The Boeing Company 767-300: certification basis

Basis entries as written on the TCDS

1. REG

   FAA TCDS – A1NM

   FAA Type Certification Data Sheet No.

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

2. REG

   Refer to FAA TCDS A1NM

   FAA Certification Basis

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

3. REG

   In accordance with Regulation (EC) 1702/2003

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

4. REG

   FAR Part 25 at Amendment 25-1 through 25-37.

   Includes 14 CFR 25 through 25-37 · current is 25-153, 115 revisions later

   Expands to 364 provision links · shown below

5. REG

   Part 25 of the Federal Aviation Regulations: Amendment 25-38 through 25-45, except portions of Amendment 25-38 (Section 25.979(d) and (e) and Section 25.1143(e)); Amendment 40 (Sections 25.901(b)(1)(i), 25.1091(e) and 25.1093(b)); Amendment 41 (Section 25.1438); Amendment 42 (Section 25.109), Amendment 46 (Sections 25.345; 25.351(a), 25.629, 25.697, 25.803, 25.901(d), 25.1103(a), (b)(2),(d), (e), (f), 25.1142, 25.1522, Amendment 49 (Section 25.733) Amendment 54 (Section 25.365(e)(1), (2))

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

6. ◆ SPECIAL

   Generic SC F-GEN-11, Non-rechargeable Lithium Batteries Installations, effective to design changes applied for after 10 November 2016. See the Notes of these special conditions for more information on which design changes must meet them. (CS 25.601, 25.863, 25.1353(c) refers)

7. ◆ SPECIAL

   D-GEN02 PTC Heat Release and Smoke Density (Note: to be applied to new seat installations after January 2011)

8. ◆ SPECIAL

   H-01 Enhanced Airworthiness Programme for Aeroplane Systems - ICA on EWIS

9. ◆ SPECIAL

   - Special Condition No. 25-ANM-18 on Lightning Protection, Protection from Unwanted Effects of Radio Frequency (RF) Energy and Propulsion Control System for Pratt and Whitney PW4000 series engines, General Electric CF6-80C2 FADEC engine, and Rolls Royce RB211-524H-36 engine installations.

   Applies to: Adopted FAA Special Conditions

10. ◆ SPECIAL

    - Special Condition No. 25-ANM-20 for installation of a longitudinal partition.

    Applies to: Adopted FAA Special Conditions

11. ◆ SPECIAL

    - Ditching Provisions 25.801 (Over- water operation can be approved when the aircraft has been equipped and installation has been approved according to FAR 25.801)

    Applies to: Compliance with the following optional requirements has been established

12. ◆ SPECIAL

    - Ice Protection Provisions 25.1419

    Applies to: Compliance with the following optional requirements has been established

13. EXEMPT

    Exemption from FAR 25: Exemption No. 4725 - Exemption from 25.785(h) - Allows one seat for a required flight attendant to be located near the overwing Type III exits.

    Applies to: Adopted FAA Exemptions

14. ELOS

    Equivalent Safety Findings exist with respect to the following regulations: FAR 25.1093(b)(1) Induction System Deicing and Anti-icing Protection

    Applies to: Adopted FAA Equivalent Safety Findings

15. ELOS

    FAR 25.1103(d) Induction System Ducts and Air Duct Systems

    Applies to: Adopted FAA Equivalent Safety Findings

16. ELOS

    Generic ESF: D-GEN7, Flammability Testing Hierarchy (JAR/CS 25.853(a) refers) G-GEN2, Engine and Auxiliary Power Unit (APU) Fire Switch Handle Design (CS 25.1555(d)(1) refers)

    Applies to: Adopted FAA Equivalent Safety Findings

17. ELOS

    FAR 25.1103(e) Induction System Ducts and Air Duct Systems RB211-524H Installation only.

    Applies to: Adopted FAA Equivalent Safety Findings

18. ELOS

    FAR 25.1181(a)(6) Designated Fire Zones; Regions Included

    Applies to: Adopted FAA Equivalent Safety Findings

19. ELOS

    FAR 25.1203 Fire Detector System for Compartment Surrounding the Turbine and Jetpipe (Zone 4A/4B) RB211-524H Installation only.

