{"id":893,"date":"2013-07-02T04:34:46","date_gmt":"2013-07-02T04:34:46","guid":{"rendered":"http:\/\/bizimkokpit.com\/?p=893"},"modified":"2015-06-05T04:37:12","modified_gmt":"2015-06-05T04:37:12","slug":"cift-motorlu-pervaneli-ucaklarla-alet-ucusu","status":"publish","type":"post","link":"https:\/\/bizimkokpit.com\/index.php\/2013\/07\/02\/cift-motorlu-pervaneli-ucaklarla-alet-ucusu\/","title":{"rendered":"\u00c7ift Motorlu Pervaneli U\u00e7aklarla Alet U\u00e7u\u015fu"},"content":{"rendered":"<div><a href=\"http:\/\/bizimkokpit.com\/wp-content\/uploads\/2015\/06\/Cessna-310.jpg\"><img loading=\"lazy\" decoding=\"async\" class=\" size-medium wp-image-894 alignleft\" src=\"http:\/\/bizimkokpit.com\/wp-content\/uploads\/2015\/06\/Cessna-310-300x240.jpg\" alt=\"Cessna-310\" width=\"300\" height=\"240\" srcset=\"https:\/\/bizimkokpit.com\/wp-content\/uploads\/2015\/06\/Cessna-310-300x240.jpg 300w, https:\/\/bizimkokpit.com\/wp-content\/uploads\/2015\/06\/Cessna-310-1024x819.jpg 1024w, https:\/\/bizimkokpit.com\/wp-content\/uploads\/2015\/06\/Cessna-310.jpg 1280w\" sizes=\"auto, (max-width: 300px) 100vw, 300px\" \/><\/a>\u00c7ift motorlu u\u00e7akla alet u\u00e7u\u015fu temel olarak tek motorlu u\u00e7aklar\u0131n benzeridir. Temel fark, ek sistemlerin karma\u015f\u0131kl\u0131\u011f\u0131, daha fazla i\u015fletme parametresi ve motor ar\u0131zas\u0131n\u0131n potansiyel problemleri ile ilgilidir. Hem u\u00e7u\u015f \u00f6ncesi pl\u00e2nlamada, hem de u\u00e7u\u015f esnas\u0131nda bu fakt\u00f6rlerle ba\u015far\u0131yla u\u011fra\u015fma yetene\u011fi, y\u00fcksek bilgi d\u00fczeyi ve kabiliyet gerektirir. Daha fazla\u2026Alet u\u00e7u\u015funu bilen ve \u00e7ift motorlu u\u00e7aklarla alet u\u00e7u\u015fu yapmak isteyen adaylar, uygulamal\u0131 test esnas\u0131nda alet u\u00e7u\u015funda yeterliliklerini g\u00f6stermek zorundad\u0131rlar. Gerekli prosed\u00fcrler, motorlar\u0131n t\u00fcm\u00fc \u00e7al\u0131\u015f\u0131rken ve tek motor \u00e7al\u0131\u015fmazken alet u\u00e7u\u015funu i\u00e7erir. Adaylar, belirli manevra ve performans kriterleri i\u00e7in uygun \u201cuygulamal\u0131 test standartlar\u0131na\u201d (\u015fahs\u00ee veya ticar\u00ee) ba\u015fvurmal\u0131d\u0131r. Alet u\u00e7u\u015f e\u011fitimi olmayan veya alet u\u00e7u\u015funda yeterlilik g\u00f6steremeyen adaylar i\u00e7in \u00e7ift motor izni sadece VFR u\u00e7u\u015f ile s\u0131n\u0131rland\u0131r\u0131l\u0131r.<\/div>\n<div><\/div>\n<div>NORMAL USULLER: Normal alet prosed\u00fcrleri \u00fc\u00e7 temel yetene\u011fi i\u00e7erir: \u00c7apraz kontrol, aletleri k\u0131ymetlendirme ve u\u00e7a\u011fa h\u00e2kimiyet. \u00c7ift motorlu u\u00e7aklarda da ayn\u0131 yetenekler gereklidir, fakat y\u00fcksek \u00e7al\u0131\u015fma s\u00fcr\u2019ati ve asimetrik g\u00fc\u00e7 ihtimali hava arac\u0131n\u0131n kontrol\u00fcn\u00fc zorla\u015ft\u0131r\u0131r.U\u00c7A\u011eIN KONTROL\u00dc: U\u00e7a\u011f\u0131n kontrol\u00fc i\u00e7in zorunlu fakt\u00f6r, normal manevralar