FLIGHT DESIGN CT User manual

THIS DOCUMENT IS THE PROPERTY OF FLIGHT DESIGN
AND MAY NOT BE CITED, REPRODUCED, DISCLOSED OR DISTRIBUTED IN WHOLE OR IN PART
WITHOUT PRIOR EXPRESS WRITTEN PERMISSION OF FLIGHT DESIGN
Template No.: PZ 0100 0034_00
Supplement S3 to the
Airplane Maintenance Manual (AMM)
CTLS-LSA with ROTAX 912 iS
Airplane Type : CT
Airplane Model : CTLS-LSA
Airplane Registration Number : _______________
Airplane Serial Number : _______________
Document Number : AF 0480 0011
Date of Issue : 05-Aug-12
This Manual is Approved on the Basis of Manufacturer Self Declaration

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 02 16-Jul-14 I-1
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
I RECORD OF SUPPLEMENT REVISIONS
Supplement revisions are provided by Flight Design GmbH as available. The updates shall
be manually entered to the individual printed version of the AMM by the Pilot/Owner of the
aircraft.
Supplement updates are provided in electronic format (pdf file) directly to aircraft
Pilots/Owners, when the Pilot/Owner leaves the correct contact information with Flight
Design GmbH. Supplement updates are also provided through the webpage of Flight
Design GmbH, in the section Service Documents:
http://www.flightdesign.com/index.php?page=service.
It is the duty of the aircraft Pilot/Owner to ensure that the supplement contains all updates
applicable to his aircraft serial number. Updates are done by manually removing invalid
sections and inserting new or updated sections. Supplement update must be logged in the
subsequent table.
Rev.
No. Date Sections Removed Sections Inserted Signature Rev. No. Date Sections Removed Sections Inserted Signature
00
01
02
05-Aug-12
20-Jan-14
16-Jul-14
n/a
01-00
01-00
04-00
05-10
all
01-00
01-00
04-00
05-10
n/a
n/a
n/a

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 02 16-Jul-14 II-1
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
II LIST OF EFFECTIVE SECTIONS
Sect.
No. Rev. No. Approval Reference
I 02 Self Declaration
II 02 Self Declaration
III 00 Self Declaration
01-00 02 Self Declaration
02-00 00 Self Declaration
04-00 02 Self Declaration
05-00 00 Self Declaration
05-10 02 Self Declaration
05-20 00 Self Declaration
05-30 00 Self Declaration
11-00 00 Self Declaration
12-00 00 Self Declaration
28-00 00 Self Declaration
71-00 00 Self Declaration
73-00 00 Self Declaration
74-00 00 Self Declaration
75-00 00 Self Declaration
76-00 00 Self Declaration
77-00 00 Self Declaration
78-00 00 Self Declaration
79-00 00 Self Declaration

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 00 05-Aug-12 III-1
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
III TABLE OF CONTENTS
I RECORD OF SUPPLEMENT REVISIONS
II LIST OF EFFECTIVE SECTIONS
III TABLE OF CONTENTS
CHAPTER 01 – INTRODUCTION
CHAPTER 02 – ORGANIZATION AND HANDLING OF THE SUPPLEMENT
CHAPTER 04 – AIRWORTHINESS LIMITATIONS
CHAPTER 05 – TIME LIMITS AND MAINTENANCE CHECK
SECTION 05-10 – TIME LIMITS
SECTION 05-20 – SCHEDULED MAINTENANCE CHECK
SECTION 05-30 – UNSCHEDULED MAINTENANCE CHECK
SECTION 12-10 – REPLENISHING
CHAPTER 28 – FUEL SYSTEM
CHAPTER 71 – ENGINE
CHAPTER 73 – ENGINE FUEL AND CONTROL
CHAPTER 74 – IGNITION
CHAPTER 75 – COOLING
CHAPTER 76 – ENGINE CONTROLS
CHAPTER 77 – ENGINE INDICATING
CHAPTER 78 – EXHAUST
CHAPTER 79 – OIL SYSTEM

