N5418A

CESSNA 310B · 1957 · Fixed-wing multi-engine · 2 engines · 5 seats · Valid Registration

Registered owner: TYLER JAMES, OK (owner ≠ operator)

Operators of this aircraft

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

No operator established for this aircraft.

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

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.

14 reports on file, 1995-02-06 – 1996-03-13.

OTHER · 1996-03-13 Matched by certificate designator
ATA 2312

Part: CONTROL UNIT — FAILED (COCKPIT VHF)

UNABLE TO PROGRAM IN MANUAL POSITION.

Source: SDR HEEA966848
OTHER · 1996-01-05 Matched by certificate designator
ATA 2312

Part: TRANSCEIVER — DEFECTIVE (COCKPIT VHF)

NO TRANSMIT DEVIATION AND WEAK RECEIVE.

Source: SDR HEEA966362
Earlier reports · 1995 · 12 reports

1995

OTHER · 1995-11-22 Matched by certificate designator
ATA 6310

Part: CLUTCH — WORN (FREEWHEEL)

INNER CAGE WORN BEYOND LIMITS AT INSPECTION. REPLACED CLUTCH WITH SERVICEABLE PART.

Source: SDR HEEA956132
OTHER · 1995-09-21 Matched by certificate designator
ATA 6510

Part: SHAFT — WORN (T/R)

OUTPUT SHAFT WORN IN AREA OF OUTBOARD BOOT.

Source: SDR HEEA955787
OTHER · 1995-09-14 Matched by certificate designator
ATA 6720

Part: BEARING — WORN (T/R PC LINK)

BEARING HAS EXCESSIVE AXIAL WEAR (.4MM MAX) REPLACED WITH SERVICEABLE T/R P/C LINK.

Source: SDR HEEA955767
OTHER · 1995-07-05 Matched by certificate designator
ATA 7931

Part: TRANSDUCER — FAILED (NR 1 ENG OIL)

WHILE ADVANCING #1 THROTTLE FROM FLIGHT IDLE TO FULL OPEN #1 ENGINE OIL PRESSURE DROPPED TO ZERO. REPLACED WITH SERVICEABLE TRANSMITTER AND RETURNED TO SERVICE.

Source: SDR HEEA955300
OTHER · 1995-06-26 Matched by certificate designator
ATA 7722

Part: INDICATOR — ERROR (EXH TEMP)

EXCESSIVE FRICTION ERROR. TIME SINCE REPAIR 5:35.

Source: SDR HEEA955240
OTHER · 1995-04-20 Matched by certificate designator
ATA 7321

Part: FUEL CONTROL — MALFUNCTION (NR 1 ENG)

#1 ENGINE OSCILLATING 10% ABOVE 55% TORQUE. REPLACED WITH SERVICEABLE FUEL CONTROL.

Source: SDR HEEA954822
OTHER · 1995-04-04 Matched by certificate designator
ATA 7321

Part: FUEL CONTROL — FAILED (NR 2 ENGINE)

ON FINAL APPROACH WHEN POWER WAS APPLIED, NR 2 ENGINE TORQUE STOPPED AT 55. REPLACED FUEL CONTROL. 250C20 IPC FIGURE 9, ITEM 91.

Source: SDR 95ZZZX2202
PARTIAL RPM/PWR LOSS · 1995-04-02 Matched by certificate designator
ATA 7321

Part: FUEL CONTROL — MALFUNCTION (NR 2 ENG)

PILOT REPORTED TORQUE SPLITS AFTER TAKEOFF. UNABLE TO MATCH TORQUES. NR 2 ENGINE SURGING. REPLACED FUEL CONTROL.

Source: SDR 95ZZZX2200
PARTIAL RPM/PWR LOSS · 1995-04-01 Matched by certificate designator
ATA 7530

Part: TUBE ASSY — LOOSE (ENGINE BLEED)

IN FLIGHT, AIRCRAFT WAS UNABLE TO MAINTAIN N2 RPM. RETURNED TO BASE. FOUND CUSTOMER BLEED AIR LINE LOOSE AT FIREWALL FITTING.

Source: SDR 95ZZZX2204
INADEQUATE Q C · 1995-03-23 Matched by certificate designator
ATA 5610

Part: WINDSHIELD — MIS MFG (COCKPIT RT)

FOUND WINDSHIELD TO HAVE IMPROPER FORM AND FIBERGLASS EDGING TOO THICK TO ALLOW PROPER FIT ON AIRFRAME. THIS CAUSED WINDSHIELD TO CRACK AT UPPER INBOARD CORNER. THE CRACK APPEARED THE FOLLOWING DAY AFTER THE INSTALLATION OF WINDOW WAS COMPLETED.

Source: SDR HEEA954626
OTHER · 1995-02-06 Matched by certificate designator
ATA 6210

Part: BLADE — CRACKED (M/R)

NOSE AND NECK SHELL CRACKED NEAR THE CUFF AREA.

Source: SDR HEEA954323
OTHER · 1995-02-06 Matched by certificate designator
ATA 6210

Part: BLADE — CRACKED (M/R)

NOSE AND NECK SHELL CRACKED NEAR THE CUFF AREA. THE INBOARD LEADING EDGE STRIP HAS SOME SEPARATION BUT WITHIN LIMITS.

Source: SDR HEEA954324