N58AM - 1984 PIPER CHEYENNE IA
Aircraft Summary
General
Year
1984
Manufacturer
PIPER
Model
CHEYENNE IA
Serial Number
31-1104005
Condition
Used
Registration #
N58AM
Description
Aircraft available for showing in VENICE, FL AIRCRAFT HAS CHEYENNE 1A Mods GARMIN PANELl, ONE OF 17 CHEYENNE IA'S PRODUCED, AIRCRAFT DELIVERED WITH A FRESH EVENT 1 AND 2 contact: [email protected]
Airframe
Total Time
7500.0
Airframe Notes
7500 Hrs
PLEASE FEEL FREE TO CONTACT US ([email protected]) FOR PERFORMANCE SPECIFICATION INFORMATION ABOUT THIS INCREDIBLY EFFICIENT AIRCRAFT.
Engine Program
Engine Program Notes
3214/1850 SINCE OVERHAUL
1375/90 Since HOT
Two Pratt and Whitney (UACL) PT6A-11
rated at 500 shaft hp each
Engine 1
Engine 1 Time
3214
Engine 1 Time Since
SOH
Engine 2
Engine 2 Time
1750
Engine 2 Time Since
SOH
Avionics
Avionics/Radios
ADF: King KR-87 digital
Altimeter: King KEA-346 encoding
Autopilot: King KFC-250 IFCS w/yaw damper
Avionics Package: King KFC-250 IFCS / Garmin / Silver Crown
Communication Radios: Garmin GNS-530 / 430 Combination DME: King KN-63
Flight Director: King KFC-250 IFCS
Weather Radar: King KWX-56 color stabalized
GPS: Garmin GNS-530
HSI: King
LORAN: Apollo 800 Flybuddy
Navigation Radios: Garmin GNS-530 / King KN-53
Radar Altimeter: King KRA-10
RMI: King KI-229
RNAV: King KNS-81
TAWS: Garmin GNS-530
Transponder: DUAL GTX-330 GI-106A, DAC GDC-31
AVIDYNE TAS-620
Additional Equipment
Additional Equipment
Cargo door, tip tanks, nickel guide vanes, dual heated windshields, known icing system, cool start kit, auto ignition, ice protection plates, auxiliary electric heat, fire extinguisher, tinted windows, engine wash rings, speed stacks, tinted windows, RAM air cowlings, Dual heated windshields, Air conditioning, Intercom, Altitude capture & preselector, Garmin audio panel, King KI-204 GC/VOR/LOC indicator, fuel totalizer, ground clearance switch, Hobbs meter, copilot instruments
Exterior
Year Painted
2008
Exterior Notes
White with Black and Gold Stripes
Interior
Year Interior
2008
Number of Seats
7
Interior Notes
March 2008: Tan leather Interior
Modifications/Conversions
Modifications/Conversions
WEIGHTS
Maximum ramp weight 8,750 lbs. (3969 kg)
Maximum take-off weight 8,700 lbs. (3946 kg)
Maximum landing weight 8,700 lbs. (3946 kg)
Standard empty weight 5,110 lbs. (2318 kg)
(includes: unusable fuel, full operating fluids
and full oil)
Standard useful load 3,640 lbs. (1651 kg)
Maximum zero fuel gross weight 7,200 lbs. (3266 kg)
Inspection Status
Inspection Status
The information contained herein does not constitute any representation or warranty of either Mercury Aircraft Sales LLC or of the aircraft owner. Please rely on your own inspection of the aircraft to verify all aircraft specifications and descriptions (including, but not limited to, aircraft and engine times, installed equipment, and interior description). Any proposed transaction for the subject aircraft is contingent on execution of an aircraft purchase agreement acceptable in form and substance to the aircraft owner. The aircraft is subject to prior sale or removal from market.
Recommended For You
View All(Recommended For You)Aircraft.com does not own the rights to the images displayed on this site. We do not have information regarding the original seller or source of these images unless explicitly stated.


