N659CA

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 36,380 hrs · 27,767 cycles

DISCREPANCY: FWD EQUIPMENT BAY RH FLOOR NEAR AIR DRIVEN GENERATOR CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O 80799 W/C 2184.

Part: STRINGER — CORRODED (BS 280-319) · airframe 36,380 hrs · 27,767 cycles

STRINGER 26L BETWEEN F.S. 280.00 TO F.S. 319.00 AND F.S. 333.OO TO F.S. 364.OO CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVAMX W/O 80799 W/C 1144.

Part: STRINGER SPLICE — CORRODED (BS 319-333) · airframe 36,380 hrs · 27,767 cycles

STRINGER 26L SPLICE BETWEEN F.S. 319.00 TO F.S 333.00 CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O 80799 W/C 1143.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 36,380 hrs · 27,767 cycles

PAX DOOR AFT PULL IN CAM BRACKETS CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O 80799 W/C 8083

Part: FITTING — DENTED (CRGO DOOR FRAME) · airframe 36,380 hrs · 27,767 cycles

AFT BAGGAGE BAY DOOR CUT OUT AREA DENT ON BOTH FWD AND AFT CROTCH FITTING ON DOOR CUT OUT. CORRECTIVE ACTION TO BE ACCOMPLISHED ON W/O 80799 W/C 8088

Part: MOUNT — CORRODED (W-B FAIRING) · airframe 36,380 hrs · 27,767 cycles

AFT WING TO BODY FAIRING 195DL AND 196DR AFT FRAME MOUNT AT F.S. 939.00 CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O 80799 W/C 1162.

Part: STRINGER — CORRODED (BS 295-319) · airframe 36,380 hrs · 27,767 cycles

STRINGER 25L BETWEEN F.S. 295.00 TO F.S. 319.00 AND STIRNGER 25L SPLICE BETWEEN F.S. 319.00 TO F.S. 333.OO CORRODED. CORRECTIVE ACTION TO BE ACCOPLISHED ON AVMAX W/O 80799 W/C 1131.

Part: FRAME — CORRODED (BS 364) · airframe 36,380 hrs · 27,767 cycles

FRAME AT F.S. 364.00 BETWEEN STRINGER 26R TO STRINGER 25R CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON W/O 80799 W/C 1147.

Part: BRACKET — CORRODED (AFT BODY FAIRING) · airframe 36,380 hrs · 27,767 cycles

AFT FUSELAGE BODY FAIRINGS 195DL AND 196DR CENTER LINE ATTACHMENT BRACKET CORRODED AND BRACKET STIFFNER RIVETS PULLED THROUGH. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O 80779 W/C 1155.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 36,380 hrs · 27,767 cycles

RH BULKHEAD LOWER WEB AT F.S. 280.00 CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O 80799 W.C 1161.

Part: STRINGER — CORRODED (BS 319-349) · airframe 36,380 hrs · 27,767 cycles

STRINGER 27 BETWEEN F.S. 319.00 TO 349.00 CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O 80799 W/C 1141.

Part: GUARD — GOUGED (CRGO DOOR ROLLER) · airframe 36,380 hrs · 27,767 cycles

AFT BAGGAGE BAY DOOR GOUGED ON FWD DOOR ROLLER TRACK GAURD. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O 80799 W/C 8085.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 36,380 hrs · 27,767 cycles

QUARTER TURN ATTACHEMENT BRACKET, ATTACHED TO F.S. 280.00 FLOOR BEAM CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON W/O 80799 W/C 1158.

Part: DOOR — CORRODED (E/E BAY) · airframe 36,380 hrs · 27,767 cycles

MAIN AVIONICS DOOR CORRODED UNDER DOOR SEAL AT FORWARD SIDE. CORRECTIVE ACTION TO BE ACCOMPISHED ON AVMAX W/O 80799 W/C 8074

Part: TRIPLER — GOUGED (BS 977) · airframe 36,380 hrs · 27,767 cycles

EXTERNAL FUSELAGE SKIN REPAIR, TRIPPLER AT F.S. 977.00 GOUGED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON W/O 80799 W/C 1167.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 36,380 hrs · 27,767 cycles

RH FLOOR SILL AT AFT SIDE OF F.S. 280.00 FLOOR BEAM CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O 80799 W/C 1173.

Part: WARNING MESSAGE — FALSE ACTIVATION (ELEVATOR SPLIT) · airframe 31,620 hrs · 23,413 cycles

ELEVATOR SPLIT CAUTION MESSAGE IN FLIGHT. PERFORMED OPS CHECK OF ELEVATOR SYS IAW AMM 27-31-00, OPS CHECKED GOOD, SUSPECT AUTO PILOT CAUSING MESSAGE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,374 hrs · 23,192 cycles

RT SKIN DAMAGED AT FRAME STATION 202.00 AT 2 O'CLOCK POSITION. REMOVED AND REPLACED SKIN IAW REO 670-53-11-1311, DATED 2017-08-15, SRM 51-24-36, 51-40-11, 51-42-06 AND CRJ700 NDTM 51-20-006.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 31,374 hrs · 23,192 cycles

VERTICAL STABILIZER LT FWD DRAG ANGLE IS CRACKED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-018 REV A DATED 2016-11-10 AND REO 670-55-31-099 DATED 2017-07-27.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 31,374 hrs · 23,192 cycles

VERTICAL STABILIZER LT AFT DRAG ANGLE IS CRACKED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-018 REV A DATED 2016-11-10 AND REO 670-55-31-099 DATED 2017-07-27.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 31,374 hrs · 23,192 cycles

GALLEY SERVICE DOOR LOWER SEAL STRIKER IS CORRODED. REMOVED AND REPLACED GALLEY SERVICE DOOR LOWER SEAL STRIKER IAW SRM 51-25-06, 51-25-16, 51-42-06, 51-42-21, 51-41-02, AND AMM 53-21-27.

Part: FRAME — CRACKED (BS 333) · airframe 31,374 hrs · 23,192 cycles

FRAME BS 333 CRACKED BETWEEN STRINGERS 0 AND 1. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-21, SRM 51-42-06, SRM 51-40-11, AND SRM 51-21-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,374 hrs · 23,192 cycles

SKIN DAMAGED AT FS 235 BETWEEN STG 13R AND 14R. CUT OUT DAMAGED SKIN AT 235 BETWEEN STGRS 13R AND 14R FABRICATED AND INSTALLED REPAIR PACKER AND DOUBLER IAW REO-670-53-11-1297 REV(P1), DATED 2017/07/29 AND REO-670-53-11-1297 REV-, DATED 2017/08/06 AND SRM 51-42-20, SRM53-11-01, SRM51-21-11, SRM51-25-06, SRM53-00-01, AND SRM51-25-01.

