TCDS A12SO

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 Rev. No. 23 19 19 19 19 19 19 19 19 19 19 20 21 21 21 21 21 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A12SO Revision 23 COMMANDER 112 112TC 112B 112TCA 114 114A 114B 114TC October 3, 2013 TYPE CERTIFICATE DATA SHEET A12SO This data sheet, which is part of Type Certificate No. A12SO, prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder: Commander Aircraft Corporation 2 Dorset Road Colonia, NJ 07067 Type Certificate Holder Record: CPAC, Inc. transferred to Commander Aircraft Corporation on October 3, 2013; Commander Aircraft Company transferred to CPAC, Inc. on September 12, 2005; Gulfstream Aerospace Corporation transferred to Commander Aircraft Company on December 27, 1988; Gulfstream American Corporation transferred to Gulfstream Aerospace Corporation on February 3, 1981; Rockwell International, Commander Aircraft Division transferred to Gulfstream American Corporation I. Model 112, 4 PCLM (Normal and Utility Category), Approved June 1, 1972 Engine Lycoming I0-360-C1D6 Fuel 100/130 minimum grade aviation gasoline Engine Limits For all operations, 2700 rpm (200 hp) Propeller and Hartzell Constant Speed, Model HC-E2YR-1BF or HC-E2YR-1B Blade, Model F766A or Propeller Limits 7666A Pitch: High 28° - 30°, Low 13° ± 0.2° at Blade Station 30 inches Diameter: Not over 76”, not under 74” Governor: Edo-Aire 34-828-014 or Edo-Aire 34-828-014-2 Spinner: Hartzell C-3533 or C-3533P or Aero Commander 46390-3 Limitations: Do not exceed 24” Hg. manifold pressure below 2400 rpm 2 A12SO, Rev.23 I. Model 112 (cont’d) Airspeed Limits Never exceed 180 Kts (207 mph) CAS Decrease speed 1 Kt per 1000 ft. above 10,000 ft. Max. structural cruising 2550 lbs. 148 Kts (170 mph) CAS Decrease speed 1 Kt per 1000 ft. above 10,000 ft. Max. structural cruising 2650 lbs. 143 Kts (165 mph) CAS Decrease speed 1 Kt per 1000 ft. above 10,000 ft. Maneuvering (Normal 2550 lbs) 111 Kts (128 mph) CAS Maneuvering (Normal 2650 lbs) 113 Kts (130 mph) CAS Maneuvering (Utility) 118 Kts (136 mph) CAS Flaps extended up to 20° 130 Kts (150 mph) CAS 20° to 35° 109 Kts (125 mph) CAS Max. gear extended 130 Kts (150 mph) CAS Max. gear operating 130 Kts (150 mph) CAS Max. cowl flaps open 130 Kts (150 mph) CAS Max. side window open 130 Kts (150 mph) CAS C.G. Range Normal Category Forward: 103.5” aft of datum (18.8% MAC) at 2650 lbs. 101.4” aft of datum (15.0% MAC) at 2550 lbs. 97.0” aft of datum (7% MAC) at 2100 lbs. 97.0” aft of datum (7% MAC) at 1600 lbs. Aft: 110.5” aft of datum (31.5% MAC) at 2650 lbs. 110.5” aft of datum (31.5% MAC) at 1600 lbs. Utility Category Forward: 100.8” aft of datum (13.9% MAC) at 2488 lbs. 97.0” aft of datum (7% MAC) at 2100 lbs. 97.0” aft of datum (7% MAC) at 1600 lbs. Aft: 106.5” aft of datum (24.25% MAC) at 2488 lbs. 106.5” aft of datum (24.25% MAC) at 1600 lbs. Straight line variations between points. Empty