N588SW

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 33,847 hrs · 29,545 cycles

FOUND CRACK ON FWD PRESSURE BULKHEAD AROUND PARKING BRAKE CABLE AT FS 202.75. REPAIRED FWD PRESSURE BULKHEAD IAW EA 10-5311-02824.

Part: CHANNEL — CRACKED (LT WING) · airframe 31,870 hrs · 27,944 cycles

DURING HMV 7 LT WING PLANK INSPECTION NDT FOUND CRACK INDICATION AT FUEL DRAIN MOUNT HOLE, FWD HOLE OF BOOST PUMP DRAIN ASSY, BETWEEN WS 0.00 AND WS 22.5, STR 5 AND STR 7. DAMAGE REMOVED BY OVERSIZING HOLE AND INSTALLING FREEZE PLUG PER EA 10-5721-02400.

Part: FLOOR SUPPORT — CORRODED (BS 589-605) · airframe 31,870 hrs · 27,944 cycles

CORROSION FOUND ON TOP FLOOR STRUCTURE AT LBL27 BETWEEN FS 589 AND 605. R&R FLOOR STRUCTURE AT LBL27 BETWEEN FS 589 AND 605 IAW REO 601R-53-00-027 AND 601R-53-00-045.

Part: INTERCOSTAL — CRACKED (FS 654.5) · airframe 31,870 hrs · 27,944 cycles

FOUND CRACK ON INTERCOSTAL FOR APU DOOR ACTUATOR. REPAIRED CRACK ON INTERCOSTAL FOR APU DOOR ACTUATOR IAW EA 10-5362-02391.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 31,839 hrs · 27,920 cycles

EMERGENCY FLOOR LIGHTS ROW 8 AFT INOP. R&R EMERGENCY BATTERY PACK NR 4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,839 hrs · 27,920 cycles

EMERGENCY FLOOR LIGHTS ROW 8 AFT INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 1.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,839 hrs · 27,920 cycles

EMERGENCY FLOOR LIGHTS ROW 8 AFT INOP. R&R EMERGENCY BATTERY PACK NR 3.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,839 hrs · 27,920 cycles

EMERGENCY FLOOR LIGHTS ROW 8 AFT INOP. R&R FLOOR LEVEL LIGHT STRIP ROW 2 THRU 8.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,839 hrs · 27,920 cycles

EMERGENCY FLOOR LIGHTS ROW 8 AFT INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 2.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 31,019 hrs · 27,248 cycles

LEFT HAND LOWER POST BRACKET CRACKED CENTER WINDSHIELD. REMOVED AND REPLACED LEFT LOWER CENTER POST WINDSHIELD BRACKET.

Part: SELECTOR VALVE — FAULTY (NLG WW) · airframe 30,195 hrs · 26,607 cycles

FLIGHT 5354 - NOSE DOOR OPEN MESSAGE RECEIVED DURING GEAR RETRACTION, FOLLOWED BY GEAR DISAGREE. EMERGENCY DECLARED, AIRCRAFT RETURNED BACK TO CHS AND LANDED SAFELY. REMOVED AND REPLACED NOSE DOOR SELECTOR VALVE.

Part: PRIORITY VALVE — FAULTY (NLG) · airframe 29,953 hrs · 26,415 cycles

FLIGHT 5391 - AFTER TAKEOFF RECEIVED GEAR DISAGREE AND NOSE DOORS OPEN MESSAGES. DECLARED EMERGENCY AND LANDED CHS WITHOUT INCIDENT. REPLACED NOSE GEAR PRIORITY VALVE.

Part: SELECTOR VALVE — FAULTY (NLG) · airframe 29,953 hrs · 26,415 cycles

FLIGHT 5391 - AFTER TAKEOFF RECEIVED GEAR DISAGREE AND NOSE DOORS OPEN MESSAGES. DECLARED EMERGENCY LANDED CHS WITHOUT INCIDENT. REPLACED NOSE GEAR SELECTOR VALVE. NO FURTHER DEFECTS.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 29,803 hrs · 26,291 cycles

