# Service difficulty reports: N811AX, cancelled Mar 20, 2007

A list on [N811AX, cancelled Mar 20, 2007](https://openairdocs.org/deregistered/N811AX-2007-03-20.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 · 85 reports

- [SDR ABXA060157](https://openairdocs.org/sdr/ABXA060157.md): Rotary Switch · faulty · Apr 5, 2006 · N811AX · Doug DC863F · Landing Gear Position and Warning
  > AFTER TAKEOFF AND GEAR RETRACTED (FROM ILN TO MEM) THE RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED ALONG WITH THE AMBER RIGHT DOOR LIGHT ON F/E'S PANEL. RECYCLED GEAR WITH NO EFFECT. PERFORMED AN UPLATCH CHECK AND ALL LIGHTS EXTINGUISHED WITH A NORMAL UPLATCH
- [SDR ABXA060132](https://openairdocs.org/sdr/ABXA060132.md): Warning Light · illuminated · Mar 16, 2006 · N811AX · Doug DC863F · Landing Gear Position and Warning
  > AFTER TAKEOFF WHEN GEAR WAS RETRACTED, RED UNSAFE LIGHT STAYED ON, LEFT MAIN GEAR DOOR LIGHT WAS ON. CYCLED GEAR, OPS CHECKED NORMAL. REMOVED AND REPLACED LEFT MAIN LANDING GEAR DOOR UPLATCH AND INDICATION IAW DC8 MM 32-60-00 AND ALSO CHECKED MIN ROLLER CLEA
- [SDR ABXA060059](https://openairdocs.org/sdr/ABXA060059.md): Skin · corroded · Jan 20, 2006 · N811AX · Doug DC863F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN LOWER SIDE OF NR 3 CARGO DOOR HAD A SPOT OF CORROSION. REPAIRED NR3 CARGO DOOR JAMB SKIN IAW SRM 53-2-1, FIG. 9. PARTIAL WORK NR1-102 FOR WORK ACCOMPLISHED (W.O. 600239852) COI 50853 INITIATED FOR REPAIR REPLACEMENT IN 1000 CYCLES.
- [SDR ABXA050004](https://openairdocs.org/sdr/ABXA050004.md): Transmitter · defective · Jan 11, 2005 · N811AX · Doug DC863F · Engine Oil Pressure
  > NR 4 ENGINE OIL PRESSURE BEGAN FLUXUATING IN CRUISE AND THEN WENT TO '0' PSI. NO LOW OIL PRESSURE LIGHT CAME ON. ALL OTHER ENG PARAMETERS NORMAL. SECURED NR 4 ENGINE AT 0340Z. REMOVED AND REPLACED ENGINE OIL STRAINER. NO CONTAMINATES NOTED. REPLACED MAIN
- [SDR ABXA040363](https://openairdocs.org/sdr/ABXA040363.md): Skin · corroded · Oct 31, 2004 · N811AX · Doug DC863F · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN BULGED AND FASTENERS HEAD SHEARED LEFT SIDE OF TAILSKID FAIRING. CUT OUT DAMAGED AREA AND INSTALLED FABRICATED DOUBLER REPAIR, TREATED, ALODINED AND PRIMED IAW DC-8 SRM 51-1-21, 53-2-1, 51-1-8, 51-1-20, AND REA D853-50297-MR.
