N420AW

Part: ELEC CONNECTOR — LOOSE (LT RVDT) · airframe 415,172 hrs · 43,906 cycles

AFTER ADDING TAKEOFF THRUST AND RELEASING BRAKES AIRCRAFT PULLED VERY HARD TO THE LEFT, ABORTED TAKE OFF. TAXIED OFF RUNWAY NO ISSUES AT NORMAL TAXI SPEED. BRAKE TEMPS NORMAL NO ABNORMAL MESSAGES AND NWS OPERATED NORMALLY. ALL OTHER INDICATIONS NORMAL. AIRCRAFT REMOVED FROM SERVICE. T/S PER FIM 32-50-02-01 FOR LATERAL DEVIATION AND FOUND LOOSE CONNECTOR ON LH FEEDBACK RVDT. RIG CHECKED RVDT IAW 32-51-02 AND CHECK IS GOOD. TAXI CHECK IS GOOD, NO ABNORMALITIES

Part: CONTROL LEVER — FAULTED (ZONE 200) · airframe 45,258 hrs · 44,002 cycles

FLAPS FAIL CAUTION MSG AT 20* FLAPS ON APPROACH. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. ACARS: A/C FLT DEP DST TIME ALT N420AW 6068 LEX PHL 1642Z 1756 STATE MINS IAS OAT FLAPS FAIL HALF AIR 00115 174 16 19 YES NO ***** AIRCRAFT REMOVED FROM SERVICE ***** R&R FLAP CONTROL LEVER IAW AMM SUPP 09-038A. OPS CHECK GOOD. REMOVED PLACARD AND REMOVED FROM MEL. PN:7-45500-1 SN OFF:0434 SN ON:0497 RAH

Part: RUDDER CONTROL — FAULTED (ZONE 300) · airframe 41,923 hrs · 40,901 cycles

ABORTED TAKE OF DUE TO LACK OF RUDDER RESPONSE LESS THAN 60 KTS FO'S LEG. PRESSURIZED ALL 3 HYD SYSTEMS, VISUALLY VERIFIED FULL DEFLECTION OF RUDDER TRAVEL FROM BOTH CA AND FO RUDDER PEDALS. EICAS INDICATION AGREES. AIRCRAFT REMOVED FROM SERVICE. PERFORMED VIS INSP ON MLG TIRE IAW AMM 32-41-01 AND NLG TIRE IAW AMM 32-42-01, NO DEFECTS NOTED. PERFORMED OPS CHECK OF BRAKE SYS IAW AMM 32-43-00, OPS CHECK GOOD. PERFORMED OPS CHECK OF RUDDER CONTROL SYS IAW AMM 27-21-00. OPS CHECK GOOD. PERFORMED OPS CEHCK OF NWS STEERING

Part: BRACKET — DAMAGED (PROXIMITY SENSOR) · airframe 43,919 hrs · 42,457 cycles

GEAR DISAGRE ON WARNING NLG DOWN MLG UP C/W QRH MANUAL EXT GEAR DOWN ALL AND LOCKED NORMAL LANDING. 6 SEC AND MANUL RELEASE WAS USED. HYD WAS IN AUTO. EMERGENCY DECLARED, 180 KNTS SPEED. NO OVERWEIGHT LDG. AIRCRAFT REMOVED FROM SERVICE. R/R NOSE LANDING GEAR PROX SENSOR BRACKET IAW AMM 32-61 OPS CHECK GOOD. GOOD TO CONTINUE SERVICE.

Part: BPSU — UNKNOWN (TE FLAPS) · airframe 43,569 hrs · 42,056 cycles

IN CRUISE, RECEIVED FLAPS FAIL CAUTION. BTMS INDICATIONS DID NOT EXCEED 10. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-018I, BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. FLAPS FAILED AGAIN APPROX 5 MINUTES AFTER RESET. AIRCRAFT REMOVED FROM SERVICE. R&R RIGHT HAND BPSU IAW AMM 27-51-10, OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,284 hrs · 41,721 cycles

ON DEPARTURE RECIEVED STEERING INOP CAUTION FOLLOWED BY WOW INPUT CAUTION AND WOW OUT PUT FAIL STATUS MSGS. RAN QRH. CYCLED NWS, MSG PERSISTED. WHEN EXTENDING GEAR ALL MSGS CLEARED. AIRCRAFT REMOVED FROM SERVICE. C/W FAULT ISOLATION OF STERING INOP MSG REF CRJ-200 FIM 32-50-01 REV 62 ADJUSTED NLG W/OFF/W SENSORS IN REF CRJ-200 AMM 32-61-05-000-805 AND 32-61-05-400-805 REV 66, & C/W OPS TESTS REF CRJ-200 AMM 32-30-00-710-802, 32-61-00-710-801 AND 32-51-00-710-801 REV 66 ALL TESTS GOOD AND NO STEERING INOP MSG SHOWN.

Part: FORMER — CORRODED (PASSENGER DOOR) · corrosion level 2 · airframe 43,186 hrs · 41,625 cycles

CORROSION FOUND ON PAX DOOR FORMER AT FS320.00 FROM DD5-UPPER FORMER AT HINGE. ***** AC REMOVED FROM SERVICE ***** INSTALL FORMER AT FS 320.00 BETWEEN DD5 DATUM AND UPPER FORMER AT HINGE REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG 601R31702 REV: -N

Part: FRAME — DAMAGED (FS379) · airframe 43,186 hrs · 41,625 cycles

SKIN DIMPLED AROUND 4 RIVETS ON FRAME FS379.00 BETWEEN STGR23LL AND STGR22L ***** AC REMOVED FROM SERVICE ***** REPAIRED FRAME AT FS 379 BETWEEN STRG23L AND STRG22L REF REO 601R-53-21-3628 REV -- DATED 2023-04-21

Part: FLOOR SUPPORT — CORRODED (FS409+128) · corrosion level 2 · airframe 43,186 hrs · 41,625 cycles

L/H PRESSURE FLOOR SILL PANEL FROM FS409+128 TO FS559 HAS MULTIPLE AREAS OF CORROSION . ***** AC HAS BEEN REMOVED FROM SERVICE ***** REPAIRED L/H PRESSURE FLOOR SILL PANEL FROM FS409+128 TO FS 559 REF REO 601R-53-41-666 REV -- DATED 27-MAY-2008 AND REO 601R-53-41-3151 REV -- DATED 2023-04-15

Part: FRAME — CORRODED (FS319) · corrosion level 2 · airframe 43,186 hrs · 41,625 cycles

FRAME AT FS 319 HAS CORROSION REF CRJ-200 SRM 51-42-06 AND SRM 51-42-21 AND DWG 601R32003 REV P ***** AC REMOVED FROM SERVICE ***** REPLACE FRAME AT FS 319 REF

Part: INTERCOSTAL — CORRODED (FS333) · corrosion level 2 · airframe 43,186 hrs · 41,625 cycles

INTERCOSTAL AT STGR21L BETWEEN FS349-FS333 HAS CORROSION ***** AC REMOVED FROM SERVICE ***** INSTALLED NEW INTERCOSTAL FROM STGR 21 LH BETWEEN FS 333.00 AND FS 349.0 REF CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21 AND DWG 601R31527 REV AM

Part: PRESSURE DECK — CORRODED (FS409+128) · corrosion level 2 · airframe 43,186 hrs · 41,625 cycles

R/H PRESSURE FLOOR SILL PANEL FROM FS409+128 TO FS559 HAS MULTIPLE AREAS OF CORROSION ***** AC REMOVED FROM SERVICE ***** REPAIRE R/H PRESSURE FLOOR SILL REF REO 601R-53-41-3149 REV A DATED 2023-04-14

Part: FRAME — DAMAGED (COCKPIT) · airframe 43,186 hrs · 41,625 cycles

REMOVE EXISTING REPAIR TO COMPLY WITH PERMANENT REPAIR AT THE REQUEST OF THE CUSTOMER ***** AC REMOVED FROM SERVICE ***** REPAIRED FRAME SECTION AT FS276 REF REO 601R-53-11-3859 REV -- DATED 2023-04-19

Part: FRAME — CORRODED (FS364) · corrosion level 2 · airframe 43,186 hrs · 41,625 cycles

CORROSION ON FRAME FS364.00 AND STRG23L ***** AC REMOVED FROM SERVICE ***** REPLACED FRAME SECTION REF REO 601R-53-21-3626 REV -- DATED 2023-04-19

Part: FLAP — DAMAGED (LH IB FLAP) · airframe 43,186 hrs · 41,625 cycles

PERFORM PERMANENT REPAIR FOR LH INBOARD FLAP INNER DOUBLER. ********AIRCRAFT REMOVED FROM SERVICE******* REPAIRED L/H INBOARD FLAP UPPER SKIN REF REO 601R-57-52-2482 REV -- DATED 2023-04-12

Part: CLEAT — CORRODED (PASSENGER DOOR) · corrosion level 2 · airframe 43,186 hrs · 41,625 cycles

CORROSION FOUND ON PAX DOOR CLEAT AT FS338.00 AND UPPER FORMER AT HINGE *********AIRCRAFT REMOVED FROM SERVICE******* INSTALLED NEW PAX DOOR CLEAT AT FS338.00 REF DWG 601R31702 REV-N CRJ 200 SRM 51-42-10

