- Registered owners
- Department Of InteriorOffice Of Aviation Services
- Location
- Boise, ID
- Owner type
- Government
- Serial number
- 36219
- Year built
- 1998
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, transport
- Airworthiness date
- December 23, 1998
- Certificate issued
- May 21, 1999
- Expires
- May 31, 2027
- Mode S code
- A1DFFB
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 37
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1997 | 1 |
|---|---|
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 3 |
| 2002 | 1 |
| 2005 | 1 |
| 2007 | 2 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 2 |
| 2012 | 4 |
| 2013 | 6 |
| 2015 | 1 |
| 2018 | 2 |
| 2019 | 1 |
| 2020 | 4 |
| 2021 | 1 |
| 2022 | 6 |
| 2023 | 1 |
| 2024 | 3 |
| 2025 | 1 |
| 2026 | 1 |
See all 46 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N22PPMatched 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 Bell 412EP aircraft
FAA incident reports
No FAA accident or incident reports matched to N22PPMatched 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 Bell 412EP aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EGRR2009063082288Bearing · debondedPILOT REPORTED SEVERE LATERAL VIBRATION. ACFT LANDED, INSPECTED ROTOR HEAD AND FOUND BEARING COMPLETELY DEBONDED. INSTALLED NEW BRG PN 412-010-106-101 AND APPROVED ACFT FOR RETURNED TO SERVICE.SDR EGRR118893Mount · shearedDURING ROUTINE INSPECTION OF EXTERNAL HOIST NOTED BOLT PN NAS6204-54 SHEARED AT HEAD. THIS IS ONE OF THE (2) BOLTS SECURING THE HOIST ASSEMBLY TO THE HOIST SUPPORT ASSEMBLY. PERFORMED INSPECTION OF THE SECOND BOLT AND NOTED NO DEFECTS. REPLACED BOTH BOLTS WITSDR 20000710SH009Disc Pack · looseDISC TO FLANGE INTERFACE FOUND LOOSE DURING QUILL SEAL CHANGE. REPLACED BOTH DISC AND FLANGE WHICH WAS MEASURED AND FOUND BEYOND LIMITS. (X)SDR 20000710SH008Flange · looseDISC TO FLANGE INTERFACE FOUND LOOSE DURING ROTOR BRAKE QUILL SEAL CHANGE. REPLACED BOTH DISC AND FLANGE WHICH WERE MEASURED AND FOUND WORN BEYOND LIMITS. (X)
STCs that may be installed · 264
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 264 STCs