# TCDS A7PC: Nomad TC Pty Ltd - Type: Type certificate data sheet - Status: Current - Holder: Nomad TC Pty Ltd - Revision: 6 - Revised: July 7, 2021 - Product: Aircraft, Small Airplane - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EC56E78130C479D28625870C0058BAB7.0001 - Page: https://openairdocs.org/tcds/A7PC ## Models (3) - N22B - N22S - N24A ## ADs (36) - [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 96-24-04](https://openairdocs.org/ad/96-24-04): Tailplane Stabilizer Center Section · Nomad TC Pty N22B, N22S and N24A. Effective Jan 17, 1997 - [AD 96-24-05](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 96-23-18](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 83-09-01](https://openairdocs.org/ad/83-09-01): Placard on Instrument Panel · Nomad TC Pty N24A. Effective May 16, 1983 - [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 - [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 --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.