# Service difficulty reports: N970AX, cancelled Nov 18, 2009

A list on [N970AX, cancelled Nov 18, 2009](https://openairdocs.org/deregistered/N970AX-2009-11-18.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 · 60 reports

- [SDR ABXA080239](https://openairdocs.org/sdr/ABXA080239.md): Power Supply · defective · Sep 9, 2008 · N970AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW DC9 MM CHAPTER 33.
- [SDR ABXA070204](https://openairdocs.org/sdr/ABXA070204.md): Engine · failed · Jun 24, 2007 · N970AX · Doug DC941 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE, 1ST STAGE TURBINE HAD SEVERAL BLADES WITH CRACKED LEADING EDGE TIPS. ALSO SEVERAL BLADES HAD MOLTEN METAL ON TIPS. OUT OF SERVICABLE LIMITS IAW JT8D MM 72-50-00-210-002. REMOVED AND REPLACED NR 1 ENGINE IAW DC9 MM ON JOB CARD 9090010.
- [SDR ABXA070182](https://openairdocs.org/sdr/ABXA070182.md): Charger · defective · Jun 13, 2007 · N970AX · Doug DC941 · Battery/Charger System
  > WHILE STARTING APU, NOTICED NOISE AND SMOKE EMITTING FROM BATTERY CHARGER. REPLACED BATTERY CHARGER IAW DC9 MM 24-30-02-2-0001. ALSO, REPLACED BOTH AIRCRAFT BATTERIES AND BATTERY TEMPERATURE SENSOR IAW DC9 MM 24-30-01-0-0001.
- [SDR ABXA070011](https://openairdocs.org/sdr/ABXA070011.md): Seat Track · corroded · Jan 3, 2007 · N970AX · Doug DC941 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR TRACK CORRODED AT STA 224 - 232, RIGHT BUTT LINE 54. REMOVED AND REPLACED TRACK IAW DC9 SRM 51-30-1.
- [SDR ABXA070010](https://openairdocs.org/sdr/ABXA070010.md): Bulkhead · cracked · Jan 2, 2007 · N970AX · Doug DC941 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD LEFT LOWER CORNER WAS CRACKED. REPAIRED AREA IAW DC9 REA D953-55282MR.
- [SDR ABXA070009](https://openairdocs.org/sdr/ABXA070009.md): Skin · cracked · Dec 28, 2006 · N970AX · Doug DC941 · Passenger/Crew Doors
  > LEFT MAIN ENTRY DOOR CORNER CRACKED ON INTERIOR WEB CUTOUT. REPAIRED MAIN ENTRY DOOR INNER SKIN/WEB IAW DC9 SRM 52-42-0 AND 52-01.
- [SDR ABXA070005](https://openairdocs.org/sdr/ABXA070005.md): Fitting · cracked · Dec 28, 2006 · N970AX · Doug DC941 · Horizontal Stabilizer, Spar/Rib
  > HORIZONTAL STABILIZER REAR SPAR FITTING WAS CRACKED AT SCREW HOLES FOR P/N: 5910405-3 COVER PLATE. REMOVED AND REPLACED REAR SPAR FITTING IAW DC9 SRM 51-30-1.
- [SDR ABXA070004](https://openairdocs.org/sdr/ABXA070004.md): Skin · damaged · Dec 27, 2006 · N970AX · Doug DC941 · Elevator, Plate/Skin
  > RIGHT ELEVATOR UPPER SKIN HAD HEAVY STATIC DISCHARGE DAMAGE 3 FEET FROM TIP. REPAIRED AREA IAW DC9 SRM 51-70-6.
- [SDR ABXA050021](https://openairdocs.org/sdr/ABXA050021.md): Pan · corroded · Jan 7, 2005 · N970AX · Doug DC941 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO DOOR CUTOUT LOWER PAN CORRODED AND FORWARD LOWER CORNER OF PAN BULGED WITH 3 RIVETS THROUGH THE SKIN POPPED. REMOVED DOOR PAN / SCUFF PLATE / WEB. REMOVED AND REPLACED -45 DOUBLER. CLEANED CORROSION ON DOOR PAN AND RE-INSTALLED DOOR PAN / WE
- [SDR ABXA050020](https://openairdocs.org/sdr/ABXA050020.md): Pan · cracked · Jan 6, 2005 · N970AX · Doug DC941 · Cargo/Baggage Doors
  > CRACK IN RADIUS OF INNER PAN AT AFT LATCH CAM. REPAIRED CRACKED PAN IAW DC-9 SRM 52-05.
