Chequeo del helicóptero bo-105

Páginas: 7 (1610 palabras) Publicado: 18 de febrero de 2011
GAF T.O 1H-BO105-6GC/CF-1CL
CHAPTER A
BO105M/B0105P-1A1/BO105P-1A
Number of reference resume

|Reference number|Title |Page |
| |1. PREPARATION |A-6 |
| | | |
|1|Helicopter |A-6 |
|2 |Fuel quantity |A-6 |
|3 |Covers protections |A-6 |
|4 |Access doors |A-6 |
|5 |Fire extinguisher|A-6 |
|6 |PREFLIGHT mechanical check |A-6 |
|7 |Technical personal |A-6 |
| | | |
| |2. GROUND RUN PRE-CONTROL|A-7 |
| | | |
|8 |PRE-FLIGTH CHECK |A-7 |
|9 |ROTOR TRACKING and ROTOR TUNE |A-7 |
|10 |INTERIOR CHECK|A-7 |
|11 |BEFORE STARTING ENGINES |A-7 |

A-1
GAF T.O 1H-BO105-6GC/CF-1CL
Number of reference resume

|Reference number |Title |Page |
| |3. STARTING PROCEDURES |A-8 |
| || |
|12 |STARTING ENGINES |A-8 |
|13 |ENGINE RUN UP |A-8 |
| | | |
| |4. GROUND RUN WITH BOTH|A-9 |
| |ENGINES IN ¨FLIGHT¨ | |
| | | |
|14 |Throttle, engine 1 and 2 |A-9 |
|15 |Audio warning fuel low|A-9 |
|16 |Torque, engine 1 and 2 |A-9 |
|17 |N1, engine 1 and 2 |A-9 |
|18 |TOT, engine 1 and 2 |A-9 |
|19 |Oil pressure turbine, engine 1 and 2|A-9 |
|20 |Oil temperature , engine 1 and 2 |A-10 |
|21 |Main transmission oil pressure, system 1 and 2 |A-10 |
|22 |Main transmission oil temperature |A-10 |
| | | |
||5. GROUND RUN WITH ONE ENGINE |A-10 |
| | | |
|23 |Throttle of the engine who it not testing |A-10 |
|24 |N2 |A-10 |
| |...
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