N653CA

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,252 hrs · 25,432 cycles

LT EMERGENCY DOOR CAUTION MESSAGE. PERFORMED OPS CHECK OF THE OVERWING EMERGENCY EXIT INDICATION SYS IAW AMM 52-21-00. NO MESSAGES NOTED AT THIS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,141 hrs · 25,328 cycles

LEFT EMERG DOOR CAUTION MSG. PERFORMED OPS CHECK OF LEFT EMERGENCY DOOR PER AMM 52-21-00, OPS CHECK GOOD VERIFIED GREEN INDICATED ON EICAS AND VISUALLY AT DOOR OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (EMERGENCY EXIT) · airframe 34,027 hrs · 25,220 cycles

LEFT EMERGENCY EXIT CAUTION MESSAGE.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 33,373 hrs · 24,653 cycles

LEFT EMERGENCY EXIT DOOR CAUTION MESSAGE. PERFORMED AN OPS TEST OF THE EMERGENCY EXIT DOOR IAW AMM 52-21-00, NO ABNORMAL MESSAGES NOTED.

Part: SKIN SPLICE — CORRODED (BS 280) · airframe 32,443 hrs · 23,778 cycles

SKIN SPLICE AT BS 280 TO 282.86 HAS SIGNS OF CORROSION BETWEEN STRINGERS 25 AND 27R. REPAIRED IAW REO 670-53-21-1446, REV -, SRM 51-25-16, 51-21-11, AND 51-25-06.

Part: STRINGER — CORRODED (BS 250-265) · airframe 32,443 hrs · 23,778 cycles

STRINGER 26R CORRODED BETWEEN BS 250 AND 265. PERFORMED A SPLICE REPAIR IAW SRM 53-00-03, 51-40-11, 51-25-06, 51-21-11, 51-42-21, 51-25-16, 51-42-06 AND NDTM PART 1 51-20-006.

Part: STRINGER — CORRODED (BS 250-265) · airframe 32,443 hrs · 23,778 cycles

STRINGER 26L CORRODED BETWEEN BS 250 AND 265. PERFORMED A STRINGER SPLICE REPAIR IAW SRM 53-00-03, 51-25-16, 51-21-11, 51-42-06, 51-42-21, 51-40-11, 51-25-06, AND NDTM PART 1, 53-20-006.

Part: FITTING — CORRODED (FUSELAGE) · airframe 32,443 hrs · 23,778 cycles

FORWARD NOSE JACK FITTING HAS SIGNS OF CORROSION IN SEVERAL LOCATIONS. REPLACED THE JACK FITTING IAW SRM 51-21-11, 51-25-16, 51-40-11, 51-42-21, AND 51-42-06.

Part: FITTING — CORRODED (ZONE 100) · airframe 32,443 hrs · 23,778 cycles

FORWARD NOSE JACK FITTING HAS SIGNS OF CORROSION IN SEVERAL LOCATIONS. REPLACED THEJACK FITTING IAW SRM 51-21-11, 51-25-16, 51-40-11, 51-42-21, AND 51-42-06.

Part: STRINGER — CORRODED (BS 295-349) · airframe 32,443 hrs · 23,778 cycles

STRINGER 25R CORRODED IN SEVERAL PLACES BETWEEN BS 295 AND 349. REPLACED THE STRINGER IAW SRM 51-42-20, 51-42-06, 51-40-11, 51-42-00, 51-26-16, AND 51-21-11.

Part: INTERCOSTAL — CORRODED (BS 333-349) · airframe 32,443 hrs · 23,778 cycles

INTERCOSTAL BETWEEN BS 333 - 349, STRINGER 20R, FOUND CORRODED OUT OF LIMITS. REPLACED THE INTERCOSTAL IAW SRM 51-42-06, 51-21-11, 51-25-06, 51-40-11, 51-25-16, 51-42-21, 51-42-20, AND AMM 38-32-01.

Part: STOP FITTING — CRACKED (ZONE 200) · airframe 32,443 hrs · 23,778 cycles

PAX DOOR SURROUND FWD TOP STOP IS CRACKED. REMOVED AND REPLACED PAX DOOR SURROUND FWD TOP STOP IAW SRM 51-42-21, 51-25-16.

Part: ANGLE — CORRODED (PAX DOOR AREA) · airframe 32,443 hrs · 23,778 cycles

PASSENGER DOOR KICK ANGLE AND MID CAP ANGLE HAVE SIGNS OF CORROSION. EVALUATED AND FOUND DAMAGE TO BE OUT OF LIMITS. REPLACED KICK ANGLE AND MID CAP IAW SRM 51-42-06, AND 51-42-21.