- [SDR ABXA050019](https://openairdocs.org/sdr/ABXA050019.md): Frame · cracked · Jan 6, 2005 · N970AX · Doug DC941 · Fuselage Main, Frame
  > FRAME CRACKED AT LONGERON 13 RIGHT, STA 1152. REPAIRED FRAME IAW DC-9 SRM 53-03 AND 51-30-5.
- [SDR ABXA050018](https://openairdocs.org/sdr/ABXA050018.md): Frame · cracked · Jan 6, 2005 · N970AX · Doug DC941 · Fuselage Main, Frame
  > FORWARD OVER WHEEL WELL FRAME RIGHT SIDE, REQUIRED REPLACEMENT PER JC NEA 53400100-002-40, FRAME CRACKED FORWARD AND AFT FLANGE. REMOVED AND RE-INSTALLED NEW FRAME AT STA 737 IAW EA 53400 322-001-3.
- [SDR ABXA050017](https://openairdocs.org/sdr/ABXA050017.md): Fitting · cracked · Jan 6, 2005 · N970AX · Doug DC941 · Cargo/Baggage Doors
  > UPPER AFT STOP TEE FITTING CRACKED FORWARD LOWER CARGO DOOR. REPLACED FITTING IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-4.
- [SDR ABXA050016](https://openairdocs.org/sdr/ABXA050016.md): Support · damaged · Jan 5, 2005 · N970AX · Doug DC941 · Horizontal Stabilizer Structure
  > HORIZONTAL STAB JACKSCREW HAD DAMAGED THREAD NEAR THE SELF-LOCKING LOWER STOP NUT. REPLACED JACKSCREW IAW DC-9 MM.
- [SDR ABXA040355](https://openairdocs.org/sdr/ABXA040355.md): Trunnion · corroded · Oct 22, 2004 · N970AX · Doug DC941 · Main Landing Gear
  > BOTH FORWARD TRUNNIONS EARS INNER SURFACES PITTED AND CORRODED ON RIGHT MAIN LANDING GEAR TRUNNION. REPAIRED AREA IAW REA D932-50887MR.
- [SDR ABXA040353](https://openairdocs.org/sdr/ABXA040353.md): Attach Fitting · corroded · Oct 22, 2004 · N970AX · Doug DC941 · Wing, Landing Gear Attach Fittings
  > DURING ROUTINE GEAR CHANGE, FOUND CORROSION BEYOND LIMITS ON THE RIGHT MAIN LANDING GEAR ATTACH FITTING FORWARD LUG FORWARD FACE AND FORWARD LUG AFT FACE. REPAIRED ATTACH FITTING LUGS BY SPOT FACING AND INSTALLING WASHERS TO REGAIN BLUE PRINT DIMENSIONS IAW R
- [SDR ABXA040052](https://openairdocs.org/sdr/ABXA040052.md): Wire · shorted · Jan 29, 2004 · N970AX · Doug DC941 · Landing Gear System Wiring
  > LEFT GEAR DOWNLOCK WIRE 16230E20 WAS SHORTED BETWEEN 53-65 AND P3-9100. ALSO FOUND WIRING CONDUIT CUT THROUGH IN OUTBOARD LEFT WHEEL WELL. REPAIRED ALL DAMAGED WIRES AND CONDUIT IN THE LEFT WHEEL WELL.
- [SDR ABXA030214](https://openairdocs.org/sdr/ABXA030214.md): Frame · corroded · May 28, 2003 · N970AX · Doug DC941 · Fuselage Main, Frame
  > FRAME FS 446 WAS CORRODED LONGERON 29 LEFT TO LONGERON 29 RIGHT. REPAIRED FRAME IAW DC-9 SRM 53-03.
