N378CA

Part: A/C PACK — ODOR (RIGHT) · airframe 34,108 hrs · 25,212 cycles

STRONG SMOKE ODOR IN CABIN. INSPECTED AND DETERMINED THE RT A/C PACK FAULTY.

Part: CABLE — BROKEN (PAX DOOR) · airframe 34,006 hrs · 25,121 cycles

PAX DOOR SUPPORT WHEEL CABLE BROKEN. REMOVED AND REPLACED PAX DOOR SUPPORT WHEEL CABLE IAW CRJ7 AMM 52-11-13 OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 33,896 hrs · 25,021 cycles

RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R THE EMERGENCY LIGHT IAW AMM 33-51-15. OPS CHECKED GOOD.

Part: DRIVE UNIT — DISCONNECTED (TE FLAPS) · airframe 33,014 hrs · 24,199 cycles

FLAPS FAILED IN FLIGHT. REATTACHED TORQUE TUBE FOR LT FLAP SYSTEM TO FLAP POWER DRIVE UNIT IAW AMM 27-52-37, ELECTRICAL RIGGED FLAP SYSTEM IAW AMM 27-52-00, OPS CHECKED FLAP SYSTEM IAW AMM 27-50-00. SYSTEM OPS CHECKED GOOD

Part: UNKNOWN — LEAKING (PAX DOOR) · airframe 32,920 hrs · 24,103 cycles

LOUD WHISTLE FROM MAIN CABIN DOOR IN FLIGHT. CLEANED AND INSPECTED MAIN CABIN DOOR SEAL. NO DEFECTS NOTED. LUBED DOOR SEAL. OPS CHECKED GOOD IAW AMM 52-11-07, AND 12-20-52.

Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR LATCH) · airframe 32,486 hrs · 23,741 cycles

PAX DOOR LATCH CAUTION MESSAGE.

Part: STIFFENER — CRACKED (BS 202 BULKHEAD) · airframe 31,726 hrs · 23,121 cycles

FWD SIDE OF BULKHEAD AT BS 202.75 FOUND INDICATION ON TOP OF STIFFENER LBL30 APPROX 1/8 INCHES LONG, STIFFENER FAILED NDT INSPECTION

Part: FRAME — CORRODED (BS 1015) · airframe 31,618 hrs · 23,035 cycles

FRAME BS 1015 AT STRINGER 24R IS CORRODED. CUT OUT THE DAMAGED FRAME, FABRICATED AND INSTALLED REPAIR IAW REO 670-53-61-1272.

Part: STRINGER — CORRODED (BS 847-863) · airframe 31,618 hrs · 23,035 cycles

STRINGER 24R CORRODED BETWEEN BS 847 AND 863. CUT OUT AND REPLACED DAMAGED STRINGER SECTION IAW SRM 53-00-03, REO SH670-37077, SRM 51-42-21, 51-42-06, 51-25-01, 51-40-11, 51-42-13, 51-25-16, AND 51-21-11. NDT PERFORMED . NO DEFECTS.

Part: FRAME — CORRODED (BS 863) · airframe 31,618 hrs · 23,035 cycles

FRAME BS 863 BETWEEN STRINGERS 25L AND 25R CORRODED OUT OF LIMITS. REPAIRED THE FRAME IAW REO 670-53-51-104 REV. NDT PERFORMED WITH NO DEFECT NOTED.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 31,618 hrs · 23,035 cycles

RT AFT FUSELAGE TO VERTICAL FWD DRAG ANGLE IS CRACKED. CUT AWAY DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-018, DATED 16 APR 2007. NDT PERFORMED.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 31,618 hrs · 23,035 cycles

LT AFT FUSELAGE TO VERTICAL FWD DRAG ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-018, DATED 16 APR 2016. NDT PERFORMED.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 31,618 hrs · 23,035 cycles

RT AFT FUSELAGE TO VERTICAL AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-090, DATED 21 SEPT 2016. NDT PERFORMED.

