N988CA

Part: PUMP — FAILED (HYD SYSTEM) · airframe 39,856 hrs · 35,709 cycles

NOSE GEAR DISAGREE WARNING MESSAGE DURING GEAR RETRACTION. R & R HYDRAULIC SYSTEM 3A PUMP IAW AMM. OPS AND LEAK CHECK GOOD. PERFORMED EXTENSION/RETRACTION OPS CHECK OF LANDING GEAR IAW AMM. NO DEFECTS OR MSGS SHOWN. OPS CHECKED GOOD.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 39,774 hrs · 35,648 cycles

SMOKE IN FLIGHT DECK. RETURNED TO FIELD. RAN ACFT AT HIGH POWER SETTING WITH BOTH PACKS ON FOR 30 MINUTES. NO SMOKE IN CABIN OR COCKPIT NOTED IAW AMM. ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE INDICATION (MLG) · airframe 39,617 hrs · 35,516 cycles

AIRCRAFT RETURNEDTO FIELD WITH A NOSE GEAR DISAGREE AND NOSE DOOR WARNING. MX JACKED ACFT AND PERFORMED THE FIM TROUBLESHOOTING. NO FAULTS FOUND.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 38,956 hrs · 34,958 cycles

EXIT LIGHT SEAT 8A INOPERATIVE. R & R NR 2 EMERGENCY LIGHT INVERTER IAW AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,729 hrs · 34,795 cycles

EMERGENCY LIGHT INOPERATIVE ON RT SIDE ABOVE THE REFUEL/DEFUEL CONTROL PANEL. R & R THE BULB IAW AMM.

Part: SERVO — FAILED (AUTOPILOT SYS) · airframe 37,667 hrs · 33,963 cycles

AUTOPILOT PITCHES UP & DOWN AGGRESSIVELY WHEN ENGAGED DURING CLIMB OUT. HAD TO DISENGAGE IMMEDIATELY & HAND FLY WITH AUTOPILOT OFF. FLT 5370 FOUND THE ELEVATOR SERVO WAS MOVING THE FLIGHT CONTROLS IN THE OPPOSITE DIRECTION FROM WHICH THEY WERE COMMANDED. REPLACED THE ELEVATOR SERVO. PN 622-5027-101, SN ON 1KROH & SN OFF 1NT2R.

Part: SKIN — DENTED (RT WING) · airframe 36,741 hrs · 33,233 cycles

DENT AT WING STATION 264 ON RT LE. C-CHECK REPLACED LE SKIN 630KL IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 36,741 hrs · 33,233 cycles

RT FLOOR SUPPORT STRAP AT FS559 RBL 36 HAS CORROSION. C-CHECK REPLACED FLOOR SUPPORT STRAP IAW SRM.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 36,741 hrs · 33,233 cycles

RT WING MIDDLE LE SKIN CRACKED. C-CHECK REPLACED LE SKIN PANEL IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 36,741 hrs · 33,233 cycles

FS 605 FLOOR BEAM UNDER CARGO DOOR THRESHOLD CRACKED AT LBL 42.00, WL 73.00. C-CHECK REPAIRED FLOOR BEAM IAW REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,741 hrs · 33,233 cycles

CRACK FOUND ON CLIP ON FS 605 AT CARGO DOOR UNDER FLOOR LEVEL. C-CHECK REPLACED CLIP IAW SRM. PN 601R35011-13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,741 hrs · 33,233 cycles

FLOOR BEAM BETWEEN BEAM & CARGO DOOR THRESHOLD IS CORRODED AT FS605. C-CHECK BLENDED CORROSION IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,741 hrs · 33,233 cycles

FS280 FWD FLOOR SUPPORT CRACKED AT RT CORNER RADIUS. C-CHECK REPLACED FWD FLOOR SUPPORT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,741 hrs · 33,233 cycles

NLG WW SKIN CUT OUT IS CRACKED AT AFT LT RADIUS. C-CHECK REPAIRED IAW REO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 36,741 hrs · 33,233 cycles

PRESSURE FLOOR HAS TWO CRACKS AT FS 459 LBL9 & RBL 9 CENTER FLOOR BEAM. C-CHECK REPAIRED IAW REO.