- [SDR ABXA030213](https://openairdocs.org/sdr/ABXA030213.md): Web · cracked · May 28, 2003 · N970AX · Doug DC941 · Fuselage Miscellaneous Structure
  > RIGHT CUSP WEB JUST FORWARD OF FS 1041 CRACKED. REPAIRED CRACK IN CUSP IAW DC-9 SRM 53-01.
- [SDR ABXA030212](https://openairdocs.org/sdr/ABXA030212.md): Fitting · corroded · May 28, 2003 · N970AX · Doug DC941 · Fuselage Miscellaneous Structure
  > CABIN FLOORBEAM END FITTINGS FS 973, RIGHT BUTTLINE 58, LEVEL I CORROSION. REPLACED FLOORBEAM END FITTINGS IAW DC-9 SRM.
- [SDR ABXA030215](https://openairdocs.org/sdr/ABXA030215.md): Attach Angle · cracked · May 28, 2003 · N970AX · Doug DC941 · Nacelle/Pylon, Attach Fittings
  > NR 2 ENGINE LOWER PYLON ATTACH ANGLE WAS CRACKED AT STA 1030. REPLACED ATTACH ANGLE IAW DC-9 SRM 51-30-1.
- [SDR ABXA030211](https://openairdocs.org/sdr/ABXA030211.md): Seat Track · corroded · May 27, 2003 · N970AX · Doug DC941 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BUTT LINE '0' WAS CORRODED, FS 541 TO FS 619. REPAIRED SEAT TRACK, BUTTLINE '0', FROM STA 160 TO STA 645 IAW DC-9 SRM.
- [SDR ABXA030210](https://openairdocs.org/sdr/ABXA030210.md): Skin · cracked · May 25, 2003 · N970AX · Doug DC941 · Fuselage Main, Plate/Skin
  > FOSELAGE SKIN AT UPPER AFT MAIN ENTRY DOOR STOP CRACKED. REPAIRED AREA IAW DC-9 SRM 53-05.
- [SDR ABXA030209](https://openairdocs.org/sdr/ABXA030209.md): Skin · cracked · May 24, 2003 · N970AX · Doug DC941 · Cargo/Baggage Doors
  > FORWARD LOWER CARGO DOOR EXTERIOR SKIN CRACKED ON LEADING EDGE. BLENDED CRACK IAW DC-9 SRM 52-01 AND REA D952-47410.
- [SDR ABXA030141](https://openairdocs.org/sdr/ABXA030141.md): Computer · malfunctioned · May 6, 2003 · N970AX · Doug DC941 · Autopilot Computer
  > WITH AUTOPILOT ON DURING TURNS, THERE WAS EXTREME AND EXCESSIVE UNCOMMANDED ELEVATOR INPUTS. VERIFIED. RERACKED PITCH AND ROLL COMPUTERS. VERSINE LIFT CHECKED GOOD IAW DC-9 AMM CHAPTER 22.
- [SDR ABXA020280](https://openairdocs.org/sdr/ABXA020280.md): Link · cracked · Nov 2, 2002 · N970AX · Doug DC941 · Engine Thrust Reverser
  > WHILE COMPLYING WITH AD 96-10-11, FOUND CRACK INDICATION ON UPPER LEFT THRUST REVERSER DRIVER LINK. INSTALLED SERVICEABLE DRIVER LINK IAW DC-9 MM 78-31-05-2-0001.
- [SDR ABXA010537](https://openairdocs.org/sdr/ABXA010537.md): Longeron · cracked · Oct 3, 2001 · N970AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > LONGERON 17 RIGHT WAS CRACKED AT FASTENERS AT FS 389. REPLACED LONGERON AT STATION 380 - 430, IAW DC-9 SRM 5302.
- [SDR ABXA000404](https://openairdocs.org/sdr/ABXA000404.md): Battery Pack · discharged · Aug 31, 2000 · N970AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT TEST ON. REPLACED EMERGENCY BATTERY POWER SUPPLY.
