N978FD

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,062 hrs · 28,070 cycles

AFT FUSELAGE POSSIBLE CORROSION AT LAP JOINT BS 1664 BTW S25R-S26R CORROSION OUT OF LIMITS AT AFT FUSELAGE LAP JOINT STA 1664 BTW STR 25R-STR26R WAS REPAIRED IAW EA F-5330-T0385225 P1.

Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,062 hrs · 28,070 cycles

AFTER REMOVAL OF EXHAUST DUCT AND CORE ON APU FOUND SEVERE CORROSIONB ON FRAME (148N1606) AT STA 1992.8 APPOX 6 INCHES AT THE 6 OCLOCK POSITION (APPROX 4-7 O CLOCK) WAS FOUND FRAME, RING AND SPLICE WITH CORROSION OUT OF LIMITS EVALUATED IAW B757 SRM 53-00-07-1A, THEY WERE FABRICATED PER BOEING DWG 148N1606 REV G AND REPLACED IAW B757 SRM 51-40-02-OG

Part: SKIN PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,062 hrs · 28,070 cycles

APU COMPARTMENT RT SIDE BS 1896.20, DOOR 316AR CUTOUT, INTERNAL SKIN, WITH CORROSION. CORROSION OUT OF LIMITS AT APU COMPT. RT SIDE B.S 1892 DOOR 316AR CUTOUT AREA ON INTERNAL SKIN WAS REPAIRED IAW SRM 53-80-01-2R AND SRM 51-70-10-2R.

Part: SHEAR PLATE — CORRODED (N/A) · corrosion level 2 · airframe 59,706 hrs · 27,262 cycles

MAIN CABIN - SHEAR PLATE AT STA 377 RBL 24 TO RBL 45 IS CORRODED ACCOMPLISHED FEDEX EA# F-5310-T0376859 FUSELAGE - MAINFRAME - MAIN CABIN SHEAR WEB, STA 377-STA 410, RBL24-RBL45, CORROSION, SPLICE REPAIR

Part: SHEAR WEB — CORRODED (N/A) · corrosion level 2 · airframe 59,706 hrs · 27,262 cycles

MAIN CABIN SHEAR PLATE UPPER SURFACE HAS CORROSION FROM APPROX STA 390-396 LBL47 ACCOMPLISHED FEDEX EA# F-5310-T0376859 FUSELAGE - MAINFRAME - MAIN CABIN SHEAR WEB, STA 377-STA 410, LBL 45-58, CORROSION, SPLICE REPAIR

Part: SHEAR WEB — CORRODED (ZONE 200) · airframe 59,706 hrs · 27,262 cycles

MAIN CABIN - SHEAR PLATE AT STA 377 LBL 24 TO 45 HAS EVIDENCE OF CORROSION ACCOMPLISHED FEDEX EA# F-5310-T0376853: FUSELAGE - MAINFRAME - MAIN CABIN SHEAR PLATE WEB, STA 377 - STA 410, LBL 24 - LBL 45, CORROSION, SPLICE REPAIR.

Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,706 hrs · 27,262 cycles

MAIN CABIN SHEAR PLATE UPPER SURFACE HAS CORROSION FROM APPROX STA 390-400, RBL 47 ACCOMPLISHED FEDEX EA# F-5310-T0376860: FUSELAGE - MAINFRAME - MAIN CABIN SHEAR WEB, STA 377 - STA 410, RBL 45 - RBL 58, CORROSION, SPLICE REPAIR

Part: ATTACH ANGLE — CRACKED (N/A) · airframe 59,706 hrs · 27,262 cycles

#2 PYLON PNEUMATIC CONTROL MODULE ATTACH ANGLE BRACKET IS CRACKED. REMOVED BRACKET, FABRICATED NEW BRACKET PER BAC DWG 312N5857 REV E, REINSTALLED NEW BRACKET PER BAC DWG 311N5040 REV D AND B757 SRM 51-40-02

Part: SHEAR WEB — CORRODED (UNKNOWN) · airframe 59,706 hrs · 27,262 cycles

MAIN CABIN FLOOR 9G SUPPORT ANGLES CORRODED AT STA 377 RBL20 TO RBL45 ACCOMPLISHED FEDEX EA# F-5310-T0376833 FUSELAGE - MAINFRAME - MAIN CABIN SHEAR WEB, STA 377-STA 440 - BL0 - RBL 24.75, CORROSION, SPLICE REPAIR

Part: SHEAR WEB — CORRODED (UNKNOWN) · airframe 59,706 hrs · 27,262 cycles

MAIN CABIN - SHEAR PLATE AT STA 377 LBL0-24 IS CORRODED ACCOMPLISHED FEDEX EA# F-5310-T0376835 FUSELAGE - MAINFRAME - MAIN CABIN SHEAR WEB, STA 377-STA 440, BL0 - LBL 24.75, CORROSION, SPLICE REPAIR

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 59,706 hrs · 27,262 cycles

MAIN CABIN - FLOOR WEB AT STA 480-500 RBL 12 IS DAMAGED REPAIRED FLOOR WEB STA 480-500 RBL 12 IAW FEDEX B757 SRM 53-00-51-2R, FIG 201

Part: TRANSMITTER — INOPERATIVE (TE FLAP SYS) · airframe 58,985 hrs · 26,907 cycles

TE FLAP ASYM AFTER FLAPS SELECTED TO 1 AT APPROXIMATELY 220 KTS RAN THE TRAILING EDGE FLAPS ASYMMETRY CHECKLIST AND LANDED WITH FLAPS BETWEEN 0 AND 1. REPLACED THE LEFT FLAP POSITION TRANSMITTER, WITH A REPAIRED TRANSMITTER IAW AMM 27-58-03-4. TESTED IAW 27-58-01/501. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: TRUNNION — GOUGED (LT MLG) · airframe 58,869 hrs · 26,833 cycles

LMLG AFT TRUNNION FITTING INBD. FLAP FAIRING BRACKET HAS GOUGES AND POSSIBLE CRACKS UNDER AND AROUND HI-LOC FASTENER HEADS. MWT4 REPAIRED FLAP FAIRING BRACKET PER EA F-5710-T0371573 P1 AND REINSTALLED PER BAC DRAWING 113N1802.

