N969TW

Part: LINE — NOT REPORTED (APU) · airframe 52,044 hrs · 26,158 cycles

AIRCRAFT WAS GROUNDED: STRONG, OILY/DIESEL LIKE ODOR IN COCKPIT SHORTLY AFTER TAKEOFF, AND DURING CLIMB OUT. ODOR DISSIPATED TO A FAINT TRACE AFTER APPROXIMATELY 10 MINUTES. FLIGHT ATTENDANTS REPORTED NO ODOR IN CABIN. MAINTENANCE REPLACED OIL LINE PER AMM 49-90-04 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 51,974 hrs · 26,111 cycles

RIGHT ENGINE HYDRAULIC PRESSURE WENT TO 0 WHEN PUMP WAS SWITCHED TO LOW. PRESSURE SHOWED 3000 WITH SWITCH ON HIGH. AN EMERGENCY WAS DECLARED, AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE RIGHT ENGINE HYDRAULIC PUMP IAW AMM 29-10-05, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: LANYARD — MISSING (DOOR SLIDE) · airframe 51,763 hrs · 25,976 cycles

AFT GALLEY DOOR SLIDE LANYARD CAME OFF. REPLACED THE SLIDE IAW AMM 25-62-00.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 51,693 hrs · 25,929 cycles

AIRCRAFT WAS NOT GROUNDED. PLEASE INSPECT SLIDE AT R1 DOOR FOR PROPER INSTALLATION. INSTALLED R1 DOOR EVACUATION SLIDE PER 25-94-20.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 51,433 hrs · 25,763 cycles

AIRCRAFT WAS NOT GROUNDED. CATERING OPENED R1 DOOR AND SLIDE PACK CAME OUT OF DOOR AND FELL ONTO THE RAMP, IT DID NOT DEPLOY. REPLACED R1 DOOR SLIDE PER MCM CARD 25-94-20 AND AMM 25-62-00.

Part: COVER — LOOSE (R1 DOOR SLIDE) · airframe 51,395 hrs · 25,736 cycles

R1 DOOR SLIDE COVER WAS LOOSE. SECURED THE SLIDE COVER IAW AMM 25-62-00. OK FOR SERVICE.

Part: CONNECTOR — MISSING (EMERGENCY LIGHT) · airframe 51,285 hrs · 25,667 cycles

STAIRWAY LEFT SIDE EMERGENCY LIGHT CONNECTOR MISSING. MAINTNENANCE REPLACED THE CONNECTOR AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER CHAPTER 20-31-01. THE AIRCRAFT WAS GROUNDED

Part: GIRT BAR — UNSECURE (R1 DOOR) · airframe 51,148 hrs · 25,588 cycles

DURING PREFLIGHT, FOUND THE R1 DOOR GIRT BAR HANGING OUTSIDE AIRCRAFT WITH THE DOOR CLOSED. SECURED THE GIRT BAR STRAP ANGLE AND REINSTALLED THE GIRT BAR IN STOWED POSITION IAW AMM 25-62-00. NO FURTHER DISCREPENCIES NOTED. AIRCRAFT OK FOR SERVICE.

Part: SLIDE — LOOSE (GALLEY DOOR) · airframe 51,148 hrs · 25,588 cycles

FORWARD GALLEY DOOR EVACUATION SLIDE DOOR WAS LOOSE AND THE GIRT BAR HOLDER LOOSE. ADJUSTED AND SECURED BOTH THE EVACUATION SLIDE DOOR AND THE GIRT BAR HOLDER IAW AMM 25-62-00. AIRCRAFT OK FOR SERVICE.

Part: HINGE FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 50,763 hrs · 25,349 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MOUNTING HOLES OF LEFT OUTBOARD FLAP CENTER FORWARD HINGE FITTING. REPLACED HINGE FITTING PER AMM 57-40-01.

Part: HINGE FITTING — CORRODED (TE FLAP) · airframe 50,763 hrs · 25,349 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION AT MOUNTING HOLES OF RIGHT WING OUTBOARD FLAP CENTER FORWARD HINGE FITTING. REPLACED HINGE FITTING PER AMM 57-40-01-201.

