N681DA

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,080 hrs · 41,316 cycles

SHIP 0681 ENTRY DOOR UNABLE TO CLOSE. CORRECTIVE ACTION: REMOVED AND REPLACED DOOR HOLD OPEN LOCK COLLAR REF B757 AMM 52-11. AC OK FOR SERVICE. (9528928)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,530 hrs · 40,954 cycles

SHIP 0681 EMERGENCY LIGHTS AT 2L&2R DOOR AND CENTER SECTION OF A/C INOPERATIVE. CORRECTIVE ACTION: REMOVED AND REPLACED BATTERY PACK AT 2L DOOR PER B757 AMM 33-51 OPS CK GOOD. (4505510)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,481 hrs · 40,919 cycles

SHIP 0681 EICAS MESSAGE "R WING SLIDE". CORRECTIVE ACTION: INSPECTED DOOR AND HINGES AND SLIDE PER W/C 2560-9901-RT AND REINGAGED DOOR PER B757 AMM 25-65-09. (4463376)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,958 hrs · 40,590 cycles

DUE TO LEFT ENGINE REVERSE EICAS MESSAGE DURING TAKEOFF. CORRECTIVE ACTION: FWD TO MEL 78-31-01A. R/R LT EEC CHANNEL SELECT RELAY K10528 PER B757 WDM 73-21. (9498838)

Part: FSEU — FAULTED (LT WING TE FLAP) · airframe 87,987 hrs · 40,009 cycles

CREW ELECTED DE DUE TO TE ASSYM INDICATION DURING APPROACH. CREW PERFORMED A GO AROUND AND LANDED WITHOUT INCIDENT. FSEU FAULTED LT FLAP POSITION XMTR. R/R LT FLAP POSITION XMTR. OPS CHECK GOOD.

Part: EXCITER — FAILED (RT ENGINE) · airframe 87,873 hrs · 39,936 cycles

FIRE/DE - ABORTED ENGINE START ON RIGHT ENGINE. MOTORED ENGINE PER QRH. SWITCHED FROM ENG START 1 TO ENGINE START 2. SECOND ENGINE START INDICATED NORMAL IN COCKPIT BUT CAUSED SMALL TAIL PIPE FIRE. CAPTAIN THEN SHOT DOWN ENGINE. PERFORMED GVI OF FLAPS AND ENGINE TAIL PIPE AREA PER B757 AMM 05 -41. NO DAMAGE FOUND. R/R RT ENG NR 1 IGNITION EXCITOR AND SYSTEM #1 IGNITION PER B757 AMM 74-21. OPS NORMAL.

Part: GIRT BAR — LACK OF LUBE (L3 DOOR) · airframe 87,722 hrs · 39,844 cycles

SHIP 681 3L SIDE ARMED LIGHT INOP. CLEANED AND LUBED 3L DOOR GIRT BAR IAW B757 AMM 12-21. DOOR ARM LIGHT OPS CHECK GOOD.

Part: LIGHT — NONE (CABIN) · airframe 87,687 hrs · 39,818 cycles

3L SLIDE LIGHT INOP. CORRECTIVE ACTION: OPS CKD SLIDE LIGHT. OPS NML. (9816114)

Part: INDICATOR — INTERMITTENT · airframe 87,628 hrs · 39,776 cycles

SHIP 681 L3 DOOR SLIDE WILL NOT ILLUMINATE. CORRECTIVE ACTION: NO FAULT FOUND. (9479974)

Part: NONE — NONE · airframe 87,421 hrs · 39,633 cycles

SHIP 681 DURING SVC CHK FOUND EMERGENCY LTS AT SEAT ROW 33-37 INOP. CORRECTIVE ACTION: REMOVED AND REPLACED PWR SUPPLY AT ROW 29 PER B757 AMM 33-51, OPS CHK GOOD. (9704452)

Part: NONE — NONE · airframe 87,349 hrs · 39,594 cycles

SHIP 681 FO WINDSHIELD OUTER PANE SHATTERED AT 380. CORRECTIVE ACTION: R/R F/O WINDSHIELD PER B757 AMM 56-11. (9704410)

Part: NONE — NONE · airframe 87,268 hrs · 39,559 cycles

SHIP 681 AISLE EMERGENCY LIGHTS FROM SEATS 23 TO 26 INOP. CORRECTIVE ACTION: R/R BATTERY PACK M10567 PER B757 AMM 33-51. OPS CK GOOD. (8620766)

Part: NONE — NONE · airframe 87,246 hrs · 39,538 cycles

SHIP 681 EMERGENCY LIGHTS INOP AT SEAT ROWS 38-42. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHT POWER SUPPLY FOR SEAT ROWS 38-42 PER B757 AMM 33-51. OPS NML. (8620728)

Part: NONE — NONE · airframe 87,201 hrs · 39,500 cycles

SHIP 681 SEAT MOUNTED EMERGENCY EXIT LIGHTS AT 38-42 INOP. CORRECTIVE ACTION: FOUND BATTERY DEAD AT M735 POWER SUPPLY. REPLACED POWER SUPPLY AND BATTERY PER B757 AMM 33-51-07 TESTS GOOD. (8618488)

Part: POWER SUPPLY — INOPERATIVE · airframe 86,952 hrs · 39,298 cycles

SHIP 681 EMERGENCY LIGHT FLOOR PROX INOP FROM ROW 38-42. CORRECTIVE ACTION: REPLACED POWER SUPPLY M735 PER M.M. 33-51-07. OPS CHECK GOOD. (8614094)

Part: SIGN — DETACHED · airframe 86,729 hrs · 39,117 cycles

SHIP 681 EMERG EXIT SIGN FELL DOWN AT DOOR 2L. CORRECTIVE ACTION: RESECURED SIGN. NO DEFECTS NOTED OK FOR SVC IAW 33-51 FROM B757 AMM. (8612002)

Part: SHIM — MIGRATED · airframe 86,454 hrs · 38,944 cycles

SHIP 681 LAMINATED SHIM MIGRATION FROM REAR SPAR AND BODY SPLICE PLATE. BS 1040. DOT 99-051. CORRECTIVE ACTION: SUMMARY OF NRC 00082 - ACCOMPLISHED REPAIR AT CENTER WING REAR SPAR RBBL 70.50 AT STA 1040 TERMINAL FITTING, ALL CDCCL AND SFAR 88 REQUIREMENTS COMPLIED WITH, IAW ER/A 598110-14AD REV ORIGINAL SECTION I. REFERENCE LOG PAGE 2193618 FOR FOLLOW ON INSPECTIONS. (2194742)

Part: NONE — NONE · airframe 86,438 hrs · 38,933 cycles

SHIP 681 REPAIR TO CENTER WING, LWR REAR SPAR, SOB SPLICE AT RBBL 70.5 REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 598110-14AD. CORRECTIVE ACTION: REF ERA 598110-14AD. (2193618)

Part: NONE — NONE · airframe 86,438 hrs · 38,932 cycles

SHIP 681 AMOC MONITOR INSPECTION LOG REF ERA 598080-14AD. CORRECTIVE ACTION: REF ERA 598080-14AD. (2188584)

