AD 82-21-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Jet Electronics Technology, Inc. | Emergency Power Supply | Airworthiness Directives; JET ELECTRONICS AND TECHNOLOGY, INC. All Model PS-835 Series Emergency Power Supply Installations |
| appliance | Jet Electronics Technology, Inc. | Emergency Power Supply | Airworthiness Directives; JET ELECTRONICS AND TECHNOLOGY, INC. All Model PS-835 Series Emergency Power Supply Installations |
Unsafe Condition
A false indication that emergency power is available could occur due to the absence of a temporary placard near the test switch or unmodified J.E.T. model PS-835 series emergency power supplies.
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Required Actions
Within 25 hours time-in-service after the effective date, check for a panel located battery test switch and install a temporary placard if present. By October 1, 1983, examine records and modify the power supply per SB501-1228-7 if it is an unmodified PS-835A, B, C, or D model. The modification must be done by an FAA-certificated repair station for flight instrument power supplies.
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 the effective date of this AD and on or before October 1, 1983
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Affected Aircraft
Jet Electronics and Technology, Inc. Model PS-835 series Emergency Power Supply installations
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Federal Register Abstract
Emergency Power Supply
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_82-21-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 82-21-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; JET ELECTRONICS AND TECHNOLOGY, INC. All Model PS-835 Series Emergency P...Show more Subject: Emergency Power Supply Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 10/21/1982 Make: Jet Electronics Technology, Inc. Model: Emergency Power Supply Product Type: Appliance Product Subtype: Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 82-21-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4475 AD NUMBER: 82-21-04 SUBJECT HEADING: Airworthiness Directives; JET ELECTRONICS AND TECHNOLOGY, INC. All Model PS-835 Series Emergency Power Supply Installations ACTION: SUMMARY: DATES: Effective October 21, 1982. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 82-21-04 JET ELECTRONICS AND TECHNOLOGY, INC.: Amendment 39-4475. Applies to all Model PS-835 series Emergency Power Supply installations. NOTE: This power supply is usually used to supply electrical power for third (standby) attitude indicators, emergency lighting, radio communications and other equipment critical to the safety of the airplane. Compliance: Required as indicated unless already accomplished. To prevent a false indication, that emergency power is available, accomplish the following: a) Within the next 25 hours time-in-service after the effective date of this AD check to determine whether the emergency power supply installation incorporates a panel located battery test switch. 1) If the installation incorporates a panel located battery test switch, prior to further flight install a temporary placard near the test switch which reads as follows: TO TEST EMER PWR SUPPLY 1. DISREGARD EMER PWR SW TEST POSITION 2. A/C MASTER/BATT SW-OFF 3. EMER PWR SW-ON 4. CK OPERATION OF ACCESSORY/INSTR b) On or before October 1, 1983, examine the aircraft manufacturer's records and/or emergency power supply installation to determine whether the emergency power supply is a J.E.T. model PS-835A, -835B, -835C or -835D. If the power supply is a PS-835A not incorporating a Mod 6, a PS-835B not incorporating a Mod 7, a PS-835C not incorporating Mod 1 or a PS-835D not incorporating a Mod 1, modify the J.E.T. power supply in accordance with J.E.T. Service Bulletin SB501-1228-7 dated May 20, 1982. Remove the temporary placard if required by paragraph a) of this AD when the modification required by this paragraph is incorporated. c) Paragraph a) of this AD may be accomplished by the owner/operator on any airplane owned or operated by the person. This person must make the prescribed aircraft record entry indicating compliance with paragraph a) of this AD. d) The modification required by paragraph b) of this AD must be accomplished by an appropriately rated, FAA certificated repair station on those power supplies used as a source of power for flight instruments. e) Aircraft may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished. f) An equivalent method of compliance with this AD may be used if approved by the Chief, Chicago Aircraft Certification Office, FAA, 2300 East Devon Avenue, Des Plaines, Illinois 60018; telephone (312) 694-7127. This amendment becomes effective on October 21, 1982. FOOTER:
Document Text
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AD Final Rules - DRS_82-21-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 82-21-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; JET ELECTRONICS AND TECHNOLOGY, INC. All Model PS-835 Series Emergency P...Show more Subject: Emergency Power Supply Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 10/21/1982 Make: Jet Electronics Technology, Inc. Model: Emergency Power Supply Product Type: Appliance Product Subtype: Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 82-21-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4475 AD NUMBER: 82-21-04 SUBJECT HEADING: Airworthiness Directives; JET ELECTRONICS AND TECHNOLOGY, INC. All Model PS-835 Series Emergency Power Supply Installations ACTION: SUMMARY: DATES: Effective October 21, 1982. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 82-21-04 JET ELECTRONICS AND TECHNOLOGY, INC.: Amendment 39-4475. Applies to all Model PS-835 series Emergency Power Supply installations. NOTE: This power supply is usually used to supply electrical power for third (standby) attitude indicators, emergency lighting, radio communications and other equipment critical to the safety of the airplane. Compliance: Required as indicated unless already accomplished. To prevent a false indication, that emergency power is available, accomplish the following: a) Within the next 25 hours time-in-service after the effective date of this AD check to determine whether the emergency power supply installation incorporates a panel located battery test switch. 1) If the installation incorporates a panel located battery test switch, prior to further flight install a temporary placard near the test switch which reads as follows: TO TEST EMER PWR SUPPLY 1. DISREGARD EMER PWR SW TEST POSITION 2. A/C MASTER/BATT SW-OFF 3. EMER PWR SW-ON 4. CK OPERATION OF ACCESSORY/INSTR b) On or before October 1, 1983, examine the aircraft manufacturer's records and/or emergency power supply installation to determine whether the emergency power supply is a J.E.T. model PS-835A, -835B, -835C or -835D. If the power supply is a PS-835A not incorporating a Mod 6, a PS-835B not incorporating a Mod 7, a PS-835C not incorporating Mod 1 or a PS-835D not incorporating a Mod 1, modify the J.E.T. power supply in accordance with J.E.T. Service Bulletin SB501-1228-7 dated May 20, 1982. Remove the temporary placard if required by paragraph a) of this AD when the modification required by this paragraph is incorporated. c) Paragraph a) of this AD may be accomplished by the owner/operator on any airplane owned or operated by the person. This person must make the prescribed aircraft record entry indicating compliance with paragraph a) of this AD. d) The modification required by paragraph b) of this AD must be accomplished by an appropriately rated, FAA certificated repair station on those power supplies used as a source of power for flight instruments. e) Aircraft may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished. f) An equivalent method of compliance with this AD may be used if approved by the Chief, Chicago Aircraft Certification Office, FAA, 2300 East Devon Avenue, Des Plaines, Illinois 60018; telephone (312) 694-7127. This amendment becomes effective on October 21, 1982. FOOTER:
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