N953AN
Service difficulty reports · 205
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N953AN' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N953AN' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AALA202308145736Door · lack of lubeAIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR STICKS. LUBRICATED FORWARD LAVATORY DOOR.SDR AALA202304240278Battery · inoperativeAIRCRAFT WAS NOT GROUNDED: AFT FLIGHT ATTENDANT JUMPSEAT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED AFT JUMPSEAT EMERGENCY FLASHLIGHT BATTERIES.SDR AALA202209068314Door · stickingAIRCRAFT WAS GROUNDED: INBOUND CREW REPORTS L1 DOOR HARD TO OPEN. PERFORMED ADJUSTMENT AND TEST AT L1 DOOR PER AMM 52-11-00, FOUND SATISFACTORY.SDR AALA202208197109Fan · vibratesAIRCRAFT WAS GROUNDED: NOISE AND VIBRATION OUT OF 12,000 FT THROUGH 14,000 AND ACCELERATING THROUGH 270 KNOTS. ALL FLIGHT ATTENDANTS HEARD AND FELT, AS WELL AS FLIGHT DECK. VERY OBVIOUS. AIR RETURNED TO PHOENIX GEAR AND FLAPS UP. EMERGENCY WAS NOT DECLARED. RESDR AALA202207086663None · noneAIRCRAFT WAS GROUNDED: AIRCRAFT MADE A LOUD NOISE WHEN ACCELERATING PASSED 250 KNOTS, SOUNDED LIKE WIND NOISE FROM A GEAR DOOR OPEN. AUTO PILOT ON OR OFF 2 DEGREES RIGHT WING DOWN ON CONTROL WHEEL. DIVERTED TO PHL EMERGENCY WAS DECLARED. **SUPPLEMENTAL REPORT SDR AALA202207068739Actuator · failedAIRCRAFT WAS GROUNDED: AT 16,000 FT 280 KNOTS ENGAGED AUTOPILOT YOKE MOVED BACK CAUSING MOMENTARY PITCH UP , THEN MOVED FORWARD NOTICEABLE VIBRATION AFTER LEVEL OFF. ACCOMPLISHED AMM 22-11-26-710-801 AUTOPILOT ACTUATOR TEST FAILED. AIRCRAFT DID NOT DECLARE AN SDR AALA202209019906Skin · dentedAIRCRAFT IN BASE MAINTENANCE: L1 PASSENGER DOOR UPPER AFT CORNER OF EXTERIOR SKIN HAS AN AREA OF DAMAGE APPROXIMATELY 1.0 INCH 0.5 INCH. **SUPPLEMENTAL REPORT FOR AALA202206289906: FOUND TO BE WITHIN LIMITS** (CLOSED)SDR AALA202206289906Skin · damagedAIRCRAFT IN BASE MAINTENANCE: L1 PASSENGER DOOR UPPER AFT CORNER OF EXTERIOR SKIN HAS AN AREA OF DAMAGE APPROXIMATELY 1.0 INCH 0.5 INCH. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)SDR AALA202206285854Support Bracket · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR BALANCE BAY SUPPORT BRACKET PART NUMBER 185A1111-14 FOUND TO BE CRACKED AND REQUIRES FABRICATION. FORMED AND HEAT TREATED NEWLY FABRICATED RIGHT ELEVATOR BALANCE BAY SUPPORT BRACKET PER DRAWING 185A1111 REVISION A.SDR AALA202206280378Floor Panel · crackedAIRCRAFT IN BASE MAINTENANCE: FLOOR BOARD RIGHT AFT OF OVER WING EXIT IS CRACKED. PANEL NUMBER 242AF. REMOVED MAIN CABIN FLOOR PANEL 242AF PER B737-NG AMM 53-21-00-000-801. INSTALLED SERVICEABLE MAIN CABIN FLOOR PANEL 242AF PER B737-AF 53-21-00-400-801.SDR AALA202206274369Latch · failedAIRCRAFT IN BASE MAINTENANCE: L1 DOOR SLIDE LATCH FAILED CLOSE TEST. REMOVED AND REPLACED L1 DOOR SLIDE LATCH AA B737NG AMM 25-66-01-400-801.SDR AALA202205248551Gusset · elongatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND OUTBOARD GUSSET AT BS 887 AND LBL 45.50 HAS ELONGATED HOLES. REPAIRED PER SRM 51-40-02.SDR AALA201910219030Control Unit · unreliableAIRCRAFT WAS GROUNDED: CREW DECLARED AN EMERGENCY ON FINAL APPROACH INTO DFW ON ACCOUNT OF FLAP DISAGREE. MAINTENANCE ACCOMPLISHED FIM TASK 27-51-00-810-820 RH FLAPS POSTED TRANSMITTER DISAGREE PROBLEM FOR MAIN MESSAGE 27-52260. REMOVED AND REPLACED FSEU IAW ASDR AALA201908139016Cylinder · leakingAIRCRAFT WAS GROUNDED: NOSE