Weight C.G. Range None Datum 62.5” forward of firewall (front face) Leveling Means Bottom of fuselage, outer surface, from F.S. 62.5 to F.S. 97.6 Maximum Weight 2550 lbs. takeoff; 2550 landing (S/N 3 thru 125). See Note 4 – Normal Category No. of Seats 2 Occupants at (+ 99.0); 2 Occupants at (+ 136.0) Normal Category Only Maximum Baggage 200 lbs. (at + 164.0) Normal Category 0 lbs. Utility Category Fuel Capacity 64 gal. usable (2 wing tanks) at +108.6. (See Note 1 for unusable fuel)(S/N 3 thru 125) 68 gal. usable (2 wing tanks) at +108.6. (See Note 1 for unusable fuel)(S/N 126 thru 155) 48 gal. usable (2 wing tanks) at +108.6. (See Note 1 for unusable fuel)(S/N 156 and up – Std.) 68 gal. usable (2 wing tanks) at +108.6. (See Note 1 for unusable fuel)(S/N 156 and up – optional.) Oil Capacity 8 qts. At +46.5 (6 qts. Usable) (See Note 1 for undrainable oil). 3 A12SO, Rev.23 I. Model 112 (cont’d) Control Surface Movements Wing Flaps Up 0° ± ½° Down 40° ± 2° (Serial Numbers 1 thru 81) (See Note 5) Up 0° ± 1° Down 35° ± 2° (Serial Numbers 82 & up) Aileron Up 20° ± 27° Down 7° ± 11° (Max. up must be within 4° left to right) Rudder Left 22° ± 2° Right 28°* ± 2° Elevator Up 30° ± 2° Down 13° ± 2° Elevator Up 15° ± 2° Down 26° ± 1° *Front vertical stabilizer centerline Nose Wheel Movement Steering ± 15° Castoring ± 30° Serial Numbers Eligible 1, 3 thru 489, and 13000 II. Model 114, 4 PCLM, (Normal Category), Approved March 8, 1976, (Utility Category) Approved March 31, 1977 Engine Lycoming I0-540-T4A5D or I0-540-T4B5D (S/N 1400 thru 14149) Lycoming I0-540-T4B5D (S/N 14150 & Subs) Fuel 100/130 minimum grade aviation gasoline Propeller and Hartzell Constant Speed, Model HC-C2YR-1BF/F8467-7R Propeller Limits Blade: Model F8467-7R Pitch: High 30° - 32°, Low 14.2° ± 0.1° at Blade Station 30” Diameter: Not over 77”, no reduction allowed. Governor: Edo-Aire 34-828-014-7 Spinner: 46390-3 Limitations: None Airspeed Limits Never exceed SL – 12,500 ft. 186 Kts (214 mph) CAS 16,000 ft. 175 Kts (201 mph) CAS 20,000 ft. 161 Kts (185 mph) CAS 24,000 ft. 147 Kts (169 mph) CAS Max. structural cruising SL – 12,500 ft. 148 Kts (170 mph) CAS 16,000 ft. 139 Kts (160 mph) CAS 20,000 ft. 128 Kts (147 mph) CAS 24,000 ft. 117 Kts (135 mph) CAS Maneuvering (Normal) 3140 lbs. 118 Kts (135 mph) CAS 2658 lbs. 109 Kts (125 mph) CAS 2023 lbs. 95 Kts (109 mph) CAS Straight line variation between points. Maneuvering (Utility) 2800 lbs. 120 Kts (138 mph) CAS 2250 lbs. 107 Kts (124 mph) CAS 2023 lbs. 102 Kts (117 mph) CAS Straight line variation between points. 