ve konfig\u00fcrasyonda istenen s\u00fcr\u2019atleri ve u\u00e7u\u015f durumlar\u0131n\u0131 sa\u011flamak i\u00e7in gerekli g\u00fc\u00e7 ayarlamalar\u0131n\u0131n \u00f6\u011frenilmesidir. \u00c7ift motorlu u\u00e7aklarda g\u00fc\u00e7 de\u011fi\u015fikliklerinde a\u015f\u0131r\u0131 kontrol, ba\u015flang\u0131\u00e7 e\u011fitimi esnas\u0131nda genel bir e\u011filimdir. \u00c7o\u011fu g\u00fc\u00e7 ayarlamalar\u0131 pervane kontrollerinden ziyade gaz kollar\u0131 (manifold bas\u0131nc\u0131) kullan\u0131larak yap\u0131l\u0131r. Bir g\u00fc\u00e7 de\u011fi\u015fikli\u011finden sonra, motorlar sabit istikameti daha kolay muhafaza etmek i\u00e7in ayn\u0131 g\u00fcc\u00fc \u00fcretecek \u015fekilde ayarlanmal\u0131d\u0131r. G\u00fc\u00e7 uygun \u015fekilde ayarland\u0131\u011f\u0131nda ve istenen durum tesis edildi\u011finde, u\u00e7a\u011f\u0131n performans\u0131 nispeten tahmin edilebilir. Pilot \u201cIFR\u201d \u015fartlarda u\u00e7a\u011fa tam olarak h\u00e2kim olmak i\u00e7in do\u011fru g\u00fc\u00e7 ayarlar\u0131n\u0131, s\u00fcr\u2019atleri ve limitleri bilmenin yan\u0131nda, gerekti\u011fi yerde do\u011fru kumandalar\u0131 vermek zorundad\u0131r.<\/div>\n<div><\/div>\n<div>TR\u0130M\u0130N KULLANILMASI: Trim, alet u\u00e7u\u015funda her zaman \u00f6nemlidir, y\u00fcksek performansl\u0131 \u00e7ift motorlu u\u00e7aklarda ise bu \u00f6nem daha fazlad\u0131r. Zay\u0131f trim tekni\u011fi, kumandalarda bas\u0131n\u00e7 olu\u015fmas\u0131na neden olarak a\u015f\u0131r\u0131 yorgunlu\u011fa sebep olur. Trim tekni\u011finin farkl\u0131 u\u00e7aklara g\u00f6re de\u011fi\u015fiklik g\u00f6stermesine ra\u011fmen, genel metot \u015fudur; U\u00e7ak yeni bir durumda ve\/veya s\u00fcr\u2019atte stabil (istikrarl\u0131) hale getirildikten sonra yap\u0131lan trim ayar\u0131 en iyisidir. Uygun trim ayar\u0131 yap\u0131lan u\u00e7ak, pilotunun i\u015f y\u00fck\u00fcn\u00fc azalt\u0131r ve pilotun alet u\u00e7u\u015f g\u00f6revleri i\u00e7in daha fazla zaman ay\u0131rmas\u0131n\u0131 sa\u011flar.<\/div>\n<div><\/div>\n<div>TE\u00c7H\u0130ZATIN KULLANILMASI: \u00c7ift motorlu u\u00e7aklar genellikle alet u\u00e7u\u015f ko\u015fullar\u0131nda u\u00e7u\u015f i\u00e7in gerekli te\u00e7hizata ve yeterli performansa sahiptirler. \u00c7ok y\u00f6nl\u00fc haberle\u015fme ve seyr\u00fcsefer radyolar\u0131 ile geli\u015fmi\u015f avionikler, b\u00f6lge seyr\u00fcsefer te\u00e7hizat\u0131, bunlar\u0131n yan\u0131nda u\u00e7u\u015f y\u00f6netim ve oto pilot sistemleri, alet u\u00e7u\u015f ko\u015fullar\u0131nda kullan\u0131lan ve pilotun i\u015fini kolayla\u015ft\u0131ran te\u00e7hizatlara \u00f6rnek olarak say\u0131labilir. Baz\u0131 u\u00e7aklarda, meteoroloji radar\u0131, kabin bas\u0131n\u00e7lama ve buz k\u0131rma veya buz \u00f6nleme sistemleri gibi u\u00e7a\u011f\u0131n kabiliyetini artt\u0131ran sistemler de vard\u0131r. Pilotlar i\u00e7in en \u00f6nemlisi daha karma\u015f\u0131k olan te\u00e7hizatlar\u0131n etkin \u015fekilde nas\u0131l