N270FE
Service difficulty reports · 46
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 = 'N270FE' 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 = 'N270FE' 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 FDEA202609101294Slat · gougedNR# 0005: #4 SLAT LWR SURFACE IS GOUGED APPROXIMATELY 36 INCHES FROM INBD EDGE. REPAIRED L/H WING #4 SLAT T/E WEDGE TOP SKIN AT WS 546.2 IN REF. TO 767 SRM 57-43-02-2R AND 767 SRM 51-70-10-2R. THIS IS A MAJOR REPAIR. SEE JPF STEPS FOR OTHER WORK ACCOMPLISHEDSDR FDEA202605050597Autothrottle Sys · failedAUTO THROTTLES UNSATISFACTORY ON DEPARTURE. SPEED HELD AT 24 KNOTS LESS THAN COMMANDED SPEED WITH THROTTLES COMMANDED TO AN INTERMEDIATE POWER SETTING. HAD TO PERFORM MULTIPLE INTERVENES TO MAINTAIN SPEED AND AVOID GETTING BELOW SAFE POWER SETTINGS AND SSDR FDEA202602120184Floor Panel · dentedMAIN DECK, AT APROX. BS 870, FLOOR PANEL 241GFF UPPER SKIN DENTED. REPAIRED THE TOP SKIN THE FLOOR PANEL IAW SRM 53-00-50-2R 4.B. INSTALLATION OF THE FLOOR PANEL WILL BE ACCOMPLISHED ON WO 91257, SEQ 149. MAJOR REPAIR.SDR FDEA202602110181Floor Panel · dentedMAIN DECK, AT APROX. BS 870, FLOOR PANEL 241FFF, SURFACE SKIN DENTED. REPAIRED THE TOP SKIN OF THE FLOOR PANEL IAW SRM 53-00-50-2R 4.B. INSTALLATION OF FLOOR PANEL 241FFF WILL BE ACCOMPLISHED ON WO 91257, SEQ 149. MAJOR REPAIR.SDR FDEA202602110180Floor Panel · dentedMAIN DECK, AT APROX. BS 820, FLOOR PANEL 241AFF DENTED. REPAIRED TOP SKIN OF MAIN DECK FLOOR PANEL IAW SRM 53-00-50-2R 4.B. INSTALLATION OF THE FLOOR PANEL 241AFF WILL BE ACCOMPLISHED ON WO 91257, SEQ 149. MAJOR REPAIR.SDR FDEA202512262291Structure · damagedWHILE UNDERGOING EXTENSIVE STRUCTURES REPAIR FOR IMPACT DAMAGE TO BS 368 - 478, S35 - 38L ACFT SUSTAINED MAJOR FIRE DAMAGE DURING REPAIR WITH ROOT CAUSE CURRENTLY BEING INVESTIGATED. MAJOR REPAIR. COMPLIED WITH EA H-5310-T0383765. MAJOR REPAIR AFTER FWD CASDR FDEA202512262289Beam · ground damageDURING RAMP PUSHBACK TOWBAR HAD DISCONNECTED FROM THE ACFT & ROLLED FWD STRIKING ACFT PUSHBACK TUG ON LOWER FWD LEFT LOWER SECTION OF THE FUSELAGE. THIS IS A MAJOR REPAIR REWORKED, REPAIRED, AND REPLACED AREA'S USING EA H-5310-T0383765 AS COMPARTMENT SDR FDEA202512242288Beam · damagedBS 137, BL 0, WL 168 BEAM P/N 141T2160-2 HAS A .350" CRACK ON AFT FLANGE 10.00" UP FROM LOWER END. REF DWR 141T2160 SHEET 2 REV, 141T2110-190#E. THIS REPAIR WAS ACCOMPLISHED ON CARD FRR-7 SIGNING OFF FEDEX PART PER E.A. H-5310-T0384867 PART 1. THIS IS A MASDR FDEA202508091393Seat Track · damagedTOOLING MARKS ON SEAT TRACK PLATE STA1351 RBL 33. PF FOR WORK ACCOMPLISHED. IAW # E.A. H-5310-T0384454 A, TRIMMED AND REMOVED DAMAGED SECTION OF PLATE. FABRICATED NEW SECTION AND INSTALLED. REF W/O 88761, SEQ. 103 AND WRI 53-10/3712.SDR FDEA202508071388Seat Track · damagedSTATION 1363-1570 RBL 55 SEAT TRACK HAS TOOLING MARKS. REPAIRED SEAT TRACK SECTION BY SPLICING IN A NEW SECTION (STA. 1570 -1363 RBL 55) USING 767 SRM 53-00-52-2R REPAIR 9 ALONG WITH EA H-5310-T0384475 P1 TITLE - MAINFRAME - MAIN CARGO DECK FLOOR STRUCTURESDR FDEA202504250649Skin · delaminatedDAMAGE FOUND ON AILERON (MPN: 113T6100-100G SN: 001204) BTM SKIN WS 530, 22.5 INCH AFT OF HINGE. REPAIRED DAMAGED AREA ON BTM SKIN OF RH INBOARD AILERON MPN: 113T6100-100G SN: 001204 WS: 530 AND 22.5 INCH AFT OF HINGE IN REF TO B767 SRM 57-60-01-2R SHEET:SDR FDEA202504250648Skin · delaminatedDAMAGE FOUND ON AILERON (MPN: 113T6100-100G SN:001204) UPR SKIN WS 444, 4.0 INCH FWD OF HINGE. REPAIRED DAMAGED AREA ON UPR SKIN OF RH INBOARD AILERON MPN: 113T6100-100G SN: 001204 WS: 444 AND 4 FWD OF HINGE IN REF TO B767 SRM 57-60-01-2R SHEET: 7 FIG: 201SDR FDEA202504250647Skin · delaminatedDAMAGE FOUND ON AILERON (MPN: 113T6100-100G SN: 001204) BTM SKIN WS 530, 22.5 INCH AFT OF HINGE. REPAIRED DAMAGED AREA ON BTM SKIN OF RH INBOARD AILERON MPN: 113T6100-100G SN: 001204 WS: 530 AND 22.5 INCH AFT OF HINGE IN REF TO B767 SRM 57-60-01-2R SHEET:SDR FDEA202504250646Skin · delaminatedDAMGE FOUND ON AILERON (MPN: 113T6100-100G SN: 001204) BTM SKIN WS 502, 22.5 INCH AFT OF HINGE. REPAIRED DAMAGED AREA ON BTM SKIN OF RH INBOARD AILERON MPN: 113T6100-100G SN: 001204 WS: 502 AND 22.5 INCH AFT OF HINGE IN REF TO B767 SRM 57-60-01-2R SHEET: 4SDR FDEA202504250645Skin · delaminatedRH INBD AILERON (MPN: 113T6100-100G SN: 001204) DAMAGE FOUND ON AILERON BTM SKIN WS 527 , 8.5 INCH AFT OF HINGE. REPAIRED DAMAGED AREA ON BTM SKIN OF RH INBOARD AILERON MPN: 113T6100-100G SN: 001204 WS: 527 AND 8.5 INCH AFT OF HINGE IN REF TO B767 SRM 57SDR FDEA202504250644Skin · delaminatedDAMGE FOUND ON AILERON (MPN: 113T6100-100G SN 1204) BTM SKIN WS 513, 33.5 INCH AFT OF HINGE. REPAIRED DAMAGED AREA ON LOWER SKIN OF RH INBOARD AILERON MPN: 113T6100-100G SN: 001204 WS: 513 AND 33.5 IN AFT OF HINGE IN REF TO B767 SRM 57-60-01-2R SHEET: 6 FISDR FDEA202408091106Frame · bentFOUND FRAME WEB DAMAGED AT FR390 BETWEEN STR35L AND STR 36L . FRAME WEB AT FR390 BETWEEN STR35L AND STR 36L REPLACED.SDR FDEA202408091105Failsafe · bentFRAME AT STA 456 BENT BETWEEN STR 37L AND STR38L FAIL-SAFE CORD REPLACED.SDR FDEA202408091104Frame · bentFRAME AT STA 434 BENT BETWEEN STR 36L AND STR 38L FRAME AT STA 434 BENT BETWEEN STR 36L AND STR 38L REPLACED.SDR FDEA202408091103Frame · bentFRAME AT STA 412 BENT BETWEEN STR 36L AND 38L FRAME AT STA 412 BENT BETWEEN STR 36L AND 38L REPLACED.SDR FDEA202408091102Failsafe · bentFRAME AT STA 390 LOWER L ANGLE (FAIL-SAFE CORD) BENT BETWEEN STR 34L AND STR 36L.SDR FDEA202408091101Stringer · bentSTRINGER 36L DAMAGED BETWEEN STA 434 TO SAT 456SDR FDEA202408091100Stringer · bentSTRINGER 38L DAMAGED FROM STA 434 TO 456SDR FDEA202408091099Stringer · bentSTRINGER 37L DAMAGED FROM STA 434 TO SAT 456.SDR FDEA202408091098Stringer · bentSTRINGER 37L DAMAGED AT STA 400 TO 434 REPLACED STRINGER 37L FROM STA 368 TO STA 434 IAW B767 SRM 51-40-02 THIS IS A MINOR REPAIR. SEE JPF FOR OTHER WORK STEPS.SDR FDEA202408091097Stringer · bentSTRINGER 36L DAMAGED FROM STA 395 TO STA 398 INSTALLED STRINGER 36L FROM STA 374 TO STA 434 P/N 141T3001-7 AND SPLICE BAC1498-203. REF B767 SRM 53-00-03-2R REPAIR 2 THIS IS A MINOR REPAIR. SEE JPF FOR ALL COMPLETED WORK STEPS.SDR FDEA202408091096Stringer · bentSTRINGER DAMAGED AT STA. 390. REPLACED STRINGER 35L FROM STA 362 TO STA 434 REF 767 SRM 53-00-03-2R-0 REPAIR 2. THIS IS A MINOR REPAIR.SDR FDEA202401220100Flap · delaminatedLH WING OUTBOARD FLAP BETWEEN INBOARD SIDE AND INBOARD FLAP TRACK AREA LEADING EDGE WITH DELAMINATE. LH WING OUTBOARD FLAP AT OTEF 345.75 WAS REPAIRED IAW B767 SRM 57-53-01-2R PAG 3-9 FIG 201 AND SRM 51-70-17-0G PAR 4.A PAG 24,25,48 FIG 10 REV 88 DEC 15/2SDR FDEA202401170084Spoiler · delaminatedLH WING SPOILER #1 UPPER SKIN WITH DELAMINATED. LH WING SPOILER #1 UPPER SKIN WAS REPAIRED IAW B767 SRM 57-70-01-2R REP 1 PAG 1-4 AND SRM 51-70-17-06 PAR 4.A FIG 10 PAG 24,48 REV 88 DEC 25/2023.SDR FDEA202401170083Skin · dentedUPPER FUSELAGE SKIN CROW AREA BETWEEN STA 1480/1510.5 AND STG 3 / 4 LH WITH DENT. UPPER FUSELAGE SKIN CROW AREA BETWEEN STA 1461/1480 AND STGR 3/4 LH WAS REPAIRED I.A.W. SRM 53-00-01-212 REPAIR 14 FIG. 201 AND INSPECTION REQUIREMENTS SEE TABLE V ZONE A - SDR FDEA202401170082Skin · dentedUPPER FUSELAGE SKIN CROW AREA BETWEEN STA 1480/1510.5 AND STG 3 / 4 LH WITH DENT. UPPER FUSELAGE SKIN CROW AREA BETWEEN STA 1461/1480 AND STGR 3/4 LH WAS REPAIRED I.A.W. SRM 53-00-01-212 REPAIR 14 FIG. 201 AND INSPECTION REQUIREMENTS SEE TABLE V ZONE A - SDR FDEA202202100273Door · crackedAFT CARGO DOOR, UPPER SEAL RETAINER & ATTACH ANGLE CRACKED REPAIRED AFT CARGO DOOR, UPPER SEAL RETAINER (143T6324-1) & ATTACH ANGLE (143T6311-5) IAW FEDEX EA # H-5230-T0366731-P1SDR FDEA202202100270Angle · crackedLEFT WING FIXED LEADING EDGE NOSE FORMER ATTACH ANGLE IS CRACKED @ OSS 441 REMOVED & REPLACED NOSE FORMER ATTACH ANGLE IAW BAC DWG 114T2241, REV - & FEDEX EA H-5720-TO366786SDR FDEA202202100269Former · crackedLEFT WING, FIXED LEADING EDGE FORMER IS CRACKED @ OSS 441 REMOVED & REPLACED FORMER IAW BAC DWG 114T2241, REV -SDR FDEA202202100268Angle · crackedLEFT WING FIXED LEADING ECGE FORMER ATTACH ANGLE IS CRACKED @ OSS 437.4 REMOVED & REPLACED ATTACH ANGLE IAW BAC DWG 114T2240, REV - & FEDEX EA H-5720- T0366762-P1SDR FDEA202202090253Angle · crackedR/W FIXED L/E, NOSE FORMER ATTACH ANGLE AT O.S.S. 441.6 REMOVED AND REPLACED THE R/W FIXED L/E NOSE FORMER ATTACH ANGLE AT