# Service difficulty reports: N822AX, cancelled Dec 30, 2003

A list on [N822AX, cancelled Dec 30, 2003](https://openairdocs.org/deregistered/N822AX-2003-12-30.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 · 149 reports

- [SDR ABXA030116](https://openairdocs.org/sdr/ABXA030116.md): Computer · defective · Mar 12, 2003 · N822AX · Doug DC863 · Autopilot System
  > IN CRUISE FLIGHT, FL350, MACH.770, AUTOPILOT ON. RUDDER GAVE UNCOMMANDED INPUT TO LEFT SIDE ON TWO OCCASIONS. RETURNED TO CENTER BY ITSELF, YAW DAMPER ON. REPLACED YAW AXIS COMPUTER. SYSTEM OPS CHECKED GOOD IAW DC-8 MM 22-10-00.
- [SDR ABXA020348](https://openairdocs.org/sdr/ABXA020348.md): Battery · discharged · Dec 4, 2002 · N822AX · Doug DC863 · Emergency Lighting
  > EMERGENCY LIGHTS DIM WHEN PERFORMED CHECK FOR (A) CHECK. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW MM.
- [SDR ABXA020215](https://openairdocs.org/sdr/ABXA020215.md): Wire · broken · Sep 20, 2002 · N822AX · Doug DC863 · Light System Wiring
  > EMERGENCY EXIT LIGHTS DISARM CHECK WAS INOPERATIVE. FOUND WIRE NR 1 BROKEN AT EMERGENCY LIGHT SWITCH (R7-61). REPAIRED WIRE IAW DC-8 WD 33-51-01. OPS CHECKED GOOD.
- [SDR ABXA010618](https://openairdocs.org/sdr/ABXA010618.md): Cylinder · defective · Dec 2, 2001 · N822AX · Doug DC863 · Landing Gear Retraction/Extension System
  > WHEN GEAR HANDLE WAS PLACED IN THE UP POSITION AFTER TAKEOFF, THE REG GEAR UNSAFE LIGHT STAYED ON. ALL GREEN LIGHTS WERE OUT. THE RIGHT MAIN LANDING GEAR DOOR NOT LOCKED LIGHT WAS ON. ABNORMALS COMPLETE. REPLACED THE RIGHT BOGIE TRIM CYLINDER DUE TO SWIVEL
- [SDR ABXA010556](https://openairdocs.org/sdr/ABXA010556.md): Battery · discharged · Oct 26, 2001 · N822AX · Doug DC863 · Emergency Lighting
  > EMERGENCY LIGHTING WAS INOPERATIVE. REPLACED BATTERY EMERGENCY LIGHT RACK ASSEMBLY. EMERGENCY LIGHT OPS CHECKED GOOD PER AMM 33-50-02.
- [SDR ABXA010355](https://openairdocs.org/sdr/ABXA010355.md): Window · obstructed · Jun 26, 2001 · N822AX · Doug DC863 · Flight Compartment Windows
  > FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. FOUND AFT LOWER LOCK ON FIRST OFFICER'S WINDOW OBSTRUCTED BY SEALANT. REMOVED SEALANT. WINDOW OPERATED NORMAL.
- [SDR ABXA010277](https://openairdocs.org/sdr/ABXA010277.md): Window · out of adj · May 31, 2001 · N822AX · Doug DC863 · Flight Compartment Windows
  > RIGHT CLEAR VIEW WINDOW WOULD NOT OPEN. ADJUSTED RIGHT CLEAR VIEW WINDOW IAW DC-8 MM 56-10-3. REPAIRED EPOCAST. PRESSURIZED AIRCRAFT TO 4 PSID. NO LEAKS NOTED. WINDOW OPENS FREELY.
- [SDR ABXA010280](https://openairdocs.org/sdr/ABXA010280.md): Fitting · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO Z-FITTING, STATION 1220, LONGERON 33 - 34 LEFT CORRODED. REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-8, AND 51-1-20D.
- [SDR ABXA010279](https://openairdocs.org/sdr/ABXA010279.md): Stringer · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Main, Longeron/Stringer
  > STATION 320 STRINGER 34 RIGHT HAD CORROSION INBOARD SIDE. REPAIRED AREA IAW DC-8 SRM 53-2-0, AND DC-8 SRM 51.
