AD 81-19-04

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AD Number:
81-19-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; RAJAY INDUSTRIES, INC. Hose Assembly Applies to All Affected Aircraft, Ce...Show more
Subject:
Hose Assembly
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
09/17/1981
Effective Date:
09/17/1981
Make:
Rajay | Twin Commander Aircraft LLC | Textron Aviation Inc. | Britten-Norman Aerospace Ltd. | The Ki...Show more
Model:
Hose Assemblies | 500A | 500B | 500S | 500U | 35 | H35 | J35 | K35 | M35 | N35 | P35 | 35-33 | 35-A3...Show more
Product Type:
Appliance
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
AIR-700: Compliance & Airworthiness Division
Office of Primary Responsibility:
AIR-760: Central Certification Branch CHI
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 81-19-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4214

AD NUMBER:   81-19-04

SUBJECT HEADING:   Airworthiness Directives; RAJAY INDUSTRIES, INC. Hose Assembly Applies to All Affected Aircraft, Certificated in All Categories

ACTION:  

SUMMARY:  

DATES:   Effective September 17, 1981.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
81-19-04 RAJAY INDUSTRIES, INC.: Amendment 39-4214. Applies to all affected aircraft, certificated in all categories modified per

Rajay Supplemental Type Certificates	
Aircraft Model	
Rajay STC No.

	
Aerocommander 500-A	
STC SA683WE

Aerocommander 500-B, 500-S & 500-U	
STC SA529WE

Beech H35, J, K, M, N & P, and 35-33, 35-A33, 35-B33, 35-C33, E33 & F33	
STC SA1252WE

Beech S35, V35, V35A, V35B, 35-C33A, E33A, E33C, F33A, F33C	
STC SA2556WE

Beech 95, B95, B95A, D95A & E95	
STC SA153SO

Britten Norman Islander, BN-2, BN-2A, BN-2A-6, BN-2A-8, BN-2A-9	
STC SA2243WE

Cessna 180-A, B, C, D, E, F, G, H & J	
STC SA1157WE

Cessna 182-A, B, C, D, E, F, G, H, J, K, L, M, N & P	
STC SA1032WE

Cessna 210-A, B, C, 210-5(205), 210-5A(205A)	
STC SA1098WE

Cessna 310-C, D, E, F & G	
STC SA2383SO

Cessna 310-I and J	
STC SA181SO

Evangel 4500-300
Evangel 4500-300, Series II	
STC SA2657WE

Helio Courier H-295	
STC SA156SO

Helio Courier H-395	
STC SA125SO

Lake 4 and 4A	
STC SA2270WE

Lake 4-200	
STC SA2990WE

Mooney 20A, M20B, M20C, M20D & M20G	
STC SA1156WE

Mooney 20E & M20F	
STC SA1411WE

Mooney 20J	
STC SA3555WE

Piper PA-23-160, Apache	
STC SA1260WE

Piper PA-23-160, Apache	
STC SA4-1637-WE

Piper PA-23-235, -250, Aztec "B"	
STC SA539WE

Piper PA-23-250, Aztec "C"	
STC SA840WE

Piper PA-24-250, Comanche	
STC SA811WE

Piper PA-24-400, Comanche	
STC SA2359WE

Piper PA-30 & 39, Twin Comanche	
STC SA787WE

Piper PA-32-260, Cherokee	
STC SA1557WE

Piper PA-32R-300, Lance	
STC SA3513WE

Piper PA-34-200, Seneca	
STC SA2937WE

Compliance required as indicated, unless already accomplished.

To prevent failure of the powerplant hoses carrying air, fuel and/or oil and resultant fire hazard, accomplish the following:

(a) Within 100 hours' time in service from the effective date of this AD, or prior to return to service after the next annual inspection, whichever occurs first, visually inspect the powerplant fuel, air and oil hose assemblies listed in Rajay Service Letter No. 28 dated August 3, 1981 to determine the general condition and age of the hose assemblies based upon the metal plate attached to the hose, and;

1) If the hose assembly is five years old or older, replace with like serviceable part prior to further flight.

2) If the hose assembly does not have a metal tag and the age cannot be determined, replace with like serviceable part prior to further flight.

3) Record hose ages in the aircraft engine log book and establish a replacement schedule for affected hoses such that a five year life will not be exceeded.

4) If the hose assembly is deteriorated (regardless of age), replace with like serviceable part prior to further flight.

(b) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate aircraft to a base for the accomplishment of inspections or modifications required by this AD.

(c) Alternative inspections, modifications or other actions which provide an equivalent level of safety may be used when approved by the Chief, Engineering and Manufacturing Branch, FAA Western Region.

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 553(a)(1). All persons affected by this directive, who have not already received these documents from the manufacturer, may obtain copies upon request to Rajay Industries, Inc., 2600 East Wardlow Road, P.O. Box 207, Long Beach, California 90801, telephone (213) 426-0346. A historical file on this AD, which includes the incorporated material in full, is maintained by the FAA at its Headquarters in Washington, D.C. and at FAA Western Region Office.

This amendment becomes effective September 17, 1981.

FOOTER: