# Service difficulty reports: N853AX, cancelled Apr 25, 2007

A list on [N853AX, cancelled Apr 25, 2007](https://openairdocs.org/deregistered/N853AX-2007-04-25.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 ABXA050068](https://openairdocs.org/sdr/ABXA050068.md): Panel · cracked · Mar 5, 2005 · N853AX · Doug DC861 · Nacelle/Pylon, Plate/Skin
  > DURING ROUTINE LINE MAINTENANCE AT ILN, FOUND A 2.250 INCH CRACK IN NR 2 PYLON OUTBOARD PLANK AT STA YN300. REPAIRED PYLON PLANK IAW ABX AIR REA D853-51551-MR USING 17-7 PH.080 INCH, PO 408448907.
- [SDR ABXA040117](https://openairdocs.org/sdr/ABXA040117.md): Downlock Switch · corroded · Mar 26, 2004 · N853AX · Doug DC861 · Landing Gear Position and Warning
  > AFTER GEAR EXTENSION, NOSE GEAR GREEN LIGHT DID NOT COME ON. NO RED UNSAFE LIGHT ON. REPLACED BULBS, NO HELP. CREW PERFORMED A GO-AROUND, CYCLED GEAR. VISUALLY CHECKED NOSE GEAR DOWN AND LOCKED, MADE NORMAL LANDING. GEAR PINNED AFTER LANDING AND AIRCRAFT
- [SDR ABXA040087](https://openairdocs.org/sdr/ABXA040087.md): Fitting · cracked · Feb 23, 2004 · N853AX · Doug DC861 · Fuselage Main, Attach Fittings
  > NR 3 PIT, AFT LOWER CARGO COMPARTMENT AFT DOOR JAMB FITTING WAS FOUND CRACKED DURING A LINE INSPECTION. REPLACED FITTING IAW DC-8 SRM 51-1-20D.
- [SDR ABXA030379](https://openairdocs.org/sdr/ABXA030379.md): Longeron · cracked · Oct 2, 2003 · N853AX · Doug DC861 · Fuselage Main, Longeron/Stringer
  > RT MAIN LANDING GEAR WHEEL WELL LONGERON 24 AT STA. 875 TO 900 TRIPLER SHOWED EVIDENCE OF CRACK. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 53-2-2, AND REA D853-48-35MR.
- [SDR ABXA030380](https://openairdocs.org/sdr/ABXA030380.md): Skin · cracked · Oct 2, 2003 · N853AX · Doug DC861 · Fuselage Main, Plate/Skin
  > AFT SERVICE DOOR JAMB UPPER AFT CORNER 3 INCHES X 8 INCHES AREA OF LIGHT SURFACE CORROSION AND A.1875 INCH CRACK AT FASTENER HOLE ON EXTERIOR FUSELAGE SKIN. REPAIRED AREA (REMOVED LIGHT SURFACE CORROSION, TRIMMED OUT CRACK, FABRICATED DOUBLERS -19, -21 AND FI
- [SDR ABXA030384](https://openairdocs.org/sdr/ABXA030384.md): Bushing · corroded · Oct 1, 2003 · N853AX · Doug DC861 · Wing, Landing Gear Attach Fittings
  > RIGHT MAIN LANDING GEAR ATTACH FITTING (TRUNION) HAD BROWN GREASE EMITTING FROM LUGS AT FORWARD AND AFT ATTACH POINTS. REMOVED RIGHT MAIN LANDING GEAR IAW DC-8 MM 32-11-01. REMOVED AND REPLACED TRUNION BUSHINGS IAW DC-8 OHM 13-1-6 AND DAC SB 57-45, DC-8 SRM 51
- [SDR ABXA030383](https://openairdocs.org/sdr/ABXA030383.md): Strut · corroded · Oct 1, 2003 · N853AX · Doug DC861 · Main Landing Gear Strut/Axle/Truck
  > RT MAIN LANDING GEAR CYLINDER FORWARD LUG AFT SIDE HAD EVIDENCE OF CORROSION. CORROSION ON RIGHT MAIN LANDING GEAR CYLINDER WAS OUT OF LIMITS. REPLACED RIGHT GEAR WITH A SERVICEABLE ASSEMBLY. TRANSFERRED BRAKE ASSEMBLY 4 EA. IAW DC-8 MM 32-42-01. TRANSFERRED W