Part: FRAME — CORRODED (FS 333) · corrosion level 2 · airframe 43,186 hrs · 41,625 cycles

FRAME AT FS 333 HAS CORROSION STGR23L-25R ********AIRCRAFT REMOVED FROM SERVICE******** REPLACED FRAME AT FS333 REF CRJ-200-SRM 51-42-06,CRJ-200-SRM 51-42-21, AND DRAWING 601R32004 REV M

Part: CLEAT — CORRODED (PASSENGER DOOR) · corrosion level 2 · airframe 43,186 hrs · 41,625 cycles

CORROSION FOUND ON PAX DOOR CLEAT AT FS313.56 DD4. *****AIRCRAFT REMOVED FROM SERVICE********* INSTALLED NEW CLEAT AT FS 313.56 DD4 REF CRJ-200-SRM 51-42-06 AND DRAWING 601R31702 REV N

Part: FORMER — CORRODED (PASSENGER DOOR) · corrosion level 2 · airframe 43,186 hrs · 41,625 cycles

PAX DOOR FWD FORMER HAS CORROSION BETWEEN DD6-DD5 *********AIRCRAFT REMOVED FROM SERVICE******* REPLACED NEW PAX DOOR FWD FORMER REF DRAWING 601R31702 REV N

Part: INTERCOSTAL — CORRODED (PASSENGER DOOR) · corrosion level 2 · airframe 43,186 hrs · 41,625 cycles

CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD4 BETWEEN FS 338.00 FS349.00 *********AIRCRAFT REMOVED FROM SERVICE********* INSTALLED A NEW PAX DOOR INTERCOSTAL FS338.00-FS349.00. REF DWG 601R31702 REV-N AND CRJ 200 SRM 51-42-06

Part: FLOOR SKIN — DENTED (FS499) · airframe 43,186 hrs · 41,625 cycles

PRESSURE FLOOR SKIN HAS 2EA DENTS BETWEEN LBL 9-BL0 FS499 *******AIRCRAFT REMOVED FROM SERVICE***** REPAIRED PRESSURE FLOOR SKIN REF REO 601R-53-41-3147 REV -- DATED 2023-04-07

Part: HINGE — UNKNOWN (PAX DOOR) · airframe 43,186 hrs · 41,625 cycles

"Ï¿½PASSENGER DOOR HINGE ON FUSELAGE LUGS FAILED THE CHECK WITH THE NO/GO GAUGE ***** AC REMOVED FROM SERVICE ***** REPLACED PAX DOOR HINGE ,BOMBARDIER DWG 601R31527 REV AM AND REO 601R-53-21-656 REV A DATED 2017/03/06"

Part: FORMER — CORRODED (PAX DOOR) · corrosion level 2 · airframe 43,186 hrs · 41,625 cycles

PAX DOOR AFT FORMER HAS CORROSION BETWEEN DD6-DD5 ***** AC REMOVED FROM SERVICE ***** REPLACED AFT PAX DOOR FORMER REF DWG 601R31702 REV N

Part: FRAME — CORRODED (FS310) · corrosion level 2 · airframe 43,186 hrs · 41,625 cycles

FRAME AT FS 310 HAS CORROSION STRG26L-26R. AC REMOVED FROM SERVICE. INSTALLED NEW LOWER FRAME SECTOR TO THE LOWER SKIN @ FS310 REF CRJ-200 SRM 51-42-06 AND DWG 601R32002 REV.AC.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 43,186 hrs · 41,625 cycles

FWD CARGO DOOR BOX SPRING FRAME SUPPORT STRUCTURE CRACKED. *******AIRCRAFT REMOVED FROM SERVICE****** REPLACED FWD CARGO DOOR BOX SPRING FRAME SUPPORT STRUCTURE BRACKET REF SRM 51-42-06

Part: INTERCOSTAL — CORRODED (PASSENGER DOOR) · corrosion level 2 · airframe 43,186 hrs · 41,625 cycles

CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD6 BETWEEN FS 320-FS 338.00 *******AIRCRAFT REMOVED FROM SERVICE******** REPLACE INTERCOSTAL ON PAX DOOR DD6 REF CRJ-200-SRM 51-42-06,CRJ-200-SRM 51-42-21

Part: INTERCOSTAL — CORRODED (FS338 TO FS349) · corrosion level 2 · airframe 43,186 hrs · 41,625 cycles

CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD5 BETWEEN FS 338.00 TO FS 349.00 ******AIRCRAFT REMOVED FROM SERVICE******** REPLACED PAX DOOR INTERCOSTAL AT DD5 BETWEEN FS 338.00 TO FS 349.00 REF DWG 601R31702 REV-N

Part: UNKNOWN — CRACKED (200 CABIN) · airframe 43,186 hrs · 41,625 cycles

FS 484.00 BETWEEN LBL 27-36 FLIGHT CONTROL CABLE ROLLER GUIDE ASSY ,INBOARD ATTACH ANGLE ********AIRCRAFT REMOVED FROM SERVICE******* REPLACE CLIP 484 CLIP REF DRAWING 601R31171 REV E , AND CRJ-200 SRM 51-42-21

Part: UNKNOWN — CRACKED (200 CABIN) · airframe 43,186 hrs · 41,625 cycles

FS484.00 BETWEEN RBL 27-36, FLIGHT CONTROL CABLE ROLLER GUIDE ASSY, INBOARD ATTACH ANGLE CRACKED(MARKED) *****AIRCRAFT REMOVED FROM SERVICE*********** REPLACED CLIP REF SRM51-42-21 AND DWRG 601R31171 REV - E

Part: FMS — ABNORMAL (FMS)

COLLINS 4200 FMS. KEYS ON KEYBOARD ARE WORE OUT AND WHEN YOU TYPE THE KEYS REPEATS THE SAME NUMBER OR LETTER, 2 TO 3 TIMES. COMPANY REFUSES TO FIX THEM. IMO THIS IS A SAFETY OF FLIGHT ISSUE. ALL AIRCRAFT IN FLEET HAVE THIS PROBLEM. 405-471AW

Part: NONE — NONE · airframe 41,410 hrs · 39,900 cycles

ON TAKE-OFF REC'D RT ENG OIL WARNING MESSAGE. MESSAGE WAS INTERMITTENT. OIL PSI FLUCTUATED BETWEEN 25 AND 35 PSI. OIL TEMP WAS NORMAL. MESSAGE WAS LESS INTERMITTENT WITH REDUCED POWER. EVENT DESCRIPTION: EN ROUTE, THE #2 ENGINE OIL PRESSURE BEGAN TO FLUCTUATE. AFTER REVIEWING THE QRH AND COORDINATING WITH DISPATCH, THE FLIGHT CREW HAS DECLARED AN EMERGENCY ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED THE OIL PRESURE TRANDSUCER O-RING AND INSTALLED MISSING TEFLON BACKER RINGS ON RIGHT ENGINE. IAW AMM 79-31-05, OPS CHECK AND LEAK CHECKS

Part: NONE — NONE · airframe 41,392 hrs · 39,880 cycles

3885 RT WING A-ICE CAUTION MSG USING STANDBY. EN ROUTE, THE FLIGHT EXPERIENCED A RIGHT WING ANTI ICE CAUTION MESSAGE. IN THE INTEREST OF SAFETY, TO AVOID ICING CONDITIONS, THE CREW AND DISPATCHER HAVE AGREED TO DIVERT TO DAY. NO EMERGENCY DECLARED AND THE FLIGHT LANDED IN DAY. WRITE UP WAS "RT WING A-ICE CAUTION MSG USING STANDBY." ***AIRCRAFT REMOVED FROM SERVICE*** R&R ANTI ICE PANEL IAW AMM 30-12-21 OPS CHECK GOOD IN BOTH STBY AND NORMAL MODE. REMOVED PLACARD REMOVED FROM MEL

Part: SEAT TRACK — CORRODED (BS 449-499) · corrosion level 2 · airframe 40,799 hrs · 39,258 cycles

LH SIDE RAIL BETWEEN FS 449 TO 499 IS OUT OF LIMITS DUE TO HEAVY CORROSION. REMOVED AND REPLACED LH SIDE RAIL

Part: WINDSHIELD — CRACKED (LEFT) · airframe 40,463 hrs · 38,909 cycles

LEFT WINDSHIELD CRACKED IN FLIGHT DURING CLIMB OUT. AIR RETURN TO IAD. AIRCRAFT REMOVED FROM SERVICE. R & R CA WINDSHIELD PER AMM 56-11-01 SEE LP 307033/1 FOR SEALANT CURE CHECK AND 307033/2 FOR OPS CHECK/LEAK CHECK OF WINDSHIELD HEAT P/N OFF:NP139321-13,S/N OFF:10293H5106 ; P/N ON:NP139321-17,S/N ON:20017H0070. MPM

Part: WINDSHIELD — CRACKED (RH COCKPIT) · airframe 40,441 hrs · 38,881 cycles

EVENT DESCRIPTION: CREW REPORTED CRACKED WINDSHIELD EN ROUTE TO MKE. FLIGHT DIVERTED TO DAY AND DECLARED AN EMERGENCY. FLIGHT IS A REPOSITION WITH ZW MECHANICS ON BOARD, REF 307026/4: AT FLT 300 OBSERVED ARCING ON F/O' WINDSCREEN TURNED F/O WINDSHIELD HEAT OFF 5 SECONDS LATER F/O WINDSCREEN SHATTERED. SWITCH WAS IN LOW POSITION, REF 307027/1: WHILE PERFORMING QRH FOR A CRACKED WINDSHIELD MAN ALT SWITCH STUCK IN UP POSITION AND WOULD NOT GO TO NEUTRAL POSITION. RECEIVED CABIN ALT WARNING AND THE PASSENGER MASKS AUTO DEPLOYED. AFTER LANDING FOUND F/A'S MASK (CONT IN BLOCK 2) ROWS 5 CD AND 6AB HANGING LOWER THAN OTHERS. AIRCRAFT REMOVED FROM SERVICE. R & R FO WINDSHIELD, IAW AMM 56-11-01. OPERATIONS AND LEAK CHECK GOOD.

