N152FE
Service difficulty reports · 25
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 = 'N152FE' 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 = 'N152FE' 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 FDEA202507211280Actuator · failedPER FTAM PG 4-31 ALTERNATE LANDING GEAR EXTEND . WHILE ACTIVATING THE ALT GEAR EXTEND SWITCH, THE ALT GEAR FAILED TO EXTEND. FLIGHT TEST LANDING GEAR ALTERNATE SYSTEM WAS TESTED, BOTH TEST WERE SATISFACTORY IAW AMM 32- 32-00-705-001 AND AMM 32-35-00-7SDR FDEA202507081141Skin · damagedDENT ON INBOARD AFT FLAP, INNER SURFACE LH WING INBOARD AFT FLAP, INNER SURFACE LH WING WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 SHEET 4 DETAIL III NOTE A, SRM 51-70-10-2R REPAIR 4 FIGURE 201 SHEET 1 AND SRM 51-70-03-0G PARAGRAPH 5L FIGURE 16 SHEET 1SDR FDEA202507041119Floor Panel · damagedMDC FLOOR PANEL 251QFF WITH HOLE MDC FLOOR PANEL 251QFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R, FIG 201 SHEET 2, PAR 4.C REV 92 APR-15-2025SDR FDEA202507041118Floor Panel · damagedMDC FLOOR PANEL 241EFF WITH HOLE MDC FLOOR PANEL 241EFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R, FIG 201 SHEET 2, PAR 4.C REV 92 APR-15-2025SDR FDEA202507041117Floor Panel · damagedMDC FLOOR PANEL 232NFF WITH HOLE MDC FLOOR PANEL 232NFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R, FIG 201 SHEET 2, PAR 4.C REV 92 APR-15-2025SDR FDEA202507041116Floor Panel · crackedMDC SECTION 45 FLOOR PANEL 241WFF WITH CRACK MDC SECTION 45 FLOOR PANEL 241WFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R, FIG 201 SHEET 2, PAR 4.B REV 92.0 APR-15-2025.SDR FDEA202507041115Floor Panel · crackedMDC SECTION 45 FLOOR PANEL 241YFF WITH SEVERAL CRACKS MDC SECTION 45 FLOOR PANEL 241YFF, WAS REPAIRED I.A.W B767 SRM 53-00-50-2R, FIG 201 SHEET 2, PAR 4.B REV 92.0 APR-15-2025SDR FDEA202403240376Rib · damagedL/H TRI RIB ASSY, 2 EA. DAMAGED HOLES IN RIB 114T2500-5 FROM BOLTS IN STOP BEING SHEARED OFF. **SDR ENTERED IN ERROR** **SDR ENTERED IN ERROR**SDR FDEA202307251293Skin · gougedGOUGE ON LH FUSELAGE SKIN AT STA 1848.35 AND LBL 9.25 LH UPPER FUSELAGE SKIN AT STA 1848.35 AND LBL 9.25 WAS REPAIRED IAW E-A,#: H-5330- T0375329SDR FDEA202307241283Unknown · unknownRUDDER TRAILING EDGE UPPER TIP WITH LIGHTNING STRIKE. RUDDER TRAILING EDGE UPPER TIP DAMAGE WAS REMOVED IAW B767 SRM 55-40-30-1A FIG.101 NOTE B DETAIL V,X PAG 1-5 REV.86 APR/15/2023.SDR FDEA202307191251Flap · dentedLH WING, OUTBOARD FLAP, LOWER SURFACE, NEAR OF OUTBOARD TRACK WITH DENT. LH WING, OUTBOARD FLAP, LOWER SURFACE, WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG.201 SHEET 3 REPAIR 1 AND SRM 51-70-10-2R REPAIR 4 FIG.201 SHEET 2 REV.86 APR 15/23SDR FDEA202307191250Floor Panel · dentedMDC FLOOR PANEL 221DFF WITH DENTS. MDC FLOOR PANEL 221 DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022SDR FDEA202307191249Floor Panel · dentedMDC FLOOR