N421ZW

Part: FLOOR SUPPORT — CORRODED (BS 580-621) · corrosion level 2 · airframe 42,084 hrs · 39,887 cycles

CARGO FLOOR BEAM CLOSET TO CARGO DOOR FS 580 TO FS 621 LBL 27 HAS SIGNS OF CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR BEAM, IAW 601R35031.

Part: RELAY — FAILED (WOW) · airframe 42,038 hrs · 39,846 cycles

WOW INPUT AND STEERING INOP CAUTION MESSAGES AFTER GEAR RETRACTION. WOW OUTPUT FAILED STATUS MESSAGE ALSO. C/W QRH MESSAGES CLEARED AFTER GEAR EXTENTION AND CYCLING NOSE WHEEL STEERING SWITCH. "AIRCRAFT REMOVED FROM SERVICE" R&R'D WOW 1 RELAY Y "K1GA" PER CMM 24-00-11. REF 308096/4 FOR JB11 OPS CHECKS & REF 308095/2 FOR GEAR EXXTENSION/RETRACTION CHECKS.

Part: ANTI-ICE VALVE — MALFUNCTIONED (LT ENGINE) · airframe 41,804 hrs · 39,597 cycles

DURING CLIMOUT AFTER SELECTING ANTI ICE OFF RECEIVED LEFT COWL ANTIICE CAUTION FOLLOWED QRH SUSPECTED HIGH PRESSURE CONDITION. AIRCRAFT REMOVED FROM SERVICE R&R'D LH COWL ANTI ICE VALVE IAW AWA SUP 10-094, OPS CHECK GOOD WITH CREW ASSISTANCE. PN ON:300013000-003 SN:1880 PN OFF: 5399-00-1 SN: 1153B

Part: PRESSURE SWITCH — MALFUNCTIONED (ANTI-ICE) · airframe 41,545 hrs · 36,340 cycles

LEFT & RIGHT WING ANTI-ICE CAUTION MESSAGES IN ICING CONDITIONS, C/W QRH, LEFT ICING & RAN ICE DISPERSAL PROCEDURES. MESSAGE CLEARED FOR 2 MINS THEN RETURNS. ANTI-ICE WAS SELECTED TO NORMAL, OPENED ISOLATION VALVE, MESSAGE REMAINED. WENT TO STBY, MESSAGE CLEARED TEMPORARILY. BOTH WINGS SHOWED YELLOW ON EICAS THEN WENT CLEAR. BOTH SOVS INDICATED OPEN. NO DUCT FAIL LIGHT OR DUCT WARNING MESSAGE. WING ANTI-ICE ON MESSAGE WENT AWAY WHEN CAUTION APPEARED. AIRCRAFT REMOVED FROM SERVICE. R & R THE LT AND RT PRESSURE SWITCHES.

Part: ACTUATOR — BROKEN (THRUST REVERSER) · airframe 41,287 hrs · 39,079 cycles

"SUPPLEMENTAL INFORMATION" L REV UNLOCK CAUTION MESSAGE IN FLIGHT TR NOT ARMED AMBER REV ICON PHYSICALLY NOT STOWED EMER STOW PRESSED MSG REMAINS. REMOVED FROM SERVICE TO MEL. FOUND BROKEN T/R BALL SCREW ACTUATOR. R&R'D LT ENGINE LOWER INBOARD BALL SCREW ACTUATOR IAW AMM 78-32. CHECKS GOOD. REMOVED "M" ACTION AND PLACARD. THIS CLEARS MEL. SN OFF 5981 SN ON 8273 LEF "SUPPLEMENTAL INFORMATION"

Part: ACTUATOR — UNLOCKED (BALLSCREW) · airframe 41,227 hrs · 39,014 cycles

LEFT REVERSER UNLOCKED IN FLT NO ADVERSE HANDLING CHARACTERISTICS. RAN QRH. L REV UNLOCK CAUTION MESSAGE IN FLIGHT TR NOT ARMED AMBER REV ICON PHYSICALLY NOT STOWED EMER STOW PRESSED MSG REMAINS. REMOVED FROM SERVICE TO MEL. FOUND BROKEN T/R BALL SCREW ACTUATOR. R&R'D L/H ENGINE LOWER INBOARD BALL SCREW ACTUATOR IAW AMM 78-32. CHECKS GOOD. REMOVED "M" ACTION AND PLACARD. THIS CLEARS MEL.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,859 hrs · 37,681 cycles

RT FLOOR SILL IS CORRODED FROM FS 559+86 TO FS 559+112 AT RBL 47. REMOVED AND REPLACED RT FLOOR SILL AT FS 559+86 TO FS 559+112 AT RBL 47 IAW SRM 51-42-06 AND 51-42-21.

Part: HINGE — GOUGED (FUSELAGE) · airframe 39,859 hrs · 37,681 cycles

PAX DOOR HINGE HALF (FUSELAGE SIDE) IS GOUGED FROM THE ROLL PIN. REMOVED AND REPLACED FUSELAGE SIDE HINGE IAW SRM 53-21-23.

Part: FLOORBEAM — CORRODED (BS 349) · corrosion level 2 · airframe 39,859 hrs · 37,681 cycles

FLOOR BEAM ANGLE UNDER STRAP CORRODED ON UPPER SURFACE FS 349 LBL 37. REPLACED REPLACED FLOOR BEAM ANGLE AT FS 349 LBL 37 IAW CRJ 200 SRM 51-42-21

Part: FLOORBEAM — CORRODED (BS 349) · corrosion level 2 · airframe 39,859 hrs · 37,681 cycles

FLOOR BEAM UPPER SURFACE AT FS 349 AND LBL 40 CORRODED REPAIRED REPAIRED FLOOR BEAM UPPER SURFACE AT FS 349 AND LBL 40 IAW ASAP EA# AWAC-CRJ253-01077 REV A

Part: FLOOR SUPPORT — CORRODED (BS 409 - 409+128) · corrosion level 2 · airframe 39,859 hrs · 37,681 cycles

CENTER ISLE FLOOR LANDINGS FROM FS 409 TO 409+128 LBL 9 IS CORRODED. REPLACED REPLACED CENTER ISLE FLOOR LANDINGS FROM FS 409 TO 409+128 LBL 9 IAW CRJ 200 SRM'S 51-42-06 AND 51-42-21

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,859 hrs · 37,681 cycles

CENTER ISLE FLOOR LANDING IS CORRODED AROUND THE FASTENER HOLES AT RBL 9 FS 409 TO 409+128. REMOVED AND REPLACED FLOORBEAM SECTION 409-409+128 IAW SRM 51-42-21 AND 51-42-34.

Part: FLOOR SUPPORT — CORRODED (BS 559-569) · corrosion level 2 · airframe 39,859 hrs · 37,681 cycles

FLOOR BEAM AT RBL 9 FROM FS 559+66 TO 559+80 CORRODED. REPLACED REPLACED FLOOR BEAM AT RBL 9 FROM FS 559 TO 569 IAW CRJ 200 SRM'S 51-42-06, 51-41-21, 51-42-22 AND 53-61-43

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 39,859 hrs · 37,681 cycles

LH INBD FLAP LOWER SKIN PANEL DENTED AND DINGED WITH HEAVY PITTING. REPLACED REPLACED LH INBD FLAP LOWER SKIN PANEL IAW CRJ 200 SRM 57-42-13

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,859 hrs · 37,681 cycles

SERVICE DOOR LOWER SILL HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED SERVICE DOOR LOWER SILL IAW SRM 51-42-21 AND 51-42-10.

Part: ANGLE — CRACKED (NLG WW BULKHEAD) · airframe 39,859 hrs · 37,681 cycles

NLG WHEEL WELL 202 BULKHEAD LH POST UNDER TRU DECK HAS AN OB CLIP CRACKED. REPLACED REPLACED NLG WHEEL WELL 202 BULKHEAD LH POST UNDER TRU DECK OB CLIP IAW CRJ 200 SRM 51-42-06

Part: LANDING — CRACKED (LT TRU DOOR) · airframe 39,859 hrs · 37,681 cycles

LH TRU DOOR PANEL LANDING SKIN IS CRACKED BY THE AFT LATCH. REPLACED REPLACED LH TRU DOOR PANEL LANDING IAW CRJ 200 SRM 51-42-06 AND AWAC SUPP 17-280

Part: RIB — CRACKED (LT AILERON) · airframe 39,859 hrs · 37,681 cycles

LH AILERON LEADING EDGE RIB AT STA 342.481 GOUGED AND CRACKED. REPLACED REPLACED LH AILERON LEADING EDGE RIB AT STA 342.481 IAW CRJ 200 SRM 51-42-21 AND 51-42-06

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 39,859 hrs · 37,681 cycles

CARGO DOOR LOWER AFT INTERCOSTAL IS CRACKED ON THE OB FLANGE. REMOVED AND REPLACED CARGO DOOR LOWER AFT INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.

Part: DRAG ANGLE — CRACKED (BS 529-544) · airframe 39,859 hrs · 37,681 cycles

LEFT BATT RIB DRAG ANGLE IS CRACKED. REPLACED LEFT BATT RIB DRAG ANGLE IAW CRJ200 SRM 51-42-21.

