Identification of parts authorized for installation in ...

LUF-A-00-20-5004-00A-001A-A

UNCLASSIFIED

UNCLASSIFIEDTO-00-20-5004

Issue No. 0042014-11-10

TECHNICAL MANUAL

IDENTIFICATION OF PARTSAUTHORIZED FOR INSTALLATION

IN NORWEGIAN MILITARY AIRCRAFT

This publication supplements each illustrated parts breakdown to each type of aircraft in the Norwegian Defence inventory.

This publication supersedes TO-00-20-5004, Issue 003 dated 2014-04-30.

Distribution statement: Approved for public release; distribution is unlimited.

ISSUED BY THE AUTHORITY OF THE

NORWEGIAN DEFENCE LOGISTICS ORGANISATIONAIR SYSTEMS DIVISION

KJELLER

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DISTRIBUTION STATEMENT: Approved for public release; distribution is unlimited.

UNCLASSIFIED TO-00-20-5004

LUF-A-00-20-5004-00A-002A-AIdentification of parts authorized for installation in RNoAF aircraft - List of effective data modulesIssue date2014-11-10Languageen/noSecurityClassificationUNCLASSIFIEDCommercialCaveatDistributionApproved for public release; distribution is unlimited.DestructionComply with distribution statement and destroy by any method that will prevent disclosure of the contents or reconstruction of the document.N0016N0016 AIR-A-00-00-00-00A-022A-D

List of effective data modules

The listed documents are included in issue 004, dated 2014-11-10, of TO-00-20-5004.C = Changed data moduleN = New data module

Document title Data module code Issue date Applic

Identification of parts authorized for installation in Norwegian military aircraft

Title page LUF-A-00-20-5004-00A-001-A-A C 2014-11-10 All


List of effective data modules

LUF-A-00-20-5004-00A-002-A-A C 2014-11-10 All


Highlights LUF-A-00-20-5004-00A-003-A-A C 2014-11-10 All


Introduction LUF-A-00-20-5004-01A-018A-A C 2014-11-10 All


Common parts LUF-A-00-20-5004-02A-040A-A C 2014-11-10 All


Type specific parts LUF-A-00-20-5004-03A-040A-A C 2014-11-10 All


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LUF-A-00-20-5004-00A-003A-A

Highlights - To issue 004Issue date2014-11-10Languageen/NorwaySecurityClassificationUNCLASSIFIEDCommercialCaveatDistributionApproved for public release; distribution is unlimited.DestructionComply with distribution statement and destroy by any method that will prevent disclosure of the contents or reconstruction of the document.N0016N0016AIR-A-00-00-00-00A-022A-D

The listed changes are introduced in issue 004, dated 2014-11-10, of TO-00-20-5004.

Table 1 Summary of changes

Data module Reason for change

LUF-A-00-20-5004-02A-040A-A Added suppliers specifically authorized by the TAA in Table 5.

LUF-A-00-20-5004-03A-040A-A Added new requirements for maintenance providers and engine and propeller parts. Added summary tables. Introduced require-ments for approved maintenance providers. Added component category in Table 2.

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Identification of parts approved for installation in Norwegian military aircraft - Introduction

LUF-A-00-20-5004-01A-018A-AIdentification of parts approved for installation in Norwegian military aircraft - Introduction

Issue date2014-11-10SecurityClassificationUNCLASSIFIEDCommercialCaveatDistributionApproved for public release; distribution is unlimited.DestructionComply with distribution statement and destroy by any method that will prevent disclosure of the contents or reconstruction of the document.N0016N0016AIR-A-00-00-00-00A-022A-D

Table of contents Page

1 General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-12 Order of precedence . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-13 Material classification . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-23.1 Common parts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-23.2 Type specific parts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-24 Definitions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-24.1 Technical Airworthiness Authority. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-24.2 Design Activity (ref ASME Y14.100). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-24.3 Part references. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-34.4 Supplier . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-34.5 Interchangeability and substitution (ref ASME Y14.100) . . . . . . . . . . . . . . . . . . . 1-35 Related publications. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-4

List of tablesTable 1 References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1Table 2 Related publications, general . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-4Table 3 Related publications, type specific . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-5

References

Description

1 General

This regulation covers Norwegian military registered aircraft specified by their approved technical documentation. Civilian registered aircraft that are temporarily used for military operation are not covered by this regulation (ref §17 Luftfartsloven). This technical order outlines the requirements for parts used on aircraft and is arranged in one general data module and one weapon system/type specific data module.

2 Order of precedence

In the event of conflict between the text of this publication and the references cited herein, the text of this publication takes precedence. Nothing in this publication however, supersedes appli-cable laws and regulations unless a specific exemption has been obtained.

Table 1 References

Reference Data Module Title

LOV-1993-06-11-101 Lov om Luftfart (Luftfartsloven)

ASME Y14.100 Engineering Drawing Practices

EASA Part M Continuing Airworthiness


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3 Material classification

The following material classifications are applicable to this publication:

3.1 Common parts

The term common parts is used in this publication to identify parts that are not designed for spe-cific aircraft types. Common parts are divided into four material classes: Standard parts, POL (petroleum, oil and lubrication), chemicals and raw materials.

3.1.1 Standard partsStandard parts are parts that are manufactured in complete compliance with an established industry, agency, competent authority or other Government specification which includes design, manufacturing, test and acceptance criteria, and uniform identification requirements. The specifi-cation must include enough information in order to produce the part with full conformity and must be official and available to all manufacturers (see also EASA Part M AMC M.A.501).

3.1.2 POLIn this publication, the abbreviation POL denotes Petroleum, Oil and Lubricants for use in aircraft maintenance.

3.1.3 ChemicalsIn this publication, the term Chemicals including cleaning, anti-ice and de-icing agents, adhe-sives, sealants, coatings, acids and bases for aircraft maintenance.