Part: WIRE HARNESS — DAMAGED (NLG STEERING) · airframe 40,439 hrs · 38,879 cycles

STEERING INOPERABLE MESSAGE AT CRUISE FL 290. CW QRH MESSAGE PERSISTED, AFTER SELECTING GEAR DOWN CYCLED STEERING OFF ON MESSAGE RETURNED. EMERGENCY DECLARED. CYCLED SW AGAIN AT 500 FT MESSAGE CLEARED. STEERING APPEARED NORM AFTER LANDING. TAXI TO GATE UNDER OWN POWER. AIRCRAFT REMOVED FROM SERVICE. R & R NOSE STEERING HARNESS, REF AMM 32-61-25. OPERATIONS CHECK GOOD NO MESSAGE DURING TAXI.

Part: WARNING MESSAGE — FALSE ACTIVATION (AOA HEAT) · airframe 40,392 hrs · 38,829 cycles

RECEIVED R AOA HEAT CAUTION MESSAGE IN-FLIGHT. C/W QRH MESSAGE PERSISTED. AIRCRAFT REMOVED FROM SERVICE. C/W FIM RESET MESSAGE CLEARED.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 40,020 hrs · 37,437 cycles

FLAP FAIL CAUTION MESSAGE DURING CRUISE AT 280 KNOTS, C/W QRH. DECLARED EMERGENCY AND SELECTED LONGEST RUNWAY. AIRCRAFT REMOVED FROM SERVICE. RESET AND PLACED ON MEL FOR 10 CYCLES.

Part: BPSU — MALFUNCTIONED (RT WING TE FLAP) · airframe 40,021 hrs · 38,438 cycles

FLAP WERE MEL'D AT ORD AND RESET. EN ROUTE TO CID THEY FAILED AGAIN. FLIGHT WILL CONTINUE TO CID. THE CAPTAIN INDICATED THAT DURING DESCENT TO KCID THE FLIGHT CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW COMPLETED THE APPROPRIATE CHECKLISTS, ADVISED THE F/A AND PASSENGERS AND DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. T/S IAW FIM 27-50-00 FIG 107 BASED ON FECU CODES INCLUDED ON RECORD OF FECU FAULT LOG, CONTENTS INCLUDED IN WORK PACK. CW HARNESS INTEGRITY TEST FROM RT BPSU TO CONNECTOR 2P5CE NO FAULT FOUND REMOVED & REPLACED RT BPSU, IAW AMM 27-51-10. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 38,693 hrs · 37,101 cycles

UPON GEAR EXTENSION RECIVED GEAR DISAGREE NOSE SHOWED UNSAFE PERFORMED EMERGENCY GEAR EXTENSION PER QRH. MESSAGE OCCURED 6 SECONDS AFTER SELECTION, NO OTHER ASSOSIATED EICAS MESSAGES.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,432 hrs · 36,852 cycles

AIRCRAFT SKIN HAS TWO PROTRUDING DENTS BETWEEN FS 621-640 AND IN BETWEEN STRINGERS 25L AND 26L. REPAIRED SKIN BETWEEN FS 621-640 BETWEEN STRINGER 25L AND 26L IAW EA# AWAC-CRJ253-01271.

Part: BRACKET — CRACKED (NOT REPORTED) · airframe 38,432 hrs · 36,852 cycles

BRACKET BETWEEN TH INBD LE AND CENTER LE CRACKED. REPLACED

Part: SKIN — CRACKED (NACELLE) · airframe 38,432 hrs · 36,852 cycles

CORE COWL 435AT UPPER SKIN AFT I/B CORNER CRACKED. REPAIRED CORE COWL IAW CMM71-12-01.

Part: CLEAT — CORRODED (BS 310-349) · corrosion level 2 · airframe 38,432 hrs · 36,852 cycles

PAX DOOR AFT LOWER CLEAT CORRODED. REPLACED CLEAT IAW CRJ 200 SRM 51-42-06, 51-42-10, 51-42-12.

Part: CLEAT — CORRODED (BS 310-349) · corrosion level 2 · airframe 38,432 hrs · 36,852 cycles

PAX DOOR LOWER SILL FWD CLEAT CORRODED. REPLACED CLEAT IAW CRJ200 SRM 51-42-06, 51-42-10, 51-42-12.

Part: BEAM — GOUGED (BS 565-621) · airframe 38,432 hrs · 36,852 cycles

CARGO DOOR BEAM GROOVED AT AFT END OF BEAM DUE TO CARGO DOOR SPRING CABLE. REPLACED CARGO DOOR BEAM MEMBER IAW CRJ200 SRM 51-42-06, 51-42-21.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 38,432 hrs · 36,852 cycles

RH INBD FLAP VANE LE CENTER SKIN IS CHAFFED. REPLACED

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 38,432 hrs · 36,852 cycles

LEFT INBD FLAP VANE MIDDLE LE CHAFED. REPLACED.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 38,432 hrs · 36,852 cycles

CENTER WINDSHIELD POST LOWER FITTING CRACKED LH SIDE IN RADIUS. REPLACED.

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 38,432 hrs · 36,852 cycles

FS 559+78 TO 559+95 RBL 27 CARGO TRACK CORRODED. REPLACED

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 38,432 hrs · 36,852 cycles

RH INBD FLAP VANE LE OUTBD SKIN IS CHAFFED. REPLACED

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 38,432 hrs · 36,852 cycles

FS 559+86 TO 559+95 LBL 9 CARGO TRACK CORRODED. REPLACED

Part: GUIDE — CHAFED (LT WING TE FLAP) · airframe 38,432 hrs · 36,852 cycles

L/H O/B FLAP, CENTER HINGE ARM I/B FAIRING GUIDE IS CHAFED. REPLACED FAIRING GUIDE IAW CRJ200 SRM 51-42-06.

Part: SKIN — CRACKED (BS 235) · airframe 38,432 hrs · 36,852 cycles

NOSE GEAR SPADE DOOR CUTOUT AFT R/H CORNER IS CRACKED. REPAIRED CUTOUT SKIN IAW REO 601R-53-11-048 REV-D.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 38,432 hrs · 36,852 cycles

RIGHT I/B FLAP VANE, L/E I/B SKIN IS CHAFED. REPLACE RIGHT I/B FLAP VANE I/B L/E SKIN IAW SRM 51-42-13.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 38,432 hrs · 36,852 cycles

LT WHEEL WELL VOLUMETRIC FUSE BRACKET IS CRACKED. REMOVED AND REPLACED CRACKED LT BRACKET IN WHEEL WELL IAW SRM TR 51-42 AND 51-42-06.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 38,432 hrs · 36,852 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED NEAR PULLEY BRACKET REPAIRED PAX DOOR AFT DRAG ANGLE IAW BOMBARDIER REO# 601R-52-11-513

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,432 hrs · 36,852 cycles

FS 559 LBL 28 TO LBL 42 PRESSURE FLOOR STRAP HAS CORROSION. REMOVED AND REPLACED FS 559 LBL 28 TO LBL 42 PRESSURE FLOOR STRAP IAW SRM 51-42-06.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 38,432 hrs · 36,852 cycles

RH WHEEL WELL VOLUMETRIC FUSE BRACKET CRACKED REMOVED AND REPLACED RH WHEEL WELL FUSE BRACKET IAW SRM 51-40-11 (TR51-42), 51-42-06

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,432 hrs · 36,852 cycles

SERVICE DOOR SURROUND STRUCTURE FS 319 RBL 43 WL 71 T-BRACKET IS EXFOLIATED. REPLACED.

Part: LANDING — CRACKED (FUSELAGE) · airframe 38,432 hrs · 36,852 cycles

TRU PANEL LAND AT LATCH CRACKED. REPAIRED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 36,133 hrs · 34,524 cycles

ON CLIMBOUT RECEIVED PAX DOOR OUTER HANDLE CAUTION WHICH CONTINUOUSLY REPEATED IN FLIGHT. ON LANDING ROLLOUT RECEIVED PAX DOOR WARNING MESSAGE. PERFORMED OPS TEST OF PAX DOOR WARNING SYSTEM IAW AMM 52-70-04, OPS CHECK GOOD. R&R PS1MB IAW AMM 52-70-04-04. OPS CK GOOD.

Part: PSEU — MALFUNCTIONED (ANTI-SKID SYSTEM) · airframe 35,912 hrs · 34,282 cycles

PROXIMITY SYSTEM FAULT CAUTION MESSAGE DURING FLIGHT, COMPLIED WITH QRH, INBOARD & OUTBOARD ANTI-SKID MESSAGES STILL PRESENT. INTERROGATED PSEU FOUND CODE NO COMM. R & R THE PSEU IAW AMM 32-61-01 OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,548 hrs · 33,906 cycles

DURING RON MAINTENANCE, THE AFT OVERWING EMERGENCY EXIT WERE FOUND TO BE INOPERATIVE BOTH RIGHT AND LEFT SIDE. REMOVED AND REPLACED NR 4 BATTERY PACK IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 35,435 hrs · 33,796 cycles

BS 333 FRAME HAS CORROSION OTBD OF STRINGER 23R.

Part: FLOOR SUPPORT — CORRODED (BS 562-621) · corrosion level 2 · airframe 35,435 hrs · 33,796 cycles

LBL 9 FLOOR SUPPORT HAS CORROSION AROUND NUTPLATE LOCATIONS BETWEEN BS 605 AND BS 621.

Part: FLOOR SUPPORT — CORRODED (BS 562-621) · corrosion level 2 · airframe 35,435 hrs · 33,796 cycles

RBL 27 FLOOR SUPPORT HAS CORROSION AT NUTPLATE LOCATION BETWEEN BS 605 AND 621.

Part: WEB — DAMAGED (BS 574-589) · airframe 35,435 hrs · 33,796 cycles

LBL 9 OTBD FLOOR SUPPORT WEB BETWEEN BS 574 AND 589 HAS 1EA ELONGATED FASTENER HOLES.

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 35,435 hrs · 33,796 cycles

FRAME FS 605 CORRODED BETWEEN STRINGERS 25L AND 26R

Part: FLOORBEAM — CRACKED (BS 280) · airframe 35,435 hrs · 33,796 cycles

FS 280 FWD FLOORBEAM ANGLE CRACKED, LBL 9 AND RBL 9.

Part: ANGLE — CRACKED (BS 280) · airframe 35,435 hrs · 33,796 cycles

BS 280, RBL 9, INBD ANGLE CRACKED

Part: ANGLE — CRACKED (BS 280) · airframe 35,435 hrs · 33,796 cycles

BS 280, LBL 9 INBD ANGLE CRACKED.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 35,435 hrs · 33,796 cycles

OTBD AND INBD ATTACH ANGLES CRACKED AT BS 280, STRINGER 3L. REPLACED INBD AND OTBD ATTACH ANGLES IAW IAW SRM 51-42-06, AND 51-42-21.

Part: WEB — BUCKLED (BS 605) · airframe 35,435 hrs · 33,796 cycles

CARGO BAY FLOORBEAM WEB BUCKLED AT FS 605.00, LBL9. REPLACED THE WEB IAW SRM 51-42-021.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 35,435 hrs · 33,796 cycles

RIGHT INBD FLAP UPPER SKIN IS DENTED ON INBD END. REPAIRED THE RT INBD FLAP UPPER SKIN DENTED IAW SRM 57-52-00, REPAIR 3.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 35,435 hrs · 33,796 cycles

CABIN FLOORBEAM CORRODED AT FS 280.00 BETWEEN RBL 12 AND LBL 12. REPLACED THE FLOORBEAM IAW REO 601R-53-11-136 REV-A.

Part: SEAT TRACK — CORRODED (BS 364-397) · corrosion level 2 · airframe 35,435 hrs · 33,796 cycles

RIGHT SEAT TRACK NR 1CORRODED FROM BS 364 TO 397, RBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW CRJ200 AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 364-397) · corrosion level 2 · airframe 35,435 hrs · 33,796 cycles

LEFT SEAT TRACK CORRODED AT BS 364 TO 397, LBL 9. REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: APU — MALFUNCTIONED · airframe 35,072 hrs · 33,461 cycles

DURING FLIGHT, APU DID NOT START ON FIRST ATTEMPT, STARTED ON SECOND ATTEMPT. AFTER TRANSFER OF 10TH STAGE BLEED THERE WAS A STRONG FUEL AND FUMES ODOR. SHUTDOWN APU, ODOR CLEARED AFTER SEVERAL MINUTES.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 34,189 hrs · 32,652 cycles

RECEIVED FLAP FAIL CAUTION MSG IN CRUISE FLIGHT. EICAS SHOWS FLAPS FAILED AT 0 DEGREES. C/W CIRCUIT BREAKER RESET IAW SUPPORT 98-018G, MSG DID NOT CLEAR.

Part: HANDLE — DEFECTIVE (SERVICE DOOR) · airframe 33,645 hrs · 32,148 cycles

SERVICE DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. OUTER HANDLE WILL NOT DEPLOY, MEL'D ON 299684/4.

Part: MODULATING VALVE — FAULTY (ANTI-ICE SYSTEM) · airframe 32,778 hrs · 31,355 cycles

WING OVERHEAT WARNING ON TAKEOFF ROLL. ABORTED TAKEOFF AT 110 KTS. MAX BTMS READS 4545, ACARS REPORTS LT WING DUCT OVERHEAT. WING & COWL ANTI-ICE WERE ON & MSG CLEARED AFTER THROTTLES RETARDED. COMPLIED WITH CM ACTION PLACARDED & PLACED ON MEL. R & R LT 14TH STAGE MODULATING VLV IAW AMM 30-12-04. OPERATIONS CHECKED GOOD, REMOVED PLACARD & FROM MEL.

Part: INDICATOR — OUT OF ADJUST (PAX DOOR) · airframe 32,214 hrs · 30,809 cycles

AT FL190, RECEIVED PAX DOOR RED WARNING MSG, ACCOMPANIED BY INCREASED NOISE FROM MAIN PAX DOOR. COMPLIED WITH QRH, PRESS NORMAL, WITNESS MARKS ARE ALIGNED BUT LOCK INDICATOR SHOWS UNSAFE. TROUBLE SHOT DOOR IAW AMM 52-11-00. ADJUSTED LOCK INDICATOR, LUBED LATCHES, CHECKED FOR CODES, NOTE NOTED. PERFORMED BITE TEST, NO DEFECTS NOTED AT THIS TIME. INSPECTED DOOR TO FUSELAGE HARNESS, NO DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 31,156 hrs · 29,793 cycles

AT APROX 90 KTS ON TAKEOFF ROLL RECEIVED A SINGLE CHANNEL ANTI-SKID MSG, MSG WENT AWAY ONCE AIRBORNE.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,082 hrs · 29,719 cycles

RIGHT FLOOR SILL UPPER SURFACE IN CARGO AREA HAS CORROSION AT MULTIPLE LOCATIONS.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 31,082 hrs · 29,719 cycles

PAX DOOR EXTERNAL HANDLE IS CRACKED.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,082 hrs · 29,719 cycles

PAX DOOR LOWER SILL & FLOORBOARD ANGLE CORRODED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,082 hrs · 29,719 cycles

LBL 27 FLOORBEAM IN CARGO AREA HAS CORROSION AT TOP AT MULTIPLE LOCATIONS FROM FS 559+112 TO 621.00.

Part: STRUCTURE — GOUGED (WING) · airframe 31,082 hrs · 29,719 cycles

RIGHT BOOST PUMP CANISTER DRAIN VLV AFT ATTACHMENT HOLE HAS NDT DEFECT INDICATION OVER 90%.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 31,082 hrs · 29,719 cycles

GND RECEPTACLE MOUNT BRACKET CRACKED AT SCREW HOLES.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 31,082 hrs · 29,719 cycles

CREW ESCAPE HATCH LT & RT HINGE CUT OUTS FRAME ON CRACK.

Part: ANGLE — CRACKED (RT WING) · airframe 31,082 hrs · 29,719 cycles

ANGLE CRACKED ON RT WING LE ABOVE TRANSITION DUCT.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 31,082 hrs · 29,719 cycles

PAX DOOR INNER HANDLE CRACKED AT KNOB.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,082 hrs · 29,719 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED BY POWER ASSIST MOTOR.

Part: COVER PLATE — CRACKED (FUSELAGE) · airframe 31,082 hrs · 29,719 cycles

PAX DOOR AFT ANCHOR FITTING COVER PLATE IS CRACKED.

Part: FITTING — CHAFED (FUSELAGE) · airframe 32,300 hrs · 29,719 cycles

PAX DOOR AFT CAM FITTING CHAFED.

Part: PLATE — CRACKED (FUSELAGE) · airframe 31,082 hrs · 29,719 cycles

AVIONICS COMPONENTS SUPPORT PLATES BELOW THE LT & RT FLIGHT DECK ARE CRACKED.

Part: NUT PLATE — CRACKED (FUSELAGE) · airframe 31,082 hrs · 29,719 cycles

NUTPLATES FOR ADF ANTENNA CORRODED.

Part: SKIN — CRACKED (LT NACELLE) · airframe 31,083 hrs · 29,719 cycles

LT ENG UPPER CORE COWL INBD FWD EDGE GOUGED & CRACKED.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,082 hrs · 29,719 cycles

PAX DOOR FWD & AFT CLEATS ARE CORRODED.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,082 hrs · 29,719 cycles

THREE EACH CARGO TIE DOWNS AT LBL 27 FLOORBEAM FROM FS 559+96 TO 574.00 HAVE CORROSION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,082 hrs · 29,719 cycles

FS 409+128 & LBL 18.00 VERTICAL POST IS CRACKED AT LOWER RADIUS.

Part: POST — CRACKED (FUSELAGE) · airframe 31,082 hrs · 29,719 cycles

FS 409+128 & RBL 9 VERTICAL POST CRACKED AT OTBD LOWER RADIUS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,082 hrs · 29,719 cycles

FLOOR SUPPORT STRUCTURE CLIP AT FS 484.00, RBL 27 IS CRACKED AT UPPER RADIUS.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 31,082 hrs · 29,719 cycles

LT WINDSHIELD SIDE SUPPORT AFT BRACKET AT WINDOW SILL LEVEL IS CRACKED.

Part: SUPPORT BRACKET — CRACKED (RT MLG WW) · airframe 31,082 hrs · 29,719 cycles

HYD LINE SUPPORT BRACKET CRACKED IN RT WW JUST FWD OF BRAKE PRESS TRANSDUCER.

Part: MOUNT BRACKET — CRACKED (LT WING) · airframe 31,082 hrs · 29,719 cycles

LEFT WING FWD FACE OF FWD SPAR, INBD MOUNTING BRACKET FOR LE PANEL 530 JL, HAS A CRACK ON UPPER END.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FS 621.00 BULKHEAD INTERCOSTAL AT STRINGER 14R IS CRACKED.

Part: ELEVATOR SYSTEM — UNKNOWN · airframe 30,191 hrs · 28,652 cycles

IN FLIGHT ELEVATOR CONTROL INCREASE INPUTS NEEDED FOR ELEVATOR MOVEMENT, ELEVATOR FEELS HEAVY ON TAXI IN.

Part: SIGN — INTERMITTENT (CABIN) · airframe 30,494 hrs · 29,145 cycles

EMERGENCY EXIT SIGN AT SERVICE DOOR & AT CEILING AT ROW 8 INTERMITTENTLY FLASHING ON & OFF.

Part: A/C PACK — MALFUNCTIONED (AC BAY) · airframe 28,845 hrs · 27,586 cycles

CANX LAVATORY SMOKE DETECTOR GOING OFF AT GATE RT PACK SPIKED AT 120 DEGREES.

Part: HOUSING — CRACKED (CRGO DOOR HANDLE) · airframe 26,598 hrs · 25,394 cycles

CARGO BAY DOOR HANDLE HOUSING CRACKED. R & R CARGO DOOR HANDLE HOUSING.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 26,598 hrs · 25,394 cycles

FLOORBEAM BS 280 RBL 9 OTBD ANGLE IS CRACKED. R & R ANGLE IAW SRM 51-42-26.

Part: SILL — CRACKED (BS 589-605) · airframe 26,598 hrs · 25,394 cycles

CARGO DOOR THRESHOLD SILL HAS TWO CRACKS AT FS 589 - 605 FROM EDGE TO FASTENER HOLES. REPAIRED SILL IAW REO 601R-53-61-433, REV C.

Part: SEAT TRACK — CORRODED (BS 424) · airframe 26,598 hrs · 25,394 cycles

LEFT WALL SEAT TRACK CORRODED. BLENDED & RESTORED FINISH IAW REO 601R-53-00-533.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,598 hrs · 25,394 cycles

RT SIDE SEAT TRACK CORRODED. BLENDED & RESTORED FINISH IAW REO 601R-53-00-533.

Part: SEAT TRACK — CORRODED (BS 422-445) · airframe 26,598 hrs · 25,394 cycles

LT SIDE SEAT TRACK CORRODED. BLEND & RESTORE FINISH IAW REO 601R-53-00-533.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,598 hrs · 25,394 cycles

RT SIDE SEAT TRACK CORRODED BS 559. BLENDED & RESTORED FINISH IAW REO 601R-53-00-533.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,598 hrs · 25,394 cycles

LT SIDE SEAT TRACK CORRODED BS 559+13 TO +26. BLENDED & RESTORED FINISH IAW REO 601R-53-00-533.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,598 hrs · 25,394 cycles

LT SIDE SEAT RAIL CORRODED. BLENDED & RESTORED FINISH IAW REO 601R-53-00-533.

Part: SEAT TRACK — CORRODED (BS 369) · airframe 26,598 hrs · 25,394 cycles

RT SIDE SEAT TRACK CORRODED. BLENDED & RESTORED FINISH IAW REO 601R-53-00-533.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,598 hrs · 25,394 cycles

RT WALL SEAT TRACK CORRODED. BLENDED & RESTORED FINISH IAW REO 601R-53-00-533.

Part: FLOOR SUPPORT — CORRODED (BS 569-621) · airframe 26,598 hrs · 25,394 cycles

CORROSION AT FASTENER HOLE LOCATIONS ENTIRE LENGTH OF FLOOR SUPPORT CAP FS 569 - 621, LBL27. REMOVED, DUPLICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT CAP SRM 51-45-00, 51-42-15, 51-25-06, 51-25-11, 51-40-11, 51-41-00, 51-42-06, 51-42-22,51-42-34, AND REO 601R-53-61-3778, REV A.

Part: BRACKET — CRACKED · airframe 26,598 hrs · 25,394 cycles

LEFT WING CENTER TRANSITION DUCT BRACKET IS CRACKED. R & R CRACKED ANGLE AND INSTALLED NEW SERVICEABLE ANGLE, PN 601R120371-27.

Part: FAIRING — CRACKED (EXHAUST NOZZLE) · airframe 26,598 hrs · 25,394 cycles

RIGHT EXHAUST NOZZLE FAIRING IS CRACKED BY PANEL 446BR. REPAIRED EXHAUST NOZZLE FAIRING IAW REO 601R-78-11-4006, REV C.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 26,598 hrs · 25,394 cycles

SERVICE DOOR THRESHOLD FRAME IS CORRODED IN SEVERAL PLACES. REMOVED CORRODED THRESHOLD FRAME AND REPLACE WITH NEW THRESHOLD FRAME.

Part: ANGLE — CRACKED (BS 589) · airframe 26,598 hrs · 25,394 cycles

ANGLE IS CRACKED AT FS 589, REMOVED & REPLACED.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 26,598 hrs · 25,394 cycles

RIGHT MLG WHEEL WELL DRAG ANGLE COMMON TO INBD BATT RIB IS CRACKED. R & R IAW SRM.

Part: SKIN — DAMAGED (BS 605-622) · airframe 26,598 hrs · 25,394 cycles

FUSELAGE SKIN DAMAGED BETWEEN FS605 AND FS621 BETWEEN STRINGERS 21-22R. REPAIRED SKIN IAW REO 601R-53-61-4922.

Part: DRAG ANGLE — CRACKED (LT MLG WW) · airframe 26,598 hrs · 25,394 cycles

LT MLG WHEEL WELL DRAG ANGLE COMMON TO INBD BATT RIB IS CRACKED. R & R IAW SRM.

Part: STIFFENER — GOUGED (RT NACELLE) · airframe 26,598 hrs · 25,394 cycles

RIGHT LOWER CORE COWL HAS GOUGE ON THE SECOND STIFFENER FROM T/E. BLENDED OUT GOUGES IAW CMM 20-12-00.

Part: SKIN — DENTED (BS 409) · airframe 26,598 hrs · 25,394 cycles

SKIN AT BS 409 S24-25L DENTED. COMPLIED WITH PERMANENT REPAIR IAW REO 601R-53-31-795.

Part: ANGLE — CRACKED (BS 621) · airframe 26,598 hrs · 25,394 cycles

CRACKED OBLIQUE ANGLE LT UPPER AT FS 621. R & R LT UPPER OBLIQUE ANGLE IAW SRM 51-40-11 & SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,598 hrs · 25,394 cycles

CORROSION BEYOND LIMITS ON SEAT TRACK FROM FS 559-559+80, RBL 9. R & R IAW AMM 53-01-11.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 26,598 hrs · 25,394 cycles

LT INBD FLAP VANE L/E AT 60.005 CHAFED. FOUND TO BE OUT OF LIMITS. R & R L/E SKIN IAW SRM 51-40-11 & SRM 51-42-13.

Part: COVER — CRACKED (FIRE LOOP) · airframe 26,598 hrs · 25,394 cycles

RT JET PIPE FIRE LOOP COVER ASSY CRACKED, . REMOVED CRACKED FIRE LOOP COVER ASSY. INSTALLED SERVICEABLE FIRE LOOP COVER ASSY.

Part: SUPPORT BRACKET — CRACKED (BS 718) · airframe 26,598 hrs · 25,394 cycles

RT NR 2 HYD MANIFOLD SUPPORT BRACKET IS CRACKED. REMOVED DAMAGE AND INSTALLED FABRICATED ANGLE.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 26,598 hrs · 25,394 cycles

CARGO TRACK AT FS 559+95, RBL 9 IS CORRODED. REMOVED CORRODED CARGO TRACK, FABRICATED & INSTALLED NEW CARGO TRACK.

