# Service difficulty reports: N819AX, cancelled Jul 21, 2009

A list on [N819AX, cancelled Jul 21, 2009](https://openairdocs.org/deregistered/N819AX-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 · 102 reports

- [SDR ABXA060271](https://openairdocs.org/sdr/ABXA060271.md): Battery · discharged · Sep 28, 2006 · N819AX · Doug DC863F · Emergency Lighting
  > ON PRE-D CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. SUSPECT EMERGENCY LIGHT SWITCH WAS ON OVERNIGHT WITH NO EXTERNAL POWER. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT RACK ASSEMBLY IAW DC8 AMM 33-50-01-2-0001. OPS CHECKED GOOD.
- [SDR ABXA050100](https://openairdocs.org/sdr/ABXA050100.md): Panel · damaged · Apr 20, 2005 · N819AX · Doug DC863F · Wing, Plate/Skin
  > DURING REMOVAL OF LOWER REAR SPAR FASTENERS SB 57-88, DOUBLER WAS DAMAGED ON EDGE FROM TRAP PANEL ON LEFT WING. REPAIRED AREA IAW REA D857-51393MR.
- [SDR ABXA050099](https://openairdocs.org/sdr/ABXA050099.md): Skin · damaged · Apr 11, 2005 · N819AX · Doug DC863F · Fuselage Main, Plate/Skin
  > FORWARD CARGO COMPARTMENT, FORWARD DOOR OPENING LOWER AFT SKIN CUTOUT, PREVIOUS SPEED TAPE REPAIR CAME LOOSE. REPAIRED AREA IAW REA D853-51391MR.
- [SDR ABXA040388](https://openairdocs.org/sdr/ABXA040388.md): Pin · sheared · Nov 18, 2004 · N819AX · Doug DC863F · Landing Gear Retraction/Extension System
  > UPON GEAR RETRACTION, "LNDG GEAR UNSAFE' LIGHT REMAINED ILLUMINATED, FAILED UPLATCH CHECK. LEFT GEAR AND LEFT DOOR LATCH LIGHT ILLUMINATED DURING ALT UPLATCH CHECK. MAINTENANCE AT FLL, FOUND LEFT MAIN GEAR RETRACT ACTUATOR ATTACH PIN SHEARED. REPLACED LEFT
- [SDR ABXA040064](https://openairdocs.org/sdr/ABXA040064.md): Seat · lack of lube · Feb 14, 2004 · N819AX · Doug DC863F · Flight Compartment Equipment
  > FIRST OFFICER'S SEAT INTERMITTENTLY SLIPPED OUT OF SELECTED FLOOR LATCHED POSITION. CLEANED AND LUBED FIRST OFFICER'S SEAT TRACKS. SYSTEM OPS CHECKED GOOD IAW DC-8 MM 28-11-01-2-0001.
- [SDR ABXA040038](https://openairdocs.org/sdr/ABXA040038.md): Light · will not test · Jan 21, 2004 · N819AX · Doug DC863F · Emergency Lighting
  > EMERGENCY EXIT LIGHT, DISARM CHECK, WOULD NOT TEST. RELAMPED, OPS CHECKED NORMAL.
- [SDR ABXA030392](https://openairdocs.org/sdr/ABXA030392.md): Switch · dirty · Oct 14, 2003 · N819AX · Doug DC863F · Landing Gear Position and Warning
  > DURING DESCENT, LANDING GEAR WAS EXTENDED TO FACILITATE DESCENT. WHEN GEAR WAS RETRACTED, LANDING GEAR UNSAFE LIGHT ILLUMINATED. LANDING GEAR AND DOOR LATCHING "NOT LATCHED" LIGHT ILLUMINATED WITH SELECTOR IN LEFT DOOR POSITION. PERFORMED ABNORMAL PROCEDURE. W
- [SDR ABXA030321](https://openairdocs.org/sdr/ABXA030321.md): Battery Pack · discharged · Aug 4, 2003 · N819AX · Doug DC863 · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY RACK ASSEMBLY IAW DC8 MM 33-50-01. CHECKED GOOD.
