N160FE
Service difficulty reports · 29
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 = 'N160FE' 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 = 'N160FE' 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 FDEA202609081287Control Panel · inoperativeON PREFLIGHT, FOUND THE EMERGENCY EXIT LIGHTS WILL NOT ARM OR TEST FROM THE OVERHEAD PANEL. ALL LIGHTS OPERATE WHEN THE TEST BUTTON IS PRESSED ON THE EMERGENCY LIGHTS POWER SUPPLY. REPLACED EMERGENCY EXIT LIGHTS O/H PANEL IAW AMM 33-51-08-4. CKS OK.SDR FDEA202607180943Warning Message · false activationTOOK OFF WITH 2.3 IN CENTER TANKS, L & R TANKS FULL. ALL PUMPS ON AND CROSS FEEDS WERE OFF. APPROX 10 MINS INTO FLIGHT, RECEIVED FUEL CONFIG EICAS. STILL 0.6 IN CENTER, BUT L WAS 35.5, R WAS 37.5. COMPLIED WITH QRH AND REBALANCED FUEL. CW FIM 28-41/854SDR FDEA202602120190Skin · delaminatedDELAMINATION IN LEADING EDGE ON OTBD FLAP AT 9.5" INBD END. RT WING LEADING EDGE FLAP WAS REPAIRED IAW SRM 51-70-03-0G, PARA 5.A., FIG 5, SHEET 1, REV 93 AND SRM 57-53-01-2R TABLE I FIG. 201 (SHEET 5) REV 93.SDR FDEA202602120189Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 241ZFF OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 93.SDR FDEA202602120188Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 242TFA OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, REPAIR GENERAL, PARA 4.B, FIG 201, SHEET 2, REV 93.SDR FDEA202602120187Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 241YFA OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, REPAIR GENERAL, PARA 4.B, FIG 201, SHEET 2, REV 93.SDR FDEA202602120186Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 242MFF OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, REPAIR, GENERAL PARA. 4.B, FIG. 201, SHEET 2, REV 93.SDR FDEA202602120185Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 242VFF OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B, FIG 201, SHEET 2, REPAIR GENERAL, REV 93.SDR FDEA202602110179Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 241QFF OF MDC. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 93, AUG 15, 2025.SDR FDEA202602110178Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 241MFF OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 93, AUG 15, 2025.SDR FDEA202602110177Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 241WFF OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 93, AUG 15, 2025.SDR FDEA202602110176Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 242SFF OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 93, AUG /15, 2025.SDR FDEA202602100169Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 241XFF OF MAIN DECK CARGO FLOOR PANEL 241XFF WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 93, AUG 15/2025.SDR FDEA202602100168Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 242KFF OF MAIN DECK CARGO FLOOR PANEL 242KFF OF MAIN DECK CARGO WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 93, AUG 15, 2025.SDR FDEA202602100167Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 242UFF OF MAIN DECK CARGO.SDR FDEA202602100166Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 242UFF OF MAIN DECK CARGO. FLOOR PANEL 242UFF OF MAIN DECK CARGO WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 93, AUG 