# N741BA: Saab-Fairchild 340A, registration cancelled 2008-02-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 13, 2008 - Status when cancelled: Triennial form not returned - Airframe: [Saab-Fairchild 340A](https://openairdocs.org/model/saab-fairchild-340a) (registry code 7850100) - 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: 340A-090 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: June 22, 1987 - Certificate issued: October 26, 2004 - Last registry action: October 16, 2007 - Mode S code: A9F65B - Owner when cancelled: [White Industries Inc](https://openairdocs.org/faa-owner/WHITE%20INDUSTRIES%20INC) - Location: [Bates City, MO](https://openairdocs.org/faa-place/MO/Bates%20City) - Owner type: Corporation - Owner's area on the map: 38.9597° N, 94.0679° W: Placed by OpenAirDocs at the center of ZIP code 64011, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N741BA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=741BA - Page: https://openairdocs.org/deregistered/N741BA-2008-02-13 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-Fairchild 340A: https://openairdocs.org/model/saab-fairchild-340a.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 PLGA001024](https://openairdocs.org/sdr/PLGA001024), Oct 24, 2000: WIRE. BROKEN. BOS-PQI - FLT 4828 - DURING FLIGHT, THE RIGHT DC GENERATOR DROPPED OFF LINE. THE AIRCRAFT WAS DIVERTED TO BGR AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AND - [SDR PLGA000729](https://openairdocs.org/sdr/PLGA000729), Jul 29, 2000: RELAY. FAILED. BGR - FLT 4662 - BOS-YHZ, DURING FLIGHT, THE LEFT MAIN BUSS LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT DIVERTED INTO BGR AND LANDED WITHOUT INCIDENT. MAINTENANCE - [SDR PLGA990211A](https://openairdocs.org/sdr/PLGA990211A), Feb 11, 1999: LINE. FAILED. LGA - FLT 6540 - AFTER GEAR EXTENSION, CREW LOST ALL HYDRAULIC PRESSURE. AIRCRAFT LANDED WITHOUT INCIDENT AND WERE TOWED FROM RUNWAY. MAINTENANCE REPLACED RUPTU - [SDR PLGA980908A](https://openairdocs.org/sdr/PLGA980908A), Sep 8, 1998: SLIDER BLOCK. DAMAGED. ALB - PROPELLER WAS REMOVED TO EVALUATE EXCESSIVE RADIAL PLAY. UPON INSPECTION, THE FOLLOWING WAS FOUND: SLIDER BLOCK HAD BECOME DETACHED FROM CROSSHEAD CAUSING - [SDR PLGA980707A](https://openairdocs.org/sdr/PLGA980707A), Jul 7, 1998: BLADE. CRACKED. ALB - PROPELLER WAS REMOVED TO EVALUATE EXCESS BLADE MOVEMENT. UPON INSPECTION, THE FOLLOWING WAS FOUND: NR 4 BLADE ROOT OUTER SLEEVE WAS CRACKED COMPLETELY ARO - [SDR PLGA980114C](https://openairdocs.org/sdr/PLGA980114C), Jan 14, 1998: CONNECTOR. DIRTY. BTV - AFTER TAKEOFF, THE CREW REPORTED THE LEFT ENGINE TORQUE STARTED FLUCTUATIONS BETWEEN 80-90 PERCENT. THE LEFT OIL PRESSURE ALSO STARTED FLUCTUATIONS OF 20 - [SDR PLGA970802A](https://openairdocs.org/sdr/PLGA970802A), Aug 2, 1997: WIRE. BROKEN. PWM - FLT 4788 - DURING PREFLIGHT, FOUND EMERGENCY EXIT LIGHT AT ROW 7BC WOULD NOT TEST. REPAIRED LIGHT WIRING. SYSTEM TESTED GOOD. (M) - [SDR PLGA970707A](https://openairdocs.org/sdr/PLGA970707A), Jul 7, 1997: TEST SWITCH. FAILED. LGA - FLT 4720 - DURING PRE-FLIGHT, THE EMERGENCY EXIT LIGHTS WOULD NOT TEST. FOUND F/A TEST SWITCH AT FAULT. SWITCH WAS REPLACED AND SYSTEM TESTED GOOD. (X) - [SDR PLGA970624A](https://openairdocs.org/sdr/PLGA970624A), Jun 24, 1997: POWER SUPPLY. INOPERATIVE. LGA - FLT 4765 - DURING PRE-FLIGHT, CREW