# Convair 22 - Type: Aircraft model (FAA registry) - Registry code: 2423302 - Manufacturer (registry): CONVAIR - Model: 22 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 4 · Turbo-jet - Seats: 152 - Weight class: 20,000 lb and over - Cruise speed: 461 mph - Certification: Type certificated - Data sheet: [TCDS 4A27](https://openairdocs.org/tcds/4A27) (OpenAirDocs) - Holder: CV Nevada, LLC - Registered aircraft: 0 - Page: https://openairdocs.org/model/convair-22 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 75-02-04](https://openairdocs.org/ad/75-02-04): Electrical Appurtenances · D & R Nevada 22, 22M, 30 and 1 more. Effective Jan 24, 1975 - [AD 73-26-10](https://openairdocs.org/ad/73-26-10): Freon Pack Fuses · D & R Nevada 22, 22M and 30A. Effective Feb 1, 1974 - [AD 73-12-08](https://openairdocs.org/ad/73-12-08): Flap Track Support Structure · D & R Nevada 22 and 22M. Effective Jun 12, 1973 - [AD 72-13-02](https://openairdocs.org/ad/72-13-02): Main Landing Gear Beams · D & R Nevada 22 and 22M. Effective Jun 30, 1972 - [AD 69-19-06](https://openairdocs.org/ad/69-19-06): Landing Gear Axle Beam · D & R Nevada 22 and 22M. Effective Oct 18, 1969 - [AD 65-02-01](https://openairdocs.org/ad/65-02-01): Engine Fuel Supply Tubes · D & R Nevada 22 and 22M. Effective Feb 4, 1965 - [AD 64-12-04](https://openairdocs.org/ad/64-12-04): Engine Start Valve Open Warning System · D & R Nevada 22, 22M, 30 and 1 more. Effective Jul 6, 1964 - [AD 64-05-03](https://openairdocs.org/ad/64-05-03): Aileron Trim Gearbox Assembly · D & R Nevada 22, 22M, 30 and 1 more. Effective Mar 23, 1964 - [AD 63-20-04](https://openairdocs.org/ad/63-20-04): Flap Actuator Screwjacks · D & R Nevada 22 and 22M. Effective Oct 28, 1963 - [AD 63-16-04](https://openairdocs.org/ad/63-16-04): Outboard Foreflaps · D & R Nevada 22 and 22M. Effective Aug 27, 1963 - [AD 62-21-02](https://openairdocs.org/ad/62-21-02): Rudder · D & R Nevada 22 and 22M. Effective Oct 25, 1962 - [AD 62-20-02](https://openairdocs.org/ad/62-20-02): Aileron Override Spring · D & R Nevada 22, 22M, 30 and 1 more. Effective Oct 9, 1962 - [AD 62-18-01](https://openairdocs.org/ad/62-18-01): Rudder Tab Balance Weights · D & R Nevada 22, 22M, 30 and 1 more. Effective Aug 18, 1962 - [AD 62-12-03](https://openairdocs.org/ad/62-12-03): Flap Carriage Support Fittings · D & R Nevada 22 and 22M. Effective May 24, 1962 - [AD 62-07-01](https://openairdocs.org/ad/62-07-01): Balance Board Trunnions · D & R Nevada 22 and 22M. Effective Mar 24, 1962 - [AD 61-25-02](https://openairdocs.org/ad/61-25-02): Engine Starter Warning Indicator · D & R Nevada 22 and 22M. Effective Dec 29, 1961 - [AD 61-22-04](https://openairdocs.org/ad/61-22-04): Cabin Pressurization Static System · D & R Nevada 22 and 22M. Effective Nov 21, 1961 - [AD 61-14-04](https://openairdocs.org/ad/61-14-04): Forward Rod End · D & R Nevada 22 and 22M. Effective Jul 7, 1961 - [AD 61-14-03](https://openairdocs.org/ad/61-14-03): Cartridge Assembly-Rudder Spring · D & R Nevada 22 and 22M. Effective Jul 7, 1961 - [AD 61-13-01](https://openairdocs.org/ad/61-13-01): AC Power Distribution Box · D & R Nevada 22 and 22M. Effective Jun 20, 1961 - [AD 61-10-02](https://openairdocs.org/ad/61-10-02): Engine