    Applies to: Adopted FAA Equivalent Safety Findings

20. ELOS

    FAR 25.1305(a)(4), (a)(6), Powerplant Instruments (c)(1) and (c)(3)

    Applies to: Adopted FAA Equivalent Safety Findings

21. ELOS

    FAR 25.1387(b) and (c) Position Light System Dihedral Angles

    Applies to: Adopted FAA Equivalent Safety Findings

22. ELOS

    FAR 25.1393 Minimum Intensities in Any Vertical Plan of Forward and Rear Position Lights

    Applies to: Adopted FAA Equivalent Safety Findings

23. ELOS

    FAR 25.1395 Maximum Intensities in Overlapping Beams of Forward and Rear Position Lights

    Applies to: Adopted FAA Equivalent Safety Findings

24. ELOS

    FAR 25.1415(d) Emergency Locator Transmitter (ELT)

    Applies to: Adopted FAA Equivalent Safety Findings

25. ELOS

    FAR 25.1549(b) Powerplant and Auxiliary Power Unit Instruments

    Applies to: Adopted FAA Equivalent Safety Findings

26. ELOS

    FAR 25.365(e)(2) Pressurized Cabin Loads

    Applies to: Adopted FAA Equivalent Safety Findings

27. ELOS

    FAR 25.803(c)(8) Emergency Evacuation Demonstration

    Applies to: Adopted FAA Equivalent Safety Findings

28. ELOS

    FAR 25.807(a)(7)(iv)and (c) Passenger Emergency Exits

    Applies to: Adopted FAA Equivalent Safety Findings

29. ELOS

    FAR 25.809 Emergency Exit Arrangement

    Applies to: Adopted FAA Equivalent Safety Findings

30. ELOS

    FAR 25.813(c) Emergency Exit Access

    Applies to: Adopted FAA Equivalent Safety Findings

31. ELOS

    FAR 25.811(f)(2) Exit Band Contrast

    Applies to: Adopted FAA Equivalent Safety Findings

32. ELOS

    FAR 25.853(c) Compartment Interiors

    Applies to: Adopted FAA Equivalent Safety Findings

33. ELOS

    FAR 25.791 Passenger Information Signs and Placards

    Applies to: Adopted FAA Equivalent Safety Findings

34. ELOS

    FAR 25.107(d), (e)(1)(iv), Minimum unstick speed (e)(4)

    Applies to: Adopted FAA Equivalent Safety Findings

35. ELOS

    FAR 25.853(d), Folding Waste Trolley Amendment 23-32

    Applies to: Adopted FAA Equivalent Safety Findings

36. ELOS

    FAR 25 (Several) Use of 1-g stall speed (non-structural Sections)

    Applies to: Adopted FAA Equivalent Safety Findings

37. OTHER

    Noise: ICAO Annex 16, Volume I, chapter 3 Note: for aircraft powered by PW4000 Ph3 NRI series engines, the noise requirements are those of ICAO Annex 16, Volume I, chapter 4.

38. OTHER

    Fuel Venting & Emissions: ICAO Annex 16, Volume II

39. OTHER

    Special Federal Aviation Regulation 27.

40. OTHER

    For all models, compliance with point 26.300(a) of Part 26 is demonstrated by complying with points

41. OTHER

    - 26.301 Compliance Plan for (R)TC holders

42. OTHER

    - 26.302 Fatigue and damage tolerance evaluation

43. OTHER

    - 26.303 Limit of Validity

44. OTHER

    - 26.304 Corrosion prevention and control programme

45. OTHER

    - 26.305 Validity of the continuing structural integrity programme

46. OTHER

    - 26.306 Fatigue critical baseline structure

47. OTHER

    - 26.307 Damage tolerance data for existing changes to fatigue critical structure

48. OTHER

    - 26.308 Damage tolerance data for existing repairs to fatigue critical structure

49. OTHER

    - 26.309 Repair Evaluation Guidelines