N976NN

Part: RETAINER — OUT OF ADJUST (GIRT BAR) · airframe 30,826 hrs · 13,101 cycles

AIRCRAFT WAS NOT GROUNDED: GIRT BAR RETAINING CLIP DOES NOT HOLD THE GIRT BAR SECURELY ON DOOR 1L. MAINTENANCE ADJUSTED GIRT BAR RETAINING CLIPS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-66-02.

Part: ELEC CONNECTOR — INOPERATIVE (ZONE 200) · airframe 30,386 hrs · 12,904 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT AISLE INDICATION INOPERATIVE AT ROWS 18ABC THROUGH ROW 25ABC. REMOVE AND REPLACED CONNECTOR AT SEAT 18ABC. PER SWPM 20-61-28. SYSTEM OPERATIONAL CHECK GOOD.

Part: INDICATOR — FALSE INDICATION (ZONE 500) · airframe 29,729 hrs · 12,593 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING THE APPROACH THE FLAPS STOPPED MOVING WITH THE LEFT FLAP AT ABOUT 20 AND RIGHT FLAP AT 15. NO WARNINGS AND CAUTIONS WERE PRESENT IN THE COCKPIT. AIRCRAFT COMMENCED A GO-AROUND AND LANDED SAFELY AT BOS. REMOVED AND REPLACED FLAP TRANSMITTER (AALA202508118950), PER AMM 27-58-01-400-801. ALSO, REPLACED FLAP POSITON INDICATOR (AALA202508110399), PER AMM 27-58-02-400-801 AND AMM 27-59-01-400-801. OPERATIONAL CHECK GOOD.

Part: TRANSMITTER — FAILED (ZONE 500) · airframe 29,729 hrs · 12,593 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING THE APPROACH THE FLAPS STOPPED MOVING WITH THE LEFT FLAP AT ABOUT 20 AND RIGHT FLAP AT 15. NO WARNINGS AND CAUTIONS WERE PRESENT IN THE COCKPIT. AIRCRAFT COMMENCED A GO-AROUND AND LANDED SAFELY AT BOS. REMOVED AND REPLACED FLAP TRANSMITTER (AALA202508118950), PER AMM 27-58-01-400-801. ALSO, REPLACED FLAP POSITON INDICATOR (AALA202508110399), PER AMM 27-58-02-400-801 AND AMM 27-59-01-400-801. OPERATIONAL CHECK GOOD.

Part: DOOR LATCH — LACK OF LUBE (ZONE 800) · airframe 29,562 hrs · 12,521 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR IS VERY DIFFICULT TO OPEN FROM THE OUTSIDE WHEN CLOSED AND FLIGHT DECK ACCESS SYSTEM IS NOT ENGAGED. LUBRICATED FLIGHT DECK DOOR LATCH. OPERATIONAL CHECK GOOD.

Part: CAP — MISSING (GIRT BAR) · airframe 28,527 hrs · 12,053 cycles

AIRCRAFT WAS GROUNDED: 1R DOOR GIRT BAR RIGHT HAND SAFETY CAP MISSING. INSTALLED NEW STOP RELEASE (AALA202504042132), PIN (AALA202504049949), AND A HEAT SHRINK TUBING (AALA20250404063) ON FORWARD RIGHT HAND DOOR SLIDE GIRT BAR. PER AMM 25-66-01 AND EO-2523J012.

Part: PIN — MISSING (ZONE 800 - DOORS) · airframe 28,527 hrs · 12,053 cycles

AIRCRAFT WAS GROUNDED: 1R DOOR GIRT BAR RIGHT HAND SAFETY CAP MISSING. INSTALLED NEW STOP RELEASE (AALA202504042132), PIN (AALA202504049949), AND A HEAT SHRINK TUBING (AALA20250404063) ON FORWARD RIGHT HAND DOOR SLIDE GIRT BAR. PER AMM 25-66-01 AND EO-2523J012.

Part: TUBE — MISSING (GIRT BAR) · airframe 28,527 hrs · 12,053 cycles

AIRCRAFT WAS GROUNDED: 1R DOOR GIRT BAR RIGHT HAND SAFETY CAP MISSING. INSTALLED NEW STOP RELEASE (AALA202504042132), PIN (AALA202504049949), AND A HEAT SHRINK TUBING (AALA20250404063) ON FORWARD RIGHT HAND DOOR SLIDE GIRT BAR. PER AMM 25-66-01 AND EO-2523J012.

