N912VV

Service difficulty reports not matched to an aircraft · 23

They name N912VV, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N912VV' AND registry_match IS NULL
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR VJ9800476Control Box · malfunctionedNO BRAKE PRESSURE INDICATION WHEN ANTI-SKID SELECTED ON, TAKING AIRCRAFT RUNWAY POSITION. MAINTENANCE INSPECTED ANTI-SKID AND BRAKE SYSTEM AND TROUBLE SHOT PROBLEM TO ANTI-SKID CONTROL BOX. .Sep 30, 1998 · N912VV · Doug DC932 · Brake Anti-Skid SectionSDR VJ9800417Control Box · failedNO BRAKE PRESSURE DURING TAXI WITH ANTISKID SYSTEM ON. REPLACED ANTISKID CONTROL BOX AND OPS CHECKED GOOD IAW MM 32-43.Sep 22, 1998 · N912VV · Doug DC932 · Brake Anti-Skid SectionSDR VJ9800410Control Cable · out of adjAFTER TAKEOFF, FLIGHT CREW WAS UNABLE TO RAISE GEAR HANDLE. AS PRECAUTIONARY MEASURE FLIGHT CREW ELECTED TO RETURN TO ATL MAINTENANCE BASE. ADJUSTED ANTI RETRACTION CABLE WHICH WAS FOUND TO BE OUT OF TOLERANCE IAW MM 32-23-1, PERFORMED GEAR SWING AND ALL CHESep 12, 1998 · N912VV · Doug DC932 · Landing Gear Retraction/Extension SystemSDR VJ9800375Doubler · corrodedFLOOR SUPPORT DOUBLERS CORRODED UNDER STA 889-908 LONGERON 29L-27L. FABRICATED SUPPORT DOUBLER FROM 7075 T6 .063 3.5 BY 3. INSTALLED REPAIR IAW DC-9 SRM 51-10-3, 53-01 FIG 1 AND 51-30-1.Jul 28, 1998 · N912VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800374Splice · corrodedLONGERON 30 SPLICE CORRODED OUT OF LIMITS, STA 794-813. REMOVED SPLICE IAW SRM 51-30-2, REMOVED CORROSION IAW SRM 51-10-3, MATERIAL LOSS .030 IAW AERO CORP GAUGE NR A-2039, OUT OF LIMITS IAW SRM 53-01 FIG 1. SPLICE P/N 3914677-501N, DRILLED AND DEBURRED NEWJul 28, 1998 · N912VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800269Longeron · corrodedSPLICE CORRODED BEYOND LIMIT AT STA 794 TO 813, L30. REMOVED SPLICE AND CORROSION IAW DC9 SRM 51-30-2 AND 51-10-3. ORDERED NEW SPLICE, DRILLED, DEBURRED AND INSTALLED SPLICE IAW DC9 SRM 51-10-4, 51-30-5.Jul 28, 1998 · N912VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800280Angle · crackedSPAR CAP XRS AT INBRD FLAP HINGE STUD HOLE HAS A .25 INCH CRACK ON FWD FACE RUNNING VERTICALLY FROM TOP EDGE OF HOLE. FABRICATED ANGLE FROM 2024, 26 1/4 BY 3 INCHES. LOCATED AND DRILLED TWO OTHER ANGLES. INSTALLED REPAIRS IAW DC9 SRM 51-30-5 AND DWG J0602T1Jul 27, 1998 · N912VV · Doug DC932 · Wing Miscellaneous StructureSDR VJ9800376Longeron · corrodedLONGERON 30 SPLICE CORRODED STA 935-965. REMOVED 2 SPLICE CORRODED. REMOVED 32 .125 FORMED SECTION LONGERON CORRODED, FABRICATED NEW LONGERON FROM EXTRUSION S1242886, IAW SRM 53-02 FIG 15, DRILLED, TRIMMED AND DEBURRED LONGERON AND SPLICE REPAIRS IAW DC-9 SRJul 22, 1998 · N912VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800372Skin · corrodedCORROSION ON INNER SKIN UNDER LONGERON 28R STA 935. REMOVED LONG 28R AND INNER SKIN FOUND TO BE OUT OF LIMITS. FABBED NEW INNER SKIN 2024 T-3 .025 EXTERNAL SKIN CORROSION OUT OF LIMITS. FABBED REPAIR DOUBLER IAW AIRTRAN RES 981106.Jul 21, 1998 · N912VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800371Skin · corrodedCORROSION ON INNER SKIN STA 935 UNDER LONGERON 29R. REMOVED LONGERON 29R AND INNER SKIN FOUND CORROSION OUT OF LIMITS. FABBED NEW INNER SKIN FROM 2024 - T3 .025 EXTERNAL SKIN CORROSION OUT OF LIMITS, FABBED REPAIR DOUBLER IAW AIRTRAN RES 981106 AND INSTALLEDJul 21, 1998 · N912VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800253Skin · corrodedCORROSION ON INNER SKIN STA 935 UNDER LONGERON 29R. REMOVED LONG 29R AND INNER SKIN FOUND CORROSION OUT OF LIMITS. FABBED NEW INNER SKIN 2024-T3.025 EXTERNAL SKIN CORROSION OUT OF LIMITS FABBED REPAIR DOUBLER IAW AIRTRAN RES 981106 AND INSTALLED LONG 29R.Jul 21, 1998 · N912VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800252Skin · corrodedCORROSION