Part: TRIPLER — GOUGED (FUSELAGE) · airframe 31,618 hrs · 23,035 cycles

AFT LOWER FUSELAGE AT FS 985.00, EXISTING MAJOR REPAIR TRIPPLER IS GOUGED. R & R TRIPPLER IAW REO670-53-00-290, REV D, AND SRM 51-42-21.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 31,618 hrs · 23,035 cycles

PASSENGER DOOR SURROUND LINTEL STR IS CRACKED AT FS 280.00. CUT AWAY DAMAGED FABRICATED AND INSTALLED REPAIR PARTS AND LINTEL STR KIT, PN:670BA53040 IAW REO 670-53-21-493, REV D DATED 2015-07-10, AND SB 670BA-53-040, REV C. NDT PERFORMED IAW WO A16-1109, DATED 22SEP13.

Part: STRINGER — CORRODED (BS 295-319) · airframe 31,618 hrs · 23,035 cycles

STRINGER 24R BETWEEN BS 295 AND 319 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06, 51-42-21.

Part: BEAM — CRACKED (FUSELAGE) · airframe 31,618 hrs · 23,035 cycles

RT FS 280 BEAM FOUND TO BE CRACKED. REMOVED AND REPLACED RT FS 280 BEAM IAW SRM 53-11-41. NDT PERFORMED. NO CRACK INDICATIONS NOTED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 31,138 hrs · 22,679 cycles

F/O WINDSHIELD CRACKED. R & R FO WINDSHIELD IAW AMM 56-11-01, OPS CHECKED GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,326 hrs · 22,078 cycles

FLOOR SQUARE EXIT LIGHT AT 12A HAS 1 LIGHT INOPERATIVE. R & R BULB IAW AMM 20-41-00. OPERATIONS CHECKED GOOD.

Part: DOOR SEAL — DIRTY (EMERGENCY EXIT) · airframe 30,057 hrs · 21,882 cycles

LEFT OVERWING EXIT WHISTLING IN FLIGHT. REMOVED LT EMER EXIT DOOR & CLEANED SEAL. REINSTALLED LT EMER EXIT DOOR IAW AMM 52-21-00.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 28,155 hrs · 20,404 cycles

FS 280.0 FLOOR CROSSBEAM IS CRACKED & CORRODED. R & R CROSSBEAM IAW SRM CHAPTERS 51 & 53.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,115 hrs · 20,404 cycles

FRAME AT FS 295 BETWEEN STRINGER 26R & 25R CORRODED. REPAIRED FRAME IAW REO 670-53-21-799 REV DATED 2012-01-30.

Part: STRINGER — CORRODED (BS 319-333) · airframe 28,115 hrs · 20,404 cycles

CORROSION FOUND ON STRINGER 25R BETWEEN BS 319.7 - 333. R & R IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,155 hrs · 20,404 cycles

LEFT & RIGHT FLOOR SEAT TRACKS CORRODED IN MULTIPLE AREAS FROM FS 280.0 - 477.00. R & R LT & RT FLOOR SEAT RAILS, PN'S SH670-32159-1 & SH670-32249-3, IAW SRM 51-41-02, AMM 53-00-49 & REO 670-53-00-013, REV J DATED 22 OCT 2014.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 28,115 hrs · 20,404 cycles

TWO INTERCOSTALS CORRODED AT FS 364.00 STRINGER 28. R & R TWO INTERCOSTALS, PN SH670-32075-3 & SH670-32075-4 IAW AMM 52-70-08, SRM 51-42-06, 51-42-21, 51-40-11, 51-21-11 & 51-25-16.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,115 hrs · 20,404 cycles

CORROSION FOUND AT FS 333, STRINGER 25R. REPAIRED FRAME IAW REO 670-53-21-1160 REV DATED 2015/02/13. SEE WO 80270 WC 1081.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 28,115 hrs · 20,404 cycles

CORROSION FOUND ON LONGERON BETWEEN FS 333 - 364 AT STRINGER 25R. R & R IAW SRM 51-42-06.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,115 hrs · 20,404 cycles

FS 364.00 AT STRINGER 26L CORRODED. REMOVED & REPAIRED SECTION IAW REO 670-53-21-687 REV DATED 2012-08-03.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 28,115 hrs · 20,404 cycles

AVIONICS COMP FS 364.00 INTERCOSTAL AT STR26R, AND 26L HAS CORROSION. R & R INTERCOSTALS AT FS 364, STR 26R AND 26L IAW SRM 51-42-06. AVMAX WO 80270 W/C 1066. PART NR 2-SH670-32077-4.

