N158FE
Service difficulty reports · 27
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 = 'N158FE' 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 = 'N158FE' 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 FDEA202511212197Skin · dentedDENT AT RT LOWER LATERAL SKIN BELOW UPPER LAP SEAM BETWEEN BS 1620 & 1650. DENT AT RT LOWER LATERAL SKIN BELOW UPPER LAP SEAM WAS REPAIRED IAW EA. H-5330-T0369691 REV NOV 19,2025. RELEASE DATE: JUL 23,2022.SDR FDEA202511122166Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN BS 698 AND STGR 32/33L. LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 32L AND STGR 33L AT STA 698 WAS REPAIRED IAW SRM 53-00-01-2R, REPAIR 29, REV 93 AUG 15, 2025.SDR FDEA202511122165Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN BS 676 AND STGR 32/33 LH. LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 32 LT AND STGR 33 LT AT STA 676 WAS REPAIRED IAW SRM 53-00-01-2R REPAIR 29 REV. 93 AUG 15,2025.SDR FDEA202511092153Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 222AFF ON MDC SEC 41. FLOOR PANEL 222AFF ON MDC SEC 41 WAS REPAIRED IAW B767 SRM 53-00-50-2R, PAR.4.B, FIG 201, REV. 93, AUG 15,2025.SDR FDEA202511082151Flap · damagedPUNCTURE ON LOWER SKIN OF AFT INBOARD TRAILING EDGE FLAP RH WING, APPROX 6.250" OF INBOARD EDGE AND 0.500" OF LOWER EDGE. PUNCTURE ON LOWER SKIN OF AFT INBOARD TRAILING EDGE FLAP RH WING WAS EVALUATED AND WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG. 201 DETASDR FDEA202511082152Floor Panel · crackedCRACKS (6EAS) ON UPPER SURFACE OF FLOOR PANEL 241WFF AT MDC. L1=1.67", L2=1.118", L3=0.845", L4=0.830", L5=0.935", AND L6=0.920". FLOOR PANEL 241WFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 93 AUG 15,2025SDR FDEA202511082150Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 251BFF ON MDC SEC 46. FLOOR PANEL 251BFF ON MDC SEC 46 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 93 AUG 15,2025SDR FDEA202511082149Floor Panel · puncturedPUNCTURES (2EA) ON UPPER SURFACE OF FLOOR PANEL 242VFF AT MDC FLOOR PANEL 242VFF AT MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 93 AUG 15,2025SDR FDEA202511082148Floor Panel · brokenBROKEN FLOOR PANEL 251QFF ON MAIN DECK CARGO SEC 46. FLOOR PANEL 251QFF ON MAIN DECK CARGO SEC 46 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 93 AUG 15,2025.SDR FDEA202511082147Skin · delaminatedDELAMINATION IN REPAIR ON UPPER SKIN OF SLAT NO. 8, APPROX. 37" OF INBD EDGE AND AFT EDGE RH WING. UPPER SKIN OF SLAT NO. 8, APPROX. 37" OF INBD EDGE AND AFT EDGE RH WING, WAS REPAIRED IAW B767 SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 8, REV. 93 AUG 15, 2SDR FDEA202511072145Floor Panel · puncturedPUNCTURES (8EAS) ON UPPER SURFACE OF FLOOR PANEL 241ZFF AT MDC. FLOOR PANEL 241 ZFF AT MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 93 AUG 15, 2025.SDR FDEA202511072144Floor Panel · damagedPUNCTURE ON FLOOR PANEL 251FFF ON MDC SEC 46. FLOOR PANEL 251 FFF ON MDC SEC 46 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 93 AUG 15, 2025.SDR FDEA202511072143Floor Panel · damagedPUNCTURE ON FLOOR PANEL 221DFF ON MDC SEC 41. FLOOR PANEL 221 DFF ON MDC SEC 41 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 93 AUG 15, 2025.SDR FDEA202402030134Skin · dentedLEFT INBOARD FLAP, AFT FLAP, LOWER SURFACE, BTW FLAP TRACK FAIRINGS, DENTS. LEFT INBOARD FLAP, AFT FLAP, LOWER SURFACE, BTW FLAP TRACK FAIRINGS WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 AND SRM 51-70-03-0G PAR 5.L FIG 16 PAG 27,52 REV 88 DEC 15/2023SDR FDEA202311161859Unknown · unknownUNSAFE GEAR INDICATION ON FINAL, LEFT MAIN NOT DOWN AND LOCKED, NO EICAS MESSAGES. WENT AROUND AND REFERENCED QRH, FLEW VISUAL LOW APPROACH AND TOWER CONFIRMED ALL GEAR SHOWED DOWN. DECLARED EMERGENCY AND LANDED UNEVENTFULLY AND STOPPED CLEAR OF RUNWAY.SDR FDEA202301020007Control Panel · failedEMERGENCY LIGHT UNARMED LIGHT; INOP AFTER SHUTDOWN WHEN SWITCH IS IN A UNARMED POSITION. REMOVED AND REPLACED PILOTS' EMERGENCY LIGHTS CONTROL PANEL WITH OPS CKS GOOD. PER SDR, MFR OF REMOVED PART IS "OASE9".SDR FDEA202211092739Seal Depressor · crackedFORWARD CARGO DOOR AFT SEAL DEPRESSOR DAMAGED APPROXIMATELY 14" ABOVE BOTTOM SEAL. INSTALLED NEW SEAL DEPRESSOR PNR:143T8542Y4 IAW SRM-51-40-02-0G.SDR FDEA202210052475Former · crackedRH WING - FIXED LEADING EDGE STRUCTURE AT WING STA 499 HAS A CRACKED FORMER BRACKET,MWT. 0000392280 : BILLMAN, CRAIG B - 05-OCT-2022 23:14 REPLACED LEADING EDGE FORMER AS REQUIRED PER EA-H-5720-T0370963 PT1.SDR FDEA202210052474Former · crackedRH WING - FIXED LEADING EDGE STRUCTURE AT WING STA 441 HAS A CRACKED FORMER BRACKET,MWT. REPAIRED PER E.A. H-5720-T0370963 P1. REPLACED CRACKED FORMERSDR FDEA202210052473Former · crackedL/H WING LEADING EDGE FORMER CRACKED WITH ONE EACH SHEARED CHERRY MAX RIVET AT LS FLE OSS 499.60. REPLACED L/W L/E FORMER STA OSS 499.6 REF E.A. H-5720-TO370966 P1.SDR FDEA202210052472Former · crackedL/H WING LEADING EDGE FORMER CRACKED WITH ONE EACH SHEARED CHERRY MAX RIVET AT LS FLE OSS 441.60. M.W.T. 0000301922 : VERNON, JAMES L - 05-OCT-2022 22:55 REPLACED L/W L/W FORMER STA. OSS 441.6 REF E.A. H-5720-T0370966 P1SDR FDEA202205141206Fitting · failedDURING LSY CHECK AT INDY, THE LH MLG DOOR STOP SHIMS (FORWARD STOP) WERE IDENTIFIED AS LOOSE AND THE STOP PAD ON THE MLG DOOR HAS GOUGING ABOUT 0.020 DEEP. THE HELICOIL INSERTS IN THE AIRCRAFT SIDE STOP FITTING ARE LOOSE AND NOT HOLDING RETENTION OF THE SCRSDR FDEA202202150299Flap · delaminatedRH WING OUTBOARD FLAP LEADING EDGE SKIN WITH DELAMINATION NEAR FLAP TRACK SUPPORT. RH WING OUTBOARD FLAP LEADING EDGE SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG. 201 TABLE 1 SHEET 5 AND SRM 51-70-03-0G PAG. 59 SHEET 1 FIG. 18 REV. 82 DEC15/2021SDR FDEA202202150298None · delaminatedRH WING -INBOARD TRAILING EDGE FLAP - MAIN FLAP LEADING EDGE WITH DELAMINATION AT 17 INCHES FROM OUTBOARD EDGE. RH WING INBOARD TRAILING EDGE FLAP, MAIN FLAP LEADING EDGE WAS REPAIRED IAW SRM 57- 53-01-2R REP.1 FIG. 201 PAG. 1-9 AND SRM 51-70-17-0G SHEET 1 SDR FDEA202202150297Slat · wornSLAT #8 WEDGE AREA REAR FACE WITH SCRATCH (OSS 431). RH WING SLAT #8 T.E. WEDGE AT OSS 431 WAS REPAIRED IAW B767 SRM 57-43-02-2R REP. 1 PAG. 1-2 FIG. 201 AND SRM 51-70-10-2R REP. 4 PAG. 97-99, 149, 162 REV. 82 DEC15/2021SDR FDEA202202150296Slat · wornLEFT WING SLAT NO 5 TRAILING EDGE/LOWER SKIN WITH WEAR TO 31.5 INCHES FROM OUTBOARD EDGE. LEFT WING SLAT NO 5 T.E. WEDGE AT OSS 500 WAS REPAIRED IAW B767 SRM 57-43-02-2R REP. 1 PAG. 1-2 FIG. 201 AND SRM 51-70-10-2R REP. 4 PAG. 97-99, 149, 162 REV.82 DEC1SDR FDEA202202150295Slat · wornLEFT WING SLAT NO 5 TRAILING EDGE/LOWER SKIN WITH WEAR TO 41 INCHES FROM INBOARD EDGE. LEFT WING SLAT NO 5 T.E. WEDGE AT OSS 430 WAS REPAIRED IAW B767 SRM 57--43-02-2R REP. 1 PAG. 1-2 FIG. 201 AND SRM 51-70-10-2R REP. 4 PAG. 97-99, 149, 162 REV.82 DEC
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