Type Certificate Data Sheet No. A20CE

(1) In full view of the pilot: a. 177RG0001 through 177RG0787 (except 177RG0419) "This airplane must be operated as a normal category airplane in compliance with the operating limitations as stated in the form of placards, markings, and manuals. Maximums Maneuvering speed 130 mph-CAS (113 knots) Gear extension speed 140 mph-CAS (122 knots) Gross weight 2800 lb. Flight load factor Flaps Up +3.8, -1.52 Flaps down +2.0 No acrobatic maneuvers, including spins, approved. Altitude loss in a stall recovery - 190 ft. Flight into known icing conditions prohibited. This airplane is certified for the following flight operations as of date of original airworthiness certificate: IFR - VFR - DAY - NIGHT" (as applicable) A20CE 4 Rev. 23 Data Pertinent to all Models (cont’d) NOTE 2. (cont’d) A. (1) b. 177RG0788 through 177RG1266 "This airplane must be operated as a normal category airplane in compliance with the operating limitations as stated in the form of placards, markings, and manuals. Maximums Maneuvering speed (IAS) 113 knots Gear extension speed (IAS) 125 knots Gross weight 2800 lbs. Flight load factor Flaps Up +3.8, -1.52 Flaps down +2.0 No acrobatic maneuvers, including spins, approved. Altitude loss in a stall recovery - 190 ft. Flight into known icing conditions prohibited. This airplane is certified for the following flight operations as of date of original airworthiness certificate. DAY - NIGHT - VFR - IFR" (as applicable) c. 177RG0419, 177RG1267 and on "This airplane must be operated as a normal category airplane in compliance with the operating limitations as stated in the form of placards, markings, and manuals. Maximums Gross weight 2800 lbs. Flight load factor Flaps Up +3.8, -1.52 Flaps Down +2.0 No acrobatic maneuvers, including spins, approved. Altitude loss in a stall recovery - 190 ft. Flight into known icing conditions prohibited. This airplane is certified for the following flight operations as of date of original airworthiness certificate: DAY - NIGHT - VFR - IFR" (as applicable) d. Near Airspeed Indicator: "Max. Speed - KIAS Maneuver 113 Gear Oper 125 Gear Down 125" (2) On control lock: "Control lock - remove before starting engine." (3) By fuel valve (at appropriate locations): 1971 and 1972 Models a. "On - 50 gal." b. "OFF" 1973 Model and On a. "BOTH - 60 gal." "LEFT - 30 gal." "RIGHT - 30 gal." "Use both for takeoff and landing." "When switching from a dry tank, turn auxiliary pump on and use full rich mixture until power is restored." Rev. 23 5 A20CE Data Pertinent to all Models (cont’d) NOTE 2. (cont’d) A. (4) Aft of fuel tank cap: "Service this airplane with 100/130 grade aviation gasoline." (1971/1972 models) "Total capacity 25.5 gal." "Capacity to line of holes inside filler neck, 22.0 gal." (1973 thru 1977 models) "Service this airplane with 100/130 grade aviation gasoline." "Total capacity 30.5 gal." "Capacity to line of holes inside filler neck, 22.0 gal." (1978 model and on) "Service this airplane with 100LL/100 aviation grade gasoline." "Total capacity 30.5 gal." "Capacity to line of holes inside filler neck, 22.0 gal." (5) In baggage compartment: a. Without hat shelf in baggage wall "120 lb. maximum baggage" "For additional loading instructions see weight and balance data." b. With hat shelf in baggage wall "120 lb. maximum baggage including 12 lb. maximum in baggage wall hat shelf." "For additional loading instructions see weight and balance data." (6) Next to door ventilation windows: a. 177RG0001 through 177RG0787 (except 177RG0419) "Do not open windows above 120 mph or when using alternate static source." b. 177RG0419, 177RG0788 and up. "Do not open