1981 Cessna 340A

General

Manufacturer

CESSNA

Model

340A

Serial Number

340A1234

Registration #

N111PJ

Condition

Used

Flight Rules

IFR

Based at

SCK

Airframe

Total time

3,618

Auxiliary Fuel Tank

Yes

Specifications

• Wingspan: 38' 1"

• Registration: N111PJ
• Serial Number:340A1234
• Airframe Time: 3,618 hours total time since new
• Price: $199,000 USD
• Location: Stockton Metropolitan Airport (KSCK), Stockton, CA
• Length: 34' 4"
• Height: 12' 7"
• Gross Weight: 6,290 lbs. (gross weight increase mod)
• Useful Load: 1,755.80 lbs. actual
• Fuel Capacity: 207-gallon capacity (203-gallon usable mains, aux, nacelles)

Propeller

Prop 1 Time

741 SOH

Prop 2 Time

741 SOH

Left Propeller

• McCauley 3AF32C505/82NEA 5.5, sn: 807652

Right Propeller

• McCauley 3AF32C505/82NEA 5.5, sn: 940316

• Three blade, electrothermal deice
• 741 Hours SPOH; 2,000-hour TBO
• Overhauled by McCauley Propeller w/new deice boots 08/25/2010
• Three blade, electrothermal deice
• 741 Hours SPOH; 2,000-hour TBO
• Overhauled by McCauley Propeller w/new deice boots 08/25/2010
• Prop governor overhauled by Ottosen Propeller & Accessories 01/21/2008

Avionics

Flight Deck Manufacturer/Model

ASPEN AVIONICS EFD1000 PRO PFD

ADS-B Equipped

Yes

WAAS

Yes

Engine Monitor

Yes

• Audio Panel: King KMA 24 audio panel with 3LMB
• EHSI: Aspen EFD1000 PFD PRO EHSI coupled to GNS 530W & 400B autopilot
• GPS/Nav/Com: Garmin GNS 530 WAAS GPS/Nav/Com coupled to Arnav FD10
• Nav System: King KNS 80 integrated Nav system (VOR/LOC, DME, RNAV, G/S)
• Com: King KY 196 TSO Com
• Compass Sys.: King KCS 55A compass system
• • • • • King KI 525A HSI
• • • • • King KG 102 gyro
• • • • • King KA 51A slave meter
• Autopilot: Cessna 400B Navomatic autopilot
• Transponder: Garmin GTX 345R remote ADS-B In/Out transponder
• Altitude Encoder: Garmin GAE 12 digital altitude encoder
• Weather Radar: King KWX 56 color radar system
• Engine Analyzer: Insight Electronics Gemeni-1200 digital engine analyzer
• Fuel Flow: Arnav FC-10 and FT-10 fuel flow indicating system
• OAT: Electronics International digital OAT indicator
• ELT: Artex ELT200 with copilot side panel mounted switch and indicator
• ICS: KMA 24 intercom system with standard cockpit and cabin ports
• Chronometer: Davtron M811B three-in-one chronometer
• Entertainment: PS Engineering PCD7100-1 TSO with crew/all isolation
• Hour Meter: Honeywell quartz recording hour meter
• Aux power: Auxiliary lighter power port with plugin USB port
• True airspeed indicator
• Pilot control yoke with PTT, electric trim, autopilot disconnect and ident switches
• Copilot control yoke PTT switch

Equipment

Vortex Generators

Yes

Oxygen System

Yes

Flight Into Known Icing (FIKI)

