FAA REGISTRY
N-Number Inquiry Results
| Serial Number | T18208687 | Status | Valid |
| Manufacturer Name | CESSNA | Certificate Issue Date | 10/28/2011 |
| Model | T182T | Expiration Date | 10/31/2027 |
| Type Aircraft | Fixed Wing Single-Engine | Type Engine | Turbo-prop |
| Pending Number Change | None | Dealer | No |
| Date Change Authorized | None | Mode S Code (base 8 / Oct) | 50343720 |
| MFR Year | 2007 | Mode S Code (Base 16 / Hex) | A1C7D0 |
| Type Registration | Corporation | Fractional Owner | NO |
| Name | AIRCRAFT GUARANTY CORP TRUSTEE | ||
| Street | 928 SW 107TH ST | ||
| City | OKLAHOMA CITY | State | OKLAHOMA |
| County | CLEVELAND | Zip Code | 73170-5244 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | 3A13 | Type Certificate Holder | TEXTRON AVIATION INC |
| Engine Manufacturer | LYCOMING | Classification | Standard |
| Engine Model | TIO-540-AK1A | Category | Normal |
| A/W Date | 03/13/2007 | 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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| None |
| Certificate Number | T117013 | Issue Date | 10/28/2011 | Expiration Date | 11/27/2011 |
| Mod Code | 28 | Mod Date | 20070612 |
| EXTENDED RANGE FUEL PER 14 CFR PART 43 APP. B. TEMPORARY FUEL SYSTEM INSTALLED AND CHECKED AND FOUND TO OPERATE SATISFACTORILY. WEIGHT ANDBALANCE COMPUTATION DATED MAY 2007. THIS TEMPORARY LONG RANGE SYSTEM INSTALLATION WAS PERFORMED IN ACCORDANCE WITH REPORT KR-1390 AS REVISED DUPLICATION ALTERATION APPROVED ON FAA FORM 337 DATED MAY 29, 1987 FOR CESSNA 182Q S/N 67283 N67283 AND EXTENDED GROSS WEIGHT PERMITINCLUDED AS PERFORMED AND FILED WITH THIS REPAIR STATION. OIL CONSUM-PTION ESTABLISHED DURING PERVIOUS FLIGHTS AND OIL SUPPLY DETERMINED TOBE ADEQUATE FOR LENGTH OF FLIGHT. FERRY SYSTEM SHALL BE REMOVED UPON ARRIVAL AT DESTINATION BY A CERTIFIED MECHANIC OR REPAIR STATION AS REQUIRED BY THE FAA ADMINISTRATOR. LOG BOOK MUST BE COMPLETED. ACFT ACTUAL GROSS WEIGHT 3100 LBS. ALLOWABLE MAXIMUM WEIGHT AUTHORIZED FOR FERRY PURPOSES 3410 LBS. ALSO NOTE IN AIRCRAFT LOG. ALSO NOTE FERRY FUEL PLACARD LOCATED IN AIRCRAFT IN FULL VIEW OF THE PILOT. ACFTIS WITHIN THE FORWARD AND AFT C.G. LIMITS. PILOT IS RESPONSIBLE FOR DETERMINING AIRCRAFT C.G. LIMITS ARE NOT EXCEEDED IN OVERWEIGHT CONDITION. | |||
