N337PJ

Part: INDICATOR — FAILED (ZONE 200) · airframe 25,248 hrs · 10,954 cycles

AIRCRAFT WAS GROUNDED: FUEL QUANTITY DISPLAY ON UPPER DISPLAY UNIT BLANKS INTERMITTENTLY. REMOVE AND REPLACED NUMBER 2 ELECTRIC DISPLAY UNIT AND INSTALLED REQUIERED SOFTWARE. SYSTEM OPERATIONAL CHECKS NORMAL. PER AMM 31-62-00. FAULT CLEARED.

Part: SIGN — MISSING (ZONE 200) · airframe 25,186 hrs · 10,920 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT DOOR EXIT LIGHT BY 16A IS MISSING. REMOVED AND REPLACED ROW 16 LEFT HAND LOWER EXIT LIGHT ASSEMBLY. PER AMM 33-51-01.

Part: BEZEL — DETACHED (ZONE 200) · airframe 24,770 hrs · 10,727 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY ESCAPE PATH LIGHT BEZEL FELL OFF ROW 20ABC. CONFIRMED ON SEAT 20C EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. (OPEN).

Part: LIGHT — DETACHED (ZONE 200) · airframe 24,770 hrs · 10,727 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY ESCAPE PATH LIGHT BEZEL FELL OFF ROW 20ABC. CONFIRMED ON SEAT 20C EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. **SUPPLEMENTAL REPORT FOR (AALA202509252319): REMOVE AND REPLACED SEAT ROW 20 ABC EMERGENCY LIGHT AND REATTACHED LIGHT BEZEL. PER AMM 33-20-00. OPERATIONAL TEST GOOD**(CLOSED).

Part: SCREEN — UNSECURE (NR 1 ENG OIL SYS) · airframe 24,375 hrs · 10,554 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING CLIMBING THRU FL220 ENGINE NUMBER 1 OIL INDICATED 3Q, OIL PRESSURE INDICATION WAS ABNORMAL AND FLUCTUATING. SHUT DOWN ENGINE NUMBER 1, OIL QUANTITY THAN DROPPED TO ZERO. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT CLT. FOUND SUMP SCAVENGE FOR ENGINE NUMBER 1 SCREEN IN THE COWL. ACCOMPLISHED T/S IAW FIM 79-05-00-810-803-F00 AND AMM 71-00-00-800-804-F00. OIL PRESSURE IS WITHIN LIMITS OF ZONE B. REMOVED AND REPLACED LUBRICATION UNIT FOR ENGINE1. PER AMM 79-21-01. IDLE RUN AND LEAK CHECK GOOD. NO LEAKS NOTED.

Part: DOOR — BINDING (ZONE 800) · airframe 23,776 hrs · 10,274 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY-D DOOR JAMMED CLOSED. LUBED LAVATORY-E DOOR, PER AMM 52-51-14. OPERTIONAL CHECK NORMAL.

Part: SIGN — MISSING (ZONE 200) · airframe 23,229 hrs · 10,041 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT SIGN LIGHT NEXT TO LAVATORY-D MISSING THE SIGN THAT SAYS EXIT. REMOVED AND REPLACED EXIT SIGN LIGHT NEXT TO LAVATORY-D. OPERTIONAL CHECKED GOOD. PER AMM 33-51-01.

Part: SLIDE — DISLODGED (ZONE 800) · airframe 22,584 hrs · 9,749 cycles

AIRCRAFT WAS GROUNDED: SLIDE ON L1 DOOR FELL OUT OF BUSTLE WHILE AIRCRAFT CLEANERS WERE OPERATING THE DOOR. THE GIRT BAR IS CURRENTLY CAUGHT BETWEEN THE DOOR AND ENTRY STAND. REMOVED AND REPLACED L1 DOOR SLIDE. PER JC 08L22125001.

