TCDS A18EU

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 Rev. No. 10 9 8 10 10 7 10 7 7 9 8 7 7 10 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A18EU Revision 10 Textron Aviation FR172E FR172F FR172G FR172H FR172J FR172K January 16, 2025 WARNING: Use of alcohol-based fuels can cause serious performance degradation and fuel system component damage and is therefore prohibited on Cessna airplanes. TYPE CERTIFICATE DATA SHEET NO. A18EU This data sheet, which is part of Type Certificate No. A18EU, 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 Textron Aviation Inc. One Cessna Boulevard Wichita, Kansas 67215 Type Certificate Holder Record Cessna Aircraft Company transferred to Textron Aviation Inc. on July 29, 2015 Type Certificate (TC) A18EU was transferred from Reims Aviation S.A., 51 Aerodrome de Reims-Prunay, Reims, France, to Cessna Aircraft Company, Wichita, Kansas, USA, on December 11, 2006. Coincident with this transfer, the Federal Aviation Administration (FAA) has accepted the status of State of Design and State of Manufacture as defined by Annex 8 to the Convention of International Civil Aviation. Prior to December 11, 2006, products identified under TC A18EU were approved by the FAA in accordance with the Federal Aviation Regulation (FAR) appropriate to Imported Products (FAR §21.29). Effective December 11, 2006, and after, these products are to be considered domestic products for the purpose of design certification, continued airworthiness, and administration under FAR §21.21 becomes appropriate. I. Model FR172E, 4 PCLM (Normal category), 2 PCLM (Utility category) approved September 19, 1967 Model FR172F, 4 PCLM (Normal category), 2 PCLM (Utility category) approved October 10, 1968 Engine Rolls Royce Continental IO-360-D *Fuel 100/130 minimum grade aviation gasoline *Engine Limits For all operations, 2800 rpm (210 hp.) A18EU 2 Rev. 10 I. Model FR172E, FR172F (cont’d) Propeller and 1. McCauley propeller Propeller Limits Hub: D2A34C67 Blades: 76C Diameter: Not over 76 in., not under 74.5 in. Pitch at 30-inch station: Low pitch: 11.7  High pitch: 22.5  a. Hydraulic governor: (1) Woodward J210452 (2) McCauley C290-D2/T6 2. McCauley propeller Hub: 1B235/DFC (T-41C) Diameter: Not over 78 in., not under 76.5 in. Static rpm. at max. permissible throttle setting: Not over 2370, not under 2270. No additional tolerance permitted. *Airspeed Limits Maneuvering 127 mph (110 knots) True Ind. (KIAS) Maximum structural cruising 145 mph (126 knots) True Ind. Never exceed 182 mph (158 knots) True Ind. Flaps extended 100 mph ( 87 knots) True Ind. C.G. Range Normal Category (+40.5) to (+47.3) at 2500 lb. (+35.0) to (+47.3) at 1950 lb. Utility Category (+37.5) to (+40.5) at 2200 lb. (+35.0) to (+40.5) at 1950 lb. Straight line variation between points given. Empty Weight C.G. Range None *Maximum Weight 2500 lb. (Normal Category) 2200 lb. (Utility Category) Number of Seats Four (two at +36, two at +70) Maximum Baggage 120 lb. (+95) Fuel Capacity 52 gal. (two 26 gal. ta nks in wings at +48; 46 gal. usable) See NOTE 1 for weight of unusable fuel. Oil capacity 10 qt. at -21.5 (1 qt. unusable) See NOTE 5 for optional oil capacity. Se e NOTE 1 for weight of undrainable oil. Control Surface Movements Wing flaps Takeoff 0  10 Landing 0  40 Ailerons Up 20  Down 15 Elevator Tab Up 28  Down 13 Elevator Up 28  Down 23 (Neutral position measured with the bottom of the balance area flush with the bottom of the stabilizer) Rudder Right 16  Left 16 Serial No’s Eligible FR172E: FR17200001 thru FR17200060 FR172F: FR17200061 thru FR17200145 Rev. 10 3 A18EU II. Model FR172G, 4 PCLM (Normal category), 2 PC LM (Utility category), Approved August 20, 1969 Engine Rolls Royce Continental IO- 360-D, IO-360-C, IO-360-DB, or IO-360-CB *Fuel 100/130 minimum grade aviation gasoline. *Engine limits For all operations, 2800 r.p.m. (210 hp.) Propeller and 1. McCauley propeller 52 lb. (-42) Propeller Limits Hub: D2A34C67 Blades: 76C Diameter: Not over 76 in., not under 74.5 in. Pitch at 30-inch station: Low pitch: 11.7  High pitch: 22.5  a. Hydraulic governor: (1) Woodward J210452, or 4 lb. (-34) (2) McCauley C290-D2/T6 (3) McCauley C290-D3/T6 2. McCauley propeller Hub: 1B235/DFC (T-41C) Diameter: Not over 78 in., not under 76.5 in. Static rpm. at max. permissible throttle setting: Not over 2370, not under 2270. No additional tolerance permitted. *Airspeed limits Maneuvering 125 mph (109 knots) True Ind. Maximum structural cruising 145 mph (126 knots) True Ind. Never exceed 185 mph (160 knots) True Ind. Flaps extended 100 mph ( 87 knots) True Ind. C.G. Range Normal Category (+41.0) to (+47.3) at 2550 lbs. (+35.0) to (+47.3) at 1950 lbs. Utility Category (+37.5) to (+40.5) at 2200 lbs. (+35.0) to (+40.5) at 1950 lbs. Straight line variation between points given. Empty weight C.G. Range None *Maximum weight 2550 lb. (Normal Category) 2200 lb. (Utility Category) Number of seats Four (two at +36, two at +70) Maximum baggage 120 lb. (+95) Fuel capacity 52 gals. (two 26 gal. tanks in wings at +48; 46 gals. usable). See NOTE 1 for weight of unusable fuel. Oil capacity 10 qts. at -21.5 (7 qt. unusable) See NOTE 1 for weight of undrainable oi l. See NOTE 5 for optional oil capacity. Control Surface Wing flaps Takeoff 0  10 Movements Landing 0  40 Ailerons Up 20   1 Down 15   1 Elevator tab Up 28   1 -0 Down 13  + 1 -0 Elevator Up 28   1 -0 Down 23  + 1 -0 (Neutral position measured with the bottom of the balance area flush with the bottom of the stabilizer) Rudder Right 16   1 Left 16   1 (Measured parallel to W.L.) Serial No’s Eligible FR17200146 thru FR17200205 FR17200207 thru FR17200225 A18EU 4 Rev. 10 III. Model FR172H, 4 PCLSM (Normal Category), 2 PC LM (Utility Category), Approved October 9, 1970 Engine Rolls Royce Continental, IO-360-D, IO-360-C, IO-360-DB, IO-360-CB, or IO-360-HB *Fuel 100/130 minimum grade aviation gasoline. *Engine Limits For all operations, 2800 r.p.m. (210 hp.) Propeller and 1. McCauley propeller Propeller Limits Hub: D2A34C67 Blades: 76C Diameter: Not over 76 in., not under 74.5 in. Pitch at 30-inch station: Low pitch: 11.7  High pitch: 22.5  a. Hydraulic governor: (1) Woodward F210452, or (2) McCauley C290-D2/T6 2. McCauley propeller Hub: 2A34C209 Blades: 78CCA Diameter: Not over 78 in., not under 76.5 in. Pitch at 30-inch station: Low pitch: 10.6  High pitch: 22.0  a. Hydraulic governor: (1) Woodward F210452, or (2) McCauley C290-D2/T6 3. McCauley propeller Hub: 2A34C209 Blades: 78CCA-2 Diameter: Not over 76 in., not under 74.5 in. Pitch at 30-inch station: Low pitch: 11.3  High pitch: 22.0  a. Hydraulic governor: (1) Woodward F210452 (2) McCauley C290-D2/T6 (3) McCauley C290-D3/T6 4. McCauley propeller Hub: 1B235/DFC Diameter: Not over 78 in., not under 76.5 in. Static rpm. at max. permissible throttle setting: Not over 2370, not under 2270. No additional tolerance permitted. *Airspeed Limits Maneuvering 125 mph (109 knots) (TIAS) Maximum structural cruising 146 mph (126 knots) Never exceed 185 mph (160 knots) Flaps extended 100 mph ( 87 knots) C.G. Range Normal Category (+41.0) to (+47.3) at 2550 lb. (+35.0) to (+47.3) at 1950 lb. Utility Category (+37.5) to (+40.5) at 2200 lb. (+35.0) to (+40.5) at 1950 lb. Rev. 10 5 A18EU III. Model FR172H (cont’d) Empty Weight C.G. Range None *Maximum Weight 2550 lb. (Normal Category) 2200 lb. (Utility Category) Number of Seats Four (two at +36; two at +70) Maximum