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FAA REGISTRY
N-Number Inquiry Results
| Serial Number | RJ-1 | Status | Cert Terminated |
| Manufacturer Name | BEECH | Certificate Issue Date | None |
| Model | 400 | Expiration Date | None |
| Type Aircraft | Fixed Wing Multi-Engine | Type Engine | Turbo-fan |
| Pending Number Change | None | Dealer | No |
| Date Change Authorized | None | Mode S Code (base 8 / Oct) | 52062311 |
| MFR Year | 1985 | Mode S Code (Base 16 / Hex) | A864C9 |
| Type Registration | Individual | Fractional Owner | NO |
| Name | SALE REPORTED | ||
| Street | 6000 E VALENCIA RD | ||
| City | TUCSON | State | ARIZONA |
| County | PIMA | Zip Code | 85756-9403 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | P&W CANADA | Classification | Standard |
| Engine Model | JT15D 5 SER | Category | Transport |
| A/W Date | 11/02/1992 | 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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| SOLD TO ARIZONA AEROSPACE FOUNDATION |
| None |
| Mod Code | 28 | Mod Date | 19851010 |
| REMOVED BRANSON AIRCRAFT CORPORATION FUSELAGE TANK BLADDER, PART NUMBER 51D090-1 SERIAL NUMBER MA61-7, AND INSTALLED BRANSON AIRCRAFT CORPORATION FUSELAGE FUEL TANK BLADDER NUMBER 51D090-1 SERIAL NUMBER MMA31-7. INSTALLATION OF LISTED FUEL BLADDER ALLOWS CONFORMANCE TO BRANSON AIRCRAFT CORP SUPPLEMENTAL TYPE CERTIFICATE NUMBER SA1596NM. ONE-TIME ONLY STC NUMBER SA2714NM IS SUPERCEDED (SEE FAA FORM 337 DATED AUGUST 6, 1985). FUEL TANK INSTALLATION WAS PREVIOUSLY ACCOM- PLISHED PER STC SA2714NM WITH A 25 HR OPERATING LIMITATION ON FUSELAGETANK BLADDER NO. 51D090-2 S/N MA61-7. ALL ENGINENERING DATA FOR STC SA1596NM AND STC SA2714NM IS IDENTICAL WITH EXCEPTION OF HOUR LIMITA-TION OF FUEL BLADDER. WEIGHT AND BALANCE DATA IS UNCHANGED. NEW OPERATING LIMITATIONS AND FLIGHT MANUAL SUPPLEMENTS HAVE BEEN REPLACEDWITH PERMANENT COPIES. THE EXTENDED RANGE FUEL TANK HAS BEEN INSPECT-ED AND FOUND IN AIRWORTHY CONDITION. | |||
