N960FD

Part: NONE — NONE (N/A) · airframe 71,630 hrs · 26,128 cycles

STRONG ORDER OF PAINT THINNER AT LEVEL OFF. COMPLIED WITH FUMES CHECKLIST IN QRH. USED 100% OXYGEN FOR REMAINDER OF FLIGHT. EMERGENCY DECLARED. CONFIRMED SPILL IN D.G. CONTAINER. (ENTERED FOR FLIGHT CREW MEMBER 5148579 OVER PHONE. GMM: 03-4-200 MET CREW ON ARRIVAL REVIEWED ITEM, RECEIVED EMD SPILL FORM REPORT. SPILL WAS CONTAINED IN HAZ CONTAINER, NO SPILLAGE IN AIRCRAFT. INSPECTED MAIN CARGO DECK FLOOR NO SPILLAGE. A/C OK TO CONTINUE

Part: LENS — CRACKED (EXTERIOR LIGHT) · airframe 71,348 hrs · 25,928 cycles

DURING SERVICE CHECK FOUND RIGHT EXTERIOR SLIDE LT INOP REF AMM 33-51-06-2-1. INSTALLED R/H OUTER EMERGENCY LIGHT GASKET AND NEW LENS COVER AND BATTERY PACK. OPS CHECK GOOD ON ALL EMERGENCY LIGHTS.

Part: NONE — NONE (N/A) · airframe 70,871 hrs · 25,592 cycles

#1 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED, REPLACED, ADJUSTED AND OPS CHECK IAW B757-2 AMM 27-81-01-4

Part: NONE — NONE (N/A) · airframe 70,871 hrs · 25,592 cycles

#6 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED,REPLACED, ADJUSTED AND OPS CHECK IAW B7578 AMM 27-81-01-4 AND FEDEX EA F- 5750-T0366777

Part: NONE — NONE (N/A) · airframe 70,871 hrs · 25,592 cycles

#5 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED, REPLACED, ADJUSTED AND OPS CHECK #5 SLAT IAW B757 AMM 27-81-01-4

Part: FAIRING — CRACKED (N/A) · airframe 70,871 hrs · 25,592 cycles

#1 PYLON AFT LOWER HEAT SHIELD IS CRACKED REPAIRED PER FEDEX EA # F-5480-T0366361 P1.

Part: NONE — NONE (N/A) · airframe 70,871 hrs · 25,592 cycles

STA 580 BL 45.5 SEAT TRACK CRACKED AT INBD FLANGE ACCOMPLISHED FEDEX EA : F-5310-T0366333-P1: FUSELAGE - MAINFRAME - SEAT TRACK, STRAP AND WEB, STA 580 LBL 45, CRACK AND OIL CANNING DAMAGE

Part: ANGLE — CRACKED (N/A) · airframe 70,871 hrs · 25,592 cycles

#1 PYLON AFT O/B LOWER PAN ATTACH ANGLE IS CRACKED REMOVED AND REPLACED PER BAC DWG # 313N5042 REV F

Part: SUPPORT — CRACKED (N/A) · airframe 70,871 hrs · 25,592 cycles

#2 ENG PYLON UPPER PANEL 443KL LANDING IS CRACKED REMOVED AND REPLACED PER BOEING DWG 313N5004 REV D

Part: BRACE — CRACKED (N/A) · airframe 70,871 hrs · 25,592 cycles

#2 ENG PYLON STRUT PANEL 433ER LANDING ATTACH ANGLE IS CRACKED REMOVED AND REPLACED ANGLE PER BOEING DWG # 313N5004 REV D

Part: RETAINER — CRACKED (N/A) · airframe 70,871 hrs · 25,592 cycles

L/W #3 SPOILER I/B SEAL RETAINER IS CRACKED REMOVED AND REPLACED PER BOEING DWG # 113N4605

Part: DOUBLER — NONE (N/A) · airframe 70,871 hrs · 25,592 cycles

APU COMPARTMENT STA 1885.2 RIGHT HAND SIDE LOWER REPAIR IS CHAFFED. AT APU COMPARTMENT STA 1885.2 RIGHT HAND SIDE LOWER REPAIR , REMOVED, FABRICATED AND INSTALLED NEW DOUBLER REPAIR IAW FED EX B757 SRM 53-80-08-2R.

Part: PANEL — CRACKED (ZONE 600) · airframe 70,871 hrs · 25,592 cycles

RIGHT WING UPPER FIXED LEADING EDGE PANEL BEHIND SLATS 7 AND 8 CRACKED AND DELAMINATED REPAIRED FIXED LEADING EDGE PANEL IAW B757 SRM 57-41-01-2R FIG. 201 AND 51-70-07-0G.

Part: WEB — CRACKED (N/A) · airframe 70,871 hrs · 25,592 cycles

#2 PYLON STRUT TO WING NACELLE STRUT WEB CRACKED PP STA 200 REPAIRED PER EA # F-5450-T0366482-P1

Part: NONE — CRACKED (N/A) · airframe 70,871 hrs · 25,592 cycles

L/W #3 FLAP TRACK AFT PHENOLIC RUB BLOCKS CRACKED REMOVED AND REPLACED 2EA RUB PLATES PER BOEING DWG # 113N2156 REV A

Part: ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 69,612 hrs · 24,718 cycles

ON TAKEOFF GEAR WOULD NOT RETRACT. RAN QRH, PROBLEM RESOLVED. NOTED AUTOBRAKES "RTO" DID NOT MOVE TO THE "OFF" POSITION AFTER LIFTOFF. REMOVED AND REPLACED RIGHT MAIN GEAR TRUCK POSITIONER ACTUATOR REF AMM 32-32-15-4. LEAK AND OPS CHECKS GOOD. OK FOR SERVICE.

