N901NN
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
95 reports on file, 2014-08-20 – 2026-08-25.
Part: SLIDE — LOW PRESSURE (ZONE 200) · airframe 41,061 hrs · 17,752 cycles
AIRCRAFT IN BASE MAINTENANCE: L1 SLIDE PACK PRESSURE GAUGE READING OUTSIDE OF THE GREEN ZONE. MAINTENANCE REPLACED L1 SLIDE REPLACED SLIDE. REF MIC 5004353.
Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 41,061 hrs · 17,752 cycles
AIRCRAFT IN BASE MAINTENANCE: DURING EMERGENCY LIGHT TEST ROWS 15 THRU 17 AND OVERWING EXIT LIGHTS ON THE LEFT SIDE DID NOT ILLUMINATE. MAINTENANCE REPLACED POWER SUPPLY IAW AMM 33-51-06.
Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 41,061 hrs · 17,752 cycles
AIRCRAFT IN BASE MAINTENANCE: DURING EMERGENCY LIGHT TEST ROWS 15 THRU 17 AND OVERWING EXIT LIGHTS ON THE LEFT SIDE DID NOT ILLUMINATE. PART RECEIVED FROM STORS WAS BAD FROM STOCK HAD TO ORDER ANOTHER ONE . SEE SDR AALA202608244714 FOR THAT.
Part: GUST LOCK — BROKEN (ZONE 800) · airframe 40,751 hrs · 17,616 cycles
AIRCRAFT WAS GROUNDED: GROUND CREW REPORTED THAT UNABLE TO OPEN OR CLOSE MAIN ENTRY L1 DOOR. FOUND SCREW BROKEN IN GUST LOCK PIN. MAINTENANCE REPLACED BROKEN SCREW IN FWD ENTRY DOOR RADIUS LINK PIN IAW MM 52-11-21.\
Part: FUEL FILTER — CLOGGED (NR 2 ENGINE) · airframe 40,234 hrs · 17,389 cycles
AIRCRAFT WAS NOT GROUNDED: FUEL FILTER BYPASS CAUTION LIGHT AFTER TAKE OFF. LIGHT IS INTERMITTENT. REMOVED AND REPLACE NUMBER 2 ENGINE FUEL FILTER (AALA202605209972), PER MM 73-11-02. ALSO, REMOVED AND REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH (AALA202605205803), PER MM 73-34-01. RAN ENGINE ALL PARAMETERS NORMAL AND LEAK CHECK GOOD.
Part: PRESSURE SWITCH — FAULTY (ZONE 400) · airframe 40,234 hrs · 17,389 cycles
AIRCRAFT WAS NOT GROUNDED: FUEL FILTER BYPASS CAUTION LIGHT AFTER TAKE OFF. LIGHT IS INTERMITTENT. REMOVED AND REPLACE NUMBER 2 ENGINE FUEL FILTER (AALA202605209972), PER MM 73-11-02. ALSO, REMOVED AND REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH (AALA202605205803), PER MM 73-34-01. RAN ENGINE ALL PARAMETERS NORMAL AND LEAK CHECK GOOD.
Part: FLASHLIGHT — INOPERATIVE (ZOEN 200) · airframe 39,873 hrs · 17,215 cycles
AIRCRAFT WAS NOT GROUNDED: NUMBER 4 FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT.
Earlier reports · 2014–2025 · 88 reports
2025
Part: DOOR LATCH — INOPERATIVE (ZONE 800) · airframe 37,198 hrs · 16,001 cycles
AIRCRAFT WAS NOT GROUNDED: LEFT AFTER LAVATORY DOOR UNLOCKED BUT UNABLE TO OPEN. REINSTALLED DOOR LOCKING LATCH BEZEL. PER AMM 25-40-15.
Part: GPWS — FAULTED (ZONE 100) · airframe 36,872 hrs · 15,847 cycles
AIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: TERRIAN FAILED ON BOTH CAPTAIN AND FIRST OFFICER NAVIGATION DISPLAYS THE (GPWS)-GROUND PROXIMITY WARNING SENSOR INOPERATIVE LIGHT DISPLAYED; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. ACCOMPLISHED FIM TASK 34-46-00 AND GPWS OPERTIONAL CHECK GOOD, NO FAULT FOUND.
