N750AT

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 93,367 hrs · 38,763 cycles

INSEAT EMERGENCY LIGHT INOPERATIVE, ROW 31 RT. FOUND CONNECTOR DISCONNECTED UNDER SEAT 31F, RECONNECTED, OPS OK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 91,048 hrs · 38,188 cycles

26D RED ESCAPE PATH LIGHT BULB INOPERATIVE, REF AMM 33-51-04, RESEAT UNDERSEAT CONNECTOR AND REPLACED SEAT LAMP ASSY. OPS CKS GOOD PLACARDS REMOVED, MCC NOTIFIED, ACFT OK FOR SERVICE.

Part: STIFFENER — CORRODED (BS 355) · corrosion level 2 · airframe 88,671 hrs · 37,569 cycles

CORROSION ON VERTICAL BEAM, BS 355 AT NLG CHORD LT NOSE TUNNEL AREA. REPAIRED IAW ERA 524339-14, REV ORG.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 86,837 hrs · 37,080 cycles

FWD CARGO DOORWAY FWD FRAME WEB, BS 560 AND OUTER ANGLE ARE CRACKED TWO INCHES ABOVE UPPER STOP FITTING. COMPLIED WITH ERA 524296-14AD, REV ORIGINAL.

Part: WIRE — CHAFED (EMERGENCY LIGHTS) · airframe 86,286 hrs · 36,939 cycles

FOUND SEAT EMERGENCY LIGHTS BETWEEN ROW 24 DEF AND 36 DEF INOPERATIVE, TROUBLESHOT IAW WDM 33-51-21. FOUND WIRING RUBBING ON SEAT FRAME, SEAT 30 DEF. REPAIRED WIRING, OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 85,411 hrs · 36,737 cycles

EMERGENCY LIGHTS ABOVE SEATS 30-45 RIGHT INOPERATIVE. FOUND FAULTY EMERGENCY LIGHT POWER SUPPLY BATTERY POST. REMOVED AND REPLACED POWER SUPPLY IAW AMM 33-51.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 85,450 hrs · 36,747 cycles

EMERGENCY LIGHT ABOVE SEAT 23 F,E,D IS INOPERATIVE. FOUND BAD FUSE AT M732 AND REPLACED, CHECKED GOOD IAW AMM 33-51.

Part: SKIN — DAMAGED (BS 640-900) · airframe 91,956 hrs · 38,433 cycles

FUSELAGE SKIN, S14R, BS 640-900;S-26L, BS 500-660; S-4R, BS 740, LAP JOINT AREAS. FOLLOW-ON ACTION IS REQUIRED, 23 MAY 15. C/W FUSELAGE INSPECTION IAW ARA 518966-14, REV A. NO ITEMS NOTED. SUPPLEMENT INSPECTION UNTIL LOG 1072025 AND ERA 478516-14 REH CAN BE UPDATED DUE TO ACFT REPAIRS OVER INSPECTION AREAS.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 84,286 hrs · 36,438 cycles

FOUND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY M731 AND BATTERY. FOUND DAMAGED WIRE AT ROW 4. REPAIRED WIRE IAW SWPM 20-10. ALSO FOUND WIRE RUN FROM SPLICE ZSP37 TO D9015 PIN 9 TOO SHORT. REPLACED WIRE, RUN EMERGENCY LIGHTS CKS GOOD. WORK IAW SWPM CH 20.

Part: CHARGER — ARCED (EMERGENCY LIGHTS) · airframe 84,204 hrs · 36,416 cycles

ACFT EMERGENCY PATH LIGHTS INOPERATIVE. FOUND WIRE DAMAGED BEHIND CONNECTOR OF BATTERY PACK ON EQUIPMENT NR M9011.793426. SPLICED WIRES COMING FROM C/P D9015 PINS 1. 7. 18 TO GROUND. THEN FOUND PINS ARCHING INTERNALLY OF C/P D9015. R & R C/P IAW SWPM CH 20. OPS CHECK GOOD. R & R POWER SUPPLY CHARGER AT M731 IAW AMM 33-51. OPS

