N321FE

Service difficulty reports · 193

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 = 'N321FE' 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 06FDEA03795Warning Light · illuminatedON APPROACH CONFIGURING NORMALY TO 22DEGS / EXT GEAR DOWN. WHEN SELECTING 35 / EXT GOT RED DIS-AGREE LIGHT. RAN RED TABS AND PUT FLAPS / SLATS IN 22 DEGS FOR LANDING. NO OTHER PROBLEMS NOTED. MEL 26OCT06 16:17 SJC R ACN RELEASED FOR SERVICE PER MEL/CDOct 26, 2006 · N321FE · Doug DC1030 · Trailing Flap Position Indicating SystemSDR 06FDEA1562Floor Support · corrodedCABIN FLOOR PANEL SUPPORT HAS CORROSION LOCATED UNDER R-1 DOOR SILL PLATE BS 421 TO 460 RBL 107.0. REPAIRED CABIN PANEL SUPPORT IAW E8-5310-96466, FUSELAGE - SEAT TRACK CORROSION AT STA 443 TO 456 INTERIM REPAIR. MAJOR REPAIR.Apr 20, 2006 · N321FE · Doug DC1030 · Fuselage Miscellaneous StructureSDR 06FDEA1318Repair · misinstalledDOUBLER REPAIR AT FS 755-787, L47L-49L EVALUATED AND FOUND NOT TO BE PER SRM. REMOVED AND REPLACED DOUBLER WITH NEW DOUBLER IAW DC10 SRM 53-20-00 FIG 6 VOL I. THIS WAS CONSIDERED TO BE A MAJOR REPAIR.Apr 6, 2006 · N321FE · Doug DC1030 · Fuselage Main, Plate/SkinSDR 06FDEA1277Seat Track · wornFOUND MAIN CABIN SEAT TRACK LBL 8 TWO LUGS WORN STA 1636 AND 1644. REPLACED DAMAGE SEAT TRACK BY SPLICING IAW DC10 SRM 53-70-00 FIG 1 VOL I FROM LBL 8 STA 1530 TO STA 1651. ALODINED AND PRIMED IAW DC10SRM 51-21-01 VOL II. INSTALLED IAW DC10 SRM 51-31-01 VOLApr 1, 2006 · N321FE · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA1149Fitting · shearedNR 1 AND NR 3 PYLONS HAVE SHEARED BOLTS AT FWD PYLON TO WING MOUNT FITTING, FASTENERS ARE COMMON TO OUTER SKIN AND TOMB-STONE FITTING AND UPPER CHORD ANGLE. REMOVED AND REPLACED FASTENERS IAW DC10-SRM 51-31-01-VOL 2 AND DC10-30 AMM 20-50-02.Mar 19, 2006 · N321FE · Doug DC1030 · Nacelle/Pylon, Attach FittingsSDR 05FDEA01852Seal · unsecureIN CRUISE AT FL330 FOR FL340 HAD A RAPID DECOMPRESSION. THE CABIN RAPIDLY CLIMBED TO THE A/C ATTITUDE & A EMERGENCY DESCENT WAS IN PROGRESS. PERFORMED QRH PHASE ONE'S AND LOSS OF PRESSURIZATION CHECKLIST. FOUND MAIN A SECTION OF MAIN CARGO DOOR SEAL PROTRUDJul 7, 2005 · N321FE · Doug DC1030 · Cargo/Baggage DoorsSDR 05FDEA01256Manifold · leakingCLIMBING OUT OF SLC THRU 10,000 FT NR 3 MANIFOLD FAIL LIGHT ILLUMINATED, RAN RED TABS AND RETURNED TO SLC DUE TO ICING CONDITIONS. ALSO WING ANTI-ICE WAS NOT ON AND NR 3 TEMP GAUGE WAS RED-LINING. PERFORMED NR 3 SYS DECAY CHECK RAN ENGINES AND DETERMINED NR May 12, 2005 · N321FE · Doug DC1030 · Pneumatic Indicating SystemSDR 04FDEA02802Skin · damagedNR 1 ENGINE IB COE COWL IS DAMAGED AT LEADING EDGE. REMOVED CORE COWL, CUT OUT DAMAGE, REMOVED FRAME AND RUBSTRIP, FABRICATED DOUBLER AND FILLER, DRILLED AND FITTED NEW FRAME AND RUBSTRIP, INSTALLED DOUBLER AND FILLER, FRAME