FLIGHT 5531 - STALL FAIL CAUTION MESSAGE EN ROUTE TO LGA. AIRCRAFT LANDED SAFELY. PERFORMED STALL PROTECTION SYSTEM RESET. OPS CHECK GOOD.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 29,733 hrs · 26,236 cycles

FLIGHT 5103 - EMERGENCY LIGHTS AT MAIN CABIN DOOR AND SERVICE DOOR INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. NO FURTHER DEFECTS.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 29,733 hrs · 26,236 cycles

FLIGHT 5103 - EMERGENCY LIGHTS AT MAIN CABIN DOOR AND SERVICE DOOR INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. NO FURTHER DEFECTS.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 29,733 hrs · 26,236 cycles

FLIGHT 5103 - EMERGENCY LIGHTS AT MAIN CABIN DOOR AND SERVICE DOOR INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. NO FURTHER DEFECTS.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 29,733 hrs · 26,236 cycles

FLIGHT 5103 - EMERGENCY LIGHTS AT MAIN CABIN DOOR AND SERVICE DOOR INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. NO FURTHER DEFECTS.

Part: RADAR — MALFUNCTIONED (COCKPIT) · airframe 29,267 hrs · 25,864 cycles

FLIGHT 5312 - EN ROUTE FROM RDU TO MCO RADAR SHOWED RADAR NOT AT THIS RANGE AND ALL DISPLAY RANGES BOTH SIDES. AIRCRAFT DIVERTED TO SAV AND LANDED SAFELY. PERFORMED TEST OF WEATHER RADAR SYSTEM ON GROUND WITH CREW. RESET SYSTEM AND NO DEFECTS NOTED.

Part: COMPUTER — MALFUNCTIONED · airframe 29,091 hrs · 25,727 cycles

FLIGHT 5482 - FAILED TO GET CONFIG MESSAGE ON TAKEOFF. IAPS DEGRADED MESSAGE FOLLOWED. TAKEOFF WAS ABORTED. CHECKED MDC FOR IAPS DEGRADED FAULT HISTORY, WITH NO FAULT CODES DISPLAYED. OPS CHECK OF IAPS GOOD.

Part: DOOR — UNKNOWN · airframe 28,926 hrs · 25,601 cycles

FLIGHT 5354 - DURING CLIMB PAX DOOR OUTER HANDLE MESSAGE DISPLAYED, AIRCRAFT RETURNED BACK TO CHS AND LANDED SAFELY. INSPECTED PAX DOOR OUTER HANDLE FOR PROPER OPERATION. ALL CHECKS GOOD.

Part: VALVE — FAULTY (LT NACELLE) · airframe 27,952 hrs · 24,838 cycles

FLIGHT 5199 - LEFT COWL ANTI-ICE CAUTION MESSAGE CAME ON EN ROUTE TO CVG. LANDED JFK WITHOUT INCIDENT. REMOVED AND REPLACED LEFT COWL ANTI-ICE VALVE AND COWL ANTI-ICE PRESSURE SWITCH. NO FURTHER DEFECTS.

Part: VALVE — FAULTY (ENGINE) · airframe 27,658 hrs · 24,604 cycles

FLIGHT 9479 - WING OVERHEAT MESSAGE ON DESCENT. REPLACED LEFT 14TH STAGE MODULATION VALVE.

Part: DUCT — SEPARATED (WATER SEPARATOR) · airframe 27,650 hrs · 24,599 cycles

FLIGHT 5246 - LOSS OF PRESSURIZATION AT ALTITUDE. A/C DIVERTED TO BUF AND LANDED WITHOUT INCIDENT. FOUND LEFT WATER SEPARATOR OUTFLOW DUCT SEPARATED, RESECURED DUCT. OPS CHECK GOOD.

Part: ANGLE — CRACKED (FS 280) · airframe 27,643 hrs · 24,592 cycles

FLOOR STRUCTURE ON RT SIDE FS 280.0 CRACKED. INSTALLED SUPPORT ANGLE ON RT SIDE FUSELAGE IAW CRJ SRM 51-42-06.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 26,557 hrs · 23,775 cycles

FLIGHT 5894 - EN ROUTE CVG-BDL THE RIGHT WINDSHIELD CRACKED, FLIGHT DIVERTED TO SYR. REPLACED THE RIGHT WINDSHIELD.

