# Service difficulty reports: N848AX, cancelled Feb 13, 2007

A list on [N848AX, cancelled Feb 13, 2007](https://openairdocs.org/deregistered/N848AX-2007-02-13.md).

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

- [SDR ABXA040135](https://openairdocs.org/sdr/ABXA040135.md): Linkage · lack of lube · Apr 1, 2004 · N848AX · Doug DC861 · Aileron Control System
  > COULD NOT MOVE AILERON TRIM WHEEL DURING DESCENT INTO ILN. LUBED AND INSPECTED LT, RT AND WHEEL WELL AILERON LINKAGES. OPERATED AILERON TRIM THROUGH NUMBEROUS TIMES. OPERATED NORMAL.
- [SDR ABXA040013](https://openairdocs.org/sdr/ABXA040013.md): Longeron · corroded · Dec 8, 2003 · N848AX · Doug DC861 · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO STA 300 TO 320, LONGERON 32 LEFT, ATTACH ANGLE HAD CORROSION. REMOVED CORROSION AND REPAIRED LONGERON IAW REA D853-48497MR AND DC-8 SRM 53-2-0.
- [SDR ABXA040004](https://openairdocs.org/sdr/ABXA040004.md): Longeron · corroded · Dec 3, 2003 · N848AX · Doug DC861 · Fuselage Main, Longeron/Stringer
  > AFT CARGO AT STA 1180, LONGERON 26 LEFT, LONGERON HAD CORROSION. REMOVED CORROSION, CUT OUT DAMAGED LONGERON, FABRICATED AND INSTALLED REPAIR ANGLES AND WEB SPLICE, ALODINED, AND PRIMED IAW DC-8 SRM 51-1-8, 53-2-0, 53-2-2, 51-1-21, 51-1-20D, AND REA D853-4848
- [SDR ABXA040007](https://openairdocs.org/sdr/ABXA040007.md): Skin · corroded · Dec 3, 2003 · N848AX · Doug DC861 · Wing, Plate/Skin
  > LEFT WING UPPER XRS 519 - 624 CORROSION AROUND FASTENER HEADS (24 EACH). REPAIRED AREA IAW REA D857-48493MR.
- [SDR ABXA040011](https://openairdocs.org/sdr/ABXA040011.md): Skin · cracked · Dec 3, 2003 · N848AX · Doug DC861 · Passenger/Crew Doors
  > L1 FORWARD PAX DOOR, LOWER AFT CORNER HAD A CRACK IN EXTERNAL SKIN. REMOVED DAMAGED AREA, REPAIRED SKIN / DOUBLER TRIM OUT IAW SRM 53-2-0 AND REA D853-48470MR.
- [SDR ABXA040006](https://openairdocs.org/sdr/ABXA040006.md): Skin · cracked · Dec 1, 2003 · N848AX · Doug DC861 · Fuselage Main, Plate/Skin
  > CRACK IN OUTER SKIN AT LOWER FORWARD CORNER OF AFT PASSENGER DOOR. REMOVED CRACKED OUTER SKIN, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D AND REA D853-48472MR.
- [SDR ABXA040010](https://openairdocs.org/sdr/ABXA040010.md): Skin · cracked · Nov 29, 2003 · N848AX · Doug DC861 · Service Doors
  > R1 FORWARD SERVICE DOOR, LOWER AFT CORNER HAD A CRACK ON EXTERNAL SKIN. REPAIRED AREA BY FABRICATING REPAIR DOUBLER, FILLERS AND TRIPLERS, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-8, 53-2-0 AND REA D853-48471MR.
- [SDR ABXA040005](https://openairdocs.org/sdr/ABXA040005.md): Longeron · corroded · Nov 28, 2003 · N848AX · Doug DC861 · Fuselage Main, Longeron/Stringer
  > AFT CARGO AT STA 1200 - 122 AND LONGERON 28 LEFT HAD CORROSION. REMOVED CORROSION, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR ANGLES IAW DC-8 SRM 51-1-8, 51-1-20D AND REA D853-48483MR.