15,2025.SDR FDEA202602100165Floor Panel · crackedPUNCTURE ON FLOOR PANEL 241WFF OF MAIN DECK CARGO. FLOOR PANEL 241WFF OF MAIN DECK CARGO WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2 REV. 93, AUG 15, 2025.SDR FDEA202602100163Skin · dentedDENT ON SKIN OF THE OUTBOARD AILERON AT WBL 879 FRON 11" OF TRAILING EDGE, LH WING LH WING OUTBOARD AILERON OF T/E AREA WAS REPAIRED IAW B767 SRM 57-60-02-2R REPAIR 1, FIG 201, SHEET 1 & 2, DETAIL II AND SRM 51-70-03-0G PAR 5L, FIG 16 REV 93 AUG 15/2025.SDR FDEA202602090156Floor Panel · crackedPUNCTURE ON FLOOR PANEL 242SFF OF MAIN DECK CARGO FLOOR PANEL 242SFF OF MAIN DECK CARGO WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 93 AUG 15,2025SDR FDEA202602090155Floor Panel · crackedPUNCTURE ON FLOOR PANEL 241LFF OF MAIN DECK CARGO FLOOR PANEL 241LFF OF MAIN DECK CARGO WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 93 AUG 15,2025SDR FDEA202602090154Floor Panel · crackedPUNCTURE AT FLOOR PANEL 251LFF OF MAIN CARGO COMPARTMENT FLOOR PANEL 251LFF OF MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 93 AUG 15,2025SDR FDEA202602090153Floor Panel · crackedPUNCTURE AT FLOOR PANEL 251MFF OF MAIN CARGO COMPARTMENT FLOOR PANEL 251MFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 93 AUG 15/2025SDR FDEA202403010226Skin · dentedLEFT WING, OUTBOARD TRAILING EDGE FLAP AT LOWER PANEL BETWEEN OTEF STA 3.75 AND OTEF STA 83.73, BETWEEN FWD SPAR AND MID SPAR WITH DENT. LEFT WING, OUTBOARD TRAILING EDGE FLAP AT LOWER PANEL BETWEEN OTEF STA 3.75 AND OTEF STA 83.73, BETWEEN FWD SPAR AND MISDR FDEA202402260216Skin · delaminatedLEFT WING, OUTBOARD TRAILING EDGE FLAP AT NOSE SKIN (LEADING EDGE) BETWEEN OTEF STA 190 AND OTEF STA 265.69 WITH DELAMINATION. LEFT WING, OUTBOARD TRAILING EDGE FLAP AT NOSE SKIN (LEADING EDGE) BETWEEN OTEF STA 190 AND OTEF STA 265.69 WAS REPAIRED IAW B767SDR FDEA202402260215Skin · delaminatedLEFT WING, OUTBOARD TRAILING EDGE FLAP AT NOSE SKIN (LEADING EDGE) BETWEEN OTEF STA 3.75 AND OTEF STA 83.73 WITH DELAMINATION. LEFT WING, OUTBOARD TRAILING EDGE FLAP AT NOSE SKIN (LEADING EDGE) BETWEEN OTEF STA 3.75 AND OTEF STA 83.73 WAS REPAIRED IAW B767SDR FDEA202402210207Skin · dentedLH WING SLAT NO. 6 EXTERNAL UPPER SURFACE WITH SEVERAL HAIL DAMAGE (DENTS) LH WING SLAT NO. 6 EXTERNAL UPPER SURFACE WAS REPAIRED IAW B767 SRM 57-43-02-2R REP 1 PAG 1-2 AND SRM 51-70-10-2R REP 4 FIG 201 SHEET 1. REV 88 DEC 15/2023SDR FDEA202203080441Door · crackedMAIN LANDING GEAR RH, MAIN DOOR OUTER SKIN AFTER SURFACE WITH HOLE. MAIN LANDING GEAR R.H. MAIN DOOR OUTER SKIN AFTER SURFACE WAS REPAIRED WITH COMPLETED TASK SEQ NO 000928 AND SRM 52-80-02-2R FIG. 201 PAG. 1-2 AND SRM 51-70-03-0G PAG. 1, 19, 20, 30, 36 FISDR FDEA202203080440Slat · wornRIGHT WING SLAT NO. 8 WITH EROSION IN TRAILING EDGE WEDGE WS. 486.2 RIGHT WING SLAT 8 WEAR IN TRAILING EDGE WEDGE AT OSS 494.35 WAS REPAIRED IAW SRM 51- 70-10-2R REPAIR 4 PAG. 149-163. FIG. 202 AND SRM 57-43-02-2R REPAIR 1 FIG. 201 PAG. 1-2 REV. 82 DEC15/2SDR FDEA2020032320600Skin · gougedR/H WING AT TOP OF #8 SLAT BOTTOM SURFACE HAS GOUGE REPAIRED R/H WING AT TOP OF #8 SLAT BOTTOM SURFACE GOUGE IAW B767-SRM-57-43-02-2R REPAIR 1, SRM 51- 70-10 10-2R REPAIR 4, AND SRM 51-70-10 REPAIR GENERAL.
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