AD 91-20-14 R1

final rule

Airworthiness Directives; Beech Models B300 and B300C Airplanes

AD Number
91-20-14 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
91-CE-76-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
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.

AI-generated summary from the source AD text. Verify against the official source before acting.

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.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

within 10 hours time-in-service after February 20, 1992

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Beech Models B300 (serial numbers FL-1 through FL-110) and B300C (serial numbers FM-1 through FM-8)

AI-generated summary from the source AD text. Verify against the official source before acting.

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
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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Superseded AD: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Superseded By: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

Show stored source text (verify against official source)
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:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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