# Service difficulty reports: N817AW A list on [N817AW](https://openairdocs.org/aircraft/N817AW.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 6 · 262 reports - [SDR AALA202610193105](https://openairdocs.org/sdr/AALA202610193105.md): Battery · inoperative · Oct 18, 2026 · N817AW · Airbus A319132 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: FWD FA JUMPSEAT FLASHLIGHT NOT WORKING. MAINTENANCE REPLACED BATTERY OK FOR SERVICE. - [SDR AALA202609225207](https://openairdocs.org/sdr/AALA202609225207.md): Power Supply · fault message · Sep 21, 2026 · N817AW · Airbus A319132 · Emergency Lighting > AIRCRAFT WAS GROUNDED: FAULT MESSAGE DISPLAYED DURING EMERGENCY LIGHTING SYSTEM TEST, - MAINTENANCE REPLACED THE FORWARD LEFT EMERGENCY POWER SUPPLY UNIT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38 - [SDR AALA202609229885](https://openairdocs.org/sdr/AALA202609229885.md): Pump · fault message · Sep 18, 2026 · N817AW · Airbus A319132 · Fuel Boost Pump > AIRCRAFT WAS NOT GROUNDED: FUEL LEFT TANK PUMP 2 LOW PRESSURE ON ECAM DURING DESCENT. (OPEN) - [SDR AALA202606155051](https://openairdocs.org/sdr/AALA202606155051.md): Life Vest · missing · Jun 12, 2026 · N817AW · Airbus A319132 · Life Jacket > AIRCRAFT WAS NOT GROUNDED: RAMP AGENT REPORTS SEAT 22D LIFE VEST MISSING AFTER SECURITY SEARCH. MAINTENANCE INSTALLED NEW LIFE VEST PER AMM 25-66-52. - [SDR AALA202507147840](https://openairdocs.org/sdr/AALA202507147840.md): Battery · discharged · Jul 13, 2025 · N817AW · Airbus A319132 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT JUMP SEAT FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT BATTERY IAW DRAWING NUMBER DFB1081. - [SDR AALA202412233473](https://openairdocs.org/sdr/AALA202412233473.md): Power Supply · no test · Dec 23, 2024 · N817AW · Airbus A319132 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: EPSU BATTERY EMER L, FAULT ON PTP PANEL. T/S PERFORMED IAW TSM 33-51-00-810-802-A. CONFIRMED BATTERY FAULT OF EPSU (11WL). MAINTENANCE REPLACED EPSU BATTERY AT 11WL IAW AMM 33-51-38. - [SDR AALA202412230338](https://openairdocs.org/sdr/AALA202412230338.md): Light · dislodged · Dec 21, 2024 · N817AW · Airbus A319132 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: SEAT 25C ESCAPE PATH LIGHTING HOUSING DISLODGED FROM SEAT. MAINTENANCE REPLACED SEAT 25C ESCAPE PATH LIGHTING ASSY ON SEAT PER AMM 33-51-18. - [SDR AALA202410161718](https://openairdocs.org/sdr/AALA202410161718.md): Megaphone · no test · Oct 15, 2024 · N817AW · Airbus A319132 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT THE FORWARD CABIN MEGAPHONE HAS NO POWER. MAINTENANCE REPACED THE MEGAPHONE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. - [SDR AALA202409260741](https://openairdocs.org/sdr/AALA202409260741.md): Proximity Switch · out of position · Sep 23, 2024 · N817AW · Airbus A319132 · Door Warning System > AIRCRAFT WAS NOT GROUNDED: 1L DOOR CABIN PRESS LIGHT FLASHES IN FLIGHT FOR MOST OF DESCENT. DOOR ECAM PAGE SHOWED 1L DOOR SLIDE DISARMED DURING THOSE TIMES. CONDITION IS INTERMITENT. FOUND DOOR ARM LEVER PROXIMITY SWITCH 4WN1 UNLOCKED AND NEARLY FALLING OFF. - [SDR