N166FE
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 = 'N166FE' 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 = 'N166FE' 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 FDEA202606190784Floor Panel · crackedCRACK L=2.500" ON UPPER SURFACE OF FLOOR PANEL 242SFF AT MDC. FLOOR PANEL 242SFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 94 DEC 15/2025SDR FDEA202606190787Skin · delaminatedDELAMINATION ON LWR SURFACE OF THE SPOILER 6 AT 12.5 INCH FROM OUTBD SIDE AND 16 INCH AFT EDGE, LH WING SPOILER 6 AT 12.5 INCH FROM OUTBD SIDE AND 16 INCH AFT EDGE LH WING WAS REPAIRED IAW B767 SRM 57-70-01-2R FIG 201 REP 1 SHEET 2 AND SRM 51-70-17-0G PAR SDR FDEA202606180778Skin · dentedDENT ON UPPER SKIN WEDGE OF SLAT NR 8 OSS 457 SLAT NR 8 OSS 457 WAS REPAIRED IAW SRM 57-43-02-2R FIG 201 SHEET 1 AND SRM 51-70-10-2R PAR G FIG 209, SHEET 1, REV 94. DEC 15 /2025SDR FDEA202606180777Floor Panel · crackedSEVEN CRACKS L=1.200" ON UPPER SURFACE OF FLOOR PANEL 241WFF AT MDC FLOOR PANEL 241WFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94. DEC 15/2025.SDR FDEA202606180776Floor Panel · puncturedTWO PUNCTURES ON UPPER SURFACE OF FLOOR PANEL 242VFF AT MDC FLOOR PANEL 242VFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94. DEC 15/2025SDR FDEA202606180775Floor Panel · puncturedPUNCTURE ON UPPER SURFACE OF FLOOR PANEL 241ZFF AT MDC FLOOR PANEL 241ZFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94. DEC 12/2025.SDR FDEA202606160758Floor Panel · puncturedPUNCTURED FLOOR PANEL 232EFF.SEC 43 OF MDC. FLOOR PANEL 232EFF SEC 43 OF MDC. WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 94 DEC 15,2025.SDR FDEA202606160756Floor Panel · puncturedPUNCTURED FLOOR PANEL 242AFF. SEC 45 OF MDC. FLOOR PANEL 242AFF. SEC 45 OF MDC. WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-B FIG. 201 SHEET 2. REV. 94 DEC 15,2025.SDR FDEA202509181741Hydraulic Line · leakingACTIVE HYDRAULIC LEAK FROM RIGHT WING JUST OUTBOARD OF RIGHT MAIN GEAR FOUND LINE LEAKING FLUID FROM LG UP CTR SYSTEM. OPENED RIGHT WING PANEL 651TB TO ACCESS LINE THAT IS LEAKING IN REFERENCE TO AMM LISTED ABOVE. REMOVED CENTER HYDRAULIC SYSTEM RIGHT MAISDR FDEA202208031855Skin · puncturedRIGHT WING SPOILER NO 7 LOWER SURFACE WITH PUNCTURE. RIGHT WING SPOILER NO 7 LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-70-01 REP. 1, FIG. 201 SHEET 1, 2, 4, PAGE 1-4 AND SRM 51-70-17-0G PARA. 4.C. PAGE 1, 25, 26, 36, 49; FIG. 11 REV.82 DEC15/2021SDR FDEA202208031854Skin · puncturedRIGHT WING SPOILER NO. 8 LOWER SURFACE WITH PUNCTURE R.H. WING SPOILER NO. 8 LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-70-01 REP. 1, FIG 201 SHEET 1, 2, 4, PAGE 1-4 AND SRM 51-70-17-0G PARA. 4.C. PAGE 1, 25, 26, 36, 49; FIG. 11 REV. 82 DEC15/2021SDR FDEA202104170945Static Inverter · faultedON FINAL APPROACH, CAPTAIN`S FLIGHT AND NAV DISPLAY WENT BLANK FOR 5 SECONDS AFTER APP TILE SELECTED. DISPLAY RETURNED TO NORMAL. UPON SHUTDOWN, STBY INVERTER ON STATUS PAGE. R & R STATIC INVERTER IAW AMM 24-33-03-4. OPS CHECK GOOD.SDR FDEA202009182252Skin · chafedLT WING NR 5 SLAT LOWER SURFACE L/E AREA DAMAGE 2 (EA), PLACE AS MARK STREAMER ATTACH. REPAIRED NR 5 SLAT LOWER SURFACE 1EA AREA 89.5" FROM O/B, IAW B767 SRM 57-43-02-2R REPAIR 1 AND 51-70-10-2R REPAIR 4 FIG. 202; 1EA AREA 47.5" FROM O/B FOUND MISSING PAINT NSDR FDEA201901090070Idg · malfunctionedPDIS 166 24-50 0296 09JAN19 MEM LOST L AND R UTILITY BUS DURING APPROACH TO MEM. THEN LOST R GENERATOR. LOST AUTOPILOT, AUTO THROTTLES, GEAR INDICATIONS. EXECUTED MID ALTITUDE GO AROUND. COULD NOT RAISE GEAR OR FLAPS. RAN QRH FOR R GEN, CYCLED UTILITY BUSSES WSDR FDEA201812063442Latch · unsecureF/O ESCAPE ROPE DOOR STILL FALLING OPEN IN FLIGHT. EMERGENCY ESCAPE ROPE COVER OVER FIRST OFFICERS HEAD WILL NOT STAY CLOSED. APPEARS LATCH IS NOT FULLY ENGAGED WHIN CLOSED. FOUND COVER LATCH STUCK. ADJUSTED LATCH. OPS CHECK GOOD PER AMM 25-61-03-2.SDR FDEA2018102963044Warning System · false activationPDIS 166 27-80 0117 26OCT18 MEM FACT U LOGPAGES:2670727 LE SLAT DISAGREE WHEN GEAR SELECTED DOWN & FLAPS 20. RAN QRH, LANDED F20. RETURNED FLAPS ON DECK VIA ALT MEANS. NO OVERSPEED. FACT 26OCT18 08:17 MEM U WITH NO HISTORY NOTED. PERFORMED BITE CHECK OF PSEU R
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