N597SW

Part: TARGET — LOOSE (RT MLG) · airframe 24,765 hrs · 20,932 cycles

ON CLIMBOUT FROM IND RECEIVED GEAR DISAGREE MSG, RT MLG INDICATED UNSAFE. FOLLOWED QRH, EMERGENCY DECLARED, A/C RETURNED TO IND LANDED SAFELY. INSPECTED A/C FOUND RT MLG UPLOCK TARGET LOOSE. RESECURED TARGET, OPS CHECKS GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 23,960 hrs · 20,269 cycles

EMERGENCY EXIT LIGHT ADJACENT TO LEFT OVERWING EXIT SIGN INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT INVERTER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,882 hrs · 20,182 cycles

DURING EDDY CURRENT INSPECTION OF THE AFT PRESSURE BULKHEAD FS 621.00, FOUND A CRACK ON SKIN AT CARGO DOOR TRACK / LINTEL ATTACHMENT FITTING AT WL 108.00. REMOVED DAMAGE SKIN AT CARGO DOOR TRACK / LINTEL ATTACHMENT FITTING AT WL 108.00 AT FS 621.00 AND APPLIED A PERMANENT REPAIR IAW REO 601R-53-61-1230 REV D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,882 hrs · 20,182 cycles

DURING EDDY CURRENT INSPECTION OF THE AFT PRESSURE BULKHEAD FS 621.00, FOUND A CRACK ON SKIN AT LBL 27.50 ABOVE THE TOP OF CARGO DOOR TRACK. REMOVED DAMAGE AT FS 621.00 WEB LBL 27.50, WL 130 AND APPLIED A PERMANENT REPAIR IAW REO 601R-53-61-1541 REV A AND REO 601R-53-61-3086.

Part: SECU — MALFUNCTIONED (SPOILER SYS) · airframe 23,576 hrs · 19,941 cycles

ON APPROACH INTO CVG, RECEIVED GND SPOILER DEPLOY, FLT SPOILERS AND SPOILERONS CAUTION MSG'S. EMERGENCY DECLARED, A/C LANDED SAFELY. RESET SECU'S, OPS CHECK OF SPOILER SYSTEM GOOD.

Part: SELECTOR VALVE — INTERMITTENT (NLG) · airframe 22,283 hrs · 18,896 cycles

FLIGHT 5662 - ON FINAL APPROACH INTO CVG SELECTED GEAR DOWN AND RECEIVED GEAR DISAGREE WARNING FOR THE NOSE LANDING GEAR. EMERGENCY DECLARED, RAN QRH, CYCLE GEAR HANDLE ALL GEAR SHOWED DOWN AND LOCKED. A/C LANDED SAFELY AT CVG. REMOVED AND REPLACED NLG SELECTOR VALVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,226 hrs · 18,836 cycles

CABIN ROW 2 EMERGENCY CEILING LIGHT FAILED TO ILLUMINATE. DEFERRED PER MEL 33-51-01-2.

Part: BPSU — FAULTY (T/E FLAP) · airframe 22,194 hrs · 18,805 cycles

FLIGHT 5450 - AT LEVEL OFF FROM CLIMB AT 260 KTS, HIGH SPEED CLACKER SOUNDED FOLLOWED SHORTLY BY FLAPS FAIL CAUTION MESSAGE. FLAPS WERE AT 0 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY IN TYS. REMOVED AND REPLACED RIGHT BPSU. ALSO COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW-UP MAINTENANCE ACTION.

Part: ECU — FAULTY (E&E BAY) · airframe 22,188 hrs · 18,801 cycles

FLIGHT 5301 - DURING DESCENT THROUGH 17,800FT AT 280 KTS INTO SRQ, RECEIVED FLAPS HALF SPEED MESSAGE FOLLOWED BY FLAPS FAIL CAUTION MESSAGE. FLAPS WERE AT 0 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED FECU. ALSO, COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW-UP MAINTENANCE ACTION.

