Supplemental type certificates
49,117 STCs, most recently changed first. Search by what an STC changes, its holder or a model.
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STC SA469NEInstallation of Lycoming turbocharged engine model TIO-540-AA1AD in accordance with Lake Aircraft Drawing List 250T, Revision E or later Federal Aviation Administration (FAA) approved revision.STC SA4NEInstallation of the Hartzell HC-E2YR-1BLF/FL7666A-2 or HC-E2YK-1BL/L7666A-2 Extended Hub Propeller on aircraft equipped with Lycoming IO-360-A1B6 engine in accordance with Aerofab, Inc. Drawing No. 160013L (Rev.E) dated December 23, 1980.STC SA631CEInstall Lycoming IO-360-A1B engine, Hartzell HC-C2YK-1BL/L7666A-2 propeller and remove wing fillets.
Data Required: Lake 4 Sales Engineering Report 62568, Rev. 9/9/68, Drawings L-0254 Rev. 3, E.O. 2-1165A, L-0255, L-2075, L-2076, L-2077, 2-5200 Rev. D, 2-6000 Rev. H, 2-7752, 2-7757 Rev. B, copy of this certificate and AFMS dated March 14, 1969.STC SA745NERemoval of rear bench seat and relocation of middle seats in accordance with Aerofab Inc. Drawing 170046, dated September 29, 1989.STC SA781EAConversion of the Lake LA-4 Amphibian to LA-4 Seaplane. Modifications consist primarily of removing landing gears and covering resultant openings with skin in accordance with Aerofab, Inc. drawing list dated January 30, 1969.STC SA7NEInstallation of the 3-bladed Hartzell HC-C3YR-1 RLF/FL 7663-8R propeller on aircraft equipped with Lycoming IO-360-A1B6 engine and Hartzell hydraulic governor Model F-2 in accordance with Aerofab Inc. Drawing No. 160015, dated March 11, 1974.STC SA822EAEligible for increase in gross weight to 2600 lb. with 200 h.p. engine installed per STC SA631CE.
Aerofab, Inc. Supplement No. 4, approved May 26, 1970, to Lake LA-4 Flight Manual, is required.STC SA855EAInstallation of a cabin air heat exchanger on the following model aircraft:
1. Lake LA-4 in accordance with Drawing No. 170040, Rev. A.
2. Lake LA-4-200 in accordance with Drawing No. 170042, Rev. A.STC SA876EA1. Models LA-4-200, LA-4, LA-4A, LA-4P:
Installation of Auxiliary Fuel System in accordance with Aerofab Drawings No. 180004, Rev. G, dated June 8, 1971,
and 180009, Rev. D, dated February 10, 1971.
2. Model LA-4-200: Increase of Gross Weight to 2690 pounds.
Limitations and Conditions (Continued):
(b) Aerofab Inc. Airplane Flight Manual Supplement:
(i) No. 5, FAA approved June 24, 1971, revised July 18, 1975, for Lake LA-4, LA-4A, LA-4P, LA-4-200 Flight Manual Dated July 11, 1960, revised April 11, 1973, or:
(ii) No. 4, FAA approved December 28, 1973, revised July 18, 1975, for Lake LA-4-200 Flight Manual reissued December 28, 1973.
is required for operations at 2690 lb. Gross Weight.STC SA92NE1. Installation of Symbolic Displays FT-101 fuel flow system in accordance with Lake Aircraft Drawing 100.
2. Installation of Symbolic Displays FT-101 or Alcor Tru-Flo fuel flow system in accordance with lake Drawing No.
100, Revision B or later FAA approved Revision.STC SA969NEInstallation of lighting panel in accordance with Lake Aircraft Drawing No. 4-7359.STC SA970NEInstallation of wing filler for auxiliary fuel tanks, miscellaneous structural modifications and optional radome, dual alternator system, bow compartment covers, upper fin revision, disassembly provisions and dual rudder/aileron electric trim system in accordance with Aerofab, Inc. Drawing List 4-0001, Revision I, dated October 23, 1996, or later FAA-approved revision. The installation is applicable in the following configurations:
United States of America
Department of Transportation - Federal Aviation Administration
Supplemental Type Certificate
(Continuation Sheet)
___________________________________________________________________________________________________________________________________
Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.
___________________________________________________________________________________________________________________________________
FAA Form 8110-2-1(10-69) PAGE 4 of 4 PAGES This certificate may be transferred in accordance with FAR 21.47.
United States of America
Department of Transportation -- Federal Aviation Administration
Supplemental Type Certificate
_____________________________________________________________________________________________________________________________________
Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.
_____________________________________________________________________________________________________________________________________
FAA Form 8110-2(10-68) PAGE 1 of 1 PAGES This certificate may be transferred in accordance with FAR 21.47.
CONFIGURATION 1:
Basic installation with aft seats installed in accordance with Configuration 1 of STC SA469NE. Optional items may be installed in any combination as follows:
Option 1: Radome
In accordance with drawings 150017, 190011, 190018 and 190019.
Mass with an equivalent weight of 35 lbs. may be installed with a center of gravity no farther forward than 6.61 inches aft
of bulkhead 190011-11, as defined in Aerofab, Inc. Engineering Report 4-250-2, dated November 4, 1991, and drawing
190019.
This STC does not approve the installation of a radar, antenna, wave guide or transmitter, nor radar/radome system
compatibility.
Option 2: Dual Alternator System
In accordance with drawings 4-7781 and 4-7782.
Option 3: Bow Compartment Covers
In accordance with drawing 4-3501.