Part: STRAP — CRACKED (FUSELAGE) · airframe 50,763 hrs · 25,349 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. CANT 1463 FRAME STRAP IS CRACKED JUST INBOARD OF L2R. REPLACED DOUBLER PER SRM 53-01-00 FIGURE 2 AND EA 280632.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,763 hrs · 25,349 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED FUSELAGE SKIN AT CANT STATION 1437, LONGERON 2 RIGHT TO LONGERON 4 RIGHT. REPAIRED FUSELAGE SKIN PER SRM 53-04-00-001 FIGURE 27 AND EA 280672.

Part: WIRE — CUT (EMERGENCY LIGHT) · airframe 49,937 hrs · 24,812 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 27 DEF. FOUND WIRES CUT IN HALF AT THE SIDEWALL. SPLICED THE WIRES IAW CHP 20S 20-10-03. TESTED SEAT 27 EMERGENCY LIGHT IAW AMM 33-53-00. TESTED GOOD.

Part: MECHANISM — LACK OF LUBE (RT MLG) · airframe 49,631 hrs · 24,605 cycles

THE AIRCRAFT WAS NOT GROUNDED. AFTER DEPARTING DFW, RT GEAR LIGHT ILLUMINATED AFTER GEAR UP. CYCLED GEAR PER QRH PROCEDURE AND LIGHT WENT OUT. INSPECTED AND LUBED PROXIMITY SENSOR UP LOCK MECHANISM PER AMM 32-60-05. OK FOR SERVICE.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 48,477 hrs · 23,867 cycles

LEFT AND RIGHT OVERWING FORWARD EMERGENCY EXIT SIGNS ARE INOPERATIVE. REMOVED AND REPLACED THE BATTERY ASSEMBLY B5-203 IAW AMM 33-53-00. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,173 hrs · 23,684 cycles

EMERGENCY EXIT LIGHT ABOVE OVERWING HATCH INOP. SEAT ROW 20D INOP. REMOVED AND REPLACED BATTERY PACK IAW 33-53-00. OP CKS OK. THE AIRCRAFT WAS NOT GROUNDED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,173 hrs · 23,684 cycles

EMERGENCY EXIT LIGHT ABOVE OVERWING HATCH VERY DIM. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-53-00. THE AIRCRAFT WAS NOT GROUNDED.

Part: GIRT BAR — DAMAGED (R1 DOOR SLIDE) · airframe 47,273 hrs · 23,114 cycles

R1 DOOR EVACUATION SLIDE GIRT BAR CLIP IS SPRUNG. REPOSITIONED GIRT BAR CLIP. OPERATIONAL CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,234 hrs · 23,087 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FUSELAGE SKIN IS CRACKED AT STATION 1380 AND L14L. REPAIRED SKIN IAW SRM 53-30-00-02.

Part: PORTABLE LIGHT — BROKEN (CABIN) · airframe 47,234 hrs · 23,087 cycles

PORTABLE EMERGENCY LIGHT ASSEMBLY IS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,234 hrs · 23,087 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. TAIL CONE VERTICAL EMERGENCY LIGHTS AND AFT CENTER CEILING EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERIES IN AFT LAVATORY OVERHEAD IAW AMM 33-53-00. SEE ALSO AALA20161128003.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,234 hrs · 23,087 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. RIGHT AND LEFT OVERWING EXIT UPPER FORWARD EMERGENCY LIGHTS ARE DIM. EMERGENCY BATTERY WILL NOT HOLD CHARGE. REMOVED AND REPLACED BATTERY IAW AMM AMM 33-53-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,234 hrs · 23,087 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. TAIL CONE VERTICAL EMERGENCY LIGHTS AND AFT CENTER CEILING EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERIES IN AFT LAVATORY OVERHEAD IAW AMM 33-53-00. SEE ALSO AALA20161128002.

Part: BATTERY — FAULTY (FLASHLIGHT) · airframe 46,858 hrs · 22,856 cycles

AFT STAIRWAY EMERGENCY FLASHLIGHT IS NOT BLINKING. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-60-00. OPS CHECKED NORMAL.

Part: BULKHEAD WEB — CRACKED (LT MLG WW) · airframe 46,291 hrs · 22,518 cycles

DAMAGE ON INNER ALUMINUM BULKHEAD, APPROXIMATELY 4" FORWARD OF THE LT SIDE GEAR TRUNNION. DAMAGE RESULTED IN A 2.75" BY 4" LOSS OF MATERIAL TO THE INNER ALUMINUM WEB AND A 0.090" DENT IN THE STEEL WEB. REPAIRED PER SRM 53-05-00-001, FIG 36 AND EA 261750. AIRCRAFT IN BASE MAINTENANCE.

