N412FE, cancelled Apr 25, 2013

Service difficulty reports · 34

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 = 'N412FE' AND deregistration_id = 'N412FE-2013-04-25'
  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 07FDEA04967Switch · failedRECEIVED AN AUDIBLE "TOO LOW-GEAR" WNG ON SHORT FINAL. ALL GEAR INDS SHOWED GREEN/DOWN, SWITCHED TO POS1, REATTEMPT LANDING ALL SYS WORK NORMAL. ACN RELEASED FOR SVC. BRIEF INCREASED ALTITUDE AND TERRAIN AWARENESS." R&R MICROSWITCH 79GB IN REF TO MM 32-Nov 29, 2007 · N412FE · Airbus A310 · Landing Gear Position and WarningSDR 07FDEA00908Skin · corrodedAVIONICS BAY, CORROSION BELOW FRAME 17 AT STR 44L REPAIRED IAW EA 6-5330-107691.Mar 15, 2007 · N412FE · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA00905Floorbeam · misrepairedMDCC - FLOORBEAM FRAME 36 CRACKED (PREVIOUS REPAIR NOT PER SRM). REWORKED PREVIOUS REPAIR IAW EA 6-5321-29042.Mar 15, 2007 · N412FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 07FDEA00902Skin · corrodedAVIONICS BAY CORROSION AROUND FASTENERS FS 16 TO 17, STR 44L TO 45L REPAIRED PER EA 6-5330-107691.Mar 15, 2007 · N412FE · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA00889Skin · corrodedFOUND CORROSION EXIST AT AVIONIC COMPARTMENT AT STA 1315/FR 16 AND 17 STGR 46 ON FUSELAGE SKIN TOTAL 2 BY 2 INCHES BELOW ACCESS PNL 121 PF ZONE 120 COMPLIED WITH FEDEX EA 6-5330-107691.Mar 15, 2007 · N412FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 07FDEA00884Unknown · corrodedFOUND CORROSION EXIST AT AVIONICS COMPARTMENT STA 1315/ FR 17 STGR 45 LT 2' BY 2' INCHES BELOW ACCESS PNL 121 PF ZONE 120 COMPLIED WITH EA 6-5330-107691.Mar 15, 2007 · N412FE · Airbus A310203 · Fuselage Structure (General)SDR 07FDEA00881Frame · corrodedFOUND CORROSION EXIST AT AVIONIC COMPARTMENT AT STA 1315/ FRAME 16 AND 17 BETWEEN S47 AND 48 BELOW ACCESS PNL 121 PF ZONE 120 COMPLIED WITH EA 6- 5330-107691.Mar 15, 2007 · N412FE · Airbus A310203 · Fuselage Main, FrameSDR 07FDEA00876Skin · crackedLT WING LOWER SKIN SURFACE HAS A CRACK OF APPROX 1 INCH LONG AT AFT END OF RIB 11, 4 INCHES AFT OF REAR SPAR, FWD INBD END OF CUTOUT FOR ACCESS PANEL 581AB. CRACK RUNS THROUGH 1 FASTENER HOLE. ACCOMPLISHED RIB 11 PERMANENT REPAIR IAW FED EX EA 6-5710-107675 Mar 15, 2007 · N412FE · Airbus A310203 · Wing, Plate/SkinSDR 07FDEA00873Floorbeam · crackedFOUND CRACK FR 38 PROFILE MDCC FLOORBEAM LT FWD CARGO COMPARTMENT BETWEEN SEAT TRACKS L-4 & L-5, REF SRM 53-10-00 AND SRM 53-10-15. REPAIRED FR 38 MDCC FLOORBEAM BETWEEN SEATRACKS L-4 AND L-5 IAW A310-200 SRM 53-10-15, FIG 201, SHT 6A.Mar 15, 2007 · N412FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 07FDEA00845Floorbeam · misrepairedPREVIOUS REPAIR ON CABIN FLOORBEAM FRAME 37 REPAIR ANGLES IMPROPERLY INSTALLED. CORRECTED REPAIR IAW EA 6-5310-107701.Mar 14, 2007 · N412FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 07FDEA00844Ferrule · crackedNR 1 PYLON PRECOOLER FERRULE PAN CRACKED BETWEEN RIBS 4 AND 8. ACCOMPLISHED PERMANENT REPAIR IAW SB A310-54-2028.Mar 14, 2007 · N412FE · Airbus A310203 · Nacelle/Pylon, Main FrameSDR 07FDEA00843Skin · corrodedAVIONICS BAY HAD A 2.5" BY 1.5" AREA OF CORROSION BETWEEN FRAMES 17 AND 18 AND STRINGERS 50L AND 51L. CORROSION OUT OF LIMITS. COMPLIED WITH EA 6-5330-107691.Mar 14, 2007 · N412FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 07FDEA00842Skin · corrodedAVIONICS BAY SKIN FWD OF FRAME 17 BETWEEN STRINGERS 48L AND 50L HAS 5" BY 5" AREA OF CORROSION AREA OUT OF LIMITS. COMPLIED WITH EA 6-5330-107691.Mar 14, 2007 · N412FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 07FDEA00803Seat Track · gougedMDCC SEAT TRACK 3L GOUGED CUT OUT AND REPLACED GOUGED SECTION OF SEAT TRACK. MAJOR REPAIR IAW FEDEX GMM 6-2-100.Mar 13, 2007 · N412FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00802Seat Track · gougedMDCC SEAT TRACK 5L GOUGED BLENDED GOUGES IAW A310-200 SRM 51-74-10. FOUND TO BE IN LIMITS. MAJOR REPAIR IAW FEDEX GMM 6-2-100.Mar 13, 2007 · N412FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03547Warning Light · false activationSOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO DOOR NOT CLOSED. AFT CARGO SW FAULT AND AN AMBER DOOR LIGHT FOR AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE IAW MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 05NOV05 MEL 52-71-01: AFT DOOR CLOSED AND LOCKED INDICAOct 27, 2005 · N412FE · Airbus A310203 · Door Warning SystemSDR 05FDEA03546Warning Light · false activationSOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO NOT CLOSED AFT CRAGO SW FAULT AND AN AMBER DOOR LIGHT FOR AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 05NOV05 "MEL 52-71-01: (IDENTIFY) AFT DOOR CLOSED AND LOCKED Oct 27, 2005 · N412FE · Airbus A310203 · Door Warning SystemSDR 05FDEA03505Door · malfunctionedSOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO NOT CLOSED AFT CARGO SW FAULT AND AN AMBER DOOR LIGHT FO R AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 05NOV05 MEL 52-71-01: AFT DOOR CLOSED AND LOCKED INDICATIOOct 26, 2005 · N412FE · Airbus A310 · Cargo/Baggage DoorsSDR 04FDEA02835Panel · damagedPANEL LAND 650KB HAS 6EA ELONGATED HOLES (RT WING). REPAIRED HOLES IAW EA 6-5710-81998 AND A310 SRM 51-40-44 FIG 1.Sep 28, 2004 · N412FE · Airbus A310 · Wing, Plate/SkinSDR 04FDEA02834Panel · damagedPANEL LAND 550JB HAS 1EA ELONGATED HOLE (LT WING). REPAIRED HOLE IAW EA 6-5710-81998.Sep 28, 2004 · N412FE · Airbus A310 · Wing, Plate/SkinSDR 04FDEA02833Panel · damagedPANEL LAND 650JB HAS 2EA ELONGATED HOLES. REPAIRED 2EA ELONGATED HOLES IAW EA 6-5710-81998Sep 28, 2004 · N412FE · Airbus A310 · Wing, Plate/SkinSDR 04FDEA02441Seat Track · corrodedMAIN CABIN CARGO FLOOR 3 AREAS OF CORROSION ON SEAT TRACKS AT FR66 AND FR67 ZONE 251 TRACK F. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW SRM 53-10-16Aug 11, 2004 · N412FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02440Pylon · crackedNR 1 ENGINE AFT UPPER PYLON HAS CRACKED UNDER PNL 473CL. STOP DRILLED CRACK AND INSTALLED U-CHANNEL IAW A310/200 SRM 54-50-00 AND 54-54-11 FIG 201 AND 54-54-51 FIG 206 BETWEEN PYLON STA 1059 AND STA 1115.Aug 11, 2004 · N412FE · Airbus A310203 · Nacelle/Pylon StructureSDR 04FDEA02439Seat Track · corrodedMDC ON RT SEAT TRACK NR 3 FR53 NOTED CORROSION INSIDE SCALLOP HOLES AND ON FLANGE. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW A310/200 SRM 53-10-16.Aug 11, 2004 · N412FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02438Dummy Rail · corrodedUPPER MAIN CABIN FR48 BETWEEN TRACK D & E HAS 1EA DUMMY TRACK WITH CORROSION BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED DUMMY TRACK IAW A310 SRM 51-72-10.Aug 11, 2004 · N412FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 04FDEA02437Dummy Rail · corrodedUPPER MAIN CABIN BETWEEN D & E HAS 3EA DUMMY TRACK WITH CORROSION (LEVEL 2) AND 1EA DUMMY TRACK CRACKED (2 INCHES IN LENGTH) BETWEEN FR 52 AND 53. REMOVED AND REPLACED 4EA DUMMY TRACKS.Aug 11, 2004 · N412FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 04FDEA02338Tee Fitting · corrodedREF. SNRM N00243 MDCC T-CAP JUST AFT OF COCKPIT DOOR HAS LEVEL 2 CORROSION REMOVED CORROED T-CAP SECTION INSTALLED A SPLICE IN SECTION IAW A310/200 SRM 53- 12-15, 51-40-20, AND 51-75-10Aug 1, 2004 · N412FE · Airbus A310 · Fixed Inner DoorsSDR 04FDEA00389Coalescer Bag · dirtyON TAKEOFF ROLL STRONG ODOR OF OIL OR AIR CONDITIONING SMOKE IN COCKPIT, REJECTED TAKEOFF. NO SIGN OF SMOKE COMING FROM VENTS, NO SMOKE WARNINGS, ALL INDICATIONS APPEAR NORMAL, RETURNED TO RAMP. FOUND NR 1 AND NR 2 PACK WATER SEPARATOR BAGS VERY DIRTY. REMOFeb 10, 2004 · N412FE · Airbus A310 · Humidity Control SystemSDR 03FDEA02008Thrust Reverser · malfunctioned1 ENG ON T/O, N1 DID NOT REACH T/O PWR. ENG N1 90 PRCT. ENG 2 N1 100 PRCT. TRIED TO MATCH N1 BY PUSHING UP 1 THROTTLE WHICH CAUSED 1 EGT TO RISE TO CAUTION RANGE ABOUT 890, RETARDED THROTTLES AT THAT TIME ECAM WARNING HP VALVE FAULT -OFF, 1 HP VALVE SELECTDec 2, 2003 · N412FE · Airbus A310 · Engine Thrust ReverserSDR 02FDEA00384Controller · failedAIRCRAFT WOULD NOT PRESSURIZE. NR 1 FWD AND AFT OUTFLOW VALVE INDICATED FULL OPEN. PERFORMED FUNCTIONAL CHECK OF NR 1 AND NR 2 PRESSURIZATION CONTROLLERS. NR 1 SYSTEM CONTROLLER CONTINUOUSLY SHOWS THE AIRCRAFT AT AN ELEVATION OF 400 FT WHEN IT SHOULD READ AJun 8, 2002 · N412FE · Airbus A310 · Cabin Pressure ControllerSDR 02FDEA00051Light · illuminated02-51 AFTER T/O MAIN DECK DOOR LIGHT CAME ON. A/C RELEASED PER MEL 52-9.Jan 15, 2002 · N412FE · Airbus A310203 · Door Warning SystemSDR 02FDEA00009Symbol Generator · inoperativeLOST F/O'S PRIMARY FLT AND NAV DISPLAY. EFIS SGU NR 2 INOP. RELEASED PER MEL 34-7.Jan 3, 2002 · N412FE · Airbus A310203 · Integrated Flight SystemSDR 00FDEA00002Switch · failedON T/O, L/G WOULD NOT RETRACT DESPITE SEVERAL RECYCLES ON SYS 1 AND 2 C/B'S. RESET BOX AND FAULTED SAME UNITS. REMOVED AND REPLACED PROXIMITY DETECTOR UNIT PER MM. OPS CK GOOD.Jan 4, 2000 · N412FE · Airbus A310203 · Landing Gear Retraction/Extension SystemSDR 99FDEA00510Relay · failed99-293 - ON DEPT GDL, F/O PITOT HEAT FAILED, THEN NR 1 ATS TRIPPED. WOULD NOT RESET. REMOVED AND REPLACED NOSE GEAR RELAY 153GB IAW MM. ALL CK GOOD, OK FOR SERVICE.Dec 22, 1999 · N412FE · Airbus A310203 · Pitot/Static Anti-Ice System
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