Part: DOOR FRAME — BENT (FUSELAGE) · airframe 28,115 hrs · 20,404 cycles

PASSENGER DOOR SURROUND BENT ON UPPER AFT CORNER. REPAIRED PAX DOOR UPPER AFT CORNER IAW REO 670-53-22-001 REV H DATED 10JUN2013. NDT PERFORMED INSPECTION SERVICES K9QR554B, JOB AV0209157J-2, PO 125285 DATED 14FEB2015.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,115 hrs · 20,404 cycles

SERVICE DOOR SILL BETWEEN FS 319.70 - 349.00 IS CORRODED. R & R CORRODED WEB FLOOR PROTECTOR, MOUNTING ANGLE & 3 LOWER SILL ANGLES IAW SRM 51-42-06, 51-42-21, 51-40-11 & AMM 20-21-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,115 hrs · 20,404 cycles

FLOOR SUPPORT AT FS 280 CORRODE. R & R FLOOR SUPPORT AT FS 280 IAW SRM 51-42-06 & 51-40-11.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 28,115 hrs · 20,404 cycles

AFT WING TO BODY FAIRING SUPPORT STRUCTURE CTR SPLICE IS CORRODED. R & R SUPPORT ANGLE IAW SRM 51-42-06.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 28,115 hrs · 20,404 cycles

LEFT & RIGHT LOWER BULKHEAD WEBS AT FS 280.00 ARE CORRODED. R & R LT & RT LOWER BULKHEAD WEBS AT FS 280.00 IAW REO 670-53-11-594 DATED 27APR2011. WEBS WERE FABRICATED IAW REO 670-53-11-594, NO PN AVAILABLE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,115 hrs · 20,404 cycles

MAIN AVIONICS BAY CRAWLWAY ANGLE AT FS 280 CORRODED. R & R MAIN AVIONICS BAY CRAWLWAY ANGLE AT FS 280 IAW SRM 51-21-11, 51-25-16, 51-42-06, 51-42-13 & 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,116 hrs · 20,404 cycles

LEFT & RIGHT SIDE SEAT RAILS 4, 5 & 6 HAVE SIGNS OF CORROSION. BLENDED DAMAGED AREAS ON RAILS LT 4, 5, 6 & RT 5 IAW REO 670-53-00-013 REV J DATED 22 OCT 2014. REPLACED RT RAILS 4 & 6 PN SH670-36255-3 & SH670-36260-5 IAW AMM 53-00-49.

Part: SKIN — GOUGED (BS 977) · airframe 28,115 hrs · 20,404 cycles

BS 977 SKIN HAS TWO GOUGES. REPAIRED THE SKIN IAW REO 67-53-00-290 REV C.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 28,115 hrs · 20,404 cycles

AFT WING TO FUSELAGE FAIRING CTR SUPPORT STRAP IS CRACKED. FABRICATED NEW STRAP IAW DWG CC670-39171 & REPLACED CHANNEL.

Part: CONDUIT — DAMAGED (PAX DOOR) · airframe 28,115 hrs · 20,404 cycles

PASSENGER DOOR TUBING DAMAGED. REPAIRED PAX DOOR HARNESS TUBING BY REPLACING THE HARNESS CONDUIT PN HCTE-0375-0-SP, THE BOOT PN B0816010-03-1-1-0 THEN HEAT SHRINKING THE TUBING IAW REO 670-52-70-006 REVISION A 2014-06-11. SEE AVMAX WORK ORDER 80270 WORK CARD 8036. THIS SDR IS TO CORRECT THE WRONG REGISTRATION NR. SEE CONTROL NR V0XD20150209041.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 28,115 hrs · 20,404 cycles

T CAS CHANNEL CORRODED. R & R IAW SRM 51-42-06, 51-42-21, 51-41-02, AMM 34-43-07, SRM 51-40-11, 51-25-16 & 51-21-11.