AND RUBSTRIP IAW DC10 SRM 54-0Sep 22, 2004 · N321FE · Doug DC10 · Nacelle/Pylon, Plate/SkinSDR 04FDEA02772Fitting · nickedLEFT HAND WING PYLON AFT ATTACH CLEVIS FITTING FORWARD LOBE HAS NICK. BLENDED AREA IAW DC10 SRM 57-00-01 VOL I, FOUND TO BE WITH IN LIMITS IAW DC10 SRM 57-00-01 VOL I, AND EA 8-5742-81464, PRIMED IAW DC10 SRM 51-21-01 VOL II. REMOVED APPROXIMATELY 0.060 INCHSep 20, 2004 · N321FE · Doug DC1030F · Nacelle/Pylon, Main FrameSDR 04FDEA02774Pipe · brokenAFT CARGO COMPARTMENT HEATING PIPE BROKEN AT STA 1910. REMOVED PIPING LINE FOR REPAIR IAW DC10 MM 20-10-01. CUT OUT AND FABRICATED AND WELDED IN NEW SECTION IAW FEDEX EA 8-2140-81471. INSTALLED PIPING AT AFT CARGO COMPARTMENT IAW DC10-30 MM 20-10-01, LEAK CSep 20, 2004 · N321FE · Doug DC1030F · Heating SystemSDR 04FDEA02773Skin · damagedREPAIR DOUBLER ON RIGHT HAND FUSELAGE STA 1781 TO 1815 BETWEEN L-29R AND L-30R, NOT IAW DC10-30 SRM. REMOVED REPAIR DOUBLERS IAW DC10-30 SRM 51-33-01 VOL II AND 51-35-01 VOL II. FABRICATED FINGER DOUBLERS AND EXTERNAL DOUBLERS AND INSTALLED IAW DC10-30 SRM 5Sep 20, 2004 · N321FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR 04FDEA02771Ventilator Panel · crackedNR 3 PYLON VENT PANEL 487 DR HAS SEVERAL CRACKS. ROUTED OUT CRACKS IN WELDED AREA, FABRICATED FILLER AND WELDED IAW FEDEX EA 8-5480-31457. REMOVED AND REPLACED CRACKED BRACKET, FABRICATED BRACKET IAW DOUGLAS DWG AUB 7054, REINSTALLED SKIN IAW DC10-30 SRM 51Sep 20, 2004 · N321FE · Doug DC1030F · Nacelle/Pylon, Main FrameSDR 04FDEA02722Bushing · wornNR 3 PYLON THRUST LINK PYLON LUGS HAS 2 WORN BUSHINGS. REMOVED AND REPLACED IAW FEDEX DC10 CMM 20-20-07.Sep 17, 2004 · N321FE · Doug DC1030F · Nacelle/Pylon Miscellaneous StructureSDR 04FDEA02720Bearing · corrodedNR 3 PYLON TOMBSTONE FITTING UPPER BEARING PITTED. REMOVED AND REPLACED NR 3 PYLON UPPER SPHERICAL BEARING IAW DC10-30 MM 54-40-02-2.Sep 17, 2004 · N321FE · Doug DC1030F · Nacelle/Pylon, Attach FittingsSDR 04FDEA02718Bearing · migratedNR 1 ENG PYLON AFT SPHERICAL BEARING ATTACH BOLT TORQUE STRIP BROKEN & THE BEARING MIGRATES. REMOVED AND REPLACED BEARING IAW DC 10-30 FEDEX MM 54-40-02-2, REMOVED CORROSION IAW DC10-30 FEDEX MM 54-40-02, REMOVED FUEL DRAIN LINE IAW FEDEX DC 10-30 MM 0- 50-01Sep 17, 2004 · N321FE · Doug DC1030F · Nacelle/Pylon, Attach FittingsSDR 04FDEA02717Fitting · migratedNR 3 ENGINE PYLON AFT SPHERICAL BEARING MIGRATES. REMOVED SPHERICAL BEARING IAW DC10-30MM FEDEX 54-40-02 HONED HOLE IAW DC 10-30 FEDX AMM 54-40-02-2, REMOVED DRAIN LINE IAW FEDEX DC10-30 MM 54-10-00, REMOVED NUT STRIPS IAW DC10-30 FEDEX SRM 51-31-01, INST NSep 17, 2004 · N321FE · Doug DC1030F · Nacelle/Pylon, Main FrameSDR 04FDEA02716Seat Track · crackedMAIN CABIN, CARGO SEAT TRACK HAS 2 CRACKS AT LBL 24 & STA 1009 TO 1059 (MRK). REMOVED 2 FLOORBOARDS. REMOVED AND REPLACED SEAT TRACK IAW 51-31-01 VOL 2 OF FEDEX DC10-30 SRM MAT ID FOR SEAT TRACK 7929147-1350 IAW FEDEX DC10-30 SRM 53-42-01 FIG 4 SH1 VOL 3 MATSep 17, 2004 · N321FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02715Seat Track · corrodedR/S AFT PIT STA 1841 TO 1902 OUTBOARD FLANG OF SEAT TRACK CORRODED. REMOVED CORROSION ON SEAT TRACK IAW FEDEX DC10-30 SRM 51-21-01 VOL 2 PG 21. FOUND TO BE OUT LIMITS, IAW FEDEX DC10 SRM 53-70-00 PG 21 VOL I, MAKE NEW SEAT TRACK IAW DAC DWG AGA3855, TREATMENSep 17, 2004 · N321FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02713Floorbeam · corrodedAFT PIT STA 1902 FLOOR SUPPORT FRAME T-CAP CORRODED UPPER SURFACE. REMOVED FRAME T-CAP IAW DC10 SRM 51-35-01 VOL 2. CORROSION OUT OF LIMITS IAW FEDEX DC10 SRM 53-00-01 VOL I, PG 8. MATERIAL FOR T-CAP ANGLE IS 7075-T6 .063 P/O 353160.4 IAW DC 10 SRM 53-16-01Sep 17, 2004 · N321FE · Doug DC1030F · Fuselage Main, Floor BeamSDR 04FDEA02712Floorbeam · corrodedAFT PIT STA 1902, 20 LBL TO 20 RBL FLOOR SUPPORT FRAME CORRODED TOP SIDE OF T-CAP. REMOVED FRAME T-CAP IAW DC10 SRM 51-35-01 VOL 3, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL I. REMOVED DAMAGE IAW DC10 SRM 53-00-01 VOL I. FAB FILLER DOUBLER IAW DC1Sep 17, 2004 · N321FE · Doug DC1030F · Fuselage Main, Floor BeamSDR 04FDEA02711Bearing · migratedNR 3 ENGINE AFT MOUNT O/B VERTICAL LINK HAS BOTH BEARINGS MIGRATING. REMOVED UNSERVICABLE NR 3 AFT ENGINE MOUNT, INSTALLED SERVICEABLE NR 3 AFT ENGINE MOUNT ASSEMBLY IAW DC10-30 MM 71-20-01-03.Sep 17, 2004 · N321FE · Doug DC1030F · Engine Mount SectionSDR 04FDEA02699Fitting · corrodedNR 1 PYLON TOMBSTONE FITTING UPPER BEARING STIFF AND PITTED. REMOVED UPPER SPHERICLE BEARING FROM NR 1 PYLON TOMBSTONE CHECKED DIAMETRICAL CLEARANCE OF NEW BEARING INSIDE DIA AND PLUG IS .0001 MAX CLEARNCE .012. CLEARANCE CHECK OK IDENTIFIED MOUNT BOLT TO BESep 16, 2004 · N321FE · Doug DC1030F · Nacelle/Pylon, Attach FittingsSDR 04FDEA02649Fitting · migratedNUMBER 1 ENGINE PYLON AFT SPHERICAL ATTACH BOLT TORQUE STRIPE BROKEN AND THE BEARING IS MIGRATING. REMOVED BEARING IAW DC10MM 54-40-02, REMOVED CORROSION IAW DC10 MM 54-40-02. REMOVED AFT BULKHEAD FITTING AUB 7025-33 IAW DC10-30 SRM 51-31-01 VOL II, LOCATED,Sep 4, 2004 · N321FE · Doug DC1030F · Nacelle/Pylon, Attach FittingsSDR 04FDEA02648Fitting · migratedNUMBER 3 ENGINE PYLON AFT SPHERICAL BEARING MIGRATING. REMOVED SPHERICAL BEARING HONED HOLE REMOVED AFT BULKHEAD FITTING, LOCATED AND DRILLED NEW FITTING IAW DAC DWG AUB 7025, INSTALLED NEW FITTING P/N AUB 7025-33 IAW DAC DWG AUB 7025 IAW FEDEX DC10 SRM 51-38Sep 4, 2004 · N321FE · Doug DC1030F · Nacelle/Pylon, Attach FittingsSDR 04FDEA02651Hinge Fitting · corrodedLEFT WING INBOARD FLAP, OUTBOARD HINGE SUPPORT, PIVOT ATTACH POINT, INBOARD BORE PITTED AND CORRODED. REMOVED CORROSION, ORIGINAL