FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 20495 | Status | Valid |
| Manufacturer Name | CESSNA | Certificate Issue Date | 06/30/2022 |
| Model | 170B | Expiration Date | 06/30/2029 |
| 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) | 50415041 |
| MFR Year | 1952 | Mode S Code (Base 16 / Hex) | A21A21 |
| Type Registration | Individual | Fractional Owner | NO |
| Name | SHANNON JON M | ||
| Street | 2117 CRESENT MILL LN | ||
| City | CONROE | State | TEXAS |
| County | MONTGOMERY | Zip Code | 77304-2155 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | CONT MOTOR | Classification | Standard |
| Engine Model | C145 SERIES | Category | None |
| A/W Date | 04/21/1956 | 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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| Certificate Number | T227740 | Issue Date | 06/30/2022 | Expiration Date | 07/30/2022 |
| Mod Code | 28 | Mod Date | 20080924 |
| ALTERED AIRCRAFT BY THE INSTALLATION OF AN 18 GALLON AUXILIARY FUEL SYSTEM MOUNTED IN THE BAGGAGE COMPARTMENT (SEE TCDS A-799 ITEM #113), ITEM NUMBER 113 IS FOR A JAVELIN AIRCRAFT COMPANY, 1405 OLIVER, WICHITA, KANSAS, AUXILIARY FUEL TANK SYSTEM FUEL WHICH WAS INSTALLED IAW JAVELIN AIRCRAFT COMPANY'S INSTALLATION INSTRUCTIONS DATED 9/15/55AND DRAWING NUMBERS 781-2 AND 787 FOR LANDPLANES, WITH THE EXCEPTIONS OF THE PULL-ON/PUSH-OFF SWITCH, COLE-HERSEE CO P/N 5007A WAS REPLACED WITH A AN3027-2 SWITCH, THE SUMP DRAIN VALVE, THOMAS ASSOCIATES P/N TA3-716D9 WAS REPLACED WITH A SAF-AIR DRAIN VALVE P/N CAV-110, ANDTHE PLACARD 782-11, READING AUXILIARY FUEL TRANSFER PUMP PULL ON, WAS REPLACED WITH A PLACARD READING, AUXILIARY FUEL TRANSFER PUMP ON-UP/ DOWN-OFF. AIRCRAFT WEIGHT AND BALANCE DATA HAS BEEN AMENDED AND RECORDED IN THE PERMANENT AIRCRAFT RECORD AS FOLLOWS: EMPTY WEIGHT 1367.0 EMPTY WEIGHT CG: 39.95 EMPTY WEIGHT MOMMENT: 54617.2 USEFUL LOAD: 833.0. A COPY OF THSI FAA FORM 337 MUST BE INCLUDED IN THE AIRCRAFT RECORDS CARRIED IN THE AIRCRAFT IN ACCORDANCE WITH 14 CFR PART 43, APPENDIX B. AD 73-17-01 WAS COMPLIED WITH PER CESSNA SERVICELETTER NO. SE69-24, BY THE ADDITION OF THE WORDING AT THE BOTTOM OF THE AUXILIARY FUEL TRANSFER PUMP PLACARD TO READ, PLACE PUMP OFF BEFORE CHANGING FROM LEFT TANK. THE PLACARD REQUIRED BY THE CESSNA SERVICE LETTER SE69-24 WILL BE MODIFIED TO ELIMINATE THE HOLE FOR THE OLD PUSH-PULL SWITCH AND WORDING WILL BE PLACED NEXT TO THE AN3027-2 SWITCH. CESSNA ITEM NUMBER 402K WAS INSTALLED IN THE AIRCRAFT, (CAA APPROVED FLIGHT MANUAL SUPPLEMENT DATED 11/18/55 (PERTINENT TO AUX. FUEL TANK INSTALLATION, ITEM #113). | |||
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