) POSSIBLE CRACK AND SPOTS WITH CORROSION AT FR 1320 BL O TO RBL 45. NO DOT. ACCOMPLISH REPAIR PER EO-87445-REQ1 AND EA 757-5360-27-A3270. REVIEWED.

Part: FLOOR PANEL — CORRODED (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

*MAJOR REPAIR* FAULT-GIVING OK TO CLOSE FLOOR PANEL MAIN CARGO COMPARTMENT, FOUND SPOTS WITH CORROSION AT FR 1280 BL O TO RBL 45. NO DOT. WORKED VERIFIED PER UPS E0 N. 87443-REQ 1 AND VT MAE EA 757-5360-27A3269. WORK COMPLETED. REVIEWED

Part: FLOORBEAM — CORRODED (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

*MAJOR REPAIR* FAULT: MAIN CARGO FLOOR BEAM STA 1440 HAS EXFOLIATION CORROSION AT BOTTOM OF BEAM RBL 24.75 ACCOMPLISH REPAIR PER EO-87428-REQ1, REV. 2 AND EA 757-5360-27-A3262. REVIEWED.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

*MAJOR REPAIR* FAULT-MAIN CARGO COMPARTMENT AT FR 1360 THE FLOOR BEAM HAS SPOTS WITH CORROSION.NO DOT ACCOMPLISH REPAIR PER EO-87430-REQ1 AND EA 757-5360-27-A3261. WORK ACCOMPLISHED PER EO-87430-REQ1. REVIEWED

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

FAULT-MAIN CARGO COMPARTMENT UNDER FLOOR, FROM FR 1400 TO FR1420 BETWEEN RBL 24 TO RBL 45 FOUND SPOTS WITH CORROSION AS MARKED IN RED. NO DOT. TREATED AND PRIMED REWORKED AREA I.A.W SRM 51-20-01. APPLIED TOP COAT A NEW CAP STRP I.A.W A.M.M 51-21-15 MIXED IN CUP P/N CCAS-1M3. INSTALLED 2EA STABILIZATION STRAPS I.A.W SRM 51-40-05. JOB COMPLETED. REVIEWED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

FLIGHT DECK DECENT DEVICE #6 EXPIRES ON AUG/2023. NO DOT INSTALLED FLIGHT DECK DECENT DEVICE #6 IAW AMM 25-61-13. REVIEWED

Part: BARRIER — CORRODED (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

9G RIGID BARRIER CORROSION ACOMMPLISHED ALL STEPS (15-21) IAW EA # 757-5310-27-A3247. REVIEWED

Part: FLOOR PANEL — DAMAGED (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

MAIN CARGO DECK FLOOR PANEL 231XCF DAMAGE. VERIFIED COMPLETION OF FABRICATED PANEL 231XCF. SRM 53-00-50-2R-1 REVIEWED.

Part: PYLON — UNKNOWN (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

FAULT: #1 PYLON DRAG FITTING REMOVAL APPLIED TOPCOAT I/B UPPER DRAG FITTING SKIN IAW E.O B757-5710-69618-I. REVIEWED

Part: DOUBLER — CORRODED (UNKNOWN) · airframe 39,956 hrs · 22,708 cycles

REPAIR DOUBLER BLENDOUT REVIEWED.REMOVED DOUBLER AND TRIPLERS IAW 51-40-02-0G.CLEANED SURFACE CORROSION & REPAIR FASTENER HOLES IAW B757 SRM 51-10-02

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

FLIGHT DECK CORR ZONE 211 REMOVED CORROSION AT FLIGHTDECK ZONE 211 LOWER FLOOR PANEL IAW SRM 51-10-02. TREATED AND PRIMED AREA IAW SRM 51-20-01. APPLIED TOP COAT IAW AMM 51-21-15, PAINT MIXED IN CUP P/N CCAS-1M3. REINSTALLED SUPPORT IAW SRM 51-40-02 REVIEWED

Part: FRAME — UNKNOWN (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

FAULT: UPON ACCOMPLISHMENT OF EO (B757-5310-73926-A) AN EXISTING REPAIR WAS FOUND AT STA 1360 RH STR 26R TO 28R. ALTERNATE INSPECTION REQUIRED ACCOMPLISHED THE WORK PER EO-86093-REQ1 AND VT-MAE EA 757-5360-27-A3229. REVIEWED

Part: TORQUE BOX — INOPERATIVE (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

L/H TORQUE BOX PANEL DISBONDED TREATED AND PRIMED PER SRM 51-20-01. INSTALLED TORQUE BOX PANEL IAW SRM 51-40-02. REVIEWED.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

MAIN CARGO COMP. VERIFIED WORK PER UPS EO-87201 AND VT MAE EA 757-5360-27-A3243. REVIEWED

Part: THRUST REVERSER — INOPERATIVE (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

FAULT: #2 ENG INBD T/R AFT HOLD OPEN ROD FITTING SHIM STACK LOOSE. WORN SCREWS REPLACED AT #2 ENG INBD T/R AFT HOLD OPEN ROD FITTING SHIM STRACK SCREWS IAW SRM 51-40-02-0G. REVIEWED

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

MAIN CARGO COMP. TREATED AND PRIMED AFFECTED AREA IAW SRM 51-20-01. APPLIED CIC ON ENTIRE AREA IAW AMM 51-00-59. REVIEWED

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

FLIGHT DECK ZONE 212 REINSTALLED NEW FASTENER IAW SRM 51-40-02 PARAGRAPH 4. APPLIED TOP COAT FLIGHT DECK ZONE 212 LOWER FLOOR PANEL VERIFIED. REVIEWED

Part: FRAME — DENTED (UNKNOWN) · airframe 39,953 hrs · 22,705 cycles

*SUPPLEMENTAL SDR* FAULT: DENT IN FRAME FRS 1500L/H OUTBD OF STR 26. L= .700, W= .600. PERFORMED COLD WORK TO 4 HOLES I.A.W. S.R.M.51-40-09. INSTALLED NEW J-SECTION REPAIR AT STA 1500 LH, I.A.W. S.R.M. 53-00-07-2R-5. TREATED AND PRIMED NEW J-SECTION I.A.W.S.R.M. 51-20-01 (OUT OF SEQUENCY). VERIFIED ALL WORK COMPLETED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,929 hrs · 22,693 cycles

*** SDR FILED OPEN *** FAULT: DENT IN FRAME FRS 1500L/H OUTBD OF STR 26. L= .700, W= .600. VERIFIED ALL WORK COMPLETED.

Part: FRAME — DENTED (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

AULT: TWO DENTS IN FRAME FRS 1520 L/H BETWEEN STR 25 AND STR 26. DENT #1 L=.800, W= .400. DENT #2 L=1.2, W = .800. INSTALLED NEW STR CLIP 26 AND 25 AT FRAME 1520 L/H IAW SRM 51-40-02 AND SRM 53-00-07-2R-5. APPLIED CIC ON J-SECTION REPAIR AND STR CLIP IAW AMM 51-00-59. REVIEWED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,929 hrs · 22,693 cycles

*** SDR FILED OPEN *** FAULT: DENT IN FRAME FRS 1460R/H INBD OF STR 26. L=1.300, W= .800 VERIFIED ALL THE WORK COMPLETED.

