TCDS A-767

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A-767 Type Certificate Holder: Univair Aircraft Corporation 2500 Himalaya Road Aurora, Colorado 80011 I. Models 108 and 108-1, 4 PCL-SM (Normal Category, 2 PCLM (Utility Category; Model 108 (Landplane) Approved July 19, 1946; Model 108 (Seaplane) and Model 108-1 (Landplane and Seaplane) Approved June 4, 1947 Engine Franklin 6A4-150-B31, -B3, or -B4 (See Item 111 for optional engine.) Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2600 r.p.m. (150 hp.) Airspeed Limits Landplane: Maximum structural cruising 117 m.p.h. (102 knots) True Ind. Never exceed Normal 148 m.p.h. (129 knots) True Ind. Never exceed Utility 158 m.p.h. (137 knots) True Ind. Flaps Extended 88 m.p.h. (77 knots) True Ind. Seaplane: Maximum structural cruising 102 m.p.h. (89 knots) True Ind. Never exceed Normal 128 m.p.h. (111 knots) True Ind. Flaps Extended 88 m.p.h. (77 knots) True Ind. Propeller Limits Static r.p.m. at maximum permissible throttle setting: (With Item 1) Not over 2350, not under 2100. No additional tolerance permitted. Diameter: Not over 76 in., not under 74 in. C.G. Range 108 Landplane: Normal and Utility (+10. 6) to (+20.0) 108-1 Landplane: Normal (+10.6) to (+21.3) Utility (+10.6) to (+16.8) 108 and 108-1 Seaplane: Normal only (+11.1) to (+19.8) Page 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 Rev. 28 28 28 28 28 28 28 28 28 28 28 28 28 28 28 28 28 A-767 Revision 28 Univair (Stinson) 108 108-1 108-2 108-3 108-5 October 1, 2011 A-767 Page 2 of 17 I. Models 108 and 108-1 (cont’d) Empty wt. C.G. Range 108 Landplane: Either Category (+9.9) to (+13.0) 108-1 Landplane: Either Category With standard baggage compartment (+9.9) to (+14.4) When Item 402 is installed (+9.9) to (+12.0) 108 Seaplane: (+10.3) to (+13.0) 108-1 Seaplane: With standard baggage compartment (+42) (+10.5) to (+12.0) When Item 402 is installed None When empty weight C.G. falls within pertinent range, computation of critical fore and aft C.G. positions is unnecessary. Ranges are not valid for non-standard arrangements except as noted. Maximum Weight 108 Landplane: Normal 2150 lb. Utility 1900 lb. 108-1 Landplane: Normal 2230 lb. Utility 1925 lb. 108 and 108-1 Seaplane: Normal only 2235 lb. No. Seats 4 (2 at +16 and 2 at +48) Maximum Baggage 108: 50 lb. (+42) under rear seat 108-1: 100 lb. (+42) or 100 lb. (+75.5) when Item 402 is installed Both models: Baggage may be increased to 350 lb. with rear seats removed. Fuel Capacity 40 gal. (Two 20 gal. tanks at +22) (See NOTE 1 regarding unusable fuel.) Oil Capacity 2 gal. (-49) Control Surface Elevator 17° up (flaps up) 20° down Movements 25.5° up (flaps down) Elevator tab 14° up 14° down Rudder 19° left 19° right Aileron 24° up 12° down Flaps 33° down Stabilizer Fixed Serial Nos. Eligible Model 108: 108-1 through 108-742 (except 108-11) Model 108-1: 108-11 and 108-743 through 108-2249 (except 108-1474) and 108-3100 Required Equipment: In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: Landplane: 1, 102, 112, 201, 202, 401(a) or (b) Seaplane: 1, 102, 112, 206, 207, 401(c) Skiplane: 1, 102, 112, and 401(a) with 401(f) or 401(b) with 401(g) A-767 Page 3 of 17 II. Model 108-2, 4 PCL-SM (Normal Category), 2 PCLM (Utility Category), Landplane Approved May 18, 1948, Seaplane Approved January 4, 1949 (Same as Model 108-1 except for engine installation and rudder bungee) Engine Franklin 6A4-165-B3 or 6A4-165-B4 Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2800 r.p.m. (165 hp.) Airspeed Limits Landplane: Max structural cruising 121 m.p.h. (105 knots) True Ind. Never exceed Normal 153 m.p.h. (133 knots) True Ind. Never exceed Utility 164 m. p.h. (143 knots) True Ind. Flaps Extended 88 m.p.h. (77 knots) True Ind. Seaplane: Max structural cruising 102 m.p.h. (89 knots) True Ind. Never exceed Normal 128 m.p.h. (111 knots) True Ind. Flaps Extended 88 m.p.h. (77 knots) True Ind. Propeller Limits Static r.p.m. at maximum permissible throttle setting: (With Item 1) Not over 2320, not under 2100. No additional tolerance permitted. Diameter: Not over 76 in., not under 74 in. C.G. Range Landplane: Normal (+10.6) to (+21.3) Utility (+10.6) to (+16.8) Seaplane: Normal only (+11.1) to (+19.8) Empty wt. C.G. Range Landplane: (Both Categories) With standard baggage compartment (+42) (+9.9) to (+14.4) When Item 402 is installed (+9.9) to (+12.0) Seaplane: (Normal Only) With standard baggage compartment (+42) (+10.5) to (+12.0) When Item 402 is installed None When empty weight C.G. falls within pertinent range, computation of critical fore and aft C.G. positions is unnecessary. Ranges are not valid for non-standard arrangements except as noted. Maximum Weight Landplane: Normal 2230 lb. Utility 1925 lb. Seaplane: Normal only 2235 lb. No. Seats 4 (2 at +16 and 2 at +48) Maximum Baggage 100 lb. (+42) under rear seat, or 100 lb. (+75.5) when Item 402 is installed Baggage may be increased to 350 lb. with rear seats removed. For station wagon model, see NOTE 3(f). Fuel Capacity 40 gal. (Two 20 gal. tanks at +22) (See NOTE 1 regarding unusable fuel.) Oil Capacity 9 qts. (-49) A-767 Page 4 of 17 II. Model 108-2 (cont’d) Control Surface Elevator 17° up (flaps up) 20° down Movements 25.5° up (flaps down) Elevator tab 14° up 14° down Rudder 19° left 19° right Aileron 24° up 12° down Flaps 33° down Stabilizer Fixed Serial Nos. Eligible 108-1474 and 108-2250 through 108-3500 (except 108-3100) Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: Landplane: 1, 102, 112, 201, 202, 401(d) Seaplane: 1, 102, 112, 206, 207, 401(e) Skiplane: 1, 102, 112, 205 and 401(d) III. Model 108-3, 4 PCL-SM (Normal Category); 2 PCLM (Utility Category), Landplane Approved September 17, 1948, Seaplane Approved September 20, 1948 (Same as Model 108-2 except for larger fuel tank, structural changes for increased gross weight, revised vertical tail surfaces and controllable rudder trim tab replaces rudder bungee.) Engine Franklin 6A4-165-B3 or 6A4-165-B4 (See Item 114 for optional engine) Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2800 r.p.m. (165 hp.) Airspeed Limits Landplane: Maximum structural cruising 126 m.p.h. (110 knots) True Ind. Never exceed Normal 158 m.p.h. (137 knots) True Ind. Never exceed Utility 170 m. p.h. (148 knots) True Ind. Flaps Extended 88 m.p.h. (77 knots) True Ind. Seaplane: Maximum structural cruising 112 m.p.h. (97 knots) True Ind. Never exceed Normal 140 m.p.h. (122 knots) True Ind. Flaps Extended 88 m.p.h. (77 knots) True Ind. Propeller Limits Static r.p.m. at maximum permissible throttle setting: Landplane (with Item 1): Not over 2315, not under 2215 Seaplane (with Item 5c): Not over 2500, not under 2400 No additional tolerance permitted. Diameter (Landplane and Seaplane): Not over 76 in., not under 74 in. C.G. Range Landplane: Normal (+16.5) to (+21.9) at 2400 lb. (+10.6) to (+21.9) at 1750 lb. or less Utility (+12.9) to (+17.2) at 2000 lb. (+10.6) to (+17.2) at 1750 lb. or less Seaplane: Normal Only (+16.5) to (+21.9) at 2500 lb. (+11.0) to (+21.9) at 2000 lb. or less A-767 Page 5 of 17 III. Model 108-3 (cont’d) Empty wt. C.G. Range Landplane: With standard baggage compartment (+42) (+10.0) to (+16.0) When Item 402 is installed (+10.0) to (+13.7) As station wagon (2 PCLM), when Item 402 is not installed (+10.0) to (+14.4) Above hold good regardless of category. Seaplane: With standard baggage compartment (+42) (+10.5) to (+16.4) When Item 402 is installed (+10.5) to (+14.2) As station wagon (2 PCSM), when Item 402 is not installed (+10.5) to (+14.9) When empty weight C.G. falls within pertinent range, computation of critical fore and aft C.G. positions is unnecessary. Ranges are not valid for non-standard arrangements except as noted. Maximum Weight Landplane: Normal 2400 lb. Utility 2000 lb. Seaplane: Normal only 2500 lb. No. Seats 4 (2 at +16 and 2 at +48) Maximum Baggage 100 lb. (+42) under rear seat, or 100 lb. (+75.5) when Item 402 is installed. Baggage may be increased to 350 lb. with rear seats removed. For station wagon model, see NOTE 3(f). Fuel Capacity 50 gal. (Two 25 gal. tanks at +22) (See Note 1 regarding unusable fuel.) Oil Capacity 9 qts. (-49) Control Surface Elevator 17° up (flaps up) 20° down Movements 25.5° up (flaps down) Elevator tab 22° up 14° down Rudder 19° left 19° right Rudder tab 18° left 18° right (Landplane) 22° left 14° right (Seaplane) Aileron 24° up 12° down Flaps 1st Position 27° down 2nd Position 33° down Stabilizer Fixed Serial Nos. Eligible 108-3501 and up Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: Landplane: 1, 102, 112, 201(a), 202, 401(h) Seaplane: 5(c), 102, 112, 206, 401(k) Skiplane: 1, 102, 112, 205(a), 401(h) IV. Model 108-5, 4 PCLM (Normal Category); 2 PCLM (Utility Category), Landplane Approved March 16, 1964(Same as Model 108-3 except for engine installation and battery location). Engine Franklin 6A4-335-B1 A-767 Page 6 of 17 IV. Model 108-5 (cont’d) Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2800 r.p.m. (180 hp.) Airspeed Limits Landplane: Maximum structural cruising 126 m.p.h. (110 knots) True Ind. Never exceed Normal 158 m.p.h. (137 knots) True Ind. Never exceed Utility 170 m. p.h. (148 knots) True Ind. Flaps Extended 88 m.p.h. (77 knots) True Ind. C. G. Range Landplane: Normal (+16.5) to (+21.9) at 2400 lb. (+10.6) to (+21.9) at 1750 lb. or less Utility (+12.9) to (+17.2) at 2000 lb. (+10.6) to (+17.2) at 1750 lb. or less Empty wt. C.G. Range Landplane: With standard baggage compartment (+42) (+10.0) to (+16.0) When Item 402 is installed (+10.0) to (+13.7) As station wagon (2 PCLM), when Item 402 is not installed (+10.0) to (+14.4) Above hold good regardless of category. When empty weight C.G. falls within pertinent range, computation of critical fore and aft C.G. positions is unnecessary. Ranges are not valid for non-standard arrangements except as noted. Maximum Weight Landplane: Normal 2400 lb. Utility 2000 lb. No. seats 4 (2 at +16 and 2 at +48) Maximum baggage 100 lb. (+42) under rear seat, or 100 lb. (+75.5) when item 402 is installed. Baggage may be increased to 350 lb. with rear seats removed. For station wagon model, see NOTE 3(f). Fuel Capacity 50 gal. (Two 25 gal. tanks at +22) (See Note 1 regarding unusable fuel.) Oil Capacity 9 qts. (-49) Control Surface Elevator 17° up (flaps up) 20° down Movements 25.5° up (flaps down) Elevator