N868CA

Part: NUT — UNSECURE (OVERHEAT LOOP) · airframe 38,863 hrs · 35,141 cycles

MLG BAY OVHT WARNING AFTER TAKEOFF AND INITIATING GEAR RETRACTION. MESSAGE WENT AWAY ABOUT 2 MINS LATER. DECLARED EMERGENCY AS A PRECAUTION AND LANDED NORMALLY. NO FURTHER WARNINGS. (FLT 4452) 06/14/2018 CLOSED RESECURED RT MLG BAY OVERHEAT LOOP MOUNTING NUT. OPS CHECK GOOD IAW AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,767 hrs · 35,046 cycles

CORROSION ON FLOORBEAM AT LBL 9 FS 559+96. (C-CHECK) 05/20/2018 COMPLIED WITH REPAIR IAW SRM.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 38,767 hrs · 35,046 cycles

CORROSION ON WARDROBE MOUNT SUPPORT PLATE AT APPROX FS 310 LBL18. (C-CHECK) 05/20/2018 REPLACED THE WARDROBE MOUNT SUPPORT PLATE AT APPROX FS310 LBL18 IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,767 hrs · 35,046 cycles

CORROSION ON FLOORBEAM AT RBL 9 FS574. (C-CHECK) 05/20/2018 INSTALLED NEW FLOORBEAM AT RBL FROM FS569-FS621 IAW REO AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,767 hrs · 35,046 cycles

CORROSION ON FLOORBEAM AT RBL 27 APPROX FS559+85. (C-CHECK) 05/20/2018 REPAIRED FLOORBEAM AT RBL.27 APPROX FS 559.85 IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,767 hrs · 35,046 cycles

CORROSION ON FLOORBEAM AT RBL 27 FROM FS605 TO FS589. (C-CHECK) 05/20/2018 REMOVED CORROSION FROM FLOORBEAM AT RBL 27 FROM FS589 TO FS605 COMPLIED WITH ALL STEPS OF REPAIR IAW REO.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 38,767 hrs · 35,046 cycles

CORROSION ON GALLEY MOUNT SUPPORT PLATE AT APPROX FS 295 RBL9. (C-CHECK) 05/20/2018 REPLACED THE GALLEY MOUNT SUPPORT PLATE AT APPROX FS 295 RBL9 IAW SRM.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 38,767 hrs · 35,046 cycles

CORROSION ON GALLEY MOUNT SUPPORT PLATE AT APPROX FS 355 RBL9. (C-CHECK) 05/20/2018 REMOVED AND REPLACED GALLEY FLOOR MOUNT PLATE AT FS 355 RBL 9.0 IAW SRM.

Part: FRAME — DAMAGED (BS 700) · airframe 35,455 hrs · 31,391 cycles

R & R FRAME SECTION AT FS 700, STR 5L-5R DUE TO DAMAGE AT APU INSTALLATION TOOLING ATTACH HOLE. R & R FRAME SECTION AT FS 700, STR 5L-5R IAW SRM.

Part: FLOOR PANEL — CORRODED · airframe 35,455 hrs · 31,391 cycles

CORROSION FOUND ON FLOOR PANEL AT RBL 36 AT FS 439 TO FS 461. CORROSION FOUND ON PRESSURE DECK, FLOOR SILL PANEL AT FS 439 TO FS 461 AT RBL 36 WAS BLENDED ON 4 EA SPOTS IAW REO.

Part: SKIN — DENTED (BS 677) · airframe 35,455 hrs · 31,391 cycles

DENT IN FUSELAGE EXTERIOR SKIN AT FS 677, STR 24R. REPAIRED DENT IN FUSELAGE EXTERIOR SKIN AT FS 677.0, STR 24R IAW STS EA.

Part: PLATE — CHAFED (PAX DOOR) · airframe 35,455 hrs · 31,391 cycles

PASSENGER DOOR BOTTOM STEP CLOSEOUT PLATE HAS CHAFING. REPLACED PLATE WITH NEW SERVICABLE PART IAW SRM.

