Rotax CESSNA 150 User manual

,
Airplane Flight Manual
CESSNA 150
Series F150L
Engine: ROTAX 912 S3
Propeller: Hoffmann HO-V352F/170FQ+10
SDF Nr. 160
Revision 1
April 2001
OK-RTX
Blue Skies Aviation Oy
Lentotie 89
17130 Vesivehmaa
E-Mail: [e-mail]
Internet: http://www.blueskies.fi www.rotax-cessna.com

Airplane Flight
Manual Cessna F150LNr. 160
Converted with conversion kit NS402S with ROTAX 912 S3 and Page: 0-2
HOFFMANN HO-V352F/170FQ+10 Edition 1
0 0 CONTENTS
Section 0: Record of revisions
Section 1: General
Section 2: Operating limits
Section 3: Emergency Procedures
Section 4: Normal Operating Procedures
Section 5: Service and maintenance
Section 6: Airplane handling
Section 7: Weight and balance
Section 8: Optional Equipment, Equipment List
This manual describes the operation and performance of the Cessna () 150 () model with the
conversion NS402S with ROTAX 912S3 and HOFFMANN HO-V352F / 170FQ + 10 propeller.
The flight manual applies to all models and was created using the original AFM of the Cessna
(F) 150M series. Deviating information under the individual model is marked accordingly.
NOTE
The content of this document replaces or supplements the information of the
original flight manual only in the relevant section; Only the data that is
affected due to conversion NS-402S is amended
DISCLAIMER
THIS TRANSLATION IS NOT AN OFFICIAL VERSION. THE GERMAN LANGUAGE
VERSION IS THE ONLY APPROVED VERSION. SHOULD THERE BE A CONFLICT
BETWEEN THIS MANUAL AND THE GERMAN VERSION, THE GERMAN VERSION IS
PREVAILING

Airplane Flight
Manual Cessna F150L Nr. 160
Converted with kit NS402S with ROTAX 912 S3 and Page: 0-3
HOFFMANN HO-V352F/170FQ+10 Edition 1 - A
SUMMARY OF REVISIONS
Change
Nr.
Changed pages
Reason for change /
Remarks
LBA –recognized
Date
endorsement
A
0-3, 0-4
2-2b
4-2, 4-3
5-6 remove
5-6a, 5-6b, 5-6c, 5-6d, 5-
6e add
Operating limits f. (F) 150M
Minor corrections
Airspeed Correction Tables
corrected type specific.
09.07.02/Sp

Airplane Flight
Manual Cessna F150LNr. 160
Converted with kit NS402S with ROTAX 912 S3 and Page: 0-4
HOFFMANN HO-V352F/170FQ+10 Edition 1- A
TYPE SPECIFIC AFM PAGES
Series
SERIES-SPECIFIC PAGES
(F)150F
1-6a, 2-2a, 2-5a, 2-7a, 5-6a, 7-2a, 7-3a, 7-4a, 7-5a, 7-6a, 8-2a, 8-3a
(F)150G
1-6a, 2-2a, 2-5a, 2-7a, 5-6a, 7-2a, 7-3b, 7-4a, 7-5a, 7-6a, 8-2b, 8-3b, 8-4b
(F)150H
1-6a, 2-2a, 2-5a, 2-7a, 5-6a, 7-2a, 7-3b, 7-4a, 7-5a, 7-6a, 8-2c, 8-3c, 8-4c, 8-
5c, 8-6c, 8-7c
(F)150J
1-6a, 2-2a, 2-5a, 2-7a, 5-6a, 7-2a, 7-3b, 7-4a, 7-5a, 7-6a, 8-2c, 8-3c, 8-4c, 8-
5c, 8-6c, 8-7c
(F)150K
1-6b, 2-2a, 2-5a, 2-7a, 5-6b, 7-2c, 7-3c, 7-4c, 7-5c, 7-6c, 7-7c, 8-2d, 8-3d, 8-
4d, 8-5d, 8-6d, 8-7d, 8-8d
(F)150L
1-6b, 2-2a, 2-5a, 2-7a, 5-6b, 7-2c, 7-3c, 7-4c, 7-5c, 7-6c, 7-7c, 8-2d, 8-3d, 8-
4d, 8-5f, 8-6f, 8-7f, 8-8f, 8-9f, 8-10f, 8-11f
(F)150M
1-6c, 2-2b, 2-5b, 2-7b, 5-6e, 7-2d, 7-3d, 7-4d, 7-5d, 7-6d, 7-7d, 7-8d, 7-9d, 7-
10d, 7-11d, 7-12d, 7-13d, 8-2d, 8-3d, 8-4d, 8-5f, 8-6f, 8-7f, 8-8h, 8-9h, 8-10h,
8-11h, 8-12h
(F)A150K
1-6b, 2-2c, 2-5c, 2-7c, 5-6c, 7-2c, 7-3c, 7-4c, 7-5c, 7-6c, 7-7c, 8-2d, 8-3d, 8-
4d, 8-5e, 8-6e, 8-7e, 8-8e
(F)A150L
1-6b, 2-2c, 2-5c, 2-7c, 5-6d ,7-2c, 7-3c, 7-4c, 7-5c, 7-6c, 7-7c, 8-2d, 8-3d, 8-
4d, 8-5f, 8-6f, 8-7f, 8-8g, 8-9g, 8-10g, 8-11g

Airplane Flight Manual Nr. 160
Page: 1-1
Cessna F150L
Converted with conversion kit NS402S with ROTAX 912 S3 and
HOFFMANN HO-V352F/170FQ+10 Revision 1
1 GENERAL
NOTE
In addition to the instructions for use, this manual also includes a list of maintenance and
periodic inspections and performance data.
DOCUMENTS TO BE CARRIED ON BOARD
1) Certificate of Airworthiness
2)Certificate of Registration
3) Radio license
4) Logbooks
5) Airplane Flight Manual
NAMEPLATE AND COLOR CODE PLACARD
In correspondence regarding your aircraft, the aircraft serial number must be specified. The
serial number, pattern, registration mark and letter D are indicated on the nameplate, which is
located on the cabin floor below the left rear corner of the pilot's seat. The sign is accessible
when the seat is forwarded, and the carpet is raised into this area. Next to the nameplate is a
color-coded label which contains a code for the color of the cabin lining and the exterior paint
of the aircraft. The code can be used in conjunction with a relevant Parts Catalog if paint and
cabin lining information is required.

