N802WA
Service difficulty reports · 51
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 = 'N802WA' 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 = 'N802WA' 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 2WAA2026FA0000318Light · inoperativeDURING PREFLIGHT INSPECTION, FLIGHT CREW REPORTED THAT THE TAIL CONE LIGHT WAS INOPERATIVE. ADDITIONALLY, WHEN THE EMERGENCY LIGHTING SYSTEM WAS ACTIVATED, MULTIPLE CEILING LIGHTS DID NOT ILLUMINATE AS REQUIRED. THE EMERGENCY EXIT LIGHT AT THE L2 DOOR WAS ALSOSDR 2026F00068Slide · no testDURING DAILY CHECK, LOW PRESSURE INDICATION WAS NOTED ON THE L2 EVACUATION SLIDE. TROUBLESHOOTING CONFIRMED EVACUATION SLIDE PRESSURE WAS BELOW ACCEPTABLE LIMITS. THE L2 EVACUATION SLIDE WAS REMOVED AND REPLACED WITH A SERVICEABLE OVERHAULED UNIT IN ACCORDANCESDR 2WAA202602230015Portable Light · inoperativeDURING PRE-FLIGHT CHECK FOUND L1 DOOR EMERGENCY EXIT PORTABLE LIGHT INOPERATIVE.SDR 2025F00266Bulb · inoperativeC-CHECK NON-ROUTINE, FOUND CEILING EMERGENCY LIGHTS INOP ON ROWS RH 2, 5, 8, 11 AND 15.SDR 2025F00263Light · inoperativeC-CHECK NON-ROUTINE, DURING ACCOMPLISHING TASK 33-051-01-01 OVER WING EMERGENCY EVACUATION LIGHTS RT FWD FOUND INOPERATIVESDR 2025F00262Light · inoperativeC-CHECK NON-ROUTINE, DURING ACCOMPLISHING TASK 33-051-01-01 OVER WING EMERGENCY EVACUATION LIGHTS, RT FWD FOUND INOPERATIVE.SDR 2025F00265Battery · dischargedC-CHECK NON-ROUTINE, MAIN CABIN FWD EMERGENCY LIGHT TEST FAILED. EMERGENCY LIGHT BATTERY CHARGED 30 HRS PASSED TEST NO DEFECTSDR 2025F00264Bulb · inoperativeC-CHECK NON-ROUTINE, DURING ACCOMPLISHING TASK 33-051-01-01 EMERGENCY LIGHT TAIL CONE COMPARTMENT FOUND INOPERATIVE.SDR 2WAA20250401086Engine · failedLH ENGINE FAILURE AFTER TAKEOFFSDR 2024F00139Clamp · looseDURING CRUISE FLOW LIGHT ON AND DURING DESCENT CABIN ALTITUDE LIGHT ON, CABIN OXYGEN LIGHT ON , OXYGEN MASKS DEPLOYED. THE CORRECTIVE ACTION RESECURED CLAMPS OF A/C COMPONENTES AT AFTER PRESSURE BULKHEAD, FUNCTIONAL TEST OF CABIN PRESSURE CONTROL SYSTEM I.A.W SDR 2024F00015Oven · odorCREW DISCREPANCY REPORT (CDR) #1 FWD CABIN GALLEY OVEN SMELL OF BURNED PLASTIC WHEN IN USE (LEFT SIDE) LP27780. OEM: BUDERUS SELL GMBH GERMANYSDR 2WAA201908200114Window · brokenDURING WALK-AROUND, DISCOVERED PASSENGER CABIN WINDOW AT ROW 11 R/H WAS DAMAGED AND ENTERED THE #2 ENGINE. R/R PASSENGER CABIN WINDOW AT ROW 11 RH IAW MD-80 AMM 56-20-00SDR 2WAA20190820014Engine · failed1. RIGHT ENGINE FAILURE DURING CRUISE, FOLLOWED QRH PROCEDURES AND DIVERTED TO BRO, DECLAIRED EMERGENCY UNEVENTFUL LANDING. 2. DURING WALK-AROUND, DISCOVERED PASSENGER CABIN WINDOW AT ROW 11 R/H WAS DAMAGED. 