Saab AB SAAB 2000: certification basis
Basis entries as written on the TCDS
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REG
Original LFV TC A 1/94 was replaced by the EASA TC EASA.A.069.
State of Design Airworthiness Authority Type Certification Data Sheet No.
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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REG
See below
State of Design Airworthiness Authority Certification Basis
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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REG
JAR 25 (CS-25) Change 13, including JAR 25.1419 (Ice Protection) and JAR 25.801 (Ditching), and excluding JAR 25.562(c)(5) for front row seats (See Note 4 and 5).
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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REG
JAR AWO (CS-AWO) at Change 1 for automatic landing and operations in low visibility.
Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.
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◆ SPECIAL
CRI Topic
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◆ SPECIAL
B-07 Propeller position in VMC demonstrations
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◆ SPECIAL
B-09 Stalling speeds
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◆ SPECIAL
B-12 Stalls, Critical Engine Inoperative
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◆ SPECIAL
B-15 Steep Approach Operation
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◆ SPECIAL
C-02 Tuned gust
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◆ SPECIAL
C-06 Stalling speeds for structural design
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◆ SPECIAL
C-07 Improved seat safety standard
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◆ SPECIAL
C-08 Factors for engine torque
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◆ SPECIAL
C-09 Rapid decompression
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◆ SPECIAL
C-12 Rudder limiter – Interaction of systems and structure
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◆ SPECIAL
C-13 PECS Interaction of systems and structure
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◆ SPECIAL
D-01 Lightning protection – Indirect effects
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◆ SPECIAL
D-02 Landing Gear Warning
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◆ SPECIAL
D-04 Cargo and service doors
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◆ SPECIAL
D-08 PECS Control signal integrity
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◆ SPECIAL
D-10 PECS Emergency Pitch Trim System
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◆ SPECIAL
E-08 Propeller reversing system
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◆ SPECIAL
F-03 Operation without normal electrical power
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◆ SPECIAL
F-04 Miscellaneous electrical requirements
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◆ SPECIAL
F-05 Effect of external radiation upon aircraft systems
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◆ SPECIAL
F-09 Function and reliability testing
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◆ SPECIAL
F-11 Head-up Guidance System
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◆ SPECIAL
F-13 Non rechargeable Lithium Battery installations
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◆ SPECIAL
H-01 Enhanced Airworthiness Programme for Airplane Systems – ICA on EWIS
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EXEMPT
Item / CRI Topic
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EXEMPT
F-10 Application of national operational regulations regarding oxygen for TC
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OTHER
No deviations have been granted.
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ELOS
CRI Topic
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ELOS
B-08 Stall and Stall Warning speeds and manoeuvre capability
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ELOS
D-05 Fire protection of engine and APU mounts
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ELOS
D-07 Emergency lights “not armed” warning
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ELOS
D-12 Aisle width (Flight Inspection configuration; S/N 051 and 054) Improved flammability standards for thermal and acoustic insulation
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ELOS
D-13 materials used in Large aeroplanes
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ELOS
J-02 APU Instruments
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OTHER
Topic
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OTHER
B-01 Controllability and manoeuvrability, stick forces
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OTHER
B-02 Stick pusher
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OTHER
B-03 Flight in Icing Conditions
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OTHER
B-04 Reduced and de-rated take-off thrust procedure
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OTHER
B-05 Temperature extrapolation limitations in take-off and climb
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OTHER
B-06 Minimum Control Speed
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OTHER
B-13 Take-off run on wet and contaminated runways
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OTHER
B-16 Take-off and Landing in Tailwind greater than 10 knots
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OTHER
B-17 Performance Credit for alternative forward centre of gravity limits Electrical bonding and protection against lightning and static
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OTHER
C-05 electricity (direct effects)
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OTHER
C-10 Fuel tank crashworthiness
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OTHER
D-03 Aeroplane wheel and wheel-brake assemblies
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OTHER
D-09 PECS Applicability of ACJ 25.1329
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OTHER
D-11 Automatic Flap retraction system (Mod. No. 5786)
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OTHER
E-03 Engine/Propeller control integration
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OTHER
E-04 Aircraft propulsion system equipped with electronic controls
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OTHER
F-02 Electronic instrument displays
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OTHER
F-06 Alerting system
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OTHER
F-07 Software verification
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OTHER
F-08 System design and analysis
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OTHER
F-12 Head-up Guidance System, CAT III, One Engine Out Landing
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OTHER
J-01 APU rotor non-containment
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OTHER
Refer to TCDSN EASA.A.069