3.1.4 Raw materialsRaw material includes raw or processed products that normally will be transformed by further processing, reshaping or combined with other materials into a new and usable product (ref ASME Y14.100). Examples are metals (plates, tubes, profiles), plastic materials, rubber, fibre materials (glass and carbon fiber) and composite materials.

3.2 Type specific parts

A part defined by the current Design Activity for specific aircraft

4 Definitions

The following definitions are applicable to this publication:

4.1 Technical Airworthiness Authority

The Technical Airworthiness Authority (TAA) is responsible for the regulation of the technical air-worthiness aspects of the design, manufacture, maintenance and materiel support of aeronauti-cal products and the determination of the airworthiness acceptability of those products prior to operational service.

For Norwegian military aircraft the TAA has been delegated the Commander of the Norwegian Defence Logistics Organistation/Air Systems Division.

4.2 Design Activity (ref ASME Y14.100)

The Design Activity is an organization that has, or has had, responsibility for the design of an item.

Note

Due to extensive modification on some Norwegian military aircraft, this activity has been divided between several organisations or manufacturers including the TAA.

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Note

The term Original Equipment Manufacturer (OEM) will not be used in this TO because it has been referred to both original and current Design Activity whether they are a manufacturer of the part or not.

4.2.1 Current Design ActivityThe Design Activity currently responsible for the design of an item. This may be the original Design Activity or a Design Activity to which the design responsibility has been transferred.

4.2.2 Original Design ActivityThe Design Activity originally responsible for the design and identification of an item whose draw-ing number and activity identification is shown in the title block of the drawings and associated documents.

4.2.3 Design Activity identificationThe application of a unique identifier that distinguishes an activity or organization from another activity or organization. Examples of Activity identification include Activity name, Activity address, or CAGE code.

4.3 Part references

The term Part Reference is a unique identifier of a part consisting of the part number and a source identifier (i.e. CAGE code).

4.3.1 Part numberThe part number (also known as P/N or PIN) is used to identify a part and assigned by the origi-nal Design Activity, or by the controlling nationally recognized standard. See also ASME Y14.100. Note: The part number is not fully item identifying without the manufacturer or govern-ing standard being specified.

4.3.2 Cage codeCommercial and Government Entity (CAGE) code, is a unique identifier of a supplier, manufac-turer, government agency or an organisation (i.e. standardization organisations ref Table 2 in LUF-A-00-20-5004-02A-040A-A). See also ASME Y14.100.

4.4 Supplier

In this Technical Order the term supplier will include vendor, distributor and broker.

4.5 Interchangeability and substitution (ref ASME Y14.100)

4.5.1 Interchangeable itemAn Interchangeable item is one which (1) possesses such functional and physical characteristics as to be equivalent in performance, reliability, and maintainability, to another item of similar or identical purposes; and (2) is capable of being exchanged for the other item (a) without selection for fit or performance, and (b) without alteration of the items themselves or of adjoining items, except for adjustments.

4.5.2 Substitute itemA substitute item is one which possesses such functional and physical characteristics as to be capable of being exchanged for another only under specified conditions or in particular applica-tions and without alteration of the items themselves or of adjoining items.

4.5.3 Form, Fit and Function

1 Form: The shape, size, dimensions, mass, weight, and other physical parameters which uniquely characterize an item. For software, form denotes the language and media.


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2 Fit: The ability of an item to physically interface or interconnect with or become an integral part of another item.

3 Function: The action or actions which an item is designed to perform.

5 Related publications

Related publications are listed in Table 2; Related publications, general and Table 3; Related publications, type specific.

Table 2 Related publications, general

Publication reference Title

BML Bestemmelser for Militær Luftfart

BMF 1000 Bestemmelser for materiellforvaltning i Forsvaret

BMF/Luft 750-1 Bestemmelser for vedlikehold av Forsvarets luftmateriell

BFL 712-1 (A) Forvaltning av drivstoff

TO 00-20-5001 Forebyggende vedlikehold av luftfartøy og bruk av blanketter

TO 1-1A-8 Structural hardware - Aircraft and missile repair

TO 1-1A-14 Aircraft electric and electronic wiring - Volume 1 - Installation and repair prac-tices

TO 42E2-1-2 Hydraulic packings and gaskets - Identification, use and disposition

CLP Regulation Regulation on Classification, Labelling and Packing (CLP) of Substances and Mixtures

DGR IATA Dangerous goods regulations

AS9100 Quality Management Systems - Requirements for Aviation, Space and Defence Organizations

AS9120 Quality Management Systems - Aerospace Requirements for Stockist Distrib-utors

AQAP 2131 NATO Quality Assurance Requirements for Final Inspection

STANAG 1135 Interchangeability of Fuels, Lubricants and Associated Products used by the Armed Forces of the North Atlantic Treaty Nations

STANAG 3149 Minimum Quality Surveillance for Fuels

STANAG 4107 Mutual Acceptance of Government Quality Assurance and Usage of the Allied Quality Assurance Publications (AQAP)

STANAG 4714 Minimum Quality Surveillance for Lubricant and Associated Products

ATA 300 Specification for packaging of airline supplies



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Table 3 Related publications, type specific

Publication reference Title

TO 1F-16AM-4 series USAF/EPAF series F-16A/B MLU aircraft - Illustrated parts breakdown

TO 1H-412-5004 series RNoAF Bell 412 - Illustrated parts breakdown

TO NO1C-130J-4 series RNoAF C-130J aircraft - Illustrated parts breakdown

DWAP 101C-0443-3A RNoAF SAR Sea King Mk43, Mk43A, Mk43B - Illustrated Parts Catalogue