Part: BATTERY — LOOSE (EMERGENCY LIGHTS) · airframe 83,866 hrs · 36,312 cycles

MX FOUND EMERGENCY LIGHTS AT SEAT 34-49 INOPERATIVE. MX RESECURED BATTERY PACK. OPERATION OF LIGHT CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 83,748 hrs · 36,275 cycles

RT AFT EMERGENCY LIGHTS INOPERATIVE SEAT 38F. R & R BATTERY IAW AMM 33-60. EMERGENCY LIGHTS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,769 hrs · 35,793 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHT AT ROW 45 INOPERATIVE. MX RELAMPED AND REPLACED FAULTY CHARGER AT M736. OPS OF LIGHT NOW CHECKED GOOD.

Part: CHARGER — WRONG PART (EMERGENCY LIGHTS) · airframe 80,705 hrs · 35,531 cycles

EMERGENCY LIGHT OVERHEAD AT ROW 36ABC INOP. REPLACED LIGHT ASSY NO HELP. RELAMPED NO HELP. NO VOLT TO LIGHT ASSY. REQUIRES FURTHER T/S. DEFER IAW MEL 33-51-01. INSTALLED, FOUND JUMPER FROM PINS 5 AND 6 BURNED PIN 1 AND 17 BURNED ON CONNECTOR D80 M737. REPLACED CONNECTOR AND PINS REPLACED BATT LIGHT STILL INOPERATIVE. BATTERY CHARGER SENT WAS WRONG BATTERY CHARGER PN RPS1-B DAL.

Part: FRAME — DAMAGED (BS 365) · airframe 77,037 hrs · 34,635 cycles

DURING HMV CHECK, FOUND DAMAGE FROM EXCESSIVE DRILL STARTS ON FRAME. REPAIRED IAW ERA 486833-14.

Part: FLOORBEAM — CORRODED (BS 385.25) · airframe 73,324 hrs · 33,705 cycles

DURING HMV CHECK, HEAVY CORROSION WAS FOUND AT MANY LOCATIONS OF THE BS 365.25 FLOORBEAM UPPER SURFACE. REPAIRED IAW ERA 486194-14

Part: SKIN — DAMAGED (BS 1896.2-1918.9) · airframe 73,324 hrs · 33,705 cycles

DURING "C" CHECK, THREE LIGHTING STRIKES ON OUTER SKIN AT FS 1896.2 TO 1918.9. REPAIRED IAW ERA 486860-14.

Part: DOUBLER — CORRODED (BS 1473 S29R) · airframe 73,324 hrs · 33,705 cycles

DURING THE MX CHECK, MX REPORTED CORROSION ON VHF ANTENNA MOUNT STRUCTURE AREA BETWEEN BS 1460 -1480, S26 -30R. AREA WAS CLEANED UP AND NO CORROSION WAS FOUND ON ANTENNA MOUNT STRUCTURE, JUST THE EXTERNAL DOUBLERS WERE FOUND CORRODED. REPAIR IAW ERA 486851-14.

Part: FLOORBEAM — DAMAGED (BS 580 RBL 24) · airframe 73,324 hrs · 33,705 cycles

DURING HMV, TOOLING DAMAGE WAS FOUND ON BS 580 FLOORBEAM LOCATED AT THE LOWER TEE FORWARD FLANGE. REPAIRED IAW ERA 486838-14.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 73,324 hrs · 33,705 cycles

CRACK ON CREASEBEAM INNER CHORD AT STA 410, RBL 53.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,324 hrs · 33,705 cycles

UPON REMOVAL OF FLOOR SUPPORT CHANNEL AT STA 717 LBL 19 WHILE WORKING N/R 182637 FOUND CORROSION AT MATING SURFACE OF HORIZ FLANGE LWR SURFACE EXISTING REPAIR ANGLE ON FLOORBEAM. REMOVED AND REPLACED REPAIR ANGLES AND FILLER REF SRM 53-00-51 REPAIR 5 PG 201 FIG 201. (DL75E103154)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,324 hrs · 33,705 cycles