Part: NONE — DELAMINATED (ZONE 200) · airframe 57,918 hrs · 26,324 cycles

COURIER AREA FLOOR BOARD 222MDF IS DELAMINATED. FABRICATED FLOOR BOARD 222MDF ON VT MAE TRAVELER # T21/1582646 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR

Part: NONE — NONE (ZONE 200) · airframe 57,918 hrs · 26,324 cycles

MAIN CABIN FLOOR PNL # 242 MCF HAS DENT DAMAGE TO UPPER SURFACE. FABRICATED ZONE 240 FLOOR BOARD 242 MCF ON VT MAE TRAVELER # T21/1584284 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR

Part: NONE — DAMAGED (ZONE 200) · airframe 57,918 hrs · 26,324 cycles

MAIN CABIN FLOOR PNL 242 MEF HAS PUNCTURE DAMAGE TO LOWER SURFACE AND DAMAGE TO LOWER CORNER STA 1020-TO-1055 BL0 TO 24 RBL. FABRICATED ZONE 240 FLOOR BOARD 242 MEF ON VT MAE TRAVELER # T21/1584285 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR

Part: NONE — DELAMINATED (ZONE 200) · airframe 57,918 hrs · 26,324 cycles

COURIER AREA FLOOR BOARD 221MAF IS DELAMINATED. FABRICATED FLOOR BOARD 221MAF ON VT MAE TRAVELER # T21/1582641 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR

Part: NONE — DELAMINATED (ZONE 200) · airframe 57,918 hrs · 26,324 cycles

COURIER AREA FLOOR BOARD 221MBF IS DELAMINATED. FABRICATED FLOOR BOARD 221MBF ON VT MAE TRAVELER # T21/1582642 IAW DWG SRZ-25-005 REVISION "R". MAJOR REPAIR

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 57,918 hrs · 26,324 cycles

COURIER AREA FLOOR PANEL 221BF IS DELAMINATED. FABRICATED FLOOR BOARD 221BF ON VT MAE TRAVELER # T21/1582643 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 57,918 hrs · 26,324 cycles

COURIER AREA FLOOR BOARD 221AF IS DELAMINATED. FABRICATED FLOOR BOARD 221AF ON VT MAE TRAVELER # T21/1582665 IAW DWGSRZ-25-005 REVISION R. MAJOR REPAIR

Part: NONE — DELAMINATED (N/A) · airframe 57,918 hrs · 26,324 cycles

COURIER AREA FLOOR BOARD 141N5361-235 IS DELAMINATED. FABRICATED FLOOR BOARD 141N5361-235 ON VT MAE TRAVELER # T21/1582578 IAW DWG SRZ-25- 005 REV R MAJOR REPAIR

Part: NONE — DELAMINATED (ZONE 200) · airframe 57,918 hrs · 26,324 cycles

COURIER AREA FLOOR BOARD 222MEF IS DELAMINATED. FABRICATED FLOOR BOARD 222MEF ON VTMAE TRAVELER # T21/1582649 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR

Part: NONE — DELAMINATED (ZONE 200) · airframe 57,918 hrs · 26,324 cycles

COURIER AREA FLOOR BOARD 141N5361-233 IS DELAMINATED. FABRICATED FLOOR BOARD 141N5361-233 ON VT MAE TRAVELER # T21/1582663 IAW DWG SRZ- 25- 005 REVISION R. MAJOR REPAIR

Part: NONE — DELAMINATED (ZONE 200) · airframe 57,918 hrs · 26,324 cycles

COURIER AREA FLOOR BOARD 222BF IS DELAMINATED. FABRICATED FLOOR BOARD 222BF ON VT MAE TRAVELER # T21/1582647 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 57,918 hrs · 26,324 cycles

COURIER AREA FLOOR BOARD 141N5361-231 IS DELAMINATED FABRICATED FLOOR BOARD 141N5361-231 ON VT MAE TRAVELER # T21/1582662 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIR

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 57,918 hrs · 26,324 cycles

COURIER AREA FLOOR BOARD 222 MBF IS DELAMINATED FABRICATED FLOOR BOARD 222 MBF ON VT MAE TRAVELER # T21/1582644 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 57,918 hrs · 26,324 cycles

COURIER AREA FLOOR BOARD 222MAF IS DELAMINATED FABRICATED FLOOR BOARD 222 MAF ON VT MAE TRAVELER # T21/1582664 IAW SRZ-25-005 REVISION R MAJOR REPAIR

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 57,918 hrs · 26,324 cycles

COURIER AREA FLOOR BOARD 222 AF IS DELAMINATED FABRICAED FLOOR BOARD 222 AF ON VT MAE TRAVELER # T21/1582648 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 57,918 hrs · 26,324 cycles