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 36,741 hrs · 33,233 cycles

FWD CARGO THRESHOLD HAS CRACK AT KICK PLATE. C-CHECK REPLACED CARGO THRESHOLD SILL IAW REO. PN 601R35011-63.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 36,741 hrs · 33,233 cycles

RT SUBFLOOR & DOUBLERS UNDER FLOOR PANEL 262DRF IS CORRODED. C-CHECK REMOVED THE CORROSION IAW REO.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 36,741 hrs · 33,233 cycles

LT SIDE SUBFLOOR & DOUBLERS UNDER FLOOR PANEL 262DLF HAS CORROSION. C-CHECK REMOVED CORROSION IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 36,741 hrs · 33,233 cycles

CRACK ON FS 621 AFT PRESSURE BULKHEAD FWD FACE AT WL131.00 LBL27.50. C-CHECK REPAIRED IAW REO 601R-53-61-1541.

Part: SILL — CORRODED (FUSELAGE) · airframe 36,741 hrs · 33,233 cycles

RBL 36 FS 559+80 TO559+112 WL 73.00 FLOOR SILL HAS CORROSION. C-CHECK REPLACED FLOOR SILL IAW SRM. PN 601R31133-86

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,741 hrs · 33,233 cycles

LBL 9 FS 280 INBD & OTBD CLIPS ARE CRACKED. C-CHECK REPLACED IAW REO. PN S6144-14.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,741 hrs · 33,233 cycles

RBL 9 FS 280 INBD & OTBD CLIPS ARE CRACKED. C-CHECK REPLACED IAW REO.

Part: DOOR — CHAFED (LT MLG) · airframe 36,741 hrs · 33,233 cycles

LT MLG DOOR FWD EDGE HAS CHAFFING. C-CHECK REPAIRED IAW REO.

Part: DOOR — CHAFED (LT MLG) · airframe 36,741 hrs · 33,233 cycles

LT MLG DOOR HAS CHAFFING AT FWD EDGE OF GEAR DOOR. C-CHECK REPAIRED IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 36,741 hrs · 33,233 cycles

RT AILERON UPPER LE HAS CHAFFING FROM CTR HINGE TO OTBD HINGE. C-CHECK REPAIRED IAW REO.

Part: UNKNOWN — SMOKE (CABIN) · airframe 36,093 hrs · 32,723 cycles

CABIN FILLED WITH SMOKE WHILE SITTING AT GATE. (SERVICE) RAN PACKS ON APU OR ENGINE BLEEDS. FOUND NO SMOKE/SMELL IN CABIN COULD NOT DUPLICATE DISCREPANCY, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,988 hrs · 32,634 cycles

NR 3 OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 6235) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,835 hrs · 32,531 cycles

NR 4 AFT EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 7394) RELAMPED EMERGENCY LIGHT.

Part: LATCH — LACK OF LUBE (CABIN DOOR) · airframe 35,724 hrs · 32,430 cycles

MAIN CABIN DOOR LATCH IS DIFFICULT TO OPERATE. (FLT 4534) LUBRICATED MAIN CABIN DOOR LATCH.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,284 hrs · 32,051 cycles

NR 3 EMERGENCY CEILING OVERHEAD LIGHT BURNED OUT. (FLT 6532) RELAMPED EMERGENCY LIGHT.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 34,811 hrs · 31,666 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN FROM OUTSIDE. (FLT 5657) COMPLIED WITH MAIN CABIN DOOR LUBE IN REFERENCE TO AMM.

Part: SIGN — BROKEN (CABIN) · airframe 34,650 hrs · 31,545 cycles

EMERGENCY EXIT SIGN ON BULKHEAD NEAR SEAT 1B IS BROKEN. (FLT 6249) INSTALLED NEW SCREW INTO EMERGENCY LIGHT ASSEMBLY NEAR SEAT 1B IN REFERENCE TO CRJ 200 AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,668 hrs · 30,637 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5588) RELAMPED EMERGENCY LIGHT.