- [SDR ABXA030382](https://openairdocs.org/sdr/ABXA030382.md): Bushing · corroded · Oct 1, 2003 · N853AX · Doug DC861 · Wing, Landing Gear Attach Fittings
  > LEFT MAIN LANDING GEAR ATTACH FITTING HAD BROWN GREASE EMITTING FROM LUGS AT BOTH ATTACH POINTS. REMOVED LEFT MAIN LANDING GEAR IAW DC-8 MM 32-11-01. REMOVED AND REPLACED TRUNION BUSHINGS IAW DC-8 OHM 13-1-6 AND DAC SB 57-45 AND DC-8 SRM 51-1-8. REINSTALLED LE
- [SDR ABXA030381](https://openairdocs.org/sdr/ABXA030381.md): Skin · cracked · Oct 1, 2003 · N853AX · Doug DC861 · Wing, Plate/Skin
  > 11 EACH HOLES HAD CRACK INDICATION ON RIGHT WING 505F PANEL. REMOVED -19 CLIP, FABRICATED NEW CLIP, ALODINED, PRIMED, INSTALLED IAW DC-8 SRM 51-1-8 AND DWG NR 5613609. FABRICATED EXTERNAL DOUBLER AND INNER DOUBLER IAW REA D857-48044MR, ALODINED, PRIMED AND INS
- [SDR ABXA030378](https://openairdocs.org/sdr/ABXA030378.md): Support Fitting · corroded · Oct 1, 2003 · N853AX · Doug DC861 · Wing, Center Box
  > CORROSION ON UPPER CHORD OF CENTER WING REAR SPAR AT PRESSURE BULKHEAD F.S. 855, LEFT BUTT LINE 11 - 21. REMOVED AND INSTALLED BLOWOUT PANEL 3 EA. VERTICAL STIFFENERS, WEB ATTACH ANGLE, DOUBLER, FITTING AND SHEAR WEB ATTACH ANGLE IAW DC-8 SRM 51-30-0 AND 51-1-
- [SDR ABXA030114](https://openairdocs.org/sdr/ABXA030114.md): Skin · corroded · Mar 11, 2003 · N853AX · Doug DC861 · Wing, Plate/Skin
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON THE LEFT WING, UPPER PLATING. REPAIRED AREA IAW REA D857-46919.
- [SDR ABXA030036](https://openairdocs.org/sdr/ABXA030036.md): Power Supply · discharged · Jan 15, 2003 · N853AX · Doug DC861 · Battery/Charger System
  > UPON MOVING AIRCRAFT, FOUND EMERGENCY POWER SUPPLY INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY. OPS CHECKED GOOD IAW DC-8 AMM 24-28-00-0.
- [SDR ABXA020149](https://openairdocs.org/sdr/ABXA020149.md): Bearing · broken · Aug 28, 2002 · N853AX · Doug DC861 · Aileron Control System
  > AILERONS WERE VERY DIFFICULT TO TURN TO THE LEFT WITH HYDRAULIC POWER ON. REPLACED THE RIGHT AILERON REVERSION MECHANISM BEARING ASSEMBLY FOR TAB LOCKOUT IAW DC-8 OVERHAUL MANUAL 27-6-2. PERFORMED TEST OF REVERSION MECHANISM IAW DC-8 MM 27-11-08. NO DISCREP
- [SDR ABXA020001](https://openairdocs.org/sdr/ABXA020001.md): Light · inoperative · Jun 24, 2002 · N853AX · Doug DC861 · Emergency Lighting
  > EMERGENCY EXIT LIGHT DISARM LIGHT, AMBER LIGHT WAS INOP. RELAMPED, OPS CHECKED NORMAL, REF DC-8 MM 33L.
- [SDR ABXA010670](https://openairdocs.org/sdr/ABXA010670.md): Fitting · corroded · Jan 15, 2002 · N853AX · Doug DC861 · Fuselage Miscellaneous Structure
  > RIGHT MAIN LANDING GEAR WHEEL WELL, LONGERON 24 RIGHT, FITTING HAD EXFOLIATION CORROSION AT STATION 879. REMOVED CORRODED FITTING. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-0. INSTALLED NEW FITTING AND REPAIR PARTS IAW DC-8 SRM 53-2-0.