DAP 101C-1386-3 Lynx Mk 86 - Illustrated Parts Catalogue

IETP JA-C0418-N0016 NH90 NFH-NNWN IETP (Refer to the Illustrated Parts Data infoset)

NA 01-75PAN-4 series RNoAF P-3N aircraft - Illustrated Parts Breakdown

NA 01-75PAU-4 series RNoAF P-3C UIP aircraft - Illustrated parts breakdown

NA 01-75PAA-4 series US Navy P-3A and P-3B aircraft - Illustrated parts breakdown

NA 01-75PAC-4 series US Navy P-3C aircraft - Illustrated parts breakdown

TO 1U-FJF-5004 series RNoAF EW/Basic Falcon 20 retrofit aircraft - Illustrated parts breakdown

TO 1T-17-4 RNoAF T-17 Saab Safari - Parts Catalog

TO 1RQ-11B-5004 RAVEN B 1RQ-11B Illustrated Part Catalog

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Identification of parts approved for installation in Norwegian military aircraft - Common parts

LUF-A-00-20-5004-02A-040A-AIdentification of parts approved for installation in Norwegian military aircraft - Common parts



1 General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-21.1 Scope . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-21.2 Arrangement . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-21.3 General requirements for suppliers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-21.4 Approved manufacturers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-21.5 Interchangeability and substitution approval . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-31.6 Approval by other organisations. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-31.7 Certification of Conformity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-41.8 Approved data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-52 Standard parts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-62.1 General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-62.2 Documentation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-62.3 Marking . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-63 Petroleum, Oil and Lubricants . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-63.1 General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-63.2 Documentation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-73.3 Marking . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-74 Chemicals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-74.1 General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-74.2 Documentation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-74.3 Marking . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-75 Raw Materials. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-85.1 General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-85.2 Documentation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-85.3 Marking . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-86 Summary tables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-8

List of tablesTable 1 References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1Table 2 The most used standardization organisations with CAGE (not exhaustive). . . . . 2-8Table 3 Documentation requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-9Table 4 Marking requirements. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-9Table 5 Suppliers specifically authorized by the TAA, see Para 1.3 . . . . . . . . . . . . . . . . . 2-10Table 6 Interchangeability and substitution approval for common parts* . . . . . . . . . . . . . 2-10

References

Table 1 References


LUF-A-00-20-5004-01A-018A-A Identification of parts approved for installation in Norwegian military aircraft - Introduction


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Description

1 General

1.1 Scope

This chapter will outline the requirements for common material to be used on Norwegian military registered aircraft. Requirement summaries can be found in Para 6, Summary tables.

1.2 Arrangement

This chapter is divided in standard parts, POL, chemicals, and raw materials.

1.3 General requirements for suppliers

In order to be an approved supplier for common parts, either of the following requirements shall be fulfilled:

1 The supplier shall be certified to the following Quality Management System:

a AS9120, or

b AS9100

2 or the supplier shall be ISO9001 certified and compliant with the following Quality Manage-ment System:

a AS9120, or

b AS9100

3 or the supplier has been specifically authorized by the TAA. Specifically authorized suppliers are listed in Table 5.

Note

Compliance to AS9100 or AS9120 implies a Quality Assurance system according to AQAP 2131.

Note

Certification to the AS91xx quality management system can be verified in the SAE database OASIS. See www.sae.org/oasis

1.4 Approved manufacturers

When a manufacturer specific Part Reference for a common part (e.g. Aeroshell-XYZ 12345) is listed in the technical documentation, that manufacturer (12345) is automatically approved as a supplier for that part.

A manufacturer not listed in the aircraft technical documentation may be approved by the TAA as a supplier on a case to case basis, providing the following is fulfilled:

1 The material is manufactured in full compliance to the valid revision of its specification at the time of manufacture.

2 Inspection criteria outlined in the specification have been met

3 Qualification requirements have been fulfilled

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4 Is listed in the applicable Qualified Product/Manufacturer/Supplier List/Database (QPL/QPD/QML/QSL) at the time of manufacture (if required by the specification).

1.5 Interchangeability and substitution approval

Interchangeability and substitutions (I&S, see Para 4.5 in LUF-A-00-20-5004-01A-018A-A) are authorized through the technical documentation for each weapon system. Additionally, Inter-changeability between different standard parts may be approved by the TAA, a TAA authorized organisation or a TAA certified person. The TAA will document an approval of an organisation in writing.

1.5.1 Personnel certified to approve interchangeabilityPersonnel within the Norwegian Armed Forces may be certified to approve the use of an inter-changeable part when the following requirements are fulfilled:

1 The person must have the right to sign off a red / (as defined in TO 00-20-5001), or function as a quality inspector for the applicable air system.

2 A course, defined by the TAA, in the use of a searchable database for standards and speci-fications has been completed

The certificate shall list the material classification for which the certification is valid.

1.5.2 Organisations authorized to approve interchangeabilityAn organisation outside of the Norwegian Defence can be authorized by the TAA to approve the use of an interchangeable Part Reference when the following is fulfilled (See Table 6 for capabil-ity list):

1 The organisation is authorized by the TAA for relevant maintenance on the applicable sys-tem, or a TAA authorized supplier (see Table 5) of the applicable class of material.

Note

The Design activity of the part has the privilege to define interchangeability of the applicable part number within the privileges granted by the certification authority. This requires the Design activity to notify the TAA of follow-on maintenance and to update any necessary technical manual.

1.6 Approval by other organisations

Only part references approved by the TAA or the design activity are authorized for use on Norwe-gian military registered aircraft. This means that a part approved by another organisation (for example a Parts Manufacture Approval by FAA, also called PMA part) is only approved when the Part Reference is described in the technical documentation.

