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 05FDEA01697Structure · corrodedWITH REFERENCE TO WORK CARD E1-5510-7-5000 D1 PART 1, NR 14L FITTING BARREL NUT BORE FOUND BADLY CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.Jun 26, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01696Structure · corrodedWITH REFERENCE TO WORK CARD E1-5510-7-5000, REQUIRE TO TRIM LT OPERATING BULKHEAD FOR NR 35L BARREL NUT REWORK ACCESS. TRIMMED OUT AS PER SRM 51-31-01 VOL. II AND FOUND EXCEEDED LIMIT AS PER FEDEX EO 1-5510-7-5000. REPAIR CARRIED OUT ON TRIMMED AREA AT LT OPJun 26, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01695Structure · corrodedWITH REFERENCE TO WORK CARD E1-5510-7-5000, RT BARREL NUT HOLE NR 36R FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-83021Jun 26, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01694Structure · corrodedWITH REFERENCE TO WORK CARD E1-5510-7-5000, LT BARREL NUT HOLE NR 1L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIR CARRIED OUT ON LT HORIZONTAL STABILIZER, LT BARREL NUT HOLE NR 1 AS PER FEDEX EA 1-5510-83020.Jun 26, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01693Structure · corrodedWITH REFERENCE TO WORK CARD E1-5510-7-5000, LT BARREL NUT HOLE NR 35L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-83022Jun 26, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01692Structure · corrodedWITH REFERENCE TO WORK CARD E1-5510-7-5000, LT BARREL NUT HOLE NR 33L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-83022Jun 26, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01691Structure · corrodedWITH REFERENCE TO WORK CARD E1-5510-7-5000, LT BARREL NUT HOLE NR 29L, FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-83022.Jun 26, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01690Structure · corrodedWITH REFERENCE TO WORK CARD E1-5510-7-5000, LT BARREL NUT HOLE NR 27L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83022.Jun 26, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer StructureSDR 05FDEA01674Fitting · corrodedEMPENNAGE WITH REFERENCE TO EO 1-5510-7-5000-01 PART 1, FOUND NR 26R FITTING BORE CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.Jun 24, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer Miscellaneous StructureSDR 05FDEA01673Fitting · corrodedEMPENNAGE WITH REFERENCE TO EO 1-5510-7-5000-01 PART 1, FOUND NR 14R FITTING BORE CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.Jun 24, 2005 · N619FE · Doug MD11 · Horizontal Stabilizer Miscellaneous StructureSDR 05FDEA01677Torque Ring · crackedNR 3 ENG, RIGHT FORWARD FRAME UPPER TORQUE RING CRACKED APPROXIMATELY 5 INCHES IN LENGTH. THRUST REVERSER REMOVED AND INSTALLED AS PER WORK CARD 78T3003-R AND WORK CARD 78T3903-R FOR WORK DETAILS. THRUST REVERSER ADJUSTMENT AND OPERATION CHECK CARRIED OJun 24, 2005 · N619FE · Doug MD11 · Engine (Turbine/Turboprop)SDR 05FDEA01679Torque Ring · crackedNR 1 ENGINE, RT THRUST REVERSER FORWARD FRAME, UPPER TORQUE RING CRACKED APPROXIMATELY 1.5 IN LENGTH. THRUST REVERSER REMOVED AND INSTALLED NEW REVERSER AS PER WORK CARD 78T3001-R AND WORK CARD 78T3901-R, GE NR 1 RIGHT REVERSER DOOR - INSTALL. REVERSER ADJUJun 24, 2005 · N619FE · Doug MD11 · Engine Thrust ReverserSDR 05FDEA01678Skin · crackedNR 2 ENGINE, NOSE INLET LIP FOUND CRACKED AT 8 O'CLOCK POSITION AND EXISTING REPAIR DOUBLER HAS LOOSE FASTENERS. REMOVED AND REPLACED AS PER AMM 54-22-01-4 AND APPLIED SEALANT AS PER AMM 54-22-01-4.Jun 24, 2005 · N619FE · Doug MD11 · Engine Air Intake SystemSDR 05FDEA01676Track · crackedNR 2 ENGINE, LT THRUST REVERSER UPPER SLIDER TRACK CRACKED. REMOVED AND INSTALLED NEW REVERSER AS PER WORK CARD 78T3002-L AND WORK CARD 78T3902-L. ADJUSTMENT AND OPERATION CHECK CARRIED OUT AS PER WORK CARD 78T3902-L, GE