- [SDR ABXA040012](https://openairdocs.org/sdr/ABXA040012.md): Frame · corroded · Nov 27, 2003 · N848AX · Doug DC861 · Fuselage Main, Frame
  > A/C ACCESS COMPARTMENT AT FS 56, BETWEEN LONGERON 35 LT AND 35 RT, FRAME LOWER FLANGE WAS CORRODED. REMOVED CORROSION, FABRICATED REPAIR ANGLE, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 53-2-0 AND REA D853-48484MR.
- [SDR ABXA040008](https://openairdocs.org/sdr/ABXA040008.md): Skin · misrepaired · Nov 26, 2003 · N848AX · Doug DC861 · Fuselage Main, Plate/Skin
  > L2 DOOR LOWER AFT CORNER HAD A REPAIR THAT DID NOT RESEMBLE SERVICE ENGINEERING SKETCH ES00863. REMOVED DISCREPANT REPAIR, FABRICATED REPAIR DOUBLERS AND FILLER, ALODINED, PRIMED, AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-21, 53-2-0 AND REA D853-48474MR.
- [SDR ABXA040009](https://openairdocs.org/sdr/ABXA040009.md): Skin · damaged · Nov 25, 2003 · N848AX · Doug DC861 · Fuselage Main, Plate/Skin
  > R1 DOOR UPPER FORWARD CORNER HAD A REPAIR THAT DID NOT RESEMBLE REWORK DRAWING SR08530021 OR ENGINEERING SKETCH ES00863. REMOVED DOUBLER AND TRIPLER, FABRICATED DOUBLER REPAIR, PRIMED, ALODINED AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0, 51-1-8, 51-1-20D, 51-
- [SDR ABXA040014](https://openairdocs.org/sdr/ABXA040014.md): Skin · cracked · Nov 24, 2003 · N848AX · Doug DC861 · Fuselage Main, Plate/Skin
  > R2 AFT SERVICE DOOR, UPPER AFT CORNER HAD CRACK INDICATION. REPAIRED CRACKED AREA, INSTALLED REPAIR DOUBLERS IAW DC-8 SRM 53-2-0 AND REA D853-48479MR.
- [SDR ABXA030281](https://openairdocs.org/sdr/ABXA030281.md): Battery Pack · discharged · Jul 10, 2003 · N848AX · Doug DC861 · Emergency Lighting
  > ON PREDEPARTURE CHECK FOUND EMERGENCY LIGHT BATTERY RACK DEAD. REPLACED EMERGENCY LIGHT BATTERY RACK ASSSEMBLY. GROUND OPS CHECKED OK IAW AMM 33-50-02.
- [SDR ABXA030115](https://openairdocs.org/sdr/ABXA030115.md): Door · missing · Mar 11, 2003 · N848AX · Doug DC861 · Landing Gear Doors
  > LEFT MAIN LANDING GEAR LOWER COVER PANEL (FOR STRUT) MISSING ON BPO WALK AROUND. INSTALLED NEW LEFT MAIN LANDING GEAR CENTER DOOR IAW DC-8 MM.
- [SDR ABXA020369](https://openairdocs.org/sdr/ABXA020369.md): Engine · malfunctioned · Dec 19, 2002 · N848AX · Doug DC861 · Engine (Turbine/Turboprop)
  > DURING CLIMB, LOW OIL PRESSURE LIGHT CAME ON. OIL PRESSURE FLUX AT 35 PSI. OIL QUANTITY DROPPED TO (0), ENGINE SHUTDOWN AT 0405Z, N1 24 PERCENT, N2 33 PERCENT, PRESS 5 PSI, TEMP 125 DEGREES C TOD PRESS 5, TEMP 84, N1 26 PERCENT, N2 36 PERCENT, TIME 0500Z. REMO
- [SDR ABXA020279](https://openairdocs.org/sdr/ABXA020279.md): Battery · discharged · Oct 31, 2002 · N848AX · Doug DC861 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS WERE VERY DIM. REPLACED EMERGENCY LIGHT BATTERY RACK ASSEMBLY AND TESTED GOOD IAW DC-8 AMM 33-50-01-2.
