# Service difficulty reports: N924VJ, cancelled Jul 17, 2002 A list on [N924VJ, cancelled Jul 17, 2002](https://openairdocs.org/deregistered/N924VJ-2002-07-17.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAD01019](https://openairdocs.org/sdr/USAAD01019.md): Battery · discharged · Feb 2, 2001 · N924VJ · Doug DC931 · Emergency Lighting > IND - THE CEILING EMERGENCY LIGHTS ABOVE SEAT ROWS 1 THROUGH 4 WERE DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAAD00064](https://openairdocs.org/sdr/USAAD00064.md): Battery · discharged · Apr 29, 2000 · N924VJ · Doug DC931 · Emergency Lighting > IND - THE COCKPIT, SERVICE DOOR AND MAIN ENTRY DOOR EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAAD00053](https://openairdocs.org/sdr/USAAD00053.md): Light · broken · Apr 15, 2000 · N924VJ · Doug DC931 · Emergency Lighting > PIT - FLOOR EMERGENCY LIGHTING FOUND OUT OF TRACK AND BROKEN. MAINTENANCE REPAIRED EMERGENCY FLOOR LIGHTING WIRE AND REINSTALLED FLOOR TRACK. (M) - [SDR USAAD000025](https://openairdocs.org/sdr/USAAD000025.md): Valve · failed · Feb 6, 2000 · N924VJ · Doug DC931 · Landing Gear Steering System > PIT - MDT - FLT 1414 - AFTER TAKEOFF THE NOSE LANDING GEAR DID NOT FULLY RETRACT AND THE RED GEAR UNSAFE LIGHT REMAINED ON. WHEN THE LANDING GEAR WAS EXTENDED ALL THREE GREEN LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. - [SDR USAAD00001](https://openairdocs.org/sdr/USAAD00001.md): Battery · discharged · Jan 1, 2000 · N924VJ · Doug DC931 · Emergency Lighting > IND - THE LEFT NACELLE SCAN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LEFT NACELLE SCAN EMERGENCY LIGHT BATTERY. (M) - [SDR USAA990411](https://openairdocs.org/sdr/USAA990411.md): Outer Pan · cracked · Apr 22, 1999 · N924VJ · Doug DC931 · Cargo/Baggage Doors > PIT - DURING Q-4 CHECK, FOUND 3 INCH CRACK IN FORWARD CARGO DOOR OUTER PAN AT UPPER HINGE OF FORWARD CARGO DOOR. INSTALLED EXTERNAL DOUBLER (A-286) PER SRM 52-03 FIG 8. (M) - [SDR USAA990410](https://openairdocs.org/sdr/USAA990410.md): Angle · cracked · Apr 22, 1999 · N924VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND 1.5 INCH CRACK ON RIGHT VERTICAL STAB DRAG ANGLE AT STATION 1140 RIGHT VERTICAL STAB ATTACH ANGLE. REMOVED CRACKED VERTICAL LEG, INSTALLED REPAIR SPLICE PER SRM 53-05 FIG 23A. (M) - [SDR USAA990409](https://openairdocs.org/sdr/USAA990409.md): Skin · cracked · Apr 22, 1999 · N924VJ · Doug DC931 · Fuselage Main, Plate/Skin > PIT - DURING Q-4 CHECK, FOUND TWO EACH 1.5 INCH CRACKS IN FUSELAGE SKIN AT STATION 1095 RIGHT, BETWEEN LONGERON 3 AND 4 RIGHT. INSTALLED EXTERNAL DOUBLER PER SRM 53-04 FIG 27. (M) - [SDR USAA990408](https://openairdocs.org/sdr/USAA990408.md): Skin · cracked · Apr 22, 1999 · N924VJ · Doug DC931 · Fuselage Main, Plate/Skin > PIT - DURING Q-4 CHECK, FOUND 1.5 INCH CRACK IN FUSELAGE SKIN AT STATION 1095 LEFT, BELOW LONGERON 3. REPAIRED WITH FILLER AND DOUBLER PER SRM 53-04 FIG 27. (M) - [SDR USAA990407](https://openairdocs.org/sdr/USAA990407.md): Beam · corroded · Apr 22, 1999 · N924VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND CORROSION 1 INCH BY.5 INCH FIVE EACH AREAS INSIDE AND OUTSIDE SURFACE (SEVERAL PLACES) AT FRAME 897 LONGERON 29R AND INTERCOSTAL BEAM, AFT CARGO. CORROSION LEVEL 1. REMOVED TIE DOWN, MANUFACTURED NEW STRAP FOR TOP OF INTERCOSTA - [SDR USAA990406](https://openairdocs.org/sdr/USAA990406.md): Frame · cracked · Apr 22, 1999 · N924VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND.25 INCH CRACK IN SKIN FRAME AT LEFT WINDOW NR 23 LOWER AFT FRAME SECTION AROUND HUCK BOLT. STOP DRILLED CRACK AND INSTALLED A REPAIR ANGLE PER TYPICAL REPAIR 53-30-06A. (M) - [SDR