4 A12SO, Rev.23 II. Model 114 (cont’d) Airspeed Limits (cont’d) Flaps extended Up to 20° 150 Kts (173 mph) CAS* 20° to 25° 120 Kts (138 mph) CAS 25° to 35° 109 Kts (125 mph) CAS Max. gear extended 186 Kts (214 mph) CAS* Max. gear operating 130 Kts (150 mph) CAS Max. cowl flaps open (S/N 14000 thru 14149) 130 Kts (150 mph) CAS Max. side window open 130 Kts (150 mph) CAS * Do not Exceed Vne Schedule C.G. Range Normal Category Forward: 106.91” aft of datum (25.0% MAC) at 3140 lbs. 101.11” aft of datum (14.5% MAC) at 2658 lbs. 99.75” aft of datum (12.0% MAC) at 2250 lbs. 99.75” aft of datum (12.0% MAC) at 2023 lbs. Aft: 110.50” aft of datum (31.5% MAC) at 3140 lbs. 110.50” aft of datum (31.5% MAC) at 2503 lbs. Straight line variation between points. Utility Category Forward: 102.82” aft of datum (17.57% MAC) at 2800 lbs. 101.11” aft of datum (14.5% MAC) at 2658 lbs. 99.75” aft of datum (12.0% MAC) at 2250 lbs. 99.75” aft of datum (12.0% MAC) at 2023 lbs. Aft: 107.46” aft of datum (26.0% MAC) at 2800 lbs. 107.46” aft of datum (26.0% MAC) at 2266 lbs. Straight line variations between points. Empty Weight C.G. Range None Datum 62.5” forward of firewall (front face) Leveling Means Bottom of fuselage, outer surface, from F.S. 62.5 to F.S. 97.6 Maximum Weight (Normal) 3140 lbs. Maximum Weight (Utility) 2800 lbs. Maximum Zero Fuel Weight Normal Category 2852 lbs. Station 106.74 (24.69% MAC) to Sta. 110.50 (31.5% MAC) 2250 lbs. Sta. 99.75 (12.0% MAC) varying Linearly to 2852 lbs. Sta. 106.74 (24.69% MAC) Utility Category 2500 lbs. Station 102.66 (17.27% MAC) to Sta. 107.46 (26.0% MAC) 2250 lbs. Sta. 99.75 (12.0% MAC) varying Linearly to 2500 lbs. Sta. 102.66 (17.27% MAC) Minimum Weight 2023 lbs. at Sta. 99.75 (12.00% MAC) to (Normal & Utility) 2028 lbs. at Sta. 101.24 (14.70% MAC) to 2266 lbs. at Sta. 107.46 (26.00% MAC) to 2503 lbs. at Sta. 110.50 (31.50% MAC) – Normal Category Only. Straight line variation between points. 5 A12SO, Rev.23 II. Model 114 (cont’d) No. of Seats 2 Occupants at (+ 99.0) 2 Occupants at (+ 136.0) Normal Category Only Maximum Baggage 200 lbs. (at + 164.0) Fuel Capacity 68 gal. usable (2 wing tanks) at 108.6 (See Note 1 for unusable fuel). Oil Capacity 8 qts. At +43.0 (6 qts. usable) (See Note 1 for data on unusable oil). Control Surface Movements Wing Flaps Up 0° ± 1° Down 35° + 0° - 2° Aileron Up 20° to 27° Down 7° to 11° (Max up must be within 4° left to right) Rudder Left 22° ± 2° Right 28°* ± 2° Elevator Up 30° ± 2° Down 13° + 2° -1° Elevator Up 15° ± 2° Down 26° ± 1° *Front vertical stabilizer centerline Nose Wheel Movement Steering ± 15° Castoring ± 30° Serial Nos. Eligible 14000 thru 14459 (See Note 7) III. Model 112TC, 4 PCLM (Normal Category), Approved April 27, 1976 Engine Lycoming TO-360-C1A6D Fuel 100/130 minimum grade aviation gasoline Engine Limits For all operations, 2575 rpm, 42” Hg. (210 hp) to 8,000 ft., 40” Hg. 8,001 ft. to 16,000 ft., 38” Hg. 16,001 ft. to 20,000 ft. Propeller and Hartzell Constant Speed, Model HC-E2YR-1BF/F8467-7R Propeller Limits Blade: Model F8467-7R Pitch: High 29° - 32°, Low 15.0° ± 0.1° at Blade Station 30” Diameter: Not over 77”, not under 76.5” Governor: Edo-Aire 34-828-014-5 Spinner: 46390-3 Limitations: Continuous operation between 2250 