Appendix 2 a list of radio communication and navigation equipment a Parts Catalogue relating to the aircraft and major equipment.
(п) a complete set of information on modifications and on special inspections (e.g. Service Bulletins) The LBA may request additional Information and data.
For language requirements see 6.1.
Note: (1) The above listed documents will be kept on file with the LBA.
The applicant must forward to the LBA all revisions (pertinent to the German type certificate) to the above listed documents, Service Bulletins and other pertinent data as soon as these are available.
The LBA reserves the right to request the documents contained in the lists under (e) and (1).
(4) Microfilm/-fiche documentation fs acceptable.
4.4.2 Radio Equipment.
4.4.2.1 For the issuance of an LBA type certificate for radio equipment, the following or equivalent documentation must be submitted: One copy each of the manufacturer's Statement of Conformance submitted to FAR.
2 TSO Authorization or other evidence of FAA approval 3 the TSO Compliance Test Report.
D) lechnical Manuals (e.g., instruction manual, Maintenance/Overhaul Manual, Installation Manual) shall contain informatior relative to the physical, mechanical, and electrical characteristics of the radio equipment concerned. The manuals shall provide all useful and necessary installation, operation, maintenance, and parts information on the major units of the system such as receivertransmitter, indicator, antenna, contro, unit. The manuals shall be the latest issue.
(c) Operational Information. If the appropriate technical manuals do not provide operational information presented from the pilot's point of view, the manufacturer has to prepare a handbook (e.g., Pilot's Guide, Pilot's Manual) has to furnish operational information and details on the control functions.
(d) One specimen of illustration each of the name plated used to mark the major units of the system.
The LBA may request additional information and data.
AC 21-2F Appendix 2 8/7/87 Note: (1) The above listed documents will be kept on file with the LBA.
(2) The applicant must forward to the LBA all revisions (pertinent to the German type certificate) to the above listed documents, Service Bulletins and other pertinent data as soon as these are available.
4.4.2.2 Radio equipment must pass a spurious emission test performed by the Fernmeldetechnisches Zentralamt (FTZ) of the Deutsche Bundespost (German Post Authority); the corresponding FTZ letter must be submitted to the above test to: The manufacturers or his authorized agent have to forward the application for Deutsche Bundespost Fernmeldetechnisches Zentralamt Postfach 800 6100 Darmstadt Federal Republic of Germany Note: The spurious emission test must have been performed before the application for certification of the equipment is submitted to the LBA.
4.4.3 Products Other Than Aircraft and Radio Equipment.
For engines, propellers: Documents corresponding to those under 4.4.1 as applicable.
For personal emergency and auxiliary parachutes: At least the documents as per para. 4.4.2.1 (a).
4.5 Changes to Type Certification. Each change of a product under LBA type certificate must be LBA-approved in accordance with the procedure under para. 4.2 for its inclusion in the type design.
nanges in this context are:
b) Changes covered by a supplemental type certificate in accordance with FAR-Part 21, Subpart E. 'Major changes according to FAR 21.93(a); and Formal LBA consent must also be sought for any revision or supplement of a Flight Manual (Pilot's Operating Handbook), regardless of such a document being required applicable. in the U.S. or not (s. para. 6.2), and including its German version as
5. HOW TO OBTAIN LBA EQUIPMENT APPROVAL.
(For radio equipment s. paras. 3.1 and 4.4.2)
5.1 Applicant. The applicant for LBA approval of U.S. Class II and Class III equipment as referred to under paras. 3.3 and 3.5 must be the manufacturer.
Appendix 2
6.5 Installation of Shoulder Harnesses.
(a) In a more stringent interpretation of FAR 23.785(g) up to Andt. 19, the front seats of normal and utility airplanes must be equipped with either a shoulder harness or a belt and diagonal shoulder strap. The installation must meet the applicable FAR requirements.
(b) Seats of acrobatic category airplanes must be equipped with a shoulder harness approved for acrobatic flight for each occupant. The installation must meet the appropriate FAR requirements.
