# Service difficulty reports: N975AX, cancelled May 22, 2017

A list on [N975AX, cancelled May 22, 2017](https://openairdocs.org/deregistered/N975AX-2017-05-22.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 · 96 reports

- [SDR ABXA080154](https://openairdocs.org/sdr/ABXA080154.md): Battery · discharged · May 24, 2008 · N975AX · Doug DC941 · Emergency Lighting
  > COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00. (A)
- [SDR ABXA070077](https://openairdocs.org/sdr/ABXA070077.md): Skin · cracked · Mar 15, 2007 · N975AX · Doug DC941 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN CRACKED 2 PLACES APPROXIMATELY FS 1197, LEFT SIDE. REPAIRED AREA IAW DC9 SRM 53-01.
- [SDR ABXA070078](https://openairdocs.org/sdr/ABXA070078.md): Frame · cracked · Mar 15, 2007 · N975AX · Doug DC941 · Fuselage Main, Frame
  > FS 1209 CANTED FRAME CRACKED BETWEEN LONGERON 14 AND 15 LEFT SIDE. REPAIRED IAW DC9 SRM 53-01.
- [SDR ABXA070075](https://openairdocs.org/sdr/ABXA070075.md): Bulkhead · corroded · Mar 15, 2007 · N975AX · Doug DC941 · Fuselage Main, Bulkhead
  > AFT LOWER CARGO, AFT BULKHEAD WEB EXFOLIATED AT LEFT BUTT LINE 18 INCHES AT TOP. REPAIRED DAMAGE IAW DC9 SRM 53-01.
- [SDR ABXA070074](https://openairdocs.org/sdr/ABXA070074.md): Bulkhead · corroded · Mar 15, 2007 · N975AX · Doug DC941 · Fuselage Main, Bulkhead
  > AFT LOWER CARGO, AFT BULKHEAD WEB AND ANGLE EXFOLIATED AT RIGHT BUTT LINE 4 INCHES AT BOTTOM SIDE. REPAIRED DAMAGED IAW ABX ENGINEERING TO DUPLICATE PRODUCTION SPLICE IAW DACO DWG 9915561 AND DC9 SRM 51-30-0.
- [SDR ABXA060184](https://openairdocs.org/sdr/ABXA060184.md): Battery · discharged · May 31, 2006 · N975AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES FOR EMERGENCY LIGHTS IAW DC9 AMM 33-51-00. OPS CHECKED GOOD. DEFERRED: DI 50256 - EMERGENCY BATTERY PACK IAW DC9 MM 33-53-008. CLEARED: DI 50256. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK IAW DC9 M
- [SDR ABXA050212](https://openairdocs.org/sdr/ABXA050212.md): Wire · broken · Sep 7, 2005 · N975AX · Doug DC941 · Light System Wiring
  > WHEN CIRCUIT BREAKER FOR CLEARVIEW & EYEBROW WINDOWS WAS PUSHED IN DURING FLIGHT, CONSIDERABLE ARCHING AND SPARKS CAME FROM CAPTAIN'S CLEARVIEW WINDOW BUY THE TERMINAL BLOCK. REPAIRED A BROKEN WIRE AT THE TERMINAL BLOCK AND REPLACED THE TERMINAL BLOCK IAW DC9
- [SDR ABXA050085](https://openairdocs.org/sdr/ABXA050085.md): Seat Track · corroded · Mar 23, 2005 · N975AX · Doug DC941 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO LEFT SIDE BUTT LINE 44 HAD FLOOR PANEL BULGED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT STA 973 - 1071, LEFT BUTT LINE 44 ON JOB CARD 0349 IAW DC-9 SRM.
- [SDR ABXA050084](https://openairdocs.org/sdr/ABXA050084.md): Seat Track · broken · Mar 22, 2005 · N975AX · Doug DC941 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BROKEN IN UPPER CARGO COMPARTMENT AT FS 1041 AND LEFT BUTT LINE 44.5. SPLICED IN NEW SECTION OF SEAT TRACK AT FS 1041 - 965, LEFT BUTT LINE 44.5 IAW DC-9 SRM 53-05.
- [SDR ABXA050078](https://openairdocs.org/sdr/ABXA050078.md): Attach Angle · cracked · Mar 21, 2005 · N975AX · Doug DC941 · Nacelle/Pylon, Attach Fittings
  > NR 1 PYLON UPPER ATTACH ANGLE HAD 1 MISSING FASTENER AND CRACKED AT STA 1056. REPAIRED AREA IAW DC-9 SRM 54-04.
- [SDR ABXA050077](https://openairdocs.org/sdr/ABXA050077.md): Frame · corroded · Mar 21, 2005 · N975AX · Doug DC941 · Fuselage Main, Frame
  > AFT LOWER SECTION OF FRAME CORRODED FS 503, LONGERON 29 LEFT TO LONGERON 29 RIGHT. REPAIRED FRAME IAW DC-9 SRM 53-03.
- [SDR ABXA050076](https://openairdocs.org/sdr/ABXA050076.md): Cargo Track · corroded · Mar 21, 2005 · N975AX · Doug DC941 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR TRACK STA 889 TO STA 1072, LEFT SIDE. REMOVED AND REPLACED TRACK IAW DC-9 SRM 51-30-1.
- [SDR ABXA050079](https://openairdocs.org/sdr/ABXA050079.md): Skin · cracked · Mar 21, 2005 · N975AX · Doug DC941 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE HAD 7 EXTERNAL SKIN CRACKS FROM CANTED STA 1197 TO 1208, LONGERON 13 LEFT TO LONGERON 14 LEFT. CRACK LENGTHS FROM.5 TO.75 INCHES. REPAIRED AREA IAW DC-9 SRM 53-01 AND 53-10.
- [SDR ABXA050083](https://openairdocs.org/sdr/ABXA050083.md): Splice · cracked · Mar 21, 2005 · N975AX · Doug DC941 · Nacelle/Pylon, Main Frame
  > INBOARD FRAME FOOT ON AFT SIDE OF LEFT PYLON BULKHEAD WAS CRACKED. REPLACED CRACKED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.
- [SDR ABXA050082](https://openairdocs.org/sdr/ABXA050082.md): Door Frame · cracked · Mar 21, 2005 · N975AX · Doug DC941 · Fuselage Main, Structure
  > DOOR JAMB WAS CRACKED AT TOP LEFT STOP AT INBOARD RIVET. REPAIRED DOOR JAMB AT TOP LEFT IAW DC-9 SRM 53-05.
- [SDR ABXA050081](https://openairdocs.org/sdr/ABXA050081.md): Bulkhead · cracked · Mar 21, 2005 · N975AX · Doug DC941 · Nacelle/Pylon, Bulkhead/Firewall
  > WEB ON LEFT PYLON BULKHEAD WAS OIL CANNED AND CRACKED AT LOWER INBOARD LIGHTNING HOLE. REPAIRED AREA IAW DC-9 SRM 53-01.
- [SDR ABXA050080](https://openairdocs.org/sdr/ABXA050080.md): Longeron · cracked · Mar 21, 2005 · N975AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > LONGERON 17 RIGHT CRACKED AT PYLON BULKHEAD. SPLICED IN REPAIR ON LONGERON 17 RIGHT AT PYLON BULKHEAD IAW DC-9 DWG K05864 AND DC-9 SRM.
- [SDR ABXA050075](https://openairdocs.org/sdr/ABXA050075.md): Fitting · cracked · Mar 18, 2005 · N975AX · Doug DC941 · Fuselage, Landing Gear Attach Fittings
  > BRACE FROM UPPER PRESSURE PANEL TO FUSELAGE CRACKED AT BOTTOM BOLT ATTACH POINT 56 INCHES LT BUTTLINE AND 19 INCHES AFT OF MAIN FRAME. REMOVED AND REPLACED BRACE IAW DC-9 SRM.
- [SDR ABXA030340](https://openairdocs.org/sdr/ABXA030340.md): Fitting · cracked · Aug 11, 2003 · N975AX · Doug DC941 · Fuselage Miscellaneous Structure
  > FS 1152 LEFT SIDE OF AFT VENTRAL STAIR CUTOUT FRAME FITTING CRACKED. INSTALLED NEW FITTING IAW DC-9 SRM 51-30-5.
- [SDR ABXA030335](https://openairdocs.org/sdr/ABXA030335.md): Attach Fitting · cracked · Aug 6, 2003 · N975AX · Doug DC941 · Elevator, Tab Structure
  > RIGHT ELEVATOR GEARED TAB ATTACH FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2.
