1972 Piper PA34 Seneca I Multi Engine Piston

General

Manufacturer

PIPER

Model

SENECA

Condition

Used

Registration #

HB-LML

Flight Rules

IFR

Based at

LSZL

Airframe

Total time

9,881

Airframe total time: 9881 hrs

Propeller

LH

CH -C2YK-2CGUF, sn AU13103B TT: 5737,

Time Since Overhaul

144:25 hrs

RH

HC-C2YK-CLGUF. sn AU13099B TT: 6648:19, Time Since Overhaul: 144:25 Overhauled with New improved hubs in July. 2007.

TBO

2000 hrs / 6 Years.

2 Bladed Hartzell Propellers

Overhauled with New improved hubs in July. 2007.

(Calendar overhaul not mandatory in Switzerland for private operation. Also read new EASA Notice of Proposed Amendment (NPA) No 2011-15 for future "Non-binding guidance on TBO limits")

Avionics

WAAS

Yes

LPV

Yes

• PS Engineering audio panel with intercom and marker beacon,
• 1 x Garmin GNS530 WAAS 8.33 kHz
• 1 x King KX125 COM 760 Ch, FM Immune,
• KN72 NAV,
• KCS55 HSI,
• KR85 ADF with RMI,
• KN62A DME,
• ME406 ELT,
• King KT79 Mode "S" XPDR,
• ACK A30 Encoder,
• Autocontr III Autopilot 3 axis coupled to HSI and VOR,
• GPS approved for VFR/IFR enroute, B-RNAV, terminal and instrument approach (GPS, VOR, VOR-DME, NDB, NDB-DME) operation. Within the US National Airspace System in accordance with AC 20-138 and such countries where GPS enroute, terminal and non-precision approaches are authorized by the appropriate airworthiness authority.
• WX900 Stormscope,
• Copilot instruments Airspeed, Attitude Indicator, Altimeter, VOR/GS, DG
• Day/Night, IFR Category 1, B-RNAV (RNP 5)

Equipment

Inadvertent Ice Protection

Yes

• Lightweight Surface Pneumatic De-icing system and propeller electrothermal de-icing system,
• Windshield hot plate,
• Pitot and stall warning heating system protected by landing gear switch
• Propellers with dampers
• Electric pitch trim installation,
• Logo light, Currently removed, hoses still present with covers installed
• Additional FOCA Approved documentation for 98 USG fuel tank for ferry flights.
• Increased MTOW approved for 4560 Lbs Remaining Useful Load with full tanks and ferry tank: 453.45 Lbs

Interior

Number of Seats

6

Blue vinyle 9/10 Gray fabric seats 9/10 Pilot and Copilot Adjustable seats Blue carpet 9/10

Exterior

Light gray with maroon stripes 7/10

Maintenance

Maximum Take Off Weight

1905 kg - 4199.00 lbs

Empty Weight

2960.55 Useful Load: 1235.45 Lbs

Fuel Capacity

93 USG

• In good conditions.
• Landing accident with one main gear collapse and wing spar repair in performed in 1991 at TT: 6557
• Missing logs from 1972 to 1981, Prior to Swiss registration.
• Replaced fuel tank vent line hoses 12/07
• EASA Noise Certificate 74.8 dB(A)
• Annual inspection and EASA ARC are overdue.
• Selling as is, where is

Engine 1

Engine 1 Time

10,251 SNEW

Engine 1 TBO

2000

Engine 1 Notes

LH

Textron-Lycoming IO-360-C1E6, sn L-1118-51A TT: 10251, TSOH: 1155:48 overhauled by Mattituck in September 1998,

RH

Textron-Lycoming LIO-360-C1E6, sn L-444-67A TT: 7758:38, TSOH: 1686:32 overhauled by Mattituck in July 1996 TBO: 2000 hrs / 12 Years

Engine 2

Engine 2 Time

7,758 SNEW

Registration

Registration

HB-LML

Registered as

Piper Aircraft Corporation PA-34-200

Year

1972

Serial number

34-7250341

Registered since

1981-02-11

Status

Registered