Boing srm

What type of information does the SRM provide?. Provides approved procedures for aircraft structural inspection and repair, including types of damage, allowable limits, materials, tools, and repair methods. Provides allowable damage limits, structural repair procedures, material selection, fastener installation, tolerance review, and more. It provides approved procedures for aircraft structural inspection and repair.

What requirements does ATA Specificaticn 100 make for manuals?. it establishes a standardized coding system to facilitate finding information. La estructura estandarizada del manual por capítulos (ATA), con formato numérico XX- ATA 100 a los manuales? YY-ZZ, facilita la navegación, consistencia y uso comúnentre fabricantes. ATA 100 establishes a standardized coding and formatting structure for aeronautical technical documentation, making it easier to locate information.

Explain the numbering system used in the SRM: It uses three elements: ATA chapter-section -subsection (e.g, 51-10-00). The ATA XX-YY-ZZ system indicates: XX = Chapter (system), YY = Subgroup (functional). 7 = elements. Specific section (details/procedures). E.g., 51-30-02 → general structure - ATA Spec 100 and SRM Chapter 00 rivet installation. First element (51): ATA chapter Second element (10): section Third element (00): subsection.

How to present allowable damage information in the old SRM forma?. Old format: Simpler organization, less visual, and with less standardized information. New format: Improved with tables, clearly defined ATA codes, detailed illustrations, and sections organized for easy navigation. Old format: Less visual and organized. New format: Tables, illustrations, clear sections. It is organized by structural chapters (ei.53 Fuselaiel, where damage limits, typical repair instructions, and attached figures are presented in the old SRM format.

HOW TO PRESENT ALLOWABLE DAMAGE, IDENTIFICATION, AND REPAIR INFORMATION IN THE NEW SRM Format?. Enhanced with tables, clearly defined ATA codes, detailed illustrations, and organized sections for easy navigation. Simpler, less visual organization with less standardized information. Old format: Less visual and organized. New format: Tables, illustrations, clear sections.

Types of SRM review service: Temporary (TR) and Permanent review. Major Revision: Updates entire sections of the manual. 2. Temporary Revision (TRI): Inserts urgent changes up to the next major revision. Chapter 00 - "List of Effective Pages. Temporary Revision (TR): Immediate changes before the general revision. Permanent Revision (Revision): Final incorporation of TR and other changes into the base document.

Chapter 51 information in both SRM formats?. Contains general criteria applicable to all structural repairs. Chapter 51 (general structure) does not change its main technical content, but in the new format it is more organized and linked to digital materials and processes. Chapter 51 (Structure) contains general criteria applicable to all structural repairs. In both formats, it includes materials, processes, tolerances, types of damage, and joining techniques.

What to do if a specific repair is not found in the SRM?. Should a repair be requested by the manufacturer's engineering department (Boeing) or SRM? Consult with the Designated Engineering Representative (DER). Contact the manufacturer to obtain authorization (Enaineering Authorization (EA). The manufacturer (OEM) must be contacted to obtain an approved repair or Engineering Authorization (EA).

What information does the BMS manual present?. Specifications for materials used in the aircraft. BMS (Boeing Material Specification) contains technical specifications for sealants, paints, composites, manufacturing processes, and surface treatment. The Boeing Material Specification (BMS) details the specifications for materials used in the aircraft, such as alloys, composites, and coatings.

What information does the BPS manual present?. Manufacturing and repair processes such as heat treatments, coatings, etc. BPS (Boeing Process Specification) details manufacturing and repair processes, such as welding, riveting, anodizing, chemical cleaning, and more. The Boeing Process Specification (BPS) describes manufacturing and repair processes such as welding, heat treatment, coating application, etc.

Define Allowable Damage: Damage allowed without affectingsafety or structural functionality. allowed without affectingsafety. is defined as damage that is permitted with no other flight restrictions.

Define Repairable Damage. Damage that requires repair following the SRM. is defined as damage that can be reworked or repaired. Damage that exceeds the allowable limit, but is repairable.

DEFINE DAMAGE BEYOND REPAIR. Damage that cannot be repaired according to the SRM limits. Damage that cannot be repaired according to the SRM and requires replacement or special authorization from the manufacturer. Damage that cannot be repaired or special authorization from the manufacturer.

DEFINE EDGE MARGIN AND EDGE DISTANCE. Edge Margin: Distance from the center of the nearest hole to the raw edge of the part before drilling. Edge Distance: Distanceof the hole to the finished edge of the part. Distance from the center of the hole to the edge of the material. Distance from the center of the nearest hole to the raw edge.