COURIER AREA FLOOR BOARD 222 MCF IS DELAMINATED FABRICATED FLOOR BOARD 222 MCF ON VT MAE TRAVELER # T21/1582661 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR

Part: CIRCUIT CARD — MALFUNCTIONED (CARGO FIRE) · airframe 56,701 hrs · 25,685 cycles

FWD AFT RED CARGO FIRE EICAS ILLUMINATED FOR APPROX 5 SECONDS PASSING FL250. WITH AUDIBLE. ON TURNBACK, LIGHTS WENT OUT WITH NO MORE WARNINGS. NO BOTTLES EXPENDED DUE TO SHORT DURATION OF LIGHT. R & R THE FIRE DETECTION PRINTED CIRCUIT CARD M10427 IAW MM 26-10-01-4, OPS CHECKED NORMAL.

Part: DOUBLER — GOUGED (RT WING TE FLAP) · airframe 56,212 hrs · 25,372 cycles

R/H OUTBOARD MAIN FLAP L/E DOUBLER IS GOUGED. COMPLIED WITH EA F-5750-T0350465 P1, AND SRM 57-53-01-2R, REP 2, FIG 201.

Part: SHEAR PANEL — CORRODED (BS 1688) · corrosion level 2 · airframe 56,212 hrs · 25,372 cycles

MAIN CABIN AT BS 1681 TO 1720, SHEAR DECK, LT SIDE FROM BL 0 TO LBL 58.0, HAVE SEVERAL POINTS OF CORROSION. REMOVED THE CORROSION ON SHEAR DECK IAW SRM 51-10-02. ALL AREA'S EXCEPT AT BS 1688, LBL 50 WERE FOUND TO BE IN LIMITS IAW SRM 53-00-51-1A FIG 101. AT BS 1688, LBL 50, FABRICATED A REPAIR DOUBLER AND INSTALLED IAW SRM 53-60-51-2R, REP 2, ALT 1.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,212 hrs · 25,372 cycles

MAIN CABIN BS 1681, BL 0 GUSSET IS CORRODED. REMOVED CORROSION ON GUSSET IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101. REMOVED, FABRICATED AND INSTALLED THE NEW GUSSET IAW SRM 51-40-02 AND DWG 146N5216 REV -.

Part: CHANNEL — CORRODED (R1 DOOR FRAME) · corrosion level 2 · airframe 56,212 hrs · 25,372 cycles

U CHANNEL AT R1 DOOR CUTOUT AFT SIDE HAS CORROSION. REMOVED THE CORROSION AT R1 DOOR CHANNEL IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101. REMOVED, FABRICATED, AND INSTALLED A NEW CHANNEL IAW SRM 51-40-02, 51-40-05, 51-40-08, AND DWG 141N5160, REV B, AND REV CD.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,212 hrs · 25,372 cycles

FWD CARGO 580 STUB BEAM IS CRACKED COMPLIED WITH FEDEX EA -F-5310-T0305456 FUSELAGE -MAINFRAME -STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.

Part: MECHANISM — LACK OF LUBE (R1 DOOR) · airframe 55,401 hrs · 24,871 cycles

R1 DOOR LIGHT WAS INOP UPON ARRIVAL AT MCI WITH DOOR LOCKED. (GIRT BAR) LUBED R1 DOOR GIRT BAR SLIDER MECHANISM PER AMM 12-21-18-3 CYCLED DOOR ARMED LEVER SEVERAL TIMES DOOR SLIDE LIGHT OPS CHECK GOOD.

Part: SPACER — CRACKED (NLG) · airframe 53,836 hrs · 23,896 cycles

LEFT NLG WHEEL SPACER IS CRACKED. REMOVED AND REPLACED SPACER.

Part: SEAL DEPRESSOR — DENTED (CARGO DOOR) · airframe 52,508 hrs · 23,076 cycles

C2 DOOR FWD LOWER RADIUS SEAL DEPRESSOR GOUGED. FOUND OUT OF LIMITS IAW SRM 52-30-02-1A DETAIL 3. REMOVED & INSTALLED NEW SEAL DEPRESSOR IAW SRM 51-40-02 & AMM 51-41-40-2. COMPLIED LEAK CHECK WITH NORMAL RESULT IAW AMM 05-51-24-2.

Part: SKIN — GOUGED (TE FLAP) · airframe 52,508 hrs · 23,076 cycles

RIGHT WING OTBD FLAP LE NEAR THE OTBD END IS GOUGED. REMOVED REPAIR IAW SRM 51-40-02. FABRICATED OTBD DOUBLER & REPAIR PLATE IAW SRM 57-53-01-2R REPAIR 2, & INSTALLED IAW SRM 57-53-01-2R REPAIR 2 & EA F-5750-T0321543 C P1.

Part: SEAL DEPRESSOR — DENTED (CARGO DOOR) · airframe 52,508 hrs · 23,076 cycles

C1 DOOR FWD LOWER RADIUS, SEAL DEPRESSOR DENTED. FOUND OUT OF LIMITS IAW SRM 52-30-02-1A NOTE B. REMOVED & INSTALLED NEW SEAL DEPRESSOR IAW SRM 51-40-02 & AMM 51-41- 00-2. COMPLIED LEAK CHECK WITH NORMAL RESULT IAW AMM 05-51-24-2.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 522 hrs · 22,900 cycles

CAPTAIN'S O2 MASK DOES NOT TRANSMIT. PDX R RESET COMM CB AT CAPTAIN`S O2 BOX IAW AMM 35-11-4. OPERATIONS CHECKED NORMAL.