Part: NONE — NONE · airframe 86,438 hrs · 38,932 cycles

SHIP 681 EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA AT STA R1300. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON FRAME AT STA 1300RH BTW STR 24-29R IAW ER /A 598080-14AD REV ORIGINAL. REFERENCE LOG PAGES 2188582 AND 2188584 FOR FOLLOW ON INSPECTIONS. (2188826)

Part: NONE — NONE · airframe 86,438 hrs · 38,932 cycles

SHIP 681 RIGHT STA 1560 FUSELAGE FRAME, S-26R, CONFIGURATION C, INBOARD FASTENER HOLE CRACKED APPROXIMATELY 1/4" AT 12 O'CLOCK POSITION. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON STA 1560 FRAME, STR 24-28R IAW ER/A 598355-14AD REV ORIGINAL. REFERENCE LOG PAGES 2187382 AND 2187385 FOR FOLLOW ON INSPECTIONS. (2187542)

Part: NONE — NONE · airframe 86,438 hrs · 38,932 cycles

SHIP 681 DTA MONITOR INSPECTION LOG REF ERA 598355-14AD. CORRECTIVE ACTION: REF ERA 598355-14AD. (2187382)

Part: NONE — NONE · airframe 86,438 hrs · 38,932 cycles

SHIP 681 LT SIDE FUSELAGE REPAIR AT STA 590 STRINGER L14. CORRECTIVE ACTION: ACCOMPLISHED REPAIRS AT STA 590-661L STR 14 AND STR 19L, IAW B757 SRM 53-30-01-2R REPAIR 2 AND ER/A 512671-14AD REV B SECTION IV. REFERENCE LOG PAGES 1143996 AND 0915957 FOR FOLLOW ON INSPECTIONS. (2186128)

Part: NONE — NONE · airframe 86,438 hrs · 38,932 cycles

SHIP 681 R2 DOOR STOP IS CRACKED TRAILING EDGE AT 2 OCLOCK POSITION. CORRECTIVE ACTION: REMOVED AND REPLACED R2 PASSENGER DOOR IAW AMDS T/C: 5211-9001- 2R. ALL MAINTENANCE ACCOMPLISHED ON AMDS T/C. (2177212)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 85,054 hrs · 38,377 cycles

AFT EMERGENCY EXIT LIGHTS INOPERATIVE AT TOP LEFT AND RIGHT DOORS. FOUND M737 EMERGENCY LIGHT BATTERY DEAD. REPLACED THE BATTERY, SYSTEM OPS NORMAL.

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 84,186 hrs · 38,019 cycles

(AIRCRAFT 681, L/P 6732288) R/H FWD O/WING EMERG LIGHT COVER INCORRECT. CORRECTIVE ACTION: EMERGENCY LIGHT COVER LENS P#BC5-0393-106 FITTED AT R/H FWD O/ WING EXIT. IAW B757 AMM 33-51.

Part: NONE — NONE · airframe 86,438 hrs · 38,932 cycles

SHIP 681 THIS ER/A 564779-14 INCORPORATES FAA FORM 8110-3. THE SUBJECT ER/A IS NOW AT REV. B. CORRECTIVE ACTION: REF ERA 564779-14 REV B. (1139132)

Part: LENS — UNSECURE (CABIN) · airframe 82,332 hrs · 37,223 cycles

(AIRCRAFT 681, L/P 1073555) EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS: 2R / EMERGENCY PLACARD FELL OFF ON TAKEOFF ROLL. / INTERIOR. RE SECURED R2 DOOR EXIT LENS PER AMM 33-51.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 82,083 hrs · 37,136 cycles

EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. REPLACED EMER EXIT LIGHT COVER AT DOOR R2 - OPS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,680 hrs · 36,934 cycles

SHIP 681 EMERGENCY LIGHTS ROW 26 THRU 32 AND OVER WINGS DOOR / WINDOW LIGHTS INOP. REMOVED AND REPLACED BATTERIE PACK AT ROW DEF 26. (5293152)

Part: BEAM — CHAFED (CARGO DOOR) · airframe 81,632 hrs · 36,908 cycles

AFT CARGO DOOR LOWER CORNERS AND CENTER SEAL DEPRESSORS CHAFFED. BLENDED AREA AND INSP, FOUND AREA ON C2 DOOR LOWER EDGE BEAM CENTER SECTION OUT OF LIMITS PER SRM. REMOVED AND REPLACED C2 DOOR LOWER EDGE BEAM CENTER SECTION IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,632 hrs · 36,908 cycles

AFT BULK CARGO COMPARTMENT BS 1540 SKIN AT SHEAR TIE CORRODED BETWEEN STRINGER 28L AND 29L I-42. REMOVED CORROSION AT AFT CARGO SHEAR TIE SAT 1540 BETWEEN STR 28L AND 29L FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED SHEAR TIE, FABRICATED NEW AND INSTALLED, ALL IAW SRM.

Part: GIRT BAR — DAMAGED (L1 DOOR SLIDE) · airframe 81,630 hrs · 36,906 cycles

SHIP 681 L-1 DOOR GRIT BAR FWD SPRING BINDING WITH SLIDER. CORRECTIVE ACITON: REMOVED AND REPLACED L-1 DOOR GIRT BAR IAW B757 AMM 25-66. (0934485)

Part: FRAME — CORRODED (BS 1160) · corrosion level 2 · airframe 81,630 hrs · 36,906 cycles

(AIRCRAFT 681, L/P 0929436) CABIN B.S. 1160 STRGR 17 LT. MAIN FRAME WEB HAS EXFOLIATED CORROSION - MARKED - DOT 064 - CP53-241-02I. CUT OUT DAMAGED SECTION OF FRAME, DIM 1.9" X .650" AND REPAIRED FRAME SECTION ALL IAW DELTA ER/A 574804-14 REV ORIGINAL.

Part: NONE — NONE · airframe 86,438 hrs · 38,932 cycles

SHIP 681 #6 SLAT T/E WEDGE DISBONDED ON UPPER AND LOWER SURFACE 62" FROM O/B EDGE AND 2" FROM T/E. CORRECTIVE ACTION: TYPE "A" WEDGE PER SB 757-57-0066, REMOVED DAMAGED SKIN 0.8" ON UPPER SKIN AND REMOVED DAMAGED SKIN 1.75" X 2.8" ON LOWER SKIN, BONDED REPAIR DOUBLERS ON UPPER AND LOWER SKIN IAW B757 SRM 57- 43-02 REPAIR 1 AND B757 SRM 51-70-10. (0927574)

Part: STRAP — BROKEN (BS 720) · airframe 81,630 hrs · 36,906 cycles

(AIRCRAFT 681, L/P 0928354) FWD. CARGO CEILING AREA RH SIDE OUTBD. OF SIDEWALL STANCHION STA. 720, CEILING STRAP BROKEN. CUTOUT DAMAGED SECTION ON FWD CARGO CEILING STRAP STA 720 DIM 2" X 1" IAW B757 SRM 53-00-51 FABRICATED AND INSTALLED REPAIR PARTS IAW B757 SRM 53-00-51 REP 12.

Part: SHEAR TIE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 81,630 hrs · 36,906 cycles

AFT BULK CARGO COMPARTMENT BS1600 FRAME SHEAR TIE CRACKED BETWEEN STRINGER 29L AND 28L I-42. REMOVED, FABRICATED, AND INSTALLED SHEAR TIE AFT CARGO COMP BS 1600, STRINGER 28L TO 29L IAW DWG AND SRM.

