FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 306 | Status | Ineffect/Invalid |
| Manufacturer Name | GLOBE | Certificate Issue Date | 07/22/2016 |
| Model | GC-1B | Expiration Date | 07/31/2029 |
| 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) | 52602700 |
| MFR Year | 1946 | Mode S Code (Base 16 / Hex) | AB05C0 |
| Type Registration | Corporation | Fractional Owner | NO |
| Name | SOUTHERN AIRCRAFT CONSULTANCY INC TRUSTEE | ||
| Street | GLEBE COTTAGE COOKES ROAD | ||
| City | BERGH APTON NFLK | State | |
| County | Zip Code | NR15 1AA | |
| Country | UNITED KINGDOM | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | LYCOMING | Classification | Standard |
| Engine Model | 0-320 SERIES | Category | None |
| A/W Date | 09/03/1976 | 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/ |
|||
| None |
| Certificate Number | T165495 | Issue Date | 07/22/2016 | Expiration Date | 08/21/2016 |
| Mod Code | 28 | Mod Date | 20000712 |
| INSTALLED ONE 35.0 US GALLON ALUMINUM TEMPORARY FUEL TANK IN THE CABINAREA FOR FERRY PURPOSES ONLY. TEMPORARY TANK WAS INSTALLED BY NORTH- EAST AIR USING THE FOLLOWING DRAWINGS: NAI BTD085, NAI M022, NAI TF001NAI TF002, NAI SC001, NAI V018, NAI PS002, AND THE INSTALLATION WAS PERFORMED PER NAI INSTALLATION INSTRUCTIONS GC-1A KIT. THE TANK ISPLACED ON A WOODEN PLATFORM AT THE PASSENGER SEAT LOCATION. THE TANK IS SECURED TO THE AIRFRAME WITH TWO 1000 LBS LOAD HUGGER STRAPS TO REAR SUPPORT STRUCTURE FWD AND AFT. THE TEMPORARY TANK IS PLACARDED FOR MAX. CAPACITY AND MIN. OCTANE AND IS PRESSURE CHECKED TO3.5 PSI. FUEL FROM TEMPORARY TANK IS PLUMBED INTO THE FUEL SUPPLY SYSTEM BETWEEN AIRCRAFT FUEL SELECTOR & AUX FUEL PUMP. CONNECTION MADEMADE BY ON-OFF VALVE, APPROPRIATE FITTINGS, AND LOW PRESSURE HOSE. THE TANK IS VENTED OVERBOARD THROUGH THE PILOTS VENT WINDOW WITH THE LINE FACING FORWARD FOR POSITIVE TANK PRESSURE. THIS TEMPORARY FUEL SYSTEM WAS CHECKED FOR OPERATION AT THIS TIME OF INSTALLATION ANDWAS DETERMINED TO BE SATISFACTORY. THIS FUEL SYSTEM HAS BEEN INSTALLEDIN ACCORDANCE WITH THE STANDARD PRACTICES FOUND IN AC 43.13-1B AND ACCEPTED INDUSTRY PRACTICES. WEIGHT AND BALANCE FOR THIS TEMPORARY FUEL SYSTEM WAS CALCULATED AND SUBMITTED TO THE FLIGHT CREW. OPERATING INSTRUCTIONS ARE SUBMITTED TO THE FLIGHT CREW AND IS ALSO ATTACHED TO THIS 337. SEE 337 FOR FURTHER INFO. EXPIRY DATE IS 8/11/98. | |||
