N101FE
Service difficulty reports · 20
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 = 'N101FE' 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 = 'N101FE' 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 FDEA202606250827Elec Connector · damagedFSS DISPLAY SHOWS UNARMED STATUS WHILE INFLIGHT. AMM: 26-90-03-2 EA: H-2624-T0387831 C/W E.A. H-2624-T0387831 TO RE-PIN D2166D PIN G8 TO F8. REACTIVATED FSS SYSTEM PER AMM REF ABOVE. CLOSED ALL DOORS AND SYSTEM PASSED AUTO ARM. NO FURTHER DEFECTS NOSDR FDEA202411291753Fitting · gouged#1 ENG WERE OB SHEAR TIE (FWD OF SKIRT BEAM) HAS CHAFFED INTO THE FWD BULKHEAD OF TORQUE BOX. DURING CURRENT HMV CHECK IN INDIANAPOLIS, IN (IND), MAINTENANCE DISCOVERED CHAFE AND GOUGE DAMAGE TO THE LH PYLON AFT ENGINE MOUNT BULKHEAD FITTING, P/N 311T2261SDR FDEA202411291752Floorbeam · damagedFOUND 2ND FROM THE BOTTOM IN WEB, WHERE STIFFENER ATTACHES AT STA. 246 LBL 24 HOLE DAMAGED, DAMAGE REMOVAL AT LBL 24 HOLE IS CURRENTLY 0.359" IN WEB MADE OF 0.025 7075-T6 WEB ATTACHES TO ANGLE ON FWD SIDE PN #141T5814-136. REPAIRED PER E.A.#:H-5310-T0381485SDR FDEA202411271750Door · delaminatedRH PYLON PNL# 447BL FOUND WITH MISSING TOP FIBERGLASS SKIN PLYS MISSING AND PAINTED OVER. REPAIRED TOP SKIN ON RH PYLON (PNL#447BL/MPN: 313T3341-9110) IN REF. TO 767 SRM 54-52-70- 2R FIG. 201 SHEET 4, AND 767 SRM: 51-70-08. THIS IS A MAJOR REPAIR. SEE JPF FSDR FDEA202411251731Floor Panel · damagedMAIN CARGO COMPARTMENT POSITION 12L APROX STA. 1383, FLOORBOARD ON LEFT SIDE HAS 1 PUNCTURE. MARKED WITH DOT #58. REPAIRED FLOORBOARD MAIN CARGO COMPARTMENT PANEL #251VFF, AT STA 1383 FLOORBOARD BETWEEN LBL 80.5"- LBL 82", P/N (146T5869-27), IN REF. TO SRMSDR FDEA202411251730Floor Panel · damagedMAIN CARGO COMPARTMENT, CENTER FLOORBOARD BETWEEN POSITION 6 AND 7 HAS 3 EA PUNCTURES. MARKED WITH DOT #'S 55, 56, AND 57. REPAIRED FLOORBOARD MAIN CARGO COMPARTMENT PANEL # 241WFF, AT STA 1033- STA 1060 CENTER FLOORBOARD BETWEEN RBL 3"- LBL 5.5", P/N (145SDR FDEA202408061091Warning Light · illuminatedMAIN CARGO DOOR EICAS MESSAGE AND CARGO DOORS LIGHT ILLUMINATED AT CRUISE FL350 TIME 0051Z. ALSO HAD RISING CABIN PRESSURE. RAN QRH AND DESCENDED TO 10,000 FEET PER QRH. AFTER LEVELING AT 10,000 FEET, EICAS MESSAGE AND CARGO DOORS LIGHT EXTINGUISHED AFTERSDR FDEA202305120861Skin · burnedFUSELAGE SKIN EXTERNAL SURFACE FOUND 4EA LIGHTNING STRIKES AT STA544- STA566 STGR38L- STGR39R REPAIRED THE FUSELAGE SKIN EXTERNAL SURFACE 4EA LIGHTNING STRIKES AT STA544- STA566 STGR38L- STGR39R PER B767 SRM51-40-02 & B767 SRM53-00-01-2R REPAIR.14. THE RESDR FDEA202210192611Apu · inoperativeAPU SHUTDOWN- FAULT LIGHT AFTER T.O. APPROXIMATELY 2000 FEET. APU IS REQUIRED PER MEL 24-00-01-01-B. ATTEMPT RESTART AS PER QRH. RESTART SUCCESSFUL. ON ARRIVAL APU SHUTDOWN AND FAULT INDICATED AGAIN. PERFORMED APU BITE PROCEDURE IAW FIM 49-11 FAULT TREESDR FDEA202106131521Skin · cracked.RH WING OUTBOARD TRAILING EDGE FLAP NOSE SKIN CRACKED , LOC:APPROX 120CM FROM INBD EDGE TO OUTBD EDGE. PERFORMED THE REPAIR ON RH WING OUTBOARD TRAILING EDGE FLAP NOSE SKIN PER B767 SRM 57-53-01-2R AND SRM 51-70-17. THE RSC TRACKING EA # :H-5750-T0362239 SDR FDEA2020060191087Unknown · odorVERY STRONG BURNING ODOR ON TAKEOFF ROLL. PERFORMED RTO AT 120 KNOTS. IAW TSI 72-00/7281 COMPLETED WITH BIRD STRIKE INSPECTION IAW FIM 71-05 FAULT TREE 872, COMPRESSOR STAGE 1 AND STAGE 12 BORESCOPE INSPECTION IAW AMM 72-00-00-6, NO DAMAGE FOUND. PERFORMED SDR FDEA201910012396Control Panel · burnedELECTRICAL FIRE IN LOWER LEFT SIDE OF OVERHEAD LIGHTS CONTROL PANEL CREW SAW AN ELECTRICAL FIRE ON OVERHEAD PANEL. SMOKE AND BURNING ODOR DETECTED. TROUBLESHOOT AND FOUND THE PANEL/FLOOD SWITCH S1 WIRES BURNED. REMOVED AND REPLACED THE LIGHT SWITCH IAWSDR FDEA201907181629Latch · wornPDIS 101 25-60 6211 18JUL19 ICN OPEN U LOGPAGES:3139917 F/O EMER ESCAPE ROPE DOORS KEEPS DROPPING OPEN AND WOULD NOT REMAINED CLOSED. ITEM DEFERRED PER THE NEF PROGRAM ITEM DEFERRED PER THE NEF: 25-10-26 FO ESCAPE ROPE STOWAGE COVER DOOR INOP.SDR FDEA201812043424Door · missingAT FL 340 HEARD LOW RUMBLING & LOW VIBRATION ON OUR FEET, NOISE & VIBRATION CEASED AT FL 160 ON DESCENT. ALL INDICATIONS NORMAL GOOD CABIN PRESSURE. AS A RESULT OF INSP FOUND RT RAD MISSING AND HINGE BROKEN. PERFORMED AIRFRAME VIBRATION CONDITIONAL INSPECTIONSDR FDEA201803160701Hook And Loop · looseTHE HOOK AND LOOP STRIP FOR THE FIRST OFFIER`S EVAS WAS FOUND LOOSE. SECURED THE EVAS HOOK AND LOOP STRIP IAW AMM 25-99-99-6. ACFT OK FOR SERVICE.SDR FDEA201707272055D-Ring · missingPOST FLIGHT, NOTED ONE ESCAPE HARNESS D-RING MISSING BELOW THE RT SUPERNUMERARY SEAT. INSTALLED THE NEW ESCAPE HARNESS D-RING.SDR FDEA201707081880Carabiner · missingDURING POST FLIGHT, FOUND DEMO ESCAPE HARNESS CARABINER MISSING. THE ESCAPE HARNESS WAS REMOVED AND A NEW CARABINER WAS INSTALLED IAW AMM 25-61-03-2. ACFT OK FOR SERVICE.SDR FDEA201612134399Converter · dirtyACRID ODOR IN THE COCKPIT, IN BEGINNING DESCENT. NO SMOKE OR OBSCURATION. INTENSE ODOR FOR 15-20 SECONDS THEN RAPIDLY DISSIPATED . NO ENGINE OR WING ANTI-ICE. NOT LIKE AN ELECTRICAL BURNING ODOR. ODOR OCCURRED THREE TIMES DURING DESCENT ON PREVIOUS FLT . OSDR FDEA201612124386Unknown · odorINTERMITTENT BURNING ODOR, DURING DESENT. CREW STATED DID NOT SEE ANY SMOKE, IT WAS A RUBBER ODOR AND NOT OVERPOWERING. PERFORMED SNIFF TEST OF THE AVIONICS IN AVIONICS BAY. MAIN CARGO COMPT, FLT DECK AND BELLIES WITH PACKS RUNNING ON APU. RAN BOTSDR FDEA201403140504Sensor · out of adjustENTRY DOOR SHOWED OPEN UPON LANDING. ACFT BLOCKED IN BEFORE DOOR WAS OPENED. RELEASED FOR SERVICE IAW MEL 52-71-01-01 CAT C. CREW ENTRY DOOR INDICATION SYS INOPERATIVE. VERIFY & RECORD IN AML & EAML THAT ASSOCIATED DOORS ARE CLOSED, LATCHED, & LOCKED PRIOR
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