N691FE
Service difficulty reports · 71
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 = 'N691FE' 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.
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 = 'N691FE' AND registry_match = 'registration' 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 FDEA201108103197Skin · chafedLT WING OTBD FLAP UPPER T/E SKIN HAS 2 EA CHAFE MARKS AS FOLLOWS 2" OTBD OF RIB 15 MEASURING 1.7" X .3" X .002 AND AT RIB 4 MEASURING .3 X .2 X .002. COMPLIED WITH EA 6-5750-145653. R & R RUB STRIPS INBD AND OTBD.SDR FDEA201108103189Skin · dentedRT WING NR 1 SLAT L/E UPPER SKIN HAS A DENT APPROX 1.5" LONG X 1" WIDE X 0.030" DEEP. BETWEEN RIB NR 2 AND RIB NR 3. REF SDR 11-3036 ISSUED ON NON ROUTINE N00140 GENERATED EA 6-5750-145656 ISSUED FOR TRACKING PUPPOSES IAW GMM 11-0-2700.SDR FDEA201108093152Channel · damagedLT MAIN CARGO DECK SIDEWALL ATTACH CHANNEL HAS 3 EA BROKEN SUPPORT BRACKETS AT APPROX 16/17, 1 AT FRAME 58 AND 1 BETWEEN FRAME 58 AND 59 ZONE 250. FABRICATED 3 BRACKETS IAW DWG A25576031, A25576802, A25576860 AND INSTALLED.SDR FDEA201108063126Skin · gougedRIGHT WING T/E FLAP UPPER EXTERIOR SKIN HAS A GOUGE APPROX. 1" LONG AND .006 DEEP AT RIB 14A. CUT OUT DAMAGED AREA, INSTALLED REPAIR IAW SRM 57-50-00.SDR FDEA201107313047Panel · delaminatedPANEL 577AB HAS SEVERAL AREAS OF DELAMINATION. RECEIVED PART AND INSTALLED PANEL 577AB IAW AMM 53-15-63-04.SDR FDEA201107303041Angle · gougedRT WING FIXED T/E STRUCTURE, RIB LOWER ANGLE GOUGED ABOVE INBD FLAP OTBD GUIDE ROLLER. R & R BOTTOM ANGLE ON RT OUTER SHROUD BOX AT INNER FLAPS OUTER ROLLER GUIDE IAW SRM 51-72-10, SRM 51-40-21.SDR FDEA201107303039Plate · crackedNR 2 PYLON OTBD SIDE FISH PLATE AT RIB 3 CRACKED. REMOVED FISH PLATE NR 2 PYLON OTBD RIB 3A IAW SRM 51-40-21, PARA 6. FABRICATED NEW FISHPLATE IAW DWG A54612371. INSTALLED NEW FISHPLATE NR 2 PYLON OTBD RIB 3A IAW FREIGHTER SRM 51-40-21, PARA 6.SDR FDEA201107303036Skin · dentedRIGHT WING NR1 SLAT L/E UPPER SKIN HAS A DENT APPROX 1.5" LONG X 1" WIDE X 0.030" DEEP BETWEEN RIB NR 2 AND RIB NR 3. FOUND DENT TO BE OUT LIMITS IAW SRM 57-40-00. REMOVED DAMAGED AREA OF NR1 SLAT L/E ON LT WING IAW SRM 57-42-11, FIG 201, PAR A 3 (A). NDT VSDR FDEA201107293030Attach Fitting · damagedAFT CARGO COMPARTMENT FR 69 10", STRINGER 51RT, WIRE ATTACH CLIP IS BROKEN. R & R ATTACH CLIP IAW SRM 51-72-10.SDR FDEA201107283009Support Bracket · crackedMDCC AT FR 54.2 BELOW SEAT TRACK 6 LT