Part: OIL CAP — LOOSE (RT ENGINE) · airframe 25,620 hrs · 22,991 cycles

FLIGHT 5690 - RT ENGINE OIL PRESSURE WARNING. FOUND OIL FILTER CAP NOT SEATED. REINSTALLED FILTER AND CAP. NO LEAKS FOUND.

Part: COMPUTER — MALFUNCTIONED · airframe 24,725 hrs · 22,261 cycles

"STALL FAIL" CAUTION MSG CAME ON AFTER T/O. REPLACED STALL PROTECTION COMPUTER IAW AMM 27-35-01. OPERATIONAL CHECK GOOD.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 24,402 hrs · 21,996 cycles

AFTER T/O RECEIVED A FLAPS FAIL CAUTION MESSAGE. REPLACED RT BPSU IAW CRJ MM 27-51-10.

Part: LIGHT — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,379 hrs · 21,980 cycles

2ND OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. REPLACED LAMP. OPERATIONAL CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 24,180 hrs · 21,820 cycles

STALL FAIL MSG AFTER TAKEOFF. REPLACED STALL PROTECTION UNIT IAW 27-34-00. OPERATIONAL CHECK GOOD. P/N: 3995100208, S/N OFF: 338.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 22,999 hrs · 20,873 cycles

AT TAKEOFF, HEARD LOUD CRACK, RIGHT WINDSHIELD OUTER PANES BROKEN. REMOVED AND REPLACED RIGHT WINDSHIELD IAW CRJ 200 MM 56-00-00, 56-11-01, 56-12-01. OPERATIONAL CHECK GOOD. P/N: NP139321-12, S/N: 03175R71B7.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 22,902 hrs · 20,799 cycles

ON TAXI OUT, SPOILERON CAUTION MESSAGE. INSTALLED SERVICEABLE SECU IN NR 1 POSITION. OPERATIONAL CHECK GOOD IAW 27-60-00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,590 hrs · 20,546 cycles

FUSELAGE FLOOR SUPPORT INTERCOSTAL AT STA 484.00 INBOARD FLANGE AT RBL 27 CRACKED. ITEM FOUND AT C-CHECK INSPECTION.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 22,590 hrs · 20,546 cycles

FS 460 RIGHT FLOORBEAM RBL 9.0 OUTBOARD FITTING IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FITTING REPLACED IAW CRJ SRM 51-40-11, 51-42-06, AND 51-42-21.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 22,590 hrs · 20,546 cycles

TRANSVERSE BEAM UPPER FLANGE CRACKED AT STA 280 LBL 9. ITEM FOUND AT C-CHECK INSPECTION. BEAM REPAIRED IAW CRJ REO 601R53-11-136. REV "NC".

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,907 hrs · 20,804 cycles

RIGHT SIDE SEAT RAILS CORRODED FROM FS 364 - 559+79. ITEM FOUND AT C-CHECK INSPECTION. SEAT RAILS REPLACED IAW CRJ SRM 51-41-02, 51-41-04, 51-23-00, REO 601R-53-00-055 REV NC.

Part: BEAM — CRACKED (FUSELAGE) · airframe 22,590 hrs · 20,546 cycles

VERTICAL BEAM CRACKED AT FS 559, RBL 9.0 IB LOWER FASTENER. (ITEM FOUND AT C-CHECK INSPECTION). REPAIRED IAW CRJ REO 601R-53-41-057 REV NC 13.

Part: ATTACH ANGLE — CRACKED (FLOORBEAM) · airframe 22,590 hrs · 20,546 cycles

STA 280, RBL, BOTH INBOARD AND OUTBOARD 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, 51-42-21, 51-25-16, AND 51-21-11.

Part: BEAM — CRACKED (FUSELAGE) · airframe 22,590 hrs · 20,546 cycles

FS 409 + 128 LEFT VERTICAL BEAM AT LBL 27 LOWER INBOARD FLANGE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED BEAM IAW CRJ REO 601R-53-41-056.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,590 hrs · 20,546 cycles

FS 625 LEFT INTERCOSTAL STR 14 LEFT CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06.