Part: FLAP — FAILED (WING) · airframe 22,185 hrs · 18,799 cycles

FLIGHT 5301 - DURING DESCENT THROUGH 17,800FT AT 280 KTS INTO SRQ, RECEIVED FLAPS HALF SPEED MESSAGE FOLLOWED BY FLAPS FAIL CAUTION MESSAGE. FLAPS WERE AT 0 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION.

Part: WARNING SYSTEM — MALFUNCTIONED (APU) · airframe 22,092 hrs · 18,745 cycles

FLIGHT 5539- RECEIVED APU OIL TEMP CAUTION MESSAGE. DECLARED EMERGENCY, DIVERTED TO CRW, LANDED WITHOUT INCIDENT. CHECKED APU OIL LEVEL AND PERFORMED OPS CHECK OF APU. NO FURTHER DEFECTS.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 20,945 hrs · 17,841 cycles

FLIGHT 9456 - RECEIVED -HYD 2 LOW PRESS- CAUTION. HYD 2 QTY IS 0%. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEAKING HYDRAULIC LINE. NO FURTHER DEFECTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,662 hrs · 17,602 cycles

FLIGHT 5460 - LOWER GREEN EMERGENCY EXIT LIGHT BY MAIN PAX DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT.

Part: PROXIMITY SWITCH — FAULTY (CABIN DOOR) · airframe 20,148 hrs · 17,187 cycles

FLIGHT 5454 - DURING CLIMBOUT OF CVG RECEIVED A CABIN DOOR HANDLE MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE CABIN DOOR PROXIMITY SWITCH, PS2MB.

Part: RESTRICTOR VALVE — DEFECTIVE (LT PACK) · airframe 20,092 hrs · 17,141 cycles

FLIGHT 5542 - RECEIVED CABIN ALT CAUTION. CABIN PRESS RISING SLOWLY BUT STEADILY THROUGH 8000 FT. PERFORMED QRH, EMERGENCY DESCENT TO 10000. CABIN PRESS STABILIZED. REPLACED LEFT PACK WATER SEPARATOR RESTRICTOR.

Part: DRAIN LINE — DEFECTIVE (LT PACK) · airframe 20,092 hrs · 17,141 cycles

FLIGHT 5542 - RECEIVED CABIN ALT CAUTION. CABIN PRESS RISING SLOWLY BUT STEADILY THROUGH 8000 FT. PERFORMED QRH, EMERGENCY DESCENT TO 10000. CABIN PRESS STABILIZED. REPLACED LEFT PACK WATER SEPARATOR DRAIN LINE.

Part: DOOR — UNKNOWN (PAX) · airframe 19,768 hrs · 16,883 cycles

FLIGHT 5549 - PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE, FOLLOWED BY A PAX DOOR WARNING MESSAGE. AIRCRAFT RETURNED BACK TO BWI AND LANDED SAFELY. DEFERRED PER MEL 52-70-01-1.

Part: CABLE — BROKEN (RT PYLON) · airframe 19,654 hrs · 16,791 cycles

WHILE PERFORMING TASK CARD CRJ-2-448001, RIGHT NACELLE INSP, FOUND THE ATR CABLE TO BE BROKEN AT THE TURNBUCKLE END IN THE PYLON, MAKING THE ATR SYSTEM INOP. REPLACED CABLE IAW AMM 78-35-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,314 hrs · 15,719 cycles

FLIGHT 5188 - OVERHEAD EMERGENCY LIGHT AT ROW 12 INOPERABLE. TRANSFERRED TO DEFERRED LIST PER MEL 33-51-10-1.

Part: FLAP — MALFUNCTIONED (WING) · airframe 18,030 hrs · 15,500 cycles

FLIGHT 5047 - FLAP FAIL CAUTION MESSAGE EN ROUTE TO RDU. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: BPSU — FAULTY (T/E FLAP) · airframe 18,034 hrs · 15,504 cycles

FLIGHT 5489 - EN ROUTE RDU - JFK RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES. FLIGHT RETURNED TO THE FIELD. REPLACED THE RIGHT BRAKE POSITION SENSING UNIT.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 17,782 hrs · 15,297 cycles

