FAA-APPROVED Airplane Flight Manual Supplement
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Aero Twin, Inc Honeywell TPE331-12JR 2403 Merrill Field Dr Aircraft Flight Manual Supplement Anchorage, AK 99501 (907)274-6166 FAA-APPROVED Airplane Flight Manual Supplement for Cessna 208 Aircraft Equipped with Honeywell TPE331-12JR Engine Doc. No. 850-AFMS Reg. No. _______________ Serial. No. _______________ This supplement must be attached to the FAA Approved Pilot’s Operating Handbook when the Honeywell TPE331-12JR engine is installed on the airplane in accordance with Aero Twin, Inc. STC SAXXXXAK. The information contained in this document supplements or supersedes the basic manual and applicable appendices only in those areas listed. For limitations, procedures, and performance information not contained in this supplement, consult Cessna’s basic Pilot’s Operating Handbook and/or Wipline’s Pilot’s Operating Handbook Supplement 8 for the aircraft equipped with Wipline gross weight increase STC SA270CH. FAA-Approved:__________________ Manager, Anchorage Aircraft Certification Office Federal Aviation Administration Anchorage, Alaska Date: __________ THIS AFMS COPY IS FOR REFERENCE ONLY. THIS AFMS COPY IS NOT CONTROLLED. THIS AFMS COPY IS NOT APPROVED FOR COPY OR DISTRIBUTION WITHOUT THE SPECIFIC CONSENT OF AERO TWIN INC. DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, Dated: September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement General Information GENERAL INFORMATION SPEED (KTAS): Maximum Cruise at 10,000 FT ......................................................... 190 KNOTS Maximum Cruise at 20,000 FT ......................................................... 181 KNOTS RANGE: With 2224 pounds usable fuel and fuel allowance for engine start, taxi, takeoff, climb, descent and 45 minutes reserve. Max Cruise at 10,000 FT .................................................... 855 NM 4.4 HRS Max Cruise at 20,000 FT .................................................... 1094 NM 5.8 HRS Max Range at 10,000 FT .................................................... 1033 NM 7.2 HRS Max Range at 20,000 FT .................................................... 1224 NM 10.0 HRS RATE OF CLIMB AT SEA LEVEL ................................................................ 1460 FPM MAXIMUM OPERATING ALTITUDE ......................................................... 25,000 FT TAKEOFF PERFORMANCE: Ground Roll ............................................................................................. 1025 FT Total Distance Over 50 FT Obstacle ....................................................... 1951 FT MAXIMUM WEIGHT: Ramp ..................................................................................................... 8395 LBS Takeoff .................................................................................................. 8360 LBS Landing ................................................................................................. 7800 LBS STANDARD EMPTY WEIGHT ...................................................................... 4085 LBS MAXIMUM USEFUL LOAD .......................................................................... 4275 LBS OIL CAPACITY .................................................................................................. 12 QTS ENGINE: Honeywell ..................................................................... TPE331-12JR-701S Fixed Shaft Turbine Flat Rated at 850 Shaft Horsepower PROPELLER: Hartzell 4-Bladed, Constant Speed, Full Feathering, Reversible. Diameter ................................................................................................... 109.5 IN NOTE The above performance figures are based on indicated weights; standard atmospheric conditions; level, hard surfaced, dry runways; and no wind. They are calculated values derived from flight tests conducted by Aero Twin, Inc. under carefully documented conditions and will vary with individual airplanes and numerous factors affecting performance. Performance for other operational conditions can be derived by reference to operational data in other sections of this supplement. DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page ii Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Contents TABLE OF CONTENTS SECTION GENERAL ................................................................................... 1 LIMITATIONS ........................................................................... 2 EMERGENCY PROCEDURES ................................................. 3 NORMAL PROCEDURES ......................................................... 4 PERFORMANCE ........................................................................ 5 WEIGHT & BALANCE/EQUIPMENT LIST ............................ 6 AIRPLANE & SYSTEMS DESCRIPTION ................................ 7 HANDLING, SERVICE & MAINTENANCE ........................... 8 The following adjuncts to the text are used to highlight or emphasize important points: WARNING : Calls attention to use of methods, procedures, or limits which must be followed precisely to avoid injury or death to persons. CAUTION: Calls attention to methods, procedures, or limits which must be followed to avoid damage to equipment. NOTE: Calls attention to additional procedures or information pertaining to the text. DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page iii Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance SUPPLEMENT SECTION 5 PERFORMANCE TABLE OF CONTENTS Page Introduction .................................................................................................................. 5-2 Figure 5-1 SRL Off EGT Limit ............................................................................... 5-3 Figure 5-2 Minimum Takeoff Torque ..................................................................... 5-4 Figure 5-3 Minimum Takeoff EGT ......................................................................... 5-5 Figure 5-4 Takeoff Distance – Short Field ............................................................. 5-6 Figure 5-5 Takeoff Distance – Flaps Up ................................................................. 5-7 Figure 5-6 Rate Of Climb – Takeoff Flap Setting .................................................. 5-8 Figure 5-7 Maximum Rate Of Climb – Flaps Up ................................................... 5-9 Figure 5-8 Cruise Climb – Flaps Up – 120 KIAS ................................................. 5-10 Figure 5-9 Rate of Climb – Balked Landing ......................................................... 5-11 Figure 5-10 Time, Fuel, And Distance To Climb - Maximum Rate Of Climb ....... 5-12 Figure 5-11 Time, Fuel, And Distance To Climb - Cruise Climb – 120 KIAS ...... 5-13 Figure 5-12 Cruise Performance – Notes ................................................................ 