# Service difficulty reports: N808AX, cancelled Mar 12, 2004

A list on [N808AX, cancelled Mar 12, 2004](https://openairdocs.org/deregistered/N808AX-2004-03-12.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 · 74 reports

- [SDR ABXA000493](https://openairdocs.org/sdr/ABXA000493.md): Valve · leaking · Nov 13, 2000 · N808AX · Doug DC862 · Hydraulic System, Main
  > FLIGHT CREW REPORTED A LOSS OF HYDRAULIC PRESSURE WITH AN ASSOCIATED HYDRAULIC QUANTITY LOSS INDICATION. THE FLIGHT CREW PERFORMED EMERGENCY PROCEDURES. MAINTENANCE INSPECTED AND REPLACED THE SLOT CONTROL VALVE IAW DC-8 MM 27-80-00. OPS CHECKED GOOD.
- [SDR ABXA9900754](https://openairdocs.org/sdr/ABXA9900754.md): Generator · defective · Oct 28, 1999 · N808AX · Doug DC862 · AC Generator-Alternator
  > FAULT ON NR 4 GENERATOR. UNABLE TO RESET IAW ABNORMAL CHECKLIST. SECURED ENGINE, MAINTAINED POSITIVE ENGINE OIL PRESSURE. INSPECTED MAIN OIL FILTER, FOUND NO CONTAMINATION. CHECKED OIL QUANTITY, RAN ALL ENGINES, ENGINE RUN WAS NORMAL. CHECKED AIRCRAFT WIRI
- [SDR ABXA9900691](https://openairdocs.org/sdr/ABXA9900691.md): Skin · corroded · Sep 2, 1999 · N808AX · Doug DC862 · Fuselage Main, Plate/Skin
  > SKIN CORRODED AT STATION 240, BELOW LONGERON 3 LEFT. REPAIRED IAW ABX REA D853-32664MR.
- [SDR ABXA9900690](https://openairdocs.org/sdr/ABXA9900690.md): Fitting · cracked · Sep 2, 1999 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > LONGERON SPLICE FITTING CRACKED AT STATION 390 AND LONGERON 33 -35 RIGHT. REPAIRED IAW ABX REA D853-32693MR.
- [SDR ABXA9900368](https://openairdocs.org/sdr/ABXA9900368.md): Duct · ruptured · May 14, 1999 · N808AX · Doug DC862 · Cabin Pressure Control System
  > ON LEVEL OFF AT 37,000 FEET, CABIN STARTED TO CLIMB AT 3,000 FEET PER MINUTE. COULD NOT CONTROL CABIN RATE. DESCENDED TO 24,000 FEET AND REGAINED CONTROL OF CABIN. MAINTAINED CABIN AT 9,000 FEET. HEARD LOUD NOISE BY THE RIGHT HAND CTC'S AT 37,000. OXYGEN
- [SDR ABXA9900280](https://openairdocs.org/sdr/ABXA9900280.md): Pump · leaking · Apr 7, 1999 · N808AX · Doug DC862 · Rudder Control System
  > DURING CRUISE, ONE HOUR AND TWENTY MINUTES INTO FLIGHT EXPERIENCED LOSS OF HYDRAULIC QUANTITY DOWN TO STANDPIPE. PERFORMED LOSS OF HYDRAULICS PROCEDURES. REPLACED STANDBY RUDDER PUMP IAW DC8 MM 29-27-00, OPS CHECKED GOOD.
- [SDR ABXA9900038](https://openairdocs.org/sdr/ABXA9900038.md): Latch · out of adjust · Jan 26, 1999 · N808AX · Doug DC862 · Fixed Inner Doors
  > DURING POSTFLIGHT CHECK, CABIN DOOR LOCK WAS STUCK IN LOCKED POSITION. FOUND OUTER LATCH ASSEMBLY MISADJUSTED 180 DEGREES. READJUSTED LATCH TO PROPER POSITION, OPS CHECKED GOOD.
- [SDR ABXA9900039](https://openairdocs.org/sdr/ABXA9900039.md): Latch · out of adjust · Jan 21, 1999 · N808AX · Doug DC862 · Fixed Inner Doors
  > DURING POSTFLIGHT, FOUND COCKPIT DOOR KNOB STUCK. ADJUSTED AND LUBRICATED INTERNAL MECHANISM IAW DC8 SRM.
- [SDR ABXA9701937](https://openairdocs.org/sdr/ABXA9701937.md): Frame · corrosion · Nov 22, 1997 · N808AX · Doug DC862 · Fuselage Main, Frame
  > FRAME 1020, UPPER FLANGE AT LONGERON 34R IS CORRODED BEYOND LIMITS. REPAIRED IAW DC8 SRM 53-2-0 AND 51-1-21.
