PIPER SENECA III

REGISTRATION # AP BBU

AIRCRAFT SERIAL # 34 8433032

FULLY AIR-CONDITIONED

OUR COMPANY IS THE FIRST OWNER SINCE NEW

 

 

Piper Seneca III                       PA34 220T  AIR-CONDITIONED                 VINTAGE 1984

Specifications                                      

Aircraft Serial #                                                    34-8433032                             DIMENSIONS

Total Aircraft Hours                                            9109                                        Wing Span (ft./m)                                                38.9/11.9

Total Aircraft Hours since Last C of A            04                                            Length (ft./m)                                                        28.6/8.7

                                                                                                                                Height (ft./m)                                                        9.9/3.0   

ENGINES                                                                                                                Cabin Length (Instrument panel to rear bulkhead)

Manufacturer                                                        Continental                           (in./cm.)                                                                  125.0/317.5

Model                                                                    TSIO-360-KB                        Cabin width (in./cm.)                                           49.0/124.5

Rating (hp @ rpm)                                               & LTSIO-360-KB  Cabin Height (in./cm.)                                         42.0/1067

Take-off Power (5 Min. Limit)                            220 @ 2800                            Headroom  (Seat to Ceiling)                                              

Maximum Continuous Power                             200 @ 2600                            Front Seats (in./cm.)                                            38/96.5

Number of Cylinders                                           06                                            Middle Seats (in./cm.)                                         36.5/90.8

Recommended TBO (hrs.)                                  1800                                        Rear Seats (in./cm.)                                              34.5/87.6

Left Engine hours                                                1320                                        Forward Baggage Door Size (in./cm.)               21/53.3 x 24/61.0

Rt.  Engine hours                                                 1133                                        Aft Baggage/Utility Door Size (in./cm.)            20.5/52.1 x 26/66.0

                                                                                                                                Forward cabin Door Size (in./cm.)                     35/88.9 x 36/91.4

PROPELLERS                                                                                                        Wheel Base (ft./m)                                               7/2.13

Manufacturer                                                         McCauley                               Wheel Treated (ft./m)                                          11.1/3.39

Number of Blades                                                3                                                             

Type                                                                       Constant Speed,                   FUEL CAPACITY

                                                                                Full Feathering                                                    

Diameter (in./cm.)                                 76/193                                     Total Capacity (gal./L)                                        128/484                   

Left  Propeller Hours/Cal. Life                            1051 / 53 months                  Useable Fuel (gal./L)                                           123/466

Right Propeller Hours/Cal Life                           893 / 48 months

 

WEIGHTS

Ramp Weight (lbs./kg)                                        4773/2165                               OIL CAPACITY (qts./L)                                    8/7.57

Gross Take-off weight (lbs./kg)                         4750/2154                                                              

Gross Landing Weight (lbs./kg)                        4513/2047                               BAGGAGE

Empty Weight (lbs./kg)                                       3291/1495                               Volume (ft.³/m³)

(Includes: unusable fuel, full oil and full                                                          Forward Compartment                                         15.3/.43  

operating fluids)                                                                                                   Aft Compartment                                                 17.3/.49

Useful Load (lbs./kg)                                           1482/673                 Capacity (lbs./kg)

Zero Fuel Weight (lbs./kg)                                 4470/2028                               Forward Compartment                                         100/45.4

                                                                                                                                Aft Compartment                                                 100/45.4

Performance                                                              FUEL CONSUMPTION                                           

MAXIMUM SPEED (kts/kmh)                                                                           High Speed Cruise Power (75%)                        29.0/110

(TAS at Mid-Cruise Weight)                             196/363                                                   (gph/lph)

                                                                                                                                Economy  Cruise Power (65%)                           23.3/88

CRUISE SPEEDS                               10.000 Ft                Opt. Altitude                         (gph/lph)                                                              

(TAS at Mid-Cruise Weight)                                                                             Long Range  Cruise Power (45%)                      16.0/61                      

High Speed Cruise Power (75%)        179/332                   193/358                                   (gph/lph)

    (kts/kmh)

Economy  Cruise Power (65%)           175/324                   191/354                   RAT E OF CLIMB                                   Takeoff Power   Continuous Power

    (kts/kmh)                                                                                                            (At see Level and Gross Wt.)