Part: BRACKET — CRACKED (RT WING SLAT) · airframe 31,374 hrs · 23,792 cycles

RIGHT WING SLAT TRACK HOUSING BRACKET CRACKED. REPAIRED THE SLAT TRACK HOUSING BRACKET IAW REO 670-57-42-577, REV -.

Part: WEB — CRACKED (BS 193) · airframe 31,374 hrs · 23,192 cycles

ELECTRICAL BAY FLOOR WEB IS CRACKED AT BS 193. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-11-43.

Part: MOUNT — CRACKED (ZONE 200) · airframe 31,374 hrs · 23,792 cycles

MOUNTING PLATE CRACKED. REMOVED AND REPLACED MOUNTING PLATE IAW SRM 51-42-06, AND 51-41-11.

Part: AXLE — CORRODED (LT MLG) · airframe 31,374 hrs · 23,192 cycles

LEFT MAIN LANDIN GEAR AXLE HAS CORROSION. REMOVED AND REPLACED THE AXLE.

Part: BRACKET — CRACKED (LE SLAT) · airframe 31,374 hrs · 23,192 cycles

LT WING SLAT TRACK (1-3) HOUSING BRACKET CRACKED. REPAIRED LT WING SLAT TRACK (1-3) HOUSING BRACKET IAW REO 670-57-42-577, DATED 2016-12-02.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 31,374 hrs · 23,192 cycles

RT FS 280 CROSSBEAM CORRODED OUT OF LIMITS. ACCOMPLISHED FS 280 CROSSBEAM REPAIR IAW SRM 53-11-41-201-003-A01.

Part: TRIPLER — GOUGED (FUSELAGE) · airframe 31,374 hrs · 23,192 cycles

TRIPLER AT FS 977 GOUGED IN 3 PLACES. REMOVED AND REPLACED TRIPLER/DOUBLER AT FS 977 IAW REO 670-53-00-290, REV D, DATED 09-10-2015.

Part: PISTON — CORRODED (RT MLG) · airframe 31,374 hrs · 23,192 cycles

EVALUATED AND REPAIRED RT MLG PISTON/AXLE ASSY IAW AMM 32-11-09, NDT MANUAL 51-20-008-230, SERVICE BULLETIN 49200-32-85 DATED 23 JUL 14, REO 670-32-11-361.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 31,374 hrs · 23,792 cycles

PASSENGER DOOR POWER ASSIST MOTOR MOUNTING BRACKET IS CRACKED. REMOVED AND REPLACED PASSENGER DOOR POWER ASSIST MOTOR MOUNTING BRACKET (P/N: 601R317745-7) IAW SRM 51-42-06 AND CRJ700 SRM 51-40-11.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 31,374 hrs · 23,192 cycles

LT FS 280 CROSSBEAM CRACKED. ACCOMPLISHED FS 280.00 CROSSBEAM REPAIR IAW SRM 53-11-41-201-003-A01.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,374 hrs · 23,192 cycles

SKIN DAMAGED AT FS 169 AT THE 3 O'CLOCK POSITION. REMOVED AND REPLACED SKIN AT FS 169 IAW REO 670-53-11-1310 DATED 2017-08-17, SRM 51-42-21, SRM 51-42-06, SRM 51-42-13, SRM 51-40-11.

Part: LIGHT — MISSING (CABIN) · airframe 30,728 hrs · 22,629 cycles

EMERGENCY EXIT ROW FLOOR LIGHTING MISSING. REPLACED EMERGENCY LIGHT IAW AMM 25-25-01.

Part: FITTING — DEFECTIVE (CABIN DOOR) · airframe 29,649 hrs · 21,794 cycles

MAIN CABIN DOOR WILL NOT CLOSE, LOCK. R & R LOCK INDICATOR FITTING IAW AMM 52-11-02. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,521 hrs · 21,693 cycles

EMERGENCY CEILING LIGHT OUT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,898 hrs · 21,215 cycles

MOST AFT CEILING LEVEL EMER FLOODLIGHTS INOPERATIVE. DEFERRED CEILING LEVEL EMER FLOODLIGHTS IAW MEL 33-51-01B-2A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,834 hrs · 21,165 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,605 hrs · 21,001 cycles

CEILING EMER FLOOD LIGHT INOPERATIVE AT ROW 9. DEFERRED CEILING EMER FLOOD LIGHT INOPERATIVE AT ROW 9 IAW MEL 33-51-01B CAT C.

Part: FLOOR SUPPORT — CORRODED (BS 1031-1051) · airframe 28,533 hrs · 20,955 cycles

CORROSION FOUND ON FLOOR SUPPORT LBL 9 BETWEEN FS 1031-1051.

Part: LIGHT — MISSING (EXIT SIGN) · airframe 28,495 hrs · 20,932 cycles

ALL THREE EMER EXIT SIGNS ARE MISSING LIGHT BULBS. REPLACED LIGHT BULBS IN ALL 3 EMER EXIT SIGNS IAW AMM 33-51-05. OPERATIONS CHECKED GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 28,444 hrs · 20,891 cycles

EMERGENCY EXIT SIGN AT ROW 4 & 5 INOPERATIVE. DEFERRED EMER FLOOD LIGHT AT ROW 4 & 5 IAW MEL 33-51-01B CAT C.

Part: SIGN — UNSECURE (CABIN) · airframe 28,382 hrs · 20,884 cycles

EMERGENCY EXIT SIGN OVER SERVICE DOOR NOT SECURE. SECURED EMER EXIT SIGN OVER SERVICE DOOR IAW AMM 20-21-00. EMER LIGHT OPERATIONS CHECK IAW AMM 33-51-00.

Part: GLOWSTRIP — UNSECURE (CABIN) · airframe 28,055 hrs · 20,593 cycles

PHOTO LUMINESCENT STRIP AT ROW 12 NOT SECURE. REINSTALLED PHOTO LUMINESCENT STRIP AT ROW 12 IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,541 hrs · 20,203 cycles

STRINGER 21L AT FS 1060 CORRODED. REPAIRED STRINGER IAW REO 670-53-61-1158 DATED 15 SEPT 2015. P1 DATED 30 AUG 2015 & P3 DATED 11 SEPT 2015, SRM 53-61-03 & AMM 21-23-21. NDT PERFORMED WO A15-1070 DATED 13 SEPT 2015.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,541 hrs · 20,203 cycles

RIGHT INBD & OTBD INTERCOSTAL AT FS 364.00, JUST AFT OF AVIONICS DOOR ARE CORRODED. R & R RT INBD & OTBD INTERCOSTAL, PN`S SH670-32075-4 & SH670-32077-4 AT FS 364.00 IAW SRM 51-42-06, 51-42-21 & 51-40-11.