1 Example:

a The P/N 6731153-1 is ordered.

b The P/N 6731153P-1 is offered by a supplier.

c The suffix "P" has been added to the P/N by the manufacturer to show that the part has been made under another approval than the original P/N, in this case by FAA (PMA part). This P/N is not approved by the TAA or the Design Activity and shall not be used on Norwegian military registered aircraft.

2 Example:

a P/N 9440791-1 is ordered and received.

b The P/N corresponds with the technical documentation for the applicable system.


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c The label is marked with "PMA".

d This is a part with the correct P/N and is authorized by the design activity for use on the applicable system. It has in addition been authorized by FAA for use on another system and is therefore also a PMA part. This part is authorized for use on Norwegian military registered aircraft.

1.7 Certification of Conformity

Certification of Conformity (CoC) is a document used by suppliers and manufacturers, and is issued to a product that meets a minimum set of regulatory, technical and safety requirement (i.e. through a drawing or specification). A supplier approved in accordance with the general require-ments in Para 1.3 will store the original manufacturers CoC to be available upon request. In case of a request it shall be possible for a supplier to trace back to the original manufacturer batch.

1.7.1 Certification of Conformity issued by a manufacturerA CoC issued by a manufacturer shall include the following:

1 Part number defined by the standard or specification

2 Manufacturers CAGE code and/or full name

3 The delivered quantity of Part References (P/N - CAGE)

4 Signature that certify the part’s conformity to its design and an approval for safe operation

5 Manufacturers Batch or Lot number if available

6 Purchase order number (for tracking purposes)

BL 3307 (NDLO) covers these items.

1.7.2 Certification of Conformity issued by a maintenance contractorA CoC issued by a maintenance contractor shall include the following:




4 Signature that certify the part’s conformity to contract

5 Manufacturers Batch or Lot number if available


7 Reference to applicable documentation for overhaul/maintenance

BL 3307 (NDLO) covers these items.

1.7.3 Certification of Conformity issued by a supplier A CoC issued by a vendor or supplier other than the manufacturer shall include the following:

Note

An exemption to the requirements above is that NDLO does accept DD250, DD1574 and DD1348 (Foreign Military Sales) despite the lack of original manufacturer and part number (NSN is used instead),




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BL 3307 (NDLO) covers these items. BL 3307 can be used to list several Part References when under the same purchase order number.

Examples of using a supplier CoC to find manufacturer:

– The part was delivered via FMS and is marked both on the package and form DD1348 with the contract number SPM5A712M1498. Using a procurement history database provider like Haystack allows tracing the manufacturer from the contract number.

– There is a difference between the P/N on the part and on the package. The CoC from the supplier show the contract number which can be used when contacting the supplier to get a copy from the manufacturer

1.8 Approved data

A common part for use on military aircraft must always have its origin from the accompanying technical documentation.

Intraspex and ASSIST are authorized as searchable databases for standards and specifications. Note that interchangeability between different standards must be approved as specified in Para 1.5.

For military aircraft where the Design Activity is originated within the USA DoD, the TO’s 1-1A-8, 1-1A-14 and 42E2-1-2 can be used for interchangeability and substitutions evaluation.

In order to find information about interchangeability between POL products, the STANAG 1135 can be used within NATO.

1 Example of interchangeability authorized through a standard:

a The aircraft technical documentation call for a clamp with the P/N MS21919DG20.

b When searching in Intraspex for the governing standard MS21919, rev E show that the material is aluminum alloy and gives the size of the clamp. The standard also has a note 4 that cancel and replace CRES and aluminum alloy clamps with the AS21919.

c The P/N MS21919WDG20 is on stock and certified personnel is tasked to check whether this part number can be used instead of the MS21919DG20. MS21919 stan-dard rev E provides an interchangeability table which can be used as a basis for approving such interchangeability.

2 Example of using Intraspex to find latest Part Reference of a standard part:

a The aircraft technical documentation call for a washer with the Part Reference AN960-1016, CAGE 88044 (Aeronautical Standards).

b When searching in Intraspex for the governing standard AN960, a cancel note is found which cancel the AN960 standard and replace it by NAS1149, CAGE 80205 (National Aerospace Standards).

c The NAS1149 standard defines the replacement Part Reference for AN960-1016 to be NAS1149F1063P in an interchangeability table.

d The Part Reference ordered should be the latest Part Reference NAS1149F1063P, CAGE 80205.

3 Example of using Intraspex to find latest Part Reference of a chemical:

a In the Technical order for the F-16 there is a reference to MIL-S-23586 sealant.

b Using Intraspex and looking up the MIL-S-23586 you will see that it has been revised.


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c In the document family Intraspex state that the MIL-PRF-23586 F is the latest revision.

d The MIL-PRF-23586 has a paragraph about qualification and refers to a Qualified Prod-ucts List (QPL-23586) and where to look it up.

e Depending on Type, Class and Grade different manufacturers are on the list and are thereby authorized for use on Norwegian military aircraft.

f The use of any other manufacturer must be authorized explicitly by the TAA.

2 Standard parts

2.1 General

Standard parts are identified by a part number defined by the Design Activity responsible for the specification and the Design Activity CAGE code. If, for a given aircraft type or component, the system technical documentation uses a manufacturer specific part number (and CAGE code), the use of this Part Reference is also approved for this specific aircraft or component.

In order to allow the use of a standard part on all applicable aircraft types, the governing Part Reference must be available for identification purposes.

Procurement of standard parts shall be done through approved suppliers, see Para 1.3.

For interchangeability purposes, standard parts are divided into structural/system parts and avi-onic parts.

2.2 Documentation

Traceability on the CoC (see Para 1.7) to the manufacturer and batch/lot is required as follows:

1 CoC from the original manufacturer showing the batch/lot or purchase number, or

2 CoC from the supplier with a batch/lot or purchase number that ensures a trace further to the manufacturer. In this case it must be ensured through contract and the suppliers quality sys-tem (see Para 1.3) that the supplier have their original manufacturer CoC archive on a safe place for at least 10 years and that the trace to the manufacturer should be readily accessi-ble within 24 hours.

