N403UP

Part: STRINGER — CORRODED (ZONE 100) · airframe 38,862 hrs · 26,844 cycles

AFT CARGO BILGE AREA AT STRG 28L HAS CORROSION AT STA 1466. FOUND DURING DVI ATA 53-05 ACCOMPLISHED REPAIR PER EO-94038-REQ1 AND VT-SAA EA 757-5360-01-B0497, REV I/R

Part: STRINGER — CORRODED (ZONE 100) · airframe 38,850 hrs · 26,837 cycles

AFT CARGO BILGE AREA AT STRG 28L HAS CORROSION AT STA 1466. FOUND DURING DVI.

Part: ESCAPE REEL — DAMAGED (ZONE 200) · airframe 38,850 hrs · 26,837 cycles

FLIGHT DECK CEILING RUBBER CABLE RETAINER FOR DESCENT DEVICE IS DIS-BONDED.

Part: RETAINER — INOPERATIVE (ZONE 200) · airframe 38,850 hrs · 26,837 cycles

FLIGHT DECK CEILING RUBBER CABLE RETAINER FOR DESCENT DEVICE IS DIS-BONDED ATA 25-61 MARKED 84-40. RE BONDED FLIGHT DECK CEILING RUBBER CABLE RETAINER IAW DWG NO. 232N1642.

Part: STRINGER — CORRODED (ZONE 100) · airframe 38,862 hrs · 26,844 cycles

FUSELAGE STA 1473 SUSPECTED CORROSION ON SKIN REPAIRED AT CTR VHF ANTENNA AREA TRIPLER METAL PLATE HAS BULGING AND 01EA FASTENER HEAD IS OUT ON METAL PLATE HOLE AS MARKED. 74-002 ATA CODE 53 ACCOMPLISH REPAIR PER EO-94040-REQ1 AND VT-SAA EA 757-5360-01-B0499, REV I/R, PRIOR TO FURTHER FLIGHT. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFF WHICH MUST BE PERFORMED BY A PROPERLY TRAINED AND CURRENTLY AUTHORIZED INDIVIDUAL. TO DETERMINE RII AUTHORIZATION, REFER TO THE CURRENT RII AUTHORIZATION LIST, SEE CHAPTER 04 OF THE GMM.

Part: SKIN — CORRODED (ZONE 100) · airframe 38,854 hrs · 26,839 cycles

MAJOR REPAIR, BOTTOM FUSELAGE STA 1600-1620 SUSPECTED CORROSION ON EXTERNAL SURFACE SKIN HAS BULGING AND FASTENER HEADS FULL THROUGH.

Part: SKIN — CORRODED (ZONE 100) · airframe 38,850 hrs · 26,837 cycles

SUSPECTED CORROSION ON SKIN REPAIRED AT CTR VHF ANTENNA AREA TRIPLER METAL PLATE HAS BULGING AND 01EA FASTENER HEAD IS OUT ON METAL PLATE HOLE AS MARKED. 74-002 ATA CODE 53 AUDIT C/W GMM RII 04-02

Part: SHEAR TIE — DENTED (FR STA 1240STR26) · airframe 37,412 hrs · 25,933 cycles

INSPECTION TYPE:CK21*MAJOR REPAIR* FRAME STA 1240 RH SIDE AT STR26R HAS A DENTFRAME WAS REPAIRED IAW 757-200PF SRM REV 116.0 CHAPTER 53-00-07-2R DETAIL V PER SRM 53-60-07-2R (RCD 288515)

Part: NONE — INOPERATIVE (POWERPLANT) · airframe 37,266 hrs · 25,833 cycles

INSPECTION TYPE:NA*DIVERSION* APPROX 1 HR INTO THE FLT AT FL400, ENG FLUCTUATIONS WERE OBSRVD ON BTH ENG. LFT 1ST, THN RT, FLLWED BY RT AGAIN APPROX 30 MINS LTER. EPR VARIED APPROX. 0.10, N1 VARIED APPROX 5%. EACH INSTNCE LESS THAN 1 MIN.PER TCH RECOM, R&R TAT PROBE AMM 34-12-02. ALL CHK GD. PERF ENG RN W/ ENG RN QUAL. MECH. & NTED NO FLUCTUATIONS IN N1 OR EPR DRING 10 MIN. ENG RN W/ BOTH ENG. ENG RUN PERF IN REF. TO AMM 71-00-00-862 AND FORM #32-13-001A. A/C OK FOR SERVICE. SEE LP 270231-3 FOR DEFFERAL OF TAT SEALANT APPLICATION.

Part: WARNING MESSAGE — FALSE ACTIVATION (SLAT SYSTEM) · airframe 35,629 hrs · 24,825 cycles

ATB - VNAV AND AUTOPILOT RETURNED AT 6000FT, BUT NOTICED LE SLAT DISGREE ON EICAS. WENT THROUGH CHECKLIST AND GOT 20 DEGREES AND LANDED. AUTOPILOT WAS NORMALREF; LE SLAT DISAGREE MSG, ACCOMPLISHED FIM 24-81-00-815-803, FIG 104 BLOCKS 1,1A,1B,1C,1D,AND 28. SYSTEM CHECKS OK.

Part: FRAME — DENTED (BS 780 S23L) · airframe 35,374 hrs · 24,649 cycles

INSPECTION TYPE:SEGTHE FRAME AT STA 780 L/H SODE STR 23 HAS A DENT ON THE UPPER SURFACE LOCATED IN THE FWD CARGO AREA NO DOTREPAIR ACCOMPLISHED PER SRM 53-00-07-2R-5 DETAIL I

Part: SKIN — DELAMINATED (FUSELAGE) · airframe 35,374 hrs · 24,649 cycles

INSPECTION TYPE:SEGDELAMINATION ON TAIL CONEREPAIRED PANEL IAW B757 SRM 51-70-10-2R-2 350 DEG F CURE PER SRM 53-80-01-2R, FIG 201

Part: SKIN — DELAMINATED (FUSELAGE) · airframe 35,374 hrs · 24,649 cycles

INSPECTION TYPE:SEGDELAMINATION ON TAIL CONEREPAIRED PANEL IAW B757 SRM 51-70-10-2R-2 350 DEG F PER SRM 53-80-01-2R, FIG 201

