N983CA

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,336 hrs · 34,299 cycles

NR 3 EMERGENCY OVERHEAD LIGHT & EMERGENCY OVERHEAD EXIT SIGN AT ROW 8 DO NOT ILLUMINATE. FLT 6394 ALLOWED ELBP TO CHARGE 7 WARM UP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,934 hrs · 33,988 cycles

NR 4 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#5622 RELAMPED.

Part: BRACKET — FAILED (NLG) · airframe 36,974 hrs · 33,264 cycles

NOSE DOOR AND GEAR DISAGREE WARNING MESSAGES, FOLLOWED QRH AND MANUALLY EXTENDED GEAR. REPLACED THE NLG LOWER AFT WEIGHT OFF WHEELS SENSOR BRACKET AND ADJUSTED THE WEIGHT OFF WHEELS SENSOR IAW AMM. PERFORMED SEVERAL GEAR SWINGS WITH NO DEFECTS NOTED. OPS CHECK GOOD AT THIS TIME. PN: 16215-105.

Part: WIRE HARNESS — FAILED (NLG) · airframe 36,955 hrs · 33,249 cycles

NOSE-GEAR UP DISAGREE MASTER WARNING. REPLACED NR 1 DOWNLOCK, NLG HARNESS IAW AMM. PERFORMED GEAR SWINGS. OPS CHECK GOOD, PN: 17300-253.

Part: DOOR SEAL — COLLAPSED (PAX DOOR) · airframe 36,625 hrs · 32,995 cycles

LOSS OF PRESSURIZATION DUE TO PORTION OF PAX DOOR SEAL COLLAPSING. (FLT 6266) REPLACED PAX DOOR SEAL. LEAK CHECKS AND OPS CHECKS GOOD.

Part: WIRE HARNESS — FAILED (NLG) · airframe 36,617 hrs · 32,987 cycles

RECEIVED GEAR DISAGREE WARNING MESSAGE SHOWING NOSE GEAR HASH MARKS. (FLT 6367) REPLACED NR 1 DOWNLOCK PROX SENSOR NLG HARNESS IAW AMM. GEAR SWINGS NORMALLY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,426 hrs · 32,841 cycles

UPPER EMERGENCY EXIT SIGN AT ROW 8 CD AND LOWER EMERGENCY EXIT SIGN IN ROW 8 A/B DO NOT ILLUMINATE. (FLT 6369) FOUND BATTERY PACK FOR EMERGENCY LIGHTS ON OVERWING EXITS TO BE LOW ON POWER. SWITCHED TO ARM AND CHARGED BATTERY.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,365 hrs · 32,788 cycles

FS 621 LEFT FLOOR SUPPORT ANGLE IS CRACKED JUST I/B OF CARGO SILL. (C-CHECK) REPLACED THE LEFT CARGO FLOOR SUPPORT ANGLE AT FS 621 IAW REO.

Part: STRUCTURE — CRACKED (LT PYLON) · airframe 36,365 hrs · 32,788 cycles

LEFT ENGINE PYLON TRAILING EDGE HAS CRACK AND DELAMINATION. (C-CHECK) REPAIRED CRACK AND DELAMINATION AT LEFT ENGINE PYLON TRAILING EDGE IAW STS EA.

Part: POST — CRACKED (FUSELAGE) · airframe 36,365 hrs · 32,788 cycles

CRACK NOTED AND MARKED IN FS 409+128 VERTICAL POST AT RBL 18, O/B C-CHANNEL IN AFT RADIUS. (C-CHECK) REMOVED AND REPLACED VERTICAL POST O/B SIDE AT FS 409+128 RBL 18 IAW REO.

Part: ARM — OUT OF ADJUST (CABIN DOOR) · airframe 36,202 hrs · 32,666 cycles

UPON ARRIVAL, COULD NOT OPEN THE MAIN CABIN DOOR. (FLT 5311) ADJUSTED INNER RELEASE ARM POWER TENSION AND INSPECTED OUTER HANDLE LINKAGES WITH NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: HANDLE — JAMMED (CABIN DOOR) · airframe 36,166 hrs · 32,633 cycles

CANNOT OPEN THE MAIN CABIN DOOR FROM THE OUTSIDE. (FLT 5349) OPENED PAX DOOR IAW AMM. AFTER INITIAL ATTEMPT DOOR HANDLE NO LONGER JAMMED. OP CHECK NORMAL UPON NUMEROUS ATTEMPTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,972 hrs · 32,458 cycles

EMERGENCY OVERHEAD LIGHT 1 AND 2, AND EMERGENCY FLOOR LIGHT 8A BURNED OUT. (FLT 5393) RELAMPED EMERGENCY.

