# Service difficulty reports: N8906E, cancelled Nov 16, 1998 A list on [N8906E, cancelled Nov 16, 1998](https://openairdocs.org/deregistered/N8906E-1998-11-16.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 9806719163](https://openairdocs.org/sdr/9806719163.md): Battery Pack · discharged · Apr 16, 1998 · N8906E · Doug DC914 · Emergency Lighting > DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE IN MID CABIN. MAINTENANCE REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 9805709163](https://openairdocs.org/sdr/9805709163.md): Heat Valve · inoperative · Apr 1, 1998 · N8906E · Doug DC914 · Fuel Heater > DURING DESCENT AT 23,000 FEET, THE LEFT ENGINE FUEL HEAT VALVE FAILED TO CLOSE. OIL TEMPERATURE CLIMBED TO THE CAUTION RANGE. CREW PERFORMED A PRECAUTIONARY SHUTDOWN OF THE LEFT ENGINE. AIRCRAFT DIVERTED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENA - [SDR 9804529163](https://openairdocs.org/sdr/9804529163.md): Batteries · discharged · Mar 16, 1998 · N8906E · Doug DC914 · Emergency Lighting > DURING LINE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK OK. - [SDR 9724169163](https://openairdocs.org/sdr/9724169163.md): Power Supply · inoperative · Dec 22, 1997 · N8906E · Doug DC914 · Emergency Lighting > DURING LINE CHECK, FOUND AFT OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY. OPERATIONAL CHECK OK. - [SDR 9716779163](https://openairdocs.org/sdr/9716779163.md): Tr Unit · failed · Aug 30, 1997 · N8906E · Doug DC914 · Weather Radar System > IN CRUISE, THE RADAR BECAME OVERLY SENSITIVE IN CONTOUR MODE. FLIGHT DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED RADAR TRANSCEIVER, OPERATIONAL CHECK OK. - [SDR 9716249163](https://openairdocs.org/sdr/9716249163.md): Fuel Control · failed · Aug 25, 1997 · N8906E · Doug DC914 · Fuel Control/Turbine Engines > DURING TAKEOFF ROLL AT 70 KNOTS, THE LEFT ENGINE SPOOLED DOWN. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE LEFT ENGINE FUEL CONTROL UNIT. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. - [SDR 9715109163](https://openairdocs.org/sdr/9715109163.md): Battery · discharged · Aug 1, 1997 · N8906E · Doug DC914 · Emergency Lighting > DURING LINE CHECK, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK OK. - [SDR 9709029163](https://openairdocs.org/sdr/9709029163.md): Skin · cracked · Apr 23, 1997 · N8906E · Doug DC914 · Fuselage Main, Plate/Skin > DURING L-CHECK, FOUND CRACK IN FUSELAGE SKIN AT FS 296 BETWEEN STR 23R AND 24R. REPAIRED PER EA 91-112877. - [SDR 9709019163](https://openairdocs.org/sdr/9709019163.md): Skin · cracked · Apr 23, 1997 · N8906E · Doug DC914 · Fuselage Main, Plate/Skin > DURING L-CHECK, FOUND CRACK IN FUSELAGE SKIN AT FS 269 BETWEEN STR 23R AND 24R. REPAIRED PER EA 91-112877. - [SDR 9708039163](https://openairdocs.org/sdr/9708039163.md): Fitting · cracked · Apr 17, 1997 · N8906E · Doug DC914 · Fuselage, Stabilizer Attach Fittings > DURING L-CHECK, FOUND CRACK ON VERTICAL STABILIZER ATTACH FITTING FS 908. REPAIRED PER EA 91-112873. - [SDR 9627399163](https://openairdocs.org/sdr/9627399163.md): Start Valve · malfunctioned · Dec 30, 1996 · N8906E · Doug DC914 · Engine Start Valves/Controls > AS TAKEOFF POWER WAS APPLIED, THE RIGHT ENGINE START VALVE LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT ENGINE STARTER AND START VALVE, OPERATIONAL CHECK OK. - [SDR 9626089163](https://openairdocs.org/sdr/9626089163.md): Position Switch · malfunctioned · Dec 3, 1996 · N8906E · Doug DC914 · Landing Gear Position and Warning > ON APPROACH, GREEN