and 2450 rpm with manifold pressure below 20” Hg. is prohibited. Continuous operation below 2350 rpm at manifold pressure above 34” Hg. is prohibited. Maximum Authorized Altitude 20,000 ft. Airspeed Limits Never exceed 180 Kts (207 mph) CAS Max. structural cruising 143 Kts (165 mph) CAS *Maneuvering 110 Kts (127 mph) CAS @ 2850 lbs. 92 Kts (106 mph) CAS @ 1998 lbs. Flaps extended Up to 20° 150 Kts (173 mph) CAS 20° to 25° 120 Kts (138 mph) CAS 25° to 35° 109 Kts (125 mph) CAS Max. gear extended 180 Kts (207 mph) CAS Max. gear operating 130 Kts (150 mph) CAS Max. cowl flap open 130 Kts (150 mph) CAS Max. side window open 130 Kts (150 mph) CAS * Assume straight line variation between points. 6 A12SO, Rev.23 III. Model 112TC (cont’d) C.G. Range Forward: 105.05” aft of datum (24.84% MAC) at 2850 lbs. 102.20” aft of datum (20.07% MAC) at 2608 lbs. 101.00” aft of datum (18.07% MAC) at 2200 lbs. 101.00” aft of datum (18.07% MAC) at 2005 lbs. Aft: 109.20” aft of datum (31.77% MAC) at 2850 lbs. 109.20” aft of datum (31.77% MAC) at 2229 lbs. Straight line variation between points. Empty Weight C.G. Range None Datum 62.5” forward of Firewall (front face) Leveling Means Bottom of fuselage, outer surface, from F.S. 62.5 to F.S. 97.6 Maximum Weight 2850 lbs. Max. Zero Fuel Weight 2720 lbs. Sta. 106.20 (26.76% MAC) to Sta. 109.20 (31.77% MAC) 2200 lbs. Sta. 101.00 (18.07% MAC) varying Linearly to 2331 lbs. Sta. 101.38 (18.70% MAC) Varying linearly to 2720 lbs. Sta. 106.20 (26.76% MAC) Minimum Weight 2005 lbs. at Sta. 101.0” (18.07% MAC) to 1998 lbs. at Sta. 102.42” (20.44% MAC) to 2035 lbs. at Sta. 106.0” (26.42% MAC) to 2229 lbs. at Sta. 109.2” (31.77% MAC) Straight line variation between points. No. of Seats 2 Occupants at (+ 99.0) 2 Occupants at (+ 136.0) Maximum Baggage 200 lbs. at (+ 164.0) Fuel Capacity 48 gal. usable (2 wing tanks) at 108.6 (Std.) 68 gal. usable (2 wing tanks) at 108.6 (Opt.) (See Note 1 for unusable fuel). Oil Capacity 8 qts. at +45.5 (6 qts. usable) (See Note 1 for undrainable oil). Control Surface Movements Wing Flaps Up 0° ± 1° Down 35° ± 2° Aileron Up 20° to 27° Down 7° to 11° (Max up must be within 4° left to right) Rudder Left 22° ± 2° Right 28°* ± 2° Elevator Up 30° ± 2° Down 13° + 2° -1° Elevator Up 15° ± 2° Down 26° ± 1° *Front vertical stabilizer centerline Nose Wheel Movement Steering ± 15° Castoring ± 30° Serial Nos. Eligible 13001 thru 13108 IV. Model 112B, 4 PCLM (Normal Category), Approved October 5, 1976, (Utility Category), Approved March 31, 1977 Engine Lycoming IO-360-C1D6 Fuel 100/130 minimum grade aviation gasoline 7 A12SO, Rev.23 IV. Model 112B (cont’d) Engine Limits For all operations, 2700 rpm (200 hp) Propeller and Hartzell Constant Speed, Model HC-E2YR-1BF/F8467-7R or Propeller Limits HC-E2YK-1BF/F8467-7R Blade: Model F8467-7R Pitch: High 29° - 32°, Low 11.6° ± 0.1° at Blade Station 30” Diameter: Not over 77”, not under 