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Data Updated Each Federal Working Day At Midnight

N4476F has Assigned/Multiple Records

N-Number Entered: 4476f Aircraft Description
Serial Number SH3731 Status Valid
Manufacturer Name SHORT BROS Certificate Issue Date 06/03/2009
Model SHORTS SD3-60 Expiration Date 07/31/2027
Type Aircraft Fixed Wing Multi-Engine Type Engine Turbo-prop
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 51263716
MFR Year 1987 Mode S Code (Base 16 / Hex) A567CE
Type Registration Corporation Fractional Owner NO
Registered Owner
Name TRANS EXECUTIVE AIRLINES OF HAWAII INC
Street PO BOX 29239
City HONOLULU State HAWAII
County HONOLULU Zip Code 96820-1639
Country UNITED STATES
Airworthiness INFORMATION PROVIDED HERE SHOULD NOT BE USED TO DETERMINE THE AIRWORTHINESS OF AN AIRCRAFT.
Refer to 14 CFR Parts 39, 43, 91, and FAA Order 8130.2 for airworthiness regulations and guidance.
Type Certificate Data Sheet None Type Certificate Holder None
Engine Manufacturer P&W Classification Standard
Engine Model PT6A SERIES Category Transport
A/W Date 09/08/2011 Exception Code No
The information contained in this record should be the most current Airworthiness information available in the historical aircraft record. However, this data alone does not provide the basis for a determination regarding the
airworthiness of an aircraft or the current aircraft configuration. For specific information, you may request a copy of the aircraft record at https://aircraft.faa.gov/e.gov/ND/
Other Owner Names
None
Temporary Certificates
Certificate Number T092780 Issue Date 06/03/2009 Expiration Date 07/03/2009
Fuel Modifications
Mod Code 28 Mod Date 20030626
INSTALLED 360 GALLON LONG RANGE FUEL TANK SYSTEM (ACFT MANUFACTURER SHORT BROTHERS MODIFICATION 7132, WITH ACFT MANUFACTURER SHORT BROS TANK P/N SD3-57-0400/SC7-57-0243), IN ACCORDANCE WITH FAA APPROVED (TCDS A41EU, SERVICE INFORMATION) AIRCRAFT MANUFACTURER SHORT BROS PLCDRAWINGS SD3-57-0400XD, >>SD3-57-0401XA, >>SD3-57-0402XA, >> SD3-57- 2422XA, >>SD3-57-6150XA, >> SD3-57-6013XJ, >> SD3-57-6152XA, >> SD3-81-1145XA, >> SD3-31-149XB, & SD3-81-6919 AND TESTED SYSTEM PER INST. CALCULATED WEIGHT AND BALANCE WITH LONG RANGE FUEL TANK AND INSTALLED EQUIPMENT, AND FOUND AIRCRAFT TO BE WITHIN THE MAXIMUM TAKEOFF WEIGHT LIMIT.
Mod Code 28 Mod Date 20090602
TEMPORARY FERRY FUEL SYSTEM INSTALLED IN PASSENGER CABIN AREA, CONSIS-TING OF 6 ALUMINUM TANKS. EACH OF THE SIX TANKS IS 210 GALLONS AND THE TANKS ARE POSITIONED AT STATION 220, 244, 268, 316 AND 340 INCHES.TANKS ARE RECTANGULAR IN SHAPE AND DESIGNED AND CONSTRUCTED FROM 5052 ALUMINUM .100 INCHES THICK IAW ABYC H-24.18.1 TANK MATERIALS. TANKS ARE DESIGNED AND WELDED TO MEET THE REQUIREMENTS OF FAR 23.963(1). TANKS ARE INTERNALLY BAFFLED, PRESSURE AND LEAK CHECKED IAW FAR 23.965(A)(1). RUBBER 3 INCH SAFETY CAPS INSTALLED. TANKS ARE VENTED TO POSITIVE EXTERNAL AIR BY A FORWARD FACING VENT LINE IN THE CABIN AIR SCOOP. FERRY FUEL TANKS ARE MOUNTED ON THE CARGO FLOOR ADN SECURED BY SIX 5000 POUND ADJUSTABLE CARGO STRAPS MOUNTED TO 12 DOUBLERING BROWNLINE CARGO RINGS INSTALLED TO EXISTING BROWNLINE SEAT/CARGO RAILS. ALL GROUPS OF TANKS ARE GROUNDED TO THE AIRCRAFT STRUCTURE. EACH FERRY FUEL TANK FEED FITTING TO SEPARATE ON/OFF FUEL SELECTOR VALVE. FROM THE VALVES THE LINES RUN TO TWO GATE VALVES ALLOWING SELECTION OF ELECTRIC TRANSFER PUMP ONE OR TWO. THE SHORTS COLLECTOR TANKS WITH INTERNAL FUEL PUMPS ARE MOUNTED ON A PLYWOOD PALLET AND SECURED TO THE FLOOR STRUCTURE USING EXISTING FLOOR ATTACH SCREWS. A/C ELECTRICAL POWER FOR THE PUMPS IS SUPPLIED VIA 2 INVERTERS WHICH IN TURN ARE POWERED VIA 2 OFF AND ON SWITCHES TO 25 AMP, 28 VOLTS C/B OF THE LANDING LIGHT CIRCUIT. THE FERRY PUMPS FEED DIRECTLY TO THE AIRCRAFT FORWARD COLLECTOR TANKS AND BOTH ENGINES CAN BE RUN VIA IN CROSSFEED MODE ON THE FRONT TANK. SYSTEM SHALL BE CHECKED FOR OPERATION AND LEAKS AND SHALL BE INSPECTED AS PART OF THE PREFLIGHT INSPECTION AT EACH REFUELING STOP FOR LEAKS AND TIGHTNESS. INSTALLA-
Deregistered Aircraft
Deregistered Aircraft 1 of 1
Aircraft Description
Serial Number 28R-7635410 Certificate Issue Date 10/15/1976
Manufacturer Name PIPER Mode S Code (base 8 / oct) 51263716
Model PA-28R-200 Mode S Code (base 16 / hex) A567CE
Year Manufacturer 1976 Cancel Date 10/15/1976
Reason For Cancellation Exported Export To NEW ZEALAND
Type Registration Corporation
Aircraft Registration Prior to Deregistration
Name GLOBE AERO LTD INC
Street PO BOX 5775
City LAKELAND
State FLORIDA Zip Code 33803
County POLK
Country UNITED STATES
Deregistered Airworthiness
Engine Manufacturer None Classification Unknown
Engine Model None Category None
A/W Date None Exception Code No
Deregistered Other Owner Names
None
The duration of aircraft registration certificates has been extended up to 7 years. The Registry will be issuing revised certificates in batches based on the former expiration date. For verification purposes, even though the expiration date on the registration certificate may not match the expiration date in the FAA Aircraft Registration database, any registration certificate displaying an expiration date of January 31, 2023 or later is still valid. This applies to all foreign Civil Aviation Authorities or anyone else with a verification need.

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