LIGHT ON RIGHT MAIN GEAR DID NOT ILLUMINATE AFTER GEAR EXTENDED. RECYCLED GEAR WITH STILL NO GREEN AND NO RED INTRANSIT LIGHT. FOLLOWED COM PROCEDURE AND GREEN LIGHT ILLUMINATED. FLIGHT LANDED WITHOUT INCIDENT. REPLACED BOTH RIGHT MAIN G - [SDR 9624359163](https://openairdocs.org/sdr/9624359163.md): Windshield · cracked · Nov 13, 1996 · N8906E · Doug DC914 · Flight Compartment Windows > DURING CLIMB MSP-CVG, THE CENTER WINDSHIELD ARCED AND CRACKED. RETURNED TO MSP WITHOUT FURTHER INCIDENT. REPLACED THE CENTER WINDSHIELD AND HEAT CONTROLLER (CONTROLLER P/N 961-5059-002, S/N 3533). - [SDR 9619019163](https://openairdocs.org/sdr/9619019163.md): Wire · broken · Aug 28, 1996 · N8906E · Doug DC914 · Light System Wiring > DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE FROM ROW 2 FORWARD. FOUND WIRE MISSING BETWEEN ROWS 1 AND 2. REPLACED WIRES, OPERATIONAL CHECK OK. - [SDR 9610019163](https://openairdocs.org/sdr/9610019163.md): Skin · cracked · Apr 26, 1996 · N8906E · Doug DC914 · Fuselage Main, Plate/Skin > DURING LINE CHECK, FOUND TWO CRACKS IN THE FUSELAGE SKIN AT FS 817, LONGERON 16L, BENEATH THE PYLON ATTACH ANGLE. REPAIRED SKIN PER EA 91-105275. - [SDR 9607619163](https://openairdocs.org/sdr/9607619163.md): Uplock Roller · out of adjust · Apr 3, 1996 · N8906E · Doug DC914 · Landing Gear Position and Warning > DURING CLIMBOUT, GEAR UNSAFE LIGHT REMAINED LIT AFTER GEAR WAS RETRACTED. PERFORMED COM PROCEDURES AND CONTINUED TO ATL AT A REDUCED AIRSPEED OF 250 KNOTS. FLIGHT LANDED NORMALLY AT ATL. FOUND LEFT GEAR DOOR UPLOCK ROLLER OUT OF TOLERANCE. ADJUSTED UPLOCK - [SDR 9607359163](https://openairdocs.org/sdr/9607359163.md): Uplimit Switch · malfunctioned · Mar 31, 1996 · N8906E · Doug DC914 · Landing Gear Position and Warning > DURING CLIMBOUT, THE GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. PERFORMED GEAR UPLATCH CHECK AND THE LIGHT EXTINGUISHED, RECYCLED GEAR AND THE LIGHT AGAIN REMAINED ON. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN LANDING GEA - [SDR 9600569163](https://openairdocs.org/sdr/9600569163.md): Nav Receiver · malfunctioned · Jan 9, 1996 · N8906E · Doug DC914 · Visual Omnirange (VOR) System > CAPTAIN'S NAV RECEIVER FAILED SHORTLY AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED NR 1 NAV RECEIVER. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. - [SDR 9521259163](https://openairdocs.org/sdr/9521259163.md): Battery Pack · discharged · Dec 19, 1995 · N8906E · Doug DC914 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD SECTION OF FLOOR PROXIMITY EMERGENCY LIGHTING INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK NORMAL. - [SDR 9520449163](https://openairdocs.org/sdr/9520449163.md): Battery Pack · discharged · Dec 13, 1995 · N8906E · Doug DC914 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD SECTION OF EMERGENCY FLOOR PROXIMITY LIGHTS INOPERATIVE. REPLACED BATTERY PACK POWER SUPPLY. OPERATIONAL CHECK OK. - [SDR 9513269163](https://openairdocs.org/sdr/9513269163.md): Skin · cracked · Aug 25, 1995 · N8906E · Doug DC914 · Fuselage Main, Plate/Skin > DURING H-CHECK, FOUND TWO CRACKS IN THE FUSELAGE SKIN AT THE MAIN CABIN DOOR CUTOUT FS 200 BETWEEN LONGERONS 12L - 14L. REPAIRED SKIN PER EA 91-102773. - [SDR 9513259163](https://openairdocs.org/sdr/9513259163.md): Spar Web · cracked · Aug 25, 1995 · N8906E · Doug DC914 · Wing Spar > DURING H-CHECK, FOUND A CRACK IN THE RIGHT WING AFT SPAR WEB AT THE NR 2 STOP HINGE, LOWER INBOARD ATTACH STUD. REPAIRED PER EA 91-97631. - [SDR 