The Latest_Draft ANO on Entertainment Aviation

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Issue 0 Page 1 of21 September 9, 2013

CIVIL AVIATION AUTHORITY OF BANGLADESH

AIR NAVIGATION ORDERS

AIRWORTHINESS REQUIREMENTS FOR ENTERTAINMENT AVIATION

(MICROLIGHT AIRCRAFT/ VEHICLE)

Sections Titles

1 General

2 Definitions

3 Applicability

4 Design standards and issue of Certificate of type approval of Microlight

Aircraft/ Vehicle

5 Import Procedure of Microlight Aircraft/Vehicle

6 Waivers

7 Special Certificate of Registration

8 Markings

9 Special Certificate of Airworthiness

10 Change of Ownership

11 Mandatory Manual

12 Documents to be carried

13 Maintenance personnel

14 Instruments and equipments


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15 Limitations of Operations

16 Occurrence Reporting

17 Data Records

18 Violation of Rules

APPENDIX-1 TECHNICAL AND AIRWORTHINESS DATA

APPENDIX-2 APPLICATION FOR ISSUE OF CERTIFICATE OF TYPE APPROVAL

APPENDIX-3 SPECIAL CERTIFICATE OF REGISTRATION OF MICROLIGHT

AIRCRAFT/VEHICLE

APPENDIX-4 SPECIAL CERTIFICATE OF AIRWORTHINESS OF MICROLIGHT

AIRCRAFT/VEHICLE

APPENDIX-5

APPLICATION FOR SPECIAL REGISTRATION OF MICROLIGHT

AIRCRAFT/ VEHICLE

1.GENERALThis order lays down specific provisions about Ultralight Aircraft/ Vehicle (hereinafter called

ULA/ULV) and prescribes rules governing the airworthiness requirements of Ultralight

Aircrafts/Vehicle in Bangladesh.

2.DEFINITIONS:

For the purpose of this Order, the definitions as mentioned under the Rule 2, 183 and 234 of the Civil

Aviation Rules, 1984 shall apply. Where a particular definition is not given under the rules, the under

mentioned group wise definitions shall apply:

a) "Aircraft appliances/components" means a major assembly of a complete Aircraft, engine orpropeller and includes for example wings, flight control surfaces, landing gears, generators, fue

pumps, actuators, avionic components etc.

b) "Aircraft parts" means, a sub-assembly of an Aircraft component and standard items includingfasteners, rivets, nuts, bolts, rigging cable and electrical wire.


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c) Certification compliance book (check list) means the book compiled by the respectivemanufacturer(s) to show means of compliance with the applicable Design Standard of the Aircraft.

d) Certificate of type approval in respect of an Aircraft means, the action taken by theChairman, as an alternative to issuing CAABs own Type Certificate (TC), in accepting a Type

Certificate including the Type Approval Data Sheet (TADS) issued by any other contracting State which

meets the design standard of the CAAB as specified in this Order.

e)"Country of origin" means, the country having airworthiness responsibility for the design approval;usually this is the country in which the aeronautical product is manufactured or assembled.

f)EASA CS means European Aviation Safety Agency Certification Specificationas determined by the aviation safety agency formed by the member states of European Union.

g)FARs means aviation regulations issued by Federal Aviation Administration (FAA) of USA.h)"Type of Aircraft" means, a design and make of Aircraft and refers to group of essentially similar

Aircraft, which although possibly existing in different models, stem from a common basic design(e.g. Boeing 747 Aircraft).

i)Special certificate of registration means a Certificate of Registration issued to an aircraft whichdoes not meet the requirements of an applicable comprehensive and detailed airworthiness code asrequired for standard category aircraft. It is the Certificate of Registration only for MicrolightAircrafts.

j) Special Certificate of Airworthiness means a Certificate of Airworthiness issued to an aircraftwhich does not meet the requirements of an applicable comprehensive and detailed airworthinesscode as required for standard category aircraft.

k)Commercial Operations- shall mean any operation of an aircraft, in return for remuneration orother valuable consideration, which is available to the public or, when not made available to the

public, which is performed under a contract between an operator and a customer, where the latterhas no control over the operator

l)Private Operations-shall mean any operation other than Commercial operation.3.APPLICABILITY:

Group A Ultralight Aircraft , is an Aircraft having no more than two seats, Vso not

exceeding 35 knots (65 KM/h) CAS, and a maximum take-off mass of no more

than:-

- 300 kg for a landplane, single seater; or

- 450 kg for a landplane, two-seater; or

- 330 kg for an amphibian or floatplane, single seater; or

- 495 kg for an amphibian or floatplane, two-seater, provided that a Microlight


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capable of operating as both a floatplane and a landplane falls below both MTOM

limits, as appropriate.