- [SDR ABXA040362](https://openairdocs.org/sdr/ABXA040362.md): Skin · corroded · Oct 31, 2004 · N811AX · Doug DC863F · Fuselage Main, Plate/Skin
  > EXTERIOR LOWER FUSELAGE SKIN CRACKED AND BULGED AT LONGERON 35 RIGHT, FS 102. REMOVED END FITTING, SHEAR TIES AND DOUBLER IAW DC-8 SRM 51-1-21. REINSTALLED END FITTING, SHEAR TIES AND DOUBLER IAW DC-8 SRM 51-1-21 AND 51-1-20D. REPAIRED SKIN IAW REA D853-502
- [SDR ABXA040366](https://openairdocs.org/sdr/ABXA040366.md): Skin · corroded · Oct 30, 2004 · N811AX · Doug DC863F · Fuselage Main, Plate/Skin
  > FORWARD CARGO RIGHT SIDE FROM STA 200 - 220, BETWEEN LONGERON 33 RIGHT - 34 RIGHT, SKIN CORRODED WITH BROKEN RIVETS. REMOVED SHEAR TIES, INSTALLED FINGER DOUBLERS, EXTERNAL DOUBLERS, FILLER AND INTERNAL DOUBLERS AND SHEAR TIES IAW REA D853-50304-MR AND DC-8 S
- [SDR ABXA040367](https://openairdocs.org/sdr/ABXA040367.md): Cusp Web · corroded · Oct 30, 2004 · N811AX · Doug DC863F · Fuselage Miscellaneous Structure
  > MAIN CABIN AT FS 1164 - 1170 AND LONGERON 21 RIGHT (CUSP) HAD CORROSION. REPAIRED AREA IAW DC-8 SRM 51-1-8 AND REA D853-50301-MR.
- [SDR ABXA040365](https://openairdocs.org/sdr/ABXA040365.md): Doubler · corroded · Oct 30, 2004 · N811AX · Doug DC863F · Fuselage Main, Plate/Skin
  > AREAS OF CORROSION NOTED ON LOWER SKIN AROUND OUTFLOW VALVE (AFT ACCESSORY COMPARTMENT) FROM FLOOR FRAME 1620 - 1640, LONGERON 34 RIGHT TO 34 LEFT. REMOVED ALL SUBSTRUCTURE AND FASTENERS COMMON TO REPAIR AREA TO FACILITATE REPAIR. REMOVED ALL CORROSION IAW D
- [SDR ABXA040364](https://openairdocs.org/sdr/ABXA040364.md): Support · corroded · Oct 30, 2004 · N811AX · Doug DC863F · Fuselage Miscellaneous Structure
  > RIGHT FUSELAGE STA 915 - 935, SUPPORT BRACE OUTBOARD OF LONGERON 24 RIGHT, EXFOLIATED. REPAIRED AREA IAW REA D853-50298-MR.
- [SDR ABXA040334](https://openairdocs.org/sdr/ABXA040334.md): Wire Harness · burned · Sep 27, 2004 · N811AX · Doug DC863F · Engine Indicating System Wiring
  > DURING LINE MAINTENANCE INVESTIGATION OF NR 3 ENGINE EPR PROBLEM, FOUND THE EPR WIRING HARNESS, THRUST BRAKE WIRING AND THRUST REVERSER EMERGENCY DUMP VALVE WIRING CHARRED AND FRAYED DUE TO A PREVIOUS PNEUMATIC DUCT LEAK. REPLACED WIRE NR 3H406E24, 3H2156B24,
- [SDR ABXA040333](https://openairdocs.org/sdr/ABXA040333.md): Wire · frayed · Sep 27, 2004 · N811AX · Doug DC863F · Engine Indicating System Wiring
  > DURING LINE MAINTENANCE, FOUND NR 3 ENGINE EPR WIRING HARNESS CHARRED AND FRAYED DUE TO PREVIOUS PNEUMATIC LEAK. REPLACED NR 3 ENGINE EPR WIRES 7E57SA24N AND 3E573A24N BETWEEN CONNECTOR P1-1449 AND GROUND 825.
- [SDR ABXA040207](https://openairdocs.org/sdr/ABXA040207.md): Escape Rope · mismanufactured · Jun 13, 2004 · N811AX · Doug DC863F · Emergency Equipment
  > CHECK EMERGENCY ROPE AT MAIN CABIN DOOR FOR PROPER LENGTH. ROBBED EMERGENCY ROPE FROM 826AX, CHECKED FOR PROPER LENGTH AND INSTALLED ON 811AX IAW DC-8 MM 25-60-02-0002. CANNIBALIZATION FORM WAS FILLED OUT.
