1965 Piper Aircraft Corporation PA 30 Twin Comanche

Caractéristiques

Cellule

Moteur & hélice

Description

Engines:

\# 1 Engine: IO-320-B1A S/N L-2785-55A , TSO: 876,5 h , compr. 8ß/77 all cyl.

\# 2 Engine: LIO-320-B1A S/N L-2635-66A ,TSO: 181,6 h, compr. 88/78 all cyl.

Propeller

\# 1 Hartzell HC-E2YL-2BSF , time since O/H : 249,4 hrs , S/N F7663-4

\# 2 Hartzell HC-E2YL-2BLSF, time since O/H : 181,6 hrs , S/N FJ7663-4

Airframe modifications:

2x 15 gal tiptank, ( 120 gal total )

one piece windshield and new side windows

LoPresti WOW- cowls with Knots2U Speed Spinners

4 x strobes

new soundproofing

all K2U- speed mods: Gap-seals, fairings, windshield cowler, dorsal fin, ect.

inflatable door seal with compressor

PA39- main gear struts with modified housing and HD-Brakes

2x Webco, Teflon- lined gear push-pull conduits

4x Webco, fuel caps

2x Webco ,Nylon main fuel-filter

12 V Alternator system

copper cables

Digital fluelflow ind.

Avionique & équipement

New Instrument panel and design

2nd electric Horizon

KMA 24 Marker, Audio selector

King KCS-55A HSI

King KLN 90B GPS- RNAV

MID-Continent MD41-324 annunciation control unit

Century Autopilot III,, Radio 1C-388-2 and GS- coupler

Auto trim, Yoke control

Stormcope WX-11

Garmin GPS-MAP 695

Garmin GTX- 330 Transponder

Garmin GTR-225 VHF/VOR/ILS

King KX-155A VHF/VOR/ILS

King KN-63 DME, with KDI-572 indicator

King KR- 87, ADF with KI- 227 indicator

King KI-204 NAV-ind. VOR/ILS