7. DOCUMENTS FOR CERTIFICATION OF THE INDIVIDUAL AERONAUTICAL PRODUCT.
7.1 Aircraft. The individual aircraft covered by an LBA type certificate and exported to the FRG should be accompanied by the following documentation:
(a) A current United States Export Certificate of Airworthiness, stating the aircraft's conformance with the LBA Geratekennblatt (T.C. Data Sheet).
(b) A copy of all relevant operating instructions stated in the LBA Geratekennblatt (T.C. Data Sheet) (1 e. Flight Manual, Weight and Balance Manual, Equipment List and placards).
(c) For used aircraft, a current aircraft file containing at least the following information: operational time of the aircraft, its engines, propellers, major equipment and components (e.g. engine logbooks, and records), maintenance repairs and modifications.
(d) A statement of compliance as to the noise requirements of para. 6.3, if noise certification was not part of the type certification of the aircraft.
of aircraft.
se neces for the purpe of me de prior registration.
(11) The Maintenance Manual must be made available on request.
(111) Further documents will be requested for the registration of an aircraft. Information on aircraft registration is available on request from the LBA.
Appendix 2
7.2 Aircraft Engines and Propellers. Engines, and propellers covered by the LBA type certificate and exported to the FRG should be accompanied by the documents as per para. 7.1 as applicable.
Parachutes. Parachutes exported to the FRG must be identified by an Airworthiness Approval Tag (FAA Form 8130-3). In addition, emergency and auxfliary parachutes covered by an LBA type certificate (s. para. 3) should be accompanied by all relevant operating instructions stated in the LBA- Geratekennblatt (T.C. Data Sheet).
Equipment and Standard Parts. For LBA approved equipment, including radio equipment and auxiliary power units, exported to the FRG see para. 3.7. As to documentation which must be furnished with radio equipment see para. 4.4.2.
For standard parts exported to the FRG see para. 3.4.
Appendix 2
5.2 Procedure.
5.2.1 The application for LBA equipment approval shall be made by letter (for address s. para. 4.2) with copy to the appropriate FAA aircraft certification office, stating the specification the equipment complies with.
Relevant documentation as per para. 5.3 must be included.
5.2.2 The LBA will acknowledge receipt of the application and inform the applicant of any additional requirements found necessary to assure an visit to the manufacturer's facilities, if such a visit is desirable. place of e visit to the manufacturer
5.3 Documents required for LBA equipment approval. The following documentation must be submitted:
(a) One copy each of 1 the manufacturer's Statement of Conformance submitted to FAA.
the design approval letter or the Letter of Acceptance issued by FAA.
3 FAA Supplemental Type Certificate (STC).
FAA approved drawing list.
The Equipment Qualification or TSO Compliance Test Report.
(b) Drawings and such descriptive information as will define the equipment sufficiently for LBA to decide, whether additional requirements according to para. 5.4 have to be prescribed.
(c) A list of operating, maintenance, overhaul and repair manuals and documentation necessary for safe operation and continuing airworthiness of the equipment.
(d) A copy of the Installation Manual, where appropriate.
(e) A complete set of information on modifications and on special inspections (e.g. Service Bulletins).
Note: A revision service shall be provided.
5.4 Notification of Additional Requirements. Additional requirements which the LBA may prescribe will be those found necessary to:
(a) Provide a level of safety equivalent to that provided for by LBA requirements and practices and as are necessary to comply with the German operating regulations.
(b) Cover features which are not covered by existing requirements and practices.
(c) Provide such failure analyses as are needed to ensure that the equipment is airworthy, when installed in accordance with the equipment manufacturer's instructions.
Appendix 2 a product requiring substantially complete investigation for showing compliance Changes of Products Under LBA Equipment Approval. Each design change of with any requirement forming part of the specification found acceptable to the LBA with written evidence of FAA approval. and hence can be classified a "major change" must be notified to the LBA together
6. ADDITIONAL REQUIREMENTS FOR TYPE CERTIFICATION OF AIRCRAFT.
6.1 Language. Except where an exemption is granted as indicated below, all operating instructions (including markings and placards) must be provided in the German language.
