# Service difficulty reports: N823AX, cancelled Mar 7, 2006

A list on [N823AX, cancelled Mar 7, 2006](https://openairdocs.org/deregistered/N823AX-2006-03-07.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR ABXA010818](https://openairdocs.org/sdr/ABXA010818.md): Downlock Switch · malfunctioned · Apr 10, 2002 · N823AX · Doug DC863 · Landing Gear Position and Warning
  > UPON LANDING, LANDING GEAR EXTENSION, THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. CHANGED BOTH BULBS, NO HELP. RECYCLED GEAR, NO HELP. RECYCLED GEAR A SECOND TIME AND GREEN LIGHT ILLUMINATED. INSPECTED NOSE LANDING GEAR, NO DEFECTS NOTED. REMOVE
- [SDR ABXA010203](https://openairdocs.org/sdr/ABXA010203.md): Light · inoperative · Apr 24, 2001 · N823AX · Doug DC863 · Emergency Lighting
  > THE EMERGENCY LIGHT AMBER LIGHT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT AMBER LIGHT BULBS IAW DC-8 MM 33-00-00.
- [SDR ABXA000494](https://openairdocs.org/sdr/ABXA000494.md): Bolt · broken · Nov 14, 2000 · N823AX · Doug DC863 · Landing Gear Retraction/Extension System
  > AFTER GEAR RETRACTION THE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE UP. GEAR WAS CYCLED WITH SAME INDICATIONS. AN UPLATCH CHECK WAS PERFORMED AND WITH THE GEAR HANDLE TO THE UPLATCH POSITION THE NOT LATCHED LIGHT ILLUMINATED. IN RIGHT
- [SDR ABXA000008](https://openairdocs.org/sdr/ABXA000008.md): Strut · failed · Jan 13, 2000 · N823AX · Doug DC863 · Nose/Tail Landing Gear Strut/Axle
  > LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. GEAR HANDLE WOULD NOT MOVE OUT OF DOWN POSITION. AIR TURN BACK TO ILN. REPACKED NOSE LANDING GEAR STRUT IAW DC8 MM 32-21-2 AND CHECKED LANDING CONTROL LEVER AND ANTI-RETRACTION LATCH IAW DC8 MM 32-31-1. OPS CHEC
- [SDR ABXA9900349](https://openairdocs.org/sdr/ABXA9900349.md): Selector · lack of lube · Apr 29, 1999 · N823AX · Doug DC863 · Landing Gear Selector
  > DURING CLIMB, UNSATISFACTORY GEAR UPLATCH CHECK WITH NOSE GEAR NOT LATCHED LIGHT ILLUMINATED. PERFORMED ALTERNATE UPLATCH CHECK PROCEDURE. FOUND LANDING GEAR LEVER STIFF AND HARD TO GO IN UPLATCH DETENT. CLEANED AND LUBED LEVER MECHANISM. OPS CHECKED GOOD.
- [SDR ABXA9801190](https://openairdocs.org/sdr/ABXA9801190.md): Insulation · out of position · Dec 24, 1998 · N823AX · Doug DC863 · Flight Compartment Equipment
  > UNABLE TO RAISE LANDING GEAR HANDLE AFTER TAKEOFF. NOSE GEAR HAD MOVED PAST CENTER, RESET GROUND CONTROL RELAY CIRCUIT BREAKER. MAIN GEAR SPOILER INOP LIGHT ILLUMINATED. RESET LOCKOUT CIRCUIT BREAKER AND LIGHT WENT OUT. GEAR THEN RETRACTED NORMALLY. INSPEC
- [SDR ABXA9801120](https://openairdocs.org/sdr/ABXA9801120.md): Plate · cracked · Nov 14, 1998 · N823AX · Doug DC863 · Wing, Plate/Skin
  > LEFT WING TRAILING EDGE SUPPORT STRUCTURE PLATE CRACKED, AFT OF NR 3 SPOILER ACTUATOR. REPAIRED IAW DC8 SRM 57-5-3 AND 57-2-0.
