N836AW
Service difficulty reports · 155
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 = 'N836AW' 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 = 'N836AW' 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 AALA202201034225Pin · disengagedAIRCRAFT WAS NOT GROUNDED: AIRCRAFT RIGHT OVERWING EMERGENCY EXIT NOT ARMED. FOUND AIRCRAFT RIGHT SLIDE DISARM PIN, DIS-ENGAGED. RE-ARMED, ALL INDICATIONS NORMAL. OK FOR SERVICE PER AMM 52-21-11-400-001-A.SDR AALA202111221601Engine · stalledAIRCRAFT WAS GROUNDED: ON CLIMB OUT THROUGH 18,000 FEET, THE RIGHT ENGINE SURGED TWICE FOLLOWED BY A LOUD BANG. EGT STARTED CLIMBING, ECAM WARNING OF EGT OVER LIMT. CREW MOVED THROTTLE TO IDLE AND EGT CONTINUED TO CLIMB AND ENGINE WAS PREPARING TO SHUTDOWN WHESDR AALA202111191601Engine · stalledAIRCRAFT WAS GROUNDED: ON CLIMB OUT THROUGH 18,000 FEET, THE RIGHT ENGINE SURGED TWICE FOLLOWED BY A LOUD BANG. EGT STARTED CLIMBING, ECAM WARNING OF EGT OVER LIMT. CREW MOVED THROTTLE TO IDLE AND EGT CONTINUED TO CLIMB AND ENGINE WAS PREPARING TO SHUTDOWN WHESDR AALA202107265981Wire Harness · chafedAIRCRAFT WAS GROUNDED: #1 ENG IDG FEEDER CABLE ":A" WIRE HARNESS CHAFFED THROUGH INSULATION. REPLACED IDG FEEDER CABLE ":A" WIRE HARNESS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 24-21-43.SDR AALA202105279005Cylinder · failedAIRCRAFT IN BASE MAINTENANCE: L1 DOOR, DOOR DAMPER FAILED OPERATIONAL CHECK. REPLACED DOOR DAMPER/EMERGENCY CYLINDER PER AMM 52-11-14.SDR AALA202001159046Hinge Fitting · wornAIRCRAFT WAS GROUNDED: LEFT ELEVATOR NR 3 HINGE HAS EXCESSIVE PLAY / WEAR ON THE LEFT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA202001159045Hinge Fitting · wornAIRCRAFT WAS GROUNDED: LEFT ELEVATOR NR 2 HINGE HAS EXCESSIVE PLAY / WEAR ON THE LEFT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA202001159044Hinge Fitting · wornAIRCRAFT WAS GROUNDED: RIGHT ELEVATOR NR 3 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA202001159043Hinge Fitting · wornAIRCRAFT WAS GROUNDED: RIGHT ELEVATOR NR 5 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA2020011439084Hinge Fitting · wornAIRCRAFT WAS GROUNDED: RIGHT ELEVATOR NR 6 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA2020011439083Hinge Fitting · wornAIRCRAFT WAS GROUNDED: RIGHT ELEVATOR NR 4 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA2020011439082Hinge Fitting · wornAIRCRAFT WAS GROUNDED: RIGHT ELEVATOR NR 2 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA2020011439081Hinge Fitting · wornAIRCRAFT WAS GROUNDED: RIGHT ELEVATOR NR 1 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA2020011439080Hinge Fitting · wornAIRCRAFT WAS GROUNDED: LEFT ELEVATOR NR 6 HINGE HAS EXCESSIVE PLAY / WEAR ON THE LEFT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA2020011439079Hinge Fitting · wornAIRCRAFT WAS GROUNDED: LEFT ELEVATOR NR 5 HINGE HAS EXCESSIVE PLAY / WEAR ON THE LEFT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA2020011439078Hinge Fitting · wornAIRCRAFT WAS GROUNDED: LEFT ELEVATOR NR 4 HINGE HAS EXCESSIVE PLAY / WEAR ON THE LEFT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA2020011439077Hinge Fitting · wornAIRCRAFT WAS GROUNDED: LEFT ELEVATOR NR 1 