- [SDR ABXA9701936](https://openairdocs.org/sdr/ABXA9701936.md): Fitting · cracked · Nov 22, 1997 · N808AX · Doug DC862 · Fuselage Main, Structure
  > STA 860 FWD SIDE AT STRINGER 18R TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
- [SDR ABXA9701935](https://openairdocs.org/sdr/ABXA9701935.md): Fitting · cracked · Nov 22, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > STA 900 AFT SIDE STRINGER 18R INTERCOSTAL TIE FITTING IS CRACKED. INSTALLED INTERCOSTAL TIE FITTING IAW DWG 4750428 AND SRM 51-1-20D.
- [SDR ABXA9701934](https://openairdocs.org/sdr/ABXA9701934.md): Fitting · cracked · Nov 22, 1997 · N808AX · Doug DC862 · Trailing Edge Flaps
  > LEFT STA 410 FLAP CANOE FITTING INBOARD SIDE SUPPORT FITTING IS CRACKED. REPAIRED IAW SRM 51-2-0.
- [SDR ABXA9701879](https://openairdocs.org/sdr/ABXA9701879.md): Fitting · cracked · Nov 22, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > STA 900 INTERCOSTAL TIE FITTING IS CRACKED AT AFT SIDE AT STR 18R. REPAIRED IAW SWG 4750428 AND SRM 51-1-20D.
- [SDR ABXA9701878](https://openairdocs.org/sdr/ABXA9701878.md): Fitting · cracked · Nov 22, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > STA 860 FWD SIDE AT STRINGER 18R TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
- [SDR ABXA9701877](https://openairdocs.org/sdr/ABXA9701877.md): Frame · corroded · Nov 22, 1997 · N808AX · Doug DC862 · Fuselage Main, Frame
  > FRAME 1020 UPPER FLANGE AT LONGERON 34R HAS CORROSION BEYOND LIMITS. REPAIRED IAW SRM 53-2-0 AND 51-1-21.
- [SDR ABXA9701889](https://openairdocs.org/sdr/ABXA9701889.md): Cap · cracked · Nov 14, 1997 · N808AX · Doug DC862 · Nacelle/Pylon Structure
  > NR 2 PYLON CAP IS CRACKED AT SCREW HOLE, OUTBOARD UPPER SIDE, JUST FWD OF TOMBSTONE FITTING. REPAIRED IAW SRM 54-2-2.
- [SDR ABXA9701927](https://openairdocs.org/sdr/ABXA9701927.md): Channel · cracked · Nov 13, 1997 · N808AX · Doug DC862 · Wing Miscellaneous Structure
  > CANTED WEB CHANNEL HAS CRACK IN NR 4 ALT TANK, AT RT WING STA 508.977. REPAIRED IAW DWG 56 1326 AND DC8 SRM 51-1-21.
- [SDR ABXA9701885](https://openairdocs.org/sdr/ABXA9701885.md): Channel · cracked · Nov 13, 1997 · N808AX · Doug DC862 · Wing Miscellaneous Structure
  > CANTED WEB CHANNEL HAS CRACK AT NR 4 ALT TANK, AT RT WING STA 508.977. REPAIRED IAW SRM 51-1-21 AND DWG 56-1326.
- [SDR ABXA9701919](https://openairdocs.org/sdr/ABXA9701919.md): Skin · cracked · Nov 12, 1997 · N808AX · Doug DC862 · Elevator, Plate/Skin
  > THE RT ELEVATOR LWR SKIN AT STA XE 55.012 AND JUST FWD OF THE TRAILING EDGE IS CRACKED. THE CRACK IS APPROX 1.8 LONG. REPAIRED IAW DC8 SRM 53-2-1.
- [SDR ABXA9701917](https://openairdocs.org/sdr/ABXA9701917.md): Angle · corroded · Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > UPPER ANGLE OF INTERCOSTAL AT FS 980 TO 1000 LONGERON 35L CORRODED BEYOND LIMITS. INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-0, 51-1-20D.
- [SDR ABXA9701916](https://openairdocs.org/sdr/ABXA9701916.md): Angle · corroded · Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > LOWER L-ANGLE IN KEEL BEAM AREA BETWEEN WHEEL WELL DOORS, 2ND FROM FRONT (APPROX FS 890) CORRODED BEYOND ALLOWABLE LIMITS. FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-0, 51-1-20D AND 51-1-21.