- [SDR ABXA010668](https://openairdocs.org/sdr/ABXA010668.md): Fitting · corroded · Jan 12, 2002 · N853AX · Doug DC861 · Fuselage Miscellaneous Structure
  > FORWARD CARGO, STATION LONGERON 29 LEFT AND LONGERON 30 LEFT Z-ANGLE CORRODED. REMOVED CORRODED FITTING. RECEIVED NEW FITTING P/N 3755822-505N. FABRICATED REPAIR ANGLES IAW DC-8 SRM 53-2-0. INSTALLED Z-FITTING AND REPAIR ANGLES IAW DC-8 SRM 53-2-0.
- [SDR ABXA010667](https://openairdocs.org/sdr/ABXA010667.md): Fitting · corroded · Jan 12, 2002 · N853AX · Doug DC861 · Fuselage Miscellaneous Structure
  > FORWARD CARGO, STATION 320, BETWEEN LONGERON 28 LEFT - LONGERON 29 LEFT, Z-ANGLE CORRODED. REMOVED OLD FITTING. RECEIVED NEW FITTING P/N 3155822-505N. FABRICATED REPAIR ANGLES IAW DC-8 SRM 53-2-0.
- [SDR ABXA010666](https://openairdocs.org/sdr/ABXA010666.md): Spar · corroded · Jan 10, 2002 · N853AX · Doug DC861 · Wing Structure
  > LEFT WING, FORWARD SPAR CAP AT XFS 520.76 HOLE HAD A CRACK INDICATION WITH HFEC DETERMINE CRACK LENGH AND LOCATION IAW ES00046. REPAIRED CRACKED HOLE IAW DAC DWG 4709980 AND DC-8 SRM 51-1-25. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8.
- [SDR ABXA010665](https://openairdocs.org/sdr/ABXA010665.md): Skin · corroded · Jan 9, 2002 · N853AX · Doug DC861 · Wing, Plate/Skin
  > RIGHT WING, TOP SURFACE BY STATION XRS 172, CORROSION ON SKIN. REPAIRED IAW ABX REA D857-40949-MR AND DC8 SRM 57-2-0, 51-1-26, 51-1-8 AND 51-1-20D.
- [SDR ABXA010793](https://openairdocs.org/sdr/ABXA010793.md): Stringer · cracked · Jan 8, 2002 · N853AX · Doug DC861 · Fuselage Main, Longeron/Stringer
  > UPPER LEFT STRINGER 1 WAS CRACKED AT FS 1870, ABOVE BULKHEAD IN TAIL CONE FORWARD AREA. REPAIRED AREA IAW DC-8 SRM 51-1-21, 51-1-20, 51-1-8, 53-2-0 AND REA D853-40948MR.
- [SDR ABXA010669](https://openairdocs.org/sdr/ABXA010669.md): Splice · cracked · Dec 29, 2001 · N853AX · Doug DC861 · Fuselage Miscellaneous Structure
  > AFT CARGO, FS 1040 - 1060, LONGERON 31 RIGHT, SPLICE FITTING WAS CRACKED. RECEIVED NEW FITTING P/N 3750257-1. INSTALLED IAW DC-8 SRM 51-1-20D. REMOVED DAMAGED FITTING IAW DC-8 SRM 51-3-2.
- [SDR ABXA010529](https://openairdocs.org/sdr/ABXA010529.md): Hydraulic System · low · Oct 6, 2001 · N853AX · Doug DC861 · Hydraulic System, Main
  > THE GENERAL HYDRAULIC SYSTEM NEEDED SERVICED. THE SYSTEM INDICATED ZERO DURING APPROACH AND LANDING. MAINTENANCE SERVICED THE GENERAL HYDRAULIC SYSTEM IAW DC-8 MAINTENANCE MANUAL.
- [SDR ABXA010217](https://openairdocs.org/sdr/ABXA010217.md): Control Valve · failed · May 2, 2001 · N853AX · Doug DC861 · Landing Gear Retraction/Extension System
  > THE NOSE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF FROM ILN. THE CREW COMPLETED THE ABNORMAL CHECKLIST AND RE-CYCLED THE LANDING GEAR. THE AIRCRAFT WAS INSPECTED FOR AND COMPLETED A MAINTENANCE FERRY FLIGHT FROM EWR TO ILN. ILN MAINTENANCE INSPECTED AND
- [SDR ABXA9900678](https://openairdocs.org/sdr/ABXA9900678.md): Handle · defective · Aug 27, 1999 · N853AX · Doug DC861 · Fixed Inner Doors
  > UNABLE TO OPEN COCKPIT DOOR FROM INSIDE COCKPIT. REPAIRED COCKPIT DOOR HANDLE, OPS CHECKED GOOD.