5-14 Cruise Performance – 2000 Feet ....................................................................... 5-15 Cruise Performance – 4000 Feet ....................................................................... 5-16 Cruise Performance – 8000 Feet ....................................................................... 5-17 Cruise Performance – 12000 Feet ..................................................................... 5-18 Cruise Performance – 16000 Feet ..................................................................... 5-19 Cruise Performance – 20000 Feet ..................................................................... 5-20 Cruise Performance – 24000 Feet ..................................................................... 5-21 Figure 5-13 Landing Distance ................................................................................. 5-22 DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 5-1 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance INTRODUCTION The information presented in the Introduction, Use of Performance Charts, and Sample Problem paragraphs in Section 5 of the basic handbook is applicable to the 850 horsepower TPE331-12JR powered aircraft. Using this information, and the performance charts in this supplement, complete flight planning may be accomplished. For information not contained in this supplement, refer to the basic Flight Manual. WARNING To ensure that performance in this section can be duplicated, the airplane and engine must be maintained in good condition. Pilot proficiency and proper preflight planning using data necessary for all flight phases is also required to assure expected performance with ample margins of safety. It should be noted that the cruise performance information presented in these charts are based on the fuel consumption and power expected from a nominal performance engine. You may observe fuel burns that vary plus or minus 10% depending on the quality and age of your engine. Takeoff, climb, and landing data has been computed from actual flight tests using average piloting techniques and an airplane with an engine in good condition. However, performance below crossover altitude is not expected to be degraded appreciably by extended engine life because the engine is derated and should always be capable of producing 850 horsepower. In some cases, performance charts in this section include data for temperatures which are outside of the operating limits. This data has been included to aid in interpolation. DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 5-2 Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance SRL OFF EGT LIMITS The following graph provides EGT limits for when the SRL is either turned off or inoperative. Anytime the SRL OFF annunciator is illuminated, figure 5-1 should be used to determine the EGT limit corresponding to the indicated outside air temperature and engine speed. Note that the 100% engine torque limit is still applicable with the SRL off, and must not be exceeded. 650 COMPENSATED EGT - SRL OFF (ºC) 640 630 620 610 600 100% RPM 590 580 570 560 96% RPM 550 540 530 520 510 500 -60 -50 -40 -30 -20 -10 0 10 20 30 40 50 60 INDICATED OUTSIDE AIR TEMPERATURE (ºC) Figure 5-1. SRL Off EGT Limit vs. OAT and Engine Speed DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 5-3 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance TARGET TAKEOFF TORQUE Figure 5-2 provides the target takeoff torque for given pressure altitudes and outside air temperatures. If the engine is temperature limited and the indicated EGT at maximum power is 650ºC, then the torque during the takeoff roll must be at least the value found in figure 5-2 for your current altitude and OAT. If the maximum torque is not achieved at maximum power prior to takeoff, the takeoff must be aborted and the aircraft returned to maintenance. CONDITIONS: 100% Engine Speed 0-60 KIAS 105 100 % ENGINE TORQUE 95 90 12000 85 10000 80 8000 75 6000 4000 70 2000 65 Sea Level 60 -40 -30 -20 -10 0 10 20 30 40 50 60 OUTSIDE AIR TEMPERATURE (ºC) Figure 5-2. Minimum Takeoff Torque vs. Pressure Altitude and OAT DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 5-4 Original Issue, September 2, 2006 LIFT OFF 72 72 70 WEIGHT LBS 8360 8000 7600 80 82 82 AT 50 FT TAKEOFF SPEED KIAS SL 2000 4000 6000 8000 10000 12000 SL 2000 4000 6000 8000 10000 12000 SL 2000 4000 6000 8000 10000 12000 PRESS ALT FT CONDITIONS: Flaps 20º 100% RPM 100% Torque or 650ºC EGT Cabin Heat – Off Zero Wind Paved, Level, Dry Runway 708 798 904 1031 1176 1426 1739 796 898 1017 1160 1323 1604 1957 881 933 1125 1283 1464 1775 2165 GRND. RUN FT. 1357 1521 1715 1938 2200 2660 3259 1526 1711 1929 2181 2476 2994 3667 TOTAL FT TO CLEAR 50 FT O 1689 1894 2135 2413 2740 3312 4058 -10º C 1437 1617 1822 2062 2411 2948 3614 1617 1819 2050 2320 2712 3317 4067 TOTAL FT TO CLEAR 50 FT O 1789 2013 2269 2567 3001 3670 4500 799 903 1028 1176 1425 1743 2131 899 1016 1157 1323 1603 1962 2398 995 1124 1280 1464 1774 2171 2654 GRND. RUN FT. 1523 1713 1933 2199 2677 3274 4025 1714 1927 2176 2475 3012 3684 4529 TOTAL FT TO CLEAR 50 FT O 1896 2133 2407 2738 3333 4076 5011 10º C Figure 5-3. Takeoff Distance 752 850 964 1098 1288 1575 1923 846 956 1085 1236 1449 1772 2164 937 1058 1201 1368 1603 1961 2395 GRND. RUN FT. 0º C 847 959 1092 1318 1597 1960 2551 953 1079 1229 1483 1797 2205 2870 1055 1194 1360 1641 1989 2440 3176 GRND. RUN FT. 1611 1813 2049 2481 3023 3710 4812 1813 2040 2305 2792 3401 4175 5415 TOTAL FT TO CLEAR 50 FT O 2006 2258 2551 3089 3763 4620 5992 20º C 896 1032 1245 1509 2085 2262 2783 1008 1162 1401 1698 2346 2545 3131 1116 1285 1550 1879 2596 2817 3465 GRND. RUN FT. 1701 1945 2359 2875 3925 4336 5361 1914 2188 2655 3236 4417 4879 6032 TOTAL FT TO CLEAR 50 FT O 2118 2422 2937 3580 4887 5399 6674 30º C 987 1190 1443 1754 2126 - 1110 1340 1624 1973 2392 - 1229 1482 1797 2183 2646 - GRND. RUN FT. 1878 2277 2775 3392 4123 - 2113 2562 3122 3816 4639 - TOTAL FT TO CLEAR 50 FT O 2338 2835 3455 4223 5134 - 40º c NOTES: 1. Decrease distance 10% for each 11 knots headwind. For operation with tailwinds up to 10 knots, increase distances by 10% for each 2.5 knots. 2. For operation on a dry, grass runway, increase distance by 15% of the “ground roll” figure. 