- [SDR ABXA9801121](https://openairdocs.org/sdr/ABXA9801121.md): Longeron · corroded · Nov 12, 1998 · N823AX · Doug DC863 · Fuselage Main, Longeron/Stringer
  > HEAVY CORROSION ON LONGERON 28R AT STATION 66O. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 3750342.
- [SDR ABXA9801124](https://openairdocs.org/sdr/ABXA9801124.md): Rib · cracked · Nov 11, 1998 · N823AX · Doug DC863 · Wing, Rib/Bulkhead
  > RIGHT WING OUTBOARD STUB WING LEADING EDGE RIB CRACKED, 7 INCHES FORWARD OF FRONT SPAR AT STATION XS 520.168. REPAIRED IAW DC8 SRM.
- [SDR ABXA9801123](https://openairdocs.org/sdr/ABXA9801123.md): Structure · corroded · Nov 11, 1998 · N823AX · Doug DC863 · Fuselage Main, Structure
  > COCKPIT SUBFLOOR STATION -60 TO -50, LBL 24-30, SHEARED RIVETS AND INTERNAL CORROSION. REPAIRED IAW ABX REA D853-24900 AND DC8 SRM 51-1-20D.
- [SDR ABXA9801126](https://openairdocs.org/sdr/ABXA9801126.md): Frame · corroded · Nov 10, 1998 · N823AX · Doug DC863 · Fuselage Main, Frame
  > BELTFRAME CORRODED AT STATION 1580 BETWEEN LONGERON 36R AND 35R. REPAIRED IAW DC8 SRM 51-1-21 AND 53-2-0.
- [SDR ABXA9801125](https://openairdocs.org/sdr/ABXA9801125.md): Rib · cracked · Nov 10, 1998 · N823AX · Doug DC863 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB AT STATION XFS 610 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW ABX DWG K05056, DC8 SRM 51-1-8 AND 51-1-20D.
- [SDR ABXA9801132](https://openairdocs.org/sdr/ABXA9801132.md): Bulkhead Bracket · cracked · Nov 9, 1998 · N823AX · Doug DC863 · Fuselage Main, Bulkhead
  > STATION 640 BULKHEAD TO FUSELAGE ATTACH BRACKET CRACKED BETWEEN LONGERON -26L AND -27L FORWARD ACCESSORY COMPARTMENT. REPAIRED IAW DC8 SRM 53-2-0.
- [SDR ABXA9801131](https://openairdocs.org/sdr/ABXA9801131.md): Fitting · corroded · Nov 9, 1998 · N823AX · Doug DC863 · Fuselage Miscellaneous Structure
  > BATH TUB FITTING AT STATION 1180 BETWEEN LONGERON 35R AND 36R CORRODED. REPAIRED IAW DC8 SRM 53-2-0.
- [SDR ABXA9801127](https://openairdocs.org/sdr/ABXA9801127.md): Fitting · cracked · Nov 9, 1998 · N823AX · Doug DC863 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL FITTING AT STATION 680 LONGERON 18L. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 3179874.
- [SDR ABXA9801122](https://openairdocs.org/sdr/ABXA9801122.md): Rib · cracked · Nov 9, 1998 · N823AX · Doug DC863 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE RIB CRACKED AT STATION XS520.168. REPAIRED IAW DC8 51-1-21, 51-1-20D AND DWG 5769523.
- [SDR ABXA9801134](https://openairdocs.org/sdr/ABXA9801134.md): Doubler · cracked · Nov 8, 1998 · N823AX · Doug DC863 · Nacelle/Pylon Structure
  > LEFT WING NR 1 PYLON STUB WING LOWER SURFACE REPAIR DOUBLER CRACKED BETWEEN 2 RIVETS. REPAIRED IAW DC8 SRM 51-1-26.
- [SDR ABXA9801152](https://openairdocs.org/sdr/ABXA9801152.md): Rib · cracked · Nov 4, 1998 · N823AX · Doug DC863 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION XFS 778.750. REPAIRED IAW ABX DWG K05056.
