RA The Air Launched Weapon Release Certificate
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1 UNCONTROLLED COPY WHEN PRINTED Regulatory Article 1350 RA The Air Launched Weapon Release Certificate Rationale The carriage, launch and jettison of Air Launched Weapons (ALW) from aircraft present Risks to Life, additional to those from the aircraft, to users, the public and military personnel. The platform Type Airworthiness Authority (TAA) is wholly responsible for the safety of the complete weapons system. The purpose of an ALW Release Certificate (ALWRC) is to assist him to discharge this responsibility. Contents 1350(1): The Air Launched Weapon Release Certificate Regulation 1350(1) The Air Launched Weapon Release Certificate 1350(1) All ALW shall be certified by the issue of an ALWRC. Acceptable Means of Compliance 1350(1) The Air Launched Weapon Release Certificate 1. The ALWRC should: a. Be certified and issued by the ALW PTL with the appropriate Letter of Air Safety Notification (LoAN). b. Be formally approved and accepted by the Air System TAA. c. Conform to the model ALWRC at Annex A. 2. The ALWRC is a living document and its content should be proportionate to the complexity of the ALW and the system hazards. Any amendments should be undertaken by ALW PT SQEP who has been authorized appropriately. Staged Releases or significant changes such as the introduction of a new host platform should be authorized by the appropriate Weapon PTL. 3. The ALW LoAN holder should inform the Air System TAA of any limitations applying to the nominated Air System as a result of ALWRC limitations. 4. The ALW PT should provide and maintain an auditable trail for all changes to airworthiness documentation and ensure the equipment and the associated reference documents can be tracked and preserved throughout the life of the effected equipment plus 5 years (see RA1335). Guidance Material 1350(1) The Air Launched Weapon Release Certificate 5. ALWs are defined as those weapons Carried, Released (including launched, fired, or dispensed) and Jettisoned (CR&J) from an aircraft or Remotely Piloted Air Vehicle (RPAV) 1. These comprise: all bombs, missiles, rockets, aerial mines/depth charges and torpedoes which have been designed for CR&J from external or internal armament installations on fixed and rotary wing aircraft or RPAV. The definition covers both live and inert variants of the subject items, but excludes guns & ammunition up to 20mm calibre, and countermeasures. 6. The ALWRC is the certification by the ALW PTL that an acceptable Safety Assessment has been prepared to assess the CR&J of the ALW within defined environments and performance envelopes on the nominated platforms, provided that the ALW has been stored, transported and maintained in accordance with the ALW Safety Assessment and manufacture to target or disposal sequence. Close consultation with the relevant platform TAAs will be required (see RA1320). Relationship with the Air System RTS 7. The host aircraft RTS applies to the ALW only whilst it is on its host platform 1 N.B. For the purposes of this RA, the word release (all lower-case) is used to signify the CR&J of the weapon, and Release (initial capital) the airworthiness document. RA 1350 Issue 5 UNCONTROLLED COPY WHEN PRINTED Page 1 of 20
2 Regulatory Article 1350 UNCONTROLLED COPY WHEN PRINTED Guidance Material 1350(1) and up to a defined distance after release (i.e. not all the way to target). The ALWRC is intended to encompass CR&J on the launch platform(s). The ALWRC document will refer directly to all the evidence required by the Safety Assessment for the ALW. 8. The chapter headings in the generic model ALWRC at Annex A are mandatory. The lower-level topics and headings will be considered by an ALW PTL, but only those appropriate to the project need be presented in the final document. The ALWRC will be used to support acceptance of the weapon and the generation of the platform RTS. 9. A platform s RTS applies to the complete weapons system, so the ALWRC informs and/or restricts the RTS for each platform that is cleared to carry the weapon. Restrictions are unlikely to be identical for different platforms. 10. An ALWRC supplements an RTS in two major areas: a. It covers all aspects of an ALW build and operation from delivery to the platform to launch at target/disposal, thus providing a link between the ALW Safety Assessment and the platform RTS. b. It records the build standard that has been assessed for safe CR&J on each Air System with its associated Air System specific limitations. 11. The ALWRC will contain (or refer to) evidence which will be relevant to all actual and potential users through the life of the ALW project, not just that directly associated with the first platform which carried the weapon. It identifies the platform(s) the ALW is cleared for use on, and reflects the differing build-standards that apply to each platform. Certificates of Design (see RA5103) will be the primary source of such information and the ALWRC is to contain a record of all those issued. Clear and firm configuration control in accordance with Def Stan must be maintained. 