# N671BC: 1987 Saab-Scania SF340A - Status: Valid registration - Airframe: [Saab-Scania SF340A](https://openairdocs.org/model/saab-scania-sf340a) (registry code 7860100, 37 seats) - Engine: [GE CT7-5A2](https://openairdocs.org/engine/ge-ct7-5a2) (registry code 30144) - Data sheets: [TCDS E8NE](https://openairdocs.org/tcds/E8NE) (General Electric Company GE Aviation) (OpenAirDocs) - Serial number: 340A-084 - Year built: 1987 - Type: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: July 7, 2008 - Certificate issued: July 15, 2022 - Expires: July 31, 2029 - Mode S code: A8DF8B - Registered owner: [Ibc Airways Inc](https://openairdocs.org/faa-owner/IBC%20AIRWAYS%20INC) - Location: [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale) - Owner type: Corporation - Owner's area on the map: 26.0870° N, 80.1530° W: Placed by OpenAirDocs at the center of ZIP code 33315, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=671BC - Page: https://openairdocs.org/aircraft/N671BC From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 11 in force ### Matched by airframe (Saab-Scania SF340A) None in force. ### Matched by engine (GE CT7-5A2) - [AD 2025-05-02](https://openairdocs.org/ad/2025-05-02): Engine (Turbine/Turboprop) · General Electric CT7-5A2, CT7-5A3, CT7-7A and 8 more. Effective Apr 8, 2025 - [AD 2023-21-07](https://openairdocs.org/ad/2023-21-07): Turbine Engine Reduction Gear · General Electric CT7-5A2, CT7-5A3, CT7-7A and 6 more. Effective Dec 11, 2023 - [AD 2007-08-01](https://openairdocs.org/ad/2007-08-01): Eddy current inspection (ECI) of boltholes · General Electric CT7-5A2, CT7-5A3, CT7-7A and 8 more. Effective May 14, 2007 - [AD 2004-07-09](https://openairdocs.org/ad/2004-07-09): PGB oil filter impending bypass button (IBB) · General Electric CT7-2A, CT7-2D, CT7-2D1 and 14 more. Effective May 11, 2004 - [AD 2002-01-03](https://openairdocs.org/ad/2002-01-03): Stage 2 Turbine Aft Cooling Plates · General Electric CT7-5A2, CT7-5A3, CT7-7A and 1 more. Effective Feb 12, 2002 - [AD 97-25-07](https://openairdocs.org/ad/97-25-07): Stage 1 or 2 Gas Generator Turbine (GGT) Disk · General Electric CT7-5A2, CT7-7A, CT7-9B and 1 more. Effective Jan 28, 1998 - [AD 96-26-01](https://openairdocs.org/ad/96-26-01): GGT Stage 2 Forward Cooling Plate · General Electric CT7-5A2, CT7-7A, CT7-9B and 1 more. Effective Mar 10, 1997 - [AD 94-17-16](https://openairdocs.org/ad/94-17-16): Propeller Gearboxes · General Electric CT7-5A2, CT7-5A3, CT7-7A and 6 more. Effective Sep 15, 1994 - [AD 93-25-17](https://openairdocs.org/ad/93-25-17): Gas Generator Turbine (GGT) Disks and Cooling Plates · General Electric CT7-2A, CT7-5A2, CT7-6 and 2 more. Effective Feb 2, 1994 - [AD 93-23-05](https://openairdocs.org/ad/93-23-05): Gas Generator Turbine (GGT) Rotor Assembly Parts and Power Turbine (PT) Disks · General Electric CT7-5A2 and CT7-7A. Effective Jan 10, 1994 - [AD 88-07-08](https://openairdocs.org/ad/88-07-08): Power Turbine