# STC SA00736DE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Pilatus Business Aircraft, United States
- Description: This Supplemental Type Certificate authorizes autopilot-coupled RNAV (GPS) approaches to LPV and LNAV/VNAV minima when there is a functioning Pilatus option radar altimeter installed and the aircraft verified to meet the requirements of  Pilatus Business Aircraft Installation Instructions Document No. P25-486-007 Revision IR, dated August 15, 2011, FAA approved October 25, 2011, or later FAA approved revision.
- Applied: March 8, 2011
- Status date: October 25, 2011
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A78EU](https://openairdocs.org/tcds/A78EU)
- Certificate PDF: https://openairdocs.org/files/sha256/55/a0/55a08a78239d16de890ff13bf4cce38e3a445029552dd7efa1e24bf3e1041690
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5DCB8A512F699BBC86257973005853A0.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00736DE

## ADs that name it (0)

None.

## Approved models (3)

- Pilatus Aircraft Limited PC-12 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU))
- Pilatus Aircraft Limited PC-12/45 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU))
- Pilatus Aircraft Limited PC-12/47 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU))

## 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.

Number SA00736DE This certificate, issued to Pilatus Business Aircraft 11755 Airport Way Broomfield, Colorado 80021 Part 23* of the Federal Aviation Regulations.*Certification Basis is set forth in Type Certificate Data Sheet A78EU Original ProductType Certificate Number: A78EU Make: Pilatus Model: PC-12, PC-12/45 & PC-12/47 Serial Numbers 101 thru 888, excluding 545 Description of the Type Design Change:

This Supplemental Type Certificate authorizes autopilot-coupled RNAV (GPS) approaches to LPV and LNAV/VNAV minima when there is a functioning Pilatus option radar altimeter installed and the aircraft verified to meet the requirements of Pilatus Business Aircraft Installation Instructions Document No. P25-486-007 Revision IR, dated August 15, 2011, FAA approved October 25, 2011, or later FAA approved revision.

1. Flight Manual Supplement, Document Number P25-486-003, Revision IR, dated October 17, 2011, or later FAA approved revision is required for this installation.

2. This STC is only applicable to Pilatus PC-12, PC- 12/45 and PC-12/47 aircraft S/Ns 101 through 888 excluding 545 which have been previously modified by installation of Honeywell STC SA01524WI-D (Installation of alternate Honeywell part number EFS 40/50 SG 465 Symbol Generator) and Garmin AML STC SA01933LA (Installation of Garmin Model 400W/500W Series GPS-WAAS Navigation System).

3. A copy of this certificate must be maintained as a part of the permanent records for the modified aircraft.

4. Compatibility of this des ign change with previously approved modifications must be determined by the installer.

5. If the holder agrees to permit another person to use this cert ificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of application: March 08, 2011 Date reissued:

Date of issuance: October 25, 2011 Date amended:

Todd G. Dixon (Signature), Manager Northwest Mountain Region Denver Aircraft Certification Office (Title)

## Every issue (1)

- October 25, 2011: Issued, Current. [certificate](https://openairdocs.org/files/sha256/55/a0/55a08a78239d16de890ff13bf4cce38e3a445029552dd7efa1e24bf3e1041690)

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