# STC SA108SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Pan Air Corporation, United States
- Description: Installation of Edo 289-2700 and 439-2705 amphibious floats.
- Applied: August 8, 1962
- Status date: March 22, 1967
- Product: Aircraft, Small Airplane
- Certification basis: Part 1, Part 21
- Data sheets: [TCDS 3A24](https://openairdocs.org/tcds/3A24)
- Certificate PDF: https://openairdocs.org/files/sha256/d5/41/d54140de88668a921483ab5a05f769ce0324b7edd0b2720287fe96ce189d68f1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6259617CA585875E86257D40006FC142.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA108SW

## ADs that name it (0)

None.

## Approved models (7)

- Cessna Aircraft Company 185 ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185A ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185B ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185C ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185D ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company A185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24))

## 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.

.federal 3toiation agency Supplemental t^uje Certificate SA108SW Pan Air corporation New Orleans, Louisiana Project A952SW-S r ^*W«'7't5^*^^ 3 v£west %*£&!*&( :$twia&&>n 3A21* Cessna 185, 185A, 185B, 185C, 185D, 185E, A185E Installation of Edo Model 289-2700 and ^39-2705 amphlbioua floats In accordance with Data Sheet PA-1 dated 10/15/62, Rev. 1, 11/15/62.

A.; In addition to placards required by I^pe Certificate Data Sheet No. 3A2U the following placards are required:

1. Identification and direction of landing gear controls (supplied by Mo ae part of float kits).

2. By water rudder control: "Water rudder up for take off and landing."

3. On instrument panel when amphibious floats are Installed: "Maximisn Design weight - 3000 Ibe."

dn0#(id^ ieA£ivte&/udJ&wdw SMvfnvnt&foeedei* s/f VXa&nau'.

August 8, 1962 November 21, 1962 March 22, 1967 Revision 1 (Signature) Glen W. Welsh Chief. Engineering and Manufacturing Branch( i ttte)

This cerlifiiale may be transferred m accordance with FAR21.47.

FOHM8110-2 [1-ftSl 0053-657-6000

The FAA will reissue the certificate in the name of the transferee and forward it lo him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) nd stiff!)

( City, Stair, and ZIP tud from (Nome of grantor) (Print or type) (Address of grantor) JSltmbfl and striel) (Csly, Slalt, an Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- March 22, 1967: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d5/41/d54140de88668a921483ab5a05f769ce0324b7edd0b2720287fe96ce189d68f1)

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