DOT logo United States Department of Transportation
Aircraft Inquiry

FAA REGISTRY

N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N96Y has Assigned/Multiple Records

N-Number Entered: 96y Aircraft Description
Serial Number LU-8 Status Valid
Manufacturer Name BEECH Certificate Issue Date 03/12/1999
Model 65-A90-4 Expiration Date 11/30/2029
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) 53255763
MFR Year 1970 Mode S Code (Base 16 / Hex) AD5BF3
Type Registration Corporation Fractional Owner NO
Registered Owner
Name DYNAMIC AVLEASE INC
Street PO BOX 7
City BRIDGEWATER State VIRGINIA
County ROCKINGHAM Zip Code 22812-0007
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 CANADA Classification Restricted
Engine Model PT6A-28 Category Forest, Aerial Surveying, Agriculture and Pest Control
A/W Date 07/31/2024 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
None
Fuel Modifications
Mod Code 28 Mod Date 20180116
INTALLATION OF TEMPORARY FERRY FUEL SYSTEM IS A DUPLICATE OF AN APPROVED INTALLATION DONE IN THE SAME MODEL AIRCRAFT (N87E, LM-05) ON DRAWING JRG09-31-0210 ON 8110-3 DATED 2/10/2009. THE ONLY DIFFERENCE IS THAT THE FERRY TANK SYSTEM WILL USE THE EXISTING BEECHCRAFT FACTORYINSTALLED FERRY FUEL LINE PLUMBING THAT GOES FROM THE FERRY TANK TO THE WING TANKS. THE INSTALLATION USES A 529 GALLON RUBBER BLADDER FERRY FUEL TANK MANUFACTURED BY TURTLE-PAC, DESIGNED SPECIFCALLY FOR FERRYING AIRCRAFT. THE TANK IS LOCATED IMMEDIATELY BEHIND THE PILOT SEAT, ON TOP OF 3/8 INCH PLYWOOD BASE AND AN ALUMINUM SECONDARY CON TAINMENT TRAY WITH AN OVERBOARD DRAIN. TANK IS SECURED WITH A TOTAL OF8 CARGO TIE DOWN STRAPS (RATED AT 5,000 LBS EASH) TO MEET FORWARD ITEMOF MASS REQUIREMENTS OF PART 43, AS REQUIRED IN FAR91.203. STRAPS ATTACH TO A TOTAL OF 8 DOUBLE STUD TYPE (RATED AT 8,000 LBS EACH) TIE DOWN RINGS ON TO THE AIRCRFT'S EXISTING BROWNLINE SEAT TRACK RAILS. FUEL IS ROUTED FORM THE BLADDER FERRY TANK OUTLET VIA 1/2 INCH FLEXIBLE FUEL COMPATIBLE TYGON TUBING TO A FERRY FUEL PUMP BOX. THIS BOX CONTAINS 2 ELECTRIC PUMPS WIRED (P/N M22759/16-12) TO THE MAIN CIRCUIT BREAKER PANEL ON THE CO-PILOTS SIDE AND PROTECTED WITH A 15AMPCIRCUIT BREAKER (P/N 7274-2-15). THE FERRY PUMP BOX ALSO HAS A MANUAL BACKUP "WOBBLE" PUMP TO USE IN CASE OF AN ELECTRICAL SYSTEM FAILURE. FUEL FROM THE FERRY FUEL PUMP BOX IS THEN ROUTED THROUGH 2 ISOLATION VALVES (FOR LEFT & RIGHT WINGS) FLOW THROUGH STATOFLEX 303-8 FUEL COMPATIBLE HOSES TO 8 ALUMINUM BULKHEAD FITTINGS MOUNTED ON THE FLOOR PANEL FORWARD OF FS 147.6 (JUST BEHIND PILOT SEATS) ON THE LEFT AND RIGHT SIDES. FROM THERE, FUEL IS THEN ROUTED VIA EXISTING FACTORY
Mod Code 28 Mod Date 20180508