Exemptions:
- Operating instructions except placards for passengers for all multiengine Maintenance instructions may be in English except for sailplanes, powered airplances and for rotorcraft of more than 2,000 kg (4,400 1bs) maximum weight.
sailplanes, manned balloons and parachutes.
Note: The LBA Gerate-Kennblatt (T.C. Data Sheet) will specify which of the documents accompanying the individual imported aircraft must be in German, if any .
6.2 Flight Manual or Pilot's Operating Handbook. Contrary to the U.S.
practice a Flight Manual is required for each kind of aircraft regardless of weight. The Flight Manual (Pilot's Operating Handbook) in the German language
(s. para. 6.1) should correspond to GAMA scheme or equivalent and needs LBA approval. As to revisions to the German Flight Manual (Flughandbuch) refer to para. 4.5.
6.3 Noise Limits. According to the "Luftverkehrsgesetz" (German Aviation Act), an aircraft will be eligible for a Certificate of Airworthiness ("Lufttuchtigkeitszeugnis") only, if its noise level is as low as technologically practicable, and appropriate to the type of aircraft to which it applies. For conformity, the German noise requirements based on ICAO-Annex 16 must be complied with. For subsonic turbine powered airplanes and propeller driven airplanes over 5,700 kg (12,500 1bs) FAR Part 36 of the Federal Aviation Regulations is an acceptable means of compliance.
6.4 Anticollision lights and color markings. All airplanes, rotorcraft and airships must be equipped with anticollision Tights in accordance with the applicable FAR s. As to sailplanes and powered sailplanes, conspicuous color painting may be used instead of anticollision lights for flights at daylight. The latter is also applicable to one and two seated airplanes with a maximum weight of less than 600 kg (1,300 lbs). Detailed information is available on request from the LBA.
AC 21-2F 8/7/87 Appendix 2
ENCLOSURE I
1. SUPERE AIRY ARRMORTHINESS REQUIREMENTS FOR NORMAL, UTILITY AND ACROBATIC Glider Towing. If certification for the purpose of use for glider towing is requested, compliance with the applicable airworthiness requirements must be shown in connection with the type certification of the airplane.
Requirements for glider towing will be available on request from the LBA.
Parachute Jumping. If certification for the purpose of use for parachute Jumping is requested, compliance with the appropriate airworthiness requirements must be shown in connection with the type certification of the airplane. Requirements concerning provision for parachute jumping will be available on request from the LBA.
requiremens of FAR 23.80(6) (5) must be shought, compilance with the
SUPPLEMENTARY AIRWORTHINESS REQUIREMENTS FOR AIRCRAFT INTENDED FOR USE IN COMMERCIAL OPERATION. In connection with additional equipment as it may be required by the German operating regulations in regard of certain operational aspects, supplementary airworthiness requirements could come into effect. The LBA is prepared to inform on an individual basis according to the case under consideration.
Appendix 2
REPUBLIC OF GUATEMALA - SPECIAL REQUIREMENTS (New - August 26, 1981)
1.- Aircraft and Aeronautical products to be eligible for export to the Republic of Guatemala from the United States must be exported in accordance - with the provisions described in part 21 of the United States Federal Aviation Regulations Sub-Part L.
a.- An export Certificate of Airworthiness will be required by the Republic of Guatemala Civil Aviation Authority for all class I products exported from - the U.S. to Guatemala.
b.- The following additional documents will be required.
1.- Log books for aircraft engines and propellers.
2.- Up to date airplane flight manual translated into the Spanish language
3.- Weight and balance report and equipment list not older than six months.
4.- Record of major repairs, alterations to Aircraft engines and propellers IE; FAA337.
5.- Maintenance Manual, structural repair manual, service bulletins incorporating latest up to date revisions for aircraft, engines, propellers and appliances.
6.- A complete list of A.D. notes and mandatory service bulletins applicable to the aircraft, engine, propeller or appliance indicating method of - compliance, date of compliance, signature of licensed individual and - certificate number.
7.- A copy of latest up to date specification for Aircraft, engines and propellers.