FLIGHT 5745 - FLAPS FAILED CAUTION MESSAGE DURING TAXI OUT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: CLIP — CRACKED (BS 625) · airframe 17,352 hrs · 14,949 cycles

CLIP ON LT SIDE FS625 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED FS 625 LT CLIP IAW CRJ200 SRM 51-24-16 PG 1-7 51-42-06 PG 1-18.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,352 hrs · 14,949 cycles

AFT FLOOR ANGLE CRACKED FS 280 LBL 11, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE PER REO 601R-53-11-138 AND SRM CRJ200 51-31-06 PG 1 PARA 3 PG 3.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,728 hrs · 14,462 cycles

EMERGENCY OVERHEAD LIGHT INOP 2ND BACK FROM FRONT. REPLACED LAMP. OPERATIONAL CHECK GOOD.

Part: OXYGEN MASK — DEPLOYED (CABIN) · airframe 16,516 hrs · 14,303 cycles

PASSENGER O2 MASKS DEPLOYED WHILE SETTING FIELD ELEVATION FROM 3860' TO 4220'. REINSTALLED MASKS AND ALL DOORS RESET PER MM 35-20-00.

Part: BEARING — WORN (RUDDER PEDAL) · airframe 16,209 hrs · 14,051 cycles

AFTER PUSHBACK FROM SLC, HEARD AUDIBLE CLICKING SOUND AS WELL AS BUMPING FEEDBACK FROM PEDALS. REPLACED LEFT RUDDER PEDAL PIVOT BEARINGS AND PEDAL ADJUSTMENT YOKE. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 16,094 hrs · 13,957 cycles

HORIZONTAL TRIM AND MACH TRIM KICKED OFF IN FLIGHT REPEATEDLY. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD IAW CRJ MM 27-41-01.

Part: SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 16,094 hrs · 13,957 cycles

STAB TRIM AND MACH TRIM CAUTION MESSAGES WILL NOT RESET. REPLACED FO'S STAB TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 15,929 hrs · 13,826 cycles

STAB TRIM CH 1 AND CH 2 AND MACH TRIM CAUTION MESSAGES INFLIGHT. REPLACED HSTCU IAW MM 22-41-01. OPERATIONAL CHECK GOOD.

Part: CONTROLLER — MALFUNCTIONED (TE FLAPS) · airframe 15,012 hrs · 13,089 cycles

FLAP FAIL AFTER LANDING. REPLACED FECU WITH SERVICEABLE UNIT IAW CRJ MM 27-51-05.

Part: ENGINE — POWER LOSS (RIGHT) · airframe 13,941 hrs · 12,244 cycles

ON DESCENT RT ENGINE N1, SPOOLED DOWN, ITT INCREASED TO 800 DEGREES, AND A BANG WAS HEARD. N1 DID NOT RESPOND TO THRUST LEVER ADVANCEMENT. ENGINE WAS LEFT AT IDLE UNTIL LANDING. REMOVED AND REPLACED RT ENGINE PER CRJ MM 71-00-00. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — MALFUNCTIONED (COCKPIT) · airframe 13,656 hrs · 12,007 cycles

CAPT SIDE TRIM SWITCH WILL COMMAND THE SURFACE NOSE DOWN BUT NOT NOSE UP. REMOVED AND REPLACED CAPTAINS TRIM SWITCH IAW 27-41-30. OPERATIONAL CHECK GOOD. P/N 309-4334.

Part: TRIM SWITCH — MALFUNCTIONED (COCKPIT) · airframe 13,624 hrs · 11,979 cycles

CAPTAIN'S TRIM SWITCH WILL NOT TRIM NOSE UP, NOSE DOWN OK. REMOVED AND REPLACED CAPTAIN TRIM SWITCH ON YOKE IAW CRJ200 MM 27-00-00. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 13,344 hrs · 11,759 cycles

FLIGHT SPLR FAULT STATUS MESSAGE FLASHES ON AND OFF DURING FLIGHT. REMOVED AND REPLACED NR 1 SECU. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 13,279 hrs · 11,706 cycles