Part: CARGO TRACK — CORRODED (BS 574-615) · corrosion level 2 · airframe 26,598 hrs · 25,394 cycles

CARGO TRACK AT FS 574 - 615, LBL 9 ARE CORRODED. R & R WITH NEW SERVICEABLE.

Part: MOUNT — CRACKED (RT MLG WW) · airframe 26,598 hrs · 25,394 cycles

RT WHEEL WELL THE RT BRAKE TRANSDUCER MOUNT BRACKET IS CRACKED, R & R.

Part: CARGO TRACK — CORRODED · airframe 26,598 hrs · 25,394 cycles

CARGO TRACK AT BS 564, LBL 9 ARE CORRODED AT FASTENER LOCATORS. R & R WITH DUPLICATED TRACKS.

Part: PITOT SYSTEM — OBSTRUCTED (MAIN) · airframe 24,697 hrs · 23,545 cycles

ON TAKEOFF CAPT AIRSPEED IND 80 KNOTS, F/O IND 60 KNOTS ABORTED TAKEOFF. PURGED MAIN PITOT STATIC SYSTEM, RAN PITOT STATIC LEAK CHECK. OPS CHECK GOOD IAW 34-11-00.

Part: WARNING MESSAGE — ILLUMINATED (NR 1 IDG) · airframe 24,440 hrs · 23,275 cycles

ON TAKE OFF ROLL, RECEIVED IDG 1 CAUTION MESSAGE. SERVICED NR 1 IDG WITH 11 PUMPS IAW AMM 12-23-01. RAN NR 1 ENGINE. OPS CHECKED GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (AILERONS) · airframe 23,033 hrs · 21,844 cycles

AILERON TRIM MOVES LT AND RT UNCOMMANDED WITH A/P ON OR OFF 3-5 DEGREES EACH WAY. R & R AILERON CONTROL PANEL IAW AMM 27-12-10. OPS CK NORMAL.

Part: PRIORITY VALVE — FAILED (LANDING GEAR) · airframe 22,558 hrs · 21,357 cycles

GEAR DISAGREE WARNING AFTER TAKE OFF. NR 1 AND 2 HYD NORMAL, NR 3 HYD HAD 90 PERCENT AND 3200 PSI. LOUD THUMPING AND SHAKING. ALL RETURNED TO NORMAL ONCE GEAR DOWN IAW QRH. R & R LANDING GEAR PRIORITY VALVE.

Part: BULKHEAD — CRACKED (BS 202.75) · airframe 21,939 hrs · 20,696 cycles

FS 202.75 HAS CRACK IN BULKHEAD AT PARKING BRAKE CABLE. REPAIRED BULKHEAD AT FS 202.75 IAW REO 601R-53-11-563, REV A.

Part: SKIN — GOUGED (SERVICE DOOR) · airframe 21,939 hrs · 20,696 cycles

SERVICE DOOR OUTER HANDLE CUTOUT GOUGED. REPAIRED SERVICE DOOR OUTER HANDLE CUTOUT IAW REO 601R-52-41-184.

Part: SILL — CORRODED (BS 559) · airframe 21,939 hrs · 20,696 cycles

RT TOP FLOOR SILL AFT OF 9G HAS CORROSION. BLENDED CORRODED AREAS ON RT FLOOR SILL AFT OF 9G IAW REO 601R-53-51-158.

Part: RIB — CRACKED (RT WING) · airframe 21,939 hrs · 20,696 cycles

BATTERY RIB CRACKED IN RT MLG W/W. WORKED REPAIR IAW REO 601R-57-51-540.

Part: STIFFENER — CHAFED (BS 621) · airframe 21,939 hrs · 20,696 cycles

CENTER VERTICAL STIFFENER ON AFT SIDE OF APB GOUGED AND CHAFED BY ISOLATION GAUGE. BLENDED DAMAGED AREA, PERFORMED LPI, ALODINED, PRIMED, AND TOP COATED IAW REO 601R-53-61-4129.

Part: PANEL — CORRODED (LT WING) · corrosion level 1 · airframe 21,939 hrs · 20,696 cycles

LT WING PANEL C/O 550AB HAS INDICATION OF CORROSION INBD. WORKED IAW EO E06/012/457 & REO 601R-57-21-030.

Part: SKIN — GOUGED (RT NACELLE) · airframe 21,939 hrs · 20,696 cycles

RT LOWER CORE COWL INNER SKIN GOUGED. REPAIRED GOUGE IAW CMM 71-12-01 AND REO 601R-71-12-4073.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 21,939 hrs · 20,696 cycles

FS 484.0 CLIP CRACKED LBL 27.0. R & R CLIP IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (BS 625) · airframe 21,939 hrs · 20,696 cycles

RT OBLIQUE ANGLE IS CRACKED. REMOVED UNSERVICEABLE RT OBLIQUE ANGLE AND INSTALLED SERVICEABLE RT OBLIQUE ANGLE PN 601-35012-52 IAW SRM 51-42-06, 51-40-11, 51-42-21, 51-23-00, 51-25-16 AND REO 601R-53-61-985.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 21,939 hrs · 20,696 cycles

RT INBD (FLAP) VANE WHERE IT CONTACTS RUBBER STOPS. BLENDED CHAFED AREA IAW REO 601R-57-52-004 ALSO NDT.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 21,939 hrs · 20,696 cycles

LT INBD VANE (FLAP) WHERE IT CONTACTS RUBBER STOPS. BLENDED CHAFED AREA IAW REO 601R-57-52-004, ALSO NDT.

Part: SKIN — CHAFED (RT AILERON) · airframe 21,939 hrs · 20,696 cycles

FOUND 5 AREAS OF MINOR TO SEMI-MODERATE CHAFING ON RT AILERON UPPER SKIN L/E BLENDED AND SMOOTHED. ALL SERVICEABLE CHAFING AREAS IAW REO 57-60-013 RETURNED FINISH TO A023.

Part: SKIN — CHAFED (LT AILERON) · airframe 21,939 hrs · 20,696 cycles

LT AILERON UPPER AND LOWER L/E HAS CHAFE MARKS. BLENDED GOUGES, TREATED AND RESTORED FINISH IAW REO 601R-57-60-020, 601R-57-60-013.

Part: GENERATOR — WARNING LIGHT (NR 1) · airframe 21,734 hrs · 20,476 cycles

AFTER TAKEOFF, GEN 1 CAUTION MESSAGE CAME ON WITH RESET CAUTION MESSAGE WENT OUT REQUEST INSPECTION GEN 1 (GEN 2 ON MEL). R & R GEN NR 1 IAW AMM 24-11-01, OPS CHECKS GOOD, LEAK CK GOOD.

Part: SKIN — DAMAGED (BS 409) · airframe 17,432 hrs · 16,020 cycles

REPAIR FUSELAGE SKIN LIGHTNING DAMAGE SITE NR 8, 0.018 INCHES DEEP X 0.075 DIA LOCATED .021 INCHES BELOW STR 24L AND 4.179 INCHES OF FS 409+32. FUSLAGE SKIN LIGHTNING AT STR 24L TO FS 409.32. REPAIRED IAW REO 601R-53-31-675. (K)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,432 hrs · 16,020 cycles

AFT PRESSURE BULKHEAD WEB IS CRACKED. AFT PRESSURE BULKHEAD WEB REPAIRED IAW REO 601R-53-61-1541, REV B. (K)

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 17,432 hrs · 16,020 cycles

CORROSION ON FLOOR SUPPORT AT FS 574-621 LB 27 AROUND NUT PLATE HOLES. CORROSION ON FLOOR SUPPORT BTWN FS 574-621, LBL 27 REPAIRED IAW REO 601R53-61-3313. (K)

Part: ANGLE — CRACKED (BS 559) · airframe 17,432 hrs · 16,020 cycles

LOWER CAP ANGLE ON PRESSURE BULKHEAD FS 559, RT SIDE CRACKED. LOWER CAP ANGLE PRESSURE BULKHEAD FS 559, RT SIDE REPAIRED IAW REO 601R-53-41-1045, 601R-53-41-1045, REV, 601R-53-41-260, REV C. (K)

Part: STRUCTURE — CRACKED (BS 349) · airframe 17,432 hrs · 16,020 cycles

PASSENGER DOOR EDGE MEMBER CRACKED ON THE AFT SIDE PASSENGER DOOR EDGE MEMBER REPAIRED IAW SRM 51-42-13 AND 51-24-16. (K)

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 17,432 hrs · 16,020 cycles

CROSSBEAM WEB FS 280.00, BTW RBL 9 TO LBL 9WL 72.00 IS CORRODED. CROSSBEAM WEB FS 280.00 BTW RBL 9 TO LBL 9.00, WL 72.00. REPAIRED IAW REO 601R-53-11-926, REV B. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 17,432 hrs · 16,020 cycles

AFT PRESSURE BULKHEAD WEB AT FS 621, LBL 36.2 AND WL 111 CRACKED. AFT PRESSURE BULKHEAD BEB AT FS 621, LBL 36.2 AND WL 111 REPAIRED IAW REO 601R-53-61-3306. (K)

Part: STRINGER CLIP — CRACKED (BS 621 S14L) · airframe 17,432 hrs · 16,020 cycles