GEAR MAKES AN UNUSUAL GRINDING SOUND ON TAKEOFF ROLL. TAXI OPS ARE NORMAL. REPLACED NOSE LANDING GEAR INNER CYLINDER PER AMM 32-21-24.SDR AALA2019061209001Pump · intermittentAIRCRAFT WAS GROUNDED: PILOT REPORTS LT FWD FUEL PUMP LO PRESSURE LT FLASHES SHORT FINAL AND STAYS ON DURING ROLLOUT. MAINTENANCE REPLACED THE LH FWD BOOST PUMP IAW AMM 28-22-41. LEAK AND OPS CHECK DOOD.SDR AALA201905039005Attach Bracket · looseAIRCRAFT NOT GROUNDED: PILOT REPORTS DURING CLIMBOUT AND THE SOLID TEN MINUTES OF MODERATE TURBULENCE, A SIZEABLE NUMBER OF PASSENGERS SEATED IN SECTION (7ABC) AND SEAT/SECTION 7DEF REPORTED THAT THE ENTIRE BULKHEAD WALL DIRECTLY IN FRONT OF SEATS 7ABC SHOOK SSDR AALA201810021010Transition Panel · corrodedCORROSION IN THE AFT CARGO COMPARTMENT, LEFT TRANSITION PANEL, BETWEEN BS 727 AND 847. REPAIRED THE TRANSITION PANEL IAW SRM 53-00-53-2R-5.SDR AALA2018100130004Intercostal · corrodedCORROSION FOUND ON THE AFT CABIN FLOOR SUPPORT BETWEEN BS 947 AND 967, LBL 50. REPLACED THE FLOOR SUPPORT IAW 51-00-05.SDR AALA2018100130003Floor Support · corrodedCORROSION FOUND ON THE AFT CABIN FLOOR SUPPORT BETWEEN BS 948 - 967, LBL 25. REPLACED THE FLOOR SUPPORT IAW 51-00-05.SDR AALA2018100128002Floor Support · corrodedCORROSION FOUND ON THE AFT CABIN FLOOR SUPPORT, BS 917, LBL 47. REPLACED THE FLOOR SUPPORT IAW 51-00-05.SDR AALA201809287002Transition Panel · corrodedCORROSION FOUND ON THE FORWARD CARGO RT TRANSITION PANEL, BS 492 - 500A. REPLACED THE TRANSITION PANEL IAW DRAWING 143A8126, AND SRM 51-10-02, PARAGRAPH 9.SDR AALA20180926006Transition Panel · corrodedCORROSION TO THE RIGHT TRANSITION PANEL BETWEEN BS 727 TO 767 IN THE AFT CARGO BAY. REPLACED THE RIGHT TRANSITION PANEL IAW SRM 51-10-02.SDR AALA20180925007Angle · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND CREASE ANGLE AT BS 890 TO BS 1016, LBL 50. REPLACED CREASE ANGLE PER 51-00-05-1 AND DRAWING 147A8540 AND 147A5700.SDR AALA201809276005Frame · dentedFORWARD CARGO FRAME DOUBLER WAS DENTED AT BS 500H, STRINGERS 23L - 24L. REPAIRED THE DOUBLER IAW SRM 51-70-11-2R, FIG 1.SDR AALA201809276004Floorbeam · corrodedAFT FLOORBEAM ANGLE AT BS 500I CORRODED. REPLACED FLOORBEAM ANGLE IAW SRM 51-10-2, PAR 9.SDR AALA20180926010Attach Angle · corrodedCORROSION TO LOWER BULKHEAD ATTACH ANGLE AT BS 947, BETWEEN LBL 20 TO RBL 20, IN THE AFT CARGO BAY. REPLACED THE BULKHEAD ATTACH ANGLE IAW 51-00-05, AND SRM 51-10-02.SDR AALA201809264004Web · corrodedCORROSION FOUND ON THE AFT CABIN FLOOR WEB, BS 987, LBL 32 TO LBL 50. REPLACED THE WEB IAW 51-00-05-1, DRAWING 147A5710, AND 147A5700.SDR AALA201809264003Floor Support · corrodedCORROSION FOUND ON THE AFT CABIN FLOOR SUPPORT, BS 992 TO 1016, LBL 32. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1, DRAWING 147A5710, AND 147A5700.SDR AALA201809264001Floor Support · corrodedCORROSION FOUND ON THE AFT CABIN FLOOR SUPPORT, BS 992 TO 1016, RBL 32. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1, DRAWING 147A5710, AND 147A5700.SDR AALA201809265006Angle · corrodedCORROSION WAS FOUND ON THE ZEE ANGLE AT LBL 33 - 45, BS 993. REPLACED THE ANGLE IAW 51-00-05.SDR AALA201809265005Angle · corrodedCORROSION WAS FOUND ON ZEE ANGLE AT BS 993, RBL 33 - 45. REPLACED THE ANGLE IAW 51-00-05 .SDR AALA201809265004Angle · corrodedRIGHT CREASE ANGLE HAD CORROSION, RBL 52, BS 890 TO 1016. REPLACED THE ANGLE IAW 51-00-05-1, DRAWINGS 147A8540, AND 147A5700.SDR AALA201809265003Floorbeam · corrodedCORROSION ON THE TOP OF THE FLOORBEAM TEE NEAR THE LAVATORY MOUNTS AND FASTENER HOLES AT BS 947.5, LBL 52 TO RBL 52. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-5.SDR AALA201809265002Web · corrodedCORROSION FOUND ON THE WEB BETWEEN BS 967 TO 986, LBL 52. REPLACED THE WEB IAW 51-00-05-1, DRAWING 147A8501, AND EA 285077, DRAFT 2.SDR AALA201809265001Web · corrodedCORROSION FOUND ON THE WEB BETWEEN BS 967 TO 986, RBL 52. REPLACED THE WEB IAW 51-00-05-1, DRAWING 147A5710, AND EA 285077.SDR AALA201809254005Floorbeam · corrodedCORROSION WAS FOUND ON THE TOP OF TEE CAP ON THE FLOORBEAM AT BS 986, LBL 52 - RBL 52. REPLACED THE FLOORBEAM TEE IAW SRM 53-70-51-2R.SDR AALA201809254002Web · corrodedCORROSION WAS FOUND ON FLOOR WEB AT BS 986 - 1016 , RBL 32 - 50. REPLACED THE WEB IAW 51-00-05.SDR AALA201809275010Transition Panel · corrodedCORROSION FOUND ON THE LEFT TRANSITION PANEL AT STATIONS 453-480 IN THE FWD CARGO BAY. REPLACED THE TRANSITION PANEL IAW SRM 51-10-2, PAR.9, AND SRM 53-00-53-2R.SDR AALA201809265011Transition Panel · corrodedFORWARD CARGO, RIGHT TRANSITION PANEL, BS 500A - 500I HAD MANY AREAS OF CORROSION. REPLACED THE TRANSITION PANEL IAW SRM 51-10-2 PAR 9, AND SRM 53-00-53-2R.SDR AALA201810086008Scuff Plate · corrodedCORROSION AROUND AFT CARGO DOOR CUTOUT LOWER CORNER SCUFF PLATE BETWEEN BS 788 TO 809, STRINGER 22R TO STRINGER 26R. INSTALLED A REPAIR DOUBLER IAW EA 285202.SDR AALA201809254007Splice Angle · corrodedCORROSION FOUND ON THE FLOORBEAM SPLICE ANGLE AT BS 887, BETWEEN RBL 20 TO LBL 20, AFT CARGO AREA. REPLACED THE FLOORBEAM SPLICE ANGLE IAW SRM 51-10-02.SDR AALA201809263002Transition Panel · corrodedCORROSION FOUND ON THE AFT CARGO, RIGHT TRANSITION PANEL, BS 847 TO 867. REPLACED THE TRANSITION PANEL IAW SRM 51-10-02, 51-00-05, AND DRAWING 146A8127.SDR AALA201809210008Transition Panel · corrodedCORRODED ON THE RIGHT TRANSITION PANEL IN THE AFT CARGO BETWEEN BS 867 TO 887. REPLACED THE TRANSITION PANEL IAW SRM 21-10-02, AND SRM 51-40-02.SDR AALA2018092019004Strap · corrodedCORROSION ON AFT CARGO DOOR SILL STRAP BETWEEN BS 790 AND 797. REPLACED THE STRAP IAW 51-00-05, SRM 51-10-02, AND DRAWING 146A8128.SDR AALA2018100128009Floor Support · corrodedCORROSION FOUND ON THE AFT CABIN FLOOR SUPPORT, BS 947 - 967, RBL 50. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.SDR AALA201806259004Window Shade · defectiveAIRCRAFT WAS NOT GROUNDED. COACH SEAT WINDOW SHADE/HANDLE SEAT 14F EMERGENCY EXIT WINDOW SHADE WILL NOT RETRACT. **SUPPLEMENT TO BE FILED UPON FINAL CORRECTIVE ACTION. (OPEN)SDR AALA201712299010Slide · dislodgedR1 DOOR SLIDE HANGING OUT OF HOUSING. ADJUSTED AND SECURED THE DOOR SLIDE IAW MM 25-66-00.SDR AALA201712129017Light · damagedAIRCRAFT WAS NOT GROUNDED. DURING INTERIOR CABIN CHECK, AFT LEFT EXIT LIGHT ASSEMBLY, WAS FOUND DAMAGED. REPLACED EXIT LIGHT ASSEMBLY PER AMM 33-51-01. OPERATIONAL CHECK GOOD.SDR AALA201712129022Light · damagedAIRCRAFT WAS NOT GROUNDED. DURING INTERIOR CABIN CHECK, RIGHT AFT EXIT LIGHT ASSEMBLY WAS FOUND DAMAGED. REPLACED AFT RIGHT EXIT LIGHT ASSEMBLY PER AMM 33-51-01. OPERATIONAL CHECK OK.SDR AALA20171211001Light · damagedAIRCRAFT WAS NOT GROUNDED. DURING INTERIOR CABIN CHECK FOUND RIGHT AFT EXIT LIGHT ASSEMBLY DAMAGED. REPLACED AFT RIGHT EXIT LIGHT ASSEMBLY PER AMM 33-51-01. OPERATIONAL CHECK GOOD.
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