TCDS 1A16

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 R e v . N o . 2 41 52 02 32 32 32 32 3 2 3 2 32 3 2 3 2 3 2 3 2 3 2 21 71 71 7 17 P a g e N o . 2 12 22 32 42 52 6 2 7 2 82 9 3 0 3 1 3 2 3 3 3 4 R e v . N o . 1 71 71 71 72 32 3 2 3 2 32 3 2 2 2 2 2 2 2 2 2 2 This revision incorporates the new type certificate holder and adds Model G-164B-20T. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 1A16 Revision No. 24 Allied Ag Cat Productions, Inc. G-164 G-164A G-164B G-164B with 73” G-164B-15T G-164B-34T G-164B-20T G-164C G-164D G-164D with 73” wing gap February 22, 2001 TYPE CERTIFICATE DATA SHEET NO. 1A16 This data sheet which is a part of type certificate No. 1A16 prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Civil Air Regulations. Type Certificate Holder Allied Ag Cat Productions, Inc. 301 West Walnut Street P.O. Box 482 Walnut Ridge, AR 72476 I - Model G-164, 1 POLB or 1 PCLB (Restricted Agricultural Category) approved January 20, 1959. Engine Continental W-670-6N (R-670-4) 479 lb. (+53.5) Continental W-670-16 (R-670-11) 486 lb. (+53.5) Continental W-670-6A (R-670-5) 470 lb. (+53.5) Continental W-670-240 (Gulf Coast) 516 lb. (+53.5) (See G-164 NOTE 3 for operating restrictions) Jacobs R-755-A2M1 503 lb. (+52.5) (See G-164 NOTE 6 for optional Jacobs engine installations) Pratt & Whitney R-985-AN-1, -AN-3, -25, -27, -39, -39A, -AN-14B; Wasp Jr. T1B2, T1B3 (One 4 1/2 and one 9th order crankcase damper) Fuel 80/87 Minimum octane aviation gasoline (R-985 series) 80 Minimum octane aviation gasoline (W-670 Series, R-755 Series) Engine For all operations: Limits: (W-670-6A, -6N or -16 engines) 2075 r.p.m. (220 hp.) (W-670-240 engine) 2075 r.p.m. (225 hp.) with item 1 propeller (W-670-240 engine) 2200 r.p.m. (240 hp.) with item 3 propeller (R-985 series engines) 2300 r.p.m. (450 hp.) with item 4 propeller (R-755-A2M1) 2200 r.p.m. (330 hp.) with item 3 propeller Manifold Pressure: (R-985-AN-14B): 36.5 in. Hg (sea level) 35.5 in. Hg (3500 ft.) Manifold Pressure: (R-985-AN-1, -AN-3, 37.5 in Hg (sea level) -25, -27, -39, -39A, T1B2, T1B3 37.0 in. Hg (1500 ft.) Manifold Pressure: (W-670 series): 28.0 in. Hg (sea level) 26.5 in. Hg (1500 ft.) Manifold Pressure (R-755): 28.0 in. Hg (sea Level) 26.5 in Hg (1500 ft.) Straight line variation between points 1A16 2 of 34 Propeller and Propeller Limits 1. McCauley ground adjustable propeller (with Continental W-670 series and Gulf Coast W-670-240 engines only) (a) Model 41D5926 with hub AAF 41D5926 and blades SS-135-6 79 lb. (+38.5) (b) Model D-1093 with hub D-1093 and blades SS-135-6M (See G-164 Note 2(a)(4) for operating restriction) 82 lb. (+38.5) Diameter: SS-135-6 blades: Max. 102 in. Min. 100 in. SS-135-6M blades: Max. 102-5/8 in. Min. 100 in. Pitch Settings at 42 in. sta. Static r.p.m. at Maximum Permissible W-670-6A, -6N, -16 Engines Throttle Setting (No additional tolerance permitted) 9.0o Not over 2055, not under 1905 9.5o Not over 1965, not under 1815 10.0o Not over 1905, not under 1755 10.5o Not over 1855, not under 1705 11.0o Not over 1815, not under 1665 W-670-240 Engine 9.7o Not over 1975, not under 1825 When installed on the above engines, the propeller must be indexed in the zero degree position (blades in line with crank throw) and the tachometer shall be placarded: "Avoid continuous operation between 1500 and 1650 RPM." A yellow arc