# Service difficulty reports: N847AX, cancelled Apr 26, 2010

A list on [N847AX, cancelled Apr 26, 2010](https://openairdocs.org/deregistered/N847AX-2010-04-26.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 · 61 reports

- [SDR ABXA070086](https://openairdocs.org/sdr/ABXA070086.md): Access Panel · missing · Mar 27, 2007 · N847AX · Doug DC861 · Service Doors
  > ON POST FLIGHT FOUND FIRE BOTTLE ACCESS PNL ON PRESS GAGES MISSING. (CENTER INBOARD DOOR ASSEMBLY). INSTALLED TEMPORARY COVER PER REA D857-55548, DEFERRED PER REA D857-55548 FOR MAINT TRACKING IAW ABX GMM 01.07.04 TO BE REPLACED ON OR BEFORE MARCH 30, 2007.
- [SDR ABXA060076](https://openairdocs.org/sdr/ABXA060076.md): Longeron · cracked · Dec 9, 2005 · N847AX · Doug DC861 · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO, LONGERON 35 LEFT, CRACKED, FS 250 - 270. INSTALLED LONGERON REPAIR AT FORWARD CARGO FS 250 - 270, LONGERON 35 LEFT IAW RFTS 40033 AND PROJECT E-40463. SPLICE REPAIR INSTALLED IAW DC8 SRM 53-2-2 AT LONGERON 35 LEFT.
- [SDR ABXA060073](https://openairdocs.org/sdr/ABXA060073.md): Skin · corroded · Dec 6, 2005 · N847AX · Doug DC861 · Fuselage Main, Plate/Skin
  > FORWARD CARGO FUSELAGE SKIN BULGED, CRACKED, FASTENER SHEARED, EVIDENCE OF EXFOLIATION CORROSION AT PREVIOUS REPAIR, FS 620 - 640, LONGERON 35 LEFT - 36 LEFT. REMOVED CORROSION FORWARD CARGO COMPARTMENT FUSELAGE SKIN IAW DC8 SRM 51-1-8 AT LONGERON 36. INSTAL
- [SDR ABXA060075](https://openairdocs.org/sdr/ABXA060075.md): Longeron · cracked · Dec 6, 2005 · N847AX · Doug DC861 · Fuselage Main, Longeron/Stringer
  > LEFT MAIN LANDING GEAR WHEEL WELL LONGERON 24, FS 879 HAD A CRACK AT LOWER FASTENER FORWARD SIDE. REMOVED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D AND 53-2-0.
- [SDR ABXA060074](https://openairdocs.org/sdr/ABXA060074.md): Longeron · cracked · Dec 1, 2005 · N847AX · Doug DC861 · Fuselage Main, Longeron/Stringer
  > RIGHT FS 879.375, LONGERON 24, HAD CRACK AT LOWER AREA. STOP DRILLED AND INSTALLED ANGLE REPAIR IAW DC8 SRM 53-2-2.
- [SDR ABXA050090](https://openairdocs.org/sdr/ABXA050090.md): Indicator · defective · Apr 11, 2005 · N847AX · Doug DC861 · Engine Oil Pressure
  > ON TAKEOFF AND CLIMB, NR 3 ENGINE OIL PRESSURE CLIMBED TO 75 - 80 PSI. TOOK THROTTLE TO IDLE, PRESSURE WENT TO 60 PSI. SECURED NR 3 ENGINE. AIR TURN BACK. AFTER SECURING THE ENGINE, THE PRESSURE READ 14 PSI STATIC ON TAXI. REPLACED NR 3 ENGINE OIL PRESSUR
- [SDR ABXA040348](https://openairdocs.org/sdr/ABXA040348.md): Bracket · bent · Oct 5, 2004 · N847AX · Doug DC861 · Aileron Control System
  > DECLARED EMERGENCY, DURING RT TURNS IN FLT AILERONS HARD TO MOVE IN POWERED MODE. WHEN AILERONS DEPOWERED, OPS NORM. FOUND RT FAIRLEAD BRACKET BENT & INTERFERRING WITH CABLE DUE TO BROKEN BUS AILERON CABLE RUNS. REPLACED BRACKET STA RW XRS 380. REPLACED DA
- [SDR ABXA040328](https://openairdocs.org/sdr/ABXA040328.md): Compressor · damaged · Sep 17, 2004 · N847AX · Doug DC861 · Cabin Compressor System
  > AFTER TURNING ON THE NR 4 CTC, THE AIRCRAFT FILLED WITH A BURNING OIL SMELL. TURNED NR 4 CTC OFF AND SMELL DISSIPATED. NOTE: DID NOT GET AN OVERHEAT LIGHT, RPM'S NORMAL. FOUND NR 4 CTC FAN BLADE DAMAGED. REMOVED AND REPLACED NR 4 CTC. OPS CHECKED GOOD IAW
- [SDR ABXA040210](https://openairdocs.org/sdr/ABXA040210.md): Engine · vibration · Jun 17, 2004 · N847AX · Doug DC861 · Engine (Turbine/Turboprop)
  > AT 2000 FEET AND LEVELING OFF, POWER ADVANCED TO MAINTAIN AIRSPEED, HAD SEVERE NR 3 ENGINE VIBRATION. AIRCRAFT WAS INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FROM IAD TO ILN. UPON ARRIVAL AT ILN, THE NR 3 ENGINE WAS REPLACED.
