N618FE
Service difficulty reports · 366
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 = 'N618FE' 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 = 'N618FE' 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 05FDEA00153Line · leakingENG - 3 A-ICE DISAG, ILLUMINATED WITH SWITCH OFF. TURNED SWITCH ON, DISAG LT STILL ON. TURNED A/I OFF, DISAG LT STAYED ON FOR APPROX 15 MINUTES THEN WENT OUT. MEL 24JAN05 RELEASED FOR SERVICE PER MEL/CDL: 30-22-01-02-A CATEGORY: C EXPIRATION: 03FEB05 ENG NSDR 04FDEA03337Doubler · crackedCENTER LANDING GEAR WHEEL WELL RT STA Y= 1381, DOUBLER FOUND CRACKED AT LOCATION ADJACENT TO RT SPOILER MIXER. DOUBLER FABRICATED PER DOUGLAS DRAWING NR AEA0526 AND PART MARKED PER GMM 7-0-1001. CRACKED DOUBLER AT CENTER LANDING GEAR WHEEL WELL RT STA Y= 138SDR 04FDEA03301Battery · failed"EMERGENCY POWER TEST FAIL" ALERT DISPLAY. TWO (2) EACH MAIN BATTERY (P/N: 31433-001) REMOVED AND REPLACED PER AMM 24-34-02-4. OPERATIONAL TEST OF THE MAIN BATTERY CARRIED OUT PER AMM 24-34-02-5. FOUND SATISFACTORY. POSITION 1, S/N OFF: 10101125, S/N ON:10SDR 04FDEA03178Fitting · corrodedBARREL NUT BORE NR 3L EXCEEDED LIMITS AFTER CORROSION REMOVAL. REFERENCE TO EO 1-5510-7-5000 C4 PT1, BARREL NUT BORE NR 3L REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS - HORIZONTAL STABILIZERS - BARREL NUT BORE REWORK/ REPAIR.SDR 04FDEA03177Fitting · corrodedBARREL NUT BORE NR 35R EXCEEDED LIMITS AFTER CORROSION REMOVAL. REFERENCE TO EO 1-5510-7-5000 C4 PT1, BARREL NUT BORE NR 35R, REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS, HORIZONTAL STABILIZERS, BARREL NUT BORE REWORK/REPAIR.SDR 04FDEA03158Fitting · corrodedBARREL NUT BORE NR 26L EXCEEDED LIMITS AFTER CORROSION REMOVAL. BARREL NUT BORE FITTING NR 26L, REMOVED AND REPLACED PER SRM 51-33-01 VOLUME 2.SDR 04FDEA03156Fitting · corrodedBARREL NUT BORE NR 30L EXCEEDED LIMITS AFTER CORROSION REMOVAL. BARREL NUT BORE NR 30L REPAIRED PER FEDEX EA 1-5510-79789, STABILIZERS - HORIZONTAL STABILIZERS - BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000.SDR 04FDEA03157Fitting · corrodedBARREL NUT BORE NR 14L EXCEEDED LIMITS AFTER CORROSION REMOVAL. BARREL NUT BORE FITTING NR 14L, REMOVED AND REPLACED PER SRM 51-33-01 VOLUME 2.SDR 04FDEA03155Structure · corrodedBARREL NUT BORE NR 28L. EXCEEDED LIMITS AFTER CORROSION REMOVAL. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03154Structure · corrodedBARREL NUT BORE NR 34R. EXCEEDED LIMITS AFTER CORROSION REMOVAL. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03152Fitting · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 21R EXCEEDED LIMITS. REF TO EO 1-5510-7-5000 C4 PT1, BARREL NUT BORE NR 21R. REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS, HORIZONTAL STABILIZERS, BARREL NUT BORE, REWORK/REPAIR, 1-5510-7-5000.SDR 04FDEA03150Fitting · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 15R EXCEEDED LIMITS. REFERENCE TO EO 1-5510-7-5000 C4 PT1, BARREL NUT NR 15R REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS, HORIZONTAL STABILIZERS, BARREL NUT BORE REWORK/REPAIR - 1-5510-7-5000.SDR 04FDEA03143Seat Track · crackedMAIN DECK SEAT TRACK AT STA Y= 635, X= -8 FOUND WITH APPROXIMATELY FOUR (4) INCHES CRACKED AFTER FORWARD CARGO CEILING PANEL OPEN UP. MAIN DECK SEAT TRACK AT STA Y= 625 TO Y= 655, X= -8 CUT AND REMOVED PER SRM 51-31-01 VOLUME II. NEW SEAT TRACK FABRICATED ASDR 04FDEA03153Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 7R EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03151Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 17R EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03149Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 1R EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03148Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 32L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03147Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 24L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03146Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 20L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03145Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 16L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789, HORIZONTAL STABILIZERS BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000SDR 04FDEA03144Structure · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 2L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03121Seat Track · crackedMAIN DECK SEAT TRACK FOUND WITH THREE (3) INCHES CRACKED AFTER FORWARD CARGO CEILING PANEL OPEN UP AT STA Y= 635, X= -8. CUT AND REMOVED AT STA Y= 625 TO Y= 655, X= 8 PER SRM 51-31-01 VOLUME II. NEW SEAT TRACK FABRICATED AND INSTALLED PER SRM 53-70-00 VSDR 04FDEA03120Structure · corrodedBARREL NUT BORE NR 36R AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03119Structure · corrodedBARREL NUT BORE NR 24R AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03118Structure · corrodedBARREL NUT BORE NR 20 RT, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIR PER FEDEX EA 1-5510-79789.SDR 04FDEA03117Structure · corrodedBARREL NUT BORE NR 16R, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03116Structure · corrodedBARREL NUT BORE NR 27L. AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03115Structure · corrodedBARREL NUT BORE NR 25L, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03114Structure · corrodedBARREL NUT BORE NR 23L, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.SDR 04FDEA03113Structure · corrodedBARREL NUT BORE NR 19L, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIR PER FEDEX EA 1-5510-79789.SDR 04FDEA03112Frame · chafedMAIN DECK CARGO COMPARTMENT, RT STA 535 FRAME FOUND CHAFED AT UPPER AND LOWER YOKE MOUNTING AREA. TRIMMED OUT AND REPAIRED PER FEDEX DRAWING SRZ-53-503 AND SRM 51-31-01 VOLUME I.SDR 04FDEA03111Track · crackedNR 1 ENGINE, RT TRUST REVERSER UPPER SLIDER TRACK CRACKED. R / R PER WORK CARD 78T3901-R.SDR 04FDEA03097Control Valve · crackedHFEC INSPECTION CARRIED OUT ON HORIZONTAL STABILIZER TRIM CONTROL VALVE AND CRACK FOUND AT UPPER CONTROL VALVE BORE APPROXIMATELY 0.25 INCH LENGTH FROM PRESSURE PASSAGE BORE. REMOVED AND REPLACED PER AMM 27-43-42-4. OPERATION CHECK CARRIED-OUT PER AMM 27-40-SDR 04FDEA03095Longeron · dentedMAIN DECK CARGO, EXISTING REPAIR ON FRAME AT RT STA Y= 1681, LONGERON 12R FOUND WITH DENT/CHAFFED. REPAIRED PER SRM 53-30-00 VOLUME I, FIGURE 1 AND SRM 51-33-01 VOLUME II. RE-INSPECTION TO BE ACCOMPLISHED AT 16,292 FLIGHT CYCLES WITH REPETITIVE INSPECTION THSDR 04FDEA03094Longeron · dentedMAIN DECK CARGO, LONGERON FOUND DENT AT RT STA Y= 1547, LONGERON 13. SMOOTHENED PER SRM 51-00-00 VOLUME I, PAGES 1 AND 2. HFEC INSPECTION CARRIED OUT PER DAC NDT SPM REV. 11, CHAPTER 06.10.01.001, NO CRACK FOUND.SDR 04FDEA03093Structure · corrodedCORROSION REMOVED ON NR 14 RT BARREL NUT BORE FOUND EXCEEDED LIMITS. FITTING REMOVED AND REPLACED (P/N ALC8106Y2) PER SRM 51-33-01 VOLUME II.SDR 