3. Where distance values have been replaced by dashes, operating temperature limits of the airplane would be greatly exceeded. Those distances which are included but the operation slightly exceeds the temperature limit are provided for interpolation purposes only. TAKEOFF DISTANCE SHORT FIELD Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 5-5 LIFT OFF 89 89 89 WEIGHT LBS 8360 8000 7600 104 104 104 AT 50 FT TAKEOFF SPEED KIAS SL 2000 4000 6000 8000 SL 2000 4000 6000 8000 SL 2000 4000 6000 8000 PRESS ALT FT CONDITIONS: Flaps 0º 100% RPM 100% Torque or 650ºC EGT Cabin Heat – Off Zero Wind Paved, Level, Dry Runway 1239 1394 1580 1787 2030 1394 1569 1777 2011 2284 1542 1736 1967 2226 2528 GRND. RUN FT. 2008 2249 2537 2856 3232 2259 2531 2854 3214 3637 TOTAL FT TO CLEAR 50 FT O 2500 2801 3158 3556 4024 -10º C 2126 2391 2692 2034 3510 2392 2691 3029 3414 3949 TOTAL FT TO CLEAR 50 FT O 2647 2977 3352 3778 4370 1395 1578 1782 2020 2463 1570 1775 2006 2273 2771 1738 1965 2219 2516 3066 GRND. RUN FT. 2252 2534 2849 3217 3923 2534 2852 3205 3619 4415 TOTAL FT TO CLEAR 50 FT O 2804 3156 3547 4005 4885 10º C Figure 5-4. Takeoff Distance 1314 1485 1681 1901 2211 1479 1671 1891 2139 2488 1636 1850 2093 2367 2753 GRND. RUN FT. 0º C 1481 1672 1889 2281 2788 1666 1882 2125 2567 3137 1844 2082 2351 2840 3471 GRND. RUN FT. 2384 2680 3016 3645 4475 2682 3015 3393 4102 5035 TOTAL FT TO CLEAR 50 FT O 1968 3337 3755 4539 5572 20º C 1566 1785 2171 2653 3241 1762 2008 2443 2958 3647 1950 2222 2703 3303 4036 GRND. RUN FT. 2516 2851 3483 4270 5244 2831 3208 3919 4805 5900 TOTAL FT TO CLEAR 50 FT O 3133 3550 4337 5317 6529 30º C 1722 2093 2555 3125 3803 1938 2356 2875 3516 4279 2144 2607 3182 3891 4735 GRND. RUN FT. 2770 3382 4145 5088 6208 3117 2806 4664 5725 6985 TOTAL FT TO CLEAR 50 FT O 3449 4211 5161 6335 7730 40º c NOTES: 1. Decrease distance 10% for each 11 knots headwind. For operation with tailwinds up to 10 knots, increase distances by 10% for each 2.5 knots. 2. For operation on a dry, grass runway, increase distance by 15% of the “ground roll” figure. 3. Where distance values have been replaced by dashes, operating temperature limits of the airplane would be greatly exceeded. Those distances which are included but the operation slightly exceeds the temperature limit are provided for interpolation purposes only. TAKEOFF DISTANCE Flaps Up Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 5-6 Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance RATE OF CLIMB – TAKEOFF FLAP SETTING FLAPS 20º CONDITIONS: Takeoff Power 100% RPM Flaps 20º NOTES: 1. Where rate of climb values have been replaced by dashes, an appreciable rate of climb for the weight shown cannot be expected or operating temperature limits of the airplane would be greatly exceeded. Those rates of climb which are included but the operation slightly exceeds the temperature limit are provided for interpolation purposes only. WEIGHT LBS 8360 8000 7600 PRESS ALT FT 0 2000 4000 6000 8000 10000 12000 0 2000 4000 6000 8000 10000 12000 0 2000 4000 6000 8000 10000 12000 CLIMB SPEED KIAS 92 92 91 91 90 90 89 91 91 90 90 89 89 88 90 90 89 89 88 88 87 RATE OF CLIMB - FPM -20º C 1441 1400 1352 1292 1245 1242 1140 1503 1460 1410 1348 1298 1296 1189 1578 1533 1481 1415 1363 1361 1248 0º C 1357 1310 1261 1204 1113 1021 927 1416 1366 1316 1256 1160 1065 967 1487 1434 1381 1318 1218 1118 1015 20º C 1267 1222 1177 1003 830 749 668 1322 1275 1228 1046 866 781 697 1388 1338 1289 1098 909 820 732 40º C 1111 936 766 587 442 1159 977 799 612 442 1217 1025 839 643 485 - Figure 5-5. Rate of Climb – Takeoff Flap Setting DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 5-7 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance MAXIMUM RATE OF CLIMB CONDITIONS: 100% RPM 100% TORQUE or 650ºC EGT Flaps – Up NOTES: 1. Where rate of climb values have been replaced by dashes, an appreciable rate of climb for the weight shown cannot be expected or operating temperature limits of the airplane would be greatly exceeded. Those rates of climb which are included but the operation slightly exceeds the temperature limit are provided for interpolation purposes only. WEIGH T LBS 8360 8000 7600 PRESS ALT FT. SL 4000 8000 12000 16000 20000 24000 SL 4000 8000 12000 16000 20000 24000 SL 4000 8000 12000 16000 20000 24000 CLIMB SPEED KIAS 107 106 105 102 98 94 90 106 105 104 101 97 93 89 106 104 103 100 96 92 87 RATE OF CLIMB - FPM -40º C 1748 1595 1429 1427 1096 743 361 1823 1664 1490 1489 1143 775 376 1914 1747 1565 1563 1200 814 395 -20º C 1651 1495 1328 1164 847 525 169 1722 1559 1385 1214 883 548 177 1808 1637 1455 1275 927 575 185 0º C 1565 1401 1203 924 638 344 1633 1461 1255 964 666 359 1714 1534 1318 1012 699 377 - 20º C 1473 1307 885 641 393 1536 1363 923 668 410 1613 1432 969 702 430 - 40º C 1315 865 455 387 1372 902 475 403 1441 947 498 424 - Figure 5-6. Maximum Rate of Climb DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 5-8 Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance CRUISE CLIMB 120 KIAS CONDITIONS: 100% RPM 100% TORQUE or 650ºC EGT Flaps – Up NOTES: 1. Where rate of climb values have been replaced by dashes, an appreciable rate of climb for the weight shown cannot be expected or operating temperature limits of the airplane would be greatly exceeded. Those rates of climb which are included but the operation slightly exceeds the temperature limit are provided for interpolation purposes only. WEIGH T LBS 8360 8000 7600 RATE OF CLIMB - FPM PRESS ALT FT. SL 2000 4000 6000 8000 10000 12000 SL 2000 4000 6000 8000 10000 12000 SL 2000 4000 6000 8000 10000 12000 -20º C 1555 1525 1466 1387 1302 1290 1103 1622 1591 1529 1447 1358 1346 1151 1704 1670 1605 1519 1426 1413 1208 0º C 1459 1431 1368 1292 1184 1023 847 1522 1493 1427 1348 1235 1067 883 1598 1568 1498 1415 1297 1120 927 20º C 1369 1334 1277 1088 841 692 561 1428 1392 1332 1135 877 722 585 1499 1461 1398 1192 921 758 615 40º C 1217 1023 808 577 357 1269 1067 842 602 373 1332 1120 885 632 391 - Figure 5-7. Cruise Climb – 120 KIAS DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 5-9 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance RATE OF CLIMB – BALKED LANDING FLAPS 30º CONDITIONS: 100% RPM 100% TORQUE or 650ºC EGT Flaps – 30º WEIGH T LBS 7800 7300 6800 PRESS ALT FT. 0 2000 4000 6000 8000 10000 12000 0 2000 4000 6000 8000 10000 12000 0 2000 4000 6000 8000 10000 12000 CLIMB SPEED KIAS 83 83 83 82 82 82 81 83 82 82 81 81 81 80 82 81 81 81 80 80 79 RATE OF CLIMB - FPM -20º C 1427 1415 1371 1306 1261 1247 1149 1518 1505 1459 1390 1342 1327 1222 1622 1608 1559 1485 1434 1418 1306 0º C 1338 1322 1278 1213 1116 1027 942 1424 1407 1360 1291 1187 1093 1002 1522 1503 1453 1380 1269 1167 1071 20º C 1250 1233 1189 1007 845 764 686 1330 1312 1265 1072 899 813 730 1421 1402 1351 1145 960 868 780 40º C 1089 947 779 601 488 454 449 1159 1008 829 640 519 483 477 1239 1077 885 683 554 516 510 Figure 5-8. Rate of Climb – Balked Landing DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 5-10 Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance TIME, FUEL, AND DISTANCE TO CLIMB MAXIMUM RATE OF CLIMB CONDITIONS: 100% RPM 100% TORQUE or 650ºC EGT Flaps – Up NOTES: 1. Add 35 pounds of fuel for engine start, taxi, and takeoff allowance. 