- [SDR ABXA040109](https://openairdocs.org/sdr/ABXA040109.md): Smoke Detector · defective · Mar 18, 2004 · N847AX · Doug DC861 · Smoke Detection
  > UPPER CARGO FIRE SMOKE SOUNDED IN FLIGHT. ISOLATED TO NR 3 DETECTOR. TESTED NORMAL AFTER LANDING. REPLACED NR 3 SMOKE DETECTOR IAW DC-8 MM 26-10-05-2-0001. OPS CHECKED GOOD.
- [SDR ABXA040063](https://openairdocs.org/sdr/ABXA040063.md): Plate · misrepaired · Feb 14, 2004 · N847AX · Doug DC861 · Fuselage Miscellaneous Structure
  > FOUND MAIN ENTRY DOOR SCUFF PLATE DID NOT MEET REQUIREMENTS OF SERVICE REWORK DRAWING SRO8530021. TEMPORARY REPAIRED MAIN ENTRY DOOR SCUFF PLATE IAW REA D853-49056MR. PLACED ON CARRY OVER NR COI 46070. PROPER FASTENERS TO BE INSTALLED ON OR BEFORE 9-6-2005.
- [SDR ABXA030417](https://openairdocs.org/sdr/ABXA030417.md): Skin · damaged · Nov 5, 2003 · N847AX · Doug DC861 · Fuselage Main, Plate/Skin
  > L1 DOOR FORWARD UPPER CORNER HAD A B-CLASS REPAIR IAW ABX JC NEA 53100102-002. REMOVED EXISTING REPAIR, PERFORMED X-RAY INSPECTION TO CUTOUT. NO CRACKS NOTED. FABRICATED DOUBLERS AND FILLER IAW DC-8 SRM 53-2-0. INSTALLED REPAIR AND REPAIRED AREA IAW DC-8 S
- [SDR ABXA030421](https://openairdocs.org/sdr/ABXA030421.md): Skin · damaged · Nov 4, 2003 · N847AX · Doug DC861 · Fuselage Main, Plate/Skin
  > L2 LOWER AFT DOOR CORNER HAD A REPAIR THAT DID NOT CONFORM TO SERVICE REWORK DWG SR08530021 OR ENG SKETCH ES00863. REMOVED EXISTING REPAIR AND STRUCTURAL COMPONENTS TO FOM. FABRICATED REPAIR DOUBLERS, ALODINED, PRIMED AND REINSTALLED COMPONENTS IAW DC-8 SRM
- [SDR ABXA030420](https://openairdocs.org/sdr/ABXA030420.md): Skin · cracked · Nov 3, 2003 · N847AX · Doug DC861 · Fuselage Main, Plate/Skin
  > L2 AFT PASSENGER LOWER FORWARD DOOR JAMB CORNER HAD CRACKS ON EXTERNAL SKIN AND INTERNAL DOUBLERS, LENGTH RANGE FROM 2 - 4 INCHES APPROXIMATELY. REMOVED DAMAGE FROM AREA, PERFORMED HFEC ON EXTERNAL SKIN AND TITANIUM DOUBLER, NO CRACKS PAST CUTOUT. FABRICATED
- [SDR ABXA030422](https://openairdocs.org/sdr/ABXA030422.md): Skin · damaged · Oct 29, 2003 · N847AX · Doug DC861 · Fuselage Main, Plate/Skin
  > R1 DOOR UPPER FORWARD CORNER HAD A REPAIR THAT DID NOT CONFORM TO SERVICE REWORK DRAWING SR08530021 OR ENG SKETCH ES00863. REMOVED EXISTING DOUBLER AND TRIPLER, PERFORMED X-RAY AND ELC INSPECTION, NO CRACKS. FABRICATED DOUBLER AND TRIPLER REPAIR, ALODINED, P
- [SDR ABXA030419](https://openairdocs.org/sdr/ABXA030419.md): Skin · cracked · Oct 29, 2003 · N847AX · Doug DC861 · Fuselage Main, Plate/Skin
