Development of a Small Aircraft Runway Length Analysis Tool (2022)

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79 8 APPENDIX B – AIRCRAFT DATA USED IN SARLAT This section contains tables with airport design information for the aircraft included in the SARLAT. There are three tables containing relevant aircraft information by engine type. Table 22 shows general information of piston-powered aircraft included in SARLAT. Table 23 shows general information of turboprop aircraft included in SARLAT. Table 24 shows general information of turbofan-powered aircraft included in SARLAT. Table 22: Piston-Powered Aircraft Included in the SARLAT. Aircraft Name FAA Type Designator Engine Type Aircraft Design Group (ADG) Aircraft Approach Category (AAC) Number of Engines Operating Empty Weight (lbs) Useful Load (lbs) Maximum Takeoff Weight (lbs) Maximum Allowable Landing Weight (lbs) Takeoff Flap Settings Landing Flap Settings Takeoff Distance Criteria in SARLAT Maximum Number of Seats Beechcraft 55 Baron BE55 Piston I B 2 3236 1864 5100 5100 Up Down Accelerate stop distance5 6 Beechcraft 58 Baron BE58 Piston I B 2 4000 1400 5400 5400 Up Down Accelerate stop distance4 6 Cessna 150 C150 Piston I A 1 1111 489 1600 1600 Up 40° Takeoff distance (short field) 2 Cessna 152 C152 Piston I A 1 1101 569 1670 1670 10° 30° Takeoff distance 2 5 Accelerate-stop-distance for a twin-engine piston aircraft is not eligible for Airport Improvement Program funds under current policy. Appendix D provides information about the differences between takeoff and accelerate-stop-distances for twin-engine piston aircraft. SARLAT provides accelerate-stop-distances as an option to be evaluated by airport operators for consideration of local funding for a desired runway length. Many operators of twin-engine piston aircraft use accelerate-stop-distance in their flight planning analysis.

80 (short field) Cessna 172 Skyhawk C172 Piston I A 1 1419 881 2300 2300 Up 40° Takeoff distance (short field) 4 Cessna 177 Cardinal C177 Piston I A 1 1533 967 2500 2500 15° 30° Takeoff distance (short field) 4 Cessna 180 Skywagon C180 Piston I A 1 1643 1157 2800 2800 20° 40° Takeoff distance (short field) 6 Cessna 182 Skylane C182 Piston I A 1 1700 1250 2950 2950 20° 40° Takeoff distance (short field) 4 Cessna 310 C310 Piston I B 2 3347 2153 5500 5400 Up 35° Accelerate stop distance5 6 Cessna 340 C340 Piston I B 2 3966 2024 5990 5990 Up 45° Accelerate stop distance6 6 Cessna 402B C402 Piston I B 2 4038 2262 6300 6200 Up 45° Accelerate stop distance5 6 6 Accelerate-stop-distance for a twin-engine piston aircraft is not eligible for Airport Improvement Program funds under current policy. Appendix D provides information on the differences between takeoff and accelerate-stop-distances for twin-engine piston aircraft. SARLAT provides accelerate-stop-distances as an option to be evaluated by airport operators for consideration of local funding for a desired runway length. Most operators of twin-engine piston aircraft use accelerate-stop-distance in their flight planning analysis.

81 Cessna 421 Golden Eagle C421 Piston I B 2 4640 2810 7450 7200 Up 45° Accelerate stop distance5 Cessna Columbia 400 COL4 Piston I A 1 2500 1100 3600 3420 12° 40° Takeoff over 50ft obstacle (short field) 4 Cessna T206 Turbo Stationair T206 Piston I A 1 2304 1296 3600 3600 20° 40° Takeoff distance (short field) 6 Cessna T210 Turbo Centurion T210 Piston I A 1 2237 1763 4000 3800 10° 30° Takeoff distance (short field) 6 Cirrus SR 20 SR20 Piston I A 1 2122 1028 3150 3150 50% flaps 100% Takeoff Distance 4 Cirrus SR 22 SR22 Piston I A 1 2272 1328 3600 3600 50% flaps 100% Takeoff Distance 4 Cirrus SR 22 Turbo S22T Piston I A 1 2354 1246 3600 3600 50% flaps 100% Takeoff Distance 4 Diamond 40 Star DA40 Piston I A 1 1746 900 2646 2407 TO LDG Takeoff over 50ft obstacle 4 Diamond 42 Twin Star DA42 Piston I A 2 2574 1174 3748 3748 Up LDG Takeoff over 50ft obstacle7 4 7 Diamond does not report accelerate-stop-distance for the DA-42 Twin Star like larger cabin-class twin-engine piston aircraft. SARLAT reports takeoff distance.

