N621FE

Service difficulty reports · 288

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 = 'N621FE' 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 FDEA200908052904Web · crackedCRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 7 SPOOL SUPPORT FITTING AT HOLE B. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 107.Aug 5, 2009 · N621FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200908052903Web · crackedCRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 7 SPOOL SUPPORT FITTING AT HOLE C. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 107.Aug 5, 2009 · N621FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200908052902Web · crackedCRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 6 SPOOL SUPPORT FITTING AT HOLE D. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 107.Aug 5, 2009 · N621FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200908052901Web · crackedCRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 5 SPOOL SUPPORT FITTING AT HOLE C. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 107.Aug 5, 2009 · N621FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200908052900Web · crackedCRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 3 SPOOL SUPPORT FITTING AT HOLE D. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 107.Aug 5, 2009 · N621FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200908052899Web · crackedCRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 7 SUPPORT FITTING HOLE A. COMPLIED WITH EA1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV.107.Aug 5, 2009 · N621FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200908042892Vane · delaminatedRIGHT WING - INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. RT WING - INBD FLAP VANE ASSY REMOVED AND REPLACED IAW AMM 27-50-22-4, REV.64. ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5 REV. 64.Aug 4, 2009 · N621FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200908042891Support · crackedRIGHT WING LEADING EDGE INTERIOR COMPARTMENT NR 16 INBD SLAT TRACK SUPPORT RIB FOUND CRACKED. RT WING L/E INTERIOR COMPARTMENT NR 16 INBD SLAT TRACK SUPPORT RIB REMOVED AND REPLACED IAW SRM 51-31-01 REV 41. NEW RIB SUPPORT FABRICATED IAW DWG ARB2850 REV G. Aug 4, 2009 · N621FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA200901150208Unknown · vibrationAFTER TAKEOFF PASSING 13000 FT IN CLIMB PWR NR 1 ENG STARTED VIBRATING. AT LEVEL OFF PULLED NR 1 THROTTLE TO IDLE AND WHEN PASSING BELOW 80 PERCENT N1 VIBRATION WENT DOWN SIGNIFICANTLY AND AT IDLE NO VIBRATION NOTED. KEPT THROTTLE BELOW 80 PERCENT TO REMAINDJan 15, 2009 · N621FE · Doug MD11F · Engine (Turbine/Turboprop)SDR 08FDEA00528Skin · dentedLEFT WING - INBOARD FLAP LOWER SURFACE FOUND SEVERAL DENTS AT XIFH 244. DENT AREA FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I AND REPAIR CARRIED OUT AT LEFT HAND WING INBOARD FLAP LOWER SURFACE AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR Feb 20, 2008 · N621FE · Doug MD11 · Trailing Edge FlapsSDR 08FDEA00466Seat Track · crackedMAIN DECK COMPARTMENT, AFTER REMOVAL OF DAMAGED LOWER CARGO CEILING PANELS FOUND SEAT TRACK AT STA 635, X = 47.50" CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 16, 2008 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00465Seat Track · crackedMAIN DECK COMPARTMENT, AFTER REMOVAL OF DAMAGED LOWER CARGO CEILING PANELS FOUND SEAT TRACK AT STA 635, X = -27.50 INCH CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 16, 2008 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00464Seat Track · corrodedMAIN DECK COMPARTMENT, AFTER REMOVAL OF DAMAGED LOWER CARGO CEILING PANELS FOUND SEAT TRACK AT STA 635, X = -8.50" CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 16, 2008 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00463Seat Track · crackedMAIN DECK COMPARTMENT, AFTER REMOVAL OF LOWER CARGO CEILING PANEL FOUND SEAT TRACK AT STA 635, X = 8.50 INCH CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 16, 2008 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00462Floor Support · crackedMAIN DECK COMPARTMENT, STA 1989, X= 55 FLOOR SUPPORT FOUND CRACKED. SUPPORT REMOVED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT MACHINED AS PER DRAWING AGA7551 AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Feb 16, 2008 · N621FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA00461Frame · damagedMAIN DECK, FRAME DOUBLER AT RIGHT STA 1701 LONGERON 12 FOUND WITH DENT. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES AS PER SRM 53-30-00 FIGURE 1Feb 16, 2008 · N621FE · Doug MD11F · Fuselage Main, FrameSDR 08FDEA00460Skin · dentedRIGHT WING, INBOARD FLAP INBOARD LOWER SEGMENT LOWER SURFACE FOUND WITH DENT. DENT AREA FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I AND REPAIR CARRIED OUT AT RT WING INBOARD FLAP INBOARD LOWER SEGMENT LOWER SURFACE AS PER SRM 57-10-00 FIGUREFeb 16, 2008 · N621FE · Doug MD11F · Trailing Edge FlapsSDR 06FDEA03097Block · corrodedCENTER LANDING GEAR, LT PILLOW BLOCK AT FORWARD NUT SIDE FOUND SPOTFACE WITH CORROSION. CENTER LANDING GEAR, LEFT HAND PILLOW BLOCK AT FORWARD NUT SIDE SPOTFACE CORROSION REMOVED AND FOUND WITHIN LIMITS PER SRM 53-40-00 VOLUME I, FIGURE 15. THICKNESS OF FAug 27, 2006 · N621FE · Doug MD11 · Main Landing GearSDR 06FDEA03098Trunnion · corrodedCENTER LANDING GEAR, RT TRUNNION AFT HOLE UPPER SURFACE FOUND CORRODED. COMPLIED WITH FEDEX E.A 1-5340-103487, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 27, 2006 · N621FE · Doug MD11F · Main Landing Gear Attach SectionSDR 06FDEA03092Attach Fitting · corrodedCENTER LANDING GEAR, LEFT HAND PILLOW BLOCK ATTACHMENT FITTING FOUND MATING SURFACE WITH FITTING CORROSION. CENTER LANDING GEAR, LEFT HAND PILLOW BLOCK ATTACHMENT FITTING MATING SURFACE - PITTING CORROSION REMOVED AND FOUND WITHIN LIMITS AS PER 53-40-00Aug 27, 2006 · N621FE · Doug MD11F · Main Landing GearSDR 06FDEA03067Trunnion · crackedNOSE LANDING GEAR, LEFT NOSE LANDING GEAR TRUNNION FITTING WEB SUSPECTED CRACKED SNRM NO.: N00556. COMPLIED WITH FEDEX EA NR 1-5310-103482, FUSELAGE, LT NOSE LANDING TRUNNION WEB CRACK. STOP DRILL DEVIATION FROM SRM. REPAIR CLASSIFIED AS MINOR PER GMM 6-2Aug 24, 2006 · N621FE · Doug MD11 · Nose/Tail Landing Gear Attach SectionSDR 06FDEA03084Frame · dentedMAIN DECK CARGO COMPT, MAIN FRAME AT STA 1721 LONGERON 12L FOUND DENT. MAIN DECK CARGO COMPT, DENT MAIN FRAME AT STA 1721 LONGERON 12L REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL REPEAT INSPECTION REAug 24, 2006 · N621FE · Doug MD11F · Fuselage Main, FrameSDR 06FDEA03083Frame · dentedMAIN DECK CARGO COMPT, MAIN FRAME AT STA 1581 LONGERON 12L FOUND DENT SNRM NO.: N00660, MAIN DECK CARGO COMPT, DENT MAIN FRAME AT STA 1581 LONGERON 12L REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL REPEAAug 24, 2006 · N621FE · Doug MD11 · Fuselage Main, FrameSDR 06FDEA03082Frame · dentedMAIN DECK CARGO COMPT, MAIN FRAME AT STA 1641 LONGERON 12R FOUND DENT SNRM NO.: N00659, MAIN DECK CARGO COMPT, DENT MAIN FRAME AT STA 1641 LONGERON 12R REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL REPEAAug 24, 2006 · N621FE · Doug MD11F · Fuselage Main, FrameSDR 06FDEA3084Frame · dentedMAIN DECK CARGO COMPT, MAIN FRAME AT STA 1721 LONGERON 12L FOUND DENT AFA7799-1.Aug 24, 2006 · N621FE · Doug MD11F · Fuselage Main, FrameSDR 06FDEA3083Frame · dentedMAIN DECK CARGO COMPT, MAIN FRAME AT STA 1581 LONGERON 12L FOUND DENT AFA7819-1.Aug 24, 2006 · N621FE · Doug MD11F · Fuselage Main, FrameSDR 06FDEA3082Frame · dentedMAIN DECK CARGO COMPT, MAIN FRAME AT STA 1641 LONGERON 12R FOUND DENT AFA7817-1.Aug 24, 2006 · N621FE · Doug MD11F · Fuselage Main, FrameSDR 06FDEA3067Trunnion · crackedNLG, LT NOSE LANDING GEAR TRUNNION FITTING WEB SUSPECT CRACK.Aug 24, 2006 · N621FE · Doug MD11F · Nose/Tail Landing Gear Attach SectionSDR 06FDEA03027Stringer · crackedLT WING, CRACK FOUND APPROX 7.5" IN LENGTH DURING HFEC INSPECTION AT STRINGER 14 (UPPER STRINGER) WING STA XORS 521 SNRM NO.: N00284, LT WING TANK STRINGER 14 AT STA XORS 521 CARRIED OUT REPAIR AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAug 22, 2006 · N621FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03026Stringer · crackedRT WING, CRACK FOUND APPROX 11" IN LENGTH DURING HFEC INSPECTION AT STRINGER 11 (UPPER STRINGER) WING STA XORS 704 SNRM NR N00285, RT WING TANK AT WING STA XORS 704 STRINGER 11, CARRIED OUT REPAIR AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AAug 22, 2006 · N621FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03025Stringer · crackedLT WING, CRACK FOUND APPROX 7.5" IN LENGTH DURING HFEC INSPECTION AT STRINGER 9 (UPPER STRINGER) WING STA XORS 819 SNRM NO.: N00283, LT WING STA XORS 819 STRINGER 9 CARRIED OUT REPAIR AS PER SRM 57-20-00 VOLUME 1, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GAug 22, 2006 · N621FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03024Stringer · crackedLT WING, CRACK FOUND APPROX 9" IN LENGTH DURING HFEC INSPECTION AT STRINGER 11 (UPPER STRINGER) WING STA XORS 704 SNRM NO.: N00282, LT WING TANK STA XORS 704 STRINGER 11 CARRIED OUT REPAIR AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR Aug 22, 2006 · N621FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA3024Stringer · crackedLT WING, CRACK FOUND APPROX 9" INCHES IN LENGTH DURING HFEC INSPECTION AT STRINGER 11 (UPPER STRINGER) WING STA XORS 704 ARB7511.Aug 22, 2006 · N621FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA3025Stringer · crackedFOUND LT WING, CRACK FOUND APPROX 7.5" INCHES IN LENGTH DURING HFEC INSPECTION AT STRINGER 9 (UPPER STRINGER) WING STA XORS 819 (ARB7509).Aug 22, 2006 · N621FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA3026Stringer · crackedRT WING, CRACK FOUND APPROX 11" IN LENGTH DURING HFEC INSPECTION AT STRINGER 11 (UPPER STRINGER) WING STA XORS 704.Aug 22, 2006 · N621FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA3027Stringer · crackedLT WING, CRACK FOUND APPROX 7.5" INCHES IN LENGTH DURING HFEC. INSPECTION AT STRINGER 14 (UPPER STRINGER) WING STA XORS 521.Aug 22, 2006 · N621FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03022Skin · crackedRIGHT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT FOUND CRACKED. RIGHT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT REPAIR CARRIED OUT PER FEDEX EA NR 1-5730-1013480, WINGS RT WING LEADING EDGE SKIN CRACKS AT TELESCOPING Aug 21, 2006 · N621FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03021Skin · crackedLEFT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT FOUND CRACKED, SNRM NR N00183. LEFT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT CRACKED AREA REPAIRED AS PER FEDEX EA NR 1-5730-103497, WINGS, LT