marking must be included on the face of the tachometer between 1500 and 1650 RPM. Note: Blade angle adjustment must be within + or -1/2 o allowable tolerance to result in 2075 r.p.m. in climb at 75 m.p.h. CAS. 2. Hartzell constant speed propeller (with Jacobs R-755-A2M1 engine only) (a) Model HC-B3Z with hub Model HC-B3Z20-1 and blades Model 10160-8 115 lb. (+34.5) Diameter 93 in. only Pitch Settings at 30 in. Sta. Low 12.5o High 28.3o (b) Governor - Hartzell G-1 4.5 lb. (+72) 3. Gulfstream ground adjustable (with Continental W-670 series, Gulf Coast W-670-240 and Jacobs R-755-A2M1 engines only). (a) Model J-5404, SR-5404, SR-5404R/MA-96K-0 86 lb. Continental W-670 series engines (+37.5) Jacobs R-755-A2M1 engine (+35.7) Diameter: 96 in. only (Continental W-670 series engines) Max. 96 in., Min. 94 in. (Jacobs R-755-A2M1 engine) Pitch Settings Static r.p.m. at Maximum at 36 in. Sta. Permissible Throttle Setting (No additional tolerance permitted) W-670-6A, -6N, -16 Engines Not over 2060, not under 1960 14.1o W-670-240 Engine Not over 2095, not under 1945 14.5o R-755-A2M1 Engine Not over 2090, not under 1990 15.0o When installed on the above engines, the propeller must be indexed in the zero degree position, (blades in line with crank throw). Note: Blade angle adjustment must be within + or - 1/2 degree allowable tolerance to result in never exceeding the maximum rated r.p.m. at rated power in a full throttle climb at 75 m.p.h. CAS. 1A16 3 of 34 Model G-164 4. Hamilton Standard: 2D30/6101A-12-13-14 with P&W R-985 Series engines (cont’d) Diameter: 108 in. max., 106 in. min. (No further reduction permitted) 2D30 Hub, Pacific Propeller AG-100-2 blades, diameter 106 in. (2% cutoff permitted) Pitch Setting: 11.75o low, 14o high (2 pos.): 10.0o low, 16.5o high at 42 in. Sta. (constant speed) Governor: 1A2-5, 1A2G-5, or 4A2-1 Static r.p.m. at maximum permissible throttle setting: Not over 2070, not under 1970 (2 position) Airspeed Limits (CAS) V NE (Never Exceed) 131 m.p.h. (114 knots) VA (Maneuvering) 104 m.p.h. (90 knots) C.G. Range (+122.0) to (+124.0) at 3750 lb. (+122.0) to (+125.3) at 2460 lb. Straight line variation between points Empty Weight None C.G. Range Datum +99.1 in. ahead of firewall bulkhead. Leveling Means Longitudinal: Leveling lugs welded on tubular fuselage frame 27 in. below upper longeron and forward lug at station 100, left hand side. Maximum Weight Configuration Engine Prop Pitch Weight With Item 1 or 2 installed Sprayer W-670-6A, -6N or -16 9.5 o 3700 lb. Sprayer W-670-6A, -6N or -16 9 o, 10o, 10.5o, 11o 3550 lb. Duster W-670-6A, - 6N or -16 9.5 o 3600 lb. Duster W-670-6A, -6N or -16 9 o, 10o, 10.5o, 11o 3450 lb. Sprayer or W-670-240 9.7 o 3750 lb. Duster Sprayer or R-755-A2M1 - 3750 lb. Duster Configuration Engine Prop Pitch Weight With Item 3 installed Sprayer W-670-6A, -6N or -16 14.1 o 3600 lb. Sprayer or Duster W-670-240 14.5 o 3750 lb. Sprayer or Duster R-755-A2M1 15.0 o 3750 lb. Configuration Engine Prop Pitch Weight With Item 4 installed Sprayer or Duster R-985 series 16.5 o high, 10o low 3750 lb. No. of Seats 1 (+180) Maximum Hopper Capacity 1200 lb. (+122) S/N 1 through 300 2000 lb. (+122) S/N 301 and up Fuel Capacity 46.3 gal. or 33 gal. (+112.5) (One tank in upper wing center section (See G-164 Note 7)) Oil Capacity 7 gal. (+94) (6.5 gal. usable) (R-985 series) 5 gal. (+94) (4.5 gal. usable) (W-670 series, R-755 series) Serial No. Eligible S/N 1 through 400 Certification Basis CAR 8.10 (a)(1) effective October 11, 1950, and CAM 8, Appendix B as amended March 19, 1957, except CAR 3.241 utilized for Ground Loads. Restricted Type Certificate No. 1A16 issued January 20, 1959. Date of application for Type Certificate June 21, 1957. 