Part: SQUIB — UNWANTED DEPLOY (ADG) · airframe 33,487 hrs · 30,494 cycles

ADG AUTO DEPLOY SQUIB INADVERTENTLY DEPLOYED. (SERVICE) REPLACED SQUIB. P/N OFF: 055046B SN OFF: 3497

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,304 hrs · 30,340 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7770) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,160 hrs · 30,217 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 8549) RELAMPED EMERGENCY LIGHT.

Part: BRACKET — BENT (NLG) · airframe 33,055 hrs · 30,144 cycles

NOSE GEAR FAILED TO RETRACT AFTER TAKEOFF. (FLT 6492) REPLACED NLG BRACKET AND ADJUSTED PROXIMITY SENSOR.

Part: POST — CRACKED (FUSELAGE) · airframe 32,580 hrs · 29,765 cycles

C-CHECK, FS 409+128 RBL 18 VERTICAL POST CRACKED AT OUTBOARD AFT RADIUS. REPLACED PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,789 hrs · 30,749 cycles

FS 333.0 FRAME MEMBER CORRODED. (C-CHECK) REPLACED FRAME MEMBER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,580 hrs · 29,765 cycles

C-CHECK, FS 574 FRAME CORRODED FROM STRINGER 26L TO 26R. REPLACED FS574 FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,789 hrs · 30,749 cycles

STA 349 FLOORBEAM RIGHT OUTBOARD SIDE HAS CORROSION ON UPPER FLANGE. (C-CHECK) REPAIRED IAW CRJ200 SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,442 hrs · 29,633 cycles

NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 2893) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,392 hrs · 29,579 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2966) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,262 hrs · 29,443 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2845) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,262 hrs · 29,443 cycles

NR 2 CEILING LEVEL EMERGENCY LIGHT IS OUT. (FLT 2855) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,197 hrs · 29,377 cycles

RIGHT SIDE AFT EXTERIOR AND NR 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 2974) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,092 hrs · 29,269 cycles

LAST EMERGENCY OVERHEAD LIGHT IS OUT. (FLT 2974) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,714 hrs · 28,888 cycles

AFT EMERGENCY CEILING LIGHT IS OUT. (FLT 6677) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,687 hrs · 28,869 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7012) RELAMPED EMERGENCY LIGHT.

Part: SKIN — CRACKED (WING) · airframe 31,145 hrs · 28,406 cycles

CRACK ON THE LOWER WING SKIN NEAR WS 148.018 IN THE AREA OF THE REAR SPAR. (SERVICE) REPAIRED PER REO.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,972 hrs · 27,384 cycles

EMERGENCY LIGHT INOPERATIVE AT SERVICE DOOR. (FLT 6293) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,954 hrs · 27,371 cycles

MAIN CABIN DOOR FLOOR LEVEL EMERGENCY FLOOD LIGHT HAS A LIGHTBULB BURNED OUT. (FLT 6883) RELAMPED EMERGENCY LIGHT.

Part: ENGINE — FAILED (NR 2) · airframe 29,187 hrs · 26,734 cycles

NR 2 ENGINE FAILED ON TAKEOFF CLIMB. (FLT 5863) REPLACED NR 2 ENGINE. P/N ON CF34-3B1, S/N OFF 807246C.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,960 hrs · 26,557 cycles

EMERGENCY EXIT ROW EMERGENCY LIGHT INOP. (FLT 4646) REPLACED INVERTERS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,588 hrs · 26,241 cycles

LEFT WING FORWARD EMERGENCY EXIT LIGHT INOP. (FLT 6333) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 28,232 hrs · 25,949 cycles

FLT 6621 - NR 1 EMERGENCY CEILING LIGHT INOP. RELAMPED.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 28,247 hrs · 25,962 cycles

FS 280 RIGHT SIDE BULKHEAD GOUGED. (C CHECK) REPAIRED PER REO.

Part: ISOLATOR — CRACKED (FUSELAGE) · airframe 28,247 hrs · 25,962 cycles

FIVE CRACKED ISOLATORS ON AFT PRESSURE BULKHEAD FS 621. (C CHECK) REPLACED PER SRM.

