N642CA

Part: RETAINER — BENT (PAX DOOR SEAL) · airframe 33,314 hrs · 24,397 cycles

PASSENGER DOOR SEAL RETAINER BENT ON BOTTOM FORWARD SIDE. REMOVED AND REPLACED THE SEAL RETAINER IAW SRM 51-42-06, 51-40-11, 51-25-16, 51-42-13, AND AMM 52-11-02.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 33,314 hrs · 24,397 cycles

PASSENGER DOOR INTERNAL STRUCTURE UPPER AFT L BRACKET IS CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-11, 51-42-06, 51-42-21, 51-42-13 AND 51-42-22.

Part: FORMER — CORRODED (PAX DOOR) · airframe 33,314 hrs · 24,397 cycles

PASSENGER FORMER AT FS 311.75 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED PASSENGER DOOR FORMER AT FS 311.75 IAW SRM 51-42-06, 51-40-11, 51-25-16, 51-42-10, 53-00-00, 51-26-00, 51-42-21 AMM 52-11-04.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 33,314 hrs · 24,397 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 51-42-06, 51-40-11, 51-25-16, 51-25-06, 51-21-11, AND 52-11-04.

Part: SKIN — CORRODED (PAX DOOR) · airframe 33,314 hrs · 24,397 cycles

PAX DOOR INTERIOR SKIN CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SKIN ON THE PAX DOOR IAW SRM 51-42-06, AND SRM 51-42-10.

Part: WEB — CRACKED (PAX DOOR) · airframe 33,314 hrs · 24,397 cycles

AFT PAX DOOR WEB AT LOWER WHEEL SUPPORT HAS A CRACK. REPAIRED THE AFT PAX DOOR WEB IAW REO 670-52-11-999.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,314 hrs · 24,397 cycles

FUSELAGE STRINGER 25R CORRODED OUT OF LIMITS BETWEEN FS 280 AND 295. REMOVED AND REPLACED DAMAGED SECTION OF STRINGER 25R IAW SRM 53-00-03, 51-25-06, 51-40-11, 51-42-06, 51-42-20, 51-21-11, 53-21-03, NDTM PART 1 51-20-006.

Part: FRAME — CORRODED (BS 310) · airframe 33,314 hrs · 24,397 cycles

FRAME BS 310 CORRODED OUT OF LIMITS AT STRINGER 27. REMOVED AND REPLACED THE SECTION OF THE FRAME IAW REO 670-53-21-799, REV A, AND REO 670-53-21-1486, REV --.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,314 hrs · 24,397 cycles

FUSELAGE STRINGER 26R CORRODED OUT OF LIMITS BETWEEN FS 295 AND 310. REMOVED AND REPLACED DAMAGED SECTION OF STRINGER 26R IAW SRM 53-00-03, 51-40-11, 51-42-06, 51-42-20, 51-21-11, 51-25-06, NDTM PART 1 51-20-006.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,314 hrs · 24,397 cycles

FRAME 364 CORRODED OUT OF LIMITS BETWEEN STRINGERS 26L AND 25R. REMOVED AND REPLACED DAMAGED FRAME 364 SECTION BETWEEN STRINGERS 25L AND 25R IAW REO 670-53-21-687 REV A DATED 2016-06-06, REO 670-53-21-1487 REV - DATED 2018-01-10, SRM 51-42-21, 51-41-02, 51-42-20, 51-42-06, 51-40-11, 51-25-06, 51-21-11, 53-21-06, AMM 21-23-64, 20-21-00, NDTM PART 1 51-20-006.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 33,314 hrs · 24,397 cycles

AFT DRAG ANGLE ON THE LH SIDE OF THE VERTICAL STABILIZER IS CRACKED. CORRECTIVE ACTION: REPAIRED AFT DRAG ANGLE ON THE LH SIDE OF THE VERTICAL STABLIZER IAW BOMBARDIER REO 670-55-31-018 REV A DATED 2016-10-11 AND REO 670-55-31-103 REV -- DATED 2017-12-27.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 33,314 hrs · 24,397 cycles

STRINGER 19L BETWEEN FS 1000 AND FS 1015 IS DAMAGED. REMOVED DAMAGED AREA OF STRINGER 19L AND SPLICED IN NEW SECTION IAW SRM 51-42-06, 51-42-21, 53-00-03, 51-25-16, 51-21-11, AND NDT MANUAL PART 1 51-20-006.

Part: HOUSING — CRACKED (AFT CARGO DOOR) · airframe 33,314 hrs · 24,397 cycles

AFT CARGO DOOR HANDLE HOUSING IS CRACKED IN TWO SPOTS. REMOVED AND REPLACED THE AFT CARGO DOOR HANDLE HOUSING IAW SRM 51-40-11, 51-42-21, 51-25-16, 51-42-06, 51-23-00, AND AMM 52-31-03.