Note: Foot-launched Aircraft are excluded from this definition.

Class 1 Powered Para Glider: An Ultralight Aircraft that sustains paramotor

with flexible wing, parachute type. It meets the following technical

conditions:

- maximum continuous power less than or equal to 45 kW for single

seater and 60 kW for two seaters

- the maximum take-off mass is less than or equal to 300 kg for single

seater and 450 kg for two seaters .

Class 2 Weightshift: is an Aircraft which sustains a rigid wing under which is

usually hung a motorized trolley. An Ultralight is a single-engine

Aircraft which sustains a flexible blade which is usually hung over a

motorized carriage. It meets the following technical conditions:

- the maximum power is less than or equal to 45 kW for a singleseat and 60 kW for a two-seater;

- maximum mass not exceeding 300 kg for single and 450 kg fortwo seaters, these masses may be increased by 5% in the case

where the ULA is equipped with a parachute, or 10% in the case

of an Ultralight float. The parachute and installation meet

technical requirements set by the Chairman of Civil Aviation

Authority of Bangladesh ;

-

the stall speed or the minimum steady flight speed in the landingconfiguration (Vs0) does not exceed 65 km / h in conventional

speed (Vc).

Class 3 Multiaxes : is an Aircraft which sustains a fixed wing. Multiaxes meet

the following technical requirements:

- maximum continuous power less than or equal to 45 kW (60.34 hp)for single seater and 60 kW (80.46 hp) for two seaters

- the maximum take-off is less than or equal 300 kg to 450 kg forsingle seater and two seaters, these masses may be increased by 5%

in the case where the ULA is equipped with a parachute or floats

- the stall speed (Vso) is less or equal to 65 km / h, or wing loading atthe maximum weight is less than 30 kg/m2.

Class 4 Ultralight gyroplane: An Ultralight gyroplane meets the following

technical requirements


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- maximum continuous power less than or equal to 60 kW forsingle seater and 80 kW for two seaters

- the maximum mass not exceeding 300 kg for single seater and450 kg for two seaters

- the rotor load to maximum mass between 4.5 and 12 kg per m2.Class 5 Lightweight balloon: A lightweight balloon meets the following

technical requirements:

- maximum continuous power less than or equal to 60 kW forsingle seater and 80 kW for two seaters

- the volume of the helium envelope is less than or equal to 900m3,

- the volume of the layer of hot air is less than or equal to 2000m3.

Group B Ultralight Vehicle, is a Vehicle that:

(a) Is used or intended to be used for manned operation in theair by a single occupant;

(b) Is used or intended to be used for recreation or sportpurposes only;

(c) If unpowered, weighs less than 155 pounds; or(d) If powered:

I. Weighs less than 254 pounds empty weight, excluding floatsand safety devices which are intended for deployment in a

potentially catastrophic situation;

II. Has a fuel capacity not exceeding 5 U.S. gallons;III. Is not capable of more than 55 knots calibrated airspeed at full

power in level flight; and

IV. Has a power-off stall speed which does not exceed 24 knotscalibrated airspeed.

Other For any other new Microlight Aircraft/ Vehicles Civil Aviation Authority ofBangladesh will decide its Group and Class according to technical documents

associated to it.


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4. DESIGN STANDARDS AND ISSUE OF CERTIFICATE OF TYPE APPROVAL OFMICROLIGHT AIRCRAFT/VEHICLE

4.1Primary design standards - Microlight Aircraft/Vehicle, powerplant and propellers.4.1.1 Unless otherwise specified by the Chairman, the primary airworthiness design

standards in respect of Microlight Aircraft, powerplant and propellers are

followed by FAA (American Society for Testing and Material (ASTM) standardsassociated with Light Sport Aircraft), EASA or National Aviation Authority of

Country of Origin/ Country of manufacturer .

4.1.2 The design standard used as the basis of certification for the importation ofa complete Microlight Aircraft or for assembly of a complete Microligh

Aircraft or complete powerplant or propeller shall be recorded with the

respective airworthiness or engineering documents and notified to the CAAB, and

that standard shall thereafter be used as the basis of approval for all modifications

and repairs to that Microlight Aircraft or powerplant or propeller.

4.1.3 For Aircraft or engine or propellers having more than one basis of certification,the standard adopted by the country of Manufacture shall apply, provided itconforms to the requirements of the section 3 of this Order.

4.1.4 At the time of issue of Special Certificate of Airworthiness by the CAAB,applicable design standard of an Aircraft as mentioned in the section 3 of this

Order shall also be mentioned in the Group & Class block of the Specia

Certificate of Airworthinessof the particular Aircraft.

4.2Primary design standardsaeronautical products4.2.1 Unless otherwise specified, the primary airworthiness design standard for

aeronautical products i.e. Microlight Aircraft materials, part, processes andappliances are:

a) Technical standard order (TSO) issued by FAA of the USA; orb) European Technical Standard Orders (CS- ETSO) issued by EASA; orc) American Society for Testing and Material (ASTM) standards associated with

Light Sport Aircraft , or

d) Other standard that may be acceptable to the Chairman.

4.3Certificate of type approval4.3.1 Either the holder of the original Type Certificate (TC) or the prospective operator

for the Microlight Aircraft type may apply to the Chairman for issue of a

Certificate of Type Approval (CTA) in respect of a type Certificated Aircraft

which meets the design standard mentioned in the section 3 provided Certificate

of Type Approval has not been issued earlier by the Chairman in respect of that

type of Microlight Aircraft or model of the Microlight Aircraft. The Certificate of


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Type Approval shall be issued in respect of the Microlight Aircraft type itself and

not the applicant.

4.3.2 The Chairman may issue a Certificate of Type Approval in respect of a TypeCertificate on acceptance of original Type Certificate issued by the Nationa

Aviation Authority (NAA) of the country of manufacture, provided the TC

conforms with the requirements of the section 3 of this Order. Certificate of Type

Approval shall not be issued on the basis of Certificate of Validation of a TC

issued by a contracting State.4.3.3 The applicant shall submit an application on AWS (ML) - 17, as shown in

Appendix-2 of this order and shall submit the preliminary technical data as

mentioned in the Appendix-1 of this order.

4.3.4 If accepted, the applicant will be asked to submit further all or selected technicaldata in the Appendix-1 to this order for examination by the Airworthiness and

Engineering Licensing Division of the CAAB. The examination will normally

include:

4.3.4.1An assessment of the adequacy of the code of design standards applied andtheir amendment status to ensure that no hazardous characteristics exist in the

design and construction of the Aircraft;

4.3.4.2An assessment of acceptability of any waivers or variations granted by theState of Design;

4.3.4.3An assessment of suitability of any special conditions specified and Certifiedby the State of Design; and

4.3.4.4An assessment of adequacy of type design in regard to specified requirements,operating conditions and airworthiness requirements of the CAAB.

4.3.5 The remaining further technical data/documents may be supplied later on,but invariably be submitted by the operator along with application for issueof Special Certificate of Airworthiness.

4.3.6 The applicant (if not holder of TC) shall also submit to the Chairman anundertaking from the TC holder and must arrange for continued supply of

revisions/ amendments to the chairman of the continuing airworthiness data listed

in the Appendix-1 to this order.

4.3.7 If accepted, the Chairman will issue Certificate of Type Approval through a letterstating the followings;

a) Name of the regulatory authority responsible for issue of Type Certificate(TC) or equivalent and Type Approval Data sheet (TADS) or equivalent

of the Microlight Aircraft.

b) Name of the Type Certificate holder.c) Microlight Aircraft Type & Model.d) TADS Number, TADS Revision Number and Date.


