# Service difficulty reports: N925AX, cancelled Apr 25, 2007

A list on [N925AX, cancelled Apr 25, 2007](https://openairdocs.org/deregistered/N925AX-2007-04-25.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 · 82 reports

- [SDR ABXA040302](https://openairdocs.org/sdr/ABXA040302.md): Pan · corroded · Aug 30, 2004 · N925AX · Doug DC914 · Fuselage Miscellaneous Structure
  > WHILE PERFORMING AN X-RAY OF THE FORWARD LOWER CARGO COMPARTMENT DOOR JAMB, FOUND THE LOWER DOOR JAMB PAN PRIOR SERVICE REWORK REPAIR CORRODED BEYOND LIMITS. REMOVED AND REPLACED SERVICE REWORK DOOR JAMB PAN P/N J060228-9 IAW DC-9 SRM 53-05.
- [SDR ABXA040078](https://openairdocs.org/sdr/ABXA040078.md): Battery · discharged · Feb 18, 2004 · N925AX · Doug DC941 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS IN COCKPIT STAYED ON AFTER POWER SHUT DOWN. REPLACED BATTERY POWER SUPPLY WITH SEVICEABLE UNIT. OPS CHECKED GOOD IAW DC-9 MM.
- [SDR ABXA040077](https://openairdocs.org/sdr/ABXA040077.md): Battery · discharged · Feb 17, 2004 · N925AX · Doug DC941 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS IN COCKPIT STAYED ON AFTER POWER SHUT DOWN. RESEATED BATTERIES IN EMERGENCY LIGHT POWER SUPPLY. LIGHTS FUNCTIONED NORMALLY IAW DC-9 MM.
- [SDR ABXA030443](https://openairdocs.org/sdr/ABXA030443.md): Floor Support · cracked · Oct 31, 2003 · N925AX · Doug DC914 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STRAP, ATTACH ANGLE CRACKED, FS 768 AT LONGERON 27 RIGHT. REPLACED ANGLE IAW DC-9 SRM 51-30-5.
- [SDR ABXA030442](https://openairdocs.org/sdr/ABXA030442.md): Floor Support · corroded · Oct 31, 2003 · N925AX · Doug DC914 · Fuselage Miscellaneous Structure
  > STA 218 FLOOR SUPPORT WAS CORRODED ABOVE LONGERON 30. REPAIRED FRAME AT FS 218, LONGERON 30 IAW DC-9 SRM 53-03.
- [SDR ABXA030441](https://openairdocs.org/sdr/ABXA030441.md): Skin · corroded · Oct 30, 2003 · N925AX · Doug DC914 · Wing, Plate/Skin
  > RIGHT WING UPPER SKIN CORRODED AND PULLED RIVETS JUST INBOARD OF SPOILER ACTUATOR. REPLACED SECTION OF STRINGER AND SPLICE IAW DC-9 SRM 51-70-5 AND 51-30-5.
- [SDR ABXA030440](https://openairdocs.org/sdr/ABXA030440.md): Fitting · cracked · Oct 30, 2003 · N925AX · Doug DC914 · Cargo/Baggage Doors
  > AFT LOWER CARGO DOOR, TRAILING EDGE NR 5 BEAM END FITTING CRACKED. INSTALLED NEW FITTING IAW DC-9 SRM 51-30-5 AND 51-30-2.
- [SDR ABXA030081](https://openairdocs.org/sdr/ABXA030081.md): Wire · burned · Feb 19, 2003 · N925AX · Doug DC914 · Electrical Power System Wiring
  > PRIMARY TRIM NR 1 CIRCUIT BREAKER TRIPPED. FOUND WIRES C104C10, C1203C10, C1202C10, C1202B10, C1203B10, C1204B10, C1213A10, C1213B10, C1211B10 BURNED. FOUND WIRE C1205D16 NOT CONNECTED. FOUND RELAY R20-16 BADLY BURNED. REPAIRED ALL WIRING AND REPLACED RELA
- [SDR ABXA020123](https://openairdocs.org/sdr/ABXA020123.md): Link · cracked · Aug 23, 2002 · N925AX · Doug DC914 · Engine Thrust Reverser
  > NR 2 LOWER AFT LEFT THRUST REVERSER DRIVER LINK WAS CRACKED. REPLACED THE NR 2 LOWER LEFT DRIVE LINK IAW DC-9 MM 78-31-05-2-0001, NEA 7830001, TASK NEA 13435, AD 75-14-06, AD 96-10-11, AND SERVICE BULLETIN 78-66.