Long Range  Cruise Power (45%)      143/265               168/311                       Two Engine (fpm/mpm)                      1400/427 1300/396

    (kts/kmh)                                                                                                            Single Engine (fpm/mpm)                   240/73                     200/61

 

CRUISE RANGE                                                                                                 STALL SPEED                                    IAS                         CAS

(Cruising range includes 45 minute reserve at long range                             Flaps Down Full 40º (kts./kmh)         64/119                     62/115

cruise power plus allowance for fuel used during taxi, take-off,                   Flaps Up (kts./kmh)                             67/124                     66/122

climb at MCP, cruise and descent)            

                                                                          Optimum Altitude                        SERVICE CEILING (MCP POWER)

                                                              Standard Fuel   Optional Fuel                Two Engines (100 fpm) (ft./m)                                  *25,000+/7620+

High Speed Cruise Power (75%)        463/858             665/1232                        Single Engine (50 fpm) (ft./m)                                    12, 300/3749

    (nm/km)

Economy  Cruise Power (65%)           550/1019           785/1455                         TAKE-OFF DISTANCE

    (nm/km)                                                                                                                (Sea Level, Zero Wind, Standard

Long Range  Cruise Power (45%)   670/1242           990/1835                            temperature, 25º Flaps)

    (nm/km)                                                                                                                Ground Run (ft./m)                                                            920/280

                      Optimum Altitude                             Total Distance over 50 ft. Obstacle (ft./m)                    1210/369

                                                           Standard Fuel    Optional Fuel

High Speed Cruise Power (75%)        450/834            640/1186                           LANDING DISTANCE                    Heavy Duty Brakes

    (nm/km)                                                                                                                 (Sea Level, Zero Wind, Standard Temperature)

Economy  Cruise Power (65%)           535/991            758/1404                           Ground Roll (ft./m)                                                            1218/371

    (nm/km)                                                                                                                 Total Distance over 50 ft. Obstacle (ft./m)                    1978/603

Long Range  Cruise Power (45%)   632/1171          903/1673                                                                         

    (nm/km)                                                                                                              ACCELERATE-STOP DISTANCE

                                                                                                                                (Sea Level, Zero Wind, Standard

                                                                                                                                Temperature, 25º Flaps) (ft./m)                                           2088/636

 

·         25, 000 feet is the maximum approved altitude for the Seneca III

 

 

OPTIONAL EQUIPMENT ON BOARD.

 

1-                   1600 BTU FREON AIR-CONDITION SYSTEM.

2-                   HEATING, VENTILATING & DEFROSTING SYSTEM IS PROVIDED BY A JANITROL COMBUSTION HEATER.

3-                   HEAVY DUTY BRAKE INSTALLED TO REDUCE ACCELERATE TO STOP DISTANCE.

 

AVIONICS ON BOARD.

 

Name of Equipment

Quantity

Manufacturer

Model

i.          HF Communication

01

Sun Air

-

ii.         VHF Communication-3

02

Collins

25TE

iii.        ADF

01

Collins

650A

iv.        ILS/VOR

01/02

Collins

VIR 351

v.         Marker

01

Collins

AMR-350

vi.        DME

01

Collins

TCR-451

vii.       Radio Altimeter

N/A

-

-

viii.      Airborne Radar System

N/A

-

-

ix.        ATC Transponder

01

Collins

TDR 950

x.         Intercommunication

01

Collins

AMR-350

xi.        SELCAL

N/A

-

-

xii.       ELT

01

ACK Technologies Inc

ELT- 01

xiii.      GPWS

N/A

-

-

xiv.      TCAS - II

N/A

-

-

xv.       GPS

01

Garmin

GPS-150