# STC SA219RM

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Rocky Mountain Airways, United States
- Description: Installation of two quick-removal poles in left side of aft baggage compartment to separate skis from baggage.
- Applied: January 6, 1981
- Status date: December 8, 1981
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A20EA](https://openairdocs.org/tcds/A20EA)
- Certificate PDF: https://openairdocs.org/files/sha256/82/36/823616225738bc7fc9e57429ad439083048e37814ab538874f5da974b2d18764
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/848CD8DC3EED26F285256CC200015AEF.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA219RM

## ADs that name it (0)

None.

## Approved models (5)

- Viking Air Limited DHC-7-1 ([TCDS A20EA](https://openairdocs.org/tcds/A20EA))
- Viking Air Limited DHC-7-100 ([TCDS A20EA](https://openairdocs.org/tcds/A20EA))
- Viking Air Limited DHC-7-101 ([TCDS A20EA](https://openairdocs.org/tcds/A20EA))
- Viking Air Limited DHC-7-102 ([TCDS A20EA](https://openairdocs.org/tcds/A20EA))
- Viking Air Limited DHC-7-103 ([TCDS A20EA](https://openairdocs.org/tcds/A20EA))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration T680Cm-s Supplemental Type Certificate Number: SA219RM This certificate issued to: Rocky Mountain Airways, Hangar 6, Stapleton Int'1 Airport Denver, Colorado 80207 Purt 25 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: A20EA Make: DeHavilland Model: DHC-7 Series Description of Type Design Change:

Installation of two quick-removal poles in left side of aft baggage compartment to separate skis from baggage in accordance with Rocky Mountain Airways' drawing number RM-101 FAA Approved December 8, 1981 or later FAA approved revision.

This approval should not be extended to other aircraft of this model on which n other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of thosen other previously approved modifications will introduce no adverse effect uponn the airworthiness of the aircraft.

Date of Application: January 6, 1981 Pule reissued:

Date of Issuance: December 8, 1981 Jale umended:

FEDERAL AVIATION By Direction of the Administrator hark c. Buldn Mark E. Baldwin (Signature) TO MINISTRATION Chief, Engineering and Manufacturing Branch, ARM-210 ( Title)

## Every issue (1)

- December 8, 1981: Issued, Current. [certificate](https://openairdocs.org/files/sha256/82/36/823616225738bc7fc9e57429ad439083048e37814ab538874f5da974b2d18764)

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