ARMY MIL-T-48297-1974 TEST SET ASSEMBLY DISPENSER CONTROL PANEL FOR M56 AIRCRAFT SUBSYSTEM《M56型航行器系统的分配器控制板测试装置组装》.pdf

1、s.3747 MIL-T-48297 (PA) 7 7ebrcary i974 MILITARY SPECIFICATION TEST SET ASSEMBLY, DISPENSER CONTROL PANEL FOR M56 AIRCRAFT SUBSYSTEM This specification is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 This specification covers the inspections and tests f

2、or a test set used to test aircraft panel controls for the M56 Aircraft Subsystem. 2. APPLICABLE DOCUMENTS 2.1 The following documents of the issue in effect on date of invitation for bids or request for proposals, form a part of this specification to the extent specified herein. SPECIFICATIONS MI L

3、I TA RY MIL-A- 2550 - Ammunition, General Specification for STANDARDS MILITARY MIL-STD-105 - Sampling Procedures and Tables for MIL-STD-109 MIL-STD-1168 MIL-STD-1235 - Single and Multilevel Continuous Inspection by Attributes - Quality Assurance Terms and Definitions - Lot Numbering of Ammunition Sa

4、mpling Procedures and Tables for Inspection by Attributes THIS DOCUMENT CONTAINS aJ PAGES. , O Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- MIL-T-Y277 33 777770b 0338597 5 MIL-T-48297 (PA) DRAWINGS U.S. ARMY PICATINNY ARSENAL PRODUCT AND PACKAGIN

5、G DRAWINGS 9280143 - Dispenser Control Panel Test Set Assembly 9280144 - Cable, Test, Control Panel 9280145 - Bench Power Cord 9287748 - Packing and Marking for Drum, Metal, Shipping for Test Set Dispenser Control Panel. (Copies of specifications, standards, and drawings required by suppliers in con

6、nection with specific procurement functions should be obtained from the procuring activity or as directed by the Contracting Officer). 3 REQUIREMENTS 3.1 Material. - Materials shall be in accordance with the applicable drawings and specifications. 3.2 Assembly. - The assembly shall comply with all r

7、equire- ments specified on Drawing (dwg.) 9280143 and with all require- ments specified in applicable specifications. 3.3 Control Panel, Test Cable 3.3.1 Continuity. - The maximum resistance between all wired corresponding pins on the connectors shall be one hundred (100) milliohms. 3.3.2 Insulation

8、 Resistance. - The maximum leakage current between all pins and the shell shall be two (2) microamperes when measured at five hundred plus fifty (500 + 50) volts direct current (V.D.C.) for a minimum time of ten (10) seconds. 3.4 Bench Power Cord 3.4.1 Continuity. - The maximum resistance between th

9、e two connectors shallbe one hundred (LOO) milliohms. 3.4.2 Insulation Resistance. - The maximum-leakage current between the pins and the shell shall be two (2) microamperes when 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-48297 (PA) meas

10、ured at five hundred plus fifty (500 + 50) V.D.C., for a minimum time of ten (10) seconds. 3.5 Input Power Circuit Functioning. - The “EXTERNAL POWER“ pilot light shall lightup when twenty eight plus or minus one volt direct current (28.0 + 1.0 V.D.C.) is applied to connector !EXTERNAL POIJER“ (J3)

11、with-the “EXTERNAL POWER“ (S1) switch in the “QN1 position. The plus twenty eight (+28) V.D.C. shall be applied to pin number riAr of 53 and the input ground shall be connected to pin number “Btl of J3. This twenty eight (28) V.D.C. input shall be present within one tenth (0.1) V.D.C. at the “PANEL

12、TEST“ (J4) Socket between pins ID and MI1, “K and M“ and “N and MIt. Pin “M“ shall be the ground reference. 3.6 “EXTERNAL POWER“ Pilot Light Manual Functioning. - The “EXTERNAL POWER pilot light shall function after twenty eight plus or minus one (28.0 2 1.0) V.D.C. is applied as in 3.5 to connector