Part: ACTUATOR — CRACKED (RT MLG) · airframe 69,610 hrs · 24,717 cycles

ON TAKEOFF GEAR WOULD NOT RETRACT. RAN QRH, PROBLEM RESOLVED. NOTED AUTOBRAKES "RTO" DID NOT MOVE TO THE "OFF" POSITION AFTER LIFTOFF. AMM: 32-32-15-4 REMOVED AND REPLACED RIGHT MAIN GEAR TRUCK POSITIONER ACTUATOR REF AMM 32-32-15-4. LEAK AND OPS CHECKS GOOD. OK FOR SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,551 hrs · 24,680 cycles

MAIN CABIN FLOOR FRAME UPPER CAP SHOWS EVIDENCE OF POSSIBLE CORROSION BL0 TO BL20R BS 1020. REMOVED CORR ON FLOOR SUPPORT STA 1020 BLO TO BL20R IAW B757 SRM 51-10-02. FOUND TO BE OUT OF LIMITS DUE TO EXFOILATION IAW B757 SRM 53-00-51-1A FIG 101. REMOVED FLOOR SUPPORT IAW B757 SRM 51-40-02. FORMED, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW SUPPORT IAW B757 SRM 51-40-05, 51-40-08, BOEING DWG 144N5005 REV - AND FEDEX EA F-5310-T0353723 P1 FUSELAGE - MAINFRAME - MAIN CARGO FLOOR SUPPORT STA 1020 CORRODED, NEW PART FABRICATION - TEMPER ALTERATION

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,551 hrs · 24,680 cycles

MAIN CABIN COMPT. SHEAR WEB HAS CORROSION, BETWEEN LBL.34", AND LBL.46", FROM BS. 1711, TO BS. 1715. REMOVED CORR ON SHEAR WEB 1711 TO 1715 LBL34 AND LBL46 IAW B757 SRM 51-10-02. LOWEST REMAINING .052 FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-60-51-2R REP 2. REPAIRED AREA IAW B757 SRM 53-60-51-2R REP 2 ALT 1

Part: WEB — CRACKED (FUSEAGE) · airframe 69,551 hrs · 24,680 cycles

MAIN CABIN INTERIOR, UPPER LOBE STRUCTURE WEB IS CRACKED, BS. 720 STR. 4R. REMOVED WEB STA 720 STR 4R, FABRICATED, LOCATED, DILLED AND INSTALLED NEW WEB IAW B757 SRM 51-40-02, 51-40-05 AND BOEING DWG 143N8323 REV M, REV C AND REV -

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,551 hrs · 24,680 cycles

SEAT TRACK RBL 44.5 STA 1320 TO 1540 HAS CORROSION ENTIRE LENGHT REMOVED CORR ON SEAT TRACK RBL 44.5 STA 1320 TO 1540 IAW B757 SRM 51-10-02. 100% MAT. LOSS DUE TO EXFOILIATION OUT OF LIMITS IAW B757 SRM 53-00-52-1A FIG 101. REMOVED SEAT TRACK, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK IAW B757 SRM 53- 60-52-01, 51-40-02 AND 51-40-05 AND 51-40-08

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,551 hrs · 24,680 cycles

SEAT TRACK AT STA 1180 LBL44.5 HAS EXFOILATION CORROSION EVALUATED SEAT TRACK STA 1180 LBL 44.5 FOUND OUT OF LIMITS DUE TO 100% MATERIAL LOSS DUE TO EXFOILATION IAW B757 SRM 53-00-52. REMOVED, TRIMMED, LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK IAW B757 SRM 51-40-02 AND 51-40-05 AND 53-60-52 FIG 101

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,551 hrs · 24,680 cycles

MAIN CABIN FLOOR FRAME UPPER CAP SHOWS EVIDENCE OF POSSIBLE CORROSION BL0 TO RBL20 BS 1060. REMOVED CORR ON FLOOR SUPPORT STA 1060 BL0 TO BL20R IAW B757 SRM 51-10-02 100% MAT. LOSS OUT OF LIMITS IAW B757 SRM 53-00-51 FIG 101. REMOVED SUPPORT IAW B757 SRM 51-040-02. FORMED, FABRICATED, LOCATED, DRILLED AND INSTALLED IAW B757 SRM 51-40-02, 51-40-05 AND FEDEX EA F-5310-T0353717 P1 FUSELAGE - MAINFRAME - MAIN CARGO FLOOR SUPPORT STA 1060 CORRODED, NEW PART FABRICATION - TEMPER ALTERATION

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,551 hrs · 24,680 cycles

MAIN CABIN INTERIOR, UPPER LOBE STRUCTURE STRINGER CLIP IS CRACKED\GOUGED BS. 720 STR. 3R REMOVED, FABRICATED AND INSTALLED MAIN CABIN INTERIOR, UPPER LOBE STRUCTURE STRINGER CLIP AT STA 720 STR. 3R IAW BOEING DWG # 140N2001, REV D AND REV. BN, B757 SRM 51-40-02-0G