- [SDR ABXA010278](https://openairdocs.org/sdr/ABXA010278.md): Longeron · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Main, Longeron/Stringer
  > AFT CARGO AT FS 1060 - 1080 LONGERON 36 WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51, DAC DWG 9758507, AND REA 853-40346MR.
- [SDR ABXA010255](https://openairdocs.org/sdr/ABXA010255.md): Fitting · cracked · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > AFT CARGO AT FS 1200, AT LONGERON 35 RIGHT Z-FITTING WAS CRACKED. REMOVED AND REPLACED Z-FITTING IAW DC-8 SRM 53-3-0, 53-2-0, 51-1-8, AND 51-1-20D.
- [SDR ABXA010254](https://openairdocs.org/sdr/ABXA010254.md): Fitting · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > AFT CARGO AT FS 1200 BETWEEN LONGERON 33 RIGHT - 34 RIGHT Z-FITTING WAS CORRODED. REMOVED AND REPLACED Z-FITTING IAW DC-8 SRM 53-2-0, 51-1-8, AND 51-1-20D.
- [SDR ABXA010253](https://openairdocs.org/sdr/ABXA010253.md): Fitting · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > AFT CARGO AT FS 1180 BETWEEN LONGERON 33 RIGHT - 34 RIGHT Z-FITTING WAS CORRODED. REMOVED AND REPLACED Z-FITTING IAW DC-8 SRM 51-1-20D, 53-2-0, AND 51-1-8.
- [SDR ABXA010252](https://openairdocs.org/sdr/ABXA010252.md): Fitting · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > AFT CARGO AT FS 1150 BETWEEN LONGERON 31 LEFT TO 32 LEFT Z-FITTING WAS CRACKED. REMOVED AND REPLACED Z-FITTING IAW DC-8 SRM 53-2-0, 51-1-8, AND 51-1-20D.
- [SDR ABXA010260](https://openairdocs.org/sdr/ABXA010260.md): Fitting · corroded · May 25, 2001 · N822AX · Doug DC863 · Wing Miscellaneous Structure
  > LEFT WING REAR SPAR SKI FITTING TO BOTTLE BOLT VERTICAL ATTACH FITTING HAD CORROSION AT LOWER SKI FITTING ATTACH AREA (P/N 3641117-1). REPAIRED AREA IAW DC-8 SRM 51.
- [SDR ABXA010271](https://openairdocs.org/sdr/ABXA010271.md): Frame · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Main, Frame
  > AFT CARGO AT FS 1340 ABOVE LONGERON 36 FRAME WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51.
- [SDR ABXA010270](https://openairdocs.org/sdr/ABXA010270.md): Fitting · corroded · May 25, 2001 · N822AX · Doug DC863 · Wing Miscellaneous Structure
  > LEFT WING TRAPEZOID FITTING VERTICAL ATTACH FITTING P/N 5616344-1 WAS CORRODED. REPLACED FITTING IAW DC-8 SRM 51.
- [SDR ABXA010269](https://openairdocs.org/sdr/ABXA010269.md): Fitting · corroded · May 25, 2001 · N822AX · Doug DC863 · Wing Miscellaneous Structure
  > LEFT WING REAR SPAR SKI FITTING TO BOTTLE BOLT VERTICAL ATTACH FITTING HAD CORROSION AT LOWER SKI FITTING ATTACH AREA. P/N 3641117-2. REPAIRED AREA IAW DC-8 SRM 51.
- [SDR ABXA010268](https://openairdocs.org/sdr/ABXA010268.md): Panel · cracked · May 25, 2001 · N822AX · Doug DC863 · Wing, Plate/Skin
  > SIX BOLT HOLES REAMED UP AFTER NDT CHECK BEYOND LIMITS OF SRM PANEL 505 F. REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1-20D, 51-1-20B, 51-1-21, DAC DWG 5613609, AND REA D857-40362MR.