13、 “EXTERNAL POWER“, 53 and the “PRESS TO TEST“ switch of DS3 is pressed downward and held for a minimum of ten (10) seconds. POWER“ pilot light shall function when twenty eight plus or minus one (28.0 + 1.0) V.D.C. is applied as in 3.5 to connector “EXTERNAL POWER“ (J3T and the IPRESS TO TEST“ switch

14、 of “LEFT JETTISON POWER1 while (DSI) is pressed downward and held for a minimum of ten (10) seconds . 3.7 Left Jettison Power Manual Switch. - The “LEFT JETTISON 3.8 Left Jettison Power Function - The “LEFT JETTISON POWER“ pilot light shall function when twenty eight plus or minus one V.D.C. (28.0

15、+ 1.0) is applied to connector J4, PANEL TEST“, Pin “JI shall be the plus voltage reference and pin lrM1 shall be at ground potential. This twenty eight (28) V.D.C. input shall be present within one tenth (0.1) V.D.C. at connector J1, “LEFT JETT- ISON POWER“ with pin “A“ used as the plus voltage ref

16、erence. 3.9 Right Jettison Power Manual Switch. - The “RIGHT JETTISON POWER“ pilot light shall function when twenty eight plus or minus one (28.0 + 1.0) V.D.C. is applied as in 3.5 to connector “EXTERNAL POWERtt (33T and the llPRESS TO TEST“ switch of “RIGHT JETTISON POWER1! while (DS2) is pressed d

17、ownward and held for a minimum of ten (10) seconds . 3.10 Right Jettison Power Function - The “RIGHT JETTISON POWER“ pilot light shall function when twenty eight plus or minus one V.D.C. (28.0 1.0) is applied to connector Jh, “PANEL TEST“. 3 O Provided by IHSNot for ResaleNo reproduction or networki

18、ng permitted without license from IHS-,-,-MIL-T-Ll8277 33 W 777990b 03118603 T MIL-T-48297 (PA) Pin “H“ shall be the plus voltage reference and pin rlMvr shall be at ground potential. This twenty eight (28) V.D.C. input shall be present within one tenth (0.1) V.D.C. at connector J6, “RIGHT JETTISON

19、POWER“ with pin “A“ used as the plus voltage reference. 3.11 Empty Test Function - Continuity shall only be present between pin G of connector 54, “PANEL TEST“ and pin “A1! of connector 52, “LEFT DISPENSER“ when switch S2 is in the “EMPTY TEST“ position. Continuity shall only be present between pin

20、iiFti of 54, “PANEL TEST“ and pin “A“ of connector 55, “RIGHT DISPENSER“ when switch S2 is in the “EMPTY TEST“ position. pins “G“ and “U“ of connector 54, “PANEL TEST“ and pin “A“ of connector J2, LEFT DISPENSER“ when switch S2 is in the “TEST“ position. Continuity shall be present between pins “F“

21、and V1 of connector J4, DISPENSER“ when switch S2 is in the “TEST“ position. Continuity shall be present between “PANEL TEST“ and pin of connector 55, “RIGHT 3.12 Left Solenoid Step Aircraft Panel Pulsing. - The test set shall be pulsed through pin “E“ of connector 54, “PANEL TEST“ in accordance wit

22、h Table No. 1. TABLE NO. 1 PULSE INPUTS Pulse Length No. of (Milliseconds) Pulse Height Series Pulses (MS) (Volts) 1 6 25 1: 1.0 26.0 5 1.0 2 10 25 5 1.0 26,O - + 1.0 3 40 25 2 1.0 26.0 - + 1.0 Time Time Between Between Pulses (fils) Series (Sec) 25 5 1.0 25 2 1.0 I 10 5 1 10 $ 1 25 2 1.0 10 2 1 The