PANEL 222CFF WITH DENTS. MDC FLOOR PANEL 222 CFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022SDR FDEA202307191248Floor Panel · dentedMDC FLOOR PANEL 222AFF WITH DENTS. MDC FLOOR PANEL 222 AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022SDR FDEA202307191247Floor Panel · dentedMDC FLOOR PANEL 222BFF WITH DENTS. MDC FLOOR PANEL 222 BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022SDR FDEA202307191246Floor Panel · dentedMDC FLOOR PANEL 221CFF WITH DENTS. MDC FLOOR PANEL 221 CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022SDR FDEA202307191245Floor Panel · dentedMDC FLOOR PANEL 221CFF WITH DENTS. MDC FLOOR PANEL 221 CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022SDR FDEA202303010358Fan · failedFWD EQ EXH FAN STATUS MESSAGE DURING CLIMB. CREW DETECTED A BURNING SCENT PRIOR TO THE MESSAGE BUT WENT AWAY IMMEDIATELY AFTER STATUS MESSAGE APPEARED. AMM: 21-58-06 PER FIM 21-58-00 TREE 992 & AMSDR FDEA202302160339Skin · failedE.A.#:H-5330-T0372987 REPAIR FOR DAMAGE TO FORWARD WING-TO-BODY FAIRING AND SKIN, R/H SIDE, STA 698-720, STR 31-32R. COMPLY WITH E..A. H-5330-T0372987 REV NO: A PS P2 EA H-5330-T0372987 REV NO, P2 WAS SUPERSEDED BY EA H-5330-T0372987 REV A, P2. COMPLIED WSDR FDEA202206131425Static Inverter · failedDURING EICAS BUS TIE TEST STANDBY INVERTER FAILED TO POWER UP. REPLACED STANDBY INVERTER REF B 767 AMM 24-33-03.SDR FDEA202107271876Skin · wornLH WING. SLAT NO 05 TRAILING EDGE WEDGE WITH TWO WEAR MARKS, LOCATED AT 37 IN FROM INNER RIB AND, 42 IN FROM INNER RIB. LH WING. SLAT NO 05 TRAILING EDGE WEDGE AT POSITION OSS (434.6-447) ON LOWER AND UPPER SKIN WERE REPAIRED I.A.W. SRM 57-43-02-2R FIG. 20SDR FDEA202107271874Skin · delaminatedDELAMINATION AT LEFT WING OUTBOARD TRAILING EDGE FLAP, AT 70" FROM INBD TO OUTBD LEADING EDGE. LEFT WING OUTBOARD FLAP, AT 70" FROM INBD TO OUTBD LEADING EDGE WAS REPAIRED I.A.W. SRM 57-53-01-2R PAG. 1-5 TABLE1 FIG. 201 (SHEET 3) AND SRM 51-70-03-0G PAG. 1SDR FDEA202107271875Skin · damagedRH WING,SLAT #8 BETWEEN LES 446 AND 436, TRAILING EDGE INNER SKIN WITH WEAR. RH WING,SLAT #8 BETWEEN LES 446 AND 436 WAS REPAIRED IAW SRM 57-43-02-2R PAG.1-2 FIG. 201 SHEET 1-2 AND SRM 51-70-10-2R REP. 4 PAG.149-159 FIG.202 SHEET 5 REV 79 DEC 15,2020SDR FDEA201803080636Line · leakingDESCENDING THROUGH 13,000 FT, RIGHT HYD QTY AND RIGHT HYD SYS PRESSURE EICAS ILLUMINATED. COMPLIED WITH QRH. LANDED UNEVENTIFULLY. FOUND A LEAK FROM A BROKEN LINE ON THE RT INBD SPOILER ACTUATOR. INSTALLED A NEW UNION ON THE LINE IAW AMM 120-10-09-8-SDR FDEA201803080633Hydraulic Line · not reportedDESCENDING THROUGH 13,000 FT, RIGHT HYD QTY AND RIGHT HYD SYS PRESS EICAS ILLUMINATED. COMPLIED WITH QRH. LAND UNEVENTFULLY INSTALLED RT ACT PRESSURE LINE REF SMP PREFORMED A SUCCESSFUL LEAK CHECK OF BOTH THE RETURN AND PRESSURE LINE. NO LEAKS FOUND.
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