N8912E, cancelled Aug 6, 2013

Service difficulty reports · 27

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 = 'N8912E' AND deregistration_id = 'N8912E-2013-08-06'
  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 0401939153Pulley · wornON FINAL APPROACH FOR LANDING AFTER SELECTING FLAPS TO 30 DEGREES DOWN, THE CREW FELT A SLIGHT ROLL AND NOTICED THAT THE LT FLAP INDICATOR WAS AT 20 DEGREES AND THE RT FLAP INDICATOR WAS AT 30 DEGREES. CREW EXECUTED MISSED APPROACH PROCEDURES TO ALLOW TIME FOOct 26, 2004 · N8912E · Doug DC914 · Trailing Edge Flap Control SystemSDR 0302039153Rib · crackedDURING L-CHECK FOUND CRACK IN PYLON CLOSING RIB AT STATION YN 165 LT. REPAIRED PER EA 91-196348.Sep 27, 2003 · N8912E · Doug DC914 · Nacelle/Pylon, Frame/Spar/RibSDR 0301439153Reservoir · defectiveWHILE AT CRUISE, THE RIGHT HYDRAULIC PRESSURE LOW ANNUNCIATOR LIGHT ILLUMINATED. THE RIGHT HYDRAULIC PRESSURE AND HYDRAULIC QUANTITY INDICATORS WENT TO ZERO. COMPLIED WITH COM PROCEDURES AND LANDED WITH LANDING GEAR DOORS OPEN. MAINTENANCE FOUND THE RIGHT HJul 31, 2003 · N8912E · Doug DC914 · Hydraulic Reservoir, MainSDR 0204199153Engine · damagedENGINE NR 1 FAILED AND SHUTDOWN AFTER A THRUST REDUCTION AT 17,000 FEET. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND ENGINE FOD DAMAGE AND REPLACED THE ENGINE.Dec 29, 2002 · N8912E · Doug DC914 · Engine (Turbine/Turboprop)SDR 9803339153Retract Mech · lack of lubeDURING CLIMB-OUT, THE FLIGHT CREW HEARD A POPPING SOUND FROM THE NOSE LANDING GEAR AREA. THE CAPTAIN RECYCLED THE LANDING GEAR AND FOLLOWED COM PROCEDURES. AFTER RECYCLING, THE RIGHT MAIN LANDING GEAR RED ANNUNCIATOR LIGHT REMAINED ILLUMINATED. THE FLIGHT RFeb 25, 1998 · N8912E · Doug DC914 · Landing Gear Position and WarningSDR 9802529153Battery Pack · dischargedDURING LINE CHECK, FOUND THE LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK OK.Feb 9, 1998 · N8912E · Doug DC914 · Emergency LightingSDR 9718879153Uplock Switches · malfunctionedDURING CLIMB, THE LANDING GEAR HANDLE UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. TROUBLESHOT SYSTEM WITH NO DEFECTS FOUND. REPLACED RIGHT LANDING GEAR UPLOCK AND DOWNLOCK SWITCHES AOct 7, 1997 · N8912E · Doug DC914 · Landing Gear Position and WarningSDR 9715789153Skin · crackedDURING LINE CHECK, FOUND CRACK IN FUSELAGE SKIN AT FASTENERS FS 76, LBL 14 TO 20. REPAIRED PER EA 91-151918.Aug 8, 1997 · N8912E · Doug DC914 · Fuselage Main, Plate/SkinSDR 9714739153Unsafe Light · illuminatedAFTER TAKEOFF, RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED. PERFORMED COCKPIT OPERATING MANUAL PROCEDURE AND RETURNED TO DTW. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. AIRCRAFT RETURNED TO SERVICE.Jul 26, 1997 · N8912E · Doug DC914 · Landing Gear Position and WarningSDR 9714249153Pressure Panel · crackedDURING L CHECK, FOUND CRACKS IN THE NOSE WHEEL WELL HORIZONTAL PRESSURE PANEL AT THE INBOARD AND OUTBOARD VERTICAL STIFFENERS FS 110 LEFT SIDE. REPAIRED PER EA 91-113358.Jul 14, 1997 · N8912E · Doug DC914 · Fuselage Miscellaneous StructureSDR 9711469153Engine · failedDURING CRUISE FLIGHT, THE RIGHT ENGINE OIL CLOG LIGHT AND MASTER CAUTION WARNING LIGHT ILLUMINATED WITH ASSOCIATED DROPPING OF OIL PRESSURE AND QUANTITY. CREW SHUT DOWN THE RIGHT ENGINE AND DIVERTED TO DSM. MAINTENANCE REPLACED THE RIGHT ENGINE, OPERATIONAL Jun 12, 1997 · N8912E · Doug DC914 · Engine (Turbine/Turboprop)SDR 9620529153Tr Unit · malfunctionedEN ROUTE TO MEM, RADAR WOULD NOT PAINT KNOWN WEATHER. FLIGHT DIVERTED TO LIT AND LANDED WITHOUT INCIDENT. REPLACED RADAR TRANSCEIVER. OPERATIONAL CHECK OK.Sep 26, 1996 · N8912E · Doug DC914 · Weather Radar SystemSDR 9616119153Battery Pack · dischargedDURING LINE CHECK, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK.Jul 