FAA REGISTRY
N-Number Inquiry Results
Serial Number | 28-8190195 | Status | Valid |
Manufacturer Name | PIPER | Certificate Issue Date | 09/20/2016 |
Model | PA-28-181 | Expiration Date | 09/30/2029 |
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) | 52670423 |
MFR Year | 1981 | Mode S Code (Base 16 / Hex) | AB7113 |
Type Registration | LLC | Fractional Owner | NO |
Name | OTTO AVIATION LLC | ||
Street | 4112 FOREST LN | ||
City | SCHWENKSVILLE | State | PENNSYLVANIA |
County | MONTGOMERY | Zip Code | 19473-2508 |
Country | UNITED STATES |
Type Certificate Data Sheet | None | Type Certificate Holder | None |
Engine Manufacturer | LYCOMING | Classification | Standard |
Engine Model | O&VO-360 SER | Category | Utility, Normal |
A/W Date | 03/11/1981 | 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 |
None |
Mod Code | 28 | Mod Date | 19960902 |
INSTALLED ONE 85.0 US GALLON ALUMINUM FUEL TANK IN THE CABIN AREA FOR FERRY PURPOSES ONLY. THE TEMPORARY TANK WAS INSTALLED BY NORTHEAST AIRUSING THE FOLLOWING DRAWINGS: BTD063, NAI TF001, NAI TF002, NAI PS002, NAI V021, NAI M022, NAI SC002, AND TEH INSTALLATION WAS PERFORMED PERNAI INSTALLATION INSTRUCTIONS PA28-181-KIT. THE 85 GALLON TEMPORARY TANK IS PLACED ON A WOODEN PLATFORM IN THE REAR PASSENGER SEAT LOCA- TION. THE TEMPORARY TANK IS SECURED TOT HE AIRFRAME WITH 1000 LBS. LOAD HUGGER STRAPS. THE TEMPORARY TANK IS PLACARDED FOR MAX. CAPACITY AND MIN. OCTANE. THE TEMPORARY TANK IS PRESSURE CHECKED TO 3.5 PSI. FUEL FROM THE TEMPORARY TANK IS SUPPLIED TO THE AIRCRAFT FUEL SYSTEM BETWEEN THE AIRCRAFT FUEL SELECTOR AND THE FUEL GASCOLATOR BOWL BY ON- OFF VALVE, APPROPRIATE FITTINGS, AND LOW PRESSURE HOSE. THE TEMPORARY TANK IS VENTED OVERBOARD THROUGH A MANUFACTURED VENT ATTACHED TO A TEMPORARY PANEL SECURED IN THE STORM WINDOW OPENING WITH THE LINE FORWARDFOR POSITIVE TANK PRESSURE. THE TEMPORARY FUEL SYSTEM WAS CHECKED FOR OPERATION AT THIS TIME OF INSTALLATION AND WAS DETERMINED TO BE SATIS-FACTORY. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE STANDARD PRACTICES FOUND IN AC 43.13-1A OR ACCEPTED INDUSTRY PRACTICE.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 FURTHERINFO. |