12. The ALWRC is a living document and must be kept up to date to reflect changes in any of the relevant information or evidence affecting the safe use of the ALW or the limitations applied to any of the platforms which carry the ALW. This requires a Safety Management System (SMS) (see RA1200 & Manual of Air Safety) to ensure that the evidence to update limitations and advice is obtained (and retained through life) by the PTL responsible for the ALW. The PTL is to ensure that the relevant platform TAAs are kept informed of all emergent hazards or equipment changes that may affect the platform RTS. Limitations 13. The maximum design CR&J envelope applicable to an ALW (e.g. speed, g, altitude) may be considerably different to that appropriate to any one of the platforms it is carried on. The ALWRC is to be prepared with the aim of documenting the weapon s limitations (e.g. Service Life, structural, environmental, altitude, Electro- Magnetic Compatibility, etc) and the information required (e.g. interface control documentation) to allow its safe integration and operation on any specified Air System type. These will be reflected in the ALWRC. The applicability of various marks or variants of the weapon on each platform type (and variant, if applicable) will be stated unambiguously in the ALWRC. 14. Procedural limitations or temporary instructions, in the form of instructions to aircrew and/or ground-crew, to enhance safety or achieve specified functions, may form part of the ALWRC, but are only issued pending inclusion in a more appropriate document once the item is in service. Where the user Service wishes to apply temporary or urgent changes to limitations on the use of the weapon, this will usually be achieved by changes to the RTS; these limitation changes may be reflected in the ALWRC. Safety Assessment 15. The ALWRC provides the additional evidence for an extension of the platform Air System Safety Cases and will include CR&J of the ALW on nominated Air Systems. Compliance with regulations, standards 2 and processes will be demonstrated to confirm to the platform TAA the safety and airworthiness of the ALW. 16. The ALW PTL will consult the Defence Ordnance Safety Group and DSA-MAA- Cert-ES4-ArmSys armament specialists in the preparation of the ALWRC and RTSR 2 MAP-01 and JSP 520. Page 2 of 20 UNCONTROLLED COPY WHEN PRINTED RA 1350 Issue 5
3 UNCONTROLLED COPY WHEN PRINTED Regulatory Article 1350 Guidance Material 1350(1) to ensure that all weapon aspects of the Safety Assessment have been addressed as described in this RA and JSP520 (Ordnance, Munitions and Explosives Safety and Environmental Management System). Advice and assistance may also be needed from independent organizations. 17. The ALWRC will be signed by the ALW PTL. Where the PTL does not hold a LoAN, then the nominated Project Engineer (PE) LoAN is to countersign the ALWRC to certify the Certificate for the nominated weapon system. RA 1350 Issue 5 UNCONTROLLED COPY WHEN PRINTED Page 3 of 20
4 Regulatory Article 1350 UNCONTROLLED COPY WHEN PRINTED ANNEX A THE MODEL AIR LAUNCHED WEAPON RELEASE CERTIFICATE (ALWRC) Presentation of the Model Text A.1 In the model text the following conventions are used: A1.1 All normal text, including headings, will be used as shown. A1.2 Italic text within brackets thus {example} is used to show where text appropriate to a specific Release is required, and be replaced or deleted before issue of the final document. A1.3 Italic text presented within shaded boxes, as this example, provides guidance on the required content. A1.4 Where normal text is shown within double-line boxes, as in this example, mandatory content is defined, but the presentation is not specified. A1.5 Where a table is shaded and italic text is used, as below, this indicates that it is an example of an acceptable format. Mod No Not Authorized Essential Affects ALWRC Affects Pubns No Effect on ALWRC Page 4 of 20 UNCONTROLLED COPY WHEN PRINTED RA 1350 Issue 5
5 UNCONTROLLED COPY WHEN PRINTED Regulatory Article 1350 THE MODEL AIR LAUNCHED WEAPON RELEASE CERTIFICATE CONTENTS Parts PRELIMINARY PAGES RELEASE CERTIFICATE PART 1 AIRWORTHINESS AND DOCUMENT MANAGEMENT PART 2 ALW SPECIFIC INFORMATION PART 3 PLATFORM SPECIFIC INFORMATION PART 4 ADDITIONAL INFORMATION AND MODIFICATIONS {Security Classification} COVER PAGE RA 1350 Issue 5 UNCONTROLLED COPY WHEN PRINTED Page 5 of 20
6 Regulatory Article 1350 UNCONTROLLED COPY WHEN PRINTED {Weapon Identifier, usually Type and Mark} Air Launched Weapon Release Certificate {Issue Status} {ALWRC Reference} COVER PAGE Page 6 of 20 UNCONTROLLED COPY WHEN PRINTED RA 1350 Issue 5