2. Distances shown are based on zero wind. 20º C BELOW STANDARD TEMP. WEIGHT LBS 8360 8000 7600 PRESS ALT FT. SL 4000 8000 12000 16000 20000 24000 SL 4000 8000 12000 16000 20000 24000 SL 4000 8000 12000 16000 20000 24000 CLIMB SPEED KIAS 107 106 105 102 98 94 90 106 105 104 101 97 93 89 106 104 103 100 96 92 87 STANDARD TEMPERATURE 20º C ABOVE STANDARD TEMP. CLIMB FROM SEA LEVEL TIME MIN 0 3 5 8 12 16 23 0 3 5 8 11 16 22 0 2 5 8 11 15 21 FUEL LBS 0 22 44 67 92 119 152 0 21 43 64 88 114 145 0 20 41 61 84 109 138 DIST NM 0 5 10 15 22 32 44 0 4 9 15 21 30 42 0 4 9 14 20 28 40 TIME MIN 0 3 6 9 14 20 29 0 3 6 9 13 19 28 0 3 5 8 13 18 26 FUEL LBS 0 23 47 72 101 135 178 0 22 45 69 97 130 171 0 21 43 66 92 123 163 DIST NM 0 5 11 18 27 40 59 0 5 10 17 26 38 56 0 5 10 16 24 36 53 TIME MIN 0 3 7 11 18 27 42 0 3 7 11 17 25 40 0 3 6 10 16 24 38 FUEL LBS 0 27 55 86 122 169 237 0 26 52 82 117 162 227 0 24 50 78 112 154 216 DIST NM 0 6 13 23 36 56 90 0 6 13 22 34 53 85 0 5 12 21 32 50 80 Figure 5-9. Time, Fuel, and Distance to Climb – Maximum Rate of Climb DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 5-11 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance TIME, FUEL, AND DISTANCE TO CLIMB CRUISE CLIMB – 120 KIAS CONDITIONS: 100% RPM 100% TORQUE or 650ºC EGT Flaps – Up NOTES: 1. Add 35 pounds of fuel for engine start, taxi, and takeoff allowance. 2. Distances shown are based on zero wind. 20º C BELOW STANDARD TEMP. WEIGHT LBS 8360 8000 7600 PRESS ALT FT. SL 2000 4000 6000 8000 10000 12000 SL 2000 4000 6000 8000 10000 12000 SL 2000 4000 6000 8000 10000 12000 TIME MIN 0 1 3 4 6 7 9 0 1 3 4 5 7 8 0 1 2 4 5 6 8 FUEL LBS 0 11 23 34 46 58 70 0 11 22 33 44 55 67 0 10 21 31 42 53 64 DIST NM 0 3 5 8 11 15 18 0 2 5 8 11 14 17 0 2 5 8 10 13 17 STANDARD TEMPERATURE 20º C ABOVE STANDARD TEMP. CLIMB FROM SEA LEVEL TIME FUEL DIST TIME MIN LBS NM MIN 0 0 0 0 2 3 12 1 3 6 24 3 5 9 36 4 7 13 49 6 10 17 62 8 13 21 76 10 0 0 0 0 2 3 11 2 3 6 23 3 5 9 35 4 7 12 47 6 9 16 60 7 12 21 73 9 0 0 0 0 3 3 11 1 6 5 22 3 10 8 33 4 13 12 45 6 18 15 57 7 23 20 70 9 FUEL LBS 0 14 28 43 59 75 94 0 13 27 41 56 72 90 0 25 52 78 107 138 171 DIST NM 0 3 7 11 16 22 29 0 3 7 11 16 21 28 0 6 13 21 30 40 52 Figure 5-10. Time, Fuel, and Distance to Climb – Cruise Climb DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 5-12 Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance CRUISE PERFORMANCE NOTES The following general information is applicable to all Cruise Performance charts contained in Figure 9, Sheet 2 through 8, in this section: 1. The highest torque shown for each temperature and altitude combination corresponds to the maximum available cruise power expected for that atmospheric condition. For any condition, do not exceed 100% torque or 650ºC EGT, whichever occurs first. 2. With the cabin heat on, fuel flow for a given torque setting will be up to 35 pounds per hour higher. 3. Cruise performance is shown at a maximum gross weight of 8360 pounds. For operation at lower weights, the actual cruise performance will be increased. 4. Some full power settings may result in exceeding the aircraft’s never exceed speed during level flight, particularly at low density altitudes. Do not exceed 175 KIAS at any time. Figure 5-11. Cruise Performance (Sheet 1 of 8) DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 5-13 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance CRUISE PERFORMANCE PRESSURE ALTITUDE 2,000 FEET CONDITIONS: 8360 Pounds 96% RPM NOTE: Do not exceed 100% torque or 650ºC EGT. OAT ºC 45 35 25 15 5 -5 -15 PERCEN T TORQUE 75.7 50 86.4 75 50 98 75 50 100 75 50 100 75 50 100 75 50 100 75 50 FUEL FLOW PPH 396 319 424 388 316 453 383 313 451 377 309 450 379 311 453 383 316 457 387 320 KTAS 172 141 179 170 140 187 168 139 187 166 137 185 164 136 183 162 134 181 160 133 Figure 5-11. Cruise Performance (Sheet 2 of 8) DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 5-14 Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance CRUISE PERFORMANCE PRESSURE ALTITUDE 4,000 FEET CONDITIONS: 8360 Pounds 96% RPM NOTE: Do not exceed 100% torque or 650ºC EGT. OAT ºC 40 30 20 10 0 -10 -20 PERCEN T TORQUE 74.6 50 85.1 75 50 96.7 75 50 100 75 50 100 75 50 100 75 50 100 75 50 FUEL FLOW PPH 380 306 407 375 303 435 369 299 440 367 298 441 369 301 444 373 305 447 376 308 KTAS 175 147 183 174 146 190 172 144 191 170 143 189 168 141 187 167 139 184 165 137 Figure 5-11. Cruise Performance (Sheet 3 of 8) DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 5-15 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance CRUISE PERFORMANCE PRESSURE ALTITUDE 8,000 FEET CONDITIONS: 8360 Pounds 96% RPM NOTE: Do not exceed 100% torque or 650ºC EGT. OAT ºC 30 20 10 0 -10 -20 -30 PERCEN T TORQUE 71.8 50 81.6 75 50 92.1 75 50 100 75 50 100 75 50 100 75 50 100 75 50 FUEL FLOW PPH 347 282 372 351 278 400 347 276 423 348 279 426 352 282 427 354 285 429 357 288 KTAS 170 144 178 172 143 185 170 141 189 168 140 187 167 139 185 165 137 183 163 135 Figure 5-11. Cruise Performance (Sheet 4 of 8) DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 5-16 Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance CRUISE PERFORMANCE PRESSURE ALTITUDE 12,000 FEET CONDITIONS: 8360 Pounds 96% RPM NOTE: Do not exceed 100% torque or 650ºC EGT. OAT ºC 20 10 0 -10 -20 -30 -40 PERCEN T TORQUE 69 50 78 50 85.6 75 50 92.3 75 50 99.4 75 50 100 75 50 100 75 50 FUEL FLOW PPH 317 259 341 257 364 331 259 386 334 262 410 336 265 412 338 267 414 341 271 KTAS 173 152 181 151 186 176 150 190 174 149 194 173 147 192 171 145 190 169 143 Figure 5-11. Cruise Performance (Sheet 5 of 8) DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 5-17 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance CRUISE PERFORMANCE PRESSURE ALTITUDE 16,000 FEET CONDITIONS: 8360 Pounds 96% RPM NOTE: Do not exceed 100% torque or 650ºC EGT. OAT ºC 10 0 -10 -20 -30 -40 -50 PERCEN T TORQUE 65.7 50 72.1 50 77.9 50 84 75 50 90.3 75 50 96.6 75 50 100 75 50 FUEL FLOW PPH 389 242 309 243 328 245 348 320 247 369 322 249 389 324 252 402 327 256 KTAS 177 156 182 154 187 153 192 182 151 197 180 150 202 178 148 203 176 147 Figure 5-11. Cruise Performance (Sheet 6 of 8) DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 5-18 Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance CRUISE PERFORMANCE PRESSURE ALTITUDE 20,000 FEET CONDITIONS: 8360 Pounds 96% RPM NOTE: Do not exceed 100% torque or 650ºC EGT. OAT ºC 0 -10 -20 -30 -40 -50 -54 PERCEN T TORQUE 60.1 50 64.8 50 70 50 75.2 50 80.4 50 85.5 75 50 87.5 75 50 FUEL FLOW PPH 260 229 276 231 293 233 310 234 327 237 345 313 240 353 314 241 KTAS 170 153 174 152 179 150 183 149 187 148 190 179 147 192 178 146 Figure 5-11. Cruise Performance (Sheet 7 of 8) DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 5-19 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance CRUISE PERFORMANCE PRESSURE ALTITUDE 24,000 FEET CONDITIONS: 8360 Pounds 96% RPM NOTE: Do not exceed 100% torque or 650ºC EGT. OAT ºC -10 -20 -30 -40 -50 -54 PERCEN T TORQUE 53.3 50 57.9 50 62.4 50 67.3 50 71.6 50 73.3 50 FUEL FLOW PPH 231 220 245 221 260 222 276 223 291 226 297 227 KTAS 162 162 168 160 175 159 189 158 192 156 193 156 Figure 5-11. Cruise Performance (Sheet 8 of 8) DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 5-20 Original Issue, September 2, 2006 PRESS ALT FT S.L. 2000 4000 6000 8000 S.L. 2000 4000 6000 8000 S.L. 2000 4000 6000 8000 SPEED AR 50 FT KIAS 78 75 72 WEIGHT LBS 7800 7300 6800 CONDITIONS: Flaps 30º Power Lever – Idle after clearing obstacles, BETA (lever against spring) range after touchdown. 