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,551 hrs · 24,680 cycles

R-1 DOOR LOWER SILL UPPER SURFACE CORROSION ON THE TOP SIDE OF THRESHOLD SUPPORT AT STA 354. REMOVED CORROSION FROM R-1 DOOR LOWER SILL UPPER SURFACE, FOUND OUT OF LIMITS WITH ORIGINAL MATERIAL .050 REMAINING MATERIAL .040, REMOVED, FABRICATED AND INSTALLED NEW SUPPORT ALL IAW DWG 141N8422 REV R AND REV Y AND SRM 51-10-02, 51-40-05 AND 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1060) · airframe 69,551 hrs · 24,680 cycles

MAIN CABIN FLOOR FRAME UPPER CAP SHOWS EVIDENCE OF POSSIBLE CORROSION BL0 TO RBL20 BS 1060. REMOVED CORR ON FLOOR SUPPORT STA 1060 BL0 TO BL20R IAW B757 SRM 51-10-02 100% MAT. LOSS OUT OF LIMITS IAW B757 SRM 53-00-51 FIG 101. REMOVED SUPPORT IAW B757 SRM 51-040-02. FORMED, FABRICATED, LOCATED, DRILLED AND INSTALLED IAW B757 SRM 51-40-02, 51-40-05 AND FEDEX EA F-5310-0353717 P1 FUSELAGE - MAINFRAME - MAIN CARGO FLOOR SUPPORT STA 1060 CORRODED.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,551 hrs · 24,680 cycles

MAIN CABIN BETWEEN STA 860-879 CREASE BEAM CORRODED. REMOVED CORR ON RH CREASE BEAM STA 860-879 IAW B757 SRM 51-10-02. ORIG MAT .071 LOWEST REM .054 LOSS .017 FOUND OUT OF LIMITS IAW B757 SRM 53-30-13-1A. REPAIRED CREASE BEAM IAW B757 SRM 53-00-13-2R REP 1.

Part: SUPPORT — CRACKED (FUSELAGE) · corrosion level 2 · airframe 69,551 hrs · 24,680 cycles

R1 DOOR LOWER SILL UPPER SURFACE HAS CORROSION ON THE THRESHOLD SUPPORT STA. 338 REMOVED CORROSION FROM R1 DOOR LOWER SILL UPPER SURFACE SUPPORT STA 338, FOUND OUT OF LIMITS WITH THE ORIGINAL MAT. .050 REMAINING MATERIAL .043, REMOVED, FABRICATED AND INSTALLED NEW SUPPORT ALL IAW BOEING DWG 141N8422 REV. R AND REV Y, B757 SRM 51-10-02, 51-40-05 AND 51-40-02

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,551 hrs · 24,680 cycles

MAIN CABIN, CORROSION ON SEAT TRACK FLANGE BETWEEN STA. 365 AND 377 RBL-44. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5310-T0353677 P1 FUSELAGE - MAINFRAME - RBL 45.50 SEAT TRACK CORROSION REPAIR FROM STA 365 TO 377

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,551 hrs · 24,680 cycles

MAIN CABIN FLOOR FRAME UPPER CAP SHOWS EVIDENCE OF POSSIBLE CORROSION AT BL20L TO BL40L BS 1020. REMOVED CORR ON FLOOR FRAME UPPER CAP (PLATE) IAW SRM 51-10-02. 100% MAT LOSS OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED, FABRICATED AND INSTALLED IAW SRM 51-40-02, 51-40-05 AND DWG 144N5070 REV B AND REV W.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,551 hrs · 24,680 cycles

CORROSION SHEAR TIE AFT PIT STA. 1440 STR 29R TO STR. 30. DOT 88-014. REMOVED FABRICATED AND INSTALLED AFT CARGO SHEAR TIE AT BS1440 STR 29R TO STR 30 IAW B757 SRM 51-40-02-0G AND BOEING DWG 146N1101 REV - , REV B.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,551 hrs · 24,680 cycles

CORROSION WEB SUPPORT AFT PIT STA. 1420 - 1440 STR 29R-30. DOT 88-010. REMOVED FABRICATED AND INSTALLED AFT CARGO INTERCOSTAL AT BS1400-1420 29R-30 IAW B757 SRM 51-40-02-0G AND BOEING DWG 146N5398 REV A , REV P.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 69,551 hrs · 24,680 cycles

RH #2 DOOR UPPER HINGE CUTOUT IS CRACKED

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 69,473 hrs · 24,625 cycles

L ENG FIRE WARNING L ENG OVHT RAN ENGINES TO POWER FOR APPROX 5 MIN. TAXIED A/C PER JRH NO WARNINGS COMPLIED WITH PNEUMATIC BLEED DUCT LEAK CHECK USING ALUMINUM FOIL WRAP DURING POWER RUNS NO LEAKS WERE NOTED REF B757 AMM 36-11-00-5 ALL FOIL REMOVED. B757 FIM 26-11 FT 803 COMPLIED WITH NO DEFECTS NOTED. AFOLTS CARD WAS CHANGED PRECAUTIONARY MPN 285N0028-36 S/N D1801 SEE WORK UP DATES FOR SIGN OFFS. FIRE/OH BITE CHECK WAS COMPLIED AND PNUE SYS BACK PRESSURE CHECK COMPLIED WITH ALL WITH NO DEFECTS. SEE WORK UPDATES FOR SIGN OFFS. UNABLE TO DUPLICATE DISCREPANCY AT THIS TIME A/C OK FOR SERVICE

Part: GUST LOCK — BROKEN (L1 DOOR) · airframe 69,265 hrs · 24,462 cycles

DURING PREFLIGHT FOUND L1 DOOR HOLD-OPEN LOCK (GUST LOCK) BROKEN. PLACING L1 DOOR ON MEL. INTALLED 1 LEFT HAND PASSENGER DOOR HOLD OPEN LOCK, IN REFERENCE TO MAITENNACE MANUAL CHAPTER 52-11-08-8, OPS CHECK NORMAL. A/C OK TO VCONTINUE.