Part: ATTACH ANGLE — CRACKED (FLOORBEAM) · airframe 22,590 hrs · 20,546 cycles

STA 280, LBL, OUTBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00, 51-42-21, 51-25-16, 51-21-11.

Part: BEAM — CRACKED (FUSELAGE) · airframe 22,590 hrs · 20,546 cycles

FS 409 + 128 RIGHT VERTICAL BEAM AT RBL 18 LOWER OUTBOARD FLANGE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALL REPAIR PIECES IAW CRJ ERO 601R-53-41-248 REV "NC" AND 601R-53-41-056 REV "NC".

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 22,590 hrs · 20,546 cycles

CLIP AT FS 202.75 AND LEFT STRINGER 21 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, AND 51-23-00.

Part: BEAM — CRACKED (FUSELAGE) · airframe 22,590 hrs · 20,546 cycles

FS 409 + 128 RIGHT VERTICAL BEAM AT RBL 27 LOWER INBOARD FLANGE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 "NC" .

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 22,590 hrs · 20,546 cycles

TRANSVERSE BEAM LOWER FLANGE CRACKED AT FS LBL 9. ITEM FOUND AT C-CHECK INSPECTION. BEAM REPAIRED IAW CRJ REO 601R-53-11-171.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 22,590 hrs · 20,546 cycles

EVIDENCE OF CORROSION FOUND ON INSIDE OF PAX DOOR FROM FS 310.00 TO FS 349.00 AT STR 16P. ITEM FOUND AT C-CHECK INSPECTION. THREE SUPPORT ANGLES REPLACED IAW CRJ SRM 51-40-11 AND 51-42-06.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,590 hrs · 20,546 cycles

FUSELAGE FLOOR SUPPORT INTERCOSTAL AT STA 484.00 INBOARD FLANGE AT LBL 27 + OUTBOARD FLANGE AT LBL 36 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV "A".

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 22,907 hrs · 20,804 cycles

AFT EQUIPMENT COMP; FIREWALL SHUT-OFF SUPPORT INTERCOSTAL HAS A CRACKED ATTACH ANGLE; FS 662.00; STR-9L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-25-16.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 22,590 hrs · 20,546 cycles

CARGO PIT EXISTING FLOOR SUPPORT ANGLE REPAIR IS CRACKED; FS 621.00, LBL 40.0. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ REO 601R-53-61-117 REV. B.

Part: SEAT TRACK — CORRODED (FUSLAGE) · airframe 22,907 hrs · 20,804 cycles

LEFT SIDE SEAT RAILS CORRODED FROM FS 364 - FS 559+79. ITEM FOUND AT C-CHECK INSPECTION. SEAT RAILS REPLACED IAW CRJ SRM 51-41-02, 51-41-04, 51-23-00, REO 601R-53-00-055 REV NC.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILER) · airframe 22,234 hrs · 20,258 cycles

FLIGHT SPOILERS SELECTED TO .2500 POSITION AND AIRCRAFT ROLLED LT. REMOVED AND REPLACED LT IB AND OB FLIGHT SPOILERS PCU IAW 27-62-01, OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (STAB MOTOR) · airframe 22,034 hrs · 20,094 cycles

STAB TRIM CHANNEL NR 2 FAILED TEST. REMOVED AND REPLACED HORIZONTAL STAB MOTOR CONTROL UNIT IAW MM 27-42-05, OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — MALFUNCTIONED (COCKPIT) · airframe 21,151 hrs · 19,401 cycles

IMMEDIATELY AFTER LIFT-OFF, STAB TRIM AND MACH TRIM CAUTION MESSAGES CAME ON. TRIM WOULD NOT RE-ENGAGE. REMOVED AND REPLACED PILOTS TRIM SWITCH IAW MM 27-41-05. SYSTEMS OPS CHECKS GOOD IAW CL600 MM 27-41-01. P/N: 996-0013.

Part: SWITCH — INTERMITTENT (STAB TRIM) · airframe 20,883 hrs · 19,204 cycles

CAPTAIN'S TRIM SWITCH INTERMITTENT. REMOVED AND REPLACED CAPTAIN'S STAB TRIM SWITCH IAW 27-41-05. OPS CHECK GOOD. P/N 309-4334.