Mount Support Fitting · D & R Nevada 22 and 22M. Effective May 11, 1961 - [AD 61-07-01](https://openairdocs.org/ad/61-07-01): Foreflaps · D & R Nevada 22 and 22M. Effective Apr 10, 1961 ## Registered aircraft None registered with this model now. ## NTSB investigations (14) 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 MIA78FA090](https://openairdocs.org/ntsb/MIA78FA090), May 25, 1978: Convair 880 (N8815E), Miami, FL, substantial damage - [NTSB DCA73AZ004](https://openairdocs.org/ntsb/DCA73AZ004), Dec 20, 1972: Convair 880 (N8807E), Chicago, IL, substantial damage, 10 fatal - [NTSB CHI73AC008](https://openairdocs.org/ntsb/CHI73AC008), Jul 22, 1972: Convair 880 (N8810E), Knoxville, TN, no damage - [NTSB FTW72AF062](https://openairdocs.org/ntsb/FTW72AF062), Mar 28, 1972: Convair 880 (N8810E), Little Rock, AR, no damage - [NTSB FTW70A0012](https://openairdocs.org/ntsb/FTW70A0012), Sep 4, 1969: Convair 880 (N8806E), Jackson, MS, no damage - [NTSB MIA68A0047](https://openairdocs.org/ntsb/MIA68A0047), Nov 2, 1967: Convair 880 (N8494H), Jacksonville, FL, no damage - [NTSB NYC67A0186](https://openairdocs.org/ntsb/NYC67A0186), Jun 24, 1967: Convair CV-880 (N8815E), Newark, NJ, substantial damage - [NTSB FTW67I0055](https://openairdocs.org/ntsb/FTW67I0055), Nov 18, 1966: Convair 880 (N8814E), Carswell Afb, TX, incident, minor damage - [NTSB NYC67I0024](https://openairdocs.org/ntsb/NYC67I0024), Aug 10, 1966: Convair 880 (N8816E), Philadelphia, PA, incident, substantial damage - [NTSB MKC66A0018](https://openairdocs.org/ntsb/MKC66A0018), Sep 13, 1965: Convair CV-880 (N820TW), Kansas City, MO, destroyed - [NTSB NYC66A0068](https://openairdocs.org/ntsb/NYC66A0068), Mar 2, 1965: Convair CV-880 (N8494H), Wilmington, NC, no damage - [NTSB UNK64X2211](https://openairdocs.org/ntsb/UNK64X2211), Jun 10, 1964: Convair CV-880 (N8813E), Newark, NJ, incident, minor damage - [NTSB UNK64X0101](https://openairdocs.org/ntsb/UNK64X0101), Jan 1, 1964: Convair CV-880 (N802TW), Boston, MA, substantial damage - [NTSB CHI63A0131](https://openairdocs.org/ntsb/CHI63A0131), Jan 1, 1963: Convair 880 (N819TW), Chicago, IL, substantial damage ## 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. - [Accident 19780525035549A](https://openairdocs.org/incident/19780525035549A), May 25, 1978: Cvac 22 (N8815E), Miami, FL, Substantial damage. A/c travelled 285FT into overrun fol abort tkof. Forward c/g exceelimit by 12.61 per cent mac. ## STCs that may be installed (OpenAirDocs) (43) 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 SA2534SW-D](https://openairdocs.org/stc/SA2534SW-D): Replacement of Switch assembly Int'l Inflatables Co. P/N 68748, with DME Corp. P/N L-140 in emergency evacuation slide lighting system. Astronics Luminescent Systems Inc - [STC SA2539SW-D](https://openairdocs.org/stc/SA2539SW-D): Replacement of light assembly, International Inflatables Co. P/N68555-1 with DME Corp. EL-104, EL-104A, and EL-104B in emergency slide lighting system. Astronics Luminescent Systems Inc - [STC SA863EA](https://openairdocs.org/stc/SA863EA): Incorporation of DME Corporation emergency evacuation slide lighting system. Astronics Luminescent Systems Inc - [STC SA1093SO](https://openairdocs.org/stc/SA1093SO): Installation