Part: STRUT — FAILED (NLG) · airframe 35,865 hrs · 32,381 cycles

GEAR DISAGREE WARNING MESSAGE WITH NOSE WHEEL REMAINING IN DOWN AND LOCKED POSITION. WOW INPUT CAUTION MESSAGE APPEARED AS WELL. (FLT 5412) REMOVED AND REPLACED NLG SHOCK STRUT ASSEMBLY IAW AMM. P/N: 16050-115 S/N: DLC976/04 P/N: OFF 16050-115 S/N: OFF DLC183/96/05R.

Part: ANTENNA — FAILED (RADIO ALTIMETER) · airframe 35,650 hrs · 32,192 cycles

CAPTAIN'S RADIO ALTIMETER AND FIRST OFFICER'S RADIO ALTIMETER DIFFER MORE THAN 300 FEET FROM 2500 FEET. (FLT 5565) REPLACED THE F/O'S RECEIVE ANTENNA IN REFERENCE TO THE CRJ 200 MM. P/N: 567-2002 S/N OFF: NSN

Part: WIRE HARNESS — FAILED (NLG) · airframe 35,439 hrs · 32,028 cycles

GEAR DISAGREE WARNING MESSAGE ASSOCIATED WITH YELLOW INDICATION FOR NOSE GEAR. (FLT 5310) REPLACED NLG DOWNLOCK NR 1 HARNESS (PSIGA) ASSEMBLY IN REFERENCE TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,344 hrs · 31,956 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5605) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,246 hrs · 31,886 cycles

EMERGENCY EXIT LIGHT ON BOTTOM OF LEFT OVERWING EMERGENCY DOOR IS OUT. (FLT 5616) REPLACED NR 2 EMERGENCY BATTERY PACK INVERTER ASSEMBLY IN REFERENCE TO AMM.

Part: PSEU — FAILED (DOOR WARNING) · airframe 35,246 hrs · 31,886 cycles

PASSENGER DOOR OUTER HANDLE CAUTION, OVERBOARD COOL CAUTION AND INBOARD COOL FAIL STATUS. (SERVICE) REPLACED PSEU IN REFERENCE TO 200 AMM. P/N: 8-648-08 S/N OFF: D692.

Part: CONNECTOR — DIRTY (CABIN) · airframe 35,246 hrs · 31,886 cycles

LOWER EXIT EMERGENCY LIGHT ON LEFT SIDE WINDOW AT EMERGENCY EXIT IS OUT. (FLT 5642) CLEANED NR 2 INVERTER CONNECTOR IN REFERENCE TO 200 MM.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 35,154 hrs · 31,816 cycles

EXIT LIGHT AT LEFT OVERWING EXIT IS OUT. (FLT 5521) RE-SECURED CONNECTOR ON NR 2 BATTERY PACK INVERTER IN REFERENCE TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,111 hrs · 31,780 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,911 hrs · 31,637 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6308) RELAMPED EMERGENCY LIGHT.

Part: UPLOCK SENSOR — OUT OF ADJUST (NLG) · airframe 34,799 hrs · 31,557 cycles

NOSE GEAR UP DISAGREE. (FLT 5451) ADJUSTED NLG UPLOCK SENSOR PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,402 hrs · 31,255 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5336) RELAMPED EMERGENCY LIGHT.

Part: HANDLE — LACK OF LUBE (CABIN DOOR) · airframe 34,344 hrs · 31,206 cycles

MAIN CABIN DOOR OUTER HANDLE WILL NOT ROTATE AND IS DIFFICULT TO OPEN DOOR FROM OUTSIDE. (FLT 5496) INSPECTED DOOR LINKAGES, DOOR FRAMES, PINS, AND ROLLERS FOR DEFECTS. LUBED AS NESSESARY PER CRJ 200 AMM.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 34,344 hrs · 31,206 cycles

LOWER PORTION OF RIGHT WINDSHIELD CRACKING IN FLIGHT. (FLT 6496) REPLACED THE RIGHT MAIN WINDSHIELD IN REFERENCE TO AMM. P/N NP-139321-14 S/N OFF 96317H2299

Part: LIGHT — UNSECURE (CABIN) · airframe 34,294 hrs · 31,164 cycles

LOWER EMERGENCY DOOR SIGN LIGHTING ON LEFT SIDE EMERGENCY EXIT ROW IS OUT. (FLT 6378) RE-SECURED LIGHT ASSEMBLY.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 34,046 hrs · 30,950 cycles

MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. (FLT 5837) LUBRICATED THE PASSENGER DOOR IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,993 hrs · 30,900 cycles

