# STC SA1753WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Vibration Isolation Products Corp, United States
- Description: Installation of VIP core assembly P/N VIP-106-18.
- Status date: September 16, 1986
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 2A5](https://openairdocs.org/tcds/2A5), TCDS LTC-13, [TCDS A-795](https://openairdocs.org/tcds/A-795), [TCDS 6A3](https://openairdocs.org/tcds/6A3), [TCDS 6A4](https://openairdocs.org/tcds/6A4), [TCDS A-781](https://openairdocs.org/tcds/A-781), [TCDS 6A6](https://openairdocs.org/tcds/6A6), [TCDS A-793](https://openairdocs.org/tcds/A-793)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A23E8CC34CE55BCF85256CC10083CFE3.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1753WE

## ADs that name it (0)

None.

## Approved models (10)

- Curtiss-Wright Corporation C-46/CW20-T ([TCDS 2A5](https://openairdocs.org/tcds/2A5))
- Lockheed Aircraft Corporation Navy PV-2 (TCDS LTC-13)
- Martin-Marietta Corporation 202 ([TCDS A-795](https://openairdocs.org/tcds/A-795))
- McDonnell Douglas Corporation DC-6 ([TCDS A-781](https://openairdocs.org/tcds/A-781))
- McDonnell Douglas Corporation DC-6A (Navy R6D-1) ([TCDS 6A3](https://openairdocs.org/tcds/6A3))
- McDonnell Douglas Corporation DC-6A (USAF C-118A) ([TCDS 6A3](https://openairdocs.org/tcds/6A3))
- McDonnell Douglas Corporation DC-6B (Navy R6D-1Z) ([TCDS 6A4](https://openairdocs.org/tcds/6A4))
- Tracor Flight Systems Inc. 240 Series ([TCDS A-793](https://openairdocs.org/tcds/A-793))
- Tracor Flight Systems Inc. 340 ([TCDS 6A6](https://openairdocs.org/tcds/6A6))
- Tracor Flight Systems Inc. 440 Military C-131E ([TCDS 6A6](https://openairdocs.org/tcds/6A6))

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