# Convair 240 - Type: Aircraft model (FAA registry) - Registry code: 2422601 - Manufacturer (registry): CONVAIR - Model: 240 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Reciprocating - Seats: 42 - Weight class: 20,000 lb and over - Cruise speed: 210 mph - Certification: Type certificated - Data sheet: [TCDS A-793](https://openairdocs.org/tcds/A-793) (OpenAirDocs) - Holder: Kelowna Flightcraft R & D Ltd. - Registered aircraft: 0 - Page: https://openairdocs.org/model/convair-240 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 98-08-17](https://openairdocs.org/ad/98-08-17): AFM - Power Levers · Kelowna Flightcraft R & D 240 Series, 340 and 440. Effective May 19, 1998 - [AD 96-03-04](https://openairdocs.org/ad/96-03-04): AFM - Limitation, Icing Conditions · Kelowna Flightcraft R & D 240 Series, 340, 440 and 4 more. Effective Feb 28, 1996 - [AD 93-21-02](https://openairdocs.org/ad/93-21-02): Elevators And Rudder · Kelowna Flightcraft R & D 240 Series. Effective Nov 26, 1993 - [AD 92-25-13](https://openairdocs.org/ad/92-25-13): Corrosion Inspection · Kelowna Flightcraft R & D 240 Series, 340, 440 and 4 more. Effective Jan 12, 1993 - [AD 91-12-04](https://openairdocs.org/ad/91-12-04): Elevator Hinge Pins · Kelowna Flightcraft R & D 240 Series. Effective Jul 25, 1991 - [AD 83-23-05](https://openairdocs.org/ad/83-23-05): Main Door Latching Systems · Kelowna Flightcraft R & D 240 Series. Effective Nov 28, 1983 - [AD 83-23-04](https://openairdocs.org/ad/83-23-04): Lock Warning Switch · Kelowna Flightcraft R & D 240 Series with STC SA4025WE or SA4026WE. Effective Nov 28, 1983 - [AD 83-01-01](https://openairdocs.org/ad/83-01-01): NLG Axle Fracture · Kelowna Flightcraft R & D 240 Series. Effective Jan 19, 1983 - [AD 81-18-05](https://openairdocs.org/ad/81-18-05): Wing Structure Inspection · Kelowna Flightcraft R & D 240 Series. Effective Nov 15, 1982 - [AD 80-08-03](https://openairdocs.org/ad/80-08-03): Aircraft Windows · Kelowna Flightcraft R & D 240 Series, 340 and 440 with STC SA1054WE or 2 others. Effective May 5, 1980 - [AD 79-21-06](https://openairdocs.org/ad/79-21-06): Elevator Flight Tab Spring Tube · Kelowna Flightcraft R & D 240 Series. Effective Jan 21, 1980 - [AD 77-10-11](https://openairdocs.org/ad/77-10-11): Landing Gear Lug · Kelowna Flightcraft R & D 240 Series, 340 and 440 with STC SA1054WE or 2 others. Effective May 26, 1977 - [AD 67-33-03](https://openairdocs.org/ad/67-33-03): Pressure Fueling Valves · Kelowna Flightcraft R & D 240 Series, 340 and 440 with STC SA1054WE or 3 others. Effective Oct 3, 1972 - [AD 70-10-03](https://openairdocs.org/ad/70-10-03): Engine Breather Oil Fumes · Kelowna Flightcraft R & D 240 Series, 340 and 440 with STC SA1054WE or SA1096WE. Effective May 12, 1970 - [AD 68-16-04](https://openairdocs.org/ad/68-16-04): Exhaust Ducts · Kelowna Flightcraft R & D 240 Series, 340 and 440 with STC SA1054WE or SA1096WE. Effective Dec 27, 1968 - [AD 67-07-05](https://openairdocs.org/ad/67-07-05): Propeller Gust Lock · Kelowna Flightcraft R & D 240 Series, 340 and 440 with STC SA1054WE or SA1096WE. Effective Feb 25, 1967 - [AD 64-19-04](https://openairdocs.org/ad/64-19-04): Emergency Circuits · Kelowna Flightcraft R & D 240 Series. Effective Sep 7, 1964 - [AD 64-18-04](https://openairdocs.org/ad/64-18-04): Nose Landing Gear