- [SDR ABXA030309](https://openairdocs.org/sdr/ABXA030309.md): Angle · corroded · Jul 21, 2003 · N819AX · Doug DC863F · Fuselage Miscellaneous Structure
  > CORROSION ON FORWARD EDGE OF ANGLES AT UPPER OUTBOARD CORNER OF RIGHT WHEEL WELL. REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1-20D, 51-1-21, 51-3-0 AND ABX JOB CARD 8078002.
- [SDR ABXA030310](https://openairdocs.org/sdr/ABXA030310.md): Door Frame · cracked · Jul 19, 2003 · N819AX · Doug DC863F · Fuselage Main, Structure
  > L2 DOOR, UPPER AFT CORNER OF DOOR CUTOUT CRACKED. REMOVED AND REPLACED DOUBLER, TRIPLER AND FILLER IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-20D, 51-1-21 AND 51-1-11.
- [SDR ABXA030311](https://openairdocs.org/sdr/ABXA030311.md): Skin · corroded · Jul 19, 2003 · N819AX · Doug DC863F · Wing, Plate/Skin
  > MAIN CARGO COMPARTMENT CORROSION ON CENTER WING UPPER SKIN AND DOUBLER FROM FS 760 - 855, LEFT BUTTLINE 3 - 23. REMOVED CORROSION, FABRICATED REPAIR DOUBLER AND BUSHINGS, ALODINED, PRIMED, INSTALLED AND LEAK CHECKED IAW REA D857-47555MR AND REA D857-47547MR,
- [SDR ABXA030312](https://openairdocs.org/sdr/ABXA030312.md): Panel · damaged · Jun 30, 2003 · N819AX · Doug DC863F · Nacelle/Pylon Miscellaneous Structure
  > COI 43055-01, NR 3 PYLON INBOARD STRESS PANEL. REPAIRED AREA IAW REA D854-47544MR, REV A.
- [SDR ABXA030146](https://openairdocs.org/sdr/ABXA030146.md): Pressure Switch · defective · May 19, 2003 · N819AX · Doug DC863F · Engine Oil Pressure
  > AT FL 330, RAT -15, NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED WITH 51 PSI AND OIL TEMP. OF 110 DEG. DURING IDLE, TEMP WAS 115 DEGREES, RPESSURE OF 48 PSI. OIL PRESSURE LIGHT FLICKERED AT IDLE. PERFORMED ENGINE SECURING PROCEDURE. NR 3 ENGINE N2 40 PERCENT AND
- [SDR ABXA030097](https://openairdocs.org/sdr/ABXA030097.md): Downlock Switch · malfunctioned · Feb 28, 2003 · N819AX · Doug DC863F · Landing Gear Position and Warning
  > UPON LOWERING LANDING GEAR, LEFT GEAR DOWN LIGHT DID NOT ILLUMINATE AS WELL AS NO RED UNSAFE LIGHT. RAISED GEAR, RED UNSAFE LIGHT ILLUMINATED WITH NO NOT LATCHED LIGHT ILLUMINATED IN ANY POSITION. UPLATCH CHECK NORMAL INDICATION. LOWERED GEAR AGAIN WITH NO
- [SDR ABXA030035](https://openairdocs.org/sdr/ABXA030035.md): Battery Pack · discharged · Jan 13, 2003 · N819AX · Doug DC863F · Emergency Lighting
  > EMERGENCY BATTERY CHARGER CIRCUIT BREAKER TRIPPED. REPLACED EMERGENCY LIGHTING BATTERY PACK ASSEMBLY IAW DC-8 MM 33-50-01-2.
- [SDR ABXA202365](https://openairdocs.org/sdr/ABXA202365.md): Light · inoperative · Dec 20, 2002 · N819AX · Doug DC863F · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT FOR FORWARD CREW DOOR WAS INOPERATIVE. REPLACED OVERHEAD EMERGENCY LIGHTS FOR FORWARD CABIN DOOR. OPS CHECKED GOOD IAW DC-8 MM.