tab 22° up 14° down Rudder 19° left 19° right Rudder tab 18° left 18° right (Landplane) 22° left 14° right (Seaplane) Aileron 24° up 12° down Flaps 1st Position 27° down 2nd Position 33° down Stabilizer Fixed Serial Nos. Eligible 108-3501 and up. A-767 Page 7 of 17 IV. Model 108-5 (cont’d) Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: Landplane: 8, 102, 112, 201(a), 202, 401(h) and 401(p) Skiplane: 8, 102, 112, 205(a) and 401(h) and 401(p) DATA PERTINENT TO ALL MODELS Datum Leading edge of wing Leveling means Inside door frame at top Certification basis Type Certificate No. 767 (CAR 3) Production basis None. Prior to original certifi cation of each aircraft manufactured subsequent to February 16, 1949, an FAA representative must perform a detailed inspection for workmanship, materials, and conformity with the approved technical data and a check of the flight characteristics. Equipment A plus (+) or minus (-) sign preced ing the weight of an item of equipment indicates net weight change when that item is installed. Approval for the installation of all items of equipment listed herein has been obtained by the aircraft manufacturer except those items preceded by an asterisk (*). The asterisk denotes that approval has been obtained by someone other than the aircraft manufacturer. An item marked with an asterisk may not have been manufactured under an FAA monitored or approved quality control system, and therefore conformity must be determined if the item is not identified by a Form FAA-186 or 8130-3 Airworthiness Approval Tag, TSO, PMA or other evidence of FAA production approval. Propellers and Propeller Accessories 1. Propeller - Sensenich 76JA-53, 76JR-53 or any other fixe d pitch wood propeller, which 14 lb. (- 65.5) is eligible for the engine power and speed and which meets the diameter and static r.p.m. limits given under "Propeller limits" (for 6A4-150-B3, -B31, or 6A4-165-B3 only). 2. Propeller spinner (108-6921000) (for fixed pitch propellers) 2 lb. (-66.5) 3. Propeller - Koppers' Aeromatic F200/0076B 32 l b. (-65.5) (a) Models 108 and 108-1 with Franklin 6A4-150-B3 or -B31 engines, (Landplane and Seaplane), Parts List Assembly No. 4243: Low pitch setting: 14° measured at 24 in. station. Static r.p.m. at maximum permissible throttle setting: Not over 2600, not under 2500. No additional tolerance permitted. Diameter: Not over 76 in., not under 74 in. The following must be inserted in designated sections of the Airplane Flight Manual: A-767 Page 8 of 17 Propellers and Propeller Accessories 3.(a) (cont’d) Limitations - "Aeromatic Propeller Model F200/0076B, Parts List Assembly No. 4243, installation and operation must be accomplished in accordance with Koppers' Installation Procedure and Operating Limitations No. 10C." Performance Information - "With Koppers' Aeromatic Propeller Model F200/0076B installed the airplane performance has been demonstrated to equal or exceed that presented herein over altitude and temperature range shown". (b) Models 108, 108-1, 108-2 and 108-3 with Fr anklin 6A4-165-B3 engines, (Landplane and Seaplane): (1) F200/0076B, Parts List Assembly No. 4320 or 4320-1 dated October 5, 32 lb. (-65.5) 1948 and Installation Procedure and Operating Limitations No. 11C. (2) F200H/0076B, Parts List Assembly No. 4320H-1 dated May 17, 1950, 2 lb. (-65.5) and adjustment Instructions and Operating Limitations No. 59. (3) Propeller Control Assembly No . 