WING LEADING EDGE SKIN CRACKAug 21, 2006 · N621FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA3021Structure · crackedLEFT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR, CUTOUT FOUND CRACKED.Aug 21, 2006 · N621FE · Doug MD11 · Wing Main, Frame StructureSDR 06FDEA3022Structure · crackedRIGHT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR, CUTOUT FOUND CRACKED.Aug 21, 2006 · N621FE · Doug MD11 · Wing Main, Frame StructureSDR 05FDEA01372Panel · corrodedHORIZONTAL STABILIZER RIGHT HAND FORWARD SPAR CAP NR 1R BARREL NUT BORE CORROSION REMOVAL FOUND EXCEEDED LIMITATIONS. REWORKED AS PER FEDEX EA 1-5510-83008.May 19, 2005 · N621FE · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR 05FDEA01296Spar Cap · corrodedHORIZONTAL STABILIZER RIGHT HAND AFT SPAR CAP NR 36R BARREL NUT BORE CORROSION REMOVAL FOUND EXCEEDED LIMITATIONS. REWORKED AS PER FEDEX EA 1-5510-83007.May 15, 2005 · N621FE · Doug MD11 · Horizontal Stabilizer, Spar/RibSDR 05FDEA01295Panel · corrodedHORIZONTAL STABILIZER RT FORWARD PLANK NR 14R BARREL NUT BORE CORROSION REMOVAL FOUND EXCEEDED LIMITATIONS. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.May 15, 2005 · N621FE · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR 05FDEA01286Bulkhead · crackedCENTER CARGO STA 1841 FLOOR AREA BULKHEAD APPROX X= -23 WEB FOUND CRACKED. CRACKED WEB AT CENTER CARGO STA 1841 FLOOR AREA BULKHEAD X= -23 CUT AT STA 1841 X= -23 AND REMOVED AS PER SRM 53-00-01 FIGURE 10 VOLUME I. REPAIR WEB AND DOUBLER FABRICATED AND INSTALLMay 14, 2005 · N621FE · Doug MD11 · Fuselage Main, BulkheadSDR 05FDEA01284Stiffener · crackedCENTER CARGO, STA 1841 FLOOR AREA BULKHEAD APPROX X= -25 VERTICAL STIFFENER FOUND CRACKED. REMOVED AS PER SRM 51-33-01 VOLUME II. NEW STIFFENER FABRICATED AS PER DRAWING AGA7170 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR IS CLASSIFIED AS MINOR May 14, 2005 · N621FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 05FDEA01285Bulkhead · crackedCENTER CARGO, STA 1841 FLOOR AREA BULKHEAD APPROX X= 3 WEB FOUND CRACKED. CRACKED AREA OF WEB AT CENTER CARGO STA 1841 FLOOR AREA BULKHEAD X= 3 TRIMMED OUT AS PER SRM 53-00-01 FIGURE 5 VOLUME I. REPAIR FILLER AND DOUBLER FABRICATED AND INSTALLED AS PER SRMMay 14, 2005 · N621FE · Doug MD11 · Fuselage Main, BulkheadSDR 05FDEA01269Seat Track · crackedMAIN DECK, SEAT TRACK LBL 47 CRACKED AT STA 755. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.May 13, 2005 · N621FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01268Splice · crackedCENTER CARGO - RIGHT HAND UTILITY TUNNEL AT STA 1531 L-37 RIGHT HAND LONGERON SPLICE FOUND CRACK. REMOVED AS PER SRM 51-33-01 VOLUME II. NEW SPLICE FABRICATED AS PER DRAWING A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR IS CLASSIFIED MAJMay 13, 2005 · N621FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 04FDEA03133Warning Light · illuminatedON CLIMB-OUT AT 14K MSL ENG 2 A-ICE DUCT LEVEL 3 ALERT WITH AURAL WARNING. FOLLWED QRH CHECKLIST AND SHUTDOWN NR 2 ENGINE RETURN TO ONT. OPENED NR 2 ENGINE COWLS FOR INSPECTION, REMOVED ANTI-ICE VALVE HEAT SHIELD, AND REMOVED TWO DUCT ELBOW JOINT HEAT SHIELDNov 16, 2004 · N621FE · Doug MD11F · Air Intake Anti/De-Ice SystemSDR 04FDEA02658Detector · burstON T/O, PRIOR TO FLAP RET, A/C DISPLAYED A MOMENTARY LVL 3 ENG 2 A-ICE DUCT ALERT. AS THROTTLE WAS BEING MOVED TO IDLE ALERT WENT AWAY. CLIMB TO FL 290 WAS UNEVENTFUL UNTIL 30 MIN INTO FLT WHEN A/C DISP LVL-1 ENG 2 A-ICE OFF ALERT, WITH A CONS OF ENG 2 A-Sep 4, 2004 · N621FE · Doug MD11F · Overheat Detection
Back to N621FE