SEAT TRACK FROM FSTA 1321-1540 RBL 24.75 HAS NUMEROUS AREAS WITH CORROSION BARE METAL AT BOTTOM SURFACES & NUMUROUS NICKS AT CROWN SURFACE. REMOVED SECTION OF SEAT TRACK AND SLICED IN NEW SECTION. (DL75E103179)

Part: FRAME — DENTED (BS 231) · airframe 73,324 hrs · 33,705 cycles

FWD E/E FRAME DENTED STA 231. REPAIRED IAW ERA 486859-14, REV O.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,324 hrs · 33,705 cycles

MAIN DECK HAVE WEB AND ANGLE CORRODED AT STA 994 S17R. FABBED ANGLES AND INSTALLED NEW ANGLES. (DL75E103178)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,324 hrs · 33,705 cycles

MAIN CABIN CUSP WEB CORRODED AT STA 961 S-17R. REMOVED CUSP WEB FABBED DOUBLER AND REPAIR WEB REF SRM 51-70-13 FIG 1 PG 2. (DL75E103156)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,324 hrs · 33,705 cycles

CORROSION ON MAIN CABIN FLOORBEAM AROUND 1 EA FASTENER HOLE AT STA 700 BL46L. REMOVED CORRSION FABBED TWO REPAIR ANGLES AND FILLER AND INSTALLED. (DL75E103180)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,324 hrs · 33,705 cycles

SEAT TRACK CORRODED BETWEEN STA 690-700 RBL 12. CUT AND SLICE NEW SECTION OF SEAT TRACK. (DL75E103177)

Part: FLOORBEAM — CORRODED (BS 377) · airframe 73,324 hrs · 33,705 cycles

CABIN FLOORBEAM, STA 377, CORROSION ON T CAP LBL 62 TO RBL 62. REPAIRED IAW ERA 486196-14, REV O.

Part: FLOORBEAM — DAMAGED (BS 640) · airframe 73,324 hrs · 33,705 cycles

FWD CARGO FLOORBEAM, STA 640, HAS HOLES DRILLED AND DOUBLE DRILLED. REPAIRED IAW ERA 486190-14, REV O.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,324 hrs · 33,705 cycles

FWD CARGO DOME NUT BROKEN STA 768 27L IN STRINGER. REMOVED NUT PLATE FOUND STRINGER CORRODED. REPLACED SECTION OF STRINGER REF SRM 53-00-03 REP 1. (DL75E103148)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,324 hrs · 33,705 cycles

CORROSION ON SEAT TRACK STA 377 BL-24R ON I/B FLANGE. REMOVED SECTION OF SEAT TRACK AND INSTALLED NEW SECTION REF 51-40-02 PAR 7C PG 4-5.

Part: FLOORBEAM — DAMAGED (BS 620) · airframe 73,324 hrs · 33,705 cycles

FWD CARGO FLOORBEAM TOOLING MARKS STA 620, RBL27. REPAIRED IAW ERA 486192-14, REV A.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,324 hrs · 33,705 cycles

AFT CARGO SHEAR TIE CORRODED STA 1260 BETWEEN STR 28 & 29R. REMOVED AND REPLACED NEW SHEAR TIE. (DL75E103181)

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,324 hrs · 33,705 cycles

AFT CARGO AIR FONE DOUBLER ASSY HAS CORROSION STA 1500-1520 BETWEEN STR 28&29R. REPAIRED IN ACCORDANCE WITH ERA 486842-14. (DL75E103152)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,324 hrs · 33,705 cycles

AFT CARGO STRINGER CORRODED STA 1507-1516 STR 29R. REMOVED DAMAGED SECTION OF STRINGER FABBED PARTS AND INSTALLED REF SRM 53-00-03 PG 201 REPAIR 1 FIG 201. (DL75E103146)