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 35,374 hrs · 24,649 cycles

INSPECTION TYPE:SEGMAIN CARGO COMPARTMENT FLOOR PANEL 231XTF DELAMINATEDFABBED PANEL 231 XTF FROM 5024N400001SS-G, BATCH# PER SREO B757-5320-9692-K

Part: SEAL — LEAKING (L1 DOOR) · airframe 35,115 hrs · 24,495 cycles

INSPECTION TYPE:N/ALOUD SQUEAL ENTRY DOOR OPERATING HANDLE FL360 CABIN ALTITUDE 6,000 DIFFENTIAL 8.4FOUND PRESSURE SEAL DAMAGE REPAIRED IAW MM 52-09-00 PG BLOCK 801 ALSO CLEANED AROUND SEAL OPS CK OK

Part: PANEL — CRACKED (DRY BAY) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3LH WING DRY BAY PNL 532DZ IS DAMAGED.REPAIRED PER RCD #116169.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3DURING REMOVAL OF DENT ON NR 115828 FOUND DAMAGE TO CHORD UNDERNEATH.REPAIRED PER RCD# 116143 UPS EO # B757-5310-72739-A AND VTMAE EA #757-5310-27-A2349-REV.

Part: SKIN — DENTED (BS 210-215) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3REF DI D607396 LH FUSELAGE NOSE SECTION STA 215 WK 210 SKIN GOUGE.REPAIRED PER RCD 115825 UPS EO B757-5330-72671-A & VT MAE EA 757-5310-27-A2348 REV.

Part: PANEL — DELAMINATED (LT WING DRY BAY) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:1C PANEL DELAMINATED. REPAIRED PER SRM 57-20-09-2R, 51-70-07-OG.

Part: FLOOR SKIN — DELAMINATED (FLIGHT DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3FLOOR PANEL 211X AF IS DELAMINATEDFABRICATED NEW PANEL FROM 5024N40000I55-G, BATCH#3489461 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3MCD FLOOR PANEL 232XJF IS DELAMINATEDFABRICATED FROM5024N40000ISS-G PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3MCD FLOOR PANEL 231XFF IS DELAMINATEDFABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3 MCD FLOOR PANEL 232XHF IS DELAMINATEDFABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3, MCD FLOOR PANEL 231XEF IS DELAMINATEDFABRICATED FROM 5024N40000ISSG IAW SREO B757-5320-9692-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3, MCD FLOOR PANEL 231XJF IS DELAMINATED. FABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3, MCD FLOOR PANEL 212XAF IS DELAMINATED, FABRICATED FROM 5024N4000ISS-G PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3 MCD FLOOR PANEL 232XGF IS DELAMINATEDFABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3 MCD FLOOR PANEL 232XDF IS DELAMINATEDFABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3, MCD FLOOR PANEL 231XHF IS DELAMINATED. FABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3MCD FLOOR PANEL 231XDF IS DELAMINATEDFABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG, 3MCD FLOOR PANEL 232XDF IS DELAMINATED. FABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3, ANGLE CRACKED, REMOVED AND REPLACED IAW SRM 51-40-02

Part: STRUCTURE — DELAMINATED (RUDDER TE) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3, TRAILING EDGE DELAMINATION WITH VOIDS OF SEALANT. REMOVED RIVETS ALONG TRAILING EDGE APPLIED SEALANT IN VOIDED AREA AND REINSTALLED RIVETS IAW BOEING DRAWING 173N2101, FL64

Part: SKIN — CORRODED (MAIN CARGO AREA) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3 LOWER SKIN CORRODED OUT OF MANFACTURES LIMITS LOWER SKIN REPLACED BY FABRICATING A NEW SKIN PER EO M-2550-11648-0

Part: SKIN — CORRODED (MAIN CARGO AREA) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3 LOWER SKIN CORRODED OUT OF MANUFACTURERS LIMITS. LOWER SKIN REPLACED BY FABRICATING NEW SKIN PER EO M-2550-11648-0

Part: ROLLER — BENT (MAIN CARGO) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3, LOCKS HAVE CORROSION AND BENT ROLLERS. REMOVED AND REPLACED IAW MM 25-50-79 AND IPC 25-56-00-01

Part: SKIN — CORRODED (MAIN CARGO AREA) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE: SEG3 LOWER SKIN CORRODEDD OUT OF MANUFACTURERS LIMITS. LOWER SKIN REPLACED BY FABRICATING NEW SKIN PER EO M-2550-11648-0

Part: THRESHOLD — CRACKED (MAIN CARGO) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3, THRESHOLD PLATE CRACKED IN SEVERAL PLACES WELDED AND INSPECTED PER EO B757-5320-35929-C

Part: SKIN — CORRODED (MAIN CARGO AREA) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE: SEG3 LOWER SKIN CORRODED OUT OF MANUFACTURERS LIMITS. LOWER SKIN REPLACED BY FABRICATING NEW SKIN PER EO M-2550-11648-0.

Part: SKIN — CORRODED (MAIN CARGO AREA) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3LOWER SKIN CORRODED OUT OF MANUFACTURERS LIMITS.LOWER SKIN REPLACED BY FABRICATING A NEW SKIN PER EO M-2550-11648-0

Part: SKIN — CORRODED (MAIN CARGO AREA) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE: SEG3 LOWER SKIN CORRODED OUT OF MANUFACTURERS LIMITS. LOWER SKIN REPLACED BY FABRICATING NEW SKIN PER EO M-2550-11648-0

Part: PIN — DEFORMED (MAIN CARGO AREA) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE: SEG3 PIN DAMAGED BEYOND MANUFACTURES LIMITS REPLACED WITH NEW PIN ASSY PER ANCRA MM 25-50-79

Part: SHAFT — DEFORMED (CARGO ROLLER) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3, ROLLER RAIL SHAFTS DEFORMED AND DAMAGEDREMOVED AND REPLACED IAW ANCRA MM 25-50-79

