# Service difficulty reports: N814AX, cancelled Jul 21, 2009 A list on [N814AX, cancelled Jul 21, 2009](https://openairdocs.org/deregistered/N814AX-2009-07-21.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 3 · 147 reports - [SDR ABXA050105](https://openairdocs.org/sdr/ABXA050105.md): Compressor · defective · Apr 28, 2005 · N814AX · Doug DC863F · Cabin Compressor System > NR 2 CTC FAILED, HAD LOUD BEARING SQUEAL ALONG WITH SOME SMOKE IN THE COCKPIT. REMOVED AND REPLACED NR 2 CABIN TURBINE COMPRESSOR IAW DC-8 MM 21-10-01-4-0001. OPS CHECKED GOOD. - [SDR ABXA050015](https://openairdocs.org/sdr/ABXA050015.md): Floorbeam · corroded · Jan 9, 2005 · N814AX · Doug DC863F · Fuselage Main, Floor Beam > CORROSION DISCOVERED ON FLOORBEAM AT STA 920, LOCATED AT OUTBOARD END OF THE BEAM LOWER RIGHT FLANGE. CORROSION IS BEYOND 20 PERCENT OF MATERIAL THICKNESS. REPAIRED BEAM BY CUTTING AND REMOVING AFFECTED AREA AND SPLICING IN NEW SECTION IAW REA D853-51248-MR. - [SDR ABXA040331](https://openairdocs.org/sdr/ABXA040331.md): Spar · cracked · Sep 11, 2004 · N814AX · Doug DC863F · Wing Spar > RIGHT WING INTERNAL FUEL TANK AT STA XRS 172 LOWER CENTER SPAR AND WEB HAD CRACK AND CORROSION AT SPAR CAP CRACK. CUT OUT DAMAGED AREA OF CENTER SPAR AND WEB IAW REA D857-49982MR. FABRICATED REPAIR PARTS IAW DAC DWG'S 5613912, 3642213, 3644709 AND SRO8570015 - [SDR ABXA040332](https://openairdocs.org/sdr/ABXA040332.md): Skin · damaged · Aug 31, 2004 · N814AX · Doug DC863F · Fuselage Main, Plate/Skin > INSPECTION DEVIATION PER ABX REA D853-50097MR, REPAIR TRIPLER, FUSELAGE SKIN, FS 273-280, LONGERON 19 LEFT - 20 LEFT. REPAIRED AREA IAW ABX REA D853-50097MR. COI GENERATED FOR MAINTENANCE TRACKING. - [SDR ABXA040329](https://openairdocs.org/sdr/ABXA040329.md): Skin · corroded · Aug 11, 2004 · N814AX · Doug DC863F · Fuselage Main, Plate/Skin > AFT CARGO LONGERON 36, BLEEDING CORROSION FROM BOTH SIDES FROM STA 1080 - 1120. REPAIRED AREA IAW REA D853-49986MR. - [SDR ABXA040330](https://openairdocs.org/sdr/ABXA040330.md): Skin · gouged · Aug 10, 2004 · N814AX · Doug DC863F · Wing, Plate/Skin > RIGHT WHEEL INBOARD AILERON, 3 RIVETS MISSING HEADS OR PART OF HEAD AND OPEN HOLE AT APPROXIMATELY XA 562, LOWER LEADING EDGE. REMOVED AND REPLACED DAMAGED SKIN SECTION AND DOUBLER IAW REA D857-49983MR. - [SDR ABXA040096](https://openairdocs.org/sdr/ABXA040096.md): Crank Assy · broken · Mar 13, 2004 · N814AX · Doug DC863F · Drag Control System > SPOILER EXTEND LIGHT STAYED ON AFTER RETRACTION. NORMAL SPOILER HYDRAULIC PRESSURE INDICATION. MAINTENANCE FOUND RIGHT WING INBOARD TWO SPOILER DRIVE ARMS THAT ATTACH TO SPOILER CABLES BROKEN. REPLACED REAR SPAR ACTUATOR CRANK ASSEMBLIES ON INBOARD SPOILER - [SDR ABXA030437](https://openairdocs.org/sdr/ABXA030437.md): Seat · defective · Nov 7, 2003 · N814AX · Doug DC863F · Flight Compartment Equipment > FLIGHT ENGINEER'S SEAT VERTICAL HOLD WOULD NOT HOLD WHILE SEAT WAS FACING FORWARD. FELL 3 TIMES DURING TAKEOFF AND INITIAL CLIMB. REPLACED SYSTEMS ENGINEER SEAT PER ABX DC8 AMM 25-11-06-2-001. LUBED AND OPS CHECKED GOOD. - [SDR ABXA030204](https://openairdocs.org/sdr/ABXA030204.md): Skin · damaged · Nov 7, 2002 · N814AX · Doug DC863F · Fuselage Main, Plate/Skin > L2 DOOR CUTOUT LOWER FORWARD CORNER HAD REPAIR. UNIT DOES NOT CONFORM TO SRM OR JOB CARD NEA 53100104-002/634. REPAIRED L2 LOWER FORWARD CORNER IAW REA D853-44023MR AND DC-8 SRM 53-2-0. - [SDR ABXA030203](https://openairdocs.org/sdr/ABXA030203.md): Fitting · cracked · Nov 7, 2002 · N814AX · Doug DC863F · Cargo/Baggage Doors > MAIN CARGO DOOR ACTUATOR ATTACH FITTING WAS SEPARATED AT WELD. REMOVED CORROSION FROM FITTING AND BLENDED FITTING IAW DC-8 SRM 51-1-8, WELDED FITTING IAW AM526856, INSTALLED FITTING IAW DC-8 SRM 51-3-0 AND 51-1-21. REINSTALLED ACTUATOR IAW DC-8 MM 52-36-03. - [SDR ABXA030207](https://openairdocs.org/sdr/ABXA030207.md): Skin · corroded · Nov 5, 2002 · N814AX · Doug DC863F · Wing, Plate/Skin > RIGHT FORWARD WHEEL WELL HAD CORROSION ON CENTER WING SKIN AFT OF OUTBOARD BLOWOUT PANEL. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER, REPAIR ANGLE AND SPLICE IAW DC-8 SRM 51-1-8 AND REA D857-44039MR. - [SDR ABXA030206](https://openairdocs.org/sdr/ABXA030206.md): Longeron · corroded · Nov 2, 2002 · N814AX · Doug DC863F · Fuselage Main, Longeron/Stringer > AFT LOWER CARGO LONGERON 34 RIGHT HAD CORROSION AT STA 1180 - 1200. REMOVED CORROSION, BEYOND LIMITS. REMOVED FASTENERS IAW DC-8 SRM 51-1-20D. FABRICATED REPAIR STRAP IAW REA D853-44041MR. PRIMED STRAP IAW DC-8 SRM 51-1-8. INSTALLED STRAP IAW DC-8 SRM 51- - [SDR ABXA030205](https://openairdocs.org/sdr/ABXA030205.md): Skin · cracked · Oct 30, 2002 · N814AX · Doug DC863F · Fuselage Main, Plate/Skin > L1 DOOR SHOWED CRACK LOWER AFT CORNER. REMOVED DAMAGE IAW DC-8 SRM 53-2-0. FABRICATED DOUBLER, TRIPLER, AND FILLER IAW DC-8 SRM 53-2-0. INSTALLED DOUBLER, TRIPLER AND FILLER IAW DC-8 SRM 51-1-20D, AND REA D853-44030MR. - [SDR ABXA020225](https://openairdocs.org/sdr/ABXA020225.md): Pressure Switch · faulty · Oct 1, 2002 · N814AX · Doug DC863F · Engine Oil Pressure > NR 4 LOW OIL PRESSURE LIGHT CAME ON. THROTTLED BACK BUT LIGHT STAYED ON. SECURED THE NR 4 ENGINE. ALSO THE NR 3 LOW OIL PRESSURE LIGHT CAME ON. THROTTLED BACK AND LIGHT WENT OUT, BUT ILLUMINATED INTERMITTENTLY. AIRCRAFT DIVERTED TO LOUISVILLE. REPLACED T - [SDR ABXA020153](https://openairdocs.org/sdr/ABXA020153.md): Engine · malfunctioned · Sep 3, 2002 · N814AX · Doug DC863F · Engine (Turbine/Turboprop) > NR 4 ENGINE LOW OIL PRESSURE LIGHT