Part: DOUBLER — CORRODED (BS 1500-1520) · airframe 73,324 hrs · 33,705 cycles

AFT CARGO AIRFONE DOUBLER ASSY HAS CORROSION, SAT 1500-1520 S28- 29. REPAIRED IAW ERA 486842-14, REV A.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,324 hrs · 33,705 cycles

AFT CARGO STRINGER CORRODED, STA 1402. REMOVED DAMAGE, INSTALLED SPLICE REF STA 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,324 hrs · 33,705 cycles

AFT CARGO STRINGER CORRODED SAT 1480 S 26-27.M REPAIRED IAW ERA 487247-14, REV 0.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 73,324 hrs · 33,705 cycles

AFT CARGO DOOR SKIN CREASE LWR CTR AREA. INSTALLED REPAIR DOUBLER IAW SRM 52-30-01, REPAIR 4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,324 hrs · 33,705 cycles

LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT STA 278 AND 7 INCHES ABOVE FLIGHT COMPARTMENT DECK RIGHT SIDE. REPAIRED PER ERA 486835-14. (DL75E103150)

Part: SKIN — DENTED (BS 625 S16L) · airframe 73,324 hrs · 33,705 cycles

DENTS ON FUSELAGE, STA 625, S16L. REPAIRED IAW ERA 486845-14, REV 0.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 73,324 hrs · 33,705 cycles

APU COMPT FWD BULKHEAD PREVIOPUS REPAIR DOUBLER GOUGED FROM PSPRING LATCH CONTACT. REMOVED DOUBLER AND FABBED NEW DOUBLER FROM TITANIUM AND INSTALLED. (DL75E103147)

Part: SKIN — DAMAGED (BS 278) · airframe 73,324 hrs · 33,705 cycles

LIGHTENING STRIKE DAMAGE ON FUSELAGE, STA 278. REPAIRED IAW ERA 486835-14, REV O.

Part: SKIN — DENTED (STA 750 S15L) · airframe 73,324 hrs · 33,705 cycles

ACCOMPLISH PERM REPAIR IAW ERA 468118-14, REV A, CODE 6-53-31 ACTL LINE 2301 FUSE SKIN STA 750 AT S15L DENT. ERA 468118-14, REV A, ACCOMPLISHED DURING HMV AT SAA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,249 hrs · 33,682 cycles

DURING A LAYOVER CHECK, MX FOUND SEAT 43 EMERGENCY PATH LIGHT INOPERATIVE. RE-PINNED WIRE AND FOLLOWING OPS CHECK WAS GOOD.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 70,463 hrs · 32,972 cycles

TOOLING DAMAGE NOTED IN FWD FRAME LOWER CORNER WEB REPAIR IN C2 SECTION 2 OF ERA SECTION 1 PERMANENT REPAIR FOR SEAL RETAINER FASTENERS.

Part: SKIN — CORRODED (BS 468 S4L) · airframe 70,463 hrs · 32,972 cycles

CORROSION FOUND AT SKIN LAP SEAM STA 468 STR 4L APPROX 75 INCHES IN LENGTH ERA 479008-14 REV A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,463 hrs · 32,972 cycles

WHILE ACCOMPLISHING THE SCRIBE LINE INSPECTIONS CALLED FOR IN AD 2007-19-07 AND IN S/B 757-53A0092 MX FOUND MULTIPLE AREAS OF PITTING CORROSION ON THE LOWER SKIN ALONG MULTIPLE LAP JOINTS. REPAIRED IAW ERA 478516-14.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 70,136 hrs · 32,894 cycles

ON PUSHBACK AFTER TURNING OFF PACKS APU SHUTDOWN WITH FAULT LIGHT. RE-SET FAULT, TRIED AGAIN. START WAS NORMAL. BIT APU ECU. CLEARED REVERSE FLOW MESSAGE PER FIM. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 70,136 hrs · 32,894 cycles

AFTER PUSHBACK APU FAULTED AND SHUTDOWN. RESTART OK. BIT APU ECU. CLEARED REVERSE FLOW MESSAGE PER FIM 49-11-00. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: SKIN — CORRODED (FUSELAGE) · airframe 65,364 hrs · 31,470 cycles

FUSELAGE SKIN FOUND CORRODED AT STA 440 BELOW STR 28L. DAMAGE WAS CUT OUT, AREA WAS INSPECTED AND A REPAIR DOUBLER WAS INSTALLED.