Part: FRAME — DAMAGED (BS 1320) · airframe 81,630 hrs · 36,906 cycles

SHIP 681 AFT CARGO FRAME DAMAGED S26R-S27R STA 1320. CORRECTIVE ACTION: REPAIRED AFT CARGO FRAME AT STA.1320 S26R-S27R IAW B757 SRM. (0921542)

Part: SKIN — DENTED (FUSELAGE) · airframe 81,630 hrs · 36,906 cycles

LOCATED DENT FUSELAGE SKIN STA 630, STR 16L. EVALUATED DENT AT STA 630 FUSELAGE SKIN STR 16L FOUND OUT OF LIMITS DUE TO PROXIMITY WITH STRINGER IAW SRM. REPAIRED FUSELAGE SKIN AT STA 630 STR 16L IAW ER/A 512671-14 AD REV A SECTION 3.

Part: STRINGER — DENTED (FUSELAGE) · airframe 81,630 hrs · 36,906 cycles

STRINGER 16L FOUND DENTED OUT OF LIMITS AT STA 630. REPAIRED STRINGER 16L AT STA 630 IAW ER/A 512671-14AD REV A.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 79,954 hrs · 36,161 cycles

ROW 19 D, E, & F EMERGENCY LIGHT COVER WAS MISSING. INSTALLED A NEW COVER. OK FOR SERVICE.

Part: FUEL LINE — LOOSE (APU) · airframe 79,864 hrs · 36,121 cycles

STRONG ODOR OF FUEL THROUGHOUT CABIN AND COCKPIT, AFTER SWITCHING FROM ENGINE BLEEDS TO APU BLEED DURING TAXI IN. DISCOVERED FUEL DRIPPING FROM THE APU. PERFORMED A NO GO ODI PREV. PROG. INSPECTION. FOUND APU FUEL SUPPLY LINE LOOSE AT THE FIREWALL IN APU BAY. SECURED THE LINE AND LEAK CHECKED GOOD.

Part: COVER — MISSING (CABIN DOOR) · airframe 79,747 hrs · 36,071 cycles

HANDLE COVER PLATE MISSING. AFT LEFT CABIN DOOR. INSTALLED HANDLE COVER PLATE ON AFT LEFT DOOR.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 78,726 hrs · 35,615 cycles

EXIT SIGN IN THE MID GALLEY AREA, A WIRE FOUND BINDING IN THE CEILING PANEL. WIRE DAMAGED. REPAIRED EXIT SIGN ASSY WIRE DAMAGE IAW SWPM 20-10-13.

Part: CREASE BEAM — CORRODED (BS 1425-1430) · airframe 75,887 hrs · 34,634 cycles

PASSENGER CABIN BS 1425-1430, RT CREASE BEAM WEB IS CORRODED. FOUND 100% MATERIAL LOSS IAW SRM 53-60-13 PG 103. REMOVED AND REPLACED THE WEB IAW SRM 51-40-02 (4) (B) AND DWG 146N5353 REV B.

Part: MOUNT — CORRODED (BS 333) · airframe 75,887 hrs · 34,634 cycles

FWD CABIN WET AREA LT SIDE AT BS 333 LBL 20 LAVATORY MOUNT HAS CORROSION. REPAIRED IAW DRAWING 27751SM007 REV. D.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 75,887 hrs · 34,634 cycles

AFT CARGO COMPARTMENT 2ND TO THE LAST TIE DOWN DOOR OPENING, HAS CORROSION, MARKED WITH A DOT. COMPLIED WITH PRI 553114-14 REVISION 0 AND ER/A 553114-14 REV ORIGINAL.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 75,887 hrs · 34,634 cycles

AFT CARGO DOOR OPENING, LOOKING AFT FROM OPEN DOOR, THIRD BOTTOM TIE DOWN IS MISSING IT'S COVER AND CORROSION HAS SET IN. COMPLIED WITH PRI 553114-14 REVISION 0 AND ER/A 553114-14 REV ORIGINAL.

Part: SUPPORT CHANNEL — CRACKED (RT MLG WW) · airframe 75,887 hrs · 34,634 cycles

RT MLG WHEEL WELL WING O BODY ATTACH FRAME AND MLG SURROUND STRUCTURE AT O/B FWD STOP FITTING UPPER FREE FLANGE IS CRACKED ALONG BEND RADIUS. REMOVED & REPLACED RT MLG WHEEL WELL SUPPORT CHANNEL IAW SRM 51-40-02 & DWG 149N7553 REV C.

Part: BEAM — DAMAGED (CARGO DOOR) · airframe 75,887 hrs · 34,634 cycles

INSPECTED AFT CARGO DOOR LOWER AFT CORNER. ADDITIONAL EDGE DAMAGE WAS FOUND BEYOND ALLOWABLE LIMITS OF SRM 52-30-01. INSTALLED REPAIR DOUBLER IAW SRM 52-30-01 REPAIR4. CATEGORY B REPAIR ADDITIONAL INSPECTIONS REQUIRED AT 37,500 FLIGHT CYCLES. CHANGED LRU FROM A/C TO AFT CARGO DOOR FTN 4GN2BC.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 75,887 hrs · 34,634 cycles

DURING NDT INSPECTION OF EXISTING REPAIR DOUBLER ON THE AFT CARGO DOOR FWD LWR CORNER A CRACK INDICATION WAS FOUND. LFEC IAW NDT PT6 53-00-06 INDICATION NOTED AT FWD LOWER CORNER. REMOVED EXISTING REPAIR DOUBLER, REAMED DISCREPANT HOLE TO .246 TO REMOVE CRACK. ACCOMPLISHED NDT INSPECTION, NO CRACKS NOTED. LOCATED DRILLED AND FABRICATED NEW REPAIR DOUBLER AND INSTALLED IAW B757-200 SRM 52-30-01 RPR 4. CATEGORY B REPAIR ADDITIONAL

Part: FLOOR SUPPORT — CRACKED (BS 760-780) · airframe 75,887 hrs · 34,634 cycles

FLOOR SUPPORT BETWEEN BS 760 AND 780, LBL 24 WAS FOUND CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM AND DWG 143N5140, REV D.

Part: SUPPORT BRACKET — CRACKED (LT PYLON) · airframe 75,887 hrs · 34,634 cycles

LEFT PYLON TOP INBD SIDE, FAIRING SUPPORT BRACKET INBD OF ACCESS DOOR 432BT IS CRACKED. REMOVED AND REPLACED THE FAIRING SUPPORT BRACKET IAW SRM 51-40-02 AND DRAWING 313N3100 REV D.

Part: WIRE — SHORTED (LAVATORY DOOR) · airframe 75,221 hrs · 34,224 cycles

DURING BOARDING, THE MID LAV DOOR SWITCH SHORTED CAUSING SMOKE TO BE OBSERVED DURING BOARDING. CAPPED AND STOWED WIRES PER ER/A 551323-14. REMOVED AND REPLACED THE MID LAV DOOR SWITCH PER SWP MANUAL 20-30 (REFERENCE: LOGPAGE 8673683). (2016-00596).