- [SDR ABXA040200](https://openairdocs.org/sdr/ABXA040200.md): Jackscrew · binding · Jun 2, 2004 · N811AX · Doug DC863F · Stabilizer Control System
  > DURING APPROACH TO GUA, STABILIZER JAMMED, WOULD NOT MOVE BOTH ELECTRIC OR HYDRAULIC. INDICATOR AT 5.2 DEGREES. FOUND GEARBOX SPROCKET SHEAR PINS SHEARED AND RIGHT JACKSCREW BINDING. INSTALLED NEW SHEAR PINS IAW DC8 OVHL MM 27-10-1. REPLACED LEFT AND RIGHT
- [SDR ABXA040116](https://openairdocs.org/sdr/ABXA040116.md): Engine · defective · Mar 24, 2004 · N811AX · Doug DC863F · Engine (Turbine/Turboprop)
  > UPON INITIAL CLIMBOUT, NR 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. NR 2 ENGINE OIL PRESSURE WAS NOTED TO BE 28 PSI AND OIL QUANTITY DECREASING. SHUT DOWN ENGINE AT 0424Z. N1 AND N2 RPM'S NOTED: 22/35. ENGINE OIL PRESSURE IN CRUISE: 3 PSI. REPLACED
- [SDR ABXA040107](https://openairdocs.org/sdr/ABXA040107.md): Actuator · bypassing · Mar 12, 2004 · N811AX · Doug DC863F · Autopilot System
  > ON CLIMBOUT, THE AIRCRAFT EXPERIENCED A VIOLENT LATERAL FLUTTER. THE AUTOPILOT WAS OFF, YAW DAMPER ENGAGED. THE YAW DAMPER WAS DISENGAGED BY PILOT WITH NO NOTEABLE DIFFERENCE. DEPOWERED THE RUDDER HYDRAULICS AND THE FLUTTER STOPPED. FURTHER TROUBLESHOOTING
- [SDR ABXA040065](https://openairdocs.org/sdr/ABXA040065.md): Uplock · damaged · Feb 14, 2004 · N811AX · Doug DC863F · Landing Gear Retraction/Extension System
  > GEAR UPLATCH CHECK FAILED. RIGHT MAIN LANDING GEAR DOOR NOT LATCHED LIGHT ILLUMINATED WITH LANDING GEAR RED UNSAFE LIGHT. IAS DID NOT EXCEED 230 KTS. DEFERRED MAIN LANDING GEAR DOOR UPLATCH SYSTEM IAW DC-8 MEL 32-14, CAT A, CODE 1. PLACARD INSTALLED. MUST
- [SDR ABXA040039](https://openairdocs.org/sdr/ABXA040039.md): Link · loose · Jan 23, 2004 · N811AX · Doug DC863F · Landing Gear Retraction/Extension System
  > UPLATCH CHECK FAILED ON INITIAL CHECK. GEAR WAS CYCLED THROUGH ONCE THEN UPLATCH CHECK WAS ACCOMPLISHED. UPLATCH CHECK WAS SATISFACTORY. FOUND LEFT MAIN LANDING GEAR LOWER SIDE BRACE LOWER LINK AND LOWER SIDE BRACE UPPER LINK WITH EXCESSIVE PLAY. REPLACE U
- [SDR ABXA030475](https://openairdocs.org/sdr/ABXA030475.md): Arm · worn · Dec 13, 2003 · N811AX · Doug DC863F · Landing Gear Door Retract Section
  > RED GEAR UNSAFE LIGHT CAME ON AFTER GEAR RETRACTION WITH RT GEAR DOOR LIGHT ON FLIGHT ENGINEER'S PANEL. RECYCLED GEAR, ALL INDICATIONS NORMAL. MAINTENANCE FOUND DOOR ROLLER OUT OF ADJUSTMENT AND AFT ARM WORN. REPLACED ARM, ADJUSTED MAIN GEAR DOOR UPLATCH ME
- [SDR ABXA030474](https://openairdocs.org/sdr/ABXA030474.md): Proximity Sensor · dirty · Dec 12, 2003 · N811AX · Doug DC863F · Landing Gear Position and Warning
