Piper CHEROKEE 180 Guía del usuario

CHEROKEE 180

PA-28-180

owner's Handbook

Piper Aircraft Corporation, Vero Beach, Florida

U.5. A.

NOTICE

THIS HANDBOOK IS NOT DESIGNED, NOR CAN ANY

HANDBOOK SERVE, AS A SUBSTITUTE FOR ADEQÚATE AND

COMPETENT FLIGHT INSTRÚCTION, OR KNOWLEDGE OF THE

CURRENT AIRWORTHINESS DIRECTIVES, THE APPLICABLE

FEDERAL AIR REGULATIONS, AND ADVISORY CIRCULARS. IT

IS NOT INTENDED TO «BE A GUIDE OF BASIC FLIGHT

INSTRUCTION, NOR A TRAINING MANUAL.

THE HANDBOOK IS DESIGNED:

1. TO HELP YOU OPERATE YOUR CHEROKEE WITH

SAFETY AND CONFIDENCE.

2. TO MORE FULLY ACQUAINT YOU WITH THE BASIC

PERFORMANCE AND HANDLING CHARACTERISTICS

OF THE AIRPLANE.

3. TO MORE FULLY EXPLAIN YOUR CHEROKEE'S

OPERATION THAN IS PERMISSIBLE TO SET FORTH IN

TI-iE AIRPLANE FLIGHT MANUAL.

IF THERE IS ANY INCONSIS'i'ENCY BETWEEN THIS

HANDBOOK AND THE AIRPLANE PLIGHT MANUAL APPROVED

BY THE F.A.A., THE FLIGHT MANUAL SHALL GOVERN.

Revised text and illustrations shall be indicated by a

black vertical lirm in the margin opposite the change.

Additional copies of this manual, Part No. 761 513,

may be obtained from your Piper Dealer.

Published by

PUBLICATIONS DEPARTMENT

Piper Aircraft Corporation

761 513

Issued: June 1972

Revised: January 1973

SECTION 1

SPECIFICATIONS

Performance .................... .......... 1

Weights ............ ...... ......... 2

PowerPlant.................... ......... 2

FuelandOil ................... ........... 2

Baggage ................... ... ......... 2

Dimensions ................................ 3

LandingGear............. .. ... ......... 3

CHEROKEE 180 SECTION I

SECTION I

SPECIFICATIONS

PERFORMANCE

Performance figures are for airplanes equipped for cross-country

transportation and flown at gross weight under standard conditions at

sea level or stated altitude. Any changes in equipment may result in

changes in performance.

Take-off Ground Run (S.L. Std., maximum effort, 25 °

flap) (ft) 720

Take-off over 50-ft Barrier S.L. Std., (maximum effort,

25°flap) (ft) 1625

Best Rate of Climb Speed (mph) 85

Rate of Climb (ft per min) 725

Service Ceiling (ft) 14,150

Absolute Ceiling (ft) 16,500

Top Speed (mph) 148

Optimum Cruise Speed (TAS) (75% power,

optimum altitude, leaned to best power) (mph) 141

Cruising Range (75% power, optimum altitude

leaned to best economy, no reserves or climb

allowance) (mi) 686

Optimum Cruising Range (55% power, 10,000 ft,

leaned to best economy, no reserves or climb

allowance (mi) 706

Stalling Speed CAS (flaps down) (mph) 61

-Stalling Speed CAS (flaps up) (mph) 68

Landing Roll S.L. Std., (flaps down) (ft) 635*

Landing Roll over 50-ft Barrier S.L. Std., (ft) 1185*

*This value applies only for the conditions indicated on the landing

distance versus density altitude chart.

761 513 1

720615

SECTION ICHEROKEE 180

SPECIFICATIONS (cont.)

WEIGHTS

Gross Weight (lbs) 2450

Empty Weight (Standard) (lbs) 1384*

USEFUL LOAD (Standard) (lbs) 1066*

POWER PLANT

Engine (Lycoming) O-360-A4A

Rated Horsepower 180

Rated Speed (rpm) 2700

Bore (in.) 5.125

Stroke (in.) 4.375

Displacement (cu in.) 361.0

Compression Ratio 8.5:1

Dry Weight (lbs) 285

Propeller 76EM8S5-0-60

FUEL AND OIL

Fuel Capacity (U.S. gal) Usable 48

Oil Capacity (qts) 8

Fuel, Aviation Grade (min octane) 100/130

BAGGAGE

Maximum Baggage (lbs) 200

Baggage Space (cu ft) 24

Baggage Door Size (in.) 20 x22

*Weight varies with each aircraft

2761513

720615

CHEROKEE 180 SECTION I

SPECIFICATIONS (cont.)

