Sierra Industries, Ltd.
PMA PQ0544SW · 7 approved parts replacing 1 OEM number · Cessna, Textron Aviation, Inc.
| PMA part | Replaces | Name | Make / model | Status | On PartsAndPlanes | DLA paid (OEM no.) |
|---|---|---|---|---|---|---|
| As specified by drawings listed on Master Data List No. C25B-MDL-0038 for installation on S1610-100-2 | Modification Part | Cabin Entry Step Assy. Kit | Textron Aviation, Inc. 525, 525A, & 525B | Current, Dec 2019 | — | — |
| As specified by drawings listed on Master Data List No. C551-MDL-0041 for installation on S1610-100-1 | Modification Part | Cabin Entry Step Assy. Kit | Textron Aviation, Inc. 501, 551 | Current, Dec 2019 | — | — |
| As specified by drawings listed on Master Data List No. C560-MDL-0037 for installation on S1610-100-1 | Modification Part | Cabin Entry Step Assy. Kit | Textron Aviation, Inc. 500. 550, S550 & 560 | Current, Dec 2019 | — | — |
| As specified by drawings listed on Master Drawing List No. SI360-000-1 | Modification Part | Citation Eagle II Fj44-2a Engine Installation Kit | Cessna 500, 501 (See AML No. ST09559AC) | Current, Sep 2007 | — | — |
| As specified by drawings listed on Master Drawing List No. SI360-000-3 | Modification Part | Citation Stallion Fj44-2a Engine Installation Kit | Cessna 500, 501 (See AML No. ST09559AC) | Current, Sep 2007 | — | — |
| As specified by drawings listed on Master Drawing List No. SI440-000 for installation on SI440-100-1 | Modification Part | Artex C406 Series Elt Installation | Cessna 500, 501, 550, 551, S550 & 560 | Current, Feb 2010 | — | — |
| As specified by drawings listed on Master Drawing List No. SI440-000- for installation on SI440-100-2 | Modification Part | Artex C406 Series Elt Installation With Nav Interface | Cessna 500, 501, 550, 551, S550 & 560 | Current, Feb 2010 | — | — |
Sell any of these? List it free and this table names you, as does the page of every OEM number it replaces.
Source: the FAA PMA database, refreshed weekly. A PMA part is approved for the specific eligibility on its FAA record; whether it may be installed on a particular aircraft, engine or component is the installer's determination.