kullan\u0131laca\u011f\u0131 ve i\u015fletilece\u011fini \u00f6\u011frenmektir. E\u011fer bir pilot geli\u015fmi\u015f aletlere ve te\u00e7hizata yabanc\u0131 ise, bu sistemler kokpit i\u015f y\u00fck\u00fcn\u00fc azaltaca\u011f\u0131 yerde pilot i\u00e7in \u015fa\u015fk\u0131nl\u0131k yaratarak verimini d\u00fc\u015f\u00fcr\u00fcr. Uygulama s\u0131nav\u0131nda \u00e7ift motor adaylar\u0131, \u00e7e\u015fitli sistemleri ve bunlar\u0131n hatalar\u0131n\u0131n sebeplerini, i\u015f\u2019arlar\u0131 ve pilot uygulamalar\u0131 ile a\u00e7\u0131klayarak bilgilerini sergilemek zorundad\u0131rlar.<\/div>\n<div><\/div>\n<div>ALET U\u00c7U\u015e KO\u015eULLARINDA\u201cIFR\u201d U\u00c7U\u015e PL\u00c2NLAMA: Bir meydandan di\u011ferine \u201cIFR\u201d u\u00e7u\u015f; ayr\u0131l\u0131\u015f, rota, var\u0131\u015f ve yakla\u015fma safhalar\u0131ndan olu\u015fur. \u00c7ift motorlu bir u\u00e7akta \u00e7o\u011funlukla u\u00e7u\u015fun b\u00fcy\u00fck bir k\u0131sm\u0131nda geni\u015f bir i\u015fletme irtifa ve s\u00fcr\u2019at se\u00e7imi m\u00fcmk\u00fcnd\u00fcr. Farkl\u0131 safhalarda, de\u011fi\u015fik s\u00fcr\u2019atler, irtifalar ve yak\u0131t t\u00fcketim oranlar\u0131 kullan\u0131laca\u011f\u0131ndan, u\u00e7u\u015f pl\u00e2nlamas\u0131 her safha i\u00e7in farkl\u0131 bir hesaplama gerektirir. Meteorolojinin bir fakt\u00f6r oldu\u011fu bir\u00e7ok durumda, yak\u0131t tasarrufu ana d\u00fc\u015f\u00fcncedir; bununla beraber menzil ve minimum zaman baz\u0131 u\u00e7u\u015flarda \u00f6ncelikli pl\u00e2nlama d\u00fc\u015f\u00fcncesi olabilir.<\/div>\n<div><\/div>\n<div>AYRILI\u015e: G\u00f6r\u00fc\u015f\u00fcn d\u00fc\u015f\u00fck, bulut tavan\u0131n\u0131n al\u00e7ak oldu\u011fu bir havada kalk\u0131\u015ftan \u00f6nce, \u00e7ift motorlu u\u00e7ak pilotu ayr\u0131l\u0131\u015f\u0131 ve ilgili prosed\u00fcrleri dikkatlice incelemelidir. \u00d6rne\u011fin; \u0131slak pist u\u00e7a\u011f\u0131n h\u0131zlanma durma mesafesini nas\u0131l etkiler? Meydan\u0131n bir SID\u2019si veya bas\u0131l\u0131 ayr\u0131l\u0131\u015f usul\u00fc var m\u0131? T\u0131rman\u0131\u015f oran\u0131 ne olmal\u0131? H\u00e2lihaz\u0131r hava durumu ini\u015f minimumlar\u0131n\u0131n alt\u0131nda ise kalk\u0131\u015fa te\u015febb\u00fcs edilmemelidir, \u00e7\u00fcnk\u00fc bir emercensi durumda ini\u015f i\u00e7in tekrar kalk\u0131\u015f meydan\u0131n\u0131 kullanmak zorunlu olabilir. Ayr\u0131ca pilot, kalk\u0131\u015fta veya t\u0131rman\u0131\u015fta meydana gelebilecek motor ar\u0131zalar\u0131nda tavsiye edilen usulleri tatbik etmeye haz\u0131rl\u0131kl\u0131 olmal\u0131d\u0131r. Kalk\u0131\u015ftan \u00f6nce motor durmas\u0131 usullerini, s\u00fcr\u2019atleri ve t\u0131rman\u0131\u015f limitlerini i\u00e7eren u\u00e7ak performans yeteneklerinin sistematik incelemesi yap\u0131lmal\u0131d\u0131r.