04FDEA03092Structure · corrodedCORROSION REMOVED ON NR 26 RT BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED (P/N ALC8107Y2) PER SRM 51-33-01 VOLUME II.SDR 04FDEA03091Stringer · crackedBOOSTER PROGRAM, RT WING STRINGER 11 END FOUND WITH APPROXIMATELY 11.5 INCH CRACK AS VIEWED FROM ACCESS PANEL NR 636AB. ARB751-1. REMOVED PER SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II.SDR 04FDEA03090Bracket · crackedLT WING OUTBOARD FLAP HINGE FWD FAIRING SUPPORT BRACKET FOUND CRACKED AT INBOARD LOWER. BRACKET REMOVED AND REPLACED PER SRM 51-05-01 VOLUME II.SDR 04FDEA03089Stringer · crackedLT WING STRINGER 11 END FOUND WITH APPROXIMATELY 11.5 INCH CRACKED AS VIEWED FROM ACCESS PANEL NR 536AB. REMOVED PER SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II.SDR 04FDEA03088Skin · damagedLT WING UPPER SURFACE STA XOS=772, ON PREVIOUS METAL FILLER REPAIR FOUND EXISTING BLENDOUT EXCEEDED SRM 57-10-00, VOLUME 1, FIGURE 32 SHEET. NR 2 LIMITS. BLENDOUT DIMENSION: LENGTH=1.5 INCH, WIDTH= 1.25 INCH, DEPTH=0.0052 INCH; ORIGINAL THICKNESS= 0.312 ISDR 04FDEA03067Frame · dentedMAIN DECK CARGO, EXISTING REPAIR ON FRAME AT RT STA 1681, LONGERON 12. FOUND WITH DENT/CHAFFED. REMOVED PER SRM 51-33-01 VOLUME II. REPAIR DOUBLER FABRICATED PER SRM. REPAIR DOUBLER INSTALLED PER SRM 51-33-01 VOLUME II. REFER TO EA 1-5310-79792, FUSELAGE SDR 04FDEA03066Longeron · dentedMAIN DECK CARGO, LONGERON FOUND DENT AT RT STA 1547, LONGERON 13. SMOOTHENED PER SRM 51-00-00 VOLUME I, PAGES 1 AND 2. HFEC INSPECTION CARRIED OUT PER DAC NDT SPM REV. 11, CHAPTER 06.10.01.001, NO CRACK FOUND.SDR 04FDEA03065Seat Track · wornMAIN DECK CARGO, SEAT TRACK FOUND WORN AT LT STA 752 - 760, X= 25. REMOVED FROM L/H STA Y= 745 - Y= 815, X= 25 PER SRM 51-31-01 VOLUME II. NEW SEAT TRACK FABRICATED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND INSTALLED PER SRM 51-31-01 VOLUME II.SDR 04FDEA03064Seat Track · corrodedMAIN DECK, L1 DOOR WAY SEAT TRACK FOUND CORROSION BETWEEN STA 425 - 445. REMOVED PER SRM 51-31-01 VOLUME II. SEAT TRACK P/N ABA760-505 FABRICATED PER DOUGLAS DRAWING ABA7680 AND SRM 51-35-01 USING ABA760-5070 RAW MATERIAL. FABRICATED SEAT TRACK INSTALLEDSDR 04FDEA03063Seat Track · wornMAIN DECK CARGO, SEAT TRACK FOUND WORN AT RT STA 999, X= - 8. TRIMMED OUT PER MD-11 SRM 53-70-00 VOLUME I FIGURE 1. REPAIR PARTS FABRICATED AND INSTALLED PER MD-11 SRM 53-70-00 VOLUME I FIGURE1.SDR 03FDEA01583Actuator · inoperativeON DEPARTURE FLAPS NO RETRACT PLEASE. REMOVED AND REPLACED FLAP LIMITER DUPLEX ACTUATOR IAW MM 27-56-01-0 4. PERFORMED ADJUSTMENT OF FLAP LIMITER ACTUATOR IAW MM 27-50-00-5, ALSO PERFORMED FUNCTIONAL TEST OF THE FLAP LIMITER ACTUATOR IAW MM 27-50-00-5, CHESDR 03FDEA01102Skin · corrodedRT WING UPPER SURFACE FOUND CORROSION AT BETWEEN XORS799.4 AND XORS826.5 FWD OF FIXED PANEL. RT WING UPPER SURFACE CORROSION AT BETWEEN XORS799.4 AND XORS826.5 FWD OF FIXED PANEL REPAIR CARRIED AS PER FEDEX EA 1-5720-69365 WINGS OUTER WING / RT OUTER AFT SKINSDR 03FDEA01101Attach Fitting · corrodedLT WING OUTBD FLAP OUTBD HINGE ( A/C SIDE ) LOWER OUTBD ATTACH POINT ( TO AFT SPAR ) HOLE CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-71841 WINGS - TRAILING EDGE FLAPS - OUTBOARD TRAILING EDGE FLAP - OUTBOARD FLAP HINGE BRACKETS LOWER OUTBOARD ATTACSDR 03FDEA01103Frame · crackedCENTER CARGO DOOR CUT OUT LOWER AFT CORNER FOUND ROLLER TRAY SUPPORT CHORD CRACK. ***** S/D COMING ****
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