Part: BRACKET — CRACKED (ZONE 100) · airframe 27,175 hrs · 11,460 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN AFT CARGO COMPARTMENT SIDEWALL PANEL ATTACH ANGLE AT STA 867, LBL 24. REPLACED BRACKET PER SRM 51-40-02-0G.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,176 hrs · 11,460 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND WHEEL WELL FORWARD WHEEL CUT OUT HAS CORROSION. WEB FOUND TO BE OUT OF LIMITS, PER B737-NG-SRM 53-40-71-1A PROCEDURE 1. - 4-D. REMOVED OUT OFLIMITS WHEEL WELL WEB, PER B737-NG SRM 51-40-02. REPAIRED WEB ASSEMBLY, PER B737-NG SRM 51-70-13-2R-4. INSTALLED REPAIRED WEB ASSEMBLY AT LEFT HAND MLG WHEEL WELL CUT OUT ON FORWARD AREA, PER B737-NG SRM 51-40-02-0G.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 27,176 hrs · 11,460 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CARGO COMPARTMENT FORWARD BULKHEAD CENTER PANEL IS CRACKED 1O INCH FROM BOTTOM OF PANEL. REMOVED AND INSTALLED AFT CARGO COMPARTMENT FORWARD BULKHEAD CENTER PANEL. PER B737NG AMM 25-52-18.

Part: BRACKET — OUT OF ADJUST (ZONE 200) · airframe 27,050 hrs · 11,398 cycles

AIRCRAFT WAS NOT GROUNDED: FWD SERVICE DOOR, GIRT BAR BRACKET ON THE LEFT SIDE IS NOT HOLDING THE GIRT BAR PROPERLY. MAINTENANCE ADJUSTED FORWARD. R1 GIRT BAR BRACKET IAW AMM 25-66-01.

Part: SLIDE — UNWANTED DEPLOY (ZONE 800) · airframe 25,557 hrs · 10,665 cycles

AIRCRAFT WAS GROUNDED: PARTIAL DEPLOYMENT OF THE FORWARD (RIGHT) SERVICE DOOR SLIDE, DUE TO GIRT BAR STILL BEING ENGAGED DURING AIRCRAFT CATERING. REMOVED AND REPLACED R1 DOOR SLIDE PACK AND COVER. PER AMM 25-66-01

Part: DOOR — OUT OF ADJUST (LAVATORY D) · airframe 25,539 hrs · 10,657 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY D DOOR IS DIFFICULT TO OPEN AND CLOSE. REMOVED AND RE-ATTACHED LAV D DOOR FOR ALIGNMENT.

Part: LIGHT — OUT OF POSITION (ROW 10C) · airframe 25,110 hrs · 10,461 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT AT 10C IS DANGLING, NOT ATTACHED. REPLACED EMERGENCY EXIT LIGHT PER AMM 33-51-11.

Part: STABILIZER — WARNING LIGHT (ZONE 300 - STABS) · airframe 23,892 hrs · 9,889 cycles

AIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED INTO MIA DUE TO STABILIZER TRIM FAILURE WITH BOTH AUTPILOTS ON AND OFF. FLIGHT CREW ALSO REPORTED PERIODIC SPEED TRIM FAILURE LIGHT ILLUMINATED. THE AIRCRAFT LANDED SAFELY AT MIA WITHOUT FURTHER INCIDENT. MAINTENANCE DETECTED MESSAGE 22-11125 AND ACCOMPLISHED AMM FIM TASK 22-12-00 WITH NO HARD FAULTS NOTED. ALSO ACCOMPLISHED STABILIZER TRIM AND ELEVATOR POSITION SYSTEM TESTS PER AMM 22-11-00 AND 22-12-00 WITH NO FAULTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,429 hrs · 9,674 cycles

AIRCRAFT WAS GROUNDED: SMOKE / FUME IN AFT GALLEY AND LAST 3 ROWS OF MAIN CABIN OCCURRED AT CRUISE. EMERGENCY DECLARED; FLIGHT DIVERTED TO CUN LANDING SAFELY. MAINTENANCE ACCOMPLISHED JOB CARD 08L00021001 AND FOUND NO EVIDENCE OF ODOR.