Retract Forks · Kelowna Flightcraft R & D 240 Series, 340 and 440. Effective Aug 28, 1964 - [AD 64-03-03](https://openairdocs.org/ad/64-03-03): Blades · Boeing DC-6, DC-6A, DC-6B and 26 more. Effective Mar 1, 1964 - [AD 53-05-01](https://openairdocs.org/ad/53-05-01): Propellers Slip Rings · Aero Spacelines 377, 377MG, 377SGT and 6 more - [AD 74-03-04](https://openairdocs.org/ad/74-03-04): Pilot and Co-pilot Window Frame Castings · Kelowna Flightcraft R & D 240 Series with STC SA1054WE. Effective Feb 4, 1947 - [AD 70-03-07](https://openairdocs.org/ad/70-03-07): Auxiliary Power Units · Airesearch Auxiliary Power Units, 240 Series, 340 and 1 more - [AD 59-04-02](https://openairdocs.org/ad/59-04-02): Pilot's Direct-Vision Window · Kelowna Flightcraft R & D 240 Series, 340 and 440 - [AD 59-02-01](https://openairdocs.org/ad/59-02-01): Forward Fire Zones · Kelowna Flightcraft R & D 240 Series and 340 - [AD 59-01-01](https://openairdocs.org/ad/59-01-01): Fire Detector System · Kelowna Flightcraft R & D 240 Series, 340 and 440 - [AD 58-25-01](https://openairdocs.org/ad/58-25-01): Elevator Torque Tube · Kelowna Flightcraft R & D 240 Series - [AD 58-06-01](https://openairdocs.org/ad/58-06-01): Main Landing Gear Axle · Kelowna Flightcraft R & D 240 Series - [AD 57-14-01](https://openairdocs.org/ad/57-14-01): Nose Gear · Kelowna Flightcraft R & D 240 Series and 340 - [AD 57-03-01](https://openairdocs.org/ad/57-03-01): Main Outboard Landing Gear Fitting · Kelowna Flightcraft R & D 240 Series - [AD 56-24-02](https://openairdocs.org/ad/56-24-02): Carburetors · Kelowna Flightcraft R & D 240 Series, 340, 440 and 2 more - [AD 56-24-01](https://openairdocs.org/ad/56-24-01): Cylinder · Kelowna Flightcraft R & D 240 Series, 340 and 440 - [AD 56-20-04](https://openairdocs.org/ad/56-20-04): Fire Seals · Kelowna Flightcraft R & D 240 Series, 340 and 440 - [AD 56-18-01](https://openairdocs.org/ad/56-18-01): Generator · Kelowna Flightcraft R & D 240 Series - [AD 56-04-02](https://openairdocs.org/ad/56-04-02): Fuel Supply Lines · Kelowna Flightcraft R & D 240 Series and 340 - [AD 55-18-01](https://openairdocs.org/ad/55-18-01): Solenoid Operated Throttle Locks · Kelowna Flightcraft R & D 240 Series and 340 - [AD 55-15-02](https://openairdocs.org/ad/55-15-02): Propeller Feathering System · Kelowna Flightcraft R & D 240 Series and 340 - [AD 53-23-01](https://openairdocs.org/ad/53-23-01): Nose Landing Gear Clutch Plate · Kelowna Flightcraft R & D 240 Series - [AD 52-14-02](https://openairdocs.org/ad/52-14-02): Electrical Circuits · Kelowna Flightcraft R & D 240 Series and 340 - [AD 52-11-02](https://openairdocs.org/ad/52-11-02): Nacelle · Kelowna Flightcraft R & D 240 Series - [AD 51-28-01](https://openairdocs.org/ad/51-28-01): Engine Accessory Section · Kelowna Flightcraft R & D 240 Series - [AD 50-52-01](https://openairdocs.org/ad/50-52-01): Blades · Boeing DC-6, DC-6A, DC-6B and 4 more - [AD 50-36-01](https://openairdocs.org/ad/50-36-01): Nose Strut Cylinder · Kelowna Flightcraft R & D 240 Series - [AD 50-19-02](https://openairdocs.org/ad/50-19-02): Rudder Flight Tab Balance Weight Brackets · Kelowna Flightcraft R & D 240 Series - [AD 50-13-01](https://openairdocs.org/ad/50-13-01): Aileron Hinge · Kelowna Flightcraft R & D 240 Series - [AD 49-45-02](https://openairdocs.org/ad/49-45-02): Reverse Lock Solenoid Linkage · Kelowna Flightcraft R & D 240 Series - [AD 49-44-02](https://openairdocs.org/ad/49-44-02): Horizontal Tail · Kelowna Flightcraft R & D 240 Series - [AD 49-43-01](https://openairdocs.org/ad/49-43-01): Augmenter Tube · Kelowna Flightcraft R & D 240 Series - [AD 49-38-01](https://openairdocs.org/ad/49-38-01): Nose Gear Landing Struts · Kelowna Flightcraft R & D 240 Series - [AD 49-34-01](https://openairdocs.org/ad/49-34-01): Cockpit Checklist · Kelowna Flightcraft R & D 240 Series - [AD 49-30-02](https://openairdocs.org/ad/49-30-02): Augmenter Vanes · Kelowna Flightcraft R & D 240 Series Historical (superseded or no longer in force): - [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996 All 55: https://openairdocs.org/model/convair-240/ads.md ## Registered aircraft None registered with this model now. ## NTSB investigations (7) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB ANC93FA128](https://openairdocs.org/ntsb/ANC93FA128), Jul 27, 1993: Convair 240 (N156PA), Boise, ID, substantial damage. Probable cause: THE PILOT'S FAILURE TO EXTEND THE LANDING GEAR, AND THE CHECK PILOT'S INADEQUATE SUPERVISIION. A FACTOR IN THE ACCIDENT WAS THE PILOT'S INADEQUATE UPGRADE TRAINING BY THE COMPANY. - [NTSB MIA80FA065](https://openairdocs.org/ntsb/MIA80FA065), May 24, 1980: Convair 240 (N300GR), Daytona Beach, FL, destroyed, 3 fatal - [NTSB DCA78AA001](https://openairdocs.org/ntsb/DCA78AA001-195024), Oct 20, 1977: Convair 240 (N55VM), Gillsburg, MS, destroyed, 6 fatal - [NTSB NYC77FA050](https://openairdocs.org/ntsb/NYC77FA050), Apr 9, 1977: Convair 240 (N10AV), Hyannis, MA, destroyed - [NTSB IAD70AI046](https://openairdocs.org/ntsb/IAD70AI046), Feb 20, 1970: Convair 240 (N741J), Hampton, VA, substantial damage - [NTSB DEN70AD045](https://openairdocs.org/ntsb/DEN70AD045), Jan 17, 1970: Convair 240 (N270L), Aspen, CO, substantial damage - [NTSB NYC65A0110](https://openairdocs.org/ntsb/NYC65A0110), Feb 22, 1965: Convair CV-240 (N1020C), Jamaica, NY, no damage ## FAA accident and incident reports (15) 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 20031024028449I](https://openairdocs.org/incident/20031024028449I), Oct 24, 2003: Cvac 240* (N99380), Pittsburgh, PA, Minor damage. (-23) At 0630E on 10/24/2003, air tahoma flight 384, a CV-240 landed on runway 32 when the right engine caught fire. The ARFF responded and extinguished the… - [Incident 19960202002979I](https://openairdocs.org/incident/19960202002979I), Feb 2, 1996: Cvac 24027 (N156PA), Memphis, TN, Minor damage. Narrative: on feb 2, 1996 at 0515 am CDT, renoun aviation CV240 aircraft N156PA landed on Memphis, TN runway 36L and slid off the runway. Ice on the runway and… - [Accident 19930727026459A](https://openairdocs.org/incident/19930727026459A), Jul 27, 1993: Cvac 240* (N156PA), Boise, ID, Substantial damage. Type rating flight test. Single engine approach. Landed gear up. Lacked training time and endorsement. FAA onboard. - [Incident 19890630045319I](https://openairdocs.org/incident/19890630045319I), Jun 30, 1989: Cvac 24027 (N156PA), Rochester, NY. NR2 engine rough. Diverted to Rochester. Shut down on approach. Found top cylinder had blown. - [Incident 19880729047129I](https://openairdocs.org/incident/19880729047129I), Jul 29, 1988: Cvac 24027 (N156PA), Cincinnati, OH, Minor damage. Left engine fire during taxi. Investigation showed it could be self induced exhaust stack fire. - [Incident 19870621037179I](https://openairdocs.org/incident/19870621037179I), Jun 21, 1987: Cvac LB30 (N12905), St. Louis, IL, Minor damage. Left wingtip struck a light and knocked it down during taxi. - [Incident 19841124066129I](https://openairdocs.org/incident/19841124066129I), Nov 24, 1984: Cvac 240* (N1020C), Daytona Beach, FL. Pilot did not perform proper preflight inspection. Power loss in left engine. Found water in fuel system. - [Incident 19841108065709I](https://openairdocs.org/incident/19841108065709I), Nov 8, 1984: Cvac 2400 (N152PA), Detroit, MI, Minor damage. Struck backhoe digger while taxiing on taxiway. Leading edge damage to aircraft. - [Incident 19830314019309I](https://openairdocs.org/incident/19830314019309I), Mar 14, 1983: Cvac 240* (N99380), Tucson, AZ, Minor damage. Foreward cabin main entrance door separated from aircraft on climbout. Jammed door plungers failed to lock. - [Incident 19830308017819I](https://openairdocs.org/incident/19830308017819I), Mar 8, 1983: Cvac 240* (N156PA), Buffalo, NY, Minor damage. The inboard wheel assembly separated from right main gear on takeoff roll. Found outer bearing failure on wheel. - [Incident 19820701036029I](https://openairdocs.org/incident/19820701036029I), Jul 1, 1982: Cvac 24027 (N152PA), Chicago, IL, Minor damage. Fuel supply line from fuel pump to carburetor ruptured on engine start. Fuel iginited. Fire put out by fire crew. - [Incident 19810228019249I](https://openairdocs.org/incident/19810228019249I), Feb 28, 1981: Cvac 24027 (N152PA), Quonset, RI. Engine cylinder head temp started rising power. Shutdown engine later. Bad cylinder head temp sensor. - [Accident 19800524015269A](https://openairdocs.org/incident/19800524015269A), May 24, 1980: Cvac 240/ (N300GR), Daytona Beach, FL, Destroyed, 1 fatal. Overgross, pilots not rated in aircraft engine fire on takeoff. No emergency action. Below VMC, lost control. - [Accident 19771020043659A](https://openairdocs.org/incident/19771020043659A), Oct 20, 1977: Cvac 240/ (N55VM), MS, Destroyed, 4 fatal - [Accident 19770409034649A](https://openairdocs.org/incident/19770409034649A), Apr 9, 1977: Cvac 240/ (N10AV), Hyannis, MA, Destroyed. Ice in r fuel tank. Crossfeed on,boost pumps on tank valves both on. Transfer ocrd. Rocks on beach. ## Service difficulty reports (11) As reported by operators and repair stations, by the model named in the report. - [SDR I5HA0824013](https://openairdocs.org/sdr/I5HA0824013), Dec 18, 2008: WING. DENTED. DURING THE LANDING FLARE, A BIRD STRUCK THE OTBD L/E OF THE LT WING. THE CREW LANDED THE ACFT WITHOUT FURTHER INCIDENT. THE LEADING EDGE WAS REMOVED AND REPLACE - [SDR I5HA0524006](https://openairdocs.org/sdr/I5HA0524006), Sep 16, 2005: ENGINE. LEAKING. DURING CLIMBOUT, THE PILOT OBSERVED A LOSS OF OIL QUANTITY FROM THE LT ENGINE. THE CREW PERFORMED AN EMERGENCY SHUTDOWN OF THE LT ENGINE AND RETURNED TO DEPARTU - [SDR I5HA0524003](https://openairdocs.org/sdr/I5HA0524003), May 28, 2005: LINE. LOOSE. WHILE ENROUTE, MAINTENANCE, THE PILOT OBSERVED A LOSS OF TORQUE PRESSURE ON THE LT ENGINE WITH NO SECONDARY INDICATIONS. AS A PRECAUTION, THE PILOT ELECTED TO S - [SDR