- [SDR ABXA010267](https://openairdocs.org/sdr/ABXA010267.md): Bulkhead · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Main, Bulkhead
  > AFT LOWER CARGO STA 980 BETWEEN LONGERON 35 RIGHT TO LONGERON 35 LEFT LOWER BULKHEAD HAD CORROSION AT PREVIOUS REPAIR. REPAIRED IAW DC-8 SRM 53-2-0, 51-1-24, 51-1-8, AND REA D853-40335 MR.
- [SDR ABXA010266](https://openairdocs.org/sdr/ABXA010266.md): Longeron · cracked · May 25, 2001 · N822AX · Doug DC863 · Fuselage Main, Longeron/Stringer
  > LONGERON 24 LEFT CRACKED BETWEEN FASTENERS, TOPSIDE STA 980. REPAIRED AREA IAW DC-8 SRM 53-2-2, 51-1-8, AND 51-1-20.
- [SDR ABXA010265](https://openairdocs.org/sdr/ABXA010265.md): Fitting · damaged · May 25, 2001 · N822AX · Doug DC863 · Wing Miscellaneous Structure
  > RIGHT WING SKI FITTING AREA HAS 2 DAMAGED FASTENER HOLES AT STA 51 AND AFT SPAR. REPAIRED AREA IAW DC-8 SRM 51-1-12, 51-1-8, 51-1-20D, AND REA D857-40385.
- [SDR ABXA010264](https://openairdocs.org/sdr/ABXA010264.md): Fitting · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > AFT CARGO AT FS 1180 BETWEEN LONGERON 32 - 33 LEFT Z-FITTING WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-3, 51-1-0, 52-2-0, AND 53-2-0.
- [SDR ABXA010263](https://openairdocs.org/sdr/ABXA010263.md): Support Fitting · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > TAILSKID LEFT UPPER SUPPORT FITTING HAD CORROSION AROUND 3 OUTBOARD FASTENERS ON UPPER SIDE OF FITTING AT FS 1766 LEFT BUTT LINE 8. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-3-0, AND DAC DWG 5753522.
- [SDR ABXA010262](https://openairdocs.org/sdr/ABXA010262.md): Fitting · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > AFT CARGO AT FS 1150 BETWEEN LONGERON 35 RIGHT - 36 RIGHT Z-FITTING WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1-20D, AND 53-2-0.
- [SDR ABXA010261](https://openairdocs.org/sdr/ABXA010261.md): Longeron · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Main, Longeron/Stringer
  > AFT LOWER CARGO STA 1050-1070 LONGERON 35 RIGHT, LONGERON AND SPLICE ASSEMBLY HAD CORROSION BETWEEN LONGERON SPLICE ASSEMBLY AND SKIN, CAUSING BULGE BETWEEN SKIN AND LONGERON. REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-8, 51-20D, 51-1-21, 51-3-0, AND DAC DWG 975
- [SDR ABXA010259](https://openairdocs.org/sdr/ABXA010259.md): Fitting · corroded · May 25, 2001 · N822AX · Doug DC863 · Wing Miscellaneous Structure
  > LEFT WING REAR SPAR XRS 0 AFT FACE OF VERTICAL WEB HAD CORROSION OMITTING AROUND FASTENERS. REPAIRED AREA IAW DC-8 SRM 51, DAC DWG'S 4753127, 4652943, 4652944, 5751690, AND REA'S D857-40389, AND D857-40382MR.
- [SDR ABXA010258](https://openairdocs.org/sdr/ABXA010258.md): Fitting · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > UPPER SIDE OF LONGERON NR 24 FITTING CORRODED AT RIGHT MAIN LANDING GEAR WHEEL WELL, AT FORWARD AND AFT SIDE OF FS 920 BATHTUB FITTING, AND FS 920 BATHTUB FITTING CORRODED ON AFT SIDE AT UPPER PRESSURE WEB. REPLACED BATHTUB FITTING IAW DC-8 SRM 51-1-8, 51-1-2
- [SDR ABXA010256](https://openairdocs.org/sdr/ABXA010256.md): Fitting · broken · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > AFT CARGO AT FS 1160, BETWEEN LONGERON 27 LEFT - 28 LEFT Z-FITTING ATTACHING FLANGES WERE MISSING. REPLACED Z-FITTING IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-20D, 51-3-0, AND 51-1-21.