Part: DOOR — STUCK (CABIN) · airframe 27,145 hrs · 25,034 cycles

MAIN CABIN DOOR WOULD NOT OPEN. (FLT 5977) INSPECTED DOOR, OPERATIONAL CHECK GOOD.

Part: PIN — OUT OF POSITION (CABIN DOOR) · airframe 26,965 hrs · 24,897 cycles

UNABLE TO OPEN MAIN DOOR FROM THE INSIDE. (FLT 6683) REPOSITIONED PRESSURE RELIEF FLAP OUTER PLUNGER PIN.

Part: FASTENER — LOOSE (PAX DOOR) · airframe 26,856 hrs · 24,808 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6676) RETORQUED HARDWARE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,321 hrs · 24,402 cycles

FLT 5801 - NR 2 CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED.

Part: SIGN — BURNED OUT (EMERGENCY LIGHTS) · airframe 25,670 hrs · 23,885 cycles

RIGHT LOWER EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. REPLACED RIGHT LOWER EMERGENCY EXIT SIGN.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 24,900 hrs · 23,053 cycles

STA 280 FLOOR SUPPORT IS CRACKED JUST OUTBOARD OF LBL 9, FOUND AT C-CHECK. COMPLETED REPAIR IAW BOMBARDIER REO 601R-53-11-136A.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 24,900 hrs · 23,053 cycles

FS 484 AT RBL 36 IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIR IAW BOMBARDIER REO 601R-53-41-059, STEPS 11-14.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,900 hrs · 23,053 cycles

FS 280 FLOOR SUPPORT BETWEEN LBL 9 AND RBL 9 IS CORRODED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS IAW CRJ 200 SRM 57-42-06 AND 51-40-11.

Part: SWITCH — LACK OF LUBE (PAX DOOR) · airframe 24,478 hrs · 22,645 cycles

FLIGHT 4956 - OVERBOARD COOL CAUTION ON CLIMBOUT. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. CLEANED AND LUBRICATED PAX DOOR OUTER HANDLE MICRO SWITCH DI 13. OPS CHECK GOOD.

Part: HOSE — FAILED (HYD SYSTEM) · airframe 23,844 hrs · 22,126 cycles

FLIGHT 5228 - HYDRAULIC 2 LOW PRESS CAUTION MESSAGE WITH 0 PRESS AND 0 QTY. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED NR 2 HYD SYS HOSE.

Part: LINE — FAILED (HYDRAULIC SYS) · airframe 23,844 hrs · 22,126 cycles

FLIGHT 5228 - HYDRAULIC LOW PRESS CAUTION MESSAGE WITH 0 PRESS AND 0 QTY. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED NR 2 HYD SYS LINE.

Part: TARGET — MISSING (RT NLG DOOR) · airframe 23,255 hrs · 21,622 cycles

NOSE DOOR OPEN WARNING MSG ILLUMINATED. DURING GEAR EXTENSION, MSG PERSISTED AFTER CYCLING OF GEAR. FOUND RIGHT NOSE DOOR PROX SENSOR TARGET MISSING, INSTALLED NEW TARGET.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 22,235 hrs · 20,801 cycles

FLIGHT 5238 - RECEIVED A GROUND SPOILER FAULT DURING TAKEOFF ROLL, ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED A RESET OF SECU NR 1 AND NR 2.

Part: FLAP SYSTEM — WARNING LIGHT (TE FLAPS) · airframe 20,133 hrs · 19,121 cycles

FLIGHT 5616 - RECEIVED A FLAP FAIL CAUTION MESSAGE INBOUND TO YYZ, FLIGHT LANDED WITHOUT INCIDENT. 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 — UNRELIABLE (RIGHT) · airframe 20,118 hrs · 19,109 cycles

FLIGHT 5667- FLAPS FAIL CAUTION. REPLACED THE RT BPSU.

Part: HOSE — LEAKING (LT ENGINE) · airframe 19,098 hrs · 18,236 cycles

FLIGHT 5234 - NR 1 HYDRAULIC SYSTEM CAUTION. REPLACED LEAKING HYDRAULIC LINE.