Part: ACCESS PANEL — OPEN (GROUND COMM) · airframe 27,961 hrs · 20,281 cycles

LOUD SQUEAL IN FLIGHT. FOUND GND COMM CONTROL ACCESS PANEL OPEN. INSPECTED DOOR, NO DEFECTS NOTED IAW AMM 05-21-00. DOOR LATCHES PROPERLY.

Part: COVER — TORN (EMERGENCY EXIT) · airframe 27,814 hrs · 20,167 cycles

LEFT EMER EXIT HATCH HANDLE GRIP COVER TORN. DEFERRED LT EMER EXIT HANDLE GRIP COVER IAW NEF 25-100-0 CAT 5.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,422 hrs · 19,853 cycles

FIRST CEILING EMER LIGHT INOPERATIVE. LAMPED FIRST EMER LIGHT IN CABIN IAW AMM 33-21-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 27,400 hrs · 19,835 cycles

PASSENGER DOOR HANDLE CAUTION MSG. INSPECTED PAX DOOR, NO DEFECTS NOTED. OPERATIONS CHECKED OF PAX DOOR WARNING SYS OPERATIONS CHECKED GOOD IAW AMM 52-70-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 27,356 hrs · 19,797 cycles

PAX DOOR MASTER CAUTION WARNING ON TAXI. PERFORMED OPERATIONS CHECK ON PSEU IAW AMM 32-60-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: CABLE — FRAYED (PAX DOOR) · airframe 27,254 hrs · 19,714 cycles

MAIN DOOR SUPPORT WHEEL CABLE FRAYED. R & R PAX DOOR WHEEL SUPPORT CABLE IAW AMM 52-11-13. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 27,042 hrs · 19,514 cycles

EMERGENCY EXIT SIGN AT ROW 12 CEILING LIGHT INOPERATIVE. REPLACED POWER SUPPLY IAW AMM 33-51-17. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: CABLE — BROKEN (DOOR) · airframe 26,883 hrs · 19,412 cycles

ICE BREAKER CABLES BROKEN. R & R ICE BREAKER CABLES IAW AMM 52-11-15.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,725 hrs · 19,289 cycles

CEILING EMER LIGHT ROW 2 WILL NOT COME ON. DEFERRED EMER CEILING FLOOR LIGHT IAW MEL 33-51-01B.

Part: DOOR — NOT SEATED (CARGO BAY) · airframe 26,710 hrs · 19,278 cycles

AIRCRAFT WILL NOT PRESSURIZE ON DEPARTURE. PERFORMED WALK AROUND & FOUND THE AFT CARGO DOOR NOT SEATED. CLOSED AFT CARGO DOOR & PERFORMED OPERATIONAL CHECK OF THE CABIN PRESSURIZATION SYS IAW AMM 21-31-00. OPERATIONS CHECK IS GOOD AT THIS TIME.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,659 hrs · 19,239 cycles

DAMAGE TO SKIN & UNDERLYING STRUCTURE AROUND NLG BAY. ACCOMPLISHED REO 670-53-11-949 REV DATED 2014-06-08.

Part: COVER — MISSING (EXIT SIGN) · airframe 26,162 hrs · 18,846 cycles

EMERGENCY LIGHT COVER MISSING IN THE GALLEY. REPLACED EMERGENCY EXIT SIGN COVER IN GALLEY IAW CRJ700 AMM 33-21-05, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 25,774 hrs · 18,567 cycles

PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE. DEFERRED ITEM IAW MEL 52-70-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,609 hrs · 18,442 cycles

EMERGENCY LIGHT OVERHEAD FLOOD LIGHT INOPERATIVE AT ROW 9. DEFERRED EMERGENCY LIGHT OVERHEAD CEILING ROW 9 IAW MEL 31-51-01B CAT C.

Part: CABLE — FRAYED (PAX DOOR) · airframe 25,095 hrs · 18,039 cycles

MAIN PAX DOOR CABLE FRAYED. R & R MAIN PAX DOOR CABLE IAW AMM 52-11-08, OP'S CHECKED GOOD AT THIS TIME.