AFTER STARTUP A SPOILERONS FAULT MESSAGE DISPLAYED. REMOVED AND REPLACED NR 2 SECU IAW MM 27-61-05, OPERATIONAL CHECK GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FLOOR SUPPORT ANGLES AT FS280, RBL9 ARE CRACKED. PROBABLE CAUSE: STRESS (EA09200402314)

Part: RIB — CRACKED (RT WING)

RT BATTERY RIB AT WS 53.60 IS CRACKED. PROBABLE CAUSE: STRESS (EA09200402314)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FLOOR SUPPORT ANGLES AT FS280, LBL9 ARE CRACKED. PROBABLE CAUSE: STRESS (EA09200402314)

Part: RIB — CRACKED (LT WING)

LEFT BATTERY RIB AT WS 53.60 IS CRACKED. PROBABLE CAUSE; STRESS. RECOMMENDATION: REPAIR IAW MFG REPAIR EO. (EA09200402314)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FLOOR SUPPORT ANGLE ON INTERCOSTAL AT FS 484, LBL 27 IS CRACKED. PROBABLE CAUSE: STRESS (EA09200402314)

Part: RIB — CRACKED (RT WING) · airframe 12,652 hrs · 11,199 cycles

RT BATT RIB AT WS 53.60 IS CRACKED. (FOUND DURING C-CHECK INSPECTION). REMOVED DAMAGE AND INSTALLED REPAIR PARTS DOUBLER AND FILLER IAW REO 601R-57-51-046 REPAIR 1.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,652 hrs · 11,199 cycles

FS 625 RT OBLIQUE ANGLE P/N 601-35012-52 CRACKED IN RADIUS. (FOUND DURING C-CHECK INSPECTION). REMOVED AND REPLACED WITH NEW ANGLES IAW CRJ 200 SRM 51-21-11, 51-21-16, 51-23-00, AND 52-42-06. SEE RII53-401.

Part: RIB — CRACKED (LT WING) · airframe 12,652 hrs · 11,199 cycles

LT BATT RIB AT WS 53.60 IS CRACKED. (FOUND DURING C-CHECK INSPECTION). COMPLIED WITH 1 THROUGH 9 OF REO 601R-57-51-046. FAB. PARTS FROM 56144-4 ANGLE .063 AND 7075T6 .050, PO 358501/1. PERFORMED REPAIR NR 1.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,652 hrs · 11,199 cycles

FLOOR SUPPORT ANGLES AT FS280, LBL 9 ARE CRACKED. (FOUND DURING C-CHECK INSPECTION). INSTALLED NEW SUPPORT ANGLES AT FS 280 RBL 9 INBOARD AND OUTBOARD AND LBL 9 INBOARD AND OUTBOARD IAW CRJ 200 SRM 51-42-06, 51-42-13, 51-42-21, AND EO 601R-53-4942. SEE RII 53-401.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,652 hrs · 11,199 cycles

FLOOR SUPPORT ANGLES AT FS 280, RBL 9 ARE CRACKED. (FOUND DURING C-CHECK INSPECTION). INSTALLED NEW SUPPORT ANGLES AT FS 280 RBL 9 IB AND OB AND LBL 9 IB AND OB IAW CRJ 200 SRM 51-42-06, 51-42-13, 51-42-21, AND EO 601R-53-4942. SEE RII 53-401.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,652 hrs · 11,199 cycles

FLOOR SUPPORT ANGLE ON INTERCOSTAL AT FS 484 LBL 27 IS CRACKED. (FOUND DURING C-CHECK INSPECTION). REMOVED AND REPLACED CRACKED CLIP AT LBL 27 BS 484 IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,652 hrs · 11,199 cycles

FS 625 LT OBLIQUE ANGLE P/N 6013501251 CRACKED IN RADIUS. (FOUND DURING C-CHECK INSPECTION). REMOVED AND REPLACED WITH NEW ANGLES IAW CRJ 200 SRM 51-21-11, 51-21-16, 51-23-00, AND 52-42-06. SEE RII53-401.