  > LANDING GEAR UNSAFE LIGHT ILLUMINATED IN CRUISE. NOT LATCHED LIGHT ON FLIGHT ENGINEER'S PANEL ILLUMINATED WITH SELECTION RT GEAR POSITION. PERFORMED ABNORMAL. LIGHTS EXTINGUISHED WHEN LANDING GEAR WAS CYCLED. MAINTENANCE FOUND RT MAIN LANDING GEAR DOOR NOT
- [SDR ABXA030308](https://openairdocs.org/sdr/ABXA030308.md): Spring · worn · Jul 22, 2003 · N811AX · Doug DC863 · Landing Gear Retraction/Extension System
  > THE GEAR UNSAFE LIGHT ILLUMINATED INTERMITTENTLY ACCOMPANIED WITH LEFT DOOR NOT LATCHED LIGHT AT FLIGHT ENGINEER'S PANEL. PERFORMED ABNORMAL CHECK, UNSAFE LIGHT WOULD NOT REMAIN ILLUMINATED LONG ENOUGHT TO DETERMINE WHICH SWITCH MAY BE MALFUNCTIONING. REPLAC
- [SDR ABXA030170](https://openairdocs.org/sdr/ABXA030170.md): Seal · torn · May 24, 2003 · N811AX · Doug DC863F · Landing Gear Position and Warning
  > GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR RETRACTED. CYCLED GEAR AND LIGHT WENT OUT. RIGHT MAIN LANDING GEAR DOOR IDENTIFIED ON FLIGHT ENGINEER'S LANDING GEAR AND DOOR LATCHING PANEL. CLEANED UP LATCH SWITCH. OPS CHECKED GOOD IAW DC-8 AMM 32-60-00-2
- [SDR ABXA030137](https://openairdocs.org/sdr/ABXA030137.md): Battery · discharged · Apr 16, 2003 · N811AX · Doug DC863F · Emergency Lighting
  > MAINTENANCE FOUND EMERGENCY LIGHT VERY WEAK IN TEST. REPLACED EMERGENCY LIGHTS BATTERY RACK ASSEMBLY. OPS CHECKED GOOD IAW DC-8 MM.
- [SDR ABXA030109](https://openairdocs.org/sdr/ABXA030109.md): Proximity Switch · dirty · Mar 5, 2003 · N811AX · Doug DC863F · Landing Gear Position and Warning
  > ON CLIMBOUT, GEAR UNSAFE LIGHT STAYED ILLUMINATED AFTER GEAR RETRACTION. RIGHT GEAR DOOR INDICATED. RECYCLED GEAR TWICE. LIGHT WENT OUT. INSPECTED RIGHT GEAR DOOR AND INDICATING SYSTEM COMPONENTS. NO DEFECTS NOTED. DOOR FAIRED ON GROUND WITH HYDRAULIC PRESSURE
- [SDR ABXA030067](https://openairdocs.org/sdr/ABXA030067.md): Transmitter · failed · Feb 11, 2003 · N811AX · Doug DC863F · Engine Oil Pressure
  > DURING CLIMBOUT, WHEN NR 1 ENGINE ANTI-ICE WAS TURNED OFF, NR 1 ENGINE COMPRESSOR STALLED ACCOMPANIED BY NR 1 OIL PRESSURE WENT TO 100 PSI AND OIL QUANTITY FLUCTUATED +/-2 GALLONS. SECURED ENGINE. ENGINE WINDMILLED ABOVE 25 PERCENT FOR 45 MINUTES. FOUND NR 1
- [SDR ABXA030062](https://openairdocs.org/sdr/ABXA030062.md): Eyebolt · worn · Feb 7, 2003 · N811AX · Doug DC863F · Landing Gear Retraction/Extension System
  > LT MLG WAS MAKING LOUD NOISE DURING RETRACT. ON SERVICE CHECK, FOUND LT MLG RETRACT CYLINGER EYE BOLT HAD EXCESSIVE PLAY. REWORKED PIN IAW 32-13-0001-001 NEA ON SHOP TRAVELER 5816-01.
- [SDR ABXA030187](https://openairdocs.org/sdr/ABXA030187.md): Skin · corroded · Feb 4, 2003 · N811AX · Doug DC863F · Fuselage Main, Plate/Skin
  > CLEAN, TREAT AND PRIME SKIN UNDER C4 SCUFF PLATE. CLEANED CORROSION, TREATED, PRIMED SKIN. FABRICATED AND INSTALLED FILLERS, DOUBLERS AND TRIPLERS IAW DC-8 REA D853-46013-MR, AND THE SRM.
