Registered owner
Ibc Airways Inc
Owner type
Corporation
Serial number
340A069
Year built
1966
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, transport
Airworthiness date
December 6, 2001
Certificate issued
July 15, 2022
Expires
July 31, 2029
Mode S code
A8690E

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every GE CT7-SER model are included below.

On this page

Airworthiness directives that may apply · 21

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1988In forceSuperseded2026
ADs by the year they took effect: 26 ADs
19881
19943
19971
19981
20021
20032
20042
20051
20061
20071
20091
20101
20112
20171
20181
20221
20231
20242
20252
See all 26 ADs

Information bulletins that may apply · 1

Advisory, not mandatory.

Engine · GE CT7-SER series

SAIB ANE-98-31Issued May 15, 1998

NTSB investigations

No NTSB investigations matched to N641BCMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Saab-Scania SF340A aircraft

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 9

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR OZCA2025002641Downlock Switch · looseON APPROACH INTO SNU, THE CREW SELECTED THE LANDING GEAR DOWN AND FAILED TO GET A DOWN AND LOCKED INDICATION ON THE LH MLG. THE CREW NOTIFIED THE TOWER AND ABORTED THE LANDING. A FLYBY PAST THE TOWER CONFORMED ALL 3 GEAR DOWN AND LOCKED. THE AIRCRAFT RETURNED May 31, 2025 · N641BC · Saab SF340A · Landing Gear Position and WarningSDR OZCA2024091706641Engine · erraticTAKING OFF FROM RUNWAY 06 IN FREEPORT, CLIMB OUT TO 1000 FT, CREW STARTED THE CLIMB CHECKLIST. UPON TURNING OFF CTOT AND SETTING CONDITION LEVERS TO CLIMB, THE RIGHT ENGINE LOST POWER AND THE OVER TEMPERATURE LIGHT ILLUMINATED. CREW PERFORMED MEMORY ITEMS ,ANDSep 16, 2024 · N641BC · Saab SF340A · Engine (Turbine/Turboprop)SDR OZCA2024004641Engine · overtempDURING DESCENT, SEVERAL LOUD BANGS WERE HEARD FROM THE RH ENGINE WITH VIBRATIONS. MAJOR FLUCTUATIONS ON THE TORQUE AND ITT. OVERTEMP LIGHT CAME ON FOR APPROX. 5 SECONDS. TORQUE SET AT 40% THEN REDUCED TO 20%. ENGINE STABILIZED AROUND 30% TORQUE. AIRCRAFT DECLAAug 12, 2024 · N641BC · Saab SF340A · Engine (Turbine/Turboprop)SDR OZCA20240219001Bleed Air Sys · looseAT FL240 RIGHT TQ AND RIGHT PROP RPM GAUGES AT ZERO. UNABLE TO MAINTAIN AIRSPEED. RIGHT ENGINE BECAME ROUGH, FUEL FLOW DECREASED. GAUGES THEN RETURNED TO NORMAL WITH HIGH RIGHT ITT. TURNED R HP OFF, ENGINE STABILIZED. MAINTENANCE INSPECTED BLEED SYSTEM AND FOUFeb 16, 2024 · N641BC · Saab SF340A · Engine Bleed Air SystemSDR OZCA20160505114Wire · shortedON CRUISE, LT TAIL PIPE HOT LIGHT ILLUMINATED ON WARNING PANEL. TROUBLE SHOT LT ENG TAIL PIPE, FOUND SHORT CIRCUIT ON WIRE 508-22. REPAIRED WIRE AS REQUIRED. OPERATIONAL CHECKED OK.May 5, 2016 · N641BC · Saab SF340A · Fire Protection System WiringSDR OZCA20160504112Test Switch · intermittentON VECTORS FOR APPROACH LT TAIL PIPE HOT ILLUMINATED ON CENTRAL WARNING PANEL. TROUBLE SHOT PROBLEM, FOUND TEST 1 PANEL FIRE TEST SWITCH INTERMITTENT. R & R TEST 1 PANEL IAW MM. OPERATIONAL CHECKED OK.May 4, 2016 · N641BC · Saab SF340A · Fire DetectionSDR OZCA20160504111Sensor · faultyLEFT TAIL PIPE HOT LIGHT ILLUMINATED. R & R LT TAIL PIPE HOT SENSORS. INSPECTED ALL TERMINALS & WIRES WITH NO DEFECTS NOTED. OPERATIONAL CHECKED OK AT THIS TIME.May 4, 2016 · N641BC · Saab SF340A · Overheat DetectionSDR OZCA20160310113Relay · failedENROUTE LOST LT MAIN BUS & ALL ASSOCIATED BUSES. R & R LT MAIN BUS RELAY. ALL OPERATIONAL CHECKED OK.Mar 3, 2016 · N641BC · Saab SF340A · Electrical Power SystemSDR OZC2008F00000Swivel · brokenPILOT NOTED THE HYD LIGHT ON DUE TO LOSS OF PRESSURE IN MAIN ACCUMULATOR AND HYD QUANTITY READING ZERO. PERFORMED AN EMERGENCY GEAR EXTENSION IAW QRH AND HAD AN UNEVENTFUL LANDING. MAINT INSPECTED THE AC AND FOUND THE HYD SWIVEL IN THE RT MAIN GEAR WELL PN LMar 26, 2008 · N641BC · Saab SF340A · Hydraulic System, Main

STCs that may be installed

No STCs matched this aircraft’s modelsSTCs are matched through the model’s type certificate data sheet, and this registry model isn’t matched to one.