Part: FRAME — DENTED (UNKNOWN) · airframe 39,953 hrs · 22,705 cycles

*SUPPLEMENTAL SDR* FAULT: DENT IN FRAME FRS 1460R/H INBD OF STR 26. L=1.300, W= .800 PERFORMED SURFACE HFEC INSP ON THE CUTOUT EDGES AND SURROUNDING SURFACE AREA TO THE FRAME REPAIR AT STA 1460 R/H SIDE. SURFACE AREA AND SURROUNDING SURFACE IS CRACK / DEFECT FREE AT THIS TIME. ACCOMPLISHED INSP IAW NTM PART 6 51-00-19. NDT COMPLETE. INSP ONLY T91112. PERFORMED COLD WORK AT 4 HOLES FROM FRAME REPAIR STA 1460 RH I.A.W. S.R.M 51-40-09. INSTALLED J-SECTION REPAIR AT STA 1460 RH, I.A.W. S.R.M. 53-00-07-2R-5. REINSTALLED TIE DOWN FITTING AT STA 1460 RH, I.A.W. .S.R.M. 51-40-02. TREATED AND PRIMED NEW J-SECTION I.A.W.S.R.M.51-20-01 (OUT OF SEQUENCY). VERIFIED ALL WORK COMPLETED.

Part: FRAME — DENTED (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

FAULT: DENT IN FRAME 800 AT S24R. L=.725, W=.375 INSTALLED STR CLIP 24 R/H AT FRAME 800 VERIFIED. TREATED AND PRIMED SHEAR TIE STR 23 RH AND STR 24 RH IAW SRM 51-20-01 IN CUP P/N 02-012-176. INSTALLED 192AR PANEL PER SRM 51-40-02.REVIEWED

Part: PYLON — CORRODED (UNKNOWN) · airframe 39,932 hrs · 22,696 cycles

FAULT: #1 ENGINE PYLON OUTBD SIDE INNER SKIN FWD OF VENT PANEL OPENING HAS EXFOLIATION CORROSION. DOT 8-001 PLACED ON OUTSIDE VERIFIED REPAIR COMPLETED PER E.O. 87155-REQ1 AND VTMAE E.A. 757-5450-27-A3238 REV. JOB COMPLETED. REVIEWED.

Part: FLOOR PANEL — NONE (MAIN DECK) · airframe 38,963 hrs · 22,132 cycles

INSPECTION TYPE:N/AMAIN DECK SIDE VERTICAL RESTRAINT ZEE DAMAGE REPAIR AT POS 15RMANUFACTURED NEW FLOOR PANEL IAW E.O. B757-5320-9692-K

Part: NONE — CORRODED (WS 770LH TE) · airframe 37,930 hrs · 21,506 cycles

INSPECTION TYPE:C**SUPPLEMENTAL SDR**LH WING LOWER SKIN AT STA 760 TE HAS A 1.30" LONG BY 4.00" WIDE AREA OF INTERGRANULAR CORROSION WHICH WHEN REMOVED HAD .110" OF MATERIAL LOSS MAX ALLOWED IS .40" PER SRM 57-20-01-1A-1 TABLE 2.REPAIR PER RCD INSTRUCTIONS EO B757-5730-82166-A.

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 37,930 hrs · 21,506 cycles

INSPECTION TYPE:SEGMAIN CARGO COMPARTMENT FLOOR PNY 241XKF 3 MISSING INSERTSFABBED PNL PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 37,930 hrs · 21,506 cycles

INSPECTION TYPE:SEGPNL 242XBF DAMAGEDFABBED PNL PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (NDC) · airframe 37,930 hrs · 21,506 cycles

INSPECTION TYPE:SEGPNL 241XJF DAMAGEDFABBED PANEL PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 37,930 hrs · 21,506 cycles

INSPECTION TYPE:SEGPNL 242XMF DAMAGEDFABBED PNL PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 37,930 hrs · 21,506 cycles

INSPECTION TYPE:SEGPNL 242XJF DAMAGEDFABBED PNL PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 37,930 hrs · 21,506 cycles

INSPECTION TYPE:SEGPNL 242XFF DAMAGEDFABBED PNL PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 37,930 hrs · 21,506 cycles

INSPECTION TYPE:SEGPNL 242XLF DAMAGEDFABBED PANEL PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 37,930 hrs · 21,506 cycles

INSPECTION TYPE:SEGPNL 242XHF DAMAGEDFABBED PNL PER SREO B757-5320-9692-K

Part: FLOOR PANEL — NONE (MDC) · airframe 37,930 hrs · 21,506 cycles

INSPECTION TYPE:SEGPNL 241XMF DAMAGEDFABBED PNL PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 37,930 hrs · 21,506 cycles

INSPECTION TYPE:SEGPNL 242XAF DAMAGEDFABBED PNL PER SREO B757-5320-9692-K

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 37,708 hrs · 21,372 cycles

INSPECTION TYPE:N/A**DIVERSION*NO EMERG*A/C LANDED W/O INCIDENT*DURING FLAP RETRACTION ON DEPARTURE WHEN FLAPS UP SELECTED, EICAS MSG LE SLAT DISAGREE DISPLAYED LE SLAT DISAGREE CHECKLIST EXITED WHEN LE DISAGREEE MSG DID NOT EXTINGUISH WHEN LE ALTN FLAP SWITCH SELECTED. ACCOMPLISHED LE SLAT ASYMETRY CHECKFOLLOWED FIM 27-51-00-815-805 AND PERFORMED BITE TEST. MSG WAS CLEARED NO FURTHER MESSAGES SHOWN. FLAP/SLAT WERE RECYCLE AS PER AMM 27-81-00-862-045. NORMAL OPERATION OK

Part: WARNING MESSAGE — FALSE ACTIVATION (SLAT SYSTEM) · airframe 37,559 hrs · 21,285 cycles

ATB, NO EMERG DECLAIRED, LANDED UNEVENTFULLY. AFTER TAKEOFF LE SLAT DISAGREE EICAS ON FLAP RETRACTION.PERFORMED BITE PROCEDURE, NO FAULT FOUND IAW FIM 27-51-00/101 AND FIM 27-81-00-815-803 SLATS OPERATIONAL TEST ALL TEST NORMAL.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 35,246 hrs · 19,940 cycles

ATB - AFTER LIFTOFF RECEIVED A MAIN CARGO DOOR MESSAGE WITH LIGHT. ACFT REMAINED PRESSURIZED. AIR TURNBACK. MAIN CARGO DOOR SYSTEM MSG. TRANSFERRED MAIN CARGO DOOR INDICATION PER MEL/DMP 52-71-1. MAIN CARGO DOOR CLOSED/LATCHED/FAIRED.CKD & ADJUSTED MCD INTERLOCK SWITCHES IAW AMM 52-72-00-825-183. CKD ADJUSTMENT OF MCD LOCK SWITCHES IAW 52-72-00-825-166. SWITCHES WERE IN LIMITS. MCD OPS CKS GOOD IAW AMM 52-32-00-715-011. THIS CLEARS M693385

Part: ENGINE — FAILED (LEFT) · airframe 34,689 hrs · 19,600 cycles

INSPECTION TYPE:N/A ATB - ENGINE FAILED IN FLIGHT. ENGINE #1 REPLACED REF LOG PAGE 196334, ITEM 2.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 34,569 hrs · 19,538 cycles

ATB -- L/E SLAT DISAGREE.TROUBLESHOT PER FIM 27-81-00 FIG 104, NO DISCREPANCIES FOUND AFTER SEVERAL HYD & ELECTRIC OPERATIONS. OK FOR SERVICE.