Part: PLACARD — WORN (PAX DOOR) · airframe 249,912 hrs · 17,957 cycles

PAX DOOR OPEN PLACARD IS WORN. PLACED PAX DOOR OPEN PLACARD ON CARRY OVER 3205 IAW REO 670-11-30-002.

Part: BRACKET — DAMAGED · airframe 24,955 hrs · 17,926 cycles

AFT CABIN FIRE EXTINGUISHER WILL NOT STAY IN BRACKET. ADJUSTED FIRE EXT BRACKET AND REINSTALLED FIRE EXT IAW AMM 26-23-01.

Part: SKIN — DAMAGED (BS 1108-1126) · airframe 24,944 hrs · 17,916 cycles

AFT FUSELAGE SKIN BETWEEN FS 1108 AND 1126 AND IN BETWEEN STRINGER 20R AND STRINGER 21R IS DAMAGED. REPAIRED IAW REO 670-53-61-991.

Part: SEAL — LACK OF LUBE (EMERGENCY EXIT) · airframe 24,446 hrs · 17,537 cycles

LEFT OVERWING EXIT DOOR IS MAKING A HIGH PITCH NOISE IN FLIGHT. LUBRICATED SEAL IAW AMM 52-21-07 & 12-20-52.

Part: SEAL — LEAKING (ESCAPE HATCH) · airframe 24,246 hrs · 17,376 cycles

CREW HATCH LEAKING. INSPECTED, RESEALED,TESTED CREW ESCAPE HATCH IAW AMM 52-22-00. NO LEAKS NOTED AT THIS TIME.

Part: ACTUATOR — FAILED (SLAT SYS) · airframe 24,128 hrs · 17,284 cycles

SLATS FAIL CAUTION MESSAGE AIRBORNE. R & R SLAT 1-1 ACTUATOR IAW AMM 27-81-09, OP'S CHECKED GOOD AT THIS TIME. PERFORMED ELECTRICAL RIGGING OF SLATS IAW 27-81-00. NO DEFECTES NOTED.

Part: ACTUATOR — MALFUNCTIONED (SLAT SYSTEM) · airframe 24,074 hrs · 17,245 cycles

SLAT FAIL CAUTION MESSAGE. R & R SLAT ACTUATORS, OPS CHECKED GOOD IAW AMM 27-81-09.

Part: SEAL — DIRTY (EMERGENCY EXIT) · airframe 24,055 hrs · 17,231 cycles

LT EMERGENCY DOOR SQUEALS LOUDLY IN FLIGHT. REMOVED EMERGENCY EXIT DOOR AND CLEANED DOOR JAM AND SEAL ASSY IAW AMM 52-21-00.

Part: ACTUATOR — CONTAMINATED (SLATS) · airframe 24,042 hrs · 17,220 cycles

SLAT FAIL MESSAGE INFLIGHT. INSPECTED SLAT ACTUATOR SYS AND FOUND RT SLAT 2-3 TO HAVE TRIPPED AND WATER INSIDE. R & R ACTUATOR.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 24,040 hrs · 17,219 cycles

AFTER TAKEOFF, WITH EMERGENCY LIGHTS IN THE ARMED POSITION, LIGHTS KEPT CYCLING ON AND OFF. PERFORMED OPS TEST OF EMERGENCY LIGHT SYSTEM IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: SEAL — LACK OF LUBE (EMERGENCY EXIT) · airframe 23,773 hrs · 17,024 cycles

LEFT OVERWING EMERGENCY EXIT WINDOW PRODUCING LOUD NOISE DURING FLIGHT. INSPECTED AND LUBRICATED LT EMERGENCY EXIT DOOR SEAL, REINSTALLED DOOR IAW AMM 52-21-07 AND 52-21-00, OP'S TEST GOOD AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,587 hrs · 16,883 cycles

EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-50-09, OPS CHECKED GOOD.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 23,486 hrs · 16,805 cycles

CAPTAIN'S WINDSHIELD OUTER LAYER SHATTERED IN FLIGHT.

