# Service difficulty reports: N801AX, cancelled Apr 2, 2004

A list on [N801AX, cancelled Apr 2, 2004](https://openairdocs.org/deregistered/N801AX-2004-04-02.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 · 52 reports

- [SDR ABXA000430](https://openairdocs.org/sdr/ABXA000430.md): Engine · seized · Sep 22, 2000 · N801AX · Doug DC862 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE SEIZED ON CLIMBOUT. NOTED EGT 800 DEGREES C, OIL QTY ZERO. REPLACED NR 1 ENGINE IAW JOB CARD 8090507.
- [SDR ABXA9900776](https://openairdocs.org/sdr/ABXA9900776.md): Engine · low power · Nov 9, 1999 · N801AX · Doug DC862 · Engine (Turbine/Turboprop)
  > DURING FUNCTIONAL CHECK FLIGHT (FCF), ON INITIAL LEVEL-OFF, WHEN POWER WAS REDUCED TO IDLE, NR 3 ENGINE N1 WAS LOWER THAN OTHER ENGINES. WHEN THROTTLES WERE ADVANCED, NR 3 ENGINE DID NOT ACCELERATE. LOW OIL PRESSURE LIGHT ILLUMINATED. INDICATED OIL PRESSUR
- [SDR ABXA9900796](https://openairdocs.org/sdr/ABXA9900796.md): Skin · cracked · Nov 8, 1999 · N801AX · Doug DC862 · Wing, Plate/Skin
  > DURING C-CHECK, CRACK INDICATIONS WERE FOUND IN SEVERAL RIGHT WING UPPER AFT SKIN PANEL 505F ATTACH HOLES. REPAIRED IAW ABX REA D857-33607MR.
- [SDR ABXA9900770](https://openairdocs.org/sdr/ABXA9900770.md): Skin · cracked · Nov 8, 1999 · N801AX · Doug DC862 · Wing, Plate/Skin
  > DURING C-CHECK, FOUND CRACK INDICATIONS IN LEFT WING UPPER AFT SKIN PANEL 505F. REPAIRED IAW ABX REA D857-33611MR.
- [SDR ABXA9900765](https://openairdocs.org/sdr/ABXA9900765.md): Longeron · cracked · Nov 3, 1999 · N801AX · Doug DC862 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LONGERON 34 AND 36 RIGHT, STATION 1185 CRACKED AT PRODUCTION SPLICE. REPAIRED IAW ABX REA D853-33152MR.
- [SDR ABXA9900792](https://openairdocs.org/sdr/ABXA9900792.md): Vane · delaminated · Oct 14, 1999 · N801AX · Doug DC862 · Trailing Edge Flaps
  > LEFT FLAP VANE ASSEMBLY WAS 50 PERCENT DELAMINATED. REPAIRED UNIT COMPLETE.
- [SDR ABXA9900129](https://openairdocs.org/sdr/ABXA9900129.md): Line · loose · Feb 22, 1999 · N801AX · Doug DC862 · Hydraulic System, Main
  > AFTER TAKEOFF AND PASSING 4000 FEET, THE HYDRAULIC RESERVOIR LOW PRESSURE LIGHT ILLUMINATED, ACCOMPANIED BY DECAYING FLUID QUANTITY. PERFORMED LOSS OF HYDRAULICS EMERGENCY CHECKLIST. TIGHTENED LOOSE LINE ON NR 2 HYDRAULIC PUMP. BLED SYSTEM, PERFORMED OPS AN
- [SDR ABXA9801084](https://openairdocs.org/sdr/ABXA9801084.md): Switch · worn · Nov 19, 1998 · N801AX · Doug DC862 · Landing Gear Position and Warning
  > ON GEAR EXTENSION, DID NOT GET LEFT MAIN GEAR (GREEN) LIGHT. RED GEAR UNSAFE LIGHT DID NOT ILLUMINATE. RECYCLED GEAR AND ACCOMPLISHED TOWER FLY-BY. LANDING WAS UNEVENTFUL. COULD NOT DUPLICATE DISCREPANCY. INSPECTED WIRING AND REPLACED MAIN GEAR DOWN SWITC
- [SDR ABXA9800942](https://openairdocs.org/sdr/ABXA9800942.md): Handle · lack of lube · Nov 3, 1998 · N801AX · Doug DC862 · Landing Gear Selector
  > ON APPROACH, WHEN GEAR EXTENDED HAD UNSAFE LIGHT AND NO GREEN DOWN INDICATION. RECYCLED GEAR, ALL INDICATIONS NORMAL. FOUND GEAR HANDLE STIFF. LUBRICATED HANDLE AND DOWNLOCK, OPS CHECKED GOOD.
