N151FE
Service difficulty reports · 26
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 = 'N151FE' 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 = 'N151FE' 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 FDEA202508271548Door · fodMAIN CARGO DOOR EICAS RAN QRH , INDICATION EXTINGUISHED ONCE WE DESCENDED AND DEPRESSURIZED TO 9000FOOT CABIN , LANDED WITHOUT ISSUE. EMERGENCY DECLARED. FIM: 52-90-18-00 FOUND DEBRIS BLOCKING MAIN CARGO DOOR CLOSED & LOCKED SENSORS. REMOVED DEBRIS PERSDR FDEA202505190767Access Panel · damagedLEFT HORIZONTAL STAB, PANEL 335LB HAS A SMALL HOLE IN PANEL. REPAIRED, PREPPED, PRIMED, AND PAINTED L/H HOR STAB ACCESS PANEL 335LB LOCATED ON LOWER HOR STAB (P/N 183T1270-27) STA 317.50-322 HSBL IN REF. TO SRM 55-10-01-2R FIG. 201 REPAIR 1 SHEET 1, SRM 51SDR FDEA202505170762Floor Panel · damagedMAIN DECK, FOUND DAMAGE ON FLOOR PANEL 242UFF. FABRICATED MAIN CARGO DECK FLOORBOARD PANEL 242UFF AT STA 970-1114.82 AT LBL 54.75"- LBL 74.25" (MPN 145T5876-112) IN REF. B767 DWG 145T5876-112 AND SRM 53-00-50-2R REPAIR 1 FIG.201 SHEET 1. THIS IS A MAJOR RESDR FDEA202505150760Floor Panel · damagedMAIN DECK, FOUND DAMAGE ON FLOOR PANEL 241ZFF. FABRICATED MAIN CARGO DECK FLOORBOARD PANEL 241ZFF AT STA. 970-1114.82 AT LBL 54.75"- LBL 77.50" (MPN: 145T5876-111) IN REF. B767 DWG 145T5876-111 AND B767 SRM 53-00-50-2R REPAIR 1 FIG.201 SHEET 1. THIS IS A MSDR FDEA202505150759Floor Panel · damagedMAIN DECK, FOUND DAMAGE ONFLOOR PANEL 241WFF. FABRICATED MAIN CARGO DECK FLOORBOARD PANEL 241WFF AT STA. 970-1114.82 AT RBL 11"- LBL 11" (MPN: 145T5876-51) IN REF. B767 DWG 145T5876-51 AND B767 SRM 53-00-50-2R REPAIR 1 FIG.201 SHEET 1. THIS IS A MAJOR REPASDR FDEA202505150755Floor Panel · dentedMAIN DECK FLOORBOARD HAS A SMALL DENT IN FIBERGLASS AT POS 2R AT LOCK. REPAIRED MAIN DECK FLOORBOARD DENT AT POSITION 2R BETWEEN STA 285 AND STA 412 LBL 54.75"- LBL 77.50" IN REF. TO SRM 53-00-50-2R REPAIR 1 FIG.201 SHEET 1. MAIN DECK FLOOR WAS NOT REMOVEDSDR FDEA202505140753Floorboard · dentedMAIN DECK, FOUND DAMAGE ON FLOORBOARD PANEL 242VFF. EVALUATED DAMAGE AND FOUND 1 EACH, 1 INCH DENT ON TOP SKIN. REPAIRED DAMAGE ON FLOORBOARD PNL# 242VFF (MPN: 145T5876-114) IN REF TO B767 SRM 53-00-50-2R PAR 4.B, FIG 201, REPAIR 1, SHEET 2. THIS IS A MAJOSDR FDEA202505120749Floor Panel · dentedMAIN DECK, FOUND DAMAGE ON FLOOR PANEL 242JFF. REPAIRED 1 INCH CIRCLE DENTED AREA ON FLOOR PANEL 242JFF MPN: 145T5876-102 RBL: 11 TO RBL: 33 AND STA: 930-980 IN REF TO B767 SRM 53-00-50-2R 4.B. TAP TEST GOOD IN REF TO B767 SRM 51-10-06-0GSDR FDEA202306251103Web · crackedAFT CARGO COMPARTMENT BETWEEN STA 1329 AND BL 0 FLOOR SUPPORT STIFFER WITH CRACK. THE PANEL THE FLOOR SUPPORT STIFFER WAS REPLACED AT AFT CARGO COMPARTMENT BETWEEN STA 1329 AND BL 0 IAW SRM 51-10-02-0G PARAGRAPH (9) REV. 85 DEC 15,2022 DRAWING 451T2612 SSDR FDEA202306211066Flap · dentedLEFT WING, OUTBOARD FLAP LOWER SKIN WITH DENT AT 6" FROM LOWER EDGE AND 21" FROM INBOARD EDGE D= 0.023" L= 2.250" W= 1.220" LEFT WING, OUTBOARD FLAP LOWER SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R, FIG 201 SHEET 1, 3-6 AND SRM 51-70-06-0G, FIG 9 SHEET SDR FDEA202306201065Panel · dentedMDC FLOOR PANEL 221DFF WITH DENTS ALONG UPPER SURFACE. SECTION 41. MDC FLOOR PANEL 221 DFF UPPER SURFACE WAS REPAIRED IAW B767 SRM 53-00-50-2R, PARA. 4.B. FIG. 201 SHEET 2, PAGE 1-16 REV. 85 DEC15/22SDR FDEA202306201064Panel · dentedMDC FLOOR PANEL 222CFF