INTALLATION OF TEMPORARY FERRY FUEL SYSTEM IS A DUPLICATE OF AN APPROVED INTALLATION DONE IN THE SAME MODEL AIRCRAFT (N87E, LM-05) ON DRAWING JRG09-31-0210 ON 8110-3 DATED 2/10/2009. THE ONLY DIFFERENCE IS THAT THE FERRY TANK SYSTEM WILL USE THE EXISTING BEECHCRAFT FACTORYINSTALLED FERRY FUEL LINE PLUMBING THAT GOES FROM THE FERRY TANK TO THE WING TANKS. THE INSTALLATION USES A 529 GALLON RUBBER BLADDER FERRY FUEL TANK MANUFACTURED BY TURTLE-PAC, DESIGNED SPECIFCALLY FOR FERRYING AIRCRAFT. THE TANK IS LOCATED IMMEDIATELY BEHIND THE PILOT SEAT, ON TOP OF 3/8 INCH PLYWOOD BASE AND AN ALUMINUM SECONDARY CON TAINMENT TRAY WITH AN OVERBOARD DRAIN. TANK IS SECURED WITH A TOTAL OF8 CARGO TIE DOWN STRAPS (RATED AT 5,000 LBS EASH) TO MEET FORWARD ITEMOF MASS REQUIREMENTS OF PART 43, AS REQUIRED IN FAR91.203. STRAPS ATTACH TO A TOTAL OF 8 DOUBLE STUD TYPE (RATED AT 8,000 LBS EACH) TIE DOWN RINGS ON TO THE AIRCRFT'S EXISTING BROWNLINE SEAT TRACK RAILS. FUEL IS ROUTED FORM THE BLADDER FERRY TANK OUTLET VIA 1/2 INCH FLEXIBLE FUEL COMPATIBLE TYGON TUBING TO A FERRY FUEL PUMP BOX. THIS BOX CONTAINS 2 ELECTRIC PUMPS WIRED (P/N M22759/16-12) TO THE MAIN CIRCUIT BREAKER PANEL ON THE CO-PILOTS SIDE AND PROTECTED WITH A 15AMPCIRCUIT BREAKER (P/N 7274-2-15). THE FERRY PUMP BOX ALSO HAS A MANUAL BACKUP "WOBBLE" PUMP TO USE IN CASE OF AN ELECTRICAL SYSTEM FAILURE. FUEL FROM THE FERRY FUEL PUMP BOX IS THEN ROUTED THROUGH 2 ISOLATION VALVES (FOR LEFT & RIGHT WINGS) FLOW THROUGH STATOFLEX 303-8 FUEL COMPATIBLE HOSES TO 8 ALUMINUM BULKHEAD FITTINGS MOUNTED ON THE FLOOR PANEL FORWARD OF FS 147.6 (JUST BEHIND PILOT SEATS) ON THE LEFT AND RIGHT SIDES. FROM THERE, FUEL IS THEN ROUTED VIA EXISTING FACTORY
Mod Code 28 Mod Date 20150518
INTALLATION OF TEMPORARY FERRY FUEL SYSTEM IS A DUPLICATE OF AN APPROVED INTALLATION DONE IN THE SAME MODEL AIRCRAFT (N87E, LM-05) ON DRAWING JRG09-31-0210 ON 8110-3 DATED 2/10/2009. THE ONLY DIFFERENCE IS THAT THE FERRY TANK SYSTEM WILL USE THE EXISTING BEECHCRAFT FACTORYINSTALLED FERRY FUEL LINE PLUMBING THAT GOES FROM THE FERRY TANK TO THE WING TANKS. THE INSTALLATION USES A 529 GALLON RUBBER BLADDER FERRY FUEL TANK MANUFACTURED BY TURTLE-PAC, DESIGNED SPECIFCALLY FOR FERRYING AIRCRAFT. THE TANK IS LOCATED IMMEDIATELY BEHIND THE PILOT SEAT, ON TOP OF 3/8 INCH PLYWOOD BASE AND AN ALUMINUM SECONDARY CON TAINMENT TRAY WITH AN OVERBOARD DRAIN. TANK IS SECURED WITH A TOTAL OF8 CARGO TIE DOWN STRAPS (RATED AT 5,000 LBS EASH) TO MEET FORWARD ITEMOF MASS REQUIREMENTS OF PART 43, AS REQUIRED IN FAR91.203. STRAPS ATTACH TO A TOTAL OF 8 DOUBLE STUD TYPE (RATED AT 8,000 LBS EACH) TIE DOWN RINGS ON TO THE AIRCRFT'S EXISTING BROWNLINE SEAT TRACK RAILS. FUEL IS ROUTED FORM THE BLADDER FERRY TANK OUTLET VIA 1/2 INCH FLEXIBLE FUEL COMPATIBLE TYGON TUBING TO A FERRY FUEL PUMP BOX. THIS BOX CONTAINS 2 ELECTRIC PUMPS WIRED (P/N M22759/16-12) TO THE MAIN CIRCUIT BREAKER PANEL ON THE CO-PILOTS SIDE AND PROTECTED WITH A 15AMPCIRCUIT BREAKER (P/N 7274-2-15). THE FERRY PUMP BOX ALSO HAS A MANUAL BACKUP "WOBBLE" PUMP TO USE IN CASE OF AN ELECTRICAL SYSTEM FAILURE. FUEL FROM THE FERRY FUEL PUMP BOX IS THEN ROUTED THROUGH 2 ISOLATION VALVES (FOR LEFT & RIGHT WINGS) FLOW THROUGH STATOFLEX 303-8 FUEL COMPATIBLE HOSES TO 8 ALUMINUM BULKHEAD FITTINGS MOUNTED ON THE FLOOR PANEL FORWARD OF FS 147.6 (JUST BEHIND PILOT SEATS) ON THE LEFT AND RIGHT SIDES. FROM THERE, FUEL IS THEN ROUTED VIA EXISTING FACTORY
