N619FE

Service difficulty reports · 242

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 = 'N619FE' 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 FDEA200910073496Doubler · crackedCTR LANDING GEAR WHEEL WELL LT WEB DOUBLER CRACKED AT STA 1392, X = 31.5. REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER AS PER SRM 51-31-01 REVISION 41. DOUBLER FABRICATED AS PER DRAWING NR AEA0526 REVISION NC. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-Oct 7, 2009 · N619FE · Doug MD11F · Fuselage Main, StructureSDR FDEA200910063480Skin · dentedFUSELAGE SKIN AT STA 1921 TO 1941, LONGERON 46 RT TO 50 RT INSPECTED BUT NO DENT FOUND. HOWEVER DENT FOUND ON STA 1921 TO 1941 LONGERON 46 LT TO 50 LT. REPAIR CARRIED OUT PER E.A. 1-5310-130882 REVISION A PART 2,Oct 6, 2009 · N619FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200910053476Rib · crackedRT WING SLAT TRACK NR 16 INBD SUPPORT RIB CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01, REVISION 41. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100, REVISION 108.Oct 5, 2009 · N619FE · Doug MD11F · Wing, Rib/BulkheadSDR FDEA200910053475Rib · crackedLT WING SLAT TRACK NR 16 INBD SUPPORT RIB CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01, REVISION 41. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100, REVISION 108.Oct 5, 2009 · N619FE · Doug MD11F · Wing, Rib/BulkheadSDR FDEA200910053474Trunnion · crackedNLG WW, LT NLG TRUNNION FITTING FOUND CRACKED. REPAIRED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2, REVISION 41. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 108. INITIAL INSPECTION TO BE CARRIED OUT AT 1500 CYCLE AND REPETITIVE INSPECTION TO CARRY OUT Oct 5, 2009 · N619FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR 08FDEA01435Support Fitting · crackedUPPER CARGO DOOR CUT OUT, NR 7 LOWER JAMB SUPPORT FITTING MOUNTING HOLE CRACKED. MOUNTING HOLES REAMED PER SRM 53-50-00 FIG. 10 VOL.I. AND BUSHING REPAIR CARRIED OUT PER SRM 53-50-00 FIG. 10. VOL.I. BUSHING FABRICATED PER SRM 53-50-00 FIG. 10 VOL.I. REPAApr 16, 2008 · N619FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA01434Support Fitting · crackedUPPER CARGO DOOR CUT OUT, NR 6 LOWER JAMB SUPPORT FITTING MOUNTING HOLE CRACKED. MOUNTING HOLES REAMED PER SRM 53-50-00 FIG. 10 VOL.I. AND BUSHING REPAIR CARRIED OUT PER SRM 53-50-00 FIG. 10. VOL.I. BUSHING FABRICATED PER SRM 53-50-00 FIG. 10 VOL.I. REPAIR Apr 16, 2008 · N619FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA01433Support Fitting · crackedUPPER CARGO DOOR CUT OUT, NR 5 LOWER JAMB SUPPORT FITTING CRACKED. FITTING REMOVED & REPLACED PER SRM 51-33-01 VOL II. MOUNTING HOLES ON NR 5 JAMB BEAM REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL I. CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.Apr 16, 2008 · N619FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA01432Support Fitting · crackedUPPER CARGO DOOR CUT OUT, NR 4 LOWER JAMB SUPPORT FITTING CRACKED. REMOVED & REPLACED PER SRM 51-33-01 VOL II. MOUNTING HOLES ON NR 4 JAMB BEAM REPAIR CARRIED OUT PER EA 1-5310-112624, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Apr 16, 2008 · N619FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA01431Support Fitting · crackedUPPER CARGO DOOR CUT OUT, NR 3 LOWER JAMB SUPPORT FITTING CRACKED. REMOVED & REPLACED PER SRM 51-33-01 VOL.II. MOUNTING HOLES ON NR 3 JAMB BEAM REPAIR CARRIED OUT PER SRM 53-50-00 FIG 10 VOL.I. CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.Apr 16, 2008 · N619FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA01430Support Fitting · crackedUPPER CARGO DOOR CUT OUT, NR 2 LOWER JAMB SUPPORT FITTING CRACKED. REMOVED & REPLACED PER SRM 51-33-01 VOL.II. MOUNTING HOLES ON NR 2 JAMB BEAM REPAIR CARRIED OUT PER SRM 53-50-00 FIG. 10 VOL I. CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.Apr 16, 2008 · N619FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA01429Support Fitting · crackedUPPER CARGO DOOR CUT OUT, NR 1 LOWER JAMB SUPPORT FITTING CRACKED. REMOVED & REPLACED AS PER SRM 51-33-01 VOL.II. MOUNTING HOLES ON NR 1 JAMB BEAM REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL.I. CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.Apr 16, 2008 · N619FE · Doug MD11F · Fuselage Miscellaneous StructureSDR 08FDEA01411Skin · crackedLT WING, ANTI-ICE TELESCOPE TUBE CUT-OUT AT L/E FIXED COMPARTMENT FOUND OUTBD CORNER CRACKED. TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 43 VOL.I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Apr 15, 2008 · N619FE · Doug MD11F · Wing, Plate/SkinSDR 06FDEA03928Frame · dentedMAIN DECK CARGO COMPARTMENT, MAIN FUSELAGE FRAME AT STA 5-93 LONGERON 12R , FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION REQUIRED AT 9,Nov 8, 2006 · N619FE · Doug MD11 · Fuselage Main, FrameSDR 06FDEA03927Panel · corrodedMAIN DECK CARGO COMPARTMENT, CENTER WING UPPER PANEL AT STA 1219 X = -60 FOUND WITH CORROSION. REWORKED AS PER FEDEX E.A.1-5710-105547, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Nov 8, 2006 · N619FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA03896Seat Track · scratchedMAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 5-53 TO STA 5-63, X = 8 FOUND SCRATCHED. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPIAR CLASSIFIED AS MAJOR PER GMM 6-2-100.Nov 5, 2006 · N619FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03895Frame · dentedMAIN DECK CARGO COMPARTMENT, MAIN FUSELAGE FRAME AT STA 1741 ABOUT LONGERON 12R AREA FOUND DENTED. DENT REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION RNov 5, 2006 · N619FE · Doug MD11 · Fuselage Main, FrameSDR 06FDEA03894Skin · corrodedLEFT WING TOP SKIN SURFACE AFT AT FORWARD OF INBOARD AILERON FOUND WITH CORROSION. LT WING TOP SKIN SURFACE AFT AT FORWARD OF INBOARD AILERON CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS = 0.430", MATERIAL REMOVED = 0.041", REMAINNov 5, 2006 · N619FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03893Skin · corrodedLEFT WING TOP SKIN SURFACE AFT AT XORS 779 FOUND WITH CORROSION. LT WING TOP SKIN SURFACE AFT AT XORS 792 CORROSION REMOVED AS PER SRM 51- 21-01 VOLUME II. ORIGINAL THICKNESS = 0.175", MATERIAL REMOVED = 0.046", REMAINED THICKNESS = 0.129" AND FOUND ENov 5, 2006 · N619FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03857Seat Track · brokenMAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 475, X = 8 CROWN AREA FOUND BROKEN. REPAIR CARRIED OUT BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 495 TO STA 525, X = 8 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Nov 3, 2006 · N619FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03856Duct · crackedRIGHT WING, TELESCOPIC DUCT CUTOUT CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-105539. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Nov 3, 2006 · N619FE · Doug MD11 · Wing Main, Frame StructureSDR 06FDEA03855Stringer · crackedCRACK FOUND (APPROX 8" LONG) DURING HFEC INSPECTION ON LT WING TANK AT THE END OF UPPER STRINGER 9 XORS 819. CRACK ON LT WING TANK AT THE END OF UPPER STRINGER 9 XORS 819 SLOTTED OUT AND ANGLE REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAINov 3, 2006 · N619FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03834Stringer · crackedCRACK FOUND (APPROX 6" LONG) DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF UPPER STRINGER 13 XORS 577. CRACKED UPPER STRINGER 13 ON RIGHT HAND WING TANK AT XORS 577 TRIMMED OUT 2 BAYS AND REPAIRED WITH SPLICE AS PER SRM 57-20-00 FIGURE 10 VOLUME INov 2, 2006 · N619FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03833Doubler · crackedRIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 643 FOUND CRACKED. CRACKED BEADED DOUBLER ON RIGHT WING FIXED LEADING EDGE AT XOS 643. REPAIRED AS PER FEDEX EA NR 1-5730-104824, PERMANENT REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Nov 2, 2006 · N619FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03832Doubler · crackedRIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 698 FOUND CRACKED. CRACKED BEADED DOUBLER ON RIGHT WING FIXED LEADING EDGE AT XOS 698. REPAIRED AS PER FEDEX EA NR 1-5730-105537, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Nov 2, 2006 · N619FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03831Doubler · crackedRIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 728 FOUND CRACKED. CRACKED BEADED DOUBLER ON RIGHT HAND WING FIXED LEADING EDGE AT XOS 728 REPAIRED AS PER FEDEX EA 1-5730-105538, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Nov 2, 2006 · N619FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03827Seat Track · gougedMAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 955, X= 8 FOUND SCRATCHED. MAIN DECK CARGO COMPARTMENT SCRATCHED SEAT TRACK AT STA 955, X= 8, REPAIR CARRIED OUT BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 869 TO 969, X= 8 AS PER SRM 53-70-00 FIG 1 VOL I. REPNov 2, 2006 · N619FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03835Stringer · crackedCRACK FOUND (APPROX 9" LONG) DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF UPPER STRINGER 14 XORS 521. CRACK ON RIGHT WING TANK AT THE END OF STRINGER 14 XORS 521 TRIMMED OUT AND REPAIRED WITH SPLICE AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIRNov 2, 2006 · N619FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03829Seat Track · damagedMAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 879 TO STA 884, X = 8 FOUND WITH NICK MARK. MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 879 TO STA 884, X = 8 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I BY SECTIONAL SEAT TRACK REPLACEMENT FROM SNov 2, 2006 · N619FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03828Seat Track · damagedMAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 879 TO STA 884, X = -8 FOUND WITH NICK MARK. MAIN DECK CARGO COMPARTMENT, NICKED SEAT TRACK AT STA 879 TO STA 884, X = -8 REPAIR CARRIED OUT BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 869 TO STA 909, X = -8 AS Nov 2, 2006 · N619FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03826Seat Track · damagedMAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 965, X = -47.5 FOUND WITH NICK MARK. MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 965, X = -47.5 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 901 TO STA Nov 2, 2006 · N619FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03825Seat Track · damagedMAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 1000 TO STA 1015, X = -47.5 FOUND WITH NICK MARK, MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA 1000 TO STA 1015, X = -47.5 CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I BY SECTIONAL SEAT TRACK REPLACEMNov 2, 2006 · N619FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03830Stringer · crackedCRACK FOUND (APPROX. 1.5 INCHES LONG) DURING HFEC INSPECTION ON RT WING TANK AT THE END OF LOWER STRINGER 41 XORS 685. CRACK ON RIGHT HAND WING TANK AT THE END OF LOWER STRINGER 41 XORS 685 SLOTTED OUT AND RESIZING ARROWHEAD REPAIR CARRIED OUT AS PER SRM Nov 2, 2006 · N619FE · Doug MD11F · Wing, Longeron/StringerSDR 06FDEA03824Stringer · crackedCRACK FOUND (APPROX 12" LONG) DURING HFEC INSPECTION ON LEFT WING TANK AT THE END OF UPPER STRINGER 13 XORS 577. CRACKED UPPER STRINGER 13 ON LT WING TANK AT XORS 577 TRIMMED OUT 2 BAYS AND REPAIRED WITH SPLICE AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIRNov 2, 2006 · N619FE · Doug MD11 · Wing, Longeron/StringerSDR 05FDEA01794Structure · corrodedREFERENCE EO 1-5510-7-5000 D1 PART 1, RT NR 1R BARREL NUT BORE CORROSION EXCEEDED TO LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83029.Jul 3, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01793Structure · corrodedREFERENCE EO 1-5510-7-5000 D1 PART 1, LT NR 36L BARREL NUT BORE CORROSION EXCEEDED TO LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83027.Jul 3, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01792Structure · corrodedREFERENCE EO 1-5510-7-5000 D1 PART 1, RT NR 34R BARREL NUT BORE CORROSION EXCEEDED TO LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83026.Jul 3, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01791Structure · corrodedREFERENCE TO EO 1-5510-7-5000 D1 PART 1, LT HAND NR 3L BARREL NUT BORE CORROSION EXCEEDED TO LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83028.Jul 3, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01758Bulkhead · damagedEMPENNAGE, TO TRIM RIGHT HAND OPERATING BULKHEAD FOR NR 35R BARREL NUT BORE REWORK ACCESS. RT OPERATING BULKHEAD TRIMMED OUT AS PER SRM 51-31-01 VOL II AND FOUND EXCEEDED LIMIT AS PER FEDEX EO NR 1-5510-7-5000. REPAIR CARRIED OUT ON TRIMMED AREA AT RT OPERATIJul 1, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01757Skin · damagedDURING AFT EXTENDED TAILCONE REMOVAL, FOUND INTERIOR SKIN DETACHED AT SEVERAL LOCATIONS. EXTENDED TAILCONE REPLACED AS PER AMM 53-52-01-4. (CLOSED)Jul 1, 2005 · N619FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 05FDEA01755Structure · corrodedLT NR 4L BARREL NUT BORE CORROSION EXCEEDED TO LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83028.Jun 30, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01730Structure · corrodedLT BARREL NUT HOLE NR 30L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83022.Jun 28, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01729Structure · corrodedLT BARREL NUT HOLE NR 28L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83022.Jun 28, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01728Structure · corrodedLT BARREL NUT HOLE NR 22L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83025.Jun 28, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01727Structure · corrodedLT BARREL NUT HOLE NR 16L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83025.Jun 28, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01726Structure · corrodedRT BARREL NUT HOLE NR 31R FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83026.Jun 28, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01725Structure · corrodedRT BARREL NUT HOLE NR 29R FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83026.Jun 28, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01724Structure · corrodedRT BARREL NUT HOLE NR 17R. FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83024.Jun 28, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01709Fitting · corrodedLT NR 26L FITTING BARREL NUT BORE FOUND CORROSION EXCEEDED TO LIMIT. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. (CLOSED)Jun 27, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01700Structure · corrodedWITH REFERENCE TO EO1-5510-7-5000 PART 1, RT NR 5R BORE CORROSION FOUND EXCEEDED LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83023.Jun 27, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer Structure
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