- [SDR ABXA9801151](https://openairdocs.org/sdr/ABXA9801151.md): Rib · cracked · Nov 4, 1998 · N823AX · Doug DC863 · Wing, Rib/Bulkhead
  > LEFT WING LEADING RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION XFS 766.250. REPAIRED IAW ABX DWG K05056.
- [SDR ABXA9801150](https://openairdocs.org/sdr/ABXA9801150.md): Rib · cracked · Nov 4, 1998 · N823AX · Doug DC863 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB STATION 628.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20D.
- [SDR ABXA9801149](https://openairdocs.org/sdr/ABXA9801149.md): Rib · cracked · Nov 4, 1998 · N823AX · Doug DC863 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB STATION XFS 622.5 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20D.
- [SDR ABXA9801129](https://openairdocs.org/sdr/ABXA9801129.md): Fitting · cracked · Nov 4, 1998 · N823AX · Doug DC863 · Fuselage Miscellaneous Structure
  > LONGERON 31L SPLICE CRACKED STATION 200 TO 220. REPLACED SPLICE IAW DC8 SRM 53-1-0 AND 51-1-20D.
- [SDR ABXA9801107](https://openairdocs.org/sdr/ABXA9801107.md): Angle · cracked · Nov 4, 1998 · N823AX · Doug DC863 · Fuselage Miscellaneous Structure
  > ELEVATOR UP CABLE FEED THROUGH BRACKET CRACKED AT RBL 24, STATION 1750. REPAIRED IAW ABX REA D853-24898MR.
- [SDR ABXA9801128](https://openairdocs.org/sdr/ABXA9801128.md): Rib · cracked · Nov 2, 1998 · N823AX · Doug DC863 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE RIB CRACKED STATION SFX 772.500. REPAIRED IAW ABX DWG K05056.
- [SDR ABXA9801153](https://openairdocs.org/sdr/ABXA9801153.md): Angle · cracked · Oct 31, 1998 · N823AX · Doug DC863 · Wing Miscellaneous Structure
  > RIGHT WING LEADING EDGE, INBOARD OF STATION XW454 RIB, VERTICAL ANGLE CRACKED AT LOWER END. REPAIRED IAW DC8 SRM 51-1-21, 51-3-0 AND DWG 9755297.
- [SDR ABXA9801106](https://openairdocs.org/sdr/ABXA9801106.md): Rib · cracked · Oct 31, 1998 · N823AX · Doug DC863 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION XFS591.250. REPAIRED IAW SRM 51-1-20D.
- [SDR ABXA9801105](https://openairdocs.org/sdr/ABXA9801105.md): Rib · cracked · Oct 31, 1998 · N823AX · Doug DC863 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION FS 785. REPAIRED IAW DWG K05056.
- [SDR ABXA9801133](https://openairdocs.org/sdr/ABXA9801133.md): Splice · cracked · Oct 23, 1998 · N823AX · Doug DC863 · Fuselage Miscellaneous Structure
  > LONGERON 31L SPLICE CRACKED BETWEEN STATION 400 AND 380. REPAIRED IAW DC8 SRM 51-1-20D.
- [SDR ABXA9701472](https://openairdocs.org/sdr/ABXA9701472.md): Temp Probe · stripped · Sep 14, 1997 · N823AX · Doug DC863 · Engine Oil Temperature
  > INFLIGHT SHUTDOWN OF NR 2 ENGINE DUE TO LOW OIL PRESSURE. FOUND OIL TEMP PROBE BACKED OUT OF OIL FILTER HOUSING. THREADS WERE STRIPPED.
- [SDR ABXA9701124](https://openairdocs.org/sdr/ABXA9701124.md): Angle · corroded · May 29, 1997 · N823AX · Doug DC863F · Service Doors
  > DURING C-CHECK, FOUND RIGHT FWD SERVICE DOOR FWD LOWER ANGLE AT CUSP CORRODED. FABRICATED AND INSTALLED NEW ANGLE IAW DC8 SRM 51-1-24 AND ABX REA D853-19482.
- [SDR ABXA9701123](https://openairdocs.org/sdr/ABXA9701123.md): Skin · corroded · May 29, 1997 · N823AX · Doug DC863F · Trailing Edge Flaps
  > RIGHT FLAP, TOP SIDE, INBOARD EDGE FOUND CORRODED DURING C-CHECK. REMOVED CORROSION, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW DC8 SRM 51-1-8 AND 57-2-1.
