Държавен вестник, бр. 86, 2010 г., стр. 84

СТР.  84	
Д Ъ Р Ж А В Е Н  В Е С Т Н И К 	
БРОЙ  86
17. A Qualification Test Guide (QTG) which shall 
be submitted in a form and manner acceptable to 
the Authority and which conforms to AMC STD 
4A.030 (para1.6).
17. Инструкции за квалификационния изпит, които се 
предоставят от оператора във форма и по начин, кои­
то са приемливи за компетентната въздухоплавателна 
администрация и които отговарят на изискванията на 
AMC STD 4A.030 (параграф 1.6).
12 – Датчик за определяне ъгъла на атаката, който 
да отговаря на този в имитирания самолет или клас 
самолети.
Appendix 2 to JAR-STD 4A.030 Table 1 – BITD 
Standards
Приложение 2 към JAR-STD 4A.030 
Таблица 1 – Стандарти за оборудване за основна подго­
товка за работа с пилотажно-навигационните прибори 
(BITD)
Table 1 below shows how the requirements, listed in 
Table 1 of Appendix 1 to JAR-STD 4A.030, shall 
be fulfilled.
В таблица 1 по-долу се дава как трябва да се изпълняват 
изискванията, изброени в таблица 1 на Приложение 1 
към JAR-STD 4A.030.
BITD STANDARDS
COMMENTS
a. Time from pilot‘s control input to recognizable system response (transport 
delay) or the attitude indicator shall be 300 ms or less. This standard shall 
be certified by the manufacturer in the QTG submitted for Qualification.
SOC required.
b. The basic flight instruments shall be displayed and arranged in the 
usual „Т-layout“. The following instruments shall be displayed so as to be 
representative for the simulated class of aeroplane:
1. An attitude indicator with at least 5° and 10° pitch markings, and bank 
angle markings for 10°. 20°. 30° and 60°.
2. Adjustable altimeter(s) with 20 ft markings.
3. An airspeed indicator with at least 5 kts markings within a representative 
speed range and colour coding.
4. An HSI or heading indicator with incremental markings each of at least 
5°, displayed on a 360° circle. The heading figures shall be radially aligned.
5. A vertical speed indicator with 100 fpm markings up to 1 000 fpm and 
500 fpm thereafter within a representative range.
6. A turn and bank indicator with incremental markings for a rate of 3“ per 
second turn for left and right turns. The 3° per second rate index shall be 
inside of the maximum deflection of the indicator.
C over s a l s o s c re en- ba s e d 
instrument panel. Instruments 
shall be displayed very nearly 
full-size as in the simulated class 
of aeroplane.
Controls to adjust the instruments, 
e.g. QNH, course or heading bugs 
shall be located spatially correct at 
the respective instrument.
A triangle slip indicator is 
acceptable if applicable for the 
simulated class of aeroplane.
7. A slip indicator representative of the simulated class of
aeroplane, where a coordinated fight condition is indicated with the ball in 
centre position.
8. A magnetic compass with incremental markings each 10“.
9. Engine instruments as applicable to the simulated class of aeroplane, with 
markings for normal ranges, minimum and maximum limits.
10. A suction gauge or instrument pressure gauge, as applicable, with a 
display as appl icable for the simulated class of aeroplane.
11. A flap position indicator which displays the current flap setting. This 
indicator shall be representative of the simulated class of aeroplane.
12. A pitch trim indicator with a display that shows zero trim and appropriate 
indices of aeroplane nose down and nose up trim.
13. A stop watch or digital timer which allows the readout of seconds and 
minutes.
c. A communication and navigation panel shall be displayed in a manner 
that the frequency in use is shown. The NAV equipment shall include ADF, 
VOR, DME and ILS indicators with the following incremental markings:
1. one-half dot or less for course and glide slope indications on the VOR 
and ILS display.
2. 5о or less of bearing deviation for ADF and RMI, as applicable.
All NAV radios shall be equipped with an aural identification feature. A 
marker beacon receiver shall also be installed with an optical and aural 
identification.
Controls to select the frequencies 
and other functions may Lie located 
on a central COM/IMAV panel 
or on a separate economically 
located panel.