76.5” Governor: Edo-Aire 34-828-014-2 Spinner: Hartzell C-3533 or C-3533P or Aero Commander 46390-3 Limitations: Do not exceed 24” Hg. manifold pressure below 2350 rpm Airspeed Limits Never exceed 180 Kts (207 mph) CAS Max. structural cruising 143 Kts (165 mph) CAS *Maneuvering (Normal) 109 Kts (125 mph) CAS @ 2800 lbs. 92 Kts (106 mph) CAS @ 1998 lbs. *Maneuvering (Utility) 115 Kts (133 mph) CAS @ 2700 lbs. 99 Kts (114 mph) CAS @ 1998 lbs. Flaps extended Up to 20° 150 Kts (173 mph) CAS 20° to 25° 120 Kts (138 mph) CAS 25° to 35° 109 Kts (125 mph) CAS Max. gear extended 180 Kts (207 mph) CAS Max. gear operating 130 Kts (150 mph) CAS Max. side window open 130 Kts (150 mph) CAS * Assume straight line variation between points. C.G. Range Normal Category Forward: 104.90” aft of datum (24.58% MAC) at 2800 lbs. 102.20” aft of datum (20.07% MAC) at 2608 lbs. 101.00” aft of datum (18.07% MAC) at 2200 lbs. 101.00” aft of datum (18.07% MAC) at 2005 lbs. Aft: 109.20” aft of datum (31.77% MAC) at 2800 lbs. 109.20” aft of datum (31.77% MAC) at 2229 lbs. Straight line variation between points. Utility Category Forward: 103.28” aft of datum (21.87% MAC) at 2700 lbs. 102.20” aft of datum (20.07% MAC) at 2608 lbs. 101.00” aft of datum (18.07% MAC) at 2200 lbs. 101.00” aft of datum (18.07% MAC) at 2005 lbs. Aft: 106.0” aft of datum (26.42% MAC) at 2700 lbs. 106.0” aft of datum (26.42% MAC) at 2035 lbs. Straight line variations between points. Empty Weight C.G. Range None Datum 62.5” forward of Firewall (front face) Leveling Means Bottom of fuselage, outer surface, from F.S. 62.5 to F.S. 97.6 Maximum Weight Normal - 2800 lbs. Utility – 2700 lbs. Max. Zero Fuel Weight Normal Category 2620 lbs. Sta. 107.00 (28.09% MAC) to Sta. 109.20 (31.77% MAC) 2200 lbs. Sta. 101.00 (18.07% MAC) varying Linearly to 2620 lbs. Sta. 107.00 (28.09% MAC) 8 A12SO, Rev.23 IV. Model 112B (cont’d) Max. Zero Fuel Weight (cont’d) Utility Category 2292 lbs. Sta. 102.33 (20.29% MAC) to Sta. 106.00 (26.42% MAC) 2200 lbs. Sta. 101.00 (18.07% MAC) varying Linearly to 2292 lbs. Sta. 102.33 (20.29% MAC) Minimum Weight 2005 lbs. at Sta. 101.0” (18.07% MAC) to 1998 lbs. at Sta. 102.42” (20.44% MAC) to 2035 lbs. at Sta. 106.0” (26.42% MAC) to 2229 lbs. at Sta. 109.2” (31.77% MAC) – Normal Category Only Straight line variation between points. No. of Seats 2 Occupants at (+ 99.0) 2 Occupants at (+ 136.0) – Normal Category Only Maximum Baggage 200 lbs. at (+ 164.0) Fuel Capacity 48 gal. usable (2 wing tanks) at 108.6 (Std.) 68 gal. usable (2 wing tanks) at 108.6 (Opt.) (See Note 1 for unusable fuel). Oil Capacity 8 qts. At +46.5 (6 qts. usable) (See Note 1 for undrainable oil). Control Surface Movements Wing Flaps Up 0° ± 1° Down 35° ± 2° Aileron Up 20° to 27° Down 7° to 11° (Max up must be within 4° left to right) Rudder Left 23° ± 1° Right 28°* ± 2° Elevator Up 30° ± 2° Down 13° + 2° -1° Elevator Up 15° ± 2° Down 26° ± 1° *Front