AALA202409195605](https://openairdocs.org/sdr/AALA202409195605.md): Megaphone · inoperative · Sep 18, 2024 · N817AW · Airbus A319132 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: EMERGENCY MEGAPHONE IN FIRST CLASS UNUSABLE. INSTALLED NEW MEGAPHONE. - [SDR AALA202408055164](https://openairdocs.org/sdr/AALA202408055164.md): Strap · unsecure · Aug 2, 2024 · N817AW · Airbus A319132 · Passenger/Crew Doors > AIRCRAFT WAS NOT GROUNDED: 2L DOOR HAS SOME GREEN CHORD HANGING DOWN FROM THE BOTTOM OF THE DOOR FORMING A LOOP. MAINTENANCE RE-SECURED STRAP PER AMM 25-62-50. - [SDR AALA202404266266](https://openairdocs.org/sdr/AALA202404266266.md): Fitting · none · Apr 24, 2024 · N817AW · Airbus A319132 · Standard Practices/Structures > AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED TO THE FLIGHT DECK WINDSJHIELD FRAMING,THE RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 4 AT Y0 NEED TO BE REPLACED PER EA 351108. REPLACED CONTINUITY FITTING PER EA 351108. - [SDR AALA202404269215](https://openairdocs.org/sdr/AALA202404269215.md): Window Frame · none · Apr 24, 2024 · N817AW · Airbus A319132 · Standard Practices/Structures > AIRCRAFT IN BASE MAINTENANCE: AS PART OF THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK WINDSHIELD FRAMING THE WINDSHIELD CENTER POST FRAMING LEFT HAND SIDE NEEDS TO BE REPLACED BETWEEN FR 2 AND FR 6 PER EA 351108. REPLACED WINDSHIELD FRAMING PER EA 35 - [SDR AALA202404235441](https://openairdocs.org/sdr/AALA202404235441.md): Power Supply · no test · Apr 22, 2024 · N817AW · Airbus A319132 · Emergency Lighting > AIRCRAFT IN BASE MAINTENANCE: INOPERATIVE EPSU-EMERGENCY POWER SUPPLY UNIT (11WL) IN PASSENGER CABIN. REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU)(11WL) - [SDR AALA202404260585](https://openairdocs.org/sdr/AALA202404260585.md): Fitting · none · Apr 21, 2024 · N817AW · Airbus A319132 · Standard Practices/Structures > AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED IN THE AVIONICS COMPARTMENT RACK 80VU PER EA 351104 THE LEFT HAND UPPER FITTING NEEDS TO BE REPLACED FR 23 AND FR 24 AT S32L AND +Y1263. REPLACED FITTING PER EA 351104. - [SDR AALA202404180898](https://openairdocs.org/sdr/AALA202404180898.md): Floor Panel · delaminated · Apr 15, 2024 · N817AW · Airbus A319132 · Fuselage Floor Panel > AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR PANEL 261DF DELAMINATED. REPLACED FLOOR PANEL PER EA 351420. - [SDR AALA202404122906](https://openairdocs.org/sdr/AALA202404122906.md): Hinge Fitting · worn · Apr 10, 2024 · N817AW · Airbus A319132 · Fuselage, Door Hinge > AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT LEFT DOOR AFT HINGE FITING WORN. REPLACED HINGE FITTING PER CMM 52-82-32. - [SDR AALA202404127050](https://openairdocs.org/sdr/AALA202404127050.md): Hinge · worn · Apr 10, 2024 · N817AW · Airbus A319132 · Fuselage, Door Hinge > AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT LEFT DOOR FORWARD HINGE WORN. REPLACED HINGE PER CMM 52-82-32. - [SDR AALA202404096286](https://openairdocs.org/sdr/AALA202404096286.md): Profile · cracked · Apr 7, 2024 · N817AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 834 LEFT HAND AND RIGHT HAND LOAD TRANSMITTING