Part: HEAT SHIELD — DELAMINATED (LT MLG DOOR) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3DELAMINATION/DISBONDS ON MULTIPLE AREASREMOVED AND REPLACED

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

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

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3 MCD FLOOR PANEL 231XCF IS DELAMINATED FABRICATED NEW PANEL FROM 5024N40000ISS-G #34489461 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3 MCD FLOOR PANEL 221XBF IS DELAMINATED FABRICATED NEW PANEL FROM 5024N40000ISS-G BATCH 33489461 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3 MCD FLOOR PANEL 232XAF IS DELAMINATED FABRICATEED NEW PANEL FROM 5024N40000ISS-G BATCH #3489461 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

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

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3 MCD FLOOR PANEL 222XCF IS DELAMINATEDFABRICATED NEW PANEL FROM 5024N40000ISS-G BATCH #348461 PER SREO B757-5320-9693-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3 MCD FLOOR PANEL 222XAF IS DELAMINATED FABRICATED NEW PANEL FROM 5024N40000ISS-G PER SREO B757-5320-9693-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

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

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3 MCD FLOOR PANEL 221XCF IS DELAMINATED FABRICATED NEW PANEL FROM 5024N4000ISS-G BATCH #3489461 PER SREO B757-5320-9693-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3 MCD FLOOR PANEL 231XAF IS DELAMINATEDFABRICATED NEW FLOOR PANEL FROM 5024N40000ISS-G BATCH 33489461 PER SREO B757-5320-9693-K

Part: SKIN — DENTED (BS 239) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3 - LH FUSELAGE NOSE SECTION SKIN AT STA 239, W.L. 210 REMOVED FASTNERS COMON TO DENT, ROTO PROBED HOLES REPLACED FASTNERS, RESTORED FINISHES PER E0 B757-5330-72670-A

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3MCD FLOOR PANEL 222XBF IS DELAMINATEDFABRICATED NEW PANEL FROM 5024N40000ISS-G BATCH #3489461 PER SREO B757-5320-9693-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

INSPECTION TYPE:SEG3 MCD FLOOR PANEL 232XCF IS DELAMINATED FABRICATED NEW PANEL FROM 5024N4000ISS-G BATCH #6489461 PER SREO B757-5320-9692-K

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

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

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 33,139 hrs · 23,305 cycles

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

Part: FLOORBEAM — CORRODED (BS 1100) · airframe 25,990 hrs · 18,215 cycles

INSPECTION TYPE:SEG3, MAIN DECK FLOORBEAM AT FS 1100 RBL 18 CORRODED.REMOVED AND REPLACED THE FLOORBEAM UPPER ANGLE IAW SRM 51-40-02-0G.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 31,441 hrs · 22,194 cycles

LEFT OTBD FLOOR PANEL DAMAGED. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-50, PARA 3C.

Part: FLOOR PANEL — DELAMINATED (MCD) · airframe 31,180 hrs · 21,992 cycles

INSPECTION TYPE: SEG2, MCD FLOOR PANEL 231XJF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.

Part: FLOOR PANEL — DELAMINATED (MCD) · airframe 31,180 hrs · 21,992 cycles

INSPECTION TYPE: SEG2, MCD FLOOR PANEL 231XFF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 31,180 hrs · 21,992 cycles

INSPECTION TYPE: SEG2, MAIN DECK FLOOR PANEL 241XDF PN 144N5361 HAS EDGE DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 29,767 hrs · 20,962 cycles

INSPECTION TYPE: C, FLIGHT DECK CAPTAIN`S SEAT TRACK MOUNTING FLANGE HAS LIGHT SURFACE CORROSION. REMOVED SEAT TRACK IAW MM 25-11-01-02-198, NO ALLOWABLE DAMAGE. INSTALLED SEAT TRACK IAW MM 25-11-01-822-078.

Part: DUCT — DAMAGED (THRUST REVERSER) · airframe 29,767 hrs · 20,962 cycles

INSPECTION TYPE: C, LT ENGINE OTBD T/R INNER BARREL OUTER SURFACE AFT EDGE SKIN HAS CHIPPED AND BENT. BLENDED, DAMAGE IAW SRM 51-10-02-0G.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 28,721 hrs · 20,184 cycles

INSPECTION TYPE:S4C4, MAIN DECK FLOORBOARD 242XJF HAS EDGE DAMAGE (PANEL RACK). FABRICATED NEW FLOORBOARD IAW B757-532 0-9692-H.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 28,721 hrs · 20,184 cycles

INSPECTION TYPE:S4C4, MAIN DECK FLOORBOARD 242XBF EDGE DAMAGED. FABRICATED NEW FLOORBOARD IAW B757-532 0-9692-H.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 28,721 hrs · 20,184 cycles

INSPECTION TYPE:S4C4, MAIN DECK FLOORBOARD 242XAF HAS EDGE DAMAGE. FABRICATED NEW FLOORBOARD IAW B757-532 0-9692-H.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 28,721 hrs · 20,184 cycles

INSPECTION TYPE:S4C4, MAIN DECK FLOORBOARD 242XEF HAS EDGE DAMAGE. FABRICATED NEW FLOORBOARD IAW B757-543 20-9692-H.

Part: FRAME — DENTED (AFT CARGO) · airframe 28,721 hrs · 20,184 cycles

INSPECTION TYPE: C1S4, AFT CARGO FRAME AT BS 1580 S26L UPPER STRUCTURE DENTED. ACCOMPLISHED FRAME REPAIR IAW SRM 53-00-07, RT REPAIR 5, DETAIL I.

Part: SKIN — DENTED (BS 495)

FUSELAGE DENTED AT BS 495, LT WL 166. INSTALLED DOUBLER REPAIR IAW EO B757-5330-47087-A.

Part: SENSOR — FAULTY (RT GEAR DOOR)

DIVERSION - "GEAR DOOR" EICAS MESAGE AND "DOOR" AMBER LIGHT APPEARED AFTER GEAR RETRACTION WITH GEAR DOWN. ALL INDICATIONS NORMAL. ACCOMPLISHED FIM 32-09-03 SHEET 1, BLOCKS 1,2,3. NO PROBLEMS FOUND. ALL SENSOR RESISTANCES UNDER 15 OHMS. REF WDM 32-61-13. FOUND RIGHT GEAR DOOR SYS 2 SENSOR TO BE 9M OHMS TO GND. REPLACED S10072 IAW MM 32-61-02-2. NO OTHER FAULTS NOTED.

