czech sport aircraft PS-28 cruiser User manual

PS-POH-1-1-11
P PS S- -2 28 8 C Cr ru ui is se er r
Date: 2012-07-03 iRev. No.: 1
P
PS S- -2 28 8 C Cr ru ui is se er r
Pilot’s Operating Handbook
Airplane Registration Number: PH - VTA
Airplane Serial Number: C0487
This Pilot’s Operating Handbook is
EASA approved under
Restricted Type Certificate No.: EASA.A.546

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P
PS S- -2 28 8 C Cr ru ui is se er r a ai ir rc cr ra af ft t
i
is s d de es si ig gn ne ed d a an nd d m ma an nu uf fa ac ct tu ur re ed d b by y: :
Czech sport aircraft a.s.
Na Záhonech 1177/212, 686 04 Kunovice
Czech Republic
Website: www.czechsportaircraft.com
E-mail: [email protected]
Phone: [phone] (Sales Dept.)
Fax: [phone]

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PS-POH-1-1-11RECORD OF REVISIONS P
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RECORD OF REVISIONS
Rev.
No. Affected pages Revision name Approved Date
1. i, v, vii, viii, 2-8, 2-12, 3-14, 4-3, 4-5, 4-6, 4-11,
4-12
BRS moved to
Supplement, specification
of engine speed at
airplane waiting
EASA AFM
Approval
10041100 21. 8. 2012

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PS-POH-1-1-11LIST OF EFECTIVE PAGES P
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LIST OF EFFECTIVE PAGES
Section Page Date Section Page Date
i 2012-07-3 2
ii 2011-09-01 EASA approved 2-9 2011-09-01
iii 2011-09-01 EASA approved 2-10 2011-09-01
iv 2011-09-01 EASA approved 2-11 2011-09-01
v 2012-07- EASA approved 2-12 2012-07-03
vi 2011-09-01
vii 2012-07-3 3
viii 2012-07-03 EASA approved 3-1 2011-09-01
ix 2011-09-01 EASA approved 3-2 2011-09-01
x 2011-09-01 EASA approved 3-3 2011-09-01
xi 2011-09-01 EASA approved 3-4 2011-09-01
xii 2011-09-01 EASA approved 3-5 2011-09-01
xiii 2011-09-01 EASA approved 3-6 2011-09-01
xiv 2011-09-01 EASA approved 3-7 2011-09-01
xv 2011-09-01 EASA approved 3-8 2011-09-01
xvi 2011-09-01 EASA approved 3-9 2011-09-01
EASA approved 3-10 2011-09-01
1 EASA approved 3-11 2011-09-01
1-1 2011-09-01 EASA approved 3-12 2011-09-01
1-2 2011-09-01 EASA approved 3-13 2011-09-01
1-3 2011-09-01 EASA approved 3-14 2012-07-03
1-4 2011-09-01
1-5 2011-09-01
1-6 2011-09-01
4
2 4-1 2011-09-01
EASA approved 2-1 2011-09-01 4-2 2011-09-01
EASA approved 2-2 2011-09-01 4-3 2012-07-3
EASA approved 2-3 2011-09-01 4-4 2011-09-01
EASA approved 2-4 2011-09-01 4-5 2012-07-3
EASA approved 2-5 2011-09-01 4-6 2012-07-3
EASA approved 2-6 2011-09-01 4-7 2011-09-01
EASA approved 2-7 2011-09-01 4-8 2011-09-01
EASA approved 2-8 2012-07-3 4-9 2011-09-01

