1、tlIL-E-6057A 28 m 7777706 0385337 3 m MIL-E- 6059A 25 FEBRUARY 1954 Supersed-hg MIGE-6059 29 March 1950 MILITARY SPECIFICATION ENGINES, AIRCRAFi, RECIPROCATING PROCESSES FOR CO.2ROSION PRCYTECTION, PREOIUNG AND GROUND OPERBTIOXS OF This specification has been approwd by the Depsrtment of Defense for
2、 use by the Departments of the Amy, the Navy, and tiie Air Force, 1. SCOPE 1.1 This specification covers the requirements for the prevention of corrosion, preoiling, and ground operation of aircraft reciprocating engines. d 2. APFLiCABIE DOCUMENTS I 2.1 The fallowing specifications and drawings, of
3、the issue in effect on date of invitation for bids, form a part of this specification: SPECIFICATIONS Federal I P441 Solvent; Dry4eaning MI GA-6 091 MIL-B-131 MIM- Water Vaporproof, Flexible Containers; Shipping, Beusable, Wood, Aircraft Engine Container; Shipping, Reusable, Metal, Aircraft Engine C
4、orrosion-Preventive Canpound, kixcrzft Engine Dssiccants (Activated) in Bags; for Static Dehumidification and Packaging Ethylene Glycol; Non-Corrosive , (Anti-beze and Cooling Liquid for Aimraft Engines) Engines, Aircraft Reciprocating, Preparation for Shippent and Stoage of Fuel; Aircraft Reciproca
5、ting Engh Light Assembly, Cyinder Inspection, Bortscop Style Lubricating Grease; High Temperature Oil, Lubricating, Jet Engine Lubricating Oil, General Purpose, Luw Lubricating Oil; Aircraft, Engine Rubber; Synthetic, Sheet, Molded, and Extruded, Temp rature s for Aircraft AppUcations Provided by IH
6、SNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-IL2 L-E -6 2 59A JAN -F-l27 Packaging and Packing for hrseas Ship-ent - Tap, Adhesive, PressureSensitive, Water Resistant DRAWEKS Air Force-Navy Aeronautical AN4060 A.N.4061 AN4062 AN4064 ANWO7 Protector - Ignition C
7、able Plug - Crankcaee Dehgdrator plugs No. Seating torque Ib in. 45 45 45 (to noma 25 18 engagenient ) 4.2 4.2.1 Inspection of engines.- Treatment of engines in the piant custodp.- 4.2.1.1 Insmction in Specification MIIrc4li6 and sin.lar containers.- Immediately upon receipt, and at least ewry 28 da
8、m thereafter, the humidity indicator shail be inspected by canparison -s or pinhcles. band of protective paper shall be removed. around the engine, and the dehydrator plugs shall be rewved. in the envelope shall be repaired. The The her The bags of dehydrating agent secured ltb revdutions while spra
9、s6ng each cylinder. Each cyIts of Spccification PiitEd058 may be required. periodic insp-or card, anri all nnenals, pwmtion, and pre- oiling shall be entered in er?gine log. apyropriate mction of the log. 4.2.5 Enaine ncord entries.- A complete record o? all inspdions, includir board, if attached to
10、 the enkine, shall be reroveti, and t!x acccssories shall be handled as indicated hereinafter. If no accessories mounting board has ken used, the pachged iccessories shall be rtmoved from the shipirig contaicer. After rwoving the shipping bolt nuts, the enpine sliall be renoved fro= bosh the shippin
11、e bcx and frm the envelope. The emelope shall than be .eIof?d, cleaced, and carefull:; foldad for subsequent mm or meclamation according to GovemzsrA directivps. shall he mounted on tim stand. asssmhled with all engine attachment parts, gaskets, closure bolts, etcb Offs, cavem, seals, and screws, th
12、at am in usable confition, shall be held as Oovernment property awaiting disposition. released and tip container top removed. care to prevent the engine fiom striIciry the mounting plate or side rails, w.d placed on a stand. Shall be removed from the engine and placed in the container. Any unmounted
13、 acces- sories shipped with the engine shall be installed on the engine. If the container is not to be remd immediately, the top shall be installed ZIi the empty container. The container skall be cleaned and complptely assembled with all erigine attachnt parts, gaskets, closure bolts, etc. Ali blank
14、 Offs, covers, seals, and screws that are in usable conrlition shall be held as Govermmnt property awaiting disposition. Cylinder treatment.- As soon as pssible after the dehydration seals on the engine are hroken and not later t!-m 24 hours thereafter, all cylinders sh3ll be sprayPd internally 4th
15、internal engice corrosion-pantive aiixture throu+ller shaft, pushiiig the cone against the grease and rotating against the thrust nut and about the shaft to displace as much of the grease as possible from the rear mating surfaces. on the cone and exposed p0rtior.s of the thrust nut shall be wiped of
16、f. mating surfaczs of the rear cone shall be cleaned and dried and the propeller in- stalled and tightened to the proper torque. The shaft shall be cleaned to remove traces of corrosion and polishing The thrust nut shallbe reinstalled a;ld tightened to proper torque. With the rear cone in place, all
17、 excess grease remining The hub seat 4.4.3 Preservation mintenafice,- The dehydrator plugs and the bagged dehy- drating agent in the inkah and exhaust systems shall be replaced when a relative hmidity above 20 percent (unsafe) is indlczted. Cylinders shall be =sprayed with internal engine corrosion-