Part: FRAME — CORRODED (BS 517) · airframe 32,443 hrs · 23,778 cycles

FRAME BS 517 BETWEEN STRINGERS 26L AND 27L IS CORRODED. REPAIRED THE FRAME IAW REO 670-53-31-419.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 32,443 hrs · 23,778 cycles

RT FLOOR SILL CORRODED OUT OF LIMITS AT FS 282. REPLACED RT FLOOR SILL IAW SRM 53-00-45 TR53-0080/51-42-13/51-42-06/51-40-11/51-21-11/51-25-16.

Part: STRINGER — CORRODED (BS 349) · airframe 32,443 hrs · 23,778 cycles

STRINGER 21R CORRODED OUT OF LIMITS AT BS 349. REPLACED THE STRINGER IAW SRM 53-21-03, 51-42-06, 51-21-00, 51-25-06, 51-25-16, 51-42-13, 51-42-21, AND 51-21-11.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 32,443 hrs · 23,778 cycles

INTERCOSTAL BETWEEN FS 310 - 319.70 AT STRINGER 20R CORRODED OUT OF LIMITS. REPLACED INTERCOSTAL IAW SRM 51-42-06/51-42-21/51-21-11/51-25-16.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 32,443 hrs · 23,778 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED HALF WAY. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-42-13, AND 51-42-06.

Part: ANGLE — CORRODED (BS 939) · airframe 32,443 hrs · 23,778 cycles

AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE AT BS 939, HAS A CORRODED ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-25-21, 51-42-06, AND 51-42-11.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 32,443 hrs · 23,778 cycles

RIGHT BS 280 FLOORBEAM IS CRACKED. REMOVED AND REPLACED THE FLOORBEAM IAW 53-11-41, 51-25-06, 51-25-16, 51-21-11, 51-42-13, 51-42-06, 51-42-20, NDTM PART 1 51-20-006, AND AMM 20-70-00.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 32,443 hrs · 23,778 cycles

VERTICAL STABILIZER LT SIDE AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-018, REV A DATED 10 NOV 2016.

Part: BRACKET — CRACKED (RT SLAT TRACK) · airframe 32,443 hrs · 23,778 cycles

RIGHT WING SLAT TRACK HOUSING BRACKET CRACKED. REMOVED THE DAMAGED BRACKET, FABRICATED AND INSTALLED A REPAIR IAW REO 670-57-42-577, SRM 51-25-34, 51-21-11, 51-26-00, AND NDTM 51-20-006.

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 32,443 hrs · 23,778 cycles

RIGHT SIDE SEAT TRACK FROM BS 785.15 - 847 HAS CORROSION. BLENDED THE AREA, AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REPLACED THE SEAT TRACK IAW AMM 53-00-49, AND SRM 51-60-11.

Part: STRINGER — CORRODED (BS 333-349) · airframe 32,443 hrs · 237,778 cycles

AVIONICS BAY STRINGER 25R, BS 333 TO 349 SHOWING SIGNS OF CORROSION. REMOVED AND REPLACED THE STRINGER IAW SRM 51-25-06, 51-25-21, 51-42-20, 51-42-06, AND 51-40-11.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 32,443 hrs · 23,778 cycles

RIGHT SEAT TRACK FROM BS 677 - 708 HAS SIGNS OF CORROSION. EVALUATED THE SEAT TRACK AND FOUND CORROSION TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.

Part: SLAT TRACK — CRACKED (LT WING SLAT) · airframe 32,443 hrs · 23,778 cycles

LEFT WING SLAT TRACK (1-3) HOUSING BRACKET CRACKED. REPAIRED IAW REO 670-57-42-577.

Part: SEAT TRACK — CORRODED (BS 377-708) · airframe 32,443 hrs · 23,778 cycles

LEFT SEAT TRACK FROM BS 677 TO 708 HAS SIGNS OF CORROSION. EVALUATED SEAT RAIL AND FOUND CORROSION TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.

Part: BRACKET — CRACKED (CARGO BAY) · airframe 32,443 hrs · 23,778 cycles

FORWARD BAG BAY RESTRAINT NET BRACKET AT FS 581 IS CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-11, 51-42-21, 51-42-06.