Part: CAP — CORRODED (PAX DOOR) · airframe 33,314 hrs · 24,397 cycles

PASSNEGER DOOR MID CAP IS CORRODED. REMOVED AND REPLACED THE CAP IAW SRM 51-42-02, 51-42-10, 51-21-23, 51-40-11, 51-42-13, AND AMM 52-70-04,

Part: SKIN — GOUGED (CARGO DOOR) · airframe 33,314 hrs · 24,397 cycles

AFT CARGO DOOR HAS A GOUGE ON THE TOP CENTER OUTER EDGE. CORRECTIVE ACTION: REPAIRED IAW REO 670-52-31-088 REV.-, SRM 51-25-16, 51-25-06, 51-21-11, 51-21-00, 51-23-00, 52-00-01, AND NDTM PART 1 51-20-006.

Part: INTERCOSTAL — CORRODED (BS 310-319) · airframe 33,314 hrs · 24,397 cycles

INTERCOSTAL BELOW GALLEY SERVICE DOOR BETWEEN BS 310 AND 319.70 HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21.

Part: INTERCOSTAL — CORRODED (BS 319-349) · airframe 33,314 hrs · 24,397 cycles

INTERCOSTAL BELOW GALLEY SERVICE DOOR BETWEEN BS 319.70 AND 349 HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,314 hrs · 24,397 cycles

LT FLOOR SEAT RAIL AT FS 581-677 HAS SIGNS OF CORROSION. EVALUATED AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013 REV J DATED 2014/10/22. REMOVED AND REPLACED LT FLOOR SEAT RAIL IAW AMM 53-00-49.

Part: WEB — CRACKED (ZONE 200) · airframe 33,314 hrs · 24,397 cycles

FWD EQUIPMENT BAY LT FLOOR WEB AT BS 192 CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR IAW REO 670-53-11-509, REV D, SRM 51-21-11, 51-25-06, 51-25-16, 51-42-06, AMM 20-70-00, AND NDTM 51-20-006

Part: RIB — CRACKED (RT WING) · airframe 33,314 hrs · 24,397 cycles

RIGHT HAND FIXED LEADING EDGE OUTBOARD RIB IS CRACKED. REMOVED AND REPLACED R/H FIXED LEADING EDGE O/B RIB(PN:CC670-12137-6) IAW SRM 51-42-06, 51-42-10, AND 51-40-11.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 33,314 hrs · 24,397 cycles

FS 280.00 CROSSBEAM LT AND RT SIDES ARE CRACKED. REMOVED AND REPLACED FS 280.00 CROSSBEAM (PN:CC670-34175-7S) IAW SRM 51-42-13, 51-42-21, 51-42-06, 51-11-41, 51-40-11, 51-25-06, 51-21-11, AMM 20-70-00, AND NDT MANUAL PART 1 51-20-006.

Part: PLATE — DAMAGED (FUSELAGE) · airframe 33,314 hrs · 24,397 cycles

DAMAGE TO AFT CARGO STRIKE PLATE BETWEEN FS1000-1047. COMPLETED REPAIR OF DAMAGE BELOW AFT CARGO STRIKE PLATE BETWEEN FS1000-1047 IAW REO 670-53-61-1428 DATED 2018-01-15.

Part: WARNING LIGHT — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 31,581 hrs · 22,881 cycles

RIGHT EMERGENCY EXIT AMBER INDICATION. PERFORMED INSPECTION AND OPS CHECK IAW AMM 52-21-00. NO DEFECTS NOTED AT THIS TIME.

Part: DOOR — NOT CLOSED (CARGO BAY) · airframe 30,354 hrs · 21,944 cycles

CABIN FAILED TO PRESSURIZE. PERFORMED GENERAL VISUAL INSPECTION AND FOUND AFT CARGO DOOR NOT COMPLETELY CLOSED. GAP WAS FOUND TO BE ENOUGH TO NOT PRESSURIZE. PERFORMED OPS CHECK IAW AMM 52-31-00. OPS GOOD.

Part: PROXIMITY SWITCH — DIRTY (PAX DOOR) · airframe 30,172 hrs · 21,810 cycles

PASSENGER DOOR LATCH CAUTION MSG DISPLAYED WITH MEL 52-70-01 & 21-24-07. CLEANED PROXIMITY SWITCH AS REQUIRED. PERFORMED OPERATIONS CHECK OF THE PAX DOOR WARNING SYS IAW AMM 52-70-00.

Part: LENS — CRACKED (CABIN) · airframe 28,683 hrs · 20,696 cycles

EMERGENCY LIGHT AT MAIN CABIN DOOR FLOOR LEVEL, HAS A CRACKED LENS. DEFERRED IAW NEF 25-100-12.