Part: FASTENER — SHEARED (SLIDING WINDOW) · airframe 69,148 hrs · 24,385 cycles

MDIS 960 56-11 6213 12SEP19 MEM FACT U FIRST OFFICER SLIDING WINDOW CRANK HANDLE HARDWARE SHEARED. FACT 12SEP19 06:08 MEM U REMOVED AND REPLACED FIRST OFFICERS #2 WINDOW CRANK HANDLE ATTACH SCREW PART NUMBER NAS1352C06-20. WORK ACCOMPLISHED REF MM 56-11-04-4. OK FOR SERVICE.

Part: ATTACH FITTING — WORN (L1 DOOR) · airframe 68,901 hrs · 24,201 cycles

PDIS 960 52-10 5966 16MAY19 MEM OPEN U LOGPAGES:3132652 LF CREW ENTRY DOOR IS VERY DIFICULT TO CLOSE. HANDLE WOULD NOT GO OVER CENTER W/O EXCESSIVE FORCE REMOVED & REPLACED L1 UPPER DOOR ATTACH FITTING REF. AMM 52-11-37-4 OPS CHECK GOOD AT THIS TIME IPC PART OFF 140N2602-25 S/N N/A IPC PART # ON 140N2602-25 S/N N/A.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 68,606 hrs · 24,002 cycles

L1 ENTRY DOOR GIRT BAR STAYED ENGAGED. L1 DOOR ASSIST BOTTLE BLEW. SLIDE PARTIALLT DEPLOYED. AMM: 25-66-01-4. REMOVED AND REPLACED L1 DOOR SLIDE/RAFT, REF AMM 25-66-01-4. OK FOR SERVICE. REMOVED SAFETY PINS INSTALLED AT L-1 DOOR EMERGENCY POWER RESERVOIR. A/C OK FOR SERVICE. MEL CLEARED AND PLACARD REMOVED. PART:EVACUATION SLIDE/RAFT.

Part: FITTING — WORN (ENTRY DOOR) · airframe 68,373 hrs · 23,858 cycles

LEFT FWD ENTRY DOOR REQUIRES MULTIPLE CLOSING ATTEMPTS TO GET CLOSED, LATCHED AND LOCKED INDICATION. R&R L1 TOP AFT LATCH FITTING, REF AMM 52-11-37-04. R&R AFT TOP DOOR LATCH ROLLER AND CHECKED DOOR AND SWITCH ADJUSTMENT, REF 52-11-00-5. OPERATION IS NORMAL WITH NO DEFECTS.

Part: SWITCH — OBSTRUCTED (GIRT BAR) · airframe 68,297 hrs · 23,810 cycles

ON ARRIVAL KMEM L1 DOOR SLIDE ARMED LIGHT INOP. CLEAND DEBRIS FROM L1 DOOR SLIDE GIRT BAR SWITCHES. OPS CHECKS NORMAL IAW AMM 25-66-00-0-0.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 68,255 hrs · 23,779 cycles

LT HYD QTY EICAS MSG INFLT ON FINAL FOUND O-RING DAMAGED ON DIFFERENTIAL PRESSURE INDICATOR AT LEFT PYLON FILTER MODULE. REMOVED AND REPLACED BOTH O-RINGS AND SERVICED LEFT SYSTEM RESERVOIR REF AMM 29-11-17-4. A/C OK FOR SERVICE.

Part: HINGE FITTING — CRACKED (THRUST REVERSER) · airframe 68,013 hrs · 23,622 cycles

NR 2 INBD THRUST REVERSER HINGE FITTING, AFT UPPER HOLE, SHOWING A CRACK INDICATION.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 68,013 hrs · 23,622 cycles

LEFT OTBD FLAP UPPER SURFACE, DELAMINATED AT MIDDLE OF FLAP 3 INCHES FROM T\E. REPAIRED IAW EA F-5750-T0339704.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 68,013 hrs · 23,622 cycles

LEFT OTBD FLAP LE, CHAFED AT THE INBD EDGE OF FLAP. REPAIRED IAW EA F-5750-T0339609 P1.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 68,013 hrs · 23,622 cycles

LEFT INBD FLAP LE, CHAFED AT THE OTBD EDGE OF FLAP. REPAIRED IAW EA F-5750-T0339646 P1.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 68,013 hrs · 23,622 cycles

RIGHT OTBD FLAP LE, CHAFED AT THE INBD EDGE OF FLAP, APPROXIMATELY 18 INCHES OTBD OF THE INBD EDGE OF FLAP. REPAIRED IAW EA F-5750-T0339592 P1.

Part: SHEAR PLATE — CORRODED (BS 377) · airframe 68,013 hrs · 23,622 cycles

SHEAR PLATE AT BS 377, LBL 8 HAS SURFACE CORROSION. BLENDED IAW EA F-5310-T0339615, P1.

Part: SEAT TRACK — CORRODED (BS 345-365) · airframe 68,013 hrs · 23,622 cycles

CORROSION FOUND ON THE COURIER SEAT, RT SEAT TRACK. REMOVED THE CORROSION ON THE SEAT TRACK, BS 345 - 365, RBL 12 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED AND REPLACED THE SEAT TRACK IAW DWG VA-3504-NC-2, SRM 51-40-02, AND DWG VA 3470, REV G.

