N115FE
Service difficulty reports · 40
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 = 'N115FE' 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 = 'N115FE' 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 FDEA202609141334Skin · damagedNR 10 SLAT HAS MINOR DAMAGE ON LOWER SURFACE APPROXIMATELY 31.5" FROM INBD EDGE. REPAIRED RT WING NR 10 SLAT T/E WEDGE AT OSS 713 .5 IAW SRM 57-43-02-2R AND SRM 51-7-10-2R. THIS IS A MAJOR REPAIR.SDR FDEA202601230081Window · hazeL3, R1, R3 WINDOWS DELAMINATING OBSCURING CRITICAL VISIBILITY AREA AND CREATING A FLIGHT SAFETY HAZARD. AMM: 56-11-00-6-0 REF WRI 56-10/1646, R1 (F/O WONDSHIELD) WINDOW IS UNDER OIL FOR DELAMINATION. NO ADDITIONAL DELAMINATION NOTICED. ALL 3 WINDOWS R1, SDR FDEA202512142251Skin · dentedLEFT WING NR 5 SLAT HAS A DENT IN UPPER TRAILING WEDGE SKIN 34 INCHES FROM INBD EDGE. REPAIRED LT WING NR 5 SLAT UPPER T/E WEDGE SKIN IAW SRM 57-43-02-0I, PG 1-2, DETAIL 1 & 2, SRM 51-70-10-2R, AND AMM 51-21-10-7. MAJOR REPAIR. SEE JPF FOR OTHER WORK ACCOMPLSDR FDEA202512142250Skin · dentedLEFT WING NR 1 SLAT HAS DENT IN UPPER TRAILING WEDGE SKIN 16" FROM I/B EDGE. REPAIRED LEFT WING NR 1 SLAT UPPER T/E WEDGE SKIN SURFACE 16" FROM I/B EDGE IAW SRM 57-43-02-0I, PG 1-2 DETAIL 1 & 2, B767 SRM 51-70-10-2R, AND AMM 51-21-10-7. MAJOR REPAIR. SEE JPFSDR FDEA202511272214Idg · failedR GEN DRIVE EICAS IN-FLIGHT. ACCOMPANIED BY ILLUMINATED R GEN DRIVE SWITCH LIGHT. COMPLIED WITH QRH. EMERGENCY DECLARED. PERFORMED RT ENG RUN TEST BER AMM 71-00-00-5-3, FOUND RT GEN CONT OFF LIGHT ON. BITE OF BPCU FOUND FAULT RT ENG GEN MPU/WIRING. WIRSDR FDEA202511112158Flap System · faultedAT APPROX 80 KTS ON TAKEOFF GOT EICAS FLAPS AND CONIF. REJECTED THE TAKEOFF RUNWAY 02R AT BKK AT 303 TOGW AND 31C TEMP. RAN CHECKLISTS, RETURNED TO THE GATE LEAVING FLAPS AT 5. PERFORMED T/S AS PER FIM 31-51 FT 808, NO FAULT FOUND. PERFORMED BITE PROCEDURSDR FDEA202409051247Battery · no testMDIS 115 33-50 0178 05SEP24 02:24 TPE FACT DURING SERVICE CHECK, FOUND EMERGENCY LIGHT DIDN'T ILLUMANATE. FACT 05SEP24 02:30 TPE FIM: 33-51-00-815-802 AMM: 33-51-07-2-0 REF ABOVE REFERENCE PERFORMED T/S AND FOUND THE BATTERY PACK OF THE POSDR FDEA202403080261Sliding Window · crackedFO NOTICE IN FLIGHT CRACKING ON PERIMETER OF WINDOWS. RAN CHECKLIST FOR CRACKED WINDOW IN FLIGHT. AS PER CREW DEBRIEF F/O SLIDING WINDOW CRACKED ALONG THE EDGE. NO ARCING AND NO LEAKAGE OR PRESSURISATION ISSUES. CARRIED OUT INSPECTION AND CHECKS FOUNDSDR FDEA202203310790None · noneON APPROACH INTO SKBO (BOG) AT APPROXIMATELY 10700 MSL, AFTER PUTTING THE LANDING GEAR DOWN, WE ONLY GOT GREEN NOSE GEAR AND A GREEN RIGHT MAIN GEAR LIGHTS. WE ACCOMPLISHED A GO AROUND AND BEGAN TO RUN THE QRH. AFTER RUNNING THE QRH, WE HAD THE SAME INDSDR FDEA202203010383None · noneRECEIVED MAIN CARGO DOOR ALERT AT FL 390. QRH WAS FOLLOWED AND DIVERTED TO KJAX. NO PRESSURIZATION ISSUES WERE NOTED AT ANY TIME. ALERT WENT AWAY ON DESCENT PASSING FL 240. REVERSED MEL 52-71-01-02. RE-PERFORMED CARGO DOOR PROX TEST RESDR FDEA202202110749None · noneMDIS 115 33-50 6883 11FEB22 BOG DURING POSFLIGHT CHECK FOUND DOOR EMERGENCY LIGHT TOO DIM. FOUND WRONG LAMP INSTALLED. RELAMPED DOOR EMERGENCY LIGHT IAW AMM33-51-03-2 AND PROPER LAMP PART NUMBER IAW IPC 33-51-50-01.SDR FDEA202201140069None · shearedREFER TO HUB STRIKE DAMAGE TO LH SLAT UPON INSPECTION OF UNDERLYING STRUCTURE AFTER REMOVAL OF BONDED PANEL ASSY 521ZB, DISCOVERED HOLE IN LEFT WING FIXED LEADING EDGE PANEL. HOLE IS APPROX. 