Part: NOSE COWL — DENTED (RT NACELLE) · airframe 35,455 hrs · 31,391 cycles

LARGE DENT RT ENGINE COWL L/E FWD LOOKING AFT. R & R RT ENGINE NOSE COWL IAW SRM.

Part: RESERVOIR — FAILED (HYD SYSTEM) · airframe 35,408 hrs · 31,354 cycles

NOSE GEAR DID NOT EXTEND. RAN QRH, PERFORMED MANUAL EXTENSION. RECEIVED A GREEN NLG ICON. R & R NR 3 HYDRAULIC RESERVOIR IAW AMM. BLED NR 3 HYDRAULIC SYS IAW AMM. PERFORMED EXTENSIONS AND RETRACTIONS IAW AMM, OPS CHECK GOOD. NO LEAKS NOTED.

Part: UNKNOWN — SMOKE (CABIN/COCKPIT) · airframe 34,278 hrs · 30,141 cycles

RETURN TO FIELD DUE TO SMOKE IN THE CABIN AND COCKPIT, ALONG WITH LAVATORY SMOKE INDICATION. INSPECTED BOTH ENGINES FOR LEAKS AND LOOSE FITTINGS. INSPECTED LT AND RT PACK DUCTS AND CLAMPS. FOUND NO DEFECTS. PERFORMED POWER ASSURANCE RUNS. OPS CHECKED GOOD.

Part: SKIN — CHAFED (RT AILERON) · airframe 30,939 hrs · 26,917 cycles

RT AILERON UPPER SKIN L/E CHAFED. C-CHECK, R & R RT AILERON UPPER SKIN L/E IAW EA.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 30,939 hrs · 26,917 cycles

CORROSION FOUND ON SEAT TRACK AT RBL 9 BETWEEN BS 364-399.5. C-CHECK, R & R SEAT TRACK, IAW REO.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 30,939 hrs · 26,917 cycles

CORROSION FOUND ON SEAT TRACK AT LBL 9 BETWEEN BS 364-399.5. C-CHECK, R & R SEAT TRACK IAW REO.

Part: HINGE — GOUGED (LT WING TE FLAP) · airframe 30,939 hrs · 26,917 cycles

LEFT OTBD FLAP OTBD HINGE ARM ASSY GOUGED BY FOD AT LOWER HINGE BOLT LUG. C-CHECK, REPAIRED LT OTBD FLAP, OTBD HINGE ARM ASSY AT LOWER HINGE BOLT LUG IAW STS EA.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 30,939 hrs · 26,917 cycles

PAX DOOR THRESHOLD CORRODED AROUND PROXIMITY SWITCH, UNDER FLOOR AREA, BS 333.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 30,939 hrs · 26,917 cycles

PAX DOOR AFT THRESHOLD CUP CORRODED. C-CHECK, R & R AFT THRESHOLD CUP IAW SRM.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 30,939 hrs · 26,917 cycles

PAX DOOR FWD THRESHOLD CUP CORRODED. C-CHECK, R & R FWD PAX DOOR THRESHOLD CUP IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,939 hrs · 26,917 cycles

BS 280 FLOORBEAM IS CRACKED AT RBL 11, LOWER TEE. C-CHECK, REPAIRED FLOORBEAM IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 349-356) · airframe 30,939 hrs · 26,917 cycles

UPPER SURFACE OF LT FLOOR SUPPORT CORRODED FROM BS 349 - 356, LBL 36. C-CHECK, BLENDED CORROSION IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,939 hrs · 26,917 cycles

AFT FLOORBEAM TEE ANGLE IS CRACKED AT BS 280, RBL 9 AND LBL 9. C-CHECK, R & R FLOORBEAM TEE IAW SRM.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 30,939 hrs · 26,917 cycles