Part: SEAL — LEAKING (EMERGENCY EXIT) · airframe 23,432 hrs · 16,760 cycles

EMERGENCY EXIT LEAKING. CLEANED DOOR SEAL AND DOOR JAM AREA, INSPECTED FOR DEFECTS, NO DEFECTS NOTED AT THIS TIME IAW AMM 52-22-00.

Part: SEAL — LEAKING (ESCAPE HATCH) · airframe 23,230 hrs · 16,613 cycles

COCKPIT ESCAPE HATCH LEAKING WATER. INSPECTED, CLEANED AND LUBRICATED SEAL ON CREW ESCAPE HATCH IAW AMM 52-22-07 & 52-22-00. RETURNED TO SERVICE.

Part: SEAL — LEAKING (EMERGENCY EXIT) · airframe 23,115 hrs · 16,527 cycles

EMERGENCY EXIT WINDOW 12 A/B SQEALING DURING FLIGHT. PERFORMED VISUAL INSP OF OVERWING EMERGENCY EXIT DOOR,SEALS AND FRAME. NO EVIDENCE OF DENTS OR OTHER DEFECTS TO THE SEAL NOTED AT THIS TIME IAW AMM 52-21-06.

Part: PAINT — WORN (PAX DOOR) · airframe 23,022 hrs · 16,453 cycles

PAX DOOR TOP CLOSED GREEN MARKINGS WORN. TOUCHED UP PAX DOOR ALIGNMENT MARKINGS IAW AMM 52-11-00.

Part: PLACARD — MISSING (SERVICE DOOR) · airframe 23,022 hrs · 16,453 cycles

SERVICE DOOR "GREEN MARKS MUST ALIGN " PLACARD MISSING. INSTALLED PLACARD IAW AMM 20-60-04.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 23,022 hrs · 16,453 cycles

PAX DOOR ENTRANCE FLOORBOARD IS CRACKED. R & R HORIZONTAL UPPER STAIR PANEL, ENTRANCE FLOORBOARD IAW AMM 52-11-04.

Part: FITTING — CORRODED (THRESHOLD) · airframe 23,020 hrs · 16,452 cycles

PASSENGER DOOR THRESHOLD FORWARD CLOSING FITTING IS CORRODED. R & R FORWARD CLOSING FITTING IAW SRM 51-42-06,51-40-11, 51-42-21, AND 51-21-11.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,020 hrs · 16,452 cycles

FS 280 RT FLOORBEAM IS CRACKED. R & R FLOORBEAM IAW REO 670-53-11-047, REO 670-53-11-751, SRM 51-42-06, AND 51-21-11.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 23,020 hrs · 16,452 cycles

FLOOR SUPPORT AT FS 280 TO 319 IS CORRODED . R & R FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-13.

Part: FLOOR SUPPORT — DAMAGED (ZONE 100) · airframe 23,020 hrs · 16,452 cycles

BS 279 BL 0 FWD FLOOR SUPPORT CRACKED. R & R FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21, 51-21-11.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 23,020 hrs · 16,452 cycles

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

Part: ANGLE — CORRODED (ZONE 100) · airframe 23,020 hrs · 16,452 cycles

PASSENGER DOOR THRESHOLD KICKPLATE ANGLE IS CORRODED. R & R PASSENGER DOOR THRESHOLD KICKPLATE ANGLE IAW SRM 51-40-11, 51-42-06, AND 51-42-20.

Part: SEAT TRACK — CORRODED (BS 349-389) · airframe 23,020 hrs · 16,452 cycles

SEAT TRACK HAS CORROSION FROM FS 349 TO 389. R & R RT SEAT TRAC IAW SRM 51-21-49, 53-00-49, 51-21-11,51-24-36, AND 51-41-02.