Overspeed · General Electric CT7-5A2. Effective May 9, 1988 ### Historical (superseded or no longer in force) - [AD 2018-03-13](https://openairdocs.org/ad/2018-03-13) (historical): Turbine Engine Reduction Gear · General Electric CT7-5A2, CT7-5A3, CT7-7A and 6 more. Effective Feb 28, 2018 - [AD 2005-18-01](https://openairdocs.org/ad/2005-18-01) (historical): Turbine aft cooling plate boltholes · General Electric Aircraft Engines CT7-5A2, CT7-5A3, CT7-7A and 4 more. Effective Oct 24, 2005 - [AD 2003-06-03](https://openairdocs.org/ad/2003-06-03) (historical): Propeller gearbox (PGB) oil filter · General Electric Aircraft Engines CT7-2A, CT7-2D, CT7-2D1 and 14 more. Effective Apr 24, 2003 ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N671BC. ## FAA accident and incident reports None matched to N671BC. ## Service difficulty reports (7) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR OZCA340076221212](https://openairdocs.org/sdr/OZCA340076221212), Dec 12, 2022: TRIMMER. FAULTY. CROSSING 11,000 FT, RIGHT ENGINE ITT INCREASE UNCOMMANDED TO 872C (802C BEFORE INCREASE). PROCEEDED WITH QRH - REDUCING POWER POWER LEVERS BROUGHT TEMPERATURES - [SDR OZCA340084221207](https://openairdocs.org/sdr/OZCA340084221207), Dec 7, 2022: PERISEAL. UNSERVICEABLE. #2 ENGINE IN CRUISE, ITT OUT OF LIMITS. C/W QRH. - REMOVED AND REPLACED R/H SIDE UNDER WING FLAP PERI-SEAL IAW SF340A AMM 36-11-40-04. RUN CHECKS SATISFACTORILY - [SDR OZCA20201014](https://openairdocs.org/sdr/OZCA20201014), Oct 14, 2020: SMOKE DETECTOR. FALSE ACTIVATION. WRITE UP, MASTER WARNING, AVIONICS SMOKE LIGHT ON. MIR STATEMENT, CLIMBING OUT OF 2000 FT DEPARTING FROM KMIA TO MBPV, AVIONICS SMOKE LIGHT ON. THE CREW PERFORM - [SDR OZCA20150921020](https://openairdocs.org/sdr/OZCA20150921020), Sep 21, 2015: PUMP. FAILED. DURING CRUISE, HYD PUMP FAILED. LANDED WITH NO INCIDENT. R & R MAIN HYD PUMP IAW MM. OPERATIONAL CHECKED SATISFACTORY. - [SDR OZCA201501160013](https://openairdocs.org/sdr/OZCA201501160013), Jan 16, 2015: HMU. MALFUNCTIONED. LEFT ENG FAILED ON LANDING ROLL AFTER USING MODERATE REVERSE THRUST. R & R LT ENG HMU IAW APPLICABLE MM. OPERATIONAL CHECKS SATISFACTORY. - [SDR OZCA20141119004](https://openairdocs.org/sdr/OZCA20141119004), Nov 19, 2014: SMOKE DETECTOR. INOPERATIVE. AIRCRAFT RETURNED DUE TO CARGO SMOKE INDICATION. AFTER TROUBLESHOOTING, FOUND ZONE A CARGO SMOKE DETECTOR INOPERATIVE. R & R ZONE A CARGO SMOKE DETECTOR IAW MM - [SDR OZCA060809001](https://openairdocs.org/sdr/OZCA060809001), Jun 8, 2009: LATCH. DEFECTIVE. ON DEPARTURE FROM MIA THE PILOT NOTED THE LT ENGINE COWLING HAD POPPED OPEN AND WAS COLLAPSED AGAINST THE ENGINE. POWER TO THE AFFECTED ENGINE WAS REDUCED AND A ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Saab-Scania SF340A aircraft: https://openairdocs.org/model/saab-scania-sf340a/aircraft.md - The GE CT7-5A2 engine: https://openairdocs.org/engine/ge-ct7-5a2.md --- 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.