CORROSION ON UPPER SURFACE OF FLOORBEAM TEE BS 280 FROM LBL 9-RBL 9. C-CHECK, REPLACED IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,939 hrs · 26,917 cycles

RBL 9 INBD AND OTBD ANGLES CRACKED AT FS 280 FLOORBEAM. C-CHECK, REPAIRED IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,939 hrs · 26,917 cycles

BS 280 FLOORBEAM IS CRACKED AT LBL 11, LOWER TEE. C-CHECK, FLOORBEAM REPAIRED IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,939 hrs · 26,917 cycles

FS 280 FLOORBEAM IS CRACKED LBL 11 - RBL 11, UPPER TEE. C-CHECK, REPAIRED FLOORBEAM IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,939 hrs · 26,917 cycles

LBL 9 INBD AND OTBD ANGLES CRACKED AT FS 280 FLOORBEAM. C-CHECK, REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 30,939 hrs · 26,917 cycles

NUMEROUS AREAS OF CORROSION ON UPPER SURFACE OF RT FLOOR SUPPORT AND DOUBLERS BETWEEN BS 409+128 - 559, RBL 36. C-CHECK, BLENDED OUT CORROSION DAMAGE IAW REO.

Part: ANGLE — CRACKED (BS 625) · airframe 30,939 hrs · 26,917 cycles

ANGLE AT BS 625 HAS CRACK, STRINGER 13R, C-CHECK, R & R RT ANGLEIAW SRM.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 30,939 hrs · 26,917 cycles

CORROSION ON UPPER SURFACE OF SEAT TRACK BS 559+50, RBL 9. C-CHECK, REPLACED SEAT TRACK IAW SRM AND EA.

Part: FLOOR SUPPORT — CORRODED (BS 449) · airframe 30,939 hrs · 26,917 cycles

UPPER SURFACE OF FLOOR SUPPORT DOUBLER CORRODED AT BS 449.85, LBL 36. C-CHECK, BLENDED OUT CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 525) · airframe 30,939 hrs · 26,917 cycles

UPPER SURFACE OF FLOOR SUPPORT DOUBLER CORRODED AT BS 525, LBL 36. C-CHECK, BLENDED OUT CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 473.15) · airframe 30,939 hrs · 26,917 cycles

UPPER SURFACE OF FLOOR SUPPORT DOUBLER CORRODED AT BS 473.15, LBL 36. C-CHECK, BLENDED OUT CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 499) · airframe 30,939 hrs · 26,917 cycles

UPPER SURFACE OF FLOOR SUPPORT DOUBLER CORRODED AT BS 499, LBL 36. C-CHECK, BLENDED OUT DAMAGE IAW REO.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 30,939 hrs · 26,917 cycles

CORROSION ON UPPER SURFACE OF SEAT TRACK BS 559+64, RBL 9. C-CHECK, REMOVED SEAT TRACK FROM BS 559+16 - 559+118 AND REPLACED WITH NEW IAW SRM AND EA.

Part: FLOOR SUPPORT — CORRODED (BS 484) · airframe 30,939 hrs · 26,917 cycles

UPPER SURFACE OF FLOOR SUPPORT DOUBLER CORRODED AT BS 484, LBL 36. C-CHECK, BLENDED OUT DAMAGE IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 479) · airframe 30,939 hrs · 26,917 cycles

UPPER SURFACE OF FLOOR SUPPORT CORRODED AT BS 479, LBL 36. C-CHECK, BLENDED OUT CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 461) · airframe 30,939 hrs · 26,917 cycles

UPPER SURFACE OF FLOOR SUPPORT DOUBLER CORRODED AT BS 461 LBL 36. C-CHECK, BLENDED OUT CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 513) · airframe 30,939 hrs · 26,917 cycles

UPPER SURFACE OF FLOOR SUPPORT DOUBLER CORRODED AT BS 513, LBL 36. C-CHECK, BLENDED OUT DAMAGE IAW REO.