Part: SWITCH — OUT OF ADJUST (MLG) · airframe 19,711 hrs · 18,305 cycles

GEAR DISAGREE, NOSE GEAR WOULD NOT RETRACT, STAYED DOWN AND LOCKED. ALSO NOSE DOOR WARNING. ADJUSTED S2GA SWITCH ON LEFT SIDE IAW CRJ MM 32-61-15. OPS CHECK GOOD.

Part: HANDLE — MALFUNCTIONED (ESCAPE HATCH) · airframe 19,680 hrs · 18,282 cycles

COCKPIT/ESCAPE HATCH WILL NOT OPEN FROM OUTSIDE HANDLE. (DISCOVERED DURING ROUTINE INSPECTION) REMOVED AND REPLACED COCKPIT ESCAPE HATCH OUTER HANDLE DUE TO CORROSION IAW MM 52-22-03. OPS CHECK GOOD .

Part: STRUT — FAILED (MLG) · airframe 19,680 hrs · 18,282 cycles

ON CLIMBOUT, WHEN LANDING GEAR LEVER WAS SELECTED UP, THE NOSE GEAR DID NOT RETRACT. COMPLIED WITH QRH AND RECYCLED GEAR, STILL NO NOSE GEAR RETRACTION. RETURN TO FIELD. REMOVED AND REPLACED NOSE LANDING GEAR AND DRAG BRACE ASSY IAW MM 32-21-01. SN OFF: DCL88/95

Part: POTENTIOMETER — DEFECTIVE (T/E FLAP) · airframe 19,643 hrs · 18,253 cycles

LEFT FLAP POSITION ON EICAS INTERMITTENTLY FLICKERS 1-3 DEGREES LOWER THAN RIGHT FLAP POSITION - BELOW 8 DEGREE SETTINGS. REPLACED POTENTIOMETER IN LEFT FLAP POSITION TRANSMITTER IAW CMM 27-55-01 & MM 27-55-01. OPS CHECK GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 19,643 hrs · 18,253 cycles

ON TAKEOFF, GEAR DISAGREE AND NOSE DOOR WARNING MSGS. INSPECTED NOSE LANDING GEAR AND ALL PROXIMITY SENSORS FOR CLEARANCE AS WELL AS SECURITY, AND WIRES. FOUND NO DISCREPANCIES. SWUNG GEAR APPROX 25+ TIMES WITH NO FAULTS IAW CL600 MM 32-61-05. OPS CHECKS GOOD AT THIS TIME.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 18,934 hrs · 17,709 cycles

FLAPS EXTENDED 41 DEGREES DURING APPROACH. AFTER LANDING THE FLAPS OSCILLATED BETWEEN 45 AND 42 DEGREES. OPERATED AND INSPECTED FLAP PANELS & ACTUATORS. INTERROGATED FECU & FCC DIAGNOSTIC SYSTEMS. FOUND TO BE OPERATING NORMALLY ON THE GROUND. OPS CHECKS GOOD AT THIS TIME IAW CL600 MM 27-51-06.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 18,844 hrs · 17,639 cycles

THE OUTBOARD GROUND SPOILERS FAULT DURING TEST. REMOVED AND REPLACED NR 1 SECU IAW CRJ AMM 27-61-05. PERFORMED OPS CHECK IAW CRJ AMM 27-61-05 AND 27-64-00. OPS CHECK GOOD.

Part: INVERTER — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 18,677 hrs · 17,514 cycles

FLOOR TRACK EMERGENCY LIGHTING AT ROW 9-13 IS INOP.REMOVED AND REPLACED NR 4 INVERTER IAW MM 33-51-07. OPS CHECK GOOD.

Part: STRINGER CLIP — MISSING (WING) · airframe 18,627 hrs · 17,470 cycles

STRINGER CLIP AT WS 106.4 LOWER WING PLANK, FORWARD INTEGRAL STRINGER MISSING. FOUND DURING C-CHECK INSPECTION.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 18,782 hrs · 17,592 cycles

FOUND FS 280 BL 9.0 LEFT AND RIGHT FLOORBEAM ANGLES CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 41-42-21 AND 51-23-00.

