N446FE, cancelled Jul 29, 2013

Service difficulty reports · 97

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 = 'N446FE' AND deregistration_id = 'N446FE-2013-07-29'
  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 FDEA201002150424Transmitter · malfunctionedAFTER TOGA POWER SET ON T/O, GOT A NR 1 ENG HIGH OIL PRESS LIGHT. REJECTED T/O. ALSO DURING START THE NR 1 ENG HIGH OIL PRESSURE LIGHT CAME ON FOR 1 MIN. GROUND RAN ENGINE IAW JRH SEVERAL TIMES. OIL PRESSURE FOR NR 1 ENG NEVER EXCEEDED 50 PSI. ALL ENGINE PAFeb 15, 2010 · N446FE · Airbus A310222 · Engine Oil PressureSDR FDEA200911244202Switch · malfunctionedON APPROACH, NO NOSE GEAR INDICATION ON NR 1 SYS (FRONT PANEL) NR 2 SYS (OVERHEAD PANEL) GOOD, DID A GO AROUND AND ON DOWNWIND, NOSE GEAR LIGHT CAME BACK AND INDICATED NORMAL. WHEN LIGHT WAS NOT INDICATING , DID ALL LIGHTS CHECK AND IT CHECKED GOOD. RELEASED Nov 24, 2009 · N446FE · Airbus A310222 · Landing Gear Position and WarningSDR 07FDEA04248Spar · failedLEFT HORIZONTAL STAB ON UPPER REAR SPAR BETWEEN RIBS 4/5 REPAIR STRAP IN WRONG MATERIAL TYPE. REMOVE AND REPLACE AS REQUIRED REMOVED STRAP IAW A310-200 FX SRM 55-11-21. FABRICATED NEW STRAP IAW FX A310-200 SRM 55-11-21 FIG 214 AND PG 285. INSTALLED NEW STSep 24, 2007 · N446FE · Airbus A310322 · Horizontal Stabilizer, Spar/RibSDR 07FDEA04251Spar · damagedLEFT HORIZONTAL STAB ON UPPER REAR SPAR BETWEEN RIBS 10 AND 11 REPAIR STRAP REQUIRES REMOVAL FOR MATERIAL TYPE VERIFICATION REMOVED STRAP IAW A310-200 SRM 55-11-21 PG 202. FABRICATED NEW STRAP IAW A310-200 SRM 55-11-21 FIG 214 AND PG 285. INSTALLED NEW STRAPSep 24, 2007 · N446FE · Airbus A310322 · Horizontal Stabilizer, Spar/RibSDR 07FDEA04247Spar · damagedRIGHT HORIZONTAL STAB ON UPPER REAR SPAR BETWEEN RIBS 9 AND 10 REPAIR STRAP REQUIRES REMOVAL FOR MATERIAL TYPE VERIFICATION REMOVED STRAP REF A310-200 SRM 51-40-21. FABRICATED STRAP IAW FED ED A310-200 SRM 55-11-21 FIG 215 AND PG 285. INSTALLED REPAIR STRAP Sep 24, 2007 · N446FE · Airbus A310222 · Horizontal Stabilizer, Spar/RibSDR 07FDEA03758Stringer Splice · misrepairedSTGR SPLICE REPAIR BETWEEN FRAME 72/73 ON STGR 56R REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA VISUALLY INSPECTED STGR SPLICE REPAIR BETWEEN FRAME 72/73 AT STGR 56 RT AND FOUND MATERIAL TYPE FOR STGRSep 14, 2007 · N446FE · Airbus A310222 · Fuselage Main, Longeron/StringerSDR 07FDEA03783Strap · misinstalledLEFT HORIZ STAB ON UPPER REAR SPAR BETWEEN RIBS 5 AND 8 REPAIR STRAP REQUIRES REMOVAL FOR MATERIAL TYPE VERIFICATION REMOVED DOUBLER STRAP DUE INCORRECT