N910SA

RAYTHEON AIRCRAFT COMPANY 58 · 1999 · Valid Registration

Registered owner: PERSISTENT ROOTS LLC, IL (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
QUEST DIAGNOSTICS INC (Q5QA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

O · 2018-12-07 Matched by certificate designator
ATA 5713

INSPECTION DISCLOSED WING STRINGER ON LOWER RH WING WAS CRACKED INBOARD AND OUTBOARD OF RIB AT W.S 108.5

Source: SDR Q5QA2018122808 · FAA SDRS
O · 2018-07-10 Matched by certificate designator
ATA 2421

DURING A ROUTINE INSPECTION OF THE ALTERNATOR DRIVE HUB, THE INSPECTOR NOTED THE CASTELLATED NUT RETAINING THE DRIVE HUB WAS LOOSE (THE COTTER PIN THROUGH THE CASTELLATED NUT WAS STILL IN PLACE). INSPECTION AFTER REMOVAL OF THE DRIVE HUB ASSEMBLY DISCLOSED EXCESSIVE WEAR ON THE THRUST WASHER, DRIVE HUB GEAR AND DRIVE HUB HOUSING FACE. INSTRUCTIONS FOR THE INSTALLATION OF THE HUB REQUIRES A LUBRICATED TORQUE OF THE CASTELLATED NUT OF 300 TO 450 INCH POUNDS (PUBLICATION M-16). THE DRIVE HUB ASSEMBLY WAS OVERHAULED WITH 396.8 HOURS SINCE INSTALLATION. REPLACED THE DRIVE HUB WITH A NEW DRIVE HUB, NEW THRUST WASHER AND NEW DRIVE KEY.

Source: SDR Q5QA201807131006 · FAA SDRS
O · 2018-07-10 Matched by certificate designator
ATA 2497

THE LT ALTERNATOR WAS REMOVED FOR ROUTINE INSPECTIONS. AFTER REMOVING THE COVER FROM THE BACK OF THE ALTERNATOR, THE TECHNICIAN NOTED SOME GREEN DISCOLORATION ON ONE OF THE DIODES. FURTHER INVESTIGATION DISCLOSED THE DIODE WIRE WAS BROKEN OFF OF THE DIODE BASE. THE SAME WIRE WAS DISCOVERED BROKEN OFF AT THE TOP OF AN ADJACENT DIODE. REPLACED THE ALTERNATOR.

Source: SDR Q5QA201807131007 · FAA SDRS
O · 2010-11-02 Unresolved
ATA 3233

THE LANDING GEAR ACTUATOR AND MOTOR ASSY WAS R & R WITH LANDING GEAR ACTUATOR PN 95-810017-23 DURING MX WITH AN O/H UNIT. DURING LANDING GEAR RIGGING, MOTOR SOUNDED OK AS THE GEAR WAS BROUGHT UP. WHEN GEAR WAS SELECTED DOWN, ACTUATOR AND MOTOR MADE A SLOW, DEEP GRINDING NOISE. MOTOR WAS REMOVED FOR INSP. IT WAS NOTICED THAT THE WASHER PN 105090CR032-4E, IPC 32-30-00-04, IN BETWEEN MOTOR AND GEAR, WAS MISSING. MOTOR HAD SIGNS OF RUBBING BY THE PINION GEAR. FURTHER INVESTIGATION REVEALED THAT THE WASHER WAS MISPLACED BETWEEN THE GEAR ACTUATOR HSG AND SPUR AND PINION GEAR PN 35-810135. IF THE UNITS ARE ASSEMBLED IAW THE MM THE NARRATIVE NEVER TELLS YOU TO INSTALL THE PN 105090CR032-4E WASHER, AND FIG 202- "LANDING GEAR ACTUATOR ASSY" DOES NOT DEPICT THE WASHER. THE IPC 32-30-00-04 FIG 2 OF 2 DOES SHOW THE WASHER (ITEM 320) IN ITS PROPER LOCATION. THIS IS CONFUSING AND MISLEADING.

Source: SDR 2010FA0001150 · FAA SDRS