OVERHEAD EMERGENCY LIGHT ABOVE ROW 2 IS OUT. (FLT 5507) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,706 hrs · 30,679 cycles

FLT 6464, NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 33,706 hrs · 30,679 cycles

FLT 5395, EMERGENCY EXIT ROW SIGN AT ROW 8A & B IS OUT. CHECKED WIRES ON EMERGENCY EXIT SIGN, RESTOWED WIRES, AND LIGHT CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 33,670 hrs · 30,653 cycles

EMERGENCY LIGHT ON SIDEWALL BY LEFT EMERGENCY DOOR OVERWING NOT LIGHTING UP. (SERVICE) RE-SECURED CONNECTION OF LIGHT ASSEMBLY.

Part: MANIFOLD — CRACKED (APU) · airframe 33,582 hrs · 30,591 cycles

STRONG ODOR SIMILAR TO GASOLINE OR BURNING OIL WHEN APU IS BLED. (FLT 6205) FOUND PRIMARY FUEL MANIFOLD CRACKED AND LEAKING. REPLACED PRIMARY FUEL MANIFOLD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,528 hrs · 30,545 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5330) RELAMPED EMERGENCY LIGHT.

Part: FAN — FAULTY (GALLEY) · airframe 33,487 hrs · 30,511 cycles

IN FLIGHT, GALLEY LAV FAN POPPED WITH A SLIGHT ELECTRIC SMELL. (FLT 5584) REPLACED GALLEY EXHAUST FAN. P/N: AE0405A01 S/N OFF: 1153.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,389 hrs · 30,422 cycles

THE 2ND FROM AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 3275) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,304 hrs · 30,347 cycles

FORWARD LEFT 2 EXTERIOR EMERGENCY LIGHTS ARE OUT. (FLT 6227) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,096 hrs · 30,171 cycles

SECOND TO AFT OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 6441) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,778 hrs · 29,933 cycles

RIGHT EXTERIOR MIDDLE OVERWING EMERGENCY LIGHT IS OUT. (FLT 6425) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,716 hrs · 29,887 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6242) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,672 hrs · 29,841 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5813) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,516 hrs · 29,720 cycles

NR 3 OVERHEAD EMERGENCY LIGHT NOT ILLUMINATING. (FLT 5534) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,172 hrs · 29,461 cycles

OVERHEAD EMERGENCY LIGHT IS OUT AT ROW 11. (FLT 5817) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,740 hrs · 29,143 cycles

FS 202 PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE. (SERVICE) REPAIRED PER REO.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,192 hrs · 27,867 cycles

LOWER BULB IN EMERGENCY LIGHT SIGN BY GALLEY SERVICE DOOR APPEARS INOPERATIVE. (FLT 6376) RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,148 hrs · 27,833 cycles

EMERGENCY LIGHT IN ROW 8 INOPERATIVE. (FLT 6503) RELAMPED EMERGENCY LIGHT.

Part: TRIM PANEL — MALFUNCTIONED (COCKPIT) · airframe 29,592 hrs · 27,366 cycles

RUDDER TRIM OCCASIONALLY RUNS AWAY. (FLT 6333) REPLACED RUDDER TRIM PANEL.

Part: UPLOCK — FAILED (RT MLG) · airframe 29,088 hrs · 26,943 cycles

RIGHT MAIN GEAR DID NOT EXTEND WHEN SELECTED DOWN. (FLT 6024) REPLACED RIGHT UPLOCK ASSEMBLY. P/N 17051-101 S/N OFF DCL4549605.

Part: CIRCUIT BREAKER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 28,933 hrs · 26,816 cycles

THE 'EMERGENCY LIGHTS' DISPLAYED ON STATUS MESSAGE. (FLT 6583) RESET CIRCUIT BREAKER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,814 hrs · 26,723 cycles

MOST AFT EMERGENCY CEILING LIGHT INOP. (FLT 6094) RELAMPED EMERGENCY LIGHT.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 28,814 hrs · 26,723 cycles

NOSE DOOR CYCLED OPEN AND CLOSE WITHOUT PILOT INPUT DURING TAXI. (FT 6426) REPLACED NLG DOOR SELECTOR VALVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,661 hrs · 26,591 cycles

OVERHEAD CEILING EMERGENCY LIGHT NR 3 INOP. (FLT 6014) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,427 hrs · 26,407 cycles

NR 1 EMERGENCY FLOOD LIGHT IN THE CEILING INOP. (FLT 5808) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,114 hrs · 26,135 cycles

NR 3 EMERGENCY CEILING LIGHT INOP. (FLT 6738) RELAMPED EMERGENCY LIGHT.