Part: CONNECTOR — DIRTY (FUEL SYSTEM) · airframe 45,034 hrs · 21,718 cycles

AIRCRAFT WAS GNDE. AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE THE CTR FUEL TANK BOOST PUMP UFI CB POPPED. REMOVED CTR TANK BOOST PUMP CONNECTORS & CLEANED. REINSTALLED PLUGS. OPERATIONAL CHECK OK IAW WITH AMM 28-20-18.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 44,978 hrs · 21,682 cycles

CENTER TANK FUEL PRESS LOW LIGHT ILLUMINATED DURING CLIMB OUT. PERFORMED QRH PROCEDURE. 5500 LBS OF FUEL TRAPPED IN CTR TANK. THE FLIGHT DIVERTED WITHOUT FURTHER INCIDENT. NO EMER WAS DECLARED. THE ACFT WAS NOT GNDED, NO FAULTS WERE FOUND. CTR TANK FUEL BOOST PUMP WAS PLACED ON MEL DEFERRAL. NO FAULTS WERE FOUND, AS A PRECAUTION, REPLACED BOTH CTR TANK UFI`S & BOTH CTR TANK RAMS IAW AMM 28-20-28.

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 44,618 hrs · 21,470 cycles

CENTER FUEL PRESS LOW LIGHT ON PUMPS APPEAR NOT TO OPERATE. NO EMER WAS DECLARED. THE FLIGHT DIVERTED & LANDED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. ACCOMPLISHED FAULT ISOLATION PROCEDURE & RESET UFI IAW MM 28-20-28. PERFORMED UFI OPERATIONAL TEST IAW MM 28-20-28. TEST CHECKED GOOD. CTR FUEL PUMPS OPERATIONS CHECKED GOOD, NO FURTHER FAULTS NOTED.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 44,278 hrs · 21,252 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB CTR FUEL PRESS LOW WARNING ILLUMINATED. R & R FWD & AFT CTR TANK BOOST PUMPS, FFC REPAIR ORDER 5150405, IAW AMM 28-20-07. PERFORMED CTR FUEL PUMP LOW PRESSURE INDICATION IAW AMM 2841-00-501. CHECKED NORMAL. ACCOMPLISHED BITE CHECK OF UFI WITH NO FAULTS NOTED. EE ALSO AALA20150823001.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 44,278 hrs · 21,252 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB CTR FUEL PRESS LOW WARNING ILLUMINATED. R & R FWD & AFT CTR TANK BOOST PUMPS, FFC REPAIR ORDER 5150405 IAW AMM 28-20-07. PERFORMED CTR FUEL PUMP LOW PRESS INDICATION IAW AMM 2841-00-501. CHECKED NORMAL. ACCOMPLISHED BITE CHECK OF UFI WITH NO FAULTS NOTED. SEE ALSO AALA20150824009.

Part: PSEU — FAULTY (LANDING GEAR) · airframe 44,123 hrs · 21,162 cycles

EMERGENCY NOT DECLARED & LANDING UNEVENTFUL. UPON LOWERING GEAR HANDLE, THE WARNING HORN SOUNDED & ALL LIGHTS RED. AIRCRAFT WAS STOPPED ON THE RUNWAY WITH GEAR DOOR OPEN LIGHT ON. R & R THE PSEU IAW AMM 32-60-04. ALSO REMOVED DEBRIS FROM GEAR CONTROL LEVER & LUBRICATED LEVER. ACCOMPLISHED GEAR SWING WITH NO FAULTS NOTED IAW AMM 32-31-01 & 32-60-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,933 hrs · 21,061 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT AT STATION 1144 & LONGERON 26R IS CORRODED. R & R SUPPORT IAW SRM 51-30-01.

Part: RIB — CRACKED (RT WING) · airframe 43,933 hrs · 21,061 cycles

RIGHT WING NR 4 SLAT TRACK INBD SUPPORT RIB IS CRACKED. INSTALLED REPAIR DOUBLER IAW MCM 57-98-06 & EA 252037.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,933 hrs · 21,061 cycles

CRACKS AT FS 1474 RT CANT. INSTALLED DOUBLER REPAIR IAW SRM 53-01-00-001 FIG 2 SHEET 3.