7 UNCONTROLLED COPY WHEN PRINTED Regulatory Article 1350 PRELIMINARY PAGES The preliminary pages of the ALWRC are to contain the following sections: Classified Supplement: When the document is a Classified Supplement, then the following statement is inserted at the head of this page as it is vital that Supplement and main document are coherent at all times: This document is the Classified Supplement to the Air Launched Weapon Release Certificate for the {weapon identifier}. This Supplement will be read in conjunction with the main document {document reference} List of Contents List of contents to be provided, to a level of detail as required by the {relevant ALW PT}, but the chapter headings are mandatory. Classified Supplement: When the document is the main ALWRC and there is a Classified Supplement, the following statement will be inserted at the end of the list of contents, and the reference included at A.8.2.3: Classified Supplement There is a Classified Supplement to this ALWRC, issued under a separate distribution. List of Amendments An amendment list must be provided to record all amendments made to the ALWRC Amendment Number Date Detail of Change List of Effective Pages An important element of document control is ensuring that the document is complete and has been correctly maintained. Therefore the ALWRC will have a List of Effective Pages which will be updated by every amendment. Page Issue / Amendment Page Issue / Amendment List of Abbreviations and Acronyms The ALWRC must provide a consolidated list of the abbreviations and acronyms used throughout the document as an aid to the reader. Where appropriate, this list will include specific labels and / or captions that are used to define limitations (in which case they must reproduce the presentation in the ALW exactly in relation to (mis-)spelling and capitalisation and not follow any particular style conventions in use in the ALWRC). RA 1350 Issue 5 UNCONTROLLED COPY WHEN PRINTED Page 7 of 20
8 Regulatory Article 1350 UNCONTROLLED COPY WHEN PRINTED Definition of Terms It is important to the use of the ALWRC and the overall airworthiness of the aircraft that there is a clear and common understanding of the terms used within the ALWRC. Therefore, every ALWRC will have a section dealing with the Definition of Terms. Wherever practicable, the definitions used are to be as contained in the following sources, listed in order of precedence: a NATO AOP-38 NATO Glossary of Terms & Definitions concerning the Safety & Suitability for Service of Munitions, Explosives and Related Products. b NATO AAP-6 The NATO Glossary of Terms and Definitions c Joint Doctrine Publication (JDP) United Kingdom Supplement to the NATO Terminology Database. Presentation of Warnings, Cautions and Notes The convention used for presenting Warnings, Cautions and Notes within the ALWRC needs to be explained. The appropriate statement will be selected from the following: The Warnings, Cautions and Notes are placed as close as practicable to the relevant limitation/procedure. Or The Warnings, Cautions and Notes are called out and numbered within each sub-section, and placed at the end of the relevant sub-section within each Part. Or The Warnings, Cautions and Notes are called out and numbered within each Part, and placed at the end of the relevant Part. Distribution Necessary to ensure amendments are promulgated to all document holders Action: {Sponsor Head Equipment Capability} {ALW PTL} {Host Aircraft TAAs and RTSAs - so that they can include weapon limitations in the aircraft RTS} {Manufacturer/Designer - for comparison with original design assumptions and limits} Information: {Aviation Duty Holders} {Resident Project Officers - for information} {OC Handling Squadron - for comparison with aircrew documentation data (under the delegated authority of relevant PTLs)} {Air Warfare Centre - for generation of operational performance information} {Military Aviation Authority DSA-MAA-Cert-ES4-ArmSys- for information} {Defence Ordnance Safety Group for ordnance aspects} {Collaborative foreign users - for comparison with their own certification documentation} {Weapons Engineering PT DES WpnsEng-Airworthiness for input to the ALWRC Library and records} Page 8 of 20 UNCONTROLLED COPY WHEN PRINTED RA 1350 Issue 5
9 UNCONTROLLED COPY WHEN PRINTED Regulatory Article 1350 RELEASE CERTIFICATE I certify that the ALW, described at Part 2 of this document, has been assessed for CR&J within the environmental 3 and performance 4 envelopes defined in Part 3 on the platform(s) nominated below; that any associated risks and hazards have been identified and bounded; and that the necessary limitations and mitigations have been included in Part 3 of this ALWRC. - e.g. Tornado GR4 / GR4A - Typhoon FGR4 - F-35 B Lightning II - MQ-9 Reaper UAS - Mantis UAS - etc The Air Launched Weapon Release Certificate only remains valid provided the Weapon, Ordnance, Munition, Explosive (WOME) has been stored, transported, handled and maintained in accordance with the Manufacture to Target or Disposal Sequence (MTDS) and the Weapon Safety Assessment. {Signature} {Name} PTL {weapon identifier} {Date} All Release Certificates to use a common standard of wording 3 The environmental envelope is the measured or predicted levels of shock, buffet, flutter, vibration, Nz, intra-store effects, rf, etc, for the nominated aircraft type(s) that the ALW qualification programme and safety assessment were based on. This data is derived from the ALW User Requirement Document/System Requirement Document (URD/SRD) and agreed in liaison with the Air System TAA. 4 The performance envelope is the CR&J heights, speeds, dive angles, acceleration and roll-rate limits, etc, as defined in the Equipment Safety Assessment/CofD for each aircraft type/srd and agreed in liaison with the Air System TAA. RA 1350 Issue 5 UNCONTROLLED COPY WHEN PRINTED Page 9 of 20