FOUND EMERGENCY EXIT LIGHT IN AFT CABIN WOULD NOT TEST. REPLACED POWER SUPPLY. (M) - [SDR PLGA970417A](https://openairdocs.org/sdr/PLGA970417A), Apr 17, 1997: CONNECTOR. DIRTY. LGA - FLT 4709 - DURING PRE TAXI CHECK, THE EMERGENCY EXIT LIGHT OVER FORWARD LEFT PASSENGER DOOR FAILED TO TEST. MAINTENANCE CLEANED LIGHT ELECTRICAL CONNECTOR - [SDR PLGA9610312](https://openairdocs.org/sdr/PLGA9610312), Oct 31, 1996: CONTL BOX. MALFUNCTIONED. PVD - FLT 4782 - DURING APPROACH WHEN THE GEAR WAS SELECTED DOWN THE N/G AND LT MAIN GEAR GREEN DOWN AND LOCKED IND DID NOT ILLUMINATE. THE CREW CYCLED THE GEAR - [SDR PLGA9610201](https://openairdocs.org/sdr/PLGA9610201), Oct 20, 1996: CONNECTOR. DIRTY. PWM - FLT 4964 - EN ROUTE YOW, THE RIGHT TAIL PIPE HOT WARNING LIGHT ILLUMINATED. THE CREW SECURED THE ENGINE AND DIVERTED TO PWM, LANDING WITHOUT INCIDENT. MAI - [SDR PLG4896EB1](https://openairdocs.org/sdr/PLG4896EB1), Apr 8, 1996: HYD SWIVEL. BROKEN. PWM/BOS - FLT 4605 - DURING CLIMB-OUT, CREW NOTED THE HYDRAULIC PRESSURE DROPPING DURING GEAR RETRACTION. THE AIRCRAFT RETURNED TO PWM AND LANDED WITHOUT INCIDE - [SDR PLG122795E1](https://openairdocs.org/sdr/PLG122795E1), Dec 23, 1995: THERM CONTROLLER. FAILED. FLT NR 4959 - JFK-BWI - DURING CLIMB-OUT, THE RIGHT INTAKE HEAT FAILED. DUE TO EXISTING WEATHER CONDITIONS, THE AIRCRAFT RETURNED TO JFK AND LANDED WITHOUT INCI - [SDR PLG121895E1](https://openairdocs.org/sdr/PLG121895E1), Dec 14, 1995: CONNECTORS. DIRTY. BDL/YYZ - FLT 4881 - DURING THE FIRST PART OF FLIGHT, RT INTAKE FAIL LIGHT ILLUMINATED. DUE TO THE EXISTING WEATHER CONDITIONS, THE AIRCRAFT RETURNED TO BDL AND - [SDR PLG121895E2](https://openairdocs.org/sdr/PLG121895E2), Dec 9, 1995: TEMP SENSOR. CONTAMINATED. PVD/LGA - FLT 4783 - AFTER TAKEOFF, THE RT TAIL PIPE HOT LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO PVD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND RE - [SDR PLGA71195J1](https://openairdocs.org/sdr/PLGA71195J1), Aug 15, 1995: STATIC SEAL. EXCESS CLEARANCE. HIGH OIL TEMPERATURE, OIL PRESSURE FLUCTUATION AND LOSS IS BELIEVED TO BE THE RESULT OF EXCESSIVE CLEARANCE BETWEEN THE NR 3 LABRYNTH SEAL AND ITS ASSOCIATED ST - [SDR 95ZZZX1532](https://openairdocs.org/sdr/95ZZZX1532), Feb 8, 1995: LOOP. FAULTY. BWI - EN ROUTE IAD/BOS, RIGHT BLEED AIR FAULT LIGHT ILLUMINATED. FLIGHT CREW PERFORMED ABNORMAL CHECK LIST. SECURED RIGHT ENGINE AND LANDED IN BWI WITHOUT INCID ## FAA accident and incident reports (3) 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 19910711032299I](https://openairdocs.org/incident/19910711032299I), Jul 11, 1991: Saab SF340A (N741BA), Rochester, NY, Minor damage. Struck a parked aircraft while maneuvering to park. - [Incident 19890113008199I](https://openairdocs.org/incident/19890113008199I), Jan 13, 1989: Saab SF340A (N741BA), Albany, NY. Engine overtemp warning. Reduced power and returned. Replaced faulty warning electric unit. - [Incident 19880520033289I](https://openairdocs.org/incident/19880520033289I), May 20, 1988: Saab SF340A (N741BA), Binghamton, NY, Minor damage. Right engine fire indication and smoking. Returned. Passengers evacuated on runway. Ac generator had failed. ## Other aircraft with N741BA - [Registered now](https://openairdocs.org/aircraft/N741BA): Icon A5, S/N 00123 --- 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.