FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 0041FF | Status | Valid |
| Manufacturer Name | HUGHES HELICOPTERS INC | Certificate Issue Date | 12/26/2024 |
| Model | 369FF | Expiration Date | 12/31/2031 |
| Type Aircraft | Rotorcraft | Type Engine | Turbo-shaft |
| Pending Number Change | None | Dealer | No |
| Date Change Authorized | None | Mode S Code (base 8 / Oct) | 51530246 |
| MFR Year | None | Mode S Code (Base 16 / Hex) | A6B0A6 |
| Type Registration | Corporation | Fractional Owner | NO |
| Name | FLIGHT TRAILS HELICOPTERS INC | ||
| Street | 4610 E FIGHTER ACES DR | ||
| City | MESA | State | ARIZONA |
| County | MARICOPA | Zip Code | 85215-2502 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | H3WE | Type Certificate Holder | MD HELICOPTERS INC (MDHI) |
| Engine Manufacturer | ALLISON | Classification | Restricted |
| Engine Model | 250-C30 SER | Category | Agriculture and Pest Control |
| A/W Date | 05/05/2005 | Exception Code | No |
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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/ |
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| None |
| Certificate Number | T243168 | Issue Date | 12/26/2024 | Expiration Date | 01/25/2025 |
| Mod Code | 28 | Mod Date | 19930115 |
| MODIFIED FARGO FUEL TANK (PREVIOUSLY APPROVED BY STC 656GL) BY INSTAL-LING A FLOAT SWITCH P/N L15H-8 IN THE LOWER RIGHT HAND CORNER OF FUEL TANK. THE FUNCTION OF THE FLOAT SWITCH IS TO OPERATE THE ANNUNICATOR LIGHT OF THE CONTROL PANEL. ALSO INSTALLED A FAUCET FUEL PUMP P/N 40154 W4V 30 6PH WITH INTERNAL CHECK VALVE IN THE DISCHARGE LINE OF THE FARGO FUEL TANK TO INSURE COMPLETE FUEL TRANSFER FROM THE TANK IN FLIGHT. THIS FUEL PUMP IS TEE'D INTO A COMMON MANIFOLD AND THEN ROUTED TO THE EXISTING AUX FUEL SHUTOFF VALVE AND TO THE MAIN FUEL TANK. MOUNTED FAUCET FUEL PUMP AND MANIFOLD ON .050 2024T3 DOUBLER RIVETTED TO STATON 124.0 BULKHEAD. INSTALLATION OF DOUBLER AS PER AC 43.13IA SECTION 3. RIGID FUEL LINES ARE ROUTED AND SECURED IN RIGHT HAND ENGINE COMPARTMENT TO CLEAR ALL MOVEABLE LINKAGE & LANDING GEAR SUPPORTS. ALL RIGID FUEL LINES ARE MADE FROM 5052-0 3/8" ALUMI- NUM TUBING WITH AN HARDWARE. TWO FLEXIBLE FUEL LINES MADE FROM STRATOFLEX 111-6 HOSE AND AN FITTINGS COVERED WITH FIRESLEEVING ARE INSTALLED FROM FUEL MANIFOLD TO AN 832-6D BULKHEAD FITTINGS ON BELLY OF THE HELICOPTER. THIS CONNECTION IS CAPPED OFF UNLESS EXTERNAL AUX-ILIARY FUEL TANKS ARE INSTALLED. THESE TWO FLEXIBLE LINES AND CONNEC-TIONS ARE FOR THE INSTALALTION OF AUXILIARY TANKS ONLY. INSTALLED A FABRICATED CONTROL PANEL ON TOP OF EXISTING INSTRUMENT PANEL & SECUREDCONTROL PANEL BY TWO AN 10-32 MACHINE SCREWS. THSI CONTROL PANEL HOUSES THREE YELLOW LIGHTS P/N 616-0599 (TO INDICATE PUMPS ARE ON) THREE WHITE LIGHTS P/N 616-0599 (TO INDICATE TANKS ARE EMPTY) THREE 5 AMP CIRCUIT BREAKERS P/N W32X2M1G5 (FOR FUEL PUMPS) AND 1 PRESS TO TEST SWITCH P/N 757-0781. THE CONTROL PANEL & ALL FUEL TANK WIRING IS | |||
| None |