Part: TERMINAL — LOOSE (LT ENG OVHT LOOP) · airframe 12,584 hrs · 11,149 cycles

LEFT JET OVERHEAT FAIL MESSAGE INTERMITTENTLY ILLUMINATED AND THEN STAYED ON STEADY EN ROUTE. THE MESSAGE STAYED ILLUMINATED WITH SELECTION OF BOTH A AND B LOOPS. MESSAGE CONTINUED TO CYCLE ON AND OFF. INSPECTED WIRING AT LEFT ENGINE JET PIPE, FOUND 3 LOOSE TERMINALS. REPAIRED LOOSE TERMINALS AS REQUIRED. OPS CHECK GOOD.

Part: FITTING — CRACKED (PAX DOOR) · airframe 12,316 hrs · 10,946 cycles

PAX DOOR AFT ANCHOR FITTING IS CRACKED THROUGH 2 FACES. DISCOVERED DURING B004 INSPECTION. REMOVED AND REPLACED PAX DOOR AFT ANCHOR FITTING PER CRJ MM 52-11-17. OPS CHECKS GOOD.

Part: SWITCH — DIRTY (AUTOPILOT) · airframe 12,152 hrs · 10,816 cycles

CLIMBING OUT OF SLC, AUTOPILOT WOULD NOT ENGAGE ON EITHER CAPT'S OR F/O'S SIDE. F/O'S WORKED BOTH SIDES. NO WARNING OR CAUTION MESSAGE DISPLAYED. CLEANED AUTOPILOT DISENGAGE SWITCHES. OPS CHECKS GOOD.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILER) · airframe 11,210 hrs · 10,128 cycles

ON APPROACH APPROX 2 MIN AFTER SELECTING FLAPS 45 A FLIGHT SPOILERS CAUTION MESSAGE IS DISPLAYED. REMOVED AND REPLACED INBOARD PCU OF LEFT FLIGHT SPOILER. OPS AND LEAK CHECK GOOD. S/N OFF 4719.

Part: ACTUATOR — MALFUNCTIONED (SPOILER) · airframe 11,173 hrs · 10,097 cycles

ON APPROACH FLT SPOILERS FAULT STATUS MESSAGE. FLT SPOILERS OPERATE NORMALLY. REMOVED AND REPLACED LT FLIGHT SPOILER INBOARD ACTUATOR PER RJ MM 27-62-01. NO LEAKS NOTED. OPS CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (NR 1 SPOILER) · airframe 11,173 hrs · 10,097 cycles

FLT SPLR FAULT STATUS MESSAGE ILLUMINATED AFTER SPOILERS DEPLOYED IN FLIGHT. MESSAGE CLEARED ON SHUTDOWN. AFTER SHUTDOWN, SPOILERON FAULT ILLUMINATED. REMOVED AND REPLACED NR 1 SPOILER ELECTRONIC CONTROL UNIT IAW CRJ MM 27-61-05. OPS CHECK GOOD.

Part: ECU — MALFUNCTIONED (SPOILER) · airframe 10,560 hrs · 9,618 cycles

'FLT SPOILERS FAULT' STATUS MESSAGE APPEARED DURING TAXI. REMOVED AND REPLACED SECU NR 2 IAW MM 27-61-05. OPS CHECK GOOD.

Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 10,457 hrs · 9,538 cycles

LEFT ENGINE OIL PRESSURE FLUCTUATING 27-32 LBS. AFTER 15 MINUTES (APPROX) PRESSURE DROPPED TO BELOW 25 PSI. ENGINE WAS SHUT DOWN. FOUND LEFT ENGINE STARTER CARBON SEAL LEAKING. INSTALLED SERVICEABLE CARBON SEAL AND SEAL RING. ALSO REPLACED IDG AND HYD PUMP CARBON SEALS AND SEAL RINGS. OPS AND LEAKS CHECKS GOOD. IAW GE SEI-756 SPECIAL PROCEDURE 63. P/N: 5018T49P01, 4018T16P04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,978 hrs · 9,181 cycles

BOTTOM PAX DOOR LIGHT INOP. REMOVED AND REPLACED BOTTOM (LOWER) PASSENGER DOOR BOARDING LIGHT IAW MM 33-23-04. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (HSCU) · airframe 9,721 hrs · 8,986 cycles