Part: HINGE — DIRTY (PAX DOOR) · airframe 28,068 hrs · 26,094 cycles

FLT 6311 - MAIN CABIN DOOR HARD TO OPEN. REMOVED DEBRIS LOWER HINGE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,670 hrs · 25,776 cycles

MULTIPLE EMERGENCY LIGHTS VERY DIM. (FLT 6069) REPLACED NR 1 ELBP.

Part: FRAME — CRACKED (BS 559 BULKHEAD) · airframe 28,089 hrs · 26,114 cycles

C-CHECK - FS 559 PRESSURE BULKHEAD FRAME CAP ANGLE RADIUS CRACKED. REPAIRED PER REO.

Part: BULKHEAD — GOUGED (BS 280) · airframe 28,089 hrs · 26,114 cycles

C-CHECK, FS 280 BULKHEAD GOUGED. REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,584 hrs · 25,703 cycles

EMERGENCY EXIT ROW LIGHT ON LEFT SIDE INOP. (FLT 6407) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — LOOSE (CABIN) · airframe 27,484 hrs · 25,617 cycles

LEFT SIDE EMERGENCY EXIT SIGN AT ROW 8 INOP. (FLT 6439) RESEATED CONNECTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,215 hrs · 25,397 cycles

NR 3 CEILING EMERGENCY LIGHT INOP. (FLT 5909) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,812 hrs · 25,065 cycles

EMERGENCY CEILING LIGHT INOP. (FLT 5944) RELAMPED CEILING LIGHT.

Part: WINDOW — CRACKED (COCKPIT) · airframe 26,559 hrs · 24,874 cycles

FLT 6399 - RIGHT SIDE WINDOW CRACKED. REPLACED WINDOW.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,460 hrs · 24,801 cycles

FLT 6512 - CEILING EMERGENCY LIGHT, SECOND FROM REAR IN CABIN, INOP. RELAMPED.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 26,408 hrs · 24,757 cycles

FLT 6631 - FLOOR EMERGENCY EXIT LIGHT BY RIGHT OVERWING EXIT INOP. REPLACED NR 3 INVERTER ON BATTERY CHARGER.

Part: CONTROLLER — FAILED (ANTI-ICE SYS) · airframe 26,352 hrs · 24,715 cycles

FLT 6306 - ANTI-ICE DUCT MESSAGE. REPLACED ANTI-ICE HEAT CONTROLLER, PN: 1151336-1 SN OFF: 062C-0116.

Part: UNKNOWN — SMOKE (CABIN) · airframe 26,134 hrs · 24,461 cycles

SMOKE REPORTED IN THE REAR OF THE PASSENGER CABIN. (FLIGHT NR 2811) INSPECTED AND RAN BOTH AIR CONDITIONING SYSTEMS. VERIFIED THAT THERE WAS NO SMOKE IN CABIN. OPS CHECK GOOD.

Part: PSEU — MALFUNCTIONED (NLG DOOR) · airframe 25,174 hrs · 23,521 cycles

RECEIVED "GEAR DISAGREE" AND "NOSE DOOR OPEN" WARNING MESSAGES, FLIGHT NR 2702. REPLACED PSEU IAW AMM 32-61-00. ALL CHECKS OK.

Part: STIFFENER — CRACKED (WING TO BODY) · airframe 25,424 hrs · 23,724 cycles

LEFT FUSELAGE TO WING STIFFENER IS CRACKED AT FS473.0 AND WL72.0, FOUND AT C-CHECK. REPLACED BRACKET ANGLE PER CRJ200 SRM 51-42-06 PG 2-4 AND SRM 51-42-21 PG 15-18.

Part: STRUCTURE — CORRODED (TE FLAP) · airframe 25,424 hrs · 23,724 cycles

LEFT INBOARD FLAP INTERIOR STRUCTURE HAS SIGNS OF CORROSION, FOUND AT C-CHECK. REPLACED FLAP ASSEMBLY PER CRJ200 AMM 57-52-08.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,424 hrs · 23,724 cycles

FS 280 AT LBL9 LOWER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED ALL REPAIR PARTS AT FS 280 AND LBL9 PER CRJ200 REO 601R-53-11-171.