- [SDR ABXA9701122](https://openairdocs.org/sdr/ABXA9701122.md): Support · cracked · May 29, 1997 · N823AX · Doug DC863F · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CRACKED AT STA 759 AND 875.375, BETWEEN SEAT TRACKS C AND D. FABRICATED SUPPORT ANGLES AND INSTALLED IAW DC8 SRM 51-1-8 AND ABX REA 853-19470.
- [SDR ABXA9701121](https://openairdocs.org/sdr/ABXA9701121.md): Skin · corroded · May 29, 1997 · N823AX · Doug DC863F · Wing, Plate/Skin
  > DURING C-CHECK, FOUND CORROSION ON LEFT WING LEADING EDGE AT XFS 285 ON UPPER SURFACE. INSTALLED FILLER AND DOUBLER IAW DC8 SRM 51-1-8.
- [SDR ABXA9701120](https://openairdocs.org/sdr/ABXA9701120.md): Skin · corroded · May 29, 1997 · N823AX · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FUSELAGE SKIN WAS FOUND BULGED AT STA 400 LONGERON 34L. REMOVED CORRODED SKIN AND REPAIRED IAW DC8 SRM 53-4-1 AND ABX REA D853-19125MR.
- [SDR ABXA9701103](https://openairdocs.org/sdr/ABXA9701103.md): Longeron · corroded · May 29, 1997 · N823AX · Doug DC863F · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND CORROSION ON LONGERON 36L AT STA 450 TO 610. *S/D* REPAIRED IAW DC8 SRM 51-1-200 AND ABX REA D853-19137MR.
- [SDR ABXA9701102](https://openairdocs.org/sdr/ABXA9701102.md): Frame · corroded · May 29, 1997 · N823AX · Doug DC863F · Fuselage Main, Frame
  > CORROSION ON FRAME 12, LOWER LEG AT L30L. *S/D* REPAIRED IAW DC8 SRM 51-1-20A AND ABX REA D853-19476MR.
- [SDR ABXA9701101](https://openairdocs.org/sdr/ABXA9701101.md): Pressure Web · corrosion · May 29, 1997 · N823AX · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, CORROSION FOUND ON PRESSURE PANEL WEB RUNNING UNDER FLOORBEAM, COCKPIT FLOOR FS 12.00. *S/D* REPAIRED IAW ABX REA D853-19472MR.
- [SDR ABXA9701100](https://openairdocs.org/sdr/ABXA9701100.md): Longeron · cracked · May 29, 1997 · N823AX · Doug DC863F · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LONGERON 35L, STA 500 TO 540 CRACKED. *S/D* REPAIRED IAW DC8 SRM 51-1-8 AND ABX REA 853-19130MR.
- [SDR ABXA9701094](https://openairdocs.org/sdr/ABXA9701094.md): Skin · corroded · May 23, 1997 · N823AX · Doug DC863F · Wing, Plate/Skin
  > DURING C-CHECK, FOUND CORROSION IN STUB-WING AT SPAR CAP ATTACH EDGE ON RIGHT HAND LEADING EDGE. *S/D* FABRICATED REPAIR DOUBLER AND INSTALLED IAW DC8 SRM 51-1-8 AND ABX REA D823-19144MR.
- [SDR ABXA9701241](https://openairdocs.org/sdr/ABXA9701241.md): Tab · delaminated · May 6, 1997 · N823AX · Doug DC863 · Rudder, Tab Structure
  > RUDDER TAB WAS FOUND TO BE DELAMINATED. REPLACED SKIN, HONEYCOMB CORE AND INTERNAL DOUBLERS.
- [SDR ABXA9700549](https://openairdocs.org/sdr/ABXA9700549.md): Aileron · broken · Apr 8, 1997 · N823AX · Doug DC863 · Ailerons
  > AIRCRAFT REQUIRED 2 UNITS OF LEFT AILERON TRIM AND 1 UNIT OF LEFT RUDDER TRIM TO MAINTAIN STRAIGHT FLIGHT DURING CLIMB AND CRUISE. REPLACED RIGHT INBOARD AILERON IAW DC-8 MM 27-10-1.