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 02 16-Jul-14 01-00-1
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
CHAPTER 01 – INTRODUCTION
Contents
01-00.1 General
01-00.2 Approval
01-00.3 Certification Basis
01-00.4 Manufacturer Contact
01-00.5 Recovery of Certification Data
01-00.6 General Safety Information
01-00.7 Source to Purchase Parts
01-00.8 List of Disposable Replacement Parts
01-00.9 Recommended Torque Values
01-00.1 General
This Supplement to the Airplane Maintenance Manual (AMM) contains the data necessary
to carry out the maintenance of the CTLS-LSA with ROTAX 912 iS, ROTAX 912 iS Sport
or ROTAX 912 iSc Sport installed. This Supplement contains a full description of the
systems options and maintenance instructions thereof. The Supplement provides only the
additional information that results from the differences of the ROTAX 912 iS, ROTAX 912
iS Sport or ROTAX 912 iSc Sport engine installation. All other information of the basic
Aircraft Maintenance Manual (AMM), that is not covered here, remain valid.
Use the following additional sources of information together with this AMM:
1. Applicable Service Notifications including referenced Service Instructions,
2. Applicable Service Bulletins including referenced Service Instructions,
3. Applicable Safety Alerts including referenced Service Instructions.
4. ROTAX 912i series manuals issued by ROTAX for the affected engine S/N:
- Operator’s Manual OM-912i
- Maintenance Manual (Line Maintenance) MML-912i
- Maintenance Manual (Heavy Maintenance) MMH-912i
▲Warning: This document is valid only for the aircraft S/N identified on the cover
sheet (call-sign might change). It may not be transferred to any other
operated aircraft.
▲Warning: This document may be applied only to CTLS aircraft that have been
factory produced with the ROTAX 912 iS injection engine.
●Note: Unless explicitly stated otherwise: When using only the term ROTAX
912 iS within this manual, this is intended to refer to all engine versions
ROTAX 912 iS, ROTAX 912 iS Sport and iSc Sport.

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 02 16-Jul-14 01-00-1
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
01-00.2 Approval
The contents of this manual is approved on the basis of Manufacturer Self Declaration
against the applicable ASTM industry standard.
01-00.3 Certification Basis
The engines Rotax 912 iS and iS Sport are in compliance with ASTM F2339. The engine
Rotax 912 iSc Sport is Type Certified in compliance with CS-E Amdt. 3.
The engine installation to the airframe is in compliance with ASTM F2245.
This supplement to the AMM is generated in compliance with ASTM F2483, and is part of
the Required Product Information per ASTM F2745.
The revision level of the standards applicable to the specific S/N is identified on the
aircraft’s Statement of Compliance.
01-00.4 Manufacturer Contact
The aircraft is manufactured by:
Flight Design GmbH
Zum Tower 4
01917 Kamenz
Germany
Web: www.flightdesign.com
e-mail: [email protected]
01-00.5 Recovery of Certification Data
If the original manufacturer will lose the ability to support the make and model of this
aircraft, you can recover certification documentation through the following contact:
EUA Engineering Ukraine Ltd.
Rabochaya 82a
73000 Kherson
Ukraine
01-00.6 General Safety Information
Consider the following warnings to avoid unnecessary risks while you carry out
maintenance of the aircraft:
▲Warning: Only the personnel with adequate qualification may carry out an
inspection and maintenance work.
▲Warning: You shall carry out inspection and maintenance in accordance with
respective national safety requirements.
▲Warning: Before you begin any work, you shall read and understand all relevant
sections of this AMM. In case of any doubt or missing information you
shall first contact the manufacturer for advice.
▲Warning: Consider the safety notes in this supplement as unconditional.

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 01 20-Jan-14 01-00-2
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
01-00.7 Source to Purchase Parts
Spare parts can be ordered directly with the airplane manufacturer:
Flight Design GmbH
Zum Tower 4
01917 Kamenz
Germany
Web: www.flightdesign.com
e-mail: [email protected]
or through the Flight Design distributor or service center that is responsible for your area.
You can find contact details of the distributors and service centers on the Flight Design
web page.
01-00.8 List of Disposable Replacement Parts
Chapter Item Overhaul Replacement Time
71-00.3.3 Air filter no 1 year
28-00.3.3 Fuel Filter no 50h
79-00.3.3 Oil filter no 50h
74 Spark plugs no 200 h
01-00.9 Recommended Torque Values
Refer to basic AMM.