1A16 4 of 34 Model G-164 (cont’d) Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see certification basis and CAM 8, Appendix B, subparagraph .51) must be installed in aircraft for certification. In addition, the following items of equipment are required: (a) For aircraft with no electrical system: Pre-stall warning indicator, Safe Flight Instrument Corporation Kit No. 164-R, 6 volt. (Dry batteries powering this unit must be dated and replaced every six months.) (b) For aircraft incorporating an electrical system: Pre-stall warning indicator, (Safe Flight Instrument Corporation 12V or 24V P/N C-35407 or P/N 164-3) Installation per Drawing No. A1011. (c) Winter front installation per Gulfstream Drawing A1605. For all aircraft with Continental W-670 series Gulf Coast W-670-240 engines if operated when the OAT is below 35oF. (d) Nose Ballast installation per Gulfstream Drawing A1073A on aircraft equipped with Continental W-670 series engines or Gulf Coast W-670-240 engines. Required only when aircraft C.G. would otherwise be outside the specific aft limits. (e) Tail Ballast installation per Gulfstream Drawing A1072B. Required only when aircraft C.G. would otherwise be outside the specified forward limit. Maximum permissible weight. (Use actual weight). (f) Cylinder head Temperature Gage and Manifold Pressure Gage required on aircraft equipped with R985 series powerplant. Agricultural Dispersal The following Agricultural Dispersal Equipment may be installed: Equipment (a) Sprayer dispensing installation per Gulfstream Drawings A1011, S/N 1 and up, A1921, S/N 1 and up, A1960, S/N 1 through 300, A1480, S/N 301 through 400. (b) Dust dispensing installation per Gulfstream Drawing (1) A1970C Sheet 3 applicable S/N 1 through 100 (2) A1970D Sheet 4 applicable S/N 101 through 300 (3) A1970F Sheet 5 applicable S/N 301 through 400 (R-755 series and R985 series) II - Model G-164A 1 PCLB (Restricted Agricultural Category) approved March 4, 1966. Engines (See G-164A Pratt and Whitney R-985-AN-1, -AN-3, -25, -27, -39, -39A NOTE 1) -AN-14B, Wasp Jr. T1B2, T1B3 (One 4 1/2 and one 9th order crankshaft damper) Pratt and Whitney R-1340-AN-1, S1H1, S3H1 (eligible S/N 526 and up only) (One 4 1/2 and one 9th order crankshaft damper) Fuel 80/87 minimum octane aviation gasoline Engine Limits R-985 2300 r.p.m. (450 hp.) all operations Manifold Pressure: (R-985-AN-14B) 36.5 in. Hg (sea level) 35.5 in. Hg (3500 ft.) Manifold Pressure: (All others) 37.5 in. Hg (sea level) 37.0 in. Hg (1500 ft.) Straight line variation between points. 