AD 67-23-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Interceptor Aircraft Corporation | 200 | Airworthiness Directives; Aero Commander (Meyers) Model 200 Series Airplanes |
| aircraft | Interceptor Aircraft Corporation | 200A | Airworthiness Directives; Aero Commander (Meyers) Model 200 Series Airplanes |
| aircraft | Interceptor Aircraft Corporation | 200B | Airworthiness Directives; Aero Commander (Meyers) Model 200 Series Airplanes |
| aircraft | Interceptor Aircraft Corporation | 200C | Airworthiness Directives; Aero Commander (Meyers) Model 200 Series Airplanes |
| aircraft | Interceptor Aircraft Corporation | 200D | Airworthiness Directives; Aero Commander (Meyers) Model 200 Series Airplanes |
Unsafe Condition
Improper rigging of the main landing gear emergency extension and down lock mechanism.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect and adjust each main landing gear in accordance with Aero Commander, Albany Division, Service Bulletin 2004, dated February 10, 1967, or later FAA approved revision, or in a manner approved by the Chief, Engineering and Manufacturing Branch, FAA Southern Region.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 25 hours' time in service after effective date of this AD unless already accomplished
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Interceptor Aircraft Corporation Model 200, 200A, 200B, 200C, 200D, serial numbers 255, 256, 260, 262, 263, 268, 272, 273, 275, 276, 277, 278, 279, 281, 282, 286, 287, 288, 289, 290, 291, 296, 306, 308, 309, 328, 329, 331, 338, and 353.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Main Landing Gear
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_67-23-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-23-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Aero Commander (Meyers) Model 200 Series Airplanes Subject: Main Landing Gear Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/15/1967 Make: Interceptor Aircraft Corporation Model: 200 | 200A | 200B | 200C | 200D Product Type: Aircraft Product Subtype: Small 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: 67-23-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-457 AD NUMBER: 67-23-01 SUBJECT HEADING: Airworthiness Directives; Aero Commander (Meyers) Model 200 Series Airplanes ACTION: SUMMARY: DATES: Effective August 15, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-23-01 AERO COMMANDER: Amdt. 39-457, Part 39, Federal Register August 5, 1967. Applies to Aero Commander (Meyers) Model 200 Series Airplanes, Serial Numbers 255, 256, 260, 262, 263, 268, 272, 273, 275, 276, 277, 278, 279, 281, 282, 286, 287, 288, 289, 290, 291, 296, 306, 308, 309, 328, 329, 331, 338, and 353. Compliance required within the next 25 hours' time in service after effective date of this AD unless already accomplished. To detect improper rigging of the main landing gear emergency extension and down lock mechanism, accomplish the following: Inspect and adjust each main landing gear in accordance with Aero Commander, Albany Division, Service Bulletin 2004, dated February 10, 1967, or later FAA approved revision, or in a manner approved by the Chief, Engineering and Manufacturing Branch, FAA Southern Region. This amendment effective August 15, 1967. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_67-23-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-23-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Aero Commander (Meyers) Model 200 Series Airplanes Subject: Main Landing Gear Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/15/1967 Make: Interceptor Aircraft Corporation Model: 200 | 200A | 200B | 200C | 200D Product Type: Aircraft Product Subtype: Small 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: 67-23-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-457 AD NUMBER: 67-23-01 SUBJECT HEADING: Airworthiness Directives; Aero Commander (Meyers) Model 200 Series Airplanes ACTION: SUMMARY: DATES: Effective August 15, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-23-01 AERO COMMANDER: Amdt. 39-457, Part 39, Federal Register August 5, 1967. Applies to Aero Commander (Meyers) Model 200 Series Airplanes, Serial Numbers 255, 256, 260, 262, 263, 268, 272, 273, 275, 276, 277, 278, 279, 281, 282, 286, 287, 288, 289, 290, 291, 296, 306, 308, 309, 328, 329, 331, 338, and 353. Compliance required within the next 25 hours' time in service after effective date of this AD unless already accomplished. To detect improper rigging of the main landing gear emergency extension and down lock mechanism, accomplish the following: Inspect and adjust each main landing gear in accordance with Aero Commander, Albany Division, Service Bulletin 2004, dated February 10, 1967, or later FAA approved revision, or in a manner approved by the Chief, Engineering and Manufacturing Branch, FAA Southern Region. This amendment effective August 15, 1967. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.
Related Airworthiness Directives
2005-01-19
final ruleAirworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders
Unsafe Condition: The GTX 33/33D/330/330D Mode S transponders may detect the S1 (suppression) interrogating pulse below the minimum trigger level (MTL) and, in some circumstances, not reply. This could lead to inacc...
96-12-22
final ruleAirworthiness Directives; Cessna Aircraft Company Engine Oil Filter Adapter Assemblies Installed on Aircraft
Unsafe Condition: Loose or separated engine oil filter adapters could cause loss of engine oil, leading to engine stoppage while in flight and loss of control of the airplane.
66-28-01
final ruleAirworthiness Directives; Aero Commander (Meyers) Model 200 Series Airplanes
Unsafe Condition: Excessive elevator trim set during takeoff could lead to uncommanded elevator movement or control difficulty.
