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N121FB is Assigned

N-Number Entered: 121fb Aircraft Description
Serial Number 51-7249 Status Valid
Manufacturer Name GRUMMAN AIRCRAFT ENG CORP Certificate Issue Date 02/24/2023
Model G-111 Expiration Date 02/28/2030
Type Aircraft Fixed Wing Multi-Engine Type Engine Reciprocating
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 50053750
MFR Year 1954 Mode S Code (Base 16 / Hex) A057E8
Type Registration LLC Fractional Owner NO
Registered Owner
Name AQUA AERO LLC
Street 13581 SE AMBLER RD
City CLACKAMAS State OREGON
County CLACKAMAS Zip Code 97015-9730
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 AMA/EXPR Classification Standard
Engine Model UNKNOWN ENG Category Transport
A/W Date 08/29/1984 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 20070912
INSTALLED 500 GAL. FERRY FUEL SYSTEM IN GRUMMAN G-111 ALBATROSS N121FBSERIAL 51-7249 IN ACCORDANCE WITH ATW-EO-P1467 REV. IR DATED 12-7-05, FAA FORM 8110-3. THIS FERRY SYSTEM IS TO BE REMOVED UPON ARRIVAL AT DESTINATION OR UPON EXPIRATION OF SPECIAL FLIGHT PERMIT AND AIRCRAFT RETURNED TO NORMAL CONFIGURATION PRIOR TO FLIGHT. THE OVERWEIGHT CONFIGURATION WEIGHT & BALANCE REPORT IS INCLUDED.
Mod Code 28 Mod Date 20091005
NSTALLED 500 GALLON FERRY FUEL SYSTEM IN THIS ACFT IN TEH FOLLOWING MANNER: 1. SYSTEM INSTALLED PER INSTRUCTIONS LISTED IN ENGINEERING ORDER ATW-EO-P1467 DATED DEC, 07, 2005 REV -IR. A). REFER TO SCHEMATIC DRAWING 001 FOR PLUMBING INSTALLATION, PAGES 2 THROUGH 13 OF THIS DOCUMENT. B0. REFER TO SCHEMATIC DRAWING 003 FOR ELECTRICAL INSTALLATION, PAGE 14 OF THIS DOCUMENT. C). REFER TO DRAWING 005 FOR FERRY FUEL TANKS INSTALLATION, RIGGING AND LOCATION, PAGES 15 THROUGH 21 OF THIS DOCUMENT. D). PERFORMED FUNCTIONAL TEST PROCEDURE AS DEFINED STEPS 1 THROUGH 40 ON PAGE 22 AND 23 OF THIS DOCUMENT, AND SYSTEM OPERATION TEST NORMAL. NOTE: SYSTE / STRUCTURAL DESIGN AND ELECTRICAL ASPECTS OF THIS ENGINEERING ORDER HAVE HAD PREVIOUS DERT APPROVAL. SEE ATTACHED DOCUMENTS. 2. COPY OF OPERATING PROCEEDURES PAGE 25 OF ENGINEERING ORDER ATW-EO-P1467 DATED DEC, 07, 2005 REV -IR PLACED IN SUPLEMENTAL DATA SECTION OF THE AIRPLANE FLIGHT MANUAL FOR THIS ACFT. 3. WEIGHT AND BALANCE RECORDS AMENDED TO REFLECT THIS INSTALLATION. 4. A LOGBOOK ENTRY WAS MADE TO REFLECT THIS INSTALLATION. 5. UPON ARRIVAL AT INTENDED DESTINATION THE REMOVAL OF THE AUXILIARY FERRY FUEL SYSTEM AND TEMPORARY EQUIPEMTN SHALL BE PERFORED AND THE ACFT RETURNED TO NORMAL CONFIGURATION WITH A LOG ENTRY MADE BY A PROPERLY CERTIFICATED PERSON PRIOR TO OPERATION THIS ACFT 3. NOTE: USE OF THIS AUXILLIARY FERRY FUEL SYSTEM WILL REQUIRE A SPECIAL FLIGHT PERMIT THAT ALLOWS FOR AN OVERWEIGHT CONDITION OF THIS ACFT.
Deregistered Aircraft
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.

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