Part: SEAT TRACK — CORRODED (BS 501-565) · airframe 32,443 hrs · 23,778 cycles

RIGHT SIDE SEAT TRACK FROM BS 501 - 565 HAS SIGNS OF CORROSION. BLENDED THE AREA, AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REPLACED THE SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 32,443 hrs · 23,778 cycles

LEFT SIDE SEAT TRACK FROM BS 581 - 677 HAS CORROSION. BLENDED THE AREA, AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REPLACED THE SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 32,443 hrs · 23,778 cycles

LEFT SIDE SEAT TRACK FROM BS 708 - 761.85 HAS SIGNS OF CORROSION. BLENDED THE AREA, AND FOUND OUT OF LIMITS IAW REO 670-53-00-013, REV J. REPLACED THE SEAT TRACK IAM AMM 53-00-49.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,443 hrs · 23,778 cycles

FS 501-FS 523 BETWEEN STRINGERS 26L AND 26R EXTERNAL FUSELAGE SKIN IS CORRODED. REPAIRED FS 501-FS 523 BETWEEN STRINGERS 26L AND 26R EXTERNAL FUSELAGE SKIN IAW REO 670-53-31-418 DATED 2017/08/30.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,443 hrs · 23,778 cycles

RT SIDE SEAT RAIL FROM FS 708-FS 761.85 HAS MULTIPLE SIGNS OF CORROSION. REMOVED AND REPLACED RT SIDE SEAT RAIL FROM FS 708-FS 761.85 IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,443 hrs · 23,778 cycles

RT FLOOR SEAT RAIL FROM FS 581-677 HAS SIGNS OF CORROSION. REMOVED AND REPLACED RT FLOOR SEAT TRACK RAIL AT FS 581-677 IAW AMM 53-00-49.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 31,647 hrs · 23,082 cycles

LEFT EMERGENCY DOOR CAUTION MESSAGE AFTER LANDING. PERFORMED AN OPS TEST OF THE LEFT OVERWING EMERGENCY DOOR IAW AMM 52-21-00. OK FOR SERVICE, NO FAULTS FOUND.

Part: SEAL — DIRTY (ESCAPE HATCH) · airframe 30,957 hrs · 22,530 cycles

WATER COMING THROUGH FLT DECK ESCAPE HATCH. CLEANED THE SEAL IAW AMM 52-22-00.

Part: ENGINE — FAILED (RIGHT) · airframe 30,770 hrs · 22,389 cycles

RIGHT ENGINE FAILED. R & R THE NR 2 ENGINE IAW AMM 71-00-00. OPS AND LEAK CHECKED GOOD.

Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR LATCH) · airframe 30,347 hrs · 22,048 cycles

PAX DOOR LATCH CAUTION MESSAGE.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1015) · airframe 29,238 hrs · 21,191 cycles

FLOOR SUPPORT CORRODED BETWEEN FS 1000-1015 AT LBL 9. REPAIRED IAW REO670-53-61-1205, REV DATED 1-27-2016.

Part: FLOOR SUPPORT — CORRODED (BS 1015-1031) · airframe 29,238 hrs · 21,191 cycles

SIDE BEAM CORRODED BETWEEN FS 1015-1031 AT RBL 42. R & R IAW SRM 51-42-06-001-001-A01 AND REO 670-53-61-1205, REV DATED 01-27-2016 .

Part: FLOOR SUPPORT — CORRODED (BS 1031-1051) · airframe 29,238 hrs · 21,191 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 1031-1051 AT RBL 9. REPAIRED IAW REO 670-53-61-1203, REV DATED 1-23-2016.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 29,238 hrs · 21,191 cycles

FS 1031 FLOORBEAM CORRODED RBL 42. REPAIRED IAW REO 670-53-61-1205, REV DATED 1-27-2016.

Part: FLOORBEAM — CORRODED (BS 1051) · airframe 29,238 hrs · 21,191 cycles

FS 1051 FLOORBEAM CORRODED RBL 42. REPAIRED IAW REO670-53-61-1205 REV, DATED 1-27-2016.

Part: FLOORBEAM — CORRODED (BS 1015) · airframe 29,238 hrs · 21,191 cycles

FS 1015 FLOORBEAM CORRODED RBL 42. REPAIRED IAW REO 670-53-61-1205, REV DATED 1-27-2016.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1015) · airframe 29,238 hrs · 21,191 cycles

SIDE FLOOR SUPPORT CORRODED BETWEEN FS 1000-1015 AT RBL 42. REPAIRED IAW REO 670-53-61-1205, REV DATED 01-27-2016 .

Part: DOOR SEAL — DIRTY (CABIN DOOR) · airframe 28,292 hrs · 20,475 cycles

MAIN CABIN DOOR SQUEALS IN FLIGHT. CLEANED & LUBED MAIN CABIN DOOR SEAL IAW AMM 12-20-52.