- [SDR ABXA010675](https://openairdocs.org/sdr/ABXA010675.md): Latch · out of adj · Jan 18, 2002 · N848AX · Doug DC861 · Fixed Inner Doors
  > COCKPIT ENTRY DOOR LATCH MECHANISM WAS JAMMED. ADJUSTED DOOR LATCH AS NEEDED IAW DC-9 MM CHAPTER 51. OPS CHECKED GOOD.
- [SDR ABXA010594](https://openairdocs.org/sdr/ABXA010594.md): Fitting · misdrilled · Sep 6, 2001 · N848AX · Doug DC861 · Fuselage Main, Attach Fittings
  > AFT LOWER CARGO FRAME WAS MISDRILLED AT STAION 1140 RIGHT AND LONGERON 30 RIGHT. INSTALLED NEW FILLER AND DOUBLER AND REPAIRED AREA IAW DC-8 SRM 51-1-8 AND REA D853-40922MR.
- [SDR ABXA010593](https://openairdocs.org/sdr/ABXA010593.md): Fitting · cracked · Aug 27, 2001 · N848AX · Doug DC861 · Fuselage Main, Attach Fittings
  > MAIN CABIN, STATION 682 AND LONGERON 10 RIGHT, LONGERON TIE FITTING WAS CRACKED. INSTALLED NEW FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-20D AND 51-1-23.
- [SDR ABXA010592](https://openairdocs.org/sdr/ABXA010592.md): Fitting · cracked · Aug 27, 2001 · N848AX · Doug DC861 · Fuselage Main, Attach Fittings
  > MAIN CABIN, STATION 682 AND LONGERON 5 RIGHT, LONGERON TIE FITTING WAS CRACKED. INSTALLED NEW FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-24, 51-1-20D AND 51-1-23.
- [SDR ABXA010591](https://openairdocs.org/sdr/ABXA010591.md): Fitting · cracked · Aug 27, 2001 · N848AX · Doug DC861 · Fuselage Main, Attach Fittings
  > MAIN CABIN, STATION 678 AND LONGERON 7 RIGHT, LONGERON TIE FITTING WAS CRACKED. INSTALLED NEW FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-20D AND 51-1-23.
- [SDR ABXA010590](https://openairdocs.org/sdr/ABXA010590.md): Fitting · cracked · Aug 27, 2001 · N848AX · Doug DC861 · Fuselage Main, Attach Fittings
  > MAIN CABIN, STATION 450 AND LONGERON 14 RIGHT, LONGERON TIE FITTING WAS CRACKED. INSTALLED NEW FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-1-8, AND DAC DWG #3887799.
- [SDR ABXA010513](https://openairdocs.org/sdr/ABXA010513.md): Fitting · cracked · Aug 27, 2001 · N848AX · Doug DC861 · Fuselage Main, Attach Fittings
  > MAIN CABIN TIE FITTING AT STA 682 L11R WAS CRACKED. MAINTENANCE REPLACED THE FITTING IAW DC-8 SRM.
- [SDR ABXA010232](https://openairdocs.org/sdr/ABXA010232.md): Control Cable · broken · May 19, 2001 · N848AX · Doug DC861 · Landing Gear Retraction/Extension System
  > THE LEFT MAIN LANDING GEAR UPLOCK HOOK WAS NOTED TO BE IN THE FLIGHT POSITION. THE MANUAL RELEASE CABLE WAS FOUND TO BE BROKEN. MAINTENANCE INSPECTED AND REPLACED THE MANUAL RELEASE CABLE RUN ASSEMBLY IAW DC-8 MM 32-31-00. ADJUSTMENT AND TEST PROCEDURES WER
- [SDR ABXA000416](https://openairdocs.org/sdr/ABXA000416.md): Latch · lack of lube · Sep 13, 2000 · N848AX · Doug DC861 · Fixed Inner Doors
  > COCKPIT ENTRY DOOR WOULD NOT OPEN FROM CABIN (CARGO) SIDE. CLEANED AND LUBRICATED LATCH ASSEMBLY IAW DC8 MM 52-10-00. OPS CHECKED GOOD.
- [SDR ABXA000067](https://openairdocs.org/sdr/ABXA000067.md): Spar · corroded · Jan 12, 2000 · N848AX · Doug DC861 · Wing Spar
  > RIGHT WING LOWER REAR SPAR CAP AFT TANG AT STATION XCW 69.5 CORRODED. REPARIED RIGHT WING AFT LOWER SPAR AFT TANG AT STATION XCW 69.5 IAW ABX REA D85733882 MR.