100% RPM Maximum Breaking and Reverse Paved, Level, Dry Runway Zero Wind 654 732 823 927 1044 718 804 903 1019 1147 786 880 988 1115 1255 GRD ROLL FT. 2. 3. 4. 1409 1526 1658 1808 1974 1548 1624 1766 1928 2107 1694 1835 1994 2174 2373 TOTAL FT TO CLEAR 50 FT OBS 1467 1591 1732 1889 2055 1612 1693 1845 2015 2194 1764 1912 2082 2270 2470 TOTAL FT TO CLEAR 50 FT OBS 731 823 926 1040 1161 803 904 1017 1143 1275 879 989 1113 1250 1396 GRD ROLL FT. 1523 1659 1806 1968 2141 1676 1767 1925 2100 2286 1834 1994 2171 2365 2573 TOTAL FT TO CLEAR 50 FT OBS 10ºC 774 869 977 1093 1225 850 955 1073 1200 1345 930 1045 1174 1313 1472 GRD ROLL FT. Figure 5-12. Landing Distances 692 775 874 984 1101 760 852 960 1081 1209 832 932 1050 1183 1323 GRD ROLL FT. 0ºC 1587 1726 1879 2043 2230 1744 1839 2004 2181 2383 1908 2074 2258 2456 2681 TOTAL FT TO CLEAR 50 FT OBS 20ºC 817 916 1033 1146 1292 896 1006 1134 1258 1420 981 1101 1241 1377 1554 GRD ROLL FT. 1649 1793 1956 2119 2324 1812 1911 2087 2263 2485 1983 2155 2351 2547 2794 TOTAL FT TO CLEAR 50 FT OBS 30ºC 859 966 1079 1203 1365 944 1060 1185 1322 1499 1033 1160 1297 1447 1641 GRD ROLL FT. 1711 1862 2023 2201 2424 1880 1986 2160 2352 2592 2057 2238 2432 2646 2914 TOTAL FT TO CLEAR 50 FT OBS 40ºC Decrease distances 10% for each 11 knots headwind. For operation in tailwinds up to 10 knots, increase distances by 10% for each 2.5 knots. For operation on a dry, grass runway, increase distances by 40% of the “ground roll” figure. If a landing with flaps up is necessary, increase the approach speed by 18 KIAS and allow for 50% longer distances. Where distance values have been replaced by dashes, operating temperature limits of the airplane would by greatly exceeded. Those distances which are included but the operation slightly exceeds the temperature limit are provided for interpolation purposes only. -10ºC NOTES: 1. MAXIMUM PERFORMANCE LANDING DISTANCE Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 5 Performance DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 5-21 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement SUPPLEMENT SECTION 9 AMPHIBIAN SUPPLEMENT TABLE OF CONTENTS PAGE Subsection 9-1, Amphibian – General ......................................................................... 9-2 Introduction ............................................................................................. 9-2 General Information .................................................................................. 9-3 Subsection 9-2, Amphibian – Limitations ................................................................... 9-4 Introduction ............................................................................................. 9-4 Airspeed Limitations ............................................................................... 9-4 Outside Air Temperature Limits ............................................................. 9-5 Placards ................................................................................................... 9-5 Other Limitations .................................................................................... 9-5 Subsection 9-3, Amphibian – Emergency Procedures ................................................. 9-6 Introduction ............................................................................................. 9-6 Airspeeds for Emergency Operation ....................................................... 9-6 Operational Checklists ............................................................................ 9-7 Subsection 9-4, Amphibian – Normal Procedures ..................................................... 9-10 Introduction ........................................................................................... 9-10 Subsection 9-5, Amphibian – Performance ............................................................... 9-11 Introduction ........................................................................................... 9-11 Takeoff Distance on Water ................................................................... 9-12 Takeoff Distance on Land ..................................................................... 9-13 Rate of Climb – Takeoff Flap Setting ................................................... 9-14 Maximum Rate of Climb ...................................................................... 9-15 Cruise Climb ......................................................................................... 9-16 Rate of Climb – Balked Landing .......................................................... 9-17 Time, Fuel, and Distance to Climb ....................................................... 9-18 Cruise Performance ............................................................................... 9-20 Landing Distance on Water .................................................................. 9-27 Landing Distance on Land .................................................................... 9-28 DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 9-1 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement SUBSECTION 9-1 AMPHIBIAN - GENERAL INTRODUCTION This section, written especially for operators of the Cessna Caravan I amphibian equipped with the Honeywell TPE331-12JR engine, provides information not found in the basic flight manual supplement. It contains procedures and data required for safe and efficient operation of the airplane equipped with Wipline Model 8000 amphibious floats. Information contained in the previous sections of this flight manual supplement, as well as that information contained in the amphibian supplement for the standard amphibious Caravan and the information contained in the Wipline gross weight increase flight manual supplement, is not generally repeated in this section. DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 9-2 Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement GENERAL INFORMATION * SPEED: Maximum Cruise at 10,000 Ft ................................................................ 162 KNOTS Maximum Cruise at 20,000 Ft ................................................................ 165 KNOTS * RANGE: With 2224 pounds usable fuel and fuel allowance for engine start, taxi, takeoff, climb, descent, and 45 minutes reserve. Maximum Cruise at 10,000 Ft ....................................................... 885 NM, 5.3 HRS Maximum Cruise at 20,000 Ft ..................................................... 