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4.3.8 The Chairman may refuse to issue Certificate of Type Approval if there areresponsible grounds not to do so or may issue a Certificate of Type Approval with

such conditions as are necessary on safety grounds.

5. IMPORT PROCEDURE OF MICROLIGHT AIRCRAFT/ VEHICLE5.1Import Procedure of new Microlight Aircraft/ Vehicle5.1.1 Need to submit an application mentioning that, the applicant wants to import a

Microlight Aircraft, to the Chairman, CAAB (Attention: AELD)

5.1.2 Any person operating a Microlight Aircraft under this part shall, upon request,allow the Chairman of Civil Aviation Authority of Bangladesh, or his designee, to

inspect the Microlight Aircraft to determine the applicability of this part.

5.1.3 Flight Test: Flight Test must be conducted under the observation of CAABAirworthiness and Flight Operation officials after importing the Microlight

Aircraft. Flight test can be accomplished by issuing onetime Special Certificate of

Airworthiness as necessity. If the Microlight Aircraft fails to prove its flight

performance in flight test to designated CAAB officials, CAAB will not issue any

certificate ( special certificate of registration, special certificate of registration)

regarding this particular Microlight Aircraft.

5.1.4 Flight test, Type Certificate inspection and other relevant inspections dependingon necessity can be conducted at a single visit. A single visit does not mean a

single day.

5.1.5 As part of the import procedure, it may require a number of visits or a single visitto inspect the airworthiness by the CAABs airworthiness officials. All costs of

such visits shall be borne by the applicant (who wants to import) as per rule 213

of the CARs 1984.

5.2Import Procedure of ageing Microlight Aircraft/Vehicle.5.2.1 Rest life time/ life cycle should be more than 50% of manufacturers mentioned

life cycle or life time of a Microlight Aircraft.

5.2.2 From para 5.1.1 to 5.1.5 will be same for ageing Microlight/Vehicles.

6. WAIVERS.No person may conduct operations that require a deviation from this part except under a written

waiver issued by the Civil Aviation Authority of Bangladesh.

7. Special Certificate of registration:7.1The owner of the Microlight Aircraft/ Vehicle holds a Special Certificate of Registration.

The Special Certificate of Registration of Microlight Aircraft/ Vehicle is issued by the


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Chairman of civil aviation in consideration of the mere declaration of the owner to have

mandatory documents listed below:

a) Proof of foreign registration cancellation.b) Bill of sale or conditional sales contract.c) Insurance Certificate.d) Import permit.e) A Bangladesh customs clearance Certificate.f) Any other documentation as may be required by the Chairman.

7.2The Chairman of Civil Aviation Authority of Bangladesh notify the Special Certificate ofRegistration identifying marks. Registration marks include the BML followed by two

or three letters. The Chairman of Civil Aviation Authority of Bangladesh may conduct by

persons or bodies authorized for this purpose, audits and surveillance as it deems

necessary to ensure that the identified Microlight Aircraft/ Vehicle complies with the

provisions of this Order.

7.3The Special Certificate of Registration includes a descriptive part which identifies theessential characteristics of the Microlight Aircraft/ Vehicle, including characteristics of

masses, and engine speed, allowing its classification of Microlight Aircraft/ Vehicle, in

accordance section 3 of this Order.

7.4 When change of ownership will take place, a new Special Certificate of Registration willbe reissued.

8. MARKINGS.8.1An Aircraft cannot operate without showing under the wing or on the structure in case of

impossibility:

a) The Registration marksb) The manufacturer model marks.

These marks, unadorned and a minimum height of fifty centimeters must be easily

readable.

9. SPECIAL CERTIFICATE OF AIRWORTHINESS: The Special certificate ofAirworthiness is renewed every two years provided that the owner has declared its ability to

fly Microlights and submitting the following documents or selected documents from the

following as necessity.