Part: DOOR — INOPERATIVE (L1) · airframe 33,539 hrs · 18,997 cycles

CREW DOOR OPEN LATCH MISSING NUT & REMOVED LATCH ASSY. LATCH ASSY ORDERED REQ 249304A JM 0557451 INSERT INSTALLED NUT TOP INBD. RE-INSTALLED LATCH ASSY REF. BOEING DRAWING 141N6015. DEFERRED PER E.O. B757-5210-70642-A.REMOVED CREW ENTRY DOOR HOLD OPEN LATCH ASSLY IAW SRM 51-40-02-06. INSTALLED NEW CREW DOOR LATCH HOLD OPEN ROD INSERT IAW EO B757-5320-3220. RE-INSTALLED CREW ENTRY DOOR HOLD OPEN LATCH ASSY IAW SRM 51-40-02. THIS CLEARS D653460

Part: NUT — MISSING (DOOR OPEN LATCH) · airframe 33,539 hrs · 18,997 cycles

THE CREW DOOR OPEN LATCH WAS MISSING A NUT. REMOVED THE LATCH ASSY. INSTALLED THE NUT AND INSTALLED THE LATCH ASSY IAW DRAWING 141N6015. OPEN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,039 hrs · 18,745 cycles

EMERGENCY LIGHT INOP EXIT. FOUND ALL BULBS BURNED OUT. RELAMPED ASSY PER MM 33-51-01-962-0001 OPS CHECKS NORMAL.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 32,978 hrs · 18,687 cycles

INSPECTION TYPE:C, MAIN DECK FLOOR PANEL 241XKF HAS A BROKEN FASTENER HOLE. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 32,978 hrs · 18,687 cycles

INSPECTION TYPE:CRH I/B FLAP T/E LWR SURFACE WEDGE PANEL STA 161 HAS 3/16" PUNCTURE. REPAIRED PER SRM 57-53-01-2R-1, AND 51-70-06-0G.

Part: TEE FITTING — CORRODED (BS 1180) · airframe 32,978 hrs · 18,687 cycles

INSPECTION TYPE: SEG4, BS 1180 FWD OF RAT FRAME CORRODED AROUND NUTPLATES. FABRICATED A NEW TEE IAW DWG 149N7528, INSTALLED THE NEW TEE IAW SRM 51-40-02-0G, AND DWG 149N7529.

Part: SMOKE GOGGLES — CRACKED (COCKPIT) · airframe 32,182 hrs · 18,188 cycles

OBSERVER`S SMOKE GOGGLES HAD A CRACKED LENS. REPLACED THE SMOKE GOGGLES.

Part: EVAS UNIT — UNSECURE (CAPTAIN'S) · airframe 32,118 hrs · 18,146 cycles

THE CAPTAIN`S EVAS UNIT IS NOT SECURE. ILAYING IN STORAGE BIN. SECURED THE CAPTAIN'S EVAS UNIT IAW 2560-45127-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: C, MAIN DECK FLOOR PANEL 231XBF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE:C, MAIN DECK FLOOR PANEL 221XCF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: SEG3, MCD FLOOR PANEL 232XSF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: SEAT TRACK — CORRODED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE:SEG,3 MAIN DECK AREA AT BS 440, RBL 45 SEAT TRACK FLANGE HAS CORROSION ON FASTENER HOLE. FABRICATED AND INSTALLED A REPLACEMENT SEAT TRACK AND REPAIR IAW SRM 53-00-52-2R-5.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: SEG3, MCD FLOOR PANEL 231XEF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: SEG3, MCD FLOOR PANEL 222XBF DAMAGED. FABRICATED FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: SEG3, MCD FLOOR PANEL 231XJF. FABRICATED FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: SEG3, MCD FLOOR PANEL 232XEF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE:SEG3, MCD FLOOR PANEL 231XGF DELAMINATED. FABRICATED FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE:SEG3, MCD FLOOR PANEL 231XDF DELAMINATED. FABRICATED FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE:SEG 3, MCD FLOOR PANEL 222 XAF DELAMINATED. FABRICATED FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE:SEG3, MCD FLOOR PANEL 252XJF BROKEN. FABRICATED FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: SEG3, MCD FLOOR PANEL 251XJF BROKEN. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: SEG3, MCD FLOOR PANEL 222XCF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: CMCD, FLOOR PANEL 232XHF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: SEG3, MCD FLOOR PANEL 252XHF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE:SEG3, MCD FLOOR PANEL 232XFF DELAMINATED. FABRICATED FLOOR PANEL 232XFF FROM A402H-48X144 BATCH 2801694 IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: SEG3, MCD FLOOR PANEL 252XUF DELAMINATED. FABRICATED FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: NUT PLATE — CORRODED (BS 1040-1060) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: C, MAIN DECK BS 1040-1060, LBL 45-64 DOME NUTPLATE HAS SURFACE CORROSION AND DAMAGED DOME NUTS. FABRICATED NEW FLOOR SUPPORT TEE ON TR T16/11-2862 IAW DWG 144N5005-7.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE:SEG3, MCD FLOOR PANEL 231XHF DELAMINATED. FABRICATED FLOOR PANEL 231XHF FROM A402H-48X144 BAT 2801694 IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — NOT REPORTED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE:SEG3, MCD FLOOR PANEL 232XDF. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: SEG3, MCD FLOOR PANEL 232XJF DELAMINATED. FABRICATED FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: SEG3, MCD FLOOR PANEL 232XWF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO 5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE:SEG3, MCD FLOOR PANEL 232XGF DELAMINATED. FABRICCATED FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: SEGS, MCD FLOOR PANEL 231XFF DELAMINATED. FABRICATED FLOOR PANEL IAW SREO B757-5320-9692-H.

Part: FLOORBEAM — CORRODED (BS 1480) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE:SEG, MAIN DECK AREA RT SIDE AT BS 1480, RBL 5 FLOORBEAM LOWER FLANGE HAS CORROSION UNDER NUTPLATE. ACCOMPLISHED REPAIR IAW EA 757-5365-27-A199 AND EO B757-5310-60238-A.

Part: FLOORBEAM — CORRODED (BS 1520) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE: C, MAIN DECK RT SIDE AT BS 1520 RBL24-RBL45 FLOORBEAM LOWER FLANGE HAS CORROSION ON NUTPLATE, REMOVED CORROSION IAW SRM 51-10-02-0G ACCOMPLISHED EO B757-5310-60220-A REV.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 31,175 hrs · 17,549 cycles

INSPECTION TYPE:C, RT VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL IS DELAMINATED. R & R PANEL IAW SRM 51-40-02-0G AND DWG 175N2001 SHEET.

Part: SKIN — PUNCTURED (BS 263 - 270) · airframe 30,791 hrs · 17,331 cycles

LEFT FUESLAGE SKIN PUNCTURE REPAIR BETWEEN BS 263 AND 270.5, S20L. REPAIRED IAW EO B757-5330-57793-B.

