AIR FORCE A-A-59110-1997 LEAK DETECTOR FUEL SYSTEM [Superseded AIR FORCE MIL-L-83774 A CANC NOTICE 1 AIR FORCE MIL-L-83774 A AIR FORCE MIL-L-83774 REINST NOTICE 2 AIR FORCE MIL-L-8.pdf
《AIR FORCE A-A-59110-1997 LEAK DETECTOR FUEL SYSTEM [Superseded AIR FORCE MIL-L-83774 A CANC NOTICE 1 AIR FORCE MIL-L-83774 A AIR FORCE MIL-L-83774 REINST NOTICE 2 AIR FORCE MIL-L-8.pdf》由会员分享,可在线阅读,更多相关《AIR FORCE A-A-59110-1997 LEAK DETECTOR FUEL SYSTEM [Superseded AIR FORCE MIL-L-83774 A CANC NOTICE 1 AIR FORCE MIL-L-83774 A AIR FORCE MIL-L-83774 REINST NOTICE 2 AIR FORCE MIL-L-8.pdf(5页珍藏版)》请在麦多课文档分享上搜索。
1、- A-A-59110 9999974 0175117 TO5 A-A-591 10 02 July 1997 SUPERSEDING MIL-L-83 774A(USAF) 05 April 1989 COMMERCIAL ITEM DESCRIPTION LEAK DETECTOR, FUEL SYSTEM The General Services Administration has authorized the use of this commercial item description as a replacement for MIL -L- 83774 for all feder
2、al agencies. 1. SCOPE. 1.1 General. This Commercial Item Description (CID) describes an explosion-proof leak detector for locating fuel leaks in aircraft fuel cells and tanks using helium, argon, or nitrous oxide as a tracer media. Beneficial comments (recommendations, additions, deletions) and any
3、pertinent data which may be of use in improving this document should be addressed to: (SA-ALC/TILDD, 485 Quentin Roosevelt Rd, Kelly AFB TX 78241) by using the Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. AMSC N/A FSC 4940 D TA E A.
4、 Approved for public release; distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-A-A-59 1 1 O 2. SALIENT CHARACTERISTICS. 2.1 Design. The leak detector shall weigh no more than 25 pounds and shall be operable by one man. The p
5、ower supply shall be capable of operating the sensing unit a minimum of 4 hours without recharging. The leak detector will be explosion proof for operation in an invironment defined by the National Electrical Code, NFPA 70, as class I, division I, group D. The leak detector will be safe for use in a
6、n explosive atmosphere at 8000 feet altitude and 125 degrees Fahrenheit. The leak detector may be enclosed in one or two housings. The weight of the hand held unit for leak searching shall not exceed 8 pounds. The dimensions of the housing shall not exceed 6 inches wide by 12 inches long by 10 inche
7、s deep. If two seperate housings are utilized, the connecting cord shall be 8 feet in length with provisions for extending the working distance an additional 8 feet. The housings shall incorporate one common static electricity grounding point. A retractable (coiled) cable and spring clip shall be at
8、tached to that ground point for grounding to the aircraft. The cable retracted length shall be 12 inches. The extended length shall be 6 feet. The leak detector shall be funiished complete with all items and accessories required for proper operation. A meter as well as audio and light indicators sha
9、ll be the means by which leaks are indicated. The sampling probe shall be flexible, semi-rigid, non-kinking, with a minimum length of 12 inches. A Carrying Case shall be supplied with the leak detector to provide for storage and ease of transportation. 2.2 Compa Char acteristicq. 2.2.1 Sensing ufll
10、t. The sensing unit shall be capable of detecting the following gasses at the specified leak rate when tested in accordance with paragraph 4.4.2: Helium 1 X 10” cubic centimeter per second Argon 4 X cubic centimeter per second Nitrous Oxide 4 X 10” cubic centimeter per second 2.2.2 Respons e time. W
11、hen utilizing the sampling probe, the sensing unit full scale deflection response time to a 1 X 10” cubic centimeter per second helium leak shall not exceed one second. 2.2.3 Recovery h. When removed fiom a leak source, the sensing unit recovery time (meter return to 10 percent of fll scale) shall n
12、ot exceed 3 seconds. 2.2.4 11s . The sensing unit shall be capable of detecting a 5 percent by volume concentration of any of the tracer gases when operating in an atmosphere containing a minimum of 0.4 percent by volume concentration of JP-8 fuel vapor. 2 Provided by IHSNot for ResaleNo reproductio
13、n or networking permitted without license from IHS-,-,-A-A-59 1 1 O 2.2.5 R anne canability . The sensing unit shall be capable of locating a leak of 1 cubic centimeter per second helium and a leak of 1 X cubic centimeters per second helium when the leaks are 4 inches apart horizontally. There shall
14、 be evidence that two seperate leaks have been located. This shall be accomplished in still air without utilizing range swiches, zero adjustment, or other controls. 2.2.6 Power suply. The power supply shall be an internal power source capable of operating the leak detector for periods of 4 hours con
15、tinuously and shall be rechargeable. Batteries shall be capable of a minimum of 500 recharging cycles om the voltage cut-off depth of discharge to a fully charged condition. The power supply shall be capable of preventing erroneous readings or indications due to low voltage. The power supply shall i
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