# Service difficulty reports: N849AX, cancelled Mar 4, 2005

A list on [N849AX, cancelled Mar 4, 2005](https://openairdocs.org/deregistered/N849AX-2005-03-04.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 3 · 118 reports

- [SDR ABXA030130](https://openairdocs.org/sdr/ABXA030130.md): Controller · defective · Apr 3, 2003 · N849AX · Doug DC861 · Windshield/Door Rain/Ice Removal
  > WINDSHIELD HEAT, SPARKS CAME FROM FORWARD RIGHT WINDSHIELD. SPARKS WERE COMING FROM LOWER RIGHT. CIRCUIT BREAKERS WERE PULLED. REPLACED RIGHT WINDSHIELD TEMP. CONTROL DUE TO WINDOW REPLACEMENT IAW DC-8 AMM 30-41-0-1-2-0001. OPS CHECKED GOOD. REPLACED RIG
- [SDR ABXA030061](https://openairdocs.org/sdr/ABXA030061.md): Control Cable · out of adjust · Jan 29, 2003 · N849AX · Doug DC861 · Landing Gear Door Retract Section
  > GEAR RETRACTION RED GEAR LIGHT STAYED ON. LANDING GEAR RT DOOR LATCHING SELECTOR ON FLT ENGINEER'S PANEL SHOWED RT DOOR. CYCLED GEAR, LIGHTS WENT OUT. ADJUSTED RT MLG DOOR FOLLOW UP MECHANISM AND CABLES 135A & 134A IAW DC-8 MM 32-31-05. CHECKED RT MLG DOOR UP
- [SDR ABXA030057](https://openairdocs.org/sdr/ABXA030057.md): Actuator · defective · Jan 27, 2003 · N849AX · Doug DC861 · Landing Gear Door Actuator
  > WHEN GEAR WAS RETRACTED AFTER TAKE-OFF, LANDING GEAR UNSAFE LIGHT REMAINED ON. RT MLG DOOR INDICATED NOT LATCHED. CYCLED GEAR PER ILN MAINTENANCE REQUEST. NO CHANGE IN PROBLEM. REPLACED RT MLG DOOR ACTUATOR IAW DC-8 MM 32-31-05. ADJUSTED FOLLOW-UP HITCH IA
- [SDR ABXA030058](https://openairdocs.org/sdr/ABXA030058.md): Roller · out of adjust · Jan 24, 2003 · N849AX · Doug DC861 · Landing Gear Door Retract Section
  > GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RT DOOR INDICATED NOT LATCHED ON FLIGHT ENGINEERS PANEL. CYCLED GEAR ONCE AND ALL CHECKED GOOD. SHIMMED RT MLG DOOR UPLATCH ROLLER IAW DC-8 MM 32-31-04. PULL CHECK OF RT MLG DOOR IAW DC-8 MM 32-31-04. PERFO
- [SDR ABXA030046](https://openairdocs.org/sdr/ABXA030046.md): Torque Tube · out of adjust · Jan 22, 2003 · N849AX · Doug DC861 · Landing Gear Retraction/Extension System
  > GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED WITH RT MLG DOOR SHOWING UNSAFE. CYCLED LANDING GEAR, LIGHTS REMAINED ON. PLACED GEAR HANDLE TO UPLATCH POSITION. LIGHT WENT OUT. EXCESSIVE INBOARD AND OUTBOARD GAPS WERE FOUND ON THE RT MLG TORQUE TUBE.
- [SDR ABXA020069](https://openairdocs.org/sdr/ABXA020069.md): Battery Pack · discharged · Jul 29, 2002 · N849AX · Doug DC861 · Emergency Lighting
  > LOST EXTERNAL POWER AND NO EMERGENCY EXIT LIGHT ILLUMINATED WITH SWITCH IN ARMED POSITION. REPLACED THE EMERGENCY BATTERY PACK. OPS CHECKED GOOD IAW DC-8 MM.