Part: SKIN — PUNCTURED (BS 263-270) · airframe 30,526 hrs · 17,171 cycles

SKIN PUNCTURED AT BS 263 TO BS 270.5 5 INCHES BELOW S20L. TEMP REPAIR IAW EO 5330-577934A TEMP REPAIR IAW EO 757-5330-57793-A. ACFT OK FOR SERVICE.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 29,483 hrs · 16,563 cycles

INSPECTION C10, MAIN CABIN FLOOR PANEL 231XVF IS DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (FS 906 RBL 10) · airframe 29,483 hrs · 16,563 cycles

INSPECTION: C10, MAIN CABIN FLOOR PANEL 241XGF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW REOB757-5320-9692.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 29,483 hrs · 16,563 cycles

INSPECTION C-10, MAIN CABIN FLOORBOARD 241XCF HAS EDGE DAMAGE. FABRICATED FLOORBOARD IAW SREO B757-5320-9692-H.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 294,830 hrs · 16,563 cycles

INSPECTION C-10, MAIN CABIN FLOORBOARD 241XAF IS DAMAGED. FABRICATED FLOORBOARD IAW SREO B757-5320 9 9692-H.

Part: ACCESS PANEL — CORRODED (HORIZONTAL STAB) · airframe 29,483 hrs · 16,563 cycles

INSPECTION C-10, CORROSION ON RT HORIZONTAL ACCESS PANEL 345HB. REPLACED ACCESSPANEL WITH NEW IAW SRM 51-40-02.

Part: FLOOR PANEL — DAMAGED (BS 1165 LBL 50) · airframe 29,483 hrs · 16,563 cycles

INSPECTION C10, MAIN CARGO FLOOR DAMAGED. FABRICATED NEW FLOOR PANEL.

Part: SWITCH — BROKEN (EMERGENCY LIGHTS)

EMERGENCY LIGHT UNARMED LIGHT BROKEN. R & R UNARMED LIGHT SWITCH ASSY IAW MM 33-13-00. OPS CHECKED GOOD.

Part: FRAME — DENTED (BS 1260 S23R) · airframe 27,652 hrs · 15,424 cycles

INSPECTION TYPE: C, BS 1260, STR 23R, FRAME IS DENTED. REPAIRED DENTED FRAME IAW EO B757-5310-46731-A.

Part: FLOORBOARD — DAMAGED · airframe 27,652 hrs · 15,424 cycles

INSPECTION TYPE: C, FLOORBOARD 212XAF HAS DAMAGE. REPLACED FLOORBOARD IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED · airframe 27,652 hrs · 15,424 cycles

INSPECTION TYPE: C, FLOOR PANEL 211XAF DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.

Part: WINDOW — STIFF (COCKPIT)

F/O'S WINDOW HARD TO LATCH PROPERLY AND IS HARD TO OPEN LAST FEW INCHES OF THROW. R & R NR 2 WINDOW AND GEARBOX ASSY.

Part: FRAME — DENTED (BS 1280 S26-27L) · airframe 27,652 hrs · 15,424 cycles

INSPECTION TYPE: C, CARGO BAY BS 1280, S26-27L FRAME DENTED. REMOVED DAMAGE AND REPAIRED FRAME IAW EA 120373 IR/U EO B757-5310-46704-A.

Part: WINDOW — LACK OF LUBE (COCKPIT)

F/O EMER EXIT WINDOW LATCH RELEASE IS VERY STIFF TO OPEN REQUIRES LARGE PULL EFFORT TO UNLATCH WINDOW TO OPEN POSITION. CLEANED/LUBED LATCH CAMS -R-2 WINDOW, PERFORMED ADJ/TEST IAW MM 56-11- 00-05, CHECKS OK.

Part: SKIN — DAMAGED (BS 1679)

FUSELAGE SKIN DAMAGE AT BS 1679. REPAIRED IAW EO B757-5330-43896-B.

Part: ACTUATOR — INOPERATIVE (LT MLG)

GEAR LEVER WOULD NOT MOVE TO UP POS IN FLIGHT.WAS FREE TO MOVE TO UP P OS WHEN LOCK OVRD PUSHED. T/S PER FIM 32-30-00. FOUND LUG ON THE END OF TRUCK POSITIONER ACTUATOR BROKEN. (LT GEAR) R&R LEFT MLG TRUCK POSITIONER ACTUATOR IAW MM 32-32-15-4.

Part: LINE — SPLIT (HYD SYSTEM)

LOST LT HYD SYS PSI. T/S SYS FOUND LT MLG DOWN LOCK ACTUATOR RETURN LINE SPLIT. R & R LINE W/REF TO IPC 32-32-51-15 AND AMM 32-11-12-4.

Part: SWITCH — INOPERATIVE (RT WING SLATS)

ATB - L/E SLAT DISAGREE. FOUND SWITCH S10339 ON RT WING OTBD INOPERATIVE. S10339 REMOVED/INSTALLED S10339 STARTING AT STEP 3 TO THE END OF M/M 27-81-42-4. ALSO REF WDM 27-81-31. SYS OPS CKS NORMAL. ACFT OK FOR CONT SVC.

Part: WINDOW — OUT OF ALIGNMENT (COCKPIT)

F/O COCKPIT WINDOW - UNABLE TO CLOSE AND LOCK. PERFORMED R2 WINDOW ADJ/TEST IAW AMM 56-11-02-5. WINDOW OPS NORMAL.

Part: WINDOW — FAILED (COCKPIT)

F/O WINDOW UNABLE TO CLOSE WITHOUT USING 2 PEOPLE. REQUIRES FORCE TO CLOSE WINDOW EXTREMELY HIGH. ABLE TO CLOSE WINDOW AFTER 8 ATTEMPTS. ACCOMPLISHED ADJUSTMENT OF INBD/OTBD OF NR2 WINDOW IAW AMM 56-11-02-5 PARA (3). OPS CK NORMAL. OK FOR CONTINUED SERVICE.

Part: LATCH — BINDING (COCKPIT WINDOW)

R2 WINDOW LATCH MECHANISM JAMMING. R & R R2 WINDOW TO STEP 4C9 OF MM 56-11-02-4. COMPLETED REMAINING STEPS 4C10 THROUGH 4C21, AMM 56-11-02-4. OPS CK GOOD RII WINDOW HEAT POWER TERMINALS IAW GMM 04-02-MM 56-11-02-4.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, AFT CARGO BAY NR 4 FLOOR PANEL DAMAGED. REPLACED IAW SRM 53-00-53-1A-1.

Part: SKIN — DENTED (BS 1314 S24-25L) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, SKIN DENT AT BS 1314, STR24-25L. REPAIRED IAW SRM 53-00-01-2R-7.

Part: FLOORBEAM — CORRODED (BS 1360) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, CORROSION ON BS 1360 FLOORBEAM LOWER FLANGE, RBL 26.5 TO 34, WL 201. REPAIRED IAW ER NR 10-2331.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 FLOOR PANEL FROM BS 1420 TO BS 1540 LBL 45 TO LBL 60 IS DELAMINATED. REMOVED AND FABRICATED FLOOR PANEL PER EO B757-5320-9692-G.