1151 NM, 6.5 HRS Maximum Range at 10,000 Ft ....................................................... 960 NM, 8.0 HRS Maximum Range at 20,000 Ft ..................................................... 1151 NM, 6.5 HRS RATE OF CLIMB AT SEA LEVEL ................................................................ 1172 FPM MAXIMUM OPERATING ALTITUDE ......................................................... 20,000 FT TAKEOFF PERFORMANCE: ON LAND ON WATER Ground Roll (or Water Run) ............................................ 1089 FT 1527 FT Total Distance Over 50-Foot Obstacle ............................ 2219 FT 2501 FT LANDING PERFORMANCE: Ground Roll (or Water Run) .............................................. 947 FT 1017 FT Total Distance Over 50-Foot Obstacle .............................. 1779 FT 1730 FT STANDARD EMPTY WEIGHT PLUS AMPHIBIAN OPTION ................... 5145 LBS MAXIMUM USEFUL LOAD WITH AMPHIBIAN OPTION ....................... 3215 LBS * Speeds and range are based on gross weight cruise data NOTE The above performance figures are based on indicated weights; standard atmospheric conditions; level, hard surfaced, dry runways or smooth, but non-glassy water; and no wind. They are calculated values derived from flight tests conducted by Aero Twin, Inc. under carefully documented conditions and will vary with individual airplanes and numerous factors affecting performance. Performance for other operational conditions can be derived by reference to operational data in other sections of this supplement. DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 9-3 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement SUBSECTION 9-5 AMPHIBIAN – PERFORMANCE INTRODUCTION The information presented in the Introduction in section 5 of this flight manual supplement is applicable to the amphibian. Using this information and the performance charts in this subsection, complete flight planning may be accomplished. WARNING To ensure that performance in this section can be duplicated, the airplane and engine must be maintained in good condition. Pilot proficiency and proper preflight planning using data necessary for all flight phases is also required to assure expected performance with ample margins of safety. DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 9-11 LIFT OFF 63 62 59 WEIGHT LBS 8360 8000 7600 78 80 80 AT 50 FT TAKEOFF SPEED KIAS CONDITIONS: Flaps 20º 100% RPM 100% Torque or 650ºC EGT Cabin Heat – Off Zero Wind SL 2000 4000 6000 8000 1732 1947 2200 2491 2834 1181 1335 1517 1730 1978 1307 1478 1678 1914 2188 SL 2000 4000 6000 8000 SL 2000 4000 6000 8000 WATER RUN FT. PRESS ALT FT -10º C 1732 1947 2200 2491 2834 1949 2191 2476 2803 3188 2156 2424 2740 3102 3528 TOTAL FT TO CLEAR 50 FT 1837 2073 2339 2655 3105 2067 2333 2632 2987 3494 2287 2581 2912 3306 3866 TOTAL FT TO CLEAR 50 FT 1189 1347 1535 1761 2129 1338 1516 1727 1981 2395 1481 1677 1911 2192 2650 WATER RUN FT. 1950 2199 2486 2836 3442 2194 2474 2798 3191 3875 2428 2738 3096 3531 4286 TOTAL FT TO CLEAR 50 FT 10º C 1263 1432 1633 1969 2385 1421 1611 1838 2216 2684 1573 1783 2034 2452 2970 2067 2329 2638 3191 3883 2325 2621 2969 3591 4369 2573 2900 3285 3973 4835 TOTAL FT TO CLEAR 50 FT 20º C WATER RUN FT. Figure 9-5.1. Takeoff Distance (Sheet 1 of 2) 1117 1267 1438 1643 1926 1257 1426 1618 1849 2167 1391 1578 1790 2046 2398 WATER RUN FT. 0º C 1338 1541 1854 2241 2713 1506 1734 2086 2521 3052 1666 1919 2309 2790 3377 WATER RUN FT. 2183 2501 3025 3678 4478 2457 2814 3404 4138 5038 2718 3114 3767 4579 5575 TOTAL FT TO CLEAR 50 FT 30º C 1471 1769 2135 2590 3123 1655 1991 2403 2915 3514 1832 2203 2659 3225 3888 WATER RUN FT. 2408 2912 3537 4315 5226 2709 3276 3979 4855 5880 2998 3625 4403 5373 6506 TOTAL FT TO CLEAR 50 FT 40ºC NOTES: 1. Decrease distance 10% for each 11 knots headwind. For operation with tailwinds up to 5 knots, increase distances by 5% for each knot. TAKEOFF DISTANCE ON WATER MAXIMUM PERFORMANCE Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 9-12 Original Issue, September 2, 2006 LIFT OFF 71 70 68 WEIGHT LBS 8360 8000 7600 78 80 80 AT 50 FT TAKEOFF SPEED KIAS CONDITIONS: Flaps 20º 100% RPM 100% Torque or 650ºC EGT Cabin Heat – Off Zero Wind Paved, Level, Dry Runway SL 2000 4000 6000 8000 SL 2000 4000 6000 8000 SL 2000 4000 6000 8000 PRESS ALT FT 750 847 959 1095 1250 844 953 1079 1232 1406 934 1054 1194 1363 1556 GRND. RUN FT. -10º C 1543 1729 1949 2206 2504 1736 1946 2193 2482 2818 TOTAL FT TO CLEAR 50 FT OBX 1921 2153 2427 2746 3118 1634 1839 2072 2346 2746 1838 2068 2332 2639 3089 TOTAL FT TO CLEAR 50 FT OBX 2034 2290 2580 2920 3418 848 958 1093 1250 1514 954 1078 1230 1406 1703 1056 1193 1361 1556 1885 GRND. RUN FT. 1732 1947 2201 2505 3046 1949 2191 2477 2819 3428 TOTAL FT TO CLEAR 50 FT OBX 2156 2424 2740 3119 3793 10º C 900 1018 1161 1400 1698 1013 1146 1306 1575 1910 1121 1268 1445 1743 2114 1833 2062 2331 2823 3439 2062 2320 2623 3177 3870 TOTAL FT TO CLEAR 50 FT OBX 2282 2567 2902 3515 4282 20º C GRND. RUN FT. Figure 9-5.1, Takeoff Distance (Sheet 2 of 2) 798 903 1023 1168 1369 898 1016 1151 1314 1540 993 1124 1247 1454 1704 GRND. RUN FT. 0º C 951 1096 1321 1600 1941 1070 1233 1486 1800 2184 1184 1365 1646 1992 2417 GRND. RUN FT. 1933 2215 2680 3264 3983 2175 2493 3016 3672 4482 TOTAL FT TO CLEAR 50 FT OBX 2406 2758 3337 4064 4960 30º C 1047 1263 1530 1859 2247 1178 1421 1721 2092 2528 1303 1572 1905 2315 2798 GRND. RUN FT. 2135 2588 3149 3847 4667 2402 2912 3543 4328 5251 TOTAL FT TO CLEAR 50 FT OBX 2658 3222 3921 4789 5811 40º c NOTES: 1. Decrease distance 10% for each 11 knots headwind. For operation with tailwinds up to 5 knots, increase distances by 5% for each knot. TAKEOFF DISTANCE ON LAND MAXIMUM PERFORMANCE Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 9-13 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement RATE OF CLIMB – TAKEOFF FLAP SETTING FLAPS 20º CONDITIONS: Takeoff Power 100% RPM Flaps 20º NOTES: Where rate of climb values have been replaced by dashes, an appreciable rate of climb for the weight shown cannot be expected or operating temperature limits of the airplane would be greatly exceeded. Those rates of climb which are included but the operation slightly exceeds the temperature limit are provided for interpolation purposes only. WEIGHT LBS 8360 8000 7600 PRESS ALT FT 0 2000 4000 6000 8000 10000 12000 0 2000 4000 6000 8000 10000 12000 0 2000 4000 6000 8000 10000 12000 CLIMB SPEED KIAS 87 86 86 85 85 84 84 86 86 85 85 84 84 83 85 85 84 84 83 83 83 Rate of Climb - FPM -20º C 1279 1230 1162 1087 1041 1034 946 1334 1283 1212 1134 1086 1079 987 1401 1347 1273 1190 1140 1133 1036 0º C 1198 1143 1074 999 905 825 746 1250 1192 1120 1042 944 861 778 1312 1251 1176 1094 991 904 817 20º C 1110 1058 989 804 642 573 499 1158 1103 1031 839 670 598 520 1216 1159 1083 880 703 627 546 40º C 959 784 597 413 273 1000 818 623 431 285 1050 859 654 453 299 - Figure 9-5.2. Rate