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,180 hrs · 34,196 cycles

FOUND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. TROUBLESHOT IAW WDM 3351. R & R THE FUSE IN POWER SUPPLY M730, R & R 1 FUSE IN POWER SUPPLY M10568, AND R & R THE FUSE IN POWER SUPPLY M737 IAW SWPM 20. CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 73,130 hrs · 33,356 cycles

DURING SERVICE CHECK FOUND SEVERAL EMERGENCY LIGHTS IN CABIN INOPERATIVE. RELAMPED & REPAIRED WIRING AS REQUIRED IAW SWPM 20-64-17. OPS CHECK GOOD, OK FOR SERVICE.

Part: CONNECTOR — MISINSTALLED (EMERGENCY LIGHTS) · airframe 73,105 hrs · 33,342 cycles

EMERGENCY EXIT CEILING LIGHT IN BETWEEN DOOR 4L AND DOOR 4R PAILS. IAW WDM 33-51-15 FOUND CONNECTORS CROSSED AT M736 AND M737, CORRECTED AND SECURED LIGHT ILLUMUNATES PROPERLY.

Part: SKIN — DAMAGED (BS 1120) · airframe 73,083 hrs · 33,332 cycles

LIGHTNING STRIKE AT BS 1120 5" BELOW STR 5R. DRILLED OUT DAMAGE AREA CONTAINED ON SKIN WITHIN ALLOWABLE DAMAGE LIMITS. SRM 53-10-01, SKIN ID SRM 53-00-01, SEC II. INSTALLED BLIND RIVET. RIVET MUST BE INSPECTED AT OR BEFORE 500 CYCLES. RIVET MUST BE REPLACED BEFORE 1000 FLIGHT CYCLES OR 24 MONTHS. REAPPLIED FINISH. GAINED ACCESS TO AREA. REMOVED BLIND FASTENER SRM 53-00 -01. PERFORMED OPEN HOLE EDDY CURRENT INSPECTION IAW SRM 53-00-01, REPAIR 6. NO CRACKS NOTED. OVERSIZED HOLE TREATED AREA AND INSTALLED SOLID FASTENER IAW SRM 53-00-01, REPAIR 6. RESTORED FINISH AND CLOSED ACCESS TERMINATING ACTION COMPLIED WITH, REQUEST TO CLOSE MONITOR.

Part: SKIN — DAMAGED (BS 983) · airframe 73,083 hrs · 33,332 cycles

LIGHTNING STRIKE AT BS 983 1" BELOW STR 4R. DRILLED OUT DAMAGE AREA CONTAINED ON SKIN WITHIN ALLOWABLE DAMAGE LIMITS. SRM 53-10-01, SKIN ID SRM 53-00-01, SEC II. INSTALLED BLIND RIVET. RIVET MUST BE INSPECTED AT OR BEFORE 500 CYCLES. RIVET MUST BE REPLACED BEFORE 1000 FLIGHT CYCLES OR 24 MONTHS. REAPPLIED FINISH. GAINED ACCESS TO AREA. REMOVED BLIND FASTENER IAW SRM 53-00 -01. PERFORMED OPEN HOLE EDDY CURRENT INSPECTION IAW SRM 53-00-01, REPAIR 6. NO CRACKS NOTED. OVERSIZED HOLE TREATED AREA AND INSTALLED SOLID FASTENER IAW SRM 53- 00-01, REPAIR 6. RESTORED FINISH AND CLOSED ACCESS. TERMINATING ACTION COMPLIED WITH, REQUEST TO CLOSE MONITOR. CLOSED LOG AND REMOVED MONITOR INSPECTION.

Part: SKIN — DAMAGED (BS 965) · airframe 73,076 hrs · 33,327 cycles

LIGHTNING STRIKE AT BS 965 1" BELOW, STR 4R. DRILLED OUT DAMAGE AREA CONTAINED ON SKIN WITHIN ALLOWABLE DAMAGE LIMITS. SRM 53-10-01, SKIN ID SRM 53-00-01, SEC II. INSTALLED BLIND RIVET. RIVET MUST BE INSPECTED AT OR BEFORE 500 CYCLES. RIVET MUST BE REPLACED BEFORE 1000 FLIGHT CYCLES OR 24 MONTHS. REAPPLIED FINISH.

Part: SKIN — DAMAGED (BS 1043) · airframe 73,076 hrs · 33,327 cycles

LIGHTINING STRIKE AT BS 1043 AT STR 5R. DRILLED OUT DAMAGE AREA CONTAINED ON SKIN WITHIN ALLOWABLE DAMAGE LIMITS. SRM 53-10-01, SKIN ID SRM 53-00-01, SEC II. INSTALLED BLIND RIVET. RIVET MUST BE INSPECTED AT OR BEFORE 500 CYCLES. RIVET MUST BE REPLACED BEFORE 1000 FLIGHT CYCLES OR 24 MONTHS. RE APPLIED FINISH. PERFORMED REPETATIVE INSPECTION IAW SRM 53-00-01 NO FURTHER DAMAGE NOTED. CONTINUE ON MONITOR.

Part: SKIN — DAMAGED (BS 629) · airframe 73,083 hrs · 33,332 cycles

LIGHTNING STRIKE AT BS 629 4" BELOW STR 7R. DAMAGE SEC I COND. 3. DRILLED OUT DAMAGE, DAMAGE CONTAINED ON SKIN WITHIN ALLOWABLE DAMAGE LIMIT SRM 53-10-01. SKIN ID SRM 53-00-01 SEC II. INSTALLED BLIND RIVET. RIVET MUST BE INSPECTED AT OR BEFORE 500 FLIGHT CYCLES. RIVET MUST BE REPLACED BEFORE 1000 FLIGHT FLIGHT CYCLES OR 24 MONTHS. REAPPLIED FINISH. GAINED ACCESS TO AREA. REMOVED BLIND FASTENER IAW SRM 53-00-01. PERFORMED OPEN HOLE EDDY CURRENT INSPECTION IAW SRM 53-00-01 REPAIR 6. NO CRACKS NOTED. OVERSIZED HOLE TREATED AREA AND INSTALLED SOLID FASTENER IAW SRM 53- 00-01 REPAIR 6. RESTORED FINISH AND CLOSED ACCESS TERMINATING ACTION COMPLIED WITH, REQUEST TO CLOSE MONITOR.

Part: SKIN — DAMAGED (BS 1070) · airframe 73,076 hrs · 33,327 cycles

LIGHTNING STRIKE AT BS 1070 2" ABOVE STR 5R. DRILLED OUT DAMAGE AREA CONTAINED ON SKIN WITHIN ALLOWABLE DAMAGE LIMITS. SRM 53-10-01, SKIN ID SRM 53-00-01, SEC II. INSTALLED BLIND RIVET. RIVET MUST BE INSPECTED AT OR BEFORE 500 CYCLES. RIVET MUST BE REPLACED BEFORE 1000 FLIGHT CYCLES OR 24 MONTHS. REAPPLIED FINISH. PERFORMED REPETATIVE INSPECTION IAW SRM 53-00-01 NO FURTHER DAMAGE NOTED. CONTINUE ON MONITOR.