Part: SEAT TRACK — CORRODED (BS 345-365) · airframe 68,013 hrs · 23,622 cycles

CORROSION ON COURIER SEAT LEFT SEAT TRACK. REMOVED THE CORROSION ON THE SEAT TRACK BS 345 - 365, LBL 6 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A. REMOVED AND REPLACED THE SEAT TRACK IAW DWG VA-3504-NC-2, SRM 51-40-02, AND DWG VA 3470, REV G.

Part: DOOR — CORRODED (LAVATORY SERVICE) · corrosion level 2 · airframe 67,281 hrs · 23,178 cycles

LAVATORY SERVICE DOOR, AFT RIGHT CORNER DELAMINATED AND HAS CORRODED. REMOVED AND REPLACED THE FWD LAVATORY SERVICE DOOR IAW SRM 51-40-02.

Part: BRACKET — OUT OF ADJUST (R1 DOOR) · airframe 66,472 hrs · 22,612 cycles

DURING POST FLIGHT DISCOVERED R1 DOOR HANDLE, ARMED, INDICATOR VISIBLE WITH NO ARMED LIGHT AND THE DOOR DISARMED. GREEN IAW CREW DEBRIEF THE, ARMED, INDICATOR MENTIONED IN WRI IS THE, KNUCKLEBUSTER, THAT RECESSES ITSELF IN THE DOOR WHEN IN THE DISARMED CONDITION. THE DOOR SLIDE ARM LIGHT AND ALL OTHER INDICATIONS WERE NORMAL. FOUND THAT, KNUCKLEBUSTER, IS HANGING UP ON GUIDE BRACKET INSIDE THE DOOR. ADJUSTED GUIDE BRACKET OF RETRACTABLE DOOR, KNUCKLEBUSTER, IAW AMM 52-11-20-5. TESTED ARM, DISARM SYS FOR R1 DOOR IAW AMM 52-11-25-5, ALL FUNCTIONS AND INDICATION NORMAL, ACFT OK FOR CONTINUED SERVICE AT THIS TIME.

Part: LEVER — OUT OF ADJUST (R1 DOOR) · airframe 66,458 hrs · 22,600 cycles

WITH THE HANDLE IN DISARMED POSITION ON THE R1 DOOR, THE SLIDE WARNING PLACARD STILL INDICATED ARMED. SLIDE LIGHT WAS EXTINGUISHED. T/S & FOUND RETRACTABLE INDICATION DOOR FOR DISARM. LEVER OUT OF ADJUSTMENT. ADJUSTED RETRACTABLE INDICATION DOOR REF AMM 52-11-20-5-0. OPS CK GOOD. SYS OK FOR SERVICE.

Part: FITTING — CRACKED (NR 2 PYLON) · airframe 66,355 hrs · 22,523 cycles

NUMBER 2 PYLON CRACK NOTED ON ALUMINUM BULKHEAD, INBD LOWER FITTING HOLE AT 6 OCLOCK. COMPLIED WITH REPAIR IAW EA 5450-T032497 PART 1 P1 DATE APR 28 2016.

Part: FLAP — PUNCTURED (LT WING) · airframe 66,355 hrs · 22,523 cycles

LEFT INBD FLAP TE LOWER SIDE PUNCTURED, LOWER SIDE AT NR 3 TRACK AFT FAIRING ATTACH AREA. REPAIRED LT INBD FLAP TE LOWER SIDE BY HOT BONDING DOUBLER ON LT INBD FLAP LOWER SIDE IAW SRM 57-53-01-2R FIG 201 & SRM 51-70-10-2R PARA 20. COMPLIED WITH EA F-5750T0324936A PART 1.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 66,285 hrs · 22,469 cycles

OVERRIDE FAIL LIGHT AT 70 KTS, REJECTED TAKE OFF FOR LOSS OF SPD, ALT, VERTICAL ON CAPTAINS SIDE, ALOS EICAS MSGS ATC FAULT, GND PROXIMITY SYS, RT SIDE WINDOW, TERR OVRD FAIL LIGHT. LOADED ACFT IN HEAVY RAIN. PERFORMED WATER ACCUMULATION INSPECTION CHECK IAW AMM 05-51-99-6. FOUND WATER LEAKING IN MAIN E & E COMPARTMENT FROM FLOORBOARDS BEHIND THE E 2 EQUIP RACK, ALONG WITH WATER LEAKING FROM FLOORBOARDS DOWN THE RT TUNNEL AREA FWD OF P-54. PERFORMED VISUAL INSPECTION OF COMPUTERS ON E2 1 - E2-4 WITH NO WATER OR MOISTURE NOTED. PERFORMED ADJUSTMENT TEST LT & RT ADC, LT & RT ATC & EGPWS WITH NO DEFECTS NOTED. REF MM 34-12-00-5,34-46-98-5 & 34-53-99-5. IAW MM 05-51-14-2 HIGH ENGERY STOP & HEAT DAMAGE CONDITION. INSPECTION NOT REQUIRED & RT SIDE WINDOW HEAT TEST IAW MM 30-41-00-5. ALL TEST PASSED. ACFT OK FOR SERVICE.

Part: SKIN — DENTED (BS 1478) · airframe 64,798 hrs · 21,447 cycles

LOWER FUSELAGE SKIN HAS A DENT AT BS 1478 BETWEEN STRINGERS 27 & 28L. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101. CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-00-01 REPAIR 16.

