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RISINGUP.COM
RisingUp.com Homepage. Performance information on over 500 general aviation aircraft. Pictures of aircraft. Submit yours! An indexed and cross-referenced database of the Federal Aviation Regulations. Indexed and searchable database of Aviation Links. Practice Private Pilot andInstrument exams.
AIRCRAFT PERFORMANCE DATABASE Aircraft Performance Database. Welcome to the Aircraft Performance Database. You will find performance information on almost any general aviation aircraft that has been in production in the past 40 years. You can find the plane you are looking for two ways. You can search the database using the form below or you can browse the Index ofAircraft
FEDERAL AVIATION REGULATIONS Part 65 - CERTIFICATION: AIRMEN OTHER THAN FLIGHT CREWMEMBERS. Appendices. Appendix C to Part 63 - Flight Engineer Training Course Requirements; Special Federal Aviation Regulation 103 - Process for Requesting Waiver of Mandatory Separation Age for a Federal Aviation Administration Air Traffic Control Specialist In Flight Service Stations, Enroute or Terminal Facilities, and the David J FEDERAL AVIATION REGULATION SEC. 23.149 Sec. 23.149 — Minimum control speed. (a) V MC. is the calibrated airspeed at which, when the critical engine is suddenly made inoperative, it is possible to maintain control of the airplane with that engine still inoperative, and thereafter maintain straight flight at the same speed with an angle of bank of not more than 5 degrees.. The method used to simulate critical engine failure must FEDERAL AVIATION REGULATIONS Federal Aviation Regulations, listing of all regulations in Part 125: CERTIFICATION AND OPERATIONS: AIRPLANES HAVING A SEATING CAPACITY OF 20 OR MORE PASSENGERS OR A MAXIMUM PAYLOAD CAPACITY OF 6,000 POUNDS ORMORE.
FEDERAL AVIATION REGULATION SEC. 23.951 The Federal Aviation Regulation Sec. 23.951 - General. Sec. 23.951 — General. (a) Each fuel system must be constructed and arranged to ensure fuel flow at a rate and pressure established for proper engine and auxiliary power unit functioning under each likely operating condition, including any maneuver for which certification is requested and during which the engine or auxiliary power unit FEDERAL AVIATION REGULATION SEC. 23.561 The Federal Aviation Regulation Sec. 23.561 - General. Sec. 23.561 — General. (a) The airplane, although it may be damaged in emergency landing conditions, must be designed as prescribed in this section to protect each occupant under those conditions. FEDERAL AVIATION REGULATION SEC. 25.807 Sec. 25.807 — Emergency exits. (a) Type. For the purpose of this part, the types of exits are defined as follows: (1) Type I. This type is a floor-level exit with a rectangular opening of not less than 24 inches wide by 48 inches high, with corner radii not greater than eight inches. (2) Type II. This type is a rectangular opening of notless
FEDERAL AVIATION REGULATION APPENDIX G TO PART 25 Appendix G to Part 25 — Continuous Gust Design Criteria. The continuous gust design criteria in this appendix must be used in establishing the dynamic response of the airplane to vertical and lateral continuous turbulence unless a more rational criteria is used. The following gust load requirements apply to mission analysis anddesign
FEDERAL AVIATION REGULATION SEC. 23.967 Sec. 23.967 — Fuel tank installation. (a) Each fuel tank must be supported so that tank loads are not concentrated. In addition—. (1) There must be pads, if necessary, to prevent chafing between each tank and its supports; (2) Padding must be nonabsorbent or treated to prevent the absorption of fuel;RISINGUP.COM
RisingUp.com Homepage. Performance information on over 500 general aviation aircraft. Pictures of aircraft. Submit yours! An indexed and cross-referenced database of the Federal Aviation Regulations. Indexed and searchable database of Aviation Links. Practice Private Pilot andInstrument exams.
AIRCRAFT PERFORMANCE DATABASE Aircraft Performance Database. Welcome to the Aircraft Performance Database. You will find performance information on almost any general aviation aircraft that has been in production in the past 40 years. You can find the plane you are looking for two ways. You can search the database using the form below or you can browse the Index ofAircraft
FEDERAL AVIATION REGULATIONS Part 65 - CERTIFICATION: AIRMEN OTHER THAN FLIGHT CREWMEMBERS. Appendices. Appendix C to Part 63 - Flight Engineer Training Course Requirements; Special Federal Aviation Regulation 103 - Process for Requesting Waiver of Mandatory Separation Age for a Federal Aviation Administration Air Traffic Control Specialist In Flight Service Stations, Enroute or Terminal Facilities, and the David J FEDERAL AVIATION REGULATION SEC. 23.149 Sec. 23.149 — Minimum control speed. (a) V MC. is the calibrated airspeed at which, when the critical engine is suddenly made inoperative, it is possible to maintain control of the airplane with that engine still inoperative, and thereafter maintain straight flight at the same speed with an angle of bank of not more than 5 degrees.. The method used to simulate critical engine failure must FEDERAL AVIATION REGULATIONS Federal Aviation Regulations, listing of all regulations in Part 125: CERTIFICATION AND OPERATIONS: AIRPLANES HAVING A SEATING CAPACITY OF 20 OR MORE PASSENGERS OR A MAXIMUM PAYLOAD CAPACITY OF 6,000 POUNDS ORMORE.
