Saab AB SAAB 340B: certification basis

Basis entries as written on the TCDS

1. REG

   No.

   State of Design Airworthiness Authority Type Certification Data Sheet

   Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.

2. REG

   Original LFV TC A 1/84 was replaced by the EASA TC EASA.A.068.

   State of Design Airworthiness Authority Type Certification Data Sheet

   Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.

3. 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.

4. REG

   JAR 25 Change 7

   Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.

5. REG

   JAR 25 Change 8 for paragraph 25.305(d)

   Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.

6. REG

   JAR 25 Change 10 for paragraph 25.807(d)

   Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.

7. REG

   JAR 25 Change 12 for paragraphs 25.341; 25.812; 25.853

   Not linked to provisions yet: the line is not interpreted, or its document is not in the dataset.

8. ◆ SPECIAL

   Special conditions in accordance with LFV Issue Book

9. ◆ SPECIAL

   Item / CRI Topic Item B-2 Stall identification and recovery characteristics Item B-4 Performance in Icing Conditions Item B-5 All engines operating, Steep Approach Landing Item B-7 Gravel runway operation Item B-8 Take-off and landing in tailwind greater than 10 knots Item B-9 High altitude take-off Item C-3 Propeller blade impact NPA 25C-112 applies in lieu of JAR 25.571(e)(2) Item C-5 Composite structure Item C-6 Structural design loads for Wing Tip Extension Item D-7 Lightning Protection, Indirect effects Item E-5 Automatic Reserve Power Item F-1 Flight guidance system (basic system)

10. ◆ SPECIAL

    Item / CRI Topic Item F-2 CAT II requirements Item F-3 Effect of external radiation upon aircraft systems

11. ◆ SPECIAL

    CRI F-04 Rechargeable Lithium battery installations

12. ◆ SPECIAL

    CRI F-06 Non rechargeable Lithium battery installations

13. ◆ SPECIAL

    CRI H-01 Enhanced Airworthiness Programme for Airplane Systems – ICA on EWIS

14. EXEMPT

    No exemption have been granted.

15. OTHER

    No deviation have been granted.

16. ELOS

    Equivalent Safety Findings in accordance with LFV Issue Book

17. ELOS

    Item / CRI Topic Requirement Item A-2 Oil quantity indicator JAR 25.1551 Item A-3 Refuelling system, auto shut-off testing JAR 25.979(b)(1) Item A-5 Static system integrity JAR 25.1333(c) Item A-6 Stand-by compass system JAR 25.1333(b) Item A-7 AC system indication JAR 25.1351(b)(6) Item A-11 Exit handle illumination JAR 25.811(e)(3)

18. ELOS

    JAR 25.103(a)(b)(c);

19. ELOS

    25.107(b)(c); 25.119(b);

20. ELOS

    25.121(c)(d); 25.125(a); Stall and stall warning speeds and Item B-6 25.145(a)(b)(c)(d); 25.147; manoeuvre capability

21. ELOS

    25.149; 25.161; 25.175; 25.177;

22. ELOS

    25.201(a)(b); 25.207(c)(d);

23. ELOS

    25.233(a); 25.237(a) Improved flammability standards for CRI D-9 thermal and acoustic insulation JAR 25.853(a); 25.855(d) materials used in Large Airplanes

24. OTHER

    Refer to TCDSN EASA.A.068