- [SDR ABXA010776](https://openairdocs.org/sdr/ABXA010776.md): Stiffener · cracked · Mar 4, 2002 · N925AX · Doug DC914 · Wing Miscellaneous Structure
  > OUTBOARD STATION 91.00, FRONT SPAR VERTICAL STIFFENER, UPPER PORTION WAS CRACKED. REPLACED STIFFENER IAW DC-9 SRM.
- [SDR ABXA010775](https://openairdocs.org/sdr/ABXA010775.md): Skin · cracked · Feb 28, 2002 · N925AX · Doug DC914 · Landing Gear Doors
  > RIGHT MAIN LANDING GEAR DOOR INNER SKIN CRACKED JUST AFT OF THE FORWARD HINGE FITTING. REPAIRED CRACKED AREA IAW DC-9 SRM 52-01.
- [SDR ABXA010774](https://openairdocs.org/sdr/ABXA010774.md): Frame · cracked · Feb 27, 2002 · N925AX · Doug DC914 · Fuselage Main, Frame
  > AUXILIARY SUPPORT FRAME CRACKED IN AFT ACCESSORY COMPARTMENT FLOOR SUPPORT, FORWARD OF MAIN FRAME AT STATION 908. REPLACED FRAME IAW DC-9 SRM DWG 505159 AND DC-9 SRM 51-30-2.
- [SDR ABXA010773](https://openairdocs.org/sdr/ABXA010773.md): Fitting · cracked · Feb 27, 2002 · N925AX · Doug DC914 · Emergency Exits
  > LEFT OVER WING EXIT DOOR PAN STIFFENER ANGLES ON OUTER PAN CRACKED 5 INCHES. REPLACED STOPS IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA010772](https://openairdocs.org/sdr/ABXA010772.md): Angle · cracked · Feb 26, 2002 · N925AX · Doug DC914 · Standard Practices/Structures
  > OUTBOARD LOWER FASTENER HOLE ON ATTACH ANGLE CRACKED WHERE WING TO FUSELAGE FAIRING ATTACHES AT F.S. 585. REPLACED ANGLE IAW DC-9 SRM 51-30-1 AND DC-9 DWG 9915547.
- [SDR ABXA010771](https://openairdocs.org/sdr/ABXA010771.md): Finger Doubler · debonded · Feb 25, 2002 · N925AX · Doug DC914 · Wing, Plate/Skin
  > OUTBOARD REMOVABLE TRAILING EDGE LOWER SKIN FINGER DOUBLERS WERE DEBONDED. REPLACED UPPER/LOWER SKINS IAW REA D957-43379.
- [SDR ABXA010676](https://openairdocs.org/sdr/ABXA010676.md): Control Cable · lack of lube · Jan 16, 2002 · N925AX · Doug DC914 · Trailing Edge Flap Control System
  > FINAL APPROACH, AIRCRAFT IN A TRIMMED DESCENT ON GLIDESLOPE, FLAPS 30, N1-60 PERCENT ON BOTH ENGINES, SPEED 10 + OVER TARGET 139. WENT TO FLAP 40, AIRCRAFT ROLLED RIGHT NOTICEABLE, 1 1/2 UNITS LEFT TO TRIM. INSPECTED AILERON AND FLAP CABLE SYSTEM. ALSO INSP
- [SDR ABXA000400](https://openairdocs.org/sdr/ABXA000400.md): Indicator · shorted · Aug 24, 2000 · N925AX · Doug DC914 · Landing Gear Position and Warning
  > AFTER SELECTING LANDING GEAR DOWN, NOSE GEAR SAFE LIGHT DID NOT ILLUMINATE. NO RED GEARWARNING LIGHT. PERFORMED ABNORMAL PROCEDURES AND GO-AROUND. VISUALLY CHECKED GEAR DOWN ANDLOCKED. LANDING WAS UNEVENTFUL. FOUND NOSE GEAR DOWN LIGHT ASSEMBLY INTERNALLY
- [SDR ABXA000349](https://openairdocs.org/sdr/ABXA000349.md): Floorbeam · corroded · Jul 19, 2000 · N925AX · Doug DC914 · Fuselage Main, Floor Beam
  > FLOORBEAM WEB AT STATION 786 AND LBL 13.0 IS EXFOLIATED. REPAIRED IAW ABX REA D957-38011.