CAME ON ACCOMPANIED BY AN OIL PRESSURE FLUCTUATION AND QUANTITY DECREASING. ENGINE WAS SECURED AND OIL PRESSURE WAS BELOW 5 PSI WITH ENGINE WINDMILLING AT 30 PERCENT N2 FOR REMAINED OF FLIGHT. REPLACED THE NR 4 ENGINE. RUN - [SDR ABXA020120](https://openairdocs.org/sdr/ABXA020120.md): Battery Pack · discharged · Aug 26, 2002 · N814AX · Doug DC863F · Emergency Lighting > EMERGENCY LIGHTS WERE VERY DIM. REPLACED EMERGENCY LIGHTS BATTERY PACK IAW DC-8 AMM 33-50-01-2. - [SDR ABXA010446](https://openairdocs.org/sdr/ABXA010446.md): Yoke · jammed · Aug 18, 2001 · N814AX · Doug DC863F · Control Column Section > ELEVATOR CONTROL YOKE JAMMED ON FINAL APPROACH. YOKE WOULD ONLY GO TO THE NEUTRAL POSITION ON THE ELEVATOR POSITION INDICATOR. VERIFIED ELEVATOR CONTROL COLUMN JAM IN NOSE DOWN POSITION. INSPECTION REVEALED ELEVATOR RIGGING FIXTURE LINK CONTACTED LOWER ELEV - [SDR ABXA010150](https://openairdocs.org/sdr/ABXA010150.md): Fitting · cracked · Apr 16, 2001 · N814AX · Doug DC863F · Wing Miscellaneous Structure > THE LEFT WING LOWER TRAPEZOID FITTING WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 57-5-2. - [SDR ABXA010139](https://openairdocs.org/sdr/ABXA010139.md): Structure · leaking · Mar 20, 2001 · N814AX · Doug DC863F · Wing, Plate/Skin > A FASTENER WAS FOUND TO BE LEAKING FUEL AT STA 795. MAINTENANCE REPAIRED THE AREA IAW REA D857-40312MR AND DC-8 SRM. - [SDR ABXA010142](https://openairdocs.org/sdr/ABXA010142.md): Fitting · corroded · Mar 13, 2001 · N814AX · Doug DC863F · Fuselage Miscellaneous Structure > CORROSION WAS FOUND ON END FITTING AT FUSELAGE STATION 8-28 LONGERON 27R IN THE FORWARD AIR-CONDITIONING COMPARTMENT. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 51-1-8, 51-2-0 AND DAC DRAWING 4711722. - [SDR ABXA010144](https://openairdocs.org/sdr/ABXA010144.md): Fitting · corroded · Mar 13, 2001 · N814AX · Doug DC863F · Fuselage Miscellaneous Structure > CORROSION WAS FOUND AT THE FORWARD AIR-CONDITIONING PRESSURE COMPARTMENT AT THE RIGHT CUSP FITTING. CORROSION WAS FOUND UNDER AND AROUND THE NUT PLATES. MAINTENANCE INSTALLED A NEW FITTING IAW DC-8 SRM 51-1-20 AND 51-3-0. - [SDR ABXA010151](https://openairdocs.org/sdr/ABXA010151.md): Fitting · cracked · Mar 13, 2001 · N814AX · Doug DC863F · Wing Miscellaneous Structure > THE RIGHT WING LOWER FORWARD TRAPEZOID FITTING WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 57-2-7. - [SDR ABXA010141](https://openairdocs.org/sdr/ABXA010141.md): Fitting · corroded · Mar 12, 2001 · N814AX · Doug DC863F · Fuselage Miscellaneous Structure > CORROSION WAS FOUND ON FITTING AT THE LEFT MLG WHEEL WELL AT FUSELAGE STATION 857. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX REA D853-40267-MR AND DC-8 SRM 53-2-0. - [SDR ABXA010147](https://openairdocs.org/sdr/ABXA010147.md): Longeron · corroded · Mar 12, 2001 · N814AX · Doug DC863F · Fuselage Main, Longeron/Stringer > CORROSION WAS FOUND ON LONGERON 33L BETWEEN FUSELAGE STA 320 - 340 IN LOWER CARGO PIT. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 53-2-0. - [SDR ABXA010148](https://openairdocs.org/sdr/ABXA010148.md): Longeron · corroded · Mar 12, 2001 · N814AX · Doug DC863F · Fuselage Main, Longeron/Stringer > CORROSION WAS FOUND AT THE FORWARD LOWER CARGO PIT BETWEEN STA 280 AND 300, LONGERON 28L. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 51-1-8 AND DAC DRAWING 9754931. - [SDR ABXA010145](https://openairdocs.org/sdr/ABXA010145.md): Skin · cracked · Mar 11, 2001 · N814AX · Doug DC863F · Fuselage Main, Plate/Skin > THE FUSELAGE EXTERIOR SKIN AT STATION 1750 LONGERON 15R-16R WAS FOUND TO BE CRACKED BETWEEN FASTENERS. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 53-2-1. - [SDR ABXA010146](https://openairdocs.org/sdr/ABXA010146.md): Skin · cracked · Mar 11, 2001 · N814AX · Doug DC863F · Fuselage Main, Plate/Skin > THE FUSELAGE EXTERIOR SKIN WAS FOUND TO BE CRACKED AT STA 1720 LONGERON 17-18R. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 53-2-1. - [SDR ABXA010149](https://openairdocs.org/sdr/ABXA010149.md): Seat Track · corroded · Mar 11, 2001 · N814AX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings > THE MAIN CARGO COMPARTMENT SEAT TRACK AT RBL 30, STATION 1723 - 1746 WAS CORRODED. MAINTENANCE INSPECTED AND INSTALLED A NEW SEAT TRACK IAW DC-8 SRM 51-3-0 AND ZANTOP DRAWING 86302. - [SDR ABXA010140](https://openairdocs.org/sdr/ABXA010140.md): Stiffener · corroded · Mar 10, 2001 · N814AX · Doug DC863F · Fuselage Miscellaneous Structure > THE RIGHT MLG WHEEL WELL HORIZONTAL PRESSURE WEB WAS FOUND TO BE CORRODED. A STIFFENER WAS FOUND TO BE BULGING AT STA 902 RBL 56 THROUGH 65. MAINTENANCE REPAIRED THE AREA IAW REA D853-40284, DAC DRAWING 5645332 AND DC-8 SRM 51-1-8. - [SDR ABXA010138](https://openairdocs.org/sdr/ABXA010138.md): Frame · cracked · Mar 10, 2001 · N814AX · Doug DC863F · Fuselage Main, Frame > A CRACK 4.5 INCH LONG WAS FOUND ON THE NOSE WHEEL WELL AFT DOOR FORWARD HINGE FRAME. MAINTENANCE REPAIRED THE CRACK IAW REA D853-40280MR. - [SDR ABXA010417](https://openairdocs.org/sdr/ABXA010417.md): Structure · leaking · Mar 9, 2001 · N814AX · Doug DC863F · Wing Main, Frame Structure > SPAR CAP LEAKED FUEL JUST INBOARD OF NR 1 PYLON AT S - 64 DOUBLER. REMOVED DOUBLER AND TRIPLER. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW ABX REA D857-40311MR AND DAC DWG SRO8570013. - [SDR ABXA010143](https://openairdocs.org/sdr/ABXA010143.md): Structure · leaking · Mar 9, 2001 · N814AX · Doug DC863F · Wing Spar > THE SPAR CAP WAS FOUND TO BE LEAKING FUEL JUST INBOARD OF THE NR 1 PYLON AT WS 444. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX REA D857-40311MR. - [SDR ABXA010152](https://openairdocs.org/sdr/ABXA010152.md): Seat Track · corroded · Mar 7, 2001 · N814AX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings > THE SEAT TRACK AT FUSELAGE STATION 920 HAD A CORRODED FASTENER HOLE. MAINTENANCE INSPECTED AND INSTALLED A NEW SEAT TRACK AT STATION 870 - 940 IAW DC-8 SRM 51-3-0 AND 51-1-21. - [SDR ABXA000109](https://openairdocs.org/sdr/ABXA000109.md): Water Heater · malfunctioned · Feb 16, 2000 · N814AX · Doug DC863F · Buffet/Galleys > ELECTRICAL BURNING SMELL WAS COMING FROM THE HOT WATER MAKER SHORTLY AFTER IT WAS TURNED ON. WATER WAS FULL, AFTER TURNING IT OFF THE SMELL WENT AWAY. REPLACED THE HOT CUP BRACKET AND HOT CUP IAW DC8 MM. OPS CHECKED GOOD. - [SDR ABXA9800371](https://openairdocs.org/sdr/ABXA9800371.md): Up Latch Switch · out of adjust · Apr 23, 1998 · N814AX · Doug DC863F · Landing Gear Position and Warning > IN CRUISE FLIGHT, LANDING GEAR UNSAFE LIGHT ILLUMINATED. RECYCLED LANDING GEAR. LANDING GEAR DOOR 'NOT LATCHED' LIGHT ILLUMINATED. SLOW FLEW AIRCRAFT AT 220 KNOTS. ADJUSTED LEFT GEAR DOOR UPLATCH IAW DC8 MM 32-31-4. - [SDR ABXA9800367](https://openairdocs.org/sdr/ABXA9800367.md): Door Spring · out of adjust · Apr 21, 1998 · N814AX · Doug DC863F · Landing Gear Door Retract Section > LANDING GEAR UNSAFE LIGHT ILLUMINATED DURING CRUISE FLIGHT WITH LEFT MAIN LANDING GEAR DOOR 'NOT LATCHED' LIGHT ILLUMINATED. RECYCLED GEAR, NO CHANGE. ADJUSTED LEFT MAIN LANDING GEAR PROXIMITY SWITCH TARGET STOP. REPLACED LEFT GEAR DOOR SPRING IAW DC8 MM 32 - [SDR ABXA9800312](https://openairdocs.org/sdr/ABXA9800312.md): Angle · cracked · Mar 28, 1998 · N814AX · Doug DC863F · Fuselage Miscellaneous Structure > KEEL BEAM AREA AT APPROXIMATELY STATION 930 TO 935 RIGHT SIDE, THE KEEL ANGLE HAS A 5 INCH CRACK. REPAIRED IAW ABX REA D853-22758 AND DC8 SRM 52-2-0. - [SDR ABXA9800301](https://openairdocs.org/sdr/ABXA9800301.md): Skin · cracked · Mar 16, 1998 · N814AX · Doug DC863F · Wing, Plate/Skin > LEFT WING LEADING EDGE BETWEEN PYLONS INTERNAL UPPER DOUBLER IS CRACKED ABOVE SLOT ACTUATOR. REPAIRED IAW DC8 SRM 51-3-0 AND 51-1-20D. - [SDR ABXA9800304](https://openairdocs.org/sdr/ABXA9800304.md): Shear Tie · corroded · Mar 15, 1998 · N814AX · Doug DC863F · Fuselage Miscellaneous Structure > FORWARD SHEAR TIE AT STATION 1000 HAS HEAVY CORROSION AT LONGERON 33R. REPAIRED IAW DC8 SRM 53-20-0 AND DWG 9755888. - [SDR ABXA9800302](https://openairdocs.org/sdr/ABXA9800302.md): Doubler · cracked · Mar 15, 1998 · N814AX · Doug DC863F · Fuselage Miscellaneous Structure > FINGER DOUBLER CRACKED AT STATION 450, LONGERON 31L. CORROSION OUT OF LIMITS. REPAIRED IAW ABX REA D853-22748. - [SDR