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Other aircraft modifications

STC SA1154CE

FAA DRS lists SA1154CE as Current · Reissued, held by Staggerwing Museum Foundation Inc., for Raytheon Aircraft E18S, Raytheon Aircraft C-45G, and Raytheon Aircraft RC-45J (SNB-5P), and 14 more aircraft configurations. Recorded change: Install crack detection system. Snapshot dated June 30, 2026.

FAA-listed holder
Staggerwing Museum Foundation Inc.
Aircraft configurations
17
FAA revision date
FAA status
Current · Reissued

Recorded modification

What the FAA record covers

SA1154CE 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: Raytheon Aircraft E18S, Raytheon Aircraft C-45G, and Raytheon Aircraft RC-45J (SNB-5P), and 14 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Raytheon Aircraft E18SA-765Raytheon Aircraft C-45GA-765Raytheon Aircraft RC-45J (SNB-5P)A-765Raytheon Aircraft 3TMA-765Raytheon Aircraft 3NMA-765Raytheon Aircraft 3NA-765Raytheon Aircraft JRB-6A-765Raytheon Aircraft UC-45J (SNB-5)A-765Raytheon Aircraft TC-45JA-765Raytheon Aircraft TC-45HA-765Raytheon Aircraft TC-45GA-765Raytheon Aircraft H18A-765Raytheon Aircraft G18SA-765Raytheon Aircraft E18S-9700A-765Raytheon Aircraft D18SA-765Raytheon Aircraft C-45HA-765Raytheon Aircraft D18CA-765

Buyer checks

Confirm before sourcing

Related other aircraft modifications STCs

ST01822AT-DOther aircraft modifications

Installation of an APU Fire Bottle in accordance with Gulfstream Aerospace Corporation Index List GC514428001 Rev L, dated July 31, 2011 or later FAA approved revision. FAA accepted Airplane Flight Manual Supplement, GC51442M001, dated April 8, 1999 or later FAA approved revision is required for fully operational configurations (non-spare). For the model GV, Instructions for Continued Airworthiness, GC51442A001, Revision C, dated September 28, 2010 or later FAA accepted revision is required, and must be made available to the operator at the time of installation. For the model GV-SP, Instructions for Continued Airworthiness, CE52442A000, Revision A, dated October 04, 2010 or later FAA accepted revision is required, and must be made available to the operator at the time of installation.

FAA holder: Gulfstream Aerospace Corporation

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