N620FE

Service difficulty reports · 352

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 = 'N620FE' 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.

SDR 07FDEA05112Engine · power lossDURING CLIMB FROM FL320 TO FL340 NOTICED A/C DETERIORATION. NR 2 ENG EPR READ .40 LESS THAN NR 1 AND NR 3. N1 READING 20 PERCENT LESS THAN 1 AND 3, N2 20 PERCENT LESS AS WELL. ENG 2 THROTTLE, MOVEMENTS RESULTED IN SLUGGISH RESPONSE W/MAX EPR OUTPUT OF 1.0Dec 20, 2007 · N620FE · Doug MD11F · Engine (Turbine/Turboprop)SDR 07FDEA04618Door · crackedRIGHT MAIN LANDING GEAR FLIPPER DOOR FOUND CRACKED PASS THROUGH STOP DRILL. 10-30-07 REMOVED AND REPLACED AS PER AMM 32-14-10-4. OPERATION CHECK CARRIED OUT AS PER AMM 32-31 -00-700-803. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 17, 2007 · N620FE · Doug MD11F · Landing Gear DoorsSDR 07FDEA04606Support Fitting · crackedCRACK FOUND DURING HFEC OPEN HOLE INSPECTION ON THE MOST OUTBOARD, LOWER FASTENER HOLE COMMON TO THE ARC4008 AND ARC4009 LEFT OUTBOARD FLAP SUPPORT FITTING. 10-30-07 REMOVED AND REPLACED AS PER MD11 CMM 57-52-04. FLAP ADJUSTMENT TEST CARRIED OUT AS PEROct 16, 2007 · N620FE · Doug MD11F · Trailing Edge FlapsSDR 07FDEA04605Support Fitting · crackedCRACK FOUND DURING HFEC OPEN HOLE INSPECTION ON THE MOST OUTBOARD, LOWER FASTENER HOLE COMMON TO THE ARC4008 AND ARC4009 RIGHT WING OUTBOARD FLAP SUPPORT FITTING. 10-30-07 REMOVED AND REPLACED AS PER MD11 CMM 57-52-04. FLAP ADJUSTMENT TEST CARRIED OUT Oct 16, 2007 · N620FE · Doug MD11F · Trailing Edge FlapsSDR 07FDEA04604Seat Track · crackedMAIN DECK CARGO COMPARTMENT RIGHT FLOOR SEAT TRACK AT STATION 755, X = -8.5, FOUND CRACKED APPROXIMATELY 3 INCHES. 10-30-07 REPAIRED BY REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 16, 2007 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04603Seat Track · crackedMAIN DECK CARGO COMPARTMENT RIGHT FLOOR SEAT TRACK AT STATION 635, X = -47.5, FOUND CRACKED APPROXIMATELY 3 INCHES. 10-30-07 REPAIRED BY REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 16, 2007 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04602Attach Fitting · crackedAFT FUSELAGE INTERIOR FOUND DOG HOUSE LOCATION WITH FRAME CLIP QUANTITY 01 EACH CRACKED AT STATION Y2069. 10-30-07 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 16, 2007 · N620FE · Doug MD11F · Fuselage Main, Attach FittingsSDR 07FDEA04601Longeron · crackedONE FASTENER HOLE FOUND CRACK AT 3 AND 9 O'CLOCK POSITION AT RIGHT SIDE TRUNNION FITTING LOWER LONGERON. 10-30-07 REMOVED AS PER SRM 51-31-01 VOLUME II. LONGERON FABRICATED AS PER FEDEX EA 1-5310-116497, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 16, 2007 · N620FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 07FDEA04584Seat Track · crackedMAIN DECK CARGO COMPARTMENT LEFT FLOOR SEAT TRACK AT STATION 635, X = 47.5 FOUND CRACKED APPROXIMATELY 3 INCHES. 10-30-07 REPAIRED BY REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 13, 2007 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04583Seat Track · crackedMAIN DECK CARGO COMPARTMENT LEFT FLOOR SEAT TRACK AT STATION 635, X = 27.5 FOUND CRACKED APPROXIMATELY 3 INCHES. 10-30-07 REPAIRED BY REPLACEMENT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 13, 2007 · N620FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04582Rib · crackedLEFT WING LEADING EDGE CAVITY AREA RIB ANGLE AT STATION XOS 584 FOUND CRACKED. 