N9409F

Service difficulty reports · 124

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N9409F' AND registry_match = 'registration'
  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 TWAA0008808Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CABIN CORROSION ON FLOOR MEMBRANE AT LONGERON 18L, STA 560 TO 579 AND STA 541 TO 522. REMOVED CORROSION PER SRM 51-10-3. PRIMED PER 51-10-3. REPAIRED PER SRM 53-01 FIG 4 PAGE 18.May 26, 2000 · N9409F · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0008810Floorbeam · corrodedDURING CHECK-C MAINT, IN LT CABIN FOUND CORROSION ON FLOOR MEMBRANE AT LONGERON 18L STA 655 TO 674. REMOVED CORROSION PER SRM 51-10-3. PRIMED PER SRM 51-10-3B. INSTALLED FASTENERS PER SRM 51-10-05.May 25, 2000 · N9409F · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0008804Seat Track · gougedDURING CHECK-C MAINT, CHAIR TRACK HAD GOUGES AT STA 356 TO 389, RBL 22, AND AT STA 243 TO 313 RBL 22. REMOVED AND BLENDED GOUGES PER SRM 53-05, FIG 4B-1, AND SPM 6-80-01. PRIMED, SANDED AREA PER SRM 51-10-3.May 25, 2000 · N9409F · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0008811Splice Plate · crackedDURING CHECK-C MAINT, ON RT WING, WING STA 164 L/E SPLICE PLATE WAS CRACKED AT BOLT HOLE. EDDY CURRENT INDICATED CRACK FROM 1 HOLE THRU ANOTHER HOLE TO EDGE PER PART 6-57-00-03 OF NDT MANUAL. FABRICATED AND INSTALLED WING L/E DOUBLER AT WING STA 164, PER SSRMay 24, 2000 · N9409F · Doug DC983 · Wing, Plate/SkinSDR TWAA0008806Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON FLOOR MEMBRANE AT LONGERON 18L, STA 674 TO 693 AND STA 845 TO 826. REMOVED CORROSION PER SPM 6-80-01. TREATED SURFACES PER SRM 51-10-3.May 24, 2000 · N9409F · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0008805Seat Track · corrodedDURING CHECK-C MAINT, FOUND CORROSION IN CHAIR TRACK AT RBL 22 AT THE FOLLOWING STATIONS: 363 TO 368, 237, 530 TO 460, 427 TO 462, 408 TO 420, 636, 788, AND 484 TO 503. REMOVED CORROSION PER SRM 51-10-3, 53-05 FIG 4B-1, AND SPM 6-80-01. PRIMED PER SRM 51-10-May 23, 2000 · N9409F · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0008803Attach Angle · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON ATTACH ANGLE AT FLOOR LEVEL OF EPC PANEL, AFT SIDE, STA 160L. REMOVED CORROSION PER SPM 6-80-01, PAGE 1 ITEM 2(A).May 23, 2000 · N9409F · Doug DC983 · Fuselage Main, Attach FittingsSDR TWAA0008802Doubler · corrodedDURING CHECK-C MAINT, FOUND DOUBLER AT AFT CARGO DOOR STA 1300 TO 1231, LONGERON 29 TO 26R, WAS CORRODED. REMOVED CORROSION PER SPM 6-80-01, PAGE 1 ITEM 3, A, B PAGE 2 AND 3.May 23, 2000 · N9409F · Doug DC983 · Fuselage Main, StructureSDR TWAA0008714Web · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON FLOOR MEMBRANE AT STA 1212 TO 1231 AT LONGERON 18L. REMOVED DAMAGED SECTION OF MEMBRANE, AND INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3.May 23, 2000 · N9409F · Doug DC983 · Fuselage Miscellaneous StructureSDR TWAA0008306Skin · crackedDURING CC 8C, FOUND A CRACK IN THE LOWER FUSELAGE AT LT AND RT SIDES OF THE SUPPORT INTERCOSTAL AT STATIONS 988, 5 INCHES LT SIDE AND 5 INCHES RT SIDE OF LONGERON 30 BETWEEN THE AFT END OF THE MAIN GEAR. INSTALLED REPAIR PER SRM 51-01 PG 1, FABRICATED PART PEMay 19, 2000 · N9409F · Doug DC983 · Fuselage Main, Plate/SkinSDR TWAA0002102Lens · crackedEGRESS LIGHT LENS AT MID CABIN CLASS DIVIDER CRACKED. REPLACED LIGHT LENS AC 04 01/29/2000 JFK.Feb 5, 2000 · N9409F · Doug DC983 · Emergency LightingSDR TWAA9917303Light · disconnectedTHE EGRESS LIGHTING AT SEAT ROW 11 WAS DISCONNECTED. REPLACED BROKEN TRACK LIGHTING COVER AND RECONNECTED THE LIGHT. CHECK-C 5-18-99 STL.Dec 26, 1999 · N9409F · Doug DC983 · Emergency LightingSDR TWAA9913802Bulb · failedTHE CABIN EGRESS LIGHTS WERE INOPERATIVE AT ROW 2, 4, 10, AND 33. REPLACED LAMP AT EACH LOCATION. CHECK-C 5-18-99 STL.Oct 7, 1999 · N9409F · Doug DC983 · Emergency LightingSDR TWAA9904601Harness · wornTHE CABIN EGRESS LIGHTS TRACK COVERS WERE BROKEN AT ROWS 15 AND 16, CAUSING WIRES TO PULL OUT OF HARNESS. REPLACED HARNESS AND TRACK COVERS. CHECK-C 5-6-98 STL.Mar 25, 1999 · N9409F · Doug DC983 · Emergency LightingSDR TWAA9809501Cover · crackedSTL - FLT 74 - THE EMERGENCY FLOOR LIGHTING STRIP AT ROW 1 WAS FOUND BROKEN. REPLACED EMERGENCY FLOOR LIGHTING STRIP AT ROW 1. CHECK-C 5-6-98 STL. ACFTR TT: 15,970 HOURS. ACFT TC: 8,193. (X)Jun 14, 1998 · N9409F · Doug DC983 · Emergency LightingSDR TWAA9801102Engine · failedAM - FLT 1508 - DURING CRUISE, VIBRATION OCCURED ON THE LEFT ENGINE. ENGINE SHUT DOWN. REPLACED LEFT ENGINE DUE TO FAILURE CAUSED BY BLUE ICE. (M)Jan 19, 1998 · N9409F · Doug DC983 · Engine (Turbine/Turboprop)SDR TWAA9750005Slide · deployedSTL - FLT 422 - WHILE AIRCRAFT WAS PARKED AT GATE, A VENDOR INADVERTENTLY DEPLOYED L-1 DOOR EMERGENCY ESCAPE SLIDE, WHICH FUNCTIONED PROPERLY. REMOVED AND REPLACED L-1 DOOR SLIDE, MFG P/N 100504-201, MANUFACTURED BY BF GOODRICH CO. (M)Apr 18, 1997 · N9409F · Doug DC983 · Escape SlideSDR 96ZZZX4917Bearing · failedSTL - FLT 315 - INVESTIGATION OF NR 2 ENGINE, S/N 1213, SHUT DOWN DUE TO VIBRATION REVEALED THE NR 3 BEARING, MFG P/N 804061, RIVETS FRACTURED LIBERATING METAL PARTICLES INTO OIL SYSTEM. THE NR 3 BEARING WAS REPLACED AND ENGINE REPAIRED AND RETURNED TO SERVICJul 20, 1996 · N9409F · Doug DC983 · Turbine Engine Compressor SectionSDR 96ZZZM1222Engine · failedSTL - DURING DESCENT, SHUT DOWN NR 2 ENGINE, S/N 1213, DUE TO VIBRATION AND OIL FILTER BYPASS LIGHT ILLUMINATION. FOUND METAL PARTICLES ON OIL SYSTEM CHIP DETECTORS. REPLACED ENGINE, ENGINE OPERATION THEN CHECKED NORMAL. ENGINE TOTAL TIME 22,333, ENGINE TOTJul 20, 1996 · N9409F · Doug DC983 · Engine (Turbine/Turboprop)SDR 96ZZZX2549Control Valve · failedSTL - FLT 463 - DURING CRUISE, AIRCRAFT CABIN PRESSURIZATION BLED OFF. REMOVED AND REPLACED NR 2 PACK FLOW CONTROL VALVE, MFG PN 396130-1-1. OPERATIONAL CHECK AND LEAK CHECK NORMAL. CHECK C-1D - 5-18-95 - MCI.Apr 28, 1996 · N9409F · Doug DC983 · Cabin Cooling SystemSDR 96ZZZM56Engine · bird strikeFLT NR 312 - SMF - AFTER TAKEOFF, SMOKE EMITTED INTO CABIN. FLIGHT RETURNED. FOUND RIGHT ENGINE HAD INGESTED A BIRD. REPLACED RIGHT ENGINE, S/N 3256. ENGINE OPERATION AND AIR CONDITIONING SYSTEMS OPERATION CHECKED NORMAL.Dec 4, 1995 · N9409F · Doug DC983 · Engine (Turbine/Turboprop)SDR 95ZZZX6970Coalescer Bags · contaminatedSTL - FLT 176 - DURING CRUISE, EXPERIENCED SMOKE IN CABIN AND COCKPIT. TURNED OFF RIGHT SUPPLY HIGH PRESSURE BLEED AIR, SMOKE DISSIPATED. FOUND WATER SEPARATOR COALESCERS OIL CONTAMINATED, MFG PN 179460-8-1. REPLACED WATER SEPARATOR COALESCERS AND AIR CONDINov 13, 1995 · N9409F · Doug DC983 · Humidity Control SystemSDR 95ZZZX6800Oil · overservicedIND - FLT 444 - DURING CRUISE, SMOKE STARTED ENTERING CABIN. DESCENDED TO 8,000 FEET. FOUND APU OIL OVERSERVICED. SERVICED APU TO PROPER LEVEL AND REPLACED BOTH COALESCER BAGS, MFG P/N 22D10. AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL. CHECK C-1A - Oct 3, 1995 · N9409F · Doug DC983 · APU Oil SystemSDR 95ZZZX6799Structure · lightning strikeSTL - FLT 464 - DURING CRUISE, EXPERIENCED A POSSIBLE LIGHTNING STRIKE WITH ACCOMPANYING AIR NOISE AND SMOKE IN THE CABIN. ALL OPERATIONS AND INDICATIONS WERE NORMAL. PERFORMED LIGHTNING STRIKE/STATIC DISCHARGE CONDITION CHECK. CHECKED NR 1 ENGINE FOR POSSISep 29, 1995 · N9409F · Doug DC983 · Aircraft Structures
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