ANNEXURE II
GOVERNMENT
OF INDIA
DIRECTOR GENERAL OF CIVIL AVIATION
APPLICATION FOR ISSUE/REVALIDATION OF TYPE CERTIFICATE OF ROTORCRAFT
This
form of application, when completed, should be forwarded to Director
General of Civil Aviation,
New Delhi.
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1. |
CONSTRUCTOR OF ROTORCRAFT |
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2. |
ADDRESS (IN FULL) |
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3. |
GENERAL DESCRIPTION OF ROTORCRAFT |
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4. |
ROTORCRAFT MODEL |
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5. |
AIRWORTHINESS CATEGORY |
TRANSPORT
CATEGORY (PASSENGER) |
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6. |
COUNTRY OF CONSTRUCTION |
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7. |
YEAR OF CONSTRUCTION |
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8. |
SERIAL NUMBER ELIGIBLE |
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9. |
CERTIFICATION BASIS |
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10. |
PRODUCTION BASIS |
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11. |
AIRWORTHINESS AUTHORITY OF THE COUNTRY |
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12. |
TYPE CERTIFICATION IN OTHER COUNTRIES |
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13. |
REGISTRATION MARKS |
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14. |
DIMENSIONS
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DIAMETER OF MAIN ROTOR |
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MAIN ROTOR BLADE CHORD |
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DIAMETER OF TAIL ROTOR |
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LENGTH OVERALL |
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LENGTH OF FUSELAGE |
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HEIGHT OVERALL |
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WHEEL TRACK |
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WHEEL BASE |
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15. |
TYPE OF ENGINE |
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16. |
NUMBER OF ENGINES |
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17. |
ENGINE OPERATING LIMITS |
ALL ENGINES OPERATING |
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18. |
ROTOR LIMITS |
POWER OFF POWER ON |
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19. |
FUEL |
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20. |
OIL |
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21. |
AIRSPEED LIMITS |
NEVER EXCEED SPEED POWER ON |
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22. |
DATUM |
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23. |
LEVELING MEANS |
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24. |
C.G. RANGE |
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25. |
MAXIMUM WEIGHT |
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26. |
MINIMUM CREW |
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27. |
NUMBER OF SEATS |
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28. |
MAXIMUM BAGGAGE |
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29. |
FUEL CAPACITY |
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30. |
OIL CAPACITY |
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31. |
ROTOR BLADE AND CONTROL MOVEMENTS |
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32. |
MAXIMUM OPERATING ALTITUDE |
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33. |
MAXIMUM OPERATING TEMPERATURE |
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34. |
IMPORT REQUIREMENTS |
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35. |
OPERATING MANUALS |
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36. |
AIRWORTHINESS LIMITATIONS |
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37. |
SERVICE INFORMATION & DOCUMENTS |
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38. |
EQUIPMENT |
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I hereby declare that the above particulars are true in every respect.SIGNATURE OF APPLICANT_________________________DESIGNATION DATE :