1A16 5 of 34 Model G-164A (cont’d) Engine Limits (cont’d) R-1340 2250 r.p.m. (600 hp.) Takeoff (5 minutes) 2200 r.p.m. (550 hp.) Max Continuous Manifold Pressure: (R-1340-AN-1, S3H1) 600 hp. 2250 r.p.m. 36.0 in. Hg (Sea Level) 550 hp. 2200 r.p.m. 34.0 in. Hg (Sea Level) to 32.5 in. Hg (5000 ft.) Manifold Pressure: (R-1340-S1H1) 600 hp. 2250 r.p.m. 36.5 in. Hg (Sea Level) 550 hp. 2200 r.p.m. 35.0 in. Hg (Sea Level) to 33.0 in. Hg (8000 ft.) Straight line variation between points Propeller and Propeller Limits R-985: Hamilton Standard 2D30 hub, 6101A-12, -13, -14 blades Diameter: 108 in. max., 106 in. min: (No further reduction permitted) Pitch Setting: 11.75o low, 14o high (2 pos.) At 42 in. station: 10o low, 16.5o high (constant speed) Governor: 1A2G-5, 1A2-5 or 4A2-1 Hamilton Standard 2D30 hub, Pacific Propeller AG-100-2 blades Diameter 106 in. (2% cutoff permitted) Pitch Setting: 11.75o low, 14o high (2 pos.) At 42 in. station: 10o low, 16.5o high (2 pos.) Governor: 1A2G-5, 1A2-5 or 4A2-1 Static r.p.m. at maximum permissible throttle setting: not over 2070, not under 1970 (2 position) R-1340: Hamilton Standard 12D40 hub, 6101A-12 blades Diameter: 108 in. (2% cutoff permitted) Pitch Setting: 11o low, 20o high Governor: 1M12 Hamilton Standard 12D40 hub, Pacific Propeller AG-100-2 blades Diameter: 106 in. (2% cutoff permitted) Pitch Setting: 11o low, 20o high Governor: 1M12 or EDO-AIRE 34-828-021 Airspeed Limits V ne (Never exceed) 147 m.p.h. (128 knots) (CAS) V a (Maneuvering) 117 m.p.h. (102 knots) C.G. Range Aircraft S/N 1571, 1583, 1616 up (401 through 1570, 1572 through 1582 R-985 and 1584 through 1615 retroactive) (+122.0) to (+125.4) at 4500 lb. C.G. Range Aircraft S/N 526 and Up R-1340 (+122.0) to (+124.0) at 4500 lb. (+120.3) to (+125.3) at 3525 lb. Empty Weight Aircraft S/N 401 and Up C.G. Range None R-985 Empty Weight Aircraft S/N 526 and Up C.G. Range None R-1340 Datum +99.1 in. ahead of firewall bulkhead. 1A16 6 of 34 Model G-164A (cont’d) Leveling Means Longitudinal: Level lugs welded on tubular fuselage frame 27 in. below upper longeron and forward lug at station 100, left hand side. No. of Seats 1 (+180) Maximum Hopper 2000 lb. (+126.2) Capacity Fuel Capacity 46.3 gal. (+112.5) (One Tank in wing center section) (See G-164A NOTE 3) Oil Capacity 7 gal. (+94.0) (6.5 gal. usable) (See G-164A NOTE 6) 8.7 gal. (+94.0) (8.2 gal. usable) (See G-164A NOTE 6) Serial No. Eligible S/N 401 and Up Certification Basis CAR 8.10 (a)(1) effective October 11, 1950, and CAM 8, Appendix B, as amended March 19, 1957. Amended Restricted Type Certificate No. 1A16 issued March 1966. Date of Application for Type Certificate Amendment November 12, 1964. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see certification basis and CAM 8, Appendix B, subparagraph .51) must be installed in aircraft for certification. In addition, the following items of equipment are required: (a) For aircraft with no electrical system: Pre-stall warning indicator, Safe Flight Instrument Corp. Kit No. 164-R, 6 volt. (Dry batteries powering this unit must be dated and replaced every six months) (b) For aircraft incorporating an electrical system: Pre-stall warning indicator, Safe Flight Instrument Corp. 12V or 24V P/N C-35407 or P/N 164-3. Installation per A1011, Sheet 2 (c) Cylinder head temperature gage and manifold pressure gage required on aircraft equipped with R-985 and R1340 series powerplants. (d) Tail ballast per Gulfstream Drawing A1074 required on all R-1340 series engine installations only when aircraft C.G. would otherwise be outside the specified forward limit. Agricultural Dispersal The following Agricultural Dispersal Equipment may be installed: Equipment (a) Sprayer Dispensing Installation per Gulfstream Drawings (1) A1480 (Leading Edge Booms), through S/N 750 (2) A2930 (Leading Edge