- [SDR ABXA030186](https://openairdocs.org/sdr/ABXA030186.md): Longeron · cracked · Jan 5, 2003 · N811AX · Doug DC863F · Fuselage Main, Longeron/Stringer
  > LONGERON 24 RIGHT CRACKED JUST UNDER BOTTLE BOLT IN BATH TUB AREA. ACCOMPLISHED LONGERON 24 RIGHT REPLACEMENT IAW ABX REA D853-46001-MR AND JOB CARD 90453100 (TIMCO).
- [SDR ABXA030185](https://openairdocs.org/sdr/ABXA030185.md): Skin · cracked · Jan 5, 2003 · N811AX · Doug DC863F · Fuselage Main, Plate/Skin
  > AFT PAX DOOR UPPER AFT CORNER HAD 4 CRACKS FOUND WITH NDT L-2. REMOVED DAMAGE IAW DC-8 SRM 53-2-0, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW DC-8 SRM 53-2-0, 51-1-20D, AND 51-1-21.
- [SDR ABXA020305](https://openairdocs.org/sdr/ABXA020305.md): Actuator · broken · Nov 12, 2002 · N811AX · Doug DC863F · Trailing Edge Flap Actuator
  > HYD QTY LOSS ON LANDING. MAINTENACE FOUND THE RT INBOARD FLAP ACTUATOR CRANK ASSEMBLY BROKEN ALONG WITH A BROKEN HYD LINE TO THE ACTUATOR AND ASSOCIATED ATTACHING HARDWARE BROKEN. OPEN: CORRECTIVE ACTION IS NOT COMPLETE.
- [SDR ABXA020306](https://openairdocs.org/sdr/ABXA020306.md): Warning System · malfunctioned · Nov 10, 2002 · N811AX · Doug DC863F · Landing Gear Position and Warning
  > DURING CLIMB, AFTER GEAR UPLATCH CHECK, AIRCRAFT HAD LIGHT TURBULANCE. THE RED GEAR UNSAFE LIGHT CAME ON CAUSED BY THE RT MAIN GEAR DOOR UPLATCH LIGHT ILLUMINATED. RECYCLED GEAR TWICE BEFORE LIGHT WENT OUT. PERFORMED ADJUSTMENT ON UPLATCH. OPS CHECKED UPLATCH
- [SDR ABXA020278](https://openairdocs.org/sdr/ABXA020278.md): Pump · defective · Oct 30, 2002 · N811AX · Doug DC863F · Hydraulic Pump (Electric/Engine), Main
  > MANUAL REVERSION LIGHTS CAME ON DURING FINAL APPROACH. RAN LOSS OF HYDRAULIC PROCEDURES. REPLACED BOTH LT AND RT ENGINE DRIVEN HYDRAULIC PUMPS IAW DC-8 MM 29-10-12-02 AND 29-10-12. SERVICED SYSTEM IAW DC-8 AMM 12-00. LEAK AND OPS CHECKED GOOD.
- [SDR ABXA020074](https://openairdocs.org/sdr/ABXA020074.md): Warning System · malfunctioned · Aug 11, 2002 · N811AX · Doug DC863F · Landing Gear Position and Warning
  > GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR, LIGHT WENT OUT. LOUD GRINDING NOISE HEARD ON 2ND ROTATION.