Part: DOOR — STUCK (ZONE 800) · airframe 22,437 hrs · 9,692 cycles

AIRCRAFT WAS NOT GROUNDED: REPEAT AFT LEFT LAVATORY DOOR JAMMED CLOSED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: DOOR — STUCK (ZONE 800) · airframe 22,437 hrs · 9,692 cycles

AIRCRAFT WAS NOT GROUNDED: REPEAT AFT LEFT LAVATORY DOOR JAMMED CLOSED. **SUPPLEMENTAL REPORT FOR (AALA202412232256): ADJUSTED AFT LEFT HAND BI-FOLD DOOR. OPERTIONAL CHECK GOOD. PER CMM IL3-25-0083.**(CLOSED).

Part: DOOR — OUT OF ADJUST (ZONE 800) · airframe 22,407 hrs · 9,675 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT AFTER LAVATORY ENTRY DOOR WILL NOT OPEN. **SUPPLEMENTAL REPORT FOR (AALA202412205196): ADJUSTED BI-FOLD DOOR AT LEFT HAND AFT LAVATORY. PER CMM IL3-25-0083**(CLOSED).

Part: DOOR — STUCK (ZONE 800) · airframe 22,407 hrs · 9,675 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT AFTER LAVATORY ENTRY DOOR WILL NOT OPEN. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: BUMPER — CONTAMINATED (ZONE 800) · airframe 21,778 hrs · 9,379 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAV DOOR BROKEN. REQUIRES REPLACEMENT. PASSENGER STUCK IN LAV OVER 35 MINS IN FLIGHT. MAINTENANC UPON INSPECTION OF LAV D BI-FOLD DOOR FOUND RUBBER STOPPER COVERED IN GOO. CLEANED DOOR AND PERFORMED OPS CHECK OF DOOR. OPS CHECK GOOD IAW CMM 25-40-64. OK FOR SVC

Part: LINK — FAILED (ZONE 700) · airframe 21,412 hrs · 9,189 cycles

AIRCRAFT WAS GROUNDED: UPON LANDING NOSE WHEEL STEERING FAILED AND TURNED 90 DEGREES FROM CENTER, AIRCRAFT PERFORMED HIGHSPEED STOP. REMOVE AND REPLACED NLG UPPER TORSION LINK ASSEMBLY (AALA202408155579), NLG LOWER TORSION LINK ASSEMBLY (AALA202408156682), AND 2 EACH NLG PIN (AALA202408159378) (AALA202408151054). PER AMM 32-21-00 AND AMM 05-51-29.

Part: LINK PIN — FAILED (ZONE 700) · airframe 21,412 hrs · 9,189 cycles

AIRCRAFT WAS GROUNDED: UPON LANDING NOSE WHEEL STEERING FAILED AND TURNED 90 DEGREES FROM CENTER, AIRCRAFT PERFORMED HIGHSPEED STOP. REMOVE AND REPLACED NLG UPPER TORSION LINK ASSEMBLY (AALA202408155579), NLG LOWER TORSION LINK ASSEMBLY (AALA202408156682), AND 2 EACH NLG PIN (AALA202408159378) (AALA202408151054). PER AMM 32-21-00 AND AMM 05-51-29.

Part: LINK PIN — FAILED (ZONE 700) · airframe 21,412 hrs · 91,898 cycles

AIRCRAFT WAS GROUNDED: UPON LANDING NOSE WHEEL STEERING FAILED AND TURNED 90 DEGREES FROM CENTER, AIRCRAFT PERFORMED HIGHSPEED STOP. REMOVE AND REPLACED NLG UPPER TORSION LINK ASSEMBLY (AALA202408155579), NLG LOWER TORSION LINK ASSEMBLY (AALA202408156682), AND 2 EACH NLG PIN (AALA202408159378) (AALA202408151054). PER AMM 32-21-00 AND AMM 05-51-29.

