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Aircraft performance

STC SA1660GL

FAA DRS lists SA1660GL as Current · Surrendered, held by ABX Air Incorporated, for McDonnell Douglas DC-9-11, McDonnell Douglas DC-9-12, and McDonnell Douglas DC-9-13, and 8 more aircraft configurations. Recorded change: Installation of dual Kollsman575-35900-A1778 mach/airspeed indicator. Snapshot dated June 30, 2026.

FAA-listed holder
ABX Air Incorporated
Aircraft configurations
11
FAA revision date
FAA status
Current · Surrendered

Recorded modification

What the FAA record covers

SA1660GL 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 DC-9-11, McDonnell Douglas DC-9-12, and McDonnell Douglas DC-9-13, and 8 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

McDonnell Douglas DC-9-11A6WEMcDonnell Douglas DC-9-12A6WEMcDonnell Douglas DC-9-13A6WEMcDonnell Douglas DC-9-14A6WEMcDonnell Douglas DC-9-51A6WEMcDonnell Douglas DC-9-15A6WEMcDonnell Douglas DC-9-31A6WEMcDonnell Douglas DC-9-32FA6WEMcDonnell Douglas DC-9-41A6WEMcDonnell Douglas DC-9-33FA6WEMcDonnell Douglas DC-9-32A6WE

Buyer checks

Confirm before sourcing

Related aircraft performance STCs

ST00719ATAircraft performance

Approval of increased operating weights as substantiated by the design data listed in Structural Integrity Engineering (SIE) Master Report List or Master Document List No. SIE-28-703, no revision, dated February 24, 1995, or later FAA approved revision. Aircraft with Increase of Maximum Takeoff or Landing Weight must also be modified in accordance with: Drawing SIE-28-901 (taxi weight up to 183,000 lb, landing weight to 164,000 lb), 28-904 (taxi weight up to 178, 500 lbs, landing weight to 164,000 lbs), 28-905 (taxi weight up to 191,000 lb, landing weight to 164,000 lbs), Rev NC or later FAA approved revisions.

FAA holder: Structural Integrity Engineering

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ST00779LAAircraft performance

Installation of side vertical restraints in accordance with approved Master Drawing List SIE 37-703, Revision A, dated May 25, 1999, or later FAA approved revisions. Structural Integrity Engineering FAA Approved Airplane Flight Manual Supplement, SIE 37-607 dated May 26, 1999, or later FAA approved revisions and Weight and Balance Supplement, SIE 37-608, dated February 9, 1999, or later FAA approved revisions, are required as part of this modification.

FAA holder: Structural Integrity Engineering

View record