AD 77-02-04

final rule

Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes

AD Number
77-02-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 100 Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes
aircraft Textron Aviation Inc. 58 Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes
aircraft Textron Aviation Inc. 58A Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes
aircraft Textron Aviation Inc. 60 Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes
aircraft Textron Aviation Inc. 65-80 Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes
aircraft Textron Aviation Inc. 70 Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes
aircraft Textron Aviation Inc. 95-B55 Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes
aircraft Textron Aviation Inc. 95-B55A Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes
aircraft Textron Aviation Inc. A100 Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes
aircraft Textron Aviation Inc. A56TC Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes
aircraft Textron Aviation Inc. A60 Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes
aircraft Textron Aviation Inc. B90 Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes
aircraft Textron Aviation Inc. C90 Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes
aircraft Textron Aviation Inc. E55 Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes
aircraft Textron Aviation Inc. E55A Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes
aircraft Textron Aviation Inc. E90 Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes

Unsafe Condition

Wing tip strobe lights such as Grimes P/N 30-0669-1 or Hoskins P/N 30-0187-21 may explode due to non-explosion proof design.

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

Required Actions

Within 100 hours' time in service after March 3, 1977, visually inspect wing tip strobe lights. Deactivate non-compliant strobe light systems using guards, blocked circuit breakers, or other approved methods. Reactivate only after installing approved explosion proof strobe lights per specified service instructions or approved data.

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

Compliance Time

within the next 100 hours' time in-service after the effective date of this AD

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

Affected Aircraft

Beech Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100, and A100 with specified serial ranges, equipped with non-excepted wing tip strobe lights.

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

Federal Register Abstract

Wing Tip Strobe Lights

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_77-02-04.html
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AD Number:
77-02-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E9...Show more
Subject:
Wing Tip Strobe Lights
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/03/1977
Make:
Textron Aviation Inc.
Model:
100 | 58 | 58A | 60 | 65-80 | 70 | 95-B55 | 95-B55A | A100 | A56TC | A60 | B90 | C90 | E55 | E55A | E90
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: 77-02-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2842

AD NUMBER:   77-02-04

SUBJECT HEADING:   Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 3, 1977.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
77-02-04 BEECH: Amendment 39-2813 as amended by Amendment 39-2842. Applies to the following Beech Models and Serial Numbers of airplanes if equipped with wing tip strobe lights, except those airplanes having Grimes Manufacturing Company (Grimes) P/Ns 30-1467-1, 30-1467-3, 30-1467-5, 30-0467-5, 30-0531-1 or 30-0692-1, Symbolic Displays P/Ns 701148-7-2, 30-0002, 30-0005, 30-0005A, 30-0005-1, 701303, 30-0218-1, 30-0218-2, 30-0020, or 30-0028, and Whelen Engineering Company P/Ns A429, A429PR, A429PG, A430, A450, A460, A460A, or A500 wing tip strobe lights installed.

MODELS	SERIAL NUMBERS
E55 and E55A	TE-768 thru TE-903
A56TC	TG-84 thru TG-94
58 and 58A	TH-1 thru TH-302
60 and 60A	P-3 thru P-222
65-B80	LD-270 thru LD-480
70	LB-1 thru LB-35
B90 and C90	LJ-318 thru LJ-502
E90	LW-1
95-B55 and 95-B55A	TC-1299 thru TC-1525
100 and A100	B-1 thru B-157

Compliance: Required as indicated, unless already accomplished.

To preclude wing tip explosion, within the next 100 hours' time in service after the effective date of this AD, accomplish the following:

1. Visually inspect the wing tip strobe lights to determine whether Grimes P/N 30-0669-1 or Hoskins P/N 30-0187-21 strobe lights or any other strobe lights other than those excepted above are installed.

2. On those airplanes having non-explosion proof strobe lights such as Grimes Manufacturing Co. P/N 30-0669-1, Hoskins P/N 30-0187-21 or strobe lights other than those excepted by this AD, deactivate the strobe light system by installing a guard over the switch, by pulling and blocking the circuit breaker so that it cannot be inadvertently reset, or by any other suitable means.