Part: STIFFENER — CRACKED (WING TO BODY) · airframe 25,424 hrs · 23,724 cycles

LEFT FUSELAGE TO WING STIFFENER IS CRACKED AT FS 461.0 AND WL 72.0, FOUND AT C-CHECK. COMPLIED WITH REPAIRS AT FS 461.00 WL 72.0 IAW CRJ200 SRM 51-42-06, PG 18 PARA 11 AND SRM 51-42-21 PG 19 PARA 11.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,424 hrs · 23,724 cycles

STA 280 BEAM CRACK FOUND AT CENTER FLOORBEAM UPPER SUPPORT, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ200 SRM 51-42-06 PG 11.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,424 hrs · 23,724 cycles

FS 280 LBL 9 AND RBL 9 UPPER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED ALL REPAIR PARTS TO FS280 LBL/RBL9 UPPER FLOOR SUPPORT PER CRJ200 REO601R 53-11-136.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 25,424 hrs · 23,724 cycles

FORWARD FLOOR SUPPORT ANGLE AT STA 280 IS CORRODED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ200 SRM 51-44-04 FIG 6 AND 51-42-06 FIG 8.

Part: PIN — CORRODED (HORIZONTAL STAB) · airframe 25,424 hrs · 23,724 cycles

LEFT HORIZONTAL STABILIZER PIVOT PIN HAS CORROSION, FOUND AT C-CHECK. REPLACED STABILIZER PIVOT PIN AS REQUIRED PER CRJ200 AMM 55-10-00-000/400-801 SUBTASK 55-10-00-020/420-001.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,424 hrs · 23,724 cycles

FS 280 AT RBL 9 LOWER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED ALL REPAIR PARTS TO RBL 9 AND FS 280 LOWER FLOOR SUPPORT PER REO 601R-53-11-171.

Part: LOOP — FAULTY (FUSELAGE LT SIDE) · airframe 23,578 hrs · 22,244 cycles

FLIGHT 5204 - LT AND RT ANTI-ICE DUCT MESSAGE ON TAKEOFF ROLL. LT AND RT ANTI-ICE BLEED LOOPS SHORTED TO GROUND. REPLACED LT FUSELAGE BLEED LOOP. NO FURTHER DEFECTS.

Part: CONNECTOR — FAULTY (ANTI ICE SYS) · airframe 23,578 hrs · 22,244 cycles

FLIGHT 5204 - LEFT AND RIGHT ANTI-ICE DUCT MESSAGE ON TAKEOFF ROLL. LEFT AND RIGHT ANTI-ICE BLEED LOOPS SHORTED TO GROUND. REPLACED RIGHT AFT BAY BLEED LOOP CONNECTOR. NO FURTHER DEFECTS.

Part: WIRE — CHAFED (ANTI-ICE SYSTEM) · airframe 23,567 hrs · 22,234 cycles

FLIGHT 5104 - DURING TAKE-OFF ROLL RECEIVED AN ANTI-ICE DUCT CAUTION MESSAGE, ABORTED TAKE-OFF AND RETURNED TO THE GATE. REPAIRED CHAFED WIRING AT SENSOR SW25K IN THE LEFT WING AND REPOSITION TERMINAL LUG TO PREVENT CHAFING.

Part: UNKNOWN — UNKNOWN · airframe 23,553 hrs · 22,223 cycles

FLIGHT 5270 - ANTI-ICE DUCT MESSAGE ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. PERFORMED OPS CHECK OF WING ANTI-ICE SYSTEM, NO DEFECTS NOTED. OPS CHECK GOOD.

Part: SWITCH — FAULTY (LT WING) · airframe 23,504 hrs · 22,176 cycles

FLIGHT 5389 - ANTI-ICE DUCT WARNING MESSAGE AT 8000 FT. PERFORMED OPS CHECK OF ANTI-ICE SYSTEM, VISUAL CHECK OF FUSELAGE LOOPS AND OHMED WING SENSORS. NO FURTHER DEFECTS.

Part: THERMAL SWITCH — FAULTY (LT WING) · airframe 23,507 hrs · 22,180 cycles

FLIGHT 5141 - TAKEOFF WITH WING AND COWL ANTI-ICE ON, ANTI-ICE DUCT WARNING AT 100 KTS. MESSAGE EXTINGUISHED AS THRUST REDUCED. ABORTED TAKEOFF. REPLACED THERMAL SWITCH AT LEFT WS 250. NO FURTHER DEFECTS.

Part: SWITCH — FAULTY (LEFT WING) · airframe 23,267 hrs · 21,988 cycles

FLIGHT 5076 - ON TAKEOFF ROLL RECEIVED ANTI-ICE DUCT WARNING MESSAGE, ABORTED TAKEOFF. REMOVED AND REPLACED THERMAL SWITCH ON LEFT WING.

Part: ACTUATOR — FAULTY (RT I/B FLAP) · airframe 22,698 hrs · 21,535 cycles

FLIGHT 5275 - FLAPS FAIL CAUTION MESSAGE CAME ON WHEN FLAP SELECTOR WAS MOVED FROM 30 TO 45 DEGREES. REMOVED AND REPLACED RIGHT I/B FLAP O/B ACTUATOR.