BLEED AIR DUCT SUPPORT BRACKET CRACKED APPROX 1 INCH LONG. R & R BLEED AIR DUCT SUPPORT BRACKET BELOW SEAT TRACK 6 LT AT FR 54.2 IAW SRM 51-72-10.SDR FDEA201107283007Bracket · chafed1 ENG INBD THRUST REVERSER LOWER HARD MOUNTED PANEL ON L/E HAS PANEL LAND FOR T/R. LATCH PANEL CHAFED ON AFT END. R & R PART IAW SRM 51-40-21.SDR FDEA201107283006Fitting · gougedNR 2 ENG OTBD THRUST REVERSER FWD LWR BUMPER FITTING GOUGED IN 2 EA AREAS. MEASUREMENTS ARE APROX .4 X .3 X .10D AND .35 X .15 X .050D. R & R BUMPER FITTING AT NR2 ENG OTBD THRUST REVERSER FWD LWR IAW MRA CMM 78-32-11 AND 78-32-00.SDR FDEA201107262987Stiffener · bentMDCC HAS 1EA BENT STIFFENER FR48 BETWEEN SEAT TRACKS 1 AND 2 LT DEFECT MEASURES 8" LONG REF; AMM 53-10-00-6. R & R STIFFENER IAW SRM 51-72-10.SDR FDEA201107262986Stiffener · bentMDCC STIFFENER BETWEEN 1 AND 2 SEAT TRACKS AT FRAME 48 IS BENT. DEFECT MEASURES 10" LONG REF; AMM 53-10-00-6. R & R STIFFENER IAW SRM 51-72-10, PG 1-3.SDR FDEA201107262985Stiffener · bentMDCC HAS 1EA BENT STIFFENER AT FR 50 BETWEEN SEAT TRACK 1 AND 2 RT DEFECT MEASURES 4" REF AMM 53-10-00-6. R & R STIFFENER IAW SRM 51-72-10, PG 1-3.SDR FDEA201107262984Stiffener · bentMDCC HAS 1EA BENT STIFFENER AT FR. 49 BETWEEN SEAT TRACK 1 AND 2 RT DEFECT, 12" LONG REF AMM 53-10-00-6. R & R CROSSBEAM STIFFENER AT FR 49 BETWEEN SEAT TRACKS 1 AND 2RT IAW SRM 51-72-10,PG 1-3.SDR FDEA201107222898Seat Track · gougedSEAT TRACK R-2 BETWEEN FRAME 57 AND 57.1 HAS A .25 INCH GOUGE IN SCALLOP. REMOVED AND REPLACED WITH NEW SEAT TRACK MATERIAL IN CONJUNTION WITH NON ROUTINE N00415. IAW SRM 53-10-16 FIG. 201.SDR FDEA201107222897Seat Track · gougedSEAT TRACK R-2 BETWEEN FRAME 57.1 AND 57.2 HAS A .37 INCH GOUGE AT SCALLOP. REMOVED AND REPLACED WITH NEW SEAT TRACK MATERIAL IN CONJUNTION WITH NON ROUTINE N00415. IAW SRM 53-10-16 FIG. 201SDR FDEA201107222903Floor Panel · damagedFLOOR PANEL 251BJ HAS 1EA CORNER BROKEN 3 X 3 FABRICATED REPLACEMENT PANEL 251BJ IAW DWG SR2 25-005.SDR FDEA201107222901Floorboard · crackedFLOORBOARD 241RJ BROKEN IN HALF FABRICATED REPLACEMENT PANEL 241RJ IAW DWG SR2 25-5 REV J WO 52630SDR 08FDEA00368Valve · inoperativeIN PREPARATION FOR APPROACH INTO KBUR, WHEN AUTOBRAKES WERE SELECTED IN LOW OR MED THE AUTOBRAKE FAULT LIGHT ILLUMINATED (PREVIOUS WRITE UP). CONTACTED GOCC AND DIVERTED TO KLAX FOR MAINTENANCE. FOUND GROUND AT PIN B AT THE VALVES. REMOVED AND REPLACED 89GG
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