# N22NM: 1977 Government Aircraft Factories N22B

- Status: Valid registration
- Airframe: [Government Aircraft Factories N22B](https://openairdocs.org/model/government-aircraft-factories-n22b) (registry code 3880102, 14 seats)
- Engine: [Allison 250 SER 250HP](https://openairdocs.org/engine/allison-250-ser-250hp) (registry code 03003)
- Data sheets: [TCDS A7PC](https://openairdocs.org/tcds/A7PC) (Nomad TC Pty Ltd) (OpenAirDocs)
- Serial number: N22B61
- Year built: 1977
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: July 9, 1999
- Certificate issued: June 6, 2000
- Expires: August 31, 2027
- Mode S code: A1DFE0
- Registered owner: [Calypso LLC](https://openairdocs.org/faa-owner/CALYPSO%20LLC)
- Location: [Palm Beach Gardens, FL](https://openairdocs.org/faa-place/FL/Palm%20Beach%20Gardens)
- Owner type: LLC
- Owner's area on the map: 26.8457° N, 80.0874° W: Placed by OpenAirDocs at the center of ZIP code 33410, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=22NM
- Page: https://openairdocs.org/aircraft/N22NM

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): 30 in force

### Matched by airframe (Government Aircraft Factories N22B)

- [AD 2010-11-06](https://openairdocs.org/ad/2010-11-06): Wings · Nomad TC Pty N22B, N22S and N24A. Effective Jul 6, 2010
- [AD 2009-26-08](https://openairdocs.org/ad/2009-26-08): Flight Controls · Nomad TC Pty N22B, N22S and N24A. Effective Feb 1, 2010
- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005
- [AD 2005-10-24](https://openairdocs.org/ad/2005-10-24): Rudder control lever shafts · Nomad TC Pty N22B, N22S and N24A. Effective Jun 30, 2005
- [AD 2004-06-10](https://openairdocs.org/ad/2004-06-10): Rear Fuselage Bulkhead · Nomad TC Pty N22B, N22S and N24A. Effective Apr 28, 2004
- [AD 2004-05-02](https://openairdocs.org/ad/2004-05-02): Wing fittings · Nomad TC Pty N22B, N22S and N24A. Effective Apr 20, 2004
- [AD 2000-02-28](https://openairdocs.org/ad/2000-02-28): Airframe Pneumatic Deicing Boots · Nomad TC Pty N22B and N24A. Effective Mar 27, 2000
- [AD 98-04-18](https://openairdocs.org/ad/98-04-18): AFM - Limitations Section - Icing · Nomad TC Pty N22B and N24A. Effective Mar 13, 1998
- [AD 97-24-05](https://openairdocs.org/ad/97-24-05): Aft Wing Break Connectors · Nomad TC Pty N22B, N22S and N24A. Effective Jan 6, 1998
- [AD 97-11-11](https://openairdocs.org/ad/97-11-11): Horizontal Stabilizer · Nomad TC Pty N22B, N22S and N24A. Effective Jul 11, 1997
- [AD 97-10-10](https://openairdocs.org/ad/97-10-10): Upper Fin/Horizontal Stabilizer Fittings · Nomad TC Pty N22B, N22S and N24A. Effective Jul 3, 1997
- [AD 97-09-08](https://openairdocs.org/ad/97-09-08): Pilot/Co-pilot Control Wheels · Nomad TC Pty N22B, N22S and N24A. Effective Jun 23, 1997
- [AD 96-24-05](https://openairdocs.org/ad/96-24-05): Flap and Aileron Control Rod Fork Ends · Nomad TC Pty N22B, N22S and N24A. Effective Jan 17, 1997
- [AD 96-24-04](https://openairdocs.org/ad/96-24-04): Tailplane Stabilizer Center Section · Nomad TC Pty N22B, N22S and N24A. Effective Jan 17, 1997
- [AD 96-23-18](https://openairdocs.org/ad/96-23-18): Fuselage Stub Fin Plate · Nomad TC Pty N22B, N22S and N24A. Effective Dec 23, 1996
- [AD 91-02-08](https://openairdocs.org/ad/91-02-08): Airplane Electrical System · Nomad TC Pty N22B, N22S and N24A. Effective Feb 7, 1991
- [AD 86-16-01](https://openairdocs.org/ad/86-16-01): Sidewall Structure & Rudder Pedals Modification · Nomad TC Pty N22B and N24A. Effective Aug 28, 1986
- [AD 85-21-05](https://openairdocs.org/ad/85-21-05): Emergency Exit Door Trim · Nomad TC Pty N22B and N24A. Effective Nov 14, 1985
- [AD 82-16-11](https://openairdocs.org/ad/82-16-11): Instln Of Horizontal Stabilizer · Nomad TC Pty N22B. Effective Aug 12, 1982
- [AD 81-07-01 R1](https://openairdocs.org/ad/81-07-01-R1): Horizontal Stabilizer Modification · Nomad TC Pty N22B and N24A. Effective Jun 10, 1982
- [AD 82-12-04](https://openairdocs.org/ad/82-12-04): Combined Power Turbine and Propeller Governor Assembly · Cessna 401, 401A, 401B and 11 more. Effective Jun 7, 1982
- [AD 81-11-01](https://openairdocs.org/ad/81-11-01): Emergency Exit Door · Nomad TC Pty N22B, N22S and N24A. Effective May 13, 1981
- [AD 81-08-03](https://openairdocs.org/ad/81-08-03): Horizontal Stabilizer Structure · Nomad TC Pty N22B and N24A. Effective Apr 23, 1981
- [AD 81-01-02 R1](https://openairdocs.org/ad/81-01-02-R1): Fuel Valves · Nomad TC Pty N22B and N24A. Effective Jan 5, 1981
- [AD 80-17-01](https://openairdocs.org/ad/80-17-01): Rudder Control Torque Shaft · Nomad TC Pty N22B and N24A. Effective Aug 18, 1980
- [AD 80-13-07](https://openairdocs.org/ad/80-13-07): Aileron Control · Nomad TC Pty N22B and N24A. Effective Jul 6, 1980
- [AD 80-12-12](https://openairdocs.org/ad/80-12-12): Trim Tab Hinge · Nomad TC Pty N22B and N24A. Effective Jun 26, 1980
- [AD 80-12-09](https://openairdocs.org/ad/80-12-09): Rudder Trim Tab Control · Nomad TC Pty N22B and N24A. Effective Jun 23, 1980
- [AD 80-12-06](https://openairdocs.org/ad/80-12-06): Replace Structural Rivets · Nomad TC Pty N22B and N24A. Effective Jun 16, 1980
- [AD 80-11-10](https://openairdocs.org/ad/80-11-10): Hot Air Check Valve · Nomad TC Pty N22B and N24A. Effective Jun 5, 1980