Part: ACTUATOR — FAULTY (RT I/B FLAP) · airframe 22,698 hrs · 21,535 cycles

FLIGHT 5275 - FLAPS FAIL CAUTION MESSAGE CAME ON WHEN FLAP SELECTOR WAS MOVED FROM 30 TO 45 DEGREES. REMOVED AND REPLACED RIGHT I/B FLAP I/B ACTUATOR.

Part: FLAP — MALFUNCTIONED (WING) · airframe 22,687 hrs · 21,526 cycles

FLIGHT 5000- FLAPS FAIL AT 30 DEGREES WHEN 45 DEGREES SELECTED ON FINAL. 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: ACTUATOR — FAULTY (TE FLAPS) · airframe 22,690 hrs · 21,527 cycles

FLIGHT 5300 - FLAPS FAILED AT 30 DEGREES WHEN FLAPS SET TO 30 DEGREES ON FINAL. REMOVED AND REPLACED RIGHT OUTBOARD FLAP OUTBOARD ACTUATOR.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 22,531 hrs · 21,403 cycles

FLIGHT 5453 - DURING CLIMBOUT OF TYS RECEIVED A SPOILERON FAULT MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. PERFORMED RESET OF THE SPOILERON ELECTRONIC CONTROL UNIT.

Part: CLIP — CRACKED (FUSELAGE) · airframe 22,186 hrs · 21,136 cycles

CLIP CRACKED AT INTERCOSTAL AT FS 625 TO REAR PRESSURE BULKHEAD, RT SIDE 3 O'CLOCK POSITION. REMOVED AND REPLACED FS 625 INTERCOSTAL CLIP IAW SRM 51-42-06 AND 51-42-21.

Part: CLIP — CRACKED (FUSELAGE) · airframe 22,186 hrs · 21,136 cycles

CLIP CRACKED AT INTERCOSTAL FS 615 TO REAR PRESSURE BULKHEAD, LEFT SIDE 9 O'CLOCK POSITION. REMOVED AND REPLACED INTERCOSTAL CLIP IAW SRM 51-42-06 AND 51-42-21.

Part: WARNING LIGHT — ILLUMINATED (ANTI ICE DUCT) · airframe 21,404 hrs · 20,481 cycles

FLIGHT 4940 - DURING TAKEOFF ROLL RECEIVED AN ANTI ICE DUCT WARNING MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED GROUND RUNS AND TAXIED AIRCRAFT, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE.

Part: LIGHT — UNRELIABLE (CABIN FLOOR) · airframe 21,229 hrs · 20,320 cycles

FLIGHT 5173 - ROW 1 EMERGENCY FLOOR LIGHT IS INOPERABLE. REPLACED THE POWER STRIP AT ROW 1.

Part: PRIORITY VALVE — FAULTY (MLG) · airframe 20,981 hrs · 20,131 cycles

FLAP 5100 - EN ROUTE RSW-CVG, RECEIVED A GEAR DISAGREE WHEN GEAR WAS LOWERED, ABORTED FIRST APPROACH AT CVG, THEN LANDED WITHOUT INCIDENT ON SECOND ATTEMPT. REPLACED THE MLG PRIORITY VALVE.

Part: PRIORITY VALVE — UNRELIABLE (NLG) · airframe 20,981 hrs · 20,131 cycles

FLIGHT 5100 - GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE.

Part: SEAL — FOD (PAX DOOR) · airframe 20,426 hrs · 19,661 cycles

FLIGHT 5154 - AIRCRAFT WILL NOT PRESSURIZE. AIR LEAK AT CABIN DOOR. REMOVED FOD FROM DOOR AND REPLACED DAMAGED DOOR SEAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,427 hrs · 17,060 cycles

FLIGHT 5682 OVERHEAD EMERGENCY LIGHT AT ROW 11 IS INOPERATIVE. DEFERRED MAINT IAW MEL.

Part: FLAP — MALFUNCTIONED (WING) · airframe 16,898 hrs · 16,618 cycles

FLIGHT 5746 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01.

Part: PRESSURE SWITCH — MALFUNCTIONED (NLG STEERING) · airframe 16,100 hrs · 15,921 cycles

FLIGHT 5262 NWS FAILED MESSAGE DURING GEAR EXTENSION. COULD NOT DUPLICATE. REPLACED THE STEERING PRESSURE SWITCHES.