vertical stabilizer centerline Nose Wheel Movement Steering ± 15° Castoring ± 30° Serial Nos. Eligible 13000, 500 thru 544 (See Note 7) V. Model 112TCA, 4 PCLM (Normal Category), Approved December 7, 1976, (Utility Category), Approved March 31, 1977 Engine Lycoming TO-360-C1A6D Fuel 100/130 minimum grade aviation gasoline Engine Limits For all operations, 2575 rpm, 42” Hg. (210 hp) to 8,000 ft., 40” Hg. 8,001 ft., 38” Hg. 16,001 ft. to 20,000 ft. Propeller and Hartzell Constant Speed, Model HC-E2YR-1BF/F8467-7R Propeller Limits Blade: Model F8467-7R Pitch: High 29° - 32°, Low 15.0° ± 0.1° at Blade Station 30” Diameter: Not over 77”, not under 76.5” Governor: Edo-Aire 34-828-014-5 Spinner: 46390-3 Limitations: Continuous operation between 2250 and 2450 rpm with manifold pressure below 20” Hg. is prohibited. Continuous operation below 2350 rpm at manifold pressure above 34” Hg. is prohibited. Max. Authorized Altitude 20,000 9 A12SO, Rev.23 V. Model 112TCA (cont’d) Airspeed Limits Never exceed 180 Kts (207 mph) CAS Max. structural cruising 143 Kts (165 mph) CAS *Maneuvering (Normal) 111 Kts (128 mph) CAS @ 2950 lbs. 98 Kts (113 mph) CAS @ 2300 lbs. 91 Kts (105 mph) CAS @ 1998 lbs. *Maneuvering (Utility) 117 Kts (135 mph) CAS @ 2800 lbs. 115 Kts (133 mph) CAS @ 2708 lbs. 99 Kts (114 mph) CAS @ 1998 lbs. Flaps extended Up to 20° 150 Kts (173 mph) CAS 20° to 25° 120 Kts (138 mph) CAS 25° to 35° 109 Kts (125 mph) CAS Max. gear extended 180 Kts (207 mph) CAS Max. gear operating 130 Kts (150 mph) CAS Max. side window open 130 Kts (150 mph) CAS * Assume straight line variation between points. C.G. Range Normal Category Forward: 106.29” aft of datum (26.91% MAC) at 2962 lbs. 102.20” aft of datum (20.07% MAC) at 2608 lbs. 101.00” aft of datum (18.07% MAC) at 2200 lbs. 101.00” aft of datum (18.07% MAC) at 2005 lbs. Aft: 109.20” aft of datum (31.77% MAC) at 2962 lbs. 109.20” aft of datum (31.77% MAC) at 2229 lbs. Straight line variation between points. Utility Category Forward: 104.44” aft of datum (23.82% MAC) at 2800 lbs. 102.20” aft of datum (20.07% MAC) at 2608 lbs. 101.00” aft of datum (18.07% MAC) at 2200 lbs. 101.00” aft of datum (18.07% MAC) at 2005 lbs. Aft: 107.0” aft of datum (28.09% MAC) at 2800 lbs. 107.0” aft of datum (28.09% MAC) at 2096 lbs. Straight line variations between points. Empty Weight C.G. Range None Datum 62.5” forward of firewall (front face) Leveling Means Bottom of fuselage, outer surface, from F.S. 62.5 to F.S. 97.6 Maximum Weight Normal Maximum Ramp – 2962 lbs. Maximum Takeoff – 2950 lbs. Utility Maximum Gross – 2800 lbs. Max. Zero Fuel Weight Normal Category 2720 lbs. Sta. 106.20 (26.76% MAC) to Sta. 109.20 (31.77% MAC) 2200 lbs. Sta. 101.00 (18.07% MAC) varying Linearly to 2331 lbs. Sta. 101.38 (18.70% MAC) Varying linearly to 2720 lbs. Sta. 106.20 (26.76% MAC) Utility Category 2500 lbs. Sta. 103.48 (22.20% MAC) to Sta. 107.0 (28.09% MAC) 