Part: SHROUD — GOUGED (CARGO DOOR) · airframe 27,541 hrs · 20,203 cycles

AFT BAGGAGE BAY DOOR HANDLE SHROUD IS GOUGED. BLENDED GOUGES TO SMOOTH CONTOUR WITHIN LIMITS IAW REO 0670-52-31-067, DATED 4 SEPT 2015.

Part: SKIN — DENTED (TE FLAP) · airframe 27,541 hrs · 20,203 cycles

LEFT INBD FLAP HAS 2 SKIN DENTS. REPAIRED LT INBD FLAP SKIN DENTS BY CUTTING OUT DAMAGE. FABRICATING REPAIR PARTS & INSTALLING IAW REO 670-57-52-323, DATED 5 SEPT 2015.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,541 hrs · 20,203 cycles

STRINGER 26R HAS CORROSION, BETWEEN FS 295 TO 310, FS 319 TO 333 & FS 333 TO 349. R & R STRINGER 26R, PN SH670-31372-4S & SH670-31634-2 IAW SRM 51-42-06, 51-42-21, 51-40--11, & 51-21-16. WO 80314 & WC 1106.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 27,541 hrs · 20,203 cycles

CROSSBEAM 349 HAS CORROSION ADJACENT TO THE OTBD SIDE OF THE RT SEAT RAIL. PERFORMED BLEND OUT OF AREA IAW REO 670-53-21-1216, DATED 03 SEPT 2015.

Part: BEAM — CORRODED (FUSELAGE) · airframe 27,541 hrs · 20,203 cycles

FS 280.00 BEAM, LT & RT HAND SIDES ARE CORRODED. R & R LT & RT BEAM AT FS 280.00 PN CC670-34175-75 IAW SRM 53-11-41, 51-42-21, 51-42-13, 51-42-06, 51-40-11, 51-42-22, AMM 20-70-00 & SB-670BA-53-026 REV B DATED 05 DEC 2006.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,541 hrs · 20,203 cycles

1/4 TURN ANGLE AT FS 280.00, FWD SIDE, IS CORRODED. R & R 1/4 TURN ANGLE AT FS 280.00, PN CC670-33292-13, IAW SRM 51-21-11, 51-25-16, 51-42-06, 51-40-11, 51-42-21 & 51-42-13.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,541 hrs · 20,203 cycles

PASSENGER ENTRY FLOORBOARD MIDCAP ANGLE IS CORRODED. R & R MIDCAP ANGLE IAW SRM 51-40-00, 51-40-11, 51-21-11, & 51-45-00. WO 80314 & WC 8067.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 27,541 hrs · 20,203 cycles

PASSENGER DOOR KICK PLATE ANGLE CORRODED. R & R PASSENGER DOOR KICK PLATE ANGLE, PN SH670-31785-3S, IAW SRM 51-42-21, 51-21-11, 51-40-11 & 51-45-00.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 27,541 hrs · 20,203 cycles

FORWARD BAGGAGE DOOR, FWD UPPER ANGLE CRACKED. R & R FWD UPPER ANGLE PN LE670-39942-5 IAW SRM 51-42-13 & 51-42-06.

Part: TRIPLER — GOUGED (FUSELAGE) · airframe 27,541 hrs · 20,203 cycles

LOWER FUSELAGE AT FS 977.00 HAS GOUGE IN PREVIOUS MAJOR REPAIR. REMOVED TRIPLER, FABRICATED TRIPLER & INSTALLED IAW REO 670-53-00-290 REV C DATED 21 MAR 2013.

Part: FITTING — CORRODED (GALLEY) · airframe 27,541 hrs · 20,203 cycles

THREE CORRODED FLOOR FITTINGS ON GALLEY 1. R & R THREE FLOOR FITTINGS PN CD8P2019-7C-760, PN CDSP2019-7C-760 & PN A661091-1 IAW CMM 25-33-42.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 27,135 hrs · 19,904 cycles

PASSENGER DOOR OUTER HANDLE CAUTION MSG IN FLIGHT. DEFERRED IAW MEL 52-70-01 CAT A.

Part: DAMPER — WEAK (PAX DOOR) · airframe 27,062 hrs · 19,850 cycles

PASSENGER DOOR OPENING DAMPER WEAK. DEFERRED AFT GAS DAMPER ON PAX DOOR IAW MEL 52-11-01B CAT C.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 26,967 hrs · 19,782 cycles

MASTER WARNING GEAR DISAGREE MSG AFTER TAKEOFF. JACKED ACFT IAW AMM 07-11-01. PERFORMED OPERATIONAL TEST OF LG PSS & SWUNG GEAR IAW AMM 32-61-00 & 32-30-00. OPERATIONS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 26,967 hrs · 19,782 cycles

MASTER WARNING GEAR DISAGREE MSG AFTER TAKEOFF. JACKED ACFT IAW AMM 07-11-01. PERFORMED OPERATIONAL TEST OF LG PSS & SWUNG GEAR IAW AMM 32-61-00 & 32-30-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,577 hrs · 19,478 cycles

SECOND FROM AFT CEILING EMER LIGHT INOPERATIVE. DEFERRED CABIN EMER LIGHT IAW MEL 33-51-01B CAT C.

Part: WHEEL — COLLAPSED (PAX DOOR) · airframe 26,488 hrs · 19,383 cycles

PAX DOOR WHEEL COLLAPSED ON DEPLOYMENT. INSPECTED FOR DAMAGE, NONE NOTED. PERFORMED OPERATIONS CHECK. CHECKED GOOD IAW AMM 52-11-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,439 hrs · 19,376 cycles

EMERGENCY LIGHT NEAR LAVATORY INOPERATIONS. R & R EMER LIGHT BULBS IAW AMM 33-50-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 25,329 hrs · 18,494 cycles

LEFT EMER EXIT ARROW PLACARD LIGHT INOPERATIVE. RE-LAMPED SIGN IAW 33-50-14. OPERATIONS CHECKED GOOD.

