Hydraulic Hose
24-5603-95-59
Price on request
Hydraulic Hose
Available on back-order
Description
24-5603-95-59 hydraulic hose for the An-32
24-5603-95-59 is a hydraulic hose assembly listed for the hydraulic system of the Antonov An-32. The assembly provides a flexible fluid connection between components of the aircraft hydraulic system where a rigid pipeline cannot adequately accommodate installation tolerances, vibration and limited relative movement between connected components.
The complete part number is essential during selection. An-32 hose assemblies can have similar external construction while differing in end fittings, reinforcement, pressure class, working medium or installation position. A visually similar hose must not be treated as a replacement until the designation, configuration and applicable aircraft records have been compared.
Function within the An-32 hydraulic system
In operation, the flexible body carries hydraulic fluid between connected system components while the end fittings maintain a sealed mechanical interface with the aircraft pipeline. Flexibility helps reduce loads transferred by normal vibration, temperature change and small movements into adjacent rigid tubes, valves, pumps or equipment connections.
The exact installation point must be established from the illustrated parts catalogue, maintenance manual or system diagram for the individual aircraft. This position is not a general-purpose industrial hose. Suitability depends on the approved pressure, temperature, internal diameter, material compatibility, bend radius and fitting geometry. These execution-specific limits should come from the passport, drawing and current An-32 documentation.
Construction and identification of 24-5603-95-59
The current catalogue data identify alternative designation 1-6-2-690-OST110853-85, Type P, TU 38.0051515-92. The assembly is described as rubber aviation hose with metal-braid reinforcement and end fittings. Reinforcement supports the flexible body against mechanical and pressure loads, while factory-installed fittings provide a repeatable connection to the aircraft pipeline. Product markings, ferrules and any identification tag should remain legible for incoming inspection.
The exact drawing reference should be confirmed from the design documentation. A standard or technical-condition reference identifies a product family but does not by itself confirm every parameter of this exact execution. Working pressure, proof pressure, temperature range, mass, internal diameter and minimum bend radius were not reliably established in open sources and are therefore not inferred from a neighbouring hose.
Installation and technical-condition checks
Before installation, inspect protective caps, internal cleanliness, fittings and the complete flexible surface. Route the hose without stretching, twisting or forcing the ends into alignment. The installed assembly needs smooth bends and adequate clearance from hot zones, moving parts, sharp edges and locations where vibration could cause abrasion. Tightening and support arrangements must follow the applicable maintenance instructions.
Inspection should cover cracks, hardening, swelling, cuts, exposed reinforcement, damaged ferrules, corrosion and loose fittings. Evidence such as fluid seepage, wet fittings, pressure loss or contamination around the connection requires assessment under an approved maintenance procedure. Manufacturing date, storage history and permitted service life should be checked when documents are available. Good appearance alone does not establish airworthiness or interchangeability.
A removed hose may have stretched, deformed or taken a permanent bend in service. Dimensional comparison must therefore use the control points and method stated in the drawing, not an arbitrary end-to-end measurement. Fitting orientation is equally important because rotating an end after installation can introduce torsional stress into the reinforced flexible section.
Ordering 24-5603-95-59 and related An-32 hoses
The product is listed in the Aviamisto Hoses for AN-32 category. Related catalogue positions include 24-5603-95-51; 24-5603-95-47; 24-5603-95-48; 24-5603-95-98. These internal links simplify navigation within the An-32 range and do not indicate confirmed interchangeability.
For a supply enquiry, specify the full designation 24-5603-95-59, required quantity and documentation requirements. If possible, provide photographs of the removed hose, its marking and both end fittings. Applicability to a particular An-32 aircraft and approval for installation must be verified against the aircraft configuration and current technical documentation before use.
