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 FDEA201506242003Longeron Splice · crackedCRACK INDICATION FOUND DURING X-RAY INSPECTION AT STATION 5-0, LONGERON 7R. STRINGER SPLICE CRACK LENGTH APPROX 1 INCH. R & R IAW SRM 51-33-01-0G. NEW LONGERON SPLICE FABRICATED BY MACHINING IAW DWG AEA7633 REVISION B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-Jun 24, 2015 · N619FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201506242002Seat Track · corrodedMAIN DECK SEAT TRACK FLANGE AT BS 1200 - 1219, X -107 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jun 24, 2015 · N619FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201506242001Skin · dentedRIGHT WING, FOUND A DENT ON RT INBD FLAP LOWER SKIN ON INBD END. REPAIRED IAW EA 1-5750-T0318573 PART 1. MAJOR IAW GMM 6-2-100.Jun 24, 2015 · N619FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201506231973Doubler · crackedLEFT WING, FIXED LE BEADED DOUBLER AT XOS 654.5, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jun 23, 2015 · N619FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201506231972Support Frame · crackedLEFT WING, FIXED LE LOWER SUPPORT FORMER AT XOS 1026, FOUND CRACKED. FORMER REMOVED IAW SRM 51-31-01-0G. FABRICATED NEW FORMER IAW DWG ARB2920 REVISION BB. INSTALLED NEW FORMER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jun 23, 2015 · N619FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201506231971Support Frame · crackedRIGHT WING, FIXED LE LOWER SUPPORT FORMER AT STATION XOS 1026, FOUND CRACK DURING OTBD SLAT CONTROL CABLE INSPECTION. FORMER REMOVED IAW SRM 51-31-01-0G. FABRICATED A NEW FORMER IAW DWG ARB2920 REVISION BB. INSTALLED NEW FORMER IAW SRM 51-31-01-0G. REPAIRJun 23, 2015 · N619FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201506221954Repair · damagedAGEING ACFT, EXISTING REPAIR ON SEAT TRACK AT MAIN DECK CARGO COMPARTMENT BETWEEN STATION 665 & 765, X=47.5. EXISTING REPAIR EVALUATED & FOUND DAMAGED. DAMAGED SEAT TRACK R & R CARRIED OUT IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1 EO 1-5100-7-5001 B5 PART 1. Jun 22, 2015 · N619FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201506221953Repair · damagedAGEING ACFT, EXISTING REPAIR ON LT FRAME AT MAIN DECK CARGO COMPARTMENT AT STATION 1681, LONGERON 12L. EXISTING REPAIR EVALUATED & FOUND DAMAGED. CARRIED OUT REPAIR IAW SRM 53-00-07-2R FIGURE 201 REPAIR 2 EO 1-5100-7-5001 B5 PART 1. CLASSIFIED MAJOR IAW GMMJun 22, 2015 · N619FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201506191878Repair · damagedAGEING ACFT, EXISTING REPAIR ON BULKHEAD SKIN AT CTR CARGO COMPARTMENT STATION 1841, LBL 3.0 TO 9.0. EXISTING REPAIR ON BULKHEAD SKIN EVALUATED & FOUND DAMAGED. EXISTING REPAIR R & R CARRIED OUT IAW SRM 53-00-00-2R FIGURE 211 EO 1-5100-7-5001 B5 PART 1. REPJun 19, 2015 · N619FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201506191880Skin · crackedLEFT WING LE DROOP UPPER SKIN FOUND CRACK FROM XDLE 328.5 TO 330. REPAIRED IAW SRM 57-40-01-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jun 19, 2015 · N619FE · Doug MD11F · Leading Edge DevicesSDR FDEA201506191879Bulkhead · crackedCENTER CARGO BAY BS 1841 BULKHEAD FOUND CRACKED AT RBL 1.5 - 3.0. REPAIRED IAW SRM 53-00-00-2R FIGURE 211. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jun 19, 2015 · N619FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201506191877Strap · crackedLEFT WING OTBD FLAP INBD FWD HINGE TENSION STRAP FOUND CRACKED XW486. TENSION STRAP REMOVED IAW SRM 51-33-01-0G & REPLACED WITH NEW SUPPORT TENSION STRAP IAW SRM 51-33-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jun 19, 2015 · N619FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201309222281Battery · failedL2 DOOR SLIDE REMOTE PRESSURE INDICATIOR PTT SWITCH FAILED TO TEST. REPLACED BATTERIES. REMOTE PRESSURE INDICATOR EVAC SLIDE TESTED NORMAL IAW MM 21-61-04-5. OK FOR SERVICE.Sep 22, 2013 · N619FE · Doug MD11F · Emergency EquipmentSDR FDEA201308061797Doubler · crackedLEFT WING FIXED L/E BEADED DOUBLER FOUND CRACKED AT XOS 701. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIGURE 203, REV 53 TYPE "A". REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 6, 2013 · N619FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201308061796Skin · crackedRT WING INBD FLAP T/E WEDGE LOWER SURFACE FOUND CRACKED AT XIFH 130 TO 134. REPAIRED IAW SRM 57-50-02, REPAIR 3, FIGURE 201, REV 53 AND EA 1- 5750-T0301707, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 6, 2013 · N619FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201308061795Floor Panel · delaminatedMAIN CARGO FLOOR PANEL 282AF FOUND DELAMINATED. FLOOR PANEL REMOVED IAW AMM 53-21-04, REV 76.1. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J AND SRM 51-90-01, REV 53, AND INSTALLED IAW AMM 53-21-04, REV 76.1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-1Aug 6, 2013 · N619FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201308061794Floor Support · corrodedFORWARD LAVATORY FLOOR SUPPORT FOUND CORRODED AT BS 421. R & R IAW SRM 51-31-01, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Aug 6, 2013 · N619FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201308061793Skin · puncturedLEFT WING INBD FLAP LOWER SURFACE, FOUND PUNCTURED ABOUT ONE INCH IN DIAMETER AT XIFH 242. REPAIRED IAW EA 1-5750-T0301706, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 6, 2013 · N619FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201308021748Skin · crackedLEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 AND XORS 713.6, SEVEN FASTENER HOLES FOUND CRACKED INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION. CARRIED OUT BUSHING REPAIR IAW SRM 57-20-02, REPAIR 5, FIGURE 201, REV 53 AND EA Aug 2, 2013 · N619FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201308021747Skin · crackedRIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 AND XORS 713.6, TEN FASTENER HOLES FOUND CRACKED INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION. CARRIED OUT BUSHING REPAIR IAW SRM 57-20-02, REPAIR 5, FIG 201 REV 53 AND EA 1-571Aug 2, 2013 · N619FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201308021746Skin · crackedLEFT WING L/E LOWER ACCESS PANEL 519CB CUTOUT SKIN INBD FWD CORNER FOUND CRACKED AT XOS 612. REPAIRED IAW SRM 57-40-02, FIG 202 REPAIR 7, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 2, 2013 · N619FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201308021745Skin · dentedRIGHT WING INBD FLAP LOWER SURFACE FOUND DENTED AT XIFH 250 AND ONE INCH FROM T/E. REPAIRED IAW SRM 57-50-01, REPAIR 1, FIGURE 201, REV 53 AND EA 1-5750-T0301707, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Aug 2, 2013 · N619FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201307311706Door Frame · crackedBS 1305.25 - 1315.42, R3 DOOR AFT FRAME LOWER WEB CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201 REPAIR 3 REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.Jul 31, 2013 · N619FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201307311705Door Frame · crackedBS 1250.75 - 1256.75, R3 DOOR FWD FRAME LOWER WEB CRACKED. REPAIRED IAW SRM 53 -40-15, FIG 201, REPAIR 3, REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Jul 31, 2013 · N619FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201307311704Door Frame · crackedBS 1305.25 - 1315.42 L3 DOOR AFT FRAME LOWER WEB CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6 -2-100, REV 116.Jul 31, 2013 · N619FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201307311703Door Frame · crackedBS 1250.75 - 1256.75 L/E DOOR FORWARD FRAME LOWER WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6 -2-100, REV 116.Jul 31, 2013 · N619FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201307291688Seat Track · corrodedFORWARD CABIN BS 610, X=-47.5 SEAT TRACK FOUND WITH SURFACE CORROSION. REPAIRED BY SECTION SEAT TRACK REPLACEMENT FROM STATION 605 TO STATION 645 X = -47.5 IAW SRM 53-00-52, FIG 201. REPAIRED BY SECTION SEAT TRACK REPLACEMENT FROM BS 605 - 645 IAW SRM 53-0Jul 29, 2013 · N619FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201307291690Skin · crackedDURING SPOILER UPPER SURFACE INSPECTION, RT WING L/E DROOP UPPER SURFACE FOUND CRACKED ABOUT 2 INCHES LONG AT XDLE 324. REPAIRED IAW SRM 57-40-01, REPAIR 5, FIGURE 201, REVISION 53. REPAIR DOUBLER INSTALLED IAW SRM 57-40-01, REPAIR 5, FIGURE 201, REV 53. Jul 29, 2013 · N619FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201307291689Spar Cap · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON NR 4 BANJO FITTING OF VERTICAL STABILIZER STA 2164, A CRACK FOUND ON RADIUS OF THE RT SIDE OF REAR SPAR CAP FWD FLANGE LOCATED AT THE UPPER SECTION APPROX. 0.75" LENGTH. REPAIRED IAW EA 1-5530-T0301678, PART 1.Jul 29, 2013 · N619FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA201307291687Floor Support · crackedFORWARD CABIN FLOOR SUPPORT AT BS 400-430, LBL 32 FOUND CRACKED. R & R IAW SRM 51-31-01, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Jul 29, 2013 · N619FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201307291686Door Frame · crackedLOWER FUSELAGE RT A/C PACK NR 3 DOOR FRAME AFT UPPER CORNER AREA FOUND CRACKED. TRIMMED OUT AND REPAIRED IAW SRM 53-20-15, FIG 201, REPAIR 3, REV 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Jul 29, 2013 · N619FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201301190148Wire Harness · damagedFORTY MINUTES INTO FLIGHT RECEIVED A LEVEL ONE "FIRE DET 1 FAULT" ALERT IT WAS FOLLOWED BY INTERMITTENT LEVEL THREE NR 1 FIRE ALERT AND "FIRE DET 1 FAIL" ALERTS. DECLARED EMERGENCY AND RETURNED TO DEPARTURE. CFDS SHOWS NOT CURRENT FAULTS FOR FDCU 1. LEG 1Jan 19, 2013 · N619FE · Doug MD11F · Fire Protection System WiringSDR FDEA201109224046Longeron · crackedCRACK INDICATION APPROX 1" IN LENGTH FOUND DURING X-RAY INSP AT STA 6-100 , LONGERON -7R AFT SECTION EDGE. CARRIED OUT REPAIR AS PER SRM 53-00-05 FIG 202 REV 47 & DRAWING AEA7478 REV A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 22, 2011 · N619FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201109224040Web · crackedLOWER PART OF VERTICAL STABILIZER, RT REAR CENTER SPAR TO REAR SPAR LOWER WEB FOUND CRACKED. CARRIED OUT REPAIR AS PER EA 1-5530-154227. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 22, 2011 · N619FE · Doug MD11F · Vertical StabilizerSDR FDEA201109224050Skin · crackedEMP - AFC RT DOGHOUSE ENTRANCE CUTOUT FOUND CRACKED AT INBD FWD CORNER. REPAIR DOUBLER FABRICATED AS PER SRM 53-70-02 FIG.201 REV 47 REPAIR DOUBLER INSTALLED AS PER SRM 51-33-01 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 22, 2011 · N619FE · Doug MD11F · Vertical Stabilizer, Plate/SkinSDR FDEA201109224039Skin · corrodedBS 2150 SKIN FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-01 REPAIR 3 FIG. 201 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 22, 2011 · N619FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201109224043Skin · cracked04 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT RT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA.XORS=683.4 AND STA=713.6. REPAIR CARRIED OUT AS PER DRAWING SG11570004 REV A. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.Sep 22, 2011 · N619FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201109224041Skin · cracked03 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA.XORS=683.4 AND STA XORS=713.6Sep 22, 2011 · N619FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201109193961Vane · delaminatedLEFT WING INBD FLAP VANE LOWER SURFACE FOUND WITH DELAMINATION. VANE ASSY REMOVED AND REPLACED AS PER AMM 27-50-22-4 REV. 70. ADJUSTED AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REV 70.0. CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.Sep 19, 2011 · N619FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201109193963Frame · dentedFRAME BS 1661 L11R, FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG 201 REPAIR 1 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 19, 2011 · N619FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201109193962Seat Track · chafedCABIN - RT STA 5-0 -STA 5-3, X=-8.75 SEAT TRACK FOUND CHAFED. DAMAGED SEAT TRACK TRIMMED AND REPAIR CARRIED OUT AS PER SRM 53-00-52 FIG. 201 REPAIR 1 REV 47 . REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.Sep 19, 2011 · N619FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201101240341Duct · rupturedAFTER TAKEOFF ICE DET SINGLE ALERT FOLLOWED BY MOMENTARY MANIFOLD FAIL LIGHT. THEN AIR 3 OFF. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX FOUND PNEU DUCT RUPTURED INBD OF NR3 ENGINE. REPLACED DUCT IAW AMM 36-14-02-4.Jan 24, 2011 · N619FE · Doug MD11F · Pneumatic Indicating SystemSDR FDEA201001070038Proximity Sensor · dirtyON GEAR EXTENSION HAD NOSE GEAR UNSAFE INDICATION ON CONFIG PAGE (SECONDARY DISPLAY) RECYCLED AND RECEIVED PROPER DISPLAY. PERFORMED INSP OF NOSE GEAR EXTENSION SYS FOUND PROXIMITY SENSORS DIRTY WITH GREASE CLEANED AND PERFORMED TARGETS AND PROXIMITY IAW AMM Jan 7, 2010 · N619FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA200910123544Fuel Tank · corrodedCABIN RT BELOW FLOOR AT STA 1229 'X' = -66.5 CTR WING TANK UPPER SURFACE FOUND CORRODED. REPAIR CARRIED OUT AS PER E.A. 1-5710-132234, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 108.Oct 12, 2009 · N619FE · Doug MD11F · Fuel StorageSDR FDEA200910093522Skin · corrodedRT WING UPPER SURFACE FOUND CORROSION AT XORS 97 AFT OF FWD EDGE 6 INCHES. REPAIRED AS PER E.A. NR 1-5710-132239, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 108.Oct 9, 2009 · N619FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200910083507Hinge · corrodedRT WING INBD FLAP OTBD HINGE (FLAP MOUNTED) PIVOT LUG OTBD BORE FOUND WITH CORROSION. REPAIRED AS PER E.A. NR 1-5750-132237. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 108.Oct 8, 2009 · N619FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200910083506Hinge · gougedLT WING INBD FLAP OTBD HINGE (FLAP MOUNTED) PIVOT LUG OTBD FOUND WITH TOOL MARKS. REPAIR CARRIED OUT AS PER E.A. 1-5750-132236, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 108.Oct 8, 2009 · N619FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200910083505Hinge · gougedLT WING INBD FLAP OTBD HINGE (FLAP MOUNTED) PIVOT LUG INBD FOUND WITH TOOL MARKS. REPAIR CARRIED OUT AS PER E.A. 1-5750-132236, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 108.Oct 8, 2009 · N619FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200910083504Hinge Fitting · corrodedLT WING OTBD FLAP INBD FWD HINGE FITTING LWR INBD ATTACH HOLE FWD AND AFT SURFACE FOUND CORROSION. REPAIR CARRIED OUT AS PER E.A. 1-5750-132235, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 108.Oct 8, 2009 · N619FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200910083503Longeron · crackedDURING HIGH FREQUENCY EDDY CURRENT INSP ON NLG LT SIDE TRUNNION FITTING TRIM OUT AREA FOUND LONGERON CRACK APPROX 0.3 INCH. TRIMMED OUT AREA CRACKED LONGERON REMOVED AND REPLACED AS PER SRM 51-31-01, REVISION 41. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, Oct 8, 2009 · N619FE · Doug MD11F · Fuselage Main, Longeron/Stringer
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