- [SDR ABXA9800430](https://openairdocs.org/sdr/ABXA9800430.md): Fitting · cracked · Apr 16, 1998 · N801AX · Doug DC862 · Fuselage Miscellaneous Structure
  > STATION 1180 TO 1200 LONGERON 34R SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D AND ABX REA D853-22783.
- [SDR ABXA9800429](https://openairdocs.org/sdr/ABXA9800429.md): Fitting · cracked · Apr 16, 1998 · N801AX · Doug DC862 · Fuselage Miscellaneous Structure
  > SHEAR TIE FITTING AT STATION 570 BETWEEN LONGERONS 36R AND 35R IS CRACKED. REPLACED SHEAR TIE FITTING IAW DC8 SRM 53-2-0.
- [SDR ABXA9800428](https://openairdocs.org/sdr/ABXA9800428.md): Longeron · corroded · Apr 16, 1998 · N801AX · Doug DC862 · Fuselage Main, Longeron/Stringer
  > LONGERON 36 AT STATION 550 TO 560 HAS CORROSION. REPLACED LONGERON IAW DC8 SRM 53-2-2 AND 53-2-0.
- [SDR ABXA9800427](https://openairdocs.org/sdr/ABXA9800427.md): Rib · cracked · Apr 16, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB AT STATION XFS 297.5 IS CRACKED AT THE AFT, UPPER END. REPAIRED RIB IAW DC8 SRM 51-1-20D AND DRAWING K05056.
- [SDR ABXA9800426](https://openairdocs.org/sdr/ABXA9800426.md): Fitting · cracked · Apr 16, 1998 · N801AX · Doug DC862 · Fuselage Miscellaneous Structure
  > STATION 500 RIGHT HAND FLOORBEAM END FITTING IS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-21 AND DRAWING 9754022.
- [SDR ABXA9800425](https://openairdocs.org/sdr/ABXA9800425.md): Frame · corrosion · Apr 16, 1998 · N801AX · Doug DC862 · Fuselage Main, Frame
  > STATION 1360 FRAME FORWARD SIDE OF STRINGER 36 IS CORRODED. REPAIRED FRAME IAW DC8 SRM 53-2-0.
- [SDR ABXA9800424](https://openairdocs.org/sdr/ABXA9800424.md): Cusp · cracked · Apr 16, 1998 · N801AX · Doug DC862 · Fuselage Miscellaneous Structure
  > LEFT HAND CUSP BETWEEN STATION 320 TO 340 IS CRACKED. REPAIRED CUSP IAW DC8 SRM 53-2-0.
- [SDR ABXA9800423](https://openairdocs.org/sdr/ABXA9800423.md): Rib · cracked · Apr 16, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE RIB AT STATION XFS 628.750 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW DC8 SRM 51-1-21 AND 51-1-20D AND DRAWING K05056.
- [SDR ABXA9800409](https://openairdocs.org/sdr/ABXA9800409.md): Rib · cracked · Apr 16, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE RIB AT STATION XFS 635.00 CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW DC8 SRM 51-1-21, 51-1-20D AND DRAWING K05056.
