# Service difficulty reports: N976AX, cancelled Feb 12, 2018

A list on [N976AX, cancelled Feb 12, 2018](https://openairdocs.org/deregistered/N976AX-2018-02-12.md).

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

- [SDR ABXA080089](https://openairdocs.org/sdr/ABXA080089.md): Skin · corroded · Mar 7, 2008 · N976AX · Doug DC941 · Fuselage Main, Plate/Skin
  > DURING LINE MAINTENANCE, FOUND CORROSION OF FUSELAGE SKIN AROUND THE LEFT STATIC PORT PLATE. REMOVED LEFT STATIC PORT PLATE, FOUND FUSELAGE SKIN UNDER THE PLATE CORRODED BEYOND LIMITS. REPAIRED SKIN IAW DC9 SRM 53-04, FIGURE 31, SHEET 1.
- [SDR ABXA080012](https://openairdocs.org/sdr/ABXA080012.md): Rib · cracked · Dec 15, 2007 · N976AX · Doug DC941 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB WAS CRACKED BETWEEN TWO FASTENERS. LOCATED JUST INBOARD OF THE NR 5 SLAT TRACK. REPAIRED RIGHT WING LEADING EDGE RIB JUST INBOARD OF NR 5 SLAT TRACK IAW REA D957-56780.
- [SDR ABXA080013](https://openairdocs.org/sdr/ABXA080013.md): Intercostal · cracked · Dec 15, 2007 · N976AX · Doug DC941 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO FLOOR SUPPORT ATTACH BRACKET CRACKED AT FS 1056, RIGHT UNDER TRACK AT 28 RIGHT. REPLACED INTERCOSTAL AND BRACKET AT STA 1056 RIGHT IAW DC9 SRM.
- [SDR ABXA080011](https://openairdocs.org/sdr/ABXA080011.md): Attach Angle · cracked · Dec 13, 2007 · N976AX · Doug DC941 · Fuselage Miscellaneous Structure
  > ATTACH ANGLE CRACKED AT APPROXIMATELY STA 775 OUTBOARD SIDE OF WHEEL WELL. APPROXIMATELY 18" AFT OF WHEEL WELL MAIN FRAME. REPLACED ANGLE IAW DC9 SRM 51-30-5 AND DOUGLAS DWG 9923435 PART -12.
- [SDR ABXA070371](https://openairdocs.org/sdr/ABXA070371.md): Window Frame · cracked · Oct 19, 2007 · N976AX · Doug DC941 · Fuselage Main, Structure
  > DURING COCKPIT WINDSHIELD FRAME MOD, FOUND FRAME 9911505-7 CRACKED AT BOTH ENDS. REPAIRED FRAME IAW DC9 SRM 53-03, FIGURE 34.
- [SDR ABXA070370](https://openairdocs.org/sdr/ABXA070370.md): Window Frame · cracked · Oct 19, 2007 · N976AX · Doug DC941 · Fuselage Main, Structure
  > DURING COCKPIT WINDSHIELD FRAME MOD, FOUND FRAME 9911505-6 CRACKED AT INBOARD END. REPAIRED FRAME IAW DC9 SRM 53-03, FIGURE 34.
- [SDR ABXA070369](https://openairdocs.org/sdr/ABXA070369.md): Window Frame · cracked · Oct 19, 2007 · N976AX · Doug DC941 · Fuselage Main, Structure
  > DURING COCKPIT WINDSHIELD FRAME MOD, FOUND FRAME 9911505-5 CRACKED AT INBOARD END. REPAIRED FRAME IAW DC9 SRM 53-03, FIGURE 34.
- [SDR ABXA070373](https://openairdocs.org/sdr/ABXA070373.md): Angle · cracked · Oct 19, 2007 · N976AX · Doug DC941 · Fuselage Main, Structure
  > DURING COCKPIT WINDSHIELD FRAME MOD, FOUND ANGLE AT INBOARD TIP OF FRAME CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA070372](https://openairdocs.org/sdr/ABXA070372.md): Angle · cracked · Oct 19, 2007 · N976AX · Doug DC941 · Fuselage Main, Structure
  > DURING COCKPIT WINDSHIELD FRAME MOD, FOUND ANGLE CRACKED IN RADIUS. REPLACED ANGLE IAW DC9 SRM 51-30-2.
- [SDR ABXA070343](https://openairdocs.org/sdr/ABXA070343.md): Power Supply · defective · Oct 12, 2007 · N976AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTING IN COCKPIT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC9 MM 33-53-00-5.
- [SDR ABXA070323](https://openairdocs.org/sdr/ABXA070323.md): Power Supply · discharged · Sep 24, 2007 · N976AX · Doug DC941 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC9 MM 33-53-02-4.
- [SDR ABXA060290](https://openairdocs.org/sdr/ABXA060290.md): Battery · discharged · Nov 6, 2006 · N976AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES IAW DC9 MM 33-53-00-00.