- [SDR ABXA9701915](https://openairdocs.org/sdr/ABXA9701915.md): Longeron · cracked · Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Main, Longeron/Stringer
  > LONGERON 35R CRACKED AT FS 1195 AT INBOARD FLANGE. REPLACED DAMAGED SECTION OF LONGERON IAW ABX REA D853-21175.
- [SDR ABXA9701914](https://openairdocs.org/sdr/ABXA9701914.md): Longeron · corroded · Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Main, Longeron/Stringer
  > LONGERON 22R CORRODED BEYOND LIMITS FROM STA 270 TO 280. REPLACED SECTION OF LONGERON IAW SRM 53-2-2 AND SRM 53-4-1.
- [SDR ABXA9701913](https://openairdocs.org/sdr/ABXA9701913.md): Fitting · cracked · Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > STA 860 AFT SIDE AT STR 18R TIE FITTING IS CRACKED. INSTALLED NEW FITTING IAW SRM 51-1-20D AND DWG 4750422.
- [SDR ABXA9701912](https://openairdocs.org/sdr/ABXA9701912.md): Fitting · cracked · Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > STA 440 TO 460 STR 31L SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING PER SRM 53-1-0 AND 51-1-20.
- [SDR ABXA9701911](https://openairdocs.org/sdr/ABXA9701911.md): Fitting · cracked · Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > ACCESSORY COMP STA 680 BL 0, THE SEAT TRACK SUPPORT FITTING IS CRACKED. REPAIRED IAW SRM 51-1-20D, DWG 4645517 AND SRM 51-1-8.
- [SDR ABXA9701898](https://openairdocs.org/sdr/ABXA9701898.md): Longeron · cracked · Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Main, Longeron/Stringer
  > LONGERON 35R CRACKED AT FS 1195, INBOARD FLANGE. REPLACED DAMAGED SECTION OF LONGERON 35R IAW REA D853-21175.
- [SDR ABXA9701897](https://openairdocs.org/sdr/ABXA9701897.md): Angle · corroded · Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > LOWER L-ANGLE IN KEEL BEAM AREA, BETWEEN WHEEL WELL DOORS, 2ND FROM FRONT (APPROX FS 890) CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-0, 51-1-20D AND 51-1-21.
- [SDR ABXA9701896](https://openairdocs.org/sdr/ABXA9701896.md): Angle · corroded · Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > UPPER ANGLE OF INTERCOSTAL AT FS 980 TO 1000 LONGERON 35L CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-0, 51-1-20D.
- [SDR ABXA9701875](https://openairdocs.org/sdr/ABXA9701875.md): Longeron · corrosion · Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Main, Longeron/Stringer
  > LONGERON 22R CORRODED BEYOND LIMITS AT STA 270-280. REPAIRED IAW SRM 53-2-2, AND SRM 53-4-1.
- [SDR ABXA9701858](https://openairdocs.org/sdr/ABXA9701858.md): Fitting · cracked · Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > SEAT TRACK SUPPORT FITTING IS CRACKED, IN ASSY COMPARTMENT, STA 680 AT BL O. REPAIRED IAW SRM 51-1-20D, DWG 4645517 AND SRM 51-1-8.
- [SDR ABXA9701857](https://openairdocs.org/sdr/ABXA9701857.md): Fitting · cracked · Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > STA 440-460, STR 31L, SPLICE FITTING IS CRACKED. REPAIRED IAW SRM 53-1-0 AND 51-1-20.
- [SDR ABXA9701856](https://openairdocs.org/sdr/ABXA9701856.md): Fitting · cracked · Nov 12, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > STA 860, AFT SIDE AT STR 18R, TIE FITTING IS CRACKED. REPAIRED IAW SRM 51-1-20D AND DWG 4750422.
- [SDR ABXA9701923](https://openairdocs.org/sdr/ABXA9701923.md): Skin · cracked · Nov 4, 1997 · N808AX · Doug DC862 · Trailing Edge Flaps
  > LEFT WING FLAP TRAILING EDGE CRACKED AT STA XW 191. REPAIRED IAW DC8 SRM 57-7-0 AND 51-1-21.
- [SDR ABXA9701920](https://openairdocs.org/sdr/ABXA9701920.md): Rib · cracked · Nov 4, 1997 · N808AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE UPPER RIB CRACKED AT FS XFS 303. REPAIRED IAW DC8 SRM 57-2-0 AND DWG KO 5606.
- [SDR ABXA9701909](https://openairdocs.org/sdr/ABXA9701909.md): Angle · corroded · Nov 4, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > FRAME SUPPORT ANGLE ON FWD SIDE OF FRAME 1280 HAS HEAVY CORROSION ABOVE LONGERON 36. REPLACED ANGLE IAW SRM 53-4-1.
