Griggs Aircraft Refinishing

STC Archive

SA00030NY

Cessna P210N. Installation of freon-type electric motor driven air conditioning system in P210N, modified with STC SA1003NE installation of RR 250-B17F/2.

STC #
Issued
Modified
Reissued
SA00030NY
8/18/1993
-
6/22/2016

SA515NE

Cessna 210L/T210L, 210M/T210M, 210N/T210N, & 210R/T210R. Config 1: install 18 gal. aft baggage compartment auxiliary fuel tank. Config 2: install 28 gal. aft baggage compartment auxiliary fuel tank.

STC #
Issued
Modified
Reissued
SA515NE
5/20/1987
-
6/22/2016

SA532NE

Cessna P210N & P210R. Installation of 29.7 gal. aft baggage compartment auxiliary fuel tank and fuel transfer system.

STC #
Issued
Modified
Reissued
SA532NE
9/18/1987
-
6/22/2016

SA540NE

Gulfstream AA-5, AA-5A, & AA-5B. Installation of aft baggage compartment 18 gal. auxiliary fuel tank and transfer system.

STC #
Issued
Modified
Reissued
SA540NE
10/14/1987
-
6/22/2016

SA615NE

Cessna 172F, G, H, I, K, L, M, N, P, & Q. Installation of 18 gal. auxiliary fuel tank in the aft baggage compartment along with fuel transfer system.

STC #
Issued
Modified
Reissued
SA615NE
10/18/1988
6/12/1989
6/22/2016

SA00606NY

Cessna 210/T210L, 210M/T210M, 210N/T210N, 210R/T210R, P210N, & P210R. Installation of low fuel warning device.

STC #
Issued
Modified
Reissued
SA00606NY
4/17/1997
12/15/1998
6/22/2016

SA846NE

Cessna 182A, B, C, & D. Installation of 18 gal. auxiliary fuel system in aft baggage compartment.

STC #
Issued
Modified
Reissued
SA846NE
4/19/1991
-
6/22/2016

SA1003NE

Cessna P210N, 210L/T210L, 210M/T210M, & 210N/T210N. Installation of Rolls-Royce (Allison) 210-B17F turboprop engine (450HP) and Hartzell HC-B3TF-7A/79212NK-2 propeller.

STC #
Issued
Modified
Reissued
SA1003NE
9/9/1992
11/11/2011
6/22/2016

SA1035NE

Cessna 150F, G, H, J, K, L, M, & 152. Installation of 14.6 gal. aft fuselage fuel tank in baggage compartment.

STC #
Issued
Modified
Reissued
SA1035NE
1/13/1993
5/31/1994
6/22/2016

SA1161SW

Piper PA-31, PA-31-325, & PA-31-350. Installation of 27 gal. auxiliary fuel tank in each nacelle (wing locker).

STC #
Issued
Modified
Reissued
SA1161SW
6/21/1970
8/16/2002
6/22/2016

SA01194NY

Cessna 210L/T210L, 210M/T210M, 210N/T210N, & 210R/T210R. Installation of a freon-type electric motor driven air conditioning system.

STC #
Issued
Modified
Reissued
SA01194NY
4/18/2000
-
6/22/2016

SA1305SW

Piper PA-31, S/N 31-2 and up. Installation of 26 gal. auxiliary fuel tank in each wing nacelle.

STC #
Issued
Modified
Reissued
SA1305SW
5/10/1971
1/21/1982
6/22/2016

SA2205SW

Piper PA-34-200T, PA-34-220T. Installation of 15 gal. auxiliary fuel cell in each engine nacelle.

STC #
Issued
Modified
Reissued
SA2205SW
7/2/1975
1/29/1993
6/22/2016

SA2277CE

Mooney M20F, M20J. Installation of fuel bladder cells in wing fuel cavities (3 configurations).

STC #
Issued
Modified
Reissued
SA2277CE
9/11/1987
12/22/2003
6/22/2016

SA2350CE

Mooney M20C, M20D, M20E, & M20G. Installation of fuel bladder cells in wing fuel cavities (3 configurations).

STC #
Issued
Modified
Reissued
SA2350CE
1/21/1988
12/22/2003
6/22/2016

SA2504CE

Cessna 310K through 310R, T310P, T310Q, & T310R. Installation of wing nacelle locker tanks and fuel transfer system.

STC #
Issued
Modified
Reissued
SA2504CE
7/28/1989
-
6/22/2016

SA2513CE

Cessna 320D, 320E, 320F, 340, & 340A. Installation of wing nacelle locker tanks and fuel transfer system.

STC #
Issued
Modified
Reissued
SA2513CE
7/28/1989
-
6/22/2016

SA2514CE

Cessna 401, 401A, 401B, 402, 402A, 402B, 411, 411A, 414, 421, 421A, 421B, & 421C. Installation of wing nacelle locker tanks and fuel transfer system.

STC #
Issued
Modified
Reissued
SA2514CE
7/28/1989
-
6/22/2016

SA03389NY

Beechcraft A36, A36TC. Installation and maintenance of O&N Aircraft Modifications bleed-air heated inlet (P/N 4505-1) on Beechcraft A36, A36TC with Rolls-Royce 250 B17/F2 engine.

STC #
Issued
Modified
Reissued
SA03389NY
5/8/2014
-
6/22/2016

SA3753NM

Cessna P210N, 210K/T210K, 210L/T210LO, 210M/T210M, & 210N/T210N. Installation of stiffening rubs in the aileron and rudder surfaces and redistribution of mass balance in the aileron, rudder, and elevator surfaces.

STC #
Issued
Modified
Reissued
SA3753NM
12/9/1987
-
6/22/2016