Option 4: Upper Fin Revision
In accordance with drawing 4-2652, Revision C.
Option 5: Disassembly Provisions
In accordance with drawing 300015.
Option 6: Dual Rudder/Aileron Electric Trim System
In accordance with drawing 4-3519 and STC SA1142SO.
CONFIGURATION 2:
Same as Configuration 1 except aft sets installed in accordance with Configuration 2 of STC SA469NE and aft seat weight restriction placard installed in accordance with drawing 4-7003.STC ST00597SE-DInstallation of interior arrangement and In-Flight Entertainment System Provisions. For Boeing model 747-444, serial numbers 28468 and 29119 only.STC ST00600SE-DInstallation of an interior arrangement and In-Flight Entertainment System ProvisionsSTC ST00611SE-DInstallation of interior arrangement and In-Flight Entertainment System ProvisionsSTC ST09091AC-DInstallation of Identification Friend or Foe (IFF) system.STC ST10058SC-DS/N 466 ONLY: Installation of partial cabin seating rearrangement within an executive cabin interior.STC ST116-004NMModification from a passenger to an all-cargo Class E Configuration.STC ST01516LA-DInstallation of 14-passenger cabin interior.STC SB02055CHLimited to installation on serial number 5239 ONLY.STC SB02056CHLimited to installation on serial number 5180 ONLY.STC ST02000NYInstallation of a VIP executive interior.STC SA10285SCInstallation of a Chelton Aviation Corp (CAC) AP-3C autopilot.STC SA10286SCInstallation of a Chelton Aviation Corp (CAC) AP-3C autopilot.STC SA1636WEInstallation of AiResearch TPE 331 series engine, tricycle landing gear and ventral fin, extension of fuse- lage and related changes.STC SB02042CHLimited to installation on serial number 6002 ONLY.STC SB02043CHLimited to installation on serial number 2344 ONLY.STC SB02054CHLimited to installation on serial number 5243 ONLY.STC SB10283SCLimited to installation on serial number B82012-3.STC SA00556DEInstallation of a left-hand exhaust stack assembly.STC ST01457SEInstallation of the General Dynamics EmPower and EmPort Systems. Concurrent installation of STC ST01942NY issued 8/17/04 for Business Class Seat installation required.STC ST01458SEIncorporation of change in aircraft weight and balance by supplementing the current aircraft weight and balance manual with Newport Aeronautical Development Report No. NAD 2004-101, Revsion A, dated June 16, 2004, or later FAA approved revision.STC ST02040CHInstall 160 passenger capacity seating configurationSTC ST02854AT-DLimited to installation of a custom interior for G-IV, serial number 1523 ONLY.STC SA2248CEInstallation of Continental 0-200-A engine and fixed pitch propellers. Data pertinent to this modification are considered inadequate for duplication in other airplanes. This approval is limited to the installation made in Luscombe Model 8A, Serial Number 4938, only.STC ST01453SEInterior reconfiguration of 777-300 Series airplanes in accordance with JAMCO America, Inc., Master Drawing List IA-115MDL, Revision A, dated September 11, 2004, or later Federal Aviation Administration (FAA) approved revision.STC ST01999NYModification of passenger cabin interior to a 12C/272Y dual class configuration. Limited to installation on Boeing 767-33A, serial number 25403 ONLY.STC ST02818AT-DLimited to installation of a custom interior for GV-SP, serial number 5031 ONLY.STC ST10057SC-DS/N 093 ONLY: Installation of an executive cabin interior.STC SA09635ACInstallation of S-TEC Meggitt Engine Instrument Display System (EIDS) in accordance with Master Data List 921230, Revision 7, dated September 17, 2004, or later FAA approved revision for Cessna 425. FAA approved Airplane Flight Manual Supplement No. 892137, dated September 20, 2004, or later FAA approved revision is required for Cessna 425 with S-TEC Meggitt EIDS.STC SA09636ACInstallation of S-TEC 01304 Digital Flight Control System (DFCS), Three Axis Automatic Flight Guidance System Part No. 01304-04-01-007, in accordance with Master Data List 921231, Revision 5, dated 9-14-2004, or later FAA approved revision for Cessna 425. FAA approved Airplane Flight Manual Supplement No. 892135, dated 9-20-2004, or later FAA approved revision is required for Cessna 425 with S-TEC 01304 DFCS.STC SA09637ACInstallation of single S-TEC Meggitt Electronic Flight Instrument System (EFIS) in accordance with Master Data List 921229-02, Revision 5; or dual S-TEC Meggitt EFIS in accordance with Master Data List 921229-03, Revision 6, both dated 9-15-2004, or later FAA approved revision for Cessna 425. FAA approved Airplane Flight Manual Supplement No. 892136, dated 9-20-2004, or later FAA approved revision is required for Cessna 425 with single or dual S-TEC Meggitt EFIS.STC SA2923SOInstallation of a Collins data link system.STC ST01270WIRunway Awareness and Advisory System (RAAS) on aircraft with Honeywell MK V and MK VII EGPWS Systems.STC ST02037CHInstallation of Michelin main landing gear tires.STC ST01444SEInstallation of B/E Aerospace Sweep-On Fullface Crew Oxygen Mask System on the flight deckSTC SR01107NYInstallation of High Visibility Composite main and aft cabin doors.STC ST02903AT-DInterior ReconfigurationSTC ST09712SC-DLimited to approval on serial number 336 ONLY.STC SR00579NYInstallation of Engine Compartment Forward Firewall Reinforcement.