Part: STOP FITTING — OUT OF ADJUST (PAX DOOR) · airframe 28,127 hrs · 20,269 cycles

MAIN CABIN DOOR INDICATION SHOWS OPEN. ADJUSTED PAX DOOR HANDLE STOP IAW AMM 52-11-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,945 hrs · 20,126 cycles

EMERGENCY EXIT LIGHT ON LT SIDE HAS BULBS OUT. R & R LT EMER EXIT BULBS. OPERATIONS CHECKED GOOD IAW AMM 33-51-05.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

FORWARD AVIONICS COMPARTMENT, STRINGER 27R HAS CORROSION BETWEEN FS 333.00 TO 349.00. R & R STRINGER 25R, PN SH670-31212-2 IAW SRM 51-42-06, 51-40-11 & 51-25-16.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

LEFT & RIGHT INTERCOSTAL AT FS 364.00 ARE CORRODED. LT & RT INTERCOSTAL AT FS 364.00, PNS SH670-32075-3 &-4, IAW SRM 51-42-06 & 51-42-21.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

STRINGER 26R BETWEEN FS 333.0 & 349.0, IS CORRODED. R & R STRINGER 26R BETWEEN FS 333.0 & 349.0, PN SH670-31372-4 IAW SRM 51-42-06, 53-21-03, 51-21-11 & 51-40-11. WO 80280 & WC 1071.

Part: MOUNT BRACKET — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

T CASS ANTENNA MOUNTING BRACKET CORRODED. R & R T CASS ANTENNA BRACKET, PN SH670-32364-7, IAW SRM 51-42-06, 51-40-11, 51-25-16, AMM 34-43-00 & 34-43-07.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

FLOOR SUPPORT AT FS 280.00 IN FWD AVIONICS COMPARTMENT IS CORRODED. R & R FLOOR SUPPORT, PN CC670-34256-3, IAW SRM 51-42-21, 51-40-11 & 51-42-06.

Part: FRAME — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

CORROSION ON FRAME 333 AT STRINGER 27. CUT OUT CORRODED FRAME 333 FROM STRINGER 25L TO 25R, FABRICATED & INSTALLED REPAIR PARTS IAW REO 670-53-21-799, DATED 30 JAN 2012. WO 80282 WC 2114. REPAIR PARTS FABRICATED IAW REO 670-53-21-799 DATED 30 JAN 2012.

Part: FRAME — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

FRAME 345.00 AT STRINGER 27 IS CORRODED. REPAIRED FRAME 345.00 AT STRINGER 27 BY CUTTING OUT CORRODED AREA & INSTALLING REPAIR PARTS IAW REO 670-53-21-1176 DATED 9 APRIL 2015.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

RIGHT FLOOR SEAT RAIL FROM FS 364.00 - 477.00 SHOWING SIGNS OF CORROSION. R & R SEAT RAIL, PN SH670-32159-1 IAW AMM 53-00-49 & SRM 53-21-49.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

SERVICE DOOR KICK ANGLE IS CORRODED. R & R SERVICE DOOR KICK ANGLE, PN SH670-31996-1, IAW SRM 51-42-06 & 51-42-21.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

RIGHT FLOOR SILL FROM FS 280.00 TO THE SERVICE DOOR SHOWING SIGNS OF CORROSION. R & R RT SILL, PN SH670-32172-3 IAW SRM 51-21-11, 51-25-16, 51-42-20, 51-42-13, 51-42-06, 51-40-11, 20-70-00 & AMM 20-70-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

FLOOR SUPPORT AT FS 279.00 IS CORRODED. R & R FLOOR SUPPORT, PN CC670-33292-13, IAW SRM 51-42-06 & 51-40-11. WO 80282 & WC 2107.

Part: STRIKER — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

SERVICE DOOR SEAL STRIKER CORRODED. CORRECTIVE ACTION: REOMOVED AND REPLACED SERVICE DOOR SEAL STRIKER, PN:SH670-31412-3, IAW CRJ700 SRM 51-40-11, 51-41-00, 51-42-06, CRJ700AMM 53.-21-23, AND 20-21-00

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

LEFT FS 280.00 BULKHEAD WEB CORRODED. REMOVED LT FS 280.00 BULKHEAD WEB, FABRICATED & INSTALLED NEW FS 280.00 BULKHEAD WEB IAW 670-53-11-594 DATED 27 APRIL 2011.

Part: BEAM — CRACKED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

LEFT & RIGHT SIDE OF FS 280.00 BEAM CRACKED & CORRODED. R & R FS 280.00 BEAM PN CC670-34175-7S IAW SRM 53-11-41, 51-42-21, 51-42-06, 51-42-13 & AMM 20-70-00.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

AFT WING TO BODY FAIRING WEB, ATTACH ANGLE IS CORRODED. R & R ANGLE, PNSH670-39189-1, IAW SRM 51-40-11, 51-42-06 & 51-42-15.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

PASSENGER DOOR CUT OUT SURROUND MID CAP ANGLE IS CORRODED. R & R MID CAP ANGLE IAW SRM 51-41-02.