- [SDR ABXA9701894](https://openairdocs.org/sdr/ABXA9701894.md): Rib · cracked · Nov 4, 1997 · N808AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING, LEADING EDGE UPPER RIB CRACKED AT FS XFS 303. REPAIRED IAW SRM 57-2-0, 51-1-20D, AND DWG K O 5056.
- [SDR ABXA9701891](https://openairdocs.org/sdr/ABXA9701891.md): Flap · cracked · Nov 4, 1997 · N808AX · Doug DC862 · Trailing Edge Flaps
  > LEFT WING FLAP, TRAILING EDGE CRACKED AT STA XW 191. REPAIRED IAW SRM 57-7-0 AND 51-1-21.
- [SDR ABXA9701860](https://openairdocs.org/sdr/ABXA9701860.md): Angle · corroded · Nov 4, 1997 · N808AX · Doug DC862 · Fuselage Miscellaneous Structure
  > FRAME SUPPORT ANGLE ON FWD SIDE OF FRAME 1280 HAS HEAVY CORROSION ABOVE LONGERON 36. REPLACED ANGLE IAW SRM 53-4-1.
- [SDR ABXA9701932](https://openairdocs.org/sdr/ABXA9701932.md): Rib · cracked · Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE UPPER RIB CRACKED AT XFS 331. REPAIRED IAW DC8 SRM 57-2-0 AND 51-1-20D.
- [SDR ABXA9701929](https://openairdocs.org/sdr/ABXA9701929.md): Rib · cracked · Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE UPPER RIB CRACKED AT XFS 432. REPAIRED IAW DC8 SRM 57-2-0 AND 51-1-20D.
- [SDR ABXA9701928](https://openairdocs.org/sdr/ABXA9701928.md): Rib · cracked · Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE UPPER RIB CRACKED AT XFS 341. REPAIRED IAW DC8 SRM 57-2-0 AND 51-1-20D.
- [SDR ABXA9701924](https://openairdocs.org/sdr/ABXA9701924.md): Rib · cracked · Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/Bulkhead
  > UPPER RIB CRACKED AT STA XFS 415 LEFT WING LEADING EDGE. REPAIRED IAW DC8 SRM 57-2-0 AND DWG KO5056.
- [SDR ABXA9701921](https://openairdocs.org/sdr/ABXA9701921.md): Rib · cracked · Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING UPPER RIB CRACKED AT STA XFS 360. REPAIRED IAW DC8 SRM 57-2-0 AND DWG KO 5056.
- [SDR ABXA9701893](https://openairdocs.org/sdr/ABXA9701893.md): Rib · cracked · Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING, LEADING EDGE HAS CRACKED UPPER RIB AT STA XFS 360. REPAIRED IAW SRM 57-2-0, 51-1-20, AND DWG K O 5056.
- [SDR ABXA9701890](https://openairdocs.org/sdr/ABXA9701890.md): Rib · cracked · Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE, UPPER RIB CRACKED XFS 415. REPAIRED IAW SRM 57-2-0, 51-1-8 AND DWG K O 5056.
- [SDR ABXA9701884](https://openairdocs.org/sdr/ABXA9701884.md): Rib · cracked · Nov 3, 1997 · N808AX · Doug DC862 · Wing Structure
  > LEFT WING, LEADING EDGE UPPER RIB CRACKED AT XFS 341. REPAIRED IAW SRM 57-2-0 AND 51-1-20D.
- [SDR ABXA9701883](https://openairdocs.org/sdr/ABXA9701883.md): Rib · cracked · Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE RIB CRACKED AT XFS 432. REPAIRED IAW SRM 51-1-120D AND 51-1-8.
- [SDR ABXA9701881](https://openairdocs.org/sdr/ABXA9701881.md): Rib · cracked · Nov 3, 1997 · N808AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING, LEADING EDGE RIB CRACKED AT XFS 331. REPAIRED IAW SRM 51-1-20D AND 51-1-8.
- [SDR ABXA9701888](https://openairdocs.org/sdr/ABXA9701888.md): Skin · corroded · Oct 31, 1997 · N808AX · Doug DC862 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STABILIZER LEADING EDGE SKIN IS CORRODED AT STA XFS 178. REPAIRED IAW SRM 51-1-21 AND 51-1-26.

Next page: https://openairdocs.org/deregistered/N808AX-2004-03-12/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 = 'N808AX' AND deregistration_id = 'N808AX-2004-03-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N808AX-2004-03-12/reports

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