STC SA2091NM

Po Sette of menco Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA209 1N1 This certificate issued to: . Precise Flight, InC.

Purt 3 of the CiViI Ait Regulations.

Original Product - Type bertificate Number. ЗА 16 Make: Beech Mirded: 95-C55 Description of Type Design Change:

Installation of Precise Flight Speedbrake System in accordance with Precise Flight, Inc. DRC System Drawing No. PFI-95-C55 and DRC Speedbrake Installation Manual Report No. 110-55.

Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation in Beech 95-C55, Serial Number TE-21 only. A copy of this Certificate, Addendum No. SA209INM, and Precise Flight, Inc, Airplane Flight Manual Supplement, must be maintained as part of the permanent records for the modified aircraft.

April 27, 1983 Yale umended: May 24, 1984 FEDERAL AVIATION By Direction of the Administrator Helatinma (Signature) TOMINIST RAIDE Manager, Seattle Aircraft Certification Office

- (Title) 47 FAA FOR 8110-2 (10-68)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) May 24, 1984 c Number: SA209 INM Supplemental Type Certificate ADDENDUM NO. SA209 INM The conditions and limitations of the original Type Certificate 3A16 apply except as follows:

This Addendum, which is part of Supplemental Type Certificate No. SA209 INM, prescribes the conditions and limitations under which the STC was issued and meets the airworthiness requirements of the Civil Air Regulations.

Supplemental Type Certificate HOLDER: Precise Flight, Inc.

BEECH MODEL 95-C55 NORMAL CATEGORY, AS MODIFIED BY STC SA2091NM Serial Number: TE-21 only.

Equipment: Beech Owner's Manual or Pilot's Operating Handbook and AFMS for DRC System must be maintained in the airplane at all times.

Note 1: Current weight and balance report including list of equipment in the certified empty weight must be in the aircraft.

Note 2: In addition to the Placards and Markings required by Type Certificate Data Sheets 3A16, Note 2, apply the following:

The following placard is to be located at the circuit breaker panel:

SPEED BRAKE

(b) The following placard is to be on the left horn of the pilot's control wheel near the speedbrake control switch:

SPEED BRAKE PUSH TO DEPLOY (Continued on Page 4 of 4)

47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) May 24, 1984Number SA209 INM Supplemental Type Certificate ADDENDUM NO. SA209 INM

(c) If the standby vacuum system is installed, the following placard is to be in front and in full view of the pilot:

LEFT ENGINE ONLY

THIS AIRCRAFT IS EQUIPPED WITH THE PRECISE FLIGHT, INC. STANDBY VACUUM SYSTEM. REFER TO AFM OR PILOT'S

OPERATING HANDBOOK FOR OPERATING LIMITATIONS.

(d) The following placard is to be placed in front and in full view of the pilot:

DESCENT RATE CONTROL FOR OPERATING INSTRUCTIONS AND

LIMITATIONS - SEE SUPPLEMENT IN OWNER'S MANUAL OR PILOT'S OPERATING HANDBOOK.

Note 3: With the described DRC System installation, performance will be at least equal to or better than that given in the Owner's Manual or Pilot's Operating Handbook for the Beech airplane.

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