1/21/2014

Applicant’s Name

STRUCTURAL

See FAA Order 8110.37, Appendix B, Chart A

DER APPLICATION EVALUATION TECHNICAL CRITERIA

Delegated Functions andAuthorized Areas

 Applicant indicates requested area(s) of delegation andattaches supporting data to establish technical expertise andexperience.

 Advisor (Adv) evaluates requested area(s), recommends area(s) to evaluation panel (EP) (Y=YES; N=NO), andprovides rationale.

 Evaluation panel evaluates area(s) recommended by advisor, marks EP column (Y=YES; N=NO), andprovides rationale.

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1/21/2014

DER APPLICANT USE ONLY / FAA USE ONLY
Requested Areas / STATIC ANALYSIS / Adv / EP
1AStructures - General (1)
1BWing Group
1CFuselage Group
1DEmpennage Group
1ELanding Gear
1FFlight Controls
1GRotor
1PStructures Special (Specify)
Requested Areas / DYNAMIC ANALYSIS / Adv / EP
2AStructures - General (1)
2ELanding Gear
2GRotor
2PStructures Special (Specify)
Requested Areas / FATIGUE ANALYSIS / Adv / EP
3AStructures - General (1)
3BWing Group
3CFuselage Group
3DEmpennage Group
3ELanding Gear
3GRotor
3PStructures Special (Specify)
Requested Areas / DESIGN ANDCONSTRUCTION / Adv / EP
4AStructures - General (1)
4BWing Group
4CFuselage Group
4DEmpennage Group
4ELanding Gear
4FFlight Controls
4GRotor
4KInterior Arrangements
4LInterior Materials
4MFire Protection
4NEvacuation Systems
4ODoor Systems
4PStructures Special (Specify)
DER APPLICANT USE ONLY / FAA USE ONLY
Requested Areas / FLUTTER/GROUND VIBRATION / Adv / EP
5AStructures - General (1)
5GRotor
5PStructures Special (Specify)
Requested Areas / SAFETY ANALYSIS / Adv / EP
6AStructures - General (1)
6ELanding Gear
6FFlight Controls
6MFire Protection
6NEvacuation Systems
6ODoor Systems
6PSpecial (Specify)
Requested Areas / FLOTATION ANDDITCHING ANALYSIS / Adv / EP
7AStructures - General (1)
7PSpecial (Specify)
Requested Areas / STRUCTURAL LOADING LIMITATIONS / Adv / EP
8HLoading Control Documents
8PSpecial (Specify)
Requested Areas / SERVICE DOCUMENTS / Adv / EP
9AStructures - General (1)
9BWing Group
9CFuselage Group
9DEmpennage Group
9ELanding Gear
9FFlight Controls
9GRotor
9KInterior Arrangements
9LInterior Materials
9MFire Protection
9NEvacuation System
9ODoor Systems
9PStructures Special (Specify)

1

1/21/2014

Applicant’s Name

STRUCTURAL

See FAA Order 8110.37, Appendix B, Chart A

DER APPLICANT USE ONLY / FAA USE ONLY
Requested Areas / MATERIAL ANDPROCESS SPECIFICATIONS / Adv / EP
10IMetallic Materials
10JNonmetallic Materials
10PStructures Special (Specify)
Requested Areas / FLAMMABILITY / Adv / EP
11LInterior Materials
11MFire Protection
11PSpecial (Specify)
Requested Areas / DAMAGE TOLERANCE EVALUATIONS / Adv / EP
12AStructural - General (1)
12GRotor
12PSpecial (Specify)

Note: The general category in the structures chart embraces all airframe articles such as wing, fuselage, empennage, landing gear, flight controls, engine mounts, andspecial articles, but does not apply to rotors.

Additional Requirements for a Delegated Function of Damage Tolerance Evaluation:

(a) Education

Circle One

YesNo1. A degree in Engineering Mechanics

YesNo2. A degree in Aerospace/Aeronautical Engineering

YesNo3. A degree in Mechanical Engineering

YesNo4. A degree in Civil Engineering

YesNo5. In addition to one of the above, a course in fractures mechanics is desirable, if not taken during the degree program

(b) Experience -

Circle One

YesNo1. 24 to 36 months of experience in airframe stress analysis

YesNo2. 36 to 60 months continuous experience in damage tolerance analysis, performing as the principal investigator andresponsible for results andconclusions for at least 2 of those years

Additional Requirements for a Delegated Function of Fatigue Analysis:

(a) Education

Circle One

YesNo1. A degree in Engineering Mechanics

YesNo2. A degree in Aerospace/Aeronautical Engineering

YesNo3. A degree in Mechanical Engineering

YesNo4. A degree in Civil Engineering

YesNo5. In addition to one of the above, a course in fatigue analysis is desirable, if not taken during the degree program

(b) Experience

Circle One

YesNo1. The equivalent of 2 full years of experience in fatigue analysis. This experience must be within the last 120 months before appointment.

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