Part: SKIN — DAMAGED (BS 600) · airframe 73,083 hrs · 33,332 cycles

LIGHTNING STRIKE AT STA 600 2" ABOVE STR 8R. DAMAGE SEC I COND. 3. DRILLED OUT DAMAGE, DAMAGE CONTAINED ON SKIN WITHIN ALLOWABLE DAMAGE LIMIT SRM 53-10-01. SKIN ID SRM 53-00-01 SEC II. INSTALLED BLIND RIVET. RIVET MUST BE INSPECTED AT OR BEFORE 500 FLIGHT CYCLES. RIVET MUST BE REPLACED BEFORE 1000 FLIGHT FLIGHT CYCLES OR 24 MONTHS. REAPPLIED FINISH. GAINED ACCESS TO AREA. REMOVED BLIND FASTENER IAW SRM 53-00 -01. PERFORMED OPEN HOLE EDDY CURRENT INSPECTION IAW SRM 53-00-01, REPAIR 6. NO CRACKS NOTED. OVERSIZED HOLE TREATED AREA AND INSTALLED SOLID FASTENER IAW SRM 53- 00-01 REPAIR 6. RESTORED FINISH AND CLOSED ACCESS TERMINATING ACTION COMPLIED WITH, REQUEST TO CLOSE MONITOR. CLOSED LOG AND REMOVED MONITOR INSP.

Part: SKIN — DAMAGED (BS 1098) · airframe 73,083 hrs · 33,332 cycles

LIGHTING STRIKE AT BS 1098 2: ABOVE STR 5R. DRILLED OUT DAMAGE AREA CONTAINED ON SKIN WITHIN ALLOWABLE DAMAGE LIMITS. SRM 53-10-01, SKIN ID SRM 53-00-01, SEC II. INSTALLED BLIND RIVET. RIVET MUST BE INSPECTED AT OR BEFORE 500 CYCLES. RIVET MUST BE REPLACED BEFORE 1000, FLIGHT CYCLES OR 24 MONTHS. REAPPLIED FINISH. GAINED ACCESS TO AREA. REMOVED BLIND FASTENER IAW SRM 53-00 -01. PERFORMED OPEN HOLE EDDY CURRENT INSPECTION IAW SRM 53-00-01, REPAIR 6. NO CRACKS NOTED. OVERSIZED HOLE TREATED AREA AND INSTALLED SOLID FASTENER IAW SRM 53- 00-01, REPAIR 6. RESTORED FINISH AND CLOSED ACCESS TERMINATING ACTION COMPLIED WITH, REQUEST TO CLOSE MONITOR. CLOSED LOG AND REMOVED MONITOR INSPECTION.

Part: SKIN — DAMAGED (BS 402) · airframe 72,225 hrs · 32,965 cycles

LIGHTNING STRIKE AT BS 402, 5" BELOW STR 11R. DRILLED DAMAGED RIVET AND INSTALLED BLIND FASTNER IAW R1 AND 539190-14. NEEDS REPEAT INSP AT 500 CYCLE INTERVALS AND SOLI FASTENER INSTALLED NO LATER THAN 3000 CYCLES/24 MONTHS. ERA 539314-14, SECT IV 1 TIME INSPECTION IS REQUIRED NTE 30S AFTER SECT I. C/W INSP IAW ERA 539314-14, SEC 2, REV ORIGINAL, NO FURTHER DEFECTS NOTED.

Part: BOLT — MISSING (L4 DOOR) · airframe 68,279 hrs · 31,219 cycles

L4 DOOR WILL NOT OPEN. FOUND BOLT MISSING FROM ROD FOR LOWER LATCH. FOUND LOCKNUT WITH INSUFFICIENT TENSION. INSTALLED BOLT WITH NEW LOCK NUT.

Part: SKIN — GOUGED (BS 1300-1320) · airframe 68,250 hrs · 31,211 cycles

FUSELAGE SKIN BS 1300-1320, S29-30R GOUGED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,298 hrs · 30,367 cycles

R1 DOOR & 1 LT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPS NORMAL.

Part: FAN — FAILED (RECIRCULATION) · airframe 65,590 hrs · 30,101 cycles

JUST PRIOR TO DESCENT, F/A REPORTED SMOKE ODOR IN REAR OF ACFT. RAN QRH ITEM TO NR 8 AND ODOR DISSIPATED. EQUIPMENT OVHT EICAS MESSAGE ON LANDING. FOUND RT RECIRCULATION FAN DAMAGED, BLADES BENT, BEARINGS GRINDING, AND SMELLED BURNED. REPLACED RT RECIRCULATION FAN AND FILTER. OPS CHECKED GOOD. NO ODOR IN CABIN.

Part: STRINGER — DENTED (BS 610-650 S15L) · airframe 64,559 hrs · 29,689 cycles

STRINGER DENTED, FUSELAGE BS 610-650, S15L. ACCOMPLISHED REPAIR IAW SRM 53-00-03. REPAIR 1, FIG 201.

Part: FLOORBEAM — CORRODED (BS 1660) · airframe 64,559 hrs · 29,689 cycles

MAIN CABIN FLOORBEAM UPPER TEE HAS CORROSION BS 1660, LBL 55. ACCOMPLISHED REPAIR IAW SRM 53-00-51, REPAIR 3, FIG 201, PAGE 203.

Part: SKIN — DENTED (BS 600 S28-29R) · airframe 64,559 hrs · 29,689 cycles

DENTED AREA ON FUSELAGE SKIN A BS 600, STR 28-29R. REPAIRED IAW SRM 53-00-01, FIR 201, REPAIR 9.

Part: FRAME — DENTED (BS 580 S23-24L) · airframe 64,559 hrs · 29,689 cycles

TWO DENTS ON UPPER FUSELAGE FLANGE OF FRAME AT BS 580 BETWEEN S23-24L & CTR OF PRODUCTION SPLICE. ACCOMPLISHED ERA 514337-1, REV ORIG.

Part: SKIN — CORRODED (BS 532-540) · airframe 64,559 hrs · 29,689 cycles

CORROSION & DENT ON FUSELAGE SKIN BS 532 TO 40 BETWEEN STR 27L & 28L. REPAIRED IAW ERA 51368-14, REV ORIG.

Part: FRAME — DENTED (BS 1480 S25-26L) · airframe 64,559 hrs · 29,689 cycles

SMALL DENT ON INNER FREE FLANGE OF FUSELAGE FRAME BS 1480 BETWEEN STR 25L & 26L. ACCOMPLISHED REPAIR IAW SMR 53-00-07, FOR 201, REPAIR 5.

Part: FRAME — DENTED (BS 640 S24R) · airframe 64,559 hrs · 29,689 cycles

DENT ON UPPER FLANGE OF FRAME AT BS 640 ABOVE S24R FWD CARGO. ACCOMPLISHED ERA 514336-4, ORIG.

Part: STRUCTURE — CORRODED (BS 1500-1520) · airframe 64,559 hrs · 29,689 cycles

AFT CARGO BAY BS 1500-1520 CORRODED. REPAIRED IAW SRM 53-00-03, FIG 201, REPAIR DETAIL III (53-00-03).

Part: DECK PLATE — CORRODED (BS 1680-1720) · airframe 64,559 hrs · 29,689 cycles

MAIN GALLEY FLOOR DECK PLATE HAS AREAS OF CORROSION FROM STA 1680-1720 BETWEEN LBL 55 TO RBL 55. R & R MAIN CABIN GALLEY DECK PLATE IAW SRM 53-60-51, PG 7.