- [SDR ABXA030338](https://openairdocs.org/sdr/ABXA030338.md): Shear Tie · cracked · Aug 4, 2003 · N975AX · Doug DC941 · Fuselage Main, Structure
  > CRACKED SHEAR TIE FS 1021 JUST BELOW LONGERON 14 RIGHT. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5.
- [SDR ABXA030339](https://openairdocs.org/sdr/ABXA030339.md): Web · cracked · Aug 4, 2003 · N975AX · Doug DC941 · Fuselage Miscellaneous Structure
  > RIGHT CUSP WEB CRACKED JUST FORWARD OF FS 1041 BULKHEAD. REPAIRED RIGHT CUSP WEB JUST FORWARD OF FS 1041 IAW DC-9 SRM 53-01.
- [SDR ABXA030336](https://openairdocs.org/sdr/ABXA030336.md): Web · cracked · Aug 1, 2003 · N975AX · Doug DC941 · Passenger/Crew Doors
  > MAIN ENTRY DOOR INTERIOR WEB JUST FORWARD OF DOOR HANDLE WAS CRACKED. REPLACED WEB IAW DC-9 SRM 51-30-2.
- [SDR ABXA030333](https://openairdocs.org/sdr/ABXA030333.md): Skin · corroded · Aug 1, 2003 · N975AX · Doug DC941 · Trailing Edge Flaps
  > BULGE IN SKIN, CUPPED FASTENERS FLAP UNDER SURFACE NR 2 EXPANSION JOINT. REPLACED UPPER AND LOWER FLAP SEGMENT SKIN.
- [SDR ABXA030332](https://openairdocs.org/sdr/ABXA030332.md): Skin · corroded · Aug 1, 2003 · N975AX · Doug DC941 · Trailing Edge Flaps
  > BULGE IN SKIN, CUPPED FASTENERS, FLAP LOWER SURFACE AT NR 3 EXPANSION JOINT. REPLACED LOWER SKIN IAW DC-9 SRM 51-30-2.
- [SDR ABXA030337](https://openairdocs.org/sdr/ABXA030337.md): Seat Track · corroded · Aug 1, 2003 · N975AX · Doug DC941 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK AT STA 275, 294, 320, 351, 380 AND 408. REPLACED CENTER SEAT TRACK STA 160 - 588 IAW DC-9 SRM 51-30-1 AND SSRM K05406.
- [SDR ABXA030334](https://openairdocs.org/sdr/ABXA030334.md): Attach Fitting · corroded · Aug 1, 2003 · N975AX · Doug DC941 · Elevator Structure
  > LT ELEVATOR WAS CORRODED ON UPPER SURFACE AT OUTBOARD BALANCE HORN ATTACH FITTING. REPLACED LT ELEVATOR ATTACH FITTING CLIP.
- [SDR ABXA020219](https://openairdocs.org/sdr/ABXA020219.md): Web · cracked · Sep 29, 2002 · N975AX · Doug DC941 · Fuselage Miscellaneous Structure
  > FOUND NUMEROUS CRACKS IN AFT CUSP WEB, LEFT HAND SIDE APPROXIMATELY AT FS 1002. REPAIRED CUSP WEB IAW DC-9 SRM 53-01.
- [SDR ABXA020070](https://openairdocs.org/sdr/ABXA020070.md): Landing Gear · malfunctioned · Jul 31, 2002 · N975AX · Doug DC941 · Landing Gear Retraction/Extension System
  > UPON GEAR EXTENSION FOR APPROACH, NOSE GEAR DID NOT EXTEND (NO GREEN LIGHT/NOSE LIGHT DID NOT SHOW). GEAR RECYCLED AFTER GO-AROUND. NOSE GEAR EXTENDED NORMALLY. INSPECTED NOSE LANDING GEAR DOWNLOCK SWITCH WIRING, NO DEFECTS NOTED. LUBED NOSE LANDING GEAR.
- [SDR ABXA010890](https://openairdocs.org/sdr/ABXA010890.md): Battery · discharged · May 24, 2002 · N975AX · Doug DC941 · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES IAW DC-9 AMM 33-53-02. OPS CHECKED GOOD.