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SL Aircraft

Group

Documents

1 A & B Conformation of having Certificate of Type Approval

2 Evidence of following import procedure

3 Flight Test Report

4 Evidence of ownership

5 Special Certificate of Registration

6 Any other documents recommended by Chairman, Civil Aviation

Authority of Bangladesh and Manufacturer

7 A Maintenance manual

8 Operation manual

9 Log books

No operation/flight is permitted without having Special Certificate of Airworthiness.

10.CHANGE OF OWNERSHIP: In the case of sale of an Ultralight, the new owner must havethe following items, provided by the previous owner:

10.1

Special Certificate of Registration10.2 Special Certificate of registration.10.3 All manuals (Maintenance manual, Operational manual etc)10.4 The record of use (maintenance log book etc),10.5 Any other associated documents recommended by CAABNew Special Certificate of Registration and Special certificate of Airworthiness shall be

issued by the Chairman, Civil Aviation Authority of Bangladesh or his designee in view of

the old map and its associated Special Certificate of Registration. The new Special Certificate

of Registration and Special Certificate of Airworthiness must be made no later than 3 (three)

months after the date of sale was annotated by the former owner.

11.MANDATORY MANUAL:11.1 For Group A category Microlight Aircraft:

11.1.1 Operation manual, Maintenance Manual, Maintenance Log Book.11.1.2 Any other documents recommended by the Manufacturer


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11.2 For Group B category Microlight Vehicle: Documents recommended by theManufacturer.

12.DOCUMENTS TO BE CARRIED: A person operating a Microlight Aircraft is notrequired to carry the Flight Manual. But, the manuals/documents which the manufacturer

provides with the Aircraft and recommends to carry in flight, are needed to carry on board.

13.MAINTENANCE PERSONNEL: Without any approval no personnel can performmaintenance of Microlight Aircraft/ Vehicle. Maintenance personnel shall be approved bythe civil aviation Authority of Bangladesh.

First means of getting approval:

I. Licence without type rating (LWTR) in A or, C or, I or, E or, RII. Oral exam on Maintenance manual on the particular aircraft.

OR,

Second means of getting Approval:

Maintenance Experience:Every Applicant should have 6 months maintenance experience

on Microlight Aircraft/ Vehicle before applying to be approved as maintenance

personnel.

Examination System:

a) Every applicant needs to appear at 50 multiple questions of every subject mentionedbellow. Pass marks will be 70%.

b) Oral exam. Pass marks 70%.Subjects need to appear at the examinations:

a) Human performance and Limitationsb) Maintenance Manual

14.INSTRUMENTS AND EQUIPMENTS:14.1 Life Jacket: Microlight Aircraft/Vehicle shall carry Life Jackets or equivalent

floatation device for each person when flying over water.

14.2 Altimeter and speedometer must be serviceable.14.3 If any instrument doesnt function properly, which will not hamper to fly but

compromise safety, must be deferred in maintenance log book. And must be repaired

within 3 days of first occurrence.

15. Limitations of Operations:15.1 Microlight aircrafts can be used for Commercial Operations but not for

Commercial Air Transport.

15.2 Microlight aircrafts can be used for private operations.


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16.OCCURRENCE REPORTING:Any incident or accidents reporting to CAAB ismandatory.

17.DATA RECORDS:17.1 Owner will maintain all relevant documents of maintenance and operations in

microlight aircrafts / vehicles operating life. Example- maintenance log book, operation

log book, incident/accident records.

17.2 All records will be preserved at least 2 years from the date of issues of records.17.3 All records will be transferred to new owner in case of change of ownership.

18.VIOLATION OF RULES: Any violation of rules and regulations associated withmicrolights demands fine according to CAR84.


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APPENDIX-1

TECHNICAL AND AIRWORTHINESS DATA

Preliminary Technical Data (Para 4.3.3 of the Order)

a) Type Certificate and Type Approval Data Sheet or equivalents documents.b) Certification Compliance Book or Certification Basis Book

Further Technical Data (Para 4.3.4 of the Order)

a) Log booksb) Operational Manualc) Maintenance Manual

Supply Of Continuing Airworthiness Data (Para 4.3.7 of the Order)

a) Amendments to the documents/manuals listed above and otherdocuments/manuals necessary for airworthiness support of the Aircraft.

b) Airworthiness Directives.c) Service Bulletins (SBs)


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Airworthiness & Engineering Licensing Division

APPLICATION FOR ISSUE OF CERTIFICATE OF TYPE APPROVAL.

