AD 69-03-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 707-100 Long Body | BOEING Models 707, 720, and 727 Airplanes |
| aircraft | The Boeing Company | 707-100B Long Body | BOEING Models 707, 720, and 727 Airplanes |
| aircraft | The Boeing Company | 707-100B Short Body | BOEING Models 707, 720, and 727 Airplanes |
| aircraft | The Boeing Company | 707-200 | BOEING Models 707, 720, and 727 Airplanes |
| aircraft | The Boeing Company | 707-300 Series | BOEING Models 707, 720, and 727 Airplanes |
| aircraft | The Boeing Company | 707-300B Series | BOEING Models 707, 720, and 727 Airplanes |
| aircraft | The Boeing Company | 707-300C Series | BOEING Models 707, 720, and 727 Airplanes |
| aircraft | The Boeing Company | 707-400 Series | BOEING Models 707, 720, and 727 Airplanes |
| aircraft | The Boeing Company | 720 Series | BOEING Models 707, 720, and 727 Airplanes |
| aircraft | The Boeing Company | 720B Series | BOEING Models 707, 720, and 727 Airplanes |
Unsafe Condition
Failure of the rudder pedal adjustment crank assembly could result in loss of rudder control.
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Required Actions
Remove the existing rudder pedal adjustment crank assembly and replace with a modified or new crank assembly in accordance with specified Boeing Service Bulletins or equivalent design approved by FAA.
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Compliance Time
Within the next 2,500 hours time in service after 1 March 1969, or within the next 1,000 hours' time in service after 6 March 1970 for additional Model 707's and 720's listed in Revision 1 of Service Bulletin 2536.
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Affected Aircraft
Boeing Models 707, 720, and 727 airplanes listed in Boeing Service Bulletins 2536 (for 707 and 720) and 27-100 (for 727), including those in Revision 1 of SB 2536 dated 23 January 1970.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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