Incident
May 8, 1997 · Winona, MNLoss of engine power due to improper maintenance installation.
- Injuries
- None
- Report
- CHI97IA127
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI97IA127)
This N-number isn't registered right now. Below is its last known registration, canceled May 8, 2015.
Safety record in brief:1 NTSB incident (May 1997)5 ADs may apply7 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.
Loss of engine power due to improper maintenance installation.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI97IA127)
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 |
|---|---|---|---|
| 2020-03-16 | Fuselage Main, Structure | Mar 9, 2020 | Airframe (T210M) |
| 2012-10-04 | Wings | Jun 5, 2012 | Airframe (T210M)Certain serial numbers: 210G 21058819–21058936; T210G T210-0198–T210-0307; 210H 21058937–21059061; T210H T210-0308–T210-0392; 210J 21059062–21059199; T210J 21058140; … |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (T210M) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (TSIO-520 SER)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
| 2008-10-02 | Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series… | May 12, 2008 | Airframe (T210M)Certain serial numbers: 172S 172S10672–172S10674; 172S 172S10676; 172S 172S10678–172S10680; 172S 172S10682; 172S 172S10683; 172S 172S10685; …. Only with: Applies only to airplanes that have a P/N 2013142-18 alternate static air source selector valve installed after November 19, 2007. |
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.
DISTRIBUTOR GEAR FINGER LOOSENED UP AT SHAFT.
From FAA Service Difficulty Reports; matched by N-number and serial number.ALTERNATOR FAILED OUT OF THE SHIPPING BOX. (ELECTROSYSTEMS OVH UNIT).
From FAA Service Difficulty Reports; matched by N-number and serial number.PROPELLER AND CRANKSHAFT PROPELLER FLANGE SEPARATED FROM ENGINE.
From FAA Service Difficulty Reports; matched by N-number and serial number.ON APPROACH TO LAND, PILOT HAD A LANDING GEAR UNSAFE LIGHT INDICATION. PILOT NOTED THERE WAS NO GREEN LIGHT ILLUMINATED TO INDICATE THE LANDING GEAR WAS IN SAFE DOWN AND LOCK CONDITION. ALSO, AN INTERMITTENT FLICKERING LIGHT FOR THE LANDING GEAR 'UP' POSITION. AN EMERGENCY LANDING WAS CONDUCTED…
From FAA Service Difficulty Reports; matched by N-number and serial number.HYDRAULIC LINE FAILED IN SERVICE CAUSING HYDRAULIC FLUID LEAK. LANDING GEAR COULD NOT BE HAND PUMPED DOWN. SUBMITTER RECOMMENDS CLOSE INSPECTION OF ALL HYDRAULIC LINES DURING ROUTINE INSPECTIONS.
From FAA Service Difficulty Reports; matched by N-number and serial number.THE NORMAL LIFE OF THIS CYLINDER IS AT 1,500 HOURS TCO. THIS ONE LASTED 1,043 HOURS. THIS PREMATURE WEAR FAILURE SEEMS TO BE AN UNFORTUNATE TREND FOR CERMICHROME CYLINDERS. SUBMITTER RECOMMENDS NORMAL OPERATIONS WATCHING ENGINE PARAMETERS AND FREQUENT OIL CHANGE INTERVALS.
From FAA Service Difficulty Reports; matched by N-number and serial number.FOUND CYLINDER EXCESS WEAR. THE NORMAL LIFE OF THIS CYLINDER IS AT 1,500 HOURS TBO. THIS CYLINDER LASTED 1,043 HOURS. PREMATURE WEAR FAILURE SEEMS TO BE AN UNFORTUNATE TREND FOR CERMICHROME CYLINDERS. SUBMITTER RECOMMENDS NORMAL OPERATIONS WATCHING ENGINE PARAMETERS AND FREQUENT OIL CHANGE…
From FAA Service Difficulty Reports; matched by N-number and serial number.