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AIRPORT/FACILITY DIRECTORY LEGEND A-12<br />

e.g., T. Aircraft weights higher than given require prior permission from the airport controlling<br />

authority. Applicable codes are:<br />

S - Single wheel type l<strong>and</strong>ing gear (F15), etc.<br />

T - Twin wheel type l<strong>and</strong>ing gear (C9A), etc.<br />

ST - Single T<strong>and</strong>em l<strong>and</strong>ing gear (C130), etc.<br />

SBTT - Single Belly Twin T<strong>and</strong>em l<strong>and</strong>ing gear (KC10), etc.<br />

TT - Twin T<strong>and</strong>em type (includes quadricycle) l<strong>and</strong>ing gear (C141), etc.<br />

TDT - Twin Delta T<strong>and</strong>em l<strong>and</strong>ing gear (C5), etc.<br />

DDT - Double Dual T<strong>and</strong>em type l<strong>and</strong>ing gear (747), etc.<br />

TRT - Triple T<strong>and</strong>em type l<strong>and</strong>ing gear (C17), etc.<br />

TTT - Twin Triple T<strong>and</strong>em type l<strong>and</strong>ing gear (777), etc.<br />

Some USN <strong>and</strong> USMC airports may associate a runway weight bearing capacity with a specific<br />

tire pressure (TP), e.g. S67/TP-400PSI. This indicates the runway weight bearing capacity for<br />

aircraft operating with the specific tire pressure. When a runway weight bearing capacity is<br />

associated with a tire pressure, it is normally lower than the runway weight bearing capacity for<br />

aircraft of the same l<strong>and</strong>ing gear configuration operating with normal tire pressure.<br />

If the above information is not available, the following data may be shown:<br />

SWL - Single Wheel Loading (includes information submitted in terms of Equivalent Single Wheel<br />

Loading (ESWL) <strong>and</strong> Single Isolated Wheel Loading). SWL Figures are shown in thous<strong>and</strong>s of<br />

pounds, the last three figures being omitted.<br />

PSI - Pounds per square inch. PSI is the actual figure expressing maximum pounds per square inch<br />

runway will support.<br />

AUW - All up weight maximum for any aircraft irrespective of l<strong>and</strong>ing gear configuration. AUW<br />

figures are shown in thous<strong>and</strong>s of pounds, the last three figures being omitted.<br />

C54, etc. - Aircraft by type based on past usage when more specific information is not known.<br />

b. The ACN/PCN System is the ICAO st<strong>and</strong>ard method of reporting pavement strength for<br />

pavements with bearing strengths greater than 12,500 pounds. The Pavement Classification<br />

Number (PCN) is established by an engineering assessment of the runway. The PCN is for use in<br />

conjunction with an Aircraft Classification Number (ACN). Consult the Aircraft Flight Manual, FIH,<br />

or other appropriate source for ACN tables or charts. Currently, ACN data may not be available<br />

for all DoD aircraft. If an ACN table or chart is available, the ACN can be calculated by taking into<br />

account the aircraft weight, the pavement type, <strong>and</strong> the subgrade category. For runways that<br />

have been evaluated under the ACN/PCN system, the PCN will be shown as a five part code (e.g.<br />

PCN 80 R/B/W/T). Details of the coded format are as follows:<br />

(1) The PCN NUMBER - The reported PCN indicates that an aircraft with an ACN equal or less<br />

than the reported PCN can operate on the pavement subject to any limitation on the tire<br />

pressure.<br />

(2) The type of pavement:<br />

R - Rigid<br />

F - Flexible<br />

(3) The pavement subgrade category:<br />

A- High<br />

B - Medium<br />

C - Low<br />

D - Ultra-low<br />

(4) The maximum tire pressure authorized for the pavement:<br />

W - High, no limit<br />

X - Medium, limited to 217 psi<br />

Y - Low, limited to 145 psi<br />

Z - Very low, limited to 73 psi

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