- [SDR ABXA000055](https://openairdocs.org/sdr/ABXA000055.md): Panel · cracked · Dec 17, 1999 · N848AX · Doug DC861 · Wing, Plate/Skin
  > DURING C-CHECK, CRACKS FOUND IN RIGHT WING UPPER AFT SKIN PANELS. REPAIRED RIGHT WING UPPER AFT SKIN PANEL IAW ABX REA D85733696 MR.
- [SDR ABXA9900646](https://openairdocs.org/sdr/ABXA9900646.md): Lock · out of adjust · Aug 17, 1999 · N848AX · Doug DC861 · Fixed Inner Doors
  > COCKPIT DOOR LOCK WAS INOPERATIVE, WOULD NOT RELEASE. REPAIRED COCKPIT DOOR IAW DC8 MM, OPS CHECKED GOOD.
- [SDR ABXA9900588](https://openairdocs.org/sdr/ABXA9900588.md): Latch · out of adjust · Jul 21, 1999 · N848AX · Doug DC861 · Fixed Inner Doors
  > COCKPIT DOOR HANDLE WOULD NOT UNLOCK. ADJUSTED INNER LATCH, OPS CHECKED GOOD.
- [SDR ABXA9900382](https://openairdocs.org/sdr/ABXA9900382.md): Latch · malfunctioned · May 24, 1999 · N848AX · Doug DC861 · Fixed Inner Doors
  > COCKPIT DOOR WOULD NOT UNLOCK. REPLACED COCKPIT DOOR LATCH ASSEMBLY IAW DC8 MM 51-30.
- [SDR ABXA9900157](https://openairdocs.org/sdr/ABXA9900157.md): Switch · failed · Mar 2, 1999 · N848AX · Doug DC861 · AC Indicating System
  > DURING TAKEOFF AT ROTATION SPEED, AC FREQ METER WENT OFF SCALE LOW IN ALL POSITIONS. UNABLE TO MONITOR GENERATORS. DUMPED FUEL AND RETURNED TO ONT. REPLACED VOLT AND FREQ SELECTOR SWITCH AND FREQ METER INDICATOR. OPS CHECKED GOOD.
- [SDR ABXA9900008](https://openairdocs.org/sdr/ABXA9900008.md): Chart Light · smoking · Jan 12, 1999 · N848AX · Doug DC861 · Flight Compartment Lighting
  > DURING CRUISE, FIRST OFFICER'S CHART LIGHT SMOKES WHEN ON. INSPECTED FIRST OFFICER'S CHART LIGHT RHEOSTAT, LIGHT BULBS AND WIRING AND NO DEFECTS NOTED. OPS CHECKED GOOD IAW DC8 MM.
- [SDR ABXA9801201](https://openairdocs.org/sdr/ABXA9801201.md): Indication · malfunctioned · Dec 30, 1998 · N848AX · Doug DC861 · Landing Gear Position and Warning
  > AFTER TAKEOFF ON GEAR RETRACTION, GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED GEAR, NO CHANGE. COMPLIED WITH GEAR UNSAFE PROCEDURES. THE LANDING AT SJC WAS UNEVENTFUL. PERFORMED PROXIMITY CONTROL BOX TEST. PERFORMED ADJUST/TEST IAW DC8 MM 32-60-0. C
- [SDR ABXA9801189](https://openairdocs.org/sdr/ABXA9801189.md): Duct · failed · Dec 22, 1998 · N848AX · Doug DC861 · Pneumatic Distribution System
  > EN ROUTE FROM ONT TO ILN, AIRCRAFT EXPERIENCED RAPID DECOMPRESSION AT 33.000 FT. CABIN CLIMED TO 20,000 FT IN APPROX 2 MIN. EXECUTED EMERGENCY DESCENT. PRESSURE WAS REGAINED AT APPROX 10,000 FT. FOUND DUCT CLAMP LOOSE AND DUCT SEPARATED. RECONNECTED DUCT
- [SDR ABXA9801060](https://openairdocs.org/sdr/ABXA9801060.md): Window · out of adjust · Nov 12, 1998 · N848AX · Doug DC861 · Flight Compartment Windows
  > FIRST OFFICER'S WINDOW WOULD NOT OPEN. ADJUSTED LOWER AFT LINKAGE ROD IAW DC-8 MM 56-10-3, OPS CHECKED GOOD.
- [SDR ABXA9800673](https://openairdocs.org/sdr/ABXA9800673.md): Pivot Arm · broken · Jul 30, 1998 · N848AX · Doug DC861 · Landing Gear Steering System
  > DURING POST FLIGHT INSP, FOUND LEFT MAIN LANDING GEAR BOGIE SWIVEL MECHANISM PIVOT ARM BROKEN. REPLACED BOGIE SWIVEL ARM IAW DC8 MM 32-51-04.
- [SDR ABXA9800634](https://openairdocs.org/sdr/ABXA9800634.md): Fitting · worn · Jul 20, 1998 · N848AX · Doug DC861 · Landing Gear Retraction/Extension System
  > RED GEAR UNSAFE LIGHT ILLUMINATED INTERMITTENTLY AFTER GEAR RETRACTION. RECYCLED GEAR AND LIGHT DID NOT ILLUMINATE AGAIN. REPLACED BOTH LEFT AND RIGHT MAIN LANDING GEAR DRAG BRACE FITTING. PERFORMED OPS CHECK OF GEAR, OPS CHECKED GOOD.
- [SDR ABXA9800472](https://openairdocs.org/sdr/ABXA9800472.md): Retract Pin · corroded · May 28, 1998 · N848AX · Doug DC861 · Main Landing Gear
  > RIGHT MAIN LANDING GEAR RETRACT PIN BOSS HOLE HAD CORROSION. REPAIRED IAW ABX REA D832-23374 MR.
- [SDR ABXA9800471](https://openairdocs.org/sdr/ABXA9800471.md): Retract Pin · corroded · May 28, 1998 · N848AX · Doug DC861 · Landing Gear Retraction/Extension System
  > LEFT MAIN LANDING GEAR RETRACT PIN BOSS HOLE HAD CORROSION. REPAIRED IAW ABX REA D832-23373 MR.
- [SDR ABXA9800249](https://openairdocs.org/sdr/ABXA9800249.md): Window · lack of lube · Mar 16, 1998 · N848AX · Doug DC861 · Flight Compartment Windows
  > DURING POST FLIGHT, FOUND FIRST OFFICER'S WINDOW (EMERG EXIT) BINDING AND WOULD ONLY OPEN PARTIALLY. LUBRICATED WINDOW IAW DC8 MAINT MANUAL, OPS CHECKED GOOD.
- [SDR ABXA9800113](https://openairdocs.org/sdr/ABXA9800113.md): Latch · out of adjust · Feb 23, 1998 · N848AX · Doug DC861 · Fixed Inner Doors
  > COCKPIT DOOR WOULD NOT OPEN. ADJUSTED DOOR LATCH IAW DC8 MM, OPS CHECKED GOOD.
- [SDR ABXA9800013](https://openairdocs.org/sdr/ABXA9800013.md): Door Assy · defective · Jan 12, 1998 · N848AX · Doug DC861 · Fixed Inner Doors
  > DURING POST FLIGHT INSPECTION, FOUND COCKPIT DOOR HARD TO OPEN. RESECURED HARDWARE ON DOOR, DOOR OPERATES NORMAL.
- [SDR ABXA9700037](https://openairdocs.org/sdr/ABXA9700037.md): Skin · punctured · Feb 19, 1997 · N848AX · Doug DC861 · Wing, Plate/Skin
  > HOLE IN STUB WING JUST OUTBOARD OF NR 3 ENGINE. FOUND DURING POST-FLIGHT INSPECTION. REPAIRED HOLE IN STUB WING I/A/W R.E.A. D857-18359. DEFERRED FOR TRACKING I/A/W R.E.A. D857-18859 AND G.M.M. 7.04, CODE 15. D.I. 848 375.