- [SDR ABXA020002](https://openairdocs.org/sdr/ABXA020002.md): Switch · defective · Jun 24, 2002 · N849AX · Doug DC861 · Engine Oil Pressure
  > # 1 engine low oil pressure light on in flight. Oil pressure was 46 psi. Engine was shut down at 0905 Z. Windmilling oil pressure on secured engine was 12 psi for 19 minutes. Replaced low pressure switch IAW DC-8 MM 79-30. Ran # 1 engine, no leaks noted. Engi
- [SDR ABXA010831](https://openairdocs.org/sdr/ABXA010831.md): Doubler · cracked · Mar 29, 2002 · N849AX · Doug DC861 · Wing Structure
  > LEFT WING 505F PANEL HAD 10 EACH CRACK INDICATIONS AT FASTENER HOLES. REPAIRED AREA IAW REA D857-43069MR.
- [SDR ABXA010832](https://openairdocs.org/sdr/ABXA010832.md): Fitting · corroded · Mar 28, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)
  > SURFACE CORROSION FOUND IN CARGO DOOR TORQUE BOX AT STA. 345, LONGERON 35 RIGHT, LOWER CARGO COMPARTMENT. REPLACED 'Z' FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-24, REA D853-43-83MR AND REA D853-43076MR.
- [SDR ABXA010833](https://openairdocs.org/sdr/ABXA010833.md): Doubler · corroded · Mar 27, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)
  > AFT CARGO, LONGERON 32 RIGHT, B/S 1200, WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-1-21 AND REA D853-43071MR.
- [SDR ABXA010801](https://openairdocs.org/sdr/ABXA010801.md): Fitting · cracked · Mar 23, 2002 · N849AX · Doug DC861 · Nacelle/Pylon Structure
  > #3 PYLON V-BLOCK SUPPORT FITTING HAD A CRACK IN IT. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D, 51-3-0, 51-1-23 AND 56-3-0.
- [SDR ABXA010800](https://openairdocs.org/sdr/ABXA010800.md): Strap · corroded · Mar 22, 2002 · N849AX · Doug DC861 · Nacelle/Pylon Structure
  > #1 PYLON "T" CAP STRAP HAD CORROSION AT WING STATION 485.00, LOWER SPAR CAP, FORWARD SPAR. REMOVED AND REPLACED THE FORWARD SPAR STRAP, REMOVED AND REINSTALLED THE #1 PYLON "T" DOUBLER IAW DC-8 SRM 51-1-20D, 51-1-8.
- [SDR ABXA010789](https://openairdocs.org/sdr/ABXA010789.md): Seat Track · cracked · Mar 20, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)
  > FORWARD CARGO AT F.S. 340 - 360, LEFT BUTT LINE 50, SEAT TRACK WAS CRACKED. REPLACED SEAT TRACK IAW DC-8 SRM 51-1-8, 51-3-0, 51-1-21 AND ZANTOP DWG. #86302.
- [SDR ABXA010788](https://openairdocs.org/sdr/ABXA010788.md): Fitting · cracked · Mar 19, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)
  > FORWARD CARGO AT F.S. 200 - 220, LONGERON 31 LEFT, SPLICE FITTING WAS CRACKED. REPLACED FITTING IAW DC-8 SRM 51-1-20D.
- [SDR ABXA010787](https://openairdocs.org/sdr/ABXA010787.md): Frame · cracked · Mar 19, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)
  > FORWARD CARGO AT F.S. 180, ABOVE LONGERON 36 FRAME, UPPER CHORD WAS CRACKED AND BENT. REPAIRED AREA IAW DC-8 SRM STD-5310-002 AND SRM 51-1-8.
- [SDR ABXA010786](https://openairdocs.org/sdr/ABXA010786.md): Seat Track · cracked · Mar 19, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)
  > FORWARD CARGO AT F.S. 580 - 600, LEFT BUTT LINE 50, SEAT TRACK WAS CRACKED. REPLACED SEAT TRACK IAW DC-9 SRM 51-3-0, 51-1-8 AND ZANTOP DWG. #86302.