FS 621 AFT SIDE OF REAR PRESSURE BULKHEAD, LT STR 14 CLIP CRACKED. CLIP FABRICATED AND REPLACED AT FS 621 AFT SIDE OF REAR PRESSURE BULKHEAD, LT SIDE STR 14 IAW REO 601R-53-61-100, REV A. (K)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 17,432 hrs · 16,020 cycles

UNDER FLOOR FS 484, RBL 27 CLIP CRACKED. UNDER FLOOR FS 484, RBL 27 CLIP, REPLACED IAW SRM 51-21-42. (K)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 17,432 hrs · 16,020 cycles

UNDER FLOOR FS484, RBL 36 CLIP CRACKED. UNDER FLOOR FS 484, RBL 36 CLIP REPAIRED IAW REO 601R-53-41-059, REV A. (K)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 17,432 hrs · 16,021 cycles

UNDER FLOOR FS 484.00 LBL 36 CLIP CRACKED. UNDER FLOOR CLIP AT FS 484.00, LBL 36 REPAIRED IAW REO 601R-53-41-059, REV A. (K)

Part: DRAG ANGLE — CRACKED (BS 349) · airframe 17,432 hrs · 16,020 cycles

PASSENGER DOOR STAIR AFT DRAG ANGLE CRACKED. AFT DRAG ANGLE REPAIR CARRIED OUT IAW REO 601R-52-11-513. (K)

Part: PRESSURE BLKHD — CRACKED (BS 621) · airframe 16,846 hrs · 15,454 cycles

MWC 136498-2 - AFT PRESSURE BLKHD WEB AT FS 621 AT THE LINTEL ASSY INSTALLATION IS CRACKED. REPAIR ON AFT PRESSURE BULKHEAD WEB AT F/S 621.00 AT THE LINTEL ASSY INSTL. PERFORMED IAW REO 601R-53-61-1230, REV D. (K)

Part: FAN — INOPERATIVE (TRU) · airframe 14,027 hrs · 12,774 cycles

TRU 1 FAN INOPERATIVE. (M)

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 12,368 hrs · 11,402 cycles

FS 589 TO FS 621 WL 73.50 LBL 27 FLOOR SUPPORT CORRODED. FLOOR SUPPORT CORROSION REMOVED IAW SRM 51-21-06. (M)

Part: SKIN — CRACKED (PAX DOOR) · airframe 12,440 hrs · 11,219 cycles

SKIN UNDER PAX DOOR AFT DRAG ANGLE IS CRACKED AT 3RD FASTENER DOWN APPROX .5 INCH LONG. (K) MAINTENANCE REPAIRED AFT DRAG ANGLE IAW EO 601R-52-12354. (M)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,440 hrs · 11,219 cycles

AFT PAX DOOR DRAG ANGLE (PN 601R31772-5) IS CRACKED AT PREVIOUS REPAIR APPROX .5 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED DRAG ANGLE ON AFT PAX DOOR IAW REO 601R-52-11-513. (M)

Part: HANDLE — DIRTY (ESCAPE HATCH)

CREW ESCAPE HATCH EXTERNAL HANDLE WILL NOT DEPLOY. CLEANED AND LUBRICATED HANDLE IAW CRJ200 AMM 12-20-52-640-803. OPERATES NORMAL. (M)

Part: MOUNT — CRACKED (ASSIST MOTOR) · airframe 12,440 hrs · 11,219 cycles

PASSENGER DOOR ASSIST MOTOR MOUNT BRACKET (PN 601R317743-7) CRACKED APPROX .2 INCH LONG AT BOTTOM OF BRACKET. (K) MAINTENANCE REMOVED AND REPLACED BRACKET IAW CRJ200 SRM 51-42-06. (M)

Part: BRACKET — CRACKED (BS 530) · airframe 12,440 hrs · 11,219 cycles

HYDRAULIC LINE Z-BRACKET (PN 601R75262-153) CRACKED APPROX .1 INCH LONG IN RT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED DAMAGED BRACKET AND INSTALLED SERVICEABLE BRACKET IAW CRJ 200 SRM 51-42-06. (M)

Part: TRACK — CRACKED (CARGO DOOR) · airframe 12,440 hrs · 11,219 cycles

CARGO DOOR FWD ROLLER TRACK U-CHANNEL (PN 601R35050-25) CRACKED APPROX .2 INCH LONG AT BOTTOM OF TRACK. (K) MAINTENANCE REMOVED AND REPLACED U-CHANNEL IAW CRJ 200 SRM 51-42-06. (M)

Part: BRACKET — CRACKED (BS 530) · airframe 12,440 hrs · 11,219 cycles

HYDRAULIC PRESSURE TRANSDUCER BRACKET (PN 601R75262-159) CRACKED APPROX .2 INCH LONG IN LT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED AND REPLACED BRACKET IAW CRJ 200 SRM 51-42-13. (M)

Part: BRACKET — CRACKED (BS 530) · airframe 12,440 hrs · 11,219 cycles

HYDRAULIC PRESSURE TRANSDUCER BRACKET (PN 601R75262-157) CRACKED APPROX .2 INCH LONG IN RT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED DAMAGED BRACKET AND INSTALLED SERVICEABLE BRACKET IAW CRJ 200 SRM 51-42-06. (M)

Part: FLOORBEAM — CRACKED (BS 460) · airframe 12,440 hrs · 11,219 cycles

RT FS 460 FLOOR SUPPORT FITTING (PN 600-31068) AT OB SIDE OF RBL 9 CRACKED APPROX 1.5 INCHES LONG. (K) MAINTENANCE REMOVED AND REPLACED FITTING P/N 600-31068-19 IAW CRJ 200 SRM 51-42-13, 51-42-21, AND 51-23-00. (M)

Part: STRUCTURE — CRACKED (BS 574) · airframe 12,440 hrs

FLOOR EDGE MEMBER CRACKED AT FS 574.00. (K) MAINTENANCE REMOVED AND REPLACED DAMAGED PART IAW REO 601R-53-61-1574. (M)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 12,440 hrs · 11,219 cycles

RT FS 484 FLOOR SUPPORT INTERCOSTAL AT RBL 36 CRACKED APPROX .2 INCH LONG. MAINTENANCE REPAIRED IAW REO 601R-53-41-059 AND EO 601R-53-003A. (M)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 12,440 hrs · 11,219 cycles

LT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE AT LBL 27 CRACKED APPROX .2 INCH LONG. (K) MAINTENANCE REPAIRED FS 484, LBL 27 ANGLE IAW BOMBARDIER STANDARD REPAIR 601R-53-0029B. (M)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 12,440 hrs · 11,219 cycles

LT FS 484 FLOOR SUPPORT INTERCOSTAL AT LBL 36 CRACKED APPROX .2 INCH LONG. MAINTENANCE REMOVED FLANGE FABRICATED AND INSTALLED ANGLE IAW BSC SR 601R-53-0030A AND BOMBARDIER REO 601R-53-41-059 REV A. (M)

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 12,440 hrs · 11,219 cycles

FS 409.0+128 VERTICAL BEAM AT RBL 27 CRACKED APPROX.2 INCH LONG ON IB SIDE AT BOTTOM RIVET. (K) MAINTENANCE REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PARTS IAW BOMBARDIER REO 601R-53-41-056 REV E AND BSC EO 601R-53-12516. (M)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 12,440 hrs · 11,219 cycles

RT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE AT RBL 27 CRACKED APPROX .2 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M)

Part: STRUCTURE — CRACKED (BS 589) · airframe 12,440 hrs · 11,219 cycles

FLOOR EDGE MEMBER CRACKED AT FS 589.00. (K) MAINTENANCE REMOVED DAMAGED AND INSTALLED REPAIR IAW REO 601R-53-61-1574 REV A. (M)

Part: FLOORBEAM — CRACKED (FS 280)

FOUND FS 280 RBL 9 INBOARD CLIP, P/N 601R31113-58 IS CRACKED. MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-13 ABD BSC SR 601R-53-0057A. (M)

Part: STRUCTURE — CRACKED (BS 280)

FS 280 RBL 9 CLIP P/N 601R31113-58 (OUTBD) IS CRACKED .25 INCH. MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-13 AND BSC SR 601R-53-0057A. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 12,440 hrs · 11,219 cycles

RT FS 621-FS 625 INTERCOSTAL ANGLE (PN 601-35012-52) CRACKED APPROX .2 INCH LONG IN AFT EQUIPMENT BAY. (K) MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-06, 51-42-21 AND BOMBARDIER REO 601R-53-61-422 REV NC. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 12,440 hrs · 11,219 cycles

LT FS 621- 625 INTERCOSTAL ANGLE (PN 601-35012-51) CRACKED APPROX .3 INCH LONG IN AFT EQUIPMENT BAY. (K) MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-06, 51-42-21 AND BOMBARDIER REO 601R-53-61-422 REV C. (M)

Part: PANEL — DENTED (FS 169) · airframe 12,076 hrs · 10,861 cycles

RT NOSE SKIN PANEL PN 600-33010-27 IS DENTED 5 INCH LONG X 4 INCHES WIDE X 0.125 INCHES DEEP FROM FS 169.00 TO FS 193.00. S/D - MAINTENANCE REMOVED AND REPLACED SKIN PANEL P/N 600-33010-27, IAW CRJ 200 SRM 51-42-06 AND BSC EO 601R-53-11942. (K)