- [SDR ABXA000105](https://openairdocs.org/sdr/ABXA000105.md): Frame · cracked · Feb 11, 2000 · N970AX · Doug DC941 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND MAIN FRAME CRACKED AT STA 756 RIGHT. REPLACED MAIN FRAME IAW DC9 SRM 51-30-1, 51-30-2, AND 51-30-5.
- [SDR ABXA000074](https://openairdocs.org/sdr/ABXA000074.md): Arm · bent · Jan 24, 2000 · N970AX · Doug DC941 · Landing Gear Door Retract Section
  > ON GEAR RETRACTION, RIGHT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ON. RECYCLED GEAR, SAME INDICATIONS. FOUND MLG INBOARD DOOR SEQUENCE ARM BROKEN, TORQUE TUBE SHEAR RIVETS SHEARED AND LINK BENT. REPLACED ARM, TORQUE TUBE AT LINK. RETRACTION AND
- [SDR ABXA9800517](https://openairdocs.org/sdr/ABXA9800517.md): Frame · cracked · Jun 8, 1998 · N970AX · Doug DC941 · Fuselage Main, Frame
  > DURING C-CHECK, FUSELAGE FRAME AT STATION 677 WAS FOUND CRACKED AT LONGERON 19R. REPLACED FRAME IAW DC9 SRM 51-30-2.
- [SDR ABXA9800516](https://openairdocs.org/sdr/ABXA9800516.md): Pan · cracked · Jun 4, 1998 · N970AX · Doug DC941 · Passenger/Crew Doors
  > DURING C-CHECK, THE FORWARD ENTRY DOOR PAN WAS FOUND CRACKED IN SEVERAL PLACES. REPLACED IAW DC9 SRM 51-30-8 AND REA D952-23898.
- [SDR ABXA9800518](https://openairdocs.org/sdr/ABXA9800518.md): Shear Tie · cracked · Jun 2, 1998 · N970AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, A SHEAR-TIE WAS FOUND CRACKED AT STATION 1021 LONGERON 15 AND 16 R. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2.
- [SDR ABXA9800515](https://openairdocs.org/sdr/ABXA9800515.md): Doubler · cracked · Jun 2, 1998 · N970AX · Doug DC941 · Cargo/Baggage Doors
  > DURING C-CHECK, THE AFT LOWER CARGO DOOR INTERNAL DOUBLER WAS FOUND CRACKED. REPAIRED IAW DC9 SRM 51-30-2.
- [SDR ABXA9800514](https://openairdocs.org/sdr/ABXA9800514.md): Longeron · cracked · Jun 2, 1998 · N970AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, LONGERON 17 LEFT WAS FOUND CRACKED AT STATION 408, 389, 294, 275 AND 256. REPLACED LONGERON IAW DC9 SRM 51-30-2.
- [SDR ABXA9800483](https://openairdocs.org/sdr/ABXA9800483.md): Angle · cracked · Jun 2, 1998 · N970AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND INTERCOSTAL FORWARD SUPPORT ANGLE CRACKED AT STATION 218 AND BL 0.0. REPLACED ANGLE IAW DC9 SRM 51-10-2A AND DRAWING 9958171.
- [SDR ABXA9800482](https://openairdocs.org/sdr/ABXA9800482.md): Shear Tie · cracked · Jun 2, 1998 · N970AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND SHEAR TIE CRACKED AT STATION 256 AND LONGERON 17R. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2 AND 51-30-1.
- [SDR ABXA9800481](https://openairdocs.org/sdr/ABXA9800481.md): Longeron · cracked · Jun 2, 1998 · N970AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LONGERON 17R CRACKED AT STATION 256 AND 275. REPAIRED LONGERON IAW DC9 SRM 53-00.
- [SDR ABXA9800519](https://openairdocs.org/sdr/ABXA9800519.md): Skin · cracked · Jun 1, 1998 · N970AX · Doug DC941 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, THE FUSELAGE SKIN WAS FOUND CRACKED AT STATION 427 LONGERON 26 R. REPAIRED IAW REA D953-23873-MR.