- [SDR ABXA000343](https://openairdocs.org/sdr/ABXA000343.md): Stiffener · cracked · Jul 12, 2000 · N925AX · Doug DC914 · Fuselage Miscellaneous Structure
  > LEFT AND RIGHT RADIAL STIFFENERS NR 14 WERE CRACKED. REPLACED IAW DC9 SRM 51-30-5.
- [SDR ABXA000344](https://openairdocs.org/sdr/ABXA000344.md): Longeron · corroded · Jul 11, 2000 · N925AX · Doug DC914 · Fuselage Main, Longeron/Stringer
  > LONGERONS 23 AND 24 LEFT WERE CORRODED AT STATIONS 817 - 823. REPAIRED LONGERONS 23 AND 24 LEFT IAW DC9 SRM 50-02.
- [SDR ABXA000342](https://openairdocs.org/sdr/ABXA000342.md): Shear Tie · cracked · Jul 10, 2000 · N925AX · Doug DC914 · Fuselage Main, Structure
  > EXTRUSION FORWARD OF AFT PRESSURE BULKHEAD T-CAP AT LONGERON 18 LEFT WAS CRACKED AT FLOOR LINE. REPLACED SHEAR TIE ANGLE IAW DC9 SRM 51-30-2.
- [SDR ABXA000341](https://openairdocs.org/sdr/ABXA000341.md): Floor Support · cracked · Jul 10, 2000 · N925AX · Doug DC914 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT WAS CRACKED AT CUSP LINE JUST FORWARD OF PRESSURE DOME ON RIGHT SIDE. REPAIRED IAW DC9 SRM.
- [SDR ABXA000340](https://openairdocs.org/sdr/ABXA000340.md): Frame · cracked · Jul 10, 2000 · N925AX · Doug DC914 · Fuselage Main, Frame
  > FRAME OUTSIDE FLANGE CRACKED AT STATION 801 AND LONGERON 17 LEFT. REPLACED FRAME IAW DC9 SRM 52-03.
- [SDR ABXA000339](https://openairdocs.org/sdr/ABXA000339.md): Fitting · cracked · Jul 7, 2000 · N925AX · Doug DC914 · Fuselage Miscellaneous Structure
  > LONGERON FITTING CRACKED AT STATION 585 AND LONGERON 11 LEFT. REPLACED FITTING IAWDC9 SRM 51-30-5.
- [SDR ABXA000337](https://openairdocs.org/sdr/ABXA000337.md): Pan · cracked · Jul 7, 2000 · N925AX · Doug DC914 · Cargo/Baggage Doors
  > FORWARD LOWER CARGO DOOR INBOARD SIDE OF PAN WAS CRACKED. INSTALLED DOUBLER IAW DC9 SRM 52-05.
- [SDR ABXA000334](https://openairdocs.org/sdr/ABXA000334.md): Stiffener · cracked · Jul 7, 2000 · N925AX · Doug DC914 · Wing Miscellaneous Structure
  > REAR SPAR STIFFENER WAS CRACKED AT STATION XRS 313. REPLACED STIFFENER IAW DC9 SRM 51-30-5.
- [SDR ABXA000338](https://openairdocs.org/sdr/ABXA000338.md): Longeron · corroded · Jul 6, 2000 · N925AX · Doug DC914 · Fuselage Main, Longeron/Stringer
  > LONGERON 30 HAD LEVEL 2 CORROSION AT STATION 642. REPLACED LONGERON IAW DC9 SRM 53-02.
- [SDR ABXA000336](https://openairdocs.org/sdr/ABXA000336.md): Skin · delaminated · Jul 5, 2000 · N925AX · Doug DC914 · Spoilers
  > RIGHT INBOARD SPOILER WAS DELAMINATED. REPLACED SPOILER IAW DC9 MM 27-62-01.
- [SDR ABXA000335](https://openairdocs.org/sdr/ABXA000335.md): Hinge · cracked · Jul 5, 2000 · N925AX · Doug DC914 · Trailing Edge Flaps
  > RIGHT FLAP HINGE CRACKED AT STATION 351. REPLACED FLAP HINGE.
- [SDR ABXA9900692](https://openairdocs.org/sdr/ABXA9900692.md): Window · stuck · Sep 3, 1999 · N925AX · Doug DC914 · Flight Compartment Windows
  > CAPTAIN'S CLEAR VIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED CAPTAIN'S CLEAR VIEW WINDOW TRACK. OPS CHECKED GOOD.
- [SDR ABXA9900060](https://openairdocs.org/sdr/ABXA9900060.md): Link · out of adjust · Feb 1, 1999 · N925AX · Doug DC914 · Landing Gear Position and Warning
  > AFTER TAKEOFF WITH GEAR HANDLE IN UP POSITION, THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. GEAR CYCLED DOWN NORMALLY. ON RETRACTION, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. AIR TURNBACK TO ILN. RESHIMMED NOSE LANDING GEAR ACTUATOR LINK AND ADJUST
- [SDR ABXA9801182](https://openairdocs.org/sdr/ABXA9801182.md): Retainer · cracked · Dec 10, 1998 · N925AX · Doug DC914 · Flight Compartment Windows
  > DURING C-CHECK, FOUND LEFT WINDOW RETAINER CRACKED. REPAIRED CRACK IAW DC9 SERVICE REWORK DRAWING 5952965.
- [SDR ABXA9801155](https://openairdocs.org/sdr/ABXA9801155.md): Jamb · cracked · Dec 2, 1998 · N925AX · Doug DC914 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND SERVICE DOOR JAMB INTERNAL WEB CRACKED 2 PLACES AT UPPER HINGE CUTOUT, STATION 160. REPAIRED IAW ABX REA D953-25631.
- [SDR ABXA9801154](https://openairdocs.org/sdr/ABXA9801154.md): Angle · cracked · Dec 2, 1998 · N925AX · Doug DC914 · Nacelle/Pylon Structure
  > DURING C-CHECK, FOUND NR 1 LOWER PYLON ATTACH ANGLE CRACKED IN RADIUS ON FORWARD EDGE. REPAIRED ANGLE IAW DC9 SRM 54-04.
- [SDR ABXA9801136](https://openairdocs.org/sdr/ABXA9801136.md): Fitting · cracked · Nov 30, 1998 · N925AX · Doug DC915 · Trailing Edge Flaps
  > DURING C-CHECK, FOUND LEFT FLAP INBOARD FIXED VANE OUTBOARD ATTACH SUPPORT FITTING BROKEN. REPLACED FITTING IAW DC9 SRM 51-30-2, 52-30-5, AND DACO DWG 9957773.
- [SDR ABXA9800405](https://openairdocs.org/sdr/ABXA9800405.md): Latch · loose · Apr 22, 1998 · N925AX · Doug DC914 · Fixed Inner Doors
  > COCKPIT DOOR EXTREMELY DIFFICULT TO OPEN FROM CABIN. TIGHTENED DOOR HANDLE/LATCH ASSEMBLY, OPS CHECKED GOOD.
- [SDR ABXA9700927](https://openairdocs.org/sdr/ABXA9700927.md): Spar Cap · corroded · Apr 22, 1997 · N925AX · Doug DC915 · Wing Spar
  > DURING C-CHECK, FOUND THE CENTER WING SPAR AFT VERTICAL FACE OF THE SPAR CAP AT STA XCW -40 SEVERLY CORRODED. REPAIRED IAW ABX REA D957-19174-MR.
- [SDR ABXA9700926](https://openairdocs.org/sdr/ABXA9700926.md): Floorbeam · corroded · Apr 22, 1997 · N925AX · Doug DC915 · Fuselage Main, Floor Beam
  > DURING C-CHECK, FOUND THE FLOORBEAM AT F/STA 786 CORRODED AT LBL 27 ON TOP SIDE. REPAIRED IAW ABX REA D953-19248-MR.
- [SDR ABXA9700925](https://openairdocs.org/sdr/ABXA9700925.md): Bulkhead Web · cracked · Apr 22, 1997 · N925AX · Doug DC915 · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND THE UPPER CARGO BULKHEAD AT F/STA 786 LT WEB CRACKED. REPAIRED IAW ABX REA D953-19255-MR.
- [SDR ABXA9700924](https://openairdocs.org/sdr/ABXA9700924.md): Web · corroded · Apr 22, 1997 · N925AX · Doug DC915 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND THE CUSP WEB AT F/STA 786 LT CORRODED. REPLACED CUSP WEB IAW DC9 SRM 51-30-2.