Technical Details
Product Type: Hydraulic hose assembly
Designation: 24-5603-95-59
Alternative Designations: 24-5603-95-59; 24 5603 95 59; 1-6-2-690 OST1 10853-85
Aircraft: Antonov An-32
Application: Hydraulic system
Function: Provides a flexible fluid connection between components of the aircraft hydraulic system
Hose Type: Type P
Construction: Rubber aviation hose with metal-braid reinforcement and end fittings
Technical Conditions: TU 38.0051515-92
Drawing: According to the applicable design documentation
Working Medium: Hydraulic fluid according to the applicable An-32 system documentation
Installation Area: An-32 hydraulic system; exact position requires aircraft documentation
Exact Working Pressure: Reliable execution-specific data were not found; confirm from the passport or drawing
End Fittings and Orientation: Confirm against the removed unit and approved drawing
Internal Diameter: Reliable data for this exact configuration were not found
Temperature Range: Reliable data for this exact configuration were not found
Mass: Reliable data for this exact configuration were not found
Related Products: 24-5603-95-51; 24-5603-95-47; 24-5603-95-48; 24-5603-95-98
Interchangeability: Not confirmed; matching appearance or one dimension is insufficient
Condition: New
Warranty: 6 Months
Stock Status: Pre-Order
Technical Documentation: Drawing, product passport and available conformity documents upon request
Payment & delivery
All shipments are carried out from our international warehouse in Dubai (UAE), as well as from our partners’ remote warehouses.
In Stock — items available in stock at the Dubai warehouse are dispatched within 5–10 business days after receiving 100% prepayment.
Remote Stock — items available at our partners’ remote warehouses are supplied within an average of 30–45 business days after receiving 100% prepayment.
Pre-Order — made-to-order products are manufactured and delivered within an average of 45–60 business days. Payment terms: 50% advance payment to start production, with the remaining 50% paid before dispatch from the Dubai warehouse after full readiness for shipment.
Returns & Changes (Restocking Fee)
For selected items, a RESTOCKING FEE of 10% may apply in case of return, order cancellation, or changes to the order specifications. This condition applies only to certain products and is confirmed at the order approval stage.
Warranty
All products are covered by a standard 6-month warranty.
Extended warranty is available upon request and is agreed individually; it may affect the final product price.
- Description
- Technical Details
- Payment & delivery
24-5603-95-59 hydraulic hose for the An-32
24-5603-95-59 is a hydraulic hose assembly listed for the hydraulic system of the Antonov An-32. The assembly provides a flexible fluid connection between components of the aircraft hydraulic system where a rigid pipeline cannot adequately accommodate installation tolerances, vibration and limited relative movement between connected components.
The complete part number is essential during selection. An-32 hose assemblies can have similar external construction while differing in end fittings, reinforcement, pressure class, working medium or installation position. A visually similar hose must not be treated as a replacement until the designation, configuration and applicable aircraft records have been compared.
Function within the An-32 hydraulic system
In operation, the flexible body carries hydraulic fluid between connected system components while the end fittings maintain a sealed mechanical interface with the aircraft pipeline. Flexibility helps reduce loads transferred by normal vibration, temperature change and small movements into adjacent rigid tubes, valves, pumps or equipment connections.
The exact installation point must be established from the illustrated parts catalogue, maintenance manual or system diagram for the individual aircraft. This position is not a general-purpose industrial hose. Suitability depends on the approved pressure, temperature, internal diameter, material compatibility, bend radius and fitting geometry. These execution-specific limits should come from the passport, drawing and current An-32 documentation.
Construction and identification of 24-5603-95-59
The current catalogue data identify alternative designation 1-6-2-690-OST110853-85, Type P, TU 38.0051515-92. The assembly is described as rubber aviation hose with metal-braid reinforcement and end fittings. Reinforcement supports the flexible body against mechanical and pressure loads, while factory-installed fittings provide a repeatable connection to the aircraft pipeline. Product markings, ferrules and any identification tag should remain legible for incoming inspection.
The exact drawing reference should be confirmed from the design documentation. A standard or technical-condition reference identifies a product family but does not by itself confirm every parameter of this exact execution. Working pressure, proof pressure, temperature range, mass, internal diameter and minimum bend radius were not reliably established in open sources and are therefore not inferred from a neighbouring hose.
