C-FGZQ - 1979 CESSNA 340A

1979

CESSNA

340A

340A-0670

C-FGZQ

Used

*PRICE REDUCED $40K USD!!* Please contact Eldon for more information: 780-975-8598 1979 Cessna 340A - C-FGZQ SN: 340A0670 TTAF: 3,593 Engines: TSIO-520NB – 1600 TBO LH: Overhauled 14 May 2011 – 400.0 hrs SMOH – 1290.0 hrs TBO RH: Overhauled 24 Jun 2011 – 400. hrs SMOH – 1290.5 hrs TBO Props: McCauley 3AF32C93 – 10 years /1200 hrs TBO Both overhauled 30 Jan 2009 – 494.5 hrs SMOH – 705.5 hrs TBO Heated, Syncrophased Avionics / Radios: Garmin 340 Radio Panel NAV/COM 1 = Garmin 530W (GPS/WAAS/VHF/VOR/ILS) NAV/COM2 = Cessna ARC RT-485A (VHF/VOR/ILS) WX-1000 Stormscope Weather Mapping System Cessna ARC AA801A Altitude Alerter Cessna ARC 400 ADF (primary, secondary) Cessna ARC IN404A RMI Terra TRI 20 Radar Altimeter Cessna ARC 400 Mode C transponder Cessna ARC 400 Nav-o-Matic Autopilot with Altitude Hold Cargo: Nose: 350 lbs Cabin: 340 lbs Lockers: 40 lbs each (reduced capacity due to wing locker fuel tanks) Weight: Empty: 4440 lbs MTOW: 6290 lbs (1850 lbs useful) MLdgW: 5990 lbs Weight and balance 3 Sep 2010 (weight 4439.14 lbs, arm 152.97”, moment 679,071.05 Fuel: Main (tip): 50 gal each (100 gal / 600 lbs) Aux: 31.5 gal each (63 gal / 378 lbs) Locker: 20 gal each (40 gal / 240 lbs) Total: 203 gal / 1218 lbs Certified for flight into known icing Aircraft is subject to verification of specifications, logs, times, damage and all equipment listed.

3593.0

C-FGZQ 1979 C340A S/N: 340A0670 Pilot / Co-pilot plus 5 passengers Equipment -Mode C transponder -Garmin 530W GPS (WAAS) -Autopilot with Altitude Hold -2 x VOR -2 x ADF -2 x VHF Normal Cruise 180 KTAS @ 180 pph / 30 gph Full Fuel Endurance: 6.5 hours (Full Fuel including wing locker tanks) Engines: TSIO-520-NB 310 hp @ 2700 RPM -Maintains sea-level horsepower to 16,000’ -Main Tanks: 50.0 gal each -Aux Tanks: 31.5 gal each -Locker Tanks: 20.0 gal each -Total: 203 gal (1218 lbs) -Empty: 4440 lbs -MTOW: 6290 lbs -MLdgW: 5990 lbs -Aft Cabin Baggage 340 lbs * STC for 7th seat used with child car seat -Nose Baggage Area 350 lbs -Wing Locker Baggage 40 lbs each -Max alt w/o O2 23,500’ -Max alt with O2 30,000’ -Vne 235 KIAS -Vno 200 KIAS -Va 155 KIAS -15 deg flap 160 KIAS -15 – 45 deg flap 140 KIAS Vle 140 KIAS Vmca 72 KIAS Vyse 100 KIAS Vr 91 KIAS Fuel System Main tip tanks: 50 gal useable Cross-fed for emergency use -Vapor and excess fuel from engines are returned to main tanks -AUX pumps supply fuel for priming and start, and backup for engine-driven pumps -Continuous tip tank transfer pump ensures availability of all tip tank fuel to engine supply line during high angles of descent Aux tanks: 31.5 gal useable -Located outboard of each engine nacelle -Feeds each engine directly -Vapor and excess fuel fed to main tanks -Aux tanks are vented into main tanks Wing locker fuel tanks: (C-FGZQ) 20 gal useable -Pumped directly to main tanks with a fuel transfer pump -Annunciator illuminates once wing locker tank completely transferred to mains AUX fuel pumps: -Located in main tanks for priming and starting -LOW runs pump at low speed (5.5 PSI) for vapor clearing and purging -ON runs pump at low speed if engine-driven pumps are functioning. If engine-driven pump fails, AUX pump runs at high speed automatically and provides sufficient fuel for all engine operations including emergency T/O Electrical System -28 volt system powered by 100 ampere engine-driven alternator on each engine -Each alternator has own regulator and over-voltage protection relay -One 24 volt battery located in left wing outboard of the engine nacelle Landing Gear -Electrically operated fully retractable system with steerable nose wheel -Safety switch on left shock strut prevents accidental retraction as long as aircraft weight compresses the strut C-FGZQ certified for known icing Prop De-Ice System -Electrically-heated boots on prop blades -2 heating elements; inboard and outboard each blade -Timer directs current to prop boots in cycles between elements and blades to reduce power drain -Fluctuation on de-ice ammeter indicated normal operation -System must be left ON for 2.5 min to check all heating elements on both props Windshield De-Ice System -Electric de-ice heat panel on pilot side. Pressurization System -Acft may be operated in either Pressurized or Ram Air mode. -Pressurization provided the engine turbocharger through the sonic venture (flow limiter), heat exchanger, and then into the cabin. -Smooth power changes will prevent sudden pressure changes -Two (L/R) push-pull controls each have 2 positions: -Pressurize (IN) -pressurization air enters the cabin -Dump (OUT) -pressurization air is expelled overboard prior to entering the cabin -only select dump if contaminated pressurization is suspected -CABIN ALT annunciator illuminates at approx 10,000’ cabin alt -Cabin altitude reaches 10,000’ at approx 23,500’ and CABIN ALT annunciator illuminates -Px diff of 4.2 PSI is limited by the pressure regulator valve at aft of cabin Heating, Ventilation and Defrosting System -System: air inlet in the nose, cabin fan, gasoline combustion heater, heat exchange selector and heat outlets in the cabin -WEMAC blower supplies unheated ventilating air when WEMAC BLOWER is set to LOW or HIGH -WEMAC blower supplies forced ventilation through overhead vents when activated -Forced ventilation provided by CABIN FAN (can be operated independently from the heater)

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