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 00 05-Aug-12 02-00-1
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
CHAPTER 02 – ORGANIZATION AND HANDLING OF THE
SUPPLEMENT
Contents
02-00.1 Supplement Structure
02-00.1.1 Chapter and Subchapter Structure
02-00.1.2 Page Numbering System
02-00.1.3 Figures
02-00.1.4 Warnings, Cautions and Notes
02-00.1.5 Abbreviations
02-00.2 Supplement Handling
02-00.2.1 Record of Revisions
02-00.2.2 List of Effective Sections
02-00.2.3 Feedback Template
02-00.1 Supplement Structure
02-00.1.1 Chapter and Subchapter Structure
This AMM Supplement is structured using the ATA 100 structure for system / subsystem
as guideline. This is reflected in the main header of each Chapter, Section and in the
section numbers. Four digits are used that represent:
25- 60
System- Subsystem
Chapter No.- Section No.
The contents of chapter and subchapter are structured similarly, so that you can find
required information quickly. For your convenience each chapter contains its own table of
contents.
02-00.1.2 Page Numbering System
Pages are numbered using a combination of the chapter and section number, followed by
the page number, each separated with a dash ”-“.
02-00.1.3 Figures
Figures are numbered using a combination of the chapter and section number, followed by
a sequential number that starts with 1 for each subsystem, each separated with a dash ”-“.

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 00 05-Aug-12 02-00-2
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
02-00.1.4 Warnings, Cautions and Notes
Please pay attention to the following symbols which are used throughout this document to
emphasize certain information:
▲Warning: Used to identify an instruction which if not followed may cause serious
injury or even death.
■Caution: Used to identify an instruction which if not followed may damage the
aircraft severely or lead to the warranty suspension.
●Note: Information useful for better handling.
“Shall”, “will”, “should” and “may”:
The words “shall” or “will” are used to express a mandatory requirement or instruction. The
word “should” is used to express non-mandatory provisions that are nevertheless highly
recommended. The word “may” is used to express permissible provisions.
02-00.1.5 Abbreviations
The table below contains the abbreviations used in this AMM.
Abbreviation Meaning
AMM Airplane Maintenance Manual
FAA Federal Aviation Administration
LSA Light Sport Aircraft
POH Pilot’s Operating Handbook
TBO Time Between Overhaul
TBR Time Between Replacement
02-00.2 Supplement Handling
02-00.2.1 Record of Revisions
This supplement has a Record of Revisions. Use the Record of Revisions to show when
changes were included in this supplement.
02-00.2.2 List of Effective Sections
This supplement has a List of Effective Sections. The List of Effective Sections shows you
the number and effective date of each section of this supplement. This system implies that
revisions are always done section wise; when information in one section changes, all
pages of that section get changed.
02-00.2.3 Feedback Template
Use the Feedback Template provided by the basic AMM to inform manufacturer about
difficulties experienced during maintenance.

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 02 16-Jul-14 04-00-1
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
CHAPTER 04 – AIRWORTHINESS LIMITATIONS
Contents
04-00.1 General
04-00.2 Environmental Limitations
04-00.3 Operational Limitation
04-00.4 Life Limited Components
04-00.1 General
This Section shows the mandatory limitations established by the airframe manufacturer.
These limitations shall be obeyed by the maintenance personnel.
In addition to this, the manufacturer recommends you to comply with the maintenance time
limits and to work with the maintenance checklists (refer to CHAPTER 05 – TIME LIMITS
AND MAINTENANCE CHECK).
In any case you must comply with the national maintenance requirements.
04-00.2 Environmental Limitations
Limitations provided in the basic aircraft AMM remain valid.
04-00.3 Operational Limitation
Limitations provided in the basic aircraft AMM remain valid.
04-00.4 Life Limited Components
The engine installation does not include life limited components. Time limits as listed in
CHAPTER 05 shall be used to ensure continued airworthiness of the Flight Design CTLS-
LSA.