Part: LOCK — INOPERATIVE (ZONE 800 - DOORS) · airframe 22,999 hrs · 9,451 cycles

AIRCRAFT WAS GROUNDED: THE LEFT AFT ENTRY DOOR HAS A GUST LOCK THAT IS INOPERABLE AND HAS PARTS MISSING. REMOVED AND REPLACED LOCK ASSEMBLY ON L2 DOOR.

Part: ADJUSTER — OUT OF ADJUST (L1 GIRT BAR) · airframe 22,256 hrs · 9,110 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD ENTRY DOOR (L1) SLIDE GIRT BAR CLIPS ADJUSTED IAW AMM 25-66-01. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)

Part: RETAINER — OUT OF ADJUST (L1 DOOR SLIDE) · airframe 22,256 hrs · 9,110 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT FORWARD SERVICE DOOR SLIDE IS HARD TO ARM DUE TO SLIDE NOT FULLY PACKED INTO SLIDE BUSTLE. ACCOMPLISHED DOOR ESCAPE SLIDE PACK CHECK FORWARD ENTRY DOOR (1L). ADJUSTED RETAINER CLIPS.

Part: UNKNOWN — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 22,256 hrs · 9,110 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD ENTRY DOOR (L1) SLIDE GIRT BAR CLIPS ADJUSTED IAW AMM 25-66-01. **SUPPLEMENTAL REPORT FOR AALA202301258913: REPLACED GIRT BAR RETAINER CLIPS PER JOB CARD 2520J031-001.** (CLOSED)

Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 21,876 hrs · 8,941 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR SLIDE EMERGENCY EXIT EXTERIOR LIGHT INOPERATIVE. REPLACED LAMP PER AMM 33-51-04.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 21,577 hrs · 8,817 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT COVER, SEAT 19C SIDE LIGHT, IS LOOSE. REPLACED LIGHT ASSEMBLY PER AMM 33-51-03. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: GROUND STUD — DAMAGED (FUEL GAUGE) · airframe 21,279 hrs · 8,678 cycles

AIRCRAFT WAS GROUNDED: RAPID FUEL QUANTITY DECREASE RIGHT NUMBER 2 MAIN TANK QUANTITY, WHILE AT CRUISE, AIRCRAFT DIVERTED TO BNA AND DECLARED AN EMERGENCY. DURING DESCENT QUANTITY IN RIGHT TANK INCREASED. SUSPECT GAGE ERROR. PERFORMED FUEL QUANTITY INDICATION SYSTEM BUILT IN TEST EQUIPMENT PER FIM 28-41-00-810-801. TESTPASSED. PERFORMED DRY CAP AND RESISTANCE CHECK PER AMM 28-41-21-710-801. ALL RESISTANCE WITHIN LIMITS. HARNESS GROUND STUDS SHOW NO DEFECTS. ALL FUEL QUANTITY INDICATION SYSTEM READINGS CHECK GOOD.

Part: CIRCUIT BREAKER — OUT OF POSITION (ZONE 200 - FUSE) · airframe 21,107 hrs · 8,589 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR STICKS CLOSED WITH RED GUARD SWITCH UP. RESET COCKPIT DOOR. CONTROL CIRCUIT BREAKER.

Part: SIGN — BROKEN (ZONE 200 - FUSE) · airframe 20,787 hrs · 8,430 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR EMERGENCY EXIT SIGN BROKEN. REPLACED EMERGENCY EXIT LIGHT SIGN PER AMM33-51-01. OPERATIONAL TEST OK.

Part: NONE — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 20,089 hrs · 8,106 cycles

AIRCRAFT WAS NOT GROUNDED: 1R DOOR GIRT BAR CLIP LOOSE. **SUPPLEMENTAL REPORT FOR AALA202205090446: ADJUSTED GIRT BAR CLIP PER AMM 25-61-01.** (CLOSED)

Part: GIRT BAR — LOOSE · airframe 20,089 hrs · 8,106 cycles

AIRCRAFT WAS NOT GROUNDED: 1R DOOR GIRT BAR CLIP LOOSE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: RETAINER — INOPERATIVE (ZONE 800 - DOORS) · airframe 20,071 hrs · 8,099 cycles

AIRCRAFT WAS NOT GROUNDED: LET BRACKET THAT HOLDS GIRT BAR ON THE DOOR DOES NOT HOLD BAR TIGHT ENOUGH R1 DOOR. ADJUSTED FORWARD R1 DOOR GIRT BAR RETAINER, OPERATIONS CHECK GOOD. PER AMM 52-41-00.