windows above 105 knots or when using alternate static source." (7) On airspeed indicator: a. 177RG0001 through 177RG0787 (except 177RG0419) "Radial red line 195 mph (CAS) Yellow arc 160-195 mph (CAS) Green arc 70-160 mph (CAS) White arc 60-110 mph (CAS)" b. 177RG0419, 177RG0788 and up. "Radial red line 174 knots (IAS) Yellow arc 142-174 knots (IAS) Green arc 59-142 knots (IAS) White arc 50- 95 knots (IAS)" (8) On oil temperature gauge: a. Red line at 245° F. b. Green arc 100° to 245° F." (9) On oil pressure gauge: a. "Red line at 25 psi b. Green arc 60 psi to 90 psi c. Red line at 100 psi" (10) Tachometer: "Normal operating - 2100 - 2500 rpm (green arc) Caution - 1400 - 1750 rpm (yellow arc) Maximum allowable - 2700 rpm (red line)" (11) On fuel flow gauge: a. "Red line 10 psi b. Green arc 6 to 13 GPH." (12) Near fuel flow gauge: a. "Max. power Alt. S.L. 4000 8000 12000 b. Mixture GPH 17 15 13 10" A20CE 6 Rev. 23 Data Pertinent to all Models (cont’d) NOTE 2. (cont’d) A. (13) On flap control and indicator: a. 177RG0001 through 177RG0787 (except 177RG0419) "0° to 10° (Blue color code and 150 mph callout; also, mechanical detent at 10°). 10° - 20° - 30° (Indices at these positions with white color code and 110 mph callout; also, mechanical detent at 20°)." b. 177RG0419, 177RG0788 and up. "0° to 10° (Blue color code and 130 knots callout; also, mechanical detent at 10°). 10° - 20° - 30° (Indices at these positions with white color code and 95 knots callout; also, mechanical detent at 20°)." (14) Proximity of tachometer: a. "Avoid continuous operation between 1400-1750 rpm with less than 10" manifold pressure." (15) On cylinder head temperature gauge: a. "Red line at 475° F. b. Green arc 200° to 475° F." . (16) On instrument panel: (1971 model only) a. "Do not turn off alternator in flight except in emergency." (17) On emergency landing gear pump handle cover: On 1971 through 1973 Models "EMERGENCY HAND PUMP PULL UP TO EXTEND GEAR MANUALLY: a. Place gear lever in down position. b. Extend pump handle. c. Pump approximately 40 pressure strokes d. Stop when resistance becomes heavy. e. Verify gear is down by observing green light. IMPORTANT To permit gear retraction after hand pump use pull relief valve knob for a minimum period of five seconds. Then move gear lever to the UP position." On 1974 models and on "EMERGENCY HAND PUMP PULL UP TO EXTEND GEAR MANUALLY: a. Pull out landing gear circuit breaker. b. Place gear lever in DOWN position. c. Extend pump handle. d. Pump approximately 40 pressure strokes. e. Stop when resistance becomes heavy. f. Verify gear is down by observing green light. IMPORTANT To permit normal gear retraction after hand pump use, push in landing gear circuit breaker." (18) On manifold pressure gauge: a. "15 to 25 in. Hg. (green arc)." Rev. 23 7 A20CE NOTE 3. The marking of the airspeed indicator in IAS provides an equivalent level of safety to FAR 23.1545 when approved airspeed calibration data presented in Section V of the Pilot's Operating Handbooks listed below is available to the pilot: 177RG, Cessna P/N D1060-13 (177RG0788 through 177RG1051) 177RG, Cessna P/N D1085-13 (177RG1052 through 177RG1266) 177RG, Cessna P/N D1112-13 (177RG0419, 177RG1267 through 177RG1366) NOTE 4. The cylinder head probe location for the Model 177RG is No. 3 cylinder. NOTE 5. 14-volt electrical system (177RG serials through S/N 177RG1266 except 177RG0419) 28-volt electrical system (177RG serials 177RG0419 and 177RG1267 and up) In addition to the placards specified above, the prescribed operating limitations indicated by an asterisk (*) under Section I of this data sheet must also be displayed by permanent markings. --- END ---