AD 71-07-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company | 1049-54 | LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes |
| aircraft | Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company | 1049B-55 (Navy R7V-1) | LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes |
| aircraft | Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company | 1049C-55 | LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes |
| aircraft | Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company | 1049D-55 | LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes |
| aircraft | Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company | 1049E-55 | LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes |
| aircraft | Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company | 1049F-55 (USAF C-121C) | LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes |
| aircraft | Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company | 1049G-82 | LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes |
| aircraft | Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company | 1049H-82 | LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes |
| aircraft | Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company | 149-46 | LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes |
| aircraft | Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company | 1649A-98 | LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes |
| aircraft | Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company | 49-46 | LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes |
| aircraft | Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company | 649-79 | LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes |
| aircraft | Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company | 649A-79 | LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes |
| aircraft | Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company | 749-79 | LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes |
| aircraft | Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company | 749A-79 | LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes |
Unsafe Condition
Failure to provide an acceptable obstacle clearance profile when computing the takeoff flight path.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise airplane flight manuals by adding specified notes to indicated pages and figures. Add correction notes subtracting 100 feet and 3000 feet as required. Reference this AD in the flight manual upon completion.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
prior to the first flight after May 3, 1971 unless already accomplished
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Lockheed Models 49, 149, 649, 749, 1049, and 1649 series airplanes certificated in all categories.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Obstacle Clearance Profile
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_71-07-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 71-07-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes Subject: Obstacle Clearance Profile Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/03/1971 Make: Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company Model: 1049-54 | 1049B-55 (Navy R7V-1) | 1049C-55 | 1049D-55 | 1049E-55 | 1049F-55 (USAF C-121C) | 1049G-82...Show more Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 71-07-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-1181 AD NUMBER: 71-07-02 SUBJECT HEADING: LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes ACTION: SUMMARY: DATES: Effective April 3, 1971. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 71-07-02 LOCKHEED AIRCRAFT CORPORATION: Amdt. 39-1181. Applies to Lockheed Models 49, 149, 649, 749, 1049, and 1649 series airplanes certificated in all categories. Compliance required prior to the first flight after May 3, 1971 unless already accomplished. To provide for an acceptable obstacle clearance profile when computing the takeoff flight path, accomplish the following: (a) Revise the airplane flight manuals by adding to the airplane flight manuals listed in this subparagraph the following note to the lower right hand portion of the specified page and adjacent to that portion showing the ground time. "NOTE: To obtain correct ground time, multiply ground time by 1.42." Lockheed Model Lockheed Report No. Page Identification 49-46 5817 Section II, Page 17, Figure 14 Appendix I, Part 2, Page 78, Figure 11 149-46 5817 Appendix V, Page 21, Figure 13 49-46 Appendix VI, Page 6, Figure 6 Appendix VI, Page 14, Figure 14 649-79 6028 Section II, Page 2-21, Figure 20 649A-79 Appendix 1, Part 1, Page I-24, Figure 17 749-79 Appendix 1, Part 2, Page I-50, Figure 45 749A-79 Appendix III, Page