Part: DRAG ANGLE — CRACKED (BS 529-544) · airframe 39,859 hrs · 37,681 cycles

RIGHT BATT RIB DRAG ANGLE IS CRACKED. REPLACED RIGHT BATT RIB DRAG ANGLE IAW CRJ 200 SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,859 hrs · 37,681 cycles

RT NR 7 SIDE SEAT RAIL CORRODED. REPLACED RT NR 7 SIDE SEAT RAIL IAW AMM 53-01-11.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 39,859 hrs · 37,681 cycles

AFT PRESSURE BULKHEAD AT UPPER END OF CARGO DOOR TRACK CRACKED. REPAIRED AFT PRESSURE BULKHEAD AT UPPER END OF CARGO DOOR TRACK IAW REO 601R-53-61-1541 REV F.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,859 hrs · 37,681 cycles

FLOOR SUPPORT AT FS 559+80 AT RBL 12 IS CORRODED. REPLACED FLOOR SUPPORT AT FS 559+80 AT RBL 12 IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,859 hrs · 37,681 cycles

FLOOR SUPPORT AT FS 559+80 AT RBL 38 CORRODED. REPLACED FLOOR SUPPORT AT FS 559+80 AT RBL 38 IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 39,859 hrs · 37,681 cycles

RIGHT FLOOR SEAT TRACK #4 CORRODED. REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 559+87-96) · corrosion level 2 · airframe 39,859 hrs · 37,681 cycles

RIGHT FLOOR SEAT TRACK #5 CORRODED. REPLACED SEAT TRACK IAW CRJ200 AMM 53-01-11.

Part: STRUCTURE — CRACKED (RT AILERON) · airframe 39,859 hrs · 37,681 cycles

R/H AILERON ON THE I/B SIDE HAS BEEN CHAFING/CRACKED. REPAIRED REPAIRED R/H AILERON ON THE I/B SIDE IAW AWAC SUPPLEMENT 18-324

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 39,859 hrs · 37,681 cycles

LT WING LE PANEL 520ML ATTACHMENT ANGLES CRACKED. REPLACED.

Part: PLATE — CRACKED (FLAP PANEL) · airframe 39,859 hrs · 37,681 cycles

FLAP PANEL 684AB HAS 2 CRACKED ATTACH PLATES. REPLACED ATTACH PLATED IAW CRJ200 SRM 51-42-06.

Part: ATTACH ANGLE — CRACKED (BS 476) · airframe 39,859 hrs · 37,681 cycles

LEFT WING TO FUSELAGE PANEL ATTACH ANGLE CRACKED AT FS 476.00. REPLACED ANGLE IAW CRJ200 SRM 51-42-06.

Part: ATTACH ANGLE — CRACKED (BS 450) · airframe 39,859 hrs · 37,681 cycles

LEFT WING TO FUSELAGE PANEL ATTACH ANGLE IS CRACKED AT FS 450.00. REPLACED ANGLE IAW CRJ200 SRM 51-42-06.

Part: ATTACH ANGLE — CRACKED (BS 476) · airframe 39,859 hrs · 37,681 cycles

RIGHT WING TO FUSELAGE PANEL ATTACH ANGLE IS CRACKED AT FS 476.00. REPLACED ANGLE IAW CRJ 200 SRM 51-42-06.

Part: ATTACH ANGLE — CRACKED (BS 450) · airframe 39,859 hrs · 37,681 cycles

RIGHT WING TO FUSELAGE PANEL ATTACH ANGLE IS CRACKED AT FS450.00. REPLACED ANGLE IAW CRJ200 SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,859 hrs · 37,681 cycles

NUMBER 3 SEAT TRACK AT RBL 9 IS CORRODED. REMOVED AND REPLACED NR 3 SEAT TRACK IAW AMM 53-01-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,859 hrs · 37,681 cycles

CARGO DOOR BEAM LOWER AFT CLIP CRACKED AT THE APB. REPLACED CARGO DOOR CLIP IAW SRM 51-24-16, 51-40-11, 51-24-36, 51-42-21.

Part: LANDING — BENT (FUSELAGE) · airframe 38,543 hrs · 36,822 cycles

FWD AND AFT LANDINGS ARE DAMAGED ON DOOR CUT OUT. REPLACED AFT LANDINGS AND REPAIRED FWD LANDING IAW SRM 51-42-06 AND SUPP. 16-191.

Part: SWITCH — MALFUNCTIONED (PAX DOOR) · airframe 35,632 hrs · 33,972 cycles

CLIMBING THROUGH 14,000 FEET RECEIVED PASSENGER DOOR OUTER HANDLE CAUTION. C/W QRH THEN RECEIVED PASSENGER DOOR MASTER WARNING. GREEN WITNESS MARKS REMAINED ALIGNED. R&R S102 MICROSWITCH AND PS1MB PROX SWITCH. PERFORMED OPS CHECKS IAW AMM 52-20-04. OPS CHECK GOOD. PRESSURIZED A/C TO 3.8 DELTA PRESSURE. CHECKED GOOD.

Part: BALL SCREW — LACK OF LUBE (THRUST REVERSER) · airframe 39,428 hrs · 37,238 cycles

RECEIVED A RIGHT THRUST REVERSER UNLOCK CAUTION MESSAGE INFLIGHT AT 31,000 FEET. COMPLIED WITH QRH, AMBER REVERSER ICON APPEARED ON N1 GAUGE, DIVERTED. FAILED TORQUE CHECK ON RT THRUST REVERSER. COMPLIED WITH A LUBE OF THE BALL SCREWS AND THRUST REVERSER TRACKS IAW AMM. RIG STOW AND THROTTLE LOCK OUT SWITCHES IAW AMM. OPS CHECKED GOOD.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,595 hrs · 36,494 cycles

ANGLE DOUBLER REPAIR ON THE BACK SIDE OF FRAME 349 HAS CORROSION BETWEEN STR 27 AND STR 26L IN THE FORWARD E & E BAY. REPLACED ANGLE DOUBLER ON THE BACK SIDE OF FRAME 349 BETWEEN STR 27 AND STR 26L IAW SRM 51-42-06, 51-42-21 AND REO 601R-53-21-1200, REV-A.

Part: HINGE — DENTED (PAX DOOR) · airframe 38,595 hrs · 36,494 cycles

PASSENGER DOOR HINGE HALF GOUGED, DENTED AT AFT END.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 38,595 hrs · 36,494 cycles

PASSENGER DOOR FS 338.90 AT LOWER STEP INTERCOSTAL IS CRACKED.

Part: DOOR SILL — CORRODED (BS 559-321) · corrosion level 2 · airframe 38,595 hrs · 36,494 cycles

CARGO DOOR SILL HAS NUMEROUS BARE METAL AND CORROSION SPOTS ON TH TOP AND BOTTOM SIDES BETWEEN BS 559+112 AND 621. REPLACED CARGO DOOR SILL IAW SRM 51-42-06, AND 51-42-21.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 38,595 hrs · 36,494 cycles

RIGHT INBOARD FLAP LOWER SKIN HAS DENT AT WS 74.0.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 38,595 hrs · 36,494 cycles

LEFT INTERCOSTAL AT FS 621 TO FS 625, STRINGER 13L IS CRACKED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,595 hrs · 36,494 cycles

FRAME 349 HAS CORROSION BETWEEN STR 25L AND STR 25R.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 38,595 hrs · 36,494 cycles

PAX DOOR STAIR ASSEMBLY LWR AFT ANGLE CRACKED AT RADIUS. REPLACED PAX DOOR STAIR AFT LOWER ANGLE IAW SRM 51-42-13, 51-42-06.

Part: BRACKET — CRACKED (SERVICE DOOR) · airframe 38,595 hrs · 36,494 cycles

SERVICE DOOR POSITION SENSOR MOUNTING BRACKET ON DOOR IS CRACKED.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 38,595 hrs · 36,494 cycles

INTERCOSTAL AT FS 621 - 625 ADJACENT TO STRINGER 14R IS CRACKED.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 38,595 hrs · 36,494 cycles

FLOOR LANDING AT FS 621 IS CRACKED AND HAS BARE METAL SPOTS BETWEEN LBL27 AND THE L/H FLOOR SILL IN THE CARGO BAY. REPLACED ANGLE, SLPICE STRAP ON LT FLOOR SILL BETWEEN LBL27 IN THE CARGO BAY IAW REO 601R-53-61-117REV C.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,595 hrs · 36,494 cycles

FLOORBEAM, RBL27 OTBD LANDING HAS CORROSION SPOTS BETWEEN FS 589.00 AND FS 621.00 IN THE CARGO BAY. REPLACE FLOORBEAM IAW SRM 51-42-21 AND AWAC SUP: 15-279.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 38,595 hrs · 36,494 cycles

NOSE HYDRAULIC BAY FORWARD SIDE OF FS 202.75, FRAME CAP BRACKET IS CRACKED, REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,595 hrs · 36,494 cycles

RIGHT INTERCOSTAL MEMBER AT FS 621-FS 625, STR 13R IS CRACKED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,595 hrs · 36,494 cycles

LEFT INTERCOSTAL MEMBER AT FS 621-625, STR 14L IS CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,595 hrs · 36,494 cycles

INTERCOSTAL, OBLIQUE ANGLE, AT FS 621-625 ADJACENT TO STR 14L IS CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,595 hrs · 36,494 cycles

CARGO SEAT TRACK ON RBL 9 HAS CORROSION BETWEEN FS 559+112 AND 574.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,595 hrs · 36,494 cycles

BATH TUB FITTING AT FS 461 AND RBL 9 IS CRACKED. REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,595 hrs · 36,494 cycles

FS 484, CLIP AT RBL 36 IS CRACKED, REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,595 hrs · 36,494 cycles

RIGHT SIDEWALL SEAT TRACK, STICK 3 BETWEEN FS 409+16 AND 409+112 CORRODED, REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,595 hrs · 36,494 cycles

FS 484, CLIP AT RBL 27 IS CRACKED, REPLACED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,595 hrs · 36,494 cycles

RIGHT WINDSHIELD POST LOWER OTBD ANGLE CRACKED.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 36,842 hrs · 34,840 cycles

GEAR DISAGREE NOSE DOWN, MAINS BOTH UP & LOCKED. PERFORMED QRH CYCLED GEAR HANDLE 2 TIMES, REPEATS. PULLED MANUAL GEAR RELEASE HANDLE, ALL GEAR DOWN & LOCKED. THE INITIAL WARNING WAS 6 SECONDS AFTER GEAR WAS ELECTED DOWN. NO INDICATION OF ANY ISSUES IN NR 3 HYD. EMER WAS DECLARED. REPLACED MLG SELECTOR VLV IAW AMM 32-32-10. LEAK & OPERATIONS CHECKED GOOD AT THIS TIME.

Part: IDG — LOW (LT ENGINE) · airframe 26,450 hrs · 25,682 cycles

RAMP AGENT REPORTS ELEC SMELL FROM LT ENG WHEN UNLOADING BAGS. INSPECTED & FOUND NR 1 IDG SIGHT GAUGE HAS NO OIL REF 274585 1 FOR MEL. NO OTHER DEFECTS NOTED. LP 274585 1 REPLACED LT ENG IDG IAW AMM CH 24. OPERATIONS & LEAK CHECKED GOOD. PLACARD REMOVED, CLEARS MEL 24-11-01-01.

Part: BOLT — SHEARED (PAX DOOR) · airframe 36,241 hrs · 34,258 cycles

PASSENGER DOOR PLUNGER IS BROKEN, INNER. FOUND TO BE PAX DOOR PULL IN HANDLE THAT WAS BROKEN. VERIFIED ALL GREEN WITNESS MARKS ARE ALIGNED WHEN DOOR LOCKED FROM OUTSIDE. VERIFIED DOOR LOCKS PROPERLY FROM OUTSIDE, PLACED ON MEL. FOUND BOLT SECURING INNER HANDLE MECHANISM SHEARED. R & R BOLT IAW AMM 52-11-02. RE-ASSEMBLED DOOR. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,525 hrs · 33,531 cycles

EMERGENCY EXIT WHITE LIGHT BY PAX DOOR INOPERATIVE. R & R BATTERY PACK IAW AMM 33-61-04. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,525 hrs · 33,531 cycles

OVERHEAD EMERGENCY EXIT LIGHT AT ROW 8, AFT SIDE INOPERATIVE. R & R BATTERY PACK IAW AMM 33-61-04. OPS CHECKED GOOD.

Part: TILLER — MALFUNCTIONED (NLG STEERING) · airframe 35,062 hrs · 33,092 cycles

DURING APPROACH, SELECTED GEAR DOWN, AT 170 KTS RECEIVED STEERING INOPERATIVE CAUTION MESSAGE. SELECTED SWITCH OFF, THEN MESSAGE WENT OUT THEN CAME BACK ON. LANDED WITHOUT INCIDENT. FOUND HAND WHEEL NOT RETURNING TO CTR. R & R PILOT HAND WHEEL IAW AMM 32-51-01. OPS & TAXI CHECKED GOOD. NO MESSAGE POSTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 30,493 hrs · 29,048 cycles

AFTER STARTING APU & TRANSFERRING PACKS TO APU BLEED, STARTED TO SMELL SMOKE, OIL SMELL FOLLOWED BY SMOKE TOILET CAUTION MSG. TRANSFERRED BACK TO ENG BLEEDS SMELL CLEARED ALONG WITH CAUTION MSG. COMPLIED WITH CM ACTION. PLACARDED & PLACED ON MEL, PLACED APU ON MEL 49-10-01-01.

Part: UNKNOWN — ODOR (CABIN-COCKPIT) · airframe 30,483 hrs · 29,041 cycles

SMOKE IN COCKPIT & CABIN AFTER STARTING APU IN AIR & TRANSFERRING BLEEDS TO APU. TRIGGERED SMOKE TOILET CAUTION. TRANSFERRED BLEEDS BACK TO ENG'S, SMOKE CLEARED. SMOKE SMELLED OF OIL.

Part: UNKNOWN — MALFUNCTIONED (RUDDER SYSTEM) · airframe 32,246 hrs · 30,161 cycles

AT 17,000 FT LEVEL WITH AUTO PILOT ON INITIATED RT TURN & RECEIVED VIOLENT YAW MOTION TO RIGHT, RT RUDDER TRIM INDICATED FULL NOSE RT NR, RN, RAN IAC FOR UNCOMMANDED YAW MOTION FOLLOWED BY QRH, DISCONNECTED AUTOPILOT. INSPECTED RUDDER SURFACE VISUALLY NO DEFECTS NOTED. PULLED RUDDER & AILERON TRIM PANEL. INSPECTED RUDDER SWITCH & CONNECTIONS VISUALLY NO DEFECT. REMOVED YAW DAMP PANEL, INSPECTED YAW DAMP SWITCH & CONNECTION. VISUALLY NO DEFECTS.