Part: DOOR LATCH — DISLODGED (ZONE 800) · airframe 36,812 hrs · 15,818 cycles
AIRCRAFT WAS NOT GROUNDED: REPEAT WRITE-UP. FORWARD LAVATORY INTERIOR DOOR LOCK KNOB FELL OFF MULTIPLE TIMES LOCKING PASSENGERS IN LAVATORY. RESECURED LAVATORY DOOR LOCK KNOB (INSIDE).
Part: KNOB — DISLODGED (ZONE 800) · airframe 36,816 hrs · 15,820 cycles
AIRCRAFT WAS NOT GROUNDED: REPEAT WRITE-UP. FORWARD LAVATORY INTERIOR DOOR LOCK KNOB FELL OFF MULTIPLE TIMES. INSTALLED NEW KNOB ON FORWARD LAVATORY DOOR. PER CMM 25-46-96.
Part: KNOB — BROKEN (ZONE 800) · airframe 36,800 hrs · 15,814 cycles
AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR LOCK IS BROKEN. REINSTALLED DOOR LOCK KNOB. PER AMM 25-40-10.
Part: KNOB — DISLODGED (ZONE 800) · airframe 36,806 hrs · 15,816 cycles
AIRCRAFT WAS NOT GROUNDED: FIRST CLASS LAVATORY DOOR LOCK KNOB FELL OFF. PASSENGER GOT LOCKED IN THE LAVATORY. REESECURED LOCK KNOB.
Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 36,775 hrs · 15,803 cycles
COMPONENT IN SHOP MAINTENANCE: AFT 2L PASSENGER DOOR INFLATION CYLINDER PRESSURE GAGE IN RED ZONE. REMOVE AND REPLACED AFT L2 ESCAPE SLIDE ASSEMBLY. PER J/C 08L22125001.
2024
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,497 hrs · 15,242 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD (T-CAP) AT STA 947, FROM LBL 51 TO RBL 51. REPLACED CHORD PER SRM 53-70-51-2R-5.
Part: ATTACH BRACKET — DAMAGED (ZONE 200) · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: DAMAGE TO R2 DOOR LOWER SILL STRUCTURE ATTACH BRACKET (CLIP) AT STA 947, RBL 51. REPLACED CLIP PER AARD 51-00-05-1.
Part: WEB — DAMAGED (ZONE 200) · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: DAMAGE TO R2 DOOR LOWER SILL STRUCTURE WEB AT STA 947, RBL 51. REPLACED WEB PER AARD 51-00-05-1.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 947, RBL 51. REPLACED INTERCOSTAL PER AARD 51-00-05-1.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 947, LBL 24. REPLACED INTERCOSTAL PER AARD 51-00-05-1.
Part: WEB — CRACKED (ZONE 100) · airframe 35,494 hrs · 15,240 cycles
AIRCARFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE WEB FROM STA 986 TO STA 1016, LBL 32. REPLACED WEB PER AARD 51-00-05-1.
Part: RAIL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT, AFT BULKHEAD LOWER LOBE RAIL ASSEMBLY AT STA 500I, FROM LBL 30 TO RBL 30. REPLACED RAIL ASSEMBLY PER AARD 51-00-05-1.
Part: RAIL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT, AFT BULKHEAD LOWER LOBE RAIL ASSEMBLY AT STA 500I, FROM LBL 30 TO RBL 30. REPLACED RAIL ASSEMBLY PER AARD 51-00-05-1.
Part: TRACK — WORN (ZONE 300) · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER SLIDING SEAL STRUCTURE, FORWARD TRACK WORN. STA 1070, LBL 10. ACCOMPLISHED DOUBLER REPAIR PER EA 357486.
Part: ELT — NO TEST (ZONE 200) · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: PORTABLE ELT FAILED CONTINUITY TEST. REMOVED AND REPLACED PORTABLE ELT. PER TASK CARDS 99T20025003 AND 99L20025003 OPERTIONAL CHECK GOOD.