Part: PLACARD — MISSING (CABIN) · airframe 25,163 hrs · 18,360 cycles

EMERGENCY EXIT DOOR PLACARD MISSING FROM TRAY TABLE IN 12A. DEFERRED IAW NEF 25-500-1.

Part: PLACARD — WORN (PAX DOOR) · airframe 25,163 hrs · 18,360 cycles

PAX DOOR OPEN PLACARD IS WORN. R & R PAX DOOR PLACARD IAW AMM 20-60-04.

Part: FITTING — LOOSE (HYDRAULIC SYS) · airframe 24,994 hrs · 18,226 cycles

NUMBER 1 ENG DRIVEN PUMP CAUTION LIGHT, LOSS OF HYD FLUID ON NR 1 SYS. INSPECTED & FOUND LOOSE FITTING GOING TO THE NR 1 ACFT HYD PUMP. TIGHTENED, LEAK & OPERATIONS CHECKED IAW AMM 29-10-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,684 hrs · 17,956 cycles

EMERGENCY CEILING LIGHT AT ROW 15 INOPERATIVE. DEFERRED LIGHT IAW MEL 33-51-01B CAT C.

Part: TRANSCEIVER — MALFUNCTIONED (RADAR ALTIMETER) · airframe 24,265 hrs · 17,657 cycles

GLD UNSAFE CAUTION MESSAGE AT TAKEOFF 70 KAIS. RE RACKED RADAR ALTIMETER TRANSCEIVER & CLEANED ANTENNA. PERFORMED BITE TEST OF RADIO ALTIMETER IAW AMM 34-44-01, NO DEFECTS AT THIS TIME.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 24,002 hrs · 17,445 cycles

STALL FAIL MESSAGE ON TAKEOFF ROLL BELOW 70 KNOTS. FOUND P3 DRAIN FULL OF FLUID, DRAINED FLUID IAW CRJ700 AMM 34-11-15. VISUALLY INSPECTED AOA VANES & FOUND NO DEFECTS. PERFORMED OPERATIONS TEST OF SPS IAW CRJ700 AMM 27-35-01, OPERATIONS CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED (PAX DOOR) · airframe 23,021 hrs · 16,659 cycles

PAX DOOR LATCH CAUTION MESSAGE WITH WHITE PROX SYS, 1 MESSAGE.

Part: DRAIN — CLOGGED (PAX DOORWAY) · airframe 22,890 hrs · 16,578 cycles

PAX DOOR DRAINS ARE FILLED WITH DEBRIS. REMOVED DEBRIS FROM PAX DOOR DRAIN AS REQUIRED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,884 hrs · 16,573 cycles

CEILING EMERGENCY LIGHT INOPERATIVE ROW 9. REPLACED LAMPS IAW AMM 33-51-07, OP'S CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,470 hrs · 16,256 cycles

EMERGENCY FLOOD LIGHT INOPERATIVE IN ROW 10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,455 hrs · 16,242 cycles

WHITE CALL LIGHT ON EXIT ROW SIGN WILL NOT ILLUMINATE.

Part: WINDSCREEN — CRACKED (COCKPIT) · airframe 22,154 hrs · 16,017 cycles

CAPTAINS WINDSHEILD SHATTERED AT 12,000 FT. R & R CAPTAINS WINDSHIELD IAW AMM 56-11-01.

Part: HANDLE — UNSECURE (EMERGENCY EXIT) · airframe 22,090 hrs · 15,957 cycles

OVERWING EMERGENCY EXIT HANDLE COVER AT SEAT 12A & 12B WILL NOT STAY UP. SECURED HANDLE IAW AMM 52-221-00. OK TO RETURN TO SERVICE.

Part: CABLE — FRAYED (PAX DOOR) · airframe 22,041 hrs · 15,927 cycles

PAX DOOR MOTOR CABLE FRAYED. R & R PAX DOOR MOTOR CABLE IAW AMM 52-11-03. OP'S CHECK GOOD AT THIS TIME.

Part: ANGLE — CORRODED (SERVICE DOORWAY) · airframe 22,041 hrs · 15,927 cycles

SERVICE DOOR LOWER CUT OUT SILL ANGLES HAVE CORROSION: R & R OUT OF LIMITS CORRODED ANGLE IAW SRM 51-42-06.

Part: LINER — DAMAGED (SERVICE DOOR) · airframe 22,041 hrs · 15,927 cycles

SERVICE DOOR LINER BOTTOM EDGE DAMAGED. R & R LINER ON SERVICE DOOR IAW AMM 25-26-07.

Part: INTERCOSTAL — CORRODED (E/E BAY DOOR) · airframe 22,041 hrs · 15,927 cycles

AVIONICS BAY DOOR SUPPORT STRUCTURE INTERCOSTAL AT LT SIDE OF STRINGER 27, CORRODED. R & R INTERCOSTAL IAW SRM 51-42-06.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 22,041 hrs · 15,927 cycles

FLOOR PANEL 193AR SHOWS SIGNS OF WEAR. R & R CORRODED FLOOR PANEL IAW SRM 51-42-13.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 22,041 hrs · 15,927 cycles

FS 280 FLOORBEAM HAS CORROSION ON BOTH SIDES. R & R FS 280 FLOORBEAM IAW REO 670 53-11-047, REV E.

Part: TENSION TIE — CHAFED (PAX DOOR) · airframe 22,041 hrs · 15,927 cycles

PAX DOOR UPPER TENSION TIE HAS CHAFE MARK. R & R UPPER TENSION TIE IAW AMM 52-11-19, OP'S CHECK GOOD AT THIS TIME.

Part: PLATE — WORN (PAX DOOR) · airframe 22,041 hrs · 15,927 cycles

PAX DOOR CLOSING PLATES HAVE A WORN FASTENER. R & R WORN FASTENERS IAW SRM 51-42-13.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,132 hrs · 15,240 cycles

ROW 12 EMERGENCY LIGHTS INOPERATIVE. LAMPED EMERGENCY LIGHT IAW IAW AMM 33-51-05.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 19,887 hrs · 14,304 cycles

EMERGENCY LIGHTS WILL NOT EXTINGUISH WHILE IN THE ARMED POSITION. RESET EMERGENCY LIGHT SYS IAW AMM 33-51-00. NO DEFECTS NOTED.

Part: PLACARD — WORN (PAX DOOR) · airframe 19,658 hrs · 14,120 cycles

PAX DOOR OPEN PLACARD WORN. INSTALLED NEW PLACARD IAW AMM 11-30-03.