Part: ACM — FAILED · airframe 520 hrs · 22,760 cycles

SMOKE & FUMES IN COCKPIT DURING FLIGHT WHEN LEFT ENGINE BLEED WAS TURNED OFF, LOUD NOISE WENT AWAY. R & R AIR CYCLE MACHINE IAW MM 21-51-03-4. OP CHECKED NORMAL. OK FOR CONTINUED SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 51,318 hrs · 22,314 cycles

COCKPIT EMER LIGHT INOPERATIVE. RELEASED FOR SERVICE IAW MEL 33-51-01-01. INTERIOR EMER LIGHTS INOPERATIVE. R & R LIGHT BULB, NO HELP. SWAPPED BATTERY PACK ASSEMBLY LIGHT STARTED TO WORK BUT VERY DIM THEN AFTER TURNING ON 3 TIMES LIGHT FAILED AGAIN. SWAPPED BACK ORIGINAL BATTERY PACK, NEEDS POWER SUPPLY. LIGHT PANEL ASSEMBLY OPEN & LADDER ON BOARD ACFT TO AID IN THE REMOVAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 51,318 hrs · 22,314 cycles

R1 DOOR OUTSIDE EMER LIGHT INOPERATIVE. RE LAMPED R1 DOOR SLIDE EMER LIGHT IAW SMP. OK TO CONTINUE.

Part: GOVERNOR — MALFUNCTIONED (LT ENGINE FUEL) · airframe 51,266 hrs · 22,271 cycles

LEFT ENGINE WOULD NOT SET TAKEOFF POWER, WOULD ROLL BACK. LT ENGINE FUEL FLOW GOVERNOR & HP FUEL PUMP R & R. ENG RUN AT HIGH POWER IAW JRH WITH THROTTLES MATCHED AT ALL POWER SETTINGS WITH NO SURGING.

Part: SWITCH — DEFECTIVE (CABIN) · airframe 51,209 hrs · 22,227 cycles

METAL CLIP ON EMER LIGHTS SWITCH CAME LOOSE. SWITCH DOES NOT OPERATE NORMALLY AFTER SHUT DOWN. R & R EMER LIGHTS SWITCH IAW 33-51-08-4. OPERATIONS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 50,916 hrs · 22,038 cycles

L1 SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-5-06-2-1. OPERATIONS CHECKED GOOD.

Part: RELIEF VALVE — FAULTY (CABIN PRESSURE) · airframe 50,853 hrs · 21,986 cycles

TEST FLIGHT OVER PRESS RELIEF VLV DID NOT OPEN UNTIL THE CABIN WAS AT 9.4 PSI. 757 FTAM SAYS VLV SHOULD OPEN BETWEEN 8.85 - 9.25. R & R UPPER PN 103642-3, SN 108-1297 & LOWER PN 103642-3 & SN 108-1263. POSITIVE PRESS RELIEF VLVS IAW B757 AMM 21-32-01-2. PERFORMED STATIC SYS LEAK CHECK IAW B757 AMM 21-32-01-2, CHECKED GOOD.

Part: WEB — CORRODED (BS 1615-1620) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

BS 1615 - 1620, S19R WEB TO STRINGER IS MISSING FIVE LOCK FASTENERS AND IS BULGING. CORROSION WAS OUT OF LIMITS IAW SRM 53-60-15, FIG 101, DET. 8, CAT "B". REPAIRED IAW 60000410860001, EA 757-5361-16-F4347, REV-.

Part: FRAME — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

NR 3 CARGO DOOR LOWER FRAME BETWEEN FWD CAVITY, INTERNAL SIDE CORRODED, REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-53, DET V, FIG 101. REMOVED DAMAGE AREA IAW SRM 51-70-13 FIG 1. INSTALLED REPAIR IAW SRM 51-40-02 AND 51-70-13, FIG 1. COMPLIED WITH EA F-5230-T0303214. CLASSIFIED AS A CATEGORY B MAJOR REPAIR.

Part: STRUCTURE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

LEFT INBD MAIN FLAP CORRODED. R & R LT INBD MAIN FLAP IAW AMM 27-51-02/401. ADJUSTED IAW AMM 27-51-02/501. PERFORMED TEST IAW AMM 27-51-02-5. CHECKED GOOD.

Part: ATTACH FITTING — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

LEFT PYLON OTBD ATTACH FITTING HAS CORROSION ON INBD AND OTBD SIDES. COMPLIED WITH EA F-5710-T0300911, PT 1. REPAIR IS CLASSIFIED AS CATEGORY B, MAJOR.

Part: SKIN — CORRODED (HORIZONT STAB) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

LEFT HORIZONTAL STAB UPPER SKIN, SS 91. 6 INCHES AFT OF FWD SPAR CORRODED. REMOVED CORROSION. FOUND OUT OF LIMITS IAW SRM 55-10-01, FIG 101 DETAIL II. COMPLIED WITH EA F-5510-T0300660B. REPAIR IS CLASSIFIED AS A CATEGORY B MAJOR.

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

LT HORIZONTAL STAB UPPER SKIN CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 55-10-01, FIG 101, DETAIL III. COMPLIED WITH EA F-5510-T0300660B. REPAIR IS CLASSIFIED AS A CATEGORY B MAJOR.

