# Service difficulty reports: N8912E, cancelled Aug 6, 2013 A list on [N8912E, cancelled Aug 6, 2013](https://openairdocs.org/deregistered/N8912E-2013-08-06.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 0401939153](https://openairdocs.org/sdr/0401939153.md): Pulley · worn · Oct 26, 2004 · N8912E · Doug DC914 · Trailing Edge Flap Control System > ON 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 FO - [SDR 0302039153](https://openairdocs.org/sdr/0302039153.md): Rib · cracked · Sep 27, 2003 · N8912E · Doug DC914 · Nacelle/Pylon, Frame/Spar/Rib > DURING L-CHECK FOUND CRACK IN PYLON CLOSING RIB AT STATION YN 165 LT. REPAIRED PER EA 91-196348. - [SDR 0301439153](https://openairdocs.org/sdr/0301439153.md): Reservoir · defective · Jul 31, 2003 · N8912E · Doug DC914 · Hydraulic Reservoir, Main > WHILE 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 H - [SDR 0204199153](https://openairdocs.org/sdr/0204199153.md): Engine · damaged · Dec 29, 2002 · N8912E · Doug DC914 · Engine (Turbine/Turboprop) > ENGINE 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. - [SDR 9803339153](https://openairdocs.org/sdr/9803339153.md): Retract Mech · lack of lube · Feb 25, 1998 · N8912E · Doug DC914 · Landing Gear Position and Warning > DURING 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 R - [SDR 9802529153](https://openairdocs.org/sdr/9802529153.md): Battery Pack · discharged · Feb 9, 1998 · N8912E · Doug DC914 · Emergency Lighting > DURING LINE CHECK, FOUND THE LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK OK. - [SDR 9718879153](https://openairdocs.org/sdr/9718879153.md): Uplock Switches · malfunctioned · Oct 7, 1997 · N8912E · Doug DC914 · Landing Gear Position and Warning > DURING 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 A - [SDR 9715789153](https://openairdocs.org/sdr/9715789153.md): Skin · cracked · Aug 8, 1997 · N8912E · Doug DC914 · Fuselage Main, Plate/Skin > DURING LINE CHECK, FOUND CRACK IN FUSELAGE SKIN AT FASTENERS FS 76, LBL 14 TO 20. REPAIRED PER EA 91-151918. - [SDR 9714739153](https://openairdocs.org/sdr/9714739153.md): Unsafe Light · illuminated · Jul 26, 1997 · N8912E · Doug DC914 · Landing Gear Position and Warning > AFTER 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. - [SDR 9714249153](https://openairdocs.org/sdr/9714249153.md): Pressure Panel · cracked · Jul 14, 1997 · N8912E · Doug DC914 · Fuselage Miscellaneous Structure > DURING 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. - [SDR 9711469153](https://openairdocs.org/sdr/9711469153.md): Engine · failed · Jun 12, 1997 · N8912E · Doug DC914 · Engine (Turbine/Turboprop) > DURING 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 - [SDR 9620529153](https://openairdocs.org/sdr/9620529153.md): Tr Unit · malfunctioned · Sep 26, 1996 · N8912E · Doug DC914 · Weather Radar System > EN ROUTE TO MEM, RADAR WOULD NOT PAINT KNOWN WEATHER. FLIGHT DIVERTED TO LIT AND LANDED WITHOUT INCIDENT. REPLACED RADAR TRANSCEIVER. OPERATIONAL CHECK OK. - [SDR 9616119153](https://openairdocs.org/sdr/9616119153.md): Battery Pack · discharged · Jul 27, 1996 · N8912E · Doug DC914 · Emergency Lighting > DURING LINE CHECK, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. - [SDR 9614089153](https://openairdocs.org/sdr/9614089153.md): Battery Pack · discharged · Jun 26, 1996 · N8912E · Doug DC914 · Emergency Lighting > DURING LINE CHECK, FOUND RIGHT ENGINE NACELLE EMERGENCY ILLUMINATION LIGHT INOPERATIVE. REPLACED RIGHT NACELLE LIGHT BATTERY PACK, OPERATIONAL CHECK OK. - [SDR 9607639153](https://openairdocs.org/sdr/9607639153.md): Light · shorted out · Apr 5, 1996 · N8912E · Doug DC914 · Emergency Lighting > DURING LINE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT EMERGENCY LIGHT INOPERATIVE. FOUND SHORT IN LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY AND OPERATIONAL CHECK GOOD. - [SDR 9602039153](https://openairdocs.org/sdr/9602039153.md): Clips · out of adjust · Jan 21, 1996 · N8912E · Doug DC914 · Aerodynamic Fairings > DURING 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 CLIPS - [SDR 9520459153](https://openairdocs.org/sdr/9520459153.md): Oxy Manifolds · malfunctioned · Dec 13, 1995 · N8912E · Doug DC914 · Passenger Oxygen System > DURING PERIODIC CHECK, MULTIPLE OXYGEN SYSTEM MANIFOLDS FAILED SYSTEM CHECK. REPLACED MANIFOLDS. OPERATIONAL CHECK OK. - [SDR 9522169153](https://openairdocs.org/sdr/9522169153.md): Skin · cracked · Dec 7, 1995 · N8912E · Doug DC914 · Fuselage Main, Plate/Skin > DURING 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. - [SDR 9519879153](https://openairdocs.org/sdr/9519879153.md): Unlock Mech · out of adjust · Dec 7, 1995 · N8912E · Doug DC914 · Emergency Exits > DURING 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. - [SDR 9519869153](https://openairdocs.org/sdr/9519869153.md): Fitting · cracked · Dec 7, 1995 · N8912E · Doug DC914 · Fuselage Miscellaneous Structure > DURING 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. - [SDR 9521529153](https://openairdocs.org/sdr/9521529153.md): Frame · cracked · Dec 4, 1995 · N8912E · Doug DC914 · Emergency Exits > DURING 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. - [SDR 9519819153](https://openairdocs.org/sdr/9519819153.md): Fitting · cracked · Dec 4, 1995 · N8912E · Doug DC914 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND A THREE INCH CRACK IN THE LONGERON 30 END FITTING AT FS 468. REPLACED FITTING PER SRM 51-30. - [SDR 9519649153](https://openairdocs.org/sdr/9519649153.md): Fitting · cracked · Dec 1, 1995 · N8912E · Doug DC914 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND A CRACK IN THE FS 237 RIGHT CUSP SPLICE FITTING. REPLACED FITTING PER SRM 51-30-1. - [SDR 9519429153](https://openairdocs.org/sdr/9519429153.md): Fitting · cracked · Nov 30, 1995 · N8912E · Doug DC914 · Fuselage Miscellaneous Structure > DURING 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. - [SDR 9516029153](https://openairdocs.org/sdr/9516029153.md): Fitting · cracked · Oct 3, 1995 · N8912E · Doug DC914 · Wing Miscellaneous Structure > DURING 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. - [SDR 9508709153](https://openairdocs.org/sdr/9508709153.md): Nav/Comm Panel · not seated · May 27, 1995 · N8912E · Doug DC914 · Automatic Direction Finder (ADF) System > LOSS 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 PRO - [SDR 9501869153](https://openairdocs.org/sdr/9501869153.md): Nav Receiver · failed · Jan 12, 1995 · N8912E · Doug DC914 · Visual Omnirange (VOR) System > NR 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. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N8912E-2013-08-06/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.