Part: RIB — CRACKED (LT WING) · airframe 43,933 hrs · 21,061 cycles

LEFT WING NR 4 SLAT TRACK INBD SUPPORT RIB IS CRACKED. INSTALLED REPAIR DOUBLER IAW MCM 57-98-05 & EA 252037.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,933 hrs · 21,061 cycles

VISUAL INDICATION OF CRACK IN FUSELAGE SKIN AT FASTENER HOLE LOCATION STATION 1418, JUST OTBD OF LONGERON 2R. INSTALLED REPAIR DOUBLER IAW SRM 53-04-00 FIGURE 40 & EA 252259.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 43,933 hrs · 21,061 cycles

AFT CARGO LT TIE-DOWN TRACK HAS CORRODED FASTENER HOLES BETWEEN FS 1155 & 1212. R & R TIE-DOWN TRACK SECTION BETWEEN STATIONS 1108 & 1220 IAW SRM 51-30-01 & 51-30-05.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 43,933 hrs · 21,061 cycles

AFT CARGO RT TIE-DOWN TRACK IS CORRODED BETWEEN FS 1117 & 1155. R & R CARGO TIE-DOWN TRACK SECTION IAW SRM 51-30-05 & 51-30-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,933 hrs · 21,061 cycles

CRACK IN FUSELAGE SKIN AT NOSE GEAR RT STRUT DOOR HINGE CUT OUT. STOP DRILLED CRACK IAW SRM 53-05-00-001. INSTALLED DOUBLER IAW SRM 53-05-00-001.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,933 hrs · 21,061 cycles

AFT CARGO WEB AT DOOR WAY IS CORRODED BETWEEN FS 1145 & 1220. R & R WEB IAW SRM 51-30-05.

Part: BEAM — CORRODED (FUSELAGE) · airframe 43,933 hrs · 21,061 cycles

AFT CARGO COMPARTMENT HAS CORROSION ALONG DOOR THRESHOLD BETWEEN FS 1155 & 1212. ACCOMPLISHED DOUBLER REPAIR IAW AARD 53-10-00-3.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 43,933 hrs · 21,061 cycles

AFT CARGO COMPARTMENT RT TIE DOWN TRACK HAS CORRODED CLIP, NUT HOLES BETWEEN FS 1212 & 1250. R & R TRACK SECTION IAW SRM 51-30-01.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 43,933 hrs · 21,061 cycles

AFT CARGO COMPARTMENT LT TIE DOWN TRACK AT STRINGER 26L HAS CORRODED CLIP, NUT HOLES BETWEEN FS 1212 & 1322. R & R TRACK SECTION IAW SRM 51-30-01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,933 hrs · 21,061 cycles

CRACK IN FUSELAGE TO VERTICAL SKATE ANGLE LT SIDE AT STATION 1463. INSTALLED DOUBLER IAW AARD 53-10-00-2 & PRINT CDK2004.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,933 hrs · 21,061 cycles

CRACK IN FUSELAGE TO VERTICAL SKATE ANGLE RT SIDE AT STATION 1463. INSTALL DOUBLER IAW AARD 53-10-00-2 & PRINT CDK2004.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,933 hrs · 21,061 cycles

SEAT TRACK NR 6 LUGS & TABS CORRODED AT FS 759. INSTALLED PLUG IAW AARD 53-20-00-10.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,933 hrs · 21,061 cycles

RIGHT CUSP IS CORRODED AT SEAT TRACK 6 FASTENER ATTACH POINT AT FS 807. INSTALLED REPAIR DOUBLER AT STATION 807 IAW AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,933 hrs · 21,061 cycles

CRACK IN RT CUSP SHEET AT STATION 398. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,933 hrs · 21,061 cycles

LEFT CUSP IS CORRODED AT FS 490. INSTALLED REPAIR DOUBLER BETWEEN STATIONS 484 & 503 IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,933 hrs · 21,061 cycles

SEAT TRACK NR 3 CORRODED BETWEEN FS 566 & 568. INSTALLED REPAIR PLUG DDK 2704 & CHANNEL 7452952-7 IAW SRM 53-05-00-001 & AARD 53-20-00-10.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,933 hrs · 21,061 cycles

LEFT CUSP CRACKED BETWEEN FS 803 & 807. R & R CUSP AT STATION 788 - 807 IAW PRINT EDK3238, SRM 53-05-00 & AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 43,933 hrs · 21,061 cycles

