AA59210D_ContinuationSheet.pdf

AFLC FORM 762, JUL 89 PREVIOUS EDITION WILL BE USED

ENGINEERING DATA LIST DATE 31 Mar 2014 PAGE 1 OF 3

NSN

1740-00-580-7990 1740-01-617-5631

REFERENCE NUMBER

A-A-59210

CAGE & NAME

98752

NOUN

Tractor, Aircraft Towing, MB-4

APPLICATION

Aircraft Towing

TECHNICIAN ENGINEER

Casey Jones

PURCHASE REQUEST

NUMBER

FD2060-14-30626

PREPARING ACTIVITY PHONE

AFLCMC/WNZEB

DSN 472-1671

NOTE: *FURNISH CODES: S-FURNISHED WITH THIS SOLICITATION; M-UNDIMENSION OR STABLE BASE COPY REQUIRED. REFERENCE COPY FURNISHED FOR INFORMATION WORKING COPY TO BE FURNISHED SUCCESSFUL BIDDER. P-PHOTO COPY REQUIRED. R- FURNISHED ON

CONTRACTOR REQUEST WITH PCO APPROVAL; 0-CONTRACTOR MUST ACQUIRE.

DOCUMENT NUMBER NAME CAGE CODE REV

NO. OF

SHEETS

FURN

CODE* REMARKS / NOTE REFERENCE

A-A-59210 98752 D 24 Dated 02/19/2014

REMARKS / NOTES (Continue on AFLC FORM 762A)

A-A-59210D, dated 02/19/2014 shall be amended in accordance with the attached pages.

AMENDMENT

A-A-59210D

19 February 2014

COMMERCIAL ITEM DESCRIPTION

TRACTOR, AIRCRAFT TOWING, MB-4

a. Change the following paragraphs in the document

Item No.

Page Paragraph Subject

Description

1. 7 3.3.2 Storage temperature range

The tow tractor shall be capable of being stored in ambient temperatures ranging from -25 oF, or -65 oF when Winterization A is specified (see 7.2), to 140 °F.

2. 7 3.4 Gross Vehicle Weight (GVW) and dimensions

Overall weight and dimensions in air transport configuration (see 3.5.1.4) shall not exceed:

Axle weight 13,000 pounds.

Length 200.00 inches, without couplers.

Width 100.00 inches, without mirrors.

Height 100.00 inches.

3. 7 3.5.1 Air transportability

The tow tractor shall be transportable on C-130, C- 17, and C-5 aircraft in accordance with MIL-STD- 1791. In all air transport configurations, the tow tractor shall be capable of being restrained and withstanding, without loss of serviceability, 2.0 G up and 4.5 G down accelerations, and shall be capable of being restrained and withstanding, without loss of structural integrity, 3.0 G forward, 1.5 G aft, and 1.5 G lateral accelerations. The tow tractor shall be equipped with pressure relief devices or configured for air transport to prevent any part from becoming a projectile in the event of catastrophic loss of aircraft cabin pressure. The tow tractor shall drive on and off the aircraft, negotiating the required maximum ramp angles, without the use of shoring if possible.

4. 19 5.5.11 Coupler analysis

A strength analysis report shall be submitted to the Government representative at pre-production verification that contains supporting calculations to show that the front and rear coupler mounting structures are in compliance with the respective strength specifications of 3.6.7. The analysis shall include methodology leading to the arrival of values for static and dynamic loading, and ultimately the design load. Additionally, the rear coupler mounting structure calculations shall be supplemented with a Finite Element Analysis (FEA) to further support compliance with the strength specification.

5. 22 7.2 Ordering data

Acquisition documents should specify the following:

a. Title, number, and date of this CID.

b. Finish color required (Dark Green or Desert Sand) (see 3.2.1.2).

c. Temporary CPC (see 3.2.1.4)

AMENDMENT

A-A-59210D

19 February 2014

d. Winterization A (see 3.3.1)

e. Packaging requirements (see 6.0)

b. Remove the following paragraphs in the document

Item No.

Page Paragraph Subject Description

1. 13 3.11 Diagnostic software

When specified (see 7.2), a copy of any diagnostic software on CD-ROM or DVD-ROM, and/or an accessory module, required or recommended for maintaining the tow tractor shall be provided.