4393 (Installed in accordance with 6 lb. (-45) Koppers Co. Dwg. No. 4320H-1). Static r.p.m. at maximum permissible throttle setting: Not over 2600, not under 2550. No additional tolerance permitted. Low pitch setting: 14.3° measured at 24 in. sta. Diameter: Not over 76 in., not under 74 in. Item 105 engine baffle required when th is propeller installed on 108, 108-1, 108-2, and 108-3 (Landplane and Seaplane). The following placards are required: 1. "Never exceed 2650 r.p.m." 2. Red line on tachometer at 2650 r.p.m. The following must be inserted in designated sections of the Airplane Flight Manual as applicable: Limitations - "Aeromatic Propeller Model ____, Parts List Assembly No. ____ Installation and operations must be accomplished in accordance with Koppers' Installation Procedure and Operating Limitations No. _____ (or Adjustment Instructions and Operating Limitations No. 59).” Performance Section - "With Koppers' Aeromatic Propeller, Model _____, the airplane performance has been demonstrated to equal or exceed that presented herein over the altitude and temperature range shown." A-767 Page 9 of 17 Propellers and Propeller Accessories (cont’d) 4. Propeller - Sensenich 2-position controllable model C-3FR4/PC-376B3: 36 lb. (-66) (a) Models 108, 108-1 and 108-2 with Franklin 6A4-165-B3 engine (Landplane and Seaplane): Diameter: Not more than 76 in., not less than 74 in. Pitch settings measured at 28.5 in. station: Landplane: Low 13.2° High 18.3° Seaplane: Low 11.5° High 17.0° Item 105 must be installed when this propeller is used. (b) Model 108-3 (Landplane and Seaplane): Diameter: Not more than 76 in., not less than 74 in. Pitch settings measured at 28.5 in. station: Landplane: Low 13° High 17.5° Seaplane: Low 11.5° High 17° 5. Propeller - McCauley model 1A170-DM or 1A170-SFC as designated below or any 33 lb. (-65.5) other Model 1A170 propeller which meets the following limits: (a) Models 108 and 108-1 with Franklin 6A4- 150 series engine, (Landplane and Seaplane): Static r.p.m. at maximum permissible throttle setting: Not over 2450 (1A170-xx7649), not under 2200 (1A170 xx7654). No additional tolerance permitted. Diameter: Not over 76 in., not under 74 in. Placard: "Avoid con tinuous engine operation between 2100 and 2300 r.p.m." (b) Models 108, 108-1 and 108-2 with Franklin 6A4-165-B3 engine, (Landplane and Seaplane) and 108-3 (Landplane only): Static r.p.m. at maximum permissible throttle setting: Not over 2500 (1A170-xx7649), not under 2250 (1A170-xx7654). No additional tolerance permitted. Diameter: Not over 76 in., not under 74 in. Tachometer should be marked with a yellow arc between 2150 and 2250 r.p.m.. (c) Model 108-3 (Seaplane only) 1A170-xx7649: Static r.p.m. at maximum permissible th rottle setting: Not over 2500, not under 2400. No additional tolerance permitted. Diameter: Not over 76 in., not under 74 in. A-767 Page 10 of 17 Propellers and Propeller Accessories 5.(c) (cont’d) Tachometer should be marked with a yellow arc between 2150 and 2250 r.p.m.. 1A170-DM propellers are applicable to 6A4-150-B3, -B31 and 6A4-165-B3 engines and 1A170-SFC propellers are applicable to 6A4-150-B4 and 6A4-165-B4 engines. *6. Propeller - Sensenich M74DR, fixed pitch metal: 30 lb. (-65.5) (a) Models 108, 108-1 and 108-2 with Franklin 6A 4-165-B3 engine, (Landplane and Seaplane), and 108-3 (Landplane): Static r.p.m. at maximum permissible throttle setting: Not over 2500, not under 2300. No additional tolerance permitted. Diameter: Not over 74 in., not under 72.5 in. Placard: "Avoid continuous operation between 2150 and 2250 r.p.m. on ground and in flight." Item 401(m) required. (b) Model 108-3 (Seaplane only): Static r.p.m. at maximum permissible throttle setting: Not over 2500, not under 2400. No additional tolerance permitted. Diameter: Not over 74 in., not under 72.5 in. Placard: "Avoid continuous operation between 2150 and 2250 r.p.m. on ground and in flight." Item 401(m) required. *7. Propeller - Hartzell HC12X20-8C/8428-6 or 8433-6 Models 108, 108-1, 108-2 and 108-3 with Lycoming 0-435 Series engine only (Item *110): Diameter: Not over 78 in., not under 76.5 in. Pitch setting measured at 30 in. station: Low 11.5°, high 22.5° Static rpm at maximum permissible throttle setting: Not over 2425, not under 2325. No additional tolerance permitted. 8. Propeller - McCauley - 2A31C21/84S: Models 108-3 and 108-5 with Franklin 6A-335-B1 engine Diameter: Not over 76 in., not under 74 in. Pitch settings measured at 30 in. station: Low 10.7°, High 21.5° Woodward governor, P/N 210453, and Cessna spinner, P/N 0552016 or P/N 0752004, are required with this propeller. A-767 Page 11 of 17 Engines and Engine Accessories - Fuel and Oil Systems 101. Starter (Delco Remy 1109651) 16 lb. (-32) 102. Carburetor air heater 5 lb. (-41) 103. Carburetor air filter (108-6221805) 1 l b . ( - 4 0 ) 104. Cabin heater and control (108-6221209) (Model 108) 1 lb. (-37) Cabin heater and control (108-3092120) (Model 108-1,-2,-3) 6 lb. (-15) 105. Undercylinder engine baffl es (108-6922010 and 108-6222219A) required with Item 3(b) propellers on 108 series (Landplane and Seaplane) with Franklin 6A4-165-B3 engine installed. 106. Oil filter - Fram PB-5 (Stinson Dwg. 108-692200 or Fram kit No. 501, Dwg. 61532). 4 lb. (-25) Weight includes one quart of oil. *107. Oil cooler shutter installation by Baker-Eberle Aviation Corp. Detroit City Airport, 2 lb. (-50) Detroit 5, Michigan, Dwgs. 1 thru 10 dated October 24, 1947. 108. Filtered carburetor hot air induction system. (Stinson Dwg.108-6922011B) (108 series No weight Franklin 6A4-165-B3 engine only) change *109. Engine fire extinguisher system (Van's Air Service Dwg. 7 1/4 - 1, dated July 15, 1949; 25 lb. (-41) with operation instructions 7 1/4 - 1). *110. P. E. Page Aircraft, Lycoming Stinson Conversion Kit for Lycoming 0-435-A or -C engine Use actual installation in Models 108-1, -2, -3, installed in accordance with instructions issued by weight P. E. Page Aircraft, 107 Cheesman, P. O. Box 450, Erie, Colorado 80516 (Landplane Only). Engine - Lycoming 0-435-A or -C Limits: For all operations, 2550 r.p.m (190 hp.) Fuel: 80 min. octane - 0-435-A 73 min. octane - 0-435-C Propeller Item 7 is required with this installation. 111. Franklin 6A4-165-B3 or 6A4-165-B4 engine. Eligible in Models 108 and 108-1 Landplane, Use actual Seaplane or Skiplane) when installed in accordance with Univair Aircraft Corporation weight (Universal Aircraft Industries) Stinson Service Information Letter No. 74A. Engine limits, fuel and propeller limits are the same as shown in Section II for this engine when installed in the Model 108-2. In addition to the required basic 108 or 108-1 CAA Approved Airplane Flight Manual (or Approved Operating Limitations), the FAA Approved Appendix A (Item 401 (n)) is required with this engine installed. Engines and Engine Accessories – Fuel and Oil Systems (cont’d) 112. Oil Cooler: 8.3 lb. (-50.0)