N812AY

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,547 hrs · 16,785 cycles

F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT ASSY IAW AMM 25-61-02.

Part: STALL WARNING — FALSE ACTIVATION · airframe 18,192 hrs · 16,425 cycles

STALL FAIL ENROUTE. QRH COMPLETED. PERSISTED WHOLE FLIGHT. FOUND OXYGEN SERVICING PANEL DOOR WAS LEFT OPEN. INSPECTED & SECURED OXYGEN SERVICE PANEL DOOR CLOSED IAW AMM 52-45-26. PERFORMED OPS CHECK OF STALL PROTECTION SYS IAW AMM 27-35-01. OPS CHECKED GOOD. MESSAGE CLEARED. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERONS) · airframe 18,046 hrs · 16,274 cycles

SPOILERONS FAULT/OTBD GROUND SPOILER FAULT STATUS MESAGES APPEARED ON APPROACH. INFORMATION ONLY: FOLLOWED THE FAULT RESET PROCEDURES IAW CHAPTER 6 FOR SPOILER FAULTS MESSAGE CLEARED & SYS OPERATES NORMAL.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,038 hrs · 16,269 cycles

CRACK FOUND IN FS559 SEMI-PRESSURE BULKHEAD CAP ANGLE AT RBL18 AND LBL18. REPAIRED IAW PA 53-025 AND REO 601R-53-41-260/601R-53-41-609.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,158 hrs · 15,404 cycles

FS 621 BULKHEAD FORWARD FACE NEXT TO LINTEL FITTING LOWER INBOARD CORNER AREA CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.

Part: BULKHEAD — CRACKED (FUSELAGE) · corrosion level 2 · airframe 17,158 hrs · 15,404 cycles

CRACKS FOUND ON FS 280 BULKHEAD AND UPPER FLOOR ANGLE AT LBL 9 AND RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-136/601R-53-11-171. BULKHEAD WEB SKIN EXFOLIATED FROM LBL 9 TO BL 0, REPAIRED IAW BOMBARDIER REO 601R-53-11-2415.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 17,158 hrs · 15,404 cycles

LEFT WING LOWER PLANK ACCESS HOLES FOR PANELS 510AB AND 540DB CORRODED IN THE NON-CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV J.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 17,158 hrs · 15,404 cycles

RIGHT WING LOWER PLANK ACCESS HOLES FOR PANELS 640BB, 640FB, 650GB, AND 650EB CORRODED IN THE NON-CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV J.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 17,077 hrs · 15,321 cycles

EMERGENCY FLOOR TRACK LIGHTING APPEARS TO BE INOPERABLE. PHOTO LUMINESCENT LIGHTING STRIPS INSTALLED OPS NORMAL IAW AMM 33-51-00. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,073 hrs · 14,176 cycles

INTERIOR OVERHEAD EMERGENCY LIGHT NR 4 INOP. REMOVED AND REPLACED BULB IN NR 4 INTERIOR OVERHEAD EMERGENCY LT IAW AMM 33 50. OPS CHECK GOOD.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 14,124 hrs · 12,020 cycles

IN AFT EQUIPMENT COMPARTMENT AT FS 672.00, STRINGER 25R. THE FRAME FLANGE ON FWD AND AFT EDGES ARE DENTED AND CRACKED. COMPLIED WITH PERMANENT REPAIR TO FS 672.00 FRAME AT STRINGER 25R ON FWD AND AFT FLANGES IAW BSC EO 601R-53-20296.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,124 hrs · 12,020 cycles

LT AND RT SIDE SEAT TRACK CORRODED BETWEEN FS 461 AND 473 UNDER OVERWING EMERGENCY EXIT DOOR CUTOUTS. REMOVED AND REPLACED LT AND RT SIDE SEAT TRACK BETWEEN FS 449 AND 473 IAW CRJ 200 AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,124 hrs · 12,020 cycles

FS 202.75 BULKHEAD AT PARKING BRAKE CABLE PASS THROUGH HOLE FAILS NDTM WITH AN INDICATION NOTED APPROX .500" IN LENGTH, 90 PERCENT FSH. COMPLIED WITH PERMANENT REPAIR OF FS 202.75 BULKHEAD AT PARKING BRAKE CABLE PASS THROUGH HOLE IAW BOMBARDIER REO 601R-53-11-563 AND BSC STANDARD REPAIR 601R-53-0101A.

Part: SKIN — DENTED (SPOILER) · airframe 14,060 hrs · 11,961 cycles

SINGLE INDENTATION WAS FOUND ON THE LEFT WING INBOARD GROUND SPOILER UPPER SURFACE AT WS 89.0. THE DAMAGE IS RECORDED AS 1.00 INCH DIAMETER AND A MAXIMUM DEPTH OF 0.009 INCH AND IS LOCATED 1.25 INCHES AFT OF THE LEADING EDGE AND 9.25 INCHES FROM THE OUTBOARD EDGE. REPAIR IAW STS ENGINEERING EA 5-2010-328. AT THE NEXT C CHECK MAINTENANCE INTERVAL, NOT TO EXCEED 5,000 FLIGHT HOURS, REPAIR THE GROUND SPOILER UPPER SKIN INDENTATION IN ACCORDANCE WITH CRJ-200 SRM 51-72-00; METAL HONEYCOMB REPAIRS.

Part: LIGHT — CONTAMINATED (COCKPIT) · airframe 12,862 hrs · 10,835 cycles

THE CREW REPORTED A FUME SMELL IN THE COCKPIT PRIOR TO APPROACH. THE FUMES SMELLED ELECTRICAL. THE APU WAS OFF AT THE TIME. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FLOODLIGHT ON F/O'S SIDE (P3LA) TO BE CONTAMINATED WITH WATER CAUSING A SHORT CIRCUIT. MAINTENANCE REMOVED AND REPLACED (P3LA) FLOODLIGHT IAW A MM 33-11-01.

Part: UNKNOWN — MALFUNCTIONED (NLG) · airframe 12,117 hrs · 10,107 cycles

GEAR DISAGREE ON TAKEOFF (NOSE GEAR WOULD NOT RETRACT). DEFERRED PER MEL 32-30-01.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 1,779 hrs · 1,308 cycles

FLAPS FAILED AT 20 DEGREES ON APPROACH. SYSTEM RESET AND PLACED UNDER 72 HOUR WATCH PER AD 98-20-01.