- [SDR ABXA9900567](https://openairdocs.org/sdr/ABXA9900567.md): Lock · defective · Jul 8, 1999 · N853AX · Doug DC861 · Fixed Inner Doors
  > DURING PREFLIGHT INSPECTION, THE COCKPIT DOOR LOCK WAS INOPERATIVE. THE DOOR WOULD NOT UNLOCK WHEN CLOSED. INSTALLED NEW LATCH HANDLE AS REQUIRED, OPS CHECKED GOOD.
- [SDR ABXA9900381](https://openairdocs.org/sdr/ABXA9900381.md): Window · lack of lube · May 24, 1999 · N853AX · Doug DC861 · Flight Compartment Windows
  > UNABLE TO OPEN CAPTAIN'S CLEARVIEW WINDOW (EMERGENCY EXIT). LUBRICATED CAPTAIN'S CLEARVIEW WINDOW LINKAGE, OPS CHECKED GOOD.
- [SDR ABXA9900139](https://openairdocs.org/sdr/ABXA9900139.md): Engine · failed · Feb 25, 1999 · N853AX · Doug DC861 · Engine (Turbine/Turboprop)
  > DURING CLIMB, NR 1 ENGINE CREATED LOUD BANG. N1 AND N2 RPM DROPPED BY ONE HALF, EGT WENT TO 640 DEGREES. ENGINE ANTI-ICE WAS ON. SHUT ENGINE DOWN. FIRE BOTTLES WERE NOT USED. REPLACED NR 1 ENGINE.
- [SDR 98ZZZX4211](https://openairdocs.org/sdr/98ZZZX4211.md): Beam · cracked · Oct 21, 1998 · N853AX · Doug DC861 · Fuselage Miscellaneous Structure
  > AT C-CHECK, CRACKS WERE FOUND IN THE J-BEAM WHICH IS ATTACHED TO THE AFT FACE OF THE AFT PRESSURE BULKHEAD. THE CRACKS ORIGINATE IN THE RADII ADJACENT TO ATTACH BOLTS APPROXIMATELY ONE INCH EACH SIDE OF THE AIRCRAFT CENTERLINE. SUBMITTER STATED THE CRACKS AP
- [SDR 98ZZZX4210](https://openairdocs.org/sdr/98ZZZX4210.md): Beam · cracked · Oct 21, 1998 · N853AX · Doug DC861 · Fuselage Miscellaneous Structure
  > AT C-CHECK, CRACKS WERE FOUND IN THE J-BEAM WHICH IS ATTACHED TO THE AFT FACE OF THE AFT PRESSURE BULKHEAD. THE CRACKS ORIGINATE IN THE RADII ADJACENT TO ATTACH BOLT APPROXIMATELY ONE INCH EACH SIDE OF THE AIRCRAFT CENTERLINE. SUBMITTER STATED THE CRACKS APP
- [SDR ABXA9800637](https://openairdocs.org/sdr/ABXA9800637.md): Turbo Comp · defective · Jul 22, 1998 · N853AX · Doug DC861 · Cabin Compressor System
  > NR 2 CTC BEGAN TO HOWL ON DESCENT, ACCOMPANIED BY SMELL LIKE BURNING RUBBER. *S/D* REPLACED NR 2 CTC IAW DC8 MM 21-10-01.
- [SDR ABXA9800606](https://openairdocs.org/sdr/ABXA9800606.md): Bulkhead Tee Cap · cracked · Jul 1, 1998 · N853AX · Doug DC861 · Fuselage Main, Bulkhead
  > AFT PRESS BULKHEAD TEE CAP CRACKED AT LONGERON 10R. REPAIRED IAW DC8 SRM 53-2-5, 51-1-20D AND 51-3-0.
- [SDR ABXA9800605](https://openairdocs.org/sdr/ABXA9800605.md): Fitting · cracked · Jul 1, 1998 · N853AX · Doug DC861 · Fuselage Miscellaneous Structure
  > MAIN CABIN LONGERON END FITTING AT STATION 860, LONGERON 10R CRACKED. REPAIRED IAW DC8 SRM'S 51-1-24 AND 51-1-20D.
- [SDR ABXA9800604](https://openairdocs.org/sdr/ABXA9800604.md): Bulkhead Web · cracked · Jul 1, 1998 · N853AX · Doug DC861 · Fuselage Main, Bulkhead
  > RADOME BULKHEAD, RIGHT WEB HAS TWO 15 INCH CRACKS, 6 ABOVE AND BELOW FRP. REPAIRED IAW ABX REA D853-23417 MR.
