N132FE
Service difficulty reports · 31
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 = 'N132FE' 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 = 'N132FE' 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 FDEA202610031473Unknown · odorOIL SMELL IN COCKPIT FROM TAKEOFF AT VTBS. DID NOT NOTICE ANY SMELL AT ALTITUDE IN CRUISE. DESCENDING INTO WMKP AT ABOUT 14000 SMELL RETURNED. COMPLIED WITH MTSI 79-00/1133 STEP 4 AND 9. WITH LEFT ENGINE N1 AT 70% AND LEFT PACK ON. NO OIL SMELL PRESENT. ALSSDR FDEA202609121330Unknown · odorACRID FUMES IN COCKPIT DURING CLIMB OUT AND DESCENDING THROUGH 14,000 . PERFORMED AIR CONDITIONING SYSTEM OIL SMOKE/FUME CONTAMINATION REMOVAL PER AMM 21-00-21-2. NO ABNORMAL NOTED. PERFORMED OIL INSPECTION CHKD IAW AMM 79-00-00-6. FOUND NORMAL. PERFORMESDR FDEA202509191747Floor Panel · crackedPERFORATED FLOOR PANEL 241KFF IN MDC SECTION 45 FLOOR PANEL 241KFF IN MDC SECTION 45 WAS REPAIRED IAW 53-00-50-2R PAR 4-B FIG .201 SHEET 2 REV.92 APR 15,2025SDR FDEA202509191746Floor Panel · crackedBROKEN FIBERS ON FLOOR PANEL 251HFF IN MDC FLOOR PANEL 251HFF IN MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV. 92 APR15,2025SDR FDEA202509191745Floor Panel · crackedBROKEN FIBERS ON FLOOR PANEL 251SFF IN MDC FLOOR PANEL 251SFF IN MDC WAS REPAIRED IAW SRM 53.00.50.2R PAR 4.B FIG. 201 SHEET 2 REV 92 APR 15,2025SDR FDEA202509191744Floor Panel · crackedPERFORATED FLOOR PANEL 251QFF IN MDC FLOOR PANEL 251QFF IN MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR4.B FIG 201 SHEET 2 REV 92 APR 15,2025SDR FDEA202509191743Floor Panel · crackedPERFORATED FLOOR PANEL 251KFF IN MDC FLOOR PANEL 251KFF IN MDC WAS REPAIRED IAW SRM 53.00.50.2R PAR 4.B FIG 201 SHEET 2 REV. 92 APR 15,2025SDR FDEA202509191742Floor Panel · crackedPERFORATED FLOOR PANEL 241EFF IN MDC SECTION 45 FLOOR PANEL 241EFF IN MDC SECTION 45 WAS REPAIRED IAW SRM 53.00.50.2R PAR. 4.B FIG.201 SHEET 2 REV 92 APR 15,2025SDR FDEA202412241830Sensor · faultedSHORTLY AFTER REACHING TOP OF CLIMB, FL360, MAIN CARGO DOOR EICAS MESSAGE ILLUMINATED ALONG WITH ASSOCIATED CARGO DOOR DISCRETE LIGHT. WE ACCOMPLISHED THE CHECKLIST AND DESCENDING THROUGH 15000FT THE LIGHTS WENT OUT. EMERGENCY DECLARED. COMPLETED SENSOR SDR FDEA202310041706Floor Panel · dentedMDC FLOOR PANEL 221DFF WITH SEVERAL DENTS. MDC FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 REV 87 AUG 15 2023SDR FDEA202310041705Floor Panel · dentedMDC FLOOR PANEL 222CFF WITH SEVERAL DENTS. MDC FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 REV 87 AUG 15 2023SDR