- [SDR ABXA010830](https://openairdocs.org/sdr/ABXA010830.md): Longeron · corroded · Mar 18, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)
  > FORWARD ACCESSORY COMPARTMENT AT F.S. 640 - 660, LONGERON 31 RIGHT, WAS CRACKED. FABBED REPAIR STRAP AND REPAIRED AREA IAW DC-8 SRM 53-2-0, 53-4-1, 51-1-20D AND REA D853-43068MR.
- [SDR ABXA010785](https://openairdocs.org/sdr/ABXA010785.md): Fitting · cracked · Mar 16, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)
  > FORWARD CARGO, F.S. 380 - 400, LONGERON 31 LEFT, SPLICE FITTING WAS CRACKED. REMOVED AND REPLACED FITTING AT STA. 390, LONGERON 31 LEFT IAW DC-8 SRM 51-1-24 AND 51-1-20D.
- [SDR ABXA010791](https://openairdocs.org/sdr/ABXA010791.md): Strap · cracked · Mar 15, 2002 · N849AX · Doug DC861 · Wing Miscellaneous Structure
  > T-CAP DOUBLER STRAP AT WS 485.00, FORWARD SPAR, LOWER CRACKED NR 4 ALT. REMOVED AND REPLACED DOUBLER STRAP IAW DC-8 SRM 51-1-20D, 51-1-24 AND DAC DWG 5803958.
- [SDR ABXA010790](https://openairdocs.org/sdr/ABXA010790.md): Fitting · cracked · Mar 15, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)
  > FORWARD LOWER CARGO, STATION 272, FITTING WAS CRACKED FORWARD OF C1 DOOR. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D, 51-3-1 AND 51-1-24.
- [SDR ABXA010784](https://openairdocs.org/sdr/ABXA010784.md): Fitting · cracked · Mar 15, 2002 · N849AX · Doug DC861 · Fuselage Main, Structure
  > SPLICE FITTING CRACKED AT LONGERON 27 RIGHT, STATION 450, FORWARD LOWER CARGO. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-1-21.
- [SDR ABXA010834](https://openairdocs.org/sdr/ABXA010834.md): Spar Cap · cracked · Mar 12, 2002 · N849AX · Doug DC861 · Wing Structure
  > RIGHT WING, FORWARD LOWER SPAR CAP HAD 9 EACH FASTENERS HOLES SHOWING CRACK INDICATIONS. REPAIRED DAMAGED HOLES IAW REA D857-43058.
- [SDR ABXA010792](https://openairdocs.org/sdr/ABXA010792.md): Seat Track · cracked · Mar 10, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)
  > FORWARD CARGO AT F.S. 580 - 600, AT LEFT BUTT LINE 55, SEAT TRACK WAS CRACKED. REMOVED AND REPLACED SEAT TRACK IAW DC-8 SRM 51-3-0, 51-1-24 AND 51-1-8.
- [SDR ABXA010777](https://openairdocs.org/sdr/ABXA010777.md): Splice · cracked · Mar 10, 2002 · N849AX · Doug DC861 · Fuselage Main, Structure
  > AFT LOWER CARGO COMPARTMENT, LONGERON SPLICE TIE CRACKED BETWEEN B.S. 1300 - 1320, LONGERON 31 LEFT. REPLACED SPLICE IAW DC-8 SRM 51-1-20D AND 51-3-2.