PROFILES CRACKED. MAINTENANCE MODIFIED THE LOAD TRANSMITTING PROFILES PER EO 5210Y228-001. - [SDR AALA202404043238](https://openairdocs.org/sdr/AALA202404043238.md): Fitting · cracked · Mar 8, 2024 · N817AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD LOWER FRAMING HAS CRACKED FITTING AT FR 9 AND +Y1000. REPLACED FITTING PER SRM 51-72-11. - [SDR AALA202404262270](https://openairdocs.org/sdr/AALA202404262270.md): Rail · worn · Feb 20, 2024 · N817AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE FLIGHT DECK WINDSHIELD LATERAL WINDSHIELD FRAME JUNCTION RAIL HAS ELONGATED HOLE AT FR 4 RIGHT. REPLACED RAIL PER EA 351108. - [SDR AALA202404260347](https://openairdocs.org/sdr/AALA202404260347.md): Fitting · worn · Feb 20, 2024 · N817AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE FLIGHT DECK WINDSHIELD LATERAL WINDSHIELD FRAME JUNCTION LOWER CORNER FITTING HAS ELONGATED HOLE AT FR 4 RIGHT. REPLACED CORNER FITTING PER EA 351108. - [SDR AALA202404261217](https://openairdocs.org/sdr/AALA202404261217.md): Fitting · worn · Feb 20, 2024 · N817AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE FLIGHT DECK WINDSHIELD LATERAL WINDSHIELD FRAME JUNCTION UP EER CORNER FITTING HAS ELONGATED HOLE AT FR 4 RIGHT. REPLACED CORNER FITTING PER EA 351108. - [SDR AALA202402201223](https://openairdocs.org/sdr/AALA202402201223.md): Visor · glazed · Feb 19, 2024 · N817AW · Airbus A319132 · Passenger/Crew Doors > AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER VISOR GLAZED. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14. - [SDR AALA202402202506](https://openairdocs.org/sdr/AALA202402202506.md): Sleeve · deformed · Feb 16, 2024 · N817AW · Airbus A319132 · Nacelle/Pylon, Main Frame > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON FORWARD ATTACH FITTING OUTBOARD LOWER SLEEVE HAS DEFORMATION. REPLACED SLEEVE PER AMM 54-51-00. - [SDR AALA202402205188](https://openairdocs.org/sdr/AALA202402205188.md): Sleeve · worn · Feb 15, 2024 · N817AW · Airbus A319132 · Wing Main, Frame Structure > AIRCRAFT IN BASE MAINTENANCE: LEFT PYLON AFT ATTACH FITTING UPPER SLEEVE WORN. REPLACED SLEEVE PER AMM 54-51-00. - [SDR AALA202402218020](https://openairdocs.org/sdr/AALA202402218020.md): Bolt · corroded · Feb 14, 2024 · N817AW · Airbus A319132 · Leading Edge Devices > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK 4 LOWER BOLT AT WS 2560 AND RIB 5. REPLACED BOLT PER TASK CARD 26C61057005. - [SDR AALA202402219285](https://openairdocs.org/sdr/AALA202402219285.md): Bolt · corroded · Feb 12, 2024 · N817AW · Airbus A319132 · Leading Edge Devices > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #6 LOWER AFT BOLT AT WS 7316 AND RIB 13. REPLACED BOLT PER TASK CARD 26C61057005. - [SDR AALA202402148546](https://openairdocs.org/sdr/AALA202402148546.md): Bolt · corroded · Feb 12, 2024 · N817AW · Airbus A319132 · Leading Edge Devices > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK 10 LOWER MID BOLT AT WS 11664 AND RIB 22. REPLACED BOLT PER TASK CARD 26C51057005. - [SDR AALA202404269124](https://openairdocs.org/sdr/AALA202404269124.md): Window Frame · cracked · Feb 11, 2024 · N817AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING LATERAL RIGHT HAND UPPER ATTACHMENT BETWEEN FR 3 AND FR 8. REPAIRED WINDSHIELD FRAME PER EA 351571. - [SDR AALA202404268089](https://openairdocs.org/sdr/AALA202404268089.md): Window Frame · cracked · Feb 11, 2024 · N817AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING LATERAL LEFT HAND UPPER ATTACHMENT BETWEEN FR 3 AND FR 8. REPAIRED WINDSHIELD FRAME PER EA 351570. - [SDR AALA202403054656](https://openairdocs.org/sdr/AALA202403054656.md): Coupling · worn · Feb 11, 2024 · N817AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT WAS NOT GROUNDED: ELONGATED HOLE ON COUPLING INBOARD SIDE UPPER POSITION LOCATED AT FR 66 AND STR 23R IN THE AFT GALLEY AREA. REPLACED COUPLING PER SRM 51-42-11-801. - [SDR AALA202404255009](https://openairdocs.org/sdr/AALA202404255009.md): Spigot · corroded · Feb 9, 2024 · N817AW · Airbus A319132 · Nacelle/Pylon, Main Frame > AIRCRAFT IN BASE MAINTENANCE: CORROSION MEASURING L= 13.571 IN, W= 1.343 IN. D= 0.002 IN. ON SPIGOT FITTING RECEPTACLE ON RIGHT PYLON, BETWEEN RIB 4 AND RIB 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-002. - [SDR AALA202402144770](https://openairdocs.org/sdr/AALA202402144770.md): Bolt · corroded · Feb 6, 2024 · N817AW · Airbus A319132 · Leading Edge Devices > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK 3 FORWARD BOLT AT WS 2580 AND RIB 5. REPLACED BOLT PER TASK CARD 26C51057005. - [SDR AALA202404251751](https://openairdocs.org/sdr/AALA202404251751.md): Spigot · corroded · Feb 4, 2024 · N817AW · Airbus A319132 · Nacelle/Pylon, Main Frame > AIRCRAFT IN BASE MIANTENANCE: CORROSION ON SPIGOT FITTING RECEPTACLE ON LEFT HAND PYLON. REPLACED SPIGOT FITTING PER AMM 54-51-12-300-002. - [SDR AALA202402098040](https://openairdocs.org/sdr/AALA202402098040.md): Web · corroded · Feb 1, 2024 · N817AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR WEB BETWEEN FR 69 AND FR 70 AT S23R. REPLACED WEB PER SRM 51-42-11. - [SDR AALA202402085058](https://openairdocs.org/sdr/AALA202402085058.md): Web · corroded · Feb 1, 2024 · N817AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR WEB BETWEEN FR 69 AND FR 70 AT S23L. REPLACED WEB PER SRM 51-72-11. - [SDR AALA202403041587](https://openairdocs.org/sdr/AALA202403041587.md): Plate · worn · Jan 30, 2024 · N817AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR PLATE HAS ELONGATED WORN FASTENER HOLES BETWEEN FR 68 AND FR 69 AT S23R. REPLACED PLATE PER SRM 51-72-11. - [SDR AALA202402297909](https://openairdocs.org/sdr/AALA202402297909.md): Splice Angle · worn · Jan 30, 2024 · N817AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE ON INBOARD LOWER SPLICE LOCATED AT FR 66 AND STR 23 IN THE LOWER SILL AREA AT PASSENGER CABIN. REPLACED SPLICE PER SRM 51-42-11-801. - [SDR AALA202402298090](https://openairdocs.org/sdr/AALA202402298090.md): Splice Angle · worn · Jan 30, 2024 · N817AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLES UPPER OUTBOARD SPLICE LOCATED AT FR 66 ON LOWER SILL RIGHT HAND AREA IN THE PASSENGER CABIN. REPLACED SPLICE PER SRM 51-42-11-801. - [SDR AALA202402298491](https://openairdocs.org/sdr/AALA202402298491.md): Splice Angle · worn · Jan 30, 2024 · N817AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLES ON LOWER OUTBOARD SPLICE LOCATED AT FR 66 ON THE LOWER SILL AREA IN THE PASSENGER CABIN. REPLACED SPLICE PER SRM 51-42-11-801. - [SDR AALA202402295592](https://openairdocs.org/sdr/AALA202402295592.md): Track Splice · corroded · Jan 30, 2024 · N817AW · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPLICE UPPER INBOARD POSITION LOCATED ON SEAT TRACK -Y1162 AT FR 68. REPLACED SPLICE PER SRM 51-42-11-801. - [SDR AALA202402284206](https://openairdocs.org/sdr/AALA202402284206.md): Track Splice · worn · Jan 30, 2024 · N817AW · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR SEAT TRACK UPPER OUTBOARD SPLICE COUPLING HAS ELONGATED / WORN FASTENER HOLE AT FR 66 AND +Y1292. REPLACED SPLICE COUPLING PER SRM 51-72-11. - [SDR AALA202402279209](https://openairdocs.org/sdr/AALA202402279209.md): Track Splice · worn · Jan 30, 2024 · N817AW · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR SEAT TRACK UPPER INBOARD SPLICE COUPLING HAS ELONGATED / WORN HOLE AT FR 64 AND +Y1292. REPLACED SPLICE COUPLING PER SRM 51-72-11. - [SDR AALA202402277539](https://openairdocs.org/sdr/AALA202402277539.md): Track Splice · worn · Jan 30, 2024 · N817AW · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR SEAT TRACK UPPER OUTBOARD SPLICE COUPLING HAS ELONGATED / WORN HOLE AT FR 64 AND +Y1292. REPLACED SPLICE COUPLING PER SRM 51-72-11. - [SDR AALA202402271924](https://openairdocs.org/sdr/AALA202402271924.md): Track Splice · worn · Jan 30, 2024 · N817AW · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR SEAT TRACK LOWER INBOARD SPLICE COUPLING HAS ELONGATED / WORN HOLE AT FR 64 AND +Y1292. REPLACED SPLICE COUPLING PER SRM 51-72-11. - [SDR AALA202402274204](https://openairdocs.org/sdr/AALA202402274204.md): Track Splice · worn · Jan 30, 2024 · N817AW · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR SEAT TRACK LOWER OUTBOARD SPLICE COUPLING HAS ELONGATED / WORN HOLE AT FR 64 AND +Y1292. REPLACED SPLICE COUPLING PER SRM 51-72-11. - [SDR AALA202402270122](https://openairdocs.org/sdr/AALA202402270122.md): Track Splice · worn · Jan 30, 2024 · N817AW · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR SEAT TRACK UPPER INBOARD SPLICE COUPLING HAS ELONGATED / WORN HOLE AT FR 66 AND +Y1292. REPLACED SPLICE COUPLING PER SRM 51-72-11. - [SDR AALA202402276004](https://openairdocs.org/sdr/AALA202402276004.md): Track Splice · worn · Jan 30, 2024 · N817AW · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR SEAT TRACK LOWER OUTBOARD SPLICE COUPLING HAS ELONGATED / WORN HOLE AT FR 66 AND +Y1292. REPLACED SPLICE COUPLING PER SRM 51-72-11. - [SDR AALA202402270942](https://openairdocs.org/sdr/AALA202402270942.md): Track Splice · worn · Jan 30, 2024 · N817AW · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR SEAT TRACK LOWER INBOARD SPLICE COUPLING HAS ELONGATED / WORN HOLE AT FR 66 AND +Y1292. REPLACED SPLICE COUPLING PER SRM 51-72-11. Next page: https://openairdocs.org/aircraft/N817AW/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 = 'N817AW' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N817AW/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.