2200 lbs. Sta. 101.00 (18.07% MAC) varying Linearly to 2331 lbs. Sta. 101.38 (18.70% MAC) Varying linearly to 2500 lbs. Sta. 103.48 (22.20% MAC) 10 A12SO, Rev.23 V. Model 112TCA (cont’d) Minimum Weight 2005 lbs. at Sta. 101.0” (18.07% MAC) to (Normal and Utility) 1998 lbs. at Sta. 102.42” (20.44% MAC) to 2035 lbs. at Sta. 106.0” (26.42% MAC) to 2229 lbs. at Sta. 109.2” (31.77% MAC) – Normal Category Only Straight line variation between points. No. of Seats 2 Occupants at (+ 99.0) 2 Occupants at (+ 136.0) – Normal Category Only Maximum Baggage 200 lbs. at (+ 164.0) Fuel Capacity 48 gal. usable (2 wing tanks) at 108.6 (Std.) 68 gal. usable (2 wing tanks) at 108.6 (Opt.) (See Note 1 for unusable fuel). Oil Capacity 8 qts. at +45.5 (6 qts. usable) (See Note 1 for undrainable oil). Control Surface Movements Wing Flaps Up 0° ± 1° Down 35° ± 2° Aileron Up 20° to 27° Down 7° to 11° (Max up must be within 4° left to right) Rudder Left 23° ± 1° Right 28°* ± 2° Elevator Up 30° ± 2° Down 13° + 2° -1° Elevator Up 15° ± 2° Down 26° ± 1° *Front vertical stabilizer centerline Nose Wheel Movement Steering ± 15° Castoring ± 30° Serial Nos. Eligible 13150 thru 13309 (See Note 7) VI. Model 114A, 4 PCLM (Normal Category), Approved January 22, 1979 Engine Lycoming IO-540-T4B5D Fuel 100/130 minimum grade aviation gasoline Engine Limits For all operations, 2700 rpm, (260 hp) Propeller and McCauley Constant Speed, Model B3D34C405/90DFA-13 Propeller Limits Blade: Model 90DFA-13 Pitch: High 33.0° ± .5°, Low 11.5° ± .2° at Blade Station 30” Diameter: Not over 77”, reduction allowed to 76” Governor: Woodward 210903 Spinner: 46390-501 Limitations: None Airspeed Limits Never exceed SL – 12,500 ft. 186 Kts (214 mph) CAS 16,000 ft. 175 Kts (201 mph) CAS 20,000 ft. 161 Kts (185 mph) CAS 24,000 ft. 147 Kts (169 mph) CAS Max. structural cruising SL – 12,500 ft. 148 Kts (170 mph) CAS 16,000 ft. 139 Kts (160 mph) CAS 20,000 ft. 128 Kts (147 mph) CAS 24,000 ft. 117 Kts (135 mph) CAS 11 A12SO, Rev.23 VI. Model 114A (cont’d) Airspeed Limits (cont’d) *Maneuvering (Normal) 3250 lbs. 118 Kts (135 mph) CAS 2658 lbs. 109 Kts (125 mph) CAS 2023 lbs. 95 Kts (109 mph) CAS Straight line variation between points. Flaps extended Up to 20° 150 Kts (173 mph) CAS* 20° to 25° 120 Kts (138 mph) CAS 25° to 35° 109 Kts (125 mph) CAS Max. gear extended 186 Kts (214 mph) CAS* Max. gear operating 130 Kts (150 mph) CAS Max. side window open 130 Kts (150 mph) CAS * Do not Exceed Vne Schedule C.G. Range Forward: 106.97” aft of datum (25.1% MAC) at 3260 lbs. 101.11” aft of datum (14.5% MAC) at 2658 lbs. 99.75” aft of datum (12.0% MAC) at 2250 lbs. 99.75” aft of datum (12.0% MAC) at 2096 lbs. Aft: 110.50” aft of datum (31.5% MAC) at 3260 lbs. 110.50” aft of datum (31.5% MAC) at 2575 lbs. Straight line variation between points. Empty Weight C.G. Range None Datum 62.5” forward of Firewall (front face) Leveling Means Bottom of