STC SA2336SW

Idiriod £taw of Slmmr a Btpattment of ^Transportation —federal Sloiarion administration Supplemental 'Cgpe Certificate *-/C?6W&t«i>-«^ SA2336SW Brit tain Industries, Inc.

P. 0. Box 51370 Tulsa, Oklahoma 74151 «^^ 3 : gee Limitations and Conditions

- See Limitations and Conditions See Limitations and Conditions Civil Air ,1100:

Install Brittain Model B-12 AccuFlite System in accordance with Brittaln Industries, Inc. Master Drawing List 403-021-519 Revision I dated 3/21/84, or later FAA approved revision.

See Continuation Sheet, page 2 of this STC.

>•«/,>.« December 18, 1975 .: July 23, 1976 -tJs Lf.,& „**—'. 9/6/78; 11/10/81; 10/26/82;

11/21/83; 4/10/84 Revision 5_/*7*C- itf,tfttftfj/' ._(Signature) ~f~ Don F. Uatcoo *r, Aircraft Certification DivUionAirt jft

This itttifiiate may be transferred in acco'danct unih I-'AR 21.47.

FAAFoiw 8110-2 (1O-6SI

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number_ to (Name of transferee) (Address of transferee) (Number and street} (City, State, and ZIP code} from (Name of grantor)(Print or type) (Address of grantor) (Number & a treet) (City, State, and ZIP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink)

tinted £tatu of Bepartmtnt of 'Cransportation—JpEdctal Eolation administration Certificate(Continuation £heet) SA2336SW Revisions Limitations and Conditions:

1. FAA Approved Airplane Flight Manual 407-021-540 dated 7/23/76 Is required with Brittain B-12 Heading Select System.

2. FAA Approved Airplane Flight Manual 407-021-545 dated 7/23/76 is required with Brittain B-12 Heading Select System when used in conjunction with Brittain B-ll AccuTrak System OR FAA Approved Airplane Flight Manual 407-021-545 dated 7/23/76 revised August 4, 1978 is required with Brittain B-12 Heading Select System when used in conjunction with Brittain B-ll AccuTrak System.

3. This modification is eligible on aircraft listed on Master Airplane Eligibility List 426-021-519 Revision H, or later FAA approved revision.

4. Compatibility of this modification with other previously approved modification must be determined by the installer.

FAA FORM 8110-2-1 (10-B9) Tliii certificate may bt tiantjcrrtd in accordance with FAR 21.47.

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