FDEA202310041704Floor Panel · dentedMDC FLOOR PANEL 222BFF WITH SEVERAL DENTS. MDC FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 REV 87 AUG 15 2023SDR FDEA202310041703Floor Panel · dentedMDC FLOOR PANEL 221CFF WITH SEVERAL DENTS MDC FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201. REV 87 AUG 15 2023SDR FDEA202310041701Floor Panel · dentedMDC FLOOR PANEL 222AFF SEVERAL DENTS MDC FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201. REV 87 AUG 15 2023SDR FDEA202310041700Flap · delaminatedRH WING INBOARD FLAP, MAIN FLAP, LEADING EDGE OUTBOARD SIDE WITH DISBONDED RH WING INBOARD MAIN FLAP LEADING EDGE OUTBOARD SIDE WAS REPAIRED IAW B767 SRM 57- 53-01-2R REPAIR 1 FIG 201 SHEET 1,2,5 TABLE 1 AND SRM 51-70-05-0G PARAG 5A PAGE 1,29,37 AND 45 FIG SDR FDEA202305010793Fuel Nozzle · failedAFTER TAKEOFF, HAD R ENG OVHT EICAS WITH ASSOCIATED R ENG OVHT CAUTION LIGHT COMPLIED WITH QRH RETURNED TO MEMPHIS MOMENTARY STATUS MESSAGE R ENG OVHT LP2 WE NEVER HAD EGT OVHT ON PRIMARY FLT INSTRUMENT PANEL. EMERGENCY DECLARED. TESTED LOOP RESISTANCE SDR FDEA202304290780Unknown · unknownPDIS 132 26-10 7156 28APR23 MEM OPEN U RIGHT ENG OVERHEAT INDICATION. ON CLIMB OUT. NO EXCEEDANCE NOTED. NO FIRE ALERT. ECAM MESSAGE OF RIGHT ENGINE OVERHEAT. RAN QRH. RETURNED TO KMEM. ***EMERGENCY DECLARED*** TROUBLESHOT PER FIM 36-10 SDR FDEA202304220745Skin · dentedRIGHT WING #11 SLAT UPPER SURFACE HAS A LARGE SMOOTH DENT 3" FORWARD OF TRAILING EDGE AND 50" FROM OUTBOARD EDGE AS MARKED. 0000493008 : CRAIL, ROGER L - 23-APR-2023 03:10 REPAIRED SLAT REF B767 SRM 51-70-10-2R. E.A. H-5750-T0374154 P1 WINGS - FLIGHT SURFASDR FDEA202210012442Case · damaged#1 ENGINE FWD FAN CASE, FWD OUTER LINER AT 1-2 O'CLOCK POSITION IS DAMAGED AROUND INBD INLET TEMP SENSOR. REF CF6-80C2 BOEING MM 72-22-02. IPC REF 72-33-01-05 ITEM 95, ORDERED LINER SEGMENT CPN 7214605 AOG ON MSN 2121530. MARKED WITH TAPE. C/W E.A. H-7233SDR FDEA202210012441Former · crackedRIGHT WING LEADING EDGE FORMER AT #5 SLAT WING STATION OSS 441 HAS EVIDENCE OF DAMAGE. REPLACE PART WITH NEW FORMER B67-57-002-02 ALONG WITH ANGLE B67-57-003-02 ON RS FLE OSS 441, ON LS FLE OSS 441, ATTACHED THE FORMER THROUGH THE SKIN AND REPLACE ALL LOSDR FDEA202210012440Former · crackedRIGHT WING LEADING EDGE FORMER AT #5 SLAT WING STATION OSS 441 HAS EVIDENCE OF DAMAGE. MWT REPLACE PART WITH NEW FORMER B67-57-002-02 ALONG WITH ANGLE B67-57-003-02 ON RS FLE OSS 441, ON LS FLE OSS 441, ATTACHED THE FORMER THROUGH THE SKIN AND REPLACE ALSDR FDEA202206221510Wire · sparksFO SEAT POWER CORD