82 Flight Design CTLS FDCT Piston I A 1 816 504 1320 1320 15° 30° Takeoff Distance 2 Mooney M20J M20P Piston I A 1 1640 1260 2900 2900 15° 33° Normal Takeoff Distance 4 Mooney M20V Acclaim Ultra M20T Piston I A 1 2319 1049 3368 3200 10° 33° Takeoff over 50ft obstacle 4 Piper 24 Comanche PA24 Piston I A 1 1455 1095 2550 2550 0° 27° Takeoff over 50ft obstacle 5 Piper 28B Dakota P28B Piston I A 1 1610 1390 3000 3000 25° 40° Takeoff over 50ft obstacle 4 Piper 30 Twin Comanche PA30 Piston I B 2 2207 1393 3600 3600 Retracted 27° Accelerate stop distance 6 Tecnam P2006T P06T Piston I A 2 1587 1014 2601 2601 TO Full Takeoff Distance 4 Vans RV 12 RV12 Piston I A 1 740 580 1320 1320 Fully extended Fully extended Takeoff over 50ft obstacle 2

83 Table 23: Turboprop-Powered Aircraft Included in the SARLAT. Aircraft Name FAA Type Designator Engine Type Aircraft Design Group (ADG) Aircraft Approach Category (AAC) Number of Engines Operating Empty Weight (lbs) Useful Load (lbs) Maximum Takeoff Weight (lbs) Maximum Allowable Landing Weight (lbs) Takeoff Flap Settings Landing Flap Settings Takeoff Distance Criteria Maximum Number of Seats Beechcraft B200 King Air BE20 Turboprop II B 2 8805 3695 12500 12500 Approach 100% Extended Accelerate stop distance 15 Beechcraft C90 King Air BE9L Turboprop II B 2 7235 3250 10485 9832 Approach Down Takeoff over 50ft obstacle 10 Beechcraft King Air 350ER B350 Turboprop II B 2 10385 6115 16500 15675 Approach Down Takeoff field length 17 Cessna 208 Caravan C208 Turboprop II A 1 4305 3695 8000 7800 20° 30° Takeoff distance (short field) 11 Pilatus PC 12 NG PC12 Turboprop II B 1 6173 4277 10450 9921 30° 40° Takeoff over 50ft obstacle 11 Piper 46 Malibu Meridian P46T Turboprop I A 1 3677 1415 5092 4850 20° 36° Takeoff over 50ft obstacle 6 Rockwell Commander 690B AC90 Turboprop I B 2 6195 4130 10325 9675 0° 40° Accelerate stop distance 7 Socata TBM 700 TBM7 Turboprop I A 1 4050 2529 6579 6250 TO LDG Takeoff Distance 6 Socata TBM 850 TBM8 Turboprop I A 1 4789 2605 7394 7024 TO LDG Takeoff Distance 6

84 Table 24: Turbofan-Powered Aircraft Included in the SARLAT. Aircraft Name FAA Type Designator Engine Type Aircraft Design Group (ADG) Aircraft Approach Category (AAC) Number of Engines Operating Empty Weight (lbs) Useful Load (lbs) Maximum Takeoff Weight (lbs) Maximum Allowable Landing Weight (lbs) Takeoff Flap Settings Landing Flap Settings Takeoff Distance Criteria in SARLAT Maximum Number of Seats Cessna 560 XL C56X Jet II B 2 12860 7340 20200 18700 15° 35° Takeoff field length 9 Cessna CitationJet 1 C525 Jet II B 2 7000 3400 10400 9700 15° Land Takeoff field length 8 Cessna CitationJet 3 C25B Jet II B 2 8760 5110 13870 12750 15° 35° Takeoff field length 9 Honda Jet 420 Elite HDJT Jet I B 2 7153 3547 10700 9960 TO/APPR LDG Takeoff field length 8 Phenom 300 E55P Jet II B 2 11583 6385 17968 16865 Flaps 2 Full Minimum Required Runway Length 11