Deregistered Aircraft
Deregistered Aircraft 1 of 2
Aircraft Description
Serial Number 16 Certificate Issue Date 07/30/1991
Manufacturer Name ESSLSTYN Mode S Code (base 8 / oct) 53255763
Model BRYAN AIRCRAFT RS-15 Mode S Code (base 16 / hex) AD5BF3
Year Manufacturer None Cancel Date 02/02/2001
Reason For Cancellation Destroyed Export To None
Type Registration Corporation
Aircraft Registration Prior to Deregistration
Name TRIAD GROUP OF SILENT KNIGHTS INC
Street C/O A EPSTEIN 3517 OAKLAND ST
City AMES
State IOWA Zip Code 50010
County STORY
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
Deregistered Aircraft 2 of 2
Aircraft Description
Serial Number 1 Certificate Issue Date 06/05/1961
Manufacturer Name FAUR HELICOPTER Mode S Code (base 8 / oct) 53255763
Model FAUR-HF1 Mode S Code (base 16 / hex) AD5BF3
Year Manufacturer None Cancel Date 07/23/1965
Reason For Cancellation Cancelled Export To None
Type Registration Individual
Aircraft Registration Prior to Deregistration
Name FAUR IRVIN H
Street BOX 236
City PRINCETON
State IOWA Zip Code 52768
County SCOTT
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.

You are accessing a U.S. Government authorized information system, which includes (1) this computer, (2) this computer network, (3) all computers connected to this network, (4) all devices and storage media attached to this network or to a computer on this network, and (5) all cloud services and hosting environments supporting this information system. This information system is provided for U.S. Government-authorized use only.

Unauthorized or improper use of this system may result in disciplinary action, as well as civil and criminal penalties.

By logging in and using this information system, you understand and consent to the following:

  • You have no reasonable expectation of privacy regarding communications or data transiting or stored on this information system.
  • At any time, and for any lawful Government purpose, communication between the user and this information system, data transiting to/from the system, or stored on this system is subject to monitoring, interception, and search.
  • Any communications or data transiting or stored on this information system may be disclosed or used for any lawful Government purpose.


D O T Triskelion

U.S. Department of Transportation

Federal Aviation Administration

800 Independence Avenue, SW

Washington, DC 20591

(866) TELL-FAA | (866) 835-5322