Piper Saratoga II TC

Engine

Manufacturer: Lycoming
Model: IO-540-AHIA
Horsepower: 300 hp to 12,000 feet
Number of Cylinders: 6

Propeller

Manufacturer: Hartzell
Number of Blades: 3
Type: Constant Speed

Weights

Standard Empty/Equipped Weight (*b,c): 2464 lbs/1118 kgs
Standard Useful Load (*a): 1151 lbs/522 kgs
Gross Weight: 3600 lbs/1633 kgs

Wing Area

Wing Area: 178.3 square feet/16.56 square meters

Dimensions

Wing Span: 36.2 feet/11.0 meters
Length: 27.9 feet/8.5 meters
Height: 8.5 feet/2.6 meters
Cabin Length: 124.25 inches/315.6 centimeters
Cabin Width: 48.75 inches/123.8 centimeters
Cabin Height: 42.0 inches/106.7 centimeters

Headroom (seat to ceiling):
Front Seats: 38 inches/96.5 centimeters
Middle Seats: 35.75 inches/90.8 centimeters Rear Seats: 34.5 inches/87.0 centimeters

Fuel Capacity

Usable Fuel: 102 gallons/386 litres

Oil Capacity

Oil Capacity:12 quarts/11.4 litres

Baggage

Volume:
Forward Compartment: 7 cubic feet/.2 cubic meters
Aft Compartment: 17.3 cubic feet/.49 cubic meters

Capacity:
Forward Compartment: 100 lbs/45.4 kgs
Aft Compartment: 100 lbs/45.4 kgs

Maximum Speed

TAS at gross Weight: 192 kts/356 kmh

Cruising Speeds

High Performance @ 8,000 feet: 174 kts/322 kmh
Cruise Speed @ 10,000 feet: 177 kts/328 kmh
Cruise Speed @ 15,000 feet: 186 kts/345 kmh

Stall Speed

Flaps Down Full 40 degrees: IAS 60 kts/IAS 111 kmh

Cruise Range

(*d) Cruise range includes 45-minute fuel reserve at cruise power plus allowance for fuel used during taxi, take-off, climb at MCP, cruise plus descent.

High Performance @ 8,000 feet: 788 nm/1460 km
Cruise Speed @ 10,000 feet: 797 nm/1477 km
Cruise Speed @ 15,000 feet: 822 nm/1523 km

Maximum Operating Altitude

Maximum Operating Altitude: 20,000 feet/6096 meters

Take-Off Distance

Ground Roll: 1200 feet/366 meters
Total over 50-foot obstacle: 1800 feet/549 meters

Landing Distance

Ground Roll: 640 feet/195 meters
Total over 50-foot obstacle: 1520 feet/463 meters

*a. Standard Useful load is ramp weight minus standard equipped weight.
*b. The standard empty weight and standard equipped weight are the same.
*c. Standard aircraft per marketing.
*d. Predicted performance based upon established analytical methods.

The New Piper Aircraft, Inc. reserves the right to make changes in specifications, materials, equipment or prices at any time without prior notice or to discontinue models as required. It is the responsibility of the pilot to conduct all operations in accordance with FAA approved Pilot's Operating Handbook, which is the only official source of data.

To visit The New Piper Aircraft Web Site, click here

STANDARD EQUIPMENT & AVIONICS

POWERPLANT & PROPELLER

Engine-Lycoming TIO-540-AH1A 300 HP At 2500 RPM, Turbocharged, Direct Drive, Six-Cylinder, Fuel-Injected

Dynafocal Engine Mounts with Internal Dampers

Three-Blade, Constant Speed Propeller

Polished Propeller Spinner

Geared Starter, 28 Volt

Air Filter

Full Flow Oil Coolers (Two) - w/Thermostatic Control

Dual Pressurized Magnetos

Alternate Induction Air with Manual Control

Oil Quick Drain

Engine Driven Vacuum Pump

FLIGHT INSTRUMENTS & INDICATORS

Piper Truespeed Indicator

Magnetic Compass (Illuminated)

ADI

HSI

Turn Rate Indicator

Rate of Climb Indicator

Electric Clock DVR 300I-XT w/Voice Recorder

Overhead Switch Panel Bar Guarded Push-to-Start Battery Master Alternator Bar Guarded Electric Fuel Pump Bar Guarded Magneto Switches, Two Taxi Lights Landing/Pulse Lights Navigation Lights Strobe Lights

Annunciator Panel with Push-to-Test and Day/Night Switch Starter Engage Low Bus Voltage Alternator Inoperative Oil Pressure Low Gyro Vacuum Inoperative Nose Baggage Door Ajar Gear Warning Flaps in Transit Pitot Heat Inoperative/Off Air Conditioning Door (Optional)

New Engine Instrument Indicators/Monitoring System

Digital Display Monitor Panel with Percent Power Fuel Management Including GPS Interface Temperature Readings Including OAT Electrical System Performance Indicators Exceedence Monitoring and Recording Manifold Pressure Indicator RPM Indicator Turbine Inlet Temperature and Fuel Flow Indicator Oil Temperature & Oil Pressure Indicator Cylinder Head Temperature & Vacuum Indicator Fuel Quantity L/R Indicator Engine Hour Recorder Alternate Instrument Static Source

COCKPIT, FLIGHT & GROUND CONTROLS

Hytrel Dual Control Wheels

Stainless Steel Control Cables

Flight Trim Controls Rudder with Indicator Stabilator with Indicator

Engine Controls - Pedestal with Friction Lock Throttle Propeller Mixture (with Lock)