of class 'B' or 'E' cargo compartment. Aeronautical Engineers, Inc - [STC ST768SO](https://openairdocs.org/stc/ST768SO): Installation of cargo loading door(forward L.H. side of fuselage). Aeronautical Engineers, Inc - [STC SA1072NW](https://openairdocs.org/stc/SA1072NW): Increase of zero fuel weight to131,000 pounds for aircraft complying complying with GD Convair strength and operating restrictions report ZS-22-300, Rev 3. This STC is limited to aircraft modified per STC Number SA1071NW. Lost Birds Aviation Historical Society & Museum - [STC SA1-562](https://openairdocs.org/stc/SA1-562): CJ805-3B modified as an alternate to CJ805-3 engine. Northeast Airlines Inc - [STC SA2728WE](https://openairdocs.org/stc/SA2728WE): Incorporation of Holcombe Industries HI-LITE SYSTEM P/N 50-1001 for emergency evacuation slide lighting. (707 AIRPLANES EQUIPPED WITH BOEING P/N 65-11685 AND 65-68862 FORWARD THRUST REVERSER DOORS). Maravia Corp of Idaho - [STC ST944SO](https://openairdocs.org/stc/ST944SO): Installation of (1) Class 'B' cargo compartment, (2) cargo restraining bulkhead, and (3) smoke detector system. STC ST906SO is a required part of this STC. (22M 880). Aeronautical Engineers, Inc - [STC SA2462SW](https://openairdocs.org/stc/SA2462SW): Installation of interior. Foster-Edwards Aircraft Co Inc - [STC SA152GL](https://openairdocs.org/stc/SA152GL): Installation of X band weather radome only on models with Convair22-71001-1 support assembly(bulk-head assembly). Norton Company, Performance Plactics - [STC SA2549WE](https://openairdocs.org/stc/SA2549WE): The installation of automatically deployable and automatically inflatable emergency exit slides. (22 CV-880). Intl Inflatables Co - [STC SA830CE](https://openairdocs.org/stc/SA830CE): Install Butler National Corporation flight recorder/ communications interface unit. Trans World Airlines Inc - [STC SA772CE](https://openairdocs.org/stc/SA772CE): Installation of Bendix P/N1978128-1 indicator and P/N1964771-3 inverter. Trans World Airlines Inc - [STC SA2341WE](https://openairdocs.org/stc/SA2341WE): Installation of battery-powered emergency exit lighting on forward and aft entry and service doors. Intl Inflatables Co - [STC SA593CE](https://openairdocs.org/stc/SA593CE): Modification of interior emergency lighting and installation of exterior emergency lighting system. (22 -1 (880)). Trans World Airlines Inc - [STC SA594CE](https://openairdocs.org/stc/SA594CE): Installation of dual low range radio altimeter system single equipment driving dual indicators. Trans World Airlines Inc - [STC SA279CE](https://openairdocs.org/stc/SA279CE): Fairchild cockpit voice recorder system. Trans World Airlines Inc - [STC SA214CE](https://openairdocs.org/stc/SA214CE): Autothrust system. Trans World Airlines Inc - [STC SA215CE](https://openairdocs.org/stc/SA215CE): Single SCAT system. Trans World Airlines Inc - [STC SA216CE](https://openairdocs.org/stc/SA216CE): Autopilot variable angle intercept. Trans World Airlines Inc - [STC SA217CE](https://openairdocs.org/stc/SA217CE): Second flight director system. Trans World Airlines Inc - [STC SA223CE](https://openairdocs.org/stc/SA223CE): Dual low range radio altimeter system. Trans