10-29-07 REMOVED CRACKED RIB ANGLE (FORMER) AS PER SRM 51-31-01 VOLUME II AND FABRICATED FORMER AS PER DOUGLAS DRAWING ARB2931 AND INSTALLED FORMER AT LEFT HAND WING LEADINGOct 13, 2007 · N620FE · Doug MD11F · Wing, Rib/BulkheadSDR 07FDEA04581Rib · crackedRIGHT WING LEADING EDGE CAVITY RIB DOUBLER AT STATION XOS 789 (XORS 683) FOUND CRACKED. 10-29-07 REMOVED CRACKED RIB DOUBLER AS PER SRM 51-31-01 VOLUME II AND FABRICATED RIB DOUBLER AS PER DOUGLAS DRAWING ARB3954 AND INSTALLED AT RIGHT HAND WING LEADINOct 13, 2007 · N620FE · Doug MD11F · Wing, Rib/BulkheadSDR 07FDEA04572Skin · dentedLT WING INBOARD FLAP LOWER SURFACE FOUND DENTED. 10-29-07 REPAIR CARRIED OUT AT LT WING INBOARD FLAP LOWER SURFACE AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 11, 2007 · N620FE · Doug MD11F · Trailing Edge FlapsSDR 07FDEA04571Trunnion · crackedNOSE LANDING GEAR RT TRUNNION FITTING CRACKED. CARRIED OUT REPAIR AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 11, 2007 · N620FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR 06FDEA03804Unknown · warning lightDURING CLIMB, SELECTED ALL ANTI-ICE TO ON. GOT IMMEDIATE LEVEL 1 "ENG 2 A-ICE OFF" ALERT COMBINED WITH ENG 2 ANTI-ICE VALVE DISAGREE LIGHT ON ENG 2 A/I SWITCH. DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ANTI-ICE VALVE AND PRESSURE SWIOct 27, 2006 · N620FE · Doug MD11 · Air Intake Anti/De-Ice SystemSDR 06FDEA2385Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND RT TRUNNION MATING SURFACE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL THICKNESS = 2.500", TOP SPOTFACE MATERIAL REMOVED = 0.007" (FWD), TOP SPOTFACE MATERIAL REMOVED = 0.0125" (AFT), LOWER MAJun 22, 2006 · N620FE · Doug MD11 · Main Landing Gear Attach SectionSDR 06FDEA2384Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND RIGHT HAND TRUNNION ALIGNMENT PIN HOLE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL HOLE DIAMETER = 1.502", FINAL HOLE DIAMETER = 1.6502", MAXIMUM ALLOWABLE LIMIT DIAMETER = 1.680" AND FOUND WITHINJun 22, 2006 · N620FE · Doug MD11 · Main Landing Gear Attach SectionSDR 06FDEA2383Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND RIGHT HAND TRUNNION AFT MOUNTING HOLE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL HOLE DIAMETER = 1.280", FINAL HOLE DIAMETER = 1.3776", MAXIMUM ALLOWABLE DIAMETER = 1.385" AND FOUND WITHIN LIMIJun 22, 2006 · N620FE · Doug MD11 · Main Landing Gear Attach SectionSDR 06FDEA2382Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND RIGHT HAND TRUNNION FORWARD MOUNTING HOLE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL HOLE DIAMETER = 1.280", REWORKED HOLE DIAMETER = 1.3768", MAXIMUM ALLOWABLE DIAMETER = 1.385" AND FOUND WIJun 22, 2006 · N620FE · Doug MD11 · Main Landing Gear Attach SectionSDR 06FDEA2381Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND LEFT HAND TRUNNION MATING SURFACE CORRODED. REWORKED AS PER FEDEX E.A. 1-5340-99703, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 22, 2006 · N620FE · Doug MD11 · Main Landing Gear Attach SectionSDR 06FDEA2380Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND LEFT HAND TRUNNION ALIGNMENT HOLE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL BORE DIAMETER = 1.502", FINAL BORE DIAMETER = 1.6766", MAXIMUM ALLOWABLE DIAMETER = 1.680" AND FOUND WITHIN LIMIT AS PJun 22, 2006 · N620FE · Doug MD11 · Main Landing Gear Attach SectionSDR 06FDEA2379Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND LEFT HAND TRUNNION AFT MOUNT HOLE CORRODED. TRUNNION REWORKED AS PER FEDEX EA 1-5340-99703, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 22, 2006 · N620FE · Doug MD11 · Main Landing Gear Attach SectionSDR 06FDEA2378Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND LEFT HAND TRUNNION FORWARD HOLE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL BORE DIAMETER = 1.281", FINAL BORE DIAMETER = 1.3685", MAXIMUM BORE DIAMETER = 1.385" AND FOUND WITHIN LIMIT AS PER SRM Jun 22, 2006 · N620FE · Doug MD11 · Main Landing Gear Attach SectionSDR 06FDEA2372Seat Track · damagedM/D CARGO SEAT TRACK (STA 1059, LT X=47.5) FOUND EDGE DAMAGED. TRIMMED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. NEW SEAT TRACK AND SPLICE REWORKED AND INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 21, 2006 · N620FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA2360Seat Track · damagedCARGO SEAT TRACK (STA 1059, LT X=47.5) FOUND EDGE DAMAGED. CRACKED BEADED DOUBLER ON LT WING FIXED LEADING EDGE BETWEEN STA XOS 629 REPAIRED AS PER FEDEX EA 1-5730-99698.Jun 16, 2006 · N620FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA2359Doubler · crackedLT WING FIXED LEADING EDGE DOUBLER BETWEEN STA XOS 625 AND STA 629 FOUND CRACKED. REPAIRED AS PER FEDEX EA 1-5730-99698. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Jun 16, 2006 · N620FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA2325Stringer · crackedHFEC INSPECTION FOUND CRACK ON RIGHT WING OUTBOARD END WING STRINGER S-11R AT XORS 704. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 16, 2006 · N620FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA2324Stringer · crackedHFEC INSPECTION FOUND CRACK ON LEFT WING TANK AT THE END OF STRINGER 49. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 16, 2006 · N620FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA2323Stringer · crackedHFEC INSPECTION FOUND CRACK ON RIGHT WING TANK AT THE END OF STRINGER 49. REPAIR CARRIED OUT AT RH WING TANK END OF STRINGER 49 CRACKED AREA AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Jun 16, 2006 · N620FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA2322Stringer · crackedHFEC INSPECTION FOUND CRACK ON LEFT WING TANK AT THE END OF STRINGER 10 XORS 760. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 16, 2006 · N620FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA2321Stringer · crackedHFEC INSPECTION FOUND CRACK ON LEFT WING TANK AT THE END OF STRINGER 13 XORS 577. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 16, 2006 · N620FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA2320Stringer · crackedHFEC INSPECTION FOUND CRACK ON RIGHT WING OUTBOARD END UPPER WING STRINGER S-14R AT XORS 521. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 16, 2006 · N620FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA2319Skin · dentedRIGHT WING I/B FLAP O/B SEGMENT LOWER SURFACE FOUND DENTS. REPAIRED AS PER SRM 57 -10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Jun 16, 2006 · N620FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA2318Structure · crackedRIGHT WING FIXED LEADING EDGE ANTI ICE TELESCOPING DUCT CUTOUT INBOARD AND OUTBOARD CORNER FOUND CRACKED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-99697.Jun 16, 2006 · N620FE · Doug MD11 · Wing Miscellaneous StructureSDR 06FDEA2317Structure · crackedLEFT WING FIXED LEADING EDGE ANTI ICE TELESCOPING DUCT CUTOUT INBOARD AND OUTBOARD CORNER FOUND CRACKED. CRACKED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-99696. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Jun 16, 2006 · N620FE · Doug MD11 · Wing Miscellaneous StructureSDR 05FDEA00294Structure · corrodedBARREL NUT BORE NR 34R CORROSION REMOVAL FOUND EXCEEDED LIMITS. CORROSION REMOVED AND REPAIRED PER FEDEX EA 1-5510-81726.Feb 15, 2005 · N620FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00285Structure · corrodedBARREL NUT BORE NR 1R CORROSION REMOVAL FOUND EXCEEDED LIMITS. CORROSION REMOVED AND REPAIRED PER FEDEX EA 1-5510-81726Feb 14, 2005 · N620FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00284Structure · corrodedBARREL NUT BORE NR 3L CORROSION REMOVAL FOUND EXCEEDED LIMITS. REMOVED AND REPAIRED PER FEDEX EA 1-5510-81726,Feb 13, 2005 · N620FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00279Structure · corrodedBARREL NUT BORE NR 26L CORROSION REMOVAL FOUND EXCEEDED LIMITS. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II.Feb 11, 2005 · N620FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00278Structure · corrodedBARREL NUT BORE NR 15R CORROSION REMOVAL FOUND EXCEEDED LIMITS. CORROSION REMOVED AND REPAIRED PER FEDEX EA 1-5510-81726.Feb 11, 2005 · N620FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00277Structure · corrodedBARREL NUT BORE NR 14R CORROSION REMOVAL FOUND EXCEEDED LIMITS. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II.Feb 10, 2005 · N620FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00260Structure · corrodedBARREL NUT BORE NR 30R CORROSION REMOVAL FOUND EXCEEDED LIMITS. CORROSION REMOVED AND REPAIRED PER FEDEX EA 1-5510-81726.Feb 6, 2005 · N620FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00259Structure · corrodedBARREL NUT BORE NR 25L CORROSION REMOVAL FOUND EXCEEDED LIMITS. CORROSION REMOVED AND REPAIRED PER FEDEX EA# 1-5510-81726.Feb 6, 2005 · N620FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA00257Stop Fitting · crackedRIGHT HAND WING, OUTBOARD FLAP STOP FITTING FOUND CRACKED. STOP FITTING REMOVED AND REPLACED PER DRAWING 4125 AND SRM 51-33-01 VOLUME II.Feb 6, 2005 · N620FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA00241Frame · dentedMAIN DECK - DENT MARKS AT RIGHT HAND FRAME AT STA Y= 1681 LONGERON 12. LONGERON 12 REPAIRED PER SRM 53-30-00 VOLUME I, FIGURE 1.Feb 4, 2005 · N620FE · Doug MD11 · Fuselage Main, FrameSDR 05FDEA00240Frame · dentedDENT MARK FOUND AT RIGHT HAND FRAME STA Y= 1641 LONGERON 12. LONGERON 12 REPAIRED PER SRM 53-30-00 VOLUME I, FIGURE 1.Feb 4, 2005 · N620FE · Doug MD11 · Fuselage Main, FrameSDR 05FDEA00239Frame · dentedDENT MARKS FOUND AT LEFT HAND FRAME STA Y= 1681 LONGERON 14. LONGERON 14 REPAIRED PER SRM 53-30-00 VOLUME I, FIGURE 1.Feb 4, 2005 · N620FE · Doug MD11 · Fuselage Main, FrameSDR 05FDEA00238Frame · chafedMAIN DECK - RIGHT HAND SIDE FRAME G-NET ATTACHED YOKE ASSEMBLY AT STA Y=535 TOP AND BOTTOM PART FOUND WITH CHAFED MARK. MAIN DECK - RIGHT HAND SIDE FRAME G-NET ATTACHED YOKE ASSEMBLY AT STA Y=535, CHAFED MARK REMOVED PER SRM 53-00-01 VOLUME I, FIGURE 3. MATEFeb 3, 2005 · N620FE · Doug MD11 · Fuselage Main, FrameSDR 05FDEA00237Frame · chafedMAIN DECK - LEFT HAND SIDE FRAME G-NET ATTACHED YOKE ASSEMBLY AT STA Y=535 TOP AND BOTTOM REPAIR ANGLE FOUND WITH CHAFED MARK. MAIN DECK - LEFT HAND SIDE FRAME G-NET ATTACHED YOKE ASSEMBLY, CHAFED EXISTING REPAIR ANGLE AT STA Y=535, REMOVED PER SRM 51-31-01 VFeb 3, 2005 · N620FE · Doug MD11 · Fuselage Main, FrameSDR 05FDEA00236Seat Track · wornMAIN DECK - SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 715, X= 47.5 FOUND WORN. MAIN DECK - SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 715, X= 47.5 REPAIR PARTS FABRICATED AND INSTALLED AS PER SRM 53-70-00 VOLUME I, FIGURE 1.Feb 3, 2005 · N620FE · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
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