Part: HAND RAIL — LOOSE (PAX DOOR) · airframe 27,743 hrs · 20,047 cycles

BOTH HAND RAILS ON THE PAX DOOR LOOSE. R & R BOTH HANDRAILS ON PAX DOOR IAW AMM 52-11-05. OPERATIONS CHECKED GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,369 hrs · 19,761 cycles

MAIN AVIONICS BAY, TWO EACH, CTR INTERCOSTAL AT FS 364 ARE CORRODED. R & R TWO CTR INTERCOSTAL IN MAIN AVIONICS BAY IAW SRM 51-42-21, 51-42-06, 51-21-11, 51-25-16 & 51-40-11.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,369 hrs · 19,761 cycles

MAIN AVIONICS BAY STRINGER 26R BETWEEN FS 349 & 364 HAS CORROSION. R & R IAW SRM 51-42-06 & 51-42-21.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,369 hrs · 19,761 cycles

FLOORBEAM AT FS 1031, LBL 27 CORRODED. REMOVED & SPLICED IN FLOORBEAM FROM FS 985 - 1045, LBL 27 IAW REO 670-53-00-029 FIG 13 REV A DATED 2010 08 31.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,369 hrs · 19,761 cycles

MAIN AVIONICS DOOR RT OTBD FWD INTERCOSTAL HAS CORROSION. R & R INTERCOSTAL IAW SRM 51-40-06, 51-42-21 & 51-40-11.

Part: FRAME — CORRODED (FUSELAGE) · airframe 27,369 hrs · 19,761 cycles

MAIN AVIONICS BAY FRAME 310 HAS CORROSION STRINGER 26L - 26R. REPAIRED IAW REO 670-53-21-799 DATED 2012 01 30.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,369 hrs · 19,761 cycles

MAIN AVIONICS BAY STRINGER 27R BETWEEN FS 295.0 & 310.0 HAS CORROSION. CUT OUT & SPLICED IN NEW STRINGER 26R BETWEEN FS 295.0 & 310.0 IAW REO 670-53-21-1162, DATED 02 MAR 2015.

Part: PROXIMITY SWITCH — INOPERATIVE (PAX DOOR) · airframe 27,369 hrs · 19,761 cycles

PSEU DISCRETE INPUT DI17, PX107, DISPLAYS GND AT ALL TIMES IN MDC. PAX DOOR OUTER HANDLE CAUTION DOES NOT DISPLAY ON EICAS. REPLACED & ADJUSTED PAX PROX SENSOR PX107 IAW AMM 52-70-04. OPERATIONS TESTED GOOD IAW AMM 52-11-00. NO DEFECTS NOTED AT THIS TIME.

Part: WEB — CRACKED (PAX DOOR) · airframe 27,369 hrs · 19,761 cycles

PASSENGER DOOR AFT STAIR WEB HAS CRACK & CORROSION. REPAIRED AFT WEB IAW REO 670-52-11-104 REV F DATED 21 OCT 2010.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 27,369 hrs · 19,761 cycles

PASSENGER DOOR AFT SIDE DRAG ANGLE IS CRACKED. R & R DRAG ANGLE SECTION IAW SRM 52-11-04 & 51-42-06.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,369 hrs · 19,761 cycles

MAIN AVIONICS BAY CRAWL WAY ANGLE AT FS 280 CORRODED. R & R PN CC671-34256-3 IAW SRMS 51-42-06, 51-42-21 & 51-42-13.

Part: BEAM — CORRODED (FUSELAGE) · airframe 27,369 hrs · 19,761 cycles

LEFT & RIGHT 280 BEAM CRACKED & CORRODED. R & R WITH NEW FS 280 BEAM IAW SRM 53-11-41. NDT PERFORMED ON 25 FEB 2015, CRS K9QR554B, JOB 40084852, PO 125168, NO DEFECTS NOTED AT THIS TIME.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,369 hrs · 19,761 cycles

RIGHT FLOOR SEAT RAIL FROM FS 350.0 - 485.0 IS CORRODED. RT FLOOR SEAT RAILS FS 485.0 - 571.0 ARE CORRODED. R & R LT FLOOR SEAT RAILS, PN'S SH670-33426-1 & SH670-32159-1, & RT FLOOR SEAT RAIL, PN SH670-33426-1, IAW AMM 53-00-49 & REO 670-53-00-013 REV J DATED 22 OCT 2014.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,369 hrs · 19,761 cycles

AFT FAIRING SUPPORT STRUCTURE AT FS 969.00 L BRACKET & VERTICAL GUSSET SHOWS SIGNS OF CORROSION. BLENDED CORROSION, REMOVED 0.02 INCHES WITHIN LIMITS IAW SRM 53-82-55. R & R ANGLE, PN SH670-39189-1 & IAW SRM 51-47-06.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 27,369 hrs · 19,761 cycles

MAIN AVIONICS BAY TCAS CHANNEL CORRODED. R & R TCAS CHANNEL, PN SH670-3234-7, IAW SRM 51-42-06, SRM 51-42-21 & SRM 51-40-11.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 27,369 hrs · 19,761 cycles

PASSENGER DOOR TOP CAP ANGLE IS CORRODED. REMOVED CORRODED CAP ANGLE & REPLACED WITH NEW CAP ANGLE, PN SH670-31825-95, IAW AMM 52-70-04 & SRM 51-41-02.