STAB TRIM AND MACH TRIM BOTH DISCONNECTED IN FLIGHT AND UPON TOUCHDOWN. RE-RACKED HSCU COMPUTER. PERFORMED BIT CHECK, NO FAULTS NOTED. CHECKS GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 9,200 hrs · 8,593 cycles

ROW 8 OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED TB105, BATTERY PACK AND BATTERY CHARGER NR 2 IAW MM 33-51-05 AND WIRING MANUAL STANDARD PRACTICES. OPS CHECK NORMAL.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 9,093 hrs · 8,512 cycles

STALL FAIL INDICATION OCCURS AT GEAR RETRACTION, INDICATION GOES AWAY AT TOUCHDOWN. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW CRJ MM 27-35-01. OPS CHECKS GOOD. S/N OFF 441.

Part: LIGHT — SHORTED (CABIN) · airframe 8,984 hrs · 8,425 cycles

EMERGENCY LIGHTING SYSTEM HAS 3 STRIPS OF FLOOR LIGHTING INOP. THE LIGHT AT EXIT ROW 8 ON THE LEFT SIDE OF AIRCRAFT AT SEAT 8A IS INOP. FOUND NR 5 FLOOR LIGHT STRIP SHORTED. DISCONNECTED STRIP, LIGHTS WORK GOOD. REMOVED AND REPLACED NR 5 EMERGENCY FLOOR LIGHT STRIP. OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,837 hrs · 8,311 cycles

EMERGENCY FLOOR LIGHTING ROW 9 THROUGH 12 INOP. FOUND NR 4 EMERGENCY BATTERY CHARGER INOP. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY CHARGER WITH SERVICEABLE UNIT IAW MM 33-51-05. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY WITH SERVICEABLE UNIT IAW MM 33-51-04. EMERGENCY LIGHTS OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 8,791 hrs · 8,269 cycles

EMERGENCY LIGHTS SEGMENT WILL NOT TEST. REMOVED AND REPLACED NR 4 EMERGENCY LIGHTS BATTERY PACK PER MM 33-50-00. OPS CHECK GOOD.

Part: ECU — MALFUNCTIONED (NR 1) · airframe 8,340 hrs · 7,922 cycles

SPOILERONS FAULT MESSAGE REAPPEARED ON EICAS. LEFT OUTBOARD SPOILERON IS WHITE BOXED AND FLUTTERING. UNABLE TO CLEAR MESSAGE. REMOVED AND REPLACED LEFT INBOARD SPOILERON PCU AND NR 1 SECU IAW MM 27-61-05 AND 27-62-01. OPS CHECK GOOD. LEAK CHECK GOOD.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 8,456 hrs · 8,012 cycles

FS 484 RBL 27 INTERCOSTAL ATTACH ANGLE FOUND CRACKED. FOUND DURING C CHECK INSPECTION. NEW ANGLE (CLIP) FITTED AND INSTALLED IAW CRJ REO 601R-53-41-059 REV ''A''.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,456 hrs · 8,012 cycles

FS 280.0 RBL 9.0 FLOORBEAM ANGLES INBOARD AND OUTBOARD FOUND CRACKED. FOUND DURING C CHECK INSPECTION. NEW ANGLES FIT AND INSTALLED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13 & 51-42-21. P/N: 601R31113-58

Part: FITTING — CRACKED (RT PYLON) · airframe 8,456 hrs · 8,012 cycles

FS 718.0 RT PYLON FITTING ANGLE CRACKED. FOUND DURING C CHECK INSPECTION. NEW TIE ANGLE FIT AND INSTALLED IAW SRM 51-40-11, 51-42-06 AND 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,456 hrs · 8,012 cycles

FS 484 LBL 27.0 INTERCOSTAL ANGLE FOUND CRACKED. FOUND DURING C CHECK INSPECTION. NEW ANGLE FIT AND INSTALLED IAW CRJ REO 601R-53-41-059 REV. ''A''.P/N: 601R31171-17

Part: SHUTOFF VALVE — MALFUNCTIONED (ENGINE) · airframe 7,791 hrs · 7,486 cycles

AFTER TAKEOFF, SET 10TH STAGE VALVES PER SOP AND LEFT 10TH ARM OPEN APPEARED ON EICAS NR 2. FIRST OFFICER'S SYNOPTIC SHOWED LEFT 10TH VALVE WAS CLOSED, BUT LEFT 10TH SWITCH WAS PUSHED IN. RETURNED TO SLC. LANDED OVERWEIGHT BY 70 LBS. REPLACED LEFT 10TH STAGE SOV. OPS CHECK GOOD. COMPLIED WITH OVERWEIGHT INSPECTION. NO DEFECTS NOTED.