Part: SKIN — GOUGED (BS 1882) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FOUND 5 INCH LONG GOUGE IN EXTERIOR SKIN AT BS 1882.7 CLOSE OUT PANEL AREA 3133L. REPLACED IAW 10-2425.

Part: SKIN — GOUGED (BS 1882) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FOUND 5 INCH LONG GOUGE IN EXTERIOR SKIN AT BS 1882.7 CLOSE OUT PANEL AREA 3133R. REPAIRED IAW SRM 53-80-01-0I, SRM 51-10-02-0G, SRM 53-80-01-1A.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 MAIN CARGO BAY FLOOR PANEL AT BS 440-480 LBL 0-25 PUNCTURED ON UPPER SURFACE. REPLACED PER SRM 53-00-50-1A1 AND UPS EO B757-5320-9692-G.

Part: FLOOR PANEL — PUNCTURED (BS 333-440) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, MAIN CARGO BAY FLOOR PANEL BS 333-440 LBL 0-25 PUNCTURED AND DENTED ON UPPER SURFACE. FABRICATED REPLACEMENT PANEL IAW SRM ADENDUM B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 MAIN CARGO BAY FLOOR PANEL BS 440-480 RBL 25-45 PUNCTURED AND DENTED ON UPPER AND LWR SURFACE. REPLACED FLOOR PANEL PER UPS EO B757-5320-9692-G AND SRM 53-00-50-1A-1.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 FIBER GLASS DELAMINATED FROM MILLED AREA ON MAIN CARGO BAY FLOOR PANEL LOWER SURFACE BS 440 TO 480 RBL 45-60. REPLACED PER SRM 53-00-50-1A1 AND UPS EO B757-5320-9692-G.

Part: FLOOR PANEL — PUNCTURED (BS 333-440) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, MAIN CARGO BAY FLOOR PANEL BS 333-440 RBL 25-45 PUNCTURED AND DENTED ON UPPER AND LOWER SURFACES. FABRICATED REPLACEMENT PANEL IAW SRM ADENDUM B757-5320-9692-G.

Part: FRAME — DAMAGED (BS 580 S22-23L) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, BS 580 FRAME BETWEEN STR 22 AND 23 LT HAD HOLES IN THE RADIUS DUE TO A SIDEWALL LINER REPAIR. REPAIRED IAW ER NR 10-2333.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 AFT CARGO BAY 3 FLOOR PANEL IS CORRODED. REPAIRED IAW SRM 53-60-53-01-1, AND SRM 51-40-05-06-A.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, AFT CARGO NR 2 FLOOR PANEL IS CORRODED. FABRICATED NEW PANEL IAW SRM 53-60-53-01.

Part: FLOORBEAM — CORRODED (BS 1020) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FOUND CORROSION ON FLOOR SUPPORT AT BS 1020 LBL 25 TO LBL 45. R & R SUPPORT IAW SRM 51-40-02

Part: FLOOR PANEL — DAMAGED (BS 1600-1680) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, MCB, BSTA. 1600 TO 1680, RBL 45 TO RBL 65, FLOOR PANEL IS DAMAGED. REPLACED IAW SRM 53-00-50-1A1, EO B757-5320-9692-G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 FOUND CORROSION ON FLOOR SUPPORT AT STA 1055 FROM BL 0 - LBL 44. REMOVED AND REPLACED SUPPORT PER SRM 51-40-02.

Part: FLOOR PANEL — DELAMINATED (BS 440) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FLOOR BOARD BROKEN AT BS440, LBL65. CORNER DELAMINATED REPLACED FLOOR PANEL IAW SRM 53-00-50-1A1 AND UPS EONR B757-5320-9692-G

Part: THRESHOLD — CORRODED (CARGO DOORWAY) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, CARGO DOOR CUTOUT LOWER SILL NUT PLATE STRIP FOR ENTRY THRESHOLD CORRODED. CORROSION REMOVAL BEYOND ALLOWABLE DAMAGE. REMOVED, FABRICATED, INSTALLED REPLACEMENT STRIP.

Part: FLOORBEAM — CORRODED (BS 1200) · airframe 25,189 hrs · 14,052 cycles

INSP TYPE:C4 BS 1200 FLOORBEAM HAS CORROSION ON UPPER SURFACE OF UPPER FLANGE AT SEVERAL NUTPLATE LOCATIONS, LBL 24 TO RBL 50, WL 208.1 (MARKED) REMOVED CORROSION IAW SRM 51-10-02 FOUND AREA TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW REPAIR DWG LOR5L53006.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 FOUND CORROSION ON FLOOR SUPPORT AT STA 1020 ON LBL 3-22. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1200) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, BS1200 FLOORBEAM HAS CORROSION ON UPPER SURFACE OF UPPER FLANGE AT SEVERAL NUTPLATE LOCATIONS, LBL24 TO RBL50 WL208.1. (MARKED) REMOVED CORROSION IAW SRM 51-10-02, FOUND AREAS TO BE OUT OF LIMITS, FABRICATED REPAIR AND INSTALLED IAW REPAIR DWG LOR5L53006.

Part: SEAT TRACK — CORRODED (BS 1201-1204) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, CORROSION ON SEAT TRACK UPPER SURFACE AT BS 1201 TO 1204 RBL 24-26 WL 208. R & R SEAT TRACK IAW SRM 51-40-02.

Part: SEAL DEPRESSOR — DAMAGED (CARGO BAY) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 MCB DOOR CUTOUT STRUCTURE, SEAL DEPRESSOR DAMAGED AT BS 480 BETWEEN STR 6L TO 9L (MARKED). REPLACED SEAL DEPRESSOR AT BS 480 STR 6L TO 9L SRM 51-10-02-0G SRM 51-40-02-0G, SRM 51-40-05, AND AMM51-21-10-7 AND AMM51-31-01-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 FOUND CORROSION ON FLOOR SUPPORT AT STA 1055 LBL 41. REMOVED AND REPLACED SUPPORT PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 FOUND CORROSION ON FLOOR SUPPORT AT STA 1015 TO 1018 RBL 30. REMOVED AND REPLACED SUPPORT PER SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1198) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 FOUND CORROSION ON SEAT TRACK AT STA 1198 ON LBL 26 R&R SEAT TRACK IAW SRM 51-40-02.-

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 SEAT TRACK GOUGED BS 1592, RBL 45, WL 208. REPAIRED PER ATS ER 10-2357 UPS EO B757-5310-37413-A.

Part: STRAP — CORRODED (BS 1401-1419) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, CORROSION ON UPPER SURFACE OF RBL 25 STABILIZER STRAP BS 1401 TO BS 1419, WL 201. BLENDED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED, LOCATED, DRILLED, ALODINED AND PRIMED, PAINTED. REPLACED STABILIZER STRAP IAW SRM 51-20-01-0G, SRM 51-40-06

Part: FLOORBEAM — CORRODED (BS 1100) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, CORROSION ON BS 1100 FLOORBEAM FROM LBL 1 TO 22 WL 208 REPAIRED IAW ER NR10-2335.