LEFT CUSP CRACKED AT STATION 457. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,933 hrs · 21,061 cycles

SEAT TRACK NR 6 CORRODED FROM FS 256 - 370. R & R SEAT TRACK SECTION BETWEEN FS 210 - 588 IAW AMM 53-40-01-2.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,933 hrs · 21,061 cycles

CORROSION BOTTOM OF LT CUSP AT STATION 734. REPAIRED CUSP IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,933 hrs · 21,061 cycles

CORROSION BOTTOM OF LT CUSP AT STATION 638. REPAIRED CUSP IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,933 hrs · 21,061 cycles

CORROSION ON BOTTOM & TOP OF LT CUSP BETWEEN STATION 680 & 684. REPAIRED CUSP IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,933 hrs · 21,061 cycles

CORROSION BOTTOM OF LT CUSP AT STATION 695. REPAIRED CUSP IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,933 hrs · 21,061 cycles

NUMBER 1 SEAT TRACK CORRODED FROM STATIONS 1030 TO 1136. R & R SEAT TRACK SECTION FROM STATIONS 1030 TO 1136 IAW AARD 51-00-05-1, PRINT 5930566 & AMM 53-40-01-2.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,699 hrs · 20,936 cycles

CEILING EMER LIGHTS ABOVE ROWS 12 & 13 INOPERATIVE. R & R CABIN EMER LIGHT BATTERY PACK ABOVE SEAT 12 & 13 IAW AMM 33-53-00. PERFORMED OPERATION CHECK. SYS CHECKED NORMAL.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,235 hrs · 19,615 cycles

SHEAR TIE CRACKED AT STATION 1437 & LONGERON 3 RT. REPLACED SHEAR TIE IAW AARD 51-00-05-1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,235 hrs · 19,615 cycles

SHEAR TIE CRACKED AT STATION 1437 & LONGERON 3 LT. REPLACED SHEAR TIE IAW AARD 51-00-05-1.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 39,910 hrs · 18,948 cycles

LT NR 1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR LT NR 1 DOOR PORTABLE EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LENS — CRACKED (CABIN) · airframe 39,537 hrs · 18,743 cycles

RT HAND FORWARD SERVICE DOOR AFT EXIT MARKER LENS & BASE PLATE ARE CRACKED. REPLACED RT HAND FORWARD SERVICE DOOR AFT EXIT MARKER LIGHT ASSEMBLY.

Part: BULLET — OBSTRUCTED (LT ENGINE) · airframe 39,257 hrs · 18,582 cycles

DFW CREW REPORTED AFTER TAKEOFF DURING CLIMB OUT RPM VARIED ON LT ENGINE. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT ENGINE INLET BULLET THAT HAD DEBRIS. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY — NOT SEATED (CABIN) · airframe 38,754 hrs · 18,297 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 7 TO 11 INOPERATIVE. RESEATED THE BATTERIES IN THE CEILING LIGHT POWER SUPPLY. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 38,754 hrs · 18,297 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RESEATED THE BATTERIES IN THE CEILING LIGHT POWER SUPPLY.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 38,754 hrs · 18,297 cycles

LEFT AND RT FORWARD OVERWING DOOR UPPER EXIT SIGNS INOPERATIVE. RESEATED BATTERY PACK FOR THE OVERWING EXIT SIGNS. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 38,754 hrs · 18,297 cycles

LEFT AND RIGHT AFT OVERWING DOOR UPPER EXIT SIGNS INOPERATIVE. RESEATED BATTERY PACK FOR THE OVERWING EXIT SIGNS. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 37,688 hrs · 17,721 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 7 TO 11 INOPERATIVE. RESEATED FORWARD EMERGENCY LIGHT BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,688 hrs · 17,721 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 18 TO 21 INOPERATIVE. RESET MID EMERGENCY LIGHT BATTERY PACK. OPS CHECK NORMAL.