10 Regulatory Article 1350 UNCONTROLLED COPY WHEN PRINTED PART 1 - AIRWORTHINESS & DOCUMENT MANAGEMENT 1.1 Introduction Purpose. This ALWRC is the certification by the {ALW PTL who holds the relevant LoAN} that an acceptable Safety Assessment has been prepared and maintained for {weapon identifier} and its equipment, and that this ALWRC can form the basis for a formal approval of {weapon identifier} for operation on the aircraft types stated in Part 3. The ALWRC provides the limitations within which airworthiness and safety in the role are declared and have been verified by a safety assessment analysis Amendment. Amendments will be promulgated automatically to the agencies detailed within the distribution list. Suggestions for amendment are to be forwarded to: 1.2 Responsibilities The Designer responsibilities for the weapon are listed below: {Overall Weapon} {Weapon Manufacturer and contact details} {Other directly-contracted designers who have a role in maintaining the configuration control of the weapon and associated equipment, e.g. Motor Manufacturer, Guidance or other major system or Co-ordinating Manufacturer} The {weapon identifier} will be managed through-life by the following agencies: {EC Sponsor} Responsible for Equipment Capability and potential performance improvements. {PT} Development, acquisition and through-life management of the weapon system with engineering and logistic support. {User (or multiple Users)} Weapon operation and training In-Service. Feedback on weapon operation and all support implementation aspects. 1.3 Incident and Fault Reporting Refer to MAP-01 & JSP 482/520 and any other weapon-specific special requirements PART 2 ALW SPECIFIC INFORMATION This part of the ALWRC contains details of the weapon design, performance and limitations on its operational use. Part 3 is for limitations that affect the use of the weapon when fitted to an aircraft, while the limitations in Part 2 are always applicable. Thus, limitations that have an impact on the operation of the weapon/aircraft combination are to be included in Part 3. All limitations are to be expressed in a manner that allows them to be complied with by the aircrew or ground-crew as appropriate. The conditions pertaining to a particular limit are to be expressed unambiguously. Where the meaning of a term is not formally defined it must be explained. Conflict, or perceived conflict, of information will be avoided. This part of the ALWRC covers those limitations that are related to the hardware or systems of the weapon. Only limitations that have an impact on the safe handling, maintenance or airworthy operation of the weapon, to a required performance standard, within Service use, are to be included. They are to be expressed in a manner that allows them to be complied with by personnel (ground or aircrew). The conditions pertaining to a particular limit are to be expressed unambiguously. Where system limitations are wholly described in Part 2 they need not be repeated in Part 3. System limitations must be comprehensively covered under the relevant heading. Aircraft-specific limitations must be presented in Part Description The {weapon identifier} is an {weapon description}, procured against {reference to agreed characteristics or User Requirements Document (URD) against which contract was let} for use by {service operator} in the following roles: Page 10 of 20 UNCONTROLLED COPY WHEN PRINTED RA 1350 Issue 5
11 UNCONTROLLED COPY WHEN PRINTED Regulatory Article 1350 Refer to the weapon Certificate of Design, Certificate of Safety OME (CSOME) and weapon Concept of Ops. Also list the roles in which the weapon can be used, i.e. Air-To-Air, Air-To-Ground, Anti-armour, hardened target etc. {Primary Roles} {Secondary Roles} {Tertiary Roles} The {weapon identifier} is designed to meets the requirements of {design standard e.g. Def Stan (or 00-56), US Military Specifications, STANAGs, etc}. It is manufactured in {country of origin} by {manufacturer} under {arrangements to ensure manufacture is to design}. Exceptions to these design standards are detailed in the {Certificates of Design} identified in Parts 2 and Part 3 for specific aircraft integration. 