Part: J-BOX — MALFUNCTIONED (ELECTRICAL SYS) · airframe 21,514 hrs · 15,338 cycles

SMOKE EMANATING FROM JB6 WITH A/C SETTING AT THE GATE. REMOVED AND REPLACED JB 6.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 20,004 hrs · 14,297 cycles

PAX DOOR AFT DRAG ANGLE CRACKED AT PULLEY BRACKET. REMOVED DAMAGED SECTION OF AFT DRAG ANGLE AND SPLICED IN A NEW SECTION IAW REO 670-52-11-072.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 20,004 hrs · 14,297 cycles

PAX DOOR EDGE MEMBER CRACKED IN AFT CORNER UNDER TOP STEP. REPAIRED PAX DOOR EDGE MEMBER IN AFT CORNER UNDER TOP STEP IAW BOMBARDIER REO 670-52-11-154 AND BOMBARDIER REO 601R-52-11-279.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,004 hrs · 14,297 cycles

LEFT 280.00 PILOTS BULKHEAD IS CORRODED NEAR FLOOR LEVEL. REPLACED BULKHEAD WEB IAW SRM 53-11-10-201-003 REPAIR "B".

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,004 hrs · 14,297 cycles

COCKPIT FLOOR SUPPORT ANGLE (CAMLOCK RECEPTACLE) AT FS 280.00 IS CORRODED. REPLACED ANGLE IAW SRM AND 51-42-21.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,004 hrs · 14,297 cycles

RIGHTS PILOT'S 280.00 BULKHEAD CORRODED NEAR FLOOR LEVEL. REPLACED BULKHEAD WEB IAW SRM 53-11-10 REPAIR B.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,004 hrs · 14,297 cycles

FS 280.00 CROSSBEAM IS CORRODED BEYOND LIMITS. REPLACED FLOORBEAM IAW SRM 51-42-06, 51-42-13 AND 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,004 hrs · 14,297 cycles

RT SIDE FLOOR SEAT TRACK CORRODED BETWEEN FS 485 AND FS 685. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,004 hrs · 14,297 cycles

RT SIDE FLOOR SEAT TRACK CORRODED BETWEEN FS 485 AND FS 685. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: SENSOR — OUT OF RIG (NLG) · airframe 19,346 hrs · 13,830 cycles

ON CLIMBOUT FROM CVG RECEIVED GEAR DISAGREE WARNING, NOSE GEAR WOULD NOT UNLOCK TO RETRACTED. EMERGENCY DECLARED, A/C RETURNED TO CVG LANDED SAFELY. RE-RIGGED LT AND RT NLG WOW SENSORS, RETORQUED BOLTS FOR BOTH NLG OUTER CYLINDER HARNESS SUPPORT BRACKETS AND RIGHT NLG CENTERED SENSOR.

Part: ACTUATOR — FAULTY (LE SLAT) · airframe 18,212 hrs · 13,061 cycles

ON APPROACH INTO MSP RECEIVED SLATS FAIL CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED RIGHT WING NR 3 SLAT O/B ACTUATOR.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 18,206 hrs · 13,057 cycles

ON APPROACH INTO MSP RECEIVED SLATS FAIL CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. AFTER RESETTING SLAT SYSTEM PER FIM RECEIVED SLAT HALF SPEED STATUS MSG. TRANSFERRED TO DEFERRED PER MEL 27-51-02-2.

Part: BPSU — CHAFED (LE SLAT) · airframe 18,196 hrs · 13,048 cycles

ON APPROACH INTO MSP RECEIVED SLAT FAIL CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED RIGHT WING SLAT BPSU.

Part: SPOILER — MALFUNCTIONED (WING) · airframe 17,292 hrs · 12,376 cycles

EN ROUTE FROM BUF TO DTW RECEIVED O/B FLT SPL CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY IN DTW. RESET FLIGHT SPOILERS, OPS CHECK GOOD.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 16,566 hrs · 11,861 cycles

ON T/O FROM CVG RECEIVED NOSE GEAR DISAGREE. EMERGENCY DECLARED, A/C RETURNED TO CVG LANDED SAFELY. REMOVED AND REPLACED NOSE LANDING GEAR LT WOW WIRE HARNESS.

Part: ACTUATOR — TRIPPED (L/E SLAT) · airframe 11,598 hrs · 8,391 cycles

FLIGHT 5172 - SLAT FAIL MESSAGE RECEIVED ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND LEFT NR 2 SLAT ACTUATOR TRIPPED. RESET ACTUATOR. NO FURTHER DEFECTS.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 11,502 hrs · 8,326 cycles

FS 280 CROSSBEAM CORRODED BEYOND LIMITS. REPLACED THE FS 280 CROSSBEAM IAW REO 670-53-11-046.

