PA28 (I-KRLS)-(I-ERNE)

I-KRLS

I-ERNE

Pilot's Operating Handbook Scaricabile per uso addestrativo

Checklist I-ERNE Scaricabile per uso addestrativo

Checklist List Emergenze PA28 Scaricabile per uso addestrativo


Apertura alare
m
10,67
Lunghezza
m
7,27
Altezza
m
2,24
Peso massimo al decollo
Kg
1.055
Autonomia
h
5
Velocità di crociera
Kts
100


PIPER PA-28-161 CADET

SPECIFICATIONS

ENGINES
Manufacturer Lycoming
Model O-320-D3G
Rating (hp @ rpm) 160 @ 2700
Number of Cylinders 4
Recommended TBO (hrs) 2000
PROPELLERS
Manufacturer Sensenich
Number of Blades 2
Type Fixed Pitch
Diameter (in/cm) 74/188
WEIGHTS
Ramp Weight (lbs/kg) NORMAL: 2332/1058 UTILITY: 2027/919
Gross Weight (lbs/kg) NORMAL: 2325/ 1055 UTILITY: 2020/916
Standard Empty Weight (lbs/kg) VFR: 1390/630 IFR: 1416/642
(Includes unusable fuel, full operating fluids and full oil)
Standard Useful Load (lbs/kg) VFR: 942/427 IFR: 916/415
WING AREA AND LOADINGS
Wing Area (ft.2/m2) 170/15.8
Wing Loading (lbs/ft.2) (kg/m2) 13.7/66.9
Power Loading (lbs/hp)/(kg/hp) 14.5/6.6
DIMENSIONS
Wing Span (ft/m) 35.0/10.7
Length (ft/m) 23.8/7.3
Height (ft/m) 7.3/2.2
Cabin Length (Instrument Panel to Rear Bulkhead) (in/cm) 98/248.9
Cabin Width (in/cm) 41.25/104.8
Cabin Height (in/cm) 44.25/112.4
Headroom (Seat to Ceiling)
Front Seat (in/cm) 38/96.5
Rear Seat (in/cm) (optional) 34/86.4
Cabin Door Size (in/cm) 36/91.4 x 35/88.9
Wheel Base (ft/m) 6.67/2.03
Wheel Tread (ft/m) 10/3.05
FUEL CAPACITY
Two 25 gal. tanks (gal/L) 50/189
Usable Fuel (gal/L) 48/182
OIL CAPACITY (qts/L) 8/7.57
BAGGAGE
Volume (ft3/m3) 24/.68
Capacity (lbs/kg) NORMAL: 50/23 UTILITY: 0
PERFORMANCE

MAXIMUM SPEED (kts/kmh)
(TAS at Mid Cruise Weight) 121/224
CRUISING SPEEDS Best Power Best Economy
(TAS at Mid Cruise Weight)
75% at 9,000 ft (kts/kmh) 119/220 115/213
65% at 12,000 ft (kts/kmh) 110/204 110/204
55% at 12,000 ft (kts/kmh) 101/187 97/180
CRUISE RANGE (Estimated; flight data not available)
(Cruising range includes 45-minute fuel reserve at max. range power plus
allowance for fuel used during taxi, take-off, climb at MCP, cruise at stated
mixture and descent)
Best Power Best Economy
75% at 9,000 ft (nm/km) 490/907 550/1019
65% at 12,000 ft (nm/km) 515/954 590/1093
55% at 12,000 ft (nm/km) 530/982 600/1111
FUEL CONSUMPTION Best Power Best Economy
75% power (gph/lph) 10.0/37.9 8.5/32.2
65% power (gph/lph) 8.8/33.3 7.5/28.4
55% power (gph/lph) 7.8/29.5 6.6/25
RATE OF CLIMB (At Sea Level and Gross Wt)
Full Throttle (fpm/mpm) 670/204
STALL SPEED IAS CAS
Flaps Down Full 40o (kts/kmh) 44/82 50/93
Flaps Up (kts/kmh) 50/93 56/104
SERVICE CEILING (100 fpm) (ft/m) 11,600/3536
TAKE-OFF DISTANCE
(Sea Level, Zero Wind, Standard Temperature, 25o flaps)
Ground Run (ft/m) 950/290
Total over 50 ft obstacle (ft/m) 1500/457
LANDING DISTANCE
(Sea Level, Zero Wind, Standard Temperature)
Ground Roll (ft/m) 590/180
Total over 50 ft obstacle (ft/m) 1050/320

Reference: Piper Aircraft Corporation Brochure, Vero Beach, FL, 1 Feb. 1989
Given data is only for information. Please refer to the manufacturer for current data.







AllegatoDimensione
IERNE PA2861.75 KB
cadet.gif32.96 KB
ls 021_rs.jpg188.76 KB
DSCF3778_rs.jpg188.42 KB
ikrls.jpg46.87 KB
DSCF3782_rs.jpg196.04 KB
I-ERNE76.09 KB

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