Part: STRAP — CRACKED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

AFT WING TO FUSELAGE FAIRING CTR STRAP IS CRACKED & CORRODED. R & R CTR STRAP, PN CC670-39251, IAW SRM 51-42-06 & 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

LEFT SEAT TRACK 3, INBD HAS CORROSION BETWEEN FS 517.00 & FS 587.00, LT SEAT TRACK 4, INBD HAS CORROSION BETWEEN FS 581.00 & FS 629.00. BLENDED DAMAGE ON LT 4 SEAT TRACK .015 OF MATERIAL LOSS, WITHIN LIMITS IAW REO 670-53-00-013 REV J 10/22/2014. REPLACED LT 3 SEAT TRACK IAW AMM 53-00-49.

Part: FLOORBEAM — CORRODED (BS 1030) · airframe 27,903 hrs · 20,097 cycles

AFT CARGO FLOORBEAM CORRODED AT FS 1030, LBL 27. R & R AFT FLOORBEAM SECTION IAW REO 670-53-00-029 REV A. NDT PERFORMED, NO CRACKS LOCATED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,903 hrs · 20,097 cycles

RIGHT SEAT TRACK 3 HAS CORROSION BETWEEN FS 517.00 & FS 587.00, RT SEAT TRACK 4 HAS CORROSION BETWEEN FS 581.00 & FS 629.00. BLENDED DAMAGE, RT SEAT TRACK 3 HAS .034 OF MATERIAL LOSS, WITHIN LIMITS. RT SEAT TRACK 4 HAS 0.10 OF MATERIAL LOSS, OUT OF LIMITS IAW REO 670-53-013 REV J 10/22/2014. R & R RT 3 SEAT TRACK IAW AMM 53-00-49.

Part: PIN — MIGRATED (PAX DOOR) · airframe 27,903 hrs · 20,097 cycles

PASSENGER DOOR HINGE AFT SAFETY PIN MIGRATED. R & R AFT SAFETY PIN IAW AMM 52-11-00.

Part: VENT — GOUGED (PAX DOOR) · airframe 27,903 hrs · 20,097 cycles

PASSENGER DOOR VENT DOOR HAS A GOUGE ON THE INSIDE. REPLACED PAX VENT DOOR IAW AMM 52-11-15.

Part: HINGE — CRACKED (PAX DOOR) · airframe 27,903 hrs · 20,097 cycles

PASSENGER DOOR BOTTOM STEP HINGE IS CRACKED ON FWD SIDE. REPLACED PAX DOOR BOTTOM STEP HINGE IAW AMM 52-11-04 & AMM 20-21-00.

Part: ANGLE — CRACKED (LT PYLON) · airframe 27,903 hrs · 20,097 cycles

LEFT PYLON ANGLE MOUNTING BRACKET FOR PANEL 433 BT IS CRACKED. R & R LT ANGLE MOUNTING BRACKET IAW SRM 51-42-06.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 27,903 hrs · 20,097 cycles

RIGHT OVERWING EMER EXIT FAILED FUNCTIONAL TEST. FORCE TO OPERATE HANDLE EXCEEDED LIMITS IAW AMM 52-21-00. LUBRICATED & TESTED IAW AMM 52-21-00 & 12-20-52. TESTED GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (SERVICE DOOR) · airframe 27,762 hrs · 19,985 cycles

SERVICE DOOR HANDLE CAUTION MSG DURING GND OPERATIONS. ADJUSTED GALLEY SERVICE DOOR PROX SENSOR PX38 IAW AMM 52-70-06. OPERATIONS CHECKED IAW AMM 52-70-00 GOOD AT THIS TIME.

Part: WHEEL — MALFUNCTIONED (PAX DOOR) · airframe 27,400 hrs · 19,695 cycles

PASSENGER DOOR SUPPORT WHEEL DID NOT DEPLOY. CYCLED PAX DOOR & INSPECTED SUPPORT ASSEMBLY. OPERATIONS CHECKED NORMAL OF PAX DOOR WHEEL SUPPORT IAW AMM 52-13-00.

Part: SWITCH — BROKEN (COCKPIT) · airframe 27,271 hrs · 19,602 cycles

FIRST OFFICER'S EMER LIGHT GUARDED SWITCH COVER BROKEN. PLACED ON NEF-25-100-39.

Part: LIGHT — DETACHED (CABIN) · airframe 27,263 hrs · 19,596 cycles

ESCAPE LIGHTING TO THE RT OF THE SERVICE DOOR IS UNATTACHED. INSTALLED ESCAPE LIGHT PANEL ON RT SIDE OF SERVICE DOOR IAW AMM 25-26-02.

