Structural Integrity Engineering
Named as the FAA publishes it on its approvals.
Holds 23 approved modifications, most of them for the Boeing 727. FAA spelling: Structural Integrity Engineering.
Approved modifications 23 · newest first
2022-09-30ST02793LA · Modification of Boeing 747-400F Airplane Weight and Balance Manual to allow transportation of the Virgin
Orbit... · 747-400F Series
2017-08-25ST00939AT · Approval of increased operating weights as substantiated by the design data listed in SIE Master Report List SIE... · 727-200 Series
2007-03-28ST00925AT · Approval of increased operating weights as substantiated by the design data listed in Structural Integrity... · 727-200 Series
2006-01-31ST01861LA · Modifications to the 9-G rigid barrier, cargo door surround structure and other attendant modifications. · DC-8-63, DC-8-73
2005-01-20ST01043AT · Approval of increased operating weights. · 727-200 Series
2005-01-20ST00795AT · Approval of maximum zero fuel weight increase (155,000 lbs.) and maximum landing weight increase(164,000 lbs.). Data... · 727-200 Series
2004-05-11ST00770LA · Increased aircraft main deck cargo floor capacity between Fuselage Stations 740 to 950. · 727-200 Series
2003-12-29ST00779LA · Installation of side vertical restraints in accordance with approved Master Drawing List SIE 37-703, Revision A,... · 727-200 Series, 727-100 Series
2003-12-29ST01181LA · Installation of modifications to the 9-G rigid barrier, cargo door surround structure and other attendant modifications. · DC-8-55, DC-8-61, DC-8-62
2003-12-29ST00926AT · Approval of increased operating weights as substantiated by the design data listed in SIE No. SIE-28-713. (727-200... · 727
2003-12-29SA00364LA · Retirement life extension of de Havilland DHC-6-300 wing in accordance with FAA approved Structural Integrity... · DHC-6-300
2003-12-29ST00671AT · Approval of maximum landing weight increase from 160,000 pounds to 164,000 pounds. (727-200 SERIES S/N 21930 AND 21931 ONLY) · 727-200 Series
2003-12-29SA6073NM · Installation of fatigue sensor and structural life extension of wing spar in accordance with FAA approved SIE Master... · 99, 99A, A99A
2003-12-29ST00782AT · Approval of maximum zero fuel weight increase to 132,000 pounds. (727-100 SERIES S/N 19183 ONLY) · 727-100 Series
2003-12-29ST00901AT · Approval of increased operating weights as substantiated by the design data listed in SIE-28-902. (727-200 S/N... · 727-200 Series
2003-12-29ST00778LA · Installation of splitter locks and floor modifications to increase the main deck cargo floor capacity. · 727-200 Series, 727-100 Series
2003-12-29ST00720AT · Approval of maximum zero fuel weight and maximum landing weight (Flaps 30) increases to 157,500 pounds and 166,000... · 727-200 Series
2003-12-29ST00949AT · Approval of increased operating weights as substantiated by the design data listed in SIE Master Report List... · 727-200 Series
2003-12-29ST00633AT · Approval of maximum zero fuel weight increase from 138,000 pounds to 146,000 pounds. (727-200 SERIES S/N 19483,... · 727-200 Series
2003-12-29SA5510NM · Modification in accordance with FAA approved SIE Drawing List 9000 N/C,, dated August 7, 1991, or later FAA approved... · DC-8-61
2003-12-29ST01013AT · Approval of increased operating weights. Limited to installation on serial numbers 21327, 21328, 21329, 21330, and... · 727-200 Series
2003-12-29ST00719AT · Approval of increased operating weights as substantiated by the design data listed in Structural Integrity... · 727-200 Series
1998-02-25ST001043AT · Approval of increased operating weights as substantiated by the design data listed in SIE Master Report List No.... · 727-200 Series
Source: FAA Dynamic Regulatory System (type certificate data sheets, supplemental type certificates, parts manufacturer approvals, technical standard order authorisations). An organisation's name is as the FAA spelled it on each record; related spellings are separate pages.