Part: TERMINAL — LOOSE · airframe 64,023 hrs · 20,868 cycles

DURING CRUISE AT FL 350 AUTOPILOT AND AUTO THROTTLES DISCONNECTED, EICAS SHOWED MACH/SPEED TRIM, RT FWD FUEL PUMP, LT AFT FUEL PUMP, AND EQPT COOLING CAUTION LIGHTS. LT AFT FUEL PUMP CB POPPED ALONG WITH THE EQPT COOLING CB. ADDITIONALLY THERE WAS A LOUD CLICKING NOISE COMING FROM BEHIND P6 CIRCUIT BREAKER PANEL. ALL INTERIOR PANEL LIGHTS WENT OUT AND STBY ADI WENT INOP. WQPT COOLING FLOW AND EQPT COOLING FAN AND WARNING ELEX STATUS MESSAGES FOUND AFTER BLOCKIN. THE P-6 PANEL, FOUND LOOSE TERMINALS ON TB5015 (REF AWM 91-21-41, SEC.TB5000, PG 12) IN PANEL P6-4 TIGHTENED NUTS MM REF AWMSP. SECURED TERMINAL IAW B757 SWPM 20-30-11. RAN MCDP BREAKOUT BOX CHECKS IAW B757 AMM 22-00-02-2. RAN BOTH ENG'S PER JRH, WHILE POWERING AC WITH BOTH ENG'S; CHECKED: AC PRESSURIZATION, REF MM 21-31-00-5, PACK OPERATION, REF MM 21-51-00-5, ELECT LOAD DISTRIBUTION, REF MM 24-50-00-5, EQUIPMENT COOLING, IAW MM 21-58-00-5-10 AND FLT COMPT ILLUMINATION, REF MM 33-11-00-5. ALL SYSTEM'S TESTED OK. AC OK FOR SERVICE

Part: GIRT BAR — OBSTRUCTED (ESCAPE SLIDE) · airframe 63,900 hrs · 20,770 cycles

EVACUTION SLIDE ARMED INDICATOR ON RIGHT SIDE IS INOPERATIVE. FOUND GRAY PAD IN THE TRACK NOT ALLOWING GIRT BAR TO FULLY SEAT AND LOCK WITH SLIDE LIGHT. OPS CHECKED GOOD.

Part: SOCKET — LOOSE (EMERGENCY LIGHT) · airframe 63,794 hrs · 20,704 cycles

EMERGENCY SLIDE LIGHT INOPERATIVE. CLEANED AREA AND TIGHTENED LAMP HOLDER TO SOCKET. PER 33-51-06-02-1. OPERATES NORMALLY.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 63,543 hrs · 20,519 cycles

ACFT ARRIVED WITH RT GEAR DOOR OPEN AND HYDRAULIC FLUID DRIPPING FROM RT WHEEL WELL, FOUND TRUCK POSITION HOSE RUPTURED. INSTALLED REPLACEMENT FLEX LINE IAW MM 20-10-10-8, LEAK CHECK OK. RT GEAR TRUCK POSITION HOSE HAS TEMPORARY LINE INSTALLED. FINAL CLOSED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,491 hrs · 20,479 cycles

DOOR SLIDE LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.

Part: STRUCTURE — DAMAGED (RT WING TE FLAP) · airframe 63,349 hrs · 20,361 cycles

AFTER REMOVAL OF THE PANEL FOUND 2EA DAMAGED HOLES ON THE RT WING OTBD FLAP. APPROX BETWEEN STA 565 & 590. COMPLIED WITH EA F-5750-160553. MAJOR REPAIR.

Part: SKIN — DENTED (R4 DOOR) · airframe 63,349 hrs · 20,361 cycles

R4 DOOR INNER SKIN HAS OUTWARD PUNCTURED HOLE IN THE UPPER HINGE CUT OUT AREA. REPAIRED IAW STAM EA 757-5211-16, F3722. CAT "A" REPAIR, REF FAA FORM 8100-9.

Part: STRAP — CORRODED (BS 1825 S3R) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

APU INLET DOOR SHROUD AFT STRAP CORRODED BS 1825 S3R. REMOVED CORROSION IAW 51-10-02 AT FS 1825, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, DETAIL V . REMOVED SHEAR TIES , FITTINGS , STRAPS AND BUTT SPLICE IAW SRM 51-40-02. FABRICATED REPLACEMENT BUTT SPLICE USING 7075-T6-.100 PO MST0029064 IAW BAC DWG 148N3138 SH 1 REV C . INSTALLED BUTT SPLICE, STRAPS, FITTINGS AND SHEAR TIES IAW SRM 51-40-02 AND DWG 148N3105 SH 1 REV C. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 500) · airframe 63,349 hrs · 20,361 cycles

SKIN MISREPAIRED AT BS 500 S28 - 29R. REPAIRED IAW-SRM-51-40-02 HFEC IAW-NTM 51-00-19 AND 51-00-16, NO CRACK INDICATIONS NOTED AROUND CUTOUT OR FASTNER HOLES, FABRICATED DOUBLER AND FILLER IAW SRM-53-00-01 FIG. 201 REPAIR 15. MAJOR REPAIR.

Part: GATE — CORRODED (R1 DOOR) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

R1 DOOR LWR GATE HAS CORROSION. UPON FURTHER INVESTIGATION, FOUND R1 DOOR LOWER GATE ASSY OUT OF LIMITS IAW SRM 52-10-02, FIG 101, DET V. REMOVED R1 DOOR LOWER GATE IAW CMM 52-11-05. R & R R1 DOOR LOWER GATE ASSY MM 52-11-38. REINSTALLED R1 DOOR LOWER GATE IAW CMM 52-11-05. ADJUSTED R1 DOOR IAW MM 52-11-00-5. MAJOR REPAIR. .

