MIL-S-6551A(USAF)
3.9 Nameplate. A nameplate, permanently and legibly filled in with the following information, shall be securely attached to the inner right side of seat bucket in a location capable of being read after the seat is installed:
Seat, Crew, Downward Ejection, Aircraft Type (Insert Applicable Type) Specification No MIL-S-655l(USAF)
Mfr's Part No -------------------------
0 rd er No ----------------------------�
Mfr's Nam_e o_r T_r_a_d_em a_r�k--------------�
US Property
3.9.1 Manufacturer's Part No. The manufacturer's part number marked in the space provided in the name plate shall be identical with the manu• facturer's engineering production drawing number, including applicable dash numbers, if the drawing is tabulated and covers more than one part.
3.9.2 Order No. Where both the order number such as "F33657-78-C-7410-0003" and the contract number, such as "F33657-78-C-7410" are given on an order
or contract, the number placed on the nameplate in the place designated "Order No" shall be the number corresponding to the Air Force order number, for example, "F33657-78-C-7410-0003."
3.9.3 Stock No. The stock number entered in the space provided on the name• plate shall be as specified by the Procuring Agency. The stock number shall include the name or standard abbreviation of the name of the service having jurisdiction of the equipment.
3.10 Workmanship. Workmanship and finish on all parts shall be in accor• dance with high grade manufacturing practice covering this class of equip• ment.
3.11 Cleaning. All parts shall be clean and free from dirt, sand, metal chips or foreign matter, while being assembled.
3.12 Lubrication. Lubrication used shall conform to the requirements of Specification MIL-STD-838. Lubrication shall function satisfactorily within the temperature range of minus 65 degrees and plus 160 degrees Fahrenheit.
* 4. QUALITY ASSURANCE PROVISIONS
4.1 Classification of tests. The inspection and testing of the seats shall be classified as follows:
a. Acceptance tests • See 4.2 b. Preproduction testing. • See 4.5
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