FEDERAL AVIATION REGULATION SEC. 23.951 The Federal Aviation Regulation Sec. 23.951 - General. Sec. 23.951 — General. (a) Each fuel system must be constructed and arranged to ensure fuel flow at a rate and pressure established for proper engine and auxiliary power unit functioning under each likely operating condition, including any maneuver for which certification is requested and during which the engine or auxiliary power unit FEDERAL AVIATION REGULATION SEC. 23.561 The Federal Aviation Regulation Sec. 23.561 - General. Sec. 23.561 — General. (a) The airplane, although it may be damaged in emergency landing conditions, must be designed as prescribed in this section to protect each occupant under those conditions. FEDERAL AVIATION REGULATION SEC. 25.807 Sec. 25.807 — Emergency exits. (a) Type. For the purpose of this part, the types of exits are defined as follows: (1) Type I. This type is a floor-level exit with a rectangular opening of not less than 24 inches wide by 48 inches high, with corner radii not greater than eight inches. (2) Type II. This type is a rectangular opening of notless
FEDERAL AVIATION REGULATION APPENDIX G TO PART 25 Appendix G to Part 25 — Continuous Gust Design Criteria. The continuous gust design criteria in this appendix must be used in establishing the dynamic response of the airplane to vertical and lateral continuous turbulence unless a more rational criteria is used. The following gust load requirements apply to mission analysis anddesign
FEDERAL AVIATION REGULATION SEC. 23.967 Sec. 23.967 — Fuel tank installation. (a) Each fuel tank must be supported so that tank loads are not concentrated. In addition—. (1) There must be pads, if necessary, to prevent chafing between each tank and its supports; (2) Padding must be nonabsorbent or treated to prevent the absorption of fuel; FEDERAL AVIATION REGULATIONS Federal Aviation Regulations, listing of all regulations in Part 33: AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES. AIRCRAFT PERFORMANCE STATS M-7 and MX-7 Series. M-7-235. MX-7-160. MX-7-180A. Manufacturer. Aeronca Aerostar American Champion American General Beechcraft Bellanca Cessna Commander EADS Socata Lake Luscombe Aircraft Maule Mooney Piper PZL. Aircraft Model. Search for aircraft meeting your performance criteria! FEDERAL AVIATION REGULATIONS Federal Aviation Regulations, listing of all regulations in Part 29: AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY ROTORCRAFT. AIRCRAFT PERFORMANCE STATS Aircraft performance stats and information for several MooneyAircraft.
FEDERAL AVIATION REGULATION SEC. 23.1435 Sec. 23.1435 — Hydraulic systems. (a) Design. Each hydraulic system must be designed as follows: (1) Each hydraulic system and its elements must withstand, without yielding, the structural loads expected in addition to hydraulic loads. (2) A means to indicate the pressure in each hydraulic system which supplies two or more primaryfunctions
FEDERAL AVIATION REGULATION SEC. 91.509 Sec. 91.509 — Survival equipment for overwater operations. (a) No person may take off an airplane for a flight over water more than 50 nautical miles from the nearest shore unless that airplane is equipped with a life preserver or an approved flotation means for each occupantof the airplane.
FEDERAL AVIATION REGULATION SEC. 23.729 Sec. 23.729 — Landing gear extension and retraction system. (a) General. For airplanes with retractable landing gear, the following apply: (1) Each landing gear retracting mechanism and its supporting structure must be designed for maximum flight load factors with the gear retracted and must be designed for the combination of friction, inertia, brake torque, and air loads, occurring during FEDERAL AVIATION REGULATION SEC. 23.1325 Sec. 23.1325 — Static pressure system. (a) Each instrument provided with static pressure case connections must be so vented that the influence of airplane speed, the opening and closing of windows, airflow variations, moisture, or other foreign matter will least affect the accuracy of the instruments except as noted in paragraph (b)(3) of this section. FEDERAL AVIATION REGULATION SEC. 23.975 Sec. 23.975 — Fuel tank vents and carburetor vapor vents. (a) Each fuel tank must be vented from the top part of the expansion space. In addition—. (1) Each vent outlet must be located and constructed in a manner that minimizes the possibility of its being obstructed by ice or other foreign matter; (2) Each vent must be constructed to FEDERAL AVIATION REGULATION SEC. 23.1353 Sec. 23.1353 — Storage battery design and installation. (a) Each storage battery must be designed and installed as prescribed in this section. (b) Safe cell temperatures and pressures must be maintained during any probable charging and discharging condition. No uncontrolled increase in cell temperature may result when the batteryis recharged
RISINGUP.COM
RisingUp.com Homepage. Performance information on over 500 general aviation aircraft. Pictures of aircraft. Submit yours! An indexed and cross-referenced database of the Federal Aviation Regulations. Indexed and searchable database of Aviation Links. Practice Private Pilot andInstrument exams.
