# STC SA3302SO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Whelen Aerospace Technologies, United States
- Description: Installation of fiberglass nose bowl.
- Applied: December 29, 1991
- Status date: January 24, 2023
- Product: Aircraft, Small Airplane
- Data sheets: [TCDS A1EA](https://openairdocs.org/tcds/A1EA)
- Certificate PDF: https://openairdocs.org/files/sha256/b0/ac/b0ac5c7037e8763fae64e354a728f8364d591679489d9e26a0c43be05e67d6bc
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179188671920230203213057.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3302SO

## ADs that name it (0)

None.

## Approved models (2)

- The New Piper Aircraft Inc. PA-30 ([TCDS A1EA](https://openairdocs.org/tcds/A1EA))
- The New Piper Aircraft Inc. PA-39 ([TCDS A1EA](https://openairdocs.org/tcds/A1EA))

## 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.

SA3302SO Whelen Aerospace Technologies 51 Winthrop Road Chester, CT 06412 Part 3 the Civil Air Regulations A1EA Piper PA-30/-39 Installation of two fiberglass nose bowls and two Hartzell propeller spinners or two fiberglass nose bowls with original equipment spinners or two Hartzell propeller spinners with original equipment nose bowls in accordance with LoPresti Speed Merchants Master Drawing List, Report No. 10, Rev "F", dated November 30, 1992, or later FAA approved revision.

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. (See continuation sheet 3 of 3) December 29, 1991 January 16, 2019; January 24, 2023 August 18, 1992 December 8, 1992; March 4, 1993 (for) Robert P. Capezzuto Acting Manager, Atlanta ACO Branch 3

SA3302SO 3

SA3302SO Date Reissued: January 24, 2023

Limitations & Conditions (Continued):

This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage. The turbocharged models must be equipped with the Rajay turbocharger in accordance with Rajay STC No. SA787WE.

--------------------END-------------------- 3 3

## Every issue (2)

- January 24, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/b0/ac/b0ac5c7037e8763fae64e354a728f8364d591679489d9e26a0c43be05e67d6bc)
- January 16, 2019: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/dd/e6/dde6e7294f2c382af3a115d7e279f8fffc51e0538736fba61e13de3246d8c869)

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