# STC SH2011CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Fuller Howard J Jr
- Description: Operation of rotorcraft on unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index (RON + MON)/2. Intermixing with aviation gasoline also approved.
- Status date: July 2, 2004
- Data sheets: H10WE, H10WE, H10WE
- Certificate PDF: https://openairdocs.org/files/sha256/d6/a1/d6a1fb4d8c768c0840cbc10041224990cbdf79c34bfcbc2ab2027339d3d9ab01
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F0D6B4B9C7B3FA9E86256EEB00527F0F.0001
- Page: https://openairdocs.org/stc/SH2011CE

## ADs that name it

None.

## Approved models (3)

- Robinson Helicopter Company R22 (TCDS H10WE)
- Robinson Helicopter Company R22 BETA (TCDS H10WE)
- Robinson Helicopter Company R22 MARINER (TCDS H10WE)

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Number SH2011CE This Certificate issued to Howard J. Fuller, Jr.

99 Boylston Circle Shrewsbury, MA 01545

Part 27 of the Federal Aviation Regulations.

Original Product Type Certificate Number : H10WE Make : Robinson

Model : R22, R22 Beta, R22 Mariner

Operation of rotorcraft on unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index (RON + MON)/2 per ASTM Specification D-439 as noted on placard to be installed in accordance with Petersen Drawing No. C718884, dated July 2, 1984, or later FAA-approved revision. Intermixing with aviation gasoline is also approved.

1. Limited to the following: R22 helicopters equipped with Lycoming 0-320-A2B or 0-320-A2C engines modified in accordance with STC SE1931CE. R22 Beta and R22 Mariner helicopters equipped with 0-320-A2C or 0-320-C2C engines installed in accordance with STC SH462NE and modified in accordance with STC SE1931CE.

2. Howard J. Fuller, Jr. Rotorcraft Flight Manual Supplement No. 003, rev. 2, dated July 2, 2004, or later FAA-approved revision is required and must be carried in the helicopter during all flights.

3. Compatibility of this design change with other previously approved modifications must be determined by the installer.

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.

Date of application : April 19, 1984

Date of issuance : August 10, 1984 Date reissued : October 17, 1984, April 15, 1985, May 23, 1990, May 7, 1991, July 2, 2004

Date amended : October 7, 1986

( Signature) Robert G. Mann Manager Boston Aircraft Certification Office

(Title)

## Every issue (1)

- July 2, 2004: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d6/a1/d6a1fb4d8c768c0840cbc10041224990cbdf79c34bfcbc2ab2027339d3d9ab01)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.