fuselage, outer surface, from F.S. 62.5 to F.S. 97.6 Maximum Weight Ramp – 3260 lbs. Takeoff – 3250 lbs. Landing – 3140 lbs. Max. Zero Fuel Weight 3000 lbs. at Sta. 106.83 (24.9% MAC) to Sta. 110.50 (31.5% MAC) 2450 lbs. at Sta. 100.48 (13.3% MAC) varying linearly to 3000 lbs. at Sta. 106.83 (24.9% MAC) Minimum Weight 2095 lbs. at Sta. 99.75” (12.00% MAC) to 2100 lbs. at Sta. 101.24” (14.70% MAC) to 2338 lbs. at Sta. 107.46” (26.00% MAC) to 2575 lbs. at Sta. 110.50” (31.52% MAC) Straight line variation between points. No. of Seats 2 Occupants at (+ 99.0) 2 Occupants at (+ 136.0) Maximum Baggage 200 lbs. at (+ 164.0) Fuel Capacity 68 gal. usable (2 wing tanks) at 108.6 (See Note 1 for unusable fuel) Oil Capacity 8 qts. at +43.0 (6 qts. usable) (See Note 1 for undrainable oil). Control Surface Movements Wing Flaps Up 0° ± 1° Down 35° + 0° - 2° Aileron Up 20° - 27° Down 7° - 11° (Max up must be within 4° left to right) *Rudder Left 22° ± 2° Right 28° ± 2° Elevator Up 30° ± 2° Down 13° + 2° -1° Elevator Up 15° ± 2° Down 26° ± 1° *Front vertical stabilizer centerline 12 A12SO, Rev.23 VI. Model 114A (cont’d) Nose Wheel Movement Steering ± 15° Castoring ± 30° Serial Nos. Eligible 14500 thru 14540 VII. Model 114B, 4 PCLM (Normal Category), Approved May 4, 1992 Engine Lycoming IO-540-T4B5 Fuel 100/130 minimum grade aviation gasoline Engine Limits For all operations, 2700 rpm, (260 hp) Propeller and McCauley Constant Speed, Model B3D32C419/82NHA-5 Propeller Limits Blade: Model 82NHA-5 Pitch: High 33.0° ± .5°, Low 12.6° ± .2° at Blade Station 30” Diameter: Not over 77”, reduction allowed to 75.5” Governor: Woodward 210903 or McCauley D-20309-37 Spinner: 615220-501 Limitations: None Airspeed Limits Never exceed SL – 12,500 ft. 186 Kts (214 mph) CAS 16,000 ft. 175 Kts (201 mph) CAS 20,000 ft. 161 Kts (185 mph) CAS 24,000 ft. 147 Kts (169 mph) CAS Max. structural cruising SL – 12,500 ft. 148 Kts (170 mph) CAS 16,000 ft. 139 Kts (160 mph) CAS 20,000 ft. 128 Kts (147 mph) CAS 24,000 ft. 117 Kts (135 mph) CAS *Maneuvering (Normal) 3250 lbs. 118 Kts (135 mph) CAS 2658 lbs. 109 Kts (125 mph) CAS 2023 lbs. 95 Kts (109 mph) CAS Straight line variation between points. Flaps extended Up to 20° 150 Kts (173 mph) CAS* 20° to 25° 120 Kts (138 mph) CAS 25° to 35° 109 Kts (125 mph) CAS Max. gear extended 186 Kts (214 mph) CAS* Max. gear operating 130 Kts (150 mph) CAS Max. side window open 130 Kts (150 mph) CAS * Do not Exceed Vne Schedule C.G. Range Forward: 106.97” aft of datum (25.1% MAC) at 3260 lbs. 104.05” aft of datum (19.8% MAC) at 3194 lbs. 101.11” aft of datum (14.5% MAC) at 2658 lbs. 99.75” aft of datum (12.0% MAC) at 2250 lbs. 99.75” aft of datum (12.0% MAC) at 2096 lbs. Aft: 110.50” aft of datum (31.5% MAC) at 3260 lbs. 110.50” aft of datum (31.5% MAC) at 2575 lbs. Straight line variation between points. Empty Weight C.G. Range None Datum 62.5” forward of Firewall (front face)