- Registered owner
- Triple Nickel Inc
- Location
- Muleshoe, TX
- Owner type
- Corporation
- Serial number
- 60-8265006
- Year built
- 1982
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- February 22, 1982
- Certificate issued
- September 27, 2025
- Expires
- September 30, 2032
- Mode S code
- ABC54A
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming IO-540 model are included below.
On this page
Airworthiness directives that may apply · 65
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1963 | 1 |
|---|---|
| 1964 | 1 |
| 1966 | 1 |
| 1967 | 1 |
| 1969 | 2 |
| 1973 | 1 |
| 1975 | 1 |
| 1977 | 2 |
| 1978 | 2 |
| 1979 | 1 |
| 1981 | 1 |
| 1982 | 1 |
| 1983 | 2 |
| 1987 | 2 |
| 1988 | 2 |
| 1989 | 2 |
| 1990 | 1 |
| 1992 | 1 |
| 1993 | 1 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 3 |
| 1997 | 2 |
| 1998 | 3 |
| 1999 | 2 |
| 2001 | 1 |
| 2002 | 3 |
| 2003 | 4 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 4 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 2 |
| 2011 | 1 |
| 2012 | 3 |
| 2015 | 2 |
| 2017 | 1 |
| 2021 | 1 |
| 2022 | 2 |
| 2023 | 1 |
| 2024 | 1 |
| 2026 | 2 |
Airframe · Piper PA-60-602P
AD 2023-09-09Exhaust Turbine System (Recip)AD 2022-03-15Fuel Quantity IndicatorAD 2020-24-10Flight ControlsInformation bulletins that may apply · 15
Advisory, not mandatory.
Airframe · Piper PA-60-602P
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-03-55Engine · Lycoming IO-540 series
SAIB NE-19-08Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve CylindersNTSB investigations
No NTSB investigations matched to N858CHMatched 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 Piper PA-60-602P aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 20010402CW001Magneto · brokenRT ENGINE, LT MAGNETO POINT CAM FOLLOWER ARM BROKE AFTER 124.9 HOURS USE. MAGNETO OVERHAULED. INSTALLED 6-2-99 AT 2180.1 HOURS. FAILED AND REMOVED AT 2305.0 HOURS.SDR 20010402CW002Manifold · malfunctionedON LT ENGINE START, RED INDICATOR BUTTON RETRACTED, GAGE DROPPED TO ZERO. PNEUMATIC PUMP SUPPLIED PRESSURE BUT ON PRESSURE WAS GETTING TO GYRO FLIGHT INSTRUMENTS, DOOR SEALS, GYRO PRESSURE REGULATOR OR PRESSURE GAGE. RIGHT ENGINE SHOWED NORMAL INDICATOR ANDSDR 20010402CW004Buckle · defectiveON BACK SIDE OF ALL SEAT BELT BUCKLES, LATCH PART, CRACKS AT EACH CORNER OF BELT ATTACH SLOT. PROBABLE CAUSE- MANUFACTURING- JOGGLE TOO SEVERE FOR ALUMINUM BECAUSE CRACKS APPEAR AT EACH JOGGLE.SDR 97ZZZX3789Washer · wornDURING C/W SB 600-131, SUBSTANTIATED BOTH SCAVANGE OIL PUMPS WERE DUE IMMINENT FAILURE. REPLACED PARTS REQUIRED.
STCs that may be installed · 266
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Piper PA-60-602P
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