WITH DENTS ALONG UPPER SURFACE. SECTION 41. MDC FLOOR PANEL 222 CFF ALONG UPPER SURFACE WAS REPAIRED IAW B767 SRM 53-00-50-2R, PARA. 4.B. FIG. 201 SHEET 2, PAGE 1-16 REV. 85 DEC15/22SDR FDEA202306201063Panel · dentedMDC FLOOR PANEL 221CFF WITH DENTS ALONG UPPER SURFACE. SECTION 41. MDC FLOOR PANEL 221 CFF, UPPER SURFACE WAS REPAIRED IAW B767 SRM 53-00-50-2R, PARA. 4.B. FIG. 201 SHHET 2, PAG. 1-16 REV.85 DEC15/22SDR FDEA202306201062Panel · dentedMDC FLOOR PANEL 222AFF WITH DENTS ALONG UPPER SURFACE. SECTION 41. MDC FLOOR PANEL 222 AFF, UPPER SURFACE WAS REPAIRED IAW B767 SRM 53-00-50-2R, PAR. 4.B. FIG. 201 SHEET 2, PAG. 1-16 REV. 85 DEC15/22SDR FDEA202306201061Panel · dentedMDC FLOOR PANEL 222BFF WITH DENTS ALONG UPPER SURFACE. SECTION 41. MDC FLOOR PANEL 222 BFF, UPPER SURFACE WAS REPAIRED IAW B767 SRM 53-00-50-2R, PARA. 4.B. FIG. 201 SHEET 2, PAGE 1-16 REV. 85 DEC15/2022SDR FDEA202306121025Flap · dentedRH WING, OUTBOARD FLAP, LOWER SURFACE WITH DENT AT 52" FROM OUTER EDGE AND 10.75" FROM LOWER EDGE. RH WING, OUTBOARD FLAP, LOWER SURFACE, DENT WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG. 201 SHEET 6 REPAIR 1 AND SRM 51-70-06-0G PAR. 5.A. FIG. 9 REV. 85 DECSDR FDEA202209292397Former · crackedL/H WING AT STATION OSS.499 L/E FORMER IS CRACKED (P/N: 114T2511-13) REPLACED FORMER (B67-57-002-3) AT LS FLE OSS 499 USING EA H-5720-T0370864P1 AS REFERENCE.SDR FDEA2022093092397Former · crackedL/H WING AT STATION OSS.499 L/E FORMER IS CRACKED (P/N: 114T2511-13) REPLACED FORMER (B67-57-002-3) AT LS FLE OSS 499 USING EA H-5720-T0370864P1 AS REFERENCE.SDR FDEA202204241044Former · crackedRH WING LEADING EDGE CRACKED FORMER AND LOOSE FASTNERSAT RS OSS 441.596 REMOVED & REPLACED FORMER, AND FASTNERS IN REF. TO E.A H-5720-T0368164 P1SDR FDEA202204241043Former · crackedLH WING LEADING EDGE CRACKED FORMER AND LOOSE FASTNERSAT LS OSS 441.596 REMOVED & REPLACED FORMER, AND FASTNERS IN REF. TO E.A H-5720-T0368164 P1SDR FDEA202204231089Former · crackedCRACKED FORMER AND LOOSE FASTENERS AT LS OSS 441.596 0000355851 : MITROVICH, DAVID T - 24-APR-2022 05:34 REMOVED & REPLACED FORMER & FASTENERS REF: E.A TH5720-T0368164 P1.SDR FDEA202204231088Former · crackedCRACKED FORMER AND LOOSE FASTENERS AT RS OSS 441.596 0000355851 : MITROVICH, DAVID T - 24-APR-2022 05:33 REMOVED & REPLACED FORMER & FASTENERS REF: E.A TH5720-T0368164 P1.SDR FDEA202107071704Skin · crackedCRACK ON LH WING SLAT #5 UPPER TRAILING EDGE INNER SURFACE TO 1060 FROM INBOARD EDGE (L=0.600" W=0.400") SLAT 5 T.E. WEDGE UPPER AND LOWER SKIN AT POSITION OSS 430.37 WERE REPAIRED IAW SRM 57-43-02-2R REP. 1 PAG 1-2 FIG. 201 AND SRM 51-70-10-2R FIG 202 SDR FDEA202008131871Lamp · inoperativeEMERGENCY LIGHT "UNARMED" LIGHT ON OVERHEAD PANEL IS INOPERABLE. UPDT 13AUG20 00:11. JAX U RELAMPED SWITCH AND OPERATIONS CHECK GOOD, REF 767 MM 33-13-00-2. OK FOR SERVICE. RELAMPED LIGHT SWITCH WITH 387 BULBS AND OPERATIONS CHECK GOOD, REF 767 MM 33-13-00SDR FDEA2020081431871Lamp · inoperativeEMER LIGHT "UNARMED" LIGHT ON OVERHEAD PANEL IS INOP. RELAMPED SWITCH AND OPS CHECK GOOD. REF 767 MM 33-13-00-2. OK FOR SERVICE.SDR FDEA201909262351Tire · wornDURING TAKEOFF ROLL, WE EXPERIENCED EXCESSIVE VIBRATIONS FROM THE GEAR ONCE AIRBORNE. VERBALLY SPOKE WITH CREW.. THE AIRPLANE EXPERIANCED A SMALL AMOUNT OF VIBRATION ON TAKE OFF ROLL AND AN EXCESSIVE AMOUNT ONCE THE ACFT BECAME AIRBORNE. IT WAS STATED T
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