N403A

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 85,730 hrs · 46,490 cycles

DURING ACCOMPLISHMENT OF WORK CARD 5403, EMERGENCY BATTERY PACK AB5-2 FAILED TO TEST. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-60-98. OPS TESTED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 85,730 hrs · 46,490 cycles

DURING ACCOMPLISHMENT OF WORK CARD 5403, EMERGENCY BATTERY PACK AB5-4 FAILED TO TEST. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-60-98. OPS TESTED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 85,730 hrs · 46,490 cycles

EMERGENCY LIGHTS IN COCKPIT AND GALLEY AREA REMAIN ILLUMINATED WITH AIRCRAFT POWER OFF. REMOVED AND REPLACED BATTERY PACK B5-23 IAW AMM AMM 33-53-00. OPS CHECKED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 85,730 hrs · 46,490 cycles

DURING ACCOMPLISHMENT OF WORK CARD 0801, THE EMERGENCY LIGHTS BETWEEN ROWS 17 AND 22 FAILED TO TEST. REMOVED AND REPLACED THE BATTERY PACK B5-104 IAW AMM 33-53-00. OPS TESTED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 85,730 hrs · 46,490 cycles

DURING ACCOMPLISHMENT OF WORK CARD 5403, EMERGENCY BATTERY PACK AB5-1 FAILED TO TEST. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-60-98. OPS TESTED NORMAL.

Part: ACTUATOR — FAULTY (OUTFLOW VALVE) · airframe 85,135 hrs · 46,138 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING FLIGHT, ACFT WOULD NOT PRESSURIZE & OUTFLOW VLV WAS OSCILLATING BACKWARD & FORTH. R & R OUTFLOW VLV ACTUATOR & ACCOMPLISHED OPERATIONAL CHECK IAW AMM 21-32-05.

Part: BATTERY — DISCHARGED (CABIN) · airframe 84,931 hrs · 46,021 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT AT AFT VAULT DOOR WILL NOT GO OUT. R & R BATTERY ASSEMBLIES B5-27 & 5B-28. ACCOMPLISHED GOOD OPERATIONAL CHECK IAW AMM 33-53-00. SEE ALSO AALA 20160330012.

Part: BATTERY — DISCHARGED (CABIN) · airframe 84,931 hrs · 46,021 cycles

AIRCRAFT WAS NOT GNDED. EMER SIGNS ABOVE RT & LT FWD OVERWING EXITS WILL NOT STAY ON. R & R BATTERY ASSEMBLY & ACCOMPLISHED GOOD OPERATIONAL CHECK IAW AMM 33-53-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 84,931 hrs · 46,021 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT AT AFT VAULT DOOR WILL NOT GO OUT. R & R BATTERY ASSEMBLIES B5-27 & 5B-28. ACCOMPLISHED GOOD OPERATIONAL CHECK IAW AMM 33-53-00. SEE ALSO AALA 20160331021.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 83,889 hrs · 45,400 cycles

DELAMINATION AT END OF LT ELEVATOR, OTBD TE. INJECTED WITH RESIN & CLAMPED IAW SRM 55-03-00-001 FIGURE 5 & EA 255658.

Part: SLIDE — LOW PRESSURE (SERVICE DOOR) · airframe 83,673 hrs · 45,274 cycles

DURING B CHECK INSPECTIONS, AMT FOUND THE FWD SERVICE DOOR ESCAPE SLIDE WITH CYLINDER PRESS THAT WAS BELOW THE SERVICEABLE LIMIT. THE FWD SERVICE DOOR ESCAPE SLIDE ASSEMBLY WAS REPLACED WITH A SERVICEABLE ASSEMBLY.

Part: SKIN — CORRODED (BS 230-257) · corrosion level 2 · airframe 82,966 hrs · 44,850 cycles

FUSELAGE SKIN BETWEEN STATIONS 230 & 257 IS CORRODED FROM LONGERONS 29L TO 30R. REPAIRED SKIN IAW SRM 53-04-03 FIG 4.