CRIMPED/SPARKED & TRIPPED CIRCUIT BREAKER. ADJUSTMENT SYSTEMS - INOP." FOUND CIRCUIT BREAKER IN. MOVED POWER CORD TO SEAT. SEAT REMAINED INOP AND CIRBUIT BREAKER DID NOT TRIP.PLACED ON MEL. ELECTRIC FUNCTION OF SEAT PLACED ON MELSDR FDEA202101220180Pseu · false activationMAIN CARGO DOOR CAUTION AT FL320 COMPLIED WITH QRH RELEASED FOR SERVICE PER MEL: 52-71-01-02. CATEGORY: C EXPIRATION: 01FEB21 "MEL 52-71-01-02: MAIN DECK CARGO DOOR INDICATION SYSTEM INOPERABLE. COMPLIED WITH QRH R&R PSEU REF B767-300 AMM 31-70-04-4-99.SDR FDEA202003060498Skin · gougedEXTERIOR FUSELAGE SKIN HAS 2EA DENT/GOUGES APPROX. 12" AFT OF THE MAIN E&E DOOR CUTOUT AT APPROX. LBL12. REPAIRED FUSELAGE SKIN AT STA 337 IAW FEDEX EA H-5310-T0352710, TITLED "FUSELAGE SKIN, STA 337, S-38L-S-39L, DENT AND GOUGES, DOUBLER REPAIRSDR FDEA202002270396Former · crackedRIGHT WING FIXED LE BEHIND SLAT 7 NOSE FORMER IS CRACKED AT FASTENER HOLE. REMOVED, FABRICATED, AND REPLACED RT WING FIXED LE NOSE FORMER IAW DWG 114T2170, DWG 114T2240 REV A AND SRM 51-40-02-OG.SDR FDEA2020022870396Former · crackedRW FIXED LE BEHIND SLAT #7 NOSE FORMER IS CRACKED AT FASTENER HOLE-DOT & STREAMER ATTACHED REMOVED, FABRICATED, AND REPLACED RW FIXED LE NOSE FORMER PER BAC DWG 1 114T2170 BAC DWG 114T2240 REV.A AND B767 SRM 51-40-02-OGSDR FDEA201802270512Relay · inoperativeTE FLAP DISAGREE MSG ON EICAS, WHEN MOVING FLAP LEVER FROM 5 TO 15, COMPLIED WITH QRH AND USED TE ALTN FLAP EXTENSION FOR FLAPS 20 LANDING. ASSOCIATED STATUS MSG "TE FLAP SHUTDOWN" IN STATUS PG. REMOVED AND REPLACED THE T/E FLAP SHUTOFF RELAY K351. AS PRECAUTISDR FDEA201708202288D-Ring · missingONE ESCAPE HARNESS UNDER THE LT SIDE JUMPSEAT IN COCKPIT MISSING A D-RING. THE D-RING WAS FOUND AND INSTALLED.SDR FDEA201702220626Switch · failedAFT CARGO DOOR ECIAS MSG DURING CRUISE. REPLACED THE SWITCH IAW AMM 52-71-03-2 AND OPS CHECKED GOOD IAW 52-71-00-5. OK FOR SERVICE.SDR FDEA201701190227Display · failedSTATUS MESSAGE FOR THE LANDING GEAR MONITOR. NO NOSE GEAR GREEN DOWN AND LOCKED LIGHT. FOLLOWED QRH ALT. EXTENDED GEAR STILL NO GREEN NOSE GEAR LIGHT. TROUBLESHOT IAW FIM 32-61 FT 812, PSEU FAULTING INTERNAL CARD CODE 010. REMOVED AND REPLACED PSEU IAW AMMSDR FDEA201607062297Warning System · activatedTAKEOFF CONFIG WARNING ACTIVATED AT 85KTS FOR 1/2, FOLLOWED BY A FLAP RED EICAS FOR 2 SECONDS. ABORTED TAKEOFF AT APPROX 100KTS. WARNING LIGHT WENT OUT IMMEDIATLY. FLAPS 5 T/O CHECKED NORMAL. TROUBLESHOT IAW FIM 31-51 FT 808, NO FAULTS FOUND. ACP BITE T
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