AIRCRAFT PERFORMANCE DATABASE Aircraft Performance Database. Welcome to the Aircraft Performance Database. You will find performance information on almost any general aviation aircraft that has been in production in the past 40 years. You can find the plane you are looking for two ways. You can search the database using the form below or you can browse the Index ofAircraft
AIRCRAFT PERFORMANCE STATS Aircraft performance stats and information for several MooneyAircraft.
FEDERAL AVIATION REGULATION SEC. 23.561 The Federal Aviation Regulation Sec. 23.561 - General. Sec. 23.561 — General. (a) The airplane, although it may be damaged in emergency landing conditions, must be designed as prescribed in this section to protect each occupant under those conditions. FEDERAL AVIATION REGULATION SEC. 23.149 Sec. 23.149 — Minimum control speed. (a) V MC. is the calibrated airspeed at which, when the critical engine is suddenly made inoperative, it is possible to maintain control of the airplane with that engine still inoperative, and thereafter maintain straight flight at the same speed with an angle of bank of not more than 5 degrees.. The method used to simulate critical engine failure must FEDERAL AVIATION REGULATION SEC. 25.807 Sec. 25.807 — Emergency exits. (a) Type. For the purpose of this part, the types of exits are defined as follows: (1) Type I. This type is a floor-level exit with a rectangular opening of not less than 24 inches wide by 48 inches high, with corner radii not greater than eight inches. (2) Type II. This type is a rectangular opening of notless
FEDERAL AVIATION REGULATION SEC. 23.951 The Federal Aviation Regulation Sec. 23.951 - General. Sec. 23.951 — General. (a) Each fuel system must be constructed and arranged to ensure fuel flow at a rate and pressure established for proper engine and auxiliary power unit functioning under each likely operating condition, including any maneuver for which certification is requested and during which the engine or auxiliary power unit FEDERAL AVIATION REGULATION SEC. 23.1435 Sec. 23.1435 — Hydraulic systems. (a) Design. Each hydraulic system must be designed as follows: (1) Each hydraulic system and its elements must withstand, without yielding, the structural loads expected in addition to hydraulic loads. (2) A means to indicate the pressure in each hydraulic system which supplies two or more primaryfunctions
FEDERAL AVIATION REGULATION SEC. 23.573 Sec. 23.573 — Damage tolerance and fatigue evaluation of structure. (a) Composite airframe structure. Composite airframe structure must be evaluated under this paragraph instead of §§23.571 and 23.572. The applicant must evaluate the composite airframe structure, the failure of which would result in catastrophic loss of the airplane, in FEDERAL AVIATION REGULATION SEC. 23.975 Sec. 23.975 — Fuel tank vents and carburetor vapor vents. (a) Each fuel tank must be vented from the top part of the expansion space. In addition—. (1) Each vent outlet must be located and constructed in a manner that minimizes the possibility of its being obstructed by ice or other foreign matter; (2) Each vent must be constructed toRISINGUP.COM
RisingUp.com Homepage. Performance information on over 500 general aviation aircraft. Pictures of aircraft. Submit yours! An indexed and cross-referenced database of the Federal Aviation Regulations. Indexed and searchable database of Aviation Links. Practice Private Pilot andInstrument exams.
AIRCRAFT PERFORMANCE DATABASE Aircraft Performance Database. Welcome to the Aircraft Performance Database. You will find performance information on almost any general aviation aircraft that has been in production in the past 40 years. You can find the plane you are looking for two ways. You can search the database using the form below or you can browse the Index ofAircraft
AIRCRAFT PERFORMANCE STATS Aircraft performance stats and information for several MooneyAircraft.
