N710BR

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,921 hrs · 10,595 cycles

FLT 6162 - 2ND TO AFT EMERGENCY LIGHT AND EXIT SIGN INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,661 hrs · 10,401 cycles

FLT 6701 - LAST EMERGENCY LIGHT IN CABIN INOP. RELAMPED.

Part: WINDOW — CRACKED (COCKPIT) · airframe 11,474 hrs · 9,276 cycles

FIRST OFFICER SIDE WINDOW IS CRACKED. (FLIGHT 2724) REPLACED SIDE WINDOW IAW AMM 56-11-01.

Part: CONTROL PANEL — FAILED (CABIN PRESSURE) · airframe 10,971 hrs · 8,806 cycles

AIRCRAFT WAS NOT PRESSURIZING ON CLIMB-OUT, FLIGHT NR 2914. REPLACED CABIN PRESSURE SELECTOR PANEL IAW AMM 21-31-10. OPS CHECK GOOD.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 10,682 hrs · 8,584 cycles

LOST SYSTEM NR 2 HYDRAULIC FLUID ON SHORT FINAL, FLIGHT NR 2591. REPLACED NR 2 HYDRAULIC SYSTEM ENGINE DRIVEN PUMP IAW AMM 29-11-01, PN: 887055, SN OFF: MX-642339.

Part: LIGHT — SHORTED (COCKPIT) · airframe 10,500 hrs · 8,459 cycles

PILOT'S FLOODLIGHT IS SHORTED OUT. REPLACED PILOTS FLOOD LIGHT ASSEMBLY IAW CRJ200 AMM 33-11-01. OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 9,308 hrs · 7,637 cycles

FORWARD BULKHEAD EXIT SIGN IS INOP, FLIGHT NR 2878. RESECURED CONNECTOR. OPS CHECK GOOD.

Part: FRAME — CRACKED (BS 280) · airframe 8,197 hrs · 6,811 cycles

LBL9 STA 280 HAS CRACK UPPER FRAME, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AT STN 280, LBL9.0 UPPER IAW CRJ200 REO 601R-53-11-138 REVNC.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,197 hrs · 6,811 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED ANGLE SECTION AND SERVICEABLE SPLICE ANGLES PER CRJ200 REO 601R 52-11-513 REV 'A'.

Part: FRAME — CRACKED (BS 280) · airframe 8,197 hrs · 6,811 cycles

LBL9 STA 280 LOWER FRAME CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AND CLIPS AS PER CRJ200 REO 601R-53-11-171.

Part: WEB — CRACKED (PAX DOOR) · airframe 8,197 hrs · 6,811 cycles

PAX DOOR FWD WEB CRACK AT HANDRAIL STOWAGE CASTING AND STEP JUST BELOW AT CORNER, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS ON FWD WEB OF PAX DOOR PER CRJ200 REO 52-11-702 REV 'A'.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,197 hrs · 6,811 cycles

RT FS 484 O/B INTERCOSTAL CRACKED AT LBL9, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE 601R 53-41-059-2 PER REO 601R 53-41-059.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 8,197 hrs · 6,811 cycles

PAX DOOR HANDLE APPEARS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PAX DOOR OUTER HANDLE P/N 601R 317634 PER CRJ200 AMM 52-11-03-400-802.

Part: WEB — CRACKED (PAX DOOR) · airframe 8,197 hrs · 6,811 cycles

PAX DOOR AFT WEB CRACKED/LOWER CORNERS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AS PER CRJ200 REO 601R-52-11-702.

Part: FRAME — CRACKED (FUSELAGE) · airframe 8,197 hrs · 6,811 cycles

RBL9 LOWER FRAME CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AS PER CRJ200 REO 601R-53-11-171 REV C.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,197 hrs · 6,811 cycles

RT FS 621 PRESSURIZED BULKHEAD FLOOR ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE, REPAIR ANGLE AND STRAP PER REO 601R 53-61-117 REV 'C'.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 8,197 hrs · 6,811 cycles

STA 625 LT INTERCOSTAL CRACKED AT RADIUS, DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL P/N 601-35012-51 PO 71471 AT STA 65 LHS PER CRJ200 REO 601R-53-61-422.

Part: STEP — CRACKED (PAX DOOR) · airframe 8,197 hrs · 6,811 cycles

PAX DOOR FWD SIDE BENEATH TOP FOLDING STEP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS ON PAX DOOR TOP STEP AREA AS PER CRJ200 REO 601R-52-11-279.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,545 hrs · 6,305 cycles

FARTHEST AFT EMERGENCY CEILING FLOODLIGHT INOP. RELAMPED AFT MOST CEILING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD.