Part: ANGLE — CRACKED (BS 625) · airframe 30,939 hrs · 26,917 cycles

ANGLE CRACKED AT BS 625, S13L. C-CHECK, R & R ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 486) · airframe 30,939 hrs · 26,917 cycles

UPPER SURFACE OF FLOOR SUPPORT CORRODED AT BS 486, LBL 36. C-CHECK, BLENDED OUT CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 449) · airframe 30,939 hrs · 26,917 cycles

UPPER SURFACE OF FLOOR SUPPORT CORRODED AT BS 449, LBL 36. C-CHECK, BLENDED OUT CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 30,939 hrs · 26,917 cycles

CORROSION ON UPPER SURFACE OF FLOOR SUPPORT AT BS 559+80, RBL 15. C-CHECK, R & R FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 513) · airframe 30,939 hrs · 26,917 cycles

UPPER SURFACE OF FLOOR SUPPORT DOUBLER CORRODED AT BS 513, LBL 36. C-CHECK, BLENDED OUT CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 439) · airframe 30,939 hrs · 26,917 cycles

UPPER SURFACE OF FLOOR SUPPORT DOUBLER CORRODED AT BS 439, LBL 36. C-CHECK, BLENDED OUT CORROSION IAW REO.

Part: DOOR SILL — CORRODED (BS 574-621) · airframe 30,939 hrs · 26,917 cycles

NUMEROUS AREAS OF CORROSION AROUND NUTPLATES ON AFT CARGO DOOR SILL, UNDER SIDE FROM BS 574 - 621, LBL 36. C-CHECK, BLENDED OUT CORROSION IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 30,939 hrs · 26,917 cycles

RIGHT AILERON UPPER L/E SKIN CHAFED. C-CHECK, REPLACED SKIN IAW REO.

Part: PANEL — CRACKED (UNKNOWN) · airframe 30,939 hrs · 26,917 cycles

PANEL 221CLC IS CRACKED. C-CHECK, REPAIRED PANEL IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,114 hrs · 26,071 cycles

CNTR AISLE EMERGENCY OVERHEAD LIGHT AT ROW 10 IS BURNED OUT. FLT 2592 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,703 hrs · 25,655 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 5 IS BURNED OUT. FLT#2576 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,578 hrs · 25,531 cycles

EMERGENCY OVERHEAD POD LIGHT BURNED OUT. FLT#2611 RELAMPED.

Part: TRANSDUCER — FAILED (LT ENGINE) · airframe 29,500 hrs · 25,457 cycles

LT ENGINE OIL TEMPERATURE INDICATING RED. RETURNED TO SLC. FLT#2627 REPLACED LT ENGINE PRESSURE TRANSDUCER. PN ON OFF 601-50919-9 & SN ON OFF NSN

Part: AUDIO PANEL — FAILED (WARNING SYSTEM) · airframe 29,442 hrs · 25,402 cycles

AURAL CHIME WARNINGS. FLT#2660 REPLACED AUDIO WARNING PANELS. PN ON OFF 601R51732-1. PN ON OFF 601R51728-13

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,849 hrs · 24,807 cycles

LAST OVERHEAD EMERGENCY LIGHT IS BURNED OUT, RELAMPED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,986 hrs · 23,866 cycles

FORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE. (C-CHECK) INSTALLED DOUBLER REPAIR IAW REO.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 27,863 hrs · 23,734 cycles

GEAR DISAGREE MSG AFTER GEAR RETRACTION ON TAKEOFF. HEARD "THUMPING" NOISE FROM NOSE GEAR, PULLED MANUAL RELEASE HANDLE, GOT 3 DOWN & LOCKED, HAD FULL NWS ON LANDING. (FLT 2616) REPLACED THE NLG PRIORITY VALVE AND THE MLG SELECTOR VALVE IAW AMM. PERFORMED SEVERAL GEAR SWINGS WITH NO FAULT INDICATIONS NOTED. OPS CHECK GOOD. PN: 750005000 SN ON: 0219 SN OFF: 0655, PN: 4622 SN ON: 1144A SN OFF: 453