2.5 X 2.0". COMPLIED WITH EA H-5720-T0366424 PART 1. "WING-SECONDASDR FDEA202104210962Transmitter · out of adjustLE SLAT DISAGREE ADJUSTED FLAP HANDLE POS. TRANSMITTERS ON TSI 27-80/6190. PERFORMED FLAP AND SLAT PRIMARY DRIVES AND POSITION INDICATING SYSTEM - TEST REF AMM 27-51-00-5. ALL TEST PASSED.SDR FDEA202102170386Floor Panel · damagedMAIN CABIN FLOOR PANEL 241DFF HAS DAMAGE TO SKIN REPAIRED FLOOR PANEL 241DFF PER B767 SRM 53-00-50-2R PARA 4.ESDR FDEA202102170385Skin · crackedLH WING, FIXED LEADING EDGE SKIN IS CRACKED @ FASTENER HOLE @ OSS 665 REPAIRED LEADING EDGE SKIN IAW B767 SRM 57-41-01-2R, FIGURE 201SDR FDEA202102160375Shear Tie · cracked#2 PYLON @ DOOR 447BL, FWD SKIRT BEAM SHEAR TIE IS CRACKED REMOVED AND REPLACED SHEAR TIE PER BAC DWG 313T2310REV -SDR FDEA202102160374Beam · crackedLEFT WING NOSE BEAM IS CRACKED @ OSS 679 REPAIRED NOSE BEAM WEB IAW B767 SRM 57-41-13-2R, RPEIAR 3SDR FDEA202102120343Support Angle · crackedAS SEEN FROM BULK PIT AREA, SEAT TRACK SUPPORT ANGLE @ STA 1576, INSIDE R/H SIDEWALL AREA IS CRACKED REMOVED AND REPLACED SEAT TRACK SUPPORT ANGLE PER BAC DWG146T5650 REV C.SDR FDEA202102120342Support · crackedSEAT TRACK SUPPORT ANGLE @ STA 1576, INSIDE L/H SIDEWALL AREA SEAT TRACK SUPPORT ANGLE IS CRACKED REMOVED AND REPLACED SUPPORT ANGLE PER BAC DWG 146T5650 REV C.SDR FDEA202102120338Beam · crackedR/W L/E LOWER NOSE WEB IS CRACKED.(FWD OF FUEL/DEFUEL PANEL 621QB.) REMOVED DAMAGED WEB SECTION AND REPAIRED IAW B767 SRM 57-41-13-2R. TREATED REPAIR AREA IAW B767 SRM 51-21-01.SDR FDEA202102110336Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241WFF HAS FIBER DAMAGE. FABRICATED FLOOR PANEL 241KFF PER SRZ-25-005 REV R.SDR FDEA202102110335Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241KFF HAS FIBER DAMAGE FABRICATED NEW FLOOR PANEL PER SRZ-25-005 REV R.SDR FDEA202102100320Seal · crackedLEFT WING FIXED L/E INNER STRAP CRACKED AT L.E.S 555. REMOVED AND REPLACED STRAP AT L.E.S 555 IAW B767 SRM 51-40-02, 51-40-05 AND BAC DWG 114T2800 REV.CSDR FDEA202102090317Floor Support · crackedBULK CARGO COMPARTMENT FLOOR SUPPORT STRINGER IS CRACKED AT RBL 36.91 AT STA.1480. REMOVED AND REPLACED FLOOR STRINGER SECTION AT RBL 36.91 IAW B767 SRM 51-40-02 AND BAC DWG 146T3002 146T3002 REV.E.SDR FDEA202102070305Attach Angle · crackedR/H WING L/E FORMER ATTACH ANGLE CRACKED @ OSS 441 REMOVED CRACKED FORMER ATTACH ANGLE/INSTALLED NEW L/E FORMER ATTACH ANGLE IAW IAW BAC DWG 114T2241 REV-SDR FDEA202102070301Former · crackedLEFT WING L/E FORMER CRACKED @OSS 441 RRMOVED CRACKED FORMER/INSTALLED NEW FORMERIAW BAC DWG114T2241 REV-SDR FDEA202102070307Former · crackedR/H