Part: LIGHT — DAMAGED (COCKPIT)

EMERGENCY EXIT UNARMED LIGHT FALLING OUT OF RECEPTACLE. REPLACED SWITCH LIGHT DRAWER ASSY, CHECKS GOOD REF AMM 33-16-02-2.

Part: FRAME — MISINSTALLED (BS 580 S14-15R) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FRAME AT STA 580 BETWEEN STRINGER 15R AND 14R FREE FLANGE HAS RIVETS WITH INSUFFICIENT SPACING. REPAIRED FRAME IAW EA 1107641R.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FLOOR PANEL 232XHF DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 232XHF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FLOOR PANEL 232XEF DAMAGED. FABRICATED FLOOR PANEL IAE EO B757-5320-969392-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 231XFF HAS EDGE DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL 231XFF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 242XGF HAS SEVERAL EDGE DAMAGES. FABRICATED REPLACEMENT FLOOR PANEL 242XGF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, EXTENSIVE EDGE DAMAGE TO MAIN CARGO FLOOR PANEL 231XDF. REPLACED PANEL 231XDF IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 232XHF HAS EDGE DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL 232XHF IAW B757-5320-9692-G.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FLOORBOARD NR 232XGF HAS EDGE DAMAGE. FABRICATED REPLACEMENT FLOORBOARD NR 232XGF HAS EDGE DAMAGE.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FLOOR PANEL 231XGF DAMAGED. FABRICATED FLOOR PANEL IAW EO B757-5320-96392-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 232XMF HAS EDGE DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL 232XMF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 231XLF HAS EDGE DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL 231XLF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 232XNF HAS EDGE DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL 232XNF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C=CK, MAIN CARGO FLOOR PANEL 242XCF HAS EDGE DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL 242XCF IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 251XBF HAS 2 EDGE DAMAGED. FABRICATED REPLACEMENT PANEL 251XBF IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CHECK, LT FLIGHT DECK COMPARTMENT CORROSION FOUND ON FLOOR DECK FWD, INBD CAPT SEAT TRACK. REMOVED CORROSION AND RESTORED FINISH IAW EA 110839.

Part: FLOOR SUPPORT — CORRODED (BS 1054 LBL 19) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1 MAIN CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE AT STA, 1054, LBL 19 HAS AREA OF CORROSION. FABRICATED NEW FLOOR SUPPORT STRUCTURE.

Part: FRAME — DAMAGED (BS 600 S12-13R) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FRAME 600 HAS DOUBLE DRILLED ON INNER CHORD NEAR STRINGER 12R AND 13R. FABRICATED AND INSTALLED FRAME REPAIR IAW EA110822 IR.

Part: FLOOR SUPPORT — CORRODED (BS 884 LBL 45.5) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1 MAIN CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE AT STA 1054, LBL 19 HAS AREA OF CORROSION. REPLACED SEAT TRACK ON NRC 107580

Part: FLOOR PANEL — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FLOOR 251XRF DAMAGED. FABRICATED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FRAME — DAMAGED (BS 560 S15-16R) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT RT SIDE FRAME 560 BETWEEN STRINGER 15R AND 16R HAS DOUBLE DRILLED FASTENERS THROUGH FREE FLANGE CUT OUT DAMAGE. FABRICATED AND ISNTALLED REPAIR IAW EA 110763 IR.

Part: FLOORBOARD — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FLOOR 251XQF DAMAGED. FABRICATED FLOORBOARD IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 251XNF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK MAIN CARGO COMPARTMENT FLOOR PANEL 251XMF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION, MAIN CARGO COMPARTMENT FLOOR PANEL 251XEF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 251XLF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 251XHF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 251XDF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 251XAF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 252XQF IS DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 252XQF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 241XFF HAS EDGE DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 241XFF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 251XGF IS DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 251XGF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1 MAIN CARGO COMPARTMENT FLOOR PANEL 231XJF HAS EDGE DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 231XJF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 251XCF HAS EDGE DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 251XCF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1 MAIN CARGO COMPARTMENT FLOOR PANEL 231XSF HAS SURFACE DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL 231XSF IAW B757-5320-9692-G

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 251XFF HAS EDGE DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 251XFF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FLOOR PANEL 252XUF HAS SEVERAL EDGE DAMAGES. FABRICATED REPLACEMENT FLOOR PANEL 252XUF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 241XJF HAS EDGE DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 241XJF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FLOOR PANEL 231XQF HAS CORNER DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 231XQF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 251XPF HAS EDGE DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 251XPF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FLOOR PANEL 251XJF HAS EDGE DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 251XJF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 241XKF HAS EDGE DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 241XKF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 232XUF HAS DAMAGED INSERTS. FABRICATED REPLACEMENT FLOOR PANEL 232XUF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 241XHF HAS DAMAGED INSERTS. FABRICATED REPLACEMENT FLOOR PANEL 241XHF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 231XKF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 241XLF HAS EDGE DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 241XLF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 241XAF HAS EDGE DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 241XAF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FLOOR PANEL 231XWF HAS SEVERAL DAMAGED INSERTS. FABRICATED REPLACEMENT FLOOR PANEL 231XWF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 241XBF HAS EDGE DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 241XBF IAW B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 241XGF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 231XVF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 231XUF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: STRUCTURE — CORRODED (BS 480-620) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT BALL MAT NR3 STA 480 TO 620 HAS LIGHT SURFACE CORROSION ON BOTTOM SIDE. REPLACE BALL MAT WITH SERVICEABLE UNIT PART 80545-12.

Part: STRUCTURE — CORRODED (BS 480-620) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT BALL MAT NR 1 STA 480 TO 620 HAS LIGHT SURFACE CORROSION ON BOTTOM SIDE. REPLACED BALL MAT WITH SERVICEABLE UNIT PN 80545-18.

