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Page 9 (ENGINE)
Tecnam P92-JS - ENGINE; PROPELLER
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F
LIGHT MANUAL
Date
:
Issue 3:
25
th
May201
0
1-5
P92-
JS
S
E
C
T
I
O
N
1
GENERAL
ENGINE
Manufactu
rer:
Bombardier
-Rotax Gm
bH
Model
912 S2
Certification basis
FA
R 33 Am
endment 15
Aus
trian Type-
Certification No.
n° TW 9
-ACG of 27 Nov. 1998
Type:
4
cylinder
hor
izontally-opposed
tw
ins
with
overall
displacem
ent
of
1352
c.c.,
m
ixed
cooling,
(w
ater-coo
led
heads
and
air-
cooled
cylin
ders),
tw
in
carburettors
,
integrated
reduction
gear
w
ith
torque
damper.
Maxim
um
power:
(engine’s rpm)
73.5 kW
(98
.6 hp
)
@ 580
0 rpm
(max.5 min
.)
69.0 kW
(92.5 hp)
@ 5500 r
pm
(contin
uous)
PROPELLER
Manufactu
rer:
HOFFMANN Propeller
Certification basis:
CAR Part 14
Type-Certification No.:
SO/E 30 o
f 10/12/199
9
Model:
HO17GHM A 174
177C
Num
ber of blad
es:
2
Diameter:
1740
m
m (no reduction permitted)
Type:
Fixed pitch - w
ood
8
10
Table of Contents
Main Page
F Light Manual
5
Flight Manual
1
Table of Contents
5
Section
5
Introduction
6
Certification Basis
6
Warnings - Cautions - Notes
6
Three-View Drawing
7
Descriptive Data
8
Control Surfaces Travel Limits
8
Engine
9
Propeller
9
Fuel
10
Oil System
10
Cooling
10
Maximum Certified Weights
11
Standard Weights
11
Specific Loadings
11
Abbreviations and Terminology
12
Unit Conversion Chart
15
Section 2
17
Airspeed Limitations
18
Introduction
18
Airspeed Indicator Markings
19
Powerplant Limitations
20
Propeller
21
Other Instrument Markings
22
Powerplant Instrument Markings
22
Center of Gravity Range
23
Weights
23
Approved Maneuvers
24
Flight Crew
24
Maneuvering Load Factor Limits
24
Fuel
25
Kinds of Operation
25
Crosswind Limitations
26
Limitation Placards
26
Maximum Passenger Seating
26
Section 3
27
Engine Failures
28
Engine Failure During Takeoff Run
28
Introduction
28
Air Start
30
Smoke and Fire
30
Glide
31
Landing Emergencies
31
Recovery from Unintentional Spin
32
Other Emergencies
33
Section 4
35
Introduction
36
Rigging and Derigging Engine Cowling
36
Pre-Flight Inspections
37
Checklists
40
Section 5
47
Introduction
48
Performance
48
Use of Performance Charts
48
Airspeed Indicator System Calibration (Approved Data )
49
Stall Speed (Approved Data )
51
Crosswind
52
Takeoff Performance (Approved Data )
53
Climb Performance
55
Cruise
56
Balked Landing
58
LANDING DISTANCE (Approved Data)
59
Consequences from Rain and Insect
60
Noise Data
60
Section 6
61
Aircraft Weighing Procedures
62
Introduction
62
Weighing Report
63
Weight and Balance
65
Equipment List
68
Loading
68
Section 7
73
Airframe
74
Introduction
74
Flight Controls
75
Instrument Panel
76
Baggage COMPARTMENT
77
Doors
77
Seats and Safety Harness
77
Fuel System
78
Powerplant
78
Electrical System
80
Pitot and Static Pressure Systems
82
Brakes
83
Marking & Placards
83
F M Light Anual
89
Aircraft Alterations or Repairs
90
Aircraft Inspection Periods
90
Ground Handling
90
Introduction
90
Cleaning and Care
91
Section 9 Supplements
93
Default Chapter
97
Emergency Procedures
97
Systems
98
Weight and Balance
98
Banner Towing
99
General
99
Limitations
99
Emergency Procedures
101
Normal Procedures
101
Performance
103
2 Introduction
99
Equipment List
106
Weight & Balance
106
Date: Issue 3: 25 Th May 2010
108
Differential Brake System
110
Emergency Procedures
110
General
110
3 Introduction
110
Limitations
110
Normal Operation
110
Performance
110
Weight and Balance
110
Systems
111
Central Throttle Control System
113
Emergency Procedures
113
General
113
4 Introduction
113
Limitations
113
Normal Operation
113
Performance
113
Systems
113
Weight and Balance
113
Emergency Procedures
115
General
115
New Analogical Instruments Panel
115
Normal Operation
115
Performance
115
Weight and Balance
115
Systems
116
5 Introduction
115
Limitations
115
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