Part: LINK — FAILED (ZONE 700) · airframe 21,412 hrs · 9,189 cycles

AIRCRAFT WAS GROUNDED: UPON LANDING NOSE WHEEL STEERING FAILED AND TURNED 90 DEGREES FROM CENTER, AIRCRAFT PERFORMED HIGHSPEED STOP. REMOVE AND REPLACED NLG UPPER TORSION LINK ASSEMBLY (AALA202408155579), NLG LOWER TORSION LINK ASSEMBLY (AALA202408156682), AND 2 EACH NLG PIN (AALA202408159378) (AALA202408151054). PER AMM 32-21-00 AND AMM 05-51-29.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 20,711 hrs · 8,839 cycles

AIRCRAFT WAS GROUNDED: PER JOB CARD 08T21033001 EMERGENCY LIGHTS FUNCTIONAL CHECK FAILED AT L1 DOOR EXIT SIGN. REMOVE AND REPLACED EMERGENCY BATTERY SUPPLY UNIT. PER AMM 33-51-06.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 20,711 hrs · 8,839 cycles

AIRCRAFT WAS GROUNDED: PER JOB CARD 08T21033001 EMERGENCY LIGHTS FUNCTIONAL CHECK FAILED AT L2 DOOR EXIT SIGN. REMOVE AND REPLACED EMERGENCY BATTERY SUPPLY UNIT. PER AMM 33-51-06.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 20,711 hrs · 8,839 cycles

AIRCRAFT WAS GROUNDED: PER JOB CARD 08T21033001 EMERGENCY LIGHTS FUNCTIONAL CHECK FAILED AT CEILING LEFT HAND ROW 17-30. REMOVE AND REPLACED EMERGENCY BATTERY SUPPLY UNIT. PER AMM 33-51-06.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 20,711 hrs · 8,839 cycles

AIRCRAFT WAS GROUNDED: PER JOB CARD 08T21033001 EMERGENCY LIGHTS FUNCTIONAL CHECK FAILED AT AFT CEILING EXIT SIGN. REMOVE AND REPALCED EMERGENCY BATTERY SUPPLY UNIT. PER AMM 33-51-06.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 20,711 hrs · 8,839 cycles

AIRCRAFT WAS GROUNDED: PER JOB CARD 08T21033001 EMERGENCY LIGHTS FUNCTIONAL CHECK FAILED AT SEAT AISLE ROW 18ABC TO 25ABC. REMOVE AND REPLACED EMERGENCY BATTERY SUPPLY UNIT. PER AMM 33-51-06

Part: TUBE — MISSING (GIRT BAR) · airframe 20,553 hrs · 8,761 cycles

AIRCRAFT WAS GROUNDED: RED HEAT SHRINK NOT INSTALLED ON R1 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: TUBE — MISSING (GIRT BAR) · airframe 20,553 hrs · 8,761 cycles

AIRCRAFT WAS GROUNDED: RED HEAT SHRINK NOT INSTALLED ON R1 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR. INSTALLED RED HEAT SHRINK ON R1 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR. PER AARD 25-66-00-4.

Part: SLIDE — FAILED (R1 DOOR) · airframe 20,549 hrs · 8,759 cycles

AIRCRAFT WAS GROUNDED: FORWARD SERVICE DOOR EMERGENCY SLIDE WAS NOT DISARMED DOOR WAS OPEN, SLIDE FELL OUT BUT FAILED TO DEPLOY. REMOVE AND REPLACED R1 (FORWARD SERVICE DOOR) DOOR EMERGENCY ESCAPE SLIDE. PER J/C 08L22125001

Part: SLIDE — DISLODGED (FWD SERVCE DOOR) · airframe 20,549 hrs · 8,759 cycles

AIRCRAFT WAS GROUNDED: FORWARD SERVICE DOOR EMERGENCY SLIDE WAS NOT DISARMED DOOR WAS OPEN, SLIDE FELL OUT BUT FAILED TO DEPLOY.**SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: WARNING LIGHT — ILLUMINATED (LT WIND OVRHEAT) · airframe 19,923 hrs · 8,469 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: LEFT WING-BODY OVERHEAT LIGHT, MASTER CAUTION. UNABLE TO EXTINGUISH IN FLIGHT; AIRCRAFT AIR DIVERTED TO AND LANDED SAFELY AT IAH. (OPEN).