Airplane Flight Manual Nr. 160
Page: 1-2
Cessna F150L
Converted with conversion kit NS402S with ROTAX 912 S3
and HOFFMANN HO-V352F/170FQ+10 Revision 1
Fig. 1 - 1

Airplane Flight Manual Nr. 160
Page: 1-3
Cessna F150L
Converted with conversion kit NS402S with ROTAX 912 S3 and
HOFFMANN HO-V352F/170FQ+10 Revision 1
DESCRIPTION AND DIMENSIONS
GENERAL DIMENSIONS
Wingspan: 10.16 m
Maximum length: 7.5 m
Maximum height: 2.63 m
WING
Wing profile: NACA 2412
Wing area: 14.9 m2
V position: + 1 ° (top at 25% line)
Setting angle wing root: + 1 °
Wingtip: 0 °
AILERONS
Area: 1.66 m2
Movement up: 20 ° + 2 °-0 °
Movement down: 14 ° + 2 °-0 °
WING FLAPS
Type of operation: Electric / cable
Area: 1.72 m2
Rash: 0 to 40 ° ± 2 °
STABILATOR AND ELEVATOR
Fin area: 1.58 m2
Angle: -3 °
Rudder area: 1.06 m2 (including trim flap)
Movement upward: 25 ° + 1 °-0 °
down: 15 ° ± 1 °

Airplane Flight Manual Nr. 160
Page: 1-4
Cessna F150L
Converted with conversion kit NS402S with ROTAX 912 S3 and
HOFFMANN HO-V352F/170FQ+10 Revision 1
ELEVATOR TRIM
Movement up: 10 ° ± 1 °
Movement down: 20 ° ± 1 °
RUDDER AND FIN
Fin area: 0.83 m2
Rudder area: 0.65 m2
Movement to the left: 23 ° + 0 ° (perpendicular to the axis of rotation) -2°
Movement to the right: 23 ° + 0 °-2 °
LANDING GEAR
Type: fixed tricycle landing gear
Strut, nose gear: air - oil
Main landing gear: width: 2,32m
Distance between main gear wheels and nose gear wheel: 1.46 m
Nose wheel tire and pressure: 5.00 - 5 30 psi (2.109 kg / cm2)
Main tires and pressure: 6.00 - 6 21 psi (1.476 kg / cm2)
Nose landing gear strut pressure: 20 psi (1,406 kg / cm2)
POWER PLANT
ENGINE: ROTAX 912S3 100HP (73.5KW)
FUEL:
Normal, Super, Super Plus unleaded, EN 288 at
least 95 RON or avgas 100ll in exceptional
cases.
OIL
Corresponding to opposite table (FIG. 1 - 2)
Use only oils meant for OTTO engines that
comply with API system with "SF" or "SG"
marking
Do not use aircraft engine oil.
Do not use any oil additives.
FIG 1-2 OIL TABLE

Airplane Flight Manual Nr. 160
Page: 1-5
Cessna F150L
Converted with conversion kit NS402S with ROTAX 912 S3 and
HOFFMANN HO-V352F/170FQ+10 Revision 1
COOLANT
Approximately 2.5 ltr.for mixing and frost prevention see ROTAX–operating handbook
CARBURETOR HEAT
Manual operation
PROPELLER
Designation: HOFFMANN HO-V352F / 170FQ + 10
Type: 2-blade, constant speed
Diameter: 1.8 m
CABIN
Seats: 2 (plus optional child seat)
Doors: 2
Luggage: 54 kg

Airplane Flight Manual Nr. 160
Page: 1-6b
Cessna F150L
Converted with kit NS402S with ROTAX 912 S3 and
HOFFMANN HO-V352F/170FQ+10 Revision 1
INSTRUMENT PANEL ()(A)150K-L
1 turn Coordinator
2 airspeed indicator
3 Direction indicator
4 Attitude indicator
5 clock
6 airplane registration No.
7 Variometer
8 Altimeter
9 Marker beacon /
indicator lights
10 Accelometer (Aerobat)
or course deviation and ILS indicator
11 Course deviation and ILS Indicator
12 Mirror
13 radios
14 Tachometer
15 Left fuel gauge
16 Ammeter
17 Right fuel gauge
18 Fuel pressure
19 Amperemeter
22 oil pressure
23 Cabin heat and air controls
24 wing flap switch
25 Cigarette lighter
26 Propeller control
27 Choke
28 Microphone
29 throttle
30 Elevator trim
31 Carburetor heat
32 electrical switches
33 Circuit breakers
34 Rheostat for instruments
35 Rheostat for radios
36 deleted
37 Magneto and starter switch
38 main switch
39 Fuel pump switch
40 Parking brake
42 Generator warning lamps and circuit breakers
46 Oil temperature
47Cylinder head temperature
NOTE
The presented instrument arrangement is only one of several possibilities. Depending on the equipment and space requirements, the
arrangement may differ. To improve the visibility, engine monitoring instruments can be switched from the right to the left side of the
instrument panel or set up on the right side. The responsible pilot must familiarize himself with the respective order before the flight.