Part: SPOILER — MALFUNCTIONED (WING) · airframe 27,232 hrs · 19,572 cycles

INBOARD FLIGHT SPOILERS CAUTION MSG & INBD SPOILERONS CAUTION MSG IN FLIGHT. PERFORMED RESET OF SPOILER SYS IAW AMM 27-61-05. OPERATIONS CHECKED GOOD. NO MSGS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,167 hrs · 19,523 cycles

EMERGENCY EXIT LIGHT AT FLOOR EXITS AT 12A & 12D ONLY HAVE 50 PERCENT OF THE LIGHTS ILLUMINATED. DEFERRED LIGHTS IAW MEL 33-51-01F.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,604 hrs · 19,074 cycles

ROW EMER CEILING FLOOD LIGHT INOPERATIVE. DEFERRED EMER CEILING FLOOD LIGHT IAW MEL 33-51=01B CAT C.

Part: DOOR SEAL — DEFECTIVE (PAX DOOR) · airframe 26,402 hrs · 18,908 cycles

PAX DOOR SQUEALS ON CLIMB. R & R PAX DOOR SEAL IAW AMM 52-11-07. LEAK CHECKED GOOD AT THIS TIME.

Part: WIRE — DAMAGED (DOOR WARNING) · airframe 26,208 hrs · 18,756 cycles

FORWARD CARGO DOOR INDICATION ERROR. REPAIRED WIRING ON CONNECTOR P376, IAW ESPM 20-33-00. OPERATIONS CHECKED GOOD IAW AMM 52-70-12.

Part: PLACARD — WORN (PAX DOOR) · airframe 25,940 hrs · 18,544 cycles

MAIN PAX DOOR TO OPEN PLACARD WORN. R & R TO OPEN PLACARD ON PAX DOOR IAW AMM 20-60-04.

Part: UNKNOWN — SMOKE (CABIN) · airframe 25,919 hrs · 18,531 cycles

LAVATORY SMOKE ALARM WENT OFF & VISIBLE SMOKE WAS SEEN. PERFORMED OPERATIONS CHECK OF LAVATORY SMOKE DETECTOR SYS IAW 26-16-00. OPERATIONS CHECKED NORMAL AT THIS TIME.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 25,807 hrs · 18,438 cycles

RIGHT ENG BLEED CAUTION MSG IN FLIGHT. R & R RT ENG PRSOV IAW AMM 36-12-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: CABLE — FRAYED (PAX DOOR) · airframe 25,441 hrs · 18,151 cycles

PASSENGER DOOR POWER ASSIST CABLE FRAYED. R & R DOOR POWER ASSIST CABLE IAW CRJ700 AMM 52-11-08, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: FAN — MALFUNCTIONED (LAVATORY) · airframe 25,125 hrs · 17,913 cycles

SMOKE AFT FAN WARNING, LAVATORY EXHAUST FAN CB POPPED. DEFERRED AFT EXHAUST FAN IAW MEL 21-23-02 CAT C.

Part: WARNING LIGHT — FALSE ACTIVATION (RT ENGINE BLEED) · airframe 24,558 hrs · 17,476 cycles

RIGHT ENGINE BLEED CAUTION MESSAGE ILLUMINATED. PERFORMED OPS TEST OF RT ENGINE PRSOV IAW AMM 36-12-01, OP'S CHECKED GOOD AT THIS TIME.

Part: SAFETY VALVE — FAILED (CABIN PRESSURE) · airframe 24,259 hrs · 17,237 cycles

RAPID DECOMPRESSION AT FL390. VERIFIED ALL DOORS CLOSED AND LATCHED, INSPECTED A/C AND FOUND SAFE FOR 1 TIME FERRY FLIGHT. ON INSPECTION OF PRESSUIZATION FOUND NR 1 SAFETY VALVE FLAGGED. R & R NR 1 SAFETY VALVE IAW AMM 21-32-03. OPS CHECKED GOOD AT THIS TIME.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 23,367 hrs · 16,550 cycles

EMERGENCY LIGHT SHOVED IN THE CARPET. SECURED EMERGENCY LIGHT IAW AMM 33-51-01. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,962 hrs · 16,252 cycles

EMERGENCY FLOOD LIGHT AT ROW 9 (CEILING) IS INOPERATIVE. R & R CEILING LIGHT IAW AMM 33-51-09. OP'S CHECKED GOOD AT THIS TIME.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 22,888 hrs · 16,200 cycles

MID CABIN CEILING EMERGENCY LIGHT OUT. SECURED MID CABIN CEILING EMERGENCY LIGHT BULB INTO SOCKET IAW AMM3 3-51-09, OPS CHECKED GOOD AT THIS TIME.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 22,589 hrs · 15,995 cycles

CORROSION FOUND ON STRINGER 25L SPLICE AT FS 333. REMOVED LIGHT SURFACE CORROSION. NO MATERIAL LOSS. ALODINED, PRIMED, TOP COATED AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-06, 51-21-16, 51-21-11, 51-25-06.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 22,589 hrs · 15,995 cycles

INTERCOSTAL AT FS 360 S26L CORRODED. R & R INTERCOSTAL IAW SRM 51-42-06, 51-42-11, 51-40-11, 51-21-11, 20-24-00.