DIMENSIONS

Wing Span (ft) 32

Wing Area (sq ft) 170

Wing Loading (lbs per sq ft) 14.4

Length (ft) 24.0

Height (ft) 7.8

Power Loading (lbs per hp) 13.6

LANDING GEAR

Wheel Base (ft) 6.7

Wheel Tread (ft) 10

Tire Pressure (psi) Nose 24

Main 24

Tire Size Nose (4 ply rating) 6.00 x6

Main (4 ply rating) 6.00 x6

761 513 3

720615

SECTION ICHEROKEE 180

50"

2.50"

10'

-24' 09"

T.ß0"

---8' 8.4"

4761513

720615

SECTION 11

DESIGN INFORMATION

EngineandPropeller ............ .. ......... 5

Structures.......... ..... .... .......... 5

LandingGear ........... ... ............ 6

ControlSystems ......... .... ........ 7

FuelSystem ........ ....... 7

Electrical System . . . ... . . . . .. . .. . . . . . 9

Heating and Ventilating System .... . . . ...... . .. . .13

CabinFeatures .......... . . ........ 13

Optional Equipment .... . . . . . ..... . . . 16

CHEROKEE 180 SECTION 11

SECTION 11

DESIGN INFORMATION

ENGINE AND PROPELLER

The Cherokee 180 is powered by a Lycoming O-360-A4A four

cylinder, direct drive, horizontally opposed engine rated at 180 HP at

2700 RPM. It is furnished with a starter, 60 ampere 12 volt alternator,

shielded ignition, vacuum pump drive, fuel pump, and a dry,

automotive type carburetor air filter.

The exhaust system is of the cross-over type to reduce back

pressure and improve performance, It is made entirely from stainless

steel and is equipped with dual mufflers. Aheater shroud around the

mufflers is provided to supply heat for the cabin and windshield

defrosting.

The Sensenich 76EM8S5-0-60 fixed-pitch propeller is made from a

one-piece alloy forging.

STRUCTURES

All structures are of aluminum alloy construction and are designed

to ultimate load factors well in excess of normal requirements. All

exterior surfaces are primed with etching primer and painted with

acrylic lacquer.

The wings are attached to each side of the fuselage by inserting the

butt ends of the respective main spars into aspar box carry-through

which is an integral part of the fuselage structure, providing in effect a

continuous main spar with splices at each side of the fuselage. There are

also fore and aft attachments at the rear spar and at an auxiliary front

spar.

761 513 5

720615

Este manual sirve para los siguientes modelos

Tabla de contenidos

Otros manuales de Aeronave de Piper

Piper

Piper Pawnee C Guía del usuario

Piper

Piper PA-24 Comanche Manual de usuario

Piper

Piper PA-28-161 Manual del propietario

Piper

Piper Navajo PA-31 Manual de usuario

Piper

Piper CHEROKEE 180 1972 Guía del usuario

Piper

Piper ARCHER II Manual del propietario

Piper

Piper Cherokee C Guía del usuario

Piper

Piper PA-24-180 Comanche Manual de usuario

Piper

Piper SARATOGA II HP PA-32R-301 Manual de usuario

Piper

Piper COMANCHE 260 Guía del usuario

Piper

Piper Arrow PA-28R-201 Manual del propietario

Piper

Piper CHEROKEE WARRIOR PA-28-151 1995 Manual de usuario

Piper

Piper Piper Cub Trainer J3 Manual de usuario

Piper

Piper Cheyenne IIIA Manual de usuario

Piper

Piper SEMINOLE 2013 Manual del propietario

Piper

Piper Cherokee Arrow PA-28R-180 Guía del usuario

Piper

Piper CHEROKEE CRUISER PA-28-140 Guía de configuración rápida

Piper

Piper CHEROKEE 180 C Guía del usuario

Piper

Piper CHEROKEE WARRIOR II Manual del propietario

Piper

Piper PA-28-181 Archer II Manual de usuario

Piper

Piper cherokee WARRIOR Manual de usuario

Piper

Piper ARROW III Manual de usuario

Piper

Piper PA-24 Comanche Manual de usuario

Piper

Piper CHEROKEE WARRIOR 1976 Manual del propietario

Manuales populares de Aeronave de otras marcas

Cessna

Cessna U206G STATIONAIR Manual del propietario

Cirrus

Cirrus SR22 Manual de usuario

Schleicher

Schleicher ASK 21 Instrucciones de instalación

Aircraft

Aircraft REIMS F152 Especificaciones técnicas

Skywalk

Skywalk Tequila 2 Manual de usuario

MAULE

MAULE M-7-235B Especificaciones técnicas

Ozone

Ozone Indy Manual

Tecnam

Tecnam P92 Echo Super Manual de usuario

Wills Wing

Wills Wing HP II Manual de instrucciones

Ozone

Ozone Roadster Manual

Cirrus

Cirrus SR20 Manual de usuario

Niviuk

Niviuk KOYOT 3 Manual de usuario

Pipistrel

Pipistrel ALPHA Trainer Manual de usuario

REVELL

REVELL SnapTite BLUE ANGELS F-18 HORNET Manual de usuario

Cessna

Cessna 172 Series 1973 Manual de usuario

Sky

Sky EOLE Manual de usuario

Sabfoil

Sabfoil Surf Foil Manual de usuario

Cessna

Cessna 182S Skylane Guía de configuración rápida