World Airlines Inc - [STC SA241EA](https://openairdocs.org/stc/SA241EA): Nose cap weather radome shell. McMillan Radiation Labs Inc - [STC SA280CE](https://openairdocs.org/stc/SA280CE): Autothrust system equipment. Trans World Airlines Inc - [STC SA281CE](https://openairdocs.org/stc/SA281CE): Single SCAT system provisions. Trans World Airlines Inc - [STC SA281WE](https://openairdocs.org/stc/SA281WE): Engine-mounted fire detector system. Trans World Airlines Inc - [STC SA308WE](https://openairdocs.org/stc/SA308WE): Voice interruption priority system. Northrop Corporation - [STC SA336SO](https://openairdocs.org/stc/SA336SO): Cockpit voice recorder. Delta Airlines Inc - [STC SA376SO](https://openairdocs.org/stc/SA376SO): Relocation of LAS 109C flight recorder and installation of a remote accelerometer. Delta Airlines Inc - [STC SA389CE](https://openairdocs.org/stc/SA389CE): Eclipse-Pioneer 15470, 15492 and18729 autopilot amplifier. Trans World Airlines Inc - [STC SA390CE](https://openairdocs.org/stc/SA390CE): Eclipse-Pioneer 18729 autopilot amplifier. Trans World Airlines Inc - [STC SA484CE](https://openairdocs.org/stc/SA484CE): Relocation of Lockheed Aircraft Service Model 109CR flight recorder. Trans World Airlines Inc - [STC SA563CE](https://openairdocs.org/stc/SA563CE): Installation of static port heater system. Trans World Airlines Inc - [STC SA579EA](https://openairdocs.org/stc/SA579EA): Replace Bendix type 15866, 15897 and 19903 vertical gyros with Bendix type 19911 or 19912 ertical gyros. (22 -1 (880)). Trans World Airlines Inc - [STC SA671CE](https://openairdocs.org/stc/SA671CE): Install logo lights in upper leading edges of horizontal stabilizer. Trans World Airlines Inc - [STC SA687SW](https://openairdocs.org/stc/SA687SW): Nose cap weather radome shell. McMillan Radiation Labs Inc - [STC SA727CE](https://openairdocs.org/stc/SA727CE): Installation of Kollsman altitude alerting system. Trans World Airlines Inc - [STC SA896WE](https://openairdocs.org/stc/SA896WE): Rain repellent system. Jay- Dee Aircraft Supply Co - [STC SA91SO](https://openairdocs.org/stc/SA91SO): Modification of rotating field element G.E. 291C777G1 of G.E. 400 cycle alternator 2CM211A1. Peninsular Armature Works Inc - [STC ST402SO](https://openairdocs.org/stc/ST402SO): Modification of interior emergency lighting. Delta Airlines Inc - [STC ST403SO](https://openairdocs.org/stc/ST403SO): Installation of exterior emergency lighting system. Delta Airlines Inc - [STC ST422SO](https://openairdocs.org/stc/ST422SO): Installation of single radar altimeter system. (22M 880). Delta Airlines Inc ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Youngster 22](https://openairdocs.org/model/youngster-22): 0 registered aircraft, registry code 0560170 - [Ortmayer W R/Parson W H 2#2](https://openairdocs.org/model/ortmayer-w-r-parson-w-h-2-2): 0 registered aircraft, registry code 05628UY - [Wedell-Williams Air Service 22](https://openairdocs.org/model/wedell-williams-air-service-22): 0 registered aircraft, registry code 05632LQ - [Volmer Sportsman 22](https://openairdocs.org/model/volmer-sportsman-22): 0 registered aircraft, registry code 95702ZT --- 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.