C.- Class II and Class III products shall be exported in accordance with the provisions prescribed in part 21 of the U.S. Federal Aviation Regulations.
Appendix 2
REPUBLIC OF HONDURAS - SPECIAL REQUIREMENTS (New - November 6, 1981) The Aeronautical products and Aircrafts Exported to the Republic of Honduras from the United States of America, should de exported in accordance with the 21 parragraf of the US Federal Aviation Regulations Sub-part L.
a) An Airworthiness Certificate for Export is necessary for the Civil Aeronautics Authorities of the Republic of Honduras for aircrafts exported from the Unites States to Honduras.
b) The following additional Documents are requested:
1) Log book for Engines and Propellers Aircraft Maintenance Manual Up to date and if possible translated to Spanish Language Weight and Balance report not older than six months;
2) Record of engines and propeller major repairs and alterations also from the aircraft IE: PAA337.
Maintenance and estructural reparation Manual Services Bulletin including the last revisions for the aircraft, engines, propeller and spare parts.
A complete list of notes A.D. and mandatory Bulletins Services applicable for the aircraft, engines, propellers and spare parts indicating the Correct Method of compliance asaid bulletins, signature of the individual licence and certificate number.
3) The products Clase II and III should be exported in - accordance with the previsions prescribed on the 21 -- part of the Federal Aviation Regulations.
Appendix 2
HONG KONG - SPECIAL REQUIREMENTS (New March 14, 1977) The territory of Hong Kong has the status of a British Crown Colony under the United Kingdom. When exporting aeronautical products to Hong Kong, the Special Requirements of the United Kingdom (Appendix 2) should be similarly observed.
Appendix 2
REPUBLIC OF INDIA - SPECIAL REQUIREMENTS When an aircraft/engine/component exported to India is the first of a model, the manufacturer must supply to the Director General of Civil Aviation the following documents and subsequent revisions:
Copies of type certification documents and relevant drawings, specification, etc.
b. Two sets of maintenance manuals.
c. Two sets of overhaul/shop manuals.
d. Two sets of engine operations manuals.
e. One set of flight manuals, if applicable.
f. One set of repair manuals.
g. Two sets of Service Bulletins and subsequent new issues in addition to revisions.
h. Recommended maintenance schedules.
2. The exporter must show evidence that the products or parts thereof were manufactured under one or more of the following approvals, unless otnerwise approved by the Government of India, Director General of Civil Aviation:
The current valid FAA Production Certificate for the product involved, as outlined in Subpart G of Part 21 of the FAR.
b. An FAA-Approved Production Inspection System (FAA-APIS) letter of approval, as stated in Subpart F of Part 21 of the FAR.
An FAA Replacement and Modification Parts Manufacturers Approval (FAA-PMA) letter of approval issued by the FAA in accordance with Subpart K of Part 21 of the FAR. in this case, each part (or package of small parts) must be marked with the symbol "FAA-PMA" to indicate approval. In addition, each part (or package of small parts) must be marked with the company's name (or trademark), the art number, and the make and model of the type certificated product on which the part is eligible for installation. The make and model information may be on a tag attached to the part (reference FAR 45.15 and FAA Advisory Circular No. 21.303-1A).
d. A Technical Standard Order (TSO) acknowledgement or authorization letter, issued by the FAA per FAR Part 21, Subpart 0, or those airworthiness parts of the FAR relative to the products involved.
Appendix 2 Reconditioned, used, or surplus parts must be accompanied by a certification statement signed by an FAA certified repair station holding a currently valid approval certificate, or by a certified aircraft and powerplant mechanic, as provided for under FAR Parts 145 and 65, respectively. The return to service maintenance records required by FAR 43, Appendix B, shall accompany the parts.
4. In all instances, suppliers must certify on the face of their invoice that the product involved was manufactured under one or more of the following procedures;
1.e., FAA PC No. ; FAA-APIS letter dated _; FAA-PMA letter dated TSO No. ; SAE No. ; MIL Spec. ; other Government or Industrial Specifications 68