Part: LANDING GEAR — LACK OF LUBE (NOSE) · airframe 17,860 hrs · 17,139 cycles

FLIGHT 5843 GEAR DISAGREE WARNING. CLEANED AND LUBED NLG. RETRACTION CHECKS NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 17,460 hrs · 16,764 cycles

RIGHT HAND NLG AFT FUSELAGE SKIN CRACKED AT RADIUS. REPAIRED IAW REO 601R-53-11-048.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,460 hrs · 16,764 cycles

RIGHT HAND FUSELAGE 718.00 CRACKED AT 2 LOCATIONS BETWEEN STRINGERS 10 AND 12. REPAIRED IAW EO 53-027.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,460 hrs · 16,764 cycles

LEFT HAND FUSELAGE 718 CRACKED BETWEEN STRINGER 11 AND 12. REPAIRED IAW EO 53-027.

Part: CONTROL UNIT — MALFUNCTIONED (ANTI SKID SYS) · airframe 16,873 hrs · 16,250 cycles

FLIGHT 5819 ANTI SKID CAUTION DURING LANDING. REPLACED THE ANTI SKID CONTROL UNIT.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 16,098 hrs · 15,628 cycles

FLIGHT 5282 EMERGENCY LIGHTS WILL NOT TEST. REPLACED THE EMERGENCY BATTERIES.

Part: CONTROLLER — MALFUNCTIONED (TE FLAPS) · airframe 15,383 hrs · 15,035 cycles

FLIGHT 5711 FLAPS FAIL WARNING. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: SENSOR — UNRELIABLE (RT WING OVERHEAT) · airframe 15,089 hrs · 14,788 cycles

FLIGHT 5429 WING OVERHEAT WARNING IFSD. REPLACED THE RIGHT WING OVERHEAT SENSOR.

Part: FLAP — MALFUNCTIONED (WING) · airframe 14,609 hrs · 14,384 cycles

FLIGHT 5073 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: DUCT — LEAKING (FUSELAGE) · airframe 13,969 hrs · 13,865 cycles

FLIGHT 5119 DURING CRUISE FLIGHT CABIN ALTITUDE WAS INCREASING, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE LEFT FUSELAGE SUPPLY (Y) DUCT.

Part: DUCT — CRACKED (CABIN) · airframe 13,968 hrs · 13,864 cycles

FLIGHT 5838 DURING CLIMB THE CABIN ALTITUDE INCREASED IN AUTO MODE FOLLOWED BY A RUMBLING NOISE, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE RIGHT 10TH FUSELAGE DUCT.

Part: CONTROLLER — FAULTY (AVIONICS BAY) · airframe 13,968 hrs · 13,864 cycles

FLIGHT 5834 DURING CRUISE FLIGHT THE AUTO PRESSURIZATION MODE FAILED CAUSING CABIN ALTITUDE INCREASE. REPLACED THE PRESSURIZATION CONTROLLER NR 2.

Part: WINDOW — CRACKED (COCKPIT) · airframe 12,756 hrs · 12,821 cycles

FLIGHT 5855 CO PILOTS SIDE WINDOW CRACKED. REPLACED WINDOW.

Part: CONTROLLER — FALSE INDICATION (AVIONICS) · airframe 12,162 hrs · 12,305 cycles

FLIGHT 9488 AFTER T/O ALL FIRE WARNINGS ON.REPLACED THE FIRE AND OVERHEAT CONTROL UNIT.

Part: DRIVE SHAFT — SHEARED (L/H #1) · airframe 11,490 hrs · 11,715 cycles

FLIGHT 5443 FLAPS FAIL CAUTION MESSAGE.REPLACED THE L/H #1 FLEX DRIVE SHAFT.

Part: COMPUTER — MALFUNCTIONED (AVIONICS) · airframe 11,064 hrs · 11,308 cycles

FLIGHT 5824 STAB TRIM AND MACH TRIM CAUTION MESSAGE.COULD NOT DUPLICATE. REPLACED THE HSTCU.