2.2 Weapon Description and Associated Operating Equipment Refer to weapon Certificate of Design e.g. The weapon is described in detail at Reference.... and weapon safety assessment for detail Brief physical overview of the weapon, with size, method(s) of carriage and release, data links, guidance, associated support (e.g. loading). If available, refer to APs for details of construction, procedures etc. Include details of: ALW Variants (operational round, practice round, drill/other training round) Key safety features, fuzing etc. Launchers Other equipment (e.g. planning tools) needed to use weapon 2.3 Weapon Interface Control Documentation Refer to the generic Interface Control Document (ICD) for the weapon and the method of configuration control. Platform-specific ICDs will be detailed in Part Statement of Operating Intent and Usage Refer to the weapon URD, SRD, CONOPS, CONEMP and SOIU. Provide the details of the Concept of Operations and the Manufacture to Target/Disposal Sequence (MTDS) (with reference to section 2.11) for a weapon system that will form the Statement of Operating Intent and Usage (SOIU). It will provide details of predicted g loads, landings, speeds etc for each carriage hour. Cross-reference must be made to the SOIU for each aircraft type as required. Outline the maintenance support philosophy, referring the reader to appropriate elements of Part C; e.g. packaging/containers, storage etc. 2.5 Weapon Service Life The limitations in parts 2 and 3 are valid for the life of the weapon. The weapon design Service Life is summarised in the following: Refer to the Joint Service Munitions Control Register (JSMCR) or weapon-specific (J)AP Topic 5). It is normally derived from the MTDS (see section 2.11) which provides the usage spectrum for the weapon. {Table of Service Life figures: Carriage Life, Storage Life (in different environments), Standby Life, assumed usage spectrum for the weapon, etc.} 2.6 Weapon Configuration The design standard and authorized modifications of {weapon identifier} to which this ALWRC applies is given below: Users of the ALWRC are to note that, unless listed or referenced below, a modification or new item of equipment is not to be fitted or used. In case of doubt, refer to: {Contact details of Desk Officer dealing with the ALWRC} RA 1350 Issue 5 UNCONTROLLED COPY WHEN PRINTED Page 11 of 20
12 Regulatory Article 1350 UNCONTROLLED COPY WHEN PRINTED Within section 2.6 the weapon configuration will be built up through the sub-sections of: Design Standard Refer to the Weapon Configuration Status Record (CSR). Definition of the design or build standard of the weapon. If there is more than one manufacturing source then multiple entries will be required. List of production Design Standard(s), Configuration Status Record (CSR) (formerly Master Record Index (MRI) {number and issue state} Statement of the Design Certification procedures applicable to the weapon and ancillary equipment (they may be different) (See RA5103). Design Certificates are then listed in a Table containing the following column headings: Weapon/Equipment Type Platform Type and Mark Type of Certificate of Design Issued (e.g. {Name-of-Designer firm} Form 111) Certificate of Design Serial No Date of Issue Weapon Software Standards Detail the weapon software standards and configuration control process, cross-referring to the appropriate element of the Designer Modification section 4.5 as required. 2.7 Weapon Performance/Effectiveness Refer to the weapon performance model, 6 DoF model and ballistic model. Overview of the optimum operational and maximum potential performance of the weapon, including range, warhead effectiveness, target engagement, etc. If there is a weapon performance/effectiveness model it must be identified with its version number. If this item (and the next) demands a high security classification for the ALWRC, the use of a classified supplement may reduce the classification of the rest of the document. 2.8 Weapon Delivery Envelope Refer to the weapon MTDS and Safety Assessment. Overview of the release parameters etc. No mention of specific host aircraft, as this section is strictly for the weapon s parameters. (i.e. the environments that the ALW has been qualified against) The weapon is cleared to max/min g, speed, height, acceleration, α, temperature, EMC, etc. as set out in the weapon MTDS and weapon Safety Assessment. 2.9 Explosive Hazard Classification Refer to the weapon ESTC Classification. Statement of explosive hazard classification, and any specific explosive related limitations, not covered elsewhere in the Certificate. List Explosives Storage and Transportation Committee (ESTC) Explosive Hazard Classification Codes and Serial Numbers Weapon and Component Security Classification Refer to the weapon Security Grading Letter. Detail the security classification of the weapon, its sub systems and equipments. Also the authority for (automatic) downgrading of Classification (over time). Page 12 of 20 UNCONTROLLED COPY WHEN PRINTED RA 1350 Issue 5