FEDERAL AVIATION REGULATION SEC. 23.561 The Federal Aviation Regulation Sec. 23.561 - General. Sec. 23.561 — General. (a) The airplane, although it may be damaged in emergency landing conditions, must be designed as prescribed in this section to protect each occupant under those conditions. FEDERAL AVIATION REGULATION SEC. 23.149 Sec. 23.149 — Minimum control speed. (a) V MC. is the calibrated airspeed at which, when the critical engine is suddenly made inoperative, it is possible to maintain control of the airplane with that engine still inoperative, and thereafter maintain straight flight at the same speed with an angle of bank of not more than 5 degrees.. The method used to simulate critical engine failure must FEDERAL AVIATION REGULATION SEC. 25.807 Sec. 25.807 — Emergency exits. (a) Type. For the purpose of this part, the types of exits are defined as follows: (1) Type I. This type is a floor-level exit with a rectangular opening of not less than 24 inches wide by 48 inches high, with corner radii not greater than eight inches. (2) Type II. This type is a rectangular opening of notless
FEDERAL AVIATION REGULATION SEC. 23.951 The Federal Aviation Regulation Sec. 23.951 - General. Sec. 23.951 — General. (a) Each fuel system must be constructed and arranged to ensure fuel flow at a rate and pressure established for proper engine and auxiliary power unit functioning under each likely operating condition, including any maneuver for which certification is requested and during which the engine or auxiliary power unit FEDERAL AVIATION REGULATION SEC. 23.1435 Sec. 23.1435 — Hydraulic systems. (a) Design. Each hydraulic system must be designed as follows: (1) Each hydraulic system and its elements must withstand, without yielding, the structural loads expected in addition to hydraulic loads. (2) A means to indicate the pressure in each hydraulic system which supplies two or more primaryfunctions
FEDERAL AVIATION REGULATION SEC. 23.573 Sec. 23.573 — Damage tolerance and fatigue evaluation of structure. (a) Composite airframe structure. Composite airframe structure must be evaluated under this paragraph instead of §§23.571 and 23.572. The applicant must evaluate the composite airframe structure, the failure of which would result in catastrophic loss of the airplane, in FEDERAL AVIATION REGULATION SEC. 23.975 Sec. 23.975 — Fuel tank vents and carburetor vapor vents. (a) Each fuel tank must be vented from the top part of the expansion space. In addition—. (1) Each vent outlet must be located and constructed in a manner that minimizes the possibility of its being obstructed by ice or other foreign matter; (2) Each vent must be constructed toPRACTICE TESTS
Reporting of Aircraft Accidents, Incidents, and Overdue Aircraft. AC 61-23 -- Pilot's Handbook of Aeronautical Knowledge. Forces Acting on the Airplane in Flight. Turning Tendency (Torque Effect) Airplane Stability. Loads and Load Factors. Flight control Systems. Engine Operation. Propeller. FEDERAL AVIATION REGULATIONS INDEX OF ALL FEDERAL AVIATION Part 1 - DEFINITIONS AND ABBREVIATIONS. Part 3 - GENERAL REQUIREMENTS. Subchapter B – Procedural Rules. Part 11 - GENERAL RULEMAKING PROCEDURES. Part 13 - INVESTIGATIVE AND ENFORCEMENT PROCEDURES. Part 14 - RULES IMPLEMENTING THE EQUAL ACCESS TO JUSTICE ACT OF 1980. Part 15 - ADMINISTRATIVE CLAIMS UNDER FEDERAL TORT CLAIMS ACT. FEDERAL AVIATION REGULATIONS Part 65 - CERTIFICATION: AIRMEN OTHER THAN FLIGHT CREWMEMBERS. Appendices. Appendix C to Part 63 - Flight Engineer Training Course Requirements; Special Federal Aviation Regulation 103 - Process for Requesting Waiver of Mandatory Separation Age for a Federal Aviation Administration Air Traffic Control Specialist In Flight Service Stations, Enroute or Terminal Facilities, and the David J AIRCRAFT PERFORMANCE STATS PA-31-300 Navajo. PA-31-310 Turbo Navajo. PA-31-310 Turbo Navajo B,C (prior to 1980 has less fuel) PA-31-325Navajo C/R. PA-31-350 Chieftain. PA-31P-350 Mojave. PA31 P Press Navajo (after 1977) FEDERAL AVIATION REGULATIONS Part 93 - SPECIAL AIR TRAFFIC RULES. Appendices. Appendix G to Part 91 - Operations in Reduced Vertical Separation Minimum (RVSM) Airspace; Special Federal Aviation Regulation 105 - Operating Limitations for Unscheduled Operations at Chicago's O'Hare International Airport AIRCRAFT PERFORMANCE STATS M-7 and MX-7 Series. M-7-235. MX-7-160. MX-7-180A. Manufacturer. Aeronca Aerostar American Champion American General Beechcraft Bellanca Cessna Commander EADS Socata Lake Luscombe Aircraft Maule Mooney Piper PZL. Aircraft Model. Search for aircraft meeting your performance criteria! FEDERAL AVIATION REGULATIONS SEARCH RESULTS FARs Search Results. Sec. 91.1015 - Management specifications. Sec. 121.187 - Airplanes: Reciprocating engine-powered: Landing limitations: Alternate airport. FEDERAL AVIATION REGULATION SEC. 23.1309 Sec. 23.1309 — Equipment, systems, and installations. (1) When performing its intended function, may not adversely affect the response, operation, or accuracy of any—. (i) Equipment essential to safe operation; or. (ii) Other equipment unless there is a means to inform the pilot of the effect. (2) In a single-engine airplane, mustbe
FEDERAL AVIATION REGULATION SEC. 23.1325 Sec. 23.1325 — Static pressure system. (a) Each instrument provided with static pressure case connections must be so vented that the influence of airplane speed, the opening and closing of windows, airflow variations, moisture, or other foreign matter will least affect the accuracy of the instruments except as noted in paragraph (b)(3) of this section. FEDERAL AVIATION REGULATION SEC. 23.993 Sec. 23.993 — Fuel system lines and fittings. (a) Each fuel line must be installed and supported to prevent excessive vibration and to withstand loads due to fuel pressure and accelerated flight conditions. (b) Each fuel line connected to components of the airplane between which relative motion could exist must have provisions forflexibility.
RISINGUP.COM
RisingUp.com Homepage. Performance information on over 500 general aviation aircraft. Pictures of aircraft. Submit yours! An indexed and cross-referenced database of the Federal Aviation Regulations. Indexed and searchable database of Aviation Links. Practice Private Pilot andInstrument exams.