- [SDR ABXA010760](https://openairdocs.org/sdr/ABXA010760.md): Sensor · faulty · Mar 11, 2002 · N975AX · Doug DC941 · Cabin Temperature Sensor
  > AFTER TAKEOFF, AIRCRAFT DID NOT HOLD PRESSURE AND FORWARD CARGO DOOR LIGHT CAME ON AND OFF IN FLIGHT. REPLACED THE CABIN/FLIGHT RATE OF CHANGE/HIGH LIMIT TEMPERATURE SENSOR IAW DC-9 MM 21-61-03-2.
- [SDR ABXA010706](https://openairdocs.org/sdr/ABXA010706.md): Light · inoperative · Feb 10, 2002 · N975AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LAMP BY THE OVERHEAD FORWARD ATTENDANCE PANEL (THE AFT LAMP INOPERATIVE). REPOSITIONED CONTACT LEVEL POINT (DOOR CONTACT) AND RELAMPED IAW DC-9 AMM 33-55-00-4.
- [SDR ABXA010381](https://openairdocs.org/sdr/ABXA010381.md): Control Unit · defective · Jul 3, 2001 · N975AX · Doug DC941 · Fire Detection
  > CARGO FIRE WARNING INDICATED FORWARD BELLY FIRE. SHORTLY AFTER, FIRE LIGHT WENT OUT, FORWARD SMOKE INOPERATIVE LIGHT CAME ON. THEN REPEATED FIRE WARNING AGAIN. COMPLETED EMERGENCY PROCEDURE. REPLACED THE CENTRAL CONTROL UNIT. OPS CHECKED GOOD IAW DC-9 AMM
- [SDR ABXA010352](https://openairdocs.org/sdr/ABXA010352.md): Fire Warning · false activation · Jun 21, 2001 · N975AX · Doug DC941 · Fire Detection
  > CREW REPORTED LOWER CARGO FIRE WARNING AT ILN ON GROUND. CFR WAS DISPATCHED TO AIRCRAFT. CFR REPORTED NO FIRES. NO DEFECTS NOTED. SYSTEM CHECKED GOOD IAW DC-9 MM 26.
- [SDR ABXA000187](https://openairdocs.org/sdr/ABXA000187.md): Skin · corroded · Apr 3, 2000 · N975AX · Doug DC941 · Fuselage Main, Plate/Skin
  > RIGHT WINDOW BELT DOUBLER CORRODED AT WINDOW NR 14. REPLACED WINDOW BELT AT FUSELAGE STATION 465 - 541 IAW DC9 SRM 51-30-2.
- [SDR ABXA000188](https://openairdocs.org/sdr/ABXA000188.md): Floor Support · cracked · Mar 30, 2000 · N975AX · Doug DC941 · Fuselage Miscellaneous Structure
  > SUB FLOOR CRACKED AT STATION 200 AND RBL 22. REPAIRED CRACK IAW DC9 SRM 53-01.
- [SDR ABXA000194](https://openairdocs.org/sdr/ABXA000194.md): Fitting · cracked · Mar 29, 2000 · N975AX · Doug DC941 · Fuselage Miscellaneous Structure
  > SUPPORT T-FITTING CRACKED AND CORRODED ON OUTBOARD SIDE OF WHEEL WELL AT APPROX STA 775. REPLACED FORWARD AND AFT FITTINGS IAW DC9 SRM 51-10-4, AND 51-30-5.
- [SDR ABXA000193](https://openairdocs.org/sdr/ABXA000193.md): Fitting · corroded · Mar 27, 2000 · N975AX · Doug DC941 · Fuselage Miscellaneous Structure
  > LEVEL 1 CORROSION ON T-FITTING OUTBOARD SIDE OF WHEEL WELL AT APPROX STA 770. REPLACED T-FITTING IAW DC9 SRM 51-10-4, AND 51-30-5.
- [SDR ABXA000192](https://openairdocs.org/sdr/ABXA000192.md): Door · corroded · Mar 27, 2000 · N975AX · Doug DC941 · Landing Gear Doors
  > LEFT FORWARD NOSE LANDING GEAR DOOR CORRODED AT AFT END UNDER DEFLECTOR. REPLACED DOOR IAW DC9 MM 32-22-01-2-0004.
