N9812S - 1981 COMMANDER 980

1981

COMMANDER

980

95060

Used

N9812S

Records, Always U.S. Corp, NDH, Owned by AAI 925/750 hrs remaining (400 hr ext avail) 20% BELOW WHOLESALE! RECENT GEAR & PROPS O/H. Hots good until 5000, EFIS, Collins, Set up for Surveillance w/Camera mount & hole, Excellent Maint, Times &

4250.0

ENGINES: Left, 4250 Hr.T.T. HOT @ 2609 Hrs. Right, 4410 Hr.T.T. HOT @ 2771 Hrs.

Dowty-Rotol, 5 Year Inspection, complied with 01/2009

Dual King KY-196A Comms Bendix/King 2 Tube EFIS 40 System Dual Collins VIR 32 Navs IDC Encoding Altimeter w/Alerter. Dual Collins TDR-90 w/CTL 92 Control Head King/Bendix 90B GPS Collins DME 42A Indicator Collins 331A-3F w/ C-14A Compass King KR87 ADF King/Bendix KWX 56 Color Radar Collins AP-106 Autopilot w/Manuel turn controller. Argus 5000 Moving Map Honeywell GNS-X FMS WX-1000E Storescope King KNI-582 RMI

Emergency Locator Transmitter Over Board Relief Tube Davtron Digital Clock Cargo Tie Down Rings Heated Baggage Compartment Enviro ACM with Freon Air Pack

Overall Matterhorn White w/ Midnight Blue, Nordic Gray and Toreador Red Trim (2 new windscreen Installed 2/2005)

Special Mission, 3 Place Aerial Photography Conversion with 22" Camera Port

LANDING GEAR: 5 Year Inspection, complied with 12/2008 12-15 Yr. Airframe: Oct. 1993 DIMENSIONS/CAPACITES Wing Span 52.12ft Length 42.98ft Total Cabin & Baggage Volume 294 cu ft Cabin Volume Exc. Baggage Comp. 224 cu ft Baggage Compartment Vol./Load Limit 70 cu ft/600 lbs Maximum Cabin Pressure Differential 5.2 psi Maximum Ramp Weight 10,375 lbs Maximum Takeoff Weight (max. gross) 10,325 lbs Maximum Landing Weight 9,675 lbs Std. Empty Wt., Aircraft w/Residual Fluids 6,702 lbs* Useful load 3,367 lbs *Std. Empty Wt. Estimated new Wt. & Balance in process MISSION PROFILE 7 pax. & Baggage (1,400 lbs) Fuel to Full Gross Weight Average Equipped Aircraft Mission Distance (w/45-min reserve) 1,236 nm Cruise Alt. 31,000 ft, Time to Climb 17 min Cruise(MCrP) 292 kts, Total Time Enroute 4.5 hrs Takeoff Distance Ground Roll 1,299 ft POWER/PREFORMANCE Engines (2) AiResearch TPE-331-10-511K (733 SHP) Maximum Cruise (TAS @355 mph/309 kts 22K ft average cruise weight) Normal Cruise (TAS @ 18K ft 348 mph/303 kts MCrP. average cruise weight) Minimum Control Speed (IAS) 107mph/93 kts Stall Speed, Clean (CAS) 89 mph/77 kts Stall Speed, Gear & Flaps(CAS) 86 mph/75 kts L-R Cruise w/45-min reserve 287 mph/249 kts @ 31,000ft (standard fuel) 2,346 sm/2,040 nm H-S Cruise Range @ 31' K 339 mph/295 kts (standard fuel) 2,139/1,860 nm Twin-Engine Initial R.O.C. 2,777 fpm Single-Engine Initial R.O.C. 982 fpm Twin-Engine Service Ceiling 37,369 ft Single-Engine Service Ceiling 24,850 ft ALL SPECIFICATIONS SUBJECT TO INSPECTION AND VERIFICATION AIRCRAFT SUBJECT TO PRIOR SALE or REMOVAL FROM MARKET