Part: FLOOR PANEL — CRACKED (BS 900-1020) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, MAIN CARGO FLOOR PANEL STA 900 TO 1020 RBL46 TO 61 WL208 FLOOR PANEL CRACKED AT STA 940. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: SUPPORT — CORRODED (CARGO BAY) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, AFT CARGO LT FLOOR TO SIDEWALL SUPPORT UPPER SURFACE IS CORRODED. CORROSION REMOVAL BEYOND ALLOWABLE DAMAGE. R & R SIDE PANEL.

Part: SUPPORT — CORRODED (CARGO BAY) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, AFT CARGO FLOOR TO SIDEWALL SUPPORT UPPER SURFACE IS CORRODED AT END AND AROUND TIE DOWN STANCHIONS, CORROSION REMOVAL BEYOND LIMITS. R & R PANEL.

Part: FLOORBEAM — CORRODED (BS 1360) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, CORROSION ON BS 1360 FLOORBEAM LOWER FLANGE, RBL 26.5 TO 34, WL 201. REPAIRED IAW ER NR 10-2331 IPXA EO NR: B757-5310-37537-A.

Part: FLOOR PANEL — PUNCTURED (BS 504) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FLOOR PANEL HAS PUNCTURE IN UPPER SURFACE AT BS 504 LBL 9. FABRICATED REPLACEMENT FLOOR PANEL IAW EO B757-5320-9692-G.

Part: SEAT TRACK — CORRODED (BS 1083) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FOUND CORROSION ON SEAT TRACK AT STA 1083, LBL 60. REMOVED CORROSION ON SEAT TRACK FOUND TO BE OUT OF LIMITS RECEIVED NEW SEAT TRACK PN 348451 DRILLED, DEBURRED INSTALLED IAW SRM 53-40-52-0I, SRM SRM 51-40-03 IAW SRM 51-10-02-0G STEP 14A. (5)(A)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 CORROSION ON SEAT TRACK O/B FLANGE, BS 592, LBL 25. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIR IAW SRM 53-30-52-01 1, SRM 53-00-52-2R, SRM 51-10-02, SRM 53-00-52-2R5, EO NO. B757-5340-20264-B.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, AFT CARGO BAY: FWD BULKHEAD TO FLOOR SUPPORT HAS SEVERAL AREAS OF CORROSION. CORROSION REMOVAL BEYOND ALLOWABLE LIMITS. REMOVED AND REPLACED STRINGER.

Part: FLOORBEAM — CORRODED (BS 1052) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 MAIN CARGO FLOOR AT STA 1052 RBL 9-RBL 21 WL 208 CORROSION AROUND NUT PLATES. R & R SUPPORT IAW SRM 51-40-02.

Part: SUPPORT — CORRODED (BS 1440-1530) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FLOOR TO SIDEWALL SUPPORT CORRODED, BS 1440 TO 1530, RBL 19-26. R & R IAW SRM 51-40-02-0G.

Part: FITTING — CORRODED (CARGO BAY) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 AFT CARGO BAY TIE DOWN BS 1372 LBL 22 HAS CORROSION. REPLACED PER SRM 53-60-53-1, 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (BS 1446-1500) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 AFT CARGO BAY FLOOR SUPPORT HAS SEVERAL AREAS OF CORROSION AT BS 1446-1500 RBL 11. R & R SUPPORT IAW SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (BS 1445-1500) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 AFT CARGO BAY FLOOR SUPPORT AT BS 1445-1500 LBL 8 HAS SEVERAL AREAS OF CORROSION. R & R SUPPORT IAW SRM 51-40-02.

Part: PANEL — CORRODED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 FLOOR TO SIDEWALL PANEL CORRODED AT BS 1200-1310, RBL 19-26. REMOVED AND REPLACED PER SRM 51-40-02-0G.

Part: CARGO TRACK — CORRODED (BS 1500) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, AFT CARGO BAY: CARGO TIE DOWN AT BS 1500, RBL 22 HAS CORROSION. REPLACED IAW SRM 53-60-53-1, SRM 51-40-05, SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 AFT CARGO BAY FLOOR SUPPORT HAS SEVERAL AREAS OF CORROSION BS 1446 - 1500 RBL 16. REPLACED PER SRM 51-40-02, 53-00-53-1A, 53-60-53-01A.

Part: FRAME — DENTED (BS 1360 S26R) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, BS 1360 FRAME IS DENTED AT STR 26 RT. REPAIRED IAW SRM 53-00-07-2R 5, FIG 201 AND SRM 53-60-07-0I 1, FIG. 1.

Part: FLOOR SUPPORT — CORRODED (BS 1446-1500) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, AFT CARGO BAY: FLOOR SUPPORT HAS SEVERAL AREAS OF CORROSION AT BS 1446 -1500, RBL 2. R & R SUPPORT IAW SRM 51-40-02.

Part: CARGO TRACK — CORRODED (BS 1280) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, AFT CARGO BAY: CARGO TIE DOWN BS 1280, RBL 22 HAS CORROSION. R & R FITTING IAW SRM 51-40-02.

Part: INTERCOSTAL — GOUGED (BS 1360-1380) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, AFT CARGO BAY INTERCOSTAL BETWEEN STR 25-26R 1360-1380 IS GOUGED 3" FROM FWD EDGE. REPLACED IAW SRM 53-00-04-1A, 51-40-02-0G, DWG 146N8536.

Part: ANGLE — CRACKED (BS 480-500) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, BS 480-500 RBL 10-RBL 10 WL 208-WL 208 L-ANGLE OF FLOOR WEB IS CRACKED. R & R UPPER CHORD IAW SRM 51-40-02

Part: SUPPORT — CORRODED (BS 1310-1380) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, AFT CARGO BAY: FLOOR TO SIDEWALL SUPPORT HAS SEVERAL AREAS OF CORROSION AT BS 1310-1380, RBL 19-26. CORRODED AREAS FOUND TO BE OUT OF LIMITS, REPLACED FLOOR TO SIDEWALL SUPPORT IAW SRM 53-60-53-0I FIG 1, SRM 53-00-53-1A FIG 101 DETAIL V, SRM 51-30-01-0G FIG 7, SRM 51-40-02-0G.

Part: CARGO TRACK — CORRODED (BS 1320) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, AFT CARGO BAY: CARGO TIE DOWN AT BS 1320, RBL 22 HAS CORROSION. REPLACED IAW SRM 53-60-53-1, SRM 51-40-05, SRM 51-40-02.

Part: PANEL — CORRODED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 FLOOR TO SIDEWALL SUPPORT CORRODED, BS 1440 TO 1530, RBL 19-26. REMOVED AND REPLACED PER SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (BS 1470) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, AFT CARGO BAY FLOOR SUPPORT LBL 2 HAS CORROSION AT BS 1470. R & R SUPPORT IAW SRM 51-40-02

Part: CARGO TRACK — CORRODED (BS 1300) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, AFT CARGO BAY: CARGO TIE DOWN AT BS 1300 RBL22 HAS CORROSION. R & R FITTING IAW SRM 51-40-02.

