Attachment 1 Salient Characteristics CDDAR Slings.pdf

67 KB Posted

Attached to
EAFB CDDAR Slings
Solicitation number
FA469024Q0072
Issued by

About this file

Written by GovTribe AI ·

This document is the Salient Characteristics for the CDDAR Slings requirement under Solicitation FA469024Q0072 issued by the Department of the Air Force Air Combat Command.

The key details are that the Government is seeking 8 aircraft synthetic webbing slings with the following specifications: Type II with documented load tests at 2 times the rated capacity, 16 inches wide, 330 inches long, made of webbed nylon or synthetic polyester, with a minimum vertical load capacity of 45,000 pounds and minimum basket load capacity of 99,000 pounds. This is a 100% Small Business set-aside under NAICS code 332618 with a size standard of 500 employees. Quotes are due by 13 September 2024 at 12:00pm MDT and should be submitted to matthew.cotton.1@us.af.mil with the subject "Quote FA469024Q0072 - Solicitation - CDDAR Slings". The award will be made on the criteria established in the solicitation.

View the file

Other files

File Type Posted
CDDAR Slings Questions and Answers.pdf PDF
Solicitation Amendment FA469024Q00720001 SF 30.pdf PDF
Attachment 2 - CDDAR Engineer Drawing.pdf PDF
Solicitation - FA469024Q0072.pdf PDF

On GovTribe

Work with this file

  • Download the original file
  • Contacts named in this file
  • Similar government files
  • Ask GovTribe AI about this file
Try for free Login

Text version

The file's text, extracted by GovTribe without its formatting.

Salient of Characteristics

Below are the characteristics that Crash Recovery needs for aircraft synthetic webbing slings.

1. Type II

2. Must have a load test documented for each sling:

o Email or hard copy of load tests o 2 times their rated capacity o metric in pounds

3. Width: 16 inches

4. Length: 330 inches

5. Material: Webbed Nylon or synthetic polyester

6. Quantity:8

7. Vertical load Capacity:

o Minimum:45,000 pounds o Maximum: no max

8. Backet Load Capacity:

o Minimum: 99,000 pounds o Maximum: no max

Explanations

1. Type II- Triangle fitting on both ends-engineer specifications

2. Load test document- requirement from ASME B30.9-2018 Chapter 9-5.6

3. Width- engineer specifications

4. Length- engineer specifications

5. Material- prevent additional damage during recovery operations TO:00-80C-1

6. Load capacities: per engineer specifications those are the minimums. There is no max according to the engineer drawing

File details come from the government source that posted it. Updated .