Lightwing AC4 Especificaciones técnicas
AFM Lightwing AC4
LW-RL-Z-002 Rev.:2 Page 1
23.03.2018
Aircraft Flight Manual
For the Airplane
Lightwing AC4
Document No: LW-RL-Z-002
This document is issued for the following airplane:
Registration: HB-WEB
Serial Number: 003
Date & Signature Lightwing:
04.04.2018, Marco Trüssel, Light Wing AG
Lightwing AC4 AFM
Page 2 Rev.:2 LW-RL-Z-002
0.1 Amendments
Any revision of the present manual has to be registered in the following
chart.
Rev.
Pages
Description
Date
Approval
-
1..85
1st Edition.
12-May-14
EASA.A.588, 17.6.14
Rev.:0
1..87
Renumbered to document
LW-RL-Z-002
- addition heating system
- addition gear fairings
02-Mar-16
ELA1-HB
LW-RL-Q-003
EASA 10056955
EASA 10056950
Rev.:1
1..88
Minor change “Project 06”
- Addition FLARM
- Addition LED sight
gauge illumination
- Addition of approved
secions
19-Sep-17
ADxC-48-DC-002
Rev.:2
1..88
AFM Change for
EASA project 10062701
Major change “Project 03”
- 912iS “Sport”
23-Mar-18
AFM Lightwing AC4
LW-RL-Z-002 Rev.:2 Page 3
0.2 List of approved sections
Section
Name
Status
2.
3.
5.
6.1 & 6.2
Limitations
Emergency procedures
Performance
Weight and Balance
Approved (EASA.A.588)
Approved (EASA.A.588)
Approved (EASA.A.588)
Approved (EASA.A.588)
Lightwing AC4 AFM
Page 4 Rev.:2 LW-RL-Z-002
0.3 List of effective pages
Page
Date
Page
Date
Page
Date
Cover
23-03-18
31
23-03-18
62
23-03-18
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AFM Lightwing AC4
LW-RL-Z-002 Rev.:2 Page 5
0.4 Table of contents
This aircraft flight manual supplement consists of the following parts:
1General
2Limitations
3Emergency procedures
4Normal procedures
5Performance
6Weight and balance / equipment
7Aircraft and systems description
8Handling and maintenance
Following the recommended structure for flight manuals as defined in
GAMA Specification No. 1.
The following documents belong to this aircraft flight manual:
- Operation manual for engine ROTAX 912iSc/iS "Sport"
- manuals for installed avionics
oSkyview System
oPower Flarm
oRadio with Intercom
oTransponder
The Airplane flight manual must be carried on board the airplane at all
times. It should be stored in the aircraft.
0.5 Contact information
Light Wing AG
Riedenmatt 1
6370 Stans
Switzerland
www.Lightwing.ch
Lightwing AC4 General
Page 6 Rev.:2 LW-RL-Z-002
1 General
1.1 Introduction
This aircraft flight manual includes information and procedures for
pilots for safe and effective operation of this aircraft. This aircraft flight
manual includes information that should be made available to the pilot
according to CS-LSA regulations. It includes further information and
procedures which Light Wing AG Company considers useful for the
pilot.
The aircraft manual is corrected and amended by EASA
CAUTION: This airplane flight manual has to be carried
on board at all times.
1.2 Certification Basis
The AC4 is certified on 17-Jun-2014 by the European Aviation Safety
Agency (EASA) under CS-LSA with type certificate EASA.A.588.
Category: Light Sport Aircraft;
Noise certificate ICAO Annex 16, Chapter X.
General Lightwing AC4
LW-RL-Z-002 Rev.:2 Page 7
1.3 Warnings, cautions and notes
Statements in this handbook, which are particularly important for safety
of flight or operation of the airplane, are highlighted by one of the
following notions:
WARNING: means that non-observance of the
respective procedure leads to immediate or
considerable reduction of flight safety.
CAUTION: means that non-observance of the respective
procedure leads to a reduction of flight safety
in the long term.
NOTE: shall bring attention to facts which are not
directly related to safety of flight, but which are
important or unusual.
Lightwing AC4 General
Page 8 Rev.:2 LW-RL-Z-002
1.4 Descriptive data
The Lightwing AC4 aircraft is a single engine two-seater light sport
airplane with side by side seating. It is built in a high strutted wing
configuration with a conventional strutted tail.
The aircraft has a dual control system with a single central control stick.
The undercarriage is fixed tricycle landing gear type, with the nose
wheel steering.
1.4.1 Dimensions and important data
Dimensions external
wing span (incl. wing tips): 9.446 m
wing span (incl. wing tips lights): 9.565 m
max. length (spinner to rudder tip): 6.950 m
max. height: 2.670 m
Wing
wing surface: 12.70 m2
Aileron
deflection up: 22° (± 2°)
deflection down: 20° (± 2°)
Flaps
control system: electric
deflection: 0°/10°/24°Down ± 2°
Horizontal tail
span: 2.910 m
deflection up: 30° ± 2°
deflection down: 30° ± 2°
Servo tab (right elevator):
Fletter tab geared to elevator deflection (angles are with respect to
elevator chord)
with elevator 30° UP 26° ± 2° dwn
with elevator neutral 12° ± 2° dwn
with elevator 30° DWN 7° ± 2° up
General Lightwing AC4
LW-RL-Z-002 Rev.:2 Page 9
Pitch trim (left elevator):
Trim tab with an electric actuator at the left hand elevator trailing edge.
Geometric deflection versus elevator: 5° up / 27° dwn ± 2°
Vertical tail surfaces
surface: 1.207 m2
deflection: left/right 25° ± 2°
Undercarriage
fixed tricycle landing gear
shock absorption/nose gear: elastomer
shock absorption/main gear: steel leaf spring
wheel base: 1.851 m
wheel track: 1.916 m
main wheels/pressure: 15x6.00-6/3.0bar
nose wheel/pressure: 4.00-6/2.7bar
Brakes
Central braking at the main gear using floating disk brakes.
Lightwing AC4 General
Page 10 Rev.:2 LW-RL-Z-002
1.4.2 Powerplant
Engine:
Rotax 912iSc/iS "Sport" naturally aspirated, 4 Stroke petrol engine,
with 4 horizontally opposed cylinders with dry sump lubrication, dual
ignition with breakerless capacitor discharge design, fuel injection
supplied by a dual electric fuel pump, liquid cooled cylinder heads, ram
air cooled cylinders, prop drive gear reduction ratio of 2.43:1.
Propeller:
Type: fixed pitch
Blade: CR3-75 3-blade
Diameter: 1.75 m
Manufacturer: Neuform Composites GmbH&Co
Blade setting (gaugeable secant): 25° at 365mm from hub centre
Otros manuales para AC4
1
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