N243AF

COMPAGNIE DAHER TBM 700 · 2024 · Valid Registration

Registered owner: AFS LLC, LA (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
COBALT AIR, LLC (6CBA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

O · 2018-09-06 Matched by certificate designator
ATA 3243

PILOT REPORTS, PILOT IN COMMAND'S SIDE RIGHT BRAKE PEDAL GOES COMPLETELY TO FLOOR. NO RIGHT BRAKE DIRECTIONAL CONTROL. THE RT PILOT BRAKE MASTER CYLINDER P/N 959.47.51.132 WAS FOUND FAULTY. IT WAS REMOVED AND REPLACED IAW THE AMM 12-B-32-40-04-00A-920A-A. OPS CHECK GOOD AND NO LEAKS NOTED.

Source: SDR 6CBA2018091018178 · FAA SDRS
O · 2017-06-29 Matched by certificate designator
ATA 5753

LEFT FLAP, BOTTOM SKIN IS CRACKED BETWEEN TWO RIVETS ON FORWARD LAP JOINT BETWEEN FORWARD AND AFT FLAP SPARS, BETWEEN FLAP RIBS FIVE AND SIX. REMOVED DAMAGE AND INSTALLED DOUBLER AND FILLER IAW SRM 12-B-57-50-00-00A-664B-A.

Source: SDR 6CBA2017062917166 · FAA SDRS
O · 2014-09-12 Matched by certificate designator
ATA 3414

PILOT AIRSPEED MIS-COMPARE BY 15 KTS, PILOTS IAS INDICATOR CONTINUED TO DROP TO 0 KTS. A SUPPLEMENTAL SDR WILL NEED TO BE FILED. MAINTENANCE IS STILL BEING COMPLETED, THE FINAL FIX IS NOT DETERMINED AT THIS TIME.

Source: SDR 6CBA20140912136 · FAA SDRS
O · 2014-09-12 Matched by certificate designator
ATA 3411

THE PITOT LINE FITTING IN LT WING AT RIB 14A WAS FOUND TO BE SEPARATED. THE POLY FLOW TUBING PITOT LINE IN LT WING, FROM WING ROOT TO BULLHEAD FITTING AT RIB 14A & FITTING PN 946.01.17.101 WAS REPLACED IAW 12-B-20-50-02-00A-901A-A & SB34-039. A PITOT & STATIC LEAK CHECK WAS ACCOMPLISHED IAW 12-B-34-11-00-00A-903A-A. NO LEAKS OR DEFECTS WERE FOUND.

Source: SDR 6CBA201409121136 · FAA SDRS
P · 2011-04-18 Matched by certificate designator
ATA 3297

WHEN GEAR DOWN SELECTED, HYD CASS, PULLED QRH THEN CASS WENT AWAY AND GEAR CAME DOWN. A POOR CONNECTION AT PIN "P" OF TB 1611-02, WIRE T1076B22 WAS FOUND TO BE AT FAULT. RELOCATED WIRES T1076B22, T1076A22 AND T1075B22 TO PINS F, M, AND X OF TB1611-02. PERFORMED 5 SUCCESSFUL, CONSECUTIVE GEAR SWINGS WITH NO DEFECTS NOTED IAW AMM 12-B-32-30-00-00A-903A-A.

Source: SDR 5APR577Y60 · FAA SDRS