Part: PLATE — CORRODED (FUSELAGE) · airframe 27,369 hrs · 19,761 cycles

MAIN AVIONICS DOOR RT, FWD NYLON GUIDE MOUNTING PLATE HAS CORROSION FS 364, STRINGER 27 - 26R. R & R PLATE IAW SRM 51-41-02, SRM 51-25-06, SRM 51-20-21, AMM 51-21-01 & SRM 53-21-23. FABRICATE PLATE SH670-32457, MATERIAL ID 2024 T3 0.032 BATCH 120647.

Part: HINGE — BROKEN (PAX DOOR) · airframe 27,369 hrs · 19,761 cycles

PASSENGER DOOR, TOP STEP MOUNTING HINGE IS BROKEN. R & R PAX DOOR, TOP STEP MOUNTING HINGE, PN CC670-31981-3, IAW AMM 52-11-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,369 hrs · 19,761 cycles

280 FLOOR SUPPORT CORRODED. R & R AFT FLOOR SUPPORT ANGLE AT FS 280 BEAM IAW SRM 51-42-06, 51-40-11, 51-25-16, 51-21-11 & 51-42-21.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 27,222 hrs · 19,640 cycles

RIGHT ENG BLEED CAUTION MSG. MANUALLY OPERATED RT ENG PRESS SOV IAW FIM 36-12-00. OPERATIONS CHECKED GOOD AT THIS TIME. COULD NOT DUPLICATE ON GND.

Part: HOOK AND LOOP — DEFECTIVE (EMERGENCY EXIT) · airframe 26,991 hrs · 19,477 cycles

LEFT EMER EXIT HANDLE COVER KEEPS FALLING OFF. REPLACED VELCRO ON COVER IAW AMM 51-22-61.

Part: PLACARD — PEELING (PAX DOOR) · airframe 25,988 hrs · 18,668 cycles

PASSENGER DOOR OPEN PLACARD IS PEELING. R & R PAX DOOR OPEN PLACARD IAW 20-60-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,817 hrs · 18,530 cycles

EMERGENCY LIGHTS INOPERATIVE. PERFORMED OPERATIONS CHECK OF THE EMERGENCY LIGHTS IAW AMM 33-51-00, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,651 hrs · 18,402 cycles

FORWARD CABIN FLOOR LEVEL FLOOD LIGHTS 2 EACH INOPERATIVE. DEFERRED BOTH FLOOR LEVEL FLOOD LIGHTS IAW MEL 33-51-01C CAT C.

Part: ROD — BROKEN (PAX DOOR) · airframe 25,540 hrs · 18,321 cycles

PAX DOOR STAIR RETRACTION ROD BROKEN. R & R PAX DOOR RETRACTION ROD IAW AMM 52-11-05, OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 24,859 hrs · 17,802 cycles

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

Part: PITOT LINE — CONTAMINATED (PITIT/STATIC SYS) · airframe 24,805 hrs · 17,762 cycles

STALL FAIL WARNING CAUTION MESSAGE. INSPECTED & FOUND WATER IN THE PITOT SYSTEM. DRAINED WATER FROM DRAIN TUBES IAW CRJ 700 AMM 34-11-00, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: AHRS — FAILED (COCKPIT) · airframe 24,728 hrs · 17,701 cycles

NUMBER 2 AHRS FAILED IN FLIGHT. R & R NR 2 AHRS COMPUTER IAW CRJ 700 AMM 34-31-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: STRUCTURE — UNKNOWN (PAX DOOR) · airframe 2,455 hrs · 17,574 cycles

PAX DOOR SLOW TO CLOSE. INSTALLED BLIND FASTENERS ON PAX DOOR STRUCTURE IAW SRM 51-42-11, OP'S CHECKED GOOD IAW AMM 52-11-08.

Part: LIGHT — INOPERATIVE (FWD CABIN) · airframe 24,382 hrs · 17,433 cycles

FORWARD EMERGENCY LIGHTS INOPERATIVE.

Part: HOOK AND LOOP — LOOSE (EMERGENCY EXIT) · airframe 24,192 hrs · 17,287 cycles

HOOK AND LOOP ON LT EMERGENCY EXIT HANDLE COVER IS LOOSE. R & R HOOK AND LOOP IAW 51-22-61.