Part: IDG — INOPERATIVE (LT ENGINE) · airframe 16,058 hrs · 15,884 cycles

FLIGHT 5406 LT ENGINE IDG AND GENERATOR CAUTION MESSAGE. REPLACED THE IDG.

Part: CONTROLLER — STICKING (ELEVATOR) · airframe 14,498 hrs · 14,559 cycles

FLIGHT 5050 ELEVATOR CONTROL STICKING TWICE DURING APPROACH. COULD NOT DUPLICATE. INSPECTED ELEVATOR CONTROL SYSTEM AND FOUND NO DEFECTS.

Part: WINDOW — CRACKED (R/H) · airframe 13,433 hrs · 13,610 cycles

FLIGHT 5774 COPILOTS SIDE WINDOW CRACKED.REPLACED WINDOW.

Part: PRIORITY VALVE — UNRELIABLE (NLG) · airframe 12,999 hrs · 13,219 cycles

FLIGHT 5819 GEAR DISAGREE WARNING WHEN SELECTED DOWN.REPLACED THE NLG PRIORITY VALVE.

Part: FLAP · airframe 12,725 hrs · 12,975 cycles

FLIGHT 5072 FLAPS FAILED AT 26 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: VALVE — MALFUNCTIONED (L/H) · airframe 12,697 hrs · 12,949 cycles

FLIGHT 5207 L/H AC HIGH PRESSURE WARNING DURING T/O.REPLACED THE L/H PRSOV.

Part: PITOT HEAD · airframe 12,635 hrs · 12,875 cycles

FLIGHT 5369 LT PITOT AND AOA HEAT CAUTION MESSAGE.COULD NOT DUPLICATE RESET SYSTEM AND OPS NORMAL.

Part: FLAP · airframe 12,038 hrs · 12,317 cycles

FLIGHT 5922 DURING LANDING AT CVG RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREE FLAP POSITION.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 FURHTER FLAP CAUTION MESSAGES.

Part: ANGLE — CRACKED (FS 621) · airframe 11,583 hrs · 11,859 cycles

FS 621 FLOOR SUPPORT ANGLE CRACKED WL 73.50 RBL 41.COMPLIED WITH REO 601R-53-61-117 REV A AND WVAC EO 601R-53-3339. LOCATED AND INSTALLED ANGLES 601R53-61-004-2, 601R53-61-004-6 AND 601R53-61-004-4. INSTALLED FABRICATED RADIUS BLOCK IAW REO 601R-53-3339.

Part: LAVATORY · airframe 10,798 hrs · 11,070 cycles

FLIGHT 5091 LAVATOR SMOKE WARNING - F/A CONFIRMED SMOKE PRESENT.COULD NOT DUPLICTE. CHECKED ALL LAV SYSTEM - NO SMOKE NOTED.

Part: SERVICE DOOR · airframe 10,009 hrs · 10,228 cycles

FLIGHT #5363 - STALL FAIL MESSAGE AFTER T/O.FOUND 02 SERVICE DOOR OPEN WHICH DISRUPTED AIR FLOW OVER THE #2 AOA VANE. CLOSED AND LATCHED DOOR.

Part: LAMP — INOPERATIVE (CABIN FLOOR) · airframe 9,686 hrs · 9,902 cycles

FLIGHT #5832. EMERGENCY FLOOR PATH LIGHTING IS INOP ROWS 2 THRU 6.REPLACED THE #2 FLOOR LIGHT STRIP.

Part: ACTUATOR — LEAKING · airframe 9,325 hrs · 9,509 cycles

FLAP FAIL CAUTION MESSAGE AT 38 DEGREE FLAP POSITION DURING APPROACH INTO CVG.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B)3 (D AND E) 4. REPLACED OUTBOARD FLAP ACTUATOR.

Part: ACTUATOR — BINDING · airframe 9,325 hrs · 9,509 cycles

FLAP FAIL CAUTION MESSAGE AT 38 DEGREE FLAP POSITION DURING APPROACH INTO CVG.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 3(D AND E)4. REPLACED INBOARD FLAP ACTUATOR.

Part: FLAP · airframe 9,325 hrs · 9,508 cycles

FLAPS FAILED AT 38 DEGREES.INSPECTED FLAP SYSTEM PER AD 98-20-01 - NO FAUTLS FOUND. LUBRICATED FLAP ACTUATORS.

Part: FIRE BOTTLE — LOW (CARGO BAY) · airframe 9,240 hrs · 9,416 cycles

CARGO FIRE BOTTLE LOW MESSAGE. REPLACED THE FIRE BOTTLE.

Part: BRACKET — BENT (NLG) · airframe 8,675 hrs · 8,834 cycles

LANDING GEAR DISAGREE MESSAGE. REPLACED BENT PROXIMITY SENSOR BRACKET ON NLG STRUT.