Define permanent and removable fasteners: Permanent: rivets. Removable: screws, bolts. Permanent: Non-reusable (rivets). Removable: Can be removed and reinstalled (screws, bolts). Can be removed Permanent: rivets; Removable: screws, bolts.

Most used metal in aircraft structures: Aluminum (alloys such as 2024 and 7075),. Aluminum (alloys such as 2025 and 7075),. Aluminum (alloys such as 2026and 7070),.

Define Tolerance: Acceptable range of dimensional variation without affecting functionality. Allowable margin of variation in a measurement. It is the acceptable margin of variation in a physical measurement without affecting the functionality or integrity of the component.

What is Primary Structure?. Supports critical loads; failure compromises safety. Components whose failure seriously affects flight safety (e.g. spars, frames, main ribs). Components whose critical loads; failure compromises safety.

What is Secondary Structure?. Not critical to the structure, but functional. Structural parts whose damage or failure does not directly compromise the integrity or safety of the aircraft (e.g. access panels, covers). Structural components that are not essential to the primary structural integrity of the aircraft, but are important to its operation and/or performance. If the secondary structure fails, failure will not occu.

What is a Category A Repair?. Permanent, requires no additional inspections. Not Permanent, requires no additional inspections. Yes Permanent, requires no additional inspections.

What is an Interim Repair?. A temporary solution to a fault or damage that allows the aircraft to continue operating while a permanent repair is planned. Temporary, allows flying until final repair. If the secondary structure fails, it will not result in the aircraft failing, but it may affect its operation or performance.

What is a Category B Repair?. Limited-use repair by time or cycles. Repairs that meet the aircraft design certification basis but are complementary. Category B as a permanent repair that allows further inspection to assess its condition.

What is a Time-Limited Repair?. Same as Category B. refers to a repair that is performed with the expectation that the part or component. expectation that the part or component.

How are rivet diameter and length expressed?. Diameter in 1/32", length in 1/16". A rivet with a diameter of 1/8 inch would be indicated as 4/32 inch (since 1/8 is equivalent to 4/32. Diameter in 1/2", length in 2/16".

What effectiveness number do we use and where is it?. According to the airplane serial number, lccated in Chapter 00. They are usually related to the speed of the aircraft in different phases of flight. They refer to key values ​​used for flight planning and operation, not to a single "effectiveness number".

Are PSES primary or secondary?. Primary Structural Elements. Secundary Structural Elements.

Where is the manual revision?. In Chapter 00, under "List of Effective Pages (LEP)". Chapter 02, under "List of Effective Pages (DEP)". Chapter 00, under "List of Effective Pages (LE)".

Typical repairs are preferred..." True or false. FALSE, it is preferred to use specific chapters (52-57). True it is preferred to use specific chapters (52-57).

Where can you see that it is FAA approved?. In the Preface or Chapter 00, usually in the approval letter. In the Preface or Chapter 02, usually in the approval letter. In the Preface or Chapter 30, usually in the approval letter.

What does"non-customized manual" mean?. Generic manual, not tailored to a specific operator. manual, Yes tailored to a specific operator. specific operator.

What type of information does the SRM show?. Damage limits, procedures, materials, fasteners, etc. Damage materials, fasteners. limits, procedures.

Examples secondary structure. Fairings, access panels, minor reinforcements. panels, covers, seats and some accessories. access panels,some accessories.

What is damage according to Chapter 51?. any type of alteration or deterioration of the structure or components of the aircraft. Alteration that affects form, function, or strength. dents and burns to more serious structural damage such as cracks or fractures.

What are the 3 categories of damage. Repairable, 3. Bevond Repair. Allowable, 2. Repairable, 3. Bevond Repair.

Restriction on corrosion removal in titanium. Do not exceed 0.010", avoid microcracks. Fairings, access panels, minor reinforcements. not exceed 0.010", avoid.

Sealants that replace BMS 5-95. PR-1422, CS3204, etc. PR-2422, CS3204, etc. PR-1422, CS32049, etc.

Edge margin values for 05/32" at 0.056. Minimum: 2D-0.312", Maximum: 4D= 0.625. Minimum: 3D-0.312", Maximum: 4D= 0.625. Minimum: 2D-0.312", Maximum: 5D= 0.625.

Aerodynamic classification of external surfaces. Class A, B,Cbased on visibility and function. Class A, B,based . Class D, B,Cbased on visibility and function.

What is Coin Dimpling?. Bending for countersinking in thin sheet metal,. countersinking sheet metal.

What is Countersinking?. holes in thick material. Countersinking holes in thick material.