Part: PAINT — WORN (INDICATOR) · airframe 19,658 hrs · 14,120 cycles

PAX DOOR UPPER AFT GREEN INDICATOR PAINT WORN. REPAINTED PAX DOOR UPPER AFT GREEN INDICATOR MARKING IAW AMM 52-11-00.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 19,658 hrs · 14,120 cycles

RT OVERWING EMERGENCY EXIT DOOR HANDLE COVER LOOSE. RESECURED RT OVERWING EMERGENCY EXIT HANDLE COVER IAW AMM 52-21-00.

Part: LIGHT — WORN (CABIN) · airframe 19,658 hrs · 14,120 cycles

EMERGENCY LIGHT WORN RT SIDE 3C. REPLACED LIGHT IAW 33-51-01.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 19,658 hrs · 14,120 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN BACK LIGHTING HAS BURN OUT BULBS. R & R BULBS IAW AMM 33-51-05.

Part: LIGHT — WORN (CABIN) · airframe 19,658 hrs · 14,120 cycles

EMERGENCY LIGHT WORN RT SIDE 2C. REPLACED LIGHT IAW 33-51-01.

Part: MEGAPHONE — DAMAGED (CABIN) · airframe 19,658 hrs · 14,120 cycles

MEGAPHONE MISSING SCREW. R & R MEGAPHONE IAW AMM 25-61-14.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,658 hrs · 14,120 cycles

PAX DOOR EMERGENCY EXIT LIGHTS BURNED OUT. R & R LAMPS IAW AMM 33-51-05.

Part: LIGHT — WORN (CABIN) · airframe 19,658 hrs · 14,120 cycles

EMERGENCY LIGHT AT 17B WORN. REPLACED LIGHT IAW 33-51-01.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND INSTALLED SERVICABLE POWER SUPPLY UNIT IAW AMM 32-51-17-000-801 (A01) AND 33-51-17-400-801. OPS CHECKED GOOD.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 17,022 hrs · 12,296 cycles

FS 280 BEAM HAS CORROSION AT SCREW HOLES. REPAIRED IAW EC/TC REO 670-53-11-047.

Part: STRINGER — CRACKED (BS 280 S3L) · airframe 17,022 hrs · 12,296 cycles

STRINGER 3 LEFT AT FS 280 ATTACHMENT POINT IS CRACKED. CUTOUT DAMAGED AREA OF STR 3L, FABRICATED REPAIR ITEMS 2 & 3 & TRIMMED TO FIT IAW STEP 2 & STEP 4 OF REO 670-53-21-493. NDT SHOWS NO INDICATIONS NOTED AT THIS TIME. INSTALLED REPAIR PARTS AND COMPLETED EC/TC REO 670-53-21-493, STEPS 5-9, COMPLIED WITH EC/TC REO 670-53-21-493. IAW REO 670-53-21-493 REV A DATED 2-17-2010.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 17,022 hrs · 12,296 cycles

FS 280 BEAM HAS CORROSION AT SCREW HOLES ALL ALONG BEAM. PICKED UP HOLES FOR DRIP TRAYS & DRILLED, INSTALLED CTR SPLICE REF SRM 51-40-11-001-001-A01 & REO 670-53-11-047 WA161715 1/5/11 5. INSTALLED FLOORBOARD NUT PLATES REF SRM 51-42-15-001-001-A01 MINOR REPAIR. INSTALL DRIP TRAYS & SEAL AREA REF SRM.

Part: SEAT TRACK — CORRODED (BS 677-830.4) · airframe 17,022 hrs · 12,296 cycles

9 RT FLOOR SEAT TRACK SEGMENT FROM FS 677 TO FS 830.40 HAS CORROSION. R & R WITH SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785-795) · airframe 17,022 hrs · 12,296 cycles

CORROSION ON LT SIDE SEAT RAIL AT FS 785.15 TO FS 795.0. REMOVED AND INSTALLED NEW SERVICABLE LT SIDE SEAT RAIL AT FS 785.15 TO FS 795.0 IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 17,022 hrs · 12,296 cycles

9 LT FLOOR SEAT TRACK SEGMENT FROM FS 677 TO FS 830 HAS CORROSION. R & R SEAT TRACK WITH NEW TRACK AT FS677 TO FS830 IAW AMM 53-00--49-000-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 17,022 hrs · 12,296 cycles

9 RT FLOOR SEAT TRACK SEGMENT FROM FS 581 TO FS 677 HAS CORROSION. R & R WITH SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 830.4-985) · airframe 17,022 hrs · 12,296 cycles

9 LT FLOOR SEAT TRACK SEGMENT FROM FS 830.40 TO FS 985 HAS CORROSION. REMOVED AND INSTALLED NEW SERVICABLE SEAT TRACK FROM F/S 830.40 TO F/S 985 IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 17,022 hrs · 12,296 cycles

9 LT FLOOR SEAT TRACK SEGMENT FROM FS 581 TO FS 677 HAS CORROSION. R & R SEAT TRACK WITH SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: BRACKET — CRACKED (FAIRING) · airframe 17,022 hrs · 12,296 cycles

LT AFT FUSELAGE FAIRING, 195DL INSIDE AFT BRACKET IS CRACKED IN 2 PLACES AND HAS SEVERAL LOOSE RIVETS. R & R "C" CHANNEL (AFT BRACKET) ON FAIRING 195DL IAW MODSUM IS67053820002. FOUND TO BE SATISFACTORY.

Part: SUPPORT ANGLE — CORRODED (E/E BAY) · airframe 17,022 hrs · 12,296 cycles

AVIONICS CRAWL WAY PANEL 131ALF, FWD SUPPORT ANGLE CORRODED. INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 453) · airframe 17,022 hrs · 12,296 cycles

LT CTR SEAT RAIL HAS CORROSION AT FS 453.00. R & R SEAT RAIL FS 374.0-485.0 IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: FRAME — CORRODED (BS 280) · airframe 17,022 hrs · 12,296 cycles

FS 280, CIRCUMFERENTIAL FRAME JOINT CORRODED BETWEEN STR 25L AND 25R. PERFORMED UT THICKNESS INSP OF BLEND AREAS ON BUTT STRAP IAW MAC NDT INSP PROCEDURE UT-3 MINIMUM MATERIAL REMAINING IS .078". ACCOMPLISHED STEP 3 IAW REO 670-53-21-637. COMPLIED WITH STEPS 4 & 5 IAW REO 670-53-21-637.