Part: SKIN — DENTED (BS 580-600) · airframe 64,559 hrs · 29,689 cycles

DENT ON FUSELAGE SKIN BETWEEN FRAME BS 580 AND 600, S25-26L. REPAIRED IAW ERA 512670-14AD, REV ORG.

Part: ATTACH ANGLE — CORRODED (BS 1378) · airframe 64,559 hrs · 29,689 cycles

TIE DOWN ATTACH FITTING ANGLE FWD SIDE BS 1378 RT AFT CARGO CORRODED. REPLACED IAW SRM 51-40-02, PG 2-3, 6-7, 37-38 AND 43-44.

Part: TEAR STRAP — CORRODED (BS 1400 S28-29R) · airframe 64,559 hrs · 29,689 cycles

CORROSION ON TEAR STRAP AT STA 1400 BETWEEN STR 28 AND 29R IN AFT CARGO. REPLACED IAW SRM 51-40-02.

Part: FRAME — CORRODED (BS 900 LBL6) · airframe 64,559 hrs · 29,689 cycles

CORROSION ON WING TO BODY FRAME BS 900 LBL6. REPAIRED IAW SRM 51-70-12, PG 1, FIG 1.

Part: FRAME — GOUGED (BS 1520 S23-24R) · airframe 64,559 hrs · 29,689 cycles

GOUGES ON FUSELAGE FRAME AND SPLICE AT STA 1520 BETWEEN STR 23R AND 24R. ACCOMPLISHED REPAIR AT FRAME STA 1520 IAW SRM 53-00-02, REPAIR 5.

Part: SKIN — DAMAGED (BS 720-740) · airframe 64,559 hrs · 29,689 cycles

DURING REMOVAL OF INTERCOASTAL FROM BS 720-740 RBL 10.45 IN FWD CARGO, FOUND NINE OVERSIZED ELONGATED HOLES AND ONE DENT AT BS 720 IN FUSELAGE SKIN. REPAIRED IAW ERA 513916-14, REV ORIG.

Part: CREASE BEAM — CORRODED (BS 780-879) · airframe 64,559 hrs · 29,689 cycles

CORROSION ON MAIN CABIN LT CREASE BEAM FROM BS 780-879. R & R IAW SRM 51-40-05.

Part: CUSP WEB — CORRODED (BS 1013 LBL69) · airframe 64,559 hrs · 29,689 cycles

LEFT CUSP WEB BS 1013 1018, LBL 69 HAS UPPER SURFACE CORROSION. REPLACED CUSP WEB IAW SRM 51-40-02, PG 6.

Part: FRAME — GOUGED (BS 1640 S5-6L) · airframe 64,559 hrs · 29,689 cycles

MAIN CABIN FUSELAGE FRAME GOUGED BS 1640 BETWEEN STR 5 - 6L. ACCOMPLISHED REPAIR IAW ERA 513907-14, REV ORIG.

Part: FRAME — CORRODED (BS 729) · airframe 64,559 hrs · 29,689 cycles

CORROSION ON MAIN CABIN FRAME INBD FLANGE AT STA 729 LT 2 INCHES ABOVE FLOOR LEVEL. ACCOMPLISHED ERA 513915-14, REV ORIG.

Part: FRAME — GOUGED (BS 1640) · airframe 64,559 hrs · 29,689 cycles

MAIN CABIN FUSELAGE FRAME GOUGED AT BS 1640 S5 - 6R ACCOMPLISHED ERA 513908-14, REV ORIG.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 64,559 hrs · 29,689 cycles

MAIN CABIN BS 365, BL 0-RBL 36 FLOORBEAM UPPER TEE HAS CORROSION. REPAIRED IAW ERA 513906-14, REV ORIG.

Part: SILL — CORRODED (BS 1380-1440) · airframe 64,559 hrs · 29,689 cycles

AFT CARGO DOOR SILL LWR STRUCTURE BS 1380-1440 HAS CORROSION ON THE VERTICAL LEG. REPLACED IAW SRM 51-40-02, PG 2-3, 6-7, 37-38 AND 43-44.

Part: FRAME — CORRODED (BS 1400 S28L/R) · airframe 64,559 hrs · 29,689 cycles

AFT CARGO FRAME BS 1400 S28L-28R HAS CORROSION FWD AND AFT SIDE. REPLACED FRAME IAW SRM 51-40-02, PG 6 AND 7.

Part: STRINGER — CORRODED (BS 1500 S29L) · airframe 64,559 hrs · 29,689 cycles

AFT CARGO STRINGER 29L BS 1500-1520, HAS CORROSION. REPAIRED IAW SRM 53-00-03, FIG 201. REPAIR 1 DETAIL III(53-00-03).

Part: FRAME — CORRODED (BS 1460 S27L/R) · airframe 64,559 hrs · 29,689 cycles

AFT CARGO FRAME STA 1460, S27L-27R HAS CORROSION FWD, TOP AND AFT SIDE. REPLACED FRAME IAW SRM 51-40-02, PARA 4, PG 2-3 AT SAA ON NR CARD 100-258.

Part: CUSP WEB — CORRODED (BS 1400-1420) · airframe 64,559 hrs · 29,689 cycles

CORROSION ON MAIN RT CUSP WEB BETWEEN BS 1400-1420. REPLACED CUSP WEB IAW SRM 51-40-02, PG 2-5.

Part: FRAME — CORRODED (BS 1160 RBL 65) · airframe 64,559 hrs · 29,689 cycles

CABIN INTERNAL FS 1160 RBL 65 FRAME WEB FWD SIDE EXFOLIATED 2"-3" ABOVE CUSP WEB. REPLACED WEB IAW SRM 51-40-05 FIG 4, SHEET 5.

Part: SHEAR TIE — CORRODED (BS 1701 S28R) · airframe 64,559 hrs · 29,689 cycles

SHEAR TIE IS CORRODED AT AREA AFT OF BULKHEAD CARGO COMPARTMENT AT FRAME BS 1701 BETWEEN STRINGER 28R AND 29R. REPLACED SHEAR TIE IAW 51-40-02, PG 2.

Part: INTERCOSTAL — CORRODED (BS 1400) · airframe 64,559 hrs · 29,689 cycles

UPON REMOVAL OF MAIN CABIN CUSP WEB FOR CORROSION BETWEEN STA 1400 TO 1420 FOUND EXFOLIATION CORROSION ON INTERCOSTAL AT BS 1400 UNDER FWD END OF REMOVED CUSP WEB. R & R RT CUSP WEB ATTACH BRACKET, IAW SRM 51-40-02, PG 2-5.

Part: SHEAR TIE — CORRODED (BS 1701 S28L) · airframe 64,559 hrs · 29,689 cycles

SHEAR TIE CORRODED AT AREA AFT OF BULKHEAD CARGO COMPARTMENT AT FRAME BS 1701 BETWEEN STRINGER 28L AND 29L. REPLACED SHEAR TIE IAW 51-40-02 PG 2.

Part: TORQUE TUBE — CORRODED (RT WING TE FLAP) · airframe 64,559 hrs · 29,689 cycles

RT WING INBD FAIL SAFE TUBE HAS CORROSION INSIDE. R & R RT WING INBD MAIN FLAP INBD FAIL SAFE TORQUE TUBE REF EA 01-097891-14, REV A.

