TUBES, HOSES, AND FITTINGS

Similar documents
C I R R U S COLLECTOR DESCRIPTION

SNS SUBJECT: RADOME IPS FLUID SYSTEM - Radome IPS Routing

STALL WARNING SYSTEM 1. DESCRIPTION A.

CIRRUS AIRPLANE MAINTENANCE MANUAL

Propeller Assembly. 1. General

Service Bulletin. ATA 27-00: Flight Controls Rudder-Aileron Interconnect Modification

Flaps System. 1. General

A. Stall Warning System - Serials w/o Ice Protection

CIRRUS AIRPLANE MAINTENANCE MANUAL

CIRRUS AIRPLANE MAINTENANCE MANUAL

CIRRUS AIRPLANE MAINTENANCE MANUAL

CIRRUS AIRPLANE MAINTENANCE MANUAL

CIRRUS AIRPLANE MAINTENANCE MANUAL

Yaw Control and Trim. 1. General. A. Yaw Control System. B. Yaw Trim System

CIRRUS AIRPLANE MAINTENANCE MANUAL

CIRRUS AIRPLANE MAINTENANCE MANUAL

CIRRUS AIRPLANE MAINTENANCE MANUAL

CIRRUS AIRPLANE MAINTENANCE MANUAL

CIRRUS AIRPLANE MAINTENANCE MANUAL

53-40 ATTACH FITTINGS

Fluid-O-Tech ROTOFLOW ROTARY VANE PUMP REBUILD MANUAL

SNS SUBJECT: NOSE GEAR - Nose Landing Gear Assembly Inspection and Reinforcement

Storage. 1. General. A. Fuel Storage System

C I R R U S COWLING DESCRIPTION

Fastener Identification And Torque Data

Service Bulletin. ATA 52-10: Passenger and Crew Doors Door Latching Assembly Upgrade

Maintenance Information

CIRRUS SR2X SB 2X R2. Service Bulletin. Issued: Revised: June 26, 2012 July 31, 2012

Escape Cylinder and Valve

57-50 FLIGHT SURFACES

SPECIAL PURPOSE EQUIPMENT

CIRRUS AIRPLANE MAINTENANCE MANUAL

GBV-G Balancing Valves

Wing Structure. 1. General

CHAPTER 32 LANDING GEAR. Section Title Page

WHEELS 1. DESCRIPTION A.

Maintenance Information

CIRRUS AIRPLANE MAINTENANCE MANUAL

18SP631 MBE 4000 Oil Gallery Threaded Plug Installation

FLIGHT SIMULATOR SYSTEMS

CIRRUS AMM TEMPORARY REVISION

2004 Toyota Truck Tundra 4WD V8 4.7L (2UZ FE)

Power Train. Chapter 5

WESTATE DIESEL SYSTEMS

CIRRUS SR2X SB 2X Service Bulletin. Issued: February 27, SNS SUBJECT: TEMPERATURE CONTROL - Cabin Air Coupler Actuator Rigging

CIRRUS AIRPLANE MAINTENANCE MANUAL

CIRRUS AIRPLANE MAINTENANCE MANUAL

Cylinder and Valve: AirHawk II Air Mask

C I R R U S CONTROLLING DESCRIPTION

Iso-Flo Coupling Repair

Storage. 1. General. A. Fuel Storage System

Type N550 Snappy Joe Emergency Shutoff Valves

CIRRUS AIRPLANE MAINTENANCE MANUAL

C I R R U S BRAKES DESCRIPTION

REFILL STATION REBUILD KIT P/N 14270NOS

CHAMBER CUSTOMIZATION GUIDE TSE

Description This Service Bulletin provides for the replacement of the Pick-up Collar Support, Aluminum Screws and Launch Tube.

33-40 EXTERIOR LIGHTING

C I R R U S DISTRIBUTION DESCRIPTION

VIS Standard and Wheel Motors 45 Series Parts and Repair Information -005

Product Customization Guide TSE Brakes, Inc.