Part: SENSOR — FAULTY (AC BAY) · airframe 82,849 hrs · 44,784 cycles

AIR INTERRUPT, EMER NOT DECLARED. DURING CLIMB, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. ACCOMPLISHED WC 36-95-14 & FOUND RT TAIL COMPARTMENT OVERHEAT SENSOR DUCT CHECK VLV STUCK CLOSED. R & R CHECK VLV ASSEMBLY & RT & LT TAIL COMPARTMENT OVERHEAT SENSORS IAW AMM 36-20-00 & 36-20-02. PERFORMED HIGH POWER ENG RUN FOR OPERATIONAL & LEAK CHECKS. SYS CHECKED NORMAL. SEE ALSO AALA20150520001 & AALA20150521012.

Part: CHECK VALVE — STUCK (AC BAY) · airframe 82,849 hrs · 44,784 cycles

AIR INTERRUPT, EMER NOT DECLARED. DURING CLIMB, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. ACCOMPLISHED WC 36-95-14 & FOUND RT TAIL COMPARTMENT OVERHEAT SENSOR DUCT CHECK VLV STUCK CLOSED. R & R CHECK VLV ASSEMBLY & RT & LT TAIL COMPARTMENT OVERHEAT SENSORS IAW AMM 36-20-00 & 36-20-02. PERFORMED HIGH POWER ENG RUN FOR OPERATIONAL & LEAK CHECKS. SYS CHECKED NORMAL. SEE ALSO AALA20150521011 & AALA20150521012.

Part: SENSOR — FAULTY (AC BAY) · airframe 82,849 hrs · 44,784 cycles

AIR INTERRUPT, EMER NOT DECLARED. DURING CLIMB, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. ACCOMPLISHED WC 36-95-14 & FOUND RIGHT TAIL COMPARTMENT OVERHEAT SENSOR DUCT CHECK VLV STUCK CLOSED. R & R CHECK VLV ASSEMBLY & RT & LT TAIL COMPARTMENT OVERHEAT SENSORS IAW AMM 36-20-00 & 36-20-02. PERFORMED HIGH POWER ENG RUN FOR OPERATIONAL & LEAK CHECKS. SYS CHECKED NORMAL. SEE ALSO AALA20150520001 & AALA20150521011.

Part: SEAL — LEAKING (AC BAY) · airframe 82,846 hrs · 44,781 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB THE AIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. ACCOMPLISHED TAIL COMPARTMENT LEAK CHECK, WC 36-95-14. FOUND DUCT LEAKING BETWEEN RT AIR CYCLE MACHINE & RT HEAT EXCHANGER. R & R PERISEALS IAW AMM 21-00-00. PERFORMED LEAK CHECK WITH NO LEAKS NOTED. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 81,581 hrs · 44,010 cycles

AFT STAIRWAY EMER EXIT SIGN INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR AFT STAIRWAY EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 80,802 hrs · 43,512 cycles

VERTICAL STABILIZER LE SKIN BELOW THE ZFS 52.267 SPLICE HAS A NR OF HOLES DAMAGED IN THE SKIN & THE LT SPAR CAP. INSTALLED PLUG BUSHING IAW SRM 55-03-00 FIGURE 30 & INSTALLED EXTERNAL DOUBLER IAW SRM 55-03-00 & EA MD80-55-035355.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 80,802 hrs · 43,512 cycles

MID CARGO STOP PAD, FWD UPPER CORNER CRACKED. R & R FITTING IAW AARD 51-00-05-1.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 80,802 hrs · 43,512 cycles

MID CARGO FWD DOOR STOP FITTING CRACKED. R & R STOP FITTING IAW AARD 51-00-05-1.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 80,802 hrs · 43,512 cycles

FORWARD CARGO STOP PAD FITTING CRACKED. R & R FITTING IAW AARD 51-00-05-1.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,575 hrs · 43,373 cycles

FORWARD TWO OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-103, OPERATIONS CHECKED NORMAL.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 80,575 hrs · 43,373 cycles

LEFT AFT LAVATORY SMOKE DETECTOR INOPERATIVE ON TEST. R & R LT AFT LAVATORY SMOKE DETECTOR, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,569 hrs · 43,369 cycles

EMERGENCY LIGHT JUST FWD OF THE AFT SERVICE DOOR ON SIDE WALL INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — FAULTY (CABIN PRESSURE) · airframe 80,566 hrs · 43,367 cycles

ABI INFLIGHT SJD - DFW. CREW REPORTED RAPID DEPRESSURIZATION DUE TO LOSS OF AUTO PRESS CONTROLLERS. EMERGENCY DECLARED FLIGHT DIVERTED ABI & LANDED WITHOUT INCIDENT. PLACARDED AUTO PRESS CONTROLLERS IAW MEL 21-23B. FLIGHT CONTINUED TO DESTINATION. REPLACED CONNECTOR P1-568 AT CABIN PRESS CONTROLLER AT DFW ON 04/19/2014. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 80,481 hrs · 43,315 cycles

CREW REPORTED NR 2 AUTOMATIC CABIN PRESSURE CONTROLLER INOPERATIVE WITH NR 1 CONTROLLER PREVIOUSLY PLACARDED. EMERGENCY DECLARED, DIVERTED, AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NR 1 & NR 2 PRESSURIZATION CONTROLLERS & ACTUATOR. SYS GROUND CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 79,402 hrs · 42,687 cycles

EMERGENCY LIGHTS AT MID CABIN POSITION FAILED TEST. REPLACED EMERGENCY LIGHT BATTERY PACK AT MID CABIN POSITION. OPERATIONS CHECKED NORMAL.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 78,503 hrs · 42,151 cycles

AIRCRAFT LOST CABIN PRESSURIZATION IN AUTO MODE. EMERGENCY DECLARED FLIGHT DIVERTED ATL LANDED WITHOUT INCIDENT. REPLACED NR 1 & 2 PRESSURE CONTROLLER. SYSTEM GROUND CHECKED NORMAL.

Part: SENSOR — LEAKING (ZONE 200) · airframe 77,542 hrs · 41,594 cycles

MCI - CREW REPORTED CABIN ALTITUDE WARNING. EMERGENCY DESCENT INITIATED AND O2 MASKS WERE MANUALLY DEPLOYED. EMERGENCY DECLARED FLIGHT LANDED MCI WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FIGHT FERRIED TO TUL FOR FURTHER MAINTENANCE. REPLACED LEAKING TEMPERATURE SENSOR AND REPAIRED 8TH STAGE DUCT IN AFT ACCESSORY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (OUTFLOW VALVE) · airframe 77,542 hrs · 41,594 cycles

ORD - CREW REPORTED UNABLE TO CONTROL PRESSURIZATION IN AUTOMATIC CONTROL. FLIGHT RETURNED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CABIN PRESSURE OUTFLOW ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 77,076 hrs · 41,340 cycles

DFW - CREW REPORTED HAD RAPID DEPRESSURIZATION WHILE IN AUTO. SWITCHED TO MANUAL CONTROL AND WAS ABLE TO CONTROL. NO FLOW LIGHTS ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 1 CABIN PRESSURE CONTROLLER AND SELECTOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TEE FITTING — SCRATCHED (FUSELAGE) · airframe 77,067 hrs · 41,331 cycles

SCRATCHES IN RADIUS OF RIGHT AFT PRESSURE BULKHEAD T CHORD, IN RIGHT AFT LAVATORY AREA, ON AFT SIDE OF FRAME, BETWEEN LONGERONS 8 AND 17 RIGHT. INSTALLED RIGHT AFT PRESSURE BULKHEAD T CHORD PER SRM 53-03-00 FIGURE 37A AND EA MD80-53-02755.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,067 hrs · 41,331 cycles

CUT BELL FRAME ANGLE BETWEEN LONGERONS 4 AND 5 RIGHT AT STATION 1338, FOR OTHER MAINTENANCE. INSTALLED BELL FRAME REPAIR ANGLE AND BELL FRAME REPAIR STRAP PER SRM 53-03-00 FIGURE 14 AND EA MD80-53-027258.

Part: SKIN — CRACKED (CENTER WING) · airframe 77,067 hrs · 41,331 cycles

STATION 826 CENTER WING SKIN CAP CRACKED. INSTALLED DOUBLER PER SRM 51-70-05 AND EA MD80-57-026832.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,067 hrs · 41,331 cycles

AFT CARGO HAS CORROSION ON LOWER DOOR BEAM FROM STATIONS 1155 TO 1165. INSTALLED DOUBLER FROM STATIONS 1155 TO 1212 PER AARD 53-10-00-3.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 77,067 hrs · 41,331 cycles

SKIN STATIC DISCHARGE BLEND BEYOND LIMITS BETWEEN FRAMES 408 AND 427 AND LONGERONS 19 AND 21 LEFT. INSTALLED CLASS 3 DOUBLER PER SRM 53-04-03 FIGURE 3.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 77,067 hrs · 41,331 cycles

LONGERON 11 LEFT AT STATION 855 DAMAGED. ACCOMPLISHED SPLICE REPAIR TO LONGERON 11 LEFT AT STATION 855 PER SRM 53-02-00 FIGURE 3.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 77,067 hrs · 41,331 cycles

PREVIOUSLY BLENDED AREA OUT OF LIMITS AT STATION 364 BETWEEN LONGERONS 21 AND 22 LEFT. INSTALLED CLASS 3 DOUBLER PER SRM 53-04-03 FIGURE 4.

Part: WEB — CRACKED (FUSELAGE) · airframe 77,067 hrs · 41,331 cycles

FORWARD WEB CRACKED AT STATION 209, LONGERON 11 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 77,067 hrs · 41,331 cycles

CRACK IN LEFT CUSP AT STATION 806 UNDER NUMBER 1 SEAT TRACK. INSTALLED NEW CUSP SHEET FROM STATIONS 788 TO 807 PER AARD 51-00-05-1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,067 hrs · 41,331 cycles

LEFT AFT LAVATORY, PRESSURE BULKHEAD OUTBOARD SIDE AT LONGERON 9 LEFT, LOWER END CLIP IS CRACKED. INSTALLED NEW CLIP PER AARD 51-00-05-1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 77,067 hrs · 41,331 cycles

FUSELAGE SKIN FROM STATIONS 389 TO 400 BETWEEN LONGERONS 20 AND 21 LEFT, BLENDED AREA OUT OF LIMITS. INSTALLED CLASS 3 DOUBLER PER SRM 53-04-03 FIGURE 2.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,067 hrs · 41,331 cycles

CORROSION FOUND UNDER G2 TIEDOWN AT STATION 218, RIGHT BUTTLINE 11. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 77,067 hrs · 41,331 cycles

SKIN STATIC DISCHARGE BLEND BEYOND LIMITS BETWEEN FRAMES 427 AND 446 AND LONGERONS 19 AND 20 LEFT. INSTALLED INTERNAL DOUBLER PER SRM 53-04-02.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,067 hrs · 41,331 cycles

FORWARD LONGERON 2 LEFT CRACKED AT STATION 160. ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,067 hrs · 41,331 cycles

FORWARD LONGERON 3 LEFT CRACKED AT STATION 160. REMOVED DAMAGED LONGERON SECTION AND ACCOMPLISHED SPLICE REPAIR PER AARD 51-00-05-1 AND SRM 53-02-00 FIGURE 18.

Part: GCU — INOPERATIVE (RIGHT) · airframe 75,387 hrs · 40,384 cycles

CREW REPORTED RIGHT GENERATOR FAILED IN FLIGHT. EMERGENCY DECLARED FLIGHT LANDED WITHOUT INCIDENT. REPLACED RIGHT GENERATOR CONTROL UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 74,631 hrs · 39,963 cycles

CEILING LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER FOR CEILING LIGHTS. OPS CHECK NORMAL.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 74,531 hrs · 39,905 cycles

DFW - CREW REPORTED RIGHT HYDRAULIC SYSTEM FAILED. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HYDRAULIC LINE THAT WAS LEAKING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DUCT — DAMAGED (AC BAY) · airframe 73,981 hrs · 39,580 cycles

ICT - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED ICT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND DUCT 1701 AND TEMPERATURE CONTROL DUCT DAMAGED. REPLACED DUCTS. REPLACED TAIL COMPARTMENT TEMPERATURE SENSOR AND LEFT PERRY SEAL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,319 hrs · 39,198 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM SEATS 20D TO 32D INOPERATIVE. REPLACED BATTERY PACK AT AB-4 POSITION. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,319 hrs · 39,198 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM SEATS 20D TO 32D INOPERATIVE. REPLACED BATTERY PACK AT AB-3 POSITION. OPS CHECK NORMAL.

Part: DUCT — DAMAGED (AC BAY) · airframe 71,118 hrs · 37,981 cycles

MSP - CREW REPORTED TAIL COMPARTMENT HIGH LIGHT ILLUMINATED DURING FLIGHT. LIGHT WENT OUT AFTER POWER REDUCED BUT CAME ON MOMENTARILY SEVERAL TIMES DURING APPROACH AS POWER WAS ADDED. FLIGHT LANDED MSP WITHOUT INCIDENT. FOUND DUCT FLANGE DAMAGED. REPLACED DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,923 hrs · 37,883 cycles

LEFT AND RIGHT AFT OVERWING HATCH OVERHEAD EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,923 hrs · 37,883 cycles

EMERGENCY LIGHTS BETWEEN FORWARD LAVATORY AND GALLEY. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS BETWEEN FORWARD LAVATORY AND GALLEY. OPS CHECKED NORMAL.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,593 hrs · 37,705 cycles

AFT PRESSURE BULKHEAD LEFT T-ANGLE SHOWS INDICATION OF CRACK LONGERON 14 LEFT. REMOVED AND REPLACED T ANGLE PER IAW EA 009163.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,314 hrs · 37,522 cycles

AFT FUSELAGE CANT FRAME WEB AT STATION 1463 CRACKED AT LONGERON 18 RIGHT. STOP DRILLED CRACK AND INSTALLED DOUBLER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 70,314 hrs · 37,522 cycles

RADOME BULKHEAD CRACKED AT RIGHT UPPER RADOME ALIGNMENT PIN. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-19.

Part: LIGHT — CRACKED (CABIN) · airframe 70,107 hrs · 37,405 cycles

EMERGENCY LIGHT COVER AT FORWARD CORNER OF FORWARD GALLEY SERVICE DOOR FELL OFF. REPLACED LIGHT ASSEMBLY.

Part: CLAMP — LOOSE (HEAT EXCHANGER) · airframe 69,673 hrs · 37,171 cycles

TAIL COMPARTMENT TEMPERATURE LIGHT CAME ON DURING CLIMB AND REMAINED ON AFTER 2 MINUTES. THE LIGHT WAS ON AND OFF DURING APPROACH. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND LOOSE CLAMP ON LEFT HEAT EXCHANGER INLET. TIGHTENED CLAMP AND NO LEAK NOTED.

Part: CONTROL CABLE — OUT OF RIG (MLG DOOR) · airframe 68,937 hrs · 36,775 cycles

JFK - INFLIGHT LGA-LGA. DURING FUNCTIONAL FLIGHT CHECK THE LANDING GEAR DOOR WAS UNABLE TO CLOSE. EMERGENCY DECLARED, LANDED JFK WITHOUT INCIDENT. ACCOMPLISHED RE-RIG OF LEFT AND RIGHT MAIN LANDING GEAR DOOR PUSH/PULL CONTROL CABLES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: VALVE — INOPERATIVE (ZONE 700) · airframe 68,936 hrs · 36,774 cycles

LGA - AFTER TAKEOFF LEFT GEAR RED LIGHT REMAINED ON AFTER RETRACTION. LANDED LGA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LANDING GEAR VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: VALVE — LEAKING (WARNING SYSTEM) · airframe 68,674 hrs · 36,624 cycles

PSP - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED, RETURNED TO PSP WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED TEMPERATURE SENSOR PNEUMATIC GROUND CONNECTION VALVE.

Part: CLAMP — LEAKING (AUGMENTATION) · airframe 66,454 hrs

TUL INFLIGHT T9610/02JUL. CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION JUST AFTER TAKEOFF. RETURNED TO TUL AND LANDED WITHOUT INCIDENT. REPLACED LT AUGMENTATION VALVE CLAMP OUTBOARD SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: ENGINE — MAKING METAL (LEFT)

BNA INFLIGHT T1531/21AUG - NUMBER ONE ENGINE OIL CLOG LIGHT ILLUMINATED DURING CLIMB. REDUCED NUMBER ONE ENGINE TO IDLE AND RETURNED TO BNA AND LANDED WITHOUT INCIDENT. FOUND METAL IN OIL FILTERS. REPLACED NUMBER ONE ENGINE ON 22 AUG AT BNA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT TAIL CONE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — MISSING (CABIN)

ORD - EMERGENCY EXIT LIGHT AT FORWARD GALLEY WALL FLOOR MISSING. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT FORWARD GALLEY WALL FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE)

DFW - FLIGHT CREW REPORTED CABIN PRESSURIZATION PROBLEM AT FLIGHT LEVEL 320. AFTER TEN MINUTES CABIN ALT LIGHT ILLUMINATED AND NO INDICATION FROM CONTROLLER THAT IT WENT TO STANDBY. CREW INITIATED DESCENT AND WENT TO MANUAL PRESSURIZATION. ALL OXYGEN MASKS DROPPED DURING DESCENT. LANDED DFW WITHOUT INCIDENT. CHANGED BOTH CABIN PRESSURE CONTROLLERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - EMERGENCY LIGHT AT TAIL CONE SLIDE INOPERATIVE. REPLACED BATTERY PACK AT B5 27 FOR EMERGENCY LIGHT AT TAIL CONE SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - CEILING EMERGENCY LIGHTS AT REAR COMPARTMENT LAVATORY DROP DOWN PANEL INOPERATIVE. REPLACED BATTERY PACK AT RIGHT HAND AFT LAVATORY F5 27 FOR INOPERATIVE CEILING EMERGENCY LIGHTS AT REAR COMPARTMENT LAVATORY DROP DOWN PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS AT ROW 21 AFT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROW 21 AFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DEN - AFT ACCY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT ACCY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - CEILING EMERGENCY LIGHTS AT ROWS 28 THROUGH 30 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 28 THROUGH 30. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: APU — SMOKE (APU BAY)

DFW INFLIGHT T563/28 SMOKE IN CABIN AFTER TAKEOFF AND REMAINED UNTIL LANDING. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED AUXILLARY POWER UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — INOPERATIVE (ZONE 600)

DFW INFLIGHT T2427/25 FLIGHT ATTENDANT REPORTED SMOKE IN CABIN INCREASING IN INTENSITY AT MAX POWER, EPR 1.95 PACKS ON AND APU OFF. RETURNED TO DFW. LANDED WITHOUT INCIDENT. FOUND PRESSURE REGULATOR VALVE ON RT PACK INOPERATIVE. REPLACED PRESSURE REGULATOR VALVE ON RT PACK AND PERFORMED ENGINE RUNS AT 1.95 EPR WITH APU OFF AND BOTH PACKS ON. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED--

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - DURING OVERNIGHT MAINTENANCE, AFT CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AFT CABIN EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CEILING EMERGENCY EXIT LIGHT GROUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPLACED FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CHARGER — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD ENTRY LIGHT DIM. REPLACED FIRST CLASS BATTERY AND CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (R1 DOOR)

PHX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHTS SEATS ROW 1 THROUGH 20 DIM. SPLICED WIRES TO EMERGENCY EXIT LIGHTS AT ROW 13. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD FLIGHT ATTENDANT PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED FORWARD FLIGHT ATTENDANT PORTABLE EMERGENCY LIGHT ASSEMBLY. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CORRODED (BS 380/402)

TUL - FOUND CORROSION ON A/C FUSELAGE SKIN STAITON 380 AND 402, UNDER ANTENNAS. REMOVED CORROSION PER SRM 51-10-3 AND TREATED AREA. (M)

Part: UNSAFE WARNING — ILLUMINATED (NLG)

ORD - FLT 2358 - DURING APPROACH TO ORD IN ICING CONDITIONS WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR INDICATED UNSAFE. RECYCLED LANDING GEAR TWO CYCLES AND ALL INDICATIONS RETURNED TO NORMAL WITH GEAR EXTENDED. AIRCRAFT LANDED ORD WITHOUT INCIDENT. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK SEVERAL CYCLES WITH NO DEFECTS FOUND. UNABLE TO DUPLICATE DISCREPANCY AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: SWITCH — DEFECTIVE (FLIGHT DECK)

DFW - FLT 1568 - EN ROUTE SJC/DFW - DURING CRUISE AT FL 370, CABIN OXYGEN LIGHT ILLUMINATED AND ALL PAX OXYGEN MASKS DROPPED SUCCESSFULLY. CABIN ALTITUDE WAS 8000 FEET. AIRCRAFT PROCEEDED DFW AND LANDED WITHOUT INCIDENT. REPLACED OXYGEN PRESSURE CABIN AIRCONDITIONING ANEROID SWITCH. RESTOWED ALL PAX OXYGEN MASKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CHARGER — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT SIDE LIGHTS ABOVE FORWARD LEFT AND RIGHT ESCAPE HATCHES INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)