# Service difficulty reports: N802WA

A list on [N802WA](https://openairdocs.org/aircraft/N802WA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 51 reports

- [SDR 2WAA2026FA0000318](https://openairdocs.org/sdr/2WAA2026FA0000318.md): Light · inoperative · May 1, 2026 · N802WA · Doug MD83 · Emergency Lighting
  > DURING 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 ALSO
- [SDR 2026F00068](https://openairdocs.org/sdr/2026F00068.md): Slide · no test · Apr 10, 2026 · N802WA · Doug DC983 · Emergency Equipment
  > DURING 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 ACCORDANCE
- [SDR 2WAA202602230015](https://openairdocs.org/sdr/2WAA202602230015.md): Portable Light · inoperative · Feb 23, 2026 · N802WA · Doug DC983 · Emergency Equipment
  > DURING PRE-FLIGHT CHECK FOUND L1 DOOR EMERGENCY EXIT PORTABLE LIGHT INOPERATIVE.
- [SDR 2025F00266](https://openairdocs.org/sdr/2025F00266.md): Bulb · inoperative · Nov 11, 2025 · N802WA · Doug DC983 · Emergency Lighting
  > C-CHECK NON-ROUTINE, FOUND CEILING EMERGENCY LIGHTS INOP ON ROWS RH 2, 5, 8, 11 AND 15.
- [SDR 2025F00263](https://openairdocs.org/sdr/2025F00263.md): Light · inoperative · Nov 11, 2025 · N802WA · Doug DC983 · Emergency Lighting
  > C-CHECK NON-ROUTINE, DURING ACCOMPLISHING TASK 33-051-01-01 OVER WING EMERGENCY EVACUATION LIGHTS RT FWD FOUND INOPERATIVE
- [SDR 2025F00262](https://openairdocs.org/sdr/2025F00262.md): Light · inoperative · Nov 11, 2025 · N802WA · Doug DC983 · Emergency Lighting
  > C-CHECK NON-ROUTINE, DURING ACCOMPLISHING TASK 33-051-01-01 OVER WING EMERGENCY EVACUATION LIGHTS, RT FWD FOUND INOPERATIVE.
- [SDR 2025F00265](https://openairdocs.org/sdr/2025F00265.md): Battery · discharged · Nov 5, 2025 · N802WA · Doug DC983 · Emergency Lighting
  > C-CHECK NON-ROUTINE, MAIN CABIN FWD EMERGENCY LIGHT TEST FAILED. EMERGENCY LIGHT BATTERY CHARGED 30 HRS PASSED TEST NO DEFECT
- [SDR 2025F00264](https://openairdocs.org/sdr/2025F00264.md): Bulb · inoperative · Nov 5, 2025 · N802WA · Doug DC983 · Emergency Lighting
  > C-CHECK NON-ROUTINE, DURING ACCOMPLISHING TASK 33-051-01-01 EMERGENCY LIGHT TAIL CONE COMPARTMENT FOUND INOPERATIVE.
- [SDR 2WAA20250401086](https://openairdocs.org/sdr/2WAA20250401086.md): Engine · failed · Mar 31, 2025 · N802WA · Doug MD83 · Engine (Turbine/Turboprop)
  > LH ENGINE FAILURE AFTER TAKEOFF
- [SDR 2024F00139](https://openairdocs.org/sdr/2024F00139.md): Clamp · loose · May 24, 2024 · N802WA · Doug MD83 · Cabin Pressure Control System
  > DURING 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 2024F00015](https://openairdocs.org/sdr/2024F00015.md): Oven · odor · Jan 22, 2024 · N802WA · Doug MD83 · Buffet/Galleys
  > CREW DISCREPANCY REPORT (CDR) #1 FWD CABIN GALLEY OVEN SMELL OF BURNED PLASTIC WHEN IN USE (LEFT SIDE) LP27780. OEM: BUDERUS SELL GMBH GERMANY
- [SDR 2WAA201908200114](https://openairdocs.org/sdr/2WAA201908200114.md): Window · broken · Aug 14, 2019 · N802WA · Doug MD83 · Passenger Compartment Windows
  > DURING 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 56-20-00
- [SDR 2WAA20190820014](https://openairdocs.org/sdr/2WAA20190820014.md): Engine · failed · Aug 14, 2019 · N802WA · Doug MD83 · Engine (Turbine/Turboprop)
  > 1. 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 D
- [SDR 2WAA2019051600001](https://openairdocs.org/sdr/2WAA2019051600001.md): Battery Pack · discharged · May 16, 2019 · N802WA · Doug MD83 · Emergency Lighting
  > FWD CABIN EMERGENCY LIGHT BATTERY PACK INOP. R/R FWD CABIN EMERGENCY LIGHT BATTERY PACK IAW AMM 33-53-00.
