N169FE, cancelled Jun 7, 2004
Service difficulty reports · 42
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 = 'N169FE' AND deregistration_id = 'N169FE-2004-06-07' 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.
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 = 'N169FE' AND deregistration_id = 'N169FE-2004-06-07' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 02FDEA00290Hydraulic Line · leakingHYDRAULIC A-QTY TO ZERO IN FLT. REMOVED AND REPLACED NR 1 ENG A-SYSTEM HYDRAULIC PRESS LINE. REMOVED AND REPLACED 1 & 2 ENGINE HYD PUMP CASE DRAIN FILTERS PER MM 29-11-041-2.SDR 00FDEA00887Sensor · failed00-366 AFT T/O STICK SHAKER ACTIVATED. PULLED AC STALL WARN NR 1 CIRCUIT BREAKER & RETURN FOR LAND. R&R RIGHT ANGLE OF ATTACK SENSOR IAW 727 MM 34-18-51, NR 1 STALL WARNING SYS OPERATIONAL CHECK NORMAL IAW 727 MM 34-18-0. OK TO CONTINUE.SDR 98FDEA00612Floorbeam · corrodedBS 680 CORROSION ON BOTTOM SIDE OF FLOORBEAM LWR FLANGE AT SEV AREAS. BLENDED OUT CORROSION PER EA 7-5310-29662 DATED 9-14-98. INSTALLED .071 7075-T6 ANGLES ON FWD AND AFT FLANGES PER AARD 53-10-7-2 AND EA 7-5310-29662.SDR 98FDEA00611Frame · crackedAFT CARGO FWD DOOR PORTAL FRAME CRACKED AT LOWER FWD DOOR STOP, OUTBD LWR FAST. REMOVED AND REPLACED AFT CARGO FWD DOOR PORTAL FRAME PER SRM 51-10-1.SDR 98FDEA00610Skin · corrodedCORROSION ON FUSELAGE SKIN 25 PERCENT LOBE OF MATERIAL BETWEEN STR 25R-26R, BS 360. CUT OUT CORROSION, INSTALLED DOUBLER AND FILLER ON OUTSIDE OF SKIN EXTENDING 3 ROWS BELOW SKIN LAP PER EA 7-5330-29666. DATED 9/18/98 AND SRM 53-30-3.SDR 98FDEA00609Floorbeam · damagedUPPER LOBE FLOORBEAM HAS DOUBLER DRILL HOLE BS 990. CUT OUT DAMAGE, INSTALLED DOUBLER PER AARD 53-10-07-02 AND EA 7-5310-29648.SDR 98FDEA00608Floorbeam · damagedCABIN FLOORBEAM HAS ONE DOUBLE DRILL HOLE BS 1010, RBL 63. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-07-02 FIG 3 AND EA 7-5310-29648.SDR 98FDEA00607Floorbeam · damageFLOORBEAM CUT ACROSS TOP FLANGE BS 1130, RBL 63. BLENDED OUT DAMAGE AND INSTALLED .080 STRAP OF 7075-T6 ALUM PER AARD 53-10-07-01 AND 7-5310-29698.SDR 98FDEA00606Floorbeam · damagedCABIN FLOORBEAM CUT ACROSS TOP FLANGE BS 1050, RBL 63. CUT OUT DAMAGE, INSTALLED DOUBLER PER AARD 53-10-07-02 AND EA 7-5310-29648.SDR 98FDEA00605Floorbeam · damagedCABIN FLOORBEAM CUT ACROSS TOP FLANGE AT STR 970, RBL 63. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-07-02 AND EA 7-5310-29648.SDR 98FDEA00603Floorbeam · corrodedUPPER LOBE, BS 1050 HEAVY CORROSION ON LWR FWD LEG OF FLOORBEAM AT LBL 29. BLENDED OUT CORROSION IN AREA NOTED PER SRM 51-10-6. BLENDED AREA OUT OF LIMITS. CUT OUT DAMAGE AND INSTALLED DOUBLER ON FLOORBEAM PER AARD 53-10-07-2.SDR 98FDEA00613Floorbeam · corrodedAFT CARGO FLOORBEAM BS 1050, LWR CHORD HAS CORROSION FROM RBL 24- RBL 43. INSTALLED FLOORBEAM REPAIR LWR CHORD PER SRM 53-10-8 PG 11-17.SDR 98FDEA00602Floorbeam · corrodedUPPER LOBE HEAVY CORROSION ON UPPER SURFACE OF LWR FLANGE OF FLOORBEAM BS 1050, RBL 39. INSTALLED FLOORBEAM LWR CHORD REPAIR PER SRM 53-10 8 PG 11-17.SDR 