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 26,958 hrs · 22,742 cycles

RIGHT SIDE SEAT TRACK HAS DAMAGE BETWEEN FS 409.00 AND FS 409.00+36. REMOVED SEAT TRACK, CUT OUT DAMAGED SECTION, INSTALLED NEW SECTION IAW REO 601R-53-00-055.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,958 hrs · 22,742 cycles

LEFT PRESSURE SILL CORRODED BETWEEN FS 559.00 AND FS 559.00+16. REMOVED CORROSION, TREATED AREA AND PAINTED IAW REO 601R-53-51-189.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,958 hrs · 22,742 cycles

CORROSION ON FRAME AT FS 333.00 BETWEEN STGR 25R AND STGR 25L. REMOVED AND REPLACED LOWER FRAME SECTION AT FS 333.00 BETWEEN STGR 23R AND 23L IAW CRJ 200 SRM 51-40-11, 51-42-06 AND 51-42-21.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,958 hrs · 22,742 cycles

RIGHT PRESSURE FLOOR SILL PANEL FOUND TO BE CORRODED BETWEEN FS 559.00+16 AND 559.00+32. REMOVED CORROSION, TREATED AREA AND PAINTED IAW REO 601R-53-51-189.

Part: BPSU — FAILED (TE FLAPS) · airframe 26,916 hrs · 22,696 cycles

ON APPROACH INTO DTW RECEIVED FLAPS FAIL CAUTION MSG ON EXTENSION. FLAPS FAILED AT 0 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY IN DTW. REMOVED AND REPLACED RIGHT BPSU. OPS CHECK GOOD.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,857 hrs · 22,627 cycles

RIGHT FS 559 BULKHEAD WEB CRACKED AT RBL 18. CRACK WAS CONFIRMED BY A LEVEL II EDDY CURRENT. REPAIRED RIGHT FS 559 BULKHEAD IAW REO 601R-53-41-260.

Part: CONNECTOR — FAILED (ZONE 400) · airframe 26,332 hrs · 22,118 cycles

ON APPROACH INTO DAY AT 6000FT WITH COWL A/I ON RECEIVED LT 14 STAGE DUCT WARNING. EMERGENCY DECLARED, PER QRH AFTER 40 SEC WENT TO IDLE ON LEFT ENGINE, AFTER 1 TO 2 MIN WARNING WENT OUT. A/C LANDED SAFELY IN DAY. REMOVED AND REPLACED FENWAL CONNECTOR P81WK. OPS CHECK GOOD.

Part: ENGINE — VIBRATION (LEFT) · airframe 26,051 hrs · 21,836 cycles

ON CLIMBOUT FROM DTW CONSTANT LEFT ENGINE N1 VIB INDICATION, AT NORMAL CRUISE POWER IN EXCESS OF 3.2. NORMAL INDICATION AT REDUCED LESS THAN 60 PERCENT POWER SETTINGS. EMERGENCY DECLARED, A/C RETURNED TO DTW LANDED SAFELY. PERFORMED INSPECTION OF LEFT ENGINE PER GE ENGINE MANUAL 72-00-00 FAULT ISOLATION 17 PROCEDURE 3B. OPS CHECKS GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 23,535 hrs · 19,480 cycles

FS 559 LEFT CAP ANGLE CRACKED AT LBL 18.00. REPAIRED CRACK AT LEFT FS 559 IN ACCORDANCE WITH REO 601-53-41-260 AND DEVIATION REO 601R-53-41-609 DEVIATION A.

Part: CONTROL HANDLE — FAILED (TE FLAPS) · airframe 20,741 hrs · 17,173 cycles

FLAPS FAILED AT 0 DEG ON APPROACH INTO DTW. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED FLAP CONTROL HANDLE.