Yes

A/C

Yes

Additional Features

• New RG24-20 aircraft battery installed 01/07/2025

• New right engine alternator installed 01/07/2025
• Right engine alternator drive coupling overhauled 01/07/2025
• Installed new electrical wire harness into pilot yoke tube 01/07/2025
• Aspen PFD standby battery replaced 02/13/2020
• Hartzell Engine Technologies left and right voltage regulators installed 03/05/2018
• Autopilot computer repaired 04/24/2015
• Left engine starter adapter overhauled 02/24/2014
• Left engine intake and exhaust system lifter bodies, and pushrods replaced 10/01/2013
• Left engine fuel flow divider overhauled 10/01/2013
• Right engine fuel flow divider overhauled 10/01/2013
• Left engine new alternator and overhauled drive coupler installed 01/25/2018
• Left engine starter and vacuum pump overhauled 04/10/2013
• Left and right engine turboGAMIjectors installed 01/18/2010 per STC SE09289SC
• RAM vacuum pump cooling shroud installed 04/15/2003 per STC SA3850SW
• Whelen anticollision strobe light installed 08/01/1997 per STC SA615EA
• J.B. freon air conditioning system installed 07/09/1981 per STC SA16RM
• Micro Aerodynamics wing and vertical stabilizer vortex generators and left and right engine strakes installed 05/05/1995 per STC SA3934NM
• FIKI certified deice system, boots in excellent condition
• Factory 76.6 cubic ft. oxygen cylinder
• Aileron, rudder and elevator trim
• Standard wingtip strobe and nav light assemblies
• Red lower forward fuselage anticollision strobe light
• Red rudder anticollision strobe light
• Standard white tail cone position light
• Dual heated pitot heads with dual alternate static air sources
• Right side cabin emergency exit window
• Pilot and copilot cockpit storm window
• External ground power receptacle
• Parking brake

Interior

• Complete interior refurbishment unknown date
• Cabin entryway light
• Ultraleather (light gray) headliner
• White plastic window trim
• Tinted windows
• Faux woodgrain trim over maroon leather side panels over gray tweed carpet side panels
• Fully articulating pilot and copilot maroon leather seats with sheepskin covers, stowable center armrests, shoulder harnesses and lap belts
• Four place club maroon leather seats with headrests, stowable center armrests and lap belts
• Right side cabin stowable wood executive writing table
• Maroon floor carpeting
• Cockpit overhead air conditioning vents, spotlights and dimming map light
• Cockpit side panel oxygen ports
• Cockpit overhead speaker
• Cabin overhead individual air conditioning vents, spotlights and oxygen ports
• Aft cabin cargo/baggage area with maroon leather covered hangers
• Spacious nose baggage compartment left and right side accessible
• Relief tube
• Condition 6 (Professional Aircraft Appraisers Organization Interior Grading Guide)

Exterior

• Aircraft stripped and refinished unknown date
• Overall off white with maroon and gray trim and accents
• Fuselage ice protection plates
• Engine nacelle lockers
• Condition 6 (Professional Aircraft Appraisal Organization Exterior Paint Grading Guide)

Maintenance

Airworthy

Yes

Inspection

• Delivered with fresh annual inspection by FAA Part 145 repair station

Logbooks

• All original and continuous airframe, engine and propeller logbooks, except:

Damage

• 06/05/1985 Left wing rear spar splice per Cessna structural manual

• IFR recertification due by 12/31/2026
• ELT battery replacement next due by 10/31/2027
• Oxygen cylinder hydrostatic test due 12/31/2027
• Combustion heater decay test due by 01/21/2026
• Right engine logbook commences on 02/25/2002 @ overhaul
• Right propeller logbook commences on 09/01/2005
• scheme, new upper wing skin, new leading edge skin on vertical stabilizer,
• new skin lower right hand nose section, new right hand lower inboard
• nacelle panel assembly installed, outboard right aux fuel tank liner repaired.

Engine 1

Engine 1 Time

1,655 SMOH

Engine 1 TBO

1600

Engine 1 Turbocharged

Yes

Engine 1 Notes

Left Engine

• Teledyne Continental Motors TSIO-520-NB, 310 HP, msn: 521085

Engine 2

Engine 2 Time

662 SMOH

Engine 2 TBO

1600

Engine 2 Turbocharged

Yes

Engine 2 Notes

Right Engine

• Teledyne Continental Motors TSIO-520-NB, 310 HP, msn: 514558

Registration

Registration

N111PJ

Registered as

Cessna 340A

Year

1981

Serial number

340A1234

Engine

Cont Motor Tsio-520 Ser · 300 hp

Certificate

Standard

Airworthiness date

1981-04-20

Registered since

2023-06-04

Registration valid to

2030-06-30

Status

Valid

Accidents and incidents

None on record