1. DURING T/S FOUND #2 ENGINE HAD CONSIDERABLE FOD DSDR 2WAA2019051600001Battery Pack · dischargedFWD CABIN EMERGENCY LIGHT BATTERY PACK INOP. R/R FWD CABIN EMERGENCY LIGHT BATTERY PACK IAW AMM 33-53-00.SDR 2WAA2018009060000Heat Exchanger · crackedAFTER TAKE OFF RED "TAIL COMPARTMENT TEMP HIGH" AND "MASTER WARNING" LIGHT ILLUMINATED. INSPECTED TAIL COMPARTMENT FOUND AIR LEAK AT LT PACK PNEUMATIC DUCT. PERFORMED INSPECTION AND CHECK OF LT SECONDARY HEAT EXCHANGER AND FOUND CRACKED. R&R LT SECONDARY HEAT SDR 2WAA2018073029001Not Reported · malfunctionedON TAKE OFF RT ENGINE APPROACHED CAUTION ZONE EGT. AFTER TAKE OFF RT ENGINE EGT 75 DEGREES CELSIUS HIGHER THAN LT ENGINE 560 DEGREES CELSIUS OIL TEMP EXCEEDED 130 DEGREES CELSIUS. FUEL FLOW RT ENGINE 1000 PPH HIGHER THAN LT ENGINESDR 2WAA201807210001Duct · leakingDURING CLIMB THRU FL270 TAIL COMPARTMENT TEMP HIGH ANNUNCIATOR LIGHT ON. FOUND PRIMARY HEAT EXCHANGER DUCT LEAKING. R&R PRIMARY HEAT EXCHANGER DUCT. NO LEAKS NOTED. OPS CHECK NORMAL.SDR 2WAA2018071970001Pump · malfunctionedAFT CENTER FUEL PUMP IS NOT PASSING TEST DURING PREFLIGHT.SDR 2WAA201808100711Bulb · burned outSMOKE REPORTED IN CABIN. FOUND ROW 2AB SIDEWALL UPPER LIGHT WALL SOCKET HAD AN ELECTRICAL ODOR AND SMOKE. REMOVED A BURNED OUT BULB AT SECTION 2AB IAW 33-21-03. SMOKE WAS CLEARED AND NO ODOR.SDR 2WAA201805181001Pump · failedFWD & AFT CENTER FUEL BOOST PUMP CIRCUIT BREAKER TRIPPED DURING FLIGHT. TROUBLESHOT THE FUEL PUMPS CONTINUITY AND RESISTANCE CHECKED UNSATISFACTORY IAW AMM 28-20-07. REMOVED AND REPLACED THE FUEL BOOST PUMPS FWD AND AFT IAW AMM 28-20-07. OPS CHECKED NORMALSDR 2WAA2018051800011Pump · failedFWD & AFT CENTER FUEL TANK BOOST PUMP CIRCUIT BREAKER TRIPPED DURING FLIGHT. TROUBLESHOT THE FUEL PUMP CONTINUITY AND RESISTANCE, CHECKED UNSATISFACTORY IAW AMM 28-20-07. REMOVED AND REPLACED THE FUEL BOOST PUMPS FWD AND AFT IAW AMM 28-20-07. OPS CHECKED TSDR 2WAA201801240001Apu · leakingAFTER LANDING AIRCRAFT WITH APU RUNNING AND 1 PACK ONLINE (RIGHT), SMOKE WAS PRESENT IN CABIN. APU TEMPERATURE RED LINE. REMOVED AND REPLACED APU IAW AMM 49-10-00. OPS CHECK NORMAL.SDR 2WAA201711170001Pressure System · malfunctionedAIRCRAFT FAILED TO PRESSURIZE AFTER TAKE OFF.SDR 2WAA2017111000001Controller · defectiveAIRCRAFT FAILED TO PRESSURIZE AFTER TAKE OFF. FOUND TO BE THE CABIN PRESSURE CONTROLLER.SDR 2WAA201740922Suppression Sys · malfunctionedCARGO DETECTION SUPPRESSION PANEL, ALL LIGHTS ILLUMINATED. PERFORMED TROUBLESHOOTING OF SMOKE DETECTION, FIRE SUPPRESSION SYSTEM IAW AAELTD SMOKE DETECTION STC DRAWINGS