- [SDR ABXA9800387](https://openairdocs.org/sdr/ABXA9800387.md): Splice · cracked · Apr 16, 1998 · N801AX · Doug DC862 · Fuselage Miscellaneous Structure
  > STRINGER 27R, SPLICE BETWEEN STATION 600 AND STATION 620 IS CRACKED. REPLACED STRINGER SPLICE IAW DC8 SRM 51-1-21.
- [SDR ABXA9800386](https://openairdocs.org/sdr/ABXA9800386.md): Splice · cracked · Apr 16, 1998 · N801AX · Doug DC862 · Fuselage Miscellaneous Structure
  > STRINGER 26R SPLICE BETWEEN STATION 600 AND STATION 620 IS CRACKED. REPLACED STRINGER SPLICE IAW DC8 SRM 51-1-21.
- [SDR ABXA9800385](https://openairdocs.org/sdr/ABXA9800385.md): Rib · cracked · Apr 16, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB AT STATION XFS 347.75 IS CRACKED AT THE AFT LOWER END. REPAIRED RIB IAW DC8 SRM 51-1-21 AND DRAWING K05056.
- [SDR ABXA9800389](https://openairdocs.org/sdr/ABXA9800389.md): Longeron · corroded · Apr 13, 1998 · N801AX · Doug DC862 · Fuselage Main, Longeron/Stringer
  > LONGERON 36 SEVERELY CORRODED AT F/S 1190. REPAIRED IAW ABX REA D853-22883 AND DC8 SRM 51-1-8.
- [SDR ABXA9800388](https://openairdocs.org/sdr/ABXA9800388.md): Fitting · cracked · Apr 13, 1998 · N801AX · Doug DC862 · Fuselage Miscellaneous Structure
  > STATION 1180-1200 STRINGER 36 SPLICE FITTING IS CRACKED. REPAIRED IAW ABX REA D853-22883 AND DC8 SRM 51-1-20D.
- [SDR ABXA9800434](https://openairdocs.org/sdr/ABXA9800434.md): Intercostal · cracked · Apr 12, 1998 · N801AX · Doug DC862 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED LOWER FWD END FASTENER HOLE FS 1480 LONGERON 35L. REPAIRED IAW DC8 SRM 53-4-1.
- [SDR ABXA9800433](https://openairdocs.org/sdr/ABXA9800433.md): Fitting · cracked · Apr 10, 1998 · N801AX · Doug DC862 · Fuselage Miscellaneous Structure
  > FRAME 880 UPPER FITTING HAS HEAVY CORROSION AND CRACKED RIGHT WHEEL WELL CEILING, BL 0. *S/D* REPAIRED IAW ABX REA D853-2280MR.
- [SDR ABXA9800436](https://openairdocs.org/sdr/ABXA9800436.md): Web · cracked · Apr 5, 1998 · N801AX · Doug DC862 · Fuselage Miscellaneous Structure
  > STATION 1164 AT STRINGER 32R, TORQUE BOX WEB IS CRACKED. REPAIRED IAW DC8 SRM 53-2-0.
- [SDR ABXA9800439](https://openairdocs.org/sdr/ABXA9800439.md): Skin · cracked · Mar 31, 1998 · N801AX · Doug DC862 · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE UPPER SKIN AT STATION XW 258 APPROXIMATELY 7 FWD OF THE SPAR IS CRACKED. REPAIRED IAW DC8 SRM 57-2-1.
- [SDR ABXA9800438](https://openairdocs.org/sdr/ABXA9800438.md): Rib · cracked · Mar 31, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB AT STATION XFS 603.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 51-1-8 AND DWG K05056.
- [SDR ABXA9800437](https://openairdocs.org/sdr/ABXA9800437.md): Rib · cracked · Mar 31, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB AT STATION XS 466.651 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 51-1-8 AND DWG K05056.
- [SDR ABXA9800440](https://openairdocs.org/sdr/ABXA9800440.md): Rib · cracked · Mar 29, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENERS AT STATION XFS 622.500. REPAIRED IAW DC8 SRM 51-1-21 AND ABX DWG K05056.