1. Name of the Organization :

2. Name of the Applicant :

3. Address :

4. Contact person of the

Organization

:

5. Telephone :

6. Fax :

7. E-mail :

8. Product Identification:

Type Certificate Supplemental TypeCertificate

Others

9. Information on payment of fees:

The fee has been deposited in the account STD-16, Sonali Bank, Kurmitola, Dhaka-1229 as

mentioned below:

Depositslip No._____________________________ Date____________________________

Amount Tk._________________ (in words)_______________________________________

10. Microlight Aircraft / Vehicle

Max. mass: Max. Volume: Max Power:

APPENDIX-2Form: AWS (ML)-17

Issue: 0


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Powerplant:

Reciprocating Engine Battery powered Other

Propeller:

11. Type and Model of the

Microlight Aircraft

Group:

Class: Other:

Remarks:

12. TC No. or Equivalent: TADS No. Equivalent:

Remarks:

13. Restriction (if Applicable)

14. List of documents enclosed

Type Certificate or, Equivalent Type Certificate Data Sheet or, Equivalent Certification Compliance Book or Certification of Basis Books Others(to be specified):

15. Applicants declaration

I do hereby state that the information contained herein is correct and complete. Moreover, I

agree to pay the fees levied by the Chairman in respect of the issuance of a Type

Certificate or approval of a derivative and am aware of the consequences of non-

payment.

16. Signature

Date: Name: Signature:

This Application should be sent by regular mail to:CHAIRMAN,

CAAB HEADQUARTERS, KURMITOLA,DHAKA-1229,

ATTENTION:AELD

Note- Application for Type Certificate or equivalent will be charged as mentioned in the ANO (AW) A.10.


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CIVIL AVIATION AUTHORITY, BANGLADESH

SPECIAL CERTIFICATE OF REGISTRATION OFMICROLIGHT AIRCRAFT/VEHICLE

1. Registration Marks 2. Manufacturer and

Manufacturers Designation of

Microlight Aircraft/Vehicle

3. Microlight Aircraft/Vehicle Serial

Number

4. Group and Class of Microlight Aircraft/ Vehicle:

5. Characteristics of Microlight Aircraft/ Vehicle

Max. takeoff of Mass: Engine power: Engine speed:

6. Name of Owner:

7. Address of owner:

8. Name and address of Operator:

It is hereby certified that the above described Microlight Aircraft/Vehicle has been duly entered on the

Microlight register of Bangladesh.

Date of Issue For Chairman, Civil Aviation Authority

Form: CA(ML)-27A

Issue: 0

APPENDIX-3


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IMPORTANT

If there is any change in the ownership of the Microlight Aircraft/ Vehicle or the Microlight Aircraft/ Vehicle is

destroyed or permanently withdrawn from use, the registration and this Certificate become void, and the

appropriate section hereunder shall be completed and this document returned immediately to the Chairman,

Civil aviation authority, Dhaka.

On change of ownership the Microlight Aircraft/Vehicle may not be flown again until such time as a new

Special Certificate of Registration has been obtained.

An application for re-registration of the Aircraft in Bangladeh shall be made on Form C.A(ML)-27C which may

be obtained from the Chairman, Civil Aviation Authority, Dhaka.

SECTION-I: NOTICE OF CHANGE OF OWNERSHIP.

I hereby notify that, with effect from the .. day of 20 the

ownership of the Microlight Aircraft/ Vehicle described overleaf was transferred to .

.

(Fill in name and address of new owner)

Date [Signature of former owner(s)]**

SECTION-II: NOTICE THAT AIRCRAFT HAS BEEN DESTROYED OR PERMANENTLY WITHDRAWN

FROM USE.

I hereby notify that the registration of Microlight Aircraft/ Vehicle described overleaf should be cancelled byreason of:

The Aircraft having been destroyed. The Aircraft having been withdrawn from use.