S ECTION SERIES

CIRRUS AIRPLANE MAINTENANCE MANUAL

S ECTION SERIES

CIRRUS AIRPLANE MAINTENANCE MANUAL

INDEX GENERAL. Page Connecting Rod 2M-3 Front Wheel Alignment 2M-4 Front Wheel Shimmy 2M-5 General 2M-1

DeZURIK R1 AND R2 POWERRAC ACTUATORS

DeZURIK R1 POWERRAC ACTUATOR ON 1/2-3" PEC ECCENTRIC VALVES

REAR SUSPENSION. Wheel Bearing and Wheel Hub. NOTE: All-Wheel Drive (AWD) shown, Front Wheel Drive (FWD) vehicles similar.

CHAPTER 15 WINCH MAINTENANCE. This chapter contains maintenance instructions for disassembly and repair of winch components at the Direct

OIL PUMP (G306709) DISCOVERY 3, ENGINE - TDV6 2.7L DIESEL SPECIAL TOOL(S) Crankshaft Front Seal Remover PUMP - OIL - RENEW

INSTRUCTION MANUAL IM-422 For HTC/COUPLING ASSEMBLY HC-8088

CIRRUS AIRPLANE MAINTENANCE MANUAL

DeZURIK " BAW AWWA BUTTERFLY VALVES WITH EPOXY-RETAINED SEAT

Non-Valved Unisex Coupling

CIRRUS AIRPLANE MAINTENANCE MANUAL

DR Series Radial Diaphragm Valves

Betico SB1 Compressor. Unloader Kit Installation Manual

2000 Chrysler SEBRING

Compression Style Transportation

Bottom Loading & Recirculation Adapters

Self-Priming Centrifugal Pumps Refer to pump manual for General Operating and Safety Instructions.

PASSENGER AND CREW DOORS

CIRRUS AIRPLANE MAINTENANCE MANUAL

Installation, Operating and Maintenance Instructions. Rotating Machine Screw Actuators. With Parts List Publication Part No.

Sachs 48mm Closed Cartridge fork Service Manual

Superlift 4 lift system for JEEP CHEROKEE XJ with coil spring suspension INSTALLATION INSTRUCTIONS

Service Bulletin No. 2916

Maintenance Manual. 3-Inch Internal Valve. F660 Series

COYOTE ENTERPRISES, INC. 9/10 BLAST WHEEL MAINTENANCE & ASSEMBLY MANUAL

CYLINDER HEAD. Cylinder Head Assembly. Sized for Print VALVES

Maintenance Manual 3-INCH INTERNAL VALVE F660 SERIES

BRAKE SYSTEM Nissan 240SX DESCRIPTION BRAKE BLEEDING * PLEASE READ FIRST * BLEEDING PROCEDURES ADJUSTMENTS BRAKE PEDAL HEIGHT SPECS TABLE

Installation Instructions

Service Bulletin SB 07-03

ANDERSON GREENWOOD SERIES 500 PILOT OPERATED SAFETY RELIEF VALVES INSTALLATION AND MAINTENANCE INSTRUCTIONS

CIRRUS AIRPLANE MAINTENANCE MANUAL

Firehawk Second Stage Regulator Fire Service

18SP660Rev2 EPA04 and EPA07 MBE 4000 Steel Low Pressure Fuel Line Kits (P/N: A and A )

Fluid Pump. Special Tool(s) Alignment Gauge, Transmission Fluid Pump Alignment Gauge, Transmission Fluid Pump

Transcription:

TUBES, HOSES, AND FITTINGS 1. DESCRIPTION This section contains instructions and specifications for aircraft system plumbing and fittings. Page 1