Part: DUCT — LOOSE (CABIN AIR) · airframe 19,923 hrs · 8,469 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: LEFT WING-BODY OVERHEAT LIGHT, MASTER CAUTION. UNABLE TO EXTINGUISH IN FLIGHT; AIRCRAFT AIR DIVERTED TO AND LANDED SAFELY AT IAH. PACK RAM AIR EXHAUST DUCT FOUND LOOSE IN LEFT AC PACK BAY. DUCT CLAMP RESECURED AS PER AMM 21-51-24. OPERATIONAL TEST SATISFACTORY, NO FURTHER DEFECTS NOTED AT THIS TIME**(CLOSED).

Part: SUPPORT ANGLE — CRACKED (ZONE 100 - FUSE) · airframe 17,599 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN SUPPORT ANGLE LOCATED 2 INCHES OUTBOARD OF KEEL BEAM AT BS 663.5 AND LBL 15. REPAIRED ANGLE PER SRM 57-10-10-2R REPAIR 5 AND EA 344807.

Part: ANGLE — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 17,599 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN Z ANGLE LOCATED AT BS 990 AND FROM RBL 34 TO RBL 47. REPLACED Z ANGLE PER SRM 51-10-02-0G.

Part: TRANSITION PANEL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 17,599 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL AROUND FASTENER HOLE LOCATED AT BS 500 + 10 INCHES AND S25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1 AND DWG 143A8126.

Part: TRANSITION PANEL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 17,599 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED AT BS 727H TO BS 767 AT S25R. REPAIRED TRANSITION PANEL PER SRM 53 -00- 53 -2R-5.

Part: WEB — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 17,599 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN SUB FLOOR WEB LOCATED FROM BS 987 TO BS 994 AT RBL 47. REPAIRED WEB PER EA 344799.

Part: SHIELD — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 17,599 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION SHIELD LOCATED FROM BS 767 TO BS 793 AT S25R. REPLACED TRANSITION SHIELD PER SRM 51-10-02.

Part: RETAINER — LOOSE (ZONE 800 - DOORS) · airframe 17,590 hrs · 7,397 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR GIRT BARS IS LOOSE WHEN ARMED. ADJUSTED L1 DOOR GIRT BAR RETAINING CLIP.

Part: RETAINER — LOOSE (ZONE 800 - DOORS) · airframe 17,590 hrs · 7,397 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR GIRT BARS IS LOOSE WHEN ARMED. ADJUSTED L2 DOOR GIRT BAR RETAINING CLIP.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 16,520 hrs · 6,913 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY SMOKE DETECTOR AURAL AND VISUAL ALERT WITH LAVATORY UNOCCUPIED AND NO SMOKE PRESENT. (OPEN)

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 16,520 hrs · 6,913 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY SMOKE DETECTOR AURAL AND VISUAL ALERT WITH LAVATORY UNOCCUPIED AND NO SMOKE PRESENT. **SUPPLEMENTAL REPORT FOR AALA202301039115: REPLACED AFT LAVATORY SMOKE DETECTOR PER AMM 26-14-01. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.** (CLOSED)

Part: COVER — INOPERATIVE (ZONE 200 - FUSE) · airframe 14,229 hrs · 5,883 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT SIGN COVER AT REAR SERVICE DOOR FELL OFF. FLIGHT ATTENDANT COULD NOT REINSTALL. INSTALLED EXIT SIGN COVER AT RIGHT REAR SERVICE DOOR.

Part: SLIDING WINDOW — JAMMED (ZONE 200 - FUSE) · airframe 13,291 hrs · 5,473 cycles

AIRCRAFT WAS GROUNDED: ON TAKEOFF ROLL, R2 WINDOW OPENED, THEN JAMMED UPON ATTEMPTING TO CLOSE. REPLACED R2 WINDOW WITH SERVICEABLE UNIT IAW WORKCARD 08L21056002, OPS CHECK GOOD.

Part: LENS — MISSING (ZONE 200 - FUSE) · airframe 13,123 hrs · 5,400 cycles

AIRCRAFT WAS NOT GROUNDED: CENTER AISLE OVERWING EMERGENCY EXIT LIGHT MISSING LENS. INSTALLED LIGHT LENS PER AMM 33-51-00.