- [SDR ABXA000189](https://openairdocs.org/sdr/ABXA000189.md): Floor Support · cracked · Mar 27, 2000 · N975AX · Doug DC941 · Fuselage Miscellaneous Structure
  > CRACK IN SUB FLOOR AT STATION 180 AND RBL 4.0. REPAIRED IAW DC9 SRM 53-04.
- [SDR ABXA9800782](https://openairdocs.org/sdr/ABXA9800782.md): Shear Tie · cracked · Aug 14, 1998 · N975AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND SHEAR TIE CRACKED AT FS 1056 BETWEEN LONGERON 14L AND 16L. REPLACED SHEAR TIE AND CLIPS IAW DC9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA9800785](https://openairdocs.org/sdr/ABXA9800785.md): Web · cracked · Aug 11, 1998 · N975AX · Doug DC941 · Cargo/Baggage Doors
  > DURING C-CHECK, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR STRUCTURE CRACKED ABOVE THE FORWARD HINGE. REPLACED WEB AND FITTING IAW DC9 SRM 51-30-1, 51-30-2 AND 51-30-5.
- [SDR ABXA9800796](https://openairdocs.org/sdr/ABXA9800796.md): Rib · cracked · Aug 7, 1998 · N975AX · Doug DC941 · Vertical Stabilizer, Spar/Rib
  > DURING C-CHECK, FOUND RIB CRACKED IN THE VERTICAL STABILIZER LEADING EDGE. REPLACED RIB IAW DC9 SRM CHAPTERS 51-30-2 AND 51-30-5.
- [SDR ABXA9800784](https://openairdocs.org/sdr/ABXA9800784.md): Shear Tie · cracked · Aug 7, 1998 · N975AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND A CRACKED SHEAR TIE AT FS 1021 BETWEEN LONGERON 15L AND 16L. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA9800783](https://openairdocs.org/sdr/ABXA9800783.md): Shear Tie · cracked · Aug 7, 1998 · N975AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND CRACKED SHEAR TIE AT FS 1021 BETWEEN LONGERON 14L AND 15L. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA9800781](https://openairdocs.org/sdr/ABXA9800781.md): Shear Tie · cracked · Aug 6, 1998 · N975AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND SHEAR TIE CRACKED AT FS 1021 BELOW LONGERON 14 RT. REPAIRED SHEAR TIE IAW DC9 SRM 53-03, FIG 6.
- [SDR ABXA9700477](https://openairdocs.org/sdr/ABXA9700477.md): Rod End · worn · Apr 3, 1997 · N975AX · Doug DC941 · Flight Compartment Windows
  > FIRST OFFICER'S CLEARVIEW WINDOW DIFFICULT TO OPEN. REPLACED THE FORWARD LOWER ROD END ON THE WINDOW LINKAGE, OPS CHECK GOOD IAW DC-9 MM 56-10-3.
- [SDR ABXA9700476](https://openairdocs.org/sdr/ABXA9700476.md): Spring · missing · Apr 2, 1997 · N975AX · Doug DC941 · Flight Compartment Windows
  > AT DEPARTURE TIME, FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT FUNCTION CORRECTLY, HARD TO CLOSE. REINSTALLED THE ACTUATING SPRING FOR THE AFT LOWER WINDOW LATCH, OPS CHECK GOOD IAW DC-9 MM 56-10-3.
- [SDR ABXA9700379](https://openairdocs.org/sdr/ABXA9700379.md): Tr Bucket · cracked · Dec 19, 1996 · N975AX · Doug DC941 · Engine Thrust Reverser
  > DURING C-CHECK, THE LOWER THRUST REVERSER BUCKET WAS FOUND CRACKED. THE BUCKET WAS REPLACED IAW DC9 MM 78-30-2.
- [SDR ABXA9700376](https://openairdocs.org/sdr/ABXA9700376.md): Skin · damaged · Dec 19, 1996 · N975AX · Doug DC941 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, THE FUSELAGE SKIN ON THE AFT SIDE OF THE FWD ENTRY DOOR LOWER CORNER WAS FOUND DAMAGED. THE SKIN WAS REPAIRED IAW REA D953-17518.

Next page: https://openairdocs.org/deregistered/N975AX-2017-05-22/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 = 'N975AX' AND deregistration_id = 'N975AX-2017-05-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N975AX-2017-05-22/reports

---
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