2.3 Marking

The part shall be marked according to the governing standard and must clearly show the Part Reference called out for by the specification.

3 Petroleum, Oil and Lubricants

3.1 General

POL products are used across all Norwegian military aircraft as well as in cross servicing within NATO. It is desirable to minimize the amount of products in this category but crucial that the pro-ducers are approved. POL products are usually governed by an official standard as defined in “Standard Parts”. For lubricants, STANAG 1135 and 4714 are applicable. For quality testing and handling of fuel, see BFL 712-5 (A) and STANAG 3149.

When a change of manufacturer within the same specification and application area is needed, the TAA must be consulted first.

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3.2 Documentation

Traceability on the CoC (see Para 1.7) to the manufacturer and batch/lot is required as follows:


2 Certificate of Analysis (CoA) (can be used in lieu of CoC when CoC requirements (see Para 1) are fulfilled in the CoA).

3 Material Safety Data Sheet (MSDS) as defined by regulation (EC) No 1907 (REACH)

4 Technical data sheet (TDS)

Consolidation of the certificates is allowed.

3.3 Marking

The part shall be marked according to the governing standard and must clearly show the Part Reference called out for by the specification. In addition POL products must be marked accord-ing to the following STANAG references:

1 For fuel products STANAG 3149.

2 For lubricant products STANAG 4714.

If the POL product with a NATO code does not meet the STANAG initially or after a defined time, the NATO code shall be crossed out with a red X.

4 Chemicals

4.1 General

The term Chemicals is a collective term for wide area of materials as defined in the introduction to this publication, ref Para 3 in LUF-A-00-20-5004-01A-018A-A. The differences in short from other general parts are the requirements for Material Safety Data Sheet (MSDS), a Certificate of analysis (CoA) and additional rules for marking.

4.2 Documentation

Traceability on the CoC (see Para 1.7) to the manufacturer and batch/lot is required as following deliverables:


2 Certificate of Analysis (CoA) (can be used in lieu of CoC when CoC requirements are ful-filled in the CoA)

3 Material Safety Data Sheet (MSDS) as defined by regulation (EC) No 1907 (REACH)

4 Technical data sheet (TDS)

Consolidation of the certificates is allowed.

4.3 Marking

Chemicals shall be marked according to the CLP Regulation (Table 3), see Regulation (EC) No. 1272/2008 (or later) made by the European Parliament and Council. Some chemicals do confirm to a NATO STANAG and will have to be marked accordingly.


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5 Raw Materials

5.1 General

Raw materials have an extra requirement compared to other general parts for a Material Inspec-tion Certificate in order to be authorized for use on aircraft.

5.2 Documentation

Traceability to the manufacturer’s batch/lot or purchase number is required. The following is required as a deliverable:

1 Test report type 2.2 in accordance with EN 10204 (to ensure the composition)

2 Material Safety Data Sheet (MSDS) if applicable as defined by regulation (EC) No 1907 (REACH).

3 Technical data sheet (TDS) if applicable

5.3 Marking

Raw materials must be marked in accordance with the prevailing standard.

6 Summary tables

Table 2 The most used standardization organisations with CAGE (not exhaustive)

Organisation name CAGE

National Semiconductor Corporation 27014

Electronic Industries Association 80131

American National Standards Institute (ANSI) 80204

National Aerospace Standards (NAS) 80205

Society Of Automotive Engineers Inc (SAE) 81343

Federal Specifications 81348

Military Specifications 81349

Joint Army-Navy Specifications 81350

Aeronautical Standards Group (AS) 88044

Military Standards 96906

Deutsches Institut Für Normung EV (DIN) D8286

Association Francaise De Normalisation (AFNOR) F0110

Bureau De Normalisation De L'aeronautique Et De L'espace F0111

Union Technique Electricite F0114

Union Technique Electricite F0115

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* If applicable

** Only needed if the CoA does not cover the requirements for a CoC

Airspace And Defense Industry Assiciation Of Europe I9005

Comite Europeen De Normalisation (CE) I9006

International Organization For Standardization (ISO) I9008

International Electrotechnical Commission (IEC) I9009

British Standards Institution (BSI) K7766

Table 3 Documentation requirements

Standard Parts (see Para 2.2)

POL Chemicals Raw material

Certificate of Conformity (CoC) (by) X(Supplier or

manufacturer)

X**(Manufacturer)

X**(Manufacturer)

Certificate of Analysis (CoA) X X

Material Safety Data Sheet (MSDS) X X X*

Test report type 2.2 X

Technical data sheet (TDS) X X X*

Table 4 Marking requirements

Standard Parts POL Chemicals Raw material

According to its Standard X X X X

CLP Regulation X X

STANAG 4714 X

STANAG 3149 X

STANAG 1135 X

Table 2 The most used standardization organisations with CAGE (not exhaustive)

Organisation name CAGE



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* The organisation must be an approved overhaul source for the applicable air system/compo-nent or part

Table 5 Suppliers specifically authorized by the TAA, see Para 1.3

Organisation Due date Standard Parts

POL Chemicals Raw mate-rial

Foreign Military Sales (FMS) 01.01.2016 X

Patria Helicopters 01.01.2016 X

Relli Technologies 01.08.2015 X

Fokker 01.01.2017 X

Lockheed Martin Aeronautics Company

X

AgustaWestland X

Dassault Falcon X

Bell Aerospace X

Rolls Royce X

Pratt & Whitney X

Honeywell X

Turbomeca X

Table 6 Interchangeability and substitution approval for common parts*

Due date Standard structural/

system Parts

Standard avionic parts

POL Chemicals Raw mate-rial

Marshall Aerospace 01.01.2016 X X

Aerospace Indus-trial Maintenance

01.01.2016 X X X

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Identification of parts approved for installation in Norwegian military aircraft - Type specific parts