Installation and technical-condition checks
Before installation, inspect protective caps, internal cleanliness, fittings and the complete flexible surface. Route the hose without stretching, twisting or forcing the ends into alignment. The installed assembly needs smooth bends and adequate clearance from hot zones, moving parts, sharp edges and locations where vibration could cause abrasion. Tightening and support arrangements must follow the applicable maintenance instructions.
Inspection should cover cracks, hardening, swelling, cuts, exposed reinforcement, damaged ferrules, corrosion and loose fittings. Evidence such as fluid seepage, wet fittings, pressure loss or contamination around the connection requires assessment under an approved maintenance procedure. Manufacturing date, storage history and permitted service life should be checked when documents are available. Good appearance alone does not establish airworthiness or interchangeability.
A removed hose may have stretched, deformed or taken a permanent bend in service. Dimensional comparison must therefore use the control points and method stated in the drawing, not an arbitrary end-to-end measurement. Fitting orientation is equally important because rotating an end after installation can introduce torsional stress into the reinforced flexible section.
Ordering 24-5603-95-59 and related An-32 hoses
The product is listed in the Aviamisto Hoses for AN-32 category. Related catalogue positions include 24-5603-95-51; 24-5603-95-47; 24-5603-95-48; 24-5603-95-98. These internal links simplify navigation within the An-32 range and do not indicate confirmed interchangeability.
For a supply enquiry, specify the full designation 24-5603-95-59, required quantity and documentation requirements. If possible, provide photographs of the removed hose, its marking and both end fittings. Applicability to a particular An-32 aircraft and approval for installation must be verified against the aircraft configuration and current technical documentation before use.
Product Type: Hydraulic hose assembly
Designation: 24-5603-95-59
Alternative Designations: 24-5603-95-59; 24 5603 95 59; 1-6-2-690 OST1 10853-85
Aircraft: Antonov An-32
Application: Hydraulic system
Function: Provides a flexible fluid connection between components of the aircraft hydraulic system
Hose Type: Type P
Construction: Rubber aviation hose with metal-braid reinforcement and end fittings
Technical Conditions: TU 38.0051515-92
Drawing: According to the applicable design documentation
Working Medium: Hydraulic fluid according to the applicable An-32 system documentation
Installation Area: An-32 hydraulic system; exact position requires aircraft documentation
Exact Working Pressure: Reliable execution-specific data were not found; confirm from the passport or drawing
End Fittings and Orientation: Confirm against the removed unit and approved drawing
Internal Diameter: Reliable data for this exact configuration were not found
Temperature Range: Reliable data for this exact configuration were not found
Mass: Reliable data for this exact configuration were not found
Related Products: 24-5603-95-51; 24-5603-95-47; 24-5603-95-48; 24-5603-95-98
Interchangeability: Not confirmed; matching appearance or one dimension is insufficient
Condition: New
Warranty: 6 Months
Stock Status: Pre-Order
Technical Documentation: Drawing, product passport and available conformity documents upon request
All shipments are carried out from our international warehouse in Dubai (UAE), as well as from our partners’ remote warehouses.
In Stock — items available in stock at the Dubai warehouse are dispatched within 5–10 business days after receiving 100% prepayment.
Remote Stock — items available at our partners’ remote warehouses are supplied within an average of 30–45 business days after receiving 100% prepayment.
Pre-Order — made-to-order products are manufactured and delivered within an average of 45–60 business days. Payment terms: 50% advance payment to start production, with the remaining 50% paid before dispatch from the Dubai warehouse after full readiness for shipment.
Returns & Changes (Restocking Fee)
For selected items, a RESTOCKING FEE of 10% may apply in case of return, order cancellation, or changes to the order specifications. This condition applies only to certain products and is confirmed at the order approval stage.
Warranty
All products are covered by a standard 6-month warranty.
Extended warranty is available upon request and is agreed individually; it may affect the final product price.