<\/div>\n<div><\/div>\n<div>ROTA: U\u00e7u\u015f rotas\u0131n\u0131n pl\u00e2nlanmas\u0131na etki eden bir \u00e7ok fakt\u00f6r vard\u0131r. U\u00e7a\u011f\u0131n performans\u0131, te\u00e7hizat\u0131, meteoroloji ve rota \u00fczerinde bir emercensi durumda ini\u015f yap\u0131labilecek meydanlar bu fakt\u00f6rlere \u00f6rnek olarak verilebilir. Buzlanma, f\u0131rt\u0131na, t\u00fcrb\u00fcl\u00e2ns ve hatta r\u00fczg\u00e2r gibi istenmeyen durumlar, u\u00e7u\u015f rotas\u0131nda ve\/veya irtifada s\u0131k s\u0131k de\u011fi\u015fikli\u011fe neden olur.<\/div>\n<div><\/div>\n<div>VARI\u015e VE BEKLEME: Rota safhas\u0131nda alet u\u00e7u\u015funun yakla\u015fma safhas\u0131na ge\u00e7i\u015f, b\u00fct\u00fcn u\u00e7u\u015f parametrelerinde de\u011fi\u015fikli\u011fi gerektirir. \u0130rtifa, ba\u015f, s\u00fcr\u2019at ve konfig\u00fcrasyon. Bu ayarlar \u00e7ift motorlu u\u00e7aklarda karma\u015f\u0131k u\u00e7u\u015f sistemlerinden dolay\u0131 daha \u00f6nemlidir. Katlanabilir ini\u015f tak\u0131m\u0131 ve hava ak\u0131m\u0131n\u0131n kolayca \u00fczerinden ge\u00e7i\u015fi, g\u00fc\u00e7 azalt\u0131ld\u0131\u011f\u0131nda daha yava\u015f bir \u015fekilde ivmenin azalmas\u0131na sebep olur. Ayn\u0131 zamanda y\u00fcksek S\/S irtifas\u0131 rahat ve ekonomik bir al\u00e7alma i\u00e7in zaman\u0131 art\u0131r\u0131r. Al\u00e7alma oran\u0131n\u0131n hesaplanmas\u0131, klerans\u0131n al\u0131nmas\u0131, ATC talimatlar\u0131n\u0131n takibi ve yakla\u015fma\/pas ge\u00e7me prosed\u00fcrlerinin incelenmesi gibi ekstra g\u00f6revler pilotun i\u015f y\u00fck\u00fcn\u00fc art\u0131r\u0131r. Pilot ayn\u0131 zamanda bekleme paternini son bir kez incelemeli, giri\u015f \u015fekline karar vermeli, uygun bekleme s\u00fcr\u2019atini tesis etmeye haz\u0131rl\u0131kl\u0131 olmal\u0131d\u0131r. Pervaneli u\u00e7aklar i\u00e7in maksimum bekleme s\u00fcr\u2019ati 175 Nat olmas\u0131na ra\u011fmen, yak\u0131t t\u00fcketimini azaltmak, irtifa kontrol\u00fcn\u00fc daha kolay sa\u011flamak ve bekleme paterninin b\u00fcy\u00fckl\u00fc\u011f\u00fcn\u00fc azaltmak i\u00e7in d\u00fc\u015f\u00fck s\u00fcr\u2019atler kullan\u0131labilir.<\/div>\n<div><\/div>\n<div>T\u00dcM MOTORLAR \u00c7ALI\u015eIRKEN ALET YAKLA\u015eMASI: \u00d6n pl\u00e2nlama her t\u00fcrl\u00fc alet yakla\u015fmas\u0131n\u0131n ka\u00e7\u0131n\u0131lmaz bir par\u00e7as\u0131d\u0131r. Bu pl\u00e2nlama, \u00f6zellikle tek pilot i\u015fletme konsepti alt\u0131nda \u00e7ift motorlu u\u00e7akla e\u011fitim yaparken \u00e7ok \u00f6nemlidir. Var\u0131\u015f meydan\u0131 ile yedek meydan\u0131n her ikisi i\u00e7in yakla\u015fma prosed\u00fcrlerinin ayr\u0131nt\u0131l\u0131 olarak incelenmesi u\u00e7u\u015f \u00f6ncesi haz\u0131rl\u0131\u011f\u0131n ka\u00e7\u0131n\u0131lmaz bir par\u00e7as\u0131d\u0131r. \u0130deal olan\u0131, pilot u\u00e7u\u015f esnas\u0131nda bir yakla\u015fma kart\u0131na bakt\u0131\u011f\u0131nda, bu ilk bak\u0131\u015f\u0131 olmamal\u0131, kart\u0131 \u00f6nceden ayr\u0131nt\u0131l\u0131 olarak incelemi\u015f olmal\u0131d\u0131r. Tek pilot alet yakla\u015fmas\u0131, \u00e7ift motorlu u\u00e7aklar\u0131n y\u00fcksek yakla\u015fma