Part: ELEMENT — MALFUNCTIONED (R/H) · airframe 10,226 hrs · 10,475 cycles

FLIGHT 5413 ANTI-ICE DUCT WARNING DURING TAXI.REPLACED THE R/H MLG WHEEL WELL AREA BLEED AIR LEAK SENSING LOOP.

Part: AILERON · airframe 9,902 hrs · 10,168 cycles

FLIGHT 5375 ABORTED T/O DUE TO AILERON CONFIG WARNING.COULD NOT DUPLICATE. AILERON TRIM AND RIGGING FOUND SATISFACTORY.

Part: PRIORITY VALVE — MALFUNCTIONED (NLG) · airframe 9,702 hrs · 9,969 cycles

FLIGHT 5369 GEAR DISAGREE WARNING.REPLACED THE NLG PRIORITY VALVE.

Part: WIRE HARNESS — CHAFED (LT FUEL TANK) · airframe 9,234 hrs · 9,508 cycles

WHILE WORKING DEFERRED MAINTENANCE ON LT FUEL QUANTITY SYSTEM, FOUND THE FUEL LEVEL PROBE WIRE HARNESS, BETWEEN NR 3 PROBE AND CONNECTOR J3QB/P3QB CHAFING ON FUEL BAFFLE P/N 601R62359-1. REPLACED THE WIRE HARNESS.

Part: COMPUTER — MALFUNCTIONED (AVIONICS) · airframe 9,220 hrs · 9,496 cycles

FLIGHT 5581 CONFIG TRIM AND CONFIG SPOILERS SPOILERS WARNING DURING T/O.REPLACED THE #1 SECU.

Part: SPOILER · airframe 8,651 hrs · 8,915 cycles

FLIGHT 5872. TAKE-OFF ABORTED BECAUSE OF SPOILERON FAULT MESSAGE.COULD NOT DUPLICATE. RESET THE S.E.C.U. AND OPERATIONAL CHECK OF SPOILERON SYSTEM WAS NORMAL.

Part: IDG · airframe 8,510 hrs · 8,775 cycles

FLIGHT #5594. DURING TAKE OFF ROLL AT MKE GENERATOR #1 DROPPED OFF LINE ACCOMPANIED BY AN IDG CAUTION MESSAGE, ABORTED TAKE OFF AT 60 KNOTS AND RETURNED TO THE GATE.SERVICED THE #1 INTEGRATED DRIVE GENERATOR WITH OIL.

Part: SPOILER · airframe 8,347 hrs · 8,605 cycles

FLIGHT #5243. DURING TAXI OUT OF CVG RECEIVED A SPOILERON FAULT STATUS MESSAGE, AIRCRAFT RETUREND TO THE GATE.PERFORMED RESET OF SPOILERON SYSTEM.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 7,906 hrs · 8,110 cycles

STALL FAIL CAUTION MESSAGE DURING T/O. RESET THE STALL COMPUTER.

Part: ANGLE — DENTED (PAX DOOR) · airframe 7,512 hrs · 7,699 cycles

PAX DOOR SEAL STRIKER DAMAGED AT F.S. 310.00 AND F.S. 349.00, PERFORMED REPAIR TO PAX DOOR SEAL STRIKER AT F.S. 310.00 AND 349.00 BY INSTALLING REPAIR STRAPS AND APPLYING AERODYNMIC FILLER I/A/W CANADAIR REO 601R-52-11-008 ISSUE B REPAIR A.

Part: DOUBLER — CRACKED (A/C RECEPTICAL) · airframe 7,412 hrs · 7,589 cycles

AIRCRAFT POWER RECEPTACLE DOOR INTERNAL DOUBLER IS CRACKED AND HAS NUMEROUS DENTS.PERFORMED A MAJOR REPAIR TO THE AIRCRAFT POWER RECEPTACLE DOOR INTERNAL DOUBLER IAW WVAC E.O. 601R-53-1953.

Part: FRAME — CRACKED (FUSELAGE) · airframe 7,412 hrs · 7,589 cycles

F.S. 718.00 FRAME AND DOUBLER IS CRACKED BETWEEN STR. 11 AND STR 12 LEFT SIDE.REPAIRED F.S. 718.00 FRAME AND DOUBLER IAW CANADAIR REO 601R-53-61-193 REV A.