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 00 05-Aug-12 05-00-1
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
CHAPTER 05 – TIME LIMITS AND MAINTENANCE CHECK
Contents
05-00.1 General
05-00.2 Levels of Certification
SECTION 05-10 – TIME LIMITS
05-10.1 General
05-10.2 Scheduled Maintenance Time Limits
05-10.3 Component Time Limits
05-10.3.1 Time between Overhaul
05-10.3.2 Time between Replacement
SECTION 05-20 – SCHEDULED MAINTENANCE CHECK
05-20.1 General
05-20.2 Scheduled Maintenance Checklist CTLS-LSA
05-20.2.1 Identification
05-20.2.2 Aircraft Records
05-20.2.3 Run-Up
05-20.2.4 Post Run-Up, Pre-inspection and Preparations
05-20.2.5 Propulsion System
05-20.2.6 Fuselage
05-20.2.7 Wings
05-20.2.8 Empennage
05-20.2.9 Landing Gear
05-20.2.10 Cabin and Baggage Compartment
05-20.2.11 Return to Service
05-20.3 Flight-Line Check
05-20.3.1 General
05-20.3.2 Pre-Flight Check
05-20.3.3 Post-Flight Check
SECTION 05-30 – UNSCHEDULED MAINTENANCE CHECK
05-00.1 General
This chapter contains time limits and maintenance checklists for the CTLS-LSA. We highly
recommend you to comply with the maintenance time limits and to work with the
maintenance checklists.
05-00.2 Levels of Certification
Levels of certification used in this manual are:
Pilot/Owner: The owner of an aircraft who holds a pilot certificate but who has not
received any specific authorized training. Note: FAA regulations
authorize SLSA aircraft owners who hold at least a sport pilot certificate
to perform maintenance as outlined in 14CFRPart43.
RLSA-M: The holder of a LSA Repairman certificate with a maintenance rating.
This is generally considered the minimum level of certification to
perform line maintenance of LSA.

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 00 05-Aug-12 05-00-2
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
A&P: An Airframe and Powerplant mechanic as defined by 14 CFR Part 65 in
the U.S. or equivalent certification in other countries.
●Note: For certificated persons such as an A&P, RLSA-M or persons working
under the auspices of a Repair Station, prior experience will be
considered when determining the training required.
●Note: Participation in training described in this manual shall not be construed
as an implicit authorization by Flight Design to perform inspections or
repairs beyond the limitations set forth in the applicable regulations of
the governing aviation authority.
For and questions or comments regarding maintenance procedures or minimum levels of
certification, email Flight Design at [email protected].

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 02 16-Jul-14 05-10-1
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
SECTION 05-10 – TIME LIMITS
05-10.1 General
All scheduled maintenance checks have time limits. You shall do the scheduled
maintenance within the time limits.
05-10.2 Scheduled Maintenance Time Limits
The table below contains scheduled maintenance time limits recommended by the
manufacturer. Different tolerances may apply due to national regulations, depending from
the type of operation.
Scheduled Maintenance Task at these times Tolerance
100 hour check * At 100 hours since new and every 100 hour
interval. Do the work of 100 hour check.
Perform all engine 100 hour inspection
items per engine manufacturer
maintenance manual
Perform all propeller 100 hour inspection
items per propeller manufacturer
maintenance manual
±10 hours
25 hour check * At 25 hours since new or at 25 hours after
change or overhaul of engine and/or
propeller.
Perform all engine 100 hour inspection
items per engine manufacturer
maintenance manual
Perform all propeller 25 hour inspection
items per propeller manufacturer
maintenance manual
±5 hours
“Other times” checks At specified time interval from checklist
since new and every specified time interval.
Do the work for “other times” interval
specified in checklist
±10 hours
Annual check At 12 month from new and every 12 month
interval.
Do the work of annual check.
±30 days
* All of the (engine) maintenance intervals relate to the number of operating hours of the engine, whereas all time during the engine is
running is counted towards the total number of operating hours, irrespective of load factor of the engine, such as idling or take-off
power.
05-10.3 Component Time Limits
The following table lists airplane components which must be replaced or overhauled (as
specified) at a specific time.
To allow monitoring the permissible service life the installation or removal of each item
must be recorded in the aircraft documentation.
■Caution: Under specific environmental circumstances the replacement or overhaul
of components may be required before reaching the time limits as listed
below. Also, authorized extensions or exceeding of time limits may exist
from particular component manufacturers.