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

LEFT HORIZONTAL STAB UPPER SKIN, CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 55-10-01, FIG 101, DETAIL III. COMPLIED WITH EA F-5510-T0300660B . REPAIR CLASSIFIED AS CATEGORY B MAJOR.

Part: STRUCTURE — DAMAGED (ZONE 500) · airframe 50,850 hrs · 21,982 cycles

HOLE ON LT WING FOUND TO BE .375 SHOULD BE .308 -.313. FOUND DURING SB 757-54-0035, REV 6. COMPLIED WITH EA F-5710-T0300911. CLASSIFIED AS A CATEGORY B, MAJOR REPAIR.

Part: SHEAR TIE — GOUGED (BS 1620) · airframe 50,850 hrs · 21,982 cycles

AFT CARGO, BS 1620 S27-28R, SHEAR TIE AFT SIDE IS GOUGED. R & R SHEAR TIE IAW DWG 146N1022, SH5, REV A AND SRM 51-40-02, CAT "A" MAJOR REPAIR.

Part: SHEAR TIE — PUNCTURED (BS 1540) · airframe 50,850 hrs · 21,982 cycles

AFT CARGO BAY FRAME BS 1540, BETWEEN S28-29L, SHEAR TIE PUNCTURED. REMOVED SHEAR TIE IAW SRM 51-40-02. FABRICATED NEW SHEAR TIE AND INSTALLED. MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

FUSELAGE SKIN CORRODED BS 1872. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET II. REMOVED SKIN IAW SRM 51-40-02. INSTALLED NEW SKIN IAW SRM 51-40-02 AND DWG148N3611. REPAIR CLASSIFIED AS CATEGORY "A" MAJOR REPAIR.

Part: STRINGER — CORRODED (BS 1872) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

STRINGER 23L, BS 1872 CORRODED. REMOVED STRINGER IAW SRM 51-40-02. REMOVED CORROSION ON STRINGER IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, FIG 101. INSTALLED NEW STRINGER IAW SRM 51-40-02 AND DWG 148N3601. THIS REPAIR CLASSIFIED AS CATEGORY "A" MAJOR.

Part: FRAME — DAMAGED (ZONE 100) · airframe 50,850 hrs · 21,982 cycles

AFT CARGO, STA 1420, FRAME, S25L-S26L, INBD FLANGE HAS 4 EA DRILLED HOLES. FOUND FRAME OUT OF LIMITS IAW SRM 53-00-07, FIG 101. REMOVED FRAME IAW SRMM 51-40-02. FABRICATED NEW FRAME AND INSTALLED IAW SRM 51-40-02 AND DWG 146N1012 SH 3. MAJOR REPAIR.

Part: FRAME — DENTED (BS 1320) · airframe 50,850 hrs · 21,982 cycles

AFT CARGO, BS 1320 S25L, FRAME UPPER FLANGE DENTED. FOUND OUT OF LIMITS IAW SRM 53-00-07, FIG 101, SHT 1. REMOVED AND REPLACED FRAME SECTION IAW SRM 51-40-02 AND DWG 146N1007. MAJOR REPAIR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 50,850 hrs · 21,982 cycles

SCRIBE LINE ON SKIN AT S26L BS 475 TO 661. REPAIRED IAW 60000411490001 AND EA 757-5331-16-F4238. . REPAIR CLASSIFIED AS A CATEGORY A MAJOR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 50,850 hrs · 21,982 cycles

SCRIBE LINE FOUND AT STRINGER 19R LAP SEAM FROM BS 439.625 TO 560.875. REPAIRED IAW EA 757-5331-16 -F4253, REV-. MAJOR REPAIR.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

AFT CARGO, BS 1300, LBL 21-RBL 21, FRAME CORRODED. REMOVED CORROSION IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW SRM 53-00-07, DETAIL 2, FIG. 101. REMOVED AND REPLACED FRAME IAW DWG 146N1006, SH.3, REV. E, AND SRM 51-40-02. MAJOR REPAIR (CAT. "A")

Part: SILL — CORRODED (BS 1862-1885) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

BS 1862.70 - 1885.20, S25L SILL CORRODED. REMOVED SILL IAW SRM 51-40-02. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03 FIG 101 DET II. INSTALLED NEW SILL IAW SRM 51-40-02 AND DWG 148N3601. REPAIR IS CLASSIFIED AS MAJOR.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

RT WING REAR SPAR BELOW RT FUEL PUMP HAS CORROSION. COMPLIED WITH EA F-5710-T0300819 STEPS 1, 2 WING -BASIC STRUCTURE-WING SPAR CORROSIONS AT AFT BOOST PUMPS MOUNT. MAJOR REPAIR.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 50,850 hrs · 21,982 cycles

RIGHT WING OTBD AFT FLAP UPPER SKIN HAS DELAMINATION. REMOVED DELAMINATED AREA AND REPAIRED IAW SRM 57-53-01 AND 51-70-17, PARA 3B - 3H.

Part: WEB — GOUGED (BS 739) · airframe 50,850 hrs · 21,982 cycles

RT UPPER LOBE FRAME SUPPORT WEB AT BS 739, S13R GOUGED.

Part: SKIN — DENTED (ZONE 100) · airframe 50,850 hrs · 21,982 cycles

RIGHT SKIN BS 395-377.7 S18-19R DENTED. REPAIRED IAW EA F-5330-T0301940. REPAIR CLASSIFIED AS CATEGORY A MAJOR.

Part: ANGLE — GOUGED (BS 739 S13R) · airframe 50,850 hrs · 21,982 cycles

RT UPPER LOBE WEB SUPPORT ANGLE GOUGED BS 739, S13R.