Part: LINK — WORN (RT AILERON) · airframe 6,829 hrs · 7,021 cycles

AIRCRAFT WANTS TO ROLL RIGHT. REQUIRES EXCESSIVE LWD TRIM. REPLACED WORN HARDWARE AT RIGHT HAND AILERON TO PCU CONNECTION.

Part: LIGHT — INOPERATIVE (ROW 8) · airframe 5,883 hrs · 6,067 cycles

EMERGENCY FLOOR LIGHT IS INOPERABLE AT ROW 8. REPLACED LIGHT STRIP.

Part: FRAME — CRACKED (BS 718)

FRAME AT FS 718.0 LHS STR 10-12 HAS AFT DOUBLER P/N 600-36030-31 IS CRACKED. PERFORMED A MAJOR REPAIR TO FRAME AFT DOUBLER AT FS 718.0 LHS STR 10-12 BY REPLACING DOUBLER IAW CRJ REO 601R-53-61-193A.

Part: SKIN — DENTED (BS 310)

FUSELAGE SKIN AT FS 31.00 STR 15-16 LHS DAMAGED BY CONTACT WITH PASSENGER DOOR BTM PIN. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN AT FS 310.00 STR 15-16 LHS IAW CRJ REO 601R-53-21-180 REV NC.

Part: STRIKER — DAMAGED (BS 310)

PAX DOOR SEAL STRIKER AT FS 310.00 STR 15-16 HAS PREVIOUS REPAIR DAMAGED IE SEALANT CRACKED AND DOUBLER BENT, DUE TO CONTACT WITH PASSENGER DOOR PIN. PERFORMED A MAJOR REPAIR TO PASSENGER DOOR SEAL STRIKER AT FS 310.00 STR 15-16 LHS IAW CRJ REO 601R-52-11-008 REV B.

Part: VALVE — MALFUNCTIONED (NLG DOORS)

LOUD PULSATING SOUND FROM NLG AREA. REPLACED THE NLG DOORS SELECTOR VALVE.

Part: HOUSING — CRACKED (APU TURBINE)

AFTER APU REMOVAL FOR MAINTENANCE FOUND TURBINE HOUSING CRACKED NEAR FUEL NOZZLE BOSSES. RETURNED TO ALLIED SIGNAL FOR REPAIR AND -3 MOD.

Part: WARNING — ACTIVATED (PAX DOOR)

DOOR WARNING AFTER TAKEOFF. INSPECTED DOOR AND DOOR WARNING SYSTEM. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — CONTAMINATED (CABIN)

FORWARD SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERATIVE. REMOVED WATER FROM WIRING CONNECTOR SYSTEM TEST NORMAL.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

CVL - FLT 5722 - CARGO SMOKE WARNING ON APPROACH, DISCHARGED CARGO FIRE EXTINGUISHER. REPLACED SMOKE DETECTOR AND BOTTLES. NO EVIDENCE OF FIRE. PART TC: 954. (X)

Part: CONNECTOR — CONTAMINATED (ROW 3-8)

EMERGENCY FLOOR LIGHTING ROWS 3 TO 8 IS INOPERABLE. DRIED MOISTURE AT FLOOR LIGHTING CONNECTORS, SYSTEM OPERATION NORMAL.

Part: VALVE — MALFUNCTION (RT ENGINE)

RIGHT ENGINE COWL ANTI-ICE MESSAGE. REPLACED ANTI-ICE VALVE.

Part: SWITCH — OUT OF ADJUST (NLG)

GEAR DISAGREE MESSAGE, NLG DID NOT RETRACT. ADJUSTED NLG WEIGHT ON WHEELS PROXIMITY SENSOR.

Part: DETECTOR — MALFUNCTIONED (CARGO)

CARGO SMOKE WARNING. FALSE WARNING, REPLACED SMOKE DETECTORS.

Part: LIGHTS — INOPERATIVE (CABIN)

ONE SECTION OF EMERGENCY FLOOR LIGHTING IS INOP. DEFERRED PER MEL.