of Climb – Takeoff Flap Setting DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 9-14 Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement MAXIMUM RATE OF CLIMB CONDITIONS: 100% RPM 100% TORQUE or 650ºC EGT Flaps – Up NOTES: 1. Where rate of climb values have been replaced by dashes, an appreciable rate of climb for the weight shown cannot be expected or operating temperature limits of the airplane would be greatly exceeded. Those rates of climb which are included but the operation slightly exceeds the temperature limit are provided for interpolation purposes only. WEIGHT LBS 8360 8000 7600 PRESS ALT FT 0 4000 8000 12000 16000 20000 0 4000 8000 12000 16000 20000 0 4000 8000 12000 16000 20000 CLIMB SPEED KIAS 98 97 96 94 90 86 97 96 95 93 89 85 96 95 94 92 88 83 Rate of Climb - FPM -20º C 1325 1240 1149 965 595 223 1382 1293 1198 1006 621 233 1451 1358 1258 1057 652 244 0º C 1243 1147 1008 732 397 46 1297 1196 1051 763 415 48 1362 1256 1104 801 435 51 20º C 1148 1058 704 461 156 1198 1103 735 480 163 1258 1158 771 504 171 - 40º C 1111 608 277 150 1159 634 289 156 1217 666 304 164 - Figure 9-5.3. Maximum Rate of Climb DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 9-15 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement CRUISE CLIMB 120 KIAS CONDITIONS: 100% RPM 100% TORQUE or 650ºC EGT Flaps – Up NOTES: 2. Where rate of climb values have been replaced by dashes, an appreciable rate of climb for the weight shown cannot be expected or operating temperature limits of the airplane would be greatly exceeded. Those rates of climb which are included but the operation slightly exceeds the temperature limit are provided for interpolation purposes only. WEIGHT LBS 8360 8000 7600 PRESS. ALT FT 0 2000 4000 6000 8000 10000 12000 0 2000 4000 6000 8000 10000 12000 0 2000 4000 6000 8000 10000 12000 -20º C 1209 1152 1077 990 903 896 719 1261 1202 1124 1033 941 934 750 1324 1262 1180 1084 988 981 787 Rate of Climb - FPM 0º C 20º C 1112 1059 979 895 785 628 463 1160 1104 1022 933 819 655 483 1218 1159 1073 980 860 688 507 1022 961 888 684 442 325 154 1066 1003 927 713 462 339 161 1120 1053 973 749 485 356 169 40º C 870 651 418 179 908 679 436 186 953 713 457 196 - Figure 9-5.4. Cruise Climb – 120 KIAS DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 9-16 Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement RATE OF CLIMB – BALKED LANDING FLAPS 30º CONDITIONS: 100% RPM 100% TORQUE or 650ºC EGT Flaps – Up WEIGHT LBS 8360 8000 7600 PRESS. ALT FT 0 2000 4000 6000 8000 10000 12000 0 2000 4000 6000 8000 10000 12000 0 2000 4000 6000 8000 10000 12000 CLIMB SPEED KIAS 80 79 79 78 78 77 77 79 78 78 77 77 76 76 78 78 77 77 76 76 76 Rate of Climb - FPM -20º C 1092 1055 998 934 893 840 705 1139 1101 1041 974 931 876 735 1196 1156 1093 1023 978 920 772 0º C 1014 968 914 846 760 647 522 1058 1010 953 883 792 675 545 1111 1060 1001 927 832 708 572 20º C 930 887 832 662 521 418 299 970 925 868 690 544 436 311 1018 972 911 725 571 458 327 40º C 781 633 741 303 179 815 660 773 316 187 856 693 812 332 196 - Figure 9-5.5. Balked Landing Rate of Climb DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 9-17 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement TIME, FUEL, AND DISTANCE TO CLIMB MAXIMUM RATE OF CLIMB CONDITIONS: 100% RPM 100% TORQUE or 650ºC EGT Flaps – Up NOTES: 1. Add 35 pounds of fuel for engine start, taxi, and takeoff allowance. 2. Distances shown are based on zero wind. 20º C BELOW STANDARD TEMP. WEIGHT LBS 8360 8000 7600 PRESS ALT FT. SL 4000 8000 12000 16000 20000 SL 4000 8000 12000 16000 20000 SL 4000 8000 12000 16000 20000 CLIMB SPEED KIAS 98 97 96 94 90 86 97 96 95 93 89 85 96 95 94 92 88 83 STANDARD TEMPERATURE 20º C ABOVE STANDARD TEMP. CLIMB FROM SEA LEVEL TIME MIN 0 3 7 10 15 21 0 3 6 10 14 20 0 3 6 9 13 19 FUEL LBS 0 26 53 80 109 148 0 25 50 76 105 144 0 24 48 73 100 137 DIST NM 0 5 11 17 25 37 0 5 10 16 24 36 0 5 10 15 23 33 TIME MIN 0 3 7 12 17 27 0 3 7 11 17 26 0 3 7 11 16 25 FUEL LBS 0 28 57 88 125 178 0 27 55 84 119 171 0 26 52 80 114 163 DIST NM 0 6 12 20 31 50 0 6 12 19 30 47 0 5 11 18 28 44 TIME MIN 0 4 9 15 24 41 0 4 9 14 23 40 0 4 8 14 21 38 FUEL LBS 0 32 70 111 161 254 0 31 67 106 155 243 0 30 64 101 147 232 DIST NM 0 7 16 27 44 80 0 6 15 26 42 76 0 6 14 25 39 71 Figure 9-5.6. Time, Fuel, and Distance to Climb – Maximum Rate of Climb DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 9-18 Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement TIME, FUEL, AND DISTANCE TO CLIMB CRUISE CLIMB – 120 KIAS CONDITIONS: 100% RPM 100% TORQUE or 650ºC EGT Flaps – Up NOTES: 1. Add 35 pounds of fuel for engine start, taxi, and takeoff allowance. 2. Distances shown are based on zero wind. 20º C BELOW STANDARD TEMP. WEIGHT LBS 8360 8000 7600 PRESS ALT FT. SL 4000 8000 12000 SL 4000 8000 12000 SL 4000 8000 12000 STANDARD TEMPERATURE 20º C ABOVE STANDARD TEMP. CLIMB FROM SEA LEVEL TIME MIN 0 4 8 12 0 4 7 12 0 3 7 12 FUEL LBS 0 30 62 96 0 29 59 92 0 27 56 88 DIST NM 0 6 13 21 0 6 12 20 0 5 11 19 TIME MIN 0 4 9 14 0 4 8 14 0 4 8 13 FUEL LBS 0 32 68 110 0 31 65 105 0 30 62 100 DIST NM 0 7 15 26 0 6 14 24 0 6 13 23 TIME MIN 0 5 12 22 0 5 11 21 0 4 11 20 FUEL LBS 0 40 91 163 0 38 87 156 0 37 83 148 DIST NM 0 8 21 41 0 8 20 39 0 8 19 37 Figure 9-5.7. Time, Fuel, and Distance to Climb – Cruise Climb DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 9-19 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement CRUISE PERFORMANCE NOTES The following general information is applicable to all Cruise Performance charts contained in Figure 9-5.8, sheets 2 through 7, in this section: 1. The highest torque shown for each temperature and altitude combination corresponds to the maximum available cruise power expected for that atmospheric condition. For any condition, do not exceed 100% torque or 650ºC EGT, whichever occurs first. 2. With the cabin heat on, fuel flow for a given torque setting will be up to 35 pounds per hour higher. 