I5HA0524001](https://openairdocs.org/sdr/I5HA0524001), Mar 31, 2005: AUGMENTOR TUBE. FIRE. RT ENG FIRE WARNING BELL SOUNDED AND ASSOC FIRE WARNING LIGHT ILLUMINATED DURING TAXI. RT FIRE BOTTLE WAS DISCHARGED AND ENG SHUTDOWN. FIRE WAS EXTINGUISHED WIT - [SDR I5HA0324002](https://openairdocs.org/sdr/I5HA0324002), Oct 24, 2003: CYLINDER. FAILED. EN ROUTE, PILOT NOTICED A DECREASE IN OIL QTY ON RT ENG. CONTINUED TO PIT. ELECTED TO KEEP RT ENG RUNNING. OIL QTY CONTINUED TO DECREASE. PILOT NOTICED MINOR TO - [SDR 2003F00529](https://openairdocs.org/sdr/2003F00529), Jul 11, 2003: ENGINE. MALFUNCTIONED. WHILE EN ROUTE TO CVG FROM PIT, IN CRUISE CONFIGURATION, THE CREW FELT A SHUDDER IN THE LEFT ENGINE. FIFTEEN MINUTES LATER FELT ANOTHER SHUDDER AND AGAIN ONE MI - [SDR 99ZZZM421](https://openairdocs.org/sdr/99ZZZM421), May 11, 1999: BEARING. FAILED. DURNIG A MAINTENANCE TEST FLIGHT, REQUIRED MORE THAN USUAL RUDDER TRIM. AFTER LANDING, NOTICED FLIGHT TAB APPEARED TO BE STUCK TO ONE SIDE. REMOVED RUDDER AND R - [SDR 97ZZZM706](https://openairdocs.org/sdr/97ZZZM706), May 26, 1997: ADI REGULATOR. RUPTURED. NR 2 ENGINE BEGAN TO BACKFIRE AND SURGE DURING CRUISE. ENGINE SHUT DOWN, LANDED SJO WITHOUT INCIDENT. FOUND ADI REGULATOR HAD RUPTURED DIAPHRAM WHICH MADE ENGIN - [SDR 96ZZZM1401](https://openairdocs.org/sdr/96ZZZM1401), Sep 17, 1996: CARBURETOR. DEFECTIVE. ON CLIMB-OUT, HAD COMPLETE POWER LOSS ON NR 2 ENGINE. ENGINE WAS FEATHERED AND AIRCRAFT RETURNED TO AIRPORT. CARBURETOR WAS FOUND TO BE DEFECTIVE AND REPLACED. - [SDR 96ZZZX4895](https://openairdocs.org/sdr/96ZZZX4895), Aug 8, 1996: CYLINDER. CRACKED. LEFT ENGINE BEGAN CONTINUOUSLY BACKFIRING AFTER LEAVING 2,000 FEET. ALL PRESSURES WERE NORMAL, TORQUE METER FLUCTUATIONS BETWEEN BACKFIRES. ENGINE WAS SHUT DOWN - [SDR 96ZZZX129](https://openairdocs.org/sdr/96ZZZX129), Oct 30, 1995: OIL COOLER. LEAKING. PSE/SJU - FLT 7026 - EN ROUTE, SHUT DOWN NR 2 ENGINE DUE TO LOW OIL PRESSURE AND QUANTITY. FOUND THE OIL COOLER LEAKING. REPLACED OIL COOLER. ## STCs that may be installed (OpenAirDocs) (109, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc - [STC SA863EA](https://openairdocs.org/stc/SA863EA): Incorporation of DME Corporation emergency evacuation slide lighting system. Astronics Luminescent Systems Inc - [STC SA16CE](https://openairdocs.org/stc/SA16CE): Float Type Fuel Gage Installation - Ground Visual Fuel. Sabreliner Aviation LLC - [STC SA3-420](https://openairdocs.org/stc/SA3-420): Main cabin seat installations(including divan and seat belts). Sabreliner Aviation LLC - [STC SA3-497](https://openairdocs.org/stc/SA3-497): Throttle reverse lock mechanism. Sabreliner Aviation LLC - [STC SA3-500](https://openairdocs.org/stc/SA3-500): General interior arrangement #1(16 passenger). General interior arrangement #2 (17 passenger). Sabreliner Aviation LLC - [STC SA3-501](https://openairdocs.org/stc/SA3-501): Typical divan installation (Divan P/N DC3-22021). Sabreliner Aviation LLC - [STC SA3-506](https://openairdocs.org/stc/SA3-506): Installation of weather radar antenna mount and radar nose. Sabreliner Aviation LLC - [STC SA3-567](https://openairdocs.org/stc/SA3-567): Chair and desk installation - Station 167. Sabreliner Aviation LLC - [STC SA3-579](https://openairdocs.org/stc/SA3-579): Rectangular Exit Exhaust Muffler Installation. Sabreliner