Part: STRUCTURE — CORRODED (BS 480-620) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT BALL MAT NR 5 STA 480 TO 620 HAS LIGHT SURFACE CORROSION ON BOTTOM SIDE. REPLACED BALL MAT WITH SERVICEABLE UNIT PN 80545-11.

Part: STRUCTURE — CORRODED (BS 480-620) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT BALL MAT NR 5 STA 480 TO 620 HAS LIGHT SURFACE CORROSION ON BOTTOM SIDE. REPLACED BALL MAT WITH SERVICEABLE UNIT PN 80545-19.

Part: FRAME — DAMAGED (BS 580 S12&14R) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FRAME 580 HAS DOUBLE DRILLED ON INNER CHORD NEAR STRINGER 12R AND 14R. FABRICATED AND INSTALLED FRAME REPAIR IAW EA110906IR.

Part: UNKNOWN — DENTED (BS 1540) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1 AFT CARGO COMPARTMENT STA 1540 STR 22-23 R HAS DENT REPAIRED IAW SRM 53-00-07-2R-5 REPAIR 5 DETAIL 2 AND 53-30-07-2R

Part: STRUCTURE — CORRODED (BS 480-620) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT BALL MAT NR 2 STA 480 TO 620 HAS LIGHT SURFACE CORROSION ON BOTTOM SIDE. REPLACED BALL MAT WITH SERVICEABLE UNIT PART 80545-11.

Part: FLOOR PANEL — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FLOOR PANEL 252XEF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 241XEF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FLOOR PANEL 242XKF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1 FLOOR PANEL 232XWF DAMAGED. FABRICATED NEW FLOOR PANEL 232XWF IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, FLOOR PANEL 242XHF DAMAGED. FABRICATED NEW FLOOR PANEL 242XHF IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, FLOOR PANEL 232XFF DAMAGED. FABRICATED NEW FLOOR PANEL 232XFF IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, FLOOR PANEL 252XCF DAMAGED. FABRICATED NEW FLOOR PANEL 252XCF IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 242XDF HAS 2 DAMAGED INSERTS. FABRICATED REPLACEMENT PANEL 242XDF IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, FLOOR PANEL 242XFF DAMAGED. FABRICATE NEW FLOOR PANEL 242XFF IAW EO B757-5320-9692-G.

Part: FLOORBOARD — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO LT SIDE FWD CABIN FLOORBOARD 221XCF HAS 2 EA PULLED INSERTS IN FWD CENTER OF FLOORBOARD. FABRICATED NEW FLOOR PANEL 221XCF IAW EO B757-5320-9692-G.

Part: FRAME — DENTED (BS 460 S9R) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FRAME DENTED ON FREE FLANGE AT STA 460 AT STR 9 R. REPAIRED IAW SRM 53-00-07-2R-1, FIG 202, DETAIL 2.

Part: FLOOR PANEL — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, FLOOR PANEL 252XPF MISSING INSERT. FABRICATED NEW FLOOR PANEL 252XPF IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, FLOOR PANEL 242XLF DAMAGED. FABRICATED NEW FLOOR PANEL 242XLF IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1 FLOOR PANEL 242XMF DAMAGED. FABRICATED NEW FLOOR PANEL 242XMF IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, FLOOR PANEL 252XTF MISSING INSERT FABRICATED NEW FLOOR PANEL 252XTF IAW EO B757-5320-9692-G.

Part: SEAT TRACK — CORRODED (BS 883) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT SEAT TRACK AT STA 883, LBL 45.5 HAS CORROSION ON OTBD FLANGE AT NUT PLATE HOLE. REMOVED CORROSION, ORIGINAL THICKNESS .085, LOSS .046 WITH .046 REMAINING IS OUT OF LIMITS REPLACED SECTION OF SEAT TRACK FROM STA 879-900 IAW DWG 143N5481.

Part: FLOORBOARD — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FLOORBOARD PANEL 232XFF AT STA 480-560 RT HAS DAMAGED INSERT HOLES. FABRICATED NEW FLOOR PANEL 232XFF IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C -1 MAIN CARGO COMPARTMENT FLOOR PANEL 231XPF IS DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 251XPF IAW B757-5320-9692-G.

Part: SEAT TRACK — CORRODED (BS 1134-1178) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO STRUCTURE AT STA 1134 TO STA 1178, LBL 26 SEVERAL FASTENER HOLES HAVE CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS. R & R SEAT TRACK FROM STA 1080 TO 1180 IAW DWG 144N5002 THIS IS A MINOR REPAIR.

Part: FRAME — DAMAGED (BS 500 S5-6R) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT RT SIDE FRAME 500 HAS DOUBLE DRILLED FA FASTENER HOLES, STRINGER 5R AND 6R AND BETWEEN 6R AND 7R. REPAIRED FRAME IAW EA 110758.

Part: FRAME — DAMAGED (BS 1173 S9L) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT STA 1173, TOP FLANGE OF S-9L HAS A TOOL MARK. REPAIRED STRINGER STA 1173 S-9L IAW EA 110793.

Part: FLOOR PANEL — CORRODED (BS 584 LBL 58) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR DECK PLATE AT STA 584, LBL 58 HAS CORROSION AT NUT PLATE HOLE. REMOVED CORROSION ORIGINAL THICKNESS .063 LOSS OF .005 WITH .058 REMAINING, NO SRM LIMITS FOR THIS AREA LOSS IS WITHIN LIMIT OF EA 110788 IR/ EO B757-5310-43449-A PERFORMED REQUIRED INSPECTIONS, TREATED AND PRIMED AREA IAW EA 110788IR/ EOB757-5310-43446-A.

Part: FRAME — DAMAGED (BS 600 S14-15R) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FUSELAGE FRAME AT STA 600 RT HAS MULTIPLE DOUBLE DRILLED FASTENER HOLES ON INNER CHORD AT S-12R AND BETWEEN S-14R AN D S-15R. REPAIRED MAIN CARGO FRAME STA 600 RT BETWEEN S-12R AND S-15R IAW EA 110765.