Alternate Induction Air

Stall Warning Horn

Steerable Nosewheel

Heavy Duty Brake System Pilot's Toe Brakes Copilot's Toe Brakes Parking Brake

Landing Gear, Retractable-Electro Hydraulic

Landing Gear Warning Horn and Position Lights

Wing Flaps, Electrically Operated with Four Preselected Positions (0, 10, 25 and 40 Degrees)

Fuel Control Selectors w/OFF/LEFT/RIGHT

Emergency Gear Extension System

ELECTRICAL SYSTEMS

28 Volt, Alternator-90 Amp

24 Volt 10 amp Hour Battery

Master Switch Relay

Alternator Control Unit

Electric Vacuum Pump (Standby)

Heated AN Pitot Head

Resettable-Type Circuit Breakers in CB Panel

Back Lighted Rocker Switches, Conveniently Grouped on Pilot's Instrument Panel and Overhead Panel

Static Discharge Wicks

Automatic Emergency Locator Beacon (ELT)

FUEL SYSTEM

Two Interconnected Fuel Tanks per Wing with 107 Gallons Total Capacity, 102 Gallons Usable

Engine Driven Fuel Pump

Electric Emergency Fuel Pump

Fuel Quantity Sight Gauge, Inboard Tanks, Two

Fuel Tank Quick Drains, Four

Fuel System Central Drain

Fuel Sampling Bottle

Flush Lockable Fuel Caps

CABIN COMFORT SYSTEM

Heater Muff, Provides Heat to Cabin Area, Regulated by Control on Panel with Six Floor Heat Outlets

Heat Regulating Levers-Located at Each Passenger Seat

Windshield Defrosters And Control

Cabin Air Exhaust Vents, Two

Cabin Fresh Air Vents, Six Individually Controlled, Overhead, and Four Individually Controlled, Floor Mounted

Ventilation Fan w/2 Speed Settings

EXTERNAL FEATURES

Exterior Paint, DuPont Imron 6000 Base-Coat/Clear-Coat System

Full Chemical Corrosion Protection

12 Inch Shadowed or Outlined Registration Numbers

Cabin Doors, Two-Right Forward and Left Rear

Main Wheels, 6.00 X 6 w/H.D. Tires and Tubes, eight-Ply

Nose Wheel, 5.00 X 5 w/H.D. Tire and Tube, six-Ply

Stowable Towbar

Tie Down Rings, Three (Retractable On Wings)

Jack Pads

Fore and Aft Cabin And Nose Baggage Doors, Lockable

Utility Door for Rear Baggage Access and Cargo Loading

External Power Receptacle

Entrance Step

Keys with Piper Logo

LIGHTING SYSTEMS

Instrument Panel Lighting

Avionics Dimming

Map Lights

Cabin Reading Lights, Four

Forward Baggage Compartment Light

Cabin Door Lights, Two

Navigation Lights

Landing/Pulsating Recognition Lights In Wing Tips

Taxi/Landing Light on Nose Landing Gear

Wing Tip Comet Strobe Lights

COCKPIT & CABIN APPOINTMENTS

Forward Cabin Door with Single-Lever Locking System

Six Seat Configuration in Club Seating

Choice of Four Interior Colors, which Includes: Leather Seats, Designer Side Panels, Wall-to-Wall Carpeting and Headliner

Pilot/Copilot Vertically Adjustable Seats with Inflatable Lumbar Support, Pilot/Copilot Folding Armrest, and Magazine Storage Pockets On Back of Each Seat with Headrests. Fore, Aft and Tilting Adjustment with Inertial Shoulder Reels and Safety Belts.

GARMIN Pilot/Copilot and Passenger Intercom System

Pilot and Copilot Stowable Armrests

Armrests-Crew Area, Two

Map Pockets, Two

Pilot's Vent Window

Sunvisors

POH Holder

Color Coordinated Throttle Quadrant and Center Console

Scuff Pads, Pilot and Copilot

Tinted Windshield and Windows

Window Shades on Passenger Windows

Deluxe Six Seat Lounge Interior Group Headrests for All Seats, Club Seating Arrangements with Shoulder Harness and Seat Belts, Rear Seats Incorporate Quick Release Feature For Easy Removal, Refreshment Console with Cup Holders, and Fold-Down Armrests on Crew and Rear Seats, Built-In Executive Writing Table.

Super Soundproofing, Quietized

Luggage Compartments with Security Straps Rear Cabin and Hat Shelf Area, 17.3 cu ft. Max Rear Baggage Area Load, 100 lbs. Fuselage Nose, 7.0 cu ft. 100 lbs.

Compass Correction Card with Holder

Halon Fire Extinguisher

PRODUCT SUPPORT/DOCUMENTS

Manufacturer's Full Two-Year Limited Warranty

Initial Pilot Training Slot with ATTITUDES INTERNATIONAL, INC.

Pilot's Operating Handbook

Aircraft Log Book

Engine Log Book

Certificate of Airworthiness

Flight Bag

Piper Warranty/Inspection Form

STANDARD GARMIN/S-TEC AVIONICS PACKAGE
Audio Panel with Marker Beacon and Intercom	GMA-340
Nav/GS/GPS/Comm	GNS-430
Nav/GS/GPS/Comm	GNS-430
#2 Indicator (Loc and GS)	GI-106
Transponder	GTX-320
Autopilot	S-TEC 55 Dual Axis Autopilot with automatic electric trim and turn indicator
ADI (Flight Director Bars)	ST-361
HSI with Slaved Compass	ST-180
DME	DME-450
Altitude Reporter Ground Clearance System Pilot/Copilot Wheel Mic Button Avionics Master Switch Microphone (Telex 100T) Headset (Telex Airman 760) Speaker w/Mic/Phone Jacks Static Discharge Wicks PS Engineering Headsets (4)	AR-850

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