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FAA-APPROVED Airplane Flight Manual Supplement for Cessna 208 PDF

45 Pages·2006·0.57 MB·English
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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: __________ DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXOrXigXinXalX IsXsuXeX, DXaXteXd:X SXepXteXmXbeXr X2, X20X0X6 XXXXXXX XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX Aero Twin, Inc. Honeywell TPE331-12JR Engine 2403 Merrill Field Dr. Aircraft Flight Manual Supplement Anchorage, AK 99501 General Information (907) 274-6166 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 XXXXXXXXXXXXXXXPaXgeX iXi XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXOXrXigXinXalX IsXsuXe,X SXepXteXmXbeXr X2,X 2X00X6 XXXXXXXXXXXXXX Aero Twin, Inc. Honeywell TPE331-12JR Engine 2403 Merrill Field Dr. Aircraft Flight Manual Supplement Anchorage, AK 99501 Contents (907) 274-6166 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 XXXXXXXXXXXXXXXOrXigXinXalX IsXsuXeX, SXepXteXmXbXerX 2X, 2X00X6X XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXPaXgXe iXii XXXXXXXXXXXXXX Aero Twin, Inc. Honeywell TPE331-12JR Engine 2403 Merrill Field Dr. Aircraft Flight Manual Supplement Anchorage, AK 99501 Section 5 (907) 274-6166 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 XXXXXXXXXXXXXXXOrXigXinXalX IsXsuXeX, SXepXteXmXbXerX 2X, 2X00X6X XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXPXagXe X5-X1 XXXXXXXXXXXXXX Aero Twin, Inc. Honeywell TPE331-12JR Engine 2403 Merrill Field Dr. Aircraft Flight Manual Supplement Anchorage, AK 99501 Section 5 (907) 274-6166 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 XXXXXXXXXXXXXXXPaXgeX 5X-2X XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXOXrXigXinXalX IsXsuXe,X SXepXteXmXbeXr X2,X 2X00X6 XXXXXXXXXXXXXX Aero Twin, Inc. Honeywell TPE331-12JR Engine 2403 Merrill Field Dr. Aircraft Flight Manual Supplement Anchorage, AK 99501 Section 5 (907) 274-6166 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. 650 640 630 ) C (º 620 F F 610 O RL 600 100% RPM S 590 - T 580 G E D 570 E T 560 A 96% RPM S 550 N E 540 P M 530 O C 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 XXXXXXXXXXXXXXXOrXigXinXalX IsXsuXeX, SXepXteXmXbXerX 2X, 2X00X6X XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXPXagXe X5-X3 XXXXXXXXXXXXXX Aero Twin, Inc. Honeywell TPE331-12JR Engine 2403 Merrill Field Dr. Aircraft Flight Manual Supplement Anchorage, AK 99501 Section 5 (907) 274-6166 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 95 E 90 U Q 12000 R O 85 T E 10000 N GI 80 8000 N E % 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 XXXXXXXXXXXXXXXPaXgeX 5X-4X XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXOXrXigXinXalX IsXsuXe,X SXepXteXmXbeXr X2,X 2X00X6 XXXXXXXXXXXXXX Aero Twin, Inc. Honeywell TPE331-12JR Engine 2403 Merrill Field Dr. Aircraft Flight Manual Supplement Anchorage, AK 99501 Section 5 (907) 274-6166 Performance o 10 knots, gure. he airplane htly exceeds the 40º c GRND. TOTAL RUN FT TO FT. CLEAR 50 FT O2338 1229 2835 1482 3455 1797 4223 2183 5134 2646 - - - - 2113 1110 2562 1340 3122 1624 3816 1973 4639 2392 - - - - 1878 987 2277 1190 2775 1443 3392 1754 4123 2126 - - - - TAKEOFF DISTANCE SHORT FIELD S: Decrease distance 10% for each 11 knots headwind. For operation with tailwinds up tincrease distances by 10% for each 2.5 knots. For operation on a dry, grass runway, increase distance by 15% of the “ground roll” fiWhere distance values have been replaced by dashes, operating temperature limits of twould be greatly exceeded. Those distances which are included but the operation sligtemperature limit are provided for interpolation purposes only. 30º C 20º C 10º C 0º C 0º C GRND. GRND. GRND. GRND. TOTAL TOTAL TOTAL TOTAL TOTAL RUN RUN RUN RUN FT TO FT TO FT TO FT TO FT TO FT. FT. FT. FT. CLEAR CLEAR CLEAR CLEAR CLEAR 50 FT 50 FT 50 FT 50 FT 50 FT OOOOO2118 2006 1896 1789 1689 1116 1055 995 937 2422 2258 2133 2013 1894 1285 1194 1124 1058 2937 2551 2407 2269 2135 1550 1360 1280 1201 3580 3089 2738 2567 2413 1879 1641 1464 1368 4887 3763 3333 3001 2740 2596 1989 1774 1603 5399 4620 4076 3670 3312 2817 2440 2171 1961 6674 5992 5011 4500 4058 3465 3176 2654 2395 1914 1813 1714 1617 1526 1008 953 899 846 2188 2040 1927 1819 1711 1162 1079 1016 956 2655 2305 2176 2050 1929 1401 1229 1157 1085 3236 2792 2475 2320 2181 1698 1483 1323 1236 4417 3401 3012 2712 2476 2346 1797 1603 1449 4879 4175 3684 3317 2994 2545 2205 1962 1772 6032 5415 4529 4067 3667 3131 2870 2398 2164 1701 1611 1523 1437 1357 896 847 799 752 1945 1813 1713 1617 1521 1032 959 903 850 2359 2049 1933 1822 1715 1245 1092 1028 964 2875 2481 2199 2062 1938 1509 1318 1176 1098 3925 3023 2677 2411 2200 2085 1597 1425 1288 4336 3710 3274 2948 2660 2262 1960 1743 1575 5361 4812 4025 3614 3259 2783 2551 2131 1923 Figure 5-3. Takeoff Distance NOTE 1. 2. 3. -1 GRND. RUN FT. 881 933 1125 1283 1464 1775 2165 796 898 1017 1160 1323 1604 1957 708 798 904 1031 1176 1426 1739 y PRESS ALT FT SL 2000 4000 6000 8000 10000 12000 SL 2000 4000 6000 8000 10000 12000 SL 2000 4000 6000 8000 10000 12000 a CONDITIONS: Flaps 20º 100% RPM 100% Torque or 650ºC EGT Cabin Heat – Off Zero Wind Paved, Level, Dry Runw TAKEOFF SPEED KIAS WEIGHT AT 50 LIFT LBS FT OFF 8360 82 72 8000 82 72 7600 80 70 DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXOrXigXinXalX IsXsuXeX, SXepXteXmXbXerX 2X, 2X00X6X XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXPXagXe X5-X5 XXXXXXXXXXXXXX Aero Twin, Inc. Honeywell TPE331-12JR Engine 2403 Merrill Field Dr. Aircraft Flight Manual Supplement Anchorage, AK 99501 Section 5 (907) 274-6166 Performance o 10 knots, gure. he airplane htly exceeds the 40º c GRND. TOTAL RUN FT TO FT. CLEAR 50 FT O3449 2144 4211 2607 5161 3182 6335 3891 7730 4735 3117 1938 2806 2356 4664 2875 5725 3516 6985 4279 2770 1722 3382 2093 4145 2555 5088 3125 6208 3803 TAKEOFF DISTANCE Flaps Up S: Decrease distance 10% for each 11 knots headwind. For operation with tailwinds up tincrease distances by 10% for each 2.5 knots. For operation on a dry, grass runway, increase distance by 15% of the “ground roll” fiWhere