27, 1996 · N8912E · Doug DC914 · Emergency LightingSDR 9614089153Battery Pack · dischargedDURING LINE CHECK, FOUND RIGHT ENGINE NACELLE EMERGENCY ILLUMINATION LIGHT INOPERATIVE. REPLACED RIGHT NACELLE LIGHT BATTERY PACK, OPERATIONAL CHECK OK.Jun 26, 1996 · N8912E · Doug DC914 · Emergency LightingSDR 9607639153Light · shorted outDURING LINE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT EMERGENCY LIGHT INOPERATIVE. FOUND SHORT IN LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY AND OPERATIONAL CHECK GOOD.Apr 5, 1996 · N8912E · Doug DC914 · Emergency LightingSDR 9602039153Clips · out of adjustDURING EO 5350-01032 TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR RELEASE HANDLE FROM THE CLIPS AND DROP THE TAILCONE. ALSO, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERIOR RELEASE HANDLE FROM THE CLIPSJan 21, 1996 · N8912E · Doug DC914 · Aerodynamic FairingsSDR 9520459153Oxy Manifolds · malfunctionedDURING PERIODIC CHECK, MULTIPLE OXYGEN SYSTEM MANIFOLDS FAILED SYSTEM CHECK. REPLACED MANIFOLDS. OPERATIONAL CHECK OK.Dec 13, 1995 · N8912E · Doug DC914 · Passenger Oxygen SystemSDR 9522169153Skin · crackedDURING H-CHECK, FOUND A CRACK IN THE FUSELAGE SKIN AT LONGERON 19L FROM APPROXIMATELY FS 607 - 609. REPLACED SKIN (P/N 5911416-1) PER EA 91-102616.Dec 7, 1995 · N8912E · Doug DC914 · Fuselage Main, Plate/SkinSDR 9519879153Unlock Mech · out of adjustDURING H-CHECK, FOUND THAT INADQUATE FORCE WAS REQUIRED TO OPERATE THE RIGHT OVERWING EMERGENCY EXIT USING THE EXTERIOR HANDLE. RE-RIGGED THE DOOR PER MM 52-21-0-501.Dec 7, 1995 · N8912E · Doug DC914 · Emergency ExitsSDR 9519869153Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE FS 786 FITTING AT THE INBOARD CORNER OF THE LEFT LAVATORY FORWARD BULKHEAD JUST BELOW THE FLOOR LINE. REPLACED FITTING PER SRM 51-30-5.Dec 7, 1995 · N8912E · Doug DC914 · Fuselage Miscellaneous StructureSDR 9521529153Frame · crackedDURING H-CHECK, FOUND A .50 INCH CRACK IN THE RIGHT OVERWING EMERGENCY EXIT DOOR PAN BY NR 14 SUPPORT. REPAIRED FRAME (P/N 5913195-1) PER EA 91-103342.Dec 4, 1995 · N8912E · Doug DC914 · Emergency ExitsSDR 9519819153Fitting · crackedDURING H-CHECK, FOUND A THREE INCH CRACK IN THE LONGERON 30 END FITTING AT FS 468. REPLACED FITTING PER SRM 51-30.Dec 4, 1995 · N8912E · Doug DC914 · Fuselage Miscellaneous StructureSDR 9519649153Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE FS 237 RIGHT CUSP SPLICE FITTING. REPLACED FITTING PER SRM 51-30-1.Dec 1, 1995 · N8912E · Doug DC914 · Fuselage Miscellaneous StructureSDR 9519429153Fitting · crackedDURING H-CHECK, FOUND .25 INCH AND 1 INCH CRACKS IN THE VERTICAL SEAT TRACK SUPPORT FITTING FS 566. REPLACED FITTING (P/N 3916209-502), PER SRM 51-30-5.Nov 30, 1995 · N8912E · Doug DC914 · Fuselage Miscellaneous StructureSDR 9516029153Fitting · crackedDURING MAINTENANCE INSPECTION, FOUND A CRACK IN THE LOWER FOOT FITTING FS 69 BETWEEN CENTER WING STRINGERS 11 AND 12. REPLACED FITTING PER SRM 51-30-5.Oct 3, 1995 · N8912E · Doug DC914 · Wing Miscellaneous StructureSDR 9508709153Nav/Comm Panel · not seatedLOSS OF NR 1 NAV RECEIVER OCCURRED AFTER TAKEOFF. VOR/LOC FLAG WAS IN VIEW AND NO BEARING WAS AVAILABLE. PULLED AND RESET NAV CIRCUIT BREAKER WITH NO HELP. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND NR 1 NAV/COMM CONTROL PANEL NOT SEATED PROMay 27, 1995 · N8912E · Doug DC914 · Automatic Direction Finder (ADF) SystemSDR 9501869153Nav Receiver · failedNR 1 VOR FAILED ON APPROACH INTO DTW. FLIGHT DIVERTED TO CMH AND LANDED WITHOUT INCIDENT. REPLACED NR 1 NAV/COMM CONTROL PANEL AND NR 1 NAV RECEIVER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.Jan 12, 1995 · N8912E · Doug DC914 · Visual Omnirange (VOR) System
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