Part: LIGHT — DAMAGED (ZONE 200 - FUSE) · airframe 19,122 hrs · 7,699 cycles

AIRCRAFT WAS NOT GROUNDED: ESCAPE PATH LIGHT AT SEAT 24C DAMAGED. SECURED LIGHT AT SEAT 24C OPERATIONS OK PER AMM 33-51-00.

Part: COVER — LOOSE (ZONE 200 - FUSE) · airframe 18,954 hrs · 7,628 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 23C EMERGENCY PATH LIGHT COVER IS LOOSE. **SUPPLEMENTAL REPORT FOR AALA202112134564: REPLACED LIGHT COVER PER AMM 33-50-00.** (CLOSED)

Part: NONE — NONE · airframe 18,954 hrs · 7,628 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 23C EMERGENCY PATH LIGHT COVER IS LOOSE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: WIRE HARNESS — FAULTY (ZONE 300 - STABS) · airframe 18,917 hrs · 7,613 cycles

AIRCRAFT WAS GROUNDED: DURING TAKE OFF ROLL, APU FAULT AND MASTER CAUTION ILLUMINATED. REJECTED TAKEOFF AT APPROXIMATELY 60 KNOTS. RETURNED TO GATE. **SUPPLEMENTAL REPORT FOR AALA202112097725: REPLACED APU WIRE HARNESS PER AMM 49-11-01.** (CLOSED)

Part: NONE — NONE · airframe 18,917 hrs · 7,613 cycles

AIRCRAFT WAS GROUNDED: DURING TAKE OFF ROLL, APU FAULT AND MASTER CAUTION ILLUMINATED. REJECTED TAKEOFF AT APPROXIMATELY 60 KNOTS. RETURNED TO GATE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: APU — ODOR (ZONE 200) · airframe 18,747 hrs · 7,544 cycles

AIRCRAFT WAS GROUNDED: SMELL OF FUEL IN COCKPIT DURING CRUISE, SMELL OF FUEL IN AFT GALLEY DURING DIVERSION DESCENT. EMERGENCY WAS DECLARED AND WAS NOT OVERWEIGHT FOR LANDING. FUEL SMELL STRONGEST IN AFT GALLEY AFTER LANDING WITH BOTH ENGINES RUNNING RIGHT PACK OFF. ON ARRIVAL, PIT MAINTENANCE CREW COULD NOT SMELL ODOR. DISAGREEMENT BETWEEN BACK END AND FRONT CREW COULD NOT ALIGN ON WHAT ODOR WAS ACCOMPLISHED JOB CARD 08L00021001 WITH NO FINDINGS FOUND.

Part: NONE — NONE · airframe 18,569 hrs · 7,472 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT LIGHT AT SEAT 24C BROKEN (ESCAPE PATH LIGHTING). **SUPPLEMENTAL REPORT REQUIRED** (OPEN)

Part: SHROUD — BROKEN (ZONE 200 - FUSE) · airframe 18,569 hrs · 7,472 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT LIGHT AT SEAT 24C BROKEN (ESCAPE PATH LIGHTING). **SUPPLEMENTAL REPORT FOR AALA202110297102: REMOVED AND REPLACED EXIT LIGHT SEAT SHROUD PER CMM 25-25-00** (CLOSED)

Part: LATCH — STICKING (ZONE 800 - DOORS) · airframe 18,410 hrs · 7,401 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY DOOR LATCH LOCK VERY DIFFICULT TO OPERATE. LUBED LAVATORY DOOR LATCH LOCK OPERATIONS CHECKS NORMAL.

Part: SLIDER — STICKING (ZONE 800 - DOORS) · airframe 18,396 hrs · 7,396 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR LATCH BROKEN. FREED STUCK LEFT AFT LAVATORY DOOR LOCK SLIDER.

