AMMAUK Session

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• AMMA-UK Session
• Leeds 5th July 2005
• Items for Discussion
• Aircraft Instrument Fit
• Instrumentation
• a. Responsible people
• b. Instrument forms
• Division of flight hours according to IOP
• Logistics
• a. Recce report
• b. Location of aircraft
• c. Location of GCs
• d. Accommodation
• e. No. of people on detachment
• f. Transport in Niamey
• g. Flights to Niamey
• h. Shipping
• i. Gases
• j. Communications (internet, phones)

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Comparing the AMMA fit to that of ITOP, there are
the following additional items the butty box
34 kg a complete CCN/CNC/FWVS rack 100 kg Cloud
Physics rack 220 kg SWS/SHIMS rack 192
kg AVAPS rack 126 kg dropsondes 30 kg LIDAR
500 kg 1 pair of seats  31 kg 1 life raft 34
kg dropsonde launch tube 14 kg which totals
1281 kg. The basic aircraft weight for ITOP
28973 kg Giving a  basic aircraft weight for AMMA
30254 kg
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Seat Person FD1 Pilot FD2 Co-pilot FD3 Mission
Scientist 1 C1 Perox/HCHO C2 FAGE C3 PTR C4 Core
Chem C5 SWS C6 PERCA C7 Dropsondes C8 NOxy C9 AMS
C10 PSAP/Filters C11 PAN/WAS C12 Cloud
physics C13 Mission Scientist 2 C14 Flight
Manger C15 Cabin Crew Manager
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HG
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