TM 55-6930-212-10 Table 8-5.  Facility-Centered Approach Plots SELECT LOCATION CALL LATITUDE LONGITUDE NOTE Approach plot data is subject to change according to gaming area and training requirements. 031 TODENDORF TDF N35 50 04 W56 49 24 032 CAIRNS OZ N31 15 00 W85 42 00 033 DANNELLY MGM N32 19 30 W86 24 00 034 DOTHAN DHN N31 15 00 W85 25 00 035 HANCHEY HEY N31 21 00 W85 32 00 036 LAWSON LS N32 15 48 W84 55 50 037 PANAMA CITY IPFN N30 13 00 W85 41 00 038 PENSACOLA PN N30 25 30 W87 15 00 039 TALLAHASSEE ITLH N30 24 00 W84 21 00 040 TROY TOI N31 49 52 W86 06 52 Table 8-6.  Landing Area Beacons TYPE IDENTIFICATION FREQUENCY ELEVATION LATITUDE LONGITUDE CLA XLW 329 512 N35 37 34 W57 00 29 PLA XPN 374 1352 N35 42 54 W57 16 07 CLA AVN 333 512 N35 26 12 W57 17 00 CLA WGR 370 512 N35 44 48 W57 22 05 MA XBZ 264 512 N35 55 08 W57 26 14 MA XAE 388 512 N35 22 53 W56 51 46 MA XFR 341 512 N35 42 38 W57 09 38 MA XGY 382 512 N35 27 22 W57 30 19 CLA XMD 352 1612 N35 28 56 W57 29 28 CLA TBS 390 1612 N35 50 05 W57 32 16 CLA DRG 350 512 N35 31 37 W56 55 11 MA XDR 231 512 N35 23 05 W57 10 48 AAF GPM 310 512 N35 20 05 W57 27 18 CLA XBB 239 612 N35 50 38 W57 20 57 AAF TDF 320 512 N35 50 04 W56 49 24 PLA - Pinnacle area; CLA = Confined landing area; MA = Marshalling area: AAF = Army airfield Table 8-7.  Sling Load Characteristics Load CRT Item Weight Sling Hook No. page Load Type simulated (lb) (feet) preference 1 061 Light load Two fuel bladders 7,008 14 Any 2 062 Light load Two fuel bladders 7,008 14 Any 3 063 Light load Two fuel bladders 7,008 14 Any 4 064 High-density load M-198 Howitzer 18.000 12 CTR 5 065 Aerodynamic load AH-64 Apache 11,015 20 CTR 6 066 Tandem load Military van 20,000 16 FWD 14 AFT 8-20