Baggage 200 lb. (+95) Fuel Capacity 52 gals. (two 26 gal. ta nks in wings at +48; 46 gal. usable) See NOTE 1 for weight of unusable fuel. Oil Capacity 10 qt. at -21.5 (7 qt. usable) See NOTE 1 for weight of undrainable oil. See NOTE 5 for optional oil capacity. Control Surface Movements Wing flaps Takeoff 0  - 10 Landing 0  - 40  2 Ailerons Up 20   1 Down 15   1 Elevator tab Up 28   1 - 0 Down 13   1 - 0 Elevator Up 28   1 - 0 Down 23   1 - 0 (Neutral position is with measured with the bottom of the balance area flush with the bottom of the stabilizer) Rudder Right 16   1 Left 16   1 (Measured parallel to W.L.) Serial No’s Eligible FR17200226 thru FR17200308 FR17200310 thru FR17200350 IV. Model FR172J, 4 PCLM (Normal Category), 2 PCLM (Utility Category) Approved October 27, 1972 FR172J (thru 1975 Model) Engine Rolls Royce Continental IO-360-H or IO-360-HB *Fuel 100/130 minimum grade aviation gasoline. *Engine Limits For all operations, 2800 r.p.m. (210 hp.) Propeller and 1. McCauley propeller Propeller Limits Hub: 2A34C209 Blades: 78CCA-2 Diameter: Not over 76 in., not under 74.5 in. Pitch at 30-inch station: Low pitch: 11.3  High pitch: 22.0  a. Hydraulic governor: (1) Woodward F210452 (2) McCauley C290-D2/T6 (3) McCauley C290-D3/T6 b. Spinner: Dwg 0550328 *Airspeed Limits (CAS) Maneuvering 118 mph (104 knots) Maximum structural cruising 146 mph (126 knots) Never exceed 185 mph (160 knots) Flaps extended 100 mph ( 87 knots) A18EU 6 Rev. 10 IV. Model FR172J (1976 Model) (cont’d) Engine Rolls Royce Continental IO-360J *Fuel 100/130 minimum grade aviation gasoline. *Engine limits Takeoff (5 min) at 2800 r.p.m. (210 hp) Max. continuous 2600 r.p.m. (195 hp) Propeller and 1. McCauley propeller Propeller Limits Hub: 2A34C209 Blades: 78CCA-2 Diameter: Not over 76 in., not under 74.5 in. Pitch at 30-inch station: Low pitch: 11.3  High pitch: 22.0  a. Hydraulic governor: (1) Woodward F210452 (2) McCauley C290-D2/T6 (3) McCauley C290-D3/T6 b. Spinner: Dwg 0550328 *Airspeed limits (IAS) Maneuve ring 118 m.p.h. (104 knots) Maximum structural cruising 146 m.p.h. (126 knots) Never exceed 185 m.p.h. (160 knots) Flaps extended 100 m.p.h. ( 87 knots) C.G. Range Normal category (+41.0) to (+47.3) at 2550 lb. (+35.0) to (+47.3) at 1950 lb. Utility category (+37.5) to (+40.5) at 2200 lb. (+35.0) to (+40.5) at 1950 lb. Empty Weight C.G. Range None Maximum Weight 2550 lb. (Normal Category) 2200 lb. (Utility Category) Number of Seats Four (two at +36, two at +70) Maximum Baggage 200 lb. (+95) Fuel Capacity 52 gals. (two 26 gal. tanks in wings at +48; 46 gals. usable) See NOTE 1 for weight of unusable fuel. Oil Capacity 10 qts. at -21.5 (7 qt. unusable) See NOTE 1 for weight of undrainable oi l. See NOTE 5 for optional oil capacity. Control Surface Wing Flaps Takeoff 0  - 10 Movements Landing 0  – 40 Ailerons Up 20   1 Down 15   1 Elevator Tab Up 28  + 1 -0 Down 13  + 1 -0 Elevator Up 28  + 1 -0 Down 23  + 1 -0 (Neutral position measured with the bottom of the balance area flush with the bottom of the stabilizer) Rudder Right 16   1 Left 16   1 (Measured parallel to W.L.) Serial No’s Eligible FR17200351 thru FR17200559 FR17200562 thru FR17200590 Rev. 10 7 A18EU V. Model FR172K, 4 PCLM (Normal category), 2 PC LM (Utility category) Approved October 27, 1976 Engine Rolls Royce Continental IO-360-K or IO-360-KB (1977 and 1978 model, 1979 model and On) *Fuel 100/130 minimum grade aviation gasoline (1977 model) 100LL/100 minimum grade aviati on gasoline (1978 model and On) *Engine Limits For all operations, 2600 r.p.m. (195 hp.) Propeller and 1. McCauley propeller Propeller Limits Hub: 2A34C203 Blades: 90DCA-14 Diameter: Not over 76 in., not under 74 in. Pitch settings at 30-inch