FC03-0282 AND -0283 AND MD80AMM 26-10-00. FOUND PIN NR 7 GROUNDED. RESEATED THE PIN IAW SWSDR 2WAA20170926001Computer · faultyDURING CLIMB DFGP INOP, FIRST OFFICER FLIGHT MODE ANNUNCIATOR INOP, AUTO THROTTLE SYSTEM INOP.SDR 2WAA201703170001Cooling Turbine · defectiveDURING CRUISE AT FL290, CABIN ALT STARTED TO CLIMB, RT PACK PRESS BEGAN OSCILLATING, FLOW LIGHT ILLUMINATED, PERFORMED QRH PROCEDURE AND BEGAN AND EMERGENCY DECENT. TROUBLE SHOT SYSTEM TO A DEFECTIVE RIGHT COOLING TURBINE. REMOVED AND REPLACED RT COOLING TURBISDR 2WAA20170206001Flap System · malfunctionedWHILE ON APPROACH, AFTER SELECTING FLAPS 11, THE AIRCRAFT WENT INTO A FLAP ASYMMETRIC CONDITION. EXTENDED THE DOWNWIND LEG WHILE REVIEWING THE QRH. A SLAT ONLY LANDING WAS EXECUTED WITH NO FURTHER ISSUES.SDR 2WAA20161213001Adapter · not reportedAT FL350 CABIN PRESSURE WAS LOST AND CABIN ALTITUDE ANNUNCIATOR ILLUMINATED.SDR 2WAA201608090001Sensing Element · out of positionFIRE DETECTOR LOOP-B FAULT, FIRE DETECTOR LOOP-A NORMAL. TS ENGINE FIRE DETECTION SYSTEM IAW AMM 26-10-00. FOUND SENSING ELEMENT ON ENGINE NR 2 GROUNDED, SPACED ELEMENT AND PERFORMED OPS TEST IAW AMM 26-10-00. OPERATIONAL TEST NORMAL.SDR 2WAA20150930001Engine · failedRIGHT ENGINE FAILURE AFTER TAKEOFF. EVENT HAPPENED ABOUT 1000 FT. ENGINE MADE A LOUD BANG, SUSPECTED CATASTROPHIC FAILURE. THRUST LOST IMMEDIATELY. R & R RT ENGINE. ACCOMPLISHED LEAK CHECK AND RUN-UP, NO LEAKS NOTED. CHECKED NORMAL IAW T/C 71-900-01-01 ANSDR 2WAA20150827007Interphone · inoperativeCOCKPIT PA LIGHT DOES NOT STAY ON WHEN PRESSED. UNABLE TO USE PA INTERPHONE.SDR 2WAA20150821004Handset · brokenAFT F/A BS HAND SET INOPERATIVE. PA BOTTOM BROKEN. R & R AFT F/A BS INTERPHONE HANDSET IAW AMM 23-40-04. PERFORMED OPS CHECK, OPS CK GOOD.SDR 2WAA20150812002Battery Pack · dischargedSEVERAL EMERGENCY EXIT IDENTIFIERS OUT FROM AFT GALLEY TO AFT STAIRWAY. TROUBLESHOT EXIT IDENTIFIER LIGHTS IAW AMM 33-53-00, PAGE 501 AND FOUND AFT BATTERY CHARGER AT FAULT. REMOVED AND INSTALLED AFT BATTERY CHARGER IAW AMM 33-53-00. OPS NORMAL.SDR 2WAA20150801001Engine · bird ingestionBIRD STRIKE, NORMAL INDICATIONS. DURING CRUISE LEFT ENGINE FLUCTUATIONS. PRECAUTIONARY SHUTDOWN. REMOVED NR 1 ENG SN 709818 IAW WAA TC 71-900-01-01. INSTALLED NR 1 ENG SN 717360 IAW WAA TC 71-900-01-01. LEAK CHECK GOOD PENDING OPERATIONS CHECK. TRIM & RUNSDR 2WAA20150130002Detector Loop · looseLOOP "A" APU LIGHT COMES ON IN FLIGHT. APU OFF. T/S APU FIRE DETECTION SYS, FOUND RT LOOP "A" CONNECTOR LOOSE. TIGHTENED CONNECTOR. OPS CHECK NORMAL IAW MM 26-10-02.SDR 2WAA20140715002Flashlight · inoperativeDOORWAY L-1 