Part: FRAME — DAMAGED (BS 560 S12R) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, MAIN CARGO COMPARTMENT FRAME 560 HAS DOUBLE DFRILLED ON INNER CHORD NEAR STRINGER 12R. FABRICATED AND INSTALLED FRAME REPAIR IAW EA 110822 IR.

Part: SKIN — DAMAGED (BS 1173 S9L) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CHECK, MAIN CARGO COMPARTMENT STA 1173 JUST ABOVE S-9L. SKIN HAS TOOL MARK. REPAIRED SKIN AT STA 1173 S-9L IAW EA 110790.

Part: FRAME — DAMAGED (BS 1500 S25L) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, LT SIDE FRAME DAMAGED AFT CARGO PIT STA 1500 BELOW S-25L. REPAIRED AFT CARGO PIT FRAME STA 1500 BELOW S-25L IAW SRM 53-00-07-2R- 5.

Part: FRAME — DAMAGED (BS 620 S11R) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FUSELAGE FRAME AT STA 620 S-11R INBD FACE OF FREE FLANGE HAS A DRILL START. REPAIRED MAIN CARGO FRAME STA 620 S-11R IAW EA 110768.

Part: FRAME — MISINSTALLED (BS 520) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FUSELAGE FRAME AT STA 520 BETWEEN S-6R AND S-7R FREE FLANGE HAS RIVETS WITH INSUFFICIENT SPACING. REPAIRED MAIN CARGO FRAME STA 520 BETWEEN S-6R AND S-7R IAW EA 110761.

Part: FRAME — MISINSTALLED (BS 540 S14-15R) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FUSELAGE FRAME STA 540 BETWEEN S-15R AND S-14R FREE FLANGE HAS RIVETS WITH INSUFFICIENT SPACING. REPAIRED MAIN CARGO FRAME STA 540 BETWEEN S-15R ANS S-14R IAW EA 1108 28.

Part: FRAME — DAMAGED (BS 1500 S24-25R) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1, RT FRAME DAMAGED, AFT CARGO PIT, STA 1500 BETWEEN STRINGER 24R AND 25R. REPAIRED IAW SRM 53-00-07-2R-5, REPAIR 5.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL HAS EDGE DAMAGE AND EDGE SEALING. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-G.

Part: SKIN — DELAMINATED (APU BAY) · airframe 27,446 hrs · 19,241 cycles

INSPECTION TYPE:C4, APU BAY INNER SKIN HAS DELAMINATED AREA APROX 5" AFT OF FRAME AT STA 1918.90 AND APROX 15" UP FROM RT APU DOOR HINGE. REPAIRED SKIN IAW EA 110406IR.

Part: FLOOR PANEL — DAMAGED · airframe 27,539 hrs · 19,319 cycles

INSPECTION TYPE:C-1 MANI CARGO COMPARTMENT FLOOR PANEL 241XMF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL IAW EO B757-5320-9692-G.

Part: SKIN — CORRODED (BS 1918-1920)

CORROSION FOUND AT APPROX STA 1918, RT SIDE ABOUT 3 IN FWD OF ELEVATOR TARGET SCALE. ADDITIONAL DAMAGE FOUND AT STA 1920 RT SIDE. INSPECTED DAMAGED AREA AND FABRICATED INTERIM DOUBLER AND FILLER IAW EO B757-530-42292-A AND SRM 51-70-18-0. INSTALLED INTERIM DOUBLER REPAIR IAW EO B757-5330-42292-A AND SRM 51-70-18-06.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHT ASSY HAS (6) LAMPS INOP. RELAMPED (6) LAMPS IN EMERGENCY LIGHT ASSY IAW AMM 33-51-01-2.

Part: SHEAR WEB — CORRODED (BS 440) · airframe 26,856 hrs · 18,810 cycles

INSPECTION TYPE:SP WHILE WORKING CUSTOMER CARD NR 893010, FOUND CORROSION AT BS 440, RBL 48, WL 208. REPAIRED IAW EO B757-5310-38276-B.

Part: WINDOW — ARCED (COCKPIT)

ATB - F/O NOTICED R FRONT WINDOW ARCING NEARING TOP OF CLIMB. CHECKED WITH FLASHLIGHT AND DISCOVERED HAIRLINE CRACK AT TOP OF WINDOW. PARTIALLY REMOVED R-1 WINDOW, THRU STEP 2D13 OF MM 56-11-01-4. SPEED TAPE APPLIED OVER FRAME TO PREVENT WATER INCURSION. COMPLETE R-1 WINDOW REMOVAL. INSTALLED NEW R-1 WINDOW IAW MM B757 56-11-01-4.

Part: FLOOR PANEL — DAMAGED (LBL 26)

FLOOR PANEL PN 141N5410-4, DAMAGED. REPAIRED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (LBL 46)

FLOOR PANEL, PN 141N5410-3, DAMAGED. REPAIRED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED

FLOOR PANEL PN 141N5410-5 DAMAGED. REPAIRED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (RBL 46)

FLOOR PANEL, PN 141N5410-8, DAMAGED. REPAIRED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO DECK)

FLOOR PANEL PN 143N5457-60, DAMAGED. REPAIRED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (RBL 26)

FLOOR PANEL PN 141N5410-4 DAMAGED. REPAIRED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO DECK)

FLOOR PANEL PN 134N5457-5, DAMAGED. REPAIRED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (BS 336)

MCD FLOOR PANEL PN 141N5410-6 DAMAGED. REPAIRED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (RBL 26)

FLOOR PANEL PN 143N5457-3, DAMAGED. REPAIRED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (CARGO DECK)

FLOOR PANEL PN 143N5457-3 DAMAGED. REPAIRED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO DECK)

FLOOR PANEL PN 143N5457-5, DAMAGED. REPAIRED IAW EO B757-5320-9692-G.

Part: FLOOR PANEL — DAMAGED (RBL 46)

FLOOR PANEL PN 143N5457-38, DAMAGED. REPAIRED IAW EO B757-5320-9692-G.

Part: SKIN — DENTED (FUSELAGE)

INSPECTION TYPE:N/A DENT WITH OIL CANNING AT STA 470 BETWEEN STR 22 AND 23R ON FUSELAGE. REPAIRED IAW EO-B757-5330-34790-A.