LUF-A-00-20-5004-03A-040A-AIdentification of parts approved for installation in Norwegian military aircraft - Type specific parts



1 General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-11.1 Arrangement . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-21.2 Approved technical documentation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-21.3 Approved manufacturers in general . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-21.4 Approved maintenance providers in general . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-21.5 Interchangeability and substitution of type specific parts . . . . . . . . . . . . . . . . . . . 3-62 Requirements based on aircraft type . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-62.1 P-3C and P-3N. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-62.2 Engine and propellers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-73 Summary tables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-7

List of tablesTable 1 References. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1Table 2 Component categories . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-5Table 3 Current design activity for Norwegian military aircraft . . . . . . . . . . . . . . . . . . . . . 3-7Table 4 Approved distributors and manufacturers for Norwegian military aircraft spare parts 3-7Table 5 Maintenance Providers that have a current license or approval from the current Design

Activity (non exhaustive) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-8Table 6 Approved distributors for Norwegian military aircraft engines . . . . . . . . . . . . . . . 3-8Table 7 Approved maintenance providers for Norwegian military aircraft engines . . . . . . 3-9Table 8 Approved distributors for Norwegian military aircraft propellers. . . . . . . . . . . . . . 3-9Table 9 Approved maintenance providers for Norwegian military aircraft propellers . . . . 3-9

References

Description

1 General

This data module aim to set the requirement for procurement and use of type specific parts (as defined in LUF-A-00-20-5004-01A-018A-A, Para 3.2). The intention is to ensure flight safety by using parts manufactured by an approved source, and that those parts have adequate documen-tation enclosed to prove it.

Table 1 References


LUF-A-00-20-5004-01A-018A-A Identification of parts approved for installation in Norwegian military aircraft - Introduction

LUF-A-00-20-5004-02A-040A-A Identification of parts approved for installation in Norwegian military aircraft - Common parts


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1.1 Arrangement

This data module is arranged in a general section and one section for each aircraft in the Norwe-gian Armed Forces inventory. The different systems will be implemented over time. Summary tables are referred to and presented in the end.

1.2 Approved technical documentation

For every aircraft type a set of technical documentation is approved by the TAA. This documenta-tion shall be the starting point for determing an authorized part.

The maintenance technician has final responsibility and authority for determining acceptability of aircraft parts.

1.2.1 FLIS dataThe Federal Logistic Information System (FLIS) is acknowledged as a data source with different restrictions depending on the aircraft type. Approved interfaces for looking up FLIS data are Hay-stack (IHS) and FedLog (DLA). It is mainly expected to be used as acceptable source for deter-mining part equivalency for aircraft where the original Design Activity is based in the United States of America (typical F-16, C-130 and P-3). See the applicable system for further require-ments before use.

1.3 Approved manufacturers in general

In general an approved manufacturer of a Norwegian military aircraft type specific part is one of the following regardless of aircraft type:

1 As determined by the current Design Activity for the applicable part, system or aircraft

a The Design Activity

b Manufacturer approved or licensed by the Design Activity

c Manufacturer chosen by a Design Activity approved or licensed supplier

2 A TAA specifically approved manufacturer or supplier of the part

In order to purchase a part directly from a manufacturer the procuring activity must verify that the manufacturer has an agreement with the design activity of the applicable part. Such an agree-ment must cover drawing updates, inspections and technical support of the manufacturer or sup-plier by the design activity.

1.3.1 Documentation requirements for manufacturers or supplier/distributorsGeneral requirements for documentation of a Part Reference are as follows:

1 A type specific part shall always be documented with a Certification of Conformity as defined in LUF-A-00-20-5004-02A-040A-A, Para 1.7 from either of the following entities:

a A Design Activity, its licensee or approved supplier/distributor

b A TAA approved manufacturer or supplier/distributor

c The aircraft manufacturer

d The aircraft manufacturer approved supplier/distributor

2 The documentation shall be readily accessible for the technician in charge of the installation or inspection of the part.

1.4 Approved maintenance providers in general

This section applies to maintenance providers outside of the Norwegian Armed Forces. Several Norwegian Military requirements for External Maintenance are identical to those stated in EASA

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Part 145, and are referred to as "Part 145 level". Part 145 requirements are not repeated herein, and are not revoked or replaced unless explicitly stated in this document.

1.4.1 General requirements for maintenance handling agents Handling agents are organisations that do not perform the maintenance in house. A handling agent in contract with Norwegian Armed Forces has the responsibility for the components agreed on until the part is maintained and returned or discarded. A handling agent must be able to prove the following before contract is agreed on:

1 The handling agent must prove that the requirements in Para 1.4.3 are fulfilled for all the maintenance providers that the handling agent intend to use.

2 The handling agent must notify the purchaser when a new maintenace provider has been choosen for one or more of the components agreed on.

1.4.2 General maintenance organisation requirementsThe Maintenance organisation, performing maintenance of Norwegian Military Aircraft, and com-ponents intended for fitment thereto, shall be approved by the TAA in accordance with the provi-sions of this document.

The TAA will issue an approval valid for external maintenance for one or more components, equivalent to a capability list, listed in Table 2 dependent on aircraft type.

In order to be an approved Maintenance organisation, either of the following requirements shall be fulfilled:

1 The Maintenance organisation shall be certified to the AS9100 or AS9110 Quality Manage-ment System.

2 or the Maintenance organisation shall be ISO9001 certified and compliant to the AS9100 or AS9110 Quality Management System.

Note

Compliance to AS9100 implies a Quality Assurance system according to AQAP 2130 and 2131.