Booms), S/N 751 through 1725 (3) A2901 (Trailing Edge Booms), S/N 751 through 1726 and up (4) A5740 (Trailing Edge Booms), S/N 1726 and up (b) Dust dispensing installation per Gulfstream Drawing (1) A1970F Sheet 5, Dust System Installation (2) A1398, Spreader Installation (R-985 and R-1340 Only) (Alternate) (3) A1490, Spreader Installation (R-985 and R-1340 Only) 1A16 7 of 34 III - Model G-164B 1 PCLB (Restricted Agricultural Category) approved November 18, 1975. Model G-164B (with 73" wing gap) - 1 PCLB (Restricted Agricultural Category) approved November 18, 1982 Model G-164B-15T and G-164B-34T 1 PCLB (Restricted Agricultural Category) approved December 23, 1985 Model G-164B-20T, 1 PCLB (Restricted Agricultural Category) approved April 1991 Engine Pratt and Whitney R-985-AN-1, AN-3, -25, -27, -39, -39A, -AN-14B; T1B2, T1B3 (One 4 1/2 and one 9th order crankshaft damper) Continental/Page R-975-46/A2 Pratt & Whitney R-1340-AN-1, S1H1, S3H1 (One 4 1/2 and one 9th order crankshaft damper) Pratt & Whitney of Canada Ltd. PT6A-15AG - G-164B-15T only. Pratt & Whitney of Canada Ltd. PT6A-34AG - G-164B-34T only. Pratt & Whitney of Canada LTD. PT6A-20B - G-164B-20T only. Fuel R-985 & R-1340 80/87 minimum octane aviation gasoline R-975 100 minimum octane aviation gasoline PT6A-15AG & PT6A-34AG, and PT6A-20B Jet A/Jet A-1/Jet B Automotive Diesel Fuel permitted for agricultural operations when free air temperature is above +5oC (+41oF) for grade DF-2 -4oC (+25oF) for grade DF-1 Engine Limits R-985 2300 r.p.m. (450 hp.) all operations Manifold Pressure (R-985-AN-14B) 36.5 in. Hg (sea level) 35.5 in. Hg (3500 ft.) Manifold Pressure (all others) 37.5 in. Hg (sea level) 37.0 in. Hg (1500 ft.) Straight line variation between points. R-975-46/PA2 2300 r.p.m. (525 hp.) Takeoff (5 minutes) 2300 r.p.m. (500 hp.) Max. Continuous Manifold Pressure: 525 hp. 42.1 in. Hg (Sea Level) 500 hp. 40.7 in. Hg (Sea Level) R-1340 2250 r.p.m. (600 hp.) Takeoff (5 minutes) 2200 r.p.m. (550 hp.) Max. Continuous Manifold Pressure: (R-1340-AN-1, S3H1) 600 hp. 2250 r.p.m. 36.0 in. Hg (Sea Level) 550 hp. 2200 r.p.m. 34.0 in. Hg (Sea Level) to 32.5 in. Hg (5000 ft.) Straight line variation between points Manifold Pressure: Wasp S1H1 600 hp. 2250 r.p.m. 36.5 in. Hg (Sea Level) 550 hp. 2200 r.p.m. 35.0 in. Hg (Sea Level) to 33.0 in. Hg (8000 ft.) Straight line variation between points 1A16 8 of 34 Model G-164B (cont’d) PT6A-15AG Operating Conditions OPERATING LIMITS POWER SETTING SHP TORQUE PSI MAXIMUM ITT oC Ng RPM % Np RMP % OIL PRESSURE PSIG OIL TEMP oC TAKEOFF (5 MINUTES) 680 53.3 725 38100 101.5 2200 100 80-100 10-99 MAXIMUM CONTINUOUS 600 47 695 -- -- 2200 100 80-100 10-99 MAX. CLIMB/ MAX CRUISE 600 47 695 -- -- -- -- 80-100 0-99 IDLE GROUND IDLE FLIGHT -- -- 660 660 19000 52 25500 68 -- -- 40 (MIN) 40 (MIN) -40-99 -40-99 STARTING -- -- 1090 -- -- -- -- -- -40 (MIN) ACCELERATION -- 68.8 825 38500 102.6 2420 110 -- 0-99 MAX. REVERSE 600 49.2 725 38100 101.5 2100 95.5 80-100 0-99 PT6A-34AG Operating Conditions OPERATING LIMITS POWER SETTING SHP TORQUE PSI MAXIMUM ITT oC Ng RPM % Np RMP % OIL PRESSURE PSIG OIL TEMP oC TAKEOFF (5 MINUTES) 750 58.7 790 38100 101.5 2200 100 85-105 10-99 MAXIMUM CONTINUOUS 600 47 740 -- -- 2200 100 85-105 10-99 MAX. CLIMB/ MAX CRUISE 600 47 740 -- -- -- -- 85-105 0-99 IDLE GROUND IDLE FLIGHT -- -- 685 685 19000 52 25500 68 -- -- 40 (MIN) 40 (MIN) -40-99 -40-99 STARTING -- -- 1090 -- -- -- -- -- -40 (MIN) ACCELERATION -- 68.4 850 38500 102.6 2420 110 -- 0-99 MAX. REVERSE 600 49.2 780 38100 101.5 2100 95.5 85-105 0-99 PT6A-20B Operating Conditions OPERATING LIMITS POWER SETTING SHP TORQUE PSI MAXIMUM ITT Ng RPM % Np RMP % Oil Press PSIG Oil Temp oC Take-off* Max. Cont.