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Other aircraft modifications

STC ST01474CH

FAA DRS lists ST01474CH as Current · Issued, held by Rosemount Aerospace Inc, for McDonnell Douglas MD-11 and McDonnell Douglas MD-11F. Recorded change: Installation of Rosemount Aerospace model 1833D pressure transducers. Snapshot dated June 30, 2026.

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FAA-listed holder
Rosemount Aerospace Inc
Aircraft configurations
2
FAA revision date
FAA status
Current · Issued

Recorded modification

What the FAA record covers

ST01474CH 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: McDonnell Douglas MD-11 and McDonnell Douglas MD-11F. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

McDonnell Douglas MD-11A22WEMcDonnell Douglas MD-11FA22WE

Related other aircraft modifications STCs

SE02881ATOther aircraft modifications

STC for the conversion of Teledyne Continental Motors (TCM) Models IO-520-B, -BA or -BB to AvPower Model IO-550-B-AP which has the same ratings and limitations as TCM Model IO-550-B, or the conversion of TCM Model IO-520-C or -CB to AvPower Model IO-550-C-AP which has the same ratings and limitations as TCM Model IO-550-C. Conversion of the Models IO-520-B, -BA, or -BB to the Model IO-550-B-AP shall be performed in accordance with AvPower Report AP1004-3 Master Parts List, Revision B dated March 26, 2004 and AvPower Report AP1004-6 Assembly Instructions, Revision B dated March 26, 2004, or later FAA approved revisions. Conversion of the Models IO-520-C or -CB to the Model IO-550-C-AP shall be performed in accordance with AvPower Report AP1004-4 Master Parts List, Revision B dated March 26, 2004 and AvPower Report AP1004-7 Assembly Instructions, Revision B dated March 26, 2004, or later FAA approved revisions.

FAA holder: AERO Aviation Company

View record

FAA record reference

STC number
ST01474CH
Product
Aircraft · Large Multi-Engine
Country
United States
Application date
Not listed
Revision date
June 7, 2001
CFR references
Part 21