Part: CIRCUIT BREAKER — TRIPPED · airframe 20,047 hrs · 16,618 cycles

EN ROUTE FROM GSO TO LGA RECEIVED DC EMERGENCY BUSS CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY IN LGA. FOUND C/B P1 R7 EMERGENCY BUSS SENSE, OUT. RESET C/B OPS CHECK GOOD. NO OTHER DEFECTS. (A)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,698 hrs · 16,333 cycles

DURING HMV 4 CHECK, NDT INSPECTION FOUND THE REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL FITTING. DAMAGED PORTION OF WEB CUT OUT AND REPAIRED DOUBLER PER REO 601R-53-61-1230.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 19,698 hrs · 16,333 cycles

DURING HMV4 INSPECTION THE STRINGER 3L TO FRAME FS 280 ATTACH CLIP WAS FOUND CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW 51-42-21.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,698 hrs · 16,333 cycles

CRACK ON AFT SIDE FS 640 FRAME JUST BELOW STR 9. REPLACED RIGHT SIDE FRAME AT 640 AND PERFORMED REPAIR IAW SB601R-53-061 PART C.

Part: LATCH — LACK OF LUBE (CABIN DOOR) · airframe 14,628 hrs · 12,358 cycles

FLIGHT 5257 - DURING YYZ APPROACH RECEIVED A CABIN DOOR WARNING, CREW DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT INCIDENT. LUBRICATED THE CABIN DOOR LATCHING MECHANISM.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 14,559 hrs · 12,296 cycles

FLIGHT 5014 - DURING YUL APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES, CREW DECLARED AN EMERGENCY. 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: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 14,520 hrs · 12,263 cycles

FLIGHT 5208 - AFTER LANDING RECEIVED A FLAP FAIL CAUTION MESSAGE. 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: START VALVE — FAULTY (RT ENGINE) · airframe 13,961 hrs · 11,772 cycles

FLIGHT 5768 - UPON TAKEOFF ROLL RECEIVED A RIGHT ENGINE START LIGHT AND STATUS MESSAGE, ABORTED TAKEOFF. DURING SECOND TAKEOFF ATTEMPT RECEIVED SAME MESSAGE ALONG WITH NO STARTER CUTOUT CAUTION MESSAGE. AIRCRAFT RETURNED TO GATE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 13,943 hrs · 11,756 cycles

FLIGHT 5031 - COPILOT WINDSHIELD SHATTERED. REPLACED WINDSHIELD.

Part: SCREEN — CLOGGED (LT ENGINE) · airframe 13,376 hrs · 11,257 cycles

FLIGHT 5653 - LEFT ENGINE OIL PRESSURE WARNING, I.F.S.D. FOUND C-SUMP SCAVENGE PUMP INLET SCREEN CLOGGED. REPLACED SUMP SCREEN FITTING.

Part: CONTROL UNIT — MALFUNCTIONED (AVIONICS) · airframe 11,300 hrs · 9,450 cycles

FLIGHT 9463 - FLAPS FAIL CAUTION. REPLACED THE FECU.

Part: PSEU — MALFUNCTIONED (AVIONICS) · airframe 11,130 hrs · 9,323 cycles

FLIGHT 5245 PROX SYSTEM CHANNEL-C MESSAGE. REPLACED THE PSEU.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 10,219 hrs · 8,570 cycles

FLIGHT 5005 PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD.

Part: IDG — LACK OF LUBE (NR 2 GENERATOR) · airframe 8,416 hrs · 7,176 cycles

NR 2 IDG CAUTION MESSAGE AND GEN 2 CAUTION. SERVICED THE IDG OIL RESERVOIR, OPERATIONAL CHECK SATISFACTORY.

Part: IDG — MALFUNCTIONED (NR 2 ENGINE) · airframe 8,423 hrs · 7,181 cycles

FLIGHT 5044 NR 2 IDG CAUTION AND NR 2 GENERATOR CAUTION, T/O ABORTED. DEFERRED MAINT ON NR 2 IDG PER MEL.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 7,328 hrs · 6,288 cycles

FLIGHT 5528 FLAPS FAILED AT 30 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: COMPUTER — MALFUNCTIONED (TE FLAPS) · airframe 6,224 hrs · 5,393 cycles

FLIGHT 5928 FLAPS FAIL CAUTION DURING LANDING. REPLACED THE FECU.