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 02 16-Jul-14 05-10-2
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
Chapter Item Overhaul Replacement
71-00.3.2 Engine shock mount no 2000 h or with engine replacement,
whichever comes first
28-00
75-00
79-00
71-00.3.3
All engine rubber parts, such as:
All rubber hoses of the cooling system
All rubber hoses of the fuel system (incl. Teflon hoses,
fuel pump and insulating flange if this is fixed with fuel
hoses)
All rubber hoses of the lubrication
Connecting hose of the air intake system
no 5 years
71-00.3.2 Engine ROTAX
®
912iS / iSc 2000h or 15 years whichever comes first
(1) On condition
(1) Refer to latest informsation issued by BRP- ROTAX
®
concerning the TBO, (Service Bulletins, Service Information,
Maintenance Manual for ROTAX
®
Engine Type 912i Series.

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 00 05-Aug-12 05-20-1
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
SECTION 05-20 – SCHEDULED MAINTENANCE CHECK
05-20.1 General
Perform the scheduled maintenance checks in this Section at the intervals (operating
hours and calendar time) marked in SECTION 05-20 with a “” or at the time specified.
●Note: Only persons authorized by the National Aviation Authority of the
country where the airplane is registered may perform these checks.
●Note: The inspection level for each item is a general visual inspection unless
differently specified.
●Note: The Maintenance Manual of the ROTAX
®
912 iS engine contains the
periodic maintenance schedule for this engine. We highly recommend
you to perform the 100-hour checks of the engine at the same time with
the airframe inspection.
05-20.2 Scheduled Maintenance Checklist CTLS-LSA
05-20.2.1 Identification
Name of
Pilot/Owner
Call-sign
Aircraft S/N
F-___-___-___
Operating Hours
Engine S/N
Operating Hours
TTSN/ TTSO
Propeller S/N
Operating Hours
TTSN/ TTSO
Maintenance
Organization
Name of Inspector
Hours since Last
Scheduled
Inspection
Type of Last
Scheduled
Inspection
100h annual
other:______________
Date of Inspection Type of Inspection
100h annual
other:______________

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 00 05-Aug-12 05-20-2
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
05-20.2.2 Aircraft Records
This chapter of AMM is not affected by this Supplement
05-20.2.3 Run-Up
▲Warning: Run-up shall be performed before any inspection.
▲Warning: Run-up shall continue until all temperatures are acceptable for take-off.
Inspection and/or Required Maintenance
Checklist
100hour
Annual
Other Times
Minimum
Level of
Certification
Initials /
Remarks
Engine and engine compartment
Clean for leakage check

Pilot/Owner
Run up of engine: Conduct per following checklist,
fill pre-inspection values only:

Pilot/Owner
Systems Pre-inspection Post-inspection
Engine oil. Check the level of oil and follow the Operator’s
Manual for all versions of ROTAX
®
912 iS or SECTION 12-10.
 
Brakes and parking brake. Check for proper operation
 
Starter. Smooth operation, starting properties
 
Oil pressure. 3…5 bar / 44…73 PSI bar/PSI
bar/PSI
Engine Instruments. Check engine parameters
 
Ignition ground test. (See Operator’s Manual for ROTAX
®
912 iS)
 
Oil temperature. 90…110°C /190…230°C °C/ °F
°C/°F
▲Warning: Ensure that cylinder head temperature (CHT) and oil temperature are within limits.
Cabin heat

Idle RPM. Tachometer should read 1400 RPM RPM
RPM
Engine full power RPM. Tachometer should read 4900 to
5000RPM RPM
RPM
Ignition check. Set RPM to 4000.
Turn “OFF” LANE selector switch A. Record rpm drop. Must
not be more than 180.
Turn “ON” LANE selector switch A.
Turn “OFF” LANE selector switch B. Record rpm drop. Must
not be more than 180.
Turn “ON” LANE selector switch B.
RPM
RPM
RPM
RPM
Directional stability of nose gear