USAA990405](https://openairdocs.org/sdr/USAA990405.md): Subfloor · corroded · Apr 22, 1999 · N924VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND 3 INCH BY 3 INCH CORROSION IN SUBFLOOR AT STATION 218, OUTBOARD OF SEAT TRACK 18, CORROSION LEVEL 1. CUT OUT DAMAGE AND SPLICED IN A NEW SECTION PER EA 51977. (M) - [SDR USAA990404](https://openairdocs.org/sdr/USAA990404.md): Support · corroded · Apr 22, 1999 · N924VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND 1 INCH BY 6 INCH CORROSION IN FLOOR SUPPORT JUST INBOARD OF SEAT TRACK 19 AT STATION 200-237, CORROSION LEVEL 1. FABRICATED NEW FLOOR SUPPORT FROM EXTRUSION AND INSTALLED SAME PER SRM 53-11-1. (M) - [SDR USAA990403](https://openairdocs.org/sdr/USAA990403.md): Web · cracked · Apr 22, 1999 · N924VJ · Doug DC931 · Fuselage Miscellaneous Structure > PIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN WEB FINGER AT STATION 207 LONGERON 15L. CUT OUT CRACK SECTION OF WEB, INSTALLED A FILLER AND A DOUBLER PER EA 51868. (M) - [SDR USAA990402](https://openairdocs.org/sdr/USAA990402.md): Floorbeam · corroded · Apr 22, 1999 · N924VJ · Doug DC931 · Fuselage Main, Floor Beam > PIT - DURING Q-4 CHECK, FOUND 1 INCH BY 8 INCH CORROSION AT GALLEY AREA FLOORBEAM NR 44 TOP AND LOWER SURFACE, CORROSION LEVEL 1. FABRICATED FLOORBEAM AND INSTALLED PER SRM 53-11-1. (M) - [SDR USAA990401](https://openairdocs.org/sdr/USAA990401.md): Floorbeam · corroded · Apr 22, 1999 · N924VJ · Doug DC931 · Fuselage Main, Floor Beam > PIT - DURING Q-4 CHECK, FOUND 1 INCH BY 5 INCH CORROSION AT STATION 218-237 FLOORBEAM CAP AT CENTER, CORROSION LEVEL 1. FABRICATED AND INSTALLED NEW SECTION BY SPLICING PER TYPICAL REPAIR 53-11-21A. (M) - [SDR USAA990400](https://openairdocs.org/sdr/USAA990400.md): Floorbeam · corroded · Apr 22, 1999 · N924VJ · Doug DC931 · Fuselage Main, Floor Beam > PIT - DURING Q-4 CHECK, FOUND 1 INCH BY 4 INCH CORROSION GALLEY AREA NR 49 FLOORBEAM TOP AND LOWER SURFACES, CORROSION LEVEL 1. MANUFACTURED FLOOR SUPPORT AND INSTALLED SAME PER SRM 53-11-1 TYPE A1 AND A2 FIG 11 SHEET 2, ITEM 10. (M) - [SDR USAAD99034](https://openairdocs.org/sdr/USAAD99034.md): Control Box · failed · Mar 2, 1999 · N924VJ · Doug DC931 · Landing Gear Position and Warning > PIT-SBN - FLT 753 - AFTER TAKEOFF, THE RIGHT MLG UNSAFE LIGHT ILLUMINATED WITH THE GEAR HANDLE UP. THE LANDING WAS CYCLED BUT THE LIGHT REMAINED ON. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SENSING C - [SDR USAAD98152](https://openairdocs.org/sdr/USAAD98152.md): Battery · discharged · Aug 28, 1998 · N924VJ · Doug DC931 · Emergency Lighting > IND - ONE SET OF CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE CEILING EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD98041](https://openairdocs.org/sdr/USAAD98041.md): Power Supply · inoperative · Mar 9, 1998 · N924VJ · Doug DC931 · Emergency Lighting > CMH - THE TAIL COMPARTMENT EVACUATION LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EVACUATION LIGHT POWER SUPPLY. (M) - [SDR USAA960265](https://openairdocs.org/sdr/USAA960265.md): Skin · cracked · Feb 19, 1996 · N924VJ · Doug DC931 · Leading Edge Devices > PIT - PILOT REPORTED AFTER WALK AROUND THAT THERE WAS A 1 INCH CRACK IN THE LEFT WING LEADING EDGE NR 1 SLAT SKIN AT STATION XF-126 ABOVE TELESCOPING ANTI-ICE DUCT. REMOVED CRACK AND INSTALLED FILLER AND DOUBLER REPAIR PER SRM 57-02 FIG 6. AIRCRAFT RETURNED ## 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 = 'N924VJ' AND deregistration_id = 'N924VJ-2002-07-17' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N924VJ-2002-07-17/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.