** 550 42.5 750 38100 101.5 2200 100 65-85 10-99 Max. Climb 538 ISA 42.5 725 -- -- 2200 100 65-85 0-99 Max. Cruise 495 ISA 42.5 705 -- -- 2200 100 65-85 0-99 Idle - Grnd Idle - Flight -- -- 685 685 19000 52 25500 68 -- -- 40 (MIN) 40 (MIN) -40-99 -40-99 Starting -- -- 1090 -- -- -- -- -- -40 (MIN) Acceleration -- 48.5 850 38500 102.6 2420 110 -- 0-99 Max Reverse 500 40.5 750 38100 101.5 2100 95.5 65-85 0-99 *Takeoff -5 mintes **Maximum Continuous - enroute emergency 1A16 9 of 34 Model G-154B (cont’d) Propeller and Propeller R-985: Limits Hamilton Standard 2D30 hub, 6101A-12, -13, -14 blades Diameter: 108 in. max., 106 in. min: (No further reduction permitted) Pitch Setting: 11.75o low, 14o high (2 pos.) At 42 in. station: 10o low, 16.5o high (constant speed) Governor: 1A2G-5, 1A2-5 or 4A2-1 Hamilton Standard 2D30 Hub, Pacific Propeller AG-100-2 blades Diameter: 106 in. (2% cutoff permitted) Pitch Setting: 11.75o low, 14o high (2 pos.) At 42 in. station: 10o low, 16.5o high (constant speed) Governor: 1A2G-5, 1A2-5 or 4A2-1 Static r.p.m. at maximum permissible throttle setting: not over 2070, not under 1970 (2 position) Hamilton Standard 2D30 hub, Pacific Propeller AG-100-48 blades Diameter: 104 in. max., 102 in. min. Pitch Settings at 42 in. station 9.5o low, 16.5o high (Constant Speed) R-975-46/PA2: Hamilton Standard 2D30 Hub, Pacific Propeller AG-100-48 blades Diameter: 104 in. max., 102 in. min. Pitch Settings at 42 in. station 9.5o low, 16.5o high (Constant Speed) Avoid continuous operation 1300-1450 r.p.m. Governor: 1A4-R-975 (Pacific Propeller) R-1340: Hamilton Standard 12D40 hub, 6101A-12 blades Diameter: 108 in. (2% cutoff permitted) Pitch Setting: 11o low, 20o high Governor: 1M12 Hamilton Standard 2D40 Hub, Pacific Propeller AG-100-48 blades Diameter: 104 in. max., 102 in. min. Pitch Settings at 42 in. station 10.5o low, 20 high (Constant Speed) Governor: 1M12 Hamilton Standard 2D40 Hub, Pacific Propeller AG-100-48 blades Diameter: 104 in. max., 102 in. min. Pitch Settings at 42 in. station 10.5o low, 20 high (Constant Speed) Governor: 1M12 Hamilton Standard 22D40 Hub, Pacific Propeller AG-100-48 blades 549B & up Diameter: 104 in. (2% cutoff permitted) Pitch Settings 11.o low, 20o high Governor: 4G10-21 PT6A-15AG, PT6A-34AG, and PT6A-20B Hartzell HC-B3TN-3D hub, T10282 + 4 blades Diameter: 106 in. max., 100 in. min. Pitch Setting: at 30 in. station low 18o, reverse 8o, feather 90o Airspeed Limits V ne (Never exceed) 147 m.p.h. (128 knots) Through S/N 548B (CAS) V a (Maneuvering) 117 m.p.h. (102 knots) S/N 549B and Up Vne (Never exceed) 145 m.p.h. I.A.S. (126 knots) Va (Maneuvering) 116 m.p.h. I.A.S. (101 knots) 1A16 10 of 34 Model G-164B (cont’d) G-164B-15T, G-164B-34T, and G-164B-20T Vne (Never exceed) 157 m.p.h. I.A.S. (136 knots) Va (Maneuvering) 125 m.p.h. I.A.S. (109 knots) C.G. Range G-164B (through S/N 708B) R-985 (+122.0) to (+125.0) at 4500 lb. R-975-46/PA2 (+122.0) to (+124.8) at 4500 lb. R-1340 (+122.0) to (+124.0) at 4500 lb. G-164B with 73" Wing