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JAR 66 (Reg 2042/2003 Part 66)
JAR 145 (Reg 2042/2003 Part 145)
JAR 147 (Reg 2042/2003 Part 147)
JAR AWO (CS AWO)
JAR APU (CS APU)
The 36 JARs and equivalent in EASA system (if any)
2.3 Joint Aviation Requirements and equivalent in EASA system
A project supported by AIRBUS and the CAAC
Date of the module
JAR E (CS E)
JAR P (CS P)
JAR TSO (CS ETSO)
JAR OPS 1
JAR OPS 3
JAR MMEL/MEL
JAR FCL Part 1
JAR FCL Part 2
JAR FCL Part 3
The 36 JARs and equivalent in EASA system (if any)
2.3 Joint Aviation Requirements and equivalent in EASA system
A project supported by AIRBUS and the CAAC
Date of the module
JAR FCL Part 4
JAR-STD 1A
JAR-STD 2A
JAR-STD 3A
JAR-STD 4A
JAR-STD 1H
JAR-STD 2H
JAR-STD 3H
The 36 JARs and equivalent in EASA system (if any)
2.3 Joint Aviation Requirements and equivalent in EASA system
A project supported by AIRBUS and the CAAC
Date of the module
Related to Airworthiness
The JAR-21 ( Part 21 of Reg 1702/2003)
Certification Procedures for aircraft, Products and Related
Parts
First Issue in 1994
The 36 JARs and equivalent in EASA system (if any)
2.3 Joint Aviation Requirements and equivalent in EASA system
A project supported by AIRBUS and the CAAC
Date of the module
Related to Airworthiness
The JAR-22 (CS-22)
Certification standards for the sailplanes and powered
sailplanes
First Issue in 1980
Based on a German regulation LSFM
The 36 JARs and equivalent in EASA system (if any)
2.3 Joint Aviation Requirements and equivalent in EASA system
A project supported by AIRBUS and the CAAC
Date of the module
Related to Airworthiness
The JAR-23 (CS 23)
Airworthiness standards for the certification of aeroplanes in the
normal, utility, aerobatic (with 9 seats or less and MTOW of 12500
lbs or less)
Airworthiness standards for the certification of commuter category
aeroplane (with 19 seats or less and MTOW of 19000 lbs or less)
The 36 JARs and equivalent in EASA system (if any)
2.3 Joint Aviation Requirements and equivalent in EASA system
A project supported by AIRBUS and the CAAC
Date of the module
Related to Airworthiness
The JAR-23 (CS 23)
First issue in 1994
Mainly based on FAR-23
The 36 JARs and equivalent in EASA system (if any)
2.3 Joint Aviation Requirements and equivalent in EASA system
A project supported by AIRBUS and the CAAC
Date of the module
Related to Airworthiness
The JAR-VLA (CS VLA)
Very Light Aircraft
Airworthiness standards for the certification o aeroplanes with a
single engine, no more than 2 seats and a MTOW no more than
750 kg
Stalling in landing conf. no more than 45 kts
The 36 JARs and equivalent in EASA system (if any)
2.3 Joint Aviation Requirements and equivalent in EASA system
A project supported by AIRBUS and the CAAC
Date of the module
Related to Airworthiness
The JAR-VLA (CS VLA)
day-VFR only
First issue in 1990
Based on a “simplified” previous FAR-23
The 36 JARs and equivalent in EASA system (if any)
2.3 Joint Aviation Requirements and equivalent in EASA system
A project supported by AIRBUS and the CAAC
Date of the module
Related to Airworthiness
The JAR-25 (CS 25)
Airworthiness standards for the certification of large
aeroplane (multi engined turbine-powered aeroplanes
with a MTOW greater than 5700 kg)
First issue in 1974
Mainly based on the FAR-25
The 36 JARs and equivalent in EASA system (if any)
2.3 Joint Aviation Requirements and equivalent in EASA system
A project supported by AIRBUS and the CAAC
Date of the module
Related to Airworthiness
The JAR-27 (CS 27)
Airworthiness standards for the certification of “small rotorcraft”
with maximum weights of 6000 lbs or less
First issue in 1993
Mainly based on the FAR-27
The 36 JARs and equivalent in EASA system (if any)
2.3 Joint Aviation Requirements and equivalent in EASA system
A project supported by AIRBUS and the CAAC
Date of the module
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