Part: CIRCUIT BREAKER — TRIPPED (FUEL SYSTEM) · airframe 37,077 hrs · 17,400 cycles

DFW - CREW REPORTED CENTER FUEL WON`T TRANSFER FUEL. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FORWARD CENTER FUEL BOOST PUMP CIRCUIT BREAKER H21 POPPED. CHECKED FUEL BOOST PUMP AND WIRING PER MM 28-20-07-1. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FAN — INOPERATIVE (CABIN) · airframe 35,090 hrs · 16,360 cycles

MCI - INFLIGHT STL-LAX. CREW REPORTED ODOR IN THE CABIN AND FLIGHT DECK. EMERGENCY DECLARED FLIGHT DIVERTED MCI LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RECIRCULATION FAN CIRCUIT BREAKER POPPED AND FAN INOPEATIVE. REPLACED RECIRCULATION FAN AND FILTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 34,873 hrs · 16,259 cycles

RIGHT AND CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES ARE INOPERATIVE. RESEAT AFT EMERGENCY LIGHT BATTERY. OPS CHECK NORMAL.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 34,873 hrs · 16,259 cycles

LEFT NUMBER 1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT NUMBER 1 DOOR PORTABLE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — MALFUNCTIONED (CABIN) · airframe 34,873 hrs · 16,259 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RESET MID EMERGENCY LIGHT BATTERY. OPS CHECKS NORMAL.

Part: BATTERY — MALFUNCTIONED (CABIN) · airframe 34,873 hrs · 16,259 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS ABOVE CATWALK ARE INOPERATIVE. RESET AFT EMERGENCY LIGHT BATTERY. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 34,299 hrs · 15,977 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 18 TO 21 INOPERATIVE. CLEANED AND RESEATED BATTERY AT ROW 20 DEF, CENTER. OPS CHECK NORMAL.

Part: SOCKET — BROKEN (CABIN) · airframe 34,299 hrs · 15,977 cycles

ESCAPE PATH LIGHT AT SEAT 29D INOPERATIVE. REPLACED SEAT EMERGENCY LIGHT SOCKET. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 33,217 hrs · 15,431 cycles

VERTICAL LEADING EDGE HAS ELONGATED HOLE. INSTALLED DOUBLER PER 55-30-00.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 33,217 hrs · 15,431 cycles

INBOARD RIVET HOLE NEXT TO LEFT LOWER RADOME ALIGNMENT PIN HAS CRACK. INSTALLED REPAIR PER AARD 53-10-00-19.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 33,217 hrs · 15,431 cycles

FLOORBEAM AT STATION 1309 HAS TOOLING DAMAGE AT UPPER FORWARD RADIUS AND AN ELONGATED HOLE FROM INTERCOSTAL REMOVAL (CENTER-LINE OF A/C). INSTALLED REPAIR DOUBLER PER EA MD80-017424.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 33,217 hrs · 15,431 cycles

FORWARD ENTRY DOOR AFT END OF NUMBER 1 BEAM CRACKED. STOP DRILLED AND DYE CHECKED CRACK. NO CRACK BEYOND STOP DRILL. INSTALLED DOUBLER, ANGLE AND CLIP PER ESO 80172.

Part: MEMBRANE — PUNCTURED (FUSELAGE) · airframe 33,217 hrs · 15,431 cycles

SUBFLOOR HAS A PUNCTURE AT STATION 129 RIGHT BUTTLINE 41. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (ENTRY DOOR) · airframe 33,217 hrs · 15,431 cycles

DENT AT LOWER LEFT CORNER OF FORWARD ENTRY DOOR. INSTALLED REPAIR DOUBLER ON LOWER EDGE OF OUTER DOOR SKIN PER AARD 52-10-00-2.

Part: SKIN — DAMAGED (ENTRY DOOR) · airframe 33,217 hrs · 15,431 cycles

FORWARD ENTRY DOOR OUTER SKIN BY HOLD OPEN HOOK DAMAGED. INSTALLED REPAIR DOUBLER PER SRM 52-05-00 AND HOLD OPEN HOOK HOUSING PER ESO 80172.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 33,217 hrs · 15,431 cycles

FORWARD ENTRY DOOR 1546 FORWARD AND AFT ENDS OF NUMBER 1 BEAM CRACKED. STOP DRILLED AND DYE CHECKED CRACKS AT FORWARD AND AFT ENDS OF NUMBER 1 BEAM NO CRACKS BEYOND STOP DRILL. INSTALLED DOUBLERS PER ESO 80172.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,217 hrs · 15,431 cycles

SKIN CRACKED PAST STOP DRILL AT AFT LEFT NOSE LANDING GEAR DOOR AFT HINGE. INSTALLED DOUBLER REPAIR PER EA AND SRM 53-05-00 FIGURE 62.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,217 hrs · 15,431 cycles

