- Registered owner
- Ryan Air Inc
- Location
- Anchorage, AK
- Owner type
- Corporation
- Serial number
- 219
- Year built
- 1998
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- July 22, 1998
- Certificate issued
- October 2, 2026
- Expires
- October 31, 2033
- Mode S code
- A1DC39
Pilatus PC-12/45TCDS A78EUAirframe · Pilatus PC-12/45TCDS E26NEEngine · Pratt & Whitney Canada PT6A-66 series
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PT6A-66 model are included below.
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Airworthiness directives that may apply · 53
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1997 | 2 |
|---|---|
| 1998 | 9 |
| 1999 | 6 |
| 2000 | 4 |
| 2001 | 3 |
| 2002 | 4 |
| 2003 | 5 |
| 2004 | 3 |
| 2005 | 6 |
| 2006 | 2 |
| 2007 | 2 |
| 2008 | 3 |
| 2009 | 3 |
| 2012 | 1 |
| 2013 | 2 |
| 2014 | 1 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2020 | 1 |
| 2022 | 2 |
| 2023 | 2 |
| 2024 | 2 |
| 2026 | 1 |
See all 68 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N219PCMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Pilatus PC-12/45 aircraft
FAA incident reports
No FAA accident or incident reports matched to N219PCMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Pilatus PC-12/45 aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR UATA2025110300701Skin · wornTOP RUDDER STATIC WICK BASE DAMAGED (MAJOR REPAIR). REPLACED DAMAGED SKIN, SEE FORM 337 DATED 10/27/25 FOR FURTHER DETAIL. INSTALLED NEW STATIC IS CHARGE BASE P/N: 984.78.81.409 AND STATIC WICK UPPER RUDDER STATIC WICK ATTACH HOLES WORN BEYOND REPAIR LIMITS. RSDR 2020F00429Drag Link · brokenDURING CRUISE, THE LANDING GEAR RETRACT/EXTEND ACTUATOR HORN BROKE OFF THE UPPER DRAG LINK ASSEMBLY, RENDERING THE NOSE LANDING GEAR INOPERATIONAL WITH REGARDS TO HYDRAULIC PRESSURE. THIS LED TO AN UNCONTROLLED EXTENSION OF THE NOSE LANDING GEAR TO THE DOWN-ASDR 2009FA0000277Wire Harness · mismanufacturedBOTH PILOT AND CO-PILOT AIRSPEED INDICATORS DECREASED IN AIRSPEED INDICATION FROM 200 KTS TO 0 KTS AT RATE OF APPROX 4 KTS PER MIN. NOTICED WHEN VOLTMETER PROBE WAS ATTACHED TO CIRCUIT BREAKER LOAD SIDE, THAT THE WIRE ATTACHED TO THE RING TERMINAL OF THE LOA
STCs that may be installed · 162
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Pilatus PC-12/45
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller