AD 91-20-14 R1
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | B300 | Airworthiness Directives; Beech Models B300 and B300C Airplanes |
| aircraft | Textron Aviation Inc. | B300C | Airworthiness Directives; Beech Models B300 and B300C Airplanes |
Unsafe Condition
The affected airplanes may not achieve required minimum takeoff and climb performance for each approved combination of takeoff configuration, weight, pressure altitude, and temperature.
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Required Actions
Incorporate takeoff and climb performance charts (B2 revision, part number 130-590031-1, dated September 1991) into the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual (AFM/POH). The charts may be installed by the owner/operator with a private pilot certificate under 14 CFR 43.7, and compliance must be recorded per 14 CFR 43.11. Special flight permits under 14 CFR 21.197/21.199 may be obtained to operate to a location where compliance can be achieved.
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Compliance Time
within 10 hours time-in-service after February 20, 1992
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Affected Aircraft
Beech Models B300 (serial numbers FL-1 through FL-110) and B300C (serial numbers FM-1 through FM-8)
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Federal Register Abstract
Performance Charts and Information
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_91-20-14_R.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 91-20-14 R1 Document Type: AD Final Rules Docket Number: 91-CE-76-AD Subject Heading: Airworthiness Directives; Beech Models B300 and B300C Airplanes Subject: Performance Charts and Information Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/12/1994 Make: Textron Aviation Inc. Model: B300 | B300C Product Type: Aircraft Product Subtype: Small/Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 91-20-14 R1 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 91-CE-76-AD AMENDMENT: 39-8992 AD NUMBER: 91-20-14 R1 SUBJECT HEADING: Airworthiness Directives; Beech Models B300 and B300C Airplanes ACTION: SUMMARY: DATES: Effective September 12, 1994. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 91-20-14 R1 BEECH AIRCRAFT CORPORATION: Amendment 39-8992; Docket No. 91-CE- 76-AD; Revises AD 91-20-14, Amendment 39-8168. Applicability: The following model and serial number airplanes, certificated in any category: Model Serial Numbers B300 FL-1 through FL-110 B300C FM-1 through FM-8 Compliance: Required within 10 hours time-in-service after February 20, 1992 (the effective date of AD 91-20-14), unless already accomplished. To ensure that the affected airplanes achieve required minimum takeoff and climb performance for each approved combination of takeoff configuration, weight, pressure altitude, and temperature, accomplish the following: (a) Incorporate the takeoff and climb performance charts, B2 revision, part number (P/N) 130-590031-1, dated September 1991, into the Model B300 and B300C Pilot's Operating Handbook and FAA Approved Airplane Flight Manual (AFM/POH). NOTE 1: The charts sent in the priority letter AD 91-20-14 package and B2 revision, P/N 130- 590031-1, dated September 1991, are the same. (b) Incorporating the climb and takeoff charts as required by this AD may be performed by the owner/operator holding at least a private pilot certificate as authorized by section 43.7 of the Federal Aviation Regulations (14 CFR 43.7), and must be entered into the aircraft records showing compliance with this AD in accordance with section 43.11 of the Federal Aviation Regulations (14 CFR 43.11). (c) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. (d) An alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be approved by the Manager, Wichita Aircraft Certification Office (ACO), FAA, 1801 Airport Road, Room 100, Wichita, Kansas 67209. The request should be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and send it to the Manager, Wichita ACO. NOTE 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Wichita ACO. (e) The takeoff and climb performance limitations required by this AD shall be done in accordance with the Beech Pilot's Operating Handbook and FAA Approved Airplane Flight Manual, B2 revision, part number 130-590031-1, dated September 1991. This incorporation by reference was previously approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51 as of February 20, 1992. Copies may be obtained from the Beech Aircraft Corporation, P.O. Box 85, Wichita, Kansas 67201-0085. Copies may be inspected at the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (f) This amendment (39-8992) revises AD 91-20-14, Amendment 39-8168. (g) This amendment becomes effective on September 12, 1994. FOOTER:
Document Text
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AD Final Rules - DRS_91-20-14_R.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 91-20-14 R1 Document Type: AD Final Rules Docket Number: 91-CE-76-AD Subject Heading: Airworthiness Directives; Beech Models B300 and B300C Airplanes Subject: Performance Charts and Information Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/12/1994 Make: Textron Aviation Inc. Model: B300 | B300C Product Type: Aircraft Product Subtype: Small/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: 91-20-14 R1 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 91-CE-76-AD AMENDMENT: 39-8992 AD NUMBER: 91-20-14 R1 SUBJECT HEADING: Airworthiness Directives; Beech Models B300 and B300C Airplanes ACTION: SUMMARY: DATES: Effective September 12, 1994. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 91-20-14 R1 BEECH AIRCRAFT CORPORATION: Amendment 39-8992; Docket No. 91-CE- 76-AD; Revises AD 91-20-14, Amendment 39-8168. Applicability: The following model and serial number airplanes, certificated in any category: Model Serial Numbers B300 FL-1 through FL-110 B300C FM-1 through FM-8 Compliance: Required within 10 hours time-in-service after February 20, 1992 (the effective date of AD 91-20-14), unless already accomplished. To ensure that the affected airplanes achieve required minimum takeoff and climb performance for each approved combination of takeoff configuration, weight, pressure altitude, and temperature, accomplish the following: (a) Incorporate the takeoff and climb performance charts, B2 revision, part number (P/N) 130-590031-1, dated September 1991, into the Model B300 and B300C Pilot's Operating Handbook and FAA Approved Airplane Flight Manual (AFM/POH). NOTE 1: The charts sent in the priority letter AD 91-20-14 package and B2 revision, P/N 130- 590031-1, dated September 1991, are the same. (b) Incorporating the climb and takeoff charts as required by this AD may be performed by the owner/operator holding at least a private pilot certificate as authorized by section 43.7 of the Federal Aviation Regulations (14 CFR 43.7), and must be entered into the aircraft records showing compliance with this AD in accordance with section 43.11 of the Federal Aviation Regulations (14 CFR 43.11). (c) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. (d) An alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be approved by the Manager, Wichita Aircraft Certification Office (ACO), FAA, 1801 Airport Road, Room 100, Wichita, Kansas 67209. The request should be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and send it to the Manager, Wichita ACO. NOTE 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Wichita ACO. (e) The takeoff and climb performance limitations required by this AD shall be done in accordance with the Beech Pilot's Operating Handbook and FAA Approved Airplane Flight Manual, B2 revision, part number 130-590031-1, dated September 1991. This incorporation by reference was previously approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51 as of February 20, 1992. Copies may be obtained from the Beech Aircraft Corporation, P.O. Box 85, Wichita, Kansas 67201-0085. Copies may be inspected at the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (f) This amendment (39-8992) revises AD 91-20-14, Amendment 39-8168. (g) This amendment becomes effective on September 12, 1994. FOOTER:
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Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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