MATL IN REF A310 SRM 55-11-21 PG 202. REPLACED STRAP DOUBLER IAW A310 SRM 55-11-21 FIG 214.Sep 14, 2007 · N446FE · Airbus A310222 · Horizontal Stabilizer StructureSDR 07FDEA03788Frame · crackedFRAME CRACKED IN FASTENER HOLE AT FRAME 43A LOWER HOLE COMMON TO CRUCIFORM FITTING LT SIDE SEE JOB CARD 41X5271ALI FROM CABIN SIDE 1ST LAYER RUNNING IN THE 5 O`CLOCK DIRECTION .075 DEEP AND RUNNING TO THE 2ND LAYER 100 PERCENT ON SCREEN AMPLITUDE REMOVED AND RSep 14, 2007 · N446FE · Airbus A310222 · Fuselage Main, FrameSDR 07FDEA03786Frame · crackedFRAME CRACKED IN FASTENER HOLE AT FRAME 42A LOWER HOLE COMMON TO CRICIFORM FITTING SEE JOB CARD 41 BY 5271ALI. RT SIDE FROM CABIN SIDE THE FIRST LAYER RUNNING IN THE 6 O`CLOCK AND 9 O`CLOCK DIRECTIONS APPROX .100 DEEP TO THE 2ND LAYER 100 PERCENT + AMPLITUDE Sep 14, 2007 · N446FE · Airbus A310222 · Fuselage Main, FrameSDR 07FDEA03753Strap · crackedLT FWD PAX/CREW DOOR CUTOUT, HFEC INSPECTION INDICATES CRACK/CORROSION IN 5 LOCATIONS ALONG EDGE OF LOWER CORNER STRAPS AS FOLLOWS; (1) FWD LOWER CORNER- ONE 1/2" LONG AND ONE 1.0" LONG AND, (2) AFT LOWER CORNER - ONE 2 1/4" LONG, ONE 3/8" LONG AND ONE 2" LOSep 14, 2007 · N446FE · Airbus A310222 · Fuselage Miscellaneous StructureSDR 07FDEA03749Strap · crackedAREA IS RT FWD PAX/CREW DOOR CUTOUT. 1 1/8 INCH CRACK WITH POSSIBLE EXFOLIATION CORROSION EXISTS ALONG TOP EDGE OF FWD CORNER STRAP, BEGINNING APPROX 1 1/8 INCH FROM AFT EDGE OF CORNER STRAP, LOWER, FWD CORNER OF DOOR CUTOUT BEHIND FAILSAFE RING. AREA MARKSep 14, 2007 · N446FE · Airbus A310222 · Fuselage Miscellaneous StructureSDR 07FDEA03727Strap · crackedAREA IS RT FWD PAX/CREW DOOR CUTOUT, 3 5/8 INCH CRACK WITH POSSIBLE EXFOLIATION CORROSION EXISTS ALONG TOP EDGE OF AFT CORNER STRAP, BEGINNING 1" FROM FWD EDGE OF CORNER STRAP. (LOWER, AFT CORNER OF DOOR CUTOUT BEHIND FAIL/SAFE RING) AREA MARKED IN RED. SEE Sep 14, 2007 · N446FE · Airbus A310322 · Fuselage Miscellaneous StructureSDR 07FDEA03131Seat Track · shearedMAIN CABIN RIGHT SEAT TRACK Y-1959 AT FRAME 47 LUGS ARE BROKE OUT.Aug 26, 2007 · N446FE · Airbus A310222 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA03053Seat Track · damagedMAIN CABIN RT SEAT TRACK NR Y-1456 AT FRAME C63 LUGS BROKEN OUT. 09-11-07 REMOVED DAMAGED SECTION OF SEAT TRACK IAW A310 SRM 53-10-16. INSTALLED NEW SECTION OF SEAT TRACK AND SPLICE IAW A310 SRM 53-10-16Aug 22, 2007 · N446FE · Airbus A310222 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02155Controller · failedON CLIMB-OUT, AIRCRAFT DID NOT PRESSURIZE. BOTH FWD AND AFT REG NR 2 