- [SDR ABXA9800421](https://openairdocs.org/sdr/ABXA9800421.md): Spoiler · corroded · Mar 29, 1998 · N801AX · Doug DC862 · Spoilers
  > LEFT SPOILER HAD WIDESPREAD CORROSION AND DELAMINATION. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.
- [SDR ABXA9800410](https://openairdocs.org/sdr/ABXA9800410.md): Rib · cracked · Mar 29, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB AT STATION XFS 741.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW ABX DWG K05056.
- [SDR ABXA9800402](https://openairdocs.org/sdr/ABXA9800402.md): Rib · cracked · Mar 29, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB AT STATION XFS 797.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW ABX DWG K05056.
- [SDR ABXA9800384](https://openairdocs.org/sdr/ABXA9800384.md): Rib · cracked · Mar 29, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB AT STATION XFS 810.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW ABX DWG K05056.
- [SDR ABXA9800383](https://openairdocs.org/sdr/ABXA9800383.md): Rib · cracked · Mar 29, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB AT STATION XFS 735.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW ABX DWG K05056.
- [SDR ABXA9800382](https://openairdocs.org/sdr/ABXA9800382.md): Rib · cracked · Mar 29, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION XFS 747.500. REPAIRED IAW ABX DWG K05056.
- [SDR ABXA9800381](https://openairdocs.org/sdr/ABXA9800381.md): Angle · cracked · Mar 29, 1998 · N801AX · Doug DC862 · Fuselage Miscellaneous Structure
  > STATION 1380 BULKHEAD RIGHT, FORWARD SIDE, LOWER INTERCOSTAL, OUTBOARD FORWARD IS CRACKED ON UNDERSIDE. REPAIRED IAW DACO DWG 5646608 AND DC8 SRM 53-2-0.
- [SDR ABXA9800380](https://openairdocs.org/sdr/ABXA9800380.md): Fitting · cracked · Mar 29, 1998 · N801AX · Doug DC862 · Fuselage Miscellaneous Structure
  > STATION 620-640 STRINGER 31R SPLICE FITTING IS CRACKED. REPAIRED IAW DC8 SRM 51-1-20D.
- [SDR ABXA9800379](https://openairdocs.org/sdr/ABXA9800379.md): Rib · cracked · Mar 28, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE RIB LOWER ARM CRACKED AT STATION XFS 785. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20D.
- [SDR ABXA9800378](https://openairdocs.org/sdr/ABXA9800378.md): Rib · cracked · Mar 28, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION XFS 578.750. REPAIRED IAW DWG K 05056 AND DC8 SRM 51-1-20D.
- [SDR ABXA9800377](https://openairdocs.org/sdr/ABXA9800377.md): Rib · cracked · Mar 28, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION XFS 785.000. REPAIRED RIB IAW DWG K05056 AND DC8 SRM 51-1-20D.
- [SDR ABXA9800435](https://openairdocs.org/sdr/ABXA9800435.md): Rib · cracked · Mar 26, 1998 · N801AX · Doug DC862 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB AT STATION XFS 778.75 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DC8 SRM 51-1-20D AND ABX DWG K05056.
- [SDR ABXA9701981](https://openairdocs.org/sdr/ABXA9701981.md): Air Distribution · odor · Dec 15, 1997 · N801AX · Doug DC862 · Air Distribution System
  > AT FL 350, 2.5 HRS INTO FLIGHT, CREW BEGAN SMELLING CHLORINE. CLIMBED CABIN AND CREW WENT ON OXYGEN. ON LANDING, MAINTENANCE PERSONNEL ENTERED COCKPIT, FOUND NO SMELL OR EVIDENCE OF CHLORINE SMELL IN COCKPIT, CABIN, OR CARGO COMPARTMENTS.
- [SDR ABXA9701455](https://openairdocs.org/sdr/ABXA9701455.md): Controller · overheated · Sep 6, 1997 · N801AX · Doug DC862 · Autopilot System
  > UNIDENTIFIED ODOR IN THE COCKPIT. APPEARS TO BE SOMETHING SMOLDERING UNDER THE CENTER CONSOLE. REPLACED AUTOPILOT CONTROLLER IAW MM 22-10-2.
