This N-number isn't registered right now. Below is its last known registration, canceled Nov 17, 2016.
Safety record in brief:1 NTSB accident (substantial damage, Nov 2012)7 ADs may apply5 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
Collision with a deer during the landing roll, which resulted in a compromised fuel tank and a postimpact fire.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA13LA061)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2015-17-12 | Air Conditioning | Sep 29, 2015 | Airframe (550)Certain serial numbers: 500 0001–0689; 501 0001–0689; 550 0002–0733; 550 0801–1136; 551 0002–0733; 551 0801–1136; …. Only with: Air conditioning system installed via Cessna STC SA3849SW, SA7580SW, SA7753SW, or SA8918SW. |
| 2013-09-11 | Air Conditioning | Jul 5, 2013 | Airframe (550)Certain serial numbers: 500 0001–0689; 501 0001–0689; 550 0002–0733; 550 0801–1136; 551 0002–0733; 551 0801–1136; … |
| 2007-11-17 | Cessna Model 500, 501, 550, 551, S550, 560, 560XL, and 750 Airplanes | Jul 6, 2007 | Airframe (550)Serial numbers per Cessna Service Bulletins SB500-26-02, SB550-26-05, SB560-26-01, SB560XL-26-02, SB750-26-05, SBS550-26-02 (Table 1 of this AD) |
| 2006-06-03 | Cessna Model 500, 501, 550, S550, 551, and 560 Airplanes | Apr 20, 2006 | Airframe (550)Certain serial numbers: 500 0001–0689; 501 0001–0689; S550 0001–0160; 550 0002–0733; 551 0002–0733; 550 0801–1075; … |
| 2004-09-05 | Cessna Model 500, 501, 550, and 551 Airplanes | Jun 2, 2004 | Airframe (550)Certain serial numbers: 500 0001–0689; 501 0001–0689; 550 0002–0733; 551 0002–0733. Only with: Equipped with BFGoodrich brake assembly P/N 2-1528-6 or 2-1530-4. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 98-04-38 | Cessna Model 500, 501, 550, 551, and 560 Series Airplanes | Mar 25, 1998 | Airframe (550)Only with: Equipped with pneumatic deicing boots. |
| 95-25-10 | Cessna Model 441, 500, 550, and 560 Series Airplanes | Jan 22, 1996 | Airframe (550)Serial numbers per Allied Signal Aerospace Service Bulletins 103576-21-4054, 103576-21-4056, and 103648-21-4055. Only with: Equipped with Allied Signal outflow/safety valves identified in Allied Signal Aerospace Service Bulletins 103576-21-4054, 103576-21-4056, and 103648-21-4055. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
DESCRIPTION AMENDED TO SAY THAT THE LOWER LUG WAS CRACKED INSTEAD OF THE UPPER LUG.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A DAILY INSPECTION OF THE AIRCRAFT A CRACK WAS FOUND ON THE UPPER LUG OF THE DOOR HINGE. DURING REPLACEMENT OF THE HINGE THE LUG COMPLETELY BROKE IN (2) PEICES.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INTERNAL INSPECTION OF THE FUEL BAYS FOUND FUEL PUMP WIRING HARNESSES IN BOTH WINGS WERE DAMAGED BY CHAFFING THROUGH THE WIRING INSULATION. WIRING WAS CHAFFING AGAINST ALUMINUM FUEL LINES AND PUMP BODY INSIDE TANK. CHAFFING CAUSED WEAR BEYOND LIMITS TO ALUMINUM FUEL LINES.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING COMPLIANCE WITH CESSNA SB 550-32-41 BRAKE INSPECTION, FOUND BOTH BRAKES HAD BROKEN STATORS. BOTH BRAKES HAD 415 LANDINGS SINCE OVERHAUL. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.LEFT WING AND RIGHT WING LEADING EDGE SKIN HAS BEEN CHAFED BY THE UPPER SCREW OF THE OUTBOARD ROW OF SCREWS ATTACHING THE HEATED LEADING EDGE TO THE WING. THE SCREWS INSTALLED WERE TOO LONG, ALTHOUGH THEY WERE THE ONES CALLED FOR IN THE PARTS CATALOG. THEY CHAFED INTO THE WING LEADING EDGE SKIN…
From FAA Service Difficulty Reports; matched by N-number and serial number.