- [SDR ABXA020352](https://openairdocs.org/sdr/ABXA020352.md): Skin · corroded · Dec 4, 2002 · N819AX · Doug DC863F · Fuselage Main, Plate/Skin
  > TEMPORARY REPAIR FUSELAGE SKIN STA. 1700 AND 1746 IAW ABX REA D853-43878. REMOVED TEMPORARY REPAIRS AND REMOVED DAMAGED AREA IAW DC-8 SRM 53-2-1. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-1. ALODINED AND PRIMED AREA AND REPAIR PARTS IAW DC-8 SRM 51-1-8. INSTAL
- [SDR ABXA020308](https://openairdocs.org/sdr/ABXA020308.md): Seat · defective · Nov 12, 2002 · N819AX · Doug DC863F · Flight Compartment Equipment
  > FIRST OFFICER'S SEAT SLIPPED BACKWARDS TWICE. FORE AND AFT POSITION. PIN DID NOT DROP IN PLACE. MUST ENSURE SEAT IS LOCKED. REPLACED FIRST OFFICER'S SEAT IAW DC-8 AMM 25-11-01-2.
- [SDR ABXA010859](https://openairdocs.org/sdr/ABXA010859.md): Attach Angle · cracked · Jan 21, 2002 · N819AX · Doug DC863F · Fuselage Miscellaneous Structure
  > LEFT MAIN WHEEL WELL INSIDE KEEL BEAM, STATION 910, VERTICAL ATTACH ANGLE, LOWER END CRACKED WITH STOP DRILL HOLE. INSTALLED REPAIR ANGLES IAW REA D853-41947.
- [SDR ABXA010862](https://openairdocs.org/sdr/ABXA010862.md): Door Frame · cracked · Jan 15, 2002 · N819AX · Doug DC863F · Fuselage Main, Structure
  > LEFT FORWARD ENTRY DOOR MADE A BINDING NOISE WHEN MOVED FROM FULL OPEN POSITION. FOUND SNUBBER SUPPORT WEB CRACKED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED NEW SPLICE AT BOTH ENDS IAW REA D853-41451MR.
- [SDR ABXA010858](https://openairdocs.org/sdr/ABXA010858.md): Skin · cracked · Jan 14, 2002 · N819AX · Doug DC863F · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE SKIN HAD CRACK WITH STOP HOLES AT XLS 710, OUTBOARD SIDE OF NR 4 ENGINE. INSTALLED DOUBLER REPAIR IAW DC-8 SRM 57-2-1.
- [SDR ABXA010860](https://openairdocs.org/sdr/ABXA010860.md): Skin · cracked · Jan 3, 2002 · N819AX · Doug DC863F · Wing, Plate/Skin
  > LEFT WING LEADING EDGE LOWER SKIN, JUST OUTBOARD OF THE NR 1 PYLON HAD 4 EACH CRACKS AT STATION XRS 525. INSTALLED DOUBLER REPAIR AND REPAIRED AREA IAW DC-8 SRM 57-2-1 AND 51-1-8.
- [SDR ABXA010857](https://openairdocs.org/sdr/ABXA010857.md): Skin · cracked · Dec 27, 2001 · N819AX · Doug DC863F · Fuselage Main, Plate/Skin
  > LEFT FREON COMPRESSOR EXHAUST CUTOUT HAD 2 SKIN CRACKS AT THE UPPER FORWARD AND AFT CORNERS. INSTALLED EXTERNAL DOUBLER REPAIR AROUND FREON COMPRESSOR EXHAUST IAW DC-8 SRM 53-2-1.
- [SDR ABXA010861](https://openairdocs.org/sdr/ABXA010861.md): Skin · cracked · Dec 23, 2001 · N819AX · Doug DC863F · Wing, Plate/Skin
  > LEFT WING TOP SKIN JUST AFT OF FRONT SPAR, SKIN HAD 1 INCH CRACK AT XW 400, INBOARD THE NR 1 PYLON. INSTALLED DOUBLER AND FILLER, REPAIRED AREA IAW REA D857-41949MR AND DC-8 SRM 51-1-20B, 51-1-20D, 51-1-12 AND 51-1-15.