FLASHLIGHT NOT WORKING. REMOVED AND REPLACED FLASHLIGHT IAW MM 33-53-00. OPS CHECKED NORMAL.SDR 2WAA20140702001Valve · leakingNLG FAILED TO RETRACT AFTER TAKEOFF, AN AIR TURNBACK WAS EXECUTED. TROUBLESHOOTING FOUND NLG STRUT FLUID LOW. R & R SERVICING VALVE, SERVICED FLUID AND NITROGEN IAW AMM 32-21-02. OPS CHECKED NORMAL.SDR 2WAA201405002Nut · missingDURING WALK-AROUND, FOUND NR 3 MWA NUT MISSING. R & R NR 3 MWA IAW 32-40-01.SDR 2WAA20140502001Engine · fireWHILE STARTING NR 1 ENGINE ON TAXI WAY, TOWER REPORTED FLAME FROM TAIL PIPE. RETURN TO GATE. INSPECTED NR 1 ENGINE INLET AND EXHAUST, NO DISCREPANCIES NOTED AT THIS TIME, AMM 72-00-00.SDR 2WAA20140128002Battery Pack · defectiveMAIN CABIN EMERGENCY LIGHTS ROW 5 AND 6 INOPERATIVE. R & R MAIN CABIN EMERGENCY BATTERY PACK IAW AMM 33-53-00. OPS NORMAL.SDR 2WAA20131224002Moisture Trap · unsecureDURING CLIMBOUT WHEN POWER REDUCED TO CLIMB THRUST VIBRATION ON RT ENGINE FOLLOWED BY FLAME OUT. PERFORMED GENERAL VISUAL INSPECTION OF RT ENGINE FOUND PRESSURE SENSE LINE FUEL CONTROL AT MOISTURE TRAP NOT SECURED. SECURED LINE AT MOISTURE TRAP IAW AMM 73-20SDR 2WAA20140319005Battery Pack · deactivatedDURING SERVICE CHECK, FOUND LT AND RT OVER WING EMERGENCY EXIT LIGHTS INOPERATIVE. R & R BATTERY POWER SUPPLY IAW AMM 33-53-00, CHECKED NORMAL.SDR 2WAA20131119001Sensor · out of adjustUNABLE TO RETRACT GEAR, RETURNED TO DEPARTURE. INSPECTION FOUND GROUND SENSING MECHANISM OUT OF ADJUSTMENT. ADJUSTED GROUND SENSING MECHANISM IAW AMM 32-23-01. PERFORMED EXTENSION AND RETRACTION TEST IAW AMM 32-30-00, CHECKED NORMAL.SDR 2WAA2012FA0000302Acm · failedDURING CRUISE AT FL 320 BOTH AUTO CONTROLS FAILED, UNABLE TO CONTROL CABIN, DECLARED AN EMERGENCY FOLLOWED QRH PROCEDURES. AIRCRAFT WAS READIED FOR MX FERRY FROM SJU TO MIA FOR REPAIRS. MX REMOVED AND REPLACED PERISEALS ON THE RIGHT SIDE PACK TURBINE INLET CSDR 2012FA0000301Unknown · smokeLIGHT SMOKE & HASE IN CABIN WAS REPORTED.SDR 2WAA20110125Motor · failedSMOKE IN COCKPIT, DECLARED EMERGENCY, DIVERTED. DISASSEMBLED, CLEANED AND INSPECTED UNIT IAW 27-60-07 REV NR 6, DATED 8/15/06. FOUND MOTOR ASSY DAMAGED, VARIOUS HARDWARE DAMAGED, CAPACITOR LEAKING, RECTIFIER OPEN, BEARINGS WORN, GEAR TRAIN LUBRICATION DRY, DASDR 2WAA20101227Hydraulic System · leakingAFTER SLAT EXT DURING THE APP, LT HYD SYS PRESSURE CYCLES TO ZERO PRESS, QTY NORMAL.SDR 2WAA20111810Wire · brokenAFTER TAKEOFF, LANDING GEAR DID NOT RETRACT, ACFT WOULD NOT PRESSURIZE.SDR 2WAA20101110Wire · brokenAFTER TAKE OFF, LANDING GEAR DID NOT RETRACT, A/C WOULD NOT PRESURIZE.
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