VALVES WERE STUCK FULL OPEN AND SHOWING AMBER ON THE ECAM. DUPLICATED PROBLEM AT GATE, REPLACED NR 2 CABIN PRESSURE CONTROLLER PER A310-200 AMM21-31-11-4, OPERATIONAL CHECK NORMAL. PREMATJun 16, 2007 · N446FE · Airbus A310222 · Cabin Pressure ControllerSDR 06FDEA04328Switch · failedNR 2 ENG REV UNLK LIGHT AND ECAM WARNING CAME ON AT FL 360, STAYED ON AFTER LANDING AND SHUTDOWN. REPEAT GRIP, FOUND THE MASTER ACTUATOR SECONDARY LOCK SWITCH RT SIDE FAILED CLOSED. REMOVED AND INSTALLED SAME REF A310-200 MM 78-31-16-4. OPS CHECKS GOOD SAMEDec 27, 2006 · N446FE · Airbus A310222 · Engine Thrust ReverserSDR 06FDEA2559Engine · unknownON INITIAL POWER-UP FOR TAKEOFF NUMBER 2 ENG WAS VERY SLOW TO ACCELERATE. TERMINATED THE TAKEOFF AT APPROXIMATELY 20 KTS AND CLEARED THE RUNWAY. TAXI'D BACK TO RUNWAY HELD THE BRAKES AND PUT NR 1 ENG TO 40 PERCENT N1. THE INDEX POINTER ON THE NR 1 THROTTLE Jul 13, 2006 · N446FE · Airbus A310222 · Engine (Turbine/Turboprop)SDR 05FDEA01850Wire · brokenABORTED TAKEOFF DUE TO ENG NR 2 FAILED TO STABILIZE AT 40 PERCENT POWER, WITH NR 1 ENG THROTTLE SET NORMALLY TO PRODUCE 40 PERCENT N1 THE NR 2 THROTTLE WAS THREE KNOB WIDTHS AHEAD AND STILL ONLY PRODUCING 25 PERCENT N1. FOUND WIRE BROKEN INSIDE RING TERMINAL.Jul 7, 2005 · N446FE · Airbus A310222 · Power LeverSDR 05FDEA01044Terminal Block · looseON CLIMB-OUT, NOTICED NR 2 EGT NEEDLE/ANALOGUE GAUGE FLUCTATING-RECEIVED ECAM FOR NR 2 ENG OVERLIMITS. PULLED POWER BACK. GAUGE STABILIZED THEN STARTED TO FLUCTUATE AGAIN. RAN QRH, DECIDED TO RETURN. BURNED DOWN FUEL TO MAX LNBW. NORMAL LANDING, TAXI IN.Apr 17, 2005 · N446FE · Airbus A310222 · Turbine Engine System WiringSDR 05FDEA00998Arm · gougedNR 7 RUDDER HINGE ATTACHMENT BRACE ( A-FRAME) HAS GOUGE MARKS AND WEAR MARKS AT ATTACHMENT BOLT. REMOVED AND REPLACED NR 7 HINGE ARM IAW A310-200 AMM 55-36-47-4-01 AND 27-21-21-4-01.Apr 14, 2005 · N446FE · Airbus A310 · Rudder Miscellaneous StructureSDR 05FDEA00603Structure · corrodedCORROSION FOUND UNDER THE NR 9 LATCH ROLLER FOR FWD CARGO DOOR. COMPLIED WITH EA 6-5310-86132.Mar 18, 2005 · N446FE · Airbus A310222 · Cargo/Baggage DoorsSDR 05FDEA00602Skin · crackedLEFT WING T/E BOTTOM SKIN HAS INDICATION OF CRACK ON I/B CORNER SIDE CUTOUT PANEL 581AB AS MARKED. COMPLIED WITH EA 6-5710-86028.Mar 18, 2005 · N446FE · Airbus A310222 · Wing, Plate/SkinSDR 05FDEA00574Skin · corrodedCORR B/T STR 34-35 FROM FS 39 AFT APPROX 8 IN LT REF N00850. COMPLIED WITH EA 6-5315-86078.Mar 16, 2005 · N446FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 05FDEA00493Floor Support · corrodedBULK PIT FLOOR SUPPORT AT FR67 FROM 12 INCHES TO LT CTR TO 36 INCHES TO LT OF CTR, 4EA AREAS OF CORROSION EXTENDING UNDER FASTENER HEADS AS MARKED. REMOVED AND REPLACED CROSS BEAM FLOOR SUPPORT IAW 51-72-10. REMOVED 4EA AREAS OF CORROSION IAW SRM 51-74-10.Mar 10, 2005 · N446FE · Airbus A310222 · Fuselage Miscellaneous StructureSDR 05FDEA00492Rib · damagedUPON REMOVAL OF EXISTING REPAIR ON N/R N00817 ON RT ELEVATOR INBOARD T/E LWR SURFACE FOUND 2EA AREAS OF CORROSION .5 X .5 INCH 1 ON INBOARD SIDE OF REPAIR, 1 ON OUTBOARD SIDE OF REPAIR (RIB 5 AND RIB 9). REMOVED CORROSION PER A310-200 SRM 51-74-10, 1EA AREA IMar 10, 2005 · N446FE · Airbus A310222 · Elevator, Spar/RibSDR 05FDEA00439Panel · damagedRT WING PANEL 650JB HAS 4 EA ELONGATED REF N00522. REPAIRED PANEL 650JB IAW EA 6-5710-86051.Mar 8, 2005 · N446FE · Airbus A310 · Wing, Plate/SkinSDR 05FDEA00425Rib · crackedRT WING 4 IN IB OF RIB 30 L/E AREA AFT PANEL LANDING IS CRACKED REF N00636. REMOVED AND REPLACED LANDING IAW SRM 51-40-21 AND 51-72-10 AND DRW A57243955.Mar 8, 2005 · N446FE · Airbus A310 · Wing, Rib/BulkheadSDR 05FDEA00447Skin · corrodedBULK PIT UNDER FLOOR AREA FS 69 STR 48 LT HAS AN AREA THAT EXTEND 2 INCHES FWD OF FS 69 OF CORROSION EXTENDING UNDER SHEAR TIE. REMOVED SHEAR TIE AND STRINGER SECTION IAW A310-200 SRM 53-10-14. INSTALLED SHEAR TIE AND STRINGER SECTION IAW A310-200 SRM 53-10-Mar 8, 2005 · N446FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 05FDEA00477Skin · corrodedBULK PIT UNDER FLOOR AREA FR69 STG48L HAS AN AREA THAT EXTEND 2" FWD OF FR 69 OF CORROSION EXTENDING UNDER SHEAR TIE. REMOVED SHEAR TIE AND STRINGER SECTION IAW A310-200 SRM 53-10-14. INSTALLED SHEAR TIE AND STRINGER SECTION IAW A310-200 SRM 53-10-14.Mar 8, 2005 · N446FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 05FDEA00453Angle · corrodedTHS ACTUATOR STRUCTURAL HOUSING HAS APPROX 12 INCH OF CORROSION (10 EA. AREAS). REMOVED CORROSION IN 10 EA AREAS ON THS ACTUATOR STRUCTURAL HOUSING. ALL AREAS WERE WITHIN LIMITS EXCEPT AREA 10 WHICH WAS OUT OF LIMITS IAW A310-200 SRM 53-10-00. REMOVED L-ANMar 8, 2005 · N446FE · Airbus A310 · Horizontal Stabilizer StructureSDR 05FDEA00452Shear Tie · corrodedBULK PIT UNDER FLOOR STG 55L FROM FS 65 TO FS 66 HAS CORROSION AND CORROSION. EXTENDS BETWEEN SPLICE ANGLE AND STG AND UNDER SHEAR TIE AT FS 66. REMOVED CORROSION IAW A310-200 SRM 51-74-10. STRINGER CORRODED BEYOND ALLOWABLE LIMITS AS PER A310-200 SRM 51-10Mar 8, 2005 · N446FE · Airbus A310 · Fuselage Internal Mounting StructureSDR 05FDEA00451Floorbeam · corrodedAFT