- [SDR ABXA010500](https://openairdocs.org/sdr/ABXA010500.md): Valve · obstructed · Sep 23, 2001 · N819AX · Doug DC863 · Pressure Regulator/Outflow Valve
  > AUTO PRESSURIZATION WAS INOPERATIVE AND CABIN PRESSURIZATION COULD NOT BE CONTROLLED MANUALLY WITH ALL BLEEDS ON HIGH AND ALL CTC'S OPERATING. THE CREW DONNED OXYGEN MASKS AND DESCENDED TO FL 10. MAINTENANCE INSPECTED AND REMOVED A PIECE OF INSULATION FROM T
- [SDR ABXA010454](https://openairdocs.org/sdr/ABXA010454.md): Smoke Detector · defective · Aug 26, 2001 · N819AX · Doug DC863F · Smoke Detection
  > DURING CRUISE, LOWER CARGO SMOKE DETECTOR YELLOW MAINTENANCE LIGHT ILLUMINATED WITH GREEN LIGHT ILLUMINATED. REPLACED SMOKE DETECTOR UNIT AT AD CNT. DUE TO FALSE ALARM FAULT CODE IAW DC-8 MM 26-15-00-4. SYSTEM OPS CHECKED GOOD.
- [SDR ABXA010221](https://openairdocs.org/sdr/ABXA010221.md): Actuator · seized · May 8, 2001 · N819AX · Doug DC863 · Stabilizer Actuator
  > THE CREW REPORTED THE STABILIZER HYDRAULIC SYSTEM TO BE INOPERATIVE. THE LEFT SUITCASE HANDLE WAS JAMMED FULL FORWARD. MAINTENANCE INSPECTED AND REPLACED THE LEFT LONGITUDINAL TRIM ACTUATOR IAW DC8 MM.
- [SDR ABXA9900641](https://openairdocs.org/sdr/ABXA9900641.md): Control Valve · leaking · Aug 11, 1999 · N819AX · Doug DC863 · Landing Gear Retraction/Extension System
  > ON FINAL APPROACH, WHEN LANDING GEAR LOWERED, HYDRAULIC PRESSURE WAS DECREASING RAPIDLY. PERFORMED LOSS OF HYDRAULICS CHECK LIST. AIRCRAFT WAS TOWED FROM RUNWAY DUE TO LACK OF BRAKE PRESSURE. REPLACED LANDING GEAR CONTROL VALVE IAW DC8 MM 22-32-7. OPS CHE
- [SDR ABXA9900367](https://openairdocs.org/sdr/ABXA9900367.md): Window · lack of lube · May 10, 1999 · N819AX · Doug DC863 · Flight Compartment Windows
  > CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN ALL THE WAY. CLEANED DEBRIS FROM TRACK AND LUBED CLEARVIEW WINDOW. ROLLERS OPS CHECKED OK IAW DC-8 SMM 56-10-3.
- [SDR ABXA9900140](https://openairdocs.org/sdr/ABXA9900140.md): Compressor · stalled · Feb 24, 1999 · N819AX · Doug DC863F · Turbine Engine Compressor Section
  > NR 4 ENGINE COMPRESSOR STALLED WHEN REDUCING POWER FROM CLIMB TO CRUISE. ENGINE OIL QUANTITY DROPPED RAPIDLY FROM 3.1 TO 1.6 GALLONS. SHUT ENGINE DOWN. REPLACED NR 4 ENGINE IAW ABX JOB CARD J-8090507. OPS AND LEAK CHECKED GOOD.
- [SDR ABXA00108](https://openairdocs.org/sdr/ABXA00108.md): Warning · illuminated · Feb 17, 1999 · N819AX · Doug DC863 · Brake Anti-Skid Section
  > DURING APPROACH, ANTISKID LIGHT CAME ON 'LF0 AND LFI' LIGHTS ON SKID CONTROL PANEL WERE ON. AFTER RECYCLING THE GEAR, LIGHTS WENT OUT. TROUBLESHOT ANTISKID SYSTEM IAW DC8 MM. NO DEFECTS WERE FOUND, OPS CHECKED GOOD.