▲Warning: Allow engine to cool down to 149°C (300°F) (CHT) be fore shutdown. Shut down the
engine, set the ignition switch and the master switch to the off position. Remove
ignition key from the aircraft.
Check for fuel and exhaust odors in cabin

Check for fuel stains on floor


Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 00 05-Aug-12 05-20-3
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
Inspection and/or Required Maintenance
Checklist
100hour
Annual
Other Times
Minimum
Level of
Certification
Initials /
Remarks
Check fuel valve off function

Notes:
05-20.2.4 Post Run-Up, Pre-inspection and Preparations
Inspection and/or Required Maintenance
Checklist
100hour
Annual
Other Times
Minimum
Level of
Certification
Initials /
Remarks
Airframe, engine, propeller
Perform a walk around to detect damage, fluid
leaks or other abnormalities,
Check visual the installation geometry between
fuselage/ wing/ empennage and engine/ propeller/
cowling
Check leveling of aircraft on ground.

Pilot/Owner
Engine cowling
Remove engine cowling.
Refer to Section 71-00.3.1
  Pilot/Owner
Spinner
Remove spinner as defined in the basic aircraft
AMM

Pilot/Owner
Make record of all malfunctions and abnormalities
  Pilot/Owner
05-20.2.5 Propulsion System
Inspection and/or Required Maintenance
Checklist
100hour
Annual
Other Times
Minimum
Level of
Certification
Initials /
Remarks
Cleaning. Clean the engine as required in the
Maintenance Manual for ROTAX
®
Engine Type
912 Series.
  Pilot/Owner
Engine. Conduct 100 hrs inspection as per
Maintenance Manual for
ROTAX
®
Engine Type 912 iS Series.
  A&P

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 00 05-Aug-12 05-20-4
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
Inspection and/or Required Maintenance
Checklist
100hour
Annual
Other Times
Minimum
Level of
Certification
Initials /
Remarks
Engine. Conduct 200 hrs inspection as per
Maintenance Manual for
ROTAX
®
Engine Type 912 iS Series. 200
hrs A&P
Engine. Conduct 600 hrs inspection as per
Maintenance Manual for
ROTAX
®
Engine Type 912 iS Series. 600
hrs A&P
Engine cowling. Inspect for cracks, chafing, heat
damage, delamination, exhaust or fluid leaks,
condition of fastening system, and condition of
paint.
  Pilot/Owner
Engine control panel. Check for full range of
travel, stop adjustment and required friction.
Remove cover and check levers for damage, cracks,
corrosion. Check cablesfor wear and security.
Refer to Section 76-00.3.1.3

RLSA-M
Cooling air ducts, engine baffling and cylinder
cooling fins. Check for obstructions, cracks, wear
and general condition. Check for signs of abnormal
temperatures.
Refer to CHAPTER 75

Pilot/Owner
Oil and coolant radiator. Check for obstructions,
leaks and security of attachment. If necessary
clean cooling ribs.
Refer to Section 75-00.3.1

Pilot/Owner
Coolant hoses and lines. Check for damage,
leakage, hardening from heat, porosity, for loose
connections and secure attachments. Check
routing for kinks and restricted elbows. Check fire
protection shielding.
Refer to CHAPTER 75

RLSA-M
Oil Lines. Inspect for damage, leakage, hardening
from heat, porosity, security of connections and
attachments. Verify routing for kinks or restricted
elbows. Check fire protection shielding.
Refer to CHAPTER 79

RLSA-M
Oil tank vent line. Check for proper routing, for
obstructions and clear passage
Refer to CHAPTER 79

Pilot/Owner
Fuel lines. Check for damage, leakage, hardening
from heat, porosity, secure connections and
attachments. Verify routing for kinks or restricted
elbows. Steel fuel lines if applicable additionally
check for cracks and for scuffing marks. Check fire
protection shielding on the all fuel lines in engine
and pilot compartment.