- [SDR ABXA970030](https://openairdocs.org/sdr/ABXA970030.md): Uplatch Mech · out of adjust · Feb 6, 1997 · N848AX · Doug DC861 · Landing Gear Door Retract Section
  > ON DEPARTURE, THE RIGHT MAIN GEAR DOOR FAILED UPLATCH ON INITIAL GEAR RETRACTION. RECYCLED GEAR AND OPS NORMAL. RIGHT MAIN GEAR DOOR DID NOT GO UP AND LATCHED ON GO-AROUND. ADJUSTED RIGHT MAIN LANDING GEAR UPLATCH MECHANISM PER DC-8 MM.
- [SDR ABXA9600665](https://openairdocs.org/sdr/ABXA9600665.md): Retract Mech · out of adjust · Nov 12, 1996 · N848AX · Doug DC861 · Landing Gear Door Retract Section
  > AFTER GEAR RETRACTION, GEAR UNSAFE LIGHT REMAINED ILLUMINATED, LANDING GEAR AND DOOR LATCHING INDICATOR INDICATED RIGHT MAIN GEAR DOOR UNLATCHED. AFTER CYCLING GEAR SEVERAL TIMES, GEAR UNSAFE LIGHT EXTINGUISHED AND NOT LATCHED LIGHT EXTINGUISHED. ADJUSTED RI
- [SDR ABXA9600486](https://openairdocs.org/sdr/ABXA9600486.md): Transmitter · defective · Apr 29, 1996 · N848AX · Doug DC861 · Engine Oil Pressure
  > DURING CLIMB, NR 4 ENGINE OIL PRESSURE INCREASED TO 61 PSI MOMENTARILY AND THEN DROPPED TO 59 PSI WITH MAXIMUM POWER SET FOR TAKEOFF. REDUCED POWER TO MCT AND OIL PRESSURE DROPPED TO 53 PSI AND THEN BEGAN TO INCREASE. ENGINE WAS SHUTDOWN WHEN THE OIL PRESSUR
- [SDR ABXA9500932](https://openairdocs.org/sdr/ABXA9500932.md): Eel Lamp · failed · Nov 9, 1995 · N848AX · Doug DC861 · Emergency Lighting
  > DURING SERVICE CHECK, FOUND THE EMERGENCY LIGHTING INOP. RELAMPED POSITIONS AND EMERGENCY LIGHTING OPS CHECKED GOOD IAW ABX WORK CARD DC-8-1 ITEM NR 8.
- [SDR ABXA9500672](https://openairdocs.org/sdr/ABXA9500672.md): Brace · cracked · Aug 14, 1995 · N848AX · Doug DC861 · Nose/Tail Landing Gear
  > DURING POST FLIGHT WALK-AROUND, FOUND A CRACK IN THE LEFT SIDE BRACE OF THE NOSE LANDING GEAR, JUST BELOW THE DOOR ATTACH POINT. REPLACED THE LEFT SIDE BRACE IAW DC-8 MM 32-21-3, OPS CHECKED NORMAL.
- [SDR ABXA9500528](https://openairdocs.org/sdr/ABXA9500528.md): Bulb · defective · Jun 5, 1995 · N848AX · Doug DC861 · Landing Gear Position and Warning
  > WHEN GEAR WAS LOWERED, NO DOWN AND LOCKED INDICATION ON RIGHT MAIN GEAR. PUT GEAR UP AND RELAMPED RIGHT MAIN GEAR INDICATION. LOWERED GEAR AND RIGHT MAIN SHOWED DOWN AND LOCKED. VERIFIED BOTH RIGHT MAIN GEAR DOWN AND LOCK INDICATION BULBS BURNED OUT. RELAM
- [SDR ABXA9500310](https://openairdocs.org/sdr/ABXA9500310.md): Hinge Pins · lack of lube · Apr 4, 1995 · N848AX · Doug DC861 · Flight Compartment Windows
  > THE FIRST OFFICER'S SLIDING WINDOW VERY DIFFICULT TO OPEN. CLEANED AND LUBED HINGE PINS AND LATCHING MECHANISM. WINDOW OPS CHECKED GOOD IAW DC-8 MM CHAPTER 56.

## 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 = 'N848AX' AND deregistration_id = 'N848AX-2007-02-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N848AX-2007-02-13/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.