Part: FLAP · airframe 4,280 hrs · 3,806 cycles

FLIGHT 6044 FLAPS FAIL MESSAGE DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.

Part: ACTUATOR — BINDING (R/H #3) · airframe 4,168 hrs · 3,715 cycles

FLIGHT 5037 FLAPS FAIL CAUTION MESSAGE.REPLACED THE R/H #3 FLAP ACTUATOR.

Part: FLAP · airframe 4,167 hrs · 3,714 cycles

FLIGHT 5020 FLAPS FAIL CAUTION MESSAGE AT 26 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.

Part: ACTUATOR — BINDING (R/H OUTBD FLAP) · airframe 4,129 hrs · 3,687 cycles

FLIGHT 5306 FLAPS FAIL MESSAGE AT 30 DEGREES.REPLACED R/H #3 AND #4 FLAP ACTUATORS.

Part: ACTUATOR — BINDING (RIGHT WING) · airframe 4,129 hrs · 3,687 cycles

FLIGHT 5306 RECEIVED A FLAP FAIL CAUTION MESSAGE AT 30 DEGREES. REPLACED THE RIGHT WING #4 FLAP ACTUATOR

Part: ACTUATOR — BINDING (RIGHT WING) · airframe 4,129 hrs · 3,687 cycles

FLIGHT 5306 RECEIVED A FLAP FAIL CAUTION MESSAGE AT 30 DEGREES.REPLACED THE RIGHT WING #3 FLAP ACTUATOR.

Part: PITOT LINE · airframe 3,631 hrs · 3,263 cycles

FLIGHT 5397 T/O ABORTED BECAUSE OF COPILOT AIRSPEED INDICATOR AMBER FLAG.PURGED PITOT/STATIC SYSTEM; SYSTEM CHECK SATISFACTORY.

Part: FLAP · airframe 3,332 hrs · 3,015 cycles

FLIGHT 5083 FLAPS FAILED AT 30 DEGREES DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: FLAP · airframe 3,050 hrs · 2,783 cycles

FLIGHT 5268 FLAPS FAILED AT 0 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: SWITCH — MALFUNCTIONED (COCKPIT) · airframe 2,541 hrs · 2,336 cycles

FLIGHT 5949 FLAPS FAIL CAUTION MESSAGE.REPLACED THE FLAP CONTROL LEVER ASSY.

Part: LAMP — BURNED OUT (EXTERIOR) · airframe 2,022 hrs · 1,865 cycles

R/H FWD EXTERIOR EMERGENCY LIGHT IS INOP.REPLACED LIGHT BULB.

Part: CONTROL BOX — FAULTY (COCKPIT) · airframe 1,879 hrs · 1,731 cycles

FLIGHT #5593. WHILE PARKED AT THE GATE RECEIVED A FLAP FAIL CAUTION MESSAGE.REPLACED THE FLAP POSITION CONTROL LEVER.

Part: SKIN — DENTED (FUSELAGE) · airframe 1,027 hrs · 943 cycles

DENTS BEHIND RT NOSE DOOR ON FUSELAGE. INSTALLED REPAIR IAW REO 601R-53-2230 REV A DATED 2-17-01.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 752 hrs · 712 cycles

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

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 677 hrs · 633 cycles

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

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 677 hrs · 633 cycles

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

Part: TIRE — FAILED (NLG) · airframe 660 hrs · 622 cycles

NLG TIRE BLEW OUT DURING T/O. REPLACED NLG WHEEL ASSY.

Part: DISPLAY — FAILED (INSTRUMENT PANEL) · airframe 28 hrs · 33 cycles

CO-PILOTS MFD WENT BLANK. REPLACED MFD.