- [SDR ABXA010242](https://openairdocs.org/sdr/ABXA010242.md): Attach Angle · cracked · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT AT FS 1260 ABOVE LONGERON 35 RIGHT, FLOOR ATTACH ANGLE CRACKED. REPAIRED AREA IAW DAC DWG 9754949 AND DC8 SRM 51.
- [SDR ABXA010251](https://openairdocs.org/sdr/ABXA010251.md): Support Fitting · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > TAILSKID RIGHT UPPER SUPPORT FITTING CORRODED AROUND (3) OUTBOARD FASTENERS ON UPPER SIDE OF FITTING AT FS 1766 RBL 8. REPLACED RIGHT TAILSKID UPPER SUPPORT FITTING IAW DC8 SRM 51-1-2, AND DWG 5753522.
- [SDR ABXA010250](https://openairdocs.org/sdr/ABXA010250.md): Fitting · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT AT FS 1230 BETWEEN LONGERON 33 - 34 RIGHT, Z-FITTING CORRODED. REPLACED Z-FITTING IAW DC8 SRM 53-2-0, AND DC8 SRM 51.
- [SDR ABXA010249](https://openairdocs.org/sdr/ABXA010249.md): Fitting · cracked · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO Z-FITTING, STA 1160 LONGERON 34 - 33 RIGHT, FLANGE CRACKED AT FASTENER HOLE. REPAIRED IAW DC8 SRM 51, AND DC8 SRM 53.
- [SDR ABXA010248](https://openairdocs.org/sdr/ABXA010248.md): Fitting · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO STA 1160 LONGERON 36 - 35 RIGHT, Z-FITTING CORRODED. REPLACED CRACKED FITTING IAW DC8 SRM 53-2-0.
- [SDR ABXA010247](https://openairdocs.org/sdr/ABXA010247.md): Angle · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO Z-FITTING, STA 1180 LONGERON 34 - 33 RIGHT CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. FABBED AND INSTALLED ANGLE IAW DC8 SRM 53-2-0.
- [SDR ABXA010246](https://openairdocs.org/sdr/ABXA010246.md): Intercostal · corroded · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO STA 980 LONGERON 35 LEFT INTERCOSTAL LOWER FLANGE CORRODED AT FASTENERS. REMOVED CORROSION IAW DC8 SRM 51-1-8. FABBED NEW INTERCOSTAL AND INSTALLED IAW DAC DWG 5779929, DC8 SRM 51-1-8, AND 51-1-20.
- [SDR ABXA010245](https://openairdocs.org/sdr/ABXA010245.md): Angle · cracked · May 25, 2001 · N822AX · Doug DC863 · Ailerons
  > RIGHT INBOARD AILERON ON OUTBOARD TRAILING EDGE CRACKED. REPAIRED AREA IAW DAC DWG 5705334, DC8 SRM 51-1-8, 51-1-24, AND 51-1-21.
- [SDR ABXA010244](https://openairdocs.org/sdr/ABXA010244.md): Web · cracked · May 25, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO COMPARTMENT (C2) DOOR TORQUE BOX WEB CRACKED/CORRODED AT FASTENER HOLE, STA 560 LONGERON 34 RIGHT. REPAIRED IAW DC8 SRM 51.
- [SDR ABXA010243](https://openairdocs.org/sdr/ABXA010243.md): Seal Bracket · cracked · May 25, 2001 · N822AX · Doug DC863 · Service Doors
  > RIGHT (TYPE I) FORWARD DOOR, FORWARD LOWER CORNER SEAL DEPRESSION CRACKED. REPAIRED IAW DC8 SRM 52-2-2.
- [SDR ABXA010239](https://openairdocs.org/sdr/ABXA010239.md): Window · stuck · May 25, 2001 · N822AX · Doug DC863 · Flight Compartment Windows
  > FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. REMOVED EXCESSIVE SEALANT FROM EPICAST AREA. WINDOW OPERATED NORMALLY IAW DC-8 MM 56-10-3.
