ASSOCIATED APPROVED FITTINGS
TABLE D
Tube Material and Fitting Selection Tables
Figure 802 (Sheet 5)
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TUBE SIZES
MATERIAL 04 05 06 121008 16 20 24
0.250 0.312 0.375 0.7500.6250.500 1.000 1.250 1.500
21-6-9 0.016 0.020 0.020 0.026 0.033 0.039 0.052
3A1-2.5V 0.016 0.019 0.026 0.032 0.039 0.052 0.070
6061-T6 0.035 0.035 0.035 0.035 0.035 0.035 0.035 0.049 0.049
304 1/8 H 0.020 0.020 0.028 0.035 0.049 0.058 0.065* 0.035* 0.049*
* NOT QUALIFIED FOR 3000 PSI SYSTEMS, LOWER PRESSURES ONLY.
NOTE: ALTERNATIVE WALL THICKNESSES FOR TUBE REPAIRS OF 3000 PSI AND LOWER SYSTEM
PRESSURE APPLICATIONS PER FLAGNOTE 8 .
CRES 321 TUBING PER MIL-T-8808 MAY BE USED AS A SUBSTITUTE FOR 304 TUBING PER MIL-T-8504, 6061-T6 ALUMINUM TUBING PER MIL-T-7081 OR AMS 4083. 6061-T6 ALUMINUM PER MIL-T-7081 OR AMS 4083 MAY BE USED AS A SUBSTITUTE FOR 6061-T6 ALUMINUM TUBING PER 22-T-700/6. CONTACT THE BOEING COMPANY WHEN CONSIDERING USE OF TUBE MATERIALS OTHER THAN THOSE SPECIFIED.
TABLE E
Tube Material and Fitting Selection Tables
Figure 802 (Sheet 6)
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TUBING MATERIAL LOCATION ON AIRPLANE SURFACE TUBING AND OPTIONS FINISH RECOMMENDATION COMMERCIAL AIRPLANES FINISH CODE FOR
CRES Titanium All All Outside Inside Outside Inside + Paint (White) Passivate + Primer Passivate + Primer (Green) Optional: None None None None F-17.09 + F-20.02 F-17.09 + F-20.02 + F-21.03 F-25.01 F-25.01 F-25.01 F-25.01
Aluminum Fuel Tanks All Other Outside Inside Inside Outside Anodize + Primer + Paint (White) Anodize plus Primer (Green) Optional: None Alodine (Transparent Gold) None F-17.19 + F-20.02 + F-21.03 F-25.01 F-17.08 F-25.01 F-17.19 and F-20.02
TYPICAL FINISHES FOR HYDRAULIC TUBING
TABLE F
Tube Material and Fitting Selection Tables
Figure 802 (Sheet 7)
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