  > R1 FORWARD SERVICE DOOR LOWER AFT CORNER HAD CRACK INDICATION ON EXTERNAL SKIN. CUT OUT DAMAGED AREA, PERFORMED HFEC AFTER DAMAGE REMOVAL. NO CRACKS NOTED. FABRICATED DOUBLERS AND FILLER, ALODINED, PRIMED, AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-20D
- [SDR ABXA030425](https://openairdocs.org/sdr/ABXA030425.md): Frame · cracked · Oct 26, 2003 · N847AX · Doug DC861 · Fuselage Main, Frame
  > FORWARD CARGO BILGE AREA HAD CRACK ON FRAME FS 240, LONG 34 RIGHT - LONG 35 RIGHT. CUT OUT DAMAGE AND FABRICATED REPAIR ANGLE AND FILLER IAW DC-8 SRM STD5310-02. ALODINED AND PRIMED ANGLE AND FILLER IAW DC-8 SRM 51-1-8. INSTALLED DOUBLER AND FILLER IAW DC-8
- [SDR ABXA030424](https://openairdocs.org/sdr/ABXA030424.md): Structure · corroded · Oct 25, 2003 · N847AX · Doug DC861 · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL STABILIZER REAR SPAR RIGHT CHORD HAD CORROSION AT ZR 270. REMOVED CORROSION AT REAR SPAR RIGHT CHORD, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 55-2-0 AND REA D855-48068MR.
- [SDR ABXA030423](https://openairdocs.org/sdr/ABXA030423.md): Structure · corroded · Oct 25, 2003 · N847AX · Doug DC861 · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL STABILIZER REAR SPAR LEFT CHORD HAD CORROSION ON AFT LEG BETWEEN ZR 262 AND ZR 268. REMOVED CORROSION ON REAR SPAR LEFT CHORD, FOUND OUT OF LIMITS. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 55-2-0 AND REA D855-48
- [SDR ABXA030330](https://openairdocs.org/sdr/ABXA030330.md): Element · missing · Aug 18, 2003 · N847AX · Doug DC861 · Fire Detection
  > ENROUTE, NR 3 ENGINE FIRE WARNING CAME ON. ONLY OTHER INDICATION WAS HIGH OIL TEMP. CREW ELECTED TO USE RT WING OB ENGINE FIRE BOTTLE. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE NR 3 ENGINE. NO EVIDENCE OF FIRE OR FIRE DAMAGE FOUND. DURING INSPECTION,
- [SDR ABXA030100](https://openairdocs.org/sdr/ABXA030100.md): Skin · damaged · Mar 6, 2003 · N847AX · Doug DC861 · Passenger/Crew Doors
  > CREW ENTRY DOOR WOULD NOT CLOSE AND LOCK, OR OPEN PROPERLY. REPAIRED AFT UPPER CORNER OF MAIN ENTRY DOOR SKIN IAW DC-8 SRM 52-2-0 AND REA D852-46903. OPS CHECKED GOOD.
- [SDR ABXA030060](https://openairdocs.org/sdr/ABXA030060.md): Link · sheared · Jan 30, 2003 · N847AX · Doug DC861 · Landing Gear Steering System
  > ON ROLLOUT, NO BRAKING BELOW 15 KNOTS. STICK SHAKER WENT OFF, BLOW AWAY JET INOPERATIVE. SUSPECT GROUND SHIFT FAILURE. FOUND NOSE LANDING GEAR STEERING SHUTOFF VALVE LINK SHEARED. REPLACED LINK ASSEMBLY IAW DC-8 MM 32-21-01. OPS CHECKED GOOD.