station: Low pitch: 12.0  High pitch: 25.1  a. Hydraulic governor: McCauley C290D3/T15 b. Spinner: Dwg 0550328 2. McCauley propeller (floatplane only) Hub: 2A34C203 Blades: 90DCA-10 Diameter: Not over 80 in., not under 78.5 in. Pitch settings at 30-inch station: Low pitch: 11.3  High pitch: 25.1  a. Hydraulic governor: McCauley C290D3/T15 b. Spinner: Dwg 0550328 *Airspeed Limits (1977 Model thru 1979 Model) (IAS, see NOTE 7) Maneuvering 105 knots Maximum structural cruising 129 knots Never exceed 153 knots Flaps extended 87 knots (1980 Model and on) Maneuvering 104 knots Maximum structural cruising 129 knots Never exceed 163 knots Flaps extended 85 knots C.G. Range Landplane Normal Category (+41.0) to (+47.3) at 2550 lb. (+35.0) to (+47.3) at 1950 lb. Utility Category (+37.5) to (+40.5) at 2200 lb. (+35.0) to (+40.5) at 1950 lb. Floatplane: (Edo 248B-2400) Normal Category (+39.5) to (+45.5) at 2550 lb. (+37.0) to (+45.5) at 2110 lb. Empty Wt. C.G. Range None Maximum Weight 2550 lb. (Normal Category) 2200 lb. (Utility Category) 2558 lb. Ramp weight (1979 model and on) No. of Seats Four (two at +36, two at +70) A18EU 8 Rev. 10 V. Model FR172K (cont’d) Maximum Baggage 200 lb. (+95) Fuel Capacity 52 gals. (two 36 gal. ta nks in wings at +48) (49 gals. usable). See NOTE 1 for weight of unusable fuel. Oil Capacity 8 qts. at -21.5 (5 qt. usable) Control Surface Movements Wing Flaps Takeoff 0  - 10 (Landplane) Landing 0  - 20 (Floatplane) 0  - 40 + 0, - 2 (1977 model thru 1980 model) Ailerons Up 20   1 Down 15   1 Elevator Tab Up 28   1, -0 Down 13   1, -0 (1977 model thru 1980 model) (All FR172K floatplanes) Up 28  + 1, -0 Down 19  + 1, - 0 (1981 model and On) Elevator Up 28  + 1, -0 Down 23  + 1, -0 (Neutral position measured with the bot tom of the balance area flush with the bottom of the stabilizer.) Rudder Right 16   1 Left 16   1 (Measured parallel to W. L.) Serial No’s Eligible FR17200591 thru FR17200675 Data Pertinent to All Models Datum Front face of firewall Leveling means Upper door sill Certification basis FAR 21.29 CAR 3 effec tive May 15, 1956, with no amendments. TC A18EU issued: September 19, 1967. Date of Application for TC: August 8, 1967. Equipment The basic required as prescribed in the applicable airworthiness requirements (see Certification Basis) must be installed in the aircraft for certification. In addition, the following item of equipment is required: Stall Warning System, Cessna dwg. 0523112 NOTE 1. 1. Model FR172E thru FR172J Current weight and balance report including list of equipment included in certificated empty weight, and loading instructions, when necessary, must be provided for each aircraft at the time of original certification. The certificated empty weight and the corresponding center of gravity location must include unusable fuel of 36 lb. at (+46) and undrainable oil of 0.0 lb. at (-21.5) for Models FR172E through FR172J. 2. Model FR172K and On The certificated empty weight and corresponding center of gravity location must include ususable fuel of 18 lb. at (+46) and full oil of 15 lb. at (-21.5). Rev. 10 9 A18EU NOTE 2. The following placards must be displayed in full view of the pilot: 1. Models FR172E, FR172F, and FR172G: “This airplane must be operated in compliance with the operating limitations stated in the form of placards, markings, and manuals. Normal Category Maximum design weight (___)** Reference weight and balance data for loading instructions. **Use 2500 lb. for Models FR172E and FR172F, and 2550 lb. for Model FR172G. Flight Maneuvering Load Factors Flaps Up +3.8 -1.52 Flaps Down +3.5’ 2. Models FR172E and FR172F only: “Utility category Maximum design weight2200 lb. Baggage compartment and rear must not be