N910FX

Part: OIL SYSTEM — LOW QUANTITY · airframe 28,815 hrs · 32,192 cycles

A LOW-SPEED ABORTED TAKEOFF OCCURRED AT APPROXIMATELY 50 KNOTS DURING THE INITIAL TAKEOFF ROLL DUE TO A MOMENTARY MASTER WARNING ALERT ON THE CREW ALERTING PANNEL. THE CREW NOTIFIED THE TOWER, AND THE AIRCRAFT EXITED THE RUNWAY. MAINTENANCE INSPECTED THE AIRCRAFT, SERVICED THE ENGINE OIL, AND THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT.

Part: FITTING — GOUGED (LT AILERON) · airframe 26,399 hrs · 29,886 cycles

LEFT AILERON CENTER FITTING ATTACH LUG IS GOUGED IN TWO SPOTS.

Part: FLOORBEAM — BENT (FRAME 39) · airframe 26,399 hrs · 29,886 cycles

FLOORBEAM AT FRAME 39 IS BENT.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 26,399 hrs · 29,886 cycles

CORROSION ON THE RT WING SPAR.

Part: ATTACH FITTING — CRACKED (LT AILERON) · airframe 26,399 hrs · 29,886 cycles

LEFT AILERON CENTER FITTING ATTACH LUG IS GOUGED IN TWO SPOTS, FOUND FITTING TO BE CRACKED AFTER REMOVAL.

Part: MASTER CYLINDER — BYPASSING (BRAKE SYSTEM) · airframe 25,039 hrs · 28,772 cycles

DURING TAXI, AFTER LANDING THE RT BRAKE WAS NOT EFFECTIVE. AFTER TROUBLESHOOTING, THE MECHANIC REPLACED THE MASTER CYLINDER IAW ATR 42, JIC 32-42-13, RAI 10000. THE SYS CHECKED GOOD.

Part: MASTER CYLINDER — LEAKING (BRAKE SYSTEM) · airframe 24,700 hrs · 28,428 cycles

F/O LT BRAKE INOPERATIVE, GOES TO THE FLOOR. TROUBLESHOT SYS AND REPLACED THE COPILOTS BRAKE MASTERCYLINDER. THE SYSTEM CHECK GOOD AND THE ACFT WAS RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 24,549 hrs · 28,319 cycles

FOUND PITTING CORROSION OUT OF LIMITS ON FRAME 41 UPPER FLOORBEAM PN S53672410284. REPLACED FLOORBEAM IAW ATR SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 24,549 hrs · 28,319 cycles

FOUND PITTING CORROSION OUT OF LIMITS ON FRAME 33 FLOORBEAM P/N S53372411200. REPLACED FLOORBEAM IAW ATR SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 24,549 hrs · 28,319 cycles

FOUND PITTING CORROSION OUT OF LIMITS ON FRAME 9 FLOORBEAM P/N S53172206258. REPLACED FLOORBEAM IAW ATR SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 24,549 hrs · 28,319 cycles

FOUND PITTING CORROSION OUT OF LIMITS ON FRAME 17 FLOORBEAM P/N S53372411204. REPLACED FLOORBEAM IAW ATR SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,549 hrs · 28,319 cycles

FOUND FILIFORM CORROSION OUT OF LIMITS ON FRAME 10 LEFT LOWER SEGMENT P/N S5317221120051. REPLACED SEGMENT IAW ATR SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,549 hrs · 28,319 cycles

FOUND FILIFORM CORROSION OUT OF LIMITS ON FRAME 10 RIGHT LOWER SEGMENT P/N S5317221120151. REPLACED SEGMENT IAW ATR SRM.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 24,549 hrs · 28,319 cycles

FLOOR PANEL 213BF UNDER 80VU ELECTRONICS RACK FOUND TO HAVE PITTING CORROSION OUT OF LIMITS. REPLACED FLOOR PANEL P/N S53173111200 IAW ATR SRM.

Part: MOUNT BRACKET — BROKEN (NR 2 ENGINE) · airframe 23,968 hrs · 27,484 cycles

DURING A ONE YEAR AND TWO YEAR INSPECTION THE NUMBER TWO ENGINE LEFT AFT LATERAL AIRFRAME MOUNT BRACKET WAS FOUND BROKEN.

Part: MOUNT — CHAFED (LT ENGINE) · airframe 23,211 hrs · 26,576 cycles

LEFT ENGINE MOUNT TUBE NR 1 HAS SMALL CHAFE MARK ON I/B SIDE OF THE TUBE. BLENDED OUT IAW ATR REPAIR REF DO/TS-677/09-11321.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 23,211 hrs · 26,576 cycles

CORROSION ON LEFT WING REAR SPAR BETWEEN RIBS 28 AND RIBS 29. BLENDED OUT IAW ATR STRUCTURAL REPAIR INSTRUCTION DO/TS/-721/09-11337.

Part: CONTROL CABLE — DIRTY (NR 2 ENGINE) · airframe 22,644 hrs · 26,119 cycles

UPON REACHING FL 210 (RAIN AND ICING TO FL 210) AN ATTEMPT WAS MADE TO ADJUST THE CONDITION LEVERS. AT THIS TIME THE CREW DISCOVERED THE NR 2 ENGINE LEVER COULD NOT BE MOVED FORWARD OR BACKWARD. IT WAS STUCK AT APPROXIMATELY 56 DEGREES. AFTER LANDING AND REACHING THE GATE DURING ENGINE SHUTDOWN THE LEVER WAS FREE TO SHUT DOWN THE ENGINE. THE CABLES WERE CLEANED AND LUBED REF: ATR 42 MM JIC12-22-76. THE PANEL REMOVED WAS INSTALLED REF: FIG 54-00-00-RAI00130-001-AFT UPPER COWL. ALL CHECKS WERE SATIFACTORY.