Part: SKIN — BULGED (BS 440) · airframe 65,364 hrs · 31,470 cycles

FUSELAGE SKIN WAS FOUND TO BE BULGING OUT AFT OF THE FWD LAVATORY SERVICE PANEL AT THE BUTT JOINT AT FS 440. REPAIRED IAW ERA 468316-14.

Part: FSEU — FAULTED (TE FLAPS) · airframe 64,669 hrs · 31,192 cycles

TE FLAP DISAGREEMENT WHEN FLAPS SELECTED TO TWENTY ON FINAL APPROACH. TROUBLESHOT TRANSMISSION FOR OVERLOAD INDICATION. NO TRIPS NOTED. CHECKED TRANSMISSION FOR SERVICE CHECKED OK. FSEU HAD INTERMITTENT FAULT FLAP LD RELIEF. PERFORMED FLAP LD RELIEF PER FIM. ALL INDICATIONS NORMAL. CONTACTED MCC WITH FINDINGS. OK FOR SVC.

Part: LINK — GOUGED (NLG WW) · airframe 64,147 hrs · 30,987 cycles

NLG LOCK LINK GOUGED ON THE LT SIDE SURFACE. LOCALLY BLENDED SURFACE TO REMOVE GOUGE.

Part: CARBON SEAL — DAMAGED (NR 1 ENGINE) · airframe 63,979 hrs · 30,910 cycles

LEFT ENGINE OIL QTY WENT TO ZERO FOLLOWED BY OIL PRESS FLUX. AS CREW WAS FOLLOWING CHECKLIST LEFT ENGINE OIL PRESSURE INDICATION STARTED FLASHING RED CREW THEN SHUT ENGINE DOWN. THIS OCCURED AT CRUISE FLT. REMOVED AND REPLACED NR 1 ENGINE PRECOOLER CARBON SEAL AND OIL PUMP. RAN NR 1 ENGINE FOUND EXCESSIVE OIL LEAK IN TAILPIPE. REPLACED NR 1 ENGINE PER TRANS 6T103.

Part: PUMP — UNSERVICEABLE (NR 2 ENGINE) · airframe 60,488 hrs · 29,559 cycles

RIGHT ENGINE FAILED IN FLIGHT POST FLT STATUS MESSAGES R ENG SEC SEL R ENG OIL PRESS R ENG LOW N1. REF ITEM 7 FOR RT ENG EEC REPLACEMENT 707812. REPLACED NR 2 FUEL PUMP PER MM 664905, NEED LEAK OPN CK. REPLACED NR 2 FUEL CONTROL PER OPN 5034 STEPS 1-3 664905 RAN ENGINE AND LEAK CK OK. PERFORMED TEST PROCEDURE PER MM. ENGINE ACHIEVED T/O POWER.

Part: COFFEEMAKER — BURNED (AFT GALLEY) · airframe 60,068 hrs · 29,399 cycles

ELECTRICAL FUMES REAR GALLEY AREA. PULLED ALL REAR GALLEY C/B`S, FUMES LESS. SUSPECT REAR GALLEY CAPTS SIDE COFFEEMAKER. RAN BREW CYCLE ON BOTH AFT GALLEY COFFEEMAKERS, CAPTS SIDE SMELLED STRONGER. REPLACED COFFEEMAKER NR 2 AFT GALLEY. RERAN BREW CYCLES NO SMELL IN AFT GALLEY.

Part: TERMINAL — CORRODED (EXTERIOR) · airframe 59,840 hrs · 29,313 cycles

FOUND DURING SVC CK L-2 DOOR EXTERIOR EMERGENCY LIGHT INOP. FOUND CORROSION CAUSING HIGH RESISTANCE TO GROUND. CLEANED RECEPTACLE AND TERMINALS. OPS CHECKED GOOD.