Note

Certification to the AS91xx quality management system can be verified in the SAE database OASIS. See www.sae.org/oasis

1.4.3 Capability requirements for Maintenance providersThe TAA recognizes several standards, procedures and approvals, as an approved basis for external maintenance. One of the following must be fulfilled:

1 Maintenance Providers that are compliant with FAA or EASA Part 145 level.

2 Maintenance Providers that are approved by a National military airworthiness authority.

a The approval shall be issued in the nation where the maintenance organisation certify-ing staff is based.

b The national military airworthiness authority must be recognized by the TAA.

3 Maintenance Providers that have a current license or approval from the current Design Activity (OEM), see Table 5.

4 TAA-specific approved maintenance Providers.


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In addition all of the following requirements have to be fulfilled:

1 The Maintenance Provider shall hold the complete and latest update of the applicable tech-nical documentation as issued by the TAA.

a The technical documentation must be specific for the applicable component or assem-bly including it’s Part Reference.

b The Maintenance Provider is required to adhere to the technical documentation includ-ing any supplements as issued by the TAA.

2 If the Maintenance organisation is not at Part 21-level, the Maintenance Provider must have an engineering support contract with the Design Activity (OEM) for any repair procedure or activity not covered by the technical documentation.

3 The TAA or its representative reserves the right to audit the Maintenance Provider and facil-ities.

4 Either of the following must be fullfilled if the Maintenance provider does not have a current license or approval from the current Design Activity (OEM):

a For components that are not on an FAA, Transport Canada (TC) or EASA capability list, and for components where EASA does not issue any component rating (i.e. compo-nents unique to State Aircraft), the Maintenance Provider must hold a current FAR/FAA Part 145 capability for components of the same category. Refer to Table 2 for compo-nent categories.

b For Maintenance providers that hold an USAF approval, the approval must be specific to the applicable Part Number or Assembly. All maintenance activities shall be docu-mented in accordance with TO-00-20-1; Aerospace equipment maintenance inspection, documentation, policies and procedures.

c For avionics components, category C2, C3, C5, C8, C14 and C18, the maintenance provider shall document prior experience on equipment in the same category and from the same Design Authority.

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1.4.4 Acceptance of maintained componentsBL3307 Certification of Conformity or equivalent is required by the TAA for identification of air-worthy components.

The release to service document shall include reference to the applicable technical documenta-tion, revision and date, used during maintenance.

Note

EASA Form 1 or FAA form 8130-9 is recognized as equivalent to BL3307.

1.4.4.1 Test reportFor avionics components, category C2, C3, C5, C8, C14 and C18, the maintenance provider shall prepare a SRU/ Sub-component test report for each S/N or individual component over-hauled or repaired. The Test report can be integrated or separate from the CoC (Release to Ser-vice document).

In addition to the CoC, the Test Report shall as a minimum contain the following information:

1 Item serial number, if applicable.

2 Maintenance activity performed.

3 Test equipment used, identified with Parts Reference.

4 System Test Specification (STS) or Drawing Specification that were used for test.

5 Certified Sub-Component Test Program with used revision, if applicable.

6 Parts replaced, if related to the maintenance activity.

7 Measurement results of the test.

Table 2 Component categories

Component class Categories

Components exept complete engines or APU’s

C1 Air Conditioning and PressureC2 Auto FlightC3 Comms and NavC4 Doors - HatchesC5 Electrical Power & LightsC6 EquipmentC7 Engine - APUC8 Flight ControlsC9 FuelC10 Helicopters - RotorsC11 Helicopter - TransC12 Hydraulic PowerC13 Indicating/Recording SystemsC14 Landing GearC15 OxygenC16 PropellersC17 Pneumatic & VacuumC18 Protection ice/rain/fireC19 WindowsC20 StructuralC21 Water BallastC21 Propulsion Augmentation


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8 Date when the test was performed.

9 Signature that certifies that the measurements are compliant to the STS or Drawing Specifi-cation.

1.5 Interchangeability and substitution of type specific parts

The TAA may authorize other organizations with engineering capability to do substitution evalua-tions depending on material class and weapon system. These organizations are listed under each aircraft type.

2 Requirements based on aircraft type

2.1 P-3C and P-3N

2.1.1 GeneralThe P-3 is a patrol aircraft produced by Lockheed, and Lockheed Martin (Marietta) is the Design Activity today. The Norwegian inventory of P-3 contain a version for Coast patrol (P-3N) and one version for Maritime patrol/Anti-submarine warfare (P-3C). The TAA have designed modifications to the P-3 system and act as Design Activity in those cases.

Technical publications for the P-3C are issued by the US Navy in the NAVAIR 01-75PAC- and NAVAIR 01-75PAI-series, supplemented with NAVAIR 01-75PAU-series from the Norwegian Defence Logistics Organisation, Air Systems Division.

Technical publications for the P-3N are issued by the TAA in the NAVAIR 01-75PAN-series.

Technical publications issued by the US Navair are approved by the TAA.

2.1.2 Technical documentation for part recognitionThe parts catalogues for the P-3 show the CAGE codes for the original manufacturers of a part number and not necessarily current or licensed manufacturers. In order to find the latest version of a part number or the current manufacturer additional information may be needed. The TAA have approved part information from the governmental agencies listed in Para 2.1.3 as part of the technical documentation for a part used on the P-3.

2.1.3 Interchangeability and substitutionsInterchangeability and substitution (I&S) engineering disposition done for type specific parts on the P-3 are generally approved by the TAA when issued by the following governmental agencies:

1 United States Navy (USN) (POC: PMA-290 at Patuxent River)

2 Royal Canadian Air Force (RCAF)

A distributor or manufacturer that are not explicitly approved by the TAA or Lockheed Martin must provide an approval from one of the above agencies for the part to be authorized for use on the Norwegian P-3 aircraft.