- [SDR ABXA010915](https://openairdocs.org/sdr/ABXA010915.md): Connector · loose · Jun 20, 2002 · N811AX · Doug DC863F · Hydraulic Pressure Sensor
  > AIR RETURN TO MIA DUE TO LOSS OF HYDRAULIC FLUID. AIRCRAFT DUMPED FUEL IN PREPARATION FOR RETURN TO MIA. FOUND CONNECTOR ON HYDRAULIC QUANTITY TRANSMITTER LOOSE. CLEANED AND RESECURED. SYSTEM OPS CHECKED GOOD. CHECKED FUEL DUMP SYSTEM AFTER USE, FOUND ALL
- [SDR ABXA010897](https://openairdocs.org/sdr/ABXA010897.md): Flap · out of rig · May 23, 2002 · N811AX · Doug DC863F · Trailing Edge Flap Control System
  > ON TAKEOFF WITH FLAPS SELECTED TO 18 DEG, THE INDICATOR INDICATED 15 DEG, THEN INCREASED TO 20 DEGREES. ON APPROACH, FLAP INDICATION WAS AS FOLLOWS, 12 SELECTED, 10 INDICATED - 23 SELECTED, 23 INDICATED - 35 SELECTED, 40 INDICATED. AIRCRAFT WAS FERRIED FROM
- [SDR ABXA010707](https://openairdocs.org/sdr/ABXA010707.md): Fuel Control · failed · Feb 8, 2002 · N811AX · Doug DC863F · Fuel Control/Turbine Engines
  > DURING DESCENT, THE NR 4 ENGINE FAILED TO ACCELERATE. EPR, EGT, RPM AND F/F DECAYED. OIL PRESSURE WAS NORMAL (WINDMILLING). PERFORMED CHECKLIST - NO HELP. DURING LEVEL OFF WITH INCREASED AIRSPEED - NEGATIVE RELIGHT. PERFORMED ENGINE SHUTDOWN ACTIONS CHECK
- [SDR ABXA010655](https://openairdocs.org/sdr/ABXA010655.md): Actuator · broken · Dec 24, 2001 · N811AX · Doug DC863F · Drag Control Actuator
  > ON SERVICE CHECK, FOUND BOTH CRANK ASSEMBLIES TO THE RIGHT WING INBOARD SPOILER RODS BROKEN. REPLACED BOTH INBOARD SPOILER REAR SPAR ACTUATOR CRANK ASSEMBLIES IAW DC-8 MM 27-61-01-2-0001.
- [SDR ABXA010397](https://openairdocs.org/sdr/ABXA010397.md): Seat Track · dirty · Jul 8, 2001 · N811AX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings
  > AFTER MOVING THE CAPTAIN'S SEAT FORWARD OR AFT, THE HANDLE DID NOT LOCK DOWN ALLOWING THE SEAT TO MOVE. CLEANED AND LUBRICATED THE SEAT TRACK. CHECKED GOOD IAW DC-8 MM 25-11-01.
- [SDR ABXA010398](https://openairdocs.org/sdr/ABXA010398.md): Brake · malfunctioned · Jul 2, 2001 · N811AX · Doug DC863F · Brake
  > ON LANDING, 5 MAIN LANDING GEAR TIRES BLEW. MECHANICS FOUND THAT THE EMERGENCY AIR BRAKE BOTTLE WENT OFF. REPLACED AFT AIR BRAKE MECHANICAL CONTROL CABLE. REF CABLE RUN 81B, 82B, IAW DC-8 MM 32-45-00. SERVICED AIR BRAKE BOTTLE. OPS CHECK OF AIR BRAKE SYST
- [SDR ABXA010339](https://openairdocs.org/sdr/ABXA010339.md): Lock · lack of lube · Jun 8, 2001 · N811AX · Doug DC863F · Flight Compartment Equipment
  > CAPTAIN'S SEAT WOULD NOT REMAIN IN SELECTED POSITION. INTERMITTENTLY CAUSED SEAT TO SLIDE BACK ON TRACK. LUBRICATED CAPTAIN'S SEAT TRACKS AND LOCKING MECHANISM. SEAT NOW STAYS IN SELECTED POSITION.
- [SDR ABXA010303](https://openairdocs.org/sdr/ABXA010303.md): Door · faulty · Jun 8, 2001 · N811AX · Doug DC863F · Fixed Inner Doors
  > COCKPIT DOOR WAS DIFFICULT TO KEEP CLOSED. UNSAFE AS IS REF, UNABLE TO KEEP CLOSED DURING EMERGENCY PROCEDURE. COCKPIT SMOKE REMOVAL, STEP 6. NOTE: DOOR CAME OPEN SEVERAL TIMES DURING FLIGHT. OPEN AND CLOSED COCKPIT DOOR SEVERAL TIMES BY USING THE COCKPIT D
- [SDR ABXA010286](https://openairdocs.org/sdr/ABXA010286.md): Longeron · corroded · Jun 4, 2001 · N811AX · Doug DC863F · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO COMPARTMENT LONGERON 28 LEFT CORRODED AT FS 280 INSIDE TORQUE BOX. REPAIRED AREA IAW DC-8 SRM 51-3-0, 51-1-21, 51-1-20D, AND REA D853-40780MR.
