1979 PIPER LANCE II

General Specs (cont.)

Total Time:4361

Engine 1 Time:950 SMOH

Prop 1 Time:390 SPOH

Useful Load:1399 lb

Condition:Used

Flight Rules:IFR

Additional Classifications

Detailed Description

1979 Piper Lance II - Only 4361 Hours Total Time, 950 Hours SMOH by Aero Engines of Winchester, 390 Hours since Propeller Overhaul, Altimatic IIIC Autopilot Featuring Altitude Hold, Garmin 400W WAAS Approved GPS, Collins Digital Avionics, DME, WX-8 Stormscope, Insight Graphic Engine Monitor, Stand-By Vacuum, Sky Beacon ADS-B, LoPresti ZIP Tips with Rec Lights, LoPresti Speed Mods, Knots 2U Speed Mods, Concord Seal Battery, Club Seating, Stowable Executive Writing Table, Club Seating, Attractive Sales Price!

Avionics / Equipment

AVIONICS

Altimatic IIIC Auto Pilot Featuring Altitude Hold
Collins Audio Panel Featuring 3 Light Marker Beacons
Garmin GNS-400W GPS - (WAAS Enabled)
Collins VH-251 COM - (Dual)
Collins VIR-351 NAV - (Dual)
Collins VOR / Glide Slope Indicator
Collins VOR Indicator
King KN-64 DME - (Display Tired)
King KT-76C Transponder / Mode C
WX-8 Stormscope - (Older System / No Guarantees)
Electric Trim
Flightcom 403 Intercom / w Digital Clearance Recorder
Dual Push to Talk Switches
Precise Flight SVS V Standby Vacuum System
Insight G3 Engine Monitor
Sky Beacon ADS-B Out Solution

ADDITIONAL OUTSTANDING FEATURES / UPGRADES

LoPresti Zip Tips with Rec Lights
LoPresti Gear Spats Speed Enhancement
LoPresti Speed Splitters Speed Enhancement
Knots 2-U Aileron Gap Seals Enhancement
Knots 2U Flap Gap Seals Speed Enhancement
Knots 2U Stabilator Gap Seal Speed Enhancement
Wing Tip Strobes
LoPresti Hubba Caps
Concorde Sealed Battery
Outside Air Temperature Gauge
Clock
Tow Bar
Avionics Master Switch
Cleveland Wheels and Brakes.
Engine Sump Heater

Airframe

AIRFRAME

4361 Hours Total Time since New

Engines / Mods / Prop

ENGINE

950 Hours SMOH by Aero Engines of Winchester, Inc. - (Completed June 19, 1998)

PROP

390 Hours Since Prop Overhaul - (Completed November 27, 2013)

Interior / Exterior

INTERIOR

Gray Leather Club Seating Configuration w harmonizing Side Panels

Aft Cabin Writing Table

Vertical Adjustable Crew Seats

Executive Writing Table - (Stowable)

Side Window Curtains

Individual Headrests for each Seat

Overhead Ventilation

Individual Reading Lights

EXTERIOR

Matterhorn White Featuring Gamma Grey and Claret Accents

New Paint - (August 15, 1998)

Information: The lower cowling near the exhaust outlet could use some paint touch-up.

Remarks

ANNUAL DUE: August 1, 2024

BI-ANNUAL IFR CHECKS DUE: April 1, 2024 - (Fresh Inspections will be accomplished)

USEFUL LOAD: 1399 Pounds

NOTATIONS / ADDITIONAL MAINTENANCE INFORMATION

Fuel stain noted on RH Inboard Fuel Tank due to a leaking lower rivet.

Wing skin part numbers 38500-917 and 38586-002 replaced in June 20, 1998.

Aft Baggage Compartment Closeout Panel is broken out at bottom.

Several top fuselage skins, both windshields, and the top cowling were replaced. See airframe log entry dated June 3, 1996. The log entry also states that the Vertical Fin and 

Horizonal Stabilator were repaired. - (See FAA 337 dated 4/3/1996)

The aircraft returned to the USA in 1990 and was assigned registration number N2200J.

The aircraft had a nose gear collapse in 1981 at 94.6 Hours Total Time.

The aircraft was exported to Canada in December of 1978.


Specifications are subject to verification by the Purchaser. We accept trades and offer finance solutions.