# N235AE: Saab-Scania SAAB 340B, registration cancelled 2013-08-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 23, 2013 - Status when cancelled: Sale reported, canceled - Airframe: [Saab-Scania SAAB 340B](https://openairdocs.org/model/saab-scania-saab-340b) (registry code 7860101) - Engine: [GE CT7-SER series](https://openairdocs.org/engine/ge-ct7-ser-series) (registry code 30031) - Data sheets: [TCDS A52EU](https://openairdocs.org/tcds/A52EU) (OpenAirDocs) - Serial number: 340B-235 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Special flight permit - Airworthiness date: April 23, 1991 - Last registry action: June 2, 2008 - Mode S code: A21B18 - Location: [Mansfield, TX](https://openairdocs.org/faa-place/TX/Mansfield) - Owner type: Individual - Owner's area on the map: 32.5707° N, 97.1448° W: Placed by OpenAirDocs at the center of ZIP code 76063, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N235AE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=235AE - Page: https://openairdocs.org/deregistered/N235AE-2013-08-23 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 SAAB 340B: https://openairdocs.org/model/saab-scania-saab-340b.md ## Service difficulty reports (18) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SIMA200505901](https://openairdocs.org/sdr/SIMA200505901), Feb 25, 2005: POWER SUPPLY. INOPERATIVE. DFW - FLT 3219 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT SEATS 8A AND 7B TO 8B TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY B - [SDR SIMA200436601](https://openairdocs.org/sdr/SIMA200436601), Dec 28, 2004: POWER SUPPLY. DISCHARGED. CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE AT ROWS 8,9, AND 10. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY POWER SUPPLY UNIT IAW MM. OPERATIO - [SDR SIMA200426908](https://openairdocs.org/sdr/SIMA200426908), Sep 22, 2004: GENERATOR. INOPERATIVE. AS AIRCRAFT WAS TAXIING IN MAINTENANCE PERSONNEL WHO WERE ON THE RAMP NOTED FLAME COMING OUT OF LT ENGINE GENERATOR VENT. CREW BLEW THE FIRE BOTTLES TO EXTINGUI - [SDR SIMA200313902](https://openairdocs.org/sdr/SIMA200313902), May 16, 2003: B-NUT. DAMAGED. DURNIG TAXI IN ARICRAFT, LOST HYDRAULIC POWER. MAINTENANCE FOUND A BAD B-NUT ON THE NR 4 BRAKE LINE. LINE AND B-NUT WERE REPLACED IAW SAAB MM. LEAK CHECK WAS GO - [SDR SIMA200129004](https://openairdocs.org/sdr/SIMA200129004), Oct 11, 2001: LIGHT. INOPERATIVE. FOUND FLOOR EMERGENCY EXIT LIGHT OUT AT 10B. REMOVED AND REPLACED LIGHT ASSEMBLY AT 10B IAW SAAB 340 AMM. OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RETURNED T - [SDR SIMA200125301](https://openairdocs.org/sdr/SIMA200125301), Sep 10, 2001: SKIN. CRACKED. ABI - DURING MBV INSPECTION, FOUND OUTER SKIN OF RIGHT ENGINE NACELLE CRACKED ON OUTBOARD SIDE. REPAIRED NACELLE SKIN IAW SAAB 340 SRM AND REPAIR STATEMENT SDS0 - [SDR SIMA200124905](https://openairdocs.org/sdr/SIMA200124905), Sep 6, 2001: FRAME. CORRODED. DURING MBV INSPECTION, FOUND FRAME 236.5 UNDER GALLEY AREA HAD CORROSION BEYOND SRM LIMITS. CORROSION WAS REMOVED FROM FRAME AND WAS REPAIRED IAW SAAB 340 SRM. - [SDR SIMA200124803](https://openairdocs.org/sdr/SIMA200124803), Sep 5, 2001: FRAME. CORRODED. ABI - DURING MBV INSPECTIONS, FOUND UPPER FLANGE OF BOTTOM FRAME 225 HAD CORROSION BEYOND SRM LIMITATIONS. REMOVED CORROSION AND REPAIRED IAW SAAB 340 SRM. (M) - [SDR SIMA200116002](https://openairdocs.org/sdr/SIMA200116002), Jun 9, 2001: WEU. FAILED. BOS - FLT 4934 - ON TAKEOFF, NUMEROUS WARNING SOUNDED. ABORTED AT 120KTS. REMOVED AND REPLACED WARNING ELECTRONIC UNIT IAW AMM. OPS CHECK GOOD. (M) - [SDR SIMA20011331](https://openairdocs.org/sdr/SIMA20011331), May 13, 2001: SMOKE DETECTOR. MALFUNCTIONED. BUF - FLT 5135 - CREW REPORTED THE AVIONICS SMOKE LIGHT ILLUMINATED INFLIGHT. PUT ON MEL AT THIS TIME. MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR IAW S - [SDR SIMA2873](https://openairdocs.org/sdr/SIMA2873), Oct 13, 2000: POWER SUPPLY. INOPERATIVE. BWI - FLT 9750 - SEVERAL EMERGENCY LIGHTS IN THE AFT SECTION OF CABIN ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT 24LN IAW SAAB MM 33-50 - [SDR SIMA1843](https://openairdocs.org/sdr/SIMA1843), Jul 2, 2000: SWITCH. DIRTY. JFK - FLT 5003 - DURING CLIMB, THE RIGHT BETA LIGHT FLASHED ON AND OFF. AFTER BRINGING THE RIGHT CONDITION LEVER TO 1070 RPM FOR CLIMB IT FLASHED ON AND OFF UNT - [SDR SIMA0704](https://openairdocs.org/sdr/SIMA0704), Mar 10, 2000: WARNING LIGHT. ILLUMINATED. AVIONICS SMOKE LIGHT CWP PANEL ILLUMINATED FOR 20 SECONDS IN FLIGHT THAN WENT OUT. INSPECTED AVIONICS COMPARTMENT MG357541 AND CLEANED SMOKE DETECTOR IAW AE WOR - [SDR 99ZZZX1484](https://openairdocs.org/sdr/99ZZZX1484), Mar 30, 1999: CAMBOX. WORN. POWER AND CONDITION CAMBOX FOUND SPLINES WORN BETWEEN HMU AND CAMBOX ASSY. PROPELLER RPM RT ENGINE FOUND ABNORMAL DUE TO SEVERELY WORN CAMBOX AND HMU SPLINES. - [SDR SIMA983621](https://openairdocs.org/sdr/SIMA983621), Dec 28, 1998: HYDRAULIC LINE. LEAKING. JFK - FLT 4830 - AFTER TAKEOFF WITH GEAR UP, NOTICED THE HYDRAULIC PUMP STILL RUNNING AND NO HYDRAULIC FLUID QUANTITY INDICATED. HYDRAULIC ACCUMULATOR PRESSURE - [SDR SIMA981461](https://openairdocs.org/sdr/SIMA981461), May 26, 1998: ACTUATOR. WORN. JFK - FLT 9852 - LEFT PROPELLER RPM SURGES. INSPECTED PROPELLER ACTUATOR. FOUND ABNORMAL WEAR. REPLACED LEFT PROP ACTUATOR. PERFORMED OPERATION CHECK SATISFACTO - [SDR NVEA235AE](https://openairdocs.org/sdr/NVEA235AE), May 4, 1997: EMERGENCY BUSS. LOST. CAPT REPORTED, EMERGENCY LIGHT CAME ON IN FLIGHT AND WENT OUT AND CAME ON AGAIN AND REMAINED ON AND LOST EMERGENCY BUSS. LT GENERATOR VOLTAGE NORMAL. C/W QRH PR - [SDR 96ZZZX3980](https://openairdocs.org/sdr/96ZZZX3980), Jun 17, 1996: HYDRAULIC LINE. FAILED. JFK - FLT 4894 - CREW REPORTS: HYDRAULIC LOW LIGHT ILLUMINATED ONE MINUTE PRIOR TO LANDING. AFTER LANDING, AIRCRAFT HAD MINIMAL BRAKE PRESSURE. FOUND HYDRAULIC --- 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.