Part: DOOR FRAME — DAMAGED (CARGO DOOR) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 WHILE ACCESSING FOR NRC 809265 FOUND 9 FASTENER HOLE DRILLED THROUGH THE EDGE OF THE MAIN CARGO DOOR AFT FRAME 3.4 INCHES ABOVE STR 15L I/B FLANGE. REMOVED DAMAGE (TRIM OUT), INSPECTED TRIMMED EDGE, FABRICATED 9 NEW ANGLE INSTALLED NEW ANGLE PER ATS ER NO 09-3166.

Part: SKIN — DENTED (BS 1900 S4R) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 REPAIR (OUT OF LIMITS) DENT ON FUSELAGE SKIN AT BS 1900, STR 4R. REMOVED DAMAGE, POTTED CORE CELLS, INSTALLED AND BONDED TWO REPAIR DOUBLERS PER SRM 51-70-10-2R2.

Part: ANGLE — DAMAGED (BS 487) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DOOR BS 487 FRAME CAP L-ANGLE INNER FLANGE HAS TOOLING DAMAGE 8.3 INCHES BELOW STR 15L ON THE AFT EDGE. REPLACED PER SRM 51-40-02.

Part: FRAME — GOUGED (CARGO DOOR) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DOOR BS 540 FRAME HAS A SCREW GOUGE 5.4 INCHES BELOW STR 15L FLANGE FWD RADIUS. REMOVED DAMAGE & REPAIRED IAW ER 09-3163 DATED 29JUNE09.

Part: FRAME — DAMAGED (CARGO DOOR) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DOOR BS 530 STUB FRAME HAS TOOLING DAMAGE 5-7.8 INCHES BELOW STR 15 INBOARD FLANGE AFT RADIUS. REMOVED DAMAGE & INSTALLED REPAIR ANGLE IAW ER 09-3149 DATED 29JUNE09.

Part: FRAME — DAMAGED (CARGO DOOR) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DOOR BS 570 STUB FRAME HAS TOOLING DAMAGE 2.6 - 8.3 INCHES BELOW STR 15L I/B FLANGE AND FWD RADIUS. REMOVED DAMAGE, FABRICATED REPAIR ANGLE, STRUCTURAL FILLER, INSTALLED REPAIR ANGLE REPAIR STRUCTURAL FILLER AND REPAIR CLIP IAW ATS ER NO 09-3154 DATED 26JUNE09.

Part: DOOR FRAME — DAMAGED (BS 606) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DOOR BS 606 STUB FRAME HAS TOOLING DAMAGE 2.6 - 8.2 INCHES BELOW STR 15L I/B FLANGES. REMOVED DAMAGE & REPAIRED PER 09-3152 DATED 19JUNE09.

Part: ANGLE — GOUGED (CARGO DOOR FRAME) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DOOR BS 613 FRAME CAP L-ANGLE INNER FLANGE HAS SCREW GOUGES 2.3 AND 6.8 INCHES BELOW STR 15L. ANGLE WAS REPLACED PER SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1180-1200) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 SEAT TRACK CORRODED BS 1180-1200 RBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK PER SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1180-1200) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DECK BS 1180-1200 LBL 25 SEAT TRACK HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED BS 1180-1200 LBL 25 PER SRM 51-40-02-06.

Part: SEAT TRACK — CORRODED (BS 1180-1200) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DECK BS 1180-1200 LBL 45 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-2.

Part: STOP FITTING — GOUGED (CARGO DOOR) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DOOR UPPER FWD STOP PIN FITTING IS GOUGED. BLENDED PER SRM ADDENDUM B757-5310-15194-C.

Part: STOP FITTING — GOUGED (CARGO DOOR) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DOOR UPPER AFT STOP PIN FITTING IS GOUGED. BLENDED PER SRM ADDENDUM B757-5310-15194-C.

Part: FLOORBEAM — CORRODED (BS 1200) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DECK BS 1200, LBL 60-RBL 60 FLOORBEAM HAS CORROSION AT SEVERAL PLACES ON UPPER SURFACE. REMOVED CORROSION FROM NUT PLATE HOLES ON FLOORBEAM MEASURED ALL BLENDED AREAS SUBMITTED AND RECEIVED ENGINEERING, FABRICATED CLIPS, STIFFENERS AND TAPER FILLERS, INSTALLED ALL REPAIR PARTS PER ATS ER NO. 09-315 9.

Part: SKIN — GOUGED (BS 479 S14L) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2, 1 INCH GOUGE IN FUSELAGE SKIN BS 479 STR 14L. BLENDED, HFED REPAIRED IAW ATS ER 09-3155.

Part: FLOORBEAM — CORRODED (BS 1100) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DECK BS 1100 RBL 5, FLOORBEAM IS CORRODED. REMOVED CORROSION, BLENDED TO A RATIO OF 10 TO 1. FLAP PEENED BLENDED AREA. FABRICATED REPAIR ANGLE. ALODINED AND PRIMED REPAIR AREA AND REPAIR ANGLE. INSTALLED REPAIR ANGLE.

Part: SEAT TRACK — CORRODED (BS 1075-1100) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DECK BS 1075-1100, LBL 45 SEAT TRACK HAS CORROSION ON UPPER SURFACE. SEAT TRACK REPLACED PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1040-1075) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 FLOOR SUPPORT CORRODED BS 1040-1075 LBL 45, WL 208. REMOVED, FABRICATED AND INSTALLED PER SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (BS 1013-1040) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DECK BS 1013-1040 LBL 45 LONGITUDINAL FLOOR SUPPORT HAS CORROSION ON UPPER SURFACE. REPAIRED PER ATS ENGINEERING 09-3129 DATED 25JUNE09.

Part: SEAT TRACK — CORRODED (BS 1198) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DECK BS 1198 RBL 25 SEAT TRACK HAS CORROSION ON UPPER SURFACE. SEAT TRACK WAS REPLACED PER SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1180-1200) · airframe 26,019 hrs · 18,239 cycles

INSPECTION TYPE:C2 MAIN CARGO DECK BS 1180-1200, LBL 25 SEAT TRACK HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED SEAT TRACK BS 1180-1200, LBL 25 PER SRM 51-40-02-06.