s\u00fcr\u2019atlerinden dolay\u0131 k\u0131sa bir s\u00fcrede bir\u00e7ok g\u00f6revin yap\u0131lmas\u0131n\u0131 gerektirir. Ayn\u0131 zamanda, fazlas\u0131yla detayl\u0131 \u00e7eklist usulleri i\u015f y\u00fck\u00fcn\u00fc art\u0131r\u0131r. Sonu\u00e7 olarak, pilot \u00e7ok iyi haz\u0131rlanmal\u0131, pl\u00e2n\u0131n\u0131 yapmal\u0131 ve yap\u0131lmas\u0131 gerekenleri mant\u0131kl\u0131 bir s\u0131raya g\u00f6re d\u00fczenlemelidir. Bu sistematik d\u00fczenleme, kokpit y\u00f6netiminin elemanlar\u0131ndan birisidir. \u00c7ift motor uygulama test standartlar\u0131na g\u00f6re, pilot bas\u0131l\u0131 alet yakla\u015fmalar\u0131nda uygun kokpit y\u00f6netim bilgilerini sergilemek zorundad\u0131r. Di\u011fer kriterler ise klerans alma, ATC talimatlar\u0131n\u0131n takibi ve uygun al\u00e7alma oran\u0131n\u0131 belirlemedir (r\u00fczg\u00e2r ve pas ge\u00e7me noktas\u0131n\u0131 de\u011ferlendirerek). Al\u00e7alma, kursu takip edilerek yap\u0131lmal\u0131 ve DH veya MDA\u2019da direkt veya meydan turlu olarak normal ini\u015fi ger\u00e7ekle\u015ftirebilecek pozisyonda olunmal\u0131d\u0131r. T\u00fcm motorlar \u00e7al\u0131\u015f\u0131rken yap\u0131lan alet yakla\u015fmas\u0131nda, pilottan belirlenmi\u015f olan MAP\u2019da pas ge\u00e7meyi uygun olarak icra etmesi ve \u00e7eklist maddelerini eksiksiz takip etmesi beklenir.<\/div>\n<div><\/div>\n<div>TEK MOTOR ARIZASI ALET USULLER\u0130: Bir motor ar\u0131zas\u0131 durumu her zaman kritiktir ve bu durum alet \u015fartlar\u0131nda u\u00e7arken daha fazla \u00f6nem arz eder. \u00c7ift motor pilotu, dikkatini emercensi prosed\u00fcrlere yo\u011funla\u015ft\u0131rmal\u0131 ve ayn\u0131 zamanda aletlerden ald\u0131\u011f\u0131 i\u015f\u2019arlara ba\u011fl\u0131 olarak u\u00e7a\u011f\u0131n kontrol\u00fcn\u00fc sa\u011flamal\u0131d\u0131r. Bundan dolay\u0131, motor stop etti\u011finde yap\u0131lmas\u0131 gereken prosed\u00fcrleri tam olarak anlamak ve hemen hat\u0131rlayabilmek hayati \u00f6nem arz etmektedir.<\/div>\n<div><\/div>\n<div>D\u00dcZ VE UFK\u00ee U\u00c7U\u015e ESNASINDA VE D\u00d6N\u00dc\u015eLERDE MOTOR ARIZASI: Uygulamal\u0131 test standartlar\u0131nda belirtildi\u011fi \u00fczere, pilot motor ar\u0131zas\u0131n\u0131 hemen te\u015fhis etmeli, motor kumandalar\u0131n\u0131 ayarlamal\u0131, geri s\u00fcr\u00fcklemeyi azaltmal\u0131 ve \u00e7al\u0131\u015fmayan motoru te\u015fhis ve teyit etmelidir. Bir motor ar\u0131zaland\u0131\u011f\u0131nda, u\u00e7ak \u00e7al\u0131\u015fmayan motor taraf\u0131na sapma ve yatma e\u011filiminde oldu\u011fundan, sun\u2019\u00ee ufuk ve d\u00f6n\u00fc\u015f kay\u0131\u015f m\u00fc\u015firi (b\u00fbl) ar\u0131zal\u0131 motor y\u00f6n\u00fcnde bir d\u00f6n\u00fc\u015f g\u00f6sterecektir. Kontrol\u00fc sa\u011flamak i\u00e7in, pilot, en iyi tek motor s\u00fcr\u2019atini tesis etmeli ve u\u00e7a\u011f\u0131 gerekti\u011fi \u015fekilde trimli u\u00e7u\u015fa ayarlamal\u0131d\u0131r. Ayn\u0131 zamanda duran motoru emniyete almak i\u00e7in uygun \u00e7eklist usulleri uygulanmal\u0131d\u0131r. D\u00fcz ve ufk\u00ee u\u00e7u\u015f esnas\u0131nda en iyi performans i\u00e7in \u00e7al\u0131\u015fan motor taraf\u0131na bir yat\u0131\u015f tavsiye edilmektedir. D\u00f6n\u00fc\u015f esnas\u0131nda, yat\u0131\u015f a\u00e7\u0131s\u0131 \u00e7ok dikkatli g\u00f6zlemlenmeli ve kontrol edilmelidir. En iyi d\u00f6n\u00fc\u015f performans\u0131 hemen hemen standart d\u00f6n\u00fc\u015f oran\u0131 ile elde edilir. U\u00e7ak tamamen kontrol alt\u0131na al\u0131nd\u0131\u011f\u0131nda ve \u00e7eklist usulleri tamamland\u0131\u011f\u0131nda, pilot motor ar\u0131zas\u0131n\u0131n sebebini tespite \u00e7al\u0131\u015fmal\u0131d\u0131r. Yo\u011funluk irtifas\u0131, servis tavan\u0131, u\u00e7ak a\u011f\u0131rl\u0131\u011f\u0131 ve arazinin (veya engellerin) y\u00fcksekli\u011fi gibi fakt\u00f6rlere ba\u011fl\u0131 olarak irtifa muhafaza edilmeli veya minimum al\u00e7al\u0131\u015f oran\u0131 tesis edilmelidir. Pilot, ayn\u0131 zamanda \u00e7al\u0131\u015fan motoru g\u00f6zlemlemeye devam etmeli ve gerekli ayarlamalar\u0131 yapmal\u0131d\u0131r. E\u011fitimde veya uygulamal\u0131 test esnas\u0131nda, motor ar\u0131zas\u0131 Pilot \u0130\u015fletme El Kitab\u0131nda belirtildi\u011fi gibi sim\u00fcle edilir. Benzetilmi\u015f usuller ger\u00e7ek motor ar\u0131zas\u0131ndaki durumla hemen hemen ayn\u0131d\u0131r. Adaylar\u0131n uygun uygulamal\u0131 test standartlar\u0131nda (\u015fahs\u00ee veya ticar\u00ee) belirtilen limitler dahilinde irtifay\u0131, s\u00fcr\u2019ati ve u\u00e7ulan ba\u015f\u0131 muhafaza etmeleri gerekir. Ek olarak \u00e7ift motor adaylar\u0131ndan motor \u00e7al\u0131\u015fmazken performans ve i\u015fletme limitleri konusunda bilin\u00e7li olmalar\u0131, her zaman u\u00e7a\u011f\u0131n pozitif kontrol\u00fcn\u00fc sa\u011flamalar\u0131 ve emniyetli ini\u015f yapabileceklerinden emin olduklar\u0131 kursa karar vermeleri beklenir.<\/div>\n<div><\/div>\n<div>TEK MOTOR ALET YAKLA\u015eMASI: \u00c7ift motorlu u\u00e7aklarda motor ar\u0131zas\u0131 u\u00e7u\u015fta kritik bir durum oldu\u011fundan pilotun se\u00e7enekleri \u015funlar olabilir: Var\u0131\u015f meydan\u0131na devam eder, en yak\u0131n meydana iner veya yak\u0131n uygun\/m\u00fcsait bir meydana iner. Duruma en uygun karar genellikle, u\u00e7a\u011f\u0131n tipi, motor ar\u0131zas\u0131n\u0131n muhtemel sebebi ve irtifa gibi fakt\u00f6rlere ba\u011fl\u0131d\u0131r. Genel bir kural olarak, uygun bir meydana m\u00fcmk\u00fcn oldu\u011funca zaman kaybetmeden inilmesi tavsiye edilir. Hava durumu, alet u\u00e7u\u015f ko\u015fullar\u0131nda d\u00fc\u015f\u00fcn\u00fclmesi gereken en \u00f6nemli fakt\u00f6rd\u00fcr. Bir\u00e7ok durumda, pilot, ini\u015fin ilk yakla\u015fmada yap\u0131laca\u011f\u0131ndan emin olmal\u0131d\u0131r. En iyi durumda bile tek motor ar\u0131zas\u0131 ile yap\u0131lan pas ge\u00e7i\u015f \u00e7ok zordur ve bir\u00e7ok durumda m\u00fcmk\u00fcn olmayabilir. Azalan performans kabiliyeti ve asimetrik \u00e7eki\u015f kuvveti, tek motorla yap\u0131lan pas ge\u00e7i\u015fi, \u00f6zellikle alet \u015fartlar\u0131nda \u00e7ok sak\u0131ncal\u0131 bir manevra haline getirebilir. M\u00fcmk\u00fcnse pilot h\u00e2lihaz\u0131r ve tahmin\u00ee meteorolojik durumu uygun ve yakla\u015fma minimalar\u0131 \u00fczerinde olan bir meydan se\u00e7melidir. Varsa hassas bir yakla\u015fma tercih edilmelidir. Bu t\u00fcr bir yakla\u015fma teker koyma noktas\u0131 i\u00e7in do\u011fru bir s\u00fcz\u00fcl\u00fc\u015f hatt\u0131 bilgisi sa\u011flar ve yakla\u015fma esnas\u0131nda irtifay\u0131 sa\u011flamak i\u00e7in gerekli olan il\u00e2ve zaman ihtiyac\u0131n\u0131 azalt\u0131r. D\u00fc\u015f\u00fck irtifada, y\u00fcksek g\u00fc\u00e7 ayarlar\u0131nda uzun s\u00fcre u\u00e7maktan m\u00fcmk\u00fcn oldu\u011funca ka\u00e7\u0131n\u0131lmal\u0131d\u0131r. E\u011fer radar hizmeti varsa talep edilmelidir. Radar vekt\u00f6rleri pilotun i\u015f g\u00fcc\u00fcn\u00fc azalt\u0131r ve yakla\u015fma esnas\u0131nda manevra ve zaman ihtiyac\u0131n\u0131 azalt\u0131r. Yakla\u015fma s\u0131ras\u0131nda pilot, g\u00fc\u00e7 kullan\u0131m\u0131, geri s\u00fcr\u00fckleme kuvveti, s\u00fcr\u2019at ve trimi i\u00e7eren \u00e7eklist usullerini aynen uygulamal\u0131d\u0131r. Ba\u015far\u0131l\u0131 bir yakla\u015fma i\u00e7in pilot, ayn\u0131 zamanda alet yakla\u015fma usullerini kullanmal\u0131, ATC talimatlar\u0131n\u0131 takip etmeli ve her an u\u00e7a\u011f\u0131n pozitif kontrollerini sa\u011flamal\u0131d\u0131r. \u015eartlar m\u00fcsaade ederse, pilot, yakla\u015fmay\u0131 t\u00fcm motorlar \u00e7al\u0131\u015f\u0131yormu\u015f gibi normal usullerde u\u00e7maya \u00e7al\u0131\u015fmal\u0131d\u0131r. Bilinen usullerden sapmalar mevcut problemleri artt\u0131rabilir. Al\u00e7alma pl\u00e2nlar\u0131nda g\u00f6sterildi\u011fi gibi s\u00fcz\u00fcl\u00fc\u015f hatt\u0131n\u0131 kesmeden \u00f6nce u\u00e7ak, tavsiye edilen yakla\u015fma s\u00fcratine yava\u015flat\u0131lmal\u0131, fakat s\u00fcr\u2019at hi\u00e7bir zaman VYSE \u2018den a\u015fa\u011f\u0131 olmamal\u0131d\u0131r. Normal yakla\u015fma prosed\u00fcrlerinden tavsiye edilen tek fark, ini\u015f tak\u0131mlar\u0131 ve flaplar\u0131n kullan\u0131m\u0131 ile ilgilidir. Genel bir kural olarak, u\u00e7ak kursa, son yakla\u015fma fiksinde ini\u015f tak\u0131mlar\u0131 ve flaplar yukar\u0131 pozisyonda oturmal\u0131d\u0131r. Ve bunlar emniyetle ini\u015f yap\u0131laca\u011f\u0131ndan emin oluncaya kadar tam kullan\u0131lmamal\u0131d\u0131r. Son yakla\u015fma esnas\u0131nda, s\u00fcr\u2019at VYSE\u2019de veya \u00fczerinde tutulmal\u0131d\u0131r. Son yakla\u015fma safhas\u0131nda \u00e7al\u0131\u015fan motorun g\u00fcc\u00fc tedr\u00eecen azalt\u0131lmal\u0131, teker koyma noktas\u0131nda r\u00f6l\u00e2ntide veya ona yak\u0131n konumda olacak \u015fekilde ayarlanmal\u0131d\u0131r. G\u00fc\u00e7teki bu kademeli de\u011fi\u015fiklik, istikamet kontrol\u00fc i\u00e7in gereken trim ayarlamalar\u0131 ve pedal