3. Systems having Grimes Manufacturing Co. P/N 30-0669-1 or Hoskins P/N 30-0187-21 strobe lights, may be reactivated upon the installation of either Grimes Manufacturing Company P/N 30-1467-1 explosion proof strobe lights in accordance with Beechcraft Service Instructions 0800-362 or later approved revisions, or upon the installation of any explosion proof strobe lights excepted by this AD.

4. Do not reactivate strobe light installations, other than those modified per Paragraph 3, until data showing that the strobe lights are explosion proof have been submitted to and approved by the Chief, Engineering and Manufacturing Branch or Division of the FAA Region issuing the original strobe light approval.

5. Any equivalent method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

Amendment 39-2813 became effective February 24, 1977.

This amendment 39-2842 becomes effective March 3, 1977.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_77-02-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
77-02-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E9...Show more
Subject:
Wing Tip Strobe Lights
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/03/1977
Make:
Textron Aviation Inc.
Model:
100 | 58 | 58A | 60 | 65-80 | 70 | 95-B55 | 95-B55A | A100 | A56TC | A60 | B90 | C90 | E55 | E55A | E90
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: 77-02-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2842

AD NUMBER:   77-02-04

SUBJECT HEADING:   Airworthiness Directives; BEECH Models E55, E55A, A56TC, 58, 58A, 60, 60A, 65-B80, 70, B90, C90, E90, 95-B55, 95-B55A, 100 and A100 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 3, 1977.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
77-02-04 BEECH: Amendment 39-2813 as amended by Amendment 39-2842. Applies to the following Beech Models and Serial Numbers of airplanes if equipped with wing tip strobe lights, except those airplanes having Grimes Manufacturing Company (Grimes) P/Ns 30-1467-1, 30-1467-3, 30-1467-5, 30-0467-5, 30-0531-1 or 30-0692-1, Symbolic Displays P/Ns 701148-7-2, 30-0002, 30-0005, 30-0005A, 30-0005-1, 701303, 30-0218-1, 30-0218-2, 30-0020, or 30-0028, and Whelen Engineering Company P/Ns A429, A429PR, A429PG, A430, A450, A460, A460A, or A500 wing tip strobe lights installed.

MODELS	SERIAL NUMBERS
E55 and E55A	TE-768 thru TE-903
A56TC	TG-84 thru TG-94
58 and 58A	TH-1 thru TH-302
60 and 60A	P-3 thru P-222
65-B80	LD-270 thru LD-480
70	LB-1 thru LB-35
B90 and C90	LJ-318 thru LJ-502
E90	LW-1
95-B55 and 95-B55A	TC-1299 thru TC-1525
100 and A100	B-1 thru B-157

Compliance: Required as indicated, unless already accomplished.

To preclude wing tip explosion, within the next 100 hours' time in service after the effective date of this AD, accomplish the following:

1. Visually inspect the wing tip strobe lights to determine whether Grimes P/N 30-0669-1 or Hoskins P/N 30-0187-21 strobe lights or any other strobe lights other than those excepted above are installed.

2. On those airplanes having non-explosion proof strobe lights such as Grimes Manufacturing Co. P/N 30-0669-1, Hoskins P/N 30-0187-21 or strobe lights other than those excepted by this AD, deactivate the strobe light system by installing a guard over the switch, by pulling and blocking the circuit breaker so that it cannot be inadvertently reset, or by any other suitable means.

3. Systems having Grimes Manufacturing Co. P/N 30-0669-1 or Hoskins P/N 30-0187-21 strobe lights, may be reactivated upon the installation of either Grimes Manufacturing Company P/N 30-1467-1 explosion proof strobe lights in accordance with Beechcraft Service Instructions 0800-362 or later approved revisions, or upon the installation of any explosion proof strobe lights excepted by this AD.

4. Do not reactivate strobe light installations, other than those modified per Paragraph 3, until data showing that the strobe lights are explosion proof have been submitted to and approved by the Chief, Engineering and Manufacturing Branch or Division of the FAA Region issuing the original strobe light approval.

5. Any equivalent method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

Amendment 39-2813 became effective February 24, 1977.

This amendment 39-2842 becomes effective March 3, 1977.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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