Part: FRAME — CORRODED (ZONE 100) · airframe 22,589 hrs · 15,995 cycles

CORROSION FOUND ON FS 349 FRAME BETWEEN STGR 27 AND 26R. BLENDED FS349 FRAME 0.015" DEEP. ALODINED, PRIMED, TOP COATED AND APPLIED CORROSION INHIBITING COMPOUND IAW REO 670-53-21-902. NDT PERFORMED. NO DEFECTS FOUND.

Part: STRINGER — CORRODED (ZONE 100) · airframe 22,589 hrs · 15,995 cycles

CORROSION FOUND ON STRINGER 26L BETWEEN FS 295 AND 310. REMOVED LIGHT SURFACE CORROSION. NO MATERIAL LOSS. ALODINED, PRIMED, TOP COATED AND APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-06, 51-21-16, 51-21-11, 51-25-06.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 22,589 hrs · 15,995 cycles

INTERCOSTAL AT FS 360 S26L CORRODED. R & R INTERCOSTAL IAW SRM 51-42-06, 51-42-11, 51-40-11, 51-21-11, 20-24-00.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 22,589 hrs · 15,995 cycles

LT FLOOR SEAT RAIL CORRODED FROM FS693 -761.85. R & R LT FLOOR SEAT RAIL FROM FS693-FS761.85 IAW AMM 53-00-49 .

Part: FRAME — CORRODED (ZONE 100) · airframe 22,589 hrs · 15,995 cycles

CORROSION FOUND ON FS 333 FRAME AT S27. BLENDED FS FRAME 333, 0.020 DEEP. ALODINED, PRIMED,TOP COATED AND APPLIED CORROSION INHIBITING COMPOUND IAW REO 670-53-21-902. NDT PERFORMED. NO DEFECTS FOUND.

Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 22,589 hrs · 15,995 cycles

EXTERNAL SUROUND STRUCTURE OF MAIN AVIONICS COMPARTMENT DOOR BETWEEN STGR 25L AND 25R HAS SIGNS OF CORROSION. REMOVED LIGHT SURFACE CORROSION. NO MATERIAL LOSS. ALODINED AREA IAW SRM 51-26-06, 51-21-11.

Part: FRAME — CORRODED (ZONE 100) · airframe 22,589 hrs · 15,995 cycles

CORROSION FOUND ON FS 310 FRAME AT STGR 27. BLENDED (2) SPOTS ON FS 310 FRAME. SPOT 1 TO .007" DEEP AND SPOT 2 TO .010" DEEP. ALODINED, PRIMED, TOP COATED AND APPLIED CORROSION INHIBITING COMPOUND IAW REO 670-53-21-902. NDT PERFORMED. NO DEFECTS FOUND.

Part: DIAPHRAGM — CORRODED (ZONE 100) · airframe 22,589 hrs · 15,995 cycles

DIAPHRAGM AT FS 360, S26L CORRODED. R & R DIAPHRAGM IAW SRM 51-42-06, 51-42-11, 51-40-11, 51-21-11, 20-24-00.

Part: FRAME — CORRODED (ZONE 100) · airframe 22,589 hrs · 15,995 cycles

CORROSION FOUND ON FS 319.7 FRAME AT STGR 27. BLENDED FS319.7, FRAME 0.010" DEEP. ALODINED, PRIMED, TOP COATED AND APPLIED CORROSION INHIBITING COMPOUND IAW REO 670-53-21-902. NDT PERFORMED. NO DEFECTS FOUND.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 22,589 hrs · 15,995 cycles

SEAT RAIL AT FS364-470 LBL9 CORRODED. R & R LT FLOOR SEAT RAIL FROM FS364-FS470 IAW AMM 53-00-49 .

Part: ANGLE — CORRODED (PAX DOOR) · airframe 22,589 hrs · 15,995 cycles

PASSENGER DOOR THRESHOLD KICKPLATE ANGLE IS CORRODED. R & R PASSENGER DOOR THRESHOLD KICKPLATE ANGLE IAW SRM 51-45-00 AND 51-42-06.

Part: BEAM — CORRODED (FUSELAGE) · airframe 22,589 hrs · 15,995 cycles

FS 280.0 BEAM IS CORRODED. REMOVED AND REPLACED FS 280.0 BEAM IAW BOMBARDIER REO 670-53-11-047 & REO 690-53-11-032 (REF W/O 80092 W/C 1044).