Part: PSU — UNSECURE (CABIN) · airframe 33,910 hrs · 32,003 cycles

IN ROWS 7A & 8A PAX PSU BOTH FELL DOWN ON CLIMB OUT.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,906 hrs · 32,001 cycles

CROSSBEAM AT FS 559.00 IS CORRODED ON UPPER SURFACE AT RBL 34 & RT SILL.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,906 hrs · 32,001 cycles

FS 310.70 IS CORRODED IN AVIONICS BAY.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,906 hrs · 32,001 cycles

FORWARD & AFT PAX DOOR CLEATS AT LOWER SILL CORRODED.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,901 hrs · 32,001 cycles

FRAME TO FLOOR SILL ATTACH FITTING AT FS 319 AT RBL 43 IS CORRODED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,901 hrs · 32,001 cycles

PASSENGER DOOR LOWER SILL INBD SURFACE HAS CORROSION.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,901 hrs · 32,001 cycles

INTERCOSTAL AFT OF AVIONICS DOOR CUT OUT AT FS 394 TO 409 IS CORRODED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,901 hrs · 32,001 cycles

CARGO BAY FLOOR SUPPORT BEAM HAS CORROSION AT FS 602 LBL 27.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,907 hrs · 32,001 cycles

LOWER FRAME SECTOR CORRODED AT FS 364.

Part: HOUSING — GOUGED (SERVICE DOOR) · airframe 33,907 hrs · 32,001 cycles

SERVICE DOOR OUTER HANDLE HOUSING INNER BORE GOUGED & WORN.

Part: SEAL — CRACKED (RT SPOILER) · airframe 33,907 hrs · 32,001 cycles

RIGHT FLIGHT SPOILER CTR SPRING SEAL IS CRACKED.

Part: HOUSING — GOUGED (PAX DOOR) · airframe 33,907 hrs · 32,001 cycles

PASSENGER DOOR OUTER HANDLE HOUSING INNER BORE GOUGED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,907 hrs · 32,001 cycles

LOWER FRAME SECTION CORRODED AT FS 333.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,907 hrs · 32,001 cycles

FS 310 LOWER FRAME SECTOR CORRODED IN AVIONICS BAY.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 33,906 hrs · 32,001 cycles

CARGO BAY FLOOR RAIL NEAR FS 615 & LBL 9 HAS CORROSION.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,907 hrs · 32,001 cycles

RIGHT OTBD FLOOR SILL CORRODED FROM FS 559 TO 559+80.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 33,906 hrs · 32,001 cycles

CARGO BAY FLOOR TRACKS RBL 9 & LBL 9 NEAR FS 574 HAVE CORROSION.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 33,906 hrs · 32,001 cycles

LOWER U BRACKET CRACKED AT RIVET AT FS 574.00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,906 hrs · 32,001 cycles

CORROSION AROUND HARDWARE & LT SEAT RAIL.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,907 hrs · 32,001 cycles

RIGHT PRESS FLOOR SILL CORRODED IN MULTIPLE LOCATIONS BETWEEN FS 409+128 & 559.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 33,608 hrs · 31,712 cycles

AFTER TAKEOFF, LEFT WINDSHIELD OUTSIDE PANE CRACKED FROM ONE CORNER TO THE OTHER, RETURNED TO DEPARTURE. INSPECTED WINDSHIELD & FOUND OUTER FACE, NON STRUCTURAL, PLY CRACKED. NO LOOSE PIECES. R & R CAPTAIN'S WINDSHIELD IAW AMM TEMP REV 56-023. RAN OPS CHECK OF WINDSHIELD HEAT IAW 30-41-01. OPS CHECKED GOOD. RAN PRESSURIZATION CHECK IAW 21-31-00. LEAK CHECKED GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 29,231 hrs · 27,858 cycles

FLAPS FAILED ON APPROACH AT 4000 FT WITH NO FLAP SELECTION. PERFORMED FLAP RESET PROCEDURE IAW SUP 98-18F BOX 12. FLAPS RESET, PLACARDED & PLACED ON MEL.