Part: SEAT TRACK — CORRODED (BS 379-394) · airframe 17,022 hrs · 12,296 cycles

LT CTR FLOOR SEAT TRACK HAS CORRSION AT FWD END BETWEEN FS 379.00 AND 394.00. R & R SEAT TRACK FS 374.0-485.0 IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 17,022 hrs · 12,296 cycles

FS 280.00 BEAM HAS CORROSION AT SCREW HOLES ALL ALONG BEAM. BEAM REMOVED & INSTALLED IAW REO 670-53-11-047.

Part: SEAT TRACK — CORRODED (BS 409-437) · airframe 17,022 hrs · 12,296 cycles

RT CTR SEAT RAIL BETWEEN FS 409.00 AND 437.00 HAS CORROSION. R & R WITH SERVICABLE SEAT TRACK AT FS 350-485 ON RT SIDE IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 533-549) · airframe 17,022 hrs · 12,296 cycles

RT CTR SEAT RAIL BETWEEN FS 533.00 AND 549.00 HAS CORROSION. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-800-801.

Part: SKIN — CRACKED (FUSELAGE) · airframe 17,022 hrs · 12,296 cycles

VIEWED FROM RT TRU DOOR 212AR SKIN AT WL 79.50 CRACKED UNDER ADG STOWAGE PUMP OTBD FWD CORNER. COMPLIED WITH STEPS 2-4 OF REO 670-53-11-509. COMPLIED WITH STEP 5 OF REO 670-53-11-509 NO INDICATIONS NOTED AT THIS TIME. FABRICATED REPAIR PARTS IAW REO 670-53-11-509 DOUBLE AND CLEAT. DRILLED HOLES AND ADDED HOLES TO FIT SURROUND STRUCTURE IAW REO 670-53-11-509. ALL HOLES STEPPED UP TO FINAL SIZE AND COUNTERSUNK READY FOR INSTALLATION. INSTALLED REPAIR DOUBLER NR 7 & CLEAT NR 8 & PLACARD CLIP WIHT SEALANT & FILLET SEALED, TOUCHED UP PAINT ON RIVETS IAW REO 670-53-11-509. COMPLIED WITH REO 670-53-11-509 AND GENERIC REO 670-53-11-509.

Part: PLACARD — MISSING (ESCAPE HATCH) · airframe 17,022 hrs · 12,296 cycles

CREW ESCAPE HATCH IS MISSING ALL EXTERIOR PLACARDS. APPLIED SILKSCREEN PLACARDS TO CREW ESCAPE HATCH IAW AMM 20-60-11-400-801.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 16,809 hrs · 12,147 cycles

FLIGHT ATTENDANTS FLASHLIGHT INOP. REMOVED AND REPLACED FLIGHT ATTENDANTS BACK FLASHLIGHT. OPS CHECK GOOD. REF CRJ-700 AMM 25-60-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,612 hrs · 12,014 cycles

NR 3 CABIN CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED NR3 CABIN EMERGENCY FLOOD LIGHT IAW AMM 33-51-09, OPS CHECK GOOD. RELAMPED NR 3 CABIN EMERGENCY FLOOD LIGHT IAW AMM 33-51-09, OPS CHECK GOOD. (CLOSED)

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,554 hrs · 11,235 cycles

MAIN CABIN INTERIOR; EMERGENCY LIGHTS INOP AT CEILING PANEL NR1 AND LT AND RT FWD EXIT LOCATOR SIGNS. R & R FUSE AT NR 1 BATTERY PACK IAW ESPM 20-29-00. OPS CHECK GOOD OF EMERGENCY LIGHTS AT OVERHEAD NR 1 LT AND RT FWD EXIT LOCATOR SIGNS IAW MM. (CLOSED)

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,343 hrs · 11,083 cycles

LOWER EXIT SIGN AT PAX DOOR HAS BULB OUT. (RESOLVED ON W/O: 154971 TASKCARD: N/R-00004/ R & R LOWER EXIT SIGN BULBS AT PAX DOOR IAW AMM 33-51-11. OPS CHECK GOOD. R & R LOWER EXIT SIGN BULBS AT PAX DOOR IAW AMM 33-51-11. OPS CHECK GOOD. (CLOSED)

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,343 hrs · 11,083 cycles

FLOOR WAY EMERGENCY EXIT LIGHTING AT PAX DOOR & SERVICE DOOR HAVE BULBS INOP. (RESOLVED ON W/O: 154971 TASKCARD: N/R-00005 ) R & R BULBS AT FLOOR EMERGENCY EXIT AT PAX DOOR AND SERVICE DOOR IAW AMM 33-51-11. OPS CHECK GOOD. R & R BULBS AT FLOOR EMERGENCY EXIT AT PAX DOOR AND SERVICE DOOR IAW AMM 33-51-11. OPS CHECK GOOD. (CLOSED)

Part: EXTRACTOR — DIRTY (A/C PACKS) · airframe 15,141 hrs · 10,931 cycles

SMELLED STRONG SMOKE SMELL IN COCKPIT AND CABIN DURING FLIGHT. (EMERGENCY DECLARED -- FIRE TRUCKS ROLLED AS A PRECAUTION). REMOVED AND CLEANED LT & RT PACKS WATER EXTRACTORS IAW CMM 21-52-23. OP'S CHECKS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: DOOR — BINDING (PAX DOOR) · airframe 12,280 hrs · 8,739 cycles

PASSENGER DOOR IS DIFFICULT TO CLOSE FROM INSIDE, CANNOT BE CLOSED FROM OUTSIDE.

Part: DOOR — BINDING (PAX DOOR) · airframe 12,280 hrs · 8,739 cycles

PASSENGER DOOR WILL NOT CLOSE. FLT 5223 DEL 99 MINS.

Part: HANDLE — BINDING (PAX DOOR) · airframe 12,198 hrs · 8,681 cycles

FORWARD DOOR IS VERY DIFFICULT TO CLOSE. THE LOCKING HANDLE IS BINDING. FLT 5314.

Part: DOOR — BINDING (PAX DOOR) · airframe 12,112 hrs · 8,606 cycles

PAX DOOR HARD TO CLOSE.