Part: SLIDE — NOT REPORTED (R1 DOOR) · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: R1 SLIDE NEEDS TO BE REPLACED. R1 SLIDE REPLACED. PER AMM 25-66-01.
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM STA 274.5 TO STA 294.5, BL 0. REPLACED INTERCOSTAL PER AARD 51-00-05.
Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM STA 380 TO STA 400, LBL 14. REPLACED INTERCOSTAL PER AARD 51-00-05-1.
Part: BAFFLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT BAFFLE FROM STA 500G TO STA 500H, LBL 25. REPLACED BAFFLE PER AARD 53-00-05.
Part: DOOR SILL — CORRODED (ZONE 200) · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L2 DOOR SILL INNER CHORD (CREASE ANGLE) FROM STA 967 TO STA 986, LBL 54. REPLACED CHORD PER AARD 51-00-05-01.
Part: BAFFLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT BAFFLE FROM STA 500F TO STA 500G, LBL 25. REPLACED BAFFLE PER AARD 51-00-05.
Part: BAFFLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT BAFFLE FROM STA 500G TO STA 500H, RBL 25. REPLACED BAFFLE PER AARD 51-00-05.
Part: BAFFLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT BAFFLE FROM STA 500H TO STA 500I, RBL 25. REPLACED BAFFLE PER AARD 51-00-05.
Part: BAFFLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT BAFFLE FROM STA 500E TO STA 500F, LBL 25. REPLACED BAFFLE PER AARD 51-00-05.
Part: BAFFLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT BAFFLE FROM STA 500B TO STA 500C, LBL 25. REPLACED BAFFLE PER AARD 53-00-05.
Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 500A TO STA 500I, RBL 25. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.
Part: BULKHEAD — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT, AFT BULKHEAD ASSEMBLY AT STA 500I, FROM LBL 30 TO RBL 30. REPLACED BULKHEAD ASSEMBLY PER AARD 51-00-05-1.
Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 400 TO STA 500, LBL 25. REPAIRED TRANSITION PANEL PER AARD 51-00-05-1 AND SRM 53-00-53-2R.
Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT, AFT BULKHEAD LOWER LOBE RAIL ASSEMBLY AT STA 500I, RBL 30. REPLACED RAIL PER AARD 51-00-05-1.
Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM STA 328 TO STA 344, LBL 45. REPLACED INTERCOSTAL PER AARD 51-00-05-1.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD (T-CAP) AT STA 947, LBL 51. REPLACED CHORD PER SRM 53-70-51-2R-5.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT STA 986, RBL 44. REPLACED UPPER CHORD (T-CAP) PER SRM 53-70-51-2R-4 ALTERNATIVE 1.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT STA 986, LBL 4. REPLACED UPPER CHORD (T-CAP) PER SRM 53-70-51-2R-4 ALTERNATIVE 1.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD (T-CAP) AT STA 947, RBL 51. REPLACED CHORD PER SRM 53-70-51-2R-5.
Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R2 DOOR SILL INNER CHORD (CREASE ANGLE) AT STA 950, RBL 54. REPLACED CHORD PER 51-00-05-01.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD (T-CAP) AT STA 947, LBL 5. REPLACED CHORD PER SRM 53-70-51-2R-5.
Part: ANGLE — CORRODED (ZONE 100) · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L2 DOOR SILL INNER CHORD (CREASE ANGLE) AT STA 950, LBL 54. REPLACED CHORD PER 51-00-05-01.
Part: FITTING — CORRODED (ZONE 300) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND HORIZONTAL STABILIZER REAR SPAR TERMINAL FITTING LOWER LUG AT STAB STA 83.05. REPAIRED PER TASK CARD 08L30055002.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT STA 947, RBL 24. REPAIRED FLOOR BEAM UPPER CHORD PER SRM 53-70-51-2R REPAIR 5.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT STA 986, LBL 30. REPLACED UPPER CHORD (T-CAP) PER SRM 53-70-51-2R-4 ALTERNATIVE 1.
Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM STA 927 TO STA 947, LBL 24. REPLACED INTERCOSTAL PER AARD 51-00-05-1.
Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM STA 312 TO STA 328, RBL 31. REPLACED INTERCOSTAL PER AARD 51-00-05-1.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD (T-CAP) AT STA 947, LBL 24. REPLACED CHORD PER SRM 53-70-51-2R-5.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD (T-CAP) AT STA 947, RBL 5. REPLACED CHORD PER SRM 53-70-51-2R-5.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 950, LBL 51. REPLACED INTERCOSTAL PER AARD 51-00-05-1.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT STA 986, RBL 23. REPLACED UPPER CHORD (T-CAP) PER SRM 53-70-51-2R-4 ALTERNATIVE 1.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,494 hrs · 15,240 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT STA 986, LBL 44. REPLACED UPPER CHORD (T-CAP) PER SRM 53-70-51-2R-4 ALTERNATIVE 1.
Part: SLIDE — UNSECURE (AFT LT DOOR) · airframe 34,329 hrs · 14,644 cycles
AIRCRAFT WAS GROUNDED: AFT LEFT ENTRY DOOR SLIDE HANGS DOWN MORE THAN NORMAL WHEN ARMED.
Part: DOOR — OUT OF ADJUST (AFT LAVATORY) · airframe 34,094 hrs · 14,534 cycles
AIRCRAFT WAS NOT GROUNDED: LEFT REAR LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE. ADJUSTED LEFT AFT LAVATORY DOOR. PER AMM 25-28-00.
2023
Part: TOILET — ODOR (ZONE 900 - LAV/G) · airframe 32,890 hrs · 13,967 cycles
AIRCRAFT WAS GROUNDED: EXCESSIVE ODOR FROM R4 LAVATORY. REMOVED AND REPLACED AFT RIGHT HAND TOILET ASSEMBLY. PER AMM 38-32-15.
Part: UNKNOWN — UNSECURE (ZONE 800 - DOORS) · airframe 31,573 hrs · 13,323 cycles
AIRCRAFT WAS NOT GROUNDED: L1 GIRT BAR CLIP LOOSE ON LEFT SIDE. ADJUSTED AND SECURED L1 GIRT BAR PER AMM 25-66-01.
Part: SLIDE — LOOSE (ZONE 900 - LAV/G) · airframe 31,117 hrs · 13,097 cycles
AIRCRAFT WAS NOT GROUNDED: R1 DOOR SLIDE PACK GIRT BAR LOOSE. REPLACED R1 DOOR SLIDE PER AMM 25-66-01 AND JOB CARD 25-9440.
2022
Part: MOUNT — DETACHED (ZONE 200 - FUSE) · airframe 30,131 hrs · 12,642 cycles
AIRCRAFT WAS NOT GROUNDED: ESCAPE PATH LIGHT IS NOT ATTACHED TO SEAT 15C. REPLACED ESCAPE LIGHT MOUNT AT SEAT 15C. EMERGENCY LIGHT OPERATIONS CHECKS NORMAL PER 33-51-11.
Part: GUIDE ARM — DAMAGED (L1 DOOR) · airframe 30,025 hrs · 12,589 cycles
AIRCRAFT WAS GROUNDED: 1L DOOR DIFFICULT TO CLOSE. REPLACED 1L DOOR GUIDE ARM ASSEMBLY PER AMM 52-11-21. OPERATIONAL CHECK GOOD.
Part: LIGHT — BROKEN (ZONE 200 - FUSE) · airframe 29,020 hrs · 12,106 cycles
AIRCRAFT WAS NOT GROUNDED: 24C EMERGENCY LIGHT FLOOR STRIP BROKEN OFF. SECURED 24C EMERGENCY LIGHT BOX TO SEAT OK FOR SERVICE.
