# N311CE: 1991 Saab-Scania SAAB 340B, registration cancelled 2014-05-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 23, 2014 - Exported to: Ukraine - Status when cancelled: Valid registration - 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-214 - Year built: 1991 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: January 23, 1991 - Certificate issued: December 8, 2005 - Last registry action: January 14, 2013 - Mode S code: A34ABF - Owner when cancelled: [Aerocentury Corp](https://openairdocs.org/faa-owner/AEROCENTURY%20CORP) - Location: [Burlingame, CA](https://openairdocs.org/faa-place/CA/Burlingame) - Owner type: Corporation - Owner's area on the map: 37.5719° N, 122.3751° W: Placed by OpenAirDocs at the center of ZIP code 94010, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N311CE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=311CE - Page: https://openairdocs.org/deregistered/N311CE-2014-05-23 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 (32) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR NSVA2010232](https://openairdocs.org/sdr/NSVA2010232), Dec 21, 2010: FRAME. CRACKED. PERFORM PERMANENT REAIR OF CRACK DAMAGE IN FRAME FLANGE IAW TD 340-55-10-15. - [SDR NSVA2010229](https://openairdocs.org/sdr/NSVA2010229), Dec 17, 2010: SKIN. DAMAGED. PERFORM PERMANENT REPAIR MULTIPLE FUSELAGE DAMAGES IAW TD 340-51-10-11. - [SDR NSVA2010217](https://openairdocs.org/sdr/NSVA2010217), Dec 2, 2010: STRUCTURE. CRACKED. PERFORM PERMANENT REPAIR OF CRACK DAMAGE ON LT NACELLE IAW TD 340-54-10-20. - [SDR NSVA2010180](https://openairdocs.org/sdr/NSVA2010180), Oct 10, 2010: UNKNOWN. MALFUNCTIONED. DURING MAINTENANCE TAXI/RUN THE AIRCRAFT VEERED RIGHT INTO A DITCH ON TAXIWAY ZULU. THE CAUSE IS UNKNOWN AT THIS TIME. IAD FIRE DEPARTMENT AND LAW ENFORCEMENT P - [SDR NSVA2010167](https://openairdocs.org/sdr/NSVA2010167), Aug 31, 2010: LIGHT. DIRTY. F/A'S EMERGENCY LIGHT BUTTON DOES NOT ILLUMINATE. INSPECTED, CLEANED AND RE-INSTALLED. - [SDR NSVA2010100](https://openairdocs.org/sdr/NSVA2010100), Jun 19, 2010: OIL SYSTEM. LOW. LEFT ENG OIL PRESS LIGHT ON TAKEOFF ROLL (FLUCTUATING OIL PRESSURE); REJECTED AT LESS THAN 50 KNOTS. SERVICED NR 1 ENG, ADDED 2.0 QTS. PERFORMED OPS CHECK ON EN - [SDR NSVA201032](https://openairdocs.org/sdr/NSVA201032), Jan 29, 2010: STRUCTURE. DAMAGED. AIRCRAFT REQUIRES MAJOR REPAIR FOR PERM REPAIR OF MISC RIVET DEVIATION ON LT OUTBOARD NACELLE IAW TD 340-54-09-58. - [SDR NSVA2009054](https://openairdocs.org/sdr/NSVA2009054), Oct 30, 2009: PLATE. CORRODED. LAV DOOR AND SURROUNDING LAV SERVICE CONNECTOR/PLATE CORROSION PLUS 5 CHERRY FASTENERS INSTALLED RT TOP/BOTTOM CORNERS. SRM REPAIR / REPLACEMENT OF RECEPTACLE I - [SDR NSVA32009034](https://openairdocs.org/sdr/NSVA32009034), Jul 24, 2009: LIGHT. INOPERATIVE. EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT INOP. RELAMPED LIGHT. - [SDR NSVA2009033](https://openairdocs.org/sdr/NSVA2009033), Jul 24, 2009: LIGHT. INOPERATIVE. EMERGENCY FLOOR LIGHT INOP BY SEAT 4DF. REPLACED BULB. - [SDR NSVA20070162](https://openairdocs.org/sdr/NSVA20070162), Jun 23, 2007: STALL WARNING. MALFUNCTIONED. PUSHER DISARM LIGHT ILLUMINATED ON GROUND. RESET DISARM SYSTEM, OPS CHECK GOOD. - [SDR NSVA20070155](https://openairdocs.org/sdr/NSVA20070155), Jun 12, 2007: STRUT. UNDERSERVICED. GEAR UNSAFE LIGHT AFTER T/O. SERVICED NLG STRUT IAW COLGAN WORKCARD 32-21-075, OPS CHECK GOOD, MEL CLEARED. - [SDR NSVA20070072](https://openairdocs.org/sdr/NSVA20070072), Mar 23, 2007: SWITCH. MALFUNCTIONED. GUST LOCK ANNUNCIATOR ILLUMINATED BEFORE TAKEOFF. REMOVED AND REPLACED GUST LOCK MICRO SWITCH AND ADJUSTED ACTUATOR SPRING TENSION AND MICRO SWITCH GAP IAW AMM - [SDR NSVA20070061](https://openairdocs.org/sdr/NSVA20070061), Mar 8, 2007: SWITCH. MALFUNCTIONED. GUST LOCK LIGHT ILLUMINATED, ENSURE GUST LOCK DISENGAGED, PULLED CB G4 DISCONNECTED C/P SWITCH. REMOVED AND REPLACED THE RUDDER GUST LOCK SWITCH3CF IAW SMM 27-7 - [SDR NSVA20070023](https://openairdocs.org/sdr/NSVA20070023), Feb 2, 2007: WIRE. BROKEN. FLIGHT IDLE STOP LIGHT CAME ON DURING LANDING. TS IAW AMM 76-10-60 AND FOUND TWO BROKEN WIRES AT 6GA-J1 PINS L AND N REQUIRED WIRES IAW SAAB WM 20-20-00. REPAIR - [SDR NSVA200600239](https://openairdocs.org/sdr/NSVA200600239), Dec 28, 2006: CONTROL CABLE. UNKNOWN. RT CONDITION LEVER DOES NOT ENGAGE IN UNFEATHERED VERIFIED RIGHT PROP WILL GO INTO FEATHER POSITION AND CONDITION LEVERS WILL SHUT DOWN ENGINE. REMOVED AND REPL - [SDR NSVA200600235](https://openairdocs.org/sdr/NSVA200600235), Dec 18, 2006: UNKNOWN. ODOR. FOUND STRONG ODOR OF EXHAUST IN CABIN THROUGHOUT FLIGHT. PERFORMED ENGINE OPS CHECKED FOR EXHAUST LEAK ON RT ENGINE AND INSPECTED ENGINE, NO FAULTS FOUND SMELL - [SDR NSVA200600158](https://openairdocs.org/sdr/NSVA200600158), Oct 1, 2006: BALLAST. FAILED. NO VISIBLE SMOKE COMING IN CABIN DURING FLIGHT BUT F/A REPORT BURNING SULFUR ODOR IN ROW 8-9. INSPECTED CABIN OF AIRCRAFT FOR FIRE, SMOKE, AND ELECTRICAL DAMAGE - [SDR NSVA200600117](https://openairdocs.org/sdr/NSVA200600117), Aug 4, 2006: SMOKE DETECTOR. DIRTY. AVIONIC SMOKE ANNUNCIATOR ILLUMINATED IN FLIGHT TWICE. CLEANED AVIONIC SMOKE DETECTOR IAW 26-13-00. OPS CHECK GOOD. INSPECTED AVIONICS COMPONENT, NO SMOKE NOTED - [SDR NSVA200600084](https://openairdocs.org/sdr/NSVA200600084), Jun 18, 2006: TIRE. UNKNOWN. NOSE WHEEL SHIMMY ON TAKEOFF. REMOVED AND REPLACED 1 AND 2 TIRE NOSE IAW SAAB AMM 32-41-15-04. LEFT P/N 5006227 S/N OFF MAY04-3133 S/N ON JUNE02-3068, RIGHT P/N - [SDR 05222006A](https://openairdocs.org/sdr/05222006A), May 18, 2006: CONNECTOR. DIRTY. DURING T/O ROLL, WHEN CTOT SELECTED TO APR RT ENGINE TORQUE ADVANCE TO SELECTED SETTING (100%) LEFT ENGINE REMAINED AT TORQUE SET BY POWER LEVER. INSPECTED CONN - [SDR 03012006B](https://openairdocs.org/sdr/03012006B), Feb 24, 2006: ELEVATOR. VIBRATES. DURING CLIMB OUT NOTICED A VIBRATION IN THE AIRCRAFT, MAINLY IN THE YOKE, VIBRATION INCREASED IN CLIMB FLIGHT AND ALSO IN CRUISE FLIGHT. REMOVED AND REPLACED LT - [SDR 01092006F](https://openairdocs.org/sdr/01092006F), Jan 5, 2006: LIGHT. NOT SEATED. ON TAKEOFF DID NOT GET RT APR LIGHT WHEN PAST 64 DEGREES SWITCH. FOUND RT APR LIGHT CAPSULE NOT SEATED IN HOUSING, RESEATED APR LIGHT OPS CHECK GOOD. - [SDR 01092006B](https://openairdocs.org/sdr/01092006B), Dec 26, 2005: UNKNOWN. UNKNOWN. AUTOCOARSEN EVENT WHEN PL WERE ADVANCED BEYOND 64 DEGREES PLA- LT ENG. NO ING LIGHT ON SHUTDOWN. PERFORMED AUTOCOARSEN AND CTOT, OPS CHECK GOOD NO DEFECTS NOTED - [SDR CX7A194J0406](https://openairdocs.org/sdr/CX7A194J0406), Feb 20, 2004: DETECTOR. MALFUNCTIONED. DURING TAILPIPE HOT LIGHT ON T/O. ABORT T/O, RAN CHECKLIST AND RETURNED TO GATE. LEFT TAILPIPE HOT LIGHT ON FOR 30 SECONDS. - [SDR CX7A194J0410](https://openairdocs.org/sdr/CX7A194J0410), Jan 28, 2004: BOSS. BROKEN. RIGHT ENGINE REQUIRES REMOVAL DUE TO 9 O'CLOCK FUEL INJECTOR BOSS BROKEN. - [SDR CX7A194J0404](https://openairdocs.org/sdr/CX7A194J0404), Jan 17, 2004: DETECTOR. CONTAMINATED. LT TAILPIPE HOT LIGHT ILLUMINATED AFTER POWER SELECTED ON. MOISTURE WAS PRESENT. RAN UP ENGINE AND LIGHT EXTINGUISHED. - [SDR CX7A194J0351](https://openairdocs.org/sdr/CX7A194J0351), Jul 2, 2003: DOOR. UNSECURE. RIGHT O/B ENGINE COWL WAS NOT PROPERLY SECURED. - [SDR CX7A194J0350](https://openairdocs.org/sdr/CX7A194J0350), Jul 1, 2003: SIGN. ODOR. F/A REPORTED ELECTRICAL SMOKE ODOR FROM EMERGENCY EXIT SIGN IN ROW 8C - [SDR CX7A194J20](https://openairdocs.org/sdr/CX7A194J20), Sep 17, 2002: FAN. BURNED OUT. F/A REPORTED A BURNING ODOR IN THE MID SECTION OF THE CABIN. - [SDR CX7A194J2](https://openairdocs.org/sdr/CX7A194J2), Apr 8, 2002: WARNING SYSTEM. FALSE ACTIVATION. ON TAKEOFF ROLL TAIL PIPE HOT LIGHT ILLUMINATED. ABORTED TAKEOFF. LIGHT WENT OFF WHEN A/C RETURNED TO THE GATE. - [SDR 2002F01111](https://openairdocs.org/sdr/2002F01111), Jan 31, 2002: WARNING SYSTEM. ACTIVATED. TAIL PIPE HOT CAME ON AFTER TAKEOFF, AIR RETURN. TAIL PIPE HOT SENSOR. (M) ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20040913025269I](https://openairdocs.org/incident/20040913025269I), Sep 13, 2004: Saab 340B (N311CE), Chicago, IL, Minor damage. (-23) Chicago express airline Saab 340B, N311CE, serial number 214, upon landing at Midway airport in Chicago, IL on runway 22L, was notified by the control… ## Other aircraft with N311CE - [Registered now](https://openairdocs.org/aircraft/N311CE): Cirrus Design SR22T, S/N 11528, built 2026 --- 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.