Date [Signature of owner(s)]**

** The signature required is that of the owner(s) as shown in this Special Certificate of Registration. If the

owner is a body corporate the signature shall be that of the Managinf Director, Secretary, or other official duly

authorised to sign under the seal of the company.


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CIVIL AVIATION AUTHORITY, BANGLADESH

AIRWORTHINESS & ENGINEERING LICENSING DIVISION

SPECIAL CERTIFICATE OF AIRWORTHINESSOF

MICROLIGHT AIRCRAFT/VEHICLE

1. Registration Marks 2. Manufacturer and

Manufacturers Designation of

Microlight Aircraft/Vehicle

3. Microlight Aircraft/Vehicle Serial

Number

4. Group and Class of Microlight Aircraft/ Vehicle:

5. Characteristics of Microlight Aircraft/ Vehicle

Max. takeoff of Mass: Engine power: Engine speed:

This Special Certificate of Airworthiness is issued in respect of the above-mentioned Aircraft, which i

considered to be airworthy when maintained and operated in accordance with the foregoing and the pertinen

operating limitations.

Date For Chairman, Civil Aviation Authority

This Card is valid for the period(s) shown below Signature, Stamp and Date

From to

From to

Form: CA(ML)-23A

Issue: 0

APPENDIX-4


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This Card is valid for the period(s) shown below Signature, Stamp and Date

From to

From to

From to

From to

From to

From to

No entries or endorsement may be made on this Certificate except in the manner and by the persons authorize

for that purpose by the Chairman, Civil Aviation Authority.

If this Certificate is lost, the Chairman, Civil Aviation Authority of Bangladesh should be informed at once, the

Certificate Number being quoted.

Any person finding this Card is requested to forward it immediately to the following address:

Airworthiness & Engineering Licensing Division

Civil Aviation Authority,

CAAB HQRS

Kurmitola

Dhaka-1229

Bangladesh.


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AIRWORTHINESS & ENGINEERING LICENSING DIVISION

APPLICATION FOR SPECIAL REGISTRATION OF

MICROLIGHT AIRCRAFT/ VEHICLE

The applicant is advised to refer thoroughly the ANO (Airworthiness)- Airworthiness requirements for

entertainment aviation (Microlight Aircraft/ Vehicle) before completing this form. When completed

shall be deposited in person to the CAAB (Airworthiness & Engineering Licensing Division) and mus

be accompanied with all the relevant documents mentioned in the application in form and ANO -

Airworthiness requirements for entertainment aviation (Microlight Aircraft/ Vehicle)

Sl Subject Remarks

1. Aircraft

Group: Class: Passenger capacity including crew: Purpose of Use: Passenger

2. Overall Dimension of the Aircraft/ Vehicle

Height: Length: Wing Span: Volume: Other:

3. Powerplant

Reciprocating Engine Engine power: Battery powered Other :

4. a) Propeller(s)b) Total number of propeller

5. Maximum certified take-off mass (kg.) :

6. Manufacturer

a) Name:b) Mailing address:

APPENDIX-5

Form: CA (ML) 27C

Issue-0


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7. a) Aircraft serial number :b) Date of manufacture:

8. a) Has the Microlight Aircraft been previously identified inBangladesh?

Yes Nob) If so, state Registration mark :

9. a) Name of the owner(s):b) Nationality:c) Address:

10. Classification of operations ( Rule 105 of the CAR 1984)

Aerial work operation General Aviation Operation

11. Proposed main base of operation in Bangladesh

Understanding fully the rules and regulations including the relevant Air

Navigation Orders regarding the Registration of Microlight Aircraft/

Vehicle in Bangladesh, I, being the owner/qualified person as per the 7

of ANO Airworthiness and operation requirements for entertainment

aviation (Microlight Aircraft/ Vehicle), hereby declare that the above

particulars are true in every respect and enclosing the Bank Deposit slip

No dated.Amount .. as the

registration fee payable in accordance with Rule 56 of the CAR 1984.

Date of Application: (Signature of qualified person)

Name:

Designation:

FOR USE IN THE CIVIL AVIATION AUTHORITY

Fee received Yes NoDate:

Registration marks allocated BML-

Date:

Signature of the AW officer

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