AD 93-07-03

final rule

Airworthiness Directives; AEROSPATIALE Model ATR42-300, ATR72-100 and - 200 Series Airplanes

AD Number
93-07-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
92-NM-163-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft ATR - GIE Avions de Transport R gional ATR42-300 Airworthiness Directives; AEROSPATIALE Model ATR42-300, ATR72-100 and - 200 Series Airplanes
aircraft ATR - GIE Avions de Transport R gional ATR42-320 Airworthiness Directives; AEROSPATIALE Model ATR42-300, ATR72-100 and - 200 Series Airplanes
aircraft ATR - GIE Avions de Transport R gional ATR72-101 Airworthiness Directives; AEROSPATIALE Model ATR42-300, ATR72-100 and - 200 Series Airplanes
aircraft ATR - GIE Avions de Transport R gional ATR72-102 Airworthiness Directives; AEROSPATIALE Model ATR42-300, ATR72-100 and - 200 Series Airplanes
aircraft ATR - GIE Avions de Transport R gional ATR72-201 Airworthiness Directives; AEROSPATIALE Model ATR42-300, ATR72-100 and - 200 Series Airplanes
aircraft ATR - GIE Avions de Transport R gional ATR72-202 Airworthiness Directives; AEROSPATIALE Model ATR42-300, ATR72-100 and - 200 Series Airplanes
aircraft ATR - GIE Avions de Transport R gional ATR72-211 Airworthiness Directives; AEROSPATIALE Model ATR42-300, ATR72-100 and - 200 Series Airplanes
aircraft ATR - GIE Avions de Transport R gional ATR72-212 Airworthiness Directives; AEROSPATIALE Model ATR42-300, ATR72-100 and - 200 Series Airplanes
aircraft ATR - GIE Avions de Transport R gional ATR72-212A Airworthiness Directives; AEROSPATIALE Model ATR42-300, ATR72-100 and - 200 Series Airplanes

Unsafe Condition

Failure of the pressurization valves to close in the event of ditching and interruption of electrical power to certain electrical equipment used during approach and landing.

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

Required Actions

Remove and identify date codes of electrical switches (part numbers 9PD and 12HM) per applicable service bulletins. Replace switches with date codes A6, A7, A8, A9, AO, AN, AD, B1, B2, B3, B4, B5, B6, or B7 before further flight. Prohibit installation of switches with those date codes. Allow alternative compliance with FAA approval.

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

Compliance Time

Within 30 days after the effective date of this AD (May 10, 1993) for removal and identification. Replacement required before further flight if date codes are listed. Compliance with (b) is immediate as of the effective date.

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

Affected Aircraft

All Model ATR42-300 series airplanes, and all Model ATR72-100 and -200 series airplanes; certificated in any category.

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

Federal Register Abstract

Electrical Switches

Applicability Source Text

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AD Number:
93-07-03
Document Type:
AD Final Rules
Docket Number:
92-NM-163-AD
Subject Heading:
Airworthiness Directives; AEROSPATIALE Model ATR42-300, ATR72-100 and - 200 Series Airplanes
Subject:
Electrical Switches
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/10/1993
Make:
ATR - GIE Avions de Transport R gional
Model:
ATR42-300 | ATR42-320 | ATR72-101 | ATR72-102 | ATR72-201 | ATR72-202 | ATR72-211 | ATR72-212 | ATR72-212A
Product Type:
Aircraft
Product Subtype:
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: 93-07-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   92-NM-163-AD

AMENDMENT:   39-8535

AD NUMBER:   93-07-03

SUBJECT HEADING:   Airworthiness Directives; AEROSPATIALE Model ATR42-300, ATR72-100 and - 200 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective May 10, 1993.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
93-07-03 AEROSPATIALE: Amendment 39-8535. Docket 92-NM-163-AD.

Applicability: All Model ATR42-300 series airplanes, and all Model ATR72-100 and - 200 series airplanes; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent failure of the pressurization valves to close in the event of ditching, and to prevent interruption of electrical power to certain electrical equipment used during approach and landing, accomplish the following:

(a) Within 30 days after the effective date of this AD, remove the electrical switches, part numbers 9PD and 12HM, and identify the date codes in accordance with Aerospatiale Service Bulletin ATR42-31-0023, dated May 15, 1992 (for Model ATR42-300 and -320 series airplanes); or Aerospatiale Service Bulletin ATR72-31-1006, dated May 15, 1992 (for Model ATR72-100 and -200 series airplanes); as applicable.