- [SDR ABXA060050](https://openairdocs.org/sdr/ABXA060050.md): Shear Tie · cracked · Jan 4, 2006 · N976AX · Doug DC941 · Fuselage Internal Mounting Structure
  > SHEAR TIE REPAIR CRACKED FS 1021 AT LONGERON 15 LEFT. REPLACED SHEAR TIE IAW DOUGLAS DWG 5911427 AND SRM 51-30-5.
- [SDR ABXA060049](https://openairdocs.org/sdr/ABXA060049.md): Longeron · cracked · Jan 4, 2006 · N976AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > LONGERON 17 RIGHT CRACKED AT FS 1056. REPLACED LONGERON SECTION AS REQUIRED IAW DC9 SRM LONGERON SPLICE REPAIR 53-02.
- [SDR ABXA060048](https://openairdocs.org/sdr/ABXA060048.md): Pan · cracked · Jan 4, 2006 · N976AX · Doug DC941 · Emergency Exits
  > RIGHT AFT OVERWING EMERGENCY EXIT DOOR PAN CRACKED AT FORWARD LOWER STOP. STOP DRILLED CRACK. INSTALLED DOOR PAN REPAIR IAW DC9 SRM K07390.
- [SDR ABXA060047](https://openairdocs.org/sdr/ABXA060047.md): Fitting · cracked · Jan 3, 2006 · N976AX · Doug DC941 · Fuselage Main, Attach Fittings
  > FORWARD UPPER FITTING ON LEFT KANTED KEEL WEB BULKHEAD WAS CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXA040191](https://openairdocs.org/sdr/ABXA040191.md): Fitting · cracked · May 21, 2004 · N976AX · Doug DC941 · Spoilers
  > LEFT INBOARD SPOILER TORSION BAR CAM OUTBOARD SUPPORT FITTING CRACKED AT TOP END. REPLACED FITTING IAW DC-9 SRM.
- [SDR ABXA040190](https://openairdocs.org/sdr/ABXA040190.md): Bulkhead · cracked · May 14, 2004 · N976AX · Doug DC941 · Fuselage Main, Bulkhead
  > NR 2 TEE CAP WAS FOUND TO BE CRACKED AT OUTBOARD END OF RADIAL Z34. REPLACED NR 2 TEE CAP IAW EA 53120033.
- [SDR ABXA040186](https://openairdocs.org/sdr/ABXA040186.md): Rib · cracked · May 13, 2004 · N976AX · Doug DC941 · Vertical Stabilizer, Spar/Rib
  > REMOVEABLE VERTICAL LEADING EDGE SECTION 5TH RIB UPON RIGHT SIDE CRACKED AT AFT END. REPAIRED RIB IAW DC-9 SSRM K05159.
- [SDR ABXA040189](https://openairdocs.org/sdr/ABXA040189.md): Frame · corroded · May 13, 2004 · N976AX · Doug DC941 · Fuselage Main, Frame
  > CORROSION ON FRAME LOWER LEG AT STA 446, LONGERON 30. REPAIRED IAW DC-9 SRM 53-03.
- [SDR ABXA040188](https://openairdocs.org/sdr/ABXA040188.md): Frame · corroded · May 13, 2004 · N976AX · Doug DC941 · Fuselage Main, Frame
  > CORROSION ON FRAME LOWER LEG AT LONGERON 30, STA 408. REPAIRED FRAME IAW DC-9 SRM 53-03.
- [SDR ABXA040185](https://openairdocs.org/sdr/ABXA040185.md): Rib · cracked · May 13, 2004 · N976AX · Doug DC941 · Vertical Stabilizer, Spar/Rib
  > REMOVEABLE VERTICAL LEADING EDGE SECTION 6TH RIB UP ON RIGHT SIDE CRACKED AT AFT END. REPAIRED RIB IAW DC-9 SSRM K05159.
- [SDR ABXA040187](https://openairdocs.org/sdr/ABXA040187.md): Rib · cracked · May 13, 2004 · N976AX · Doug DC941 · Vertical Stabilizer, Spar/Rib
  > 2ND RIB DOWN FROM REMOVEABLE VERTICAL LEADING EDGE SECTION CRACKED ON RIGHT AFT SIDE. REPAIRED IAW ABX SSRM K05159 DRAWING.
- [SDR ABXA020265](https://openairdocs.org/sdr/ABXA020265.md): Door Frame · cracked · Oct 9, 2002 · N976AX · Doug DC941 · Fuselage Main, Structure
  > CRACKED IN BEND RADIUS AT LEFT UPPER VENTRAL DOOR CORNER. CRACK LENGTH APPROXIMATELY 1.25 INCH IN LENGTH. REPAIRED CRACK IAW DC-9 SRM 51-10-02.
- [SDR ABXA020264](https://openairdocs.org/sdr/ABXA020264.md): Panel · cracked · Oct 9, 2002 · N976AX · Doug DC941 · Fuselage Main, Bulkhead
  > NOSE WHEEL WELL UPPER PRESSURE PANEL HAD CRACK AT STA. 110 RIGHT TUNNEL, APPROXIMATELY 14 INCHES INBOARD. REPAIRED PANEL IAW DC-9 SRM 51-30-2, 51-30-1 AND 51-30-5.
