Adhesives
Stabilator Repairs
Vacuum Bag and Cure Procedures
General Composites
Advanced Composites
100

If no technical data is present, how much resin is required for each square foot of dry fabric?

25 grams

REFRENCE: TM 1-1500-204-23-11, page 6-48, paragraph 6-17. c. (2).

100

How much resistance is required to verify continuity in an EMI repair.

1 OHM or less 

REFERENCE: TM 1-1520-280-23&P, EMI Shielding / Lightning Strike Protection

(Copper Mesh), step 7.

100

What is the minimum permissible vacuum for composite repairs?

20inches Hg

REFERENCE: TM 1-1500-280-23&P Vacuum Bag and Cure Procedure

100

  What is acute toxicity?

The harmful effect of a material after a single or short-term exposure.

REFERENCE: TM 1-1500-204-23-11, page 2-2, paragraph 2-3. a. (1).

100

What are the three types of moisture damage?

Bond line voids, laminate blistering, and skin to core disbond.

REFERENCE: TM 1-1500-204-23-11, page 6-12, para. 6-6. b.  

200

What is the mix ratio for EA 956?

100:58

REFERENCE: TM 1-1500-204-23-11, page 6-49, Figure 6-29, Example 2.

200

What is the maximum cleaned up diameter of removed core in Zone H?

Cleaned up damage of removed core NTE 3 inches diameter. 

REFERENCE: TM 1-1520-280-23&P AIRFRAME MAINTENANCE PROCEDURES/MAINTENANCE PROCEDURES/AIRFRAME/STABILATOR/Stabilator Inspections, Table 1. General Repair Criteria - Composite Stabilator Repair.

200

Where are vacuum pucks placed?

Opposite ends of the 4 ounce non-woven breather cloth

TM 1-1500-280-23&P Vacuum Bag and Bleeder Schedule  

200

What is a cold zone?

The area within 2 inches of the edge of any heat blanket which is unreliable for achieving and maintaining the proper cure temperature.

REFERENCE: EM 0284, TM 1-1520-280-23&P AIRFRAME MAINTENANCE

PROCEDURES/MAINTENANCE PROCEDURES/AIRFRAME/AIRFRAME REPAIR

PROCEDURES/Outboard Stabilator Composite Structure Repair - Vacuum Bag and Cure Procedures

OR 1-1500-204-23-11 CH6 par6-18c(2)

 

200

What are the disadvantages of the external bond patch?

Creates eccentric load path caused by offset of the neutral axes of the part and the patch which can cause interlaminar failure of the part or the patch and premature failure of the adhesive. 

REFERENCE: TM 1-1500-204-23-11, page 6-28, paragraph 6-15. c. (1).

300

Why is it important to properly mix 2-part adhesives?

Using incorrect mix ratios will reduce the strength of adhesive and may result in loss of structural integrity.

REFERENCE: TM 1-1520-280-23&P, Airframe Maint Procedures/Maint Procedures/Airframe/Airframe Repair Procedures/Outboard Stabilator Composite Structure

300

How many repair plies are used to repair the far-side laminate and in which direction are they oriented?

2 Plies oriented at ±45 IML* 

REFERENCE: TM 1-1520-280-23&P AIRFRAME MAINTENANCE PROCEDURES/MAINTENANCE PROCEDURES/AIRFRAME/AIRFRAME REPAIR PROCEDURES/Outboard Stabilator Composite Structure Repair - Composite Skin Repair/FARSIDE

LAMINATE REPAIRS, Table 2.

300

What is the bleeder schedule for Liquid Removal?

Steel Screen, 4oz Non-Woven Breather, Heat Blanket, 4oz Non-Woven Breather, Vacuum Bagging Film

REFERENCE: TM 1-1500-280-23&P Vacuum Bagging and Cure Procedures  

300

What is "Wet Lay-up"?

A process in which dry woven cloth is impregnated with a liquid adhesive and then cured to form a laminate. 

REFERENCE: TM 1-1500-204-23-11, Pg. 6-39, PARA 6-16, PDF 157.

300

What is cross-linking?

A chemical reaction which bonds the molecules of two-part resins together. 

REFERENCE: TM 1-1500-204-23-11, page 4-12, paragraph 4-4. c.

400

What is the cure cycle for 1652 using an elevated temperature cure?

Gel at room temperature for 1 hour followed by an elevated temperature cure at 150°F for 2-3 hours.

REFERENCE: TM 1-1520-280-23&P AIRFRAME MAINTENANCE PROCEDURES/MAINTENANCE PROCEDURES/AIRFRAME/AIRFRAME REPAIR PROCEDURES/Outboard Stabilator Composite Structure Repair - Core Repair/CORE POTTING PROCEDURE, Step 4.b.(2)(a) and Table 1


400

What is the repair limit for Partial Thickness damage, Deep Scratches, Gouges and Cracks?

Up to Full Skin Depth Zone B, C, D - 6 inch diameter or less. NTE 0.015 inches deep.

TM 1-1500-280-23&P Stabilator Inspections Table 1

400

Where should thermocouples be placed?

1 inch from the edge of the repair area

REFERENCE: TM 1-1500-280-23&P Composite Skin Repair  

400

What features should a composite fastener have?

Non-hole filling, large footprint, limited torque, limited or adjustable

clamping force.

REFERENCE: TM 1-1500-204-23-11, PG, PG 3-14, para 3-46, PDF 48.

400

What is the most practical cutout shape for damage removal?

A Circle

REFERENCE: TM 1-1500-204-23-11, page 6-3, para. 6-4.

500

To mix a total of 50 grams of EA 956, how much of Part A and Part B is required?

32 grams of Part A and 18 grams of Part B.

REFERENCE: TM 1-1500-204-23-11, page 6-49, Figure 6-29, Example 2.  

500

How will wire mesh material be removed when repairing near side laminate?

0.25 inch larger than the largest repair ply using scouring pad. 

TM 1-1500-280-23&P Remove Paint and Electromagnetic Interference (EMI) Protection

500

What is the cure cycle for EA 9396 at room temperature?

5 days

TM 1-1500-280-23&P Vacuum Bag and Cure Procedures

500

What is the formula for calculating the resistance of a heat blanket?

R = V2 ÷ W, where V is voltage and W is watts.

REFERENCE: TM 1-1500-204-23-11, page 3-4, paragraph 3-3 h. (3).  

500

The warp clock measures positive angles in what direction?

Counterclockwise

REFERENCE: TM 1-1500-204-23-11, PDF 114.