- [SDR ABXA9600496](https://openairdocs.org/sdr/ABXA9600496.md): Engine · malfunctioned · May 22, 1996 · N801AX · Doug DC862 · Engine (Turbine/Turboprop)
  > NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED DURING CRUISE. THE OIL TEMPERATURE INDICATED 125 DEGREES CELSIUS AND BEGAN TO INCREASE WHILE THE OIL PRESSURE AND OIL QUANTITY INDICATIONS WERE NORMAL. SHUTDOWN THE NR 3 ENGINE AT 0203Z AND THE ENGINE WINDMILLED AT
- [SDR ABXA9600309](https://openairdocs.org/sdr/ABXA9600309.md): Bulkhead Fitting · leaking · Mar 13, 1996 · N801AX · Doug DC862 · Hydraulic System, Main
  > HYDRAULIC QUANTITY GAUGE INDICATION BEGAN DECREASING DURING DESCENT. EMERGENCY CHECKLIST WAS ACCOMPLISHED. HYDRAULIC FLUID QUANTITY STABILIZED AT THE STANDPIPE LEVEL. REPLACED NR 2 ENGINE HYDRAULIC PRESSURE LINE BULKHEAD FITTING. GROUND RAN ENGINE AND LEA
- [SDR ABXA9500913](https://openairdocs.org/sdr/ABXA9500913.md): Bulb · failed · Oct 26, 1995 · N801AX · Doug DC862 · Emergency Lighting
  > DURING PRE-FLIGHT INSPECTION, FOUND EMERGENCY LIGHTS DISARM LIGHT INOP. RELAMPED EMERGENCY LIGHTS DISARM LIGHT. OPS CHECK WAS GOOD.
- [SDR ABXA9500890](https://openairdocs.org/sdr/ABXA9500890.md): Eel Socket · stuck · Oct 23, 1995 · N801AX · Doug DC862 · Emergency Lighting
  > DURING PREFLIGHT INSPECTION, FOUND DISARM LIGHT INOPERATIVE FOR THE EMERGENCY EXIT LIGHTS. FOUND PRESS-TO-TEST SOCKET FOR THE EMERGENCY EXIT LIGHTING DISARM SWITCH STUCK. FREED SOCKET AND OPERATIONAL CHECK OF DISARM LIGHT WAS GOOD.
- [SDR ABXA9500886](https://openairdocs.org/sdr/ABXA9500886.md): Fire Loop · defective · Oct 20, 1995 · N801AX · Doug DC862 · Fire Detection
  > FIRE WARNING INDICATION OCCURRED ON NR 3 ENGINE DURING CLIMB AND BOTH FIRE EXTINGUISHERS WERE DISCHARGED. FIRE WARNING INDICATION PERSISTED FOR SEVERAL MINUTES AND ENGINE WAS SHUTDOWN. ENGINE WINDMILLED FOR APPROXIMATELY 25 TO 30 MINUTES WITH 10 TO 15 PSI OF
- [SDR ABXA9500748](https://openairdocs.org/sdr/ABXA9500748.md): Oil Temp Sensor · defective · Sep 28, 1995 · N801AX · Doug DC862 · Engine Oil Temperature
  > DURING CRUISE, NR 4 ENGINE OIL TEMP INDICATION INCREASED TO 140 DEGREES CELSIUS. ENGINE OIL PRESSURE AND ALL OTHER ENGINE PARAMETERS REMAINED NORMAL. ENGINE THRUST WAS INCREASED TO MAX CRUISE AND OIL TEMP REMAINED HIGH. ENGINE THRUST WAS REDUCED TO IDLE AND

Next page: https://openairdocs.org/deregistered/N801AX-2004-04-02/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 = 'N801AX' AND deregistration_id = 'N801AX-2004-04-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N801AX-2004-04-02/reports

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