SA00736DE
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. Held by Pilatus Business Aircraft, which holds 16 approved modifications in all. Last revised October 25, 2011. System: flight controls.
What it applies to
- Kind of product
- Aircraft
- Design holder
- Pilatus Aircraft Limited; Pilatus Aircraft Limited; Pilatus Aircraft Limited
- Models
- PC-12, PC-12/45, PC-12/47
- Type certificates
- A78EU, A78EU, A78EU
- On this site
- Pilatus PC-12 1,441 registered
- The FAA's record
- On the FAA's site
What an approved modification is
A supplemental type certificate is the FAA's approval of a change to a certified design: a new engine or propeller, avionics, an autopilot, floats, a parachute, a larger fuel tank, an ice-protection kit. The company holding it may sell the kit and the paperwork to owners of the listed models; the modification then becomes part of that aircraft's record. The FAA's list says what was approved and for which models, not how many aircraft carry it.
Source: FAA supplemental type certificates (Dynamic Regulatory System). Register counts from the FAA register of October 8, 2026.