Part: ANGLE — CORRODED (PAX DOOR) · airframe 22,589 hrs · 15,995 cycles

PASSENGER DOOR MID CAP ANGLE IS CORRODED. R & R PASSENGER MID CAP ANGLE IAW SRM 51-42-06 AND 51-25-01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 22,589 hrs · 15,995 cycles

SEAT TRACK CORRODED FROM FS 693 TO 761. REMOVED LIGHT SURFACE CORROSION IAW REO 670-53-00-013. NO MATERIAL LOSS.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 22,589 hrs · 15,995 cycles

SEAT TRACK CORRODED FROM FS 785.15 TO 939. REMOVED LIGHT SURFACE CORROSION IAW REO 670-53-00-013. NO MATERIAL LOSS.

Part: BONDING JUMPER — FRAYED (PAX DOOR) · airframe 22,589 hrs · 15,995 cycles

PAX DOOR TOP STEP BONDING JUMPER FRAYED. R & R BONDING JUMPER IAW AMM 51-80-00.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 22,589 hrs · 15,995 cycles

SEAT TRACK CORRODED FROM FS 6770 TO 761.85. REMOVED LIGHT SURFACE CORROSION IAW REO 670-53-00-013. NO MATERIAL LOSS.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 22,398 hrs · 15,855 cycles

EMERGENCY LIGHTS INOPERATIVE. PLACED SWITCH IN ARM POS FOR CHARGE, AFTER 30 MIN, PERFORMED OP'S CHECK OF EMERGENCY LIGHTS, OP'S CHECK GOOD IAW AMM 33-51-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,383 hrs · 15,844 cycles

EMERGENCY LIGHT OVER ROW 6 & 7 INOPERATIVE. LAMPED CEILING EMERGENCY LIGHT IAW AMM 33-51-09. OPS CHECKED GOOD.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 22,298 hrs · 15,771 cycles

LOWER GREEN LOCK INDICATOR NOT ALIGNED WHEN MAIN CABIN DOOR IS CLOSED AND LOCKED. ADJUSTED DOOR RIG IAW AMM 52-11-00. FUNCTIONAL TEST OF PAX DOOR GOOD.

Part: SENSOR — FAULTY (RT ENGINE) · airframe 22,043 hrs · 15,622 cycles

ON CLIMBOUT FROM DFW RECEIVED HIGH OIL TEMP WARNING MSG NR 2 ENGINE. PERFORMED IFSD A/C RETURNED TO DFW LANDED SAFELY. REMOVED AND REPLACED RIGHT ENGINE OIL LEVEL/TEMP SENSOR. OPS CHECK GOOD.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,842 hrs · 14,744 cycles

CORROSION ON RT SILL PLATE FROM FS 280 TO FS 319.70. REMOVED SILL PLATE AND INSTALLED NEW SILL PLATE IAW SRM 51-42-06, 51-42-21, AND 51-42-13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,840 hrs · 14,744 cycles

TOP FLANGE OF FS 280 LATERAL FLOORBEAM CORRODED. REMOVED AND REPLACED FS 280 CROSS BEAM IAW TASK CARD REO-B-53R0005.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,839 hrs · 14,744 cycles

PAX DOOR SILL MID CAP ANGLE CORRODED PART SH670-31825-5. REPLACED MID CAP ANGLE PART SH670-31825-9 IAW BOMBARDIER AMM 20-21-00.

Part: CONTROL UNIT — FAULTY (SPOILER) · airframe 19,990 hrs · 26,730 cycles

DURING CRUISE FLIGHT (CVG-DFW) LOST NR 1 HYDRAULIC SYSTEM FLUID. CREW DECLARED AN EMERGENCY AND DIVERTED TO MEM. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE MULTI FUNCTION SPOILER POWER CONTROL UNIT.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 19,497 hrs · 13,829 cycles

F/A IS UNABLE TO OPEN MAIN PASSENGER DOOR. ADJUSTED PAX DOOR FWD AND AFT MICRO ADJUSTERS AND CABLES, ALSO ADJUSTED FWD HANDRAIL.

Part: WARNING SYSTEM — MALFUNCTIONED (ANTI-SKID SYS) · airframe 15,528 hrs · 11,066 cycles

ON FINAL APPROACH INTO OKC RECEIVED ANTI SKID O/B AND O/B GND SPLR FAULT CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. ALL MSG'S CLEARED AFTER LANDING CHECKS COMPLETED. PERFORMED OPS CHECK OF ANTI SKID AND GRD SPOILED SYSTEMS. NO DEFECTS NOTED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 11,616 hrs · 8,343 cycles

FLIGHT 5219 - RECEIVED NOSE DOOR OPEN WARNING AND PROX SYSTEM 1 FAULT MESSAGES. DECLARED EMERGENCY, RETURNED TO SDF, LANDED WITHOUT INCIDENT. ADJUSTED PX31 GAP TO AMM LIMITS, REMOVED SNOW AND ICE FROM AREA. NO FURTHER DEFECTS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 10,703 hrs · 7,769 cycles

FLIGHT 5273 - SEVERAL CABIN EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 10,703 hrs · 7,769 cycles

FLIGHT 5273 - SEVERAL CABIN EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 10,703 hrs · 7,769 cycles

FLIGHT 5273 - SEVERAL CABIN EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED NR 3 EMERGENCY BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 10,703 hrs · 7,769 cycles

FLIGHT 5273 - SEVERAL CABIN EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY PACK.