LEFT CUSP STATION 1174 HAS CORROSION ON THE UNDERSIDE GOING AROUND THE FRAME FOOT AND H FITTING. INSTALLED LEFT CUSP SHEET REPLACEMENT SECTION STATIONS 1174 TO 1193 PER BOEING DRAWING SG09530019.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,217 hrs · 15,431 cycles

AFT CARGO INTERCOSTAL CRACKED ON CENTERLINE BETWEEN FLOORBEAMS STATION 1287 TO 1309. INSTALLED NEW INTERCOSTAL PER AARD 51-10-00-5.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 33,217 hrs · 15,431 cycles

HOLE IN LEFT SUB FLOOR STATION 198 LEFT BUTTLINE 44 BELOW NUMBER 2 SEAT TRACK. INSTALLED REPAIR DOUBLER AS PER AARD 53-20-00-16 PART 6.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 33,217 hrs · 15,431 cycles

FORWARD ENTRY DOOR DOOR FORWARD END OF NUMBER 1 BEAM CRACKED. STOP DRILLED AND DYE CHECKED CRACK. NO CRACK BEYOND STOP DRILL. INSTALLED DOUBLER AND ANGLE PER ESO 80172.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,217 hrs · 15,431 cycles

LEFT CUSP STATION 605 CORROSION AROUND LIGHTNING HOLE. INSTALLED DOUBLER FOR LEFT CUSP AT STATION 605 PER AARD 53-20-00-16.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 33,217 hrs · 15,431 cycles

SUBFLOOR CRACKED AT STATION 218 RIGHT BUTTLINE 24. CUT OUT CRACKED AREA AND INSTALLED DOUBLERS PER AARD 53-20-00-16.

Part: GUSSET — DAMAGED (FUSELAGE) · airframe 33,217 hrs · 15,431 cycles

GUSSET CRACKED STATION 209 LONGERON 15 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: SHUTOFF VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 33,161 hrs · 15,397 cycles

DFW - CREW REPORTED ELECTRICAL ODOR IN COCKPIT DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT PRESSURE REGULATOR SHUT-OFF VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,551 hrs · 13,684 cycles

THE 1418 FRAME IS CRACKED ON AFT SIDE OF FRAME AT LONGERON 2 LEFT AND 2 RIGHT. REPAIRED PER SRM 53-03 FIGURE 31A.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 25,233 hrs

SFO EMERGENCY SEAT MOUNTED LIGHTS AT SEAT ROW 29D INOPERATIVE. REPAIRED WIRING AT SEAT ROW 29D FOR EMERGENCY SEAT MOUNTED LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,233 hrs

SFO SEAT MOUNTED EMERGENCY LIGHT AT SEAT 32D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 32D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY — LOOSE (EMERGENCY LIGHTS) · airframe 23,288 hrs

SFO - EMERGENCY EXIT LIGHTS AT OVERHEAD RIGHT AND LEFT OVERWING EXIT DOORS INOPERATIVE. RESEATED BATTERIES IN BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT OVERHEAD RIGHT AND LEFT OVERWING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 22,603 hrs

LGA - EMERGENCY LIGHT AT SEAT ROW 12DEF INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 12DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COMPRESSOR — STALLED (LT ENGINE)

DFW INFLIGHT DURING CLIMBOUT LEFT HAND ENGINE COMPRESSOR STALLED. ENGINE PRESSURE RATIO WENT BACK TO 1.73. ALL INDICATIONS NORMAL AFTER BRINGING FLIGHT TO IDLE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND METAL IN TAILPIPE. REPLACED LEFT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

LGA - EMERGENCY LIGHT MID BATTERY CHARGER INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SEA - EMERGENCY CEILING LIGHTS AT ROWS 28 AND 29 AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING LIGHTS AT ROWS 28 AND D29 AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY CEILING LIGHT AT ROW 28 AND AT AFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING LIGHT AT ROW 28 AND AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DIRTY (EMERGENCY LIGHT)

DFW EMERGENCY CEILING LIGHTS AT ROWS 4, 5 AND 7 ARE INOPERATIVE. CLEANED CONTACTS FOR EMERGENCY CEILING LIGHTS BATTERY PACK B5-100 FOR ROWS 4, 5 AND 7. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW OVERHEAD EMERGENCY PATH AISLE LIGHTS AFT OF ACCESSORY RAMP AREA INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY PATH AISLE LIGHTS AFT OF ACCESSORY RAMP AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — LOOSE (CABIN)