AIRCRAFT PERFORMANCE DATABASE Aircraft Performance Database. Welcome to the Aircraft Performance Database. You will find performance information on almost any general aviation aircraft that has been in production in the past 40 years. You can find the plane you are looking for two ways. You can search the database using the form below or you can browse the Index ofAircraft
AIRCRAFT PERFORMANCE STATS M-7 and MX-7 Series. M-7-235. MX-7-160. MX-7-180A. Manufacturer. Aeronca Aerostar American Champion American General Beechcraft Bellanca Cessna Commander EADS Socata Lake Luscombe Aircraft Maule Mooney Piper PZL. Aircraft Model. Search for aircraft meeting your performance criteria! FEDERAL AVIATION REGULATION SEC. 23.149 Sec. 23.149 — Minimum control speed. (a) V MC. is the calibrated airspeed at which, when the critical engine is suddenly made inoperative, it is possible to maintain control of the airplane with that engine still inoperative, and thereafter maintain straight flight at the same speed with an angle of bank of not more than 5 degrees.. The method used to simulate critical engine failure must AIRCRAFT PERFORMANCE STATS Aircraft performance stats and information for several MooneyAircraft.
FEDERAL AVIATION REGULATION SEC. 25.807 Sec. 25.807 — Emergency exits. (a) Type. For the purpose of this part, the types of exits are defined as follows: (1) Type I. This type is a floor-level exit with a rectangular opening of not less than 24 inches wide by 48 inches high, with corner radii not greater than eight inches. (2) Type II. This type is a rectangular opening of notless
FEDERAL AVIATION REGULATION SEC. 23.951 The Federal Aviation Regulation Sec. 23.951 - General. Sec. 23.951 — General. (a) Each fuel system must be constructed and arranged to ensure fuel flow at a rate and pressure established for proper engine and auxiliary power unit functioning under each likely operating condition, including any maneuver for which certification is requested and during which the engine or auxiliary power unit FEDERAL AVIATION REGULATION SEC. 23.1435 Sec. 23.1435 — Hydraulic systems. (a) Design. Each hydraulic system must be designed as follows: (1) Each hydraulic system and its elements must withstand, without yielding, the structural loads expected in addition to hydraulic loads. (2) A means to indicate the pressure in each hydraulic system which supplies two or more primaryfunctions
FEDERAL AVIATION REGULATION SEC. 23.573 Sec. 23.573 — Damage tolerance and fatigue evaluation of structure. (a) Composite airframe structure. Composite airframe structure must be evaluated under this paragraph instead of §§23.571 and 23.572. The applicant must evaluate the composite airframe structure, the failure of which would result in catastrophic loss of the airplane, in FEDERAL AVIATION REGULATION SEC. 23.975 Sec. 23.975 — Fuel tank vents and carburetor vapor vents. (a) Each fuel tank must be vented from the top part of the expansion space. In addition—. (1) Each vent outlet must be located and constructed in a manner that minimizes the possibility of its being obstructed by ice or other foreign matter; (2) Each vent must be constructed toRISINGUP.COM
RisingUp.com Homepage. Performance information on over 500 general aviation aircraft. Pictures of aircraft. Submit yours! An indexed and cross-referenced database of the Federal Aviation Regulations. Indexed and searchable database of Aviation Links. Practice Private Pilot andInstrument exams.
AIRCRAFT PERFORMANCE DATABASE Aircraft Performance Database. Welcome to the Aircraft Performance Database. You will find performance information on almost any general aviation aircraft that has been in production in the past 40 years. You can find the plane you are looking for two ways. You can search the database using the form below or you can browse the Index ofAircraft
AIRCRAFT PERFORMANCE STATS M-7 and MX-7 Series. M-7-235. MX-7-160. MX-7-180A. Manufacturer. Aeronca Aerostar American Champion American General Beechcraft Bellanca Cessna Commander EADS Socata Lake Luscombe Aircraft Maule Mooney Piper PZL. Aircraft Model. Search for aircraft meeting your performance criteria! FEDERAL AVIATION REGULATION SEC. 23.149 Sec. 23.149 — Minimum control speed. (a) V MC. is the calibrated airspeed at which, when the critical engine is suddenly made inoperative, it is possible to maintain control of the airplane with that engine still inoperative, and thereafter maintain straight flight at the same speed with an angle of bank of not more than 5 degrees.. The method used to simulate critical engine failure must AIRCRAFT PERFORMANCE STATS Aircraft performance stats and information for several MooneyAircraft.
