FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 40.690 | Status | Valid |
| Manufacturer Name | DIAMOND AIRCRAFT IND INC | Certificate Issue Date | 11/05/2013 |
| Model | DA 40 | Expiration Date | 11/30/2029 |
| Type Aircraft | Fixed Wing Single-Engine | Type Engine | Reciprocating |
| Pending Number Change | None | Dealer | No |
| Date Change Authorized | None | Mode S Code (base 8 / Oct) | 52230250 |
| MFR Year | 2006 | Mode S Code (Base 16 / Hex) | A930A8 |
| Type Registration | Corporation | Fractional Owner | NO |
| Name | GEORGE'S AVIATION SERVICES INC | ||
| Street | 18 LAGOON DR | ||
| City | HONOLULU | State | HAWAII |
| County | HONOLULU | Zip Code | 96819-1813 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | LYCOMING | Classification | Standard |
| Engine Model | IO-360-M1A+ | Category | Utility, Normal |
| A/W Date | 11/22/2006 | 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 |
| Mod Code | 28 | Mod Date | 20070807 |
| A TEMP FERRY FUEL AND OIL SYSTEM HAS BEEN INSTALLED. THE TEMP FERRY FUEL SYSTEM CONSISTS OF TWO ALUMINUM FERRY FEL TANKS MOUNTED IN THE CABIN. ONE 45-GAL TANK AT STATION 87 AND ONE 75-GAL TANK AT STATION 124. THE TOTAL CABIN FUEL CAPACITY IS 120-GALLONS. THE RIGHT HAND COPILOTS SEAT IS REMOVED, IAW PROCEDURES IN THE DIAMOND DA40 MAINTEN. MANUAL. THE REAR SEATS ARE FOLDED TO THE CARGO CONFIG. PLYWOOD PALLETS ARE FITTED ACROSS THE REAR CARGO AREA AND SUPPORTED BY TRUSS STRUCTURE TO THE CABIN FLOOR AREA. THE COPILOTS YOKE IS DISCONNECTED AND SECURED WITH THE AUTOPILOT AND PUSH TO TALK WIRING HARNESS IN TACKTHE COPILOTS CONTROL LINKAGE AND SHROUDED IN AN ALUMINUM HOUSING CLAMPED TO THE ELEVATOR CONTROL ARM TO ALLOW FREEDOM OF MOVEMENT WITHOUT ANY OBSTRUCTION. THE AILERON CONTROL LINKAGE RIDES FREELY IN THE ALUMINUM TUBE. THE TWO TANKS WERE MFRD BY ROYOL INDUSTRIES OF SHINGLE SPRINGS,CA. THE TANKS ARE RECTANGULAR IN DESIGN CONSTRUCTED IAW ABYC H-24.18(2-12) AND 46 CFR SEC 58.50(A) (4-6) FROM 5052 ALUM. .100 INCHES THICK IAW ABYC H-24.18.1 TANK MATERIALS. THE TANKS ARE DESIGNED AND WELDED TO MEET THE REQUIREMENTS OF FAR 23.963(A). THE TANKS ARE GROUNDED TO THE AIRCRAFT STRUCTURE, PRESSURE CHECKED AND LEAK CHECKED IAW FAR 23.965(A)(1). THE TANKS ARE VENTED TO POSITIVE RAM AIR PRESSURE THROUGH A VENT SYSTEM FROM A SINGLE VENT FITTING IN THE BOTTOM OF THE FUSELAGE. THE TWO CABIN TANKS ARE MOUNDED ON A 1/2 INCH PLYWOOD PALLET STRUCTURE THAT IS MOUNTED TO THE FLOOR AND SEAT RAILS. THE TANKS ARE SECURED BY A 10 POINT TIE DOWN SYSTEM. THE SYS USES A STEEL RAIL SECURED TO THE FORWARD SEAT BRACKETS AND 4 REAR CARGO TIE DOWN RINGS ALONG WITH CARGO STRAPS SECURED COMPLETELY | |||