3. Cruise performance is shown at a maximum gross weight of 8360 pounds. For operation at lower weights, the actual cruise performance will be slightly better. Figure 9-5.8. Cruise Performance (Sheet 1 of 7) DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 9-20 Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement CRUISE PERFORMANCE PRESSURE ALTITUDE 2000 FEET CONDITIONS: 8360 Pounds 96% RPM NOTE: Do not exceed 100% torque or 650ºC EGT. OAT ºC 45 35 25 15 5 -5 -15 % Tq 74.3 50 84.6 75 50 96.2 75 50 100 75 50 100 75 50 100 75 50 100 75 50 Wf (PPH) 393 320 420 390 317 449 384 313 452 378 309 452 384 312 455 388 316 458 402 320 KTAS 141 123 148 144 122 155 143 121 160 142 120 159 140 118 157 138 117 156 137 116 Figure 9-5.8. Cruise Performance (Sheet 2 of 7) DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 9-21 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement CRUISE PERFORMANCE PRESSURE ALTITUDE 4000 FEET CONDITIONS: 8360 Pounds 96% RPM NOTE: Do not exceed 100% torque or 650ºC EGT. OAT ºC 40 30 20 10 0 -10 -20 % Tq 73.4 50 83.6 75 50 95.1 75 50 100 75 50 100 75 50 100 75 50 100 75 50 Wf (PPH) 377 307 403 376 303 432 370 300 442 368 299 442 370 301 446 374 306 448 377 309 KTAS 148 123 156 148 122 163 147 121 163 145 120 160 144 119 159 143 117 156 141 116 Figure 9-5.8. Cruise Performance (Sheet 3 of 7) DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 9-22 Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement CRUISE PERFORMANCE PRESSURE ALTITUDE 8000 FEET CONDITIONS: 8360 Pounds 96% RPM NOTE: Do not exceed 100% torque or 650ºC EGT. OAT ºC 30 20 10 0 -10 -20 -30 % Tq 70.8 50 80.7 75 50 90.9 75 50 99.1 75 50 100 75 50 100 75 50 100 75 50 Wf (PPH) 345 283 370 352 278 397 348 277 422 349 279 427 352 283 428 355 285 430 357 289 KTAS 147 119 156 155 120 161 153 121 165 152 121 167 150 120 165 148 119 163 147 118 Figure 9-5.8. Cruise Performance (Sheet 4 of 7) DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 9-23 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement CRUISE PERFORMANCE PRESSURE ALTITUDE 12000 FEET CONDITIONS: 8360 Pounds 96% RPM NOTE: Do not exceed 100% torque or 650ºC EGT. OAT ºC 20 10 0 -10 -20 -30 -40 % Tq 67.9 50 76.9 50 83.8 75 50 90.3 75 50 97.6 75 50 100 75 50 100 75 50 Wf (PPH) 315 260 338 258 360 332 260 382 335 263 405 336 265 413 338 268 415 341 271 KTAS 144 129 152 128 156 153 126 159 151 125 167 149 124 174 148 122 172 146 121 Figure 9-5.8. Cruise Performance (Sheet 5 of 7)) DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 9-24 Original Issue, September 2, 2006 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement CRUISE PERFORMANCE PRESSURE ALTITUDE 16000 FEET CONDITIONS: 8360 Pounds 96% RPM NOTE: Do not exceed 100% torque or 650ºC EGT. OAT ºC 10 0 -10 -20 -30 -40 -50 % Tq 64.8 50 70.8 50 76.4 50 82.4 75 50 88.5 75 50 94.7 75 50 100 75 50 Wf (PPH) 287 242 306 243 325 246 344 321 248 364 322 250 384 324 253 403 328 257 KTAS 148 133 154 131 159 130 164 161 128 170 160 126 176 158 125 183 157 125 Figure 9-5.8. Cruise Performance (Sheet 6 of 7) DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 9-25 Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement CRUISE PERFORMANCE PRESSURE ALTITUDE 20000 FEET CONDITIONS: 8360 Pounds 96% RPM NOTE: Do not exceed 100% torque or 650ºC EGT. OAT ºC 0 -10 -20 -30 -40 -50 -54 % Tq 59.5 50 64.1 50 69.2 50 74.3 50 79.4 50 84.5 75 50 86.5 75 50 Wf (PPH) 259 230 275 232 291 233 308 235 325 237 343 313 240 350 314 241 KTAS 155 118 159 121 163 124 167 126 171 129 175 165 131 177 164 131 Figure 9-5.8. Cruise Performance (Sheet 7 of 7) DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 9-26 Original Issue, September 2, 2006 PRESS ALT FT S.L. 2000 4000 6000 8000 S.L. 2000 4000 6000 8000 S.L. 2000 4000 6000 8000 SPEED AT 50 FT KIAS 79 77 75 WEIGHT LBS 8360 7800 7300 CONDITIONS: Flaps 30º Power Lever – Idle after clearing obstacles, BETA (lever against spring) range after touchdown. 100% RPM Zero Wind 0ºC 1304 1422 1560 1713 1874 1467 1601 1755 1927 2109 1623 1771 1942 2132 2334 TOTAL FT TO CLEAR 50 FT OBS 793 893 1004 1128 1259 893 1004 1130 1270 1417 988 1111 1250 1405 1568 WATER RUN FT. 1360 1489 1632 1790 1958 1530 1675 1836 2014 2203 1693 1854 2032 2228 2438 TOTAL FT TO CLEAR 50 FT OBS 10ºC 839 943 1060 1185 1328 944 1061 1192 1333 1494 1045 1174 1319 1475 1654 WATER RUN FT. 1419 1554 1703 1863 2045 1597 1748 1916 2096 2301 1767 1934 2120 2320 2547 TOTAL FT TO CLEAR 50 FT OBS 20ºC 885 993 1120 1242 1402 996 1118 1260 1397 1577 1102 1237 1394 1546 1745 WATER RUN FT. 1479 1619 1778 1937 2138 1665 1821 2001 2179 2405 1842 2015 2214 2411 2662 TOTAL FT TO CLEAR 50 FT OBS 30ºC 932 1047 1170 1305 - 1049 1178 1316 1469 - 1160 1303 1457 1625 - WATER RUN FT. 1540 1687 1844 2017 - 1733 1898 2074 2270 - 1917 2100 2296 2511 - TOTAL FT TO CLEAR 50 FT OBS 40ºC Decrease distances 10% for each 11 knots headwind. For operation in tailwinds up to 5 knots, increase distances by 5% for each knot. If a landing with flaps up is necessary, increase the approach speed by 18 KIAS and allow for 50% longer distances. Where distance values have been replaced by dashes, operating temperature limits of the airplane would by greatly exceeded. Those distances which are included but the operation slightly exceeds the temperature limit are provided for interpolation purposes only Figure 9-5.9. Landing Distances (Sheet 1 of 2) 751 841 947 1068 1194 845 946 1066 1201 1343 935 1047 1180 1329 1486 WATER RUN FT. . 3. 2. NOTES: 1. MAXIMUM PERFORMANCE LANDING DISTANCE ON WATER Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Original Issue, September 2, 2006 Page 9-27 PRESS ALT FT S.L. 2000 4000 6000 8000 S.L. 2000 4000 6000 8000 S.L. 2000 4000 6000 8000 SPEED AR 50 FT KIAS 77 75 72 WEIGHT LBS 7800 7300 6800 CONDITIONS: Flaps 30º Power Lever – Idle after clearing obstacles, BETA (lever against spring) range after touchdown. 100% RPM Maximum Breaking and Reverse Paved, Level, Dry Runway Zero Wind 0ºC 1391 1513 1653 1809 1973 1528 1616 1767 1935 2113 1673 1819 1987 2174 2372 TOTAL FT TO CLEAR 50 FT OBS 765 861 969 1088 1215 841 946 1064 1196 1334 920 1035 1165 1308 1460 GRD ROLL FT. 1449 1581 1726 1887 2058 1592 1689 1846 2020 2205 1742 1900 2075 2268 2474 TOTAL FT TO CLEAR 50 FT OBS 10ºC 809 910 1022 1143 1281 889 999 1123 1256 1407 973 1093 1229 1374 1540 GRD ROLL FT. 1510 1647 1799 1962 2147 1659 1760 1924 2100 2301 1815 1980 2162 2358 2581 TOTAL FT TO CLEAR 50 FT OBS 20ºC 854 958 1080 1198 1352 938 1053 1187 1316 1485 1027 1152 1299 1440 1626 GRD ROLL FT. 1571 1713 1875 2037 2241 1726 1832 2007 2182 2402 1889 2059 2254 2448 2694 TOTAL FT TO CLEAR 50 FT OBS 30ºC 899 1010 1129 1259 - 987 1109 1240 1383 - 1081 1214 1357 1514 - GRD ROLL FT. 1633 1782 1942 2118 - 1793 1906 2079 2270 - 1963 2142 2334 2546 - TOTAL FT TO CLEAR 50 FT OBS 40ºC Decrease distances 10% for each 11 knots headwind. For operation in tailwinds up to 10 knots, increase distances by 10% for each 2.5 knots. For operation on a dry, grass runway, increase distances by 40% of the “ground roll” figure. If a landing with flaps up is necessary, increase the approach speed by 18 KIAS and allow for 50% longer distances. Where distance values have been replaced by dashes, operating temperature limits of the airplane would by greatly exceeded. Those distances which are included but the operation slightly exceeds the temperature limit are provided for interpolation purposes only. Figure 9-5.9. Landing Distances (Sheet 2 of 2) 724 811 914 1030 1152 796 891 1004 1131 1265 871 975 1099 1238 1385 GRD ROLL FT. 4. 2. 3. NOTES: 1. MAXIMUM PERFORMANCE LANDING DISTANCE ON LAND Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement Section 9 Amphibian Supplement DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Page 9-28 Original Issue, September 2, 2006