### Matched by engine (Allison 250 SER 250HP)

None in force.

### Historical (superseded or no longer in force)

- [AD 2006-21-12](https://openairdocs.org/ad/2006-21-12) (historical): Supersedes AD 2003-22-13, to inspect ailerons. · AeroSpace Technologies Of Australia Pty N22B, N22S and N24A. Effective Nov 8, 2006
- [AD 2003-22-13](https://openairdocs.org/ad/2003-22-13) (historical): Ailerons · AeroSpace Technologies Of Australia Pty N22B and N24A. Effective Dec 23, 2003
- [AD 2003-14-20](https://openairdocs.org/ad/2003-14-20) (historical): Rudder control shafts · AeroSpace Technologies Of Australia Pty N22B and N24A. Effective Sep 8, 2003
- [AD 97-11-12](https://openairdocs.org/ad/97-11-12) (historical): Front Spar · AeroSpace Technologies Of Australia Pty N22B, N22S and N24A. Effective Jul 11, 1997
- [AD 82-12-06](https://openairdocs.org/ad/82-12-06) (historical): Rudder Control System · AeroSpace Technologies Of Australia Pty N22B and N24A. Effective Jun 17, 1982

## Information bulletins (advisory) (1 in force)

- [SAIB CE-05-32](https://openairdocs.org/saib/CE-05-32): . Issued Feb 11, 2005

## NTSB investigations

None matched to N22NM.

## FAA accident and incident reports

None matched to N22NM.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## STCs that may be installed (OpenAirDocs) (5)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Government Aircraft Factories N22B)

- [STC SA00674WI-D](https://openairdocs.org/stc/SA00674WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II system installation. Rockwell Collins Inc
- [STC SA00681WI-D](https://openairdocs.org/stc/SA00681WI-D): Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation. Rockwell Collins Inc
- [STC SA01306WI-D](https://openairdocs.org/stc/SA01306WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation. Rockwell Collins Inc
- [STC SP00400SE](https://openairdocs.org/stc/SP00400SE): Installation of various propeller electrical de-icer models. SMR Technologies
- [STC SA01141WI-D](https://openairdocs.org/stc/SA01141WI-D): Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94 Mode S Transponder System installation with CTL-92E control head. Rockwell Collins Inc

## Related

- Other Government Aircraft Factories N22B aircraft: https://openairdocs.org/model/government-aircraft-factories-n22b/aircraft.md
- The Allison 250 SER 250HP engine: https://openairdocs.org/engine/allison-250-ser-250hp.md

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