Part: PANEL — CRACKED (RT WING) · airframe 18,782 hrs · 17,592 cycles

RIGHT LOWER WING PLANK AT WS 148.19 CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED RIGHT LOWER WING PLANK IAW CRJ REO 601R-57-21-130 REV D AND 601R-57-21-131 REV NC. NDT-HFEC CARRIED OUT IAW REO 601R-57-21-130. NO CRACKS NOTED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 18,782 hrs · 17,592 cycles

FS 589.00 FLOORBEAM LEFT SIDE CRACKED BETWEEN LBL 42.5 AND 45.0. FOUND DURING C-CHECK INSPECTION. NDT-HFEC CARRIED OUT IAW NDTM PART 1 51-20-01. NO CRACKS NOTED. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-694 REV NC. CARGO DOOR CLEARANCES CHECKED IAW CRJ AMM 52-31-00-820-801.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,782 hrs · 17,592 cycles

VERTICAL ANGLE AT FS 280 AT LBL 12.0 BETWEEN WL 79.5 AND 69.1 IS CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-11-034 REV A.

Part: RIB — CRACKED (LT PYLON) · airframe 18,782 hrs · 17,592 cycles

LEFT PYLON RIB AT FS 605.00 CRACKED LOWER OUTBOARD FLANGE. FOUND DURING C-CHECK INSPECTION. REPLACED RIB IAW CRJ SRM 51-40-11, 51-42-21, AND 51-23-00.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 18,782 hrs · 17,592 cycles

RIGHT AND LEFT ELECTRICAL BAY FLOOR PANELS AT FS 193 CRACKED. FOUND DURING C-CHECK INSPECTION. NDT HFEC CARRIED OUT IAW REO 601R-53-11-081. NO CRACKS NOTED. REPAIRED DAMAGED FLOOR IAW CRJ REO 601R-53-11-245 REV NC.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,782 hrs · 17,592 cycles

FS 484 RBL 36 RT INTERCOSTAL O/B FL6 CRACKED. FOUND DURING C-CHECK INSPECTION. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 -A-. NDT-HFEC CARRIED OUT IAW REO 601R-53-41-059. NO CRACKS NOTED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 18,799 hrs · 17,603 cycles

FS 589 AND 605 FLOOR TRANSVERSE BEAMS LEFT SIDE ATTACH ANGLES CRACKED. FOUND DURING C CHECK INSPECTION. AFT ANGLE AT FS 605 REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00. FORWARD ANGLE AT FS 589 REPLACED IAW CRJ SRM 51-40-11, 51-40-06, 51-42-21, AND 51-23-00.

Part: INDICATOR — MALFUNCTIONED (MACH TRIM) · airframe 18,340 hrs · 17,246 cycles

STAB TRIM/MACH TRIM WILL NOT ENGAGE. REMOVED AND REPLACED HSTCU WITH SERVICEABLE UNIT IAW 27-41-00. NO DEFECTS NOTED AT THIS TIME. A/C RELEASE TO CAT II STATUS. S/N OFF: 540.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 18,340 hrs · 17,246 cycles

BOARDING LIGHT ON PASSENGER DOOR STAIR INOP. REPLACED THE LAMP IN THE LIGHT ASSEMBLY. OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (CABIN) · airframe 17,840 hrs · 16,850 cycles

EMERGENCY ESCAPE PATH LIGHTING DOES NOT ILLUMINATE FROM ROW 9 AND AFT WHEN EMERGENCY LIGHTS SWITCHED TO ON. CLEANED THE CONNECTORS FOR THE AFT SECTION OF EMERGENCY LIGHTS. OPS CHECK GOOD.

Part: PITOT TUBE — MALFUNCTIONED (#2) · airframe 16,930 hrs · 16,155 cycles

AMBER CAUTION MESSAGE FOR PITOT BASE HEAT ILLUMINATED @ 10,000. RETURNED TO SLC. REMOVED AND REPLACED #2 PITOT TUBE IAW CRJ MM 34-11-01. PERFORMED OPS CHEAK & LEAK CHECK IAW 34-11-00. OPS CHECKS GOOD. PN 667-0658 SN 201354.