98FDEA00601Floorbeam · misdrilledUPPER LOBE FLOORBEAM BS 1070, RBL 625 HAS DOUBLE DRILL HOLE IN FLOORBEAM. CUT OUT AREA OF DAMAGE AND REPAIR PER AARD 53-10-07.SDR 98FDEA00559Floorbeam · corrodedNR 0936 - UPPER LOBE, FLOORBEAM BS 680 CORROSION ON UPPER FLANGE LBL 10- RBL 6. CORROSION REMOVAL OUT OF LIMITS AT LBL 5 FWD SIDE OF FLANGE. INSTALLED ANGLE DOUBLER PER AARD 53-10-07-2.SDR 98FDEA00557Skin · damagedNR 0698 - LFEC IND 10 PERCENT MATERIAL LOSS JUST ABOVE STR 23 LT, 2 AFT OF BS 360 FRAME. DAMAGED AREA, REMOVED AND REPLACED DOUBLER INSTALLED PER SRM 53-30-3 PG 14B-14D.SDR 98FDEA00556Skin · corrodedNR 0342 - UPPER LOBE BS 886 HEAVY CORROSION AT WINDOW BELT AND ON SKIN 8 ABOVE STR 14L. REMOVED CORROSION FRAME WAS TAKEN OUT OF LIMITS. WINDOW FRAME REPLACED FOR EA 7-5330-29636 AND SRM 51-30-2 DOUBLER INSTALL PER EA 7-5330-29636.SDR 98FDEA00549Skin · damagedLOW FREQ EDDY CURRENT IND 15 PERCENT MATERIAL LOSS BS 360 AFT FASTENER ROW STR 4 RT BOTTOM OF SKIN LAP TO ONE INCH BELOW. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 5.SDR 98FDEA00550Floorbeam · corrodedUPPER LOBE BS 380 HEAVY CORROSION ON FLOORBEAM AT LBL 34. REMOVED CORROSION PER SRM 51-10-6. CORROSION REMOVAL OUT OF LIMITS. INSTALLED REPAIR PER AARD 53-10-07-2 PG 1 AND 2 FIG 3.SDR 97FDEA00299Engine · failedPASSING 16,000 FEET ON DESCENT POWER AT IDLE, NR 2 ENGINE FLAMED OUT. ONLY ABNORMAL INDICATION WAS ZERO OIL PRESSURE. QUANTITY OK WITH N1 ROTATION. NO N2 WAS OBSERVED. FOUND OIL SCREEN FULL OF METAL. REMOVED AND REPLACED NR 2 ENGINE PER WORK CARD 70T0502 ASDR 96FDEA00194Fitting · crackedCRACK IN HOLES NR 2 AND NR 4 OF ROW 2, FWD O/B FLANGE, AT BS 870 JUST BELOW STR 9R. REPAIRED CRACK IN HOLES NR 2 AND NR 4 OF ROW 2 FWD O/B FLANGE, AT BS 870 JUST BELOW STR 9R PER FEDEX EA 7-5310-26957.SDR 96FDEA00193Skin · corrodedCORROSION ON SKIN INTERIOR AT BS 875 TO 878 BELOW STR 9R. REPAIRED CORROSION ON INTERIOR SKIN AT BS 875 TO 878 BELOW STR 9R PER FEDEX EA 7-5310-26957.SDR 96FDEA00192Fitting · crackedDURING UT INSPECTION, CRACK INDICATION FOUND AT FUSE BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6. REPAIRED CRACK AT BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6 PER FEDEX EA'S 7-5310-26957 AND 7-5310-26913.SDR 96FDEA00183Stiffener · corrodedCORROSION (C53-224-03-1/2), ON VERTICAL STIFFENER BS 336 WL 181 RBL 15. REMOVED CORROSION AND INSTALLED REPAIR IAW FEDEX SRM 51-40-4.SDR 96FDEA00182Stiffener · corrodedCORROSION (C53-111-03-1/2), ON VERTICAL STIFFENER BS 319 WL 181 RBL 15. REMOVED CORROSION AND INSTALLED REPAIR IAW FEDEX SRM 51-40-4.SDR 96FDEA00167Fitting · crackedCRACK IN AFT FLANGE OF TERMINAL FITTING AT BS 870 STR 13R. HFEC DAMAGE FABRICATED REPAIR PARTS AND INSTALLED PER EWO NR 96-2-43.SDR 96FDEA00157Rib · corrodedCORROSION ON NR 6 K-FLAP MOST OUTBOARD RIB WHERE LANDING LIGHT CONDUIT ATTACHES TO RIB UPPER BOLT HOLE. REMOVED CORROSION, REPAIRED PER EWO NR 96-2025.SDR 96FDEA00156Hinge · corrodedRIGHT WING OUTBOARD AILERON INBOARD HINGE FITTING IS CORRODED (NR 2 HINGE FITTING). REMOVED CORROSION, FABRICATED REPAIR