PS-POH-1-1-11LIST OF EFECTIVE PAGES P
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LIST OF EFFECTIVE PAGES (Cont’d)
Section Page Date Section Page Date
4 6
4-10 2011-09-01 EASA approved 6-12 2011-09-01
4-11 2012-07-3 EASA approved 6-13 2011-09-01
4-12 2012-07-3 EASA approved 6-14 2011-09-01
EASA approved 6-15 2011-09-01
5 EASA approved 6-16 2011-09-01
EASA approved 5-1 2011-09-01
EASA approved 5-2 2011-09-01 7
EASA approved 5-3 2011-09-01 7-1 2011-09-01
EASA approved 5-4 2011-09-01 7-2 2011-09-01
EASA approved 5-5 2011-09-01 7-3 2011-09-01
EASA approved 5-6 2011-09-01 7-4 2011-09-01
EASA approved 5-7 2011-09-01 7-5 2011-09-01
EASA approved 5-8 2011-09-01 7-6 2011-09-01
EASA approved 5-9 2011-09-01 7-7 2011-09-01
EASA approved 5-10 2011-09-01 7-8 2011-09-01
EASA approved 5-11 2011-09-01
EASA approved 5-12 2011-09-01 8
8-1 2011-09-01
6 8-2 2011-09-01
EASA approved 6-1 2011-09-01 8-3 2011-09-01
EASA approved 6-2 2011-09-01 EASA approved 8-4 2011-09-01
EASA approved 6-3 2011-09-01 EASA approved 8-5 2011-09-01
EASA approved 6-4 2011-09-01 8-6 2011-09-01
EASA approved 6-5 2011-09-01 8-7 2011-09-01
EASA approved 6-6 2011-09-01 8-8 2011-09-01
EASA approved 6-7 2011-09-01
EASA approved 6-8 2011-09-01 9
EASA approved 6-9 2011-09-01 9-1 2011-09-01
EASA approved 6-10 2011-09-01 9-2 2011-09-01
EASA approved 6-11 2011-09-01

PS-POH-1-1-11LIST OF ABBREVIATIONS P
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Date: 2011-09-01 ix Rev. No.: -
LIST OF ABBREVIATIONS
ADI Attitude direction indicator
AGL Above Ground Level
ALT Altitude or Altimeter
ATC Air Traffic Control
ASI Airspeed Indicator
bar Pressure unit (1 bar = 14.5037 psi)
BEACON Anti-collision beacon
°C Temperature in degree of Celsius (°C = (°F - 32) / 1.8)
CAS Calibrated Airspeed
CDI Course deviation indicator
C.G. Center of Gravity
CHT Cylinder head temperature
COMM Communication transceiver
EFIS Electronic Flight Information System
ELT Emergency Locator Transmitter
EMS Engine Monitoring System
°F Temperature in degree of Fahrenheit (°F = (°C x 1.8) + 32)
ft Foot or feet (1 ft = 12 in = 0.305 m = 305 mm)
fpm Vertical speed in feet per minute (1 fpm = 0.0051 m/s)
GPS Global Positioning System
hp Power unit (1 hp = 0.7457 kW)
IAS Indicated Airspeed
IC Intercom
IFR Instrument Flight Rules
in Inch (1 in = 25.4 mm)
ISA International Standard Atmosphere
KCAS Calibrated Airspeed in Knots
kg Kilogram (1 kg = 2.205 lb)
KIAS Indicated Airspeed in Knots
km Kilometer (1 km = 1000 m = 0.54 NM = 0.621 SM)
km/h Airspeed in kilometers per hour
(1 km/h = 0.54 knots = 0.621 mph = 0.278 m/s)
knot Airspeed in NM per hour
(1 knot = 1.151 mph = 1.852 km/h = 0.514 m/s)
KTAS True Airspeed in Knots
kW Power unit (1 kW = 1.341 hp)
L Liter (1 L = 0.22 UK gal = 0.264 US gal)
lb Pound (1 lb = 0.454 kg)
lbf Force unit (1 lbf = 4.448 N)
m Meter (1 m = 1000 mm = 3.28 ft = 39.37 in)
mm Millimeter (1 mm = 0.03937 in)
MAC Mean Aerodynamic Chord
max. Maximum
min. Minimum or minute
mph Airspeed in statute miles per hour(1 mph = 0.87 knots = 1.61 km/h)

PS-POH-1-1-11LIST OF ABBREVIATIONS P
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Date: 2011-09-01 xRev. No.: -
MTOW Maximum TakeOff Weight
m/s Vertical speed in meters per second
(1 m/s = 196.8 fpm = 1.944 knots = 3.6 km/h)
N Newton - force unit (1 N = 0.225 lbf)
NM Nautical mile (1 NM = 1,852 m)
OFF System is switched off or control element is in off-position
ON System is switched on or control element is in on-position
OAT Outside Air Temperature
POH Pilot’s Operating Handbook
psi Pressure unit - pound per square inch (1 psi = 0.0689bar)
rpm Revolutions per minute
s or sec Second
SM Statute Mile (1 SM = 1,609 m)
TAS True Airspeed
US gal US gallon (1 US gal = 0.83 UK gal = 3.785 L)
V Volt
VFR Visual Flight Rules
VMC Visual Meteorological Conditions
VSI Vertical Speed Indicator
VTU Vertical tail unit
VAManoeuvring airspeed
VFE Maximum flaps extended speed
VNE Never exceed speed
VNO Maximum structural cruising speed
VSStall speed with wing flaps in retracted position
VS1 Stall speed with wing flaps in takeoff position
VSO Stall speed with wing flaps in extended position
VXBest angle of climb speed
VYBest rate of climb speed