13 UNCONTROLLED COPY WHEN PRINTED Regulatory Article Manufacture to Target/Disposal Sequence Refer to the weapon MTDS. Describe the MTDS. Cross-refer to the AOP 15 Environmental Questionnaire complying with STANAG 4297 and NATO Allied Ordnance Publication (AOP) 15) 2.12 Maintenance and In-Service Testing Refer to weapon maintenance plan and procedures. Detail the Maintenance Policy and in-service testing with reference to documentation. Testing is in-service testing, e.g. to determine weapon serviceability/reliability etc. not development testing Weapon Loading and Unloading Refer to any relevant procedures. Generic process, with reference to Part 3 for specific platform procedures Laser Safety Refer to weapon safety assessment. Provide details of all laser safety, or laser-related limitations. If no laser is fitted, or is aircraft-mounted, this section will contain the statement: No laser limitations are applicable to this weapon 2.15 Emergency and Contingency Arrangements Refer to the weapon safety assessment and WOME safety instructions. Emergency and Contingency Arrangements must be reflected in the relevant APs and Aircrew Flight Reference Cards etc. This section must indicate that credible emergencies have been addressed and identify the relevant references. At a minimum, it must include reference to procedures for: Crash-site hazards and precautions (environmental and personnel safety precautions). Aircraft emergencies affecting the weapon (e.g. emergency removal in event of undercarriage failure). Aircraft at non-military airfields (e.g. additional safety precautions to protect the public (and protect the weapon)) Aircraft landing away-from-base (unplanned) Other Equipment (optional) Subject to the ALW PTLs discretion, modifications or authorizations for any equipment that is fitted to the weapon but is not covered by sub-sections 2.6; i.e. "equipment not-basic to the weapon". The following are possible further sub divisions that are suggested, but others may be used at the discretion of the PTL. Role equipment (when applicable) Ground Handling and Storage Equipment (when applicable) Test Equipment (when applicable) 2.17 Related Documents Weapon Document Set Refer to MAP-01, MAP-02, Topic 5X, Topic 5A6, etc. Create entry in the forms as detailed below for all airworthiness-related documents, including: host aircraft RTS, Technical Publications (or Interactive Electronic Technical Publications (IETPs)), etc. RA 1350 Issue 5 UNCONTROLLED COPY WHEN PRINTED Page 13 of 20
14 Regulatory Article 1350 UNCONTROLLED COPY WHEN PRINTED The production design is airworthy when operated by qualified service personnel within the limitations promulgated in Parts 2, 3 and 4 of this ALWRC and in accordance with the information and provisions contained in the following related documents: {Document} to the latest issue, published and maintained by {publishing organization under the authority of the Platform/ALW PTL} and on behalf of {Director of the appropriate Front Line Command Capability Organization} To ensure the continuing airworthiness of the weapon, it will be serviced and maintained in accordance with: {Technical Publication reference} to the latest issue, published and maintained by {publishing organization} under the authority of {document sponsor}. Note that the weapon product data to support entries in the Air System Document Set(s) must be provided to those responsible for publishing the platform-specific references, and a robust updating system maintained through life to ensure all appropriate changes are reflected in the complete document chain Other Documentation (optional) Other documents referred to in this ALWRC which contain information relevant to the airworthiness of the operation of this weapon are: {Document Reference} to the latest issue, published and amended by {publication authority} under the authority of {document sponsor}. The following sub-section is used when appropriate to a main ALWRC document that has a Classified Supplement, or to the Supplement itself. The Classified Supplement {Document Reference}, {Issue}, {Amendment}. Or the main ALWRC {Document Reference}, {Issue}, {Amendment} Page 14 of 20 UNCONTROLLED COPY WHEN PRINTED RA 1350 Issue 5
15 UNCONTROLLED COPY WHEN PRINTED Regulatory Article 1350 PART 3 PLATFORM SPECIFIC INFORMATION The {ALW Identifier} is approved for use within the limits contained in this ALWRC on the following aircraft types: Part 3 of the ALWRC is for the presentation of weapon information and limitations that are specific to a particular weapon/aircraft combination. It is important to note that this certificate identifies the limits to which the weapon has been cleared and is not a copy of the relevant platform TAA s statement of the aircraft s limits when carrying the weapon. Thus, included in this part are the weapon manufacturer s stated or evaluated safe limits for weapon carriage on a specified platform but excluded are the integrated carriage, release and jettison limits for the aircraft while carrying this weapon (usually with others). It is expected (but will not always be the case) that information for this section will come from the weapon manufacturer s aircraft-specific Certificates of Design, while information for the aircraft RTS will also be derived from the aircraft manufacturer s Certificate of Design and Military Flight Test Permit and weapon/aircraft integration trials. 