Part: BRACKET — LOOSE (ZONE 800 - DOORS) · airframe 12,931 hrs · 5,300 cycles

AIRCRAFT WAS NOT GROUNDED: 1R GIRT BAR BRACKET IS LOOSE. ADJUSTED 1R GIRT BAR BRACKET PER AMM 25-66-00-201-440-801.

Part: NONE — LOOSE (ZONE 800 - DOORS) · airframe 12,836 hrs · 5,253 cycles

AIRCRAFT WAS NOT GROUNDED: AFT ENTRY DOOR SLIDERAFT MAKING RATTLING NOISE OF METAL NATURE BEHIND PLASTIC COVER. SECURED GIRT BAR HOLDER.

Part: SMOKE DETECTOR — FALSE INDICATION (ZONE 900 - LAV/G) · airframe 12,818 hrs · 5,246 cycles

AIRCRAFT WAS NOT GROUNDED: MOMENTARY, RIGHT AFT LAVATORY SMOKE WARNING, NO SMOKE CONFIRMED BY FLIGHT ATTENDANT. COMPLIED WITH FUNCTIONAL TEST OF THE RIGHT AFT LAVATORY PER AMM 26-14-00. CHECKS GOOD.

Part: TRACK — STICKING (COCKPIT WINDOW) · airframe 12,504 hrs · 5,127 cycles

AIRCRAFT WAS GROUNDED: FIRST OFFICERS SLIDING WINDOW DIFFICULT TO OPEN AND CLOSE. FOUND FIRST OFFICERS WINDOW STICKING IN TRACK. VISUAL INSPECTION FOUND DEBRIS IN WINDOW TRACK. REMOVED DEBRIS AND LUBRICATED WINDOW TRACKS AS PER AMM 12-25-81.

Part: SLIDING WINDOW — CRACKED (COCKPIT) · airframe 12,500 hrs · 5,126 cycles

AIRCRAFT WAS GROUNDED: R2 WINDOW CRACKED DUE TO DAMAGED HUMP SEAL. REPLACED R2 WINDOW WITH SERVICEABLE UNIT IAW WORKCARD 08L21056002, LEAK AND OPS CHECK GOOD.

Part: SWITCH — OUT OF POSITION (MANUAL EXTEND) · airframe 11,373 hrs · 4,642 cycles

AIRCRAFT WAS GROUNDED: LANDING GEAR FAILED TO RETRACT ON TAKEOFF, FLIGHT RETURNED TO FIELD; DISCOVERED FIRE EXTINGUISHER FELL FROM MOUNT, HITTING ALTERNATE EXTENSION HANDLE DOOR AND TRIGGERING MICROSWITCH. CLOSED MANUAL EXTENSION DOOR AND PERFORMED FUNCTIONAL TEST IAW AMM 32-32-00, OPS CHECK GOOD.

Part: HOOK — LOOSE (R1 GIRT BAR) · airframe 11,294 hrs · 4,609 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 1R SLIDE GIRT BAR CLIP LOOSE. SECURED GIRT BAR CLIP PER AMM 25-66-00.

Part: CYLINDER — DAMAGED (LT MLG BRAKE) · airframe 8,684 hrs · 3,507 cycles

AIRCRAFT WAS GROUNDED: ON TAXI-IN AFTER LANDING, TRAFFIC BEHIND REPORTED OCCASIONAL SPARKS OFF L BRAKE ASSEMBLY. REMOVED AND REPLACED LH MLG INNER CYLINDER, BOTH BRAKES, AND BOTH TIRES PER MCM 32-94-08.

Part: GIRT BAR — OUT OF POSITION (DOOR SLIDE) · airframe 7,429 hrs · 2,978 cycles