Note

There are systems used by the P-3 where the Design Activity is the TAA. For those cases only the TAA can approve an I&S for a part on the applicable system.

2.1.4 Approved Distributors and Manufacturers Lockheed Martin (LM) has approved distributors and manufacturers for the P-3 aircraft on their web page as denoted in Table 3, Table 4, Table 6 and Table 8. When a part has been purchased by a LM approved distributor or manufacturer, the sourcing responsibility has been transferred to LM. This implies that the CAGE found in the technical documentation not necessarily have to match the part delivered by the LM approved distributor or manufacturer.

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2.2 Engine and propellers

2.2.1 GeneralEngine and propeller parts are authorized seperatly from the aircraft it is utilized on. For the Nor-wegian inventory of engines and propellers the design authority is the original manufacturer and they either are the main supplier or have licensed the manufacturing and/or distribution of the type specific parts. See Table 6, Table 7, Table 8 and Table 9.

2.2.2 Technical documentation for part recognitionEvery engine and propeller has it’s own technical documentation where the parts catalogue show the P/N and the belonging Cage. For the type specific parts no other combination of P/N and Cage (part reference) is allowed except when the Design Authority for the engine or propeller or the TAA has granted a substitute.

3 Summary tables

Table 3 Current design activity for Norwegian military aircraft

A/C Current Design Activity

F-16 A/B Lockheed Martin (81755)

P-3C/P-3N Lockheed Martin (98897)

Table 4 Approved distributors and manufacturers for Norwegian military aircraft spare parts

A/C Approved supplier Supplier type

F-16 A/B Lockheed Martin F-16 Certified Parts Licensees (www.lockheedmartin.com/us/products/global-supply-chain-ser-vices/hologram-products/certfied-parts-licensees-list.html)

Manufacturers

Foreign Military Sales (FMS) Distributor

Fokker Structures, H0643 Distributor, structural parts

Fokker Landing Gear, H1632 Manufacturer, Landing Gear parts

Mecanex USA Inc, 1XU80 Distributor

AAR Corp, 81868 Distributor

Simtech, Inc, 1KVK9 Distributor

Kellstrom Industries, 1ZK21 Distributor

Blue Aerospace, 1WZW9 Distributor

P-3C/P-3N P-3 Certified Parts Authorized Distribu-tors (www.lockheedmartin.com/us/aero-nautics/eoc/p-3-certified-parts.html)

Manufacturers/Distributors

Foreign Military Sales (FMS) Distributor

P-3 Source Point (https://p3sourcepoint.osi-atl.net/login.jsp)

Manufacturers/Distributors


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Table 5 Maintenance Providers that have a current license or approval from the current Design Activity (non exhaustive)

Aircraft/Engine type

Maintenance provider Applicable component

F-16 A/B Lockheed Martin Approved Repair Centers (www.lockheedmartin.com/us/products/global-supply-chain-services/hologram-products/approved-repair-centers-list.html)

As directed by website

P-3C/P-3N P-3 Certified Service centers(www.lockheedmartin.com/us/aeronautics/eoc/p-3-service-centers.html)

As directed by website

Table 6 Approved distributors for Norwegian military aircraft engines

Engine A/C Current Design Activity Approved supplier

AE2100D3 C-130J Rolls-Royce (US) Rolls-Royce (Performance Based)

AEIO-360 T-17 Lycoming Norrøna Fly

F100 F-16 A/B Pratt & Whitney United Technologies Com-pany (Performance Based)

GEM MK 86 Rolls-Royce (UK) Rolls-Royce

GNOME MK 43 A/B Rolls-Royce (UK) Rolls-Royce

PT6T-3B/BE Bell-412SP Pratt & Whitney (Canada) United Technologies Com-pany

RTM322 NH-90 RTM/Rolls-Royce/Turbomeca NHI (Performance Based)

T-56 P-3C/P-3N Rolls-Royce (US) Rolls-Royce

TFE731 DA-20 Honeywell Fred Olsen Flyveselskap



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Table 7 Approved maintenance providers for Norwegian military aircraft engines

Engine A/C Current Design Activity Maintenance providers

AE2100D3 C-130J Rolls-Royce (US) Rolls-Royce (Performance Based)

AEIO-360 T-17 Lycoming Norrøna Fly

F100 F-16 A/B Pratt & Whitney - AIM Norway- Pratt & Whitney Belgium Engine Center

GEM MK 86 Rolls-Royce (UK)

GNOME MK 43 A/B Rolls-Royce (UK) AIM Norway

PT6T-3B/BE Bell-412SP Pratt & Whitney (Canada) Pratt & Whitney (Canada)

RTM322 NH-90 RTM/Rolls-Royce/Turbomeca NHI/Turbomeca

T-56 P-3C/P-3N Rolls-Royce (US) - AIM Norway- Rolls-Royce (US)

TFE731 DA-20 Honeywell GKN (Sweden)

Table 8 Approved distributors for Norwegian military aircraft propellers

Propeller A/C Current Design Activity Approved supplier

54H60-77 P-3C/P-3N Hamilton Sundstrand - Hamilton Sundstrand- Pacific Propeller International LLC (PPI)

HC-C2YK-4BF

T-17 Hartzell Hartzell

R391 C-130J Dowty Dowty (Performance Based)

Table 9 Approved maintenance providers for Norwegian military aircraft propellers

Propeller A/C Current Design Activity Maintenance providers

54H60-77 P-3C/P-3N Hamilton Sundstrand - AIM Norway- Pacific Propeller International LLC (PPI)

HC-C2YK-4BF

T-17 Hartzell - Norrøna Fly- Hartzell

R391 C-130J Dowty - Dowty- Rolls-Royce (Performance Based)

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