Part: SILL — CRACKED (FUSELAGE) · airframe 12,031 hrs · 8,536 cycles

LT CABIN FLOOR SILL CRACKED BETWEEN FS 409.00 AND 421.00 FRAMES. DAMAGED LT CABIN FLOOR SILL AT FS 409-421 REPAIRED PER REO 670-53-21-431. RECEIVED REO 670-53-21-431. COMPLIED WITH STEPS 1 AND 2 OF REO. PERFORMED EDDY CURRENT INSPECTION IAW REO 670-53-21-431 PER NDTM 51-20-006 NO DEFECTS NOTED. FABRICATED REPAIR PARTS AND APPLIED FINISH PER REO 670-55-21-431. INSTALLED ALL REPAIR PARTS PER REO 670-53-21-431.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 12,031 hrs · 8,536 cycles

RT 280 FLOORBEAM HAS CORROSION. REMOVED AND REPLACED RT FS 280 FLOORBEAM WORK DONE IAW SRM 51-42-06, IS670-53-11-00026, SRM 51-40-11, NDTM 51-20-006, SRM 51-42-21.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 12,031 hrs · 8,536 cycles

LT 280 FLOORBEAM HAS CORROSION. REMOVED AND REPLACE LEFT FS 280 FLOORBEAM IAW SRM 51-42-06 & IS670-53110026, SRM 51-40-11, SRM 51-42-21, 51-42-00.

Part: HANDLE — CRACKED (E/E BAY DOOR) · airframe 12,031 hrs · 8,536 cycles

AVIONICS DOOR HANDLE CRACKED. NDT FOR CONFIRMATION.

Part: WEB — CORRODED (FUSELAGE) · airframe 12,031 hrs · 8,536 cycles

RIGHT WEB CORROSION AT FS 280. REMOVED AND REPLACED RT FS 280 WEB WORK DONE IAW SRM 51-42-06, REO 670-53-11-381, SRM 51-42-21, AND SRM 51-42-13.

Part: SILL — CORRODED (FUSELAGE) · airframe 12,031 hrs · 8,536 cycles

RIGHT FLOOR SILL CORROSION AT FS 280. REPAIRED RIGHT FLOOR SILL CORROSION REF EO 700-53-0061.

Part: WEB — CORRODED (FUSELAGE) · airframe 12,031 hrs · 8,536 cycles

LEFT WEB CORROSION AT FS 280. REMOVED AND REPLACED LEFT 280 WEB WORK DONE IAW SRM 51-42-06 & REO 670-53-11-052 REF M-234.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 12,031 hrs · 8,536 cycles

FWD FLOOR SUPPORT ANGLE CORROSION AT FS 280. REMOVED AND REPLACED FWD FLOOR SUPPORT ANGLE AT FS 280. WORK DONE IAW SRM 51-42-06 & SB 670BA-53-026.

Part: INTERCOSTAL — CRACKED (ASD) · airframe 12,031 hrs · 8,536 cycles

ASD -318 INTERCOSTAL CRACKED, AFT LOWER CORNER IS CRACKED.

Part: HANDLE — CRACKED (ASD) · airframe 12,031 hrs · 8,536 cycles

ASD OUTER HANDLE CRACKED. THIS SDR WILL REMAIN OPEN PENDING MX DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. INSTALL SB HANDLE. REMOVED ASD OUTER HANDLE & REINSTALLED NEW HANDLE WORK DONE IAW S.B. 670BA-52-030.

Part: FRAME — CORRODED (FUSELAGE) · airframe 12,031 hrs · 8,536 cycles

CORROSION ON FWD AND AFT LOWER FRAMES IN CARGO FIREX BOTTLES COMPT RT AFT FUSELAGE FS879.00 TO FS909.00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,031 hrs · 8,536 cycles

FLOOR SEAT TRACKS AT LBL9 HAVE MINOR CORROSION FROM FS349 TO 977. BLENDED ON 2 SEAT TRACKS ON LBL 9, FS 349-FS 581 BOTH WERE BLENDED OUT OF LIMITS. REMOVED 2 SEAT TRACKS ON LBL 9, FS 349-FS 581. ON REMOVAL, NOTICED THAT THERE WAS FURTHER MORE EXTENSIVE CORROSION ON INBOARD SIDE OF TRACK. RECOMEND THAT ALL SEAT TRACKS ON LBL9 BE PULLED UP TO CHECK FOR CORROSION ON INBOARD SIDE. ALL WORK DONE IAW CRJ 700 SRM 51-41-02, CRJ SRM 51-21-06 SAND CRJ 700 SRM 51-21-09. REMOVED AND REPLACED FLOOR SEAT TRACKS AT LBL9 HAVE MINOR CORROSION FROM FS349 TO 977 IAW CRJ700 AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,031 hrs · 8,536 cycles

FLOOR SEAT TRACKS AT RBL9 HAVE MINOR CORROSION FROM FS349 TO 977.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,031 hrs · 8,536 cycles

LT SIDEWALL SEATTRACK HAS MINOR CORROSION FROM FS465 TO 510(MARKED).

Part: PANEL — CRACKED (SPOILER) · airframe 12,031 hrs · 8,536 cycles

RT MULTI-FUNCTION SPOILER CLOSEOUT PANEL CRACKED AT INBD AFT CORNER. R & R RT MFS CLOSE OUT PANEL IAW SRM 51-42-06, 51-42-13, 51-42-21. REMOVED MFS CLOSEOUT PANEL PER SRM 51-42-00. REMOVE RT O/B FLAP VANE PER CMM 57-53-02. FITTED & DRILLED PER SB670BA-57-010 AND SRM 51-40-11. COUNTER SUNK & FINAL SIZED MOUNTING HOLES & DRILLED P-SEAL FASTENER HOLES PER SB670BA-57-010. OK TO INSTALL. INSTALLED RT MFS CLOSEOUT IAW SRM 51-42-21 AND 51-42-06 REFERENCE FASTENERS SB670BA-57-010. RESTORED A023 FINISH ON RT MFS CLOSE OUT PANEL IAW SRM 51-21-06 JOB COMPLETE. INSTALLATION OF RT FLAP VANE PERFORMER IN COMPLIANCE WITH EO 700-57-0062.

Part: PANEL — CRACKED (SPOILER) · airframe 12,031 hrs · 8,536 cycles

LT WING MULTI-FUNCTION SPOILER CLOSEOUT PANEL CRACKED AT INBD AFT CORNER. R & R RT MFS CLOSE OUT PANEL IAW SRM 51-42-06, 51-42-13, 51-42-21. REFER TO M-234 FORM FOR WORK ACCOMPLISHED. REMOVED MFS CLOSEOUT PANEL PER SRM 51-42-00. REMOVED RT O/B FLAP VANE PER CMM 57-53-02. FITTED & DRILLED RT MULTI FUNCTION SPOILER CLOSEOUT PANEL PER SB670BA-57-010 & SRM 51-40-11. COUNTER SUNK & FINAL SIZED MULTI-FUNCTION SPOILER MOUNTING HOLES & DRILLED P-SEAL FASTENER HOLES PER SB670BA-57-010. OK TO INSTALL. INSTALLED IAW SRM 51-42-21 & 51-42-06 REFERENCE FASTENERS SB670BA-57-010. RESTORED A023 FINISH ON RT MFS CLOSE OUT PANEL IAW SRM 51-21-06. INSTALLATION OF RT FLAP VANE PERFORMER ICW EO 700-57-0062.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 11,587 hrs · 8,207 cycles

AIR RETURN DUE TO "RED" RT ENGINE OIL PRESSURE EICAS MSG IN FLIGHT. RT ENGINE OIL PRESSURE AT ZERO PSI. OIL QUANTITY STATUS MSG AT 15 PERCENT. FLT 5052 DEL 58 MINS. AIRCRAFT RETURNED TO ICT AFTER T/O. EMERGENCY DECLARED. FLT 5052 CX.

