# STC SH381NW - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Siam Hiller Holdings Inc - Description: Installation and maintenance of engine auto reignition system. (UH-12E modified per STC SH178WE) - Status date: April 15, 2009 - Data sheets: 4H11 - Certificate PDF: https://openairdocs.org/files/sha256/5e/b5/5eb53dbf7adbed21713ed9756e0fa721cb520e3e947eaaa83dba7ebac3933c6e - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B03E5301B961954B862575AF0049D90E.0001 - Page: https://openairdocs.org/stc/SH381NW ## ADs that name it None. ## Approved models (1) - Hiller Aircraft Corporation UH-12E (TCDS 4H11) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. ~ltit£o ~tltt£5 OD!J\mcriclt ~cpartmcnt of W:ranzportation - JlfcacraI J\&iation J\aminiztration ~uppI£m£ntaI «ITllP£@£rtifirat£This certificate has been reissued to replace' the original certificate reported as lost. ./f~~ SH381NW Siam Hiller Holdings, Inc. 925 M Street Firebaugh, California 93622 C(,"'/~J /4-/.-/do.c4//'.7"" VI'do. wv('.@J~/tft/. do.ftll:'l/Jvw /t/'f",z(H:/ I/Jtd do.t2,,/I.i/o:/U'/tJ 17./ta!Cf'/Kd:/UVtJ do./,~/, 0'-; +,VI"r.~a! /f!:.,/W'/b//VI"r.?Jdo.ain./JN',t,{';;,bI"J..)/'/'j7//V'I"//b/'/t?J /;/:71'/../'/27//'//f!:., .g?;,tk/'I7.1'./6t:"«/.-/V'/b .%3ry/dfdu,/tJ . Jfboh, .' Hiller V#b/'tk/. UH-12E !?lft,Jc/.yt/uw t/'~b" ~J~/b >J'4/./'.7A Installation and maintenance of engine auto-reif,rnition system III accordance with FAA approved Soloy Conversions, Ltd. Drawing List 560-401 dated December 9, 1976, or later FAA approved revision. NOTE: Only those Hiller UH-12E rotorcraft, which have been converted to turbine power in accordance with STC SH178WE are eligible for this modification. $v/ukd@/tJ o./ta!'!:f~'/t/d:/@/tJ. Approval of this change in type design applies to the above model rotorcraft only. This approval should not be extended to other rotorcraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that rotorcraft. A copy of this Certificate must be maintained as part of the permanent records for the modified rotorcraft. Continued on page 3 of this STC. ~. m4~a/('. o..rta!I'/fJ.,Jo/ytUd~ ah..k/.-.I/~£ i.; do.tfu~iJ ,/lv' o/f/t/'t:'tN7£ J/h~'/'//taVb Vb#d eNd,;/' J///'/,/'/«~/'/'d J,/.,yVl"/«.kd /'/'/!f"kd /N' t:/.-/i"/'//w«//uw d-/.-/('. iJ t:,do./'I/Ji.;" /'J/at1k';;/f!:.,dtJrdo..AMwti.Jkau'/' I/'I'/fJ., .!J?;a:;,/'a/.AoUz/uw ../bMwtiJk'a/uvt. February 24, 1976 January 11,1977 !YJL/('./'/'?;J((M! 06/02/83; 10/25/84; OS/28/91; 11/30/95; 04/15/05,04/15/09 .~ dU'/'C?U'/b(/' do..At:dn.vtiJ/nzuv' c=N1LcNx1-+-~--Supervisor, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office (Title) )lny a{terationof this certifiJ:ateispunisfUl6fe6y afine of not e:>\!eetfinB$1,000, or imprisonmentnot e:>\!eedl11{j3 years, or 60tfi. FAA Form 8110-2 (l0-68) 1 of 3 'T1iiscertifiJ:atemay6etran.sferret!illacco,,!a7ICewith 'F.JI'1(21.47. TRANSFER ENDORSEMENT Transfer the ownership of the Supplemental Type Certificate Number _ to (:Nameof transferee) _ (fi.aaressoftransfer)~ _ (J-{um6erana street) (City, State, ana Zip cod'e) from (:Nameofgrantor)(Print or type) _ (fi.aaressojgrantor) ('Num6erana street) (City, State, ana Zip cotle) Extent of Authority (if licensing agreement): _ Date ofTransfer: _ Signature of grantor (In inkJ: _ 2 of 3 ~nilea ~l1Ile5 ODfAmerica J8cpnrtmcnt of Wrnnsportntion - JIfcocrnI j\&intion ci\oministrntion ~uppl£m£ntal m~p£ QI£rtifirat£ (QIontinuation ~qeet) ,A0"ntfer< SH381NW The limitations and conditions of Rotorcraft Type Certificate 4H11 and STC SH178WE apply except as detailed below: 1. Rotorcraft Flight Manual FAA approved Soloy Conversions, Ltd. Rotorcraft Flight Manual dated April 10, 1975 with Supplement NO.7 is required in lieu of that specified for the basic unmodified Model UH-12E. Refer to the applicable portions of this FAA approved Soloy Conversions, Ltd. Rotorcraft Flight Manual for required placards and instrument markings. 2. Maintenance and Preflight Inspections Refer to the applicable portions of Soloy Conversions, Ltd. Maintenance Manual for the required maintenance of this system. Refer to the RFM Supplement for the required preflight inspection and check of this system. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. -END- )Iny a(teration of tfiis certificate is punisfia6Ce 6y a fine of noe e~eedinB $1,000, or imprisonment not e~eedlnB 3 years, or 60tfi. FAA Form 8110-2 (10-68) 3 of 3 '71iis certificate may 6e transferreain accordance witfi 'F)l'1(21.47. ## Every issue (2) - April 15, 2009: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/5e/b5/5eb53dbf7adbed21713ed9756e0fa721cb520e3e947eaaa83dba7ebac3933c6e) - April 15, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/b9/11/b911c7d8e8168291dece953d1e400e6ac08b75c0da086e87e51e8d9bd96239af) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.