bas\u0131n\u00e7 de\u011fi\u015fiklikleri i\u00e7in kolay bir ge\u00e7i\u015fe m\u00fcsaade eder. Tek motor ile yap\u0131lan bir alet yakla\u015fmas\u0131 i\u00e7in performans kriterleri uygulamal\u0131 test standartlar\u0131nda listelenmi\u015ftir. Pilotlardan kurs \u00fczerinde al\u00e7almalar\u0131 ve DH (karar irtifas\u0131) veya MDA (minimum al\u00e7alma irtifas\u0131) (hangisi uygulan\u0131yorsa) da normal bir ini\u015f yapabilecekleri pozisyonda olmalar\u0131 beklenir. Normal alet yakla\u015fma usullerine itaat mecbur\u00eedir.<\/div>\n<div><\/div>\n<div>Bu yaz\u0131da \u00e7ift motor alet u\u00e7u\u015f prosed\u00fcrleri genel olarak anlat\u0131lm\u0131\u015ft\u0131r. Kesin prosed\u00fcrler her u\u00e7ak i\u00e7in farkl\u0131l\u0131k g\u00f6sterebilece\u011finden dolay\u0131 pilotlar u\u00e7tuklar\u0131 u\u00e7aklar i\u00e7in haz\u0131rlanan pilot el kitaplar\u0131ndaki tavsiyeleri takip etmelidir.<\/div>\n","protected":false},"excerpt":{"rendered":"<p>\u00c7ift motorlu u\u00e7akla alet u\u00e7u\u015fu temel olarak tek motorlu u\u00e7aklar\u0131n benzeridir. Temel fark, ek sistemlerin karma\u015f\u0131kl\u0131\u011f\u0131, daha fazla i\u015fletme parametresi ve motor ar\u0131zas\u0131n\u0131n potansiyel problemleri ile ilgilidir. Hem u\u00e7u\u015f \u00f6ncesi pl\u00e2nlamada, hem de u\u00e7u\u015f esnas\u0131nda bu fakt\u00f6rlerle ba\u015far\u0131yla u\u011fra\u015fma yetene\u011fi, y\u00fcksek bilgi d\u00fczeyi ve kabiliyet gerektirir. Daha fazla\u2026Alet u\u00e7u\u015funu bilen ve \u00e7ift motorlu u\u00e7aklarla alet<\/p>\n","protected":false},"author":1,"featured_media":894,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[69],"tags":[82],"class_list":["post-893","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-ucus","tag-cift-motor"],"_links":{"self":[{"href":"https:\/\/bizimkokpit.com\/index.php\/wp-json\/wp\/v2\/posts\/893","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/bizimkokpit.com\/index.php\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/bizimkokpit.com\/index.php\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/bizimkokpit.com\/index.php\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/bizimkokpit.com\/index.php\/wp-json\/wp\/v2\/comments?post=893"}],"version-history":[{"count":1,"href":"https:\/\/bizimkokpit.com\/index.php\/wp-json\/wp\/v2\/posts\/893\/revisions"}],"predecessor-version":[{"id":895,"href":"https:\/\/bizimkokpit.com\/index.php\/wp-json\/wp\/v2\/posts\/893\/revisions\/895"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/bizimkokpit.com\/index.php\/wp-json\/wp\/v2\/media\/894"}],"wp:attachment":[{"href":"https:\/\/bizimkokpit.com\/index.php\/wp-json\/wp\/v2\/media?parent=893"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/bizimkokpit.com\/index.php\/wp-json\/wp\/v2\/categories?post=893"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/bizimkokpit.com\/index.php\/wp-json\/wp\/v2\/tags?post=893"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}