Part: DOOR — BINDING (MAIN PAX) · airframe 9,812 hrs · 6,959 cycles

FA SAID DOOR WAS A LITTLE DIFFICULT TO CLOSE IN THE LAST INCH OR SO OF TRAVEL, IT SEEMED TO BIND A LITTLE BUT OPERATED NORMALLY OTHERWISE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 9,178 hrs · 6,534 cycles

G4 GALLEY EMERGENCY LIGHT HAS SEVERAL INOP BULBS.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 8,702 hrs · 6,207 cycles

F/A REPORTS, DOOR MAIN CABIN NOT ALIGNED AND DIFFICULT TO CLOSE. LUBE UP PAX STOW HANDLE. OPS CHECK GOOD. NO DEFECTS NOTED IAW CRJ 200 700 52-12-00. ALL TOOLS AND EQUIP REMOVED.

Part: STEP — BROKEN (AIRSTAIR DOOR) · airframe 8,581 hrs · 6,118 cycles

ASD LOWER STEP BROKEN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,428 hrs · 6,014 cycles

RIGHT EMERGENCY EXIT LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 7,680 hrs · 5,509 cycles

AFT MEGA PHONE INOP.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 7,642 hrs · 5,477 cycles

INTERCOSTAL AFT OF EXTERNAL POWER RECEPTICAL BOX DAMAGED IN RADIUS.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,642 hrs · 5,477 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. [5-1-07] CUTOUT DAMAGED SECTION OF PAX DOOR AFT DRAG ANGLE AS REQUIRED. FABRICATED SPLICE ANGLE, AND SPLICE DOUBLERS. COMPLIED WITH LPI OF PAX DOOR AFT GRAG ANGLE CUTLINES IAW REO 670-52-11-072. NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 7,642 hrs · 5,477 cycles

CORROSION ON LEFT SIDE SEAT RAIL IMMEDIATELY AFT OF EMERGENCY EXIT FS 785.

Part: STEP — CRACKED (PAX DOOR) · airframe 7,642 hrs · 5,477 cycles

PAX DOOR, TOP STEP, FWD BASE RADIUS CRACKED, (MARKED).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 7,642 hrs · 5,477 cycles

FLOOR ANGLE AT PAX DOOR ENTRANCE IS CORRODED. REMOVED FLOOR ANGLE AT PAX DOOR ENTRANCE. REPAIRED IAW SRM.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 7,642 hrs · 5,477 cycles

FOUND CORROSION ON RT SIDE SEAT RAIL IMMEDIATELY AFT OF EMERGENCY EXIT, FS 785.

Part: STEP — CRACKED (PAX DOOR) · airframe 7,642 hrs · 5,477 cycles

PAX DOOR TOP STEP AFT BASE RADIUS CRACKED (MARKED).

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 7,642 hrs · 5,477 cycles

FS 280.00 CROSSBEAM CORRODED & CRACKED ON UPPER FLANGE. [SUP 05-03-07] REPAIRED IAW ALL SRM`S.

Part: WEB — CORRODED (FUSELAGE) · airframe 7,642 hrs · 5,477 cycles

LEFT LOWER FS 280.00 WEB HAS CORROSION. [5-1-07] BLENDED OUT MINOR SURFACE CORROSION ON LT LOWER FS 280 WEB IAW CRJ 700 SRM 53-11-10. APPROX .003 MATERIAL REMOVED IN WORST AREAS IAW CRJ 700 SRM 51-25-06. TOPCOATED REPAIRED AREA IAW CRJ SRM 51-25-16.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 7,642 hrs · 5,477 cycles

FS 280.00 FWD CENTER FLOOR SUPPORT ANGLE CORRODED. [5-1-07] REMOVED 280 FWD CENTER FLOOR SUPPORT ANGLE. LOCATED HOLES AND NUTPLATES ON NEW SERVICEABLE FWD CENTER FLOOR SUPPORT ANGLE IAW CRJ SRM 51-41-11. OK TO INSTALL FWD CENTER FLOOR SUPPORT ANGLE. INSTALLED SERVICEABLE FWD CENTER FLOOR SUPPORT ANGLE AT FS 280.00 CROSSBEAM IAW CRJ SRM 51-42-06 & CRJ SRM 51-42-06 & CRJ SRM 51-42-21.

Part: WEB — CORRODED (FUSELAGE) · airframe 7,642 hrs · 5,477 cycles

RIGHT LOWER FS 280.00 WEB HAS CORROSION. [SUP 05-03-07] REPAIRED IAW ALL SRM`S.

Part: ACCESS PANEL — UNSECURE (FUSELAGE) · airframe 2,871 hrs · 2,228 cycles

FLIGHT 5296 - DURING CLIMBOUT OF BUF AN ABNORMAL AIR NOISE EMINATING FROM THE NOSE AREA. AIRCRAFT RETURNED TO THE FIELD. CLOSED THE EXTERNAL POWER ACCESS PANEL.

Part: COMPUTER — FAULTY (AVIONIC BAY) · airframe 2,294 hrs · 1,774 cycles

FLIGHT 5230 DURING CRUISE FLIGHT (CVG/PHL) RECEIVED A FUEL CHANNEL NR 2 FAIL STATUS MESSAGE, AIRCRAFT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO CVG FOR REPLACEMENT OF THE FUEL SYSTEM COMPUTER (FSCU).

Part: LATCH — DIRTY (CARGO DOOR) · airframe 1,070 hrs · 831 cycles

FLIGHT 5540 CARGO DOOR CAUTION MESSAGE. LATCH BUTTON ON DOOR HANDLE STUCK. CLEANED PUSH BUTTON, OPERATIONAL CHECK SATISFACTORY.