Part: LIGHT — UNKNOWN (CABIN) · airframe 23,888 hrs · 17,047 cycles

OVERWING EMERGENCY EXIT SMALL LIGHT REMAINS ON. PERFORMED NUMEROUS OP'S CHECKS OF OVERWING EMERGENCY EXIT LIGHTS IAW AMM 33-51-00, OPS' CHECKED GOOD AT THIS TIME.

Part: SPOILER SYS — MALFUNCTIONED · airframe 23,858 hrs · 17,023 cycles

SPOILERON & SPOILER IS INDICATING PARTIALLY UP. SWAPPED SSCU NR 1 AND NR 2 FOR TROUBLESHOOTING PURPOSES IAW AMM 27-61-05, PERFORMED OP'S CHECKED, NO FIX, REINSTALLED SSCU'S IN ORIGINAL POSITIONS.

Part: DOOR — LEAKING (PAX) · airframe 23,353 hrs · 16,635 cycles

PASSENGER DOOR HAS AN AIR LEAK, MAKING A LOUD NOISE. INSPECTED, CLEANED AND LUBRICATED AS REQUIRED, PERFORMED OPS TEST OF THE PASSENGER DOOR IAW AMM 52-11-00, NO DAMAGE OR DEFECTS FOUND, OP'S CHECK GOOD AT THIS TIME.

Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR) · airframe 22,946 hrs · 16,334 cycles

LT DOOR CAUTION MESSAGE. PERFORMED OP'S CHECK OF EMERGENCY DOOR WARNING SYS IAW AMM 52-70-00, NO MESSAGES AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 22,865 hrs · 16,272 cycles

LEFT EMERGENCY EXIT DOOR UNSAFE INDICATION. REMOVED AND INSPECTED DOOR, INSTALLED DOOR, NO DEFECTS NOTED. PERFORMED OPS CHECK IAW AMM 52-21-00. OPS CHECEDK GOOD, NO MESSAGE NOTED.

Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR) · airframe 22,799 hrs · 16,221 cycles

PAX DOOR CAUTION MESSAGE. R & R PX47 IAW AMM 52-70-04. OPS CHECKED OK IAW AMM 52-70-00.

Part: COVER — BROKEN (OVERWING DOOR) · airframe 22,395 hrs · 15,920 cycles

RT OVERWING DOOR HANDLE COVER BROKE OFF. SECURED EMERGENCY DOOR HANDLE IAW AMM 56-30-02.

Part: WARNING MESSAGE — ILLUMINATED (SERVICE DOOR) · airframe 2,217,304 hrs · 15,764 cycles

SERVICE DOOR OUTER HANDLE CAUTION MESSAGE.

Part: SEAL — TORN (PAX DOOR) · airframe 22,137 hrs · 15,734 cycles

PAX DOOR SEAL HAS A TEAR AT TOP LT CORNER. REPLACED SEAL IAW AMM 52-11-07.

Part: LENS — CRACKED (EMERGENCY LIGHTS) · airframe 22,137 hrs · 15,734 cycles

LEFT OVERWING EMERGENCY EXIT SIDE LIGHTS LENS CRACKED. R & R LT OVERWING EMERGENCY EXIT SIDE LIGHT LENS IAW AMM 33-51-15.

Part: PLACARD — MISINSTALLED (CABIN) · airframe 22,137 hrs · 15,734 cycles

PAX DOOR CLOSED PLACARD UPSIDE DOWN. R & R CLOSED PLACARD ON PAX DOOR IAW 20-60-04.

Part: BATTERY — DISCONNECTED (FLASHLIGHT) · airframe 22,137 hrs · 15,734 cycles

CABIN FLASHLIGHT INOPERATIVE. CONNECTED BATTERY CONTACTS ON FLASHLIGHT AS REQUIRED. OP'S CHECKED GOOD AT THIS TIME, IAW AMM 25-61-00.

Part: ANGLE — CORRODED (ZONE 100) · airframe 22,135 hrs · 15,733 cycles

GALLEY SERVICE DOOR SILL MOUNTING ANGLE IS CORRODED. R & R SERVICE DOOR SILL MOUNTING ANGLE IAW SRM 53-21-23,51-11-00, 51-21-06, AND 51-42-06.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 22,135 hrs · 15,733 cycles

SERVICE DOOR THRESHOLD LOWER SEAL STRIKER IS CORRODED. REMOVED SERVICE DOOR PROTECTOR PLATE IAW AMM 53-21-23, REMOVED SEAL STRIKER IAW SRM 51-42-06, INSTALLED NEW SEAL STRIKER IAW SRM 51-42-06. INSTALLED SERVICE DOOR PROTECTOR PLATE IAW AMM 53-21-23.

Part: FITTING — CORRODED (ZONE 100) · airframe 22,135 hrs · 15,733 cycles

RT INBD INTERCOSTAL FLOOR MOUNT MACHINE FITTING IS CORRODED. R & R RT INBD INTERCOSTAL FLOORMOUNT MACHINE FITTING IAW SRM 51-42-21.