DIAMETER 1.240, FINAL DIAMETER 1.2819, MATERIAL REMOVED .0419 IS BEYOND LIMITS. FABRICATED OVERSIZED BUSHING, INSTALLED AND HONESep 4, 2004 · N321FE · Doug DC1030F · Trailing Edge FlapsSDR 04FDEA02650Hinge Fitting · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE SUPPORT, PIVOT ATTACH POINT, INBOARD BORE CORRODED. REMOVED CORROSION, ORIGINAL DIAMETER 1.1885 FINAL DIAMETER 1.3817, FOUND TO BE OUT OF LIMITS. FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED TO FINAL INSIDE DIAMETESep 4, 2004 · N321FE · Doug DC1030F · Trailing Edge FlapsSDR 04FDEA02645Liner · crackedAFT LOWER CARGO COMPARTMENT FORWARD THRESHOLD ATTACH EAR IS CRACKED. WELD REPAIRED AFT CARGO DOOR LINER IAW FEDEX EA 8-5320-81459. REFERENCE N/R N00682.Sep 4, 2004 · N321FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 04FDEA02646Panel · delaminatedRIGHT WING PANEL 635 GL DELAMINATED AND ONE GOUGE. REPAIRED PANEL 635 GL BY FABRICATING AND BONDING NEW SKINS, DOUBLERS AND CORE IAW TPS 1001 REV E, DAC DWG ARC2008 AND FEDEX EA 8-5750-81442. REFERENCE N/R N00239.Sep 4, 2004 · N321FE · Doug DC1030F · Wing, Plate/SkinSDR 04FDEA02641Doubler · tornLEFT WING LEADING EDGE CAVITY, CORRUGATED SKIN TORN ABOVE ANTI-ICE TELESCOPE DUCT, STA XORS 372. REMOVED AND INSTALLED TELESCOPING DUCT IAW DC10 MM 30-11-01-2. REPAIRED DAMAGED SKIN IAW FEDEX EA 8-5710-81456 STEP 1-10, REFERENCE N/R N00730.Sep 4, 2004 · N321FE · Doug DC1030F · Wing, Plate/SkinSDR 04FDEA02640Panel · delaminatedLEFT WING LOWER TRAILING EDGE PANE 541KB DELAMINATED INTERIOR SURFACE. REMOVED INNER SKIN, OUTER SKIN, DOUBLER AND CORE IAW FEDEX EA 8-5750-81445. BONDED NEW INNER SKIN, OUTER SKIN DOUBLER AND CORE IAW FEDEX EA 8-5750-81445 AND TPS 1001 REV E, REFERENCE N/R Sep 4, 2004 · N321FE · Doug DC1030F · Wing, Plate/SkinSDR 04FDEA02639Roller · corrodedLEFT WING INBOARD FLAP INBOARD TRACK 1 EACH AFT UPPER SMALL ROLLER IS PITTED. REMOVED AND REPLACED LEFT HAND INBOARD FLAP INBOARD TRACK AFT UPPER SMALL LOAD ROLLER IAW FEDEX EA> 8-5750-81449. ORIGINAL COPY OF EA 8-5750-81449 IS ATTACHED TO FEDEX N/R N00910, Sep 4, 2004 · N321FE · Doug DC1030F · Trailing Edge FlapsSDR 03FDEA00341Line · faultyAFTER APPROX 3 HRS OF FLT WHILE CRUISING AT FL 330 NO 1 HYD SYSTEM QTY SLOWLY DECREASED FROM 6.0 GALS TO 2.8 GALS AND STILL SLOWLY DECREASING. TURNED OFF #1 HYD PUMPS C/W RED TABS. TURNED PUMPS ON FOR LANDING, CONFIGURATION TO FLAP 35 EXTENSION NOTED 2.3 Mar 19, 2003 · N321FE · Doug DC1030 · Hydraulic System, MainSDR 02FDEA00529Fitting · crackedFOUND DURING B-CHECK R/OUTBD FLAP CARRIAGE SUPPORT FITTING CRACKED APPROX 80 PERCENT OF FITTING. THIS IS SECOND CRACK FOUND IN THIS AREA.Jul 29, 2002 · N321FE · Doug DC1030 · Trailing Edge FlapsSDR 01FDEA00793Hydraulic Line · leakingHYD NR 1 QUANTITY DECREASED TO ZERO & PRESS LESS THAN 1000. REMOVED AND