Part: CIRCUIT BREAKER — PULLED (ZONE 200 - FUSE) · airframe 28,543 hrs · 11,887 cycles
AIRCRAFT WAS GROUNDED: AT CRUISE, 370 NOTICED BOTH ENGINE SPAR VALVE CLOSED LIGHTS ILLUMINATED BRIGHT. AIRCRAFT DIVERTED TO PHX AND DECLARED AN EMERGENCY. FOUND CIRCUIT BREAKER B3 FUEL SPAR VALVE ENGINE 1 AND CIRCUIT BREAKER B4 FUEL SPAR VALVE ENGINE 2 OPEN ON P6-3. CLOSED CIRCUIT BREAKERS. ACCOMPLISHED FIM 28-22-00-810-809 AND FIM 28-22-00-810-810 AND ENGINES IDLE RUN. SYSTEM OPERATE NORMAL.
Part: NONE — INOPERATIVE (ZONE 800 - DOORS) · airframe 28,093 hrs · 11,687 cycles
AIRCRAFT WAS NOT GROUNDED: FORWARD ENTRY DOOR GIRT BAR CLIP IS BENT AND NEEDS ADJUSTMENT. ADJUSTED GIRT BAR CLIP ON L1 DOOR SYSTEM CHECK GOOD.
2021
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 26,823 hrs · 11,090 cycles
AIRCRAFT WAS NOT GROUNDED: EMERGENCY AISLE LIGHTS INOPERATIVE AT ROWS 22-25. SECURED P2 CONNECTOR AT ROW 21ABC IAW AMM 33-51-00, OPS CHECK GOOD.
Part: ANTI-SKID VALVE — FAULTY (MLG) · airframe 26,374 hrs · 10,882 cycles
AIRCRAFT WAS GROUNDED: ANTI-SKID INOPERATIVE LIGHT ILLUMINATED IN FLIGHT, FLIGHT DECLARED EMERGENCY AND RETURNED TO FIELD. REPLACED #4 ANTI-SKID VALVE IAW AMM 32-42-31, LEAK AND OPS CHECK GOOD.
Part: COVER — DAMAGED (DOOR SLIDE) · airframe 25,871 hrs · 10,655 cycles
AIRCRAFT WAS NOT GROUNDED: RH REAR EVACUATION SLIDE HAS HANDLE STICKING OUT. REPLACED COVER OVER EVACUATION SLIDE HANDLE, OPS CHECK GOOD.
Part: DISPLAY — INOPERATIVE (SNDBY ATTITUDE) · airframe 25,547 hrs · 10,518 cycles
AIRCRAFT WAS GROUNDED: STANDBY ATTITUDE INDICATOR FAILED, FLIGHT DIVERTED TO PHX AND LANDED WITHOUT INCIDENT. REPLACED INTEGRATED STANDBY FLIGHT DISPLAY WITH SERVICEABLE UNIT IAW AMM 34-24-02, OPS CHECK GOOD.
Part: WINDOW — NOISY (R2) · airframe 25,518 hrs · 10,504 cycles
AIRCRAFT WAS GROUNDED: AIRCRAFT RETURNED AFTER TAKE OFF DUE TO MILD RAPID BANGING SOUND ON RIGHT SIDE OF FORWARD FUSELAGE NEAR R2 WINDOW. REPLACED COCKPIT WINDOW #2 IAW CARD 08L21056002.
Part: RING — MISSING (GIRT BAR) · airframe 25,325 hrs · 10,428 cycles
AIRCRAFT WAS NOT GROUNDED. FORWARD SERVICE DOOR GIRT BAR MISSING PLASTIC RING THAT SECURES THE BAR IN THE BRACKET. INSTALLED MISSING LOCK RING AT FORWARD SERVICE DOOR GIRT BAR BY CLIPPING IT IN PLACE.
2020
Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 24,573 hrs · 10,109 cycles
AIRCRAFT WAS NOT GROUNDED: RIGHT HAND MAIN LANDING GEAR WHEEL WELL VAPOR BARRIER PREVIOUS REPAIR RE-CRACKED AT BS 663 AND THE 4TH BAY OUT-BOARD. REPAIRED VAPOR BARRIER PER AARD 57-10-10-9.