2. MAINTENANCE PRACTICES A. Ice Protection System Compression Fittings (See Figure 1) The following procedures are intended for stainless steel and aluminum Ice Protection System Compression Fittings. The fittings covered in this section are intended for use with nylon and stainless steel tubing. Compression fittings covered are 3/16, 5/16, 3/8 and 1/2 sizes. Compression fittings consist of a nut, olive, and o-ring where the nut is tightened to compress the o-ring between the olive and the mating surface. Compression fittings are available in a range of configurations to facilitate assembly of a system; Straight equal fittings where both fitting outlets are the same size are generally used to connect a joint in nylon tubing. Straight unequal fittings are used to connect a joint between two nylon tubes of different size. Equal tees and unequal tees are used in the same way as equal and unequal straight fittings but are configured to accept three tubes. Unequal tees are configured to accept both two small tubes and one larger tube or two large tubes and one smaller tube. Bulkhead fittings are used in the same way as straight fittings or tees except that one side of the fitting has an extended thread which passes through a bulkhead and a lock nut to secure the fitting in position. Compression fittings to equipment on the aircraft are configured to accept one tube. The remaining end of the fitting is screwed into the equipment and sealed with an o-ring seal or bonded seal. The threaded portion of the fitting may have either a parallel thread or a tapered thread. Tubing and compression fittings used on the Ice Protection System are specified in the Illustrated Parts Catalog. With a few exceptions, the use of dissimilar metals within an assembled fitting is to be avoided. CAUTION: When replacing components, cap all supply lines and remake connections as quickly as possible to avoid large amounts of air from entering the system. Procedures for priming the metering pump(s) are described in the Servicing - Metering Pump Procedures as found in the ICE PROTECTION - Distribution Sections of the AMM for the appropriate aircraft configuration; Serials 22-0334 thru 22-2437 w/ Basic Ice Protection: (Refer to 30-05) Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection: (Refer to 30-06) Serials w/ FIKI: (Refer to 30-07) Procedures for removing air from the arterial supply lines and the leading edge panels are described in the Porous Panel Purging procedure as found in the ICE PROTECTION - Distribution Sections of the AMM for the appropriate aircraft configuration. (Refer to 30-00) CAUTION: During disassembly and assembly of compression fittings, apply back torque to fitting nuts to avoid kinking or twisting distribution line. Page 2

(1) Disassembly - Ice Protection System Compression Fittings (a) Unscrew the coupling fittings and extract the tubing from fitting. (b) Remove and discard o-ring(s). (c) Inspect existing components for cracks, burrs, corrosion, and wear. Signs of burnishing/ abrasion on the sealing surface are typical and acceptable. Replace damage or worn components as necessary: 1 Slide nut away from the olive. 2 As close as possible behind the olive, cut tubing square to remove damaged olive. 3 If necessary, slide nut off tubing and replace. (2) Assembly - Ice Protection System Compression Fittings (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Clenching Tool T300-112A CAV Aerospace Installation of 3/16 O.D. tubing. Clenching Tool T300-120A CAV Aerospace Installation of 5/16 O.D. tubing. Clenching Tool T300-145 CAV Aerospace Installation of 3/8 O.D. tubing. Clenching Tool T300-144 CAV Aerospace Installation of 1/2 O.D. tubing. Coupling Refer to IPC Cirrus Design Compression Fitting Assembly O-Ring Refer to IPC Cirrus Design Compression Fitting Assembly Olive Fitting Refer to IPC Cirrus Design Compression Fitting Assembly Nut Refer to IPC Cirrus Design Compression Fitting Assembly (b) (c) (d) If disassembly inspection required nut and/or olive replacement: 1 Cleanly cut end of tubing square. 2 Assemble nut and olive onto the tubing Position nut, olive, and nylon tubing to clenching tool and press tubing fully into end of clenching tool. Ensure tubing extends past the olive to the full depth of the clenching tool. Finger tighten compression nut. CAUTION: Note: Do not clench olive with O-Ring installed. It is typical for the torque drag to rise rapidly during olive clenching. (e) Tighten compression nut to the appropriate Tightening Angle. (See Figure 1) (f) Unscrew nut and remove tubing from clenching tool. (g) Perform Inspection/Check - Compression Fitting to ensure olive fitting has been properly clenched. (Refer to ) (h) Reassemble compression fitting. 1 Install new O-Ring. 2 Finger tighten compression nut. 3 Tighten compression nut 180 past finger tight. Page 3

(3) Inspection/Check - Ice Protection System Compression Fittings (a) If necessary, place shop towel below compression fitting to catch fluid drip. (b) If necessary, disconnect distribution line from component. (c) Inspection Criteria (See Figure 1) 1 A correctly installed olive will exhibit the following characteristics: Angled sealing surface of olive has signs of burnishing/abrasion; Forward edge of olive is no longer visible and is "curled" into nylon tubing; Nylon tubing exhibits slight flare on the sealing surface side of the olive; Olive is physically secure and does not spin or pull off by hand. 2 An under tightened olive will exhibit the following characteristics: Angled sealing surface of olive has no or insignificant signs of burnishing/abrasion; Forward edge of olive is visible and has not been "curled" into nylon tubing; Nylon tubing does not exhibit a flare on the sealing surface side of the olive; Olive is not physically secure and may spin easily or pull off by hand. 3 An over tightened olive will exhibit the following characteristics: Angled sealing surface concave and signs of excessive burnishing/abrasion; Nylon tubing exhibits excessive flaring on the sealing surface side of the olive. (d) Verify required length of tubing extends beyond end of olive fitting. (See Figure 1) Page 4