ON INNER SKIN UNDER LONG 28R STA 935. REMOVED LONG 28R AND INNER SKIN FOUND CORROSION OUT OF LIMITS, FABBED NEW INNER SKIN 2024-T3.025. EXTERNAL SKIN CORROSION OUT OF LIMITS, FABBED REPAIR DOUBLER IAW AIRTRAN RES 981106 AND INSTALLED LONG. 28R.Jul 21, 1998 · N912VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800373Intercoastal · corrodedINTERCOASTAL STA 813-832 LONG 27L HAS CORROSION. REMOVED INTERCOASTAL AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1. FABBED NEW INTERCOASTAL 18.5 BY 5 USING 7075 -0 .040 IAW DC-9 SRM 53-11-3. HEAT TREATED IAW SRM 51-10-2A. TREATED AND PRIMED IAW SRM 51Jul 19, 1998 · N912VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800370Intercoastal · corrodedINTERCOSTAL STA 851-870 LONG 27L AND BUBBLED ON LONG. REMOVED INTERCOSTAL AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1. FABBED NEW INTERCOASTAL 18 1/8 BY 5 USING 7075-0-.050 IAW DC-9 SRM 51-10-2 AND 53-11 FIG 3A. HEAT TREATED IAW SRM 51-10-2A. TREATEDJul 19, 1998 · N912VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800254Intercostal · corrodedINTERCOSTAL STA 851-870 LONG 27L IS CORRODED AND BUBBLED ON LONGERON. REMOVED INTERCOSTAL AND FOUND TO BE OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1. FABBED NEW INTERCOSTAL 18 1/8X5 USING 7075-0.050 IAW SRM 51-10-2 AND 53-11 FIG 3A. HEAT TREATED IAW DC-9 SRM 51Jul 19, 1998 · N912VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800242Intercoastal · corrodedDURING C CHECK, FOUND INTERCOSTAL STA 813 - 832 27L HAS CORROSION. REMOVED INTERCOSTAL AND FOUND IT TO BE OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1. FABBED NEW INTERCOASTAL 18.5 X 5 USING 7075-0-.040 IAW DC-9 SRM 51-10-3. HEAT TREATED IAW DC-9 SRM 51-10-2A. TJul 19, 1998 · N912VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ970333Longeron · chafedSTATION 1019 FRAME CHAFED APPROXIMATELY .015 DEEP AT 14L. CUT OUT CHAFED AREA, INSTALLED FILLER AND DOUBLERS IAW SRM 53-03, FIG 4.Oct 24, 1997 · N912VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ970325Switch · failedON GEAR RETRACTION AFTER TAKEOFF, LT GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR DOOR LIGHT OUT. RECYCLED GEAR AND UNSAFE GEAR LIGHT REMAINED ON. AIRCRAFT LANDED NORMAL AND WITHOUT INCIDENT. REPLACED LT GEAR UPLOCK SWITCH. ACCOMPLISHED LANDING GEAOct 14, 1997 · N912VV · Doug DC932 · Landing Gear Position and WarningSDR VJ970282Lanyard · looseMAIN CABIN DOOR SLIDE PACK PIN NOT CONNECTED. REINSTALLED DOOR SLIDE LANYARD IAW MM 25-60.Jul 26, 1997 · N912VV · Doug DC932 · Emergency EquipmentSDR VJ970118Battery Charger · failedEMERGENCY PATH FLOOR LIGHTS BETWEEN SEAT ROWS 15-20 OUT. ALSO, LEFT SIDE INOP AFT ACCESSORY COMPARTMENT. REPLACED BATTRY CHARGER AT FUSELAGE STATION 936 AND REPAIRED WIRING TO CHARGER PER MM 33-53-0. OPS CHECKED GOOD. (M)Feb 18, 1997 · N912VV · Doug DC932 · Emergency LightingSDR 95ZZZM475Eel Wire · shortedAFT SECTION OF EPL'S AND TAIL COMPARTMENT EMERGENCY LIGHTS INOP. FOUND WIRING SHORTED BEHIND PANEL IN TAIL COMPARTMENT. REPAIRED WIRING AND REPLACED FUSES IN BATTERY CHARGER IAW MM CH 33.Aug 12, 1995 · N912VV · Doug DC932 · Emergency LightingSDR 95ZZZM375Eel · inopAFT SECTION OF EPL'S AND TAIL COMPARTMENT EMERGENCY LIGHTS INOP. FOUND WIRING SHORTED BEHIND PANEL IN TAIL COMPARTMENT. REPAIRED WIRING AND REPLACED FUSES IN BATTERY CHARGER IAW MM CH 33. (M)Aug 12, 1995 · N912VV · Doug DC932 · Emergency LightingSDR 95ZZZX3976Hyd Pump · failedFLT 574 - AFTER TAKEOFF, LEFT HYDRAULIC TEMP HIGH LIGHT CAME ON. AIRCRAFT RETURNED TO ATLANTA. REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP. P/N AS66411LS, S/N OFF 165614, S/N ON 179506. OPS CHECK GOOD, NO LEAKS FOUND IAW MM CHAPTER 29-10-5.Jul 20, 1995 · N912VV · Doug DC932 · Hydraulic Pump (Electric/Engine), Main
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