- [SDR ABXA010292](https://openairdocs.org/sdr/ABXA010292.md): Longeron · corroded · Jun 1, 2001 · N811AX · Doug DC863F · Fuselage Main, Longeron/Stringer
  > LEFT MAIN LANDING GEAR WHEEL WELL LONGERON 24 HAD CORROSION ON UPPER SURFACE BETWEEN STATION 879 - 902. CORROSION ALSO RUNS UNDER FITTING AT STATION 902. REPLACED LEFT LONGERON 24 IAW DAC DWG 5750198.
- [SDR ABXA010285](https://openairdocs.org/sdr/ABXA010285.md): Longeron · corroded · May 30, 2001 · N811AX · Doug DC863F · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO COMPARTMENT CORROSION ON LONGERON 34 RIGHT AT FS 280 INSIDE TORQUE BOX. REPAIRED AREA IAW DC-8 SRM 51-3-0, 51-1-20D, 53-2-2, AND REA D853-40226MR.
- [SDR ABXA010284](https://openairdocs.org/sdr/ABXA010284.md): Stiffener · cracked · May 29, 2001 · N811AX · Doug DC863F · Fuselage Miscellaneous Structure
  > LEFT MAIN LANDING GEAR STATION 940 STIFFENER CRACKED ADJACENT TO CABLE PULLEY ON OUTBOARD WEB. REPAIRED AREA IAW DC-8 DAC DWG 5643402, DC-8 SRM 53-2-0, 51-1-8, 51-1-11, 51-1-21A, AND 51-1-20D.
- [SDR ABXA010234](https://openairdocs.org/sdr/ABXA010234.md): Fitting · cracked · May 23, 2001 · N811AX · Doug DC863F · Fuselage Miscellaneous Structure
  > FITTING AT STA 980 IN LEFT MAIN LANDING GEAR WHEEL WELL ABOVE LONGERON 24 IS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM.
- [SDR ABXA010223](https://openairdocs.org/sdr/ABXA010223.md): Fitting · cracked · May 12, 2001 · N811AX · Doug DC863F · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON LONGERON 24 BACK UP FITTING AT STA 879, LEFT MAIN LANDING GEAR WHEEL WELL. FOUND TO BE CRACKED AFTER CORROSION REMOVAL.
- [SDR ABXA010291](https://openairdocs.org/sdr/ABXA010291.md): Skin · corroded · Apr 30, 2001 · N811AX · Doug DC863F · Fuselage Main, Plate/Skin
  > FS 660 - 680 LONGERON 36 - 35 RIGHT AIRCRAFT SKIN WAS CORRODED UNDER ACCELEROMETER BRACKET INSIDE AND OUTSIDE AIRCRAFT. REPAIRED AREA IAW DC-8 SRM 51-1-21, 51-1-8, 53-2-0, 51-1-20D, AND 53-2-1.
- [SDR ABXA010290](https://openairdocs.org/sdr/ABXA010290.md): Fitting · corroded · Apr 26, 2001 · N811AX · Doug DC863F · Fuselage, Landing Gear Attach Fittings
  > RIGHT MAIN LANDING GEAR WHEEL WELL HAD CORROSION ON INBOARD UPPER CHAMBER ON TRAP FITTING. BLENDED AND REMOVED CORROSION FOUND WITHIN LIMITS IAW DC-8 SRM 53-2-0, FIGURE 1, SHEET 3. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8.
- [SDR ABXA010204](https://openairdocs.org/sdr/ABXA010204.md): Brake · defective · Apr 25, 2001 · N811AX · Doug DC863F · Landing Gear Brake System
  > THE BRAKES WERE SPONGY AND INEFFECTIVE ON LANDING.

Next page: https://openairdocs.org/deregistered/N811AX-2007-03-20/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 = 'N811AX' AND deregistration_id = 'N811AX-2007-03-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N811AX-2007-03-20/reports

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