COUPLING BODY NUT COMPRESSION FITTINGS RECESS TUBE OLIVE NUT TUBE O-RING (NYLON TUBE ONLY) COUPLING BODY O-RING (NYLON TUBE ONLY) OLIVE INSPECTION AND INSTALLATION CRITERIA A UNDER TIGHTENED CORRECT OVER TIGHTENED NYLON TUBING AND ALUMINUM ALLOY FITTINGS TUBE O.D. OLIVE DISTANCE "A" ±0.05" TIGHTENING ANGLE ±30 3/16" 5/16" 3/8" 360 315 315 1/2" 0.38" 270 NYLON TUBING AND STAINLESS STEEL FITTINGS TUBE O.D. 3/16" 5/16" OLIVE DISTANCE "A" ±0.05" TIGHTENING ANGLE ±30 315 315 STAINLESS STEEL TUBING AND STAINLESS STEEL FITTINGS TUBE O.D. OLIVE DISTANCE "A" ±0.05" TIGHTENING ANGLE ±30 3/16" 270 SR22_MM20_3315 Figure 1 Compression Fittings and Inspection Criteria Page 5

B. Hydraulic Fittings (See Figure 2) Hydraulic fittings must be torqued to the following specifications to prevent loosening while in flight, or damage due to over tightening. CAUTION: The tube nut must never be used to pull the tube assembly to seat against the fitting. Page 6

Torque for AN-818 Nuts with Steel Tubing Inch-Pounds Nm Minimum Maximum Minimum Maximum -3 3/16 95 105 10.7 11.9-4 1/4 135 150 15.3 16.9-6 3/8 270 300 30.5 33.9-8 1/2 450 500 50.8 56.5-10 5/8 650 700 73.4 79.0-12 3/4 900 1000 101.7 112.9 Torque for AN-818 Nuts with Aluminum oy Tubing Inch-Pounds Nm Minimum Maximum Minimum Maximum -3 3/16 25 35 2.8 3.9-4 1/4 50 65 5.6 7.3-6 3/8 110 130 12.4 14.7-8 1/2 230 260 25.9 29.4-10 5/8 330 360 37.3 40.6-12 3/4 460 500 52.0 56.4 Torque for AN-818 Nuts with Flexible Hoses Aluminum/Brass Fittings Inch-Pounds Nm Minimum Maximum Minimum Maximum -3 3/16 70 105 7.9 11.9-4 1/4 100 140 11.3 15.8-6 3/8 150 195 16.9 22.0-8 1/2 270 350 30.5 39.5-10 5/8 360 430 40.7 48.6-12 3/4 460 550 52.0 62.1 Figure 2 Hydraulic Fittings Torque Values (Sheet 1 of 2) Page 7 01 Jan 2016

Torque for AN-818 Nuts with Flexible Hoses Steel Fittings Inch-Pounds Nm Minimum Maximum Minimum Maximum -3 3/16 95 140 10.7 15.8-4 1/4 135 190 15.3 21.5-6 3/8 215 280 24.3 31.6-8 1/2 470 550 53.1 62.1-10 5/8 620 745 70.1 84.2-12 3/4 855 1055 96.6 119.1 Torque for Bulkhead Fittings Gasketed Fittings Jamnuts and Fittings without Gaskets Aluminum or Steel Aluminum Steel Minimum Maximum Minimum Maximum Minimum Maximum -3 3/16 50 75 65 80 70 90-4 1/4 55 80 90 105 110 130-6 3/8 100 150 125 145 225 275-8 1/2 180 230 240 280 400 450-10 5/8 250 350 330 370 550 650-12 3/4 420 600 540 660 800 960 Figure 2 Hydraulic Fittings Torque Values (Sheet 2 of 2) Page 8 01 Jan 2016