Part: WEB — CORRODED (DOOR SILL) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

L2 DOOR SILL WEB, UPON REMOVAL OF SILL SUPPORT ANGLE FOUND WEB EXFOLIATED. REMOVED CORROSION, ORIGINAL MAT THICKNESS .071", REMOVED .030", REMAINING .041", FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, SHT 5. R & R L2 DOOR SILL WEB IAW SRM 51-40-02, BS 690-780. MAJOR REPAIR.

Part: WEB — CORRODED (BS 1681-1720) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

BS 1681.8 TO 1720 AT BL 0 TO LBL 60 CABIN FLOOR SHEAR WEB HAS CORROSION. BLENDED AREAS IAW SRM 51-10-02. CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG 201, SH. 1. REMOVED CABIN FLOOR WEB, IAW SRM 51-40-02. FABRICATED NEW SHEAR WEB IAW SRM 51-10-02, SRM 53-60-51, FIG 1, DETAIL III, AND DWG 146N 5318. INSTALLED NEW WEB IAW SRM 51-40-02, AND DWG 146N5318. MAJOR REPAIR.

Part: SKIN — CORRODED (BS 1661-1681) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

CARGO BAY BS 1661 - 1681 S24-25R DOUBLER CORRODED.

Part: FLOOR SUPPORT — CRACKED (BS 1661-1680) · airframe 63,349 hrs · 20,361 cycles

BS 1661 TO 1680, RBL 10 FLOOR SUPPORT ANGLE CRACKED. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-40-02.

Part: STRINGER SPLICE — CORRODED (BS 686) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

BS 686, STRINGER 18 LT SPLICE CORRODED, REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-03. R & R STRINGER SPLICE IAW SRM 51-40-02 AND DWG DL 143N3800. MAJOR REPAIR.

Part: STRUCTURE — CORRODED (BS 665-755) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

S-17R INBD STRUCTURE BS 665 -755 RBL 64, CORRODED. REMOVED AND REPLACED INBOARD STRUCTURE IAW SRM 51-40-02 & DWG 143N8328. REMOVED CORROSION IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW 53-30-15 FIG 101 DETAIL III. MAJOR REPAIR .

Part: ANGLE — CORRODED (ZONE 200) · airframe 63,349 hrs · 20,361 cycles

L2 DOOR CUT-OUT, DOOR SILL SUPPORT ANGLE CORRODED BETWEEN STA 680 -750. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS .080", REMOVED MATERIAL .070", REMAINING MATERIAL .010", FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13, DEATAIL 2, FIG 101, PAGE 103. R & R SILL INBD CREASE BEAM IAW SRM 51-40-02. MAJOR REPAIR.

Part: GATE — CORRODED (R4 DOOR) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

R4 DR LOWER GATE CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 52-10-02, FIG 101, DET VII, INSTALLED NEW LOWER GATE IAW AMM 52-11-38-4 AND DWG 146N6106. MAJOR REPAIR.

Part: TRUSS — CORRODED (ZONE 200) · airframe 63,349 hrs · 20,361 cycles

S17R, STA 800 - 820 , TRUSS CORRODED.

Part: FRAME — CORRODED (BS 1560) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

CABIN FRAME INBD FLANGE STA 1560, RBL 61, WL 208.1 TO WL 215.1 CORRODED. REPAIRED ON MAE N/R 47658060001 AND MAE EA 757-5362-16-F3673. CLASSIFED AS A MAJOR REPAIR.

Part: GATE — CORRODED (R2 DOOR) · airframe 63,349 hrs · 20,361 cycles

R-2 DOOR LOWER GATE FWD AND AFT CORNER EDGE HAS CORROSION. FOUND R2 DOOR LWR GATE ASSY. OUT OF LIMITS IAW SRM 52-10-02, FIG 101, DET V. R & R R2 DOOR LWR GATE ASSY IAW MM 52-11-38. ADJUSTED R2 DOOR IAW MM 52-11-00-5. NO DEFECTS NOTED. MAJOR REPAIR.

Part: GATE — CORRODED (L2 DOOR) · airframe 63,349 hrs · 20,361 cycles

L2 DOOR LOWER GATE FROM FWD TO AFT EDGE HAS CORROSION. REPAIR IS CLASSIFIED AS MINOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 63,349 hrs · 20,361 cycles

SEAT TRACK BS 418 AND 440, LBL 24.75 GOUGED. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 63,349 hrs · 20,361 cycles

SEAT TRACK BS 418 - 440, LBL 24.75 GOUGED. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW SRM 51-40-02 AT STA 418-440, LBL 24.75. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 418-440) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

SEAT TRACK FROM BS 418 TO BS 440 , RBL 45.5 HAS CORROSION. DOT 124 - 118. REMOVED CORROSION IAW SRM 53-00-52. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL I. R & R SEAT TRACK IAW SRM 53-10-02, FIG I, DET 3 AND DWG 141N, 5134 SHEET I AT BS 418 - 440, RBL 45.5. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 1325) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

BS 1325 INBD CREASE BEAM CORRODED AT 17L. REMOVED CORROSION IAW SRM 53-60-13 SHT 4 OF 5 FIG 101. FOUND TO BE OUT OF LIMITS, ORIG .100, MATERIAL REMOVED .040 MATERIAL REMAINING .060 IAW SRM 53-60-13, SH 3 OF 5 FIG 101. R & R CREASE BEAM IAW SRM 51-40-02 AND DWG NR146N8326-1. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 440-680) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

MAIN CABIN STA 440 TO 640, LBL 24.75 SEAT TRACK GOUGED AND CORRODED. R & R SEAT TRACK IAW DWG 143N5090 AND SRM 51-40-02, REMOVED GOUGES/CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-52, DET I, FIG 101. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 440-640) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

SEAT TRACK, BS 440-640, RBL 45.5, CORRODED AND GOUGED. R & R SEAT TRACK, IAW DWG 143N5090 AND SRM 51-40-02. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

CREASE BEAM INBD CHORD STA 1240-1290, S17R CORRODED. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS MAT THICKNESS .080, BLENDED MAT .040 REMAINING MAT .040 FOUND OUT OF LIMITS IAW SRM 53-60=13, FIG 101, DET VIII. REMOVED IAW 51-40-02, FABRICATED IAW SRM 53-60-03. INSTALLED IAW 51-40-02 AND DWG 146N5600. MAJOR REPAIR

Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 63,349 hrs · 20,361 cycles

CREASE BEAM AT STRINGER 17R BS 1620-1630 CORRODED. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS ORIG MAT .080, BLENDED MAT .018, REMAINING MAT .062. FOUND OUT OF LIMITS IAW SRM 53-60-13, FIG 101 DET VIII. REMOVED CREASE BEAM SECTION IAW SRM 51-40-02. FABRICATED USING BAC 1515-553, IAW 53-60-13. INSTALLED IAW 51-40-02 AND DWG 146N8722 AT STA 1410 TO STA 1630. MAJOR REPAIR.

Part: GATE — CORRODED (L4 DOOR) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

L-4 DOOR LOWER GATE EDGE HAS CORROSION. REMOVED CORROSION FROM L-4 DOOR LOWER GATE IAW SRM 51-10-02. CHECKED LIMITS; FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02, DETAIL 4, FIG 101, PAGE 104. R & R LOWER GATE ASSY IAW AMM 52-11-38-004-001. RIG AND OPS CHECK ACCOMPLISHED ON N/R N00049. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

SEAT TRACK, STA 440- 640, RBL 24.75 CORRODED AND GOUGED. REMOVED CORROSION AND GOUGES IAW SRM 51-10-02, CHECKED LIMITS ORIG MAT = .250 AFTER REWORK =.211 AT STA 440 - 465 OUT OF LIMITS IAW SRM 53-00-52 DETAIL 1. SPLICED IN NEW SECTION OF SEAT TRACK STA 440-465, RBL 24.75 IAW SRM 53-00-52, FIG 201, OPTION 1. CATEGORY A REPAIR. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

SEAT TRACK FROM BS 418 TO BS 440, LBL 45.5 HAS CORROSION. REMOVED CORROSION IAW SRM 53-00-52 FIG 101, DETAIL 1. CHECKED LIMITS ORIG MAT = .050, AFTER REWORK = .024, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 1. R & R SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

SEAT TRACK BS 1320 -1540, LBL 45 CORRODED AND GOUGED. REMOVED CORROSION IAW SRM 51-10-02 CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. REMOVED SEAT TRACK IAW SRM 51-40-02, AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02 AND DWG 146N5130.

Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 63,349 hrs · 20,361 cycles

CREASE BEAM, LEFT SIDE ATTACHED SUPPORT ANGLE UPPER SKIN CORRODED AT BS 760. R & R INBD CHORD CREASE BEAM IAW SRM 53-30-13N AND DWG 143N5520 FROM STA 760 TO STA 900. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 1240-1360) · airframe 63,349 hrs · 20,361 cycles

S-17L, CREASE BEAM INBD CHORD, STA 1240-1360 CORRODED. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS FLANGE THICKNESS AND FOUND OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DET VIII. REMOVED, FABRICATED IAW SRM 53-60-13. INSTALLED IAW SRM 51-40-02 AND DWG 146N5610. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 440-640) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

MAIN CABIN STA 440 TO 640 LBL 45.50 SEAT TRACK GOUGED AND CORRODED. R & R SEAT TRACK IAW SRM 51-40-02 AND DWG 143N5090. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 1020-1040) · airframe 63,349 hrs · 20,361 cycles

CREASE BEAM S17L BS 1020-1040, CORRODED. REMOVED CORROSION WITH MATERIAL LOSS OF .023 OF ORIGINAL .090 FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13. R & R CREASE BEAM IAW SRM 51-40-02. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 450-665) · corrosion level 2 · airframe 63,349 hrs · 20,361 cycles

RT CREASE BEAM S17R BS 450 TO 665 CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS PER SRM 53-30-13, FIG.101, DETAIL 8. REMOVED AND REPLACED RT CREASEBEAM, PER SRM 51-40-02, AND DRAWING 143N5520. MAJOR REPAIR

Part: SKIN — MISREPAIRED (BS 1612) · airframe 63,349 hrs · 20,361 cycles

FUSELAGE SKIN AT BS 1612, S19-20L MISREPAIRED. IAW SRM 51-40-02, HFEC IAW NTM 51-00-19 PT 6, NO CRACKS NOTED ON CUT-OUT OR HOLES. FABRICATED DOUBLER IAW SRM 53-00-01 FIG.201 REPAIR 16 PG 201. INSTALLED DOUBLER IAW SRM 51-40-02 AND SRM 53-00-01, REPAIR 16. CATAGORY B MAJOR REPAIR.