23、 pulses shall register on the counter, 141, “LEFT SOLENOID STEP“ in the sequence described in Table No. 1. 3.13 Left Solenoid Step Test Set Panel Pulsing. - The Test Set shall be pulsed through connector 57 and Switch S3 in the “LEFT SOL- ENOID STEP“ position and into Counter M1, “LEFT SOLENOID STEP

24、“. Pul- 4 U I Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-4 8 29 7 (PA) sing shall be in accordance with Table No. 1 of 3.12. The pulses shall be registered on counter M1 in the sequence described in Table No. L. 3.14 Righi; Solenoid Step A

25、ircraft Panel Pulsing. - The test set shall be pulsed through pin IL1 of connector 54, “PANEL TEST“ in accordance with Table No. 2. TABLE NO. 2 PULSE INPUTS Pulse Length Time No. of (Milliseconds) Pulse Height Time Between Between Series Pulses (MS 1 (Volts ) Pulses (MS) Series (sec) 1 6 25 2 1.0 26

26、.0 - + 1,O 25 5 1.0 10 t 1 10 - 4- 1 10 .t 1 - 2 10 25 5 1.0 26.0 - t 1.0 25 - + 1.0 3 40 25 .t - 1.0 26.0 - + 1.0 25 - t 1.0 The pulses shall register on the counter, M2, “RIGHT SOLENOID STEP! in the sequence described in Table No. 2, 3.15 Right Solenoid Step Test Set Panel Pulsing. - The Test Set

27、shall be pulsed through connector 57 and Switch S3 in the “RIGHT SOLENOID STEP“ position and into counter 142, “RIGHT SOLENOID STEP“. Pulsing shall be in accordance with Table No. 2 of 3.14. The pulses shall be registered on counter M2 in the sequence described in Table No. 2. 3.16 Left Canister Fir

28、e Aircraft Panel Pulsing. - The test set shall be pulsed through pin iiP1c of connector J4, “PANEL TEST“ in accordance with Table No. 3 TABLE NO. 3 PULSE INPUTS Pulse Length Time No. of (Milliseconds) Pulse Height Time Between Between Series Pulses (MS) (Volts) Pulses (MS) Serks (Sec) 10 t 1 10 t 1

29、10 t 1 26 - + 1.0 12 2 1.0 - 12 2 1.0 12 2 1.0 - 1 6 12 5 1.0 3 40 12 1.0 - 26 t 1.0 10 12 5 1.0 - 26 + 1.0 2 - 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-HIL-T-Y247 13 W 9999906 031b03 3 = MIL-T-4 8 29 7 (PA ) The pulses shall be registered o

30、n the counter, M3, “LEFT CANISTER FIRE“ in the sequence described in Table No. 3. 3.17 Left Canister Fire Test Set Panel Pulsing. - The test set shall be pulsed through connector J7 and switch S3 In the “LEFT CANISTER FIRE“ position and into counter M3, “LEFT CANISTER FIRE“. Pulsing shall be in acco

31、rdance with Table No. 3 of 3.16. The pulses shall be registered on counter M3 in the sequence described in Table No. 3. 3.18 Right Canister Fire Aircraft Panel Pulsing. - The test set shall be pulsed through pin tiR“ of connector 54, “PANEL TEST“ in accordance with Table No. 4. TABLE NO. 4 PULSE INP

32、UTS Pulse Length Time No. of (Milliseconds) Pulse Height Time Between Between Series Pulses (Ms) (VO 1 t s ) Pulses (Ms) Series (Sec 10 - + 1 12 t 1.0 - 1 6 12 jL 1.0 26 - + 1.0 2 10 12 2 1.0 26 - t 1.0 12 - i- 1.0 10 2 1 3 40 12 +_ 1.0 10 + 1 26 - -k 1.0 12 - + 1.0 - The pulses shall be registered

33、on the counter, 144, “RIGHT CANISTER FIRE“ in the sequence described in Table No. 4. Right Canister Pire Test Set Panel Pulsing. - The test set shall be pulsed through connector J7 and Switch S3 in the “RIGHT CANISTER FIRE“ position and into counter 144, “RIGHT CANISTER FIRE“. Pulsing shall be in ac