occupied. Flight Maneuvering load factors Flaps up +4.4 -1.76 Flaps down +3.5 No acrobatic maneuvers approved except those listed below: Maneuver: Entry Speed: Chandelles 127 mph (110 knots) Lazy eights 127 mph (110 knots) Steep turns 127 mph (110 knots) Spins Slow deceleration Stalls (Except whip stalls) Slow deceleration” 3. Model FR172G only: “Utility category Maximum design weight 2200 lb. Baggage compartment and rear seat must not be occupied. Flight Maneuvering load factors Flaps up +4.4 -1.76 Flaps down +3.5 No acrobatic maneuvers approved except those listed below: Maneuver Entry Speed Chandelles 125 mph (109 knots) Lazy eights 125 mph (109 knots) Steep turns 125 mph (109 knots) Spins Slow deceleration Stalls (Except whip stalls) Slow deceleration” 4. Model FR172H only: “This airplane must be operated in compliance with the operating limitations as stated in the form of placards, markings, and manuals. MAXIMUMS Normal Category Utility Category Maneuvering Speed 125 mph CAS (109 knots) 125 mph. CAS (109 knots) Gross Weight 2550 lb. 2200 lb. Flight Load Factor Flaps Up +3.8 -1.52 +4.4 -1.76 Flaps Down +3.5 +3.5 A18EU 10 Rev. 10 NOTE 2 (cont’d) Normal category – No acrobatic maneuvers including spins approved. Utility category – Baggage compartment and rear seat must not be occupied. NO ACROBATIC MANEUVERS APPROVED EXCEPT THOSE LISTED BELOW Maneuver Max Entry Speed Chandelles 125 mph (109 knots) Lazy eights 125 mph (109 knots) Steep turns 125 mph (109 knots) Spins Slow deceleration Stalls (Except whip stalls) Slow deceleration Spin recovery: Opposite rudder – Forward elevator – Neutralize controls Known icing conditions to be avoided. This airplane is certified for the following flight operations as of date of original airworthiness certificate: (DAY NIGHT VFR IFR) (As applicable)” 5. Model FR172J only “This airplane must be operated in compliance with the operating limitations as stated in the form of placards, markings, and manuals. MAXIMUMS Normal Category Utility Category Maneuvering Speed 118 mph CAS (104 knots) 118 mph. (104 knots) Gross Weight 2550 lb. 2200 lb. Flight Load Factor Flaps Up +3.8 -1.52 +4.4 -1.76 Flaps Down +3.5 +3.50 Normal category – No acrobatic maneuvers including spins approved. Utility category – Baggage compartment and rear seat must not be occupied. NO ACROBATIC MANEUVERS APPROVED EXCEPT THOSE LISTED BELOW Maneuver Recommended Entry Speed Chandelles 125 mph (109 knots) Lazy eights 125 mph (109 knots) Steep turns 118 mph (104 knots) Spins Slow deceleration Stalls (except whip stalls) Slow deceleration Altitude loss in stall recovery – 160 ft. Abrupt use of controls prohibited above 118 mph. Spin Recovery – opposite rudder – forward elevator – neutralize controls. Intentional spins with flaps extended are prohibited. 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)” Rev. 10 11 A18EU NOTE 2 (cont’d) 6. Model FR172K (1977 & 1978 models) (Landplane) “This airplane must be operated in compliance with the operating limitations as stated in the form of placards, markings, and manuals. MAXIMUMS Normal Category Utility Category Maneuvering Speed 105 knots 105 knots Gross Weight 2550 lb. 2200 lb. Flight Load Factor Flaps Up +3.8 -1.52 +4.4 -1.76 Flaps Down +3.0 +3.0 Crosswind 20 knots at 90  Normal category: No acrobatic maneuvers including spins approved. Utility category: Baggage compartment and rear seat must not be occupied. NO ACROBATIC MANEUVERS APPROVED EXCEPT THOSE LISTED BELOW Maneuver Recommended Entry Speed Chandelles 110 knots Lazy eights 110 knots Steep turns 105 knots Spins low deceleration Stalls (except whip stalls) low deceleration Altitude loss in stall recovery – 160 ft. Abrupt use of controls prohibited