Part: INTERCOSTAL — CORRODED (BS 1360-1380) · airframe 64,559 hrs · 29,689 cycles

AFT CARGO INTERCOSTAL BENT AT CENTER AND GOUGED ON AFT END BETWEEN BS 1360-1380 BELOW S24R. REPLACED INTERCOSTAL IAW 51-40-02, PG 7,21.

Part: SKIN — DENTED (BS 600-620) · airframe 64,559 hrs · 29,689 cycles

DENT IN SKIN AT BS 600-620, STR 17L. ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE SKIN, BS 600-620, S17L IAW ERA 512671-14 AD REV ORIG.

Part: SKIN — DENTED (BS 1698 S14L) · airframe 64,559 hrs · 29,689 cycles

LT EXTERIOR FUSELAGE DENTED AT STA 1698 ABOVE LAP SPLICE S14L, REPAIRED IAW ERA 512679-14, REV ORG.

Part: LIGHT — INOPERATIVE (SEAT 25D) · airframe 59,922 hrs · 27,643 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY PATH LIGHT AT 25D INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 58,667 hrs · 27,096 cycles

DURING A LAYOVER CHECK, MX FOUND THE EMERGENCY PATHLIGHTS AT SEATS 23, 37, & 45 INOPERATIVE. MX REPAIRED THE WIRING. OPS CHECK WAS GOOD.

Part: FUSE — LEAKING (HYD SYSTEM) · airframe 55,807 hrs · 25,679 cycles

DURING TAXI OUT RT HYD QTY DROPPED TO 11 AFTER SHUTDOWN AT GATE QTY RETURNED TO 33 FOUND NORMAL ANTISKID MODULE IN LT WW WITH THE TOP HYD FUSE LEAKING REPLACED FUSE AND ASSOC PACKINGS SERVICED RT HYD SYS AS REQUIRED LEAK CKS GOOD.

Part: SKIN — DAMAGED (BS 520 S7-8L) · airframe 55,499 hrs · 25,468 cycles

LIGHTNING STRIKE AT FS 520 BETWEEN STR 7 AND 8L. REPAIRED REF ERA ON N/R 100-2.

Part: SWITCH — FAILED (AFT CARGO BAY) · airframe 55,207 hrs · 25,282 cycles

RAMP REPORTS AFT CARGO LIGHT SWITCH IS SMOKING. FOUND S429 AFT CARGO DOOR SWITCH ON FIRE. PULLED EXTERNAL POWER CORD. FIRE EXTINGUISHED. INSPECTED WIRING AND SURROUNDING AREA FOR DAMAGE. NONE NOTED PAST SWITCH. REPLACED S429 DOOR SWITCH ASSY AND TERMINALS AFT CARGO DOOR LIGHTS. OPERATED NORMAL. A/C OK FOR SERVICE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 54,872 hrs · 25,121 cycles

WHILE ACCOMPLISHING LAYOVER - FOUND A GOUGE ON FUSELAGE BELLY SKIN AT APPROX FS 1300-1320, S-29R TO S-30. GOUGE WAS OUT OF LIMITS AND REQUIRED TO BE CUT OUT AND REPAIRED.

Part: CLAMP — BROKEN (RT A/C PACK) · airframe 47,989 hrs · 22,034 cycles

AT FL340 WITH SINGLE PACK DISPATCH CABIN CONTINUED TO CLIMB TO 500FPM AND IN AUTO ONE. VALVE DID NOT SHOW FULLY CLOSED, 7 PSID CBN ALT 10000. MANUALLY CLOSED VLV IAW QUICK REF CKLIST, CBN REACHED 13000 FT. DESCENT AND RETURN TO CVG. FOUND CLAMP BROKEN ON RT PACK OUTPUT DUCT. REPLACED BOTH CLAMPS. PRESSURIZED ACFT. ALL CKS NORMAL.

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE SKIN BS 1400 BETWEEN S-30R AND S-29R SKIN DENTED. CUT OUT DENTED AREA, HFEC SKIN CUT OUT, NO CRACKS NOTED. FABRICATED AND INSTALLED REPAIR FILLER 3-3/4" BY 2-1/4" FROM 2024-T3 .071" AND DOUBLER 12-3/4" BY 5" FROM 2024-T3 .080" IAW DELTA ERA 458714-14 DATED 11-15-06 REV ORIG AND B757 SRM 51-20-01. REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE ONLY. ADDITIONAL ENGINEERING AUTHORIZATION, (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR LONGER THAN 12 MONTHS FROM FAA FORM 8100-9 APPROVAL DATE.

Part: SKIN — DENTED (FUSELAGE) · airframe 46,669 hrs · 21,463 cycles

DURING CURRENT HMV AT TIMCO LCQ, A DENT WAS NOTED ON THE BELLY SKIN AT FS 1398, FROM S-30 TO S-29R. THE DENT IS IN CLOSE PROXIMITY OF THE CIRCUMFERENTIAL BUTT SPLICE AT FS 1401. A BOEING APPROVED REPAIR WAS INSTALLED PER 458714-14.

Part: FRAME — DENTED (FUSELAGE)

DENT ON FRAME UPPER CAP ON AFT PIT BS 1400 BETWEEN S-25L TO S-26L. CUT OUT DENTED AREA, FABRICATED AND INSTALLED FRAME SUPPORT REPAIR 8.2" BY 2.4" FROM 2075-T6 .071" IAW B757 SRM 51-70-11, 51-20-01 AND 51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2

CORROSION (HEAVY) ON AFT PIT FRAME SHEAR TIE AT FS 1480 BETWEEN S-29L AND S-30. FABRICATED AND INSTALLED SHEAR TIE 4-3/4" BY 1" BY 3-1/2" FROM 7075-T6 .050" AT FS 1480 BETWEEN S-29L AND S-30 IAW BOEING DRAWING 140N2002 AND 51-20-01.

Part: FRAME — DENTED (FUSELAGE)

DENT ON FRAME UPPER CAP ON AFT PIT AT BS 1260 BETWEEN S-25R - 26R. FABRICATED AND INSTALLED DOUBLER 8" BY 7" BY 2-1/2" BY 1" FROM CALS 7075-T6 .080" IAW B757 SRM 51-40-02, 51-20-01 AND 51-70-01 FIG 2.

Part: SKIN — DENTED (BS 1430 S29-30R)

S/O NR 291026, N/R 21232 FUSELAGE SKIN BS 1430 BETWEEN S-30R AND S-29R SKIN HAS 2 EA. DENTS. FABRICATED AND INSTALLED REPAIR DOUBLER 13.5 X 12.5 FROM 2024-T3 .100 IAW SRM 53-00-01 FIG. 201 REPAIR 3, AS DIRECTED BY RFTS NR 60014. NOTE: THIS IS A CATEGORY B REPAIR IN ZONE A AND WILL REQUIRE REPEAT INSPECTION AT 58,963 TOTAL AIRCRAFT CYCLES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON MAIN CABIN FLOORBEAM UPPER CAP AT BS 377.7 THRU FASTENER HOLES (2 EA.) AT RBL 1 AND 5 (ON TOP SIDE). CUT OUT UPPER CAP AT BS 377.7. FABRICATED AND INSTALLED FLOORBEAM REPAIR 102.5" BY 7" FROM BAC1505-100617 IAW B757 SRM 53-10-51D, 51-40-05 AND 51-20-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON MAIN CABIN FLOORBEAM UPPER CAP AT BS 365 FROM BL 0 TO RBL 24. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED FLOORBEAM REPAIR 130-3/4" BY 36-1/4" FROM 7075T73 .125" "T", 7-1/2" BY 1" FROM 7075-T6 .090", 11" BY 3/4" BY 1-7/8" FROM 7075-T6 .050", 8-1/4" BY 1" AND 71" BY 2" BY 2" FROM 7075-T6 .063", AND 9" BY 1/2" FROM 7075-T6 .125" IAW B757 SRM 53-10-51D, 51-40-05 AND 51-20-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