Part: WARNING SYSTEM — ACTIVATED (PAX DOOR) · airframe 10,585 hrs · 7,684 cycles

FLIGHT 5070 - PAX DOOR OUTER HANDLE MESSAGE ON T/O. T/O ABORTED SAFELY. TRANSFERRED TO DMI LIST PER MEL 52-70-01.

Part: ACM — SEIZED (A/C BAY) · airframe 10,454 hrs · 7,594 cycles

FLIGHT 5650 - SMOKE IN CABIN DURING TAXI. DECLARED EMERGENCY, EVACUATED PASSENGERS ON RAMP, RETURNED TO GATE. REPLACED RIGHT ACM. NO FURTHER DEFECTS.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 9,702 hrs · 7,068 cycles

FLIGHT 5521- ON APPROACH RECEIVED AN O/B SPOILERONS CAUTION MESSAGE AND O/B FLIGHT SPOILERONS CAUTION MESSAGE. PERFORMED SYSTEM RESET AND RAN POST TEST, OPS CHECK GOOD.

Part: SERVICE DOOR — OPEN (GPU DOOR) · airframe 8,671 hrs · 6,342 cycles

FLIGHT 5258 - DURING CLIMBOUT OF CVG THE GPU DOOR OPENED, FLIGHT RETURNED TO THE FIELD. INSPECTED CONDITION OF DOOR AND LATCHES, NO DISCREPANCIES NOTED, CLOSED DOOR.

Part: PCU — FAULTY (LT WING SPOILERS) · airframe 7,976 hrs · 5,877 cycles

FLIGHT 5175 - AFTER TAKEOFF RECEIVED A SPOILERON AND FLIGHT SPOILER CAUTION MESSAGE. AIRCRAFT RETURNED TO CVG, FLIGHT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LEFT OUTBOARD MFS PCU.

Part: BULKHEAD — CORRODED (BS 280) · corrosion level 2 · airframe 7,603 hrs · 5,628 cycles

CORROSION FOUND ON AFT SIDE OF WEB AT FS 280 BULKHEAD AT WL 79.50. REPLACED WEB WITH WEB FABRICATED FROM .040" 7075-T6 PO 13577 IAW BOMBARDIER REO 670-53-11-052 REV A.

Part: FITTING — CHAFED (HORIZONTAL STAB) · airframe 7,603 hrs · 5,628 cycles

HORIZONTAL STAB PINS ROTATING INTO THE ANTI-ROTATION FITTINGS CAUSING CHAFE DAMAGE LEFT AND RIGHT. BLENDED ANTI-ROTATION FITTINGS, PERFORMED LPI, ROTOPEENED REPAIR AREA, REAPPLIED PROTECTIVE FINISH IAW REO 70-2530-01322.

Part: ACM — MALFUNCTIONED (RIGHT) · airframe 6,584 hrs · 5,009 cycles

FLIGHT 5379 - DURING TAKEOFF ROLL AT CVG RECEIVED A SMOKE WARNING IN THE AFT LAVATORY, ABORTED TAKEOFF AND CREW DECLARED AN EMERGENCY. ALL PASSENGERS DEPLANED SAFELY ON TAXIWAY. DEFERRED THE RIGHT AIR CONDITIONING PACK AND APU.

Part: TILLER — MALFUNCTIONED (COCKPIT) · airframe 4,792 hrs · 3,740 cycles

FLIGHT 5197- STEERING INOP CAUTION DURING LANDING. REPLACED THE STEERING TILLER.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 3,283 hrs · 2,571 cycles

FLIGHT 5683 LT THRUST REVERSER UNSAFE CAUTION MESSAGE. DEFERRED MAINT PER MEL.

Part: PUMP — FAILED (NR 1) · airframe 2,538 hrs · 1,991 cycles

FLIGHT 5860 EDP NR 1 INOP WARNING. REPLACED THE EDP.

Part: WARNING LIGHT — FALSE ACTIVATION (ANTI ICE SYSTEM) · airframe 167 hrs · 142 cycles

FLIGHT 5773 LEFT ENGINE COWL ANTI ICE CAUTION MESSAGE. COULD NOT DUPLICATE. SYSTEM TEST SATISFACTORY AFTER CLEARING DEFERRED MAINT ON LEFT ACM.