- [SDR ABXA9800600](https://openairdocs.org/sdr/ABXA9800600.md): Fitting · cracked · Jun 30, 1998 · N853AX · Doug DC861 · Wing Miscellaneous Structure
  > CRACK IN LOWER NR 2 MAIN TANK JUST INBOARD OF XRS 74 STRINGER NR 51 ON FWD AND AFT SIDE OF SPLICE. REPAIRED TWO CRACKED FITTINGS IAW DC8 SRM'S 51-1-24, 51-1-8, AND 51-1-20D.
- [SDR ABXA9800599](https://openairdocs.org/sdr/ABXA9800599.md): Fitting · cracked · Jun 30, 1998 · N853AX · Doug DC861 · Fuselage, Wing Attach Fittings
  > STRINGER END FITTING CRACKED AFT SIDE OF STRINGER NR 51 OUTBOARD IN NR 2 MAIN TANK AT STATION 74.000. REPAIRED IAW DC8 SRM 51-1-24 AND 51-1-20D.
- [SDR ABXA9800598](https://openairdocs.org/sdr/ABXA9800598.md): Fitting · cracked · Jun 30, 1998 · N853AX · Doug DC861 · Fuselage Miscellaneous Structure
  > MAIN CABIN, LONGERON END FITTING AT STATION 900 LONGERON 8R CRACKED. REPAIRED IAW DC8 SRM 51-3-2 AND 51-1-20D.
- [SDR ABXA9800597](https://openairdocs.org/sdr/ABXA9800597.md): Longeron · corroded · Jun 30, 1998 · N853AX · Doug DC861 · Fuselage Main, Longeron/Stringer
  > AFT LOWER CARGO COMPARTMENT STATION 1230, LONGERON 29L INSIDE TORQUE BOX, WEB CORRODED. REPAIRED IAW ABX REA D853-23409MR REV-A,
- [SDR ABXA9800553](https://openairdocs.org/sdr/ABXA9800553.md): Beam · cracked · Jun 22, 1998 · N853AX · Doug DC861 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD AFT SIDE, HORIZONTAL BEAM HAS 3.5 CRACK ON LOWER FLANGE AND 1 CRACK ON UPPER FLANGE AT AIRCRAFT CENTERLINE, 24 ABOVE FRP. REPAIRED PER ABX REA D853-23406MR.
- [SDR ABXA9800552](https://openairdocs.org/sdr/ABXA9800552.md): Flange · cracked · Jun 22, 1998 · N853AX · Doug DC861F · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD AFT SIDE HORIZONTAL BEAM HAS 3 CRACK ON LOWER FLANGE AT AIRCRAFT CENTERLINE. REPAIRED IAW ABX REA D853-23407MR.
- [SDR ABXA9800551](https://openairdocs.org/sdr/ABXA9800551.md): Trunnion · corroded · Jun 22, 1998 · N853AX · Doug DC861 · Main Landing Gear Attach Section
  > RIGHT HAND MAIN LANDING GEAR TRUNNION CORRODED. FABRICATED BUSHINGS PER AD 71-25-09 AND ABX REA D832-23410MR.
- [SDR ABXA9800550](https://openairdocs.org/sdr/ABXA9800550.md): Longeron · cracked · Jun 22, 1998 · N853AX · Doug DC861 · Fuselage Main, Longeron/Stringer
  > LONGERON 2R CRACKED AT STATION 1790 CANTED BULKHEAD. REPAIRED IAW ABX REA D853-23411MR.
- [SDR ABXA9800571](https://openairdocs.org/sdr/ABXA9800571.md): Frame · corroded · Jun 6, 1998 · N853AX · Doug DC861 · Fuselage Main, Frame
  > FORWARD LOWER CARGO CIRCUMFERENTIAL FRAME CORRODED AT STATION 80, LONGERON 29R. REPAIRED IAW DC8 SRM 55-2-2 AND 51-1-9A.