HEAVY CORROSION ON MAIN CABIN FLOORBEAM UPPER CAP AT BS 720 LBL 4. FABRICATED AND INSTALLED FLOORBEAM REPAIR 12" BY 1.6" FROM BAC1505-100617, 9" BY .7" FROM 7075-T6 .125", 11.25" BY .9" FROM 7075-T6 .063", 11.25" BY .9" FROM 7075-T6 .090", AND 9" BY 1/2" FROM 7075-T6 .125" IAW B757 SRM 53-10-51D, 51-40-05 AND 51-20-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

HEAVY CORROSION ON MAIN CABIN FLOORBEAM UPPER CAP FWD EDGE OF FASTENER HOLE AT BS 740 LBL 4. FABRICATED AND INSTALLED REPAIR SECTION 12 FROM BAC1505-100617, REINFORCEMENT STRAPS 1 14-1/2 BY 7/8 FROM 7075-T6 .063 AND 1 14-1/2 BY 7/8 FROM 7075-T6 .090 AND RADIUS FILLER 15 IN LENGTH FROM 7075-T6 .125 IAW B757 SRM 53-00-51D, 51-40-02 AND 51-20-01.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2

HEAVY CORROSION ON EXTERIOR FUSELAGE SKIN AT AIRPHONE ANTENNAS MOUNT BETWEEN BS 1500 - BS 1520, S-28L - S-29L AND INSIDE DOUBLER. FABRICATED AND INSTALLED DOUBLER 11" BY 6.5" FROM 2024-T3 .050" AND FILLER 2.5" BY 1.8" FROM 2024-T3 .040" IAW B757 SRM 51-20-01, 53-00-01 AND DELTA ERA 458484-14 REV ORIGINAL DATED 10-31-2006.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON SHEAR DECK BS 1716 BL 0 TO LBL 42. FABRICATED AND INSTALLED REPAIR DOUBLER 8.8" BY 6.5" FROM 2024-T3 .063" IAW B757 SRM 53-60-51 FIG 203 REPAIR 2 ALT I.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 43,238 hrs · 20,235 cycles

NR 1 ENGINE COMPRESSOR STALL ON CLIMBOUT AT FL140. PULLED PWR BACK AND ENGINE INDS NORMAL. VISUALLY SAW SPARKS FROM TAILPIPE. DID NOT SHUT ENG DOWN. REPLACED ENGINE DUE TO INTERNAL DAMAGE.

Part: COALESCER BAG — CRACKED (LT A/C BAY) · airframe 42,378 hrs · 19,893 cycles

DURING CLIMBOUT NOTICED A/C WAS NOT COOLING OR PRESSURIZING. REPLACED BLOWN DUCT ON LEFT WATER SEPARATOR.

Part: WINDOW — FAILED (ROW 25 SEAT F) · airframe 41,675 hrs · 19,619 cycles

CABIN WINDOW AT ROW 25F OUTER PANE BROKE AWAY IN FLIGHT. REPLACED SAME.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 40,507 hrs · 19,177 cycles

ON CHECK FOUND EMERGENCY LIGHTS IN F/C AISLE INOP. REPAIRED BROKEN WIRE UNDER SEAT 1D AND REPLACED FUSE ON POWER SUPPLY. LIGHTS OP NORMAL.

Part: MEGAPHONE — CRACKED (CABIN) · airframe 32,952 hrs · 16,027 cycles

CRACKED PLASTIC AROUND MOUTHPIECE. REMOVED AND REPLACED MEGAPHONE.

Part: TERMINAL — BURNED (COCKPIT) · airframe 30,149 hrs · 14,672 cycles

A/C DIVERTED TO DEN WITH SMOKE IN COCKPIT. FOUND TERMINAL ON LEFT NR 1 WINDOW FOR WINDOW HEAT BURNT WHERE TERMINAL BLOCK IS BONDED TO WINDOW SURFACE AT LOWER LEFT CORNER OF WINDOW.

Part: TERMINAL — LOOSE (CONTROL PANEL) · airframe 27,274 hrs · 13,355 cycles

TURNED ON THE RUNWAY TURNOFF LIGHTS AND SAW HAZE UNDER EDGE OF CONTROL PANEL THEN TURNED LIGHTS OFF AND HAZE WENT AWAY. FOUND LOOSE TERMINAL ON LIGHT CONTROL PANEL. REPLACED PANEL.

Part: ROLLER — DRAGGING (TE FLAP)

LEADING EDGE SLAT DISAGREE MSG AND LEADING EDGE LIGHT WHEN FLAPS HANDLE MOVED TO 0 AFTER TAKEOFF. FLAP INDICATOR FROZE BETWEEN 0 AND 1 DEG. RECEIVED FLAP ISLN VAL STATUS MSG. PASSENGER (RETIRED DAL PILOT) REPORTED INBOARD SLATS REMAINED EXTENDED APPROX 5 IN. RETURNED TO DFW LANDING WITH TRAILING EDGE FLAPS 20. RAN BIT ON FSEU, FOUND LEFT INBOARD AND LEFT OUTBOARD TORQUE INDICATORS TRIPPED. RESET SAME, LUBED FLAP TRANSMISSION TORQUE BRALE AND AFT FLAP TRACK ROLLERS, BOTH SIDES OPERATED FLAPS FULL TRAVEL OPERATION NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND ON L/O, EXTERIOR MID OVERWING EMER LIGHT AND AFT OVERWING EMER LIGHT AND CENTER AISLE LIGHTS INOP. REPLACED BATTERY PACK AT M735, EMERGENCY LIGHTS CK GOOD.

Part: APU — FAILED (AFT FUSELAGE)

SMOKE IN COCKPIT/FOUND APU PUTTING OIL INTO DUCT. REPLACED APU.

Part: MEGAPHONE — DAMAGED (CABIN)

AFT MEGAPHONE INOP. REPLACED SAME, NOW OPN NORM.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ESCAPE PATH LIGHT INOP FROM MID GALLEY TO FWD GALLEY. REPLACED POWER SUPPLY.

Part: FAN — FAILED (CABIN)

ELECT SMELL AT MID GALLEY AREA AND SEAT ROW 20 TO 26. FOUND COOLING FAN BEARING FAILED.

Part: FIRE BOTTLE — EMPTY (CABIN)

DURING LAYOVER, FOUND FWD CABIN HALO FIRE BOTTLE EMPTY. REPLACED BOTTLE.

Part: COFFEE MAKER — ODOR (AFT GALLEY)

REPORTED BY FLIGHT ATTENDANT, AFT GALLEY NR 1 COFFEE MAKER HAS SLIGHT ELE SMELL. FWD TO MCO, THEN REPLACED COFFEE MAKER.