Part: CREASE BEAM — CORRODED (BS 680-730) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

RT CREASE BEAM INBD ANGLE UPPER SURFACE HAS CORROSION BS 680 - 730. REMOVED CORROSION IAW SRM 51-00-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13 FIG 101, DETAIL VIII. R & R RT INBD CREASE BEAM ANGLE IAW SRM 51-40-02 AND DWG 143N8328. REPAIR IS CLASSIFIED AS CATEGORY A MAJOR.

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

NR 2 STRUT BETWEEN PPSTA 128.05 TO PPSTA 209.5 LT SKIN INTERNAL SURFACES WITH SEVERAL AREAS OF CORROSION. FOUND OUT OF LIMITS IAW SRM 54-50-01, PAGE 103, DETAIL II, SECTION A-A. REMOVED SKIN IAW SRM 51-40-02. DRILLED AND INSTALLED NEW SKIN SRM 51-40-02 AND DWG 311N5002. REPAIR CLASSIFIED AS CATEGORY A MAJOR.

Part: SKIN — DENTED (BS 500-520) · airframe 50,850 hrs · 21,982 cycles

EXTERNAL FUSELAGE SKIN BS 500 -520 BETWEEN S26-27R HAS A DENT. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET III. REPAIRED BY REPAIR NR 16 OF SRM 53-00-01, PG 201. THIS IS A CATEGORY B REPAIR.

Part: FRAME — CORRODED (BS 1280) · airframe 50,850 hrs · 21,982 cycles

AFT CARGO, BS 1280 BETWEEN S28-29L FRAME LOWER WEB CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL I. R & R FRAME IAW DWG 146N1005, SH3 REV E AND SRM 51-40-02. MAJOR REPAIR.

Part: FRAME — DENTED (BS 1440) · airframe 50,850 hrs · 21,982 cycles

AFT CARGO BS 1440, S23-24L FRAME UPPER ANGEL DENTED. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1028. MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

FUSELAGE SKIN INTERNAL JUST OTBD OF S25L, BS 1850 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET II . REPAIRED SKIN IAW EA F-5330-T0300943. MAJOR REPAIR.

Part: SKIN — CORRODED (BS 1852) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

FUSELAGE SKIN INTERNAL JUST OTBD OF S25L, BS 1850 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET II. REPAIRED SKIN IAW EA F-5330-T0300943. MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

NR 2 STRUT BETWEEN STA 209.50 -128.08, RT INTERNAL SKIN WITH CORROSION ON SEVERAL AREAS. REMOVED RT OTBD SKIN IAW SRM 51-40-02. REMOVED CORROSION IAW SRM 54-50-01. FOUND TO BE OUT OF LIMITS IAW SRM 51-50-01, DETAIL V, PAGE 104. LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 311N5046. INSTALLED IAW SRM 51-40-02 AND DWG 311N5046. CLASSIFIED AS A CATERGORY A MAJOR REPAIR.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 50,850 hrs · 21,982 cycles

RIGHT HORIZONTAL STAB UPPER SKIN CORRODED. REPAIRED IAW EA F-5510-T0301861, PT1 AND EA F-5510-T0301002. PT1, MAJOR REPAIR, CAT. "B".

Part: PANEL — CRACKED (LT ELEVATOR) · airframe 50,850 hrs · 21,982 cycles

LEFT ELEVATOR FWD LOWER L/E HINGE LINE PANEL HAS A CRACKED IN TWO CUT-OUT AREAS BETWEEN STA 52 & 76. REPAIRED LT ELEVATOR IN 2 CUT-OUT IAW SRM 51-70-04, PARA 4E. MAJOR REPAIR.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 50,850 hrs · 21,982 cycles

RIGHT ELEVATOR , STA 78.5, UPPER L/E SKIN CRACKED. REPAIRED RT ELEVATOR IAW SRM 51-70-04, PARA 4E. MAJOR REPAIR.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 50,850 hrs · 21,982 cycles

RIGHT ELEVATOR L/E, STA 102.5, CRACKED. REPAIRED RT ELEV L/E IAW SRM 51-70-04, PARA 4E. MAJOR REPAIR.

Part: CREASE BEAM — DAMAGED (ZONE 200) · airframe 50,850 hrs · 21,982 cycles

MDC LT CREASE BEAM INBD ANGLE FROM BS 1370-1630 HAS DOUBLE DRILLED HOLES, NUMEROUS SHORT EDGED MARGIN HOLES AND SEVERAL AREAS AROUND FASTENERS HOLES SHOW BARE METAL. R & R INBD CHORD FROM BS 1370 - 1630 LT IAW SRM 51-40-02, DWG 146N5590. PART OUT OF LIMITS FOR SHORT EDGE MARGIN IAW SRM 51-40-06. CAT "A" MAJOR REPAIR.

Part: FRAME — DENTED (BS 1540) · airframe 50,850 hrs · 21,982 cycles

AFT CARGO, BS 1540 S25-26L, FRAME UPPER ANGLE DENTED. REMOVED FRAME, IAW SRM 51- 40-02. FABRICATED FRAME. INSTALLED NEW FRAME IAW SRM 51-40-02 AND DWG 146N1048. MAJOR REPAIR

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 50,850 hrs · 21,982 cycles

RT WING INBD MAIN FLAP LOWER SKIN PUNCTURED. REPAIRED IAW SRM 57-53-01 AND 51-70-06, PAR 5, B.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 50,850 hrs · 21,982 cycles

RT WING INBD MAIN FLAP LOWER SKIN PUNCTURED LOC. 85IN FROM INBD END, 6IN FROM T/E. REPAIRED IAW SRM 57-53-01 AND 51-70-06, PAR 5.B. MAJOR REPAIR.

