What it approves
Installation of Tricycle landing gear and revised nose assembly with optional radome.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
This Certificate issued to Southwestern Aero Exchange, Inc.
18502 East 108th Street, North Owasso, OK 74055 Part CAR 3 of the Civil Air Regulations.
A-765
BEECHCRAFT C-45G, C-45H, TC-45G, TC-45H & D-18S Description of Type Design Change: Installation of Tricycle Landing Gear and Revised Nose Assembly with Optional Radome in accordance with Volpar Drawing List No. 428.
Limitations and Conditions: If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. This approval of this change in type design applies basically to the Standard Beech Models C-45G & H, TC-45G & H, and D-18S only. This approval should not be extended to other specific airplanes of these models on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.
See Reverse Side for Additional Limitations for Applicability.
This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.
Date of application: May 25, 1961
Date of issuance: June 20, 1961
Date reissued: Jan. 23, 1998; Feb. 27, 2006
Date amended: Sep. 1, 1961; May 29, 1963
( Signature) Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office ( Title)
Number SA4-1531
LIMITATIONS OF APPLICABILITY (CONTINUED)
AD-53-6-3 is to be accomplished prior to installation of the new gear assembly.
All nose gear cylinder castings are to be inspected per Volpar “Quality Control Procedure Cylinder Casting P/N 309A” dated July 25, 1961.
Volpar Airplane Flight Manual Supplement dated September 1, 1961, is required as part of this modification.
The agency installing this STC Kit will provide an adequate weight and balance report with each modification.
The maximum gross weight of each airplane incorporating this STC must not exceed the FAA approved maximum gross weight for that particular model airplane listed in Aircraft Specification A-765. The airplane gross weight may be increased to 9800 pounds when the provisions of STC’s SA2-820 or SA4-1462 are incorporated. The approved C. G. ranges for airplanes incorporating this new landing gear are as follows:
(a) Maximum gross weight of 9300 pounds:
8600 pounds from station 107.0 to station 118.8 9300 pounds from station 109.8 to station 118.8.
linear variation between above weights.
(b) Maximum gross weight of 9800 pounds:
8600 pounds from station 107.0 to station 118.8 9800 pounds from station 111.7 to station 117.7 linear variation between above weights.
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ADs that name this STC · 4
An AD can apply because an STC is installed, or mention one in its text.