Part: SKIN — DENTED (FS 169-174) · airframe 12,076 hrs · 10,861 cycles

RT NOSE SKIN PANEL PN 600-33052-141 IS DENTED 3 INCHES LONG BY 2 INCHES WIDE BY 0.100 DEEP BETWEEN FS 169.00 AND FS 174.00. S/D - MAINTENANCE REMOVED AND REPLACED SKIN PANEL P/N 600-33052-141 BETWEEN FS 169.00 AND 174 IAW CRJ 200 SRM 51-42-06. (K)

Part: CONTROL PANEL — MALFUNCTIONED (STAB TRIM)

STAB TRIM AND MACH TRIM CAUTION INFLIGHT NEITHER CHANNEL 1 AND 2 WOULD RE-ENGAGE COMPLIED WITH QRH. REMOVED AND REPLACED STAB TRIM AND MACH TRIM CONTROL PANEL IAW CRJ AMM 27-41-25, OPS CHECK GOOD. (M)

Part: STATOR — DAMAGED (COMPRESSOR)

SHORTLY AFTER TAKEOFF, ENGINE NR 2 FAN VIBE WENT TO 3.3 TWO, YELLOW RANGE. COMPLIED WITH QRH, ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO ELM. CLEANED INLET AREA, REPLACED BLADES 1, 2, 4, 5, 6, 14, 16, 18, 19, 29 AND REPLACED SPACER ON STATOR ASCEND AT 10 O`CLOCK COMPRESSOR DAMAGE VTR .3 ON TAKEOFF AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — MALFUNCTIONED (RT BLEED SYSTEM)

ANTI-ICE DUCT WARNING CASS IN FLIGHT RIGHT WING INDICATED RED ON SYNOPTIC PAGE. COMPLIED QRH, WARNING EXTINGUISHED. REMOVED AND REPLACED RIGHT BLEED LEAK CONTROL UNIT IAW 36-31-10. PERFORMED OPS CHECK OF ANTI-ICE CONTROL AND INDICATION, OPS CHECK GOOD IAW 30-30-00. (M)

Part: WHEEL — INOPERATIVE (LT MLG) · airframe 8,713 hrs · 7,637 cycles

(TIRE BLOWN OUT ON LANDING) LT IB TIRE NEEDS TO BE REPLACED. THRUST REVERSER USED IAW FOM BRAKE TEMPS AND GATE WAS 4,1,4,4. REMOVED AND REPLACED MLG NR2 WHEEL ASSEMBLY IAW AMM. (K)

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 8,233 hrs · 7,149 cycles

STAB TRIM AND MACH TRIM MESSAGE APPEARED DURING CLIMB. COMPLIED WITH QRH, MESSAGE PERSISTED. REMOVED AND REPLACED HSTCU PN 7060-9, IAW AMM. OPS CHECK GOOD.

Part: SPOILER — OUT OF ADJUST (NR 4)

CONFIG SPOILER MESSAGE ON TAKEOFF. ABORTED TAKEOFF AT 120 KNOTS. BRAKE TEMPS 5, 6 AND 7. AIRCRAFT WEIGHT 50,900 LBS. ADJUSTED GAP ON LEFT INBOARD GROUND SPOILER NR 4 TO WITHIN LIMITS IAW AMM 27-60-00-220-801. (M)

Part: IDG — LACK OF LUBE (NR 2 GENERATOR) · airframe 7,604 hrs · 6,517 cycles

DURING TAKEOFF ROLL 70 KNOTS IDG NR FAIL, GEN NR 2 OFF APPEARED MODERATE BREAKING BTMS READOUT 4, 5,6,7 FOUND NR 2 IDG OIL LEVEL LOW SERVICED NR 2 IDG RAN ENGINE NO LEAKS NOTED OPS CHECK GOOD IAW MM. PERFORMED RTO INSPECTION. (K)

Part: FITTING — LOOSE · airframe 6,373 hrs · 5,444 cycles

HORIZONTAL STABILIZER FORWARD STEADY FITTING HAS 3 LOOSE MOUNT BOLTS ON LT SIDE OF FITTING. REMOVED BOLTS, VISUALLY INSPECTED HARDWARE AND HOLES, REINSTALLED BOLTS AND TORQUED IAW AMM. (K)

Part: DRAG ANGLE — CRACKED (PASSENGER DOOR) · airframe 6,373 hrs · 5,444 cycles

PASSENGER DOOR STAIR AFT DRAG ANGLE IS CRACKED, .5 INCH LONG IN RADIUS (ADJACENT TO MOUNT FOR PASSENGER DOR ASSIST CABLE PULLEY). REMOVED DAMAGED SECTION OF ANGLE, FABRICATED REPAIR ANGLE AND INSTALLED ANGLE IAW REO. (K)

Part: BEAM — DENTED (FS 625) · airframe 7,548 hrs · 6,459 cycles

NESTED ANGLE ON FWD WEB OF ENGINE BEAM HAS A DEEP GOUGE IN RADIUS APPROX .300 INCH LONG X .075 INCH WIDE AND .050 DEEP. REMOVED DAMAGED SECTION OF NESTING ANGLE. FABRICATED AND INSTALLED REPAIR PARTS IAW EO. (K)

Part: DOOR — DAMAGED (FUEL TANK)

RT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL 640BB HAS FRETTING DAMAGE. 2 INCH LONG X .125 INCH WIDE. REPAIRED BY BLENDING AND TREATING DAMAGED AREA IAW REO. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,548 hrs · 6,459 cycles

FS 280, RBL 9, IB ATTACH CLIP CRACKED. REPLACED ANGLE IAW SRM AND EO. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,548 hrs · 6,459 cycles

FS700, LBL 9 IB ATTACH CLIP CRACKED. REPLACED ANGLE IAW CRM AND EO. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,548 hrs · 6,459 cycles

FS 280, RBL 9, OB ATTACH CLIP CRACKED. (K) REPLACED ANGLE P/N 601R31113-58 IAW CRJ SRM 51-42-06 AND BRAS EO 601R-53-6888. (M)

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 7,548 hrs · 6,459 cycles

RT LOWER WING PLANK AT WS 45, FUEL ACCESS PANEL 640BB CUT OUT, RAS FRETTING DAMAGE 2 INCH LONG X .175 INCH WIDE. (K)

Part: ANGLE — CRACKED (FS 280) · airframe 7,548 hrs · 6,459 cycles

FS 280, LBL 9, IB ATTACH CLIP CRACKED. REPLACED ANGLE IAW SRM AND EO. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,548 hrs · 6,459 cycles

FS 280, LBL 9, OB ATTACH CLIP CRACKED. (K) REPLACED ANGLE P/N 601R31113-58 IAW CRJ CRM 51-42-06 AND BRAS EO 601R-53-6888. (M)

Part: SKIN — DENTED (FUSELAGE) · airframe 7,548 hrs · 6,459 cycles

PROTRUDING DENT AT FS 679, BETWEEN STR 23 AND STR 24, RT MEASURES .5 INCH X .020 INCH DEEP. PERFORMED REPAIR TO FUSELAGE SKIN FROM FS 672 TO 682 BETWEEN STRING STR 23 AND 24 BY CUTTING OUT DAMAGED AREA, PERFORMED NDT OF CUT LINE FAB AND DOUBLER AND INSTALLED IAW SRM. (K)

Part: ANGLE — CRACKED (RT FS 625) · airframe 7,548 hrs · 6,459 cycles

RT FS 625, OBLIQUE ANGLE IS CRACKED. REMOVED CRACKED OBLIQUE ANGLE AND REPLACED WITH NOW IAW SRM. (K)

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 7,548 hrs · 6,459 cycles

WO 84084, MWC 131, RT SIDE UNDERFLOOR SUPPORT STRUCTURE IS CRACKED 1.0 INCH AT FS 621, RBL 40, WL 73. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING AND INSTALLING REPAIR ANGLES IAW REO. (K)

Part: CONTROL PANEL — MALFUNCTIONED (RUDDER TRIM)

ABORTED TAKEOFF DUE TO CONFIG TRIM WARNING. ABORTED AT 60 KNOTS, RUDDER IN GREEN BAND, WILL TRAVEL TO LEFT BUT NOT TO THE RIGHT. REMOVED AND REPLACED RUDDER TRIM CONTROL PANEL, IAW AMM 27-10-01, OPS CHECK GOOD. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FLOOR ANGLE AT FS 621, LEFT SIDE, NEXT TO CARGO DOOR IS CRACKED. REPAIR IAW BOMBARDIER REO 601R-53-61-117. SEALED AND PAINTED IAW BOMBARDIER REO 601-53-61-117. PRESSURIZED AIRCRAFT IAW AMM 21-32-00-863-801. NO LEAKS NOTED. (M)

Part: APU — SEIZED (AFT)

AFTER ROTATION SMELLED SOMETHING HOT, APU EGT ABOVE RED LINE, APU SHUTDOWN AND TRANSFERRED BLEEDS TO ENGINE. SMOKEY ODOR DISAPPEARED. REMOVED APU SEIZED. REMOVED AND REPLACED APU. NO FURTHER INCIDENT. (M)