- [SDR ABXA010472](https://openairdocs.org/sdr/ABXA010472.md): Indicator · defective · Sep 12, 2001 · N849AX · Doug DC861 · Hydraulic Quantity Indicator
  > DURING GEAR DOWN EXTENTION INTO LAX, THE HYDRAULIC QUANTITY BEGAN TO RAPIDLY DECREASE. CREW DECLARED AN EMERGENCY INTO LAX. FOUND THE HYDRAULIC INDICATOR INTERMITTENTLY INOPERATIVE. REPLACED THE INDICATOR. BLED THE HYRDRAULIC SYSTEM AND CYCLED ALL FLIGHT CONTR
- [SDR ABXA010471](https://openairdocs.org/sdr/ABXA010471.md): Tire · defective · Sep 12, 2001 · N849AX · Doug DC861 · Landing Gear Retraction/Extension System
  > DURING DEPARTURE FROM ILN, UPON GEAR RETRACTION, WHEN THE NOSE GEAR ENTERED THE WELL, A VIBRATION WAS FELT IN THE THROTTLE QUADRANT AREA. CREW RECYCLED GEAR AND DID A TOWER FLYBY THEN CONTINUED ON TO LAX. FOUND THE LEFT NOSE TIRE DEFORMED AND OUT OF ROUND. REP
- [SDR ABXA010458](https://openairdocs.org/sdr/ABXA010458.md): Switch · malfunctioned · Aug 30, 2001 · N849AX · Doug DC861 · Door Warning System
  > MAIN CARGO DOOR, NON-DOUGLAS, SYSTEM A-LIGHT CAME ON IN FLIGHT WITH PRESSURIZATION HOLDING. PER ABNORMALS, CREW DESCENDED TO 10,000 FEET. DEPRESSURIZED AIRCRAFT AND INSPECTED DOOR. LIGHT WENT OUT BELOW 6.0 PSID. DOOR INSPECTION, ALL LATCHED APPEARED LOCKED
- [SDR ABXA010445](https://openairdocs.org/sdr/ABXA010445.md): Seal · leaking · Aug 17, 2001 · N849AX · Doug DC861 · Leading Edge Slat Control System
  > LOSS OF HYDRAULICS DURING CLIMB, HAPPENED ABOUT WHEN GEAR UPLATCH CHECK WAS ACCOMPLISHED. DURING HYDRAULIC PRESSURE CHECK (TERMINAL AREA) HYDRAULIC QUANTITY DECREASED. FOUND SLOT CONTROL VALVE SEALS LEAKING. REPACKED VALVE. SERVICED HYDRAULIC SYSTEM. SYST
- [SDR ABXA010225](https://openairdocs.org/sdr/ABXA010225.md): Seal · damaged · May 13, 2001 · N849AX · Doug DC861 · Cargo/Baggage Doors
  > AN EXTREMELY LOUD NOISE WAS NOTED IN THE MAIN CARGO COMPARTMENT AROUND THE MAIN CARGO DOOR. THE CREW REPORTED HEARING A THUMP AND PRESSURIZATION INCREASED TO 1000 FPM RATE OF CLIMB. PRESSURIZATION COULD NOT BE CONTROLLED MANUALY AT FL21. THE CREW DONNED O2
- [SDR ABXA010123](https://openairdocs.org/sdr/ABXA010123.md): Rod · broken · Apr 7, 2001 · N849AX · Doug DC861 · Landing Gear Door Retract Section
  > THE RIGHT MAIN LANDING GEAR FLYING DOOR CONNECTING ROD WAS BROKEN. MAINTENANCE INSPECTED AND REPLACED THE RIGHT MAIN LANDING GEAR FLYING DOOR CONNECTING ROD, IAW DC-8 MM 32-12-01.
- [SDR ABXA000333](https://openairdocs.org/sdr/ABXA000333.md): Door · out of adj · Jul 16, 2000 · N849AX · Doug DC861 · Landing Gear Door Retract Section
  > ON GEAR RETRACTION RED LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH RIGHT MAIN GEAR DOOR NOT LATCHED LIGHT ON. ACCOMPLISHED GEAR RECYCLE AND LOWERED FLAPS. LIGHTEXTINGUISHED. RERIGGED RIGHT MAIN LANDING GEAR DOOR FOLLOW-UP MECHANISM IAW DC8 MM. OPSCHECK
- [SDR ABXA000332](https://openairdocs.org/sdr/ABXA000332.md): Actuator · out of adj · Jul 14, 2000 · N849AX · Doug DC861 · Landing Gear Door Actuator
  > ON GEAR RETRACTION, GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RIGHT MAIN DOOR INDICATED NOT LATCHED. RECYCLED GEAR, NO HELP. ADJUSTED RIGHT MAIN GEAR DOOR FOLLOW-UP MECHANISM IAW DC8 MM 32-31-05.