O.S.S. 441.6 IAW BAC DWG 114T2241, REV. - AND FEDEX EA H-5720-T0366759, TITLE: WINGS - SECONDARY WING STRCT - RH WING, LEADING EDGE, SDR FDEA202202090252Angle · crackedR/W FIXED L/E, NOSE FORMER ATTACH ANGLE AT O.S.S. 437.4 IS CRACKED REMOVED AND REPLACED THE R/W FIXED L/E NOSE FORMER ATTACH ANGLE AT O.S.S. 437.4 IAW BAC DWG# 114T2240, REV. - AND FEDEX EA H-5720-T0366760, TITLE: WINGS - SECONDARY WING STRCT - RH WING, LESDR FDEA202202090251Former · crackedRW #8 SLAT INBD AUX TRACK OTBD NOSE FORMER IS CRACKED REMOVED AND REPLACED THE NOSE FORMER AT STA O.S.S. 441.6, R/W FIXED L/E AT THE #8 SLAT AUX TRACK O/B SIDE IAW BAC DWG# 114T2241, REV. - AND B767 SRM 51-40-02-0G.SDR FDEA202202080247Former · crackedLH WING OUTBD FIXED LEADING EDGE FORMER IS CRACKED AT APPROX. OFSS 490 REMOVED AND REPLACED THE L/W FIXED O/B L/E NOSE FORMER AT STA O.S.S. 499.6 IAW BAC DWG# 114T2161, REV. - AND FEDEX EA H-5720-T0366757, TITLE: WINGS - SECONDARY WING STRCT - LH WING, LEASDR FDEA202202080246Former · crackedRW FIXED L/E AT #8 SLAT OTBD ROTARY ACTUATOR SLAT CURTAIN, THE OTBD NOSE FORMER IS CRACKED REMOVED AND REPLACED THE R/W FIXED L/E NOSE FORMER AT STA O.S.S. 499.6 IAW BAC DWG# 114T2161, REV. - AND FEDEX EA H-5720-T0366756, TITLE: WINGS - SECONDARY WING STRCT SDR FDEA202202080245Wedge · gougedRIGHT WING #8 SLAT TRAILING EDGE LOWER SKIN GOUGED AT THE INBOARD AUX TRACK REPAIRED RIGHT WING #8 SLAT TRAILING EDGE LOWER SKIN IAW B767 SRM 57-43-02-2R FIG 201 AND 51-70-10- 2R REPAIR 4.SDR FDEA202202080244Former · crackedR/H WING LEADING EDGE #9 SLAT INBD TRACK AREA HAS CRACKED FORMER ON INBD SIDE OF CURTAIN REMOVED AND REPLACED THE R/H WING FIXED L/E NOSE FORMER AT O.S.S. 565.9 IAW BAC DWG #114T2162, REV. - AND FEDEX EA H-5720-T0366755, TITLE: WINGS - SECONDARY WING STRCT -SDR FDEA202202080243Bracket · crackedLH WING OUTBD FIXED LEADING EDGE FORMER ATTACH ANGLE IS CRACKED ON THE INBD SIDE AT APPROX. OFSS 475 REMOVED AND REPLACED BRACKET 114T2171-4 ON THE L/W O/B FIXED L/E AT O.S.S. 484 IAW FEDEX EA H- 5720-T0366792, TITLE: WINGS - SECONDARY STRCT - LH WING, LEADSDR FDEA202202030211None · cracked#1 PYLON, AFT FAIRING ASSY, NAC STA 377 FRAME HAS 2EA CRACKED BRACKETS REMOVED & REPLACED SUPPORT BRACKETS IAW B767 SRM 51-40-02, ALL PARTS VERIFIED PER AIPC 54-53-02-20ASDR FDEA202202030210Bracket · crackedRIGHT WING INBD LEADING EDGE, LES 284, TORQUE TUBE GUIDE BRACKET IS CRACKED REMOVED & REPLACED BRACKET IAW BAC DWG 114T1240, REV -SDR FDEA202105051123Pseu · failedABOVE 1000 FT AGL, LE SLAT DISAGREE EICAS WARNING. DISCONTINUED APPROACH, RAN CHECKLIST, DECLARED EMERGENCY, LANDED. T/S SLATS PER FIM 27-51, FOUND FAULT CODE 27-81045. DURING T/S FOUND PSEU HAD FAULT CODE 007 - CARD 7 FALTED. REMOVED AND REPLACED PSEU
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