- [SDR ABXA010238](https://openairdocs.org/sdr/ABXA010238.md): Downlock Switch · failed · May 25, 2001 · N822AX · Doug DC863 · Landing Gear Position and Warning
  > RIGHT MAIN GEAR DOWN GREEN LIGHT DID NOT COME ON, ON GEAR EXTENSION. REPLACED RIGHT MAIN GEAR LOCK SWITCH PER DC-8 MM 32-60-00.
- [SDR ABXA010214](https://openairdocs.org/sdr/ABXA010214.md): Trunnion · corroded · May 2, 2001 · N822AX · Doug DC863 · Main Landing Gear Attach Section
  > THE LEFT MAIN LANDING GEAR TRUNNION FORWARD FITTING HAS CORROSION IN BOTH FWD BORES.
- [SDR ABXA010213](https://openairdocs.org/sdr/ABXA010213.md): Fitting · corroded · May 2, 2001 · N822AX · Doug DC863 · Main Landing Gear
  > THE LEFT MAIN LANDING GEAR FORWARD LUG IS CORRODED AND GOUGED INSIDE THE BORE.
- [SDR ABXA010117](https://openairdocs.org/sdr/ABXA010117.md): Shaft · sheared · Apr 5, 2001 · N822AX · Doug DC863 · Stabilizer Control System
  > THE HORIZONTAL STABILIZER OPERATING BULKHEAD, LEFT SIDE AFT END, HAD A SHEARED SHAFT.
- [SDR ABXA010190](https://openairdocs.org/sdr/ABXA010190.md): Panel · cracked · Apr 2, 2001 · N822AX · Doug DC863 · Wing, Plate/Skin
  > PANEL 505F BOLT HOLES HAVE CRACK INDICATIONS FOUND DURING NDT INSPECTION.
- [SDR ABXA010196](https://openairdocs.org/sdr/ABXA010196.md): Doubler · corroded · Mar 24, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > ALC STATION 1220-1228 LONGERON 30R-31R TORQUE BOX INTERNAL DOUBLER HAD DEEP EXFOLIATION CORROSION. MAINTENANCE REPAIRED THE AREA IAW ABX REA D853-40368.
- [SDR ABXA010356](https://openairdocs.org/sdr/ABXA010356.md): Doubler · corroded · Mar 20, 2001 · N822AX · Doug DC863 · Fuselage Main, Plate/Skin
  > AFT LOWER CARGO AT STATION 1040 - 1060.0 BETWEEN LONGERON 31 LEFT TO LONGERON 31 RIGHT CIRCUMFERENTIAL SPLICE TEAR STRAP AND FINGER DOUBLER HAD CORROSION BETWEEN SKIN TEAR STRAP AND FINGER DOUBLER. REPAIRED AREA AND REPLACED TEAR STRAP, LONGERON SPLICES, INTE
- [SDR ABXA010197](https://openairdocs.org/sdr/ABXA010197.md): Frame · corroded · Mar 20, 2001 · N822AX · Doug DC863 · Fuselage Main, Frame
  > AFT CARGO PIT FRAME AT FS 1120 ABOVE LONGERON 35R-36R WAS CORRODED UNDER AND AROUND NUT PLATES. MAINTENANCE REPAIRED THE AREA IAW DC-8 SRM 53-2-0.
- [SDR ABXA010192](https://openairdocs.org/sdr/ABXA010192.md): Fitting · corroded · Mar 20, 2001 · N822AX · Doug DC863 · Fuselage Miscellaneous Structure
  > Z-FITTING IN AFT CARGO PIT AT FS 1220 LONGERON 34L-35L IS CORRODED.
- [SDR ABXA010191](https://openairdocs.org/sdr/ABXA010191.md): Frame · corroded · Mar 20, 2001 · N822AX · Doug DC863 · Fuselage Main, Frame
  > AFT CARGO PIT FRAME AT FS 1480 ABOVE LONGERON 36 FRAME IS CORRODED.

Next page: https://openairdocs.org/deregistered/N822AX-2003-12-30/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 = 'N822AX' AND deregistration_id = 'N822AX-2003-12-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N822AX-2003-12-30/reports

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