Part: FRAME — DENTED (BS 680) · airframe 50,850 hrs · 21,982 cycles

FWD CARGO BAY BS 680 S24L FRAME UPPER FLANGE DENTED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101. R & R FRAME AT BS 680 S17-24L IAW DWG 143N1024 AND SRM 51-40-02. CAT "A" MAJOR REPAIR.

Part: FRAME — DENTED (BS 1520) · airframe 50,850 hrs · 21,982 cycles

AFT CARGO, BS 1520 S-26L, FRAME UPPER ANGLE DENTED. NO DENTS ALLOWED IAW SRM 53-00-07. REMOVED FRAME IAW SRM 51-40-02. FABRICATED NEW FRAME AND INSTALLED IAW SRM 51-40-02 AND DWG 146N1017. REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR.

Part: CREASE BEAM — CORRODED (BS 1290-1370) · airframe 50,850 hrs · 21,982 cycles

MDC LT CREASE BEAM INBD ANGLE AT BS 1290 -1370 , HAS CORROSION , SCRATCHES , AND DOUBLE DRILLED HOLES. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15, FIG 101, DETAIL VIII. R & R LT CREASE BEAM INBD ANGLE IAW SRM 51-40-02 AND DWG 146N8326.

Part: SKIN — DENTED (EMPENNAGE) · airframe 50,850 hrs · 21,982 cycles

EMPENNAGE STA 1900, RBL 12, DENTED. REPAIRED IAW SRM 53-80-01 & 51-70-10, REP 2. EMPENNAGE STA 1900 RBL 12, CAT "A". MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 1290-1405) · airframe 50,850 hrs · 21,982 cycles

MDC RT CREASE BEAM AT BS 1290-1405 HAS CORROSION, TOP AND BOTTOM SURFACES INCLUDED. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS ON INBD CHORD FOUND OUT OF LIMITS IAW SRM 53-60-15, FIG 101, DETAIL VIII. R & R STRUCTURE IAW SRM 51-40-02 AND DWG 146N8326. RT BS 1290-1405. CAT "A" MAJOR REPAIR.

Part: SKIN — DENTED (CARGO DOOR) · airframe 50,850 hrs · 21,982 cycles

NR 2 CARGO DOOR LOWER FWD CORNER DENT ON SKIN EDGE CAUSED REPAIR TO SEPARATE. FOUND TO BE OUT OF LIMITS IAW SRM 52-30-01, FIG 101, DETAIL VI. REPAIRED NR 2 CARGO DOOR LOWER FWD CORNER SKIN EDGE IAW SRM 52-30-01 REPAIR NR 4. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

FLOORBEAM AT BS 1640 UPPER TEE HAS CORROSION AND GOUGED ON ENTIRE UPPER SURFACE. FOUND TO BE OUT OF LIMITS IAW-SRM-53-00-51, FIG 101, DETAIL VI. R & R FLOORBEAM AT BS 1640 IAW-SRM-51-40-02 AND DWG 146N5089. MAJOR REPAIR.

Part: SKIN — DENTED (BS 250) · airframe 50,850 hrs · 21,982 cycles

LEFT EXTERNAL FUSELAGE HAS DENTED BETWEEN S16-17L, BS 250. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101, DETAIL III. REPAIRED SKIN IAW SRM 53-00-01, FIG 201, REPAIR 16. REPAIR MAJOR.

Part: SEAT TRACK — DAMAGED (BS 1540-1640) · airframe 50,850 hrs · 21,982 cycles

SEAT TRACK BS 1540 - 1640 RBL 24.75 DAMAGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL I, FIG 101. R & R SEAT TRACK IAW SRM 51-40-02, DWG 146N5130. THIS IS CATEGORY "A" MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 560-600) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

RT CREASE BEAM UPPER SURFACE HAS CORROSION, BS 560- 600. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG.101, DETAIL VIII. R & R CREASE BEAM RT INBD ANGLE BS 450 - 665 IAW SRM 51-40-02 & DWG. 143N5520. CATEGORY "A" MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 50,850 hrs · 21,982 cycles

FLOORBEAM AT BS 1280 UPPER CHORD HAS NICKS, GOUGES, MISDRILLED HOLE AND NUMEROUS SHORT EDGED MARGIN HOLES. CLEANED AND REWORKED 3 EA. MISDRILLED HOLES, CHECKED LIMITS, EDGE MARGINS HOLES, FLOORBEAM FOUND TO BE OUT OF LIMITS IAW-SRM-51-40-06, REMOVED FLOORBEAM IAW SRM-51-40-02, FABRICATED NEW FLOORBEAM IAW DWG 146N5005 IAW-8SRM-53-60-51, PG 3, FIG.1. INSTALLED NEW FLOOR BEAM IAW-SRM-51-40-02 AND DWG 146N5005, CAT."A"MAJOR REPAIR.

Part: STRINGER — CORRODED (BS 1787-1862) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

STRINGER 25L, BS 1787-1862, CORRODED. REMOVED CORROSION IAW SRM 51-10-02 . FOUND OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DET II . R & R STRINGER IAW SRM 51-40-02 AND DWG 148N3206, SH 1, REV B. MAJOR REPAIR.

