N210CM

CESSNA 560 · 1996 · Fixed-wing multi-engine · 2 engines · 11 seats · Valid Registration

Registered owner: JET WAY LLC, OH (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
Sterling Aviation, LLC (DBCA)Certificate holderMatched by certificate designator

Accident & incident history

CESSNA T210L Minor injury Part 91operator not named in the NTSB record
Source: NTSB case OAK77DVD19

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

6 reports on file, 2018-06-22 – 2022-06-10.

WARNING INDICATION · 2022-06-10 Matched by certificate designator
ATA 3260

Part: TRANSDUCER — FAULTED (LT MLG) · airframe 12,363 hrs · 12,371 cycles

ON APPROACH CREW NOTED BRAKE FAILURE WITH ANTI-SKID INOP ANNUNCIATOR. CREW STOPPED THE AIRCRAFT WITH EMERGENCY BRAKE LEVER. PERFORMED ROTARY TEST OF ANTISKID SYSTEM, NO FAULTS NOTED. MAINTENANCE PERFORMED OHM READINGS OF LT AND RT WHEEL TRANDUCERS AND NOTED LT WHEEL TRANSDUCER READINGS ERRATIC AND SPIKING. MELD TRANSDUCER AND RETURNED TO HOME BASE. MTN REPLACED LT MAIN WHEEL SPEED TRANSDUCER WITH SERVICEABLE UNIT.

Source: SDR DBCA202206100005
WARNING INDICATION · 2021-07-07 Matched by certificate designator
ATA 2910

Part: PRESSURE VALVE — FAILED (HYD SYSTEM) · airframe 11,646 hrs · 11,614 cycles

AFTER TAKE-OFF LANDING GEAR WOULD NOT RETRACT. CREW DECLARED AN EMERGENCY AND RETURNED TO CHS. MAINTENANCE TROUBLESHOT TO DEFECTIVE HYDRAULIC PRESSURE REGULATING VALVE. PRESSURE REGULATING VALVE WAS REPLACED WITH AN OVERHAULED UNIT. PERFORMED MULTIPLE EXTENSION/RETRACTION CYCLE TESTS. OPS CHECKS GOOD.

Source: SDR DBCA2021071270002
PARTIAL RPM/PWR LOSS · 2020-08-17 Matched by certificate designator
ATA 7322

Part: FUEL CONTROL — FAILED (ENGINE) · airframe 11,141 hrs · 11,106 cycles

AFTER STARTING BOTH ENGINES CREW NOTED 5% SPLIT IN N2 INDICATIONS. CREW ADVANCED POWER ON BOTH ENGINES TO BEGIN TAXIING OUT OF PARKING, ONLY RT ENGINE WOULD ADVANCE IN POWER. CREW SHUT DOWN BOTH ENGINES AND CONTACTED MX. MX TROUBLESHOT AND NOTED NR 1 FUEL CONTROL REQUIRES REPLACEMENT. REMOVED AND REPLACED WITH OVH UNIT. OPS CHECKS GOOD.

Source: SDR DBCA202008170002
WARNING INDICATION · 2019-04-28 Matched by certificate designator
ATA 3297

Part: WIRE HARNESS — CHAFED (LT MLG) · airframe 10,125 hrs · 10,097 cycles

1) ON APPROACH WITH LANDING GEAR SELECTED DOWN THE 3 DOWN AND LOCKED INDICATOR LIGHTS DIDN'T ILLUMINATE 2) CREW ABORTED APPROACH TO ASSESS SITUATION 3)CREW FOUND 2 AMP LANDING GEAR WARNING CB TRIPPED. CREW ATTEMPTED ONE TIME RESET FOR CHECKLIST AND DOWN AND LOCKED LIGHTS ILLUMINATED FOR SEVERAL SECONDS BEFORE CB TRIPPED AGAIN. 4)CREW PERFORMED FLY BY OF TOWER, TOWER AND ANOTHER AIRCRAFT WAITING TO DEPART VISUALLY OBSERVED LANDING GEAR APPEARED DOWN AND LOCKED 5) CREW DECLARED AN EMERGENCY AND PROCEEDED WITH LANDING. LANDING WAS UNEVENTFUL. 6) STERLING AVIATION MAINTENANCE CONTROL CONTACTED TO TROUBLESHOOT. 7) PERFORMED 10 PLUS LANDING GEAR RETRACTION, EXTENSION CYCLES WITH NORMAL OPERATION, CB DIDN'T TRIP. INSPECTED UPLOCK AND DOWNLOCK SWITCHES AND ALL ASSOCIATED WIRING. NO DEFECTS NOTED. COMPLETED UPLOCK AND DOWNLOCK SWITCH PARALLELING CIRCUIT TESTS. NO DEFECTS NOTED. 8) TECHNICIANS ARE CONTINUING TROUBLESHOOTING EFFORTS. SUPPLEMENTAL: TECHNICIANS TROUBLESHOT AND FOUND LEFT MAIN LANDING GEAR WIRE HARNESS CHAFING ON HYDRAULIC LINE. REPAIRED WIRING. OPS CHECKED GOOD.

Source: SDR DBCA201904280003
OTHER · 2019-03-11 Matched by certificate designator
ATA 2150

Part: COUPLER — LOOSE (AC BAY) · airframe 10,011 hrs · 9,972 cycles

1)ON CLIMBOUT CREW NOTED CABIN PRESSURIZATION NOT HOLDING CORRECT CABIN ALTITUDE. 2)CREW RETURNED TO HOME BASE. 3)MAINTENANCE TROUBLESHOT AND FOUND THE AIR CYCLE MACHINE DUCT COUPLER COMING LOOSE. 4) RESECURED DUCT COUPLER, OPS CHECK GOOD.

Source: SDR DBCA201903110001
OTHER · 2018-06-22 Matched by certificate designator
ATA 3423

Part: SWITCH — STUCK (PFD) · airframe 9,670 hrs · 9,567 cycles

DURING DEPARTURE TAXI, CREW NOTICED THE COPILOT PFD BUTTON STUCK IN TEST MODE. CREW RETURNED TO BLOCKS. MAINTENANCE CLEANED THE SELECTOR SWITCH. OPS CHECKED GOOD.

Source: SDR DBCA2018062920003