- [SDR ABXA9800475](https://openairdocs.org/sdr/ABXA9800475.md): Longeron · cracked · May 31, 1998 · N970AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LONGERON 16L CRACKED AT STATION 237. REPAIRED LONGERON IAW DC9 SRM 53-02.
- [SDR ABXA9700323](https://openairdocs.org/sdr/ABXA9700323.md): Bulkhead Web · damaged · Nov 4, 1996 · N970AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING C-CHECK, THE AFT PRESSURE BULKHEAD WEB WAS FOUND DAMAGED AT LONGERON 271LT. REPAIRED IAW REA D953-17185-MR.
- [SDR ABXA9700322](https://openairdocs.org/sdr/ABXA9700322.md): Driver Link · cracked · Nov 4, 1996 · N970AX · Doug DC941 · Engine Thrust Reverser
  > DURING C-CHECK, THE RT ENGINE THRUST REVERSER UPPER OUTBOARD DRIVER LINK WAS FOUND CRACKED. REPLACED DRIVER LINK IAW DC-9 M.M. 78-31-5.
- [SDR ABXA9700321](https://openairdocs.org/sdr/ABXA9700321.md): Angle · cracked · Nov 4, 1996 · N970AX · Doug DC941 · Nacelle/Pylon Structure
  > DURING C-CHECK, THE RT PYLON LOWER ATTACH ANGLE WAS FOUND CRACKED AT STA 1056. REPAIRED IAW DC-9 SRM 54-04.
- [SDR ABXA9700320](https://openairdocs.org/sdr/ABXA9700320.md): Bulkhead · cracked · Nov 4, 1996 · N970AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING C-CHECK, THE BULKHEAD AT STA 1041 WAS FOUND CRACKED ON THE RT SIDE AT ENGINE MOUNT SPAR. REPAIRED IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.
- [SDR ABXA9700319](https://openairdocs.org/sdr/ABXA9700319.md): Bulkhead · cracked · Nov 4, 1996 · N970AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING C-CHECK, THE BULKHEAD AT STA 1072 WAS FOUND CRACKED ON THE RT SIDE OF THE DOOR JAMB 24 FROM FLOOR. REPAIRED IAW REA D953-17165MR.
- [SDR ABXA9700318](https://openairdocs.org/sdr/ABXA9700318.md): Bulkhead · cracked · Nov 4, 1996 · N970AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING C-CHECK, THE BULKHEAD AT STA 76 WAS FOUND CRACKED NEXT TO RT CUSP. REPAIRED IAW REA D953-17160.
- [SDR ABXA9700317](https://openairdocs.org/sdr/ABXA9700317.md): Frame · cracked · Nov 4, 1996 · N970AX · Doug DC941 · Fuselage Main, Frame
  > DURING C-CHECK, THE STA 1185 FRAME WAS FOUND CRACKED AT LONGERON 3 RT. REPAIRED IAW SSRM DWG NR K05159.
- [SDR ABXA9700316](https://openairdocs.org/sdr/ABXA9700316.md): Frame · cracked · Nov 4, 1996 · N970AX · Doug DC941 · Fuselage Main, Frame
  > DURING C-CHECK, THE STA 1185 FRAME WAS FOUND CRACKED AT LONGERON 6RT. REPAIRED IAW SRM DWG NR K051-59.
- [SDR ABXA9700315](https://openairdocs.org/sdr/ABXA9700315.md): Frame · cracked · Nov 4, 1996 · N970AX · Doug DC941 · Fuselage Main, Frame
  > DURING C-CHECK, THE STA 1231 FRAME WAS FOUND CRACKED AT LONGERON 2 RT. REPAIRED IAW DC-9 SRM 51-10-2 AND 51-10-5.
- [SDR ABXA9700314](https://openairdocs.org/sdr/ABXA9700314.md): Tee Cap · corroded · Nov 4, 1996 · N970AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, THE STA 110 TEE CAP WAS FOUND CORRODED AT LONGERON 25RT. REPAIRED IAW REA D953-17189.

Next page: https://openairdocs.org/deregistered/N970AX-2009-11-18/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 = 'N970AX' AND deregistration_id = 'N970AX-2009-11-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N970AX-2009-11-18/reports

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