Part: SKIN — DENTED (TE FLAP)

DENT IN LOWER SURFACE PANEL NR113N2402. DENT MEASURES 1.250 INCHES IN DIA. X .060 INCH DEEP WITH .250 INCH HOLE AT CENTER OF DENT. AFTER CUTOUT OF DAMAGE RESULTS IN 1.5 INCHES DIA. CORE CUTOUT OF 1.5 DIA INCHES. REPAIRED IAW EO B757-5750-31769-B AND SRM 57-53-01-2R REPAIR 1 AND REPAIR 2.

Part: DOOR — INOPERATIVE (NLG)

INSPECTION TYPE:N/A ATB - AFTER TAKEOFF CREW REPORTED GEAR WOULD NOT RETRACT. GEAR DISAGREE & GEAR DOOR LIGHT ILLUMINATED (AIRFRAME VIBRATION) LEVEL OFF AT 5000. GEAR RETRACTS AT 5000 WITH LIGHTS EXTINGUISHED. GEAR DEPLOYED NORMALLY UPON LANDING. REPLACED NOSE GEAR DOOR.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 24,500 hrs · 17,143 cycles

INSPECTION TYPE:C FWD SPAR WEB I/B OF RIB 9 FS STA 208 CRACKED. REPAIRED PER UPS EO 757-55-20032 AND GOODRICH EA 07-3396.

Part: DUCT — CRACKED (LT WING)

LEFT BLEED DUCT LEAK EICAS MESSAGE QRH PROCEDURE ACCOMPLISHED. AIR TURNBACK DUE TO INABILITY TO REMAIN OUT OF ICING CONDITIONS EN ROUTE TO DSM. REMOVED AND REPLACED CRACKED DUCT AT LT WING LEADING EACU CHECKS NORMAL. ACCOMPL. LEAK DETECTION BITE PROCEDURE AND MEMORY ERASE PROCEDURES SYSTEM TEST NORMAL OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (STA 320) · airframe 22,393 hrs · 15,685 cycles

INSPECTION TYPE:C BS 320 FIVE INCHES I/B OF CREW ENTRY DOOR FRAME CORROSION ON LWR SIDE OF FLOOR SUPPORT STRUCTURE AROUND NUT PLATES. REPLACED THE PART IAW SRM 51-40-05.

Part: FLOORBEAM — CORRODED (BS 620) · airframe 22,393 hrs · 15,685 cycles

INSPECTION TYPE:C MAIN CARGO BAY FLOORBEAM CORRODED BS 620 LBL 4-10. REPAIR PER SRM 51-20-06 AND ER 05-3962.

Part: ELBOW — LEAKING (COCKPIT OXYGEN)

INSPECTION TYPE:N/A PER TECH ALERT H29535 FOUND CAPT'S SUPPLY HOSE ELBOW FITTING SLOW LEAK (ELBOW FITTING ATTACHED TO STOWAGE BOX) LIMNE CAPPED. REPLACED CAPT'S AND F/O`S ELBOW FITTING AND AS A PRECAUTION, R2 CAPTS AND F/O`S MASK AND MASK STOWAGE BOXES PER MM 35-11-51-4, LEAKS NOTED.

Part: SKIN — DENTED (FUSELAGE)

DENT STA 450 JUST ABOVE STR 19L. REPAIR DOUBLER INSTALLED PER EO B757-5330-19636-C.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:PFLT LEFT ENGINE FIRE HANDLE LIGHTS INOP. RELAMPED HANDLE, OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,230 hrs · 12,676 cycles

INSPECTION TYPE:C CORROSION ON SEAT TRACK FLANGES STA-1080-1180. RBL 45, WL 208. REMOVED CORROSION FROM SEAT TRACK FLANGES, FROM BS-1080 TO 1180 RBL 45 WL 208, WITH MATERIAL LOSS OUT OF LIMITS IAW UPS SRM 53-00-52. REMOVED SEAT TRACK FROM BS 1080-1180 RBL 45 WL 208 AND INSTALLED NEW FABRICATED TRACK PER SRM 51-40-08 AND SRM 51-40-02.

Part: CONTROLLER — DAMAGED (NR 6 SPOILER)

INSPECTION TYPE:N/A, LEFT WING SPOILERS FLOAT. HAPPENS WHEN FLAPS SELECTED 15. REMOVED AND REPLACED NR 6 SPOILER RVDT PER MM 27-61-02, OPS CHECKS GOOD PER MM 27-61-00 PROCEDURE 4.

Part: TRUNNION — CORRODED (LT MLG)

INSPECTION TYPE:C LT MLG FWD TRUNNION BRG BORE HAS CORROSION AT REAR SPAR. REMOVED LT FWD TRUNNION BRG SUPPORT BRACKET. REMOVED LT BEARING SUPPORT. REMOVED BEARING FROM SUPPORT CLEAN AND INSPECT SUPPORT REINSTALLED.

Part: TRUNNION — CORRODED (RT MLG)

INSPECTION TYPE:C CORROSION (C57-651-02-11) RT MLG TRUNNION BRG BORE HAS CORRODED AT REAR SPAR REMOVED AND REPLACED FWD TRUNNION BEARING MM 57-54-05 PARA 2 PG 401

Part: SUPPORT — CRACKED (BS 1240)

INSPECTION TYPE:C4 IN AFT BAY, FLOOR SUPPORT AT STA 1240, LBL 12 IS DAMAGED AND HAS SHEARED FASTENERS. REMOVED DAMAGED SECTION OF FLOOR SUPPORT AND REPLACED SECTION WITH NEW PER SRM 51-70-12, 51-20-01.

Part: STRUT — REQD SERVICE (NLG)

INSPECTION TYPE-N/A, EXCESSIVE NOSE STRUT EXTENSION NOTICED AT BLOCK OUT. NOSE WHEEL CAME OFF GRD AT APPLICATION OF BRAKES LOAD RECONFIGURED. NOSE STRUT AIR VOLUME DECREASED TO BRING STRUT WITHIN LIMITS.