- [SDR 2WAA2018009060000](https://openairdocs.org/sdr/2WAA2018009060000.md): Heat Exchanger · cracked · Aug 30, 2018 · N802WA · Doug MD83 · Cabin Cooling System
  > AFTER 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 2WAA2018073029001](https://openairdocs.org/sdr/2WAA2018073029001.md): Not Reported · malfunctioned · Jul 29, 2018 · N802WA · Doug MD83 · Engine Indicating System
  > ON 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 ENGINE
- [SDR 2WAA201807210001](https://openairdocs.org/sdr/2WAA201807210001.md): Duct · leaking · Jul 21, 2018 · N802WA · Doug MD83 · Air Distribution System
  > DURING 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 2WAA2018071970001](https://openairdocs.org/sdr/2WAA2018071970001.md): Pump · malfunctioned · Jul 17, 2018 · N802WA · Doug MD83 · Fuel Boost Pump
  > AFT CENTER FUEL PUMP IS NOT PASSING TEST DURING PREFLIGHT.
- [SDR 2WAA201808100711](https://openairdocs.org/sdr/2WAA201808100711.md): Bulb · burned out · Jul 11, 2018 · N802WA · Doug MD83 · Passenger Compartment Lighting
  > SMOKE 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 2WAA201805181001](https://openairdocs.org/sdr/2WAA201805181001.md): Pump · failed · May 11, 2018 · N802WA · Doug MD83 · Fuel Boost Pump
  > FWD & 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 NORMAL
- [SDR 2WAA2018051800011](https://openairdocs.org/sdr/2WAA2018051800011.md): Pump · failed · May 11, 2018 · N802WA · Doug MD83 · Fuel Boost Pump
  > FWD & 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 T
- [SDR 2WAA201801240001](https://openairdocs.org/sdr/2WAA201801240001.md): Apu · leaking · Jan 20, 2018 · N802WA · Doug MD83 · APU Core Engine
  > AFTER 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 2WAA201711170001](https://openairdocs.org/sdr/2WAA201711170001.md): Pressure System · malfunctioned · Nov 10, 2017 · N802WA · Doug MD83 · Cabin Pressure Control System
  > AIRCRAFT FAILED TO PRESSURIZE AFTER TAKE OFF.
- [SDR 2WAA2017111000001](https://openairdocs.org/sdr/2WAA2017111000001.md): Controller · defective · Nov 10, 2017 · N802WA · Doug DC983 · Cabin Pressure Control System
  > AIRCRAFT FAILED TO PRESSURIZE AFTER TAKE OFF. FOUND TO BE THE CABIN PRESSURE CONTROLLER.
- [SDR 2WAA201740922](https://openairdocs.org/sdr/2WAA201740922.md): Suppression Sys · malfunctioned · Sep 22, 2017 · N802WA · Doug MD83 · Detection System
  > CARGO 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 SW
- [SDR 2WAA20170926001](https://openairdocs.org/sdr/2WAA20170926001.md): Computer · faulty · Sep 22, 2017 · N802WA · Doug MD83 · Autopilot Computer
  > DURING CLIMB DFGP INOP, FIRST OFFICER FLIGHT MODE ANNUNCIATOR INOP, AUTO THROTTLE SYSTEM INOP.
- [SDR 2WAA201703170001](https://openairdocs.org/sdr/2WAA201703170001.md): Cooling Turbine · defective · Mar 13, 2017 · N802WA · Doug MD83 · Cabin Cooling System
  > DURING 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 TURBI
- [SDR 2WAA20170206001](https://openairdocs.org/sdr/2WAA20170206001.md): Flap System · malfunctioned · Feb 5, 2017 · N802WA · Doug MD83 · Trailing Edge Flap Control System
  > WHILE 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 2WAA20161213001](https://openairdocs.org/sdr/2WAA20161213001.md): Adapter · not reported · Dec 12, 2016 · N802WA · Doug MD83 · Cabin Pressure Control System
  > AT FL350 CABIN PRESSURE WAS LOST AND CABIN ALTITUDE ANNUNCIATOR ILLUMINATED.
- [SDR 2WAA201608090001](https://openairdocs.org/sdr/2WAA201608090001.md): Sensing Element · out of position · Jul 15, 2016 · N802WA · Doug DC983 · Fire Detection
  > FIRE 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 2WAA20150930001](https://openairdocs.org/sdr/2WAA20150930001.md): Engine · failed · Sep 30, 2015 · N802WA · Doug DC983 · Engine (Turbine/Turboprop)
  > RIGHT 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 AN
- [SDR 2WAA20150827007](https://openairdocs.org/sdr/2WAA20150827007.md): Interphone · inoperative · Aug 27, 2015 · N802WA · Doug DC983 · Interphone/Passenger Announcement (PA) System
  > COCKPIT PA LIGHT DOES NOT STAY ON WHEN PRESSED. UNABLE TO USE PA INTERPHONE.