Part: SECU — MALFUNCTIONED (SPOILERS) · airframe 5,617 hrs · 4,739 cycles

FLIGHT SPOILER FAULT ON TAXI OUT. REPLACED 2 SECU. OPERATIONAL CHECK GOOD IAW MM 27-61-05 PN ON 49-164-20 OFF 49-164-06 SN ON 03040 OFF 01654

Part: UNKNOWN — UNKNOWN (FLT CONTROLS) · airframe 5,460 hrs · 4,601 cycles

ON CLIMB-OUT A/C ROLLS TO LEFT AND REQUIRES SIGNIFICANT RT WING DOWN AILERON TRIM. ON APPROACH IT REVERSES. WITH TRIM NEUTRAL A/C ROLLS STRONGLY TO RIGHT. PERFORMED OPERATIONAL TEST OF SKEW DETECTION UNIT, FECU, SECU 1, SECU 2. NO DEFECTS NOTED AT THIS TIME. CHECK RIGGING OF FLAPS AND FREEDOM OF MOVEMENT OF AILERONS. RIGGED WITHIN LIMITS. NO DEFECTS NOTED. ALL IAW CRJ 200 AMM 27-00-00. FLIGHT TEST REQUESTED AND PASSED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 3,898 hrs · 3,328 cycles

FS 280 FLOORBEAM LBL 9.0 OUTBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-00, 51-42-13, 51-23-00.

Part: ESCAPE HATCH — FAILED (EMERGENCY EQUIP) · airframe 3,898 hrs · 3,328 cycles

CREW ESCAPE HATCH FAILED FUNCTIONAL TEST. ITEM FOUND AT C-CHECK INSPECTION. LUBRICATED CREW ESCAPE HATCH IAW AMM 12-20-52-640-803. OPERATIONAL CHECK GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 3,898 hrs · 3,328 cycles

FLOOR SUPPORT ANGLE AT FS 621, LT SIDE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE AT FS 621 LT SIDE IAW CRJ REO 601R-53-61-114 REV B.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 3,898 hrs · 3,328 cycles

RT FS 625 CLIP CRACKED AT STR 14R. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06 AND 51-25-16.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 4,657 hrs · 3,947 cycles

FS 280 RT FLOORBEAM INBOARD AND OUTBOARD RBL 9.0 ATTACH ANGLES CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 3,813 hrs · 3,262 cycles

FLIGHT SPOILERS FAULT STATUS MESSAGE. REPLACED RIGHT FLIGHT SPOILER OUTBOARD PCU PER MM 27-62-01. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 3,769 hrs · 3,228 cycles

STAB TRIM AND MACH TRIM CAUTION MSGS AT ALTITUDE. REPLACED F/O'S TRIM SWITCH IAW CRJ MM 27-41-30. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 3,417 hrs · 2,950 cycles

SPOILERON FAULT STATUS MESSAGE AFTER TAKEOFF. REPLACED SPOILERON PCU AND REPLACED NR 1 AND NR 2 SECU'S IAW 27-61-00. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 3,387 hrs · 2,926 cycles

SPOILERON FAULT STATUS MSG. REPLACED NR 2 SECU IAW CRJ200 MM 27-61-05. OPERATIONAL CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 2,887 hrs · 2,543 cycles

STALL FAIL MESSAGE ON INFLIGHT. REMOVED AND REPLACED STALL WARNING COMPUTER IAW MM 27-35-01. OPERATIONAL CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 2,835 hrs · 2,504 cycles

CAPTAINS WINDSHIELD CRACKED AT 350. REMOVED AND REPLACED CAPTAINS WINDSHIELD ASSY IAW AMM 56-11-01. P/N OFF 601R33033-17, S/N OFF 03150H5464.

Part: INDICATOR — MALFUNCTIONED (TE FLAPS) · airframe 2,638 hrs · 2,347 cycles

WHILE CLIMBING THROUGH FL260 THE GEAR AND FLAP DISPLAYS APPEARED ON ED-1. FLAPS DEGRADED STATUS MESSAGE. REPLACED LEFT FLAP POSITION INDICATOR. OPERATIONAL CHECK GOOD IAW 27-55-01.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING)

STICKER SHAKER WENT OFF. MX REMOVED AND REPLACED STALL PROTECTION COMPUTER.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING INSPECTION THE LEFT HAND FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING INSPECTION THE RIGHT HAND EXTERNAL EMERGENCY LIGHT WAS FOUND INOEPRATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 937 hrs · 786 cycles

DURING INSPECTION THE RIGHT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 917 hrs · 771 cycles

DURING INSPECTION THE RIGHT HAND FORWARD EMERGENCY EXIT LAMP WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 907 hrs · 765 cycles

DURING INSPECTION THE RIGHT HAND OVERWING AND THE SERVICE DOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 881 hrs · 742 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOP. REPLACED THE RIGHT FORWARD OVERWING EMERGENCY LIGHT. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 844 hrs · 708 cycles

THE SECOND EMERGENCY LIGHT ON THE RIGHT SIDE OF THE AIRPLANE WAS INOP. THE LIGHT WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: ECU — FALSE ACTIVATION (T/E FLAP) · airframe 730 hrs · 613 cycles

DURING APPROACH THE CREW REPORTED A FLAP FAIL MESSAGE AT 30 DEGREES. FLIGHT LANDED WITHOUT INCIDENT AND PASSENGERS DEPLANED NORMALLY. A SATISFACTORY OPERATIONAL CHECK OF THE FLAP SYSTEM WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 730 hrs · 613 cycles

DURING INSPECTION THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 642 hrs · 539 cycles

DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.