Part: ENGINE — FAILED (RIGHT) · airframe 8,369 hrs · 8,528 cycles

RIGHT ENGINE FAILED, HIGH N1 VIB AND ZERO OIL PRESSURE. REPLACED ENGINE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 7,684 hrs · 7,818 cycles

FRAME AT FS 718.00 RT IS CRACKED AT STR 11 - 12. REPAIRED FRAME AT FS 718.00 RT, STR 11 - 12 IAW REO 601R-53-61-193, REV A.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 7,684 hrs · 7,818 cycles

SMALL HOLE FOUND IN BELLY SKIN 2.0 INCHES AFT OF FS 654.0 BETWEEN STR 27 CL AND STR 26 RT. PEFORMED MAJOR REPAIR BY CUTTING AWAY DAMAGED AREA, FABING EXTERNAL DOUBLER AND INSTALLING IAW WVAC EO 601R-53-1534A.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 7,661 hrs · 7,794 cycles

LEFT HAND AND RIGHT HAND SIDE FS 718.00 DOUBLERS BETWEEN STR 11 AND 12 CRACKED. INSTALLED NEW DOUBLERS IAW CANADAIR REO 601R-53-61-193 REV A.

Part: SKIN — DENTED (FUSELAGE) · airframe 7,661 hrs · 7,794 cycles

FUSELAGE SKIN DAMAGE AT FS 310.00 BY LOWER PASSENGER DOOR LATCH PIN. PEFROMED A MAJOR REPAIR TO DAMAGED SKIN AT FS 310.0 IAW CRJ REO 601R-53-21-180.

Part: CONTROL PANEL — INOP (COCKPIT)

AILERON TRIM IS INOPERABLE. REPLACED TRIM PANEL.

Part: STRIKER — DAMAGED (PASSENGER DOOR)

PASSENGER DOOR SEAL STRIKER AT FS 310 DAMAGED. REPAIRED IN ACCORDANCE CRJ REO 601R-52-11-008 ISSUE B REPAIR A.

Part: ANGLE — CRACKED (BS 621)

AIRCRAFT CAME IN FOR 24 MONTH CHECK WITH DMI 205443 FLOOR SUPPORT ANGLE AT FS 621.0 LHS CRACKED. REMOVED AND REPLACED FLOOR SUPPORT ANGLE AT FS 621.0 (P/N 601R-53-61-117) IAW CRJ REO 601R53-61-117 ATTACHED.

Part: STRIKER — DAMAGED (PASSENGER DOOR)

PASSENGER DOOR SEAL STRIKER AT FS 310.349 DAMAGED. REPAIRED IN ACCORDANCE WITH CRJ REV 601R-52-11-008 ISSUE B REPAIR A.

Part: ANGLE — CRACKED (BS 621)

FLOOR SUPPORT ANGLE AT FS 621 IS CRACKED. REPLACED LEFT HAND FLOOR SUPPORT ANGLE AT FS 6210 IN ACCORDANCE WITH CRJ REO 601R-53-61-117A.

Part: UPLOCK — MALFUNCTIONED (NLG)

NOSE GEAR SLAMS VERY LOUDLY INTO GEARWELL WHEN RETRACTED. REMOVED AND REPLACED NLG UPLOCK ASSEMBLY.

Part: FLEXSHAFT — SEPARATED (RT TE FLAP)

DURING C-CHECK, FOUND RIGHT WING NR 5 FLEXSHAFT UNSERVICEABLE DUE TO STRAND SEPARATION. REPLACED FLEXSHAFT.

Part: CHECK VALVE — LOOSE (APU)

DURING C-CHECK, FOUND APU AIR SUPPLY CHECK VALVE UPPER PIN EXTREMELY LOOSE. REPLACED VALVE.

Part: DAMPENER — LEAKING (LT ELEVATOR)

DURING C-CHECK, FOUND LEFT INBOARD ELEVATOR FLUTTER DAMPENER TO BE LEAKING. REPLACED FLUTTER DAMPENER.

Part: LAMP — FAILED (CABIN)

LOW PRESSURE WARNING, HYDRAULIC SYSTEM NR 1. REPLACED LEAKING LINE ASSY IN AFT EQUIPMENT BAY.

Part: SPEED CONTROL — MALFUNCTIONED (LT ENGINE)

LT ENGINE WOULD ACHIEVE ONLY 76 PERCENT N1 DURING TAKEOFF. ENGINEELECTRONIC SPEED CONTROL SYSTEM PLACED ON DEFERRED MAINTENANCE LIST.