~1titeu ~tatez u£ J\merica ~cpartmcut nf W:rauspnrtatinu --JIfcncral j\&iatinu j\nmiuistratinu ~uppI£m£utal «fi~p£ QI£rtifirat£ ./Vt:I'/n&p SA489EA ,giZ~ ceA~aue bMuA3d /~ Aircraft & Rotorcraft Products (ARP), Inc. 2 Middle Cross Road Shoreham, New York 11786-1440 ced~~ //fa/ //Ie c/~ Vb //Ie (fr/l6 r~~~ ft/' //Ie ftClf,rDUtp /'POr.tac/ t:t:'rd //Ie t"t:.inrbdriwM tZ/U'? cu/U".t"dr"o-/M //IePeftp ~ o/u30r;4'erl>{~/'£!~/un~~ //Ie av'r~p//fvlR~/'£!?-a~e~ 0/'{.7't:Y'/ 2/23/6/27~///Ie CivillFederal Aviation .96t:j.fNL&/r"o-/M. @'~Vbat".9~bu)/ -- .-$/l6 ~W;40a/6 ./W;~, .' See Master Eligibility List - Attached ,Arde.' ,A~r~t".. Normal, Utility and Acrobatic category airplanes and helicopters equipped with engines and carburetors as described below. !!!2k:.wPYtU"o-/b 0/'~J"lt'3 ~~ ?33f:znpe: Installation of ARP, Inc. Carburetor Ice Detection System Model 107AP (-12, -24, -R-12, -R-24, -U-12, and -U-24 series) in single and twin engine aircraft and single engine helicopters powered by Continental, Franklin, and Lycoming type engines equipped with Precision Air-Motive (Facet or Marvel-Schebler) MA-2, MA-3, MA-3A, MA-3SPA, MA-4, MA-4-5, MA-4SPA, MA-5, MA-6, MA- 6AA and HA-6 series carburetors, in accordance with ARP, Inc. Installation Kit Parts List PLi 07AP-INST (Rev. B), dated January 31,2002. $t:.in.i/rdro/l~ u/u/ ~/I£?dr"o-/M.. 1. This instrument is approved as optional equipment only and flight operations should not be predicated on its use. It is used as an early warning device for detecting formation of carburetor ice in accordance with ARP, Inc. Flight Manual Supplement 107AP- SUPP (Rev. B), dated December 5, 2002. (See continuation sheets 2-6) ,giZ.;;. ce/,c~'ca/e a/u/ //Ie J'o/"/lO/,cUtp rk/a:, r~d t:4 //Ie tft'Mt:4 ft/' o/yt/'£U,a-e; J.4a~ /'eo,"urF" Vb ~c/ wdr't" Ju/¥'wu~/'6r/. ,ju~/le./l£~rL /'£iN/.kr/ ~/'. a /e/¥7,"r/ffdw/b rk/e t:4 ~//IePt:Dt:46 M/atf6;;kr/ ~ //Ie ,./"6ro,,"Vbt:4/nz/op o/'//Ie ,r.Y;;;rk/d./6ot'izuon ../,grkvu4/nz/w/I/. szra/6 0/' 'o/"/l&'ct:dr"o-/b: November II, 1966 szra/e /'£ibMuer/ : November 21, 1997 szra/6 0/' bMU.-tZ/bce: April 28, 1967 ~ szra/6 t:Yn£!/l£h.t": June 25, 1968, June II, 1971, October 31, 1975, November 20, 1978, April 25, 1994, November 21,1997, December 28,1998, December 5, 2002 $?~r~ ~ (S'g='"~) Vito A. Pulera Manager, New York Aircraft Certification Office (Title) Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA Form 8110-2 (10-68) Page 1 of 6 This certificate may be transferred in accordance with FAR 21. 47. "
@'~Vbat".9~bu)/ -- .-$/l6 ~W;40a/6 ./W;~, .' See Master Eligibility List -Attached
,Arde.'
,A~r~t"..
Normal, Utility and Acrobatic category airplanes andhelicopters equipped with engines and carburetors as describedbelow.
!!!2k:.wPYtU"o-/b0/'~J"lt'3 ~~ ?33f:znpe:Installation of ARP, Inc. Carburetor Ice Detection System Model 107AP (-12, -24, -R-12, -R-24, -U-12, and -U-24 series) in singleand twin engine aircraft and single engine helicopters powered by Continental, Franklin, and Lycoming type engines equipped withPrecision Air-Motive (Facet or Marvel-Schebler) MA-2, MA-3, MA-3A, MA-3SPA, MA-4, MA-4-5, MA-4SPA, MA-5, MA-6, MA-6AA and HA-6 series carburetors, in accordance with ARP, Inc. Installation Kit Parts List PLi 07AP-INST (Rev. B), datedJanuary 31,2002.
$t:.in.i/rdro/l~ u/u/ ~/I£?dr"o-/M..
1. This instrument is approved as optional equipment only and flight operations should not be predicated on its use. It is used as anearly warning device for detecting formation of carburetor ice in accordance with ARP, Inc. Flight Manual Supplement 107AP-SUPP (Rev. B), dated December 5, 2002.
szra/6 0/' 'o/"/l&'ct:dr"o-/b: November II, 1966 szra/e /'£ibMuer/ : November 21, 1997
szra/6 0/' bMU.-tZ/bce: April 28, 1967
~
szra/6 t:Yn£!/l£h.t": June 25, 1968, June II, 1971,October 31, 1975, November 20, 1978, April 25, 1994,November 21,1997, December 28,1998, December 5, 2002
$?~r~~ (S'g='"~)Vito A. PuleraManager,New York Aircraft Certification Office
(Title)
Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.
FAA Form 8110-2 (10-68) Page 1 of 6 This certificate may be transferred in accordance with FAR 21. 47.
2. Inspect the ice detector sensing probe for secure fit in carburetor during annual inspection or 100 hour inspection whicheveroccurs first. Inspect ice detector light sensor for condition and deposits following condition of an engine backfire.
3. This approval should not be extended to other specific airplanes or helicopters of those models on which other previouslyapproved modifications are incorporated unless it is determined that the interrelationship between this change and any of thoseother previously approved modifications will introduce no adverse affect upon the airworthiness of that airplane or helicopter.
4. If holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person writtenevidence of that permission.
(See Continuation Sheets 3-6)
Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.
FAA Form 8110-2-1 (10-69) Page 2 of 6 This ce;;:Uficate may be ~ransferred in accordance wi th FAR 21.47.