9513349163](https://openairdocs.org/sdr/9513349163.md): Skin · cracked · Aug 24, 1995 · N8906E · Doug DC914 · Fuselage Main, Plate/Skin > DURING H-CHECK, FOUND FUSELAGE SKIN CRACKED AT FS 585, 623 AND 642 BETWEEN LONGERONS 1R AND 2R AT FASTENERS IN FRAME CLIP. FABRICATED AND INSTALLED DOUBLER PER EA 91-097634. - [SDR 9513339163](https://openairdocs.org/sdr/9513339163.md): Bulkhead · corroded · Aug 24, 1995 · N8906E · Doug DC914 · Fuselage Main, Bulkhead > DURING H-CHECK, FOUND AFT PIT FORWARD BULKHEAD LOWER CHORD CORRODED IN SEVERAL AREAS AT FS 642 BETWEEN LONGERONS 28L AND 28R. SPLICED IN NEW SECTION OF T-CHORD PER EA 91-097635. - [SDR 9513329163](https://openairdocs.org/sdr/9513329163.md): Floorbeam · corroded · Aug 24, 1995 · N8906E · Doug DC914 · Fuselage Main, Floor Beam > DURING H-CHECK, FOUND FLOORBEAM AT LEFT LAVATORY CORRODED AT FS 817. REPAIRED PER EA 91-102775. - [SDR 9513319163](https://openairdocs.org/sdr/9513319163.md): Skin · cracked · Aug 23, 1995 · N8906E · Doug DC914 · Fuselage Main, Plate/Skin > DURING H-CHECK, FOUND FUSELAGE SKIN AT AFT SIDE OF FORWARD ENTRY DOOR CRACKED AT THIRD AND FOURTH DOOR STOPS. ACCOMPLISHED TEMPORARY REPAIR PER EA 91-102773. - [SDR 9513039163](https://openairdocs.org/sdr/9513039163.md): Skin · cracked · Aug 22, 1995 · N8906E · Doug DC914 · Fuselage Main, Plate/Skin > DURING H-CHECK, FOUND THREE SKIN CRACKS AT FS 585, FS 623 AND FS 642. REPAIRED PER EA 91-097634 SEC 1 AND SEC 2, PERMANENT REPAIR WILL BE ACCOMPLISHED IN ONE YEAR FROM 24 AUG 95. - [SDR 9513029163](https://openairdocs.org/sdr/9513029163.md): Bulkhead · cracked · Aug 22, 1995 · N8906E · Doug DC914 · Fuselage Main, Bulkhead > DURING H-CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AROUND PERIMETER OF PLUG DOOR OPENING. STOP DRILLED CRACK AT LOWER LEFT RADIAL NR 16. REPAIRED RIGHT UPPER RADIAL PER SB 53-127. - [SDR 9512969163](https://openairdocs.org/sdr/9512969163.md): Door Flange · cracked · Aug 19, 1995 · N8906E · Doug DC914 · Emergency Exits > DURING H-CHECK, FOUND LEFT OVERWING EMERGENCY EXIT DOOR CRACKED AT AFT LOCKING PIN FLANGE. REPAIRED CRACK PER SRM 52-05 FIG 51 VIEW H. PERMANENT REPAIR WILL BE ACCOMPLISHED AT NEXT PERIODIC CHECK. - [SDR 9507269163](https://openairdocs.org/sdr/9507269163.md): Handle · out of adjust · Apr 28, 1995 · N8906E · Doug DC914 · Aerodynamic Fairings > DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL BOTH THE INTERIOR AND EXTERIOR HANDLES FROM THE CLIPS. ALSO, FOUND THAT THE TAILCONE DID NOT DROP USING THE INTERIOR HANDLE. ADJUSTED BOTH THE CLIPS AND THE LATCHES. CHECKED OK. - [SDR 9506099163](https://openairdocs.org/sdr/9506099163.md): Te Panel · cracked · Apr 11, 1995 · N8906E · Doug DC914 · Trailing Edge Flaps > DURING LINE CHECK, FOUND THAT THE RIGHT SIDE TRIPLE SLOTTED FLAP ARM BECAME DISCONNECTED RESULTING IN A 5 INCH CRACK IN THE TRAILING EDGE PANEL XEF 111.250, 2 FEET FORWARD OF THE TRAILING EDGE. ALSO, FOUND A CRACK IN THE -12R ANGLE. REPLACED PANEL AND REPAIR - [SDR 9501119163](https://openairdocs.org/sdr/9501119163.md): Voltage Reg · malfunctioned · Jan 14, 1995 · N8906E · Doug DC914 · AC Regulator > LEFT ENGINE GENERATOR DROPPED OFF LINE DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. FOUND VOLTAGE REGULATOR FAULT SET ON LEFT GENERATOR CONTROL UNIT. REPLACED THE LEFT VOLTAGE REGULATOR. 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 = 'N8906E' AND deregistration_id = 'N8906E-1998-11-16' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N8906E-1998-11-16/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.