Part: SHEAR WEB — DAMAGED (BS 1681-1720) · airframe 50,850 hrs · 21,982 cycles

AFT SHEAR WEB FROM BS 1681-1720, LBL 58-RBL 58, HAS SEVERAL AREAS WITH NICKS, SCRATCHES AND CORROSION AROUND FASTENER HOLES AND GALLEY TRACKS AND SUPPORT CHANNELS. FOUND TO BE OUT OF LIMITS IAW-SRM-53-00-51, FIG 101 DETAIL II. R & R AFT SHEAR WEB (DECK PLATE IAW-SRM-51-40-02 "CAT A REPAIR" AND DWG 146N5300, MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (BS 1300) · airframe 50,850 hrs · 21,982 cycles

FLOORBEAM AT BS 1300, RT SIDE UPPER ANGLE HAS DOUBLE DRILLED HOLE. CHECKED LIMITS, HOLE HAS SHORT EDGE MARGIN, AREA FOUND TO BE OUT OF LIMITS IAW SRM-51-40-06. REPAIRED FLOORBEAM AT STA 1300 AT RBL 35 IAW SRM-53-00-51, REPAIR 5. NOTE: THIS REPAIR IS CATEGORY "A" MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 475-661) · airframe 50,850 hrs · 21,982 cycles

SKIN HAS A SCRIBE LINE AT S26L BS 475 - 661. REPAIRED IAW EA 757-5331-16-F4238. REPAIR CLASSIFIED AS CATEGORY "A" MAJOR.

Part: CREASE BEAM — DAMAGED (BS 1210) · airframe 50,850 hrs · 21,982 cycles

CREASE BEAM INNER ANGLE HAS DOUBLE DRILLED HOLE AT BS 1210, RT SIDE. CHECKED LIMITS OF DOUBLE DRILLED HOLE ON CREASE BEAM, STA 1180-1290 RT SIDE. CREASE BEAM FOUND TO BE OUT OF LIMITS IAW-51-40-06. R & R INBD CREASE BEAM FROM BS 1180-1290, RT SIDE IAW-51-40-02 AND DWG 146N5590, CAT "A" MAJOR REPAIR.

Part: CREASE BEAM — DAMAGED (BS 1180-1290) · airframe 50,850 hrs · 21,982 cycles

LEFT CREASE BEAM INBD ANGLE BS 1180-1290, HAS SEVERAL SHORT EDGE MARGIN HOLES. FOUND TO BE OUT OF LIMITS IAW SRM-51-40-06. R & R LT CREASEBEAM INBD CHORD IAW-SRM-51-40-02 AND DWG 146N5590, CAT "A" MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 418-440) · airframe 50,850 hrs · 21,982 cycles

SEAT TRACK BS 418 - 440 RBL 25 HAS SCRATCHES, GOUGES AND CORROSION. R & R SEAT TRACK IAW DWG 141N5131 AND SRM-51-40-02, CAT "A" MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 418-440) · airframe 50,850 hrs · 21,982 cycles

SEAT TRACK SCRATCHED, GOUGED AND CORRODED BS 418 - 440, RBL 45. R & R SEAT TRACK IAW-DWG 141N5131 AND SRM-51-40-02, CAT "A" MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 395-418) · airframe 50,850 hrs · 21,982 cycles

CABIN FLOOR SEAT TRACK FROM BS 395 - 418 HAS SCRATCHED, GOUGED AND CORROSION RBL 25. BLENDED AREA CHECKED LIMITS IAW SRM 53-00-52, FIG 101, DETAIL II, FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 51-40-02 & DWG 141N5130. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 395-400) · airframe 50,850 hrs · 21,982 cycles

CABIN FLOOR SEAT TRACK HAS SCRATCHES/GOUGES AND CORROSIONS FROM STA 395 - 418, RBL 45. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL II. R & R SEAT TRACK IAW SRM 51-40-02 & DWG 141N5130. CAT "A" REPAIR. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 377-418) · airframe 50,850 hrs · 21,982 cycles

SEAT TRACK CROWN SUPPORT AT LBL 45 BS 377-418 IS CORRODED. BLENDED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS, FABRICATED NEW SUPPORT IAW DWG 141N5130. R & R SUPPORT IAW SRM 51-40-02 AND DWG 141N5130. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 377.7) · corrosion level 2 · airframe 50,850 hrs · 21,982 cycles

FLOORBEAM BS 377.7 BL 0 TO LBL 70 UPPER TEE CORRODED. BLENDED CORROSION IAW SRM-51-10-02, CHECKED LIMITS IAW SRM-53-00-51, FIG 101, DETAIL III, PAGE 4, FOUND TO BE OUT OF LIMITS, REPAIRED FLOORBEAM IAW SRM 53-00-51, FIG 201, PAGES 201-206. REPAIR IS A CAT."A" MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 365.25) · airframe 50,850 hrs · 21,982 cycles

FLOORBEAM BS 365.25 UPPER TEE LBL 61 TO RBL 61 CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL II AND III. R & R UPPER TEE RBL 32 -RBL 52 IAW SRM 53-00-51, FIG 201, REPAIR 3. CAT "A" MAJOR REPAIR.

Part: SKIN — BULGED (BS 1720) · airframe 50,850 hrs · 21,982 cycles

BS 1720 S23-24R BULGING SKIN. ACCOMPLISHED EA F-5330-T0300788. MAJOR REPAIR.