WING L/E FORMER CRACKED @ OSS499 REMOVED CRACKED R/H L/E FORMER/INSTALLED NEW R/H L/E FORMER @ OSS 499SDR FDEA202102070306Former · crackedR/H WING L/E FORMER CRACKED @ OSS 565 REMOVED CRACKED R/H L/E FORMER/INSTALLED NEW R/H L/E FORMER IAW BAC DWG 114T2512 114T2512 REV DSDR FDEA202102070304Former · crackedR/H WING L/E FORMER CRACKED @ OSS 441 REMOVED CRACKED FORMER/INSTALLED NEW FORMER IAW BAC DWG 114T2241 REV-SDR FDEA202102070303Former · crackedL/H WING L/E FORMER CRACKED @ OSS 565 REMOVED CRACKED FORMER/INSTALLED NEW FORMER IAW BAC DWG 114T2162 REV-SDR FDEA202102070302Attach Angle · crackedL/H WING L/E FORMER ATTACH ANGLE CRACKED @ OSS 437 REMOVED CRACKED FORMER ATTACH ANGLE/INSTALLED NEW FORMER ATTACH ANGLE IAW BAC DWG 114T2240 REV-SDR FDEA202102070300Attach Angle · crackedL/H WING FORMER ATTACH ANGLE CRACKED @OSS441 REMOVED CRACKED FORMER ATTACH ANGLE/INSTALLED NEW ANGLE IAW BAC DWG114T2241,REV-SDR FDEA202102010262Flange · crackedAFT LOWER CARGO PIT STA. 1087 VERTICAL FLANGE BELOW FLOOR LINE AT LBL25 UPPER END IS CRACKED. REMOVED AND REPLACED AFT LOWER CARGO PIT STA.1087 VERTICAL FLANGE BELOW FLOOR LINE AT LBL25 IAW B767 SRM 51- 40-02 AND BAC DWG 140T0130 REV.G.SDR FDEA2019122313277Ecu · malfunctionedCRUISE FL370 SCANNING OVERHEAD PRIOR TO DESCENT. OBSERVED RT EEC ALTN IN MODE SWITCH. NO ACCOMPANY EICAS. REFERENCED QRH, DECIDED TO PUT BOTH EEC IN SAME MODE "ALTN". ACCOMPLISHED QRH. UPON PUSHING THROTTLES UP N1 AND EGT BEGAN FLUXING. FF AT IDLE WOULD NSDR FDEA2018080311862Light · inoperativeUPON LOWERING GEAR HAD NOSE & LEFT GEAR INDICATION BUT NO RIGHT GEAR INDICATION. RAN CHECKLIST FOR GEAR DISAGREE. JUMPSEATER WAS ABLE TO GET US A BULB TO REPLACE AND GEAR SHOWED ALL GREEN. CREW HAD REPLACED 1 BULB ON GO-AROUND, REPLACED OTHER BULB I/R/T MM 33SDR FDEA201803070639Module · malfunctionedCAPT ALTIMETER INDICATING 300' LOW DURING CLIMB AFTER 18,000' AT FL340 AND AFTER DESCENT TO FL280. ERROR WENT AWAY AFTER 15-20 MINUTES F/O & STBY ALT INDICATED SAME READING. REMOVED AND REPLACED CAPTAINS AIR DATA MODULE PER AMSDR FDEA201710263047Switch · failedAFTER FLYING THIS AIRPLANE FOR A COUPLE DAYS IN A ROW, THE SOURSE OF BURNING RUBBER SMELL IS FROM THE RIGHT "RUNWAY TURNOFF" LIGHT. EACH TIME WE TURNED IT ON, WE GOT THE ODER. IT'S NOT THE RIGHT PACK. (RIGHT) RUNWAY TURNOFF LIGHT INOP. R&R RT SIDE RUNWAY TURNSDR FDEA201708172244Indicator · inoperativeALTERNATE GEAR EXTEND WAS USED DUE TO THE RIGHT MLG GEAR INDICATION INOPERATIVE. COMPLIED WITH CHECK OF NOSE AND MLG LOAD LIMITER CLEARANCES, ALL WITHIN LIMITS IAW 32-35-00-5., OK TO CONTINUE.SDR FDEA201708162241Lamp · inoperativeRIGHT MAIN GEAR LIGHTS DID NOT WORK ON GEAR EXTENSION. COMPLIED WITH RED TABS. REPLACED THE LAMPS IN THE RIGHT MAIN GEAR DOWN INDICATION IAW 20-84-18. OK TO CONTINUE. REPLACED THE LAMPS IN THE RIGHT RIGHT MAIN GEAR DOWN INDICATOR.SDR FDEA201507202282Light · inoperativeEXTERNAL EMER LIGHT IS INOPERATIVE, RIGHT BELOW DOOR. RELAMPED EXTERIOR EMER LIGHT IAW AMM33-51-16-2. OPERATIONS CHECKED GOOD.
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