Part: CABLE — BROKEN (PAX DOOR) · airframe 22,135 hrs · 15,733 cycles

PASSENGER DOOR, BOTTOM CABLE ASSY IS BROKEN. R & R PASSENGER DOOR, BOTTOM CABLE ASSY IAW AMM 52-11-13.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 22,135 hrs · 15,733 cycles

FS 279.0, BL 0.0 FLOOR SUPPORT IS DAMAGED. R & R FS 279.0 BL 0.0 FLOOR SUPPORT IAW SRM 51-42-21,51-42-06, 51-45-00.

Part: ATTACH FITTING — CORRODED (BS 290) · airframe 22,135 hrs · 15,733 cycles

STORAGE CLOSET FLOOR FITTING AT BS 290 LT OTBD SIDE IS CORRODED. R & R STORAGE CLOSET FLOOR FITTING IAW SRM 51-42-21.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 21,730 hrs · 15,451 cycles

ON APPROACH INTO SDF RECEIVED O/B SPOILERON CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. C/W CRJ 700 FIM TASK 27-61-00-810-820, MSG NO LONGER PRESENT. OPS CHECK GOOD.

Part: RESERVOIR — FAILED (HYDRAULIC SYS) · airframe 20,880 hrs · 14,831 cycles

EN ROUTE, RECEIVED HYD 3 HI TEMP MSG. EMERGENCY DECLARED, A/C DIVERTED, LANDED SAFELY. REMOVED AND REPLACED NR 3 RESERVOIR. OPS CHECK GOOD.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,693 hrs · 14,646 cycles

FLOOR SILL FWD OF SERVICE DOOR CORRODED. CUT OUT DAMAGED AREA AND INSTALLED A DOUBLER IAW BOMBARDIER REO 670-53-21-803.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,578 hrs · 14,598 cycles

LEFT SIDE FS 280.00 LOWER BULKHEAD WEB IS CORRODED BEYOND ALLOWABLE LIMITS. REPLACED LOWER FS280.00 LOWER BULKHEAD WEB BY REMOVING DISCREPANT WEB AND FABRICATING NEW SERVICABLE WEB FROM 7075-T6 .040, TRANSFERRING HOLES AND WET INSTALLING IAW BOMBARDIER SRM53-11-10 201-003-A01 REPAIR "B" PRIMED & PAINTED.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,578 hrs · 14,598 cycles

PAX DOOR THRESEHOLD MID ANGLE CAP CORRODED P/N SH670-31825-5. REPLACED PART SH670-31825-5 IAW BOMBARDIER SRM 51-452-06, AMM 20-21-00.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,578 hrs · 14,598 cycles

RIGHT SIDE FS 280 LOWER BULKHEAD WEB IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED RIGHT SIDE FS 280 LOWER BULKHEAD IAW SRM 53-11-10-201-003.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,578 hrs · 14,598 cycles

FS 280 BEAM CORRODED. REMOVED AND REPLACED FS 280 FLOORBEAM IAW REO-B-53R0005.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,578 hrs · 14,598 cycles

PAX DOOR THRESHOLD FORWARD ANGLE CAP CORRODED P/N: SH670-31821-3. REPLACED PART SH670-31821-3 IAW BOMBARDIER SRM 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 20,578 hrs · 14,598 cycles

ANGLE AT FS 280.00 LBL 9.0 IS CRACKED PART CC670-34144-1. REPLACED ANGLE PART CC670-34144-1 AT FS 280.00 BEAM AND LBL 9.0 IAW BOMBARDIER SRM 51-42-21.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,578 hrs · 14,598 cycles

FS 280.00 CAMLOCK ANGLE CORRODED P/N CC670-33292-13. REPLACED CAMLOCK ANGLE PART CC670-33292-13 AT FS 280.00 CROSSBEAM IAW BOMBARDIER SRM 51-42-06.

Part: TRU — FAILED (NR 2) · airframe 16,262 hrs · 11,557 cycles

RAMP CREW REPORTED HOT BURNING SMELL COMING FROM NOSE OF A/C. OPENED TRU DOOR, SMOKE OBSERVED. A/C EVACUATED AND SHUT DOWN. SMOKE STOPPED, BURNING SMELL LINGERED. INSPECTED A/C FOUND ESS TRU NR 2 FAILED. TRANSFERRED TO DEFERRED LIST PER MEL 24-31-01 CAT B.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 14,947 hrs · 10,654 cycles

LEFT SIDE OF FS 280 LATERAL FLOORBEAM HAS LEVEL 2 & 3 CORROSION FROM LBL 9 - LBL 36. CUT OUT CORRODED SECTION OF BEAM AND SPLICED IN A NEW SECTION USING REPAIR DOUBLERS PER REO 670-53-11-047.