- [SDR ABXA9700923](https://openairdocs.org/sdr/ABXA9700923.md): Fitting · cracked · Apr 22, 1997 · N925AX · Doug DC915 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND THE FLOORBEAM FITTING AT F/STA 786 LT CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5 AND 51-30-1.
- [SDR ABXA9700922](https://openairdocs.org/sdr/ABXA9700922.md): Rib · cracked · Apr 22, 1997 · N925AX · Doug DC915 · Wing, Rib/Bulkhead
  > DURING C-CHECK, FOUND THE RIGHT WING LEADING EDGE RIB AT STA 172 CRACKED. CUTOUT CRACKED SECTION OF RIB, AND REPAIRED IAW ABX REA D957-19252.
- [SDR ABXA9700921](https://openairdocs.org/sdr/ABXA9700921.md): Bulkhead Fitting · cracked · Apr 22, 1997 · N925AX · Doug DC915 · Wing, Rib/Bulkhead
  > DURING C-CHECK, FOUND THE RIGHT WING BULKHEAD FITTING AT W/STA XRS 69 BETWEEN STRINGERS 12 AND 13 INSIDE LT WING FUEL TANK CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-05.
- [SDR ABXA9700920](https://openairdocs.org/sdr/ABXA9700920.md): Door Pan · cracked · Apr 22, 1997 · N925AX · Doug DC915 · Cargo/Baggage Doors
  > DURING C-CHECK, FOUND THE FORWARD CARGO COMPARTMENT DOOR PAN CRACKED BOTH SIDES OF NR 1 PRESSURE STOP. REPAIRED UPPER CRACK IAW DC9 SRM 52-05, FIGURE 50 AND LOWER CRACK IAW DC9 SRM 52-03, FIGURE 1.
- [SDR ABXA9700919](https://openairdocs.org/sdr/ABXA9700919.md): Skin · cracked · Apr 22, 1997 · N925AX · Doug DC915 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND THE FUSELAGE SKIN CRACKED 4 INCHES LONG AT LONGERON 18R, FS 544. REPAIRED CRACKED SKIN IAW DC9 SRM 53-04, FIGURE 12B.
- [SDR ABXA9700914](https://openairdocs.org/sdr/ABXA9700914.md): Trapezoidal Pnl · cracked · Apr 19, 1997 · N925AX · Doug DC915 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND THE RT TRAPEZOIDAL PANEL CRACKED JUST ABOVE THE RT MLG FIXED STRUT ATTACH POINT. REPLACED TRAPEZOIDAL PANEL IAW DC9 SRM 57-09, FIGURE 34 AND DACO SB 53-182.
- [SDR ABXA9700913](https://openairdocs.org/sdr/ABXA9700913.md): Fitting · cracked · Apr 19, 1997 · N925AX · Doug DC915 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND FORWARD INTERCOSTAL FS 218 BETWEEN LONG 27 AND 28 L CRACKED. REPLACED ATTACH ANGLE (FITTING) P/N 5956034-527 PER DC9 SRM 51-30-2.
- [SDR ABXA9700912](https://openairdocs.org/sdr/ABXA9700912.md): Skin · damaged · Apr 19, 1997 · N925AX · Doug DC915 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND FUSELAGE SKIN DAMAGED AT STA 408, LONGERON 21L. REPAIRED SKIN IAW DC9 SRM 53-04, FIGURE 38, SHT 20.
- [SDR ABXA9700911](https://openairdocs.org/sdr/ABXA9700911.md): Floorbeam · cracked · Apr 19, 1997 · N925AX · Doug DC915 · Fuselage Main, Floor Beam
  > DURING C-CHECK, FOUND FLOORBEAM AT FS 503 AND LBL 57 CRACKED. REPLACED FLOORBEAM IAW DC9 SRM.
- [SDR ABXA9700910](https://openairdocs.org/sdr/ABXA9700910.md): Frame · cracked · Apr 19, 1997 · N925AX · Doug DC915 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND FUSELAGE FRAME STA 801 CRACKED AT LONGERON 17R. REMOVED AND REPLACED CRACKED SECTION OF FRAME IAW DC9 SRM 53-03, FIGURE 32.

Next page: https://openairdocs.org/deregistered/N925AX-2007-04-25/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 = 'N925AX' AND deregistration_id = 'N925AX-2007-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N925AX-2007-04-25/reports

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