N959AF

No registry detail on file · not in current registry

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

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.

3 reports on file, 2009-12-21 – 2014-09-20.

AFFECT SYSTEMS · 2014-09-20 Matched by certificate designator
ATA 3411

Part: FITTING — LOOSE (PITOT/STATIC SYS) · airframe 3,549 hrs · 3,545 cycles

THE FLIGHT CREW REPORTED LT SIDE AIRSPEED INDICATION FAILURE. THE NR 1 PITOT FITTING WAS FOUND LOOSE. THE FITTING WAS TIGHTENED IAW SB34-039. THE PITOT STATIC AIRSPEED SYS OPERATIONALLY CHECKED GOOD IAW THE AMM 12-B-34-11-00-00A-903A-A & 12-B-34-16-00-00A-903A-A.

Source: SDR 6CBA20140920137
OTHER · 2011-09-30 Matched by certificate designator
ATA 5510

Part: FITTING — OUT OF ALIGNMENT (HORIZONTAL STAB) · airframe 1,373 hrs · 1,409 cycles

THE HORIZONTAL STABILIZER ATTACHMENT FITTING, WHERE THE PITCH TRIM ACTUATOR IS SECURED TO THE STABILIZER. EACH SIDE OF THE ATTACHMENT FITTING HAS 2 LUGS. ON THE LT SIDE, THESE 2 LUGS ARE SEPARATING. THE GAP WAS MEASURED WITH A FEELER GAUGE, AND FOUND TO BE .406MM. THERE IS NO EVIDENCE OF DAMAGE TO THE STABILIZER. THE BRACKET PN IS 555.10.12.150, ANGLE FITTING LT. RESOLUTION: THE ACFT MFG ISSUED A REPAIR MEMO WITH STATEMENT OF APPROVED DESIGN DATA (ECC-12-RM-11-220) WITH THE FOLLOWING INSTRUCTIONS. CHECK THE LUGGED FACE OF THE LT BRACKET PN 555.10.12.150 (ANGLE FITTING LT ) FOR STRAIGHTNESS. IF WITHIN LIMITS, COMPLETE A VISUAL AND NDT INSPECTION (DYE PENETRANT OR EDDY CURRENT) OF THE ANGLE FITTING AND THE BOLTS. IF NO CRACKS OR DEFECTS NOTED, REINSTALL THE FITTING AND HARDWARE USING SEALANT.

Source: SDR 5APR20110930093
WARNING INDICATION · 2009-12-21 Unresolved
ATA 3010

Part: BOOT — SPLIT (HS DE-ICE SYS) · airframe 266 hrs · 262 cycles

DURING FLIGHT, CREW REPORTED AN AIRFRAME DEICE BOOT CAWS ANNUNCIATION. UPON INVESTIGATION FOUND RT HORIZONTAL STABILIZER DEICE BOOT WAS SPLIT ALONG THE UPPER AFT CELL FWD SEEM, 58 INCHES IN LENGTH, STARTING AT THE INBD SIDE OF THE DEICE BOOT. PN 959.89.01.036, MFG PN 27S-7D5221-14, SN MALP810, REMOVED AND REPLACED DEICE BOOT IAW MM.

Source: SDR 5APR577Y21