AD 75-19-04

Airworthiness directive · Valve System · Aerostar International RX-6, S-40A, S-50A and 2 more

Effective
September 17, 1975
Models
RX-6, S-40A, S-50A, S-55A, S-60A
Data sheet
TCDSA15CE
Registered aircraft
224 matched by model
Product
Aircraft · Balloon
Amendment
39-2363

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

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The airworthiness directive

75-19-04 RAVEN: Amendment 39-2363. Raven Model S-40A, S-50A, S-55A, S-60A, and RX-6 Hot Air Balloons:

Applies to Rego 7553S series blast valves installed on all models of the Raven hot air balloons certificated in all categories.

Compliance required as indicated below after the effective date of this AD unless already accomplished.

To prevent failures of the "O" ring on the valve stem; valve seat washer loosening; or valve actuating handle rollpin becoming dislodged, accomplish the following or an equivalent modification approved by the Chief, Engineering and Manufacturing Branch, FAA Rocky Mountain Region.

Within the next 25 hours time in service unless already accomplished within the last 25 hours time in service, accomplish Paragraph a, b, c, and d. Paragraph "a" and "c" are to be accomplished thereafter at each 100 hours time in service or at intervals not to exceed 12 calendar months from the last inspection, whichever comes first.

a. Remove the valveactuating lever rollpin P/N 7553S-8 from actuating lever. (Be careful to remove any burrs in the stem area around the rollpin hole before removing the valve stem P/N 7553S-1 from the bonnet P/N 7553-5). Replace the "O" ring stem seal with a new Rego "O" ring P/N 1421.7. Lubricate the new "O" ring with Orange Solid Oil (Rego P/N 5555GS) or unmedicated Vaseline lubricant before reassembly. Other lubricants may cause shrinkage of the "O" ring.

b. Check the torque of the valve seat retaining screw to 8 to 10 in-lbs in the counter-clockwise (loosening) direction. If it turns, the screw must be removed, cleaned of lubricant and reinstalled using MIL-S 22473 high strength thread locking compound, or equivalent. Recheck torque after thread locking compound has cured.

CAUTION: Do not permit the thread locking compound to adhere to the rubber seating surface.

c. Reinstall valve actuating lever on the valve body with rollpin, P/N 7553S-8. Install a number three machine screw and stop nut or a 3/32 inch stainless steel cotter pin or .040 inch diameter safety wire through the hole in the rollpin, holding the actuating handle to the valve body and secure.

d. Appropriate maintenance records must be kept in accordance with FAR 91.173.

This amendment becomes effective on September 17, 1975.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 224

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Raven106 aircraft
  • Aerostar International105 aircraft
  • Raven Industries13 aircraft
By year built
19692007
Registered aircraft by year built: 161 aircraft
19691
19711
19724
19732
19745
19751
19764
19774
19789
19797
19805
19817
19828
19837
19848
19855
198611
19879
19884
19895
19902
19911
19923
19934
19945
19957
19967
19974
19986
19993
20005
20012
20021
20032
20041
20071

63 with no year recorded

By model

Aircraft

See all 224 aircraft