# STC SA2908WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: HydroAire Division of the Crane Co, United States
- Description: Installation of fuel tank boost pump.
- Status date: February 16, 1998
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A14CE](https://openairdocs.org/tcds/A14CE)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/31428D14B7B9B9E085256CC20008CA98.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2908WE

## ADs that name it (0)

None.

## Approved models (7)

- Raytheon Aircraft Company 100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Raytheon Aircraft Company 99 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Raytheon Aircraft Company 99A(FACH) ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Raytheon Aircraft Company A100 (U-21F) ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Raytheon Aircraft Company A99 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Raytheon Aircraft Company A99A ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Raytheon Aircraft Company B99 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))

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