Part: RELEASE PIN — MISINSTALLED (OXYGEN GEN) · airframe 24,215 hrs · 9,948 cycles
AIRCRAFT IN BASE MAINTENANCE: O2 GENERATOR RELEASE PIN WAS FOUND TO BE INCORRECTLY INSTALLED AT PASSENGER SEAT ROW 25ABC .IT WAS POSITIONED TOO FAR INTO THE O2 GENERATOR AND WAS RESTING ON THE FIRING PIN COLLAR. REPOSITIONED RELEASE PIN ON THE O2 GENERATOR FIRING PIN TO THE CORRECT POSITION PER TASK CARD 2234.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 23,753 hrs · 9,760 cycles
AIRCRAFT WAS NOT GROUNDED: WHILE ACCOMPLISHING CARD 2904, EMERGENCY LIGHTS INOPERABLE AT SEAT 23DEF. MAINTENANCE FOUND PLUG DISCONNECTED UNDER SEAT AND RECONNECTED PLUG PER AMM 33-50-00.
2018
Part: TRANSITION PANEL — CORRODED (BS 727-847) · corrosion level 2 · airframe 19,125 hrs · 7,697 cycles
CORRODED LEFT TRANSITION PANEL BETWEEN BS 727 TO 847. REPAIRED THE TRANSITION PANEL IAW SRM 53-00-53-2R.
Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 19,125 hrs · 7,697 cycles
CORROSION FOUND ON THE FLOORBEAM FLANGE AT BS 947 AND LBL 52 - 53. REPLACED THE FLOORBEAM IAW SRM 53-70-51-2R-5.
Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 19,125 hrs · 7,697 cycles
A CRACK FOUND ON CABIN SUBFLOOR SUPPORT AT BS 328 - 344, LBL 43. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1 AND PRINT 141A5400.
Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 19,125 hrs · 7,697 cycles
FOUND A CRACKED FLOOR SUPPORT. FORWARD CABIN SUB FLOOR AT BS 312 - 328, LBL 43. REPLACED THE FLOOR SUPPORT IAW 51-00-5-1.
Part: FLOOR SUPPORT — CORRODED (BS 950) · corrosion level 2 · airframe 19,125 hrs · 7,697 cycles
CORROSION FOUND ON TOP OF CABIN FLOOR SUPPORT AT BS 950, LBL 52. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1R1.
Part: ANGLE — CRACKED (BS 787) · airframe 19,125 hrs · 7,697 cycles
RIGHT FORWARD TRANSITION PANEL ANGLE CRACKED AT BS 787. REPLACED THE ANGLE IAW SRM 53-60-15, AND SRM 51-10-02.
Part: FLOOR SUPPORT — CORRODED (BS 950) · corrosion level 2 · airframe 19,125 hrs · 7,697 cycles
CORROSION FOUND ON THE CABIN FLOOR SUPPORT, BS 950, RBL 52. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1.
Part: SLIDING WINDOW — BINDING (COCKPIT) · airframe 18,824 hrs · 7,559 cycles
FIRST OFFICER`S R2 SLIDING WINDOW DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS GROUNDED. REPLACED THE WINDOW IAW MCM 56-94-02. OPS CHECKED GOOD.
Part: BLOCK — DEFECTIVE (R1 DOOR SLIDE) · airframe 18,704 hrs · 7,508 cycles
ON REMOVAL OF THE R1 DOOR SLIDE, FOUND BLOCK ASSEMBLY DEFECTIVE PIN NOT SEATING PROPERLY. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED R1 DOOR SLIDE AND BLOCK ASSEMBLY PER MM 245-66-00. OK FOR SERVICE.
Part: LENS — DETACHED (CABIN) · airframe 17,785 hrs · 7,117 cycles
AIRCRAFT WAS NOT GROUNDED: MAINTENANCE FOUND EMERGENCY EXIT LENS ON FORWARD GALLEY TABLE. REPLACED EMERGENCY EXIT SIGN AT R1 DOOR AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER MM 33-51-01.