3. Integration Limits for {Aircraft Identifier} 3.1 Aircraft Type & Mark Refer to the Weapon CofD. State the aircraft or aircraft derivative that the weapon can be fitted to and cross-refer to the associated RTS. 3.2 {Aircraft Identifier} SOIU Refer to the Aircraft RTS. 3.3 Configuration Requirements. Refer to aircraft RTS. Detail configuration requirements (i.e. aircraft carriage equipment, any aircraft specific modification state of weapon and aircraft modifications essential to support the weapon). 3.4 {Aircraft Identifier} Interface Control Document Refer to the specific ICD for weapon/platform combination. 3.5 {Aircraft Identifier} Limitations and Constraints. Detail weapon integration limitations and constraints for this specific host aircraft. May include: Airborne carriage and/or flight hour limitations CR&J limitations Mission management, or other data transfer limitations Gun firing, including effect on missile of blast, vibration and inertia loads Adjacent weapon considerations EMC limitations TEMPEST limitations 3.6 {Aircraft Identifier} Certificates of Design Refer Platform CofD. Cross-Refer to the Certificates of Design that are specific to the weapon and its equipment for this aircraft type. They will be detailed in section 2.1 RA 1350 Issue 5 UNCONTROLLED COPY WHEN PRINTED Page 15 of 20
16 Regulatory Article 1350 UNCONTROLLED COPY WHEN PRINTED 3.7 {Aircraft Identifier} TEACASE Limitations The Thermal Effects on Airborne Conventional Armament Stores and Equipment (TEACASE) limitations are necessary to ensure that ALW do not exceed their nominated upper or lower temperature limits during air carriage. Liaison with the DOSG Air Weapons Advisory Committees will be required to generate these data. 3.8 {Aircraft Identifier} Aircraft Self Damage (ASD) This section will provide information to the platform PT on the weapon characteristics which could pose a risk of damage to the launch aircraft or other nominated aircraft following successful ALW release, arising from the timely detonation of the weapon at the point of arming or at the target as detailed in ASD Note 12. Liaison with the DOSG Air Weapons Advisory Committees will be required to generate these data. Include any limitations on pre- and post-launch weapon settings, launch and post-launch management required to avoid aircraft self-damage, or damage to aircraft in the same formation. It must address the case where the weapon detonates on arming and cover aircraft self-damage prior to propulsion initiation (or failure) whilst in the vicinity of the platform. It must include any work carried out or statement made describing the debris pattern when the weapon successfully engages a target. 3.9 {Aircraft Identifier} Air Weapons Ballistics This section will provide information to the platform PT on Weapon Danger Areas (WDA), as defined in JSP 403, for nominated weapon releases. Liaison with the DOSG Air Weapons Advisory Committees will be required to generate these data {Aircraft Identifier} Document Set 3.11 {Aircraft Identifier} Misfire, Hang Fire and Hang Up Procedures Page 16 of 20 UNCONTROLLED COPY WHEN PRINTED RA 1350 Issue 5
17 UNCONTROLLED COPY WHEN PRINTED Regulatory Article 1350 PART 4 - ADDITIONAL INFORMATION AND MODIFICATIONS 4.1 Temporary Information The purpose of Part 4 of the ALWRC will enable any information of a temporary nature to be managed. Each element of Part 4 will have been derived from a supplementary Safety Assessment, and will provide information (limitations) on one or more aspects of the weapon system operation. Examples are an Operational Emergency Clearance (OEC) for the employment of the weapon on an aircraft type not covered in Part 3, or an OEC for a modification to the weapon. A record of all (past and present) temporary certificate information. The definition of the applicability of each change (e.g. weapon batch number, Operational Evaluation Unit (OEU) flying only, named exercise). The arrangements for withdrawal of each change (e.g. calendar, embodiment of a modification, formal clearance). A definition of the parts of the weapon document set affected by each change. The location of the temporary information. The ALW PTL has the option to place the temporary information entirely within Part 4 of the ALWRC, or to use insert pages in the appropriate places throughout the weapon documentation set, whichever method is best suited the particular circumstances. 4.2 Service Derived Information Part 4 of the ALWRC is for recording and giving authority to Service-derived information, such as authorisations and limitations related to the introduction of a Service Modification (SM). If, as is likely, there is no Service-derived information for a particular weapon, then this section must contain the statement: There is no Service-derived information for {weapon identifier}. 4.3 AUDIT TRAIL [Not part of promulgated ALWRC] Information Audit Part contains the data that enables the content of Parts 1, 2, 3 and 4 to be auditable and traceable. It will be maintained by the ALW PTL throughout the life of the weapon. Some elements may exist as databases in their own right. The minimum that is required is an index of where the following information can be found: Attribution matrix specifying the source of every element of the earlier parts Design documentation (CSR, Certificates of Design, etc.) List of Trials and associated Reports not covered by the design documentation Details of any Safety Assessments relating to the weapon or its systems Details of sentencing of trial recommendations Other references and base-line data used in generating the first issue Details of all changes to the initial issue (amendments and subsequent issues) to include their nature, the reason for their introduction and the individual authorizing their implementation. RA 1350 Issue 5 UNCONTROLLED COPY WHEN PRINTED Page 17 of 20