- [SDR ABXA9800443](https://openairdocs.org/sdr/ABXA9800443.md): Switch · defective · May 3, 1998 · N853AX · Doug DC861 · Engine Oil Pressure
  > NR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED ON CLIMBOUT. OIL QUANTITY, TEMPERATURE AND PRESSURE WERE NORMAL. PERFORMED ABNORMAL PROCEDURE. LIGHT REMAINED ON. PRECAUTIONARY ENGINE SHUTDOWN. REPLACED NR 1 ENGINE LOW OIL PRESSURE SWITCH. OPS CHECKED NORM
- [SDR ABXA9800136](https://openairdocs.org/sdr/ABXA9800136.md): Retract Mech · out of adjust · Mar 2, 1998 · N853AX · Doug DC861 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF AND GEAR RETRACTION, VIBRATION COULD BE FELT AND HEARD FROM NOSE GEAR AREA. ALL INDICATIONS WERE GOOD. RECYCLED GEAR THREE TIMES, ON THIRD TIME, VIBRATION CEASED. REPLACED DOOR BUMPERS, AND PERFORMED ADJUST/TEST IAW DC8 MM 32-20-00, NO DEFECTS
- [SDR ABXA9701338](https://openairdocs.org/sdr/ABXA9701338.md): Control Cable · defective · Jul 31, 1997 · N853AX · Doug DC861 · Landing Gear Door Retract Section
  > ON CLIMBOUT WITH GEAR HANDLE UP GEAR UNSAFE AND LEFT DOOR NOT LATCHED LIGHTS ILLUMINATED. RECYCLED GEAR TWICE, LIGHTS REMAINED ON. IN CRUISE LEFT DOOR AND LEFT AND RIGHT GEAR NOT LATCHED LIGHTS CAME ON. REPLACED CABLE RUN 112C, RIGHT MLG DOOR LATCH AND ROLL
- [SDR ABXA9700898](https://openairdocs.org/sdr/ABXA9700898.md): Spring · out of adjust · Apr 18, 1997 · N853AX · Doug DC861 · Flight Compartment Windows
  > FIRST OFFICER'S WINDOW WOULD NOT OPEN. REPOSITIONED WINDOW LATCH SPRING. FIRST OFFICER'S WINDOW OPS CHECKED GOOD IAW DC-8 M.M. 56-40.
- [SDR ABXA9700289](https://openairdocs.org/sdr/ABXA9700289.md): Window · out of adjust · Mar 26, 1997 · N853AX · Doug DC861 · Flight Compartment Windows
  > DURING PREFLIGHT, WAS UNABLE TO OPEN FIRST OFFICER'S CLEARVIEW WINDOW. CLEANED AND LUBRICATED WINDOW AND SEAL. ADJUSTED LOWER AFT HOOK FITTING PER DC-8 MM 56-10-3. OPS CHECKED GOOD.
- [SDR ABXA9700021](https://openairdocs.org/sdr/ABXA9700021.md): Fitting · loose · Jan 29, 1997 · N853AX · Doug DC861 · Hydraulic System, Main
  > WHEN GEAR HANDLE WAS PLACED UP AFTER TAKEOFF, THE AILERON CONTROL MANUAL LIGHT ILLUMINATED ACCOMPANIED BY PRESSURE LOSS. QUANTITY REMAINED AT FULL. PERFORMED GEAR SWING WITH EXTERNAL HYDRAULIC SOURCE AND AILERON POWER ON. FOUND HYDRAULIC LEAK AT NR 3 PYLON
- [SDR ABXA9700013](https://openairdocs.org/sdr/ABXA9700013.md): Lock Bar · out of adjust · Jan 20, 1997 · N853AX · Doug DC861 · Flight Compartment Windows
  > FIRST OFFICER'S SLIDING WINDOW/EMERGENCY EXIT WOULD NOT OPEN. ADJUSTED UPPER LOCK BAR IAW DC-8 MM, OPS CHECKED GOOD.
- [SDR ABXA9600678](https://openairdocs.org/sdr/ABXA9600678.md): Gear Indication · malfunctioned · Dec 5, 1996 · N853AX · Doug DC861 · Landing Gear Position and Warning
  > ON FINAL WHEN GEAR HANDLE PUT IN DOWN POSITION, NO NOSE GEAR GREEN LIGHT, HAD GEAR UNSAFE LIGHT. RECYCLED GEAR, GOT NORMAL INDICATION. PERFORMED ADJUSTMENT TEST OF NOSE LANDING GEAR SYSTEM IAW DC-8 MM 32-31-0. OPERATIONAL CHECK OF INDICATION AND MECHANICAL

Next page: https://openairdocs.org/deregistered/N853AX-2007-04-25/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 = 'N853AX' AND deregistration_id = 'N853AX-2007-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N853AX-2007-04-25/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.