distance values have been replaced by dashes, operating temperature limits of twould be greatly exceeded. Those distances which are included but the operation sligtemperature limit are provided for interpolation purposes only. 30º C 20º C 10º C 0º C 0º C GRND. GRND. GRND. GRND. TOTAL TOTAL TOTAL TOTAL TOTAL RUN RUN RUN RUN FT TO FT TO FT TO FT TO FT TO FT. FT. FT. FT. CLEAR CLEAR CLEAR CLEAR CLEAR 50 FT 50 FT 50 FT 50 FT 50 FT OOOOO3133 1968 2804 2647 2500 1950 1844 1738 1636 3550 3337 3156 2977 2801 2222 2082 1965 1850 4337 3755 3547 3352 3158 2703 2351 2219 2093 5317 4539 4005 3778 3556 3303 2840 2516 2367 6529 5572 4885 4370 4024 4036 3471 3066 2753 2831 2682 2534 2392 2259 1762 1666 1570 1479 3208 3015 2852 2691 2531 2008 1882 1775 1671 3919 3393 3205 3029 2854 2443 2125 2006 1891 4805 4102 3619 3414 3214 2958 2567 2273 2139 5900 5035 4415 3949 3637 3647 3137 2771 2488 2516 2384 2252 2126 2008 1566 1481 1395 1314 2851 2680 2534 2391 2249 1785 1672 1578 1485 3483 3016 2849 2692 2537 2171 1889 1782 1681 4270 3645 3217 2034 2856 2653 2281 2020 1901 5244 4475 3923 3510 3232 3241 2788 2463 2211 Figure 5-4. Takeoff Distance NOTE 1. 2. 3. -1 GRND. RUN FT. 1542 1736 1967 2226 2528 1394 1569 1777 2011 2284 1239 1394 1580 1787 2030 RESS ALT FT SL 2000 4000 6000 8000 SL 2000 4000 6000 8000 SL 2000 4000 6000 8000 y P a CONDITIONS: Flaps 0º 100% RPM 100% Torque or 650ºC EGT Cabin Heat – Off Zero Wind Paved, Level, Dry Runw TAKEOFF SPEED KIAS WEIGHT AT 50 LIFT LBS FT OFF 8360 104 89 8000 104 89 7600 104 89 DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXPaXgeX 5X-6X XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXOXrXigXinXalX IsXsuXe,X SXepXteXmXbeXr X2,X 2X00X6 XXXXXXXXXXXXXX Aero Twin, Inc. Honeywell TPE331-12JR Engine 2403 Merrill Field Dr. Aircraft Flight Manual Supplement Anchorage, AK 99501 Section 5 (907) 274-6166 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. PRESS CLIMB RATE OF CLIMB - FPM WEIGHT ALT SPEED LBS FT KIAS -20º C 0º C 20º C 40º C 8360 0 92 1441 1357 1267 1111 2000 92 1400 1310 1222 936 4000 91 1352 1261 1177 766 6000 91 1292 1204 1003 587 8000 90 1245 1113 830 442 10000 90 1242 1021 749 - 12000 89 1140 927 668 - 8000 0 91 1503 1416 1322 1159 2000 91 1460 1366 1275 977 4000 90 1410 1316 1228 799 6000 90 1348 1256 1046 612 8000 89 1298 1160 866 442 10000 89 1296 1065 781 - 12000 88 1189 967 697 - 7600 0 90 1578 1487 1388 1217 2000 90 1533 1434 1338 1025 4000 89 1481 1381 1289 839 6000 89 1415 1318 1098 643 8000 88 1363 1218 909 485 10000 88 1361 1118 820 - 12000 87 1248 1015 732 - Figure 5-5. Rate of Climb – Takeoff Flap Setting DRAFT MARKETING RELEASE - NOT CONTROLLED NOT APPROVED FOR COPY OR DISTRIBUTION XXXXXXXXXXXXXXXOrXigXinXalX IsXsuXeX, SXepXteXmXbXerX 2X, 2X00X6X XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXPXagXe X5-X7 XXXXXXXXXXXXXX

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Aero Twin, Inc. 2403 Merrill Field Dr. Anchorage, AK 99501 (907) 274-6166 Honeywell TPE331-12JR Engine Aircraft Flight Manual Supplement General Information
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