FEDERAL AVIATION REGULATION SEC. 25.807 Sec. 25.807 — Emergency exits. (a) Type. For the purpose of this part, the types of exits are defined as follows: (1) Type I. This type is a floor-level exit with a rectangular opening of not less than 24 inches wide by 48 inches high, with corner radii not greater than eight inches. (2) Type II. This type is a rectangular opening of notless
FEDERAL AVIATION REGULATION SEC. 23.951 The Federal Aviation Regulation Sec. 23.951 - General. Sec. 23.951 — General. (a) Each fuel system must be constructed and arranged to ensure fuel flow at a rate and pressure established for proper engine and auxiliary power unit functioning under each likely operating condition, including any maneuver for which certification is requested and during which the engine or auxiliary power unit FEDERAL AVIATION REGULATION SEC. 23.1435 Sec. 23.1435 — Hydraulic systems. (a) Design. Each hydraulic system must be designed as follows: (1) Each hydraulic system and its elements must withstand, without yielding, the structural loads expected in addition to hydraulic loads. (2) A means to indicate the pressure in each hydraulic system which supplies two or more primaryfunctions
FEDERAL AVIATION REGULATION SEC. 23.573 Sec. 23.573 — Damage tolerance and fatigue evaluation of structure. (a) Composite airframe structure. Composite airframe structure must be evaluated under this paragraph instead of §§23.571 and 23.572. The applicant must evaluate the composite airframe structure, the failure of which would result in catastrophic loss of the airplane, in FEDERAL AVIATION REGULATION SEC. 23.975 Sec. 23.975 — Fuel tank vents and carburetor vapor vents. (a) Each fuel tank must be vented from the top part of the expansion space. In addition—. (1) Each vent outlet must be located and constructed in a manner that minimizes the possibility of its being obstructed by ice or other foreign matter; (2) Each vent must be constructed toPRACTICE TESTS
Reporting of Aircraft Accidents, Incidents, and Overdue Aircraft. AC 61-23 -- Pilot's Handbook of Aeronautical Knowledge. Forces Acting on the Airplane in Flight. Turning Tendency (Torque Effect) Airplane Stability. Loads and Load Factors. Flight control Systems. Engine Operation. Propeller. FEDERAL AVIATION REGULATIONS INDEX OF ALL FEDERAL AVIATION Part 1 - DEFINITIONS AND ABBREVIATIONS. Part 3 - GENERAL REQUIREMENTS. Subchapter B – Procedural Rules. Part 11 - GENERAL RULEMAKING PROCEDURES. Part 13 - INVESTIGATIVE AND ENFORCEMENT PROCEDURES. Part 14 - RULES IMPLEMENTING THE EQUAL ACCESS TO JUSTICE ACT OF 1980. Part 15 - ADMINISTRATIVE CLAIMS UNDER FEDERAL TORT CLAIMS ACT. FEDERAL AVIATION REGULATIONS Part 65 - CERTIFICATION: AIRMEN OTHER THAN FLIGHT CREWMEMBERS. Appendices. Appendix C to Part 63 - Flight Engineer Training Course Requirements; Special Federal Aviation Regulation 103 - Process for Requesting Waiver of Mandatory Separation Age for a Federal Aviation Administration Air Traffic Control Specialist In Flight Service Stations, Enroute or Terminal Facilities, and the David J AIRCRAFT PERFORMANCE STATS PA-31-300 Navajo. PA-31-310 Turbo Navajo. PA-31-310 Turbo Navajo B,C (prior to 1980 has less fuel) PA-31-325Navajo C/R. PA-31-350 Chieftain. PA-31P-350 Mojave. PA31 P Press Navajo (after 1977) FEDERAL AVIATION REGULATIONS SEARCH RESULTS FARs Search Results. Sec. 91.1015 - Management specifications. Sec. 121.187 - Airplanes: Reciprocating engine-powered: Landing limitations: Alternate airport. FEDERAL AVIATION REGULATIONS SEARCH RESULTS FARs Search Results. Sec. 65.104 - Repairman certificate—experimental aircraft builder—Eligibility, privileges and limitations. Sec. 141.61 - Applicability. FEDERAL AVIATION REGULATIONS Part 93 - SPECIAL AIR TRAFFIC RULES. Appendices. Appendix G to Part 91 - Operations in Reduced Vertical Separation Minimum (RVSM) Airspace; Special Federal Aviation Regulation 105 - Operating Limitations for Unscheduled Operations at Chicago's O'Hare International Airport FEDERAL AVIATION REGULATION SEC. 23.561 The Federal Aviation Regulation Sec. 23.561 - General. Sec. 23.561 — General. (a) The airplane, although it may be damaged in emergency landing conditions, must be designed as prescribed in this section to protect each occupant under those conditions. FEDERAL AVIATION REGULATION SEC. 23.993 Sec. 23.993 — Fuel system lines and fittings. (a) Each fuel line must be installed and supported to prevent excessive vibration and to withstand loads due to fuel pressure and accelerated flight conditions. (b) Each fuel line connected to components of the airplane between which relative motion could exist must have provisions forflexibility.
FEDERAL AVIATION REGULATION SEC. 23.1353 Sec. 23.1353 — Storage battery design and installation. (a) Each storage battery must be designed and installed as prescribed in this section. (b) Safe cell temperatures and pressures must be maintained during any probable charging and discharging condition. No uncontrolled increase in cell temperature may result when the batteryis recharged
RISINGUP.COM
RisingUp.com Homepage. Performance information on over 500 general aviation aircraft. Pictures of aircraft. Submit yours! An indexed and cross-referenced database of the Federal Aviation Regulations. Indexed and searchable database of Aviation Links. Practice Private Pilot andInstrument exams.