above 105 knots. Spin Recovery – opposite rudder – forward elevator – neutralize controls. Intentional spins with flaps extended are prohibited. Flight into known icing conditions prohibited. This airplane is certified for the following flight operations as of date of or original airworthiness certificate. (DAY NIGHT VFR IFR) (As applicable)” 7. Model FR172K (1977 and 1978 model) (Floatplane with Edo 248B-2440floats) “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. Maneuvering speed (IAS) 105 knots Gross Weight 2550 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 – 250 feet. 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)” “The markings and placards installed in this airplane contain operating limitations which must be complied with when operating this airplane in the Normal Category. Other operating limitations which must be complied with when operating this airplane in this category or in the Utility Category are contained in the Pilot’s Operating Handbook (POH) and FAA Approved Airplane Flight Manual (AFM). Normal Category – No acrobatic maneuvers, including spins, approved. Utility Category – No acrobatic maneuvers approved except those listed in the POH. A18EU 12 Rev. 10 NOTE 2 (cont’d) Baggage compartment and rear seat must not be occupied. Spin Recovery – Opposite rudder, forward elevator, neutralize controls. 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)” 8. Model FR172K (1979 model and on) (Floatplane with Edo 248B-2440 floats) “The markings and placards installed in this airplane contain operating limitations which must be complied with when operating this airplane in the Normal Category. Other operating limitations which must be complied with when operating this airplane in this category are contained in the POH and FAA Approved AFM. No acrobatic maneuvers, including spins, approved. Flight into known icing conditions prohibited. This airplane is certificated for the following flight operations as of date of original airworthiness certificate: (DAY NIGHT VFR IFR) (As applicable)” 9. Near fuel selector (all models) “When switching from dry tank, turn pump on ‘HIGH’ momentarily” 10. Near flap handle or switch: a. Model FR172E thru FR172J “Avoid slips with extended” b. Model FR172K (1977 model thru 1980 model) W 0  I 10  N 20  G F L 40  A P S AVOID SLIPS WITH FLAPS EXTENDED Rev. 10 13 A18EU NOTE 2 (cont’d) c. FR172K (1981 model and On) W 0  I 10  N 20  G F L 30  A P S AVOID SLIPS WITH FLAPS EXTENDED 11. The following placard must be displayed on the instrument panel: a. Models FR172G and FR172H “Do not turn off alternator in flight except in emergency.” The following placard must be displayed in the baggage compartment. b. Model FR172E thru FR172H “200 pounds maximum baggage or 120 lb. aux. seat passenger. For additional loading instructions see weight and balance data. c. Model FR172J and On “200 lb. baggage or 120 lb. aux. seat passenger forward of baggage door latch. 50 lb. maximum baggage aft of baggage door latch. Maximum 200 lb. combined. For additional loading instructions, see weight and balance data.” d. On control lock: (FR172K and On) “Control lock – Remove before starting engine” e. Near fuel selector va lve handle: (FR172K and On) “BOTH – 49 gal. LEFT – 24.5 gal. RIGHT – 24.5 gal. f. Near fuel tank filter: FR172K (1977 model) “Fuel 100/130 min. grade aviation gasoline Cap. 26 U.S. gal.” FR172K (1978 model and On) “Fuel 100LL or 100 min. grade aviation gasoline Cap. 26 U.S. gal.” g. On instrument panel near manifold pressure/fuel flow gauge: (FR172K and On) “FUEL FLOW AT FULL THROTTLE 2600 RPM S.L. 16 GHP 4000 ft. 14 GHP 8000 ft. 12 GHP 12000 ft. 10 GHP” A18EU 14 Rev. 10 NOTE 3. RESERVED. NOTE 4. RESERVED.