RLSA-M

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 00 05-Aug-12 05-20-5
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
Inspection and/or Required Maintenance
Checklist
100hour
Annual
Other Times
Minimum
Level of
Certification
Initials /
Remarks
Refer to Section 28-00.3
Gascolator. Open the gascolator, remove the filter
and check for cleanliness. Clean filter and re-
install. Check gascolator drain valve for correct
function and leakage.
Refer to Section 28-00.3
  Pilot/Owner
Fuel shut off valve. Checkfor securityof attachment
and signs of fuel leaks. Check that valve engages
noticeable into the position ON/OFF.
Refer to Section 28-00.3

RLSA-M
Fuel Flow Rate. Check the value of fuel flow rate
as defined in the basic aircraft AMM.
Fuel flow rate: L 40 /____ / (l/h)
R 40 /____/ (l/h).
  RLSA-M
Fuel contamination test. Take fuel samples from
both wings. Inspect for contamination, as defined
in the basic aircraft AMM.
  Pilot/Owner
Induction system. Check connection of manifolds
between NACA-Inlet, Air filter box and carburetors
for damage, security of attachments and condition.
Inspect connected air hoses for condition and
leakage.
Refer to Section 71-00.3.3
  Pilot/Owner
Air filter box. Check that the sealing surfaces are
in good condition and clean. Inspect and clean
filter. Replace if necessary. Clean air filter box
inside. Check the drain hole at the bottom of the
box for obstructions or blockage.
Refer to Section 71-00.3.3
  Pilot/Owner
Cabin heater. Check heat shroud and heater
attachments. Check the manifold for holes and
attachments. Check the heater activation system
for proper operation. Check activation system for
wear and security of attachments, as defined in the
basic aircraft AMM
 Pilot/Owner
Exhaust system. Checks attachment screws and
springs for security and fit. Inspect system for
damage and missing parts. Visual inspection of
muffler, exhaust pipes and mounting flanges for
cracks, corrosion and leakage.
Refer to CHAPTER 78
  RLSA-M
Exhaust muffler. Remove heat shroud from
muffler and inspect muffler for condition, corrosion
and leakage
200h RLSA-M

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS AF 0480 0011 00 05-Aug-12 05-20-6
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
Inspection and/or Required Maintenance
Checklist
100hour
Annual
Other Times
Minimum
Level of
Certification
Initials /
Remarks
Refer to CHAPTER 78
▲Warning: Failure to inspect Muffler for leaks could result in Carbon monoxide entering the
cabin, leading to serious injury or death!
Firewall. Inspect for cracks, delamination,
buckling, and other signs of damage. Inspect all
items attached to firewall for security.
Inspect fire protection coat for condition, signs of
overheating and full coverage of firewall.
  Pilot/Owner
Engine mount. Lift up the nose landing gear off of
the ground and inspect for deformation, cracks,
corrosion, damage from heat, loose hardware,
chafing by cables, wires, hoses, etc., and make
sure that any flexible item is secured to the engine
mount. Check mounting bolts for condition and
visual signs for loss of torque. If necessary check
correct torque value (see 200h).
Refer to Section 71-00.3.2
  RLSA-M
Engine mount. Check mounting bolts for condition
and correct values.
At engine (4 bolts M10): 35 Nm
At shock mounts (4 bolts M10): 35 Nm
At firewall (6 bolts M8): 22.5 Nm
Replace safety wire where necessary
Refer to Section 71-00.3.2
200h RLSA-M
Engine shock mounts. Inspect for porosity, cuts,
damage and deformations
Refer to Section 71-00.3.2
  RLSA-M
Battery attachment. Inspect for security of
mounting and condition as defined in the basic
aircraft AMM. Ensure that the vent holes are clean.
  Pilot/Owner
Starter. Check security of attachment and
electrical connections, as defined in the basic
aircraft AMM.

RLSA-M
Electrical wiring system. Verify the complete
electrical wiring system for security, damage, wear
and secure fit. Check all cable connections for tight
fit, good contact, corrosion and condition.

RLSA-M
Other engine external accessories. Inspect
screws and nuts of all other external engine parts
and accessories for tight fit.

Pilot/Owner
Foreign objects. Check the engine compartment
for foreign objects.
  Pilot/Owner