Part: EXTINGUISHER — DISCHARGED (CARGO BAY) · airframe 59,839 hrs · 29,312 cycles

NR 2 CARGO FIRE BOTTLE FIRED. REMOVED NR 2 FIRE BOTTLE PER MM 481754, INSTALLED NR 2 FIRE BOTTLE AND REPLACED CARGO FIRE CONTROL PANEL PER AMM. MCO A PLAC REMOVED.

Part: CONTROL UNIT — UNSERVICEABLE (CABIN PRESSURE) · airframe 58,070 hrs · 28,741 cycles

AIR TURNBACK DUE TO UNABLE TO MAINTAIN CABIN PRESS. REPLACED PRIMARY EQUIPMENT COOLING CONTROL CARD.

Part: CONTROL CABLE — WORN (LEFT OVERIDE) · airframe 54,559 hrs · 27,486 cycles

HMV-3 VISIT IN DFW. CABLE WORN, AILERON CABLE WORN AT LEFT WING OVERRIDE QUADRANT. CABLE FOUND TO BE IN POSITION A1B-4 AND PN BACC2C4AD06518FG. REPLACED CABLE PER OPN 2000 AND INSTALLED RECOMMENDED OPTIONAL CABLE PN BACC2C4CD06518FG ON RC 1388-1392 WITH RII INSPECTION CW.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,058 hrs · 27,294 cycles

FUSELAGE, SKIN L1 DOOR CUTOUT, UPPER FWD CORNER REPAIR OF CRACK FATIGUE CRACK FOUND DURING INSPECTION OF THE L1 DOOR CUTOUT. ERA WAS GENERATED INSTALLING A REPAIR DOUBLER, TRIPLER AND QUADRUPLER TO REPAIR THE DAMAGE. ERA 097855-14AD REVISION ORIGINAL

Part: TIRE — SEPARATED (MLG) · airframe 53,207 hrs · 26,998 cycles

NR 4 AND NR 8 MAIN TIRES BLOWN/DEFLATED CONFIRMED BY GROUND PERSONNEL ON TAKEOFF AT LGA. NR 8 TIRE LOST CAP, NR 4 TIRE FLAT. REPLACED ALL 4 WHEEL ASSYS ON RIGHT TRUCK. ALSO REPLACED NR 8 BRAKE LINE AND NR 4 AND 8 BRAKE ASSYS DAMAGED BY TIRE CAP. REPLACED NR 7 SPOILER PANEL DUE TO DAMAGE.

Part: CONNECTOR — NOT SEATED (PRESSURE SWITCH) · airframe 47,051 hrs · 24,446 cycles

LEFT HYD ELECT PUMP EICAS MSG CAME ON AND PRESS LIGHT IN THE LEFT HYD PUMP SWITCH ILLUMINATED. FOUND PUMP OPN NORMAL. RESEATED PRESSURE SWITCH PLUG. PUMP, LIGHT, AND MSG ALL CHECK OK. REPLACED OVERHEAD HYD CONTROL PANEL AND LEFT SYS HYD ELECT PUMP LOW PRESSURE SWITCH AS PRECAUTION. ALL CHECKS OK.

Part: FSEU — MALFUNCTIONED (FLAP/SLAT SYS) · airframe 46,248 hrs · 24,115 cycles

IN CRUISE RECEIVED EICAS MSG LEADING EDGE SLAT ASYMMETRY WITH LEADING EDGE INDICATOR LIGHT. FLAPS INDICATED BETWEEN UP AND 1 POSITION. HANDLE WAS IN UP OR 0 POSITION. VISUAL CHECK CONFIRMED LEADING EDGE SLATS IN UP POSITION. CYCLED FLAPS AND SLATS AFTER CLEARING FSEU NR 1. FAULTING SLAT HANDLE OUT OF DETENT, ALL MESSAGES CLEARED. FSEU NR 1 REPLACED PRECAUTIONARY. GOOD FOR SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,239 hrs · 24,111 cycles