- [SDR ABXA9801059](https://openairdocs.org/sdr/ABXA9801059.md): Drive Link · cracked · Nov 15, 1998 · N819AX · Doug DC863F · Trailing Edge Flap Control System
  > WHILE COMPLYING WITH AD 88-10-7, FOUND CRACK INDICATION ON LEFT FLAP DRIVE LINK STATION 98 AT POINT J, OUTBOARD LUG. REPLACED LINK IAW DC8 MM 27-51-4.
- [SDR ABXA9800498](https://openairdocs.org/sdr/ABXA9800498.md): Angle · cracked · Jun 6, 1998 · N819AX · Doug DC863F · Wing Miscellaneous Structure
  > RIGHT WING INBOARD SLOT BOX, OUTBOARD AFT VERTICAL ANGLE IS CRACKED AT THE BOTTOM. REPAIRED IAW DC8 SRM 51-1-20D.
- [SDR ABXA9800497](https://openairdocs.org/sdr/ABXA9800497.md): Skin · cracked · Jun 6, 1998 · N819AX · Doug DC863F · Wing, Plate/Skin
  > LEFT WING UPPER TRAILING EDGE SKIN STATION XRS 160 AT THE REAR SPAR IS CRACKED IN 2 PLACES. REPAIRED SKIN IAW DC8 SRM 57-2-0.
- [SDR ABXA9800496](https://openairdocs.org/sdr/ABXA9800496.md): Skin · cracked · Jun 6, 1998 · N819AX · Doug DC863F · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE SKIN UPPER SURFACE AT STATION XFS 197 IS CRACKED AT A FASTENER HOLE. REPAIRED LEADING EDGE SKIN IAW DWG 5769859 AND DC8 SRM 57-2-0.
- [SDR ABXA9800489](https://openairdocs.org/sdr/ABXA9800489.md): Skin · cracked · Jun 5, 1998 · N819AX · Doug DC863F · Wing, Plate/Skin
  > LEFT WING LEADING EDGE UPPER SKIN INTERNAL DOUBLER AT STATION XS 251 CRACKED. REPAIRED IAW DACO DWG 5769759 AND DC8 SRM 51-3-0.
- [SDR ABXA9800657](https://openairdocs.org/sdr/ABXA9800657.md): Bulkhead Web · cracked · Jun 3, 1998 · N819AX · Doug DC863F · Fuselage Main, Bulkhead
  > 1.5 INCH CRACK AT AFT BULKHEAD STATION 1890, UPPER RIGHT CORNER ABOVE BRACKET WITH MOUNT BOLT FOR RUDDER POWER MECHANISM. REPAIRED IAW DC8 SRM 52-2-0.
- [SDR ABXA9800658](https://openairdocs.org/sdr/ABXA9800658.md): Bulkhead · cracked · May 27, 1998 · N819AX · Doug DC863F · Wing, Rib/Bulkhead
  > LEFT WING CANTED BULKHEAD LOWER FLANGE CRACKED AT XRS 508.977 BETWEEN STRINGERS 63-64. REPAIRED IAW ABX REA D853-22858MR AND DC8 SRM 51-1-20D.
- [SDR ABXA9800656](https://openairdocs.org/sdr/ABXA9800656.md): Fitting · cracked · May 23, 1998 · N819AX · Doug DC863F · Wing Miscellaneous Structure
  > ATTACH FITTING AT CANTED STATION XRS 495 TO STRINGER 63 (UPPER SKIN) HAS CRACK AT LAST FASTENER HOLE. FABRICATED REPLACEMENT ATTACH FITTING IAW DWG 3648143 AND ABX REA 857-22859.
- [SDR ABXA9800655](https://openairdocs.org/sdr/ABXA9800655.md): Angle · cracked · May 23, 1998 · N819AX · Doug DC863F · Fuselage Miscellaneous Structure
  > CRACK IN LEFT WING REAR SPAR LOWER CAP STATION 857 LBL 70 INBOARD APPROXIMATELY 9 LEFT MLG WHEEL WELL, FORWARD, LOWER, OUTBOARD. REPAIRED IAW DWG SR08570009 AND DC8 SRM 51-1-8 AND 51-1-20D.