NR 2 LEFT THRUST REVERSER DOOR - INSJun 24, 2005 · N619FE · Doug MD11 · Engine Thrust ReverserSDR 05FDEA01675Track · crackedNR 2 ENGINE, RT THRUST REVERSER UPPER SLIDE TRACK CRACKED. REMOVED AND REPLACED AS PER WORK CARD 78T3002-R AND WORK CARD 78T3902-R. ADJUSTMENT AND OPERATIONAL CHECK CARRIED OUT AS PER WORK CARD 78T3902-R, GE NR 2 RIGHT THRUST REVERSER DOOR - INSTALL.Jun 24, 2005 · N619FE · Doug MD11 · Engine Thrust ReverserSDR 05FDEA01654Cargo Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR CARGO TRACK AT STA 1119, LBL 8.5, FOUND WITH CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOL I FIG 1.Jun 22, 2005 · N619FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01623Seat Track · crackedMAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT LBL 47, STATION 635 FOUND CRACKED APPROXIMATELY 2 INCHES LONG. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Jun 21, 2005 · N619FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01622Seat Track · crackedMAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT LBL 27, STATION 635 FOUND CRACKED APPROXIMATELY 2 INCHES LONG. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE I.Jun 21, 2005 · N619FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01620Seat Track · damagedMAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 1230 - 1239, LBL 47 FOUND CROWN ELONGATED. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOL I FIG 1.Jun 20, 2005 · N619FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA00778Fitting · crackedRT WING I/B FLAP I/B SIDE LOAD ROLLER FITTING ATTACHMENT IS CRACKED AT BASE RADIUS. REMOVED AND REPLACED R/H WING SIDELOAD ROLLER FITTING IAW M/M 20-50-02-2.Mar 30, 2004 · N619FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA00777Fitting · crackedLT WING I/B FLAP I/B SIDE LOAD ROLLER FITTING ATTACHMENT IS CRACKED AT BASE UPPER RADIUS. CRACK VERIFIED BY NDT. ORDERED NEW FITTING. INSTALLED NEW BEARINGS PER W/C E-1-5750-7-5003BL, SEQ 459 STEPS 33-34. INSTALLED NEW FITTING, TORQUED BOLTS PER SMP M/M 20-50-Mar 30, 2004 · N619FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA00776Support · crackedRT O/B TRAILING EDGE FLAP STOP BOLT SUPPORT ISLAND IS CRACKED (2 PLACES) REFER FIGURE 1 (SHEET 10 OF 11 ) FIGURE AV OF 1-5750-7-5002 B. REMOVED & REPLACED SUPPORT FITTINGS PER SRM51-31-01 & DAC DWG. ARC4100. COMPLIED BY AMT 357288.Mar 30, 2004 · N619FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA00759Fitting · corrodedLT WING INBOARD FLAP OUTBOARD HINGE SUPPORT FITTING AT PIVOT BEARING, FUSE PIN IS HEAVILY CORRODED. REMOVED & REPLACED HINGE PIN, BUSHING, WASHER, NUT & COTTER PIN AND INSTALLED IAW M/M 27-50-20-4.Mar 26, 2004 · N619FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA01028Pseu · malfunctionedON CLIMBOUT OF FRA, RECEIVED A SLAT DISAGREE ALERT WHEN SLATS RETRACTED WITH A STRONG ROLL TO RIGHT. RED TABS COMPLIED WITH AND SLATS EXTENDED A/S 270 KIAS. SLATS EXTENDED FINE WITH NO CONTROL PROBLEMS. DUMPED FUEL AND DIVERTED TO PARIS. T/S AS PER FIM 31-Jul 2, 2003 · N619FE · Doug MD11 · Leading Edge Slat Position Indicating SystemSDR 03FDEA01008Pump · failedHYD PUMP 1R OFF DISPLAYED DURING CRUISE AT FL280. PUMP 1R FAULT LIGHT ON HYD OVERHEADD ILLUMINATED. HYD SYS 1 TEMP INDICATED 94 DEG C. SUBSEQUENTLY HYD 1 OFF ALERT AND NR 2 AUTOPILOT DISCONNECT. RETURNED TO RPLB. TEMP DECREASED TO 79 DEG C, WHEN ON APPROAJun 30, 2003 · N619FE · Doug MD11 · Hydraulic Pump (Electric/Engine), MainSDR 03FDEA00346Sensing Element · damagedAFTER DEPARTURE AT TPE TURNED ON ANTI ICE (ENGINE NR 2 A-ICE), WE WERE IN ICING CONDITION, DESCENDED LOWERED AND RETURNED TO TPE. FACT 23MAR03 22:52 TPE R RECEIVED A/C PARTS AT 2110Z, REPLACED SENSING ELEMENTS D1-90 IAW MM 30-22-11-4, AND PERFORMED ANMar 23, 2003 · N619FE · Doug MD11F · Air Intake Anti/De-Ice SystemSDR 02FDEA00834Rccb · faultyJUST PRIOR TO TOP OF CLIMB, RIGHT EMERGENCY AC BUS OFF. CONSULTED WITH MOCC, RETURNED TO AIRPORT. EPCU FAULT LOGGED AND FOUND B1-138 RCCB IN CAC SHOWED OPEN INDICATOR BUT B1-139 CONT CB WAS CLOSED. REMOVED AND REPLACED B1-138 RCCB IAW AMM, ALSO PRECAUTION RNov 13, 2002 · N619FE · Doug MD11 · AC Generation SystemSDR 02FDEA00766Attach Fitting · corrodedINBD AFT TOILET MOUNTING ATTACHMENT CORRODED AT BS 421. R&R SUPPORT PER SRM 51-33-01, VOL II.Oct 25, 2002 · N619FE · Doug MD11 · Fuselage, Equipment Attach FittingsSDR 02FDEA00767Seat Track · corrodedFWD CABIN LT SEAT TRACK AT BS 470 FOUND CORRODED. R&R SEAT TRACK PER SRM 53-70-00.Oct 25, 2002 · N619FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 01FDEA00993Landing Gear · malfunctionedFLT 5081 WRI, AFTER T/O NOSE GEAR WOULD NOT RETRACT.Nov 15, 2001 · N619FE · Doug MD11F · Landing Gear Retraction/Extension SystemSDR 01FDEA00981Warning System · activatedNOSE GEAR UNSAFE IND AFTER GEAR RETRACTION, CYCLED GEAR.Nov 11, 2001 · N619FE · Doug MD11F · Landing Gear Position and WarningSDR 01FDEA00980Warning System · false indicationNOSE GEAR LIGHT STAYED AFTER GEAR RETRACTION. CHECKED PHYSICAL CONDITION SENSORS AND TARGETS. NO DEFECTS NOTED. OK FOR SERVICE.Nov 9, 2001 · N619FE · Doug MD11F · Landing Gear Position and WarningSDR 01FDEA00790Frame · crackedFUSELAGE TRANSVERSE FRAME DENTED AT STA 1701 LEFT ALONG LONGERON 12L. R&R FRAME PER SRM 53-30-00 FIG 1 VOL 1.Aug 24, 2001 · N619FE · Doug MD11F · Fuselage Main, FrameSDR 01FDEA00791Frame · crackedFUSELAGE TRANSVERSE FRAME DENTED AT STA 1661 RIGHT ALONG LONGERON 12R. R&R FRAME PER SRM 53-30-00 FIG 1 VOL 1.Aug 24, 2001 · N619FE · Doug MD11F · Fuselage Main, FrameSDR 01FDEA00792Frame · crackedFUSELAGE TRANSVERSE FRAME DENTED AT STA 1701 RIGHT ALONG LONGERON 12R. R&R FRAME PER SRM53-30-00 FIG 1 VOL 1.Aug 24, 2001 · N619FE · Doug MD11F · Fuselage Main, FrameSDR 01FDEA00788Frame · crackedFUSELAGE TRANSVERSE FRAME CRACKED AT STA Y=1601 LEFT 3.0 INCH LENGTH, ALONG LONGERON 12L. REMOVED AND REPLACED FRAME PER SRM 53-30-00 FIG 1 VOL 1.Aug 24, 2001 · N619FE · Doug MD11F · Fuselage Main, FrameSDR 01FDEA00789Frame · crackedN 527 FUSELAGE TRANSVERSE FRAME CRACKED AT STA Y=1571 LEFT ALONG LONGERON 12L. ** S/D ** COMINGAug 24, 2001 · N619FE · Doug MD11F · Fuselage Main, StructureSDR 01FDEA00155Harness · faultyIN CRUISE GEAR UP RECD INTERMITTENT FIRE DET 3 FAIL ALERT. CLEARANCE AND PERM TO DUMP FUEL ON RADAR VECTORS. FOUND TERMINAL LUG LOOSE AT DH22C FOR LOOP-B TIGHTENED. FOUND OPEN WIRE BETWEEN DH23C & DH4C OF LOOP-A. REMOVED AND REPLACED WIRE HARNESS PER MM. Feb 21, 2001 · N619FE · Doug MD11F · Fire DetectionSDR 00FDEA00669Fire Detector · inoperativeNR 1 ENG FIRE DETECT FAIL ALERT 30 MIN AFT T/O FIRE TEST CAUSED NR 1 FIRE ALERT. REMOVED AND REPLACED NR 1 ENG LWR TURBINE DETECTOR LOOP PER MM 26-11-03-4. OPS CK GOOD.Sep 18, 2000 · N619FE · Doug MD11F · Fire DetectionSDR 00FDEA00414Cargo Track · crackedUPPER CARGO COMP BALLMAT AREA, FLOOR TRACK AT BS 635 X=8.5L CRACKED. UPPER CARGO COMP BALLMAT AREA, FLOOR TRACK AT BS 635 X=8.5R CRACKED. *S/D* REMOVED AND REPLACED PER SRM 53-70-00 VOL 1.Jun 27, 2000 · N619FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 99FDEA00141Hose · inoperativeRT MLG DID NOT RETRACT. CYCLED GEAR, NO HELP. REMOVED AND REPLACED NR 7 BRAKE HOSE AND SUPPORT IN RT MLG LOWER TORQUE LINK PER 32-40-00 AND 32-45-00-5, 32-31-00-5. AC OK FOR RELEASE.Apr 13, 1999 · N619FE · Doug MD11F · Hydraulic System, MainSDR 99FDEA00138Seat Track · crackedCRACK APPROX 10 INCHES LONG FOUND ON SEAT TRACK AT STA 905, X= 27.5 (RT) ON UPPER CARGO AREA.Apr 6, 1999 · N619FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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