(1) If the date code is identified as A6, A7, A8, A9, AO, AN, AD, B1, B2, B3, B4, B5, B6, or B7, prior to further flight, replace the currently-installed switch with a serviceable switch marked with a date code other than those listed above.

(2) If the date code is other than those listed in paragraph (a)(1) of this AD, reinstall the switch. No further action is necessary.

(b) As of the effective date of this AD, no person shall install an electrical switch, part numbers 9PD and 12HM, having a date code of A6, A7, A8, A9, AO, AN, AD, B1, B2, B3, B4, B5, B6, or B7, on any airplane.

(c) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Standardization Branch, ANM-113. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch, ANM-113.

NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113.

(d) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.

(e) The removal and identification shall be done in accordance with Aerospatiale Service Bulletin ATR42-31-0023, dated May 15, 1992 (for Model ATR42-300 and -320 series airplanes); or Aerospatiale Service Bulletin ATR72-31-1006, dated May 15, 1992 (for Model ATR72-100 and -200 series airplanes); as applicable. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from Aerospatiale, 316 Route de Bayonne, 31060 Toulouse, Cedex 03, France. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.

(f) This amendment becomes effective on May 10, 1993.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_93-07-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
93-07-03
Document Type:
AD Final Rules
Docket Number:
92-NM-163-AD
Subject Heading:
Airworthiness Directives; AEROSPATIALE Model ATR42-300, ATR72-100 and - 200 Series Airplanes
Subject:
Electrical Switches
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/10/1993
Make:
ATR - GIE Avions de Transport R gional
Model:
ATR42-300 | ATR42-320 | ATR72-101 | ATR72-102 | ATR72-201 | ATR72-202 | ATR72-211 | ATR72-212 | ATR72-212A
Product Type:
Aircraft
Product Subtype:
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: 93-07-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   92-NM-163-AD

AMENDMENT:   39-8535

AD NUMBER:   93-07-03

SUBJECT HEADING:   Airworthiness Directives; AEROSPATIALE Model ATR42-300, ATR72-100 and - 200 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective May 10, 1993.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
93-07-03 AEROSPATIALE: Amendment 39-8535. Docket 92-NM-163-AD.

Applicability: All Model ATR42-300 series airplanes, and all Model ATR72-100 and - 200 series airplanes; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent failure of the pressurization valves to close in the event of ditching, and to prevent interruption of electrical power to certain electrical equipment used during approach and landing, accomplish the following:

(a) Within 30 days after the effective date of this AD, remove the electrical switches, part numbers 9PD and 12HM, and identify the date codes in accordance with Aerospatiale Service Bulletin ATR42-31-0023, dated May 15, 1992 (for Model ATR42-300 and -320 series airplanes); or Aerospatiale Service Bulletin ATR72-31-1006, dated May 15, 1992 (for Model ATR72-100 and -200 series airplanes); as applicable.

(1) If the date code is identified as A6, A7, A8, A9, AO, AN, AD, B1, B2, B3, B4, B5, B6, or B7, prior to further flight, replace the currently-installed switch with a serviceable switch marked with a date code other than those listed above.

(2) If the date code is other than those listed in paragraph (a)(1) of this AD, reinstall the switch. No further action is necessary.

(b) As of the effective date of this AD, no person shall install an electrical switch, part numbers 9PD and 12HM, having a date code of A6, A7, A8, A9, AO, AN, AD, B1, B2, B3, B4, B5, B6, or B7, on any airplane.

(c) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Standardization Branch, ANM-113. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch, ANM-113.

NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113.

(d) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.

(e) The removal and identification shall be done in accordance with Aerospatiale Service Bulletin ATR42-31-0023, dated May 15, 1992 (for Model ATR42-300 and -320 series airplanes); or Aerospatiale Service Bulletin ATR72-31-1006, dated May 15, 1992 (for Model ATR72-100 and -200 series airplanes); as applicable. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from Aerospatiale, 316 Route de Bayonne, 31060 Toulouse, Cedex 03, France. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.

(f) This amendment becomes effective on May 10, 1993.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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