Airframe:
Total Time: 6,562
Total Landings: 5,931

Engines:
PRATT & WHITNEY JT15D-5D
Time: 6501
Cycles: 5855
TBO: 3500

Honeywell Primus 1000 – 3 Tube EFIS
 EFIS: Dual 8x7” PFDs and one 8x7” MFD
 COMMUNICATIONS: (2) Honeywell RCZ-851F
 HF RADIO: Honeywell KHF-950
 NAVIGATION: (2) Honeywell RNZ-850
 FLIGHT DIRECTOR: Honeywell Primus-1000
 AUTOPILOT: Honeywell Primus-1000 Flight Control
 RADAR: Honeywell Primus-660 Color Weather
 TRANSPONDER: (2) Honeywell Transponders
 AUTOMATIC DIRECTION FINDER: (2) Honeywell RNZ-850
 AIRBORNE DISTANCE MEASURING EQUIPMENT: (2) Honeywell RNZ-850
 RMI: (2) Honeywell RM-850 RMI
 TRAFFIC COLLISION AND AVOIDANCE SYSTEM: TCAS II-CAS-67A
 TAWS: Honeywell EGPWS
 FLIGHT MANAGEMENT SYSTEM: Universal UNS-1ESPW
 EMERGENCY LOCATOR TRANSMITTER: Artex C406-N ELT (3 frequencies)
 COCKPIT VOICE RECORDER: A200S (30 minutes)

2009
Sturgis Aviation, Inc

2009
Forward Cabin: Right hand single seat across from Deluxe left side Refreshment Center with hot liquid dispenser, ice drawer, food storage and trash drawer.

Mid Cabin: Four place club arrangement with left hand folding table.

Aft Cabin: Two single seats facing forward.

Aft Lavatory Area: The aircraft is equipped with a belted lav.

USB Charging Ports installed

Phase 1 Inspection 10/26/2022 @ 6,346 Hours 10/2024
Phase 2 Inspection 10/26/2022 @ 6,346 Hours 10/2024
Phase 3 Inspection 10/26/2022 @ 6,346 Hours 10/2024
Phase 4 Inspection 10/26/2022 @ 6,346 Hours 10/2024
Phase 5 Inspection 05/26/2022 @ 6,269 Hours 05/2025