What it approves
Modification of the Aircraft
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.
FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:
Part Original Product – Type Certificate Number: Make:
Date of Application: D ate Reissued:
By Direction of the Administrator Signature Title of the Civil Air Regulations.
Textron Aviation (Formerly Beechcraft, or Hawker Beechcraft, or Raytheon Aircraft or Beech ) Jim Grigg Manager, Fort Worth ACO Branch Compliance & Airworthiness Division Aircraft Certification Service 3A15 General Aviation Modifications, Inc.
2800 Airport Road - Hanger A Ada, OK 74820 3 SA09881AC
3 E33A; E33C; F33A; F33C; G33; S35; V35; V35A; V35B; 35-C33A 36; A36; G36 Modification of the Aircraft in Accordance with General Aviation Modifications , Inc., Report 37-7560001, titled "Installation Instructions For Maximum Weight Increase on Textron (Beechcraft) 33, 35, and 36 Series Aircraft," Rev. None dated June 14, 2017, or later FAA approved revision.
1) FAA approved Airplane Flight Manual Supplement (AFMS) 37-6090001, Rev IR, dated 07/10/2018 or later FAA approved AFMS is required.
2) Instructions for Continued Airworthiness provided with the certified modifications installed by this STC should be used.
(continuation of page 3 of 3)
June 21, 2017 July 10, 2018
FAA Form 8110-2 (5/14) Page 2 of 3
To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):
SA09881AC
FAA Form 8110-2 (5/14) Page 3 of 3 Limitation and Conditions (continued):
3) The installation of this STC should not be incorporated to aircraft of these models in 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, are compatible. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.
4) The following propellers are authorized for installation on the Continental IO-550-B engine for this Weight Increase by either STC SA09852SC or SA09851AC.
McCauley: D3A32C409/82NDB model in the 80" to 78" diameter range or 3A32C406/82NDB model in the 80" to 78" diameter range D3A37C3401/C80MNF-1 model in the 79" to 76" diameter range
Hartzell: PHC-C3YF-1RF/F8468A-6R model in the 80" to 78" diameter range or PHC-C3YF-1RF/F8068 model in the 82" to 78" diameter range.
5) The Models and Gross Weight Combinations listed below are authorized in the "Normal Category"
S35, V35, V35A, V35B Gross Wt. 3571 lbs AFMS 37-6090001
35-C33A, E33A, E33C, F33A, Gross Wt. 3600 lbs AFMS 37-6090001 F33C, G33
36, A36, (S/N E-1 thru E2110 except E-1946 and E-2104) Gross Wt. 3850 lbs AFMS 37-6090001
A36, G36 (S/N E-1946, E-2104, E-2111 and subsequent) Gross Wt. 3900 lbs AFMS 37-6090001
Certification Basis:
Certification Basis is per the certified modifications installed by this STC.
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SA09881AC
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 11
| Make | Model | Data sheet |
|---|---|---|
| Textron Aviation Inc. | 35-C33A | 3A15 |
| Textron Aviation Inc. | 36 | 3A15 |
| Textron Aviation Inc. | A36 | 3A15 |
| Textron Aviation Inc. | E33A | 3A15 |
| Textron Aviation Inc. | E33C | 3A15 |
| Textron Aviation Inc. | F33A | 3A15 |
| Textron Aviation Inc. | F33C | 3A15 |
| Textron Aviation Inc. | G33 | 3A15 |
| Textron Aviation Inc. | G36 | 3A15 |
| Textron Aviation Inc. | S35 | 3A15 |
| Textron Aviation Inc. | V35 | 3A15 |