Part: CONTROLLER — MALFUNCTIONED (PITOT HEAT) · airframe 16,926 hrs · 16,152 cycles

CRUISE FLT AT 310 RECEIVED A CAUTION (PITOT BASE HEAT) FOLLOWED BY A (ESSN TRU 1) CAUTION. CB 3-A2 POPPED ON IT'S OWN. REMOVED & REPLACED NR 3 AIR DATA SENSOR HEAT CONTROLLER. OPS CHECKED FOR 30 MIN. REMOVED AND REPLACED ESS TRU CB3-A2. CHECKS GOOD AT THIS TIME.

Part: TRU — FAILED (NR 1) · airframe 16,878 hrs · 16,116 cycles

ESSENTIAL TRU 1 FAILED ON CLIMBOUT. PERFORMED QRH PROCEDURE. RETURNED TO AIRPORT. REMOVED & REPLACED ESSENTIAL TRU 1 AND NR 1 ESS TRU SHUNT. OPS CHECKS GOOD.

Part: ENGINE — OVERTEMP (LEFT) · airframe 16,824 hrs · 16,074 cycles

DURING TAKEOFF, LEFT ENGINE ITT WENT TO 907 DEGREES, FLASHING RED. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGINE IAW MM 71-00-00.

Part: SWITCH — MALFUNCTIONED (RT WING) · airframe 16,805 hrs · 16,058 cycles

SELECTING WING ANTI-ICE ON RECEIVED AN ANTI-ICE DUCT MESSAGE. RETURNED TO SLC. REMOVED AND REPLACED RIGHT WING THERMAL SWITCHES FOR OUTBOARD RIGHT WING SEGMENT P/N 60159320-1. INSPECTED PICCOLO TUBE FOR OUTBOARD AND MIDDLE WINGS, NO CRACKS NOTED. RAN WING ANIT-ICE, NO LEAKS NOTED AT REMOVED SECTIONS. WING ANITI-ICE CHECKS GOOD ON GROUND RUN UP.

Part: FUSE — MALFUNCTIONED (F3PA) · airframe 16,731 hrs · 15,999 cycles

STANDBY PITOT HEAT CAUTION MESSAGE CYCLES ON AND OFF IN FLIGHT. RETURNED TO SLC. SERVICE TRU AND MAIN BATTERY SHOW 100 AMPS. REMOVED AND REPLACED FUSE F3PA. RAN LEFT AND RIGHT ENGINES ON GROUND, COULD NOT DUPLICATE CAUTION MESSAGE. OPS CHECK GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 16,644 hrs · 15,929 cycles

PITOT BASE HEAT MESSAGE ON DURING CLIMBOUT. QRH PROCEDURES WOULD NOT CLEAR MESSAGE. RETURNED TO SLC. POWERED DOWN AND POWERED UP. PITOT BASE HEAT MESSAGE CLEARED. OPS CHECK GOOD.

Part: PLACARD — INOPERATIVE (CABIN) · airframe 16,594 hrs · 15,893 cycles

EMERGENCY EXIT PLACARD NEAR FORWARD PASSENGER DOOR IS INOP. REMOVED AND REPLACED THE LIGHTED PLACARD.

Part: WINDSHIELD — CRACKED (FIRST OFFICER'S) · airframe 16,247 hrs · 15,624 cycles

RIGHT WINDSCREEN CRACKED WHILE ON THE GROUND. REPLACED FIRST OFFICER'S WINDSHIELD IAW 56-11-01. OPS CHECK GOOD. PN ON 601R33033-14 SN OFF 95032H2520.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 15,728 hrs · 15,224 cycles

LEFT OUTER WINDSHIELD SHATTERED DURING DESCENT. REMOVED AND REPLACED LEFT WINDSHIELD IAW 56-11-01.

Part: SCREW — LOOSE (SERVICE DOOR) · airframe 15,356 hrs · 14,940 cycles

AMBER SERVICE DOOR EICAS MESSAGE CAME ON THOUGH 10,000 FT. FOLLOWED QRH, THEN RETURNED TO SLC AIRPORT. CAUTION INDICATION REMAINED ILLUMINATED. PSEU SHOWED S38 FOR FORWARD SERVICE DOOR INNER HANDLE SCREWS LOOSE. TIGHTENED SCREWS AS REQUIRED. OPS CHECK GOOD.