- [SDR ABXA9800651](https://openairdocs.org/sdr/ABXA9800651.md): Frame · cracked · May 21, 1998 · N819AX · Doug DC863F · Fuselage Main, Frame
  > STATION 1040 FRAME UPPER CHORD, LOWER SURFACE AFT SIDE, AT LONGERON 31R AND 32R HAS HEAVY EXFOLIATION CORROSION AND IS CRACKED. REPAIRED IAW ABX REA D853-22857, SRM 51-1-21, 51-1-20D AND 51-1-11.
- [SDR ABXA9800591](https://openairdocs.org/sdr/ABXA9800591.md): Skin · cracked · May 20, 1998 · N819AX · Doug DC863F · Fuselage Main, Plate/Skin
  > TWO.25 INCH CRACK ON FWD PASSENGER ENTRY DOOR LOWER AFT CORNER SKIN PANEL. REPAIRED IAW DC8 SRM 53-2-0.
- [SDR ABXA9800592](https://openairdocs.org/sdr/ABXA9800592.md): Rib · cracked · May 19, 1998 · N819AX · Doug DC863F · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE AT STATION XFS 641.25 IS CRACKED AT UPPER END. REPAIRED IAW DRAWING ABX K05056.
- [SDR ABXA9800556](https://openairdocs.org/sdr/ABXA9800556.md): Fitting · cracked · May 19, 1998 · N819AX · Doug DC863F · Fuselage Miscellaneous Structure
  > STATION 440 TO 460 LONGERON 31R SPLICE FITTING IS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-21D AND 51-1-20D.
- [SDR ABXA9800555](https://openairdocs.org/sdr/ABXA9800555.md): Fitting · cracked · May 19, 1998 · N819AX · Doug DC863F · Fuselage Miscellaneous Structure
  > STATION 600 TO 620 LONGERON 31L SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D.
- [SDR ABXA9800593](https://openairdocs.org/sdr/ABXA9800593.md): Fitting · cracked · May 18, 1998 · N819AX · Doug DC863F · Fuselage Miscellaneous Structure
  > STATION 1120 FRAME TO CUSP FITTING, RIGHT SIDE IS CRACKED. REPAIRED IAW DC8 SRM 51-1-18 AND DWG 9755584.
- [SDR ABXA9800594](https://openairdocs.org/sdr/ABXA9800594.md): Rib · cracked · May 16, 1998 · N819AX · Doug DC863F · Fuselage Main, Bulkhead
  > LEFT WING LEADING EDGE STUB UPPER RIB CRACKED AT APPROXIMATELY XFS.550. REPAIRED IAW DC8 SRM 51-1-8, 51-1-20D AND ABX DWG K05056.
- [SDR ABXA9800595](https://openairdocs.org/sdr/ABXA9800595.md): Doubler · corrosion · May 15, 1998 · N819AX · Doug DC863F · Wing Miscellaneous Structure
  > RIGHT WING LEADING EDGE LOWER SKIN DOUBLER FORWARD EDGE BETWEEN STATION XFS 372.75 AND XF 379.0 HAS HEAVY EXFOLIATION CORROSION. REPAIRED IAW DC8 SRM 51-3-0 AND DWG 5641253.
- [SDR ABXA9800596](https://openairdocs.org/sdr/ABXA9800596.md): Fitting · cracked · May 13, 1998 · N819AX · Doug DC863F · Fuselage Miscellaneous Structure
  > AFT END FITTING ON LONGERON INTERCOSTAL AT STATION 717, LONGERON 14L IS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-20D.
- [SDR ABXA9800564](https://openairdocs.org/sdr/ABXA9800564.md): Angle · cracked · May 11, 1998 · N819AX · Doug DC863F · Fuselage Miscellaneous Structure
  > TORQUE BOX WEB LOWER SUPPORT ANGLE CRACKED FROM FS 190 TO FS 200, LONGERON 21R. REPAIRED IAW DWG 575700 AND DC8 SRM 51-1-21, 51-1-21D AND 51-1-8.

Next page: https://openairdocs.org/deregistered/N819AX-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 = 'N819AX' AND deregistration_id = 'N819AX-2009-07-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N819AX-2009-07-21/reports

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