III-12, Figure 11 Appendix V, Page V-12, Figure 11 749-79 6028 Appendix III, Supplement A, Page IIIA-12, Figure 11 749A-79 1049-54 7787 Appendix II, Page II-17, Figure II-14 1049C-55 9154 Supplement A, Section III, Part 2, Page A-32.1, Figure A-25 1049E-55 Supplement A, Section III, Part 3, Page A-54.1, Figure A-47 Supplement A, Section III, Part 4, Page A-77, Figure A- 70 1049C 9153 Supplement A, Section III, Part 2, Page A-35, Figure A- 29, Sheet 2 1049E Supplement A, Section III, Part 3, Page A-57, Figure A- 51, Sheet 2 Supplement B, Section III, Part 2, Page B-37, Figure B- 29, Sheet 2 Supplement B, Section III, Part 3, Page B-59, Figure B- 51, Sheet 2 1049C 9153 Supplement B, Section III, Part 4, Page B-83, Figure B- 74, Sheet 2 1049E Supplement C, Section III, Part 3, Page C-35, Figure C- 29, Sheet 2 Supplement C, Section III, Part 4, Page C-56A, Figure C-52, Sheet 2 Supplement E, Section III, Part 2, Page E-31, Figure E- 24, Sheet 2 Supplement E, Section III, Part 3, Page E-57, Figure E- 48, Sheet 2 1049G-82 10051 Section IV, Part II, Page 4-38, Figure 4-34 Section IV, Part II, Page A4-38, Figure 4-34 Section IV, Part III, Page 4-59, Figure 4-54 Section IV, Part III, Page A4-59, Figure 4-54 DA-1 Supplement, Part 2, Page 33, Figure 29 DA-1 Supplement, Part 3, Page 54, Figure 50 1049G-82 10052 Section IV, Part II, Page 4-39, Figure 4-34 Section IV, Part II, Page A4-39, Figure 4-34 Section IV, Part II, Page B4-39, Figure 4-34 Section IV, Part II, Page C4-39, Figure 4-34 Section IV, Part III, Page 4-61, Figure 4-55 Section IV, Part III, Page A4-61, Figure 4-55 DA-1 Supplement, Section III, Part 2, Page 33, Figure 29 DA-1 Supplement, Section III, Part 3, Page 54, Figure 50 DA-3 Supplement, Section III, Part 2, Page 31, Figure 27 DA-3 Supplement, Section III, Part 3, Page 52, Figure 48 1049D 11020 Section IV, Part 2, Page A4-39, Figure 4-35 1049H Section IV, Part 2, Page B4-39, Figure 4-35 Section IV, Part 2, Page C4-39, Figure 4-35 Section IV, Part 2, Page D4-39, Figure 4-35 Section IV, Part 2, Page E4-39, Figure 4-35 Section IV, Part 2, Page F4-39, Figure 4-35 Section IV, Part 3, Page A4-61, Figure 4-56 Section IV, Part 3, Page B4-61, Figure 4-56 Section IV, Part 3, Page C4-61, Figure 4-56 DA-1 Supplement, Section III, Part 2, Page A33, Figure 29 DA-1 Supplement, Section III, Part 3, Page A54, Figure 50 DA-1 Supplement, Section III, Part 2, Page 33, Figure 29 1049D 11020 DA-1 Supplement, Section III, Part 3, Page 54, Figure 50 1049H DA-3 Supplement, Section III, Part 2, Page 31, Figure 27 DA-3 Supplement, Section III, Part 2, Page A31, Figure 27 DA-3 Supplement, Section III, Part 2, Page B31, Figure 27 DA-3 Supplement, Section III, Part 3, Page 52, Figure 48 DA-3 Supplement, Section III, Part 3, Page A52, Figure 48 DA-3 Supplement, Section III, Part 3, Page B52, Figure 48 1649A-98 11560 Section IV, Part 2, Page 4-31, Figure 4-23, Sheet 1 Section IV, Part 2, Page B4-31, Figure 4-23, Sheet 1 Section IV, Part 3, Page 4-52, Figure 4-43 Appendix II, Page II-29, Figure II-26 (b) For the airplane flight manuals listed in this subparagraph there is a note in the top central portion of the page stating: "These lines and this grid are used only in the determination of airplane height and distance at end of 2 minute period." Add to this note the following: CORRECTION: At the end of 2 minute period, correct the airplane height by subtracting 100 feet and the airplane distance by subtracting 3000 feet. Lockheed Model Lockheed Report No. Page Identification 1049C 9153 Section III, Supplement D, Part 2, Page D-39, Figure D-34, Sheet 2 1049E Section III, Supplement D, Part 3, Page D-61, Figure D-55, Sheet 2 (c) Reference this Airworthiness Directive in the airplane flight manual at the time of accomplishment. This amendment becomes effective April 3, 1971. FOOTER:
Document Text
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AD Final Rules - DRS_71-07-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 71-07-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes Subject: Obstacle Clearance Profile Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/03/1971 Make: Lockheed Aircraft Corporation | Lockheed Martin Aeronautics Company Model: 1049-54 | 1049B-55 (Navy R7V-1) | 1049C-55 | 1049D-55 | 1049E-55 | 1049F-55 (USAF C-121C) | 1049G-82...Show more Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 71-07-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-1181 AD NUMBER: 71-07-02 SUBJECT HEADING: LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes ACTION: SUMMARY: DATES: Effective April 3, 1971. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 71-07-02 LOCKHEED AIRCRAFT CORPORATION: Amdt. 39-1181. Applies to Lockheed Models 49, 149, 649, 749, 1049, and 1649 series airplanes certificated in all categories. Compliance required prior to the first flight after May 3, 1971 unless already accomplished. To provide for an acceptable obstacle clearance profile when computing the takeoff flight path, accomplish the following: (a) Revise the airplane flight manuals by adding to the airplane flight manuals listed in this subparagraph the following note to the lower right hand portion of the specified page and adjacent to that portion showing the ground time. "NOTE: To obtain correct ground time, multiply ground time by 1.42." Lockheed Model Lockheed Report No. Page Identification 49-46 5817 Section II, Page 17, Figure 14 Appendix I, Part 2, Page 78, Figure 11 149-46 5817 Appendix V, Page 21, Figure 13 49-46 Appendix VI, Page 6, Figure 6 Appendix VI, Page 14, Figure 14 649-79 6028 Section II, Page 2-21, Figure 20 649A-79 Appendix 1, Part 1, Page I-24, Figure 17 749-79 Appendix 1, Part 2, Page I-50, Figure 45 749A-79 Appendix III, Page III-12, Figure 11 Appendix V, Page V-12, Figure 11 749-79 6028 Appendix III, Supplement A, Page IIIA-12, Figure 11 749A-79 1049-54 7787 Appendix II, Page II-17, Figure II-14 1049C-55 9154 Supplement A, Section III, Part 2, Page A-32.1, Figure A-25 1049E-55 Supplement A, Section III, Part 3, Page A-54.1, Figure A-47 Supplement A, Section III, Part 4, Page A-77, Figure A- 70 1049C 9153 Supplement A, Section III, Part 2, Page A-35, Figure A- 29, Sheet 2 1049E Supplement A, Section III, Part 3, Page A-57, Figure A- 51, Sheet 2 Supplement B, Section III, Part 2, Page B-37, Figure B- 29, Sheet 2 Supplement B, Section III, Part 3, Page B-59, Figure B- 51, Sheet 2 1049C 9153 Supplement B, Section III, Part 4, Page B-83, Figure B- 74, Sheet 2 1049E Supplement C, Section III, Part 3, Page C-35, Figure C- 29, Sheet 2 Supplement C, Section III, Part 4, Page C-56A, Figure C-52, Sheet 2 Supplement E, Section III, Part 2, Page E-31, Figure E- 24, Sheet 2 Supplement E, Section III, Part 3, Page E-57, Figure E- 48, Sheet 2 1049G-82 10051 Section IV, Part II, Page 4-38, Figure 4-34 Section IV, Part II, Page A4-38, Figure 4-34 Section IV, Part III, Page 4-59, Figure 4-54 Section IV, Part III, Page A4-59, Figure 4-54 DA-1 Supplement, Part 2, Page 33, Figure 29 DA-1 Supplement, Part 3, Page 54, Figure 50 1049G-82 10052 Section IV, Part II, Page 4-39, Figure 4-34 Section IV, Part II, Page A4-39, Figure 4-34 Section IV, Part II, Page B4-39, Figure 4-34 Section IV, Part II, Page C4-39, Figure 4-34 Section IV, Part III, Page 4-61, Figure 4-55 Section IV, Part III, Page A4-61, Figure 4-55 DA-1 Supplement, Section III, Part 2, Page 33, Figure 29 DA-1 Supplement, Section III, Part 3, Page 54, Figure 50 DA-3 Supplement, Section III, Part 2, Page 31, Figure 27 DA-3 Supplement, Section III, Part 3, Page 52, Figure 48 1049D 11020 Section IV, Part 2, Page A4-39, Figure 4-35 1049H Section IV, Part 2, Page B4-39, Figure 4-35 Section IV, Part 2, Page C4-39, Figure 4-35 Section IV, Part 2, Page D4-39, Figure 4-35 Section IV, Part 2, Page E4-39, Figure 4-35 Section IV, Part 2, Page F4-39, Figure 4-35 Section IV, Part 3, Page A4-61, Figure 4-56 Section IV, Part 3, Page B4-61, Figure 4-56 Section IV, Part 3, Page C4-61, Figure 4-56 DA-1 Supplement, Section III, Part 2, Page A33, Figure 29 DA-1 Supplement, Section III, Part 3, Page A54, Figure 50 DA-1 Supplement, Section III, Part 2, Page 33, Figure 29 1049D 11020 DA-1 Supplement, Section III, Part 3, Page 54, Figure 50 1049H DA-3 Supplement, Section III, Part 2, Page 31, Figure 27 DA-3 Supplement, Section III, Part 2, Page A31, Figure 27 DA-3 Supplement, Section III, Part 2, Page B31, Figure 27 DA-3 Supplement, Section III, Part 3, Page 52, Figure 48 DA-3 Supplement, Section III, Part 3, Page A52, Figure 48 DA-3 Supplement, Section III, Part 3, Page B52, Figure 48 1649A-98 11560 Section IV, Part 2, Page 4-31, Figure 4-23, Sheet 1 Section IV, Part 2, Page B4-31, Figure 4-23, Sheet 1 Section IV, Part 3, Page 4-52, Figure 4-43 Appendix II, Page II-29, Figure II-26 (b) For the airplane flight manuals listed in this subparagraph there is a note in the top central portion of the page stating: "These lines and this grid are used only in the determination of airplane height and distance at end of 2 minute period." Add to this note the following: CORRECTION: At the end of 2 minute period, correct the airplane height by subtracting 100 feet and the airplane distance by subtracting 3000 feet. Lockheed Model Lockheed Report No. Page Identification 1049C 9153 Section III, Supplement D, Part 2, Page D-39, Figure D-34, Sheet 2 1049E Section III, Supplement D, Part 3, Page D-61, Figure D-55, Sheet 2 (c) Reference this Airworthiness Directive in the airplane flight manual at the time of accomplishment. This amendment becomes effective April 3, 1971. FOOTER:
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