- [SDR ABXA000190](https://openairdocs.org/sdr/ABXA000190.md): Window · lack of lube · Apr 12, 2000 · N849AX · Doug DC861 · Flight Compartment Windows
  > CAPTAIN''S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. INSPECTED AND LUBRICATEDWINDOW MECHANISM. OPS CHECKED GOOD.
- [SDR ABXA000018](https://openairdocs.org/sdr/ABXA000018.md): Window · sticking · Jan 19, 2000 · N849AX · Doug DC861 · Flight Compartment Windows
  > DURING PREFLIGHT, CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN INTERMITTENTLY. CLEANED AND LUBRICATED MECHANISM. OPS CHECKED GOOD.
- [SDR ABXA9900865](https://openairdocs.org/sdr/ABXA9900865.md): Window · lack of lube · Dec 28, 1999 · N849AX · Doug DC861 · Flight Compartment Windows
  > CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. LUBRICATED UPPER GUIDE PIN. OPS CHECKED GOOD.
- [SDR ABXA9900107](https://openairdocs.org/sdr/ABXA9900107.md): Controller · defective · Feb 16, 1999 · N849AX · Doug DC861 · Windshield/Door Rain/Ice Removal
  > DURING ENGINE START FOR REPOSITIONING FLIGHT, CREW REPORTED SMELL OF SMOKE IN COCKPIT. REPLACED LEFT AND CENTER WINDSHIELD TEMPERATURE CONTROLLERS. DETERMINED BAD FILTER WAS CAUSING ODOR.
- [SDR ABXA9900010](https://openairdocs.org/sdr/ABXA9900010.md): Switch · damaged · Jan 14, 1999 · N849AX · Doug DC861 · Door Warning System
  > AFTER CLIMB-OUT, AFTER TURNING LAST CTC ON, CARGO DOOR WARNING LIGHT ILLUMINATED. DUMPED 20,000 POUNDS OF FUEL AND RETURNED TO ILN. FOUND LOWER DOOR JAMB SWITCH ARM BENT. REPLACED SWITCH. PRESSURIZED AIRCRAFT. DOOR INDICATION LIGHT, OPS CHECKED GOOD.
- [SDR ABXA9900003](https://openairdocs.org/sdr/ABXA9900003.md): Retract Mech · lack of lube · Jan 4, 1999 · N849AX · Doug DC861 · Landing Gear Retraction/Extension System
  > ON GEAR RETRACTION, GEAR HANDLE APPEARED TO BE HITTING STOP. RECYCLED HANDLE TWICE. GEAR CAME UP. LUBRICATED LANDING GEAR HANDLE LINKAGE. INSPECTED HANDLE AND CONTROL VALVE. NO DEFECTS NOTED. OPS CHECKED GOOD.
- [SDR ABXA9800889](https://openairdocs.org/sdr/ABXA9800889.md): Window · lack of lube · Oct 9, 1998 · N849AX · Doug DC861 · Flight Compartment Windows
  > CAPTAIN'S SLIDING WINDOW (EMERG EXIT) VERY DIFFICULT TO OPEN. CLEANED AND LUBRICATED MECHANISM, OPS CHECKED GOOD.
- [SDR ABXA9800714](https://openairdocs.org/sdr/ABXA9800714.md): Fitting · cracked · Jul 12, 1998 · N849AX · Doug DC861F · Fuselage Miscellaneous Structure
  > STATION 980-1000 STRINGER 22R END FITTING WAS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-8 AND DWG 37532351.
- [SDR ABXA9800670](https://openairdocs.org/sdr/ABXA9800670.md): Strap · cracked · Jun 27, 1998 · N849AX · Doug DC861F · Wing Miscellaneous Structure
  > RIGHT WING LEADING EDGE AT STATION XFS 610.000, UPPER RIB TRAILING EDGE STRAP IS CRACKED. REPLACED STRAP IAW DWG 5655441 AND DC8 SRM 51-1-21A.