PIT FLOOR FS 66 10 INCH TO RT OF CTR HAS A 5 INCH BY 2 INCH AREA OF CORROSION. REMOVED CORROSION PER A310-200 SRM 51-74-10. CORROSION OUT OF LIMITS PER SRM 51-10-00. REMOVED CORRODED FLOORBEAM AND INSTALLED NEW BEAM PER A310-200 SRM 51-72-10. REPROTECTMar 8, 2005 · N446FE · Airbus A310 · Fuselage Main, Floor BeamSDR 05FDEA00450Skin · corrodedAFT PIT UNDER FLOOR 16 INCH FWD OF FS 54.1, STG 47R HAS CORROSION. REMOVED CORROSION IAW A310-200 SRM 51-74-10. AREA WAS OUT OF LIMITS IAW A310-200 SRM 53-10-00. REMOVED AND REPLACED DAMAGED AREA IAW A310-200 SRM 53-10-14. TREATED, PRIMED, TOPCOATED IAW A3Mar 8, 2005 · N446FE · Airbus A310 · Fuselage Main, Plate/SkinSDR 05FDEA00449Shear Tie · corrodedBULK PIT UNDER FLOOR STG 53R FROM 1 INCH FWD OF 66 TO FR 67 HAS CORROSION EXTENDING UNDER SHEAR TIE AT FR 66 AND EXTENDING UNDER FASTENERS IN SEVERAL AREAS. REMOVED CORROSION, CHECK LIMITS MAT'L LOSS EXCEEDED LIMITS IAW A310-200 SRM 53-10-00 FIG 104. REMOVEMar 8, 2005 · N446FE · Airbus A310 · Fuselage Internal Mounting StructureSDR 05FDEA00448Structure · corrodedAFT PIT UNDER FLOOR FROM 12 INCH FWD OF FS 59 TO 3 INCHES FWD OF FS 59 STG44L HAS CORROSION. REMOVED CORROSION IAW A310-200 SRM 51-74-10. THE AREA WAS FOUND OUT OF LIMITS IAW A310-200 SRM 53-10-00. REPAIRED STRINGER IAW A310-200 SRM 53-10-14. TREATED, PRIMEMar 8, 2005 · N446FE · Airbus A310 · Fuselage Main, StructureSDR 05FDEA00443Flap Track · corrodedRT WING FLAP O/B UPPER SURFACE AT NR 3 FLAP TRACK AND NR 4 FLAP TRACK HAS 2 EA AREAS OF NOTED CORROSION REF N00771. REMOVED CORR IAW SRM 51-74-10, FOUND IN LIMITS IAW SRM 57-53-12.Mar 8, 2005 · N446FE · Airbus A310 · Trailing Edge FlapsSDR 05FDEA00442Skin · puncturedRT WING I/B FLAP UPPER SURFACE 3.9 IN FROM T/E AND 30 IN FROM I/B END SKIN PUNCTURED REF N00914. REPAIRED FLAP IAW SRM 57-52-12 FIG 4D.Mar 8, 2005 · N446FE · Airbus A310 · Trailing Edge FlapsSDR 05FDEA00441Attach Fitting · corrodedVERTICAL STAB UPPER EDGE LEFT AND RIGHT FORE TO AFT HAS CORROSION AROUND CAP ATTACH FASTENER HOLES REF N00734. REMOVED AND REPLACED RT CHORD IAW SRM 51-40-21 AND DRW A55371360 AND REPAIRED LT CHORD IAW SRM 51-74-40 FIG 201Mar 8, 2005 · N446FE · Airbus A310 · Vertical Stabilizer, Attach FittingsSDR 05FDEA00440Doubler · damagedREPAIR ON RT ELEVATOR I/B T/E LOWER SURFACE REQUIRES EVALUATION REF N00817. REMOVED EXISTING REPAIR AND INSTALLED CORRECT REPAIR IAW SRM 55-21-11 CONF 1 FIG 203 AND EA 6-5510-86111.Mar 8, 2005 · N446FE · Airbus A310 · Elevator, Plate/SkinSDR 05FDEA00438Panel · damagedRT WING PANEL 650KB HAS 4 EA ELONGATED