Part: TRIM PANEL — LOOSE · airframe 18,286 hrs · 7,350 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT TRIM CAME LOOSE AT SEAT 22C. SECURED TRIM.

Part: HOOK — LOOSE (R1 GIRT BAR) · airframe 17,194 hrs · 6,907 cycles

AIRCRAFT WAS NOT GROUNDED: 1R GIRT BAR STOWAGE CLIP LOOSE. ADJUSTED GIRT BAR STOWAGE CLIP ON DOOR 1R PER AMM 25-61-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (CONFIGURATION) · airframe 14,200 hrs · 5,686 cycles

AIRCRAFT NOT GROUNDED: ERRONEOUS TAKEOFF CONFIG WARNING JUST BEFORE V1 ON TAKEOFF MOMENTARY. PSEU FAULTS MSG 31-53007. PERFORMED FIM TASK 27-62-00. NO FAULTS.

Part: DUCT — FAILED (RT A/C PACK) · airframe 12,865 hrs · 5,104 cycles

AIRCRAFT WAS GROUNDED: STRONG BURNING, ELECTRICAL ODOR COMING FROM GROUND PCA CONNECTOR. MAINTENANCE ACCOMPLISHED ODOR CARD 05-96-70 AND FOUND BAD DUCT IN RIGHT PACK BAY. MAINTENANCE REPLACED DUCT, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SWITCH — FAULTY (COCKPIT) · airframe 6,456 hrs · 2,529 cycles

THE AIRCRAFT WAS GROUNDED. CAPT BACKGROUND LIGHT BEHIND CAPT GLARESHIELD MIC SWITCH BURNED OUT WITH ACCOMPANIED FAINT ELEC SMELL. RMVD & RPLCD MAIN PANEL FLOOD LT DIMMER CONTROL UNIT, IAW 34-61-01. OPS OK, NO EVIDENCE OF FAINT ELECT SMELL NOTED AT THIS TIME. (SEE ALSO SDR AALA201707069020)

Part: CONTROL PANEL — FAILED (COCKPIT LIGHTS) · airframe 6,456 hrs · 2,529 cycles

CAPT BACKGROUND LIGHT BEHIND CAPTAIN`S GLARESHIELD MIC SWITCH BURNED OUT WITH ACCOMPANIED FAINT ELECTRICAL ODOR. REMOVED & REPLACED THE FLOOD LIGHT CONTROL PANEL IAW 33-11-21, OPS OK. THE AIRCRAFT WAS GROUNDED.

Part: LENS — BROKEN (CABIN) · airframe 5,491 hrs · 2,176 cycles

EMERGENCY FLOOD LIGHT ASSY LENS ARE CRACKED & BROKE ON AISLE RT SIDE OF F/C GALLEY. REPLACED EMERGENCY FLOOD LIGHT ASSY FWD RT AISLE AT F/C GALLEY IAW 33-51-01. OPS CK GOOD IAW GPM. THE AIRCRAFT WAS NOT GROUNDED.

Part: OVERHEAT SENSOR — FAULTY (ZONE 500) · airframe 5,305 hrs · 2,123 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. DCA-DFW FLIGHT. LEFT ENGINE WING TO BODY OVERHEAT INDICATION DURING DESCENT. LANDING UNEVENTFUL. INSPECTION FOUND NO INDICATION OF HEAT. REMOVED AND REPLACED LEFT FORWARD STRUT CAVITY OVERHEAT DETECTOR M1671 IAW AMM 26-18-02. OPERATIONAL CHECK GOOD.

Part: SIGN — DAMAGED (CABIN) · airframe 1,196 hrs · 462 cycles

EMERGENCY EXIT SIGN AT DOOR R1 REPORTED DAMAGED & BROKEN. REPLACED EMER EXIT LIGHT ASSEMBLY. THE ACFT WAS NOT GNDED.

Part: CONTROL PANEL — FAULTY (ZONE 200) · airframe 308 hrs · 121 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB MULTIPLE FAILURE INDICATIONS WERE RECEIVED, INCLUDING FMC FAILURE, WING TO BODY OVERHEAT & PRESSURIZATION FAULT. R & R FIRE CONTROL PANEL IAW AMM 26-00-01. OPERATIONAL CHECKED NORMAL.