- [SDR ABXA020081](https://openairdocs.org/sdr/ABXA020081.md): Indicator · defective · Aug 19, 2002 · N847AX · Doug DC861 · Engine Oil Temperature
  > NR 1 ENGINE OIL TEMP WENT TO 150 DEG CELSIUS FOR APPROXIMATELY 20 MINUTES. SECURED THE NR 1 ENGINE. ALL OTHER INDICATIONS WERE NORMAL. REPLACED THE NR 1 ENGINE OIL TEMP BULB IAW DC-8 AMM 79-34-01-2 AND THE NR 1 ENGINE OIL TEMP GAUGE IAW DC-8 AMM 31-00-00-2.
- [SDR ABXA010799](https://openairdocs.org/sdr/ABXA010799.md): Longeron · corroded · Feb 5, 2002 · N847AX · Doug DC861 · Fuselage Main, Longeron/Stringer
  > FORWARD ACCESSORY COMPARTMENT LONGERON 36 WAS CORRODED AT FS 662. REPAIRED AREA AND INSTALLED NEW REPAIR ANGLE IAW DC-8 SRM 53-2-0, 51-1-20D, 51-1-8 AND REA D853-40966MR.
- [SDR ABXA010797](https://openairdocs.org/sdr/ABXA010797.md): Longeron · cracked · Feb 5, 2002 · N847AX · Doug DC861 · Fuselage Main, Longeron/Stringer
  > RIGHT WHEEL WELL, LONGERON 24 RIGHT WAS CRACKED AND CORRODED AT STATION 980. REPAIRED AREA AND INSTALLED NEW DOUBLER AND ANGLE IAW DC-8 SRM 51-1-21, 51-1-8, 51-1-20D AND REA D853-40964MR.
- [SDR ABXA010798](https://openairdocs.org/sdr/ABXA010798.md): Web · corroded · Jan 30, 2002 · N847AX · Doug DC861 · Fuselage Miscellaneous Structure
  > FORWARD CARGO, AT FS 80, RIGHT CUSP AT LONGERON 21 RIGHT, ATTACH ANGLE WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-8 AND REA D853-40960MR.
- [SDR ABXA010795](https://openairdocs.org/sdr/ABXA010795.md): Thrust Link · chafed · Jan 28, 2002 · N847AX · Doug DC861 · Nacelle/Pylon Structure
  > #2 PYLON THRUST LINK CHAFED ON BOTTOM SIDE FROM PNEUMATIC DUCT CLAMP (REF. EA 5403277MR) REPAIR OR REPLACEMENT PER CARD 8821016, STEP 02.A) REPAIRED AREA IAW DC-8 SRM 51-1-8, MM 71-00-00, SB 54-92 AND REA D854-40959MR.
- [SDR ABXA010739](https://openairdocs.org/sdr/ABXA010739.md): Fitting · cracked · Jan 23, 2002 · N847AX · Doug DC861 · Wing Miscellaneous Structure
  > RIGHT WING REAR SPAR, XRS 340, ACTUATOR ATTACH FITTING TO REAR SPAR WAS CRACKED. REPLACED FITTING IAW DC-8 DAC DWG 5773254, MM 20-16-00, 20-14-00 AND 27-51-09.
- [SDR ABXA010738](https://openairdocs.org/sdr/ABXA010738.md): Fitting · cracked · Jan 23, 2002 · N847AX · Doug DC861 · Wing, Attach Fittings
  > RIGHT WING AUX SPAR, LOWER "L" ANGLE, WAS CRACKED APPROXIMATELY 10 INCHES LONG AT XRS 47. REPLACED FITTING IAW DC-8 SRM 51-1-24, 51-1-8 AND 51-1-20D.
- [SDR ABXA010737](https://openairdocs.org/sdr/ABXA010737.md): Splice · cracked · Jan 22, 2002 · N847AX · Doug DC861 · Fuselage Miscellaneous Structure
  > FORWARD CARGO AT FS 600 - 620, LONGERON 25 RIGHT, SPLICE FITTING WAS CRACKED. REPLACED FITTING IAW DC-8 SRM 51-3-2, 51-1-20D AND 51-1-11.