AIRCRAFT WAS GROUNDED: AT IAD, ON ARRIVAL, FORWARD GALLEY DOOR GIRT BAR WAS NOT IN PLACED. AS A RESULT, FORWARD RIGHT HAND DOOR SLIDE PRESSURE GAUGE BELOW GREEN MARK. MAINTENANCE REPLACED FORWARD RIGHT HAND DOOR SLIDE PER MCM 25-94-11.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 6,966 hrs · 2,784 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS ONLY FOR ONE MINUTE THE FOLLOWING WERE OBSERVED: AFTER TWO HRS IN CRUISE FOS CDU BLANKED, THEN FMS FUNCTIONS GRADUALLY RETURNED, ALT IM NEXT TO N,S, VTR TRK ON CAS ND, LDG ALT AND NO LOW SPEED YELLOW AIRSPEED TAPE CAS PFD. MAINTENANCE ACCOMPLISHED FMC AND MCDU BUTE CHECKS IAW FIM 34-61-11. ALSO REALIGNED IRUS, FOUND NO FAULTS.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 6,966 hrs · 2,784 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS CABIN EMERGENCY LIGHTS C/B (A-1 ON P6-11 PANEL) FOUND OPEN ON PRE FLIGHT. MAINTENANCE RESET C/B ON P6-11 FOR CAB EMERGENCY LIGHTS. ALL TEST PASSED IAW FIM 33-50-00.

Part: CONTROL LEVER — FAULTY (MLG) · airframe 6,960 hrs · 2,782 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS LANDING GEAR DISAGREEMENT LIGHTS ON, ALL SIX GREEN LDG GEAR LIGHTS ON AFTER GEAR DOWN SELECTION. RED LIGHTS OUT AFTER TOUCHDOWN. MAINTENANCE REPLACED LANDING GEAR CONTROL LEVER MODULE IAW AMM 32-31-11-400-801. SYSTEM TEST NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 6,756 hrs · 2,703 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS DURING APPROACH WHEN LANDING GEAR WAS SELECTED DOWN RED AND GREEN LIGHTS ILLUMINATED ON MAIN PANEL, OVERHEAD PANEL SHOWED 3 GREEN LIGHTS. AFTER GO AROUND, GEAR WAS CYCLED AND NORMAL LANDING GEAR INDICATION DISPLAYED. MAINTENANCE PERFORMED LANDING GEAR POSITION INDICATING AND WARNING SYSTEM CHECKS IAW AMM 32-61-00. NO DEFECTS FOUND.

Part: DOOR — LACK OF LUBE (ZONE 800) · airframe 6,544 hrs · 2,606 cycles

AIRCRAFT WAS NOT GROUNDED: MANUAL GEAR EXTENSION ACCESS DOOR UNABLE TO OPEN. MAINTENANCE CLEANED AND LUBED DOOR AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — BROKEN (CABIN) · airframe 4,913 hrs · 1,928 cycles

THE R2 DOOR EMERGENCY EXIT LIGHT ON THE RIGHT SIDE OF DOOR IS COMPLETELY BROKEN. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY, OPS CHECKED NORMAL IAW AMM 33-51-01.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 4,836 hrs · 1,891 cycles

FORWARD FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT SEAL AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: ELECTRICAL BOX — FAULTY (ENTERTAIN SYS) · airframe 4,170 hrs · 1,625 cycles

ON FINAL DECENT, CREW REPORTED SMOKE COMING FROM INFLIGHT ENTERTAINMENT SYSTEM AT ROW 18DEF. NO EMERGENCY DECLARED, FLIGHT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED THE SEAT POWER BOX AT SEAT ROW 18DEF IAW AMM 44-22-44.

Part: PUMP — LEAKING (A SYSTEM) · airframe 559 hrs · 214 cycles

DURING CLIMB, COMPLETE LOSS OF SYSTEM A HYDRAULIC SYSTEM. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. ACCOMPLISHED HYDRAULIC SYSTEM A FLUSH AND REPLACED LEFT ENGINE HYDRAULIC PUMP IAW AMM 29-11-00. OPS CHECKED GOOD. THE AIRCRAFT WAS GROUNDED.

Part: COFFEEMAKER — DEFECTIVE (GALLEY) · airframe 124 hrs · 41 cycles

THE AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANTS REPORTED THAT WHEN TRYING TO USE THE LOWER AFT GALLEY COFFEE MAKER, A BURNING SMELL EMANATED AND THEY TURNED IT OFF. REPLACED AFT GALLEY COFFEE MAKER NUMBER 5 IAW AMM 25-32-00 CKS GOOD.