# N118SD: Saab-Scania SF340A, registration cancelled 2007-01-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 5, 2007 - Exported to: Sweden - Status when cancelled: Triennial form not returned - Airframe: [Saab-Scania SF340A](https://openairdocs.org/model/saab-scania-sf340a) (registry code 7860100) - Engine: [GE CT7-SER series](https://openairdocs.org/engine/ge-ct7-ser-series) (registry code 30031) - Serial number: 340A-118 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: July 28, 1988 - Certificate issued: May 12, 1988 - Last registry action: December 19, 2005 - Mode S code: A04B7F - Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N118SD - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=118SD - Page: https://openairdocs.org/deregistered/N118SD-2007-01-05 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Saab-Scania SF340A: https://openairdocs.org/model/saab-scania-sf340a.md ## Service difficulty reports (15) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR NSVA200600101](https://openairdocs.org/sdr/NSVA200600101), Jul 9, 2006: PERISEAL. FOD. ON TAKE-OFF RT ITT REACHED 933 DEGREES, 96 PERCENT SET MANUALLY ON POWER NO CTOT. REPLACED FWD AND AFT PERI-SEALS IAW 36-11-40, INSPECTED FOR FOD, PERFORMED ITT - [SDR NSVA200600086](https://openairdocs.org/sdr/NSVA200600086), Jun 21, 2006: ENGINE. OVERHEATED. DURING TAKEOFF ROLL, RIGHT ENGINE REACHED 934 DEGREES CELSUIS TAKEOFF ABORTED. INSPECTED RT ENGINE FOR FOD DAMAGE, NO DAMAGED NOTED AT THIS TIME. THIS A/C HAS B - [SDR NSVA200600070](https://openairdocs.org/sdr/NSVA200600070), Jun 9, 2006: ITT TRIMMER. MALFUNCTIONED. ON TAKEOFF RT ENGINE ITT REACHED 950 DEGREES WITH CTOT AT 98 SET AND ARMED. R&R RT ENGINE TRIMMER, OPS CHECK GOOD. - [SDR 05312006A](https://openairdocs.org/sdr/05312006A), May 28, 2006: WIRE HARNESS. DEFECTIVE. RIGHT ENGINE OVERTEMP LIGHT ON. ITT APPROX 960 DEGREES FOR LESS THAN 2 SECONDS. R&R RT ENGINE WIRE HARNESS PN ON/OFF 7292533-503, SN ON/OFF NSN OPS CHECK GOOD. - [SDR SF200510201](https://openairdocs.org/sdr/SF200510201), Oct 20, 2005: ODOR. DETECTED. FLT 9003 FWA-DAY FOUL ODOR IN COCKPIT & FWD GALLEY AREA. - [SDR 166921](https://openairdocs.org/sdr/166921), Mar 31, 2005: CONTROL MODULE. MALFUNCTIONED. NO NOSE WHEEL DOWN AND LOCKED INDICATION WHEN SELECTED IN THE DOWN AND LOCKED POSITION. REMOVED AND REPLACED LANDING GEAR CONTROL ASSEMBLY. - [SDR 243781](https://openairdocs.org/sdr/243781), Jan 16, 2005: CTOT PANEL. MALFUNCTIONED. LEFT ENGINE TORQUE MOMENTARILY DROPPED ON CLIMB-OUT WITH CTOT ON. AIRCRAFT RETURNED TO FIELD AND MTX DETERMINED THAT THE TORQUE DROP ONLY OCCURS WITH CTOT ENGAG - [SDR 243733](https://openairdocs.org/sdr/243733), Jan 13, 2005: ECU. FAILED. LEFT ENGINE ERRATIC TQ FLUXUATES, ENGINE OVERTEMPS MULTIPLE TIMES. ENGINE SHUT DOWN MANUALLY. REMOVED AND REPLACED ECU, IAW GE CT7 M/M 74-00-00, GROUND RAN 45 M - [SDR 101171](https://openairdocs.org/sdr/101171), Feb 18, 2004: BOOT. MALFUNCTIONED. THE AIRCRAFT ENTERED ICING CONDITIONS AIRCREW SELECTED WING AND EMPENAGE DE-ICING. TIMER LIGHT ILLUMINATED IN SINGLE CYCLE, AIRCREW SELECTED CONTINUOUS CYCLE AN - [SDR 181161](https://openairdocs.org/sdr/181161), Jan 28, 2004: INDICATOR. ERRATIC. ON 01-28-04, APPROX 1535 (UTC), FLT 4501 PIT-LEX, AIRCRAFT RETURN TO FIELD WHEN THE CAPTAIN'S AIRSPEED INDICATOR HAS ERRATIC READING ALONG WITH THE RUDDER LIMIT - [SDR 180131](https://openairdocs.org/sdr/180131), Sep 17, 2003: MOTOR. INOPERATIVE. FLT 4588 PIT-IPT. DURING CLIMB OUT AND DESCENT FLIGHT CREW NOTICED THAT THE MAIN ELEVATOR WARNING LIGHT WAS ILLUMINATED. THE CREW FOLLOWED THE QRH AND DISCONNEC - [SDR 127461](https://openairdocs.org/sdr/127461), Jul 16, 2003: TILLER. MALFUNCTIONED. FLIGHT 4515 TTN-BED. DURING T/O ROLL AT ABOUT 60 KNOTS AFTER RELEASING THE NOSE STEER TILLER, THE A/C TURNED TO THE RIGHT. THE CREW CORRECTED WITH THE TILLER TO - [SDR 2003F00134](https://openairdocs.org/sdr/2003F00134), Nov 25, 2002: INDICATOR. MALFUNCTIONED. FLT 4480 - PIT-TOL - AIRCRAFT RETURNED TO GATE, CO-PILOTS AHARS FLAGGED / EADI 25 DEGREES PITCH DOWN AND 10 DEGREES LEFT, EHSI COMPASS SLEWS CLOCKWISE, NORMAL A - [SDR 2003F00133](https://openairdocs.org/sdr/2003F00133), Nov 25, 2002: PUMP. INTERMITTENT. FLT 4480 - PIT-TOL, ON TAXI OUT, AIRCRAFT RETURNED TO GATE, HYDRAULIC PUMP INTERMITTENT IN AUTO AND OVERRIDE. FIRST OF TWO SQUAWKS THIS FLIGHT. (M) - [SDR 2003F00081](https://openairdocs.org/sdr/2003F00081), Oct 31, 2002: STRUT. LOW. ON CLIMB-OUT FROM FWA, COULD NOT RETRACT LANDING GEAR WITHOUT DEPRESSING DOWN LOCK RELEASE. UPON BRINGING CONDITION LEVERS BACK IN CLIMB, CONFIG WARNING HORN SO ## Other aircraft with N118SD - [Registered now](https://openairdocs.org/aircraft/N118SD): Bell OH-58, S/N 72-21285 --- 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.