- [SDR ABXA020263](https://openairdocs.org/sdr/ABXA020263.md): Panel · cracked · Oct 9, 2002 · N976AX · Doug DC941 · Fuselage Main, Bulkhead
  > NOSE WHEEL WELL UPPER PRESSURE PANEL HAD CRACK AT STA. 110 LEFT TUNNEL, APPROXIMATELY 24 INCHES INBOARD. REPAIRED PANEL IAW DC-9 SRM 53-01, 51-30-2, 51-30-1 AND 51-30-5.
- [SDR ABXA020262](https://openairdocs.org/sdr/ABXA020262.md): Panel · cracked · Oct 9, 2002 · N976AX · Doug DC941 · Fuselage Main, Bulkhead
  > NOSE WHEEL WELL UPPER PRESSURE PANEL STA. 89 LEFT, APPROXIMATELY 3 INCHES INBOARD, HAD CRACK. REPAIRED CRACK IAW REA D953-45373.
- [SDR ABXA020261](https://openairdocs.org/sdr/ABXA020261.md): Splice · corroded · Oct 8, 2002 · N976AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > LEVEL II CORROSION AT F.S. 1013, LONGERON 27 LEFT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REPLACED FRAME SPLICE IAW DC-9 SRM.
- [SDR ABXA020260](https://openairdocs.org/sdr/ABXA020260.md): Fitting · cracked · Oct 8, 2002 · N976AX · Doug DC941 · Fuselage Structure (General)
  > ANGLE CRACKED AT LONGEON 30 JUST AFT OF FORWARD 'P' DOME, KEEL AREA. REPLACED ANGLE IAW DC-9 SRM 51-30-5.
- [SDR ABXA020259](https://openairdocs.org/sdr/ABXA020259.md): Support · cracked · Oct 8, 2002 · N976AX · Doug DC941 · Wing Structure
  > RIGHT WING OUTBOARD SPOILER TORSION BAR SUPPORT FITTING CRACKED AT UPPER END. REPLACED FITTING IAW DC-9 SRM 51-30-1.
- [SDR ABXA010281](https://openairdocs.org/sdr/ABXA010281.md): Battery · discharged · Jun 2, 2001 · N976AX · Doug DC941 · Emergency Lighting
  > THE EMERGENCY EXIT LIGHTS WERE DIM. REPLACED EMERGENCY LIGHTS BATTERIES AND BATTERY POWER SUPPLY. OPS CHECKED GOOD IAW DC-9 MM 33-53-00.
- [SDR ABXA010209](https://openairdocs.org/sdr/ABXA010209.md): Rod End · broken · Apr 17, 2001 · N976AX · Doug DC941 · Leading Edge Slat Actuator
  > DURING A SERVICE CHECK, MAINTENANCE FOUND THE UPPER LEFT OUTBOARD SLAT ACTUATOR ROD END TO BE BROKEN. DAMAGE WAS ALSO NOTED UNDER THE LEFT INBOARD SLAT AND UPPER WING PANEL 1142A. MAINTENANCE REPLACED THE SLAT ACTUATOR ROD END ASSY IAW DC-9 MM 27-80-05. THE
- [SDR ABXA010054](https://openairdocs.org/sdr/ABXA010054.md): Control Unit · contaminated · Feb 15, 2001 · N976AX · Doug DC941 · Brake Anti-Skid Section
  > THE WHEEL BRAKES FAILED TO OPERATE ON LANDING AT JAN. WHEN ANTI-SKID WAS SELECTED OFF, BRAKES WORKED NORMALLY. MAINTENANCE INSPECTED AND REPLACED THE ANTI-SKID CONTROL UNIT DUE TO WATER INTRUSION IAW DC-9 MM. MAINTENANCE DEFERRED THE ANTI-SKID SYSTEM IAW DC
- [SDR ABXA010026](https://openairdocs.org/sdr/ABXA010026.md): Switch · failed · Jan 31, 2001 · N976AX · Doug DC941 · Landing Gear Position and Warning
  > DURING APPROACH WHEN LANDING GEAR WAS SELECTED DOWN, THE NOSE LANDING GEAR DOWN (GREEN) LIGHT FAILED TO ILLUMINATE. MISSED APPROACH, PROCEDURES WERE COMPLIED. THE CREW REPLACED THE NOSE LANDING GEAR DOWN INDICATOR LIGHT BULBS AND RECYCLED THE LANDING GEAR.
- [SDR ABXA0100026](https://openairdocs.org/sdr/ABXA0100026.md): Proximity Switch · failed · Jan 31, 2001 · N976AX · Doug DC941 · Landing Gear Position and Warning
  > DURING APPROACH WHEN LANDING GEAR WAS SELECTED DOWN, THE NOSE LANDING GEAR DOWN (GREEN) LIGHT FAILED TO ILLUMINATE. MISSED APPROACH PROCEDURES WERE COMPLIED WITH. THE CREW REPLACED THE NOSE LANDING GEAR DOWN INDICATOR LIGHT BULBS AND RECYCLED THE LANDING GEA

## 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 = 'N976AX' AND deregistration_id = 'N976AX-2018-02-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N976AX-2018-02-12/reports

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