REPLACED HYD LINES. LEAK CHECK OK.Aug 29, 2001 · N321FE · Doug DC1010CF · Hydraulic System, MainSDR 00FDEA00607Bracket · crackedLEFT NR 3 DOOR FWD FROM THE TOP NR 5 MOUNTING TOP-STUD BRACKET FOUND CRACKED. *S/D* REMOVED AND REPLACED PER DC10 SRM 51-35-02 VOL II.Aug 28, 2000 · N321FE · Doug DC1030F · Passenger/Crew DoorsSDR 99FDEA00368Seat Track · crackedMAIN DECK UPPER FUSELAGE, CRACK FOUND ON SEAT TRACK AT BS 635 X=27.5 LH-687. MAIN DECK UPPER FUSELAGE CRACK ON SEAT TRACK AT BS 635 X=75.25 RH-688. MAIN DECK CRACK ON SEAT TRACK AT BS 775X=8.5 RH-700. *S/D* REPAIRED SEAT TRACKS 687, 688, 700 AS PER SRM 53-Aug 31, 1999 · N321FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 98FDEA00765Ins · inop98-312 - COULD NOT GET INS UNIT TO R-NAV UPDATE. GOT R-NAV YELLOW LIGHTS BUT WOULD NEVER GO TO GRN. UPDATED ALL 3 INS WITH SOFTWARE FX9813 PER MM 34-43-00-3. CKD SYS PER MM 34-43-00-1 ON GRD ALL CKD OK. OK TO CONT.Dec 27, 1998 · N321FE · Doug DC1030F · Integrated Flight SystemSDR 98FDEA00715Control · inopNR 5 BRAKE TEMP 150 DEG, LEFT GEAR DOWN. REMOVED AND REPLACED NR 5 BRAKE ASSY TEMP SENSOR AND ANTISKID CONTROL UNIT, PERF BITE TEST.Nov 19, 1998 · N321FE · Doug DC1030F · Brake Anti-Skid SectionSDR 98ZZZX3587Spar · corrodedRT WING UPPER SURFACE JUST INBOARD AND FORWARD OF NR 2 SPOILER HAS CORROSION THAT RUNS FROM (XORS 480) TO (XORS 492). REPAIR WAS C/W BY DOUGLAS PROVIDED E.A. NOTE: MAXIUM DEPTH OF CORROSION WAS .050 INCH.Aug 28, 1998 · N321FE · Doug DC1030F · Wing SparSDR 96FDEA01345Strap · crackedSNRM 5074. LEFT WING - OTBD FLAP INBD HINGE SUPPORT FITTING OTBD TENSION STRAP IS CRACKED LOWER BOLT HOLE EXTERNAL SURFACE. REMOVED AND REPLACED SUPPORT FITTING TENSION STRAP PER EA 8-5710-29040 AND EO 8-5750-7-4320B3 PT 1.Aug 10, 1996 · N321FE · Doug DC1030 · Trailing Edge FlapsSDR 96FDEA01329Fitting · crackedSNRM 3063. HORIZONTAL STABILIZER CENTER SECTION FITTING IS CRACKED AT RT FORWARD UPPER TORQUE BOX PLANE, STA 2033, STR 13R. ****S/D***** VERIFIED CRACK WITH HFEC. FABRICATE REPAIR ANGLE AND DOUBLER. INSTALLED PER EA 8-5310-29041.Aug 7, 1996 · N321FE · Doug DC1030 · Fuselage Miscellaneous StructureSDR 96FDEA01346Bracket · crackedSNRM 6004 R/H WING - O/B SLAT DRIVE MECHANISM, OUTER BRKT HAS CRACK INDICATION IN FWD FLANGE FILLET RADIUS. R/R SLAT DRIVE MECHANISM BRACKET PER MM 27-83-02.Jul 26, 1996 · N321FE · Doug DC1030 · Flight Control SystemSDR 95FDEA00102Retract Mech · malfunctionedLANDING GEAR DIDN'T EXTEND WHEN LANDING GEAR HANDLE WAS PLACED IN DOWN POSITION. DOORS OPENED, BUT GEAR DIDN'T EXTEND. HYD PRESS WAS OK AND GEAR NOT DOWN CONFIRMED BY GEAR HORN ON STDY AT FLAPS 35 DEGREES. RECYCLED GEAR AND GEAR EXTNEDED ON SECOND ATTEMPT, Jan 31, 1995 · N321FE · Doug DC1030F · Landing Gear Retraction/Extension System
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