AIRCRAFT PERFORMANCE DATABASE Aircraft Performance Database. Welcome to the Aircraft Performance Database. You will find performance information on almost any general aviation aircraft that has been in production in the past 40 years. You can find the plane you are looking for two ways. You can search the database using the form below or you can browse the Index ofAircraft
AIRCRAFT PERFORMANCE STATS M-7 and MX-7 Series. M-7-235. MX-7-160. MX-7-180A. Manufacturer. Aeronca Aerostar American Champion American General Beechcraft Bellanca Cessna Commander EADS Socata Lake Luscombe Aircraft Maule Mooney Piper PZL. Aircraft Model. Search for aircraft meeting your performance criteria! FEDERAL AVIATION REGULATION SEC. 23.149 Sec. 23.149 — Minimum control speed. (a) V MC. is the calibrated airspeed at which, when the critical engine is suddenly made inoperative, it is possible to maintain control of the airplane with that engine still inoperative, and thereafter maintain straight flight at the same speed with an angle of bank of not more than 5 degrees.. The method used to simulate critical engine failure must AIRCRAFT PERFORMANCE STATS Aircraft performance stats and information for several MooneyAircraft.
FEDERAL AVIATION REGULATION SEC. 25.807 Sec. 25.807 — Emergency exits. (a) Type. For the purpose of this part, the types of exits are defined as follows: (1) Type I. This type is a floor-level exit with a rectangular opening of not less than 24 inches wide by 48 inches high, with corner radii not greater than eight inches. (2) Type II. This type is a rectangular opening of notless
FEDERAL AVIATION REGULATION SEC. 23.951 The Federal Aviation Regulation Sec. 23.951 - General. Sec. 23.951 — General. (a) Each fuel system must be constructed and arranged to ensure fuel flow at a rate and pressure established for proper engine and auxiliary power unit functioning under each likely operating condition, including any maneuver for which certification is requested and during which the engine or auxiliary power unit FEDERAL AVIATION REGULATION SEC. 23.1435 Sec. 23.1435 — Hydraulic systems. (a) Design. Each hydraulic system must be designed as follows: (1) Each hydraulic system and its elements must withstand, without yielding, the structural loads expected in addition to hydraulic loads. (2) A means to indicate the pressure in each hydraulic system which supplies two or more primaryfunctions
FEDERAL AVIATION REGULATION SEC. 23.573 Sec. 23.573 — Damage tolerance and fatigue evaluation of structure. (a) Composite airframe structure. Composite airframe structure must be evaluated under this paragraph instead of §§23.571 and 23.572. The applicant must evaluate the composite airframe structure, the failure of which would result in catastrophic loss of the airplane, in FEDERAL AVIATION REGULATION SEC. 23.975 Sec. 23.975 — Fuel tank vents and carburetor vapor vents. (a) Each fuel tank must be vented from the top part of the expansion space. In addition—. (1) Each vent outlet must be located and constructed in a manner that minimizes the possibility of its being obstructed by ice or other foreign matter; (2) Each vent must be constructed toRISINGUP.COM
RisingUp.com Homepage. Performance information on over 500 general aviation aircraft. Pictures of aircraft. Submit yours! An indexed and cross-referenced database of the Federal Aviation Regulations. Indexed and searchable database of Aviation Links. Practice Private Pilot andInstrument exams.
AIRCRAFT PERFORMANCE DATABASE Aircraft Performance Database. Welcome to the Aircraft Performance Database. You will find performance information on almost any general aviation aircraft that has been in production in the past 40 years. You can find the plane you are looking for two ways. You can search the database using the form below or you can browse the Index ofAircraft
AIRCRAFT PERFORMANCE STATS M-7 and MX-7 Series. M-7-235. MX-7-160. MX-7-180A. Manufacturer. Aeronca Aerostar American Champion American General Beechcraft Bellanca Cessna Commander EADS Socata Lake Luscombe Aircraft Maule Mooney Piper PZL. Aircraft Model. Search for aircraft meeting your performance criteria! FEDERAL AVIATION REGULATION SEC. 23.149 Sec. 23.149 — Minimum control speed. (a) V MC. is the calibrated airspeed at which, when the critical engine is suddenly made inoperative, it is possible to maintain control of the airplane with that engine still inoperative, and thereafter maintain straight flight at the same speed with an angle of bank of not more than 5 degrees.. The method used to simulate critical engine failure must AIRCRAFT PERFORMANCE STATS Aircraft performance stats and information for several MooneyAircraft.