ANGLE ON FLANGE ON RIGHT WING OUTBOARD AILERON HINGE FITTING IAW FEDEX EA 7-5750-26969.SDR 96FDEA00155Skin · dentedDENT TO SKIN DUE TO TOOL BOX AT STA 1083 AND BETWEEN STR 28 - 29L. REPAIRED DAMAGED SKIN AT BS 1083, BETWEEN STR 28 - 29L PER FEDEX SRM 53-30-3 PER ENGINE REPAIR REQUEST REPLY. MFG PART NUMBER M502776.SDR 96FDEA00137Fitting · corrosionCORROSION ON STR TO FRAME TIE AT BS 360 STR 20L. REMOVED AND REPLACED STR TIE AT BS 360 20L, DUE TO CORROSION OUT OF LIMITS.SDR 96FDEA00136Fitting · crackedLT VERTICAL FIN FRONT SPAR TERMINAL FITTING FWD O/B FLANGE IS CRACKED. REPAIRED LT VERTICAL FIN FRONT SPAR TERMINAL FITTING FWD O/B FLANGE IAW FEDEX EA 7-5510-26907.SDR 96FDEA00135Stringer · delaminationDELAMINATION OF SKIN LAP STRINGER 19L BS 360 TO 368. REMOVED FASTENERS IN SKIN LAP AT STR 19L. UPON REMOVAL OF FASTENERS FOUND NO FURTHER INDICATIONS OF DELAMINATION. INSTALLED NEW STR TIE AND INSTALLED STR 19 SPLICE. ALL WORK DONE IAW FEDEX SRM 53-10-3.SDR 96FDEA00077Fitting · crackedDURING UT INSP, CRACK IND FOUND AT FUSE BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6. REPAIRED CRACK AT BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6 PER FEDEX EA'S 7-5310-26957 AND 7-5310-26913.SDR 96FDEA00076Fitting · crackedCRACK IN AFT FLANGE OF TERMINAL FITTING AT BS 870 STR 13R. HFEC DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER EWO NR 96-2043.SDR 96FDEA00075Skin · lightning strikeLIGHTNING STRIKES AT BS 706, 793, 824 AND 888 BETWEEN STR 4 AND 5. REPAIRED LIGHTNING STRIKES AT BS 750, 793, 824 BY INSTALLING NEW FASTENERS. REPAIRED BS 888 BY CUTTING OUT DAMAGED AREA AND FABRICATING REPAIR PARTS. INSTALLED IAW 53-30-3.SDR 96FDEA00074Skin · chafingRT WING I/B FOREFLAP IS CHAFING APPROX 24 INCHES O/B FROM I/B LEADING EDGE. REPAIRED DAMAGE AREA ON RT WING I/B FOREFLAP APPROX 24 INCHES O/B FROM I/B LEADING EDGE.SDR 96FDEA00078Skin · corrodedCORROSION ON SKIN INTERIOR AT BS 875 TO 878 BELOW STR 9R. REPAIRED CORROSION ON INTERIOR SKIN AT BS 875 TO 878 BELOW STR 9R PER FEDEX EA 7-5310-26957.SDR 96FDEA00067Te Skin · disbondedRIGHT WING INBD FORE FLAP UPPER SURFACE HAS DISBOND ON T/E AREA MARKED. REPAIRED RT WING INBOARD FORE FLAP IAW SRM 51-40-6.SDR 96FDEA00066Stringer · corrodedCORROSION (C53-224-03-1/2) ON STR 22R, BS 396. REMOVED CORROSION AT BS 396, STR 22R. REMOVED IN A 1 INCH BY 2 INCH AREA. ORIGINAL METAL THICKNESS IS .040 INCH. REMOVED .009 INCH, FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. FABRICATED AND INSTALLED RESDR 96FDEA00065Stiffener · corrodedCORROSION (C53-111-03-1/2), ON VERTICAL STIFFENER BS 319 WL 181 RBL 15. REMOVED CORROSION AND INSTALLED REPAIR IAW FEDEX SRM 51-40-4.SDR 96FDEA00060Skin · gougedTHERE'S A GOUGE ON THE RT WING FOREFLAP UPPER SURFACE ABOVE THE NR 8 FLAP TRACK. REMOVED AND REPLACED DAMAGE ON O/B RT WING FOREFLAP IAW FEDEX SRM 51-40-6.SDR 96FDEA00064Stiffener · corrodedCORROSION (C53-224-03-1/2), ON VERTICAL STIFFENER, BS 336 WL 181 RBL 15. REMOVED CORROSION AND INSTALLED REPAIR IAW FEDEX SRM 51-40-4.
Back to N169FE, cancelled Jun 7, 2004