PS-POH-1-1-11CS-LSA STANDARDS
P PS S- -2 28 8 C Cr ru ui is se er r
Date: 2011-09-01 xi Rev. No.: -
CS-LSA STANDARD
The P
PS S- -2 28 8 C Cr ru ui is se er raircraft is designed and built according to CS-LSA standard.
CS-LSA, Initial Issue 27 June 2011
Certification Specification for Light Sport Aeroplanes

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PS-POH-1-1-11CONTACT INFORMATION P
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CONTACT INFORMATION
Czech Sport Aircraft a.s.
Na Záhonech 1177/212, 686 04 Kunovice
Czech Republic
Website: www.czechsportaircraft.com
E-mail: [email protected]
Phone: [phone] (Sales Dept.)
Fax: [phone]

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PS-POH-1-1-11TABLE OF CONTENTS P
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TABLE OF CONTENTS
1. General Information
2. Limitations
3. Emergency Procedures
4. Normal Procedures
5. Performance
6. Weight and Balance
7. Description of Airplane and Systems
8. Handling and Servicing
9. Supplements

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PS-POH-1-1-11
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SECTION 1
GENERAL INFORMATION P
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SECTION 1
TABLE OF CONTENTS
1. GENERAL INFORMATION
1.1 Airplane specification 1-2
1.2 Summary of performances 1-5

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1. GENERAL INFORMATION
This Pilot’s Operating Handbook (POH) has been prepared to provide pilots
with information for the safe and efficient operation of the P PS S- -2 28 8 C Cr ru ui is se er r
aircraft and contains 9 sections. It also contains supplementary information
considered to be important by the aircraft manufacturer.
Date of issue is written in the yy-mm-dd format.
NOTE
All airspeeds shown in the POH are IAS, except of shown otherwise.
Warnings, Cautions and Notes
The following definitions apply to warnings, cautions and notes in the POH.
WARNING
Means that the non-observation of the corresponding procedure leads to an
immediate or important degradation of the flight safety i.e. to injury or death of
persons.
CAUTION
Means that the non-observation of the corresponding procedure leads to a minor or
possible long term degradation of the flight safety.
NOTE
Draws attention to any special item not directly related to safety but which is
important or unusual.
1.1 Airplane specification
P
PS S- -2 28 8 C Cr ru ui is se er ris the airplane intended especially for recreational and cross-
country flying, and non-aerobatics operation.
P
PS S- -2 28 8 C Cr ru ui is se er ris a single-engine, all metal, low-wing monoplane of semi-
monocoque structure with two side-by-side seats. The airplane is equipped
with a fixed tricycle undercarriage with castering nose wheel.

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PS S- -2 28 8 C Cr ru ui is se er r
aircraft layout:

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Main airplane dimensions:
Wing span......................................................8.600 m
Length............................................................6.620 m
Height............................................................2.315 m
Wing area......................................................12.30 m2
Wing loading..................................................49 kg/m2
Cockpit width .................................................1.170 m
Flight control surfaces travel:
Rudder...........................................................30° ±2° to each side
Elevator .........................................................+24° / -24° ±2°
Aileron ...........................................................+15° / -15° ±1°
Flaps..............................................................0° to 30° ±1°
Aileron trim ....................................................+20° / -20° ±2°
Elevator trim ..................................................+22° / -28° ±2°
Anti-balance tab.............................................+25° / -19° ±2°
Engine:
Manufacturer .................................................BRP-Powertrain GmbH&Co.KG
Model number................................................912 S2
Maximum power rating ..................................73.5 kW at 5,800 RPM
Cooling ..........................................................liquid and air
Type ......................4-stroke, 4 cylinder, horizontally opposed, spark ignition
engine with one central camshaft-push-rod-OHV
Propeller:
Manufacturer .................................................WOODCOMP s.r.o.
Model number................................................KLASSIC 170/3/R
Number of blades ..........................................3
Diameter........................................................1,712 mm
Pitch setting...................................................17.5 ±0.5°
Type ..............................................................three composite blades,
ground adjustable