FEDERAL AVIATION REGULATION SEC. 25.807 Sec. 25.807 — Emergency exits. (a) Type. For the purpose of this part, the types of exits are defined as follows: (1) Type I. This type is a floor-level exit with a rectangular opening of not less than 24 inches wide by 48 inches high, with corner radii not greater than eight inches. (2) Type II. This type is a rectangular opening of notless
FEDERAL AVIATION REGULATION SEC. 23.951 The Federal Aviation Regulation Sec. 23.951 - General. Sec. 23.951 — General. (a) Each fuel system must be constructed and arranged to ensure fuel flow at a rate and pressure established for proper engine and auxiliary power unit functioning under each likely operating condition, including any maneuver for which certification is requested and during which the engine or auxiliary power unit FEDERAL AVIATION REGULATION SEC. 23.1435 Sec. 23.1435 — Hydraulic systems. (a) Design. Each hydraulic system must be designed as follows: (1) Each hydraulic system and its elements must withstand, without yielding, the structural loads expected in addition to hydraulic loads. (2) A means to indicate the pressure in each hydraulic system which supplies two or more primaryfunctions
FEDERAL AVIATION REGULATION SEC. 23.573 Sec. 23.573 — Damage tolerance and fatigue evaluation of structure. (a) Composite airframe structure. Composite airframe structure must be evaluated under this paragraph instead of §§23.571 and 23.572. The applicant must evaluate the composite airframe structure, the failure of which would result in catastrophic loss of the airplane, in FEDERAL AVIATION REGULATION SEC. 23.975 Sec. 23.975 — Fuel tank vents and carburetor vapor vents. (a) Each fuel tank must be vented from the top part of the expansion space. In addition—. (1) Each vent outlet must be located and constructed in a manner that minimizes the possibility of its being obstructed by ice or other foreign matter; (2) Each vent must be constructed toPRACTICE TESTS
Reporting of Aircraft Accidents, Incidents, and Overdue Aircraft. AC 61-23 -- Pilot's Handbook of Aeronautical Knowledge. Forces Acting on the Airplane in Flight. Turning Tendency (Torque Effect) Airplane Stability. Loads and Load Factors. Flight control Systems. Engine Operation. Propeller. FEDERAL AVIATION REGULATIONS INDEX OF ALL FEDERAL AVIATION Part 1 - DEFINITIONS AND ABBREVIATIONS. Part 3 - GENERAL REQUIREMENTS. Subchapter B – Procedural Rules. Part 11 - GENERAL RULEMAKING PROCEDURES. Part 13 - INVESTIGATIVE AND ENFORCEMENT PROCEDURES. Part 14 - RULES IMPLEMENTING THE EQUAL ACCESS TO JUSTICE ACT OF 1980. Part 15 - ADMINISTRATIVE CLAIMS UNDER FEDERAL TORT CLAIMS ACT. FEDERAL AVIATION REGULATIONS Part 65 - CERTIFICATION: AIRMEN OTHER THAN FLIGHT CREWMEMBERS. Appendices. Appendix C to Part 63 - Flight Engineer Training Course Requirements; Special Federal Aviation Regulation 103 - Process for Requesting Waiver of Mandatory Separation Age for a Federal Aviation Administration Air Traffic Control Specialist In Flight Service Stations, Enroute or Terminal Facilities, and the David J AIRCRAFT PERFORMANCE STATS PA-31-300 Navajo. PA-31-310 Turbo Navajo. PA-31-310 Turbo Navajo B,C (prior to 1980 has less fuel) PA-31-325Navajo C/R. PA-31-350 Chieftain. PA-31P-350 Mojave. PA31 P Press Navajo (after 1977) FEDERAL AVIATION REGULATIONS SEARCH RESULTS FARs Search Results. Sec. 91.1015 - Management specifications. Sec. 121.187 - Airplanes: Reciprocating engine-powered: Landing limitations: Alternate airport. FEDERAL AVIATION REGULATIONS SEARCH RESULTS FARs Search Results. Sec. 65.104 - Repairman certificate—experimental aircraft builder—Eligibility, privileges and limitations. Sec. 141.61 - Applicability. FEDERAL AVIATION REGULATIONS Part 93 - SPECIAL AIR TRAFFIC RULES. Appendices. Appendix G to Part 91 - Operations in Reduced Vertical Separation Minimum (RVSM) Airspace; Special Federal Aviation Regulation 105 - Operating Limitations for Unscheduled Operations at Chicago's O'Hare International Airport FEDERAL AVIATION REGULATION SEC. 23.561 The Federal Aviation Regulation Sec. 23.561 - General. Sec. 23.561 — General. (a) The airplane, although it may be damaged in emergency landing conditions, must be designed as prescribed in this section to protect each occupant under those conditions. FEDERAL AVIATION REGULATION SEC. 23.993 Sec. 23.993 — Fuel system lines and fittings. (a) Each fuel line must be installed and supported to prevent excessive vibration and to withstand loads due to fuel pressure and accelerated flight conditions. (b) Each fuel line connected to components of the airplane between which relative motion could exist must have provisions forflexibility.
FEDERAL AVIATION REGULATION SEC. 23.1353 Sec. 23.1353 — Storage battery design and installation. (a) Each storage battery must be designed and installed as prescribed in this section. (b) Safe cell temperatures and pressures must be maintained during any probable charging and discharging condition. No uncontrolled increase in cell temperature may result when the batteryis recharged
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