Part: BPSU — FAULTY (TE FLAP) · airframe 33,408 hrs · 31,519 cycles

FLAP FAIL CAUTION MSG IN CRUISE FLT WITH FLAPS AT ZERO POSITION. NOT CAUSED BY IMPROPER HANDLE MOVEMENT OR PHYSICAL RESTRICTION. LANDED AT FLAP ZERO. BTMS READS 6, 8, 3 & 4. REPLACED LT WING BPSU IAW AMM 27-51-10. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 32,183 hrs · 30,338 cycles

EN ROUTE FROM ORF TO CLT, ACFT ENTERED ICING CONDITIONS. RECEIVED MULTIPLE LT, RT WING ANTI-ICING CAUTION MESSAGE'S WITH WING SELECTED ON. COMPLIED WITH QRH ACTIONS, MESSAGE'S CONTINUED. QRH DIRECTED TO LEAVE ICING CONDITIONS BUT NO PLACE IN FUEL RANGE WHERE ICING CONDITIONS COULD AVOIDED & ACFT WAS ACCUMULATING ICE. EMERGENCY WAS DECLARED TO EXPEDITE ARRIVAL INTO CLT, NORMAL LANDING & TAXI. INSPECTED 14TH STAGE DUCTING IN AFT OF ACFT NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK OF WING ANTI-ICE SYSTEM IAW CRJ AMM 30-12-00. OPERATIONS CHECKED NORMAL.

Part: CONTROL LEVER — MALFUNCTIONED (TE FLAPS)

AFTER LANDING, FLAPS FAILED AT 30 DEG DURING RETRACTION. PERFORMED FLAP RESET PROCEDURE IAW SUP 98-18F BOX 12. FLAPS RESET. REMOVED AND REPLACED FLAP CONTROL LEVER REF AMM 27-51-01. OPS CHECKED GOOD.

Part: HYDRAULIC LINE — CHAFED (HYDRAULIC SYS) · airframe 26,349 hrs · 25,025 cycles

NR 1 HYD LOW PRESS IN FLIGHT, PRESSURE + QTY WENT TO ZERO, C/W QRH AT ZERO QTY FOR 18 MINUTES. REMOVED AND REPLACED CHAFED LINE IN AFT EQUIPMENT BAY AND LEAKING LINE IN PYLON. OPS AND LEAK CHECK GOOD AT THIS TIME IAW AMM 20-22-00.

Part: LUG — GOUGED (TE FLAP) · airframe 23,225 hrs · 22,305 cycles

LEFT O/B FLAP CENTER HINGE AFT LUG IS GOUGED ON ALL ATTACHING POINTS. BLENDED 4 GOUGED AREAS IAW REO 601R-57-21-1753.

Part: HINGE BRACKET — GOUGED (THRUST REVERSER) · airframe 23,225 hrs · 22,305 cycles

RIGHT UPPER TRANS COWL HINGE BRACKET IS GOUGED. BLENDED AREAS REMOVING SHARP EDGES TO SMOOTH CONTOUR IAW REO 601R-78-33-4002.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,225 hrs · 22,305 cycles

FRAME AT FS 280 HAS A CRACK IN RADIUS LEFT SIDE & CORROSION OF FLOOR SUPPORT ANGLE WITH CRACKED CLIPS AT LBL 9 & RBL 9. REPAIRED FS 280 BULKHEAD IAW GREO 601R-53-11-926.

Part: HINGE BRACKET — GOUGED (THRUST REVERSER) · airframe 23,225 hrs · 22,305 cycles

RIGHT LOWER TRANS COWL HINGE BRACKET IS GOUGED. BLENDED AREAS REMOVING SHARP EDGES TO SMOOTH CONTOUR IAW REO 601R-78-33-4002.

Part: HINGE BRACKET — GOUGED (TRANS COWL) · airframe 23,225 hrs · 22,305 cycles

LEFT UPPER TRANS COWL HINGE BRACKET IS GOUGED. BLENDED AREAS REMOVING SHARP EDGES TO SMOOTH CONTOUR IAW REO 601R-78-33-4002.

Part: NOZZLE — CRACKED (RT ENGINE) · airframe 23,225 hrs · 22,305 cycles

RIGHT JET PIPE FAIRING HAS HOT SPOT WITH CRACKS. REPAIRED RIGHT EXHAUST NOZZLE FAIRING INNER FIRESHIELD IAW BOMBARDIER CMM 78-11-00 REPAIR #SRS027.

Part: SILL — CORRODED (FUSELAGE) · airframe 23,225 hrs · 22,305 cycles

LEFT FLOOR SILL AT APPROX FS 353 HAS CORROSION. BLEND CORROSION TO ALLOWABLE LIMITS IAW REO 601R-53-21-2352.

Part: HINGE BRACKET — GOUGED (THRUST REVERSER) · airframe 23,225 hrs · 22,305 cycles

LEFT LOWER TRANS COWL HINGE BRACKET IS GOUGED. BLENDED AREAS REMOVING SHARP EDGES TO SMOOTH CONTOUR IAW REO 601R-78-33-4002.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 23,225 hrs · 22,305 cycles

CLIP CRACKED UNDER CARGO DOOR SILL AT FS 589. REPLACE UNSERVICEABLE CLIP ANGLE WITH NEW SERVICEABLE UNDER CARGO DOOR SILL.