2017
Part: ANTENNA — FAULTY (ZONE 100) · airframe 16,984 hrs · 6,800 cycles
AIRCRAFT WAS GROUNDED: AFTER TAKEOFF AT 1000 FEET UNABLE TO ENGAGE NAVIGATION AUTO THROTTLE STAYED IN TOGA AT 5000 FT WHEN THROTTLES RETARD, LANDING GEAR WARNING HORN ON STEADY. HORN STAYED ON UNTIL GEAR WAS EXTENDED. LANDING WAS BELOW MAX LANDING. WEIGHT CONTAINS RADIO ALTIMETER WAS NOT DISPLAYING ON TAKE OFF. MAINTENANCE REPLACED ANTENNA PER AMM 34-33-11 AND PERFORMED SUCCESSFUL OPERATIONS CHECK.
Part: ANTENNA — FAULTY (ZONE 100) · airframe 16,984 hrs · 6,800 cycles
AIRCRAFT WAS GROUNDED: AFTER TAKEOFF AT 1000 FEET UNABLE TO ENGAGE NAVIGATION AUTO THROTTLE STAYED IN TOGA AT 5000 FT WHEN THROTTLES RETARD, LANDING GEAR WARNING HORN ON STEADY. HORN STAYED ON UNTIL GEAR WAS EXTENDED. LANDING WAS BELOW MAX LANDING. WEIGHT CONTAINS RADIO ALTIMETER WAS NOT DISPLAYING ON TAKE OFF. MAINTENANCE REPLACED ANTENNA PER AMM 34-33-21 AND PERFORMED SUCCESSFUL OPERATIONS CHECK.
Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 16,950 hrs · 6,783 cycles
AIRCRAFT WAS NOT GROUNDED. LAVATORY SMOKE DETECTOR WENT OFF IN AFT LEFT LAVATORY. NO INDICATION OF SMOKE COCKPIT OVERHEAD AND 6-PACK ALSO ILLUMINATED. PERFORMED OPERATIONAL CHECK OF LAVATORY SMOKE DETECTION PER AMM 26-14-00. NO DEFECTED NOTED.
Part: COMPUTER — FAULTY (GUIDANCE) · airframe 16,528 hrs · 6,595 cycles
EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE ACCOUNT TAIL STRIKE INDICATION ON TAKEOFF. LANDING UNEVENTFUL. REMOVED AND REPLACED HEADS UP GUIDANCE SYSTEM COMPUTER IAW AMM 34-36-01. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.
Part: BEZEL — BROKEN (CABIN) · airframe 16,442 hrs · 6,553 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT THE L1 DOOR HAS A BROKEN BEZEL. REPLACED BEZEL PER AMM 20-00-00. OPERATIONAL CHECK GOOD.
Part: LIGHT — DAMAGED (CABIN) · airframe 16,394 hrs · 6,530 cycles
EMERGENCY EXIT PROXIMITY LIGHT AT THE G2 GALLEY IS DAMAGED. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM 33-51-14. OPERATIONAL CHECK GOOD.
Part: COVER — BROKEN (CABIN) · airframe 15,361 hrs · 6,133 cycles
EMERGENCY LIGHT PANEL COVER G2 GALLEY IS BROKEN. REPLACED EMERGENCY LIGHT PANEL COVER AT G2 GALLEY. OPS CHECK NORMAL. THE AIRCRAFT WAS NOT GROUNDED.
2015
Part: OVERHEAT SENSOR — DEFECTIVE (LT STRUT) · airframe 7,835 hrs · 3,064 cycles
AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB CREW RECEIVED A LT WING TO BODY OVERHEAT INDICATION. THE INDICATION WENT OUT ON APPROACH. R & R LT FWD STRUT CAVITY OVERHEAT DETECTOR M1761. PERFORMED OPERATIONAL CHECK IAW AMM 26-18-02. SYS CHECKED NORMAL.
2014
Part: FUSE — DAMAGED (CABIN) · airframe 6,976 hrs · 2,733 cycles
MID CABIN EMER EXIT SIGN INOPERATIVE. REPLACED POWER SUPPLY FUSE. OPERATIONS CHECKED NORMAL.
Part: SKIN — DENTED (FUSELAGE) · airframe 6,427 hrs · 2,516 cycles
TWO DENTS IN FUSELAGE SKIN FROM STATIONS 245 TO 249 AT WL 215.5 TO 219.5. ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-00-01-2R-3 & EA B737-53-036224.