Aviation LLC - [STC SA3-580](https://openairdocs.org/stc/SA3-580): General Interior Configuration - Floor Plan Arrangement #2. Sabreliner Aviation LLC - [STC SA3-582](https://openairdocs.org/stc/SA3-582): General interior configuration floor plan arrangement #3. Sabreliner Aviation LLC - [STC SA3-583](https://openairdocs.org/stc/SA3-583): General Interior Configuration - Floor Plan #4. Sabreliner Aviation LLC - [STC SA3-584](https://openairdocs.org/stc/SA3-584): Forward Lavatory Installation (Sta. 287). Sabreliner Aviation LLC - [STC SA3-585](https://openairdocs.org/stc/SA3-585): Rear galley installation (STA 644). Sabreliner Aviation LLC - [STC SA3-589](https://openairdocs.org/stc/SA3-589): Removal and Closure of Rear Service Door - Sta. 672. Sabreliner Aviation LLC - [STC SA3-590](https://openairdocs.org/stc/SA3-590): Installation Stewart-Warner 940-F24 cabin heater - STA 620. Sabreliner Aviation LLC - [STC SA3-601](https://openairdocs.org/stc/SA3-601): Typical swivel seat installation (Hardman Tool & Engineering Co. Seat Model 3004, TSO C-39). Sabreliner Aviation LLC - [STC SA3-645](https://openairdocs.org/stc/SA3-645): General interior configuration floor plan #5. Sabreliner Aviation LLC - [STC SA3-646](https://openairdocs.org/stc/SA3-646): Navigator chair and desk installation (STA 155). Sabreliner Aviation LLC - [STC SA3-648](https://openairdocs.org/stc/SA3-648): Flight Observer Jump Seat Installation - Sta. 109. Sabreliner Aviation LLC - [STC SA3-710](https://openairdocs.org/stc/SA3-710): Rear airstair door installation STA 628- 812. Sabreliner Aviation LLC - [STC SA3-711](https://openairdocs.org/stc/SA3-711): Closure installation L.H. entrance door (F.S. 638). Sabreliner Aviation LLC - [STC SA3-712](https://openairdocs.org/stc/SA3-712): Fabrication and installation of 360 degree swivel seat. Sabreliner Aviation LLC - [STC SA3-713](https://openairdocs.org/stc/SA3-713): General interior configuration floor plan #6. Sabreliner Aviation LLC - [STC SA3-714](https://openairdocs.org/stc/SA3-714): Utility shower installation - aft cabin. Sabreliner Aviation LLC - [STC SA3-734](https://openairdocs.org/stc/SA3-734): Lavatory/vanity installation - station 644. Sabreliner Aviation LLC - [STC SA3-735](https://openairdocs.org/stc/SA3-735): General interior configuration floor plan #8. Sabreliner Aviation LLC - [STC SA32CE](https://openairdocs.org/stc/SA32CE): Interior General Arrangement, Floor Plan #9. Sabreliner Aviation LLC - [STC SA35CE](https://openairdocs.org/stc/SA35CE): Installation of generator overheat indicator. Sabreliner Aviation LLC - [STC SA4-1179](https://openairdocs.org/stc/SA4-1179): Outer wing fuel tank installation. Sabreliner Aviation LLC - [STC SA7CE](https://openairdocs.org/stc/SA7CE): Cockpit auxiliary heater installation. Sabreliner Aviation LLC - [STC SA83CE](https://openairdocs.org/stc/SA83CE): Utility avionics rack installation (in radar nose). Sabreliner Aviation LLC - [STC SA1054WE](https://openairdocs.org/stc/SA1054WE): Installation of Rolls-Royce model Dart 542-4 engines with Dowty Rotol R245/4-40-4.5/13 propellers and associated modifications to engine mounting, nacelle, empennage, accessories, systems and equipment. Executive Jet Aircraft Co. LTD. c/o Southeast Aero Tek Inc - [STC SA1993NM](https://openairdocs.org/stc/SA1993NM): Installation