Part: CONTROL PANEL — MALFUNCTIONED (AUTOPILOT SYS) · airframe 7,743 hrs · 7,452 cycles

NR 2 YAW DAMPER INOP. REMOVED AND REPLACED FCP IAW 22-11-07. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (NLG) · airframe 7,594 hrs · 7,344 cycles

ON TAKEOFF FROM SLC, GEAR DISAGREEMENT FOLLOWED BY NOSE DOOR OPEN. RAN QRH. INDICATIONS CLEARED WHEN MLG LOWERED. RETURNED TO SLC. REMOVED AND REPLACED ACTUATOR IAW CRJ MM 32-23-01. NOSE LANDING GEAR SLOW TO STOW (GEAR DISAGREE) WITH ONE PUMP RUNNING. REMOVED AND REPLACED NLG PRIORITY VALVE PER MM 32-33-15. CYCLED GEAR. OPS CHECK GOOD. PERFORMED EMERGENCY EXTENSION. OPS CHECKS GOOD. NO LEAKS NOTED.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 7,493 hrs · 7,259 cycles

RECEIVED LEFT SPOILERON CAUTION MESSAGE. INSTALLED SERVICEABLE PCU ON LEFT OUTBOARD SPOILERON IAW 27-60-00.

Part: SERVICE DOOR — OPEN (OXYGEN) · airframe 7,405 hrs · 7,193 cycles

ON ROTATION WE RECEIVED A STALL FAIL CAUTION MESSAGE. RAN QRH. ON DESCENT, AS AIRSPEED SLOWED, WE RECEIVED A MACH TRIM FAIL MESSAGE. RETURNED TO SLC. FOUND O2 SERVICE DOOR OPEN. INSPECTED O2 SERVICE DOOR AND FOUND NO DAMAGE. OPS CHECKED STALL SYSTEM. NO DEFECTS NOTED IAW 27-35-00.

Part: WINDSHIELD — BROKEN (RIGHT SIDE) · airframe 6,982 hrs · 6,859 cycles

RIGHT SIDE WINDSHIELD SHATTERED INFLIGHT. DIVERTED TO CPR. REMOVED AND REPLACED FIRST OFFICER'S WINDSHIELD IAW MM 56-11-01. OPS AND LEAK CHECK GOOD. PN ON NP139321-10 SN OFF 99147H8942.

Part: DOOR — OPEN (O2 SERVICE) · airframe 6,504 hrs · 6,491 cycles

STALL FAIL MESSAGE ONCE AIRBORNE. RETURNED TO SLC. FOUND O2 SERVICE DOOR OPEN. INSPECTED DOOR AND SECURED DOOR. OPS CHECK GOOD.

Part: WINDOW (LEFT SIDE COCKPI) · airframe 6,334 hrs · 6,356 cycles

LEFT WINDOW HEAT CAUTION MESSAGE ON CONTINUOUSLY AFTER TAKEOFF. RETURNED TO SLC.REMOVED AND REPLACED THE LEFT SIDE WINDOW IAW AMM 56-12-01. LEAK AND OPS GOOD. P/N: NP-139322-5 S/N OFF: 98294H1164.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 5,526 hrs · 5,713 cycles

IAPS RIGHT AFCS BREAKER POPS GIVING A YD2 INOP AND IAPS DEGRADED MESSAGE. REMOVED AND REPLACED FLIGHT CONTROL PANEL IAW AMM 22-13-00. OPS CHECK GOOD. S/N ON: CYJL S/N OFF: 315