- [SDR ABXA010736](https://openairdocs.org/sdr/ABXA010736.md): Splice · cracked · Jan 22, 2002 · N847AX · Doug DC861 · Fuselage Miscellaneous Structure
  > FORWARD CARGO AT FS 600 - 620, LONGERON 31 RIGHT, SPLICE FITTING WAS CRACKED, OUTBOARD SIDE. REPLACED FITTING IAW DC-8 SRM 51-1-24, 51-3-2 AND 51-1-20D.
- [SDR ABXA010796](https://openairdocs.org/sdr/ABXA010796.md): Link · chafed · Jan 21, 2002 · N847AX · Doug DC861 · Nacelle/Pylon Miscellaneous Structure
  > NR 3 PYLON THRUST LINK CHAFED ON LOWER SIDE FROM PNEUMATIC DUCT CLAMP (REF EA AD 54-03277MR) FOR REPAIR OR REPLACEMENT PER ABX CARD 8931015, STEP 02.A). REPAIRED AREA IAW DC-8 SB 54-92.
- [SDR ABXA010455](https://openairdocs.org/sdr/ABXA010455.md): Warning System · malfunctioned · Aug 15, 2001 · N847AX · Doug DC861 · Central Warning
  > YELLOW MAINTENANCE LIGHT ILLUMINATED WITH GREEN SYSTEM OK. LED ILLUMINATED AND NO MALFUNCTION CODES DISPLAYED. CREW DEFERRAL IAW MEL 26-10-3A. MAINTENANCE ACTION REQUIRED. CDU MX TEST INDICATED AC 4725 FALSE ALARM, RESET BREAKERS. FINAL CDU INDICATION SYS
- [SDR ABXA010272](https://openairdocs.org/sdr/ABXA010272.md): Retainer · bent · May 31, 2001 · N847AX · Doug DC861 · Passenger/Crew Doors
  > UNABLE TO OPEN CREW ENTRY DOOR FROM INSIDE AIRCRAFT AFTER LANDING. FOUND BENT SEAL RETAINER AND DOOR JAMB. STRAIGHTENED RETAINER AS REQUIRED. DOOR OPS CHECKED GOOD WITH AIRCRAFT PRESSURIZED IAW DC8 MM 52-11-01.
- [SDR ABXA010226](https://openairdocs.org/sdr/ABXA010226.md): Skin · corroded · May 16, 2001 · N847AX · Doug DC861 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS CORRODED AND FASTENERS WERE BULGING AND MISSING AT FUSELAGE STA 50, LONGERON 34R. MAINTENANCE INSPECTED AND REPAIRED AND DEFERRED IAW ABX REA D853-41127-MR.
- [SDR ABXA000480](https://openairdocs.org/sdr/ABXA000480.md): Battery Pack · discharged · Oct 24, 2000 · N847AX · Doug DC861 · Emergency Lighting
  > EMERGENCY LIGHTING INOP. REPLACED EMERGENCY LIGHT BATTERY PACK ASSEMBLY IAW DC8 MM. OPS CHECKED GOOD.
- [SDR ABXA9801017](https://openairdocs.org/sdr/ABXA9801017.md): Link · worn · Nov 11, 1998 · N847AX · Doug DC861 · Landing Gear Door Retract Section
  > ON GEAR RETRACTION EXPERIENCED VIBRATION FROM AREA UNDER THE COCKPIT. RECYCLED LANDING GEAR TWICE, NOISE CEASED AFTER SECOND RECYCLED. REPLACED NOSE GEAR DOOR LEFT CRANK ASSEMBLY AND ADJUSTED IAW DC8 MM 32-22-1.
- [SDR ABXA9801079](https://openairdocs.org/sdr/ABXA9801079.md): Skin · corroded · Aug 18, 1998 · N847AX · Doug DC861 · Fuselage Main, Plate/Skin
  > CORROSION ON LOWER SKIN BETWEEN STATION 1640 TO 1660 LONGERON 22R-26R. REPAIRED IAW ABX REA D853-17876MR.
- [SDR ABXA9801083](https://openairdocs.org/sdr/ABXA9801083.md): Stringer · corroded · Aug 16, 1998 · N847AX · Doug DC861 · Wing, Longeron/Stringer
  > LEVEL 2 CORROSION, ON LEFT WING STRINGERS, AFTER TRAILING EDGE SKIN REMOVAL STATION XRS 162 TO 436. REPAIRED IAW ABX REA D857-17828MR.