18、preventive mixture at this the, in accordance mith pra- graph 4.2.3. When necessary, any one cylinder dehydrator plug of each cylinder may bc? removed and spark plugs installed to permit installation of cowling. 4.5 Preparatjon of engine for initial ground runup.- 4.5.1 Remoi-a1 of dehydrating agent
19、 and corrosion-preventive s.- 811 breather openings shall be adequately sealed against oil and moisture with suitable covers such as materiala conforming to Specification EIIrB-l3l and secmd with materiale conforming to SpecFfication Fuel lines.- The fuel lines of the airplanes fuel system shall be
20、4.8.12 Water injection equiFment.- When the water injection equipent is mer draining as much water a8 practical oub of the regulator JAN-P-127 4.8.U khydrating engine and exhaust.ports,- A rewr.tiw zixtre in the lubricating system, internal engine corrosion-preventive zixture ir. a,. a-.mxt sriffici
21、ent to insu-e adequate lubrication durir,g successiire ri-q shali be added. 4.9.2.2 men it is not known that the a-rplane has irtemd snginx! corr3sion- pre;i?r.tive mixture in the system, the following procedure sholl be follovi: (a) The oil tank and engine sun? shall be drzkned. (b) Drain plugs sha
22、ll be replaced and safety Hired. (c) The oil tank shall be filled with internal enghe corm- sion-preservative mixbure to the level necessary to provid5 adequate lubrication during the pesemtior, runups. (d) A tag shall be placed on the instrument pnel .static4 that internal engine corrosion-pevextiv
23、e m-L the idle cutoff position. (c) At completior! of shutdmn, the cylinders shll be tnated in accordance with paragraph 4.2.3. 17 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-E-b57A 28 777770b Oll35356 3 4.9.5 Coolant s Ttm coolant system (hc
24、ludSng after-cookt system if present), sha /O- be kept entirely full of coolant of the type (conceztratfor.) prescribed for the partic:*,“O b-eed no depreservation. If it is desired to represem the engine after 30 dayc idleness, the semation.- For restricted flight operations, erGines prepared 4.10
25、4.10.1 Preparation of engines for flyaway delivsry.- Mixture already in system.- When the aircraft has irkernal er.gLm corrosion-preventive mixture in the system, the engine shall be opsratsd on cerro- sion-preventiqe mixture and engine oil added as necessary. corrosiong-ewntive mixture in the syste
26、m, the oil tank and the eqir.e shall be drained and the systen shall be refilled with internal engine corrosioa-preventive mixture. 4.10.2 Mixture not in system.- When the airplanes do not ha= htsrrial engine 4.10.3 Placard a?d log books.- An appropriate entry shall be nade in t:le log book concerni
27、.ig the method of presermtion, the name of the activitr, and the date. This information shall be duplicated on a placard which shall be placed in a prominent position in the pilots cockpit. 4.lO.4 Depresemtion.- Engines need no dopresemtior 4.11 Inspection.- 4.ll.l Tho processss for !nnJling epgines
28、 arad all materiaals entarkg kts the 4.U.l.l Tie tenu “3owrrnsnt Ins:sctorll refers to 1- 3. S. Force %pa- procedure thereor s!-alJ. bz subject to inspecti0.i by Government Icsrocclors. asntative doaigazkd by tiis Ins+ction Ssstion, Air Yateriel Cox=r.S, sr to tke Bueau of Aeronautics R-przsentative
29、 , as apFli3ablS. or in part for final detemination of cornpliance with the specificatizn. 4.11.2 The procuring activity reserves the right to c$r.:r.duct %,sets ir. rrkole Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-li.12 Effectiveness of equime
30、nt na j I*-E6058. 5.2 Sq.tptrseirq da+Ya.- This specification supersdes S?eclfication MIL-E- 6059 which specificaticn incorporated the requirenents o? Sp2.fication hbE-9. 5.2 A list of the ecdlpxent nececsary for cornpliance kist, the instructions contained herein, nay be o5tained upon applicztion t
31、o eitkeer . S. Air Force, Air Hateriei Co?rand, i;righ+-Patteruon Ai:, Fwce Sase, Ohio, ir =O the Bureau of Aeronautics, Xavy Depart.ner,t, :askington 25, D. C. shipping plates, accessory tirive covers, etc, removed fre ezgines ; inicator car%, wine envelopes, PATENT NOTICZ: k%en Govern?eTlt raijing
32、s, specifications, or other data are ase6 for aw prpose other t5an in con- nection with a definitely related Government procurement operation, the United States Government therep burs no responsibilitr nor any obligation whatsoever; d the fact that the Government !cay have fodated, furnished, or in
33、any way supplied the said drawings, spec2fizat:ons, or other data is not to be regarded by implication or otnervise as n any manner Ucensing the holder 6z a3y other person or corporation, or conveylng any rigkts or pemission to mufacture, use, or sell any pa*&nted invention that may in way be related thereto. Custodians: - Transportation Orps Navy - Bureau of Aeronautics Air Force 19 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
