N199FE
Service difficulty reports · 16
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 = 'N199FE' 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 = 'N199FE' 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 FDEA202510061902Skin · crackedLOOSE FASTENERS ON UPPER SURFACE SKIN, LOCATED AT 16.5" TO 30" FROM OUTBOARD EDGE OF SLAT 10. THE DAMAGE ON UPPER SURFACE SKIN LOCATED AT 16.5" TO 30" FROM OUTBOARD EDGE OF SLAT 10 WAS REPAIRED IAW E.A. # H-5750-T0385148 PART 1 (P1) RELEASE DATE OCT 05, SDR FDEA202509271840Skin · dentedDENT ON INBD AFT FLAP WS 420 EXTERNAL SURFACE AT LH WING ON INBD AFT FLAP WS420 EXTERNAL SURFACE AT LH WING WAS EVALUATED AND REQUIRED REPAIR I.A.W SRM B767 57-53-01-2R FIG.201 SHEET 4 REV. 92 APR 15,2025 AND REPAIR I.A.W SRM B767 51-70-10-2R FIG 201 SHEETSDR FDEA202509241798Skin · dentedDENT ON SLAT WEDGE UPPER SKIN LOCATED AT 42'' FROM INBOARD EDGE AND 5.5'' FROM AFT EDGE SLAT 1 DENT ON SLAT 1 T/E WEDGE UPPER SKIN LOCATED AT 42'' FROM INB EDGE AND 5.5'' FROM AFT EDGE OF SLAT, WAS REPAIRED IAW B767 SRM 57-43-02-2R REPAIR 1 FIG 201 SHEET SDR FDEA202509241797Floor Panel · crackedPUNCTURE ON FLOOR PANEL 251EFF. MDC AREA FLOOR PANEL 251EFF MDC AREA WAS REPAIRED IAW SRM 53-00-50-2R PAR 4B FIG 201, SHEET 2, REV 92, APR 15/25.SDR FDEA202509241796Floor Panel · crackedPUNCTURE ON FLOOR PANEL 241DFF ON MDC FLOOR PANEL 241DFF ON MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201, SHEET 2, REV 92 APR 15/25.SDR FDEA202509241795Floor Panel · crackedPUNCTURE ON FLOOR PANEL 251XFF. MDC AREA FLOOR PANEL 251XFF MDC AREA WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 92 APR 15/2025SDR FDEA202509231774Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 252HFF. MDC FLOOR PANEL 252HFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 92 APR 15/2025SDR FDEA202509231773Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 251PFF. MDC AREA FLOOR PANEL 251PFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 92 APR 15/2025SDR FDEA202509231772Floor Panel · crackedPUNCTURE ON FLOOR PANEL 251KFF. MDC AREA FLOOR PANEL 251KFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 92 APR 15/2025SDR FDEA202501240132Indicator · failedTRAILING EDGE ASYMMETRY INDICATION AFTER FLAPS SET TO 25. L FLAP INDICATION 25. R FLAP INDICATION 19. NO EICAS OR OTHER ANNUNCIATION. AMM: 27-58-02-4-0 AMM: 27-58-00-5-0 REMOVED AND REPLACED SUSPECTED FAULTY FLAP POSITION INDICATOR WITH SERVICABLE FLASDR FDEA202410301619Outflow Valve · failedFWD EQPT VAL EICAS MESSAGE IN CRUISE AT FL370. PERFORMED CHECKLIST NON-NORMAL PROCEDURES. VALVE LIGHT REMAINED ON. DESCENDED TO 10000FT. EMERGENCY DECLARED. FACT 30OCT24 17:29 MEM AMM: 21-58-05-4 FIM: 21-58-00-2 T/S PER FIM. PERFORMED FWD EQP VALVES SDR FDEA202402110153Idg · failedAPPROXIMATELY 2 20 INTO THE FLIGHT WE FELT THE AIRPLANE SHUDDER AND SAW EICAS MESSAGES: L & R UTILITY BUS. RAN QRH AND COMPLIED WITH CHECKLIST. AFTER SEVERAL MINUTES WE NOTICED THE APU HAD SHUT DOWN. DUE TO LOWER WEATHER IN BNA CONTINUED TO MEM. EMERGESDR FDEA202309301670Elevator · delaminatedRH ELEVATOR IS MISSING PLIES ON UPPER SURFACE L/E MIDDLE I/B AREA REPAIRED RH O/B ELEVATOR UPPER SKIN AT STA 163.74 IAW FEDEX EA H-5520-T0376409SDR FDEA202309281667Bracket · crackedLEFT WING L/E CAVITY LOCATED APPROX IFSS 280, TORQUE TUBE SUPPORT BRACKET CRACKED REMOVED AND REPLACED LEFT WING IB L/E TORQUE TUBE SUPPORT BRACKET IAW BAC DWG 114T1240, REV -SDR FDEA202309281665Seal · crackedRIGHT WING FIXED L/E INNER LIPS AREA UNDER LIGHTNING HOLE, STRAP CRACKED AT LES 510 REMOVED AND REPLACED R/W FIXED INNER SEAL STRIP AT LES 510 IAW BAC DWG 114T2800, REV A AND B767 SRM 51-40-02SDR FDEA202210062501Former · crackedLH WING HAS A CRACKED LEADING EDGE FORMER AT SLAT #5 INBOARD TRACK AREA REPLACED PARTS WITH NEW FORMER B67-57-002-01 ALONG WITH ANGLE B67-57-003-02 ON LS FOR FLE OSS 441, ATTACH FORMER THROUGH SKIN AND REPLACE ALL LOOSE FASTENERS ON FLEÏ¿½S. WITH SCREWS AN
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