34、cordance with Table No. 4 of 3.18. The pulses shall be registered on counter M4 in the sequence described in Table No. 4. 3.19 3.20 Workmanship. - All parts and assemblies shall be fab- ricated and finished in a thorough, workmanlike manner. They shall be free of burrs, chips, sharp edges, cracks, u

35、nblended radii, sur- face defects, dirt, grease, rust, corrosion products, and other 6 o Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-48297 (PA) foreign matter. The cleaning agent or method used shall not be injurious to any part, nor shall

36、the part be contaminated by the cleaning agents. All required markings shall be neat, legible and sharply defined. 3.21 Submission of Results of Contractor-conducted Examinations and Tests. - The contractor shall forward copies of the results as required by the contract. Results shall be submitted w

37、ithin thirty (30) days at the completion of each lot tested (see 6.4). 3.22 First Article Inspection. - This specification makes provisions for first article inspection. Requirement for the sub- mission of first article samples by the contractor shall be as specified in the contract, 4. QUALITY ASSU

38、RANCE PROVISIONS 4.1 Responsibility for Inspection.-Unless otherwise specified in the contract or purchase order, the supplier is responsible for khe performance of all inspection requirements as specified herein. Except as otherwise specified in the contract or order, the supplier may use his own o

39、r any other facilities suitable for the performance of the inspection re- quirements specified herein, unless disapproved by the Govern- ment. The Government reserves the right to perform any of the inspections set forth in the specification where such inspections are deemed necessary to assure supp

40、lies and ser- vices conform to prescribed requirements. Reference shall be made to MIL-STD-109 Go define terms used herein. The provi- sions of MIL-A-2550 shall apply. 4.1.1 Submission of Product.-At the time each completed lot of items deliverable under the contract is submitted to the Government f

41、or acceptance, the contractor shall supply the fol- lowing information accompanied by a certificate which attests that the information provided is correct and applicable to the product being submitted. a. A statement that the lot complies with all of the quality assurance provisions specified in thi

42、s specification. b. Drawing and specification number and date, together with identification and date of changes thereto. c. A statement that all material purchased by the con- tractor meets requirements, when such material is controlled by Government or commercial specifications referenced in any of

43、 the 7 o Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-J MIL-T-48277 33 m 737770b 0338605 7 m MIL-T-48297 (PA) contractual documents, and that certificates of conformance are on file and available for review. d. Number of items in the lot. e. Date

44、submitted. The certificate shall be signed by a responsible agent of the certifying organi zat ion. The Fni t ia1 certificat e submit te d shall be substantiated by evidence of the agents authority to bind his principal. Substantiation of the agents authority will not be required with subsequent cer

45、tificates unless, dur- ing the course of the contract, this authority is vested in another agent of the certifying organization. 4.2 First Article Inspection 4.2.1 Submission.-Prior to the start of regular production the contractor shall submit a first article sample (see 6.1) to a Government; appro

46、ved facility as designated by the contracting officer for evaluation in accordance with the provisions of 4.2.2 and 4.2.3. The first article sample shall consist of five (5) sets of parts and five (5) complete test set assemblies which have been produced by the contractor or furnished by a supplier

47、and which have been manufactured using the same production processes, pro- cedures and equipment which will be used in fulfilling the contract. All parts and materials including packaging and packing shall be obtained from the same source of supply as will be used in regular production. Prior to sub

48、mission, the contractor shall inspect the sample to the degree necessary to assure that it conforms to the requirements of the contract and submit a record of this inspection with the sample, including a certificate of conformance for materials. A sample containing known defects will not be submitte

49、d unless specifi- cally authorized by the Contracting Officer. A first article sample, or portion thereof, as directed by the Contracting Officer, shall also be submitted whenever there is a lapse in production for a period in excess of 90 days or whenever a change occurs in manufacturing process, material used, drawing or spec- ification such as to significantly affect product uniformity as determined by the Government. 4.