STC SA1235SO
FAA DRS lists SA1235SO as Current · Reissued, held by Saf-Air Products Inc., for Cessna Aircraft 152, Cessna Aircraft A152, and Cessna Aircraft 150 Series, and 1 more aircraft configuration. Recorded change: Replacement of the lower fuselage fuel drain cap (P/N AN929-6) with an adapter type coupling, (belly drain P/N MT-101) and an exposed quick drain valve P/N CAV-160D). (A152 SERIES AIRPLANES STARTING WITH MODEL150F (S/N 15061533) AND SUBSEQUENT). Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Replacement of the lower fuselage fuel drain cap (P/N AN929-6) with an adapter type coupling, (belly drain P/N MT-101) and an exposed quick drain valve P/N CAV-160D). (A152 SERIES AIRPLANES STARTING WITH MODEL150F (S/N 15061533) AND SUBSEQUENT).
SA1235SO identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.
Applicability
Aircraft named in FAA DRS
Named aircraft: Cessna Aircraft 152, Cessna Aircraft A152, and Cessna Aircraft 150 Series, and 1 more aircraft configuration. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Cessna Aircraft 152 and Cessna Aircraft A152, and 2 more aircraft configurations model, serial range, and configuration?
- 02Which tanks, plumbing, usable-fuel assumptions, and inspections apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related fuel systems STCs
Increase in aircraft operating weights (Maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs.) (DC-8-51 s/n 45410 only).
FAA holder: Aircraft Modification Design Services
Increase in aircraft operating weights(maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs. (DC-8-51 s/n 45935 only).
FAA holder: Aircraft Modification Design Services
Increase in aircraft operating weights(max takeoff weight - 328,000 lbs., max landing weight - 258,000 lbs., max zero fuel weiht - 245,000 lbs.) (DC-8-71 SN 46099 only).
FAA holder: Aircraft Modification Design Services
Increase in aircraft operating weights(maximum landing weight - 240,000 lbs., maximum zero fuel weight - 224,000 lbs.) (DC-8F-54 S/N 45637).
FAA holder: Aircraft Modification Design Services