Gap (S/N 709B and Up) R-1340 (+122.0) to (+125.5) at 5200 lb. (S/N 709B and up) R-985 (+122.0) to (+126.0) at 5200 lb. (S/N 752B and up) PT6A-15AG & (+122.0) to (+125.5) at 5200 lb. PT6A-34AG (+122.0) to (+125.5) at 5200 lb. PT6A-20B (+122.0) to (+125.5) at 5200 lb. Empty Weight G-164B (through S/N 708B) and G-164B with 73" Wing Gap (S/N 709B and Up) C.G. Range None Datum +99.1 in. ahead of firewall bulkhead. Leveling Means Longitudinal: Leveling lugs welded on tubular fuselage frame 27 in. below upper longeron and forward lug at station 100, left hand side. No. of Seats 1 (+180) Maximum Hopper 2000 lb. (+126.2) Capacity Fuel Capacity 46.3 gal. (+112.5) (One tank in wing center section) (See G-164B NOTE 3) 80 gal. (+112.5) (S/N 660B through 708B) 80 gal. (+112.6) (S/N 709B and up with 73" in. wing gap) (see G-164B Note 6). Oil Capacity 8.7 gal. (+94.0) (8.2 gal. usable) 2.8 gal. (+72.0) (PT6A-15AG & PT6A-34AG), and PT6A-20B Serial No. Eligible Model G-164B 1B and up Model G-164B-15T, -34T, & -20T 709B & up Certification Basis G-164B and G-164B with 73" wing gap: CAR 8.10(a)(1) effective October 11, 1950, and CAM 8, Appendix B, as amended March 19, 1957. Amended Restricted Type Certificate No. 1A16 issued November 18, 1975. Date of application for Type Certificate Amendment March 11, 1975. G-164B-15T and G-164B-34T CAR 8.10(a)(1) effective October 11, 1950 and CAM 8, Appendix B, as amended March 19, 1957, and applicable FAR paragraphs. Amended Restricted Type Certificate No. 1A16 issued December 23, 1985. Date of application for Type Certificate Amendment, January 23, 1983. G-164B-20T CAR 8.10(a)(1) effective October 11, 1950 and CAM 8, Appendix B, as amended March 19, 1957, and applicable FAR paragraphs. Amended Restricted Type Certificate No. 1A16 issued April 23, 1991. Date of application for Type Certificate Amendment, March, 1991. 1A16 11 of 34 Model G-164B (cont’d) Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see certification basis and CAM 8, Appendix B, subparagraph .51) and applicable FAR 23 paragraphs for the models G-164B-15T, G-164B-34T, and G-164B-20T must be installed in aircraft for certification. In addition, the following items of equipment are required: (a) For aircraft with no electrical system: Pre-Stall warning indicator, Safe Flight Instrument Corporation Kit No. 164-R, 6 volt. (Dry batteries powering this unit must be dated and replaced every six months). (b) For aircraft incorporating an electrical system: Pre-stall warning indicator, (Safe Flight Instrument Corporation 12v or 24v P/N C-35407) or P/N 164-3 Installation per drawing A3011. (c) Cylinder head temperature gage and manifold pressure gage. (R975, R985, R1340 only). (d) Fixed Ballast Inst. STA 46.5 (G-164B-15T & G-164B-34T) or sta 45.8 (G- 164B-20T) per drawing A7534. Agricultural Dispersal The following Agricultural Equipment may be installed: Equipment Equipment (a) Sprayer dispensing installation per Gulfstream Drawing: (1) A2901 (Trailing Edge Booms) through A/C 334B. (2) A3740 (Trailing Edge Booms) 335B through 659B (3) A3740 (Trailing Edge Booms) 660B and up. (R-1340 Eng.) (4) A3723 (Trailing Edge Booms) 752B and up. (R-985 Eng.) (b) Dust Dispensing Installation per Gulfstream Drawing: A1970A Sheet 6, Dust System Installation (S/N 1B through 659B). (1) A1398 Spreader Installation. (2) A1490 Spreader Installation.