Term
| What side of the DD Form 365-4 Form F should be completed for the TH-67? |
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Definition
| The transport side of the DD Form 365-4 Form F should be completed for the TH-67. |
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Term
| Where can the basic weight and moment data be obtained for completing a DD Form 365-4? |
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Definition
| Basic weight and moment data can be obtained from the last entry on DD Form 365-3 Chart C in the file folder or from reference 1 on a current DD Form 365-4 Form F in the logbook or flight planning area. |
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Term
| Should the fire extinguisher and first aid kit's weight and moment be placed in the emergency equipment line reference 6? |
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Definition
| The TH-67's emergency equipment is already included in the basic weight entry. |
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Term
| Can the aircraft be flown at operating weight (reference 9)? |
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Definition
| No, the aircraft is missing usable fuel at the term operating weight. |
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Term
| Is the term zero fuel weight (reference 14) required to be computed for the TH-67? |
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Definition
| Zero fuel weight is required to be computed for the TH-67. |
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Term
| If temporary or permanent changes are made in the aircraft's basic weight, can the aircraft be flown? |
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Definition
| The aircraft cannot be flown unless temporary or permanent changes are accounted for. |
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Term
| What is the limitations section of DD Form 365-4 Form F used for? |
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Definition
| It is used to provide the pilot with data to make an informed decision in the event of mission changes and also to verify that the aircraft is within weight and CG limitations. |
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Term
| What is the pilot's rule of thumb for gross weight changes? |
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Definition
| For every 30 pounds change in gross weight expect a change of 1% torque. |
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Term
| Other than gross weight, what are other considerations for mission changes at the landing phase of the mission? |
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Definition
| Space and fuel are additional considerations in addition to gross weight for mission changes during the landing phase of the mission. |
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Term
| Which three critical gross weights are used to determine the forward and aft CG limits? |
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Definition
| The three critical gross weights that are used to determine the forward and aft CG limits are takeoff, landing, and zero fuel gross |
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