AD 77-15-17

final rule

Airworthiness Directives; ISRAEL AIRCRAFT INDUSTRIES (IAI) Model 1123 Airplanes

AD Number
77-15-17
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Israel Aircraft Industries, Ltd. 1123 Airworthiness Directives; ISRAEL AIRCRAFT INDUSTRIES (IAI) Model 1123 Airplanes

Unsafe Condition

Rupture of the hydraulic pressure line between the hydraulic pump and the firewall

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

Required Actions

Remove and discard hose P/N 6723087-43, remove and discard brackets P/N 5723548-3 and -5 for specified serial numbers, reinstall AN837-6 elbow with washer P/N 5723548-7, and install hose P/N 6723087-57 with a minimum 5.0-inch bend radius.

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

Compliance Time

within the next 150 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

Israel Aircraft Industries, Model 1123 airplanes, serial numbers 107, 151, 152, 153, 155 through 180, and 182 through 186, except those previously modified per IAI Service Bulletin No. WW-7A

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

Federal Register Abstract

Hydraulic Pressure Line

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_77-15-17.html
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Details
AD Number:
77-15-17
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; ISRAEL AIRCRAFT INDUSTRIES (IAI) Model 1123 Airplanes
Subject:
Hydraulic Pressure Line
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/29/1977
Make:
Israel Aircraft Industries, Ltd.
Model:
1123
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Superseded AD: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Superseded By: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: 77-15-17
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2990

AD NUMBER:   77-15-17

SUBJECT HEADING:   Airworthiness Directives; ISRAEL AIRCRAFT INDUSTRIES (IAI) Model 1123 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 29, 1977.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
77-15-17 ISRAEL AIRCRAFT INDUSTRIES (IAI): Amendment 39-2990. Applies to Model 1123 airplanes, S/N's 107, 151, 152, 153, 155 through 180, and 182 through 186, certificated in all categories, except those previously modified in accordance with IAI Service Bulletin No. WW-7A.

Compliance is required within the next 150 hours time in service after the effective date of this AD, unless already accomplished.

To prevent possible rupture of the hydraulic pressure line between the hydraulic pump and the firewall, accomplish the following:

(a) Remove and discard hose P/N 6723087-43 attached between the hydraulic pump pressure port and the AN837-6 elbow installed on pylon.

(b) For airplanes S/N's 175 through 180 and 182 through 186, remove and discard brackets P/N's 5723548-3 and -5.

(c) Remove the AN837-6 elbow from pylon, and reinstall with washer P/N 5723548- 7 on engine side of firewall.

(d) Install hose P/N 6723087-57 between hydraulic pump pressure port and AN837- 6 elbow, with 45-degree fitting of hose attached to elbow on pylon. (NOTE: Position the elbow on pylon to allow hose to be as straight as possible. Bend radius of hose may not be less than 5.0 inches.)

This amendment becomes effective August 29, 1977.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_77-15-17.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
77-15-17
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; ISRAEL AIRCRAFT INDUSTRIES (IAI) Model 1123 Airplanes
Subject:
Hydraulic Pressure Line
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/29/1977
Make:
Israel Aircraft Industries, Ltd.
Model:
1123
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: 77-15-17
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2990

AD NUMBER:   77-15-17

SUBJECT HEADING:   Airworthiness Directives; ISRAEL AIRCRAFT INDUSTRIES (IAI) Model 1123 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 29, 1977.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
77-15-17 ISRAEL AIRCRAFT INDUSTRIES (IAI): Amendment 39-2990. Applies to Model 1123 airplanes, S/N's 107, 151, 152, 153, 155 through 180, and 182 through 186, certificated in all categories, except those previously modified in accordance with IAI Service Bulletin No. WW-7A.

Compliance is required within the next 150 hours time in service after the effective date of this AD, unless already accomplished.

To prevent possible rupture of the hydraulic pressure line between the hydraulic pump and the firewall, accomplish the following:

(a) Remove and discard hose P/N 6723087-43 attached between the hydraulic pump pressure port and the AN837-6 elbow installed on pylon.

(b) For airplanes S/N's 175 through 180 and 182 through 186, remove and discard brackets P/N's 5723548-3 and -5.

(c) Remove the AN837-6 elbow from pylon, and reinstall with washer P/N 5723548- 7 on engine side of firewall.

(d) Install hose P/N 6723087-57 between hydraulic pump pressure port and AN837- 6 elbow, with 45-degree fitting of hose attached to elbow on pylon. (NOTE: Position the elbow on pylon to allow hose to be as straight as possible. Bend radius of hose may not be less than 5.0 inches.)

This amendment becomes effective August 29, 1977.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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