- [SDR ABXA9700003](https://openairdocs.org/sdr/ABXA9700003.md): Skin · damaged · Dec 30, 1996 · N823AX · Doug DC863 · Fuselage Main, Plate/Skin
  > DURING SORT OPERATIONS, A CARGO LOADER WAS DRIVEN INTO THE AIRCRAFT PUTTING A HOLE IN THE FUSELAGE SKIN AT STATION 28 LEFT. REPAIRED IAW ABX REA D853-17575.
- [SDR ABXA9600663](https://openairdocs.org/sdr/ABXA9600663.md): Engine · defective · Nov 7, 1996 · N823AX · Doug DC863 · Engine (Turbine/Turboprop)
  > DURING SERVICE CHECK, FOUND NR 4 ENGINE C1 COMPRESSOR BLADE HAD RUBBED A.75 BY 2.25 INCH HOLE; HOUSING BETWEEN C1 AND C2 HAD A.25 BY 3 INCH GAP, BOTH AT THE 4 O'CLOCK POSITION. THREE ENGINE FERRIED AIRCRAFT BACK TO ILN. REPLACED NR 4 ENGINE IAW JOB CARD J7
- [SDR ABXA9600029](https://openairdocs.org/sdr/ABXA9600029.md): Bolt · loose · Jan 15, 1996 · N823AX · Doug DC863 · Power Lever
  > DURING CLIMB, NR 3 ENGINE COULD NOT BE CONTROLLED WITH THROTTLE INPUTS. ENGINE REMAINED AT MAX CONTINUOUS THRUST WITH THE THROTTLE LEVER PULLED BACK TO IDLE. ENGINE WAS SHUTDOWN AND MAINTAINED A POSITIVE OIL PRESSURE DURING SHUTDOWN PROCEDURES. SECURED AND
- [SDR ABXA9600030](https://openairdocs.org/sdr/ABXA9600030.md): C1 Disk · cracked · Jan 14, 1996 · N823AX · Doug DC863 · Turbine Engine Compressor Section
  > DURING COMPLIANCE OF AD 80-12-51, PRATT AND WHITNEY SB 5136, FOUND CRACK INDICATIONS IN C-1 DISK, FIRST STAGE FAN BLADES. REPLACED C-1 DISK, FIRST STAGE FAN BLADES IAW ABX TEST AND MAINTENANCE RECORD WORK SHEETS, BS374A, BS375A, BS376A AND BS377A.
- [SDR ABXA9500370](https://openairdocs.org/sdr/ABXA9500370.md): Heat Syst · odor · Apr 25, 1995 · N823AX · Doug DC863 · Heating System
  > EN ROUTE TO EWR, WITH SUPPLEMENTAL HEAT ON, A BURNING ODOR WAS REPORTED IN THE COCKPIT. THE ODOR DISSIPATED WHEN THE HEAT WAS TURNED OFF. COULD NOT DUPLICATE. THE SUPPLEMENTAL HEAT WAS OPERATED FOR SEVERAL MINUTES ON THE GROUND AND NO ODOR WAS NOTED. HEATE
- [SDR ABXA9500022](https://openairdocs.org/sdr/ABXA9500022.md): Proximity Box · defective · Jan 13, 1995 · N823AX · Doug DC863 · Landing Gear Position and Warning
  > LEFT MAIN GEAR DOOR LATCH LIGHT ILLUMINATED. RECYCLED LANDING GEAR 3 TIMES, LIGHT REMAINED ILLUMINATED. AIRCRAFT REDUCED AIRSPEED AND CONTINUED TO ILN. REMOVED AND REPLACED FAULTY PROXIMITY CONTROL BOX. REPLACED BENT PROXIMITY SWITCH PADDLE FOR LEFT GEAR D

## 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 = 'N823AX' AND deregistration_id = 'N823AX-2006-03-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N823AX-2006-03-07/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.