AFT ACCESSORY RAMP AREA EMERGENCY PATH AISLE LIGHT INOPERATIVE. CONNECTED LOOSE WIRES TO AFT ACCESSORY RAMP AREA EMERGENCY PATH AISLE LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — LOOSE (CABIN)

FORWARD EMERGENCY PATH AISLE LIGHT IN AFT ACCESSORY RAMP AREA INOPERATIVE. RECONNECTED LOOSE WIRES TO FORWARD EMERGENCY PATH AISLE LIGHT IN AFT ACCESSORY RAMP AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CELL · airframe 9,073 hrs · 4,840 cycles

THE FIRST CLASS CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY. CHECK-C 6-2-01 STL. --CLOSED--

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,620 hrs · 2,962 cycles

THE FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LIGHT ASSEMBLY. CHECK-C 7-28-00 JFK.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 5,323 hrs · 2,818 cycles

THE EGRESS LIGHTS WERE INOPERATIVE IN FIRST CLASS AND AT ROW 12 TO 24, AND THE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 15 TO 22. REPLACED LIGHT MODULE P/N 0105606-003 IN FIRST CLASS. FOR THE EGRESS LIGHTS AT ROW 12 TO 24 AND THE OVERHEAD EMERGENCY LIGHTS, REPLACED THE POWER SUPPLY 60-0304-51LB AND CELLS P/N 408822-101 AT EACH LOCATION. CHECK-C 7-28-00 JFK.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 5,069 hrs · 2,693 cycles

THE EGRESS LIGHT WAS EXPOSED AND INOPERATIVE AT ROW 10 AND 17. RE-CONNECTED LIGHT STRIP AT ROW 17 AND REPLACED LIGHT COVER AT ROW 10 DEFERRED CORRECTIONS. THE NEXT STATION REPLACED THE COVER, (P/N 0105601-001), AND RE-CONNECTED THE LIGHT STRIP AT ROW 17. CHECK-C 7-28-00 JFK.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 4,980 hrs · 2,653 cycles

THE EGRESS LIGHT STRIP AT ROW 15 TO 20, AND ROW 24 TO 28 WERE INOPERATIVE. RECONNECTED EGRESS LIGHT POWER FEEDER TO THE STRIP. CHECK-C 7-28-00 JFK.

Part: LENS — OUT OF POSITION (ROW 10) · airframe 4,786 hrs · 2,560 cycles

THE EGRESS LIGHTING FROM ROW 12 TO 16 WERE INOPERATIVE, AND A RED EGRESS LENS WAS LOCATED WHERE A WHITE LENS WAS REQUIRED. RE-ATTACHED THE EGRESS LIGHT CONNECTOR AT ROW 16, AND INSTALLED A WHITE LENS. CHECK-C 7-28-00 JFK.

Part: ECU — WORN (SMOKE DETECTOR) · airframe 3,967 hrs · 2,130 cycles

MID CARGO SMOKE DETECTION ACTIVATED, BOTH SYSTEMS. CREW FIRED BOTH FIRE EXTINGUISHING BOTTLES AND MADE AN UNSCHEDULED LANDING AT IND. THERE WAS NO SMOKE OR FIRE. PLACARD MID CARGO SMOKE DETECTION AND FIRE EXTINGUISHING SYSTEMS PER MEL. THE MID CARGO COMPARTMENT CEU WAS REPLACED TO CORRECT THE SMOKE DETECTION SYSTEM MALFUNCTION. CHECK-C 7-28-00 JFK.

Part: LIGHT — INOP (ROW 3-8)

THE EGRESS LIGHTS WERE INOPERATIVE AT ROWS 3 TO 8 AND AT ROW 11. THE AFT EMERGENCY PATHWAY LIGHTS AND TWO TAIL CONE LIGHTS WERE INOPERATIVE. REPLACED THE ELBOW ASSEMBLY (P/N 0105614-001), FOR ROWS 3 TO 8. REPLACED THE BULB, (P/N 7732) AT ROW 11 AND REPLACED THE BATTERY, (P/N 408822-101) FOR TAIL CONE AREA.