THE UPPER CAP OF THE FS 1681 PASSENGER FLOORBEAM WAS FOUND CORRODED IN SEVERAL AREAS. THE ENTIRE CAP WAS CUT OFF TO REMOVE ALL CORROSION. A NEW CAP WAS FABRICATED AND INSTALLED IN PLACE OF THE REMOVED CAP PER ER/A 381633-14, REV A.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 46,239 hrs · 24,111 cycles

THE FWD FRAME OF THE C2 DOOR OPENING AT FS 1380 WAS FOUND WITH CORROSION ON THE OUTER FRAME CAP NEAR STRINGER 27R. THE CHORD WAS CUT JUST ABOVE THE DAMAGE AND THE LOWER SECTION REMOVED. A NEW SECTION OF CHORD WAS FABRICATED AND SPLICED IN WITH REPAIR ANGLES. THE REPAIR WAS ACCOMPLISHED PER ER/A 381629-14, REV A.

Part: SKIN — DENTED (FS 690, S-24R) · airframe 46,239 hrs · 24,111 cycles

FUSELAGE / SKIN / FS 690 / STRG. 24R-25R : SKIN CUTOUT REPAIR AN EXISTING SKIN REPAIR DOUBLER WAS DAMAGED AND REMOVED. THE UNDERLYING SKIN WAS CLEANED UP WITH A 8" X 4" CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 381721-14, REV A.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 46,239 hrs · 24,111 cycles

THE LOWER SILL BEAM OF THE C2 DOOR OPENING WAS BADLY CORRODED AND REQUIRED REPLACEMENT. TO REMOVE AND INSTALL A NEW SECTION, THE OUTER CHORD OF THE FS 1440 OPENING FRAME WAS CUT AT STRINGER 26R AND THE WEB CUT AT STRINGER 23R. THE LOWER SECTIONS WERE REMOVED AND RE-INSTALLED AFTER THE SILL REPLACEMENT. THE WEB WAS SPLICED PER SRM AND THE CHORD WITH ALUMINUM ANGLES PER ER/A 381623-14, REV A.

Part: SKIN — DENTED (FS 278, WL 208) · airframe 46,239 hrs · 24,111 cycles

FUSELAGE / SKIN / FS 278 / WL 208 : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED NEAR FS 278 AT WL 208. THE DENT WAS REMOVED WITH A 5" X 4" CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PERER/A 381653-14.

Part: BULKHEAD — GOUGED (FS 1720, BL 0) · airframe 45,646 hrs · 23,906 cycles

FUSELAGE / SKIN & BULKHEAD / FS 1700-1780 / STRG. 26L-26R : GROUND DAMAGE REPAIR THE FUSELAGE SKIN FWD AND AFT OF THE FS 1720 BULKHEAD WAS GOUGED AND PUNCTURED FROM A TAIL STRIKE DURING LANDING. THEBULKHEAD WEB WAS SLIGHTLY BUCKLED AND THE LOWER CHORDS GOUGED. THE DAMAGE TO THE SKIN AND WEB WAS CUTOUT AND REPAIRED WITH ALUMINUM DOUBLERS. THE DAMAGE TO THE CHORD WAS REPAIRED WITH A STEEL STRAP. THE REPAIRS ARE INTERIM UNTIL PART REPLACEMENT AT HMV PER ER/A 381027-14, REV A.

Part: WIRE — BROKEN (CABIN) · airframe 44,839 hrs · 23,591 cycles

EMERGENCY LIGHT INOP AT SEAT ROW 33DEF. REPAIRED BROKEN WIRE AT SEAT ROW 33DEF, EMERGENCY LIGHT OPS CK. GOOD

Part: PWR SUPPLY — INOPERATIVE (CABIN)

FWD CABIN FLOOR TRACK EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

CHS OPS CALLED TO REPORT A/C RTB DUE TO COMPRESSOR STALL AND NR 2 ENG FIRE REPORTED BY THE TOWER. PER FLT CREW, ON TAXI-OUT EXPERIENCED STALL AND TOWER REPORTED FIRE FROM THE BACK OF NR 2 ENGINE. NO EPCS MESSAGES, NO OVERTEMPS. CREW PUSHED THROTTLE UP A FEW MORE TIMES WITH SUBSEQUENT STALLS. FIRE BOTTLES NOT DISCHARGED. ATL MTC CHANGING NR 2 ENGINE.