Part: CARGO TRACK — CORRODED (BS 1440) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, AFT CARGO BAY CARGO TIE DOWN BS 1440 RBL 22 HAS CORROSION. R & R FITTING IAW SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 AFT CARGO BAY: FLOOR TO SIDEWALL SUPPORT HAS SEVERAL AREAS OF CORROSION AT BS 1455-1520 LBL 16-26. REPLACED PER SRM 51-40-02, 53-60-53-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 AFT CARGO BAY FLOOR SUPPORT AT LBL 16 HAS CORROSION AT BS 1470. REPLACED PER SRM 53-00-53-1A-1, 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1446-1500) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, AFT CARGO BAY: FLOOR SUPPORT HAS SEVERAL AREAS OF CORROSION AT BS 1446 -1500, RBL 7. R & R SUPPORT IAW SRM 51-40-02.

Part: FRAME — DENTED (BS 1360 S26R) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, BS 1360 FRAME IS DENTED AT STR 26 RT. REPAIRED IAW SRM 53-00-07-2R 5, FIG. 201 AND SRM 53-60-07-0I 1, FIG. 1.

Part: FRAME — GOUGED (BS 700) · airframe 25,189 hrs · 14,052 cycles

INSP TYPE:C4, FRAME GOUGED, BS 700, LBL 67, WL222. REPAIRED IAW EO B757-5310-19952.

Part: FRAME — GOUGED (BS 1280) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FRAME GOUGED AT BS 1280, STR15L. REPAIRED IAW ATS ER 10-2370.

Part: FRAME — GOUGED (BS 1200 S15L) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FRAME GOUGED, BS 1200, STR 15L, REPAIRED IAW EO B757-5310-19952.

Part: FRAME — GOUGED (BS 1500 S15R) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, INBD SURFACE OF FRAME GOUGED BS 1500, STR 15 RT REPAIRED IAW ER NR 10-2376.

Part: FRAME — GOUGED (BS 860) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FRAME GOUGED, BS 860, LBL 67, WL 122. REPAIRED IAW EO B757-5310-19952.

Part: FRAME — GOUGED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 INBOARD SURFACE OF FRAME GOUGED AT BS 1260, STR 15 RT. REPAIRED PER ER 10-2369.

Part: SUPPORT CHANNEL — CRACKED (BS 1065) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, RT WHEEL WELL, SUPPORT IS CRACKED BS 1065, RBL 60. R & R SUPPORT CHANNEL IAW SRM 51-40-02.

Part: FRAME — GOUGED (BS 660) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FRAME GOUGED, BS 660, RBL67, WL 122. REPAIRED IAW EO B757-5310-19952.

Part: SHOCK MOUNT — CRACKED (CARGO DOOR) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, MAIN CARGO DOOR ISOLATOR/RECEPTACLE FOR DOOR LINER IS CRACKED LOCATED 40" FROM FWD EDGE AND 7" FROM BOTTOM EDGE. REPLACED IAW SRM 51-40-02.

Part: FRAME — GOUGED (BS 1340 S15R) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FRAME GOUGED, BS 1340, STR 15R. REPAIRED IAW EO B757-5310-19952.

Part: FRAME — GOUGED (BS 620) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FRAME GOUGED, BS 620, RBL 67, WL 222. REPAIRED IAW EO B757-5310-19952.

Part: FRAME — GOUGED (BS 740) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FRAME GOUGED, BS 740, RBL 67, WL 222. REPAIRED IAW EO B757-5310-19952.

Part: FRAME — GOUGED (BS 1500 S15L) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FRAME GOUGED, BS 1500, STRINGER 15L INBD FACE. REPAIRED IAW EO B757-5310-19952.

Part: FRAME — GOUGED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 INBOARD FACE OF FRAME GOUGED BS 1300 APPROXIMATELY STR 15 LT. REPAIR PER ER 10-2374.

Part: FRAME — GOUGED (BS 1380 S15L) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FRAME GOUGED, BS 1380, STR 15L. REPAIRED IAW EO B757-5310-19952.

Part: FRAME — GOUGED (BS 1380 S15R) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, INBD SURFACE OF FRAME GOUGED BS 1380, STR 15 RT. REPAIRED IAW ER NR 10-2371.

Part: FRAME — GOUGED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 INBOARD FACE OF FRAME GOUGED BS 1340, STR 15 LT. REPAIRED PER ER 10-2375.

Part: FRAME — GOUGED (BS 1280 S15R) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, FRAME GOUGED BS 1280, STR 15R. REPAIRED IAW ATS ER 10-2373.

Part: FRAME — GOUGED (BS 720) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4 FRAME GOUGED, BS 720, LBL67, WL222. REPAIRED IAW EO B757-5310-19952.

Part: WEDGE — CHAFED (NR 4 SLAT) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, NR 4 SLAT UPPER T/E LOWER SURFACE IS CHAFED AT INBD MAIN TRACK. REPAIR IAW SRM 51-70-10-2R REPAIR GENERAL AND SRM 51-70-10-2R-4 REPAIR 4.

Part: FRAME — CHAFED (FUSELAGE) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, APU COMPARTMENT ACCESS PANEL NR 316AD FWD OTBD CORNER FRAME IS CHAFED ON INNER SURFACE. (MARKED) REPAIRED CHAFED FRAME IAW ER NR 10-2353.

Part: FRAME — CHAFED (ACCESS PANEL) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, APU COMPARTMENT ACCESS PANEL NR 315AL FWD OTBD CORNER FRAME IS CHAFED ON INNER SURFACE. REPAIRED CHAFED FRAME IAW ER NR 10-2353.

Part: SKIN — CORRODED (BS 1790-1820) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, APU INLET TO FUSELAGE SKIN CONTACT AREA IS CORRODED AT NUTPLATES BS 1790 TO 1820. FOUND AREAS TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-07-1A, SRM 53-00-03-1A, SRM 51-40-02, SRM 51-40-05.

Part: ATTACH BRACKET — CRACKED (FUEL MANIFOLD) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, NR 1 ENGINE FUEL MANIFOLD ATTACH BRACKET CRACKED AT 7:00 POSITION. R & R BRACKET IAW M/M 70-51-00-2.

Part: SKIN — WRONG PART (A 250 Z 200) · airframe 25,189 hrs · 14,052 cycles

INSPECTION TYPE:C4, BLIND RIVET REPAIR ON FUSELAGE SKIN AT BS 1680, ABOVE STR 17 LT. REPAIRED IAW ER NR 10-2414.

Part: TRANSMITTER — LEAKING (LT ENGINE EPR)

LT ENGINE ROLLED BACK, CREW COULD NOT MAINTAIN ALTITUDE. DECLARED EMERGENCY. DIVERTED TO BIL. PERFORMED EPR INDICATING SYSTEM AIR INSPECTION AND FOUND LEAK AT ZONE 1 OF MM 77-11-00-5 AND MM 77-11-04-6. REPLACED EPR TRANSMITTER PER MM 71-11-01-4 AND ENG POWER RUN TEST NR 5.

Part: FLOORBOARD — DAMAGED (CABIN)

INSPECTION TYPE:N/A DAMAGED FLOORBOARD POS 15R CNT. MFG FLOORBOARD USING OLD BOARD AS TEMPLATE PER B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CABIN)

INSPECTION TYPE:N/A FLOOR PANEL 15L CENTER DAMAGED. REPAIRED PER EO B757-5320-9692-G.