ABXA9800303](https://openairdocs.org/sdr/ABXA9800303.md): Fitting · corrosion · Mar 14, 1998 · N814AX · Doug DC863F · Fuselage Miscellaneous Structure > CORRODED VERTICAL FITTING RBL 65 STATION 920. REPAIRED IAW DC8 SRM 51-1-20D. - [SDR ABXA9800315](https://openairdocs.org/sdr/ABXA9800315.md): Shear Tie · cracked · Mar 13, 1998 · N814AX · Doug DC863F · Fuselage Miscellaneous Structure > SHEAR TIE CRACKED, STATION 1160 BETWEEN LONGERON 34R TO 35R. REPAIRED IAW DC8 SRM 51-1-20D. - [SDR ABXA9800305](https://openairdocs.org/sdr/ABXA9800305.md): Longeron · corroded · Mar 13, 1998 · N814AX · Doug DC863F · Fuselage Main, Longeron/Stringer > LONGERON 31R AT STATION 25 HAS HEAVY CORROSION. REPAIRED IAW DC8 SRM 51-1-20. - [SDR ABXA9800314](https://openairdocs.org/sdr/ABXA9800314.md): Fitting · cracked · Mar 12, 1998 · N814AX · Doug DC863F · Fuselage Miscellaneous Structure > SHEAR TIE AT STATION 1150 BETWEEN LONGERON 30R AND 33R HAS 6 INCH CRACK. REPAIRED IAW SRM 51-1-20D. - [SDR ABXA9800310](https://openairdocs.org/sdr/ABXA9800310.md): Stringer · corroded · Mar 12, 1998 · N814AX · Doug DC863F · Fuselage Main, Longeron/Stringer > STRINGERS 34R AND 34L AT STATION 1460 CORRODED BEYOND LIMITS. REPAIRED IAW DC8 SRM 53-2-0 AND 51-1-20. - [SDR ABXA9800307](https://openairdocs.org/sdr/ABXA9800307.md): Rib · cracked · Mar 12, 1998 · N814AX · Doug DC863F · Wing, Rib/Bulkhead > LEFT WING LEADING EDGE RIB CRACKED AT WS 354 UPPER AFT. REPAIRED IAW DC8 SRM 51-1-20D. - [SDR ABXA9800248](https://openairdocs.org/sdr/ABXA9800248.md): Rib · cracked · Mar 12, 1998 · N814AX · Doug DC863F · Wing, Rib/Bulkhead > RIGHT WING LEADING EDGE RIB AT STATION XFS 791.25 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW SRM 57-2-0 AND DWG K 05056. - [SDR ABXA9800219](https://openairdocs.org/sdr/ABXA9800219.md): Rib · cracked · Mar 12, 1998 · N814AX · Doug DC863F · Wing, Rib/Bulkhead > RIGHT WING LEADING EDGE RIB AT STA XFS 822.50 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05056. - [SDR ABXA9800217](https://openairdocs.org/sdr/ABXA9800217.md): Rib · cracked · Mar 12, 1998 · N814AX · Doug DC863F · Wing, Rib/Bulkhead > RIGHT WING LEADING EDGE RIB AT STA XFS 747.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05056. - [SDR ABXA9800216](https://openairdocs.org/sdr/ABXA9800216.md): Rib · cracked · Mar 12, 1998 · N814AX · Doug DC863F · Wing, Rib/Bulkhead > RIGHT WING LEADING EDGE RIB AT STA XFS 628.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05056. Next page: https://openairdocs.org/deregistered/N814AX-2009-07-21/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 = 'N814AX' AND deregistration_id = 'N814AX-2009-07-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N814AX-2009-07-21/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.