Part: ACM — SEIZED (A/C BAY) · airframe 11,384 hrs · 8,243 cycles

FLIGHT 5642 - SMOKE REPORTED ENTERING CABIN DURING TAXI. DECLARED EMERGENCY, RETURNED TO BLOCK. REPLACED RIGHT PACK (ACM). NO FURTHER DEFECTS.

Part: SHIMMY DAMPENER — WORN (LT MLG) · airframe 13,996 hrs · 8,115 cycles

FLIGHT 5058 - MLG SHIMMY ON TAKEOFF AND GEAR RETRACTION. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LEFT MLG SHIMMY DAMPENER.

Part: SHIMMY DAMPENER — WORN (RT MLG) · airframe 13,996 hrs · 8,115 cycles

MLG SHIMMY ON TAKEOFF AND GEAR RETRACTION. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED RIGHT MLG SHIMMY DAMPENER.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 10,370 hrs · 7,539 cycles

FLIGHT 5280 - F/O WINDSHIELD CENTER PANE AT FL 390. LANDED WITHOUT INCIDENT. REPLACED WINDSHIELD.

Part: NONE — NONE · airframe 10,360 hrs · 7,534 cycles

FLIGHT 5526 - ELEVATOR SPLIT CAUTION MESSAGE ON CLIMBOUT. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. INSPECTED AIRCRAFT, NO FAULTS IN MDC, NO HISTORY IN TRAX OR AIRCRAFT LOG BOOK. PERFORMED OPS CHECK WITH NO DEFECTS FOUND.

Part: WINDOW — CRACKED (COCKPIT) · airframe 8,460 hrs · 6,314 cycles

FLIGHT 5258 - CAPTAIN'S WINDOW CRACKED DURING SRQ APPROACH. REPLACED THE CAPTAIN'S SIDE WINDOW.

Part: WEB — CORRODED (FS 280) · airframe 7,622 hrs · 5,790 cycles

FS 280 BULKHEAD LOWER WEBS ARE CORRODED BEYOND LIMITS FROM LBL 36 TO RBL 36. REPLACED THE FS 280 BULKHEAD LOWER WEBS IAW BRAS REO 670-53-11-052 REV A REPAIR NR 2.

Part: BEAM — CORRODED (FS 280) · airframe 7,622 hrs · 5,790 cycles

TRANSVERSE BEAM AT FS 280 FROM LBL 36 TO RBL 36 IS CORRODED ALONG THE UPPER AND LOWER EDGES. REPLACED THE TRANSVERSE BEAM AT FS 280 IAW BRAS REO 670-53-11-047 REV C.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT) · airframe 4,057 hrs · 3,106 cycles

FLIGHT 5639 EMERGENCY EXIT SIGN AT SERVICE DOOR IS INOP. RECONNECTED WIRES TO EXIT SIGN.

Part: SENSOR — MALFUNCTIONED (LT A/C PACK) · airframe 3,605 hrs · 2,724 cycles

FLIGHT 5582 LEFT ENGINE BLEED CAUTION MESSAGE. REPLACED THE LEFT PACK INLET PRESSURE SENSOR.

Part: CONTROL BOX — FAULTY (BRAKE SYS) · airframe 3,461 hrs · 2,619 cycles

FLIGHT 5661 DURING TAKEOFF ROLL RECEIVED A BRAKE OVERTEMP WARNING ON ED1, ABORTED AND RETURNED TO THE GATE. REPLACED THE ANTI SKID CONTROL UNIT.

Part: WARNING LIGHT — ILLUMINATED (SLATS) · airframe 2,354 hrs · 1,801 cycles

FLIGHT 5073, SLATS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE, NO FAULTS IN COMPUTER, OPERATIONAL TEST SATISFACTORY.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 1,253 hrs · 962 cycles

F S 1098.20 BULKHEAD BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPARIED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING I/A/W MFG REO 670-53-61-034 REV B.