18 Regulatory Article 1350 UNCONTROLLED COPY WHEN PRINTED Specialist Advice This section provides reference to the specialist advice received for this weapon, whether or not it forms part of the Audit Trail at To include reference to: DOSG Safety Advice Ordnance Safety Review Panel (OSRP) Certificate of Safety OME (CSOME) Recommendations, Caveats and Provisos Magazine Safety Statement Naval Ordnance Safety Statements Test & Evaluation Reports Safety Assessment Refer to weapon safety assessment. This section provides a reference to the top level safety assessment for the weapon, whether or not it forms part of the Audit Trail at Integrated Test, Evaluation and Acceptance Plan Refer to the weapon ITEAP. This section provides a reference to the Integrated Test, Evaluation and Acceptance (ITEA) Plan for the weapon. Statement as to how the ITEA links with the Safety Assessment. It details: The agency responsible for maintaining the ITEA. The overview of the ITEA. The test methodology. Trials and modelling conducted, including: Safety and suitability trials Flight Trials Weapon performance trials Warhead trials Fuse integration trials Computer modelling, where appropriate Six degree of freedom mathematical modelling Non-Compliance/Further Work Refer to the weapon URD/SRD. This section details the extent to which the weapon fails to comply with the original requirements (URD/SRD) and any outstanding work planned to clear the non-compliance, including statements on those issues that will not be addressed Engineering Actions from Weapon Safety Assessment Refer to the weapon safety assessment. The limitations expressed within the ALWRC are the procedural mitigations to reduce operating hazards to an acceptable level. This section will include Advice to User information from the DOSG or information derived from equipment trials that form the procedural information necessary for safety. These limitations are therefore an output of an implicit, or if the weapon has a formal safety assessment. From the safety assessment there may well be engineering mitigations in addition to operational ones. It is important that these engineering mitigations, on which the safety of the weapon is based, are recognised as safety critical, and are not lost in the general maintenance actions. The majority of general weapon maintenance is safety critical; however, if the safety of the weapon is based upon any specific engineering actions these must be detailed in section A6. Many of the engineering hazard mitigations will be fatigue life related, although other engineering actions could result from the safety assessment; e.g. detection of dormant faults. Moreover, a weapon may have no safety critical engineering actions. Page 18 of 20 UNCONTROLLED COPY WHEN PRINTED RA 1350 Issue 5
19 UNCONTROLLED COPY WHEN PRINTED Regulatory Article Service Modifications (SM) This sub-section must give a list, or provide cross-reference to a list that is under the configuration control of the Weapon PT, of all Service Engineered modifications: i.e., SMs etc that may be embodied on the weapon. The full list must indicate for each modification whether it is: Not Authorized; Essential; Affects ALWRC; Affects Weapon Publications; No Effect on ALWRC. 4.5 Designer Modification Identify, by listing or cross-reference to a full list that is under the configuration control of the weapon manufacturer, all Designer modifications introduced since the initial design, including those that represent full design incorporation of Service modifications. The full list must indicate for each modification whether it is: Not Authorized; Essential; Affects ALWRC; Affects Weapon Publications; No Effect on ALWRC. 4.6 OEC and CLE Identify, by listing or cross-reference to a full list of special clearances (See RA1300 & RA1330) required to satisfy the operational imperative or detail the shortfalls in evidence for the weapon. The full list must indicate for each special clearance: OEC/CLE Number; Applicability; Withdrawal arrangements; Affected parts of ADS; Review date; Affected Weapon Publications; No Effect on ALWRC. RA 1350 Issue 5 UNCONTROLLED COPY WHEN PRINTED Page 19 of 20
20 Regulatory Article 1350 UNCONTROLLED COPY WHEN PRINTED Intentionally Blank for Print Pagination Page 20 of 20 UNCONTROLLED COPY WHEN PRINTED RA 1350 Issue 5
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