Part: FLOOR PANEL — CONTAMINATED (CARGO BAY)

INSPECTION TYPE:N/A MCD FLOOR PANEL 16R IS URINE SOAKED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CABIN)

INSPECTION TYPE:N/A FLOOR PANEL POS 15L CENTER DAMAGED. REPAIRED PER EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A MCD FLOOR PANEL POS 16L DAMAGED. REPAIRED PER EO B757-5320-9692-G, B757-5320-35318-A.

Part: SEAT TRACK — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A SEAT TRACK DAMAGED STA 1661 RBL 24.75. REPAIRED SEAT TRACK PER EO B757-5310-35370-A.

Part: FLOOR PANEL — DAMAGED (CABIN)

INSPECTION TYPE:N/A DAMAGE AND CORROSION FOUND ON FLOOR PANEL BD 15L OUTBOARD AND NOTED IN IP IPS AS "S". FABRICATED NEW FLOORBOARD USING OLD AS TEMPLATE PER EO B757-5320-9692 -G.

Part: SEAT TRACK — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A SEAT TRACK DAMAGE AT STA 1585 RBL 45.5. REPAIRED PER SRM 51-40-02 DWG 146N5220 AND 146N5217.

Part: PLATE — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A MAIN DECK PLATE CORROSION STA 1681. REPAIRED PER EO B757-5310-35303-A.

Part: SEAT TRACK — CORRODED (BS 1661-1681)

M/D SEAT TRACK AT LBL 45.5 BETWEEN STA 1681.5 AND 1661 HAS CORROSION. REPAIR IAW 757 SRM 53-0052-2R.

Part: SEAT TRACK — DAMAGED (BS 1495.5 RBL 45)

MCD SEAT TRACK DAMAGED AT STA 1585 RBL 45.5. REMOVED AND REPLACED SEAT TRACK PER EO B757-5310-34863-B.

Part: FLOORBOARD — DAMAGED (MAIN DECK)

FLOORBOARD DAMAGED. FABRICATED FLOOR IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO DECK)

MCD FLOOR PANEL DAMAGED. REPAIRED PER EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO DECK)

MCD POS NR 15 RT INBD FLOOR PANEL DAMAGED, C/W EO B757-5320-9692-G AND EO B757-5100-33281-A, MANUFACTURED NEW FLOOR BD AND INSTALLED SAFETY WALK (NON SKID FINISH).

Part: FLOORBOARD — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A FLOORBOARD HAS DAMAGE. REPAIRED FLOORBOARD IAW EO B757-5320-34922-A.

Part: SEAL — LEAKING (COCKPIT WINDOW)

INSPECTION TYPE:N/A DIVERSION - L2 WINDOW AIR LEAK IN FLIGHT. T/S PER FIM 56-11-53-4 TO L2 WINDOW. R&R L2 WINDOW SEAL PER MM 56-11-53-4 UP TO AND INCLUDING STEP 4(J) PAGE 2 NEEDS STEPS 4K THROUGH M. COMPLETED INSTALLATION PER MM 56-11-53-4.

Part: PUMP — FAILED (LT ENGINE)

INSPECTION TYPE:N/A LEFT EDP HYD LOW PRESS LIGHT ILLUM. EICAS MSG DISPLAYED L HYD ENG PUMP. EICAS MSG L HYD SYS MAINT WAS NOT DISPLAYED. HYD QTY NORMAL. POWER XFER UNIT STATUS MSG DISPLAYED. REPLACED LT HYD EDP, CASE DRAIN FILTER, AND PRESSURE FILTER. ACCOMPLISHED OPS CHECK GOOD.

Part: BRACE — CRACKED (RT PYLON) · airframe 23,308 hrs · 12,916 cycles

INSPECTION TYPE:MOD RT UNDERWING FAIRING STRUCTURE, RT FWD SIDE SUPPORT BRACE IS CRACKED AT PPS 185.0. REMOVED AND REPLACED FWD SIDE SUPPORT BRACE IAW SRM 51-40-02-0G.

Part: SUPPORT CHANNEL — CHAFED (NR 2 PYLON) · airframe 23,308 hrs · 12,916 cycles

INSPECTION TYPE:MOD NR 2 PYLON UPPER UNDERWING FAIRING, FWD SUPPORT CHANNEL ASSY IS WORN AND CHAFED. REPLACED FWD SUPPORT CHANNEL IAW SRM 51-40-02-0G.

Part: CHANNEL — CHAFED (PYLON) · airframe 23,308 hrs · 12,916 cycles

INSPECTION TYPE:MOD CHANNEL CHAFED. REMOVED AND REPLACED CHANNEL IAW 51-40-02-0G.

Part: OVERHEAT LOOP — MALFUNCTIONED (RT ENGINE)

INSPECTION TYPE:N/A RT ENGINE OVHT LOOP 2 CAME ON FOR SEVERAL SECONDS IN FLIGHT THEN DISAPPEARED. STATUS MESSAGE NEVER RETURNED. PLACED ON DMI LIST MEL REF 26-11-2-1. PERFORMED TEST OF FIRE DET SYSTEM. OPS NORMAL PER MM 26-11-00-5.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHT ASSY HAS SIX LAMPS INOP. RELAMPED THE SIX LAMPS IN THE EMERGENCY LIGHT ASSY PER MM 33-51-01-2, OPS CHECKS GOOD.

Part: RADOME — FAILED (FUSELAGE)

PILOT REPORT - DURING CLIMB HEARD SINGLE THUMP ON LOWER RIGHT SIDE OF NOSE OF A/C. RADOME SUSTAINED STRUCTURAL FAILURE. [SUP 05-18-07] R & R NOSE RADOME IAW AMM 53-12-01-4 AND PERFORMED WEATHER RADAR TEST. ALL CHECKS NORMAL.

Part: SMOKE GOGGLES — CRACKED (COCKPIT)

OBSERVERS SMOKE GOGGLES CRACKED. REPLACED OBSERVERS SMOKE GOGGLES.

Part: SMOKE GOGGLES — INOPERATIVE (CABIN)

SMOKE GOGGLES MISSING UNDER JUMPSEAT. INSTALLED SERV SMOKE GOGGLES.

Part: SMOKE DETECTOR — INOPERATIVE (MAIN DECK 2B)

INSPECTION TYPE:N/A SMOKE DETECTOR 2B IS FAILING TEST IN MAIN CARGO AREA. REMOVED AND INSTALLED SMOKE DETECTOR. MM REF 26-16-01 OPS/CK GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,730 hrs · 6,378 cycles

INSPECTION TYPE:MOD FLOORBEAM CORRODED STA 1200 TOP SURFACE LBL 25 - 45.

Part: BVCU — FAILED (RT ENGINE)

INSPECTION TYPE-N/A, RT ENG FLAMEOUT, RESTART NOT ATTEMPTED FOLLWING NORMAL APPROACH AND LANDING AFTER THRUST REVERSER STOW. PERFORMED BITE TEST PROCEDURE PER MM 75-32-OOP201, FOUND RT ENG BVCU FAULTS. REPLACED BVCU FLT CREW RAN ENG GROUND IDLE. CHECK PERFORMED BVCU BITE TEST AFTER RUN, NO FAULTS NOTED, FOUND SATISFACTORY. (P/N C8E38-12) (S/N 3005) ON, (S/N 3069).