of a de-icing system on the Rolls Royce RK45524A engine inlet cowl. ROBERT W. MURRAY - [STC SA3106NM](https://openairdocs.org/stc/SA3106NM): Installation of a de-icing system externally on the Dowty Rotol (C) 4CM/71 propeller spinner. ROBERT W. MURRAY - [STC SA125CE](https://openairdocs.org/stc/SA125CE): Installation of Hoskins Supplemental Model B of F High Intensity Wing Tip Lights, Model C or 30-0329-3 Dual Tail Light, with or without Model 2 High Intensity Fuselage Lights. BF Goodrich Aerospace - [STC SA1048SO](https://openairdocs.org/stc/SA1048SO): Conversion of USAF Model T-29B into the civil Model 240-27 with deviations to TCDS A-793. Pemco Aeroplex Inc - [STC SA1248SO](https://openairdocs.org/stc/SA1248SO): Installation of single point seat belt and shoulder harness restraint systems for the pilot's, co-pilot's, forward observer's and flight attendant's seat assemblies. Pemco Aeroplex Inc - [STC SA4-470](https://openairdocs.org/stc/SA4-470): ADF loop. Vanaero Company - [STC SA1-392](https://openairdocs.org/stc/SA1-392): 2008X series radome. Saint-Gobain Performance Plastics Corp - [STC SA1627SO](https://openairdocs.org/stc/SA1627SO): Conversion of a military model C-131A to Civil Model 240-53 freighter with a Class B cargo compartment. Associated Design - [STC SA1890WE](https://openairdocs.org/stc/SA1890WE): Installation of executive interior. Approved for Convair model 240, serial number 160 ONLY. Kelowna Flightcraft Ltd - [STC SA13SW](https://openairdocs.org/stc/SA13SW): Installation of ground operated APU. Signature Flight Support Corporation - [STC SA2-286](https://openairdocs.org/stc/SA2-286): Installation of three-place divan. Signature Flight Support Corporation - [STC SA2-969](https://openairdocs.org/stc/SA2-969): Installation of Lawrence auxiliary power unit in aft baggage compartment for ground operation only. Signature Flight Support Corporation - [STC SA2-985](https://openairdocs.org/stc/SA2-985): Installation of high rate discharge fire extinguisher system. Signature Flight Support Corporation - [STC SA189SW](https://openairdocs.org/stc/SA189SW): Modification of Convair 240, N618S, to change existing General Electric 2CM-76C4 engine driven DC generators to Jack & Heintz G29-7B, and to add to left engine an auxiliary J & H G29-7B DC generator controlled by Bendix Feeder Fault System. Rockwell Collins Inc - [STC SA2-1508](https://openairdocs.org/stc/SA2-1508): Modification of CV-240, N618S to incorporate the following changes: Interior arrangement, Generator control system, electrical distribution system, radio, communication and electronic systems, cockpit instrumentation, miscellaneous mechanical installations. Rockwell Collins Inc - [STC SA4077WE](https://openairdocs.org/stc/SA4077WE): Conversion of military model T29A to model 240-17, T-29B to Model240-27, T29D to Model 240-52 and C131-A to Model 240-53. (240 SERIES 17). Luft Air, Inc All 109: https://openairdocs.org/model/convair-240/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Aerolift 240](https://openairdocs.org/model/aerolift-240): 0 registered aircraft, registry code 0150240 - [General Dynamics 240](https://openairdocs.org/model/general-dynamics-240): 0 registered aircraft, registry code 3790202 --- 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.