- [SDR ABXA9800712](https://openairdocs.org/sdr/ABXA9800712.md): Angle · cracked · Jun 26, 1998 · N849AX · Doug DC861F · Fuselage Miscellaneous Structure
  > 680 BULKHEAD UPPER ATTACH FITTING TO FLOOR BOARD FRAME CRACKED AT RBL24. REPLACED FLOOR SUPPORT ANGLE IAW DWG 4645517 AND DC8 SRM 51-1-20D.
- [SDR ABXA9800669](https://openairdocs.org/sdr/ABXA9800669.md): Web · corrosion · Jun 24, 1998 · N849AX · Doug DC861F · Fuselage Miscellaneous Structure
  > HEAVY CORROSION ON TORQUE BOX WEB AT STATION 1210-1250. REPAIRED WEB IAW DWG 9754945, DC8 SRM 53-2-0 AND 51-1-21.
- [SDR ABXA9800717](https://openairdocs.org/sdr/ABXA9800717.md): Rib · cracked · Jun 23, 1998 · N849AX · Doug DC861F · Wing, Rib/Bulkhead
  > LEFT WING LEADING EDGE LOWER RIB ARM CRACKED BY AFT FASTENER AT STATION XFS 816.250. REPAIRED IAW DC8 SRM 57-2-0 AND 51-1-21.
- [SDR ABXA9800716](https://openairdocs.org/sdr/ABXA9800716.md): Angle · cracked · Jun 23, 1998 · N849AX · Doug DC861F · Wing Miscellaneous Structure
  > RIGHT WING LEADING EDGE AT STATION XFS 766.250, THE INTERNAL DOUBLER ANGLE FORWARD OF ACCESS HOLE HAS A 5 CRACK. REPAIRED IAW DC8 SRM 51-1-8 AND 51-1-20D.
- [SDR ABXA9800703](https://openairdocs.org/sdr/ABXA9800703.md): Rib · cracked · Jun 23, 1998 · N849AX · Doug DC861F · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE AT STATION XOLDI 6.225, UPPER LEADING EDGE RIB HAS A 4 CRACK. REPAIRED IAW DC8 SRM 51-1-20D AND 51-1-21.
- [SDR ABXA9800702](https://openairdocs.org/sdr/ABXA9800702.md): Fitting · cracked · Jun 23, 1998 · N849AX · Doug DC861F · Fuselage Miscellaneous Structure
  > FLOORBOARD ATTACH ANGLE CRACKED AT STATION 1140, RBL 55. REPAIRED IAW ABX REA NR D853-22888 AND DC8 SRM 51-3-0.
- [SDR ABXA9800706](https://openairdocs.org/sdr/ABXA9800706.md): Fitting · cracked · Jun 21, 1998 · N849AX · Doug DC861F · Fuselage Miscellaneous Structure
  > SPLICE FITTING CRACKED AT STATION 1300 - 1320 STRINGER 31L. REPLACED FITTING IAW DC8 SRM 51-1-20D.
- [SDR ABXA9800705](https://openairdocs.org/sdr/ABXA9800705.md): Web · cracked · Jun 21, 1998 · N849AX · Doug DC861F · Fuselage Miscellaneous Structure
  > LEFT WHEEL WELL AFT TORQUE BOX WEB CRACKED. REPAIRED IAW DC8 SRM 53-2-0, 51-1-8 AND 51-1-21.
- [SDR ABXA9800704](https://openairdocs.org/sdr/ABXA9800704.md): Fitting · cracked · Jun 21, 1998 · N849AX · Doug DC861F · Fuselage Miscellaneous Structure
  > LEFT LOWER FRAME TO CUSP FITTING CRACKED AT STATION 1070. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 9755584.

Next page: https://openairdocs.org/deregistered/N849AX-2005-03-04/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 = 'N849AX' AND deregistration_id = 'N849AX-2005-03-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N849AX-2005-03-04/reports

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