Part: SLIDE — DEPLOYED (DOOR R-1)

R-1 DOOR SLIDE DEPLOYED AT GATE BY PERSONNEL.

Part: SLIDE — OUT OF POSITION (3R DOOR)

AFTER T/O, R AFT ENTRY DOOR LIGHT CAME ON. F/A TRIED TO GET HANDLE TO LOCK DOWN, NO LUCK. RETURNED TO ATL. FOUND 3R DOOR SLIDE SHIFTED OFF FWD SUPPORT. REPOSITIONED SLIDE, DOOR CLOSES NORM.

Part: SWITCH — INTERMITTENT (CABIN)

INFLIGHT, FLIGHT ATTENDANT AND PASSENGER REPORTED FUMES WHICH SMELLED LIKE SMOLDERING RUBBER IN THE AREA OF THE LAST THREE ROWS IN PASSENGER CABIN. STRONGER ON CO-PILOTS SIDE. FUMES WERE INTERMITTENT. MAINTENANCE CHECKED AREA, NO VISIBLE SIGNS OF FUMES. NO HOT AREAS LOCATED BEHIND PSU'S OR SIDEWALLS. FOUND 45F READING LIGHT FLICKERING. REPLACED READING LIGHT SWITCH. OPERATION CHECKS NORMAL.

Part: WIRE — SHORTED (L-1 DOOR)

ON SHORT FINAL, AN APPARENT STATIC DISCHARGE OCCURED BY THE L-1 DOOR. A SHOWER OF SPARKS CAME FROM THE WALK-AROUND O2 BOTTLE MOUNTED ON THE BULKHEAD. F/A-S ON JUMPSEAT WITNESSED LARGE DISPLAY OF SPARKS AS WELL AS PASSENGERS FIVE ROWS BACK. FOUND TERMINAL SPLICE TO 115V AC SERVICE OUTLET SHORTING. C/B POPPED PER NORMAL OPERATION. RESPLICED WIRE, RESET C/B AND OPERATION CKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

FIRST CLASS TRACK LIGHTING INOP. REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHK NML.

Part: CHARGER ASSY — INOPERATIVE (CABIN)

IND - EMERGENCY LIGHT IN BULLNOSE ABOVE 25ABC INOP. EMERGENCY LIGHT IN BULL NOSE ABOVE 27DEF INOP. REMOVED AND REPLACED BATTERY CHARGER AT FUSELAGE STATION 1243 LEFT, LIGHT OPS NORMAL.

Part: BLEED LINKAGE — WORN (LT ENGINE)

IND - LEFT ENGINE POWER FLUCTUATES AT 9 CONSTANT POWER SETTINGS. FL 27,000, OAT -29, MACH .80, N1 77.8 TO 78.3, EPR 1.03 TO 1.04 EGT 415 TO 418. PERFORMED FIM PROCEDURES PER FIM 73-21-00 FIG 107. FOUND 2.5 BLEED LINKAGE WORN TO .125 INCH ITEM PLACED ON MCI AEE 1400/375. (M)

Part: EGT SYS — MALFUNCTION (RT ENG)

ATL - FLT 400 - RT ENG EGT INCREASED TO 649 DEGREES CELSIUS FOR 2 SECONDS, ON TAKEOFF FROM HOWARD AFB, PANAMA. NO SURGE ASSOCIATED. NO OTHER PARAMETERS EXCEEDED, OAT PLUS 35. INSPECTED ENGINE PER MM 72-00-00 P615, NO DAMAGE NOTED. EICAS RT ENG 649 DEGREES CELSIUS AT, 07 SECONDS. ON 3/8/95 REMOVED AND REPLACED ENGINE RT POS.