HINGE HAS EXCESSIVE PLAY / WEAR ON THE LEFT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA2020011539074Hinge · wornAIRCRAFT WAS GROUNDED: RUDDER HINGE NR 4 HAS EXCESSIVE PLAY / WEAR AT RIB 6 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.SDR AALA2020011439076Hinge · wornAIRCRAFT WAS GROUNDED: RUDDER HINGE NR 7 HAS EXCESSIVE PLAY / WEAR AT RIB 11 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.SDR AALA2020011439075Hinge · wornAIRCRAFT WAS GROUNDED: RUDDER HINGE NR 5 HAS EXCESSIVE PLAY / WEAR AT RIB 7 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.SDR AALA2020011439073Hinge · wornAIRCRAFT WAS GROUNDED: RUDDER HINGE NR 3 HAS EXCESSIVE PLAY / WEAR AT RIB 5 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.SDR AALA2020011439072Hinge · wornAIRCRAFT WAS GROUNDED: RUDDER HINGE NR 2 HAS EXCESSIVE PLAY / WEAR AT RIB 4 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.SDR AALA2020011439071Hinge · wornAIRCRAFT WAS GROUNDED: RUDDER HINGE NR 1 HAS EXCESSIVE PLAY/WEAR AT RIB 2 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.SDR AALA201908139011Water Heater · overtempAIRCRAFT WAS GROUNDED: FORWARD LAVATORY WATER HEATER EXCEEDED NORMAL TEMPERATURE, ECAM MESSAGE DISPLAYED LAVATORY FIRE-SMOKE MESSAGE. MAINTENANCE REPLACED WATER HEATER PER AMM 38-12-16.SDR AALA201908059012Battery · no testAIRCRAFT WAS NOT GROUNDED: AISLE JUMPSEAT FLASHLIGHT WAS NOT CHARGING. MAINTENANCE REPLACED BATTERY PER AMM 25-60-00.SDR AALA2018112769018Smoke Detector · false indicationLAVATORY SMOKE WARNING, FLIGHT ATTENDANT TURNED OFF THE RIGHT AFT LAVATORY E. MAINTENANCE TROUBLESHOT THE SMOKE WARNING IAW TSM 26-17-00-819-801-A , NO FAULTS FOUND.SDR AALA2018090549037Switch · malfunctionedEMERGENCY EXIT OFF LIGHT DISAGREES WITH ARM SWITCH. OPERATED EMERGENCY LIGHT SWITCH SEVERAL TIMES, LIGHT CORRESPONDS WITH SWITCH IAW AMM 33-51-00.SDR AALA201805259004Sliding Window · delaminatedCAPTAIN`S SLIDING WINDOW DELAMINATED AT THE TOP AND CRACKING AFT FROM EDGE. ACCOMPLISHED INSPECTION OF CAPTAIN SLIDING WINDOW IAW 56-12-11-200-001-A, CHECKED AND FOUND TO BE WITHIN LIMITS. REPLACED L2 SLIDING WINDOW ASSEMBLY IAW AMM 56-12-11.SDR AALA201803059014Hook And Loop · wornSLIDE CAUTION INDICATOR, YELLOW STRAP, WILL NOT STAY AFFIXED TO THE R1 DOOR. REPLACED THE HOOK AND LOOP FOR THE STRAP, SECURE. OPS CHECKED GOOD.SDR AALA201803059024Sliding Window · delaminatedAIRCRAFT WAS GROUNDED. FLIGHT OFFICER'S SLIDING SIDE WINDOW SHOWING DELAMINATION IN TWO AREAS, BOTTOM MIDDLE AND BOTTOM RIGHT. WINDOW IS ALSO VERY HOT. REPLACED FLIGHT OFFICER'S SLIDING WINDOW PER AMM 56-12-11.SDR AALA201803019007Cover · unsecureLEFT EMERGENCY EXIT DOOR ECAM CAB V/S NORMAL. SECURED PULL COVER FOR THE LEFT EMERGENCY DOOR OVERWING EXIT.SDR AALA201802229024Slide · debondedLEFT OVERWING SLIDE ASSEMBLY WAS DISBONDED. MAINTENANCE REPLACED THE SLIDE ASSEMBLY AND PERFORMED SATISFACTORY OPERATIONAL CHECK.SDR AALA201802079002Lug · corrodedCOMPOSITE DAMAGE AT THE INBD SERVO LUG, CORROSION UNDER THE STATIC WICK MOUNT. REPLACED THE RIGHT AILERON IAW AMM 27-14-41.SDR AALA201802019018Floor Support · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. CORROSION AT FASTENER HOLES OF R2 DOOR FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT PER SRM 51-42-11SDR AALA201801269008Shear Web · corrodedCRACK AND CORROSION ON TOP SURFACE OF RIGHT AFT SHEAR WEB. REPLACED THE SHEAR WEB IAW EO 5315Y015, AND SRM 51-42-11.SDR AALA201802029012Door Sill · corrodedCORROSION ON R2 DOOR THRESHOLD SILL PLATE BEAM NUTPLATE AREAS AT FRAME 68 AND STRINGER 23R. REPAIRED R2 DOOR THRESHOLD SILL PLATE BEAM IAW SRM 51-41-14-300-01.SDR AALA201802019005Plate · corrodedCORRODED PLATE ON THE L2 DOOR THRESHOLD, 1 INCH FORWARD OF FRAME 68, 2 INCHES INBOARD OF DOOR OPENING. REPLACED THE PLATE IAW SRM 51-42-11, AND DRAWING D53480076.SDR AALA201801269007Shear Web · crackedCRACK AND CORROSION ON THE TOP SURFACE OF THE AFT SHEAR WEB BETWEEN FRAMES 66 TO 68, +Y54. REPLACED THE SHEAR WEB IAW EO 5315Y015, AND SRM 51-42-11.SDR AALA201801269006Angle · corrodedCORRODED CORNER ANGLE AT FRAME 64 PLUS 1 INCH, INBOARD FROM OUTER SKIN. REPLACED THE ANGLE IAW SRM 52-41-11.SDR AALA201801249001Mount · corrodedCORRODED AFT ENGINE MOUNT SHEAR PINS. REPLACED AFT ENGINE MOUNT IAW AMM 71-22-11-400.SDR AALA201802129019Threshold · corrodedCORROSION FOUND ON THE L2 DOOR THRESHOLD FORWARD END AT NUTPLATE HOLE, FRAME 66. REPLACED THE THRESHOLD PLATE IAW SRM 51-42-12, AND DRAWING 53480076.SDR AALA201802129018Threshold · corrodedCORROSION FOUND ON THE L2 DOOR THRESHOLD AT FORWARD GIRT BAR FITTING ATTACH POINT. REPLACED THRESHOLD PLATE IAW SRM 51-42-12.SDR AALA201802129017Threshold · corrodedCORROSION FOUND UNDER THE CENTER CARGO TRACK ON THE AFT CARGO DOOR THRESHOLD PLATE. REPLACED THE THRESHOLD PLATE IAW SRM 51-42-11, AND DWG 17 E534 76320.SDR AALA201802019004Floorbeam · corrodedCORRODED FLOORBEAM AT FRAME 66, Y1292. REPLACED THE FLOORBEAM IAW SRM 51-42-11.SDR AALA201802019003Angle · corrodedCORRODED AFT CORNER ANGLE TO L2 DOOR CUT OUT AT FRAME 68, STRINGER 23L, LBL 66. REPLACED THE ANGLE IAW DRAWING 53480505, AND SRM 51-42-11.SDR AALA201802019002Door Sill · corrodedCORRODED DOOR SILL AT FRAME 68, STRINGER 23L, LBL 66. REPLACED THE DOOR SILL IAW SRM 51-42-11, AND DRAWING 53480076.SDR AALA201801269005Angle · corrodedCORROSION FOUND ON THE CENTER ANGLE OF THE L2 DOOR THRESHOLD, FRAME 66 PLUS 8 INCHES, .050 INCHES INBOARD OF DOOR OPENING, STRINGER 23L. REPLACED THE THRESHOLD ANGLE IAW SRM 51-42-11.SDR AALA201712289026Line · leakingMODERATELY STRONG ODOR IN COCKPIT AFTER TAKEOFF AND DURING CRUISE. NO SMOKE OR FUMES VISIBLE. SWEET ODOR LIKE PERFUME OR CLEANER. FOUND APU TO BE SOURCE OF THE COCKPIT ODOR. RETURN OIL LINE FROM LUBE MODULE TO OIL COOLER INBOARD WAS LEAKING. ACCOMPLISHED JSDR AALA201712279004O-Ring · damagedTHE AIRCRAFT WAS GROUNDED. AIRCRAFT COCKPIT AND CABIN FILLED WITH OIL FUMES (SMOKE) AFTER TAKE OFF. THE FLIGHT RETURNED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. FOUND LEAK (OIL) FROM CAP OF REGULATOR AND RELIEF VLV ASSY. REPLASDR AALA201707319051Sdac · faultedFLIGHT WARNING SYSTEM SDAC 2 FAULT Q6, SDAC 2 POWER CIRCUIT BREAKER TRIPPED, ASSOCIATED WITH ELECTRICAL ODOR IN THE FLIGHT DECK. REPLACED THE RN 2 SDAC IAW MM 31-55-34-400. ACCOMPLISHED SATISFACTORY SYSTEM OPERATIONS CHECKS IAW 31-50-00-710-003.
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