Part: CONTROLLER — FAULTY (ACS) · airframe 13,881 hrs · 9,873 cycles

EN ROUTE FROM ORD TO JFK RECEIVED RT ENG BLEED CAUTION MSG. A/C RETURNED TO ORD LANDED SAFELY. REMOVED AND REPLACED ACS CONTROLLER. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 13,880 hrs · 9,872 cycles

EN ROUTE FROM ORD TO JFK RECEIVED RT ENG BLEED CAUTION MSG. A/C RETURNED TO ORD LANDED SAFELY. PERFORMED OPS CHECK OF BLEED AIR SYSTEM PER FIM. NO FAULTS FOUND.

Part: PRECOOLER — FAULTY (A/C BAY) · airframe 7,816 hrs · 5,731 cycles

FLIGHT 5169 - AFTER TAKEOFF FROM CVG RECEIVED AN AIR DUCT WARNING FOLLOWED BY LEFT PACK SHUT-OFF CAUTION, FLIGHT RETURNED TO THE FIELD. REPLACED THE LEFT PACK PRE-COOLER.

Part: ACM — SMOKE (RIGHT) · airframe 7,654 hrs · 5,623 cycles

FLIGHT 5237 - DURING TAXI-OUT OF CVG THE CABIN FILLED WITH SMOKE, CREW DECLARED AN EMERGENCY. DEPLANED PASSENGERS ON TAXI-WAY AND BUSSED BACK TO THE TERMINAL. VERIFIED THAT THE RIGHT ACM HAD SEIZED, DEFERRED THE RIGHT ACM PER MEL 21-51-01.

Part: SEAT TRACK — GOUGED (BS 669-977) · airframe 7,609 hrs · 5,594 cycles

TWO GOUGES ON RIGHT FLOOR SEAT TRACK EXCEED DAMAGE LIMITATIONS PER SRM 53-11-49. REPLACED SEAT TRACK IAW REO 670-53-00-074.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 3 · airframe 7,609 hrs · 5,594 cycles

FLOOR SUPPORT ANGLE CORRODED. REPLACED ANGLE IAW SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 7,609 hrs · 5,594 cycles

FLOOR SUPPORT BEAM AT FS 280.0 FOUND CRACKED. REPAIRED CRACKED AREA IAW COMAIR EA 70-5310-01329.

Part: FITTING — CHAFED (HORIZONTAL STAB) · airframe 7,609 hrs · 5,594 cycles

LEFT AND RIGHT HORIZONTAL STAB PIVOT PIN ANTI-ROTATION TAB FITTINGS ARE CHAFED. REPAIRED IAW REO 670-55-11-047.

Part: BULKHEAD — CORRODED (BS 280) · corrosion level 2 · airframe 7,609 hrs · 5,594 cycles

CORROSION FOUND ON FS 280 BULKHEAD WEBS (MINOR SURFACE CORROSION). BLENDED MINOR SURFACE CORROSION (LESS THAN 10%) AND RESTORED PROTECTIVE FINISH IAW SRM 51-21-16.

Part: MOTOR — MALFUNCTIONED (STAB TRIM) · airframe 5,262 hrs · 4,105 cycles

FLIGHT 5764 - STAB TRIM AND MACH TRIM CAUTION. CND RESET SYSTEM, OPERATIONAL CHECK WAS NORMAL.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 4,419 hrs · 3,463 cycles

FLIGHT 5430 - LEFT REVERSER UNSAFE. DEFERRED MAINTENANCE PER MEL.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 3,253 hrs · 2,554 cycles

FLIGHT 5399 COPILOT WINDSHIELD IS CRACKED. REPLACED WINDSHIELD.

Part: DOOR — OPEN (O2 SERVICE DOOR) · airframe 890 hrs · 707 cycles

FLIGHT 5640 CREW 02 PRESSURE GAUGE READS----. COULD NOT DUPLICATE. FOUND 02 SERVICE DOOR OPEN, CLOSED DOOR, SYSTEM FUNCTION NORMAL.

Part: PSEU — MALFUNCTIONED (MLG) · airframe 191 hrs · 182 cycles

FLIGHT 5084 GEAR DISAGREE WARNING, L/G FAILED TO EXTEND. REPLACED THE PSEU.

Part: SELECTOR VALVE — UNRELIABLE (LANDING GEAR) · airframe 188 hrs · 180 cycles

FLIGHT 5661 GEAR DISAGREE WARNING AFTER T/O. REPLACED THE L/G SELECTOR VALVE.