- [SDR ABXA9801082](https://openairdocs.org/sdr/ABXA9801082.md): Stringer · corroded · Aug 16, 1998 · N847AX · Doug DC861 · Wing, Longeron/Stringer
  > RIGHT REAR SPAR, ANGLE SUPPORT CORRODED UNDER TRAILING EDGE UPPER SKIN STRINGER. REPAIRED IAW ABX REA D857-17836.
- [SDR ABXA9801080](https://openairdocs.org/sdr/ABXA9801080.md): Skin · corroded · Aug 16, 1998 · N847AX · Doug DC861 · Fuselage Main, Plate/Skin
  > LEVEL 2 CORROSION ON CUSP UPPER SKIN BETWEEN STATION 1280 TO 1300, LEFT SIDE. REPAIRED IAW ABX D853-17871MR.
- [SDR ABXA9801078](https://openairdocs.org/sdr/ABXA9801078.md): Intercostal · corroded · Aug 16, 1998 · N847AX · Doug DC861 · Wing Miscellaneous Structure
  > RIGHT WING LEADING EDGE CORROSION ON INTERCOSTAL AND INNER DOUBLER AT STATION XFS 13.250. REPAIRED IAW ABX REA D857-17831.
- [SDR ABXA9801077](https://openairdocs.org/sdr/ABXA9801077.md): Stiffener · corroded · Aug 16, 1998 · N847AX · Doug DC861 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION ON STIFFENER AT LONGERON 24L, STATION 940, LEFT WHEEL WELL. REPAIRED IAW ABX REAS D853-17845 AND D853-17844.
- [SDR ABXA9801076](https://openairdocs.org/sdr/ABXA9801076.md): Skin · corroded · Aug 16, 1998 · N847AX · Doug DC861 · Fuselage Main, Plate/Skin
  > CORROSION FOUND UNDER SKIN AT STATION 360 TO 380, STRINGER 35L. REPAIRED IAW ABX REA D853-17894MR.
- [SDR ABXA9801075](https://openairdocs.org/sdr/ABXA9801075.md): Skin · corrosion · Aug 16, 1998 · N847AX · Doug DC861 · Wing, Plate/Skin
  > DEEP CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN. REPAIRED IAW ABX REA D857-17828MR.
- [SDR ABXA9801074](https://openairdocs.org/sdr/ABXA9801074.md): Longeron · corrosion · Aug 16, 1998 · N847AX · Doug DC861 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION AND CRACK ON LONGERON 24 AT STATION 920 IN RIGHT WHEEL WELL. REPAIRED IAW DC8 SRM 53-2-2.
- [SDR ABXA9801073](https://openairdocs.org/sdr/ABXA9801073.md): Skin · corroded · Aug 16, 1998 · N847AX · Doug DC861 · Wing, Plate/Skin
  > FOUND CORROSION, LEFT WING EXTERIOR AT XFS 310.250. REPAIRED IAW ABX REA D857-17806MR.
- [SDR ABXA9801081](https://openairdocs.org/sdr/ABXA9801081.md): Web · corroded · May 15, 1998 · N847AX · Doug DC861 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION ON LOWER WEB BETWEEN STRINGER 36L - 35L, STATION 680 LOWER SKIN. REPAIRED IAW ABX REA D853-17877.
- [SDR ABXA9701478](https://openairdocs.org/sdr/ABXA9701478.md): Battery · discharged · Sep 19, 1997 · N847AX · Doug DC861 · Emergency Lighting
  > EMERGENCY LIGHTS SYSTEM FAILED. REPLACED EMERGENCY LIGHTS BATTERY IAW DC8 MM 33-50-11, SYSTEM CHECKED NORMAL.
- [SDR ABXA9701394](https://openairdocs.org/sdr/ABXA9701394.md): Wire · burned · Aug 10, 1997 · N847AX · Doug DC861 · Light System Wiring
  > DURING CRUISE, EXPERIENCED SMELL OF BURNING PLASTIC. TURNED ALL LIGHTING OFF AND ODOR WENT AWAY. REPAIRED WIRE IN NR 4 FUEL CONSOLE LIGHTING PANEL. OPS CHECKED GOOD IAW DC8 MM CHAPTER 33.

Next page: https://openairdocs.org/deregistered/N847AX-2010-04-26/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 = 'N847AX' AND deregistration_id = 'N847AX-2010-04-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N847AX-2010-04-26/reports

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