- [SDR 2WAA20150821004](https://openairdocs.org/sdr/2WAA20150821004.md): Handset · broken · Aug 21, 2015 · N802WA · Doug DC983 · Interphone/Passenger Announcement (PA) System
  > AFT 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 2WAA20150812002](https://openairdocs.org/sdr/2WAA20150812002.md): Battery Pack · discharged · Aug 12, 2015 · N802WA · Doug DC983 · Emergency Lighting
  > SEVERAL 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 2WAA20150801001](https://openairdocs.org/sdr/2WAA20150801001.md): Engine · bird ingestion · Aug 1, 2015 · N802WA · Doug DC983 · Engine (Turbine/Turboprop)
  > BIRD 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 & RUN
- [SDR 2WAA20150130002](https://openairdocs.org/sdr/2WAA20150130002.md): Detector Loop · loose · Jan 29, 2015 · N802WA · Doug DC983 · Fire Detection
  > LOOP "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 2WAA20140715002](https://openairdocs.org/sdr/2WAA20140715002.md): Flashlight · inoperative · Jul 12, 2014 · N802WA · Doug DC983 · Emergency Equipment
  > DOORWAY L-1 FLASHLIGHT NOT WORKING. REMOVED AND REPLACED FLASHLIGHT IAW MM 33-53-00. OPS CHECKED NORMAL.
- [SDR 2WAA20140702001](https://openairdocs.org/sdr/2WAA20140702001.md): Valve · leaking · Jul 2, 2014 · N802WA · Doug DC983 · Nose/Tail Landing Gear Strut/Axle
  > NLG 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 2WAA201405002](https://openairdocs.org/sdr/2WAA201405002.md): Nut · missing · May 22, 2014 · N802WA · Doug DC983 · Main Landing Gear
  > DURING WALK-AROUND, FOUND NR 3 MWA NUT MISSING. R & R NR 3 MWA IAW 32-40-01.
- [SDR 2WAA20140502001](https://openairdocs.org/sdr/2WAA20140502001.md): Engine · fire · Apr 12, 2014 · N802WA · Doug DC983 · Engine (Turbine/Turboprop)
  > WHILE 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 2WAA20140128002](https://openairdocs.org/sdr/2WAA20140128002.md): Battery Pack · defective · Jan 28, 2014 · N802WA · Doug DC983 · Emergency Lighting
  > MAIN CABIN EMERGENCY LIGHTS ROW 5 AND 6 INOPERATIVE. R & R MAIN CABIN EMERGENCY BATTERY PACK IAW AMM 33-53-00. OPS NORMAL.
- [SDR 2WAA20131224002](https://openairdocs.org/sdr/2WAA20131224002.md): Moisture Trap · unsecure · Dec 24, 2013 · N802WA · Doug DC983 · Engine Fuel Distribution
  > DURING 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 73-20
- [SDR 2WAA20140319005](https://openairdocs.org/sdr/2WAA20140319005.md): Battery Pack · deactivated · Dec 5, 2013 · N802WA · Doug DC983 · Emergency Lighting
  > DURING 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 2WAA20131119001](https://openairdocs.org/sdr/2WAA20131119001.md): Sensor · out of adjust · Nov 19, 2013 · N802WA · Doug DC983 · Landing Gear Position and Warning
  > UNABLE 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 2WAA2012FA0000302](https://openairdocs.org/sdr/2WAA2012FA0000302.md): Acm · failed · Jun 15, 2012 · N802WA · Doug MD83 · Cabin Cooling System
  > DURING 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 C
- [SDR 2012FA0000301](https://openairdocs.org/sdr/2012FA0000301.md): Unknown · smoke · May 11, 2012 · N802WA · Doug MD83 · Air Distribution System
  > LIGHT SMOKE & HASE IN CABIN WAS REPORTED.
- [SDR 2WAA20110125](https://openairdocs.org/sdr/2WAA20110125.md): Motor · failed · Jan 25, 2011 · N802WA · Doug MD83 · Drag Control System
  > SMOKE 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, DA
- [SDR 2WAA20101227](https://openairdocs.org/sdr/2WAA20101227.md): Hydraulic System · leaking · Dec 21, 2010 · N802WA · Doug MD83 · Hydraulic System, Main
  > AFTER SLAT EXT DURING THE APP, LT HYD SYS PRESSURE CYCLES TO ZERO PRESS, QTY NORMAL.
- [SDR 2WAA20111810](https://openairdocs.org/sdr/2WAA20111810.md): Wire · broken · Nov 17, 2010 · N802WA · Doug MD83 · Landing Gear System Wiring
  > AFTER TAKEOFF, LANDING GEAR DID NOT RETRACT, ACFT WOULD NOT PRESSURIZE.
- [SDR 2WAA20101110](https://openairdocs.org/sdr/2WAA20101110.md): Wire · broken · Nov 17, 2010 · N802WA · Doug MD83 · Landing Gear System Wiring
  > AFTER TAKE OFF, LANDING GEAR DID NOT RETRACT, A/C WOULD NOT PRESURIZE.

Next page: https://openairdocs.org/aircraft/N802WA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N802WA/reports

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