HOLES REF N00521. REPAIRED PANEL IAW EA 6-5710-86051.Mar 8, 2005 · N446FE · Airbus A310 · Wing, Plate/SkinSDR 05FDEA00437Panel · damagedLT WING PANEL 550HB HAS 2 EA ELONGATED HOLES REF N00520. REPAIRED HOLES IAW EA 6-5710-85051.Mar 8, 2005 · N446FE · Airbus A310 · Wing, Plate/SkinSDR 05FDEA00436Panel · damagedRT WING PANEL 650HB HAS 3 EA ELONGATED HOLES REF N00523. REPAIRED PANEL 650HB IAW EA 6-5710-86051.Mar 8, 2005 · N446FE · Airbus A310 · Wing, Plate/SkinSDR 05FDEA00426Rib · crackedRT WING L/E UPPER SIDE OF PANEL LANDING, LANDING FOR PANEL HAS 2 EA CRACKS AT 11 IN I/B OF RIB 14 AND 11 IN O/B OF RIB 14 REF N00631. REMOVED AND REPLACED PANEL LANDING IAW SRM 51-40-21 AND DRW A57244165.Mar 8, 2005 · N446FE · Airbus A310 · Wing, Rib/BulkheadSDR 05FDEA00424Door · damagedNOSE LANDING GEAR DOORS HAS STRUCTURAL DAMAGE REF N00748. REPAIRED RT GEAR DOORS IAW SRM 52-82-11 C1 FIG 201.Mar 8, 2005 · N446FE · Airbus A310 · Landing Gear DoorsSDR 05FDEA00423Skin · crackedRT WING T/E SKIN HAS A .4 CRACK ON IB CORNER OF CUTOUT FOR PANEL 681 AB REF N00265. REPAIRED SKIN IAW EA 6-5710-86028.Mar 8, 2005 · N446FE · Airbus A310 · Wing, Plate/SkinSDR 05FDEA00422Skin · damagedREPAIR FUSELAGE AT LT ELEVATOR T/E AFT FROM OB END HAS NO DATA REF N00806. REMOVED AND INSTALLED CORRECT REPAIR IAW EA 6-5100-87090 REF A310 SRM 55-21-11, REPAIR NR 5 G.Mar 8, 2005 · N446FE · Airbus A310 · Elevator, Plate/SkinSDR 05FDEA00421Seat Track · corrodedNR 4 SEAT TRACK LT OF CENTER FROM FS 16 TO FS 18 HAS CORROSION REF N00519. REMOVED AND REPLACED SEAT TRACK FROM FS 16 TO FS 18 IAW SRM 51-40-21 AND EA 6-5310-86038.Mar 8, 2005 · N446FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA00420Seat Track · corrodedMDC NR 4 SEAT TRACK RT OF CENTER AT FR19 ON I/B SPLICE HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED SPLICE ANGLE AT FR19 IAW SRM 51-40-21.Mar 8, 2005 · N446FE · Airbus A310222 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA00419Plate · corrodedBULK CARGO DOOR CUTOUT ON LWR FWD TOP EDGE OF SCUFF PLATE SURFACE CORROSION. REMOVED SCUFF PLATE AND REMOVED CORROSION IAW SRM 51-74-10 FOUND IN LIMITS IAW SRM 53-10-00. RESTORED FINISH AND REINSTALLED SCUFF PLATE IAW SRM 53-10-18-4.Mar 8, 2005 · N446FE · Airbus A310222 · Fuselage Miscellaneous StructureSDR 05FDEA00418Panel · crackedUPON REMOVAL OF LANDING AT RT WING HINGE PANEL ON L/E FOUND PANEL LANDING CRACKED REF N00915. REMOVED AND REPLACED PANEL LANDING IAW SRM 51-40-21 AND DRW A572-434548.Mar 8, 2005 · N446FE · Airbus A310222 · Wing, Plate/Skin
Back to N446FE, cancelled Jul 29, 2013