Part: ANGLE — CRACKED (RT WING) · airframe 23,225 hrs · 22,305 cycles

RIGHT WING ANTI-ICE TRANSITION DUCT MOUNTING PLATE UPPER ANGLE BETWEEN 620JL & 630JL IS CRACKED IN OUTBOARD. REMOVED AND REPLACED UPPER ANGLE IAW CRJ 200 SRM 51-42-10, 51-42-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,225 hrs · 22,305 cycles

CLIP CRACKED AT FS 484 RBL 27. REMOVED & REPLACED CRACKED CLIP WITH SERVICEABLE P/N S6144A33 IAW REO 601R-53-41-059.

Part: FITTING — CHAFED (TE FLAP) · airframe 23,225 hrs · 22,305 cycles

LEFT O/B FLAP ROLLER FITTING CHAFED AND ROLLER WORN. REPAIRED LEFT O/B ROLLER FITTING IAW BOMBARDIER REO 601R-57-53-948. REMOVED WORN ROLLER INSTALLED NEW SERVICEABLE ROLLER (P/N NAS562-5R5) IAW CRJ 200 SRM 51-41-04.

Part: ANGLE — CRACKED (LT WING) · airframe 23,225 hrs · 22,305 cycles

LEFT WING ANTI-ICE TRANSITION DUCT MOUNTING PLATE UPPER ANGLE BETWEEN 520JL & 530L IS CRACKED IN OUTBOARD CORNER. REMOVED AND REPLACED UPPER ANGLE IAW CRJ 200 SRM 51-42-10, 51-41-02.

Part: PANEL — MISSING (EXHAUST) · airframe 23,450 hrs · 22,235 cycles

MISSING PANEL AT O`CLOCK POSITION. INSTALLED EXHAUST NOZZLE FAIRING MOUNT BOLT ACCESS PANEL IAW AMM 78-11-01, REF L/P 249882/3 FOR MEL.

Part: DUCT — CONTAMINATED (A/C PACK) · airframe 23,247 hrs · 22,010 cycles

F/A REPORTED "SMOKE" IN CABIN DURING FLIGHT. FOUND PACK DUCT CONTAMINATED WITH COMPRESSOR WASH FLUID, MX PERFORMED POST COMPRESSOR WASH RUN IAW SUPP 06-047A AND CLEARING OF CONTAMINATION DUCTING IAW SUPP 09-037A. NO SMOKE ODOR PRESENT.

Part: PDU — FAILED (TE FLAPS) · airframe 23,219 hrs · 21,983 cycles

FLAPS FAIL CAUTION MESSAGE IN FLIGHT, WHEN FLAPS WERE SELECTED FROM 0 TO 8 FLAPS FAILED AT 0. R & R FLAP PDU. OPS CHECKED GOOD AT THIS TIME REF AMM 27-52-01.

Part: POWER SUPPLY — FAILED (TE FLAPS) · airframe 23,219 hrs · 21,983 cycles

AT 3000 FT APPROX 190 KNTS, FLAP FAILED AT ZERO ON APPROACH. PERFORMED FLAP RESET PROCEDURE IAW SUP 98-18E, BOX 12 FLAPS RESET. R & R RT BPSU IAW AMM 27-51-10 FLAPS OPS CHECK GOOD.

Part: BPSU — FAILED (RT WING TE FLAPS) · airframe 22,992 hrs · 21,754 cycles

FLAPS FAIL AT 0 DEGREES EXTENDING TO 8 DEGREES AT THE TIME. PERFORMED RIG OF FLAPS FECU REPORTS R-BPSU FAULT. REPLACED RT BPSU IAW AMM 27-50. OPS CHECK GOOD CLEARS PLACARD AND MEL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,542 hrs · 21,272 cycles

FLOOR LEVEL EMERGENCY LIGHTS NEXT TO ROWS 1-5 AND 9-12 WILL NOT ILLUMINATE. INSPECTED AND RECONNECTED EMERGENCY LIGHT CONNECTORS FOR INOP LIGHTS EMERGENCY LIGHT FROM ROW 1-5 OPS NORMALLY. FLOOR LEVEL LIGHTS 9-12 REMAIN INOPERATIVE. R & R BATTERY PACK OPS CHECKED GOOD.

Part: TILLER — BINDING (NLG STEERING) · airframe 22,429 hrs · 21,155 cycles

UPON APPLICATION OF T/O THRUST, ACFT VEERED TO LEFT EVEN WITH FULL RT RUDDER. FOUND NOSE STEERING TILLER STICKING AND NOT RETURNING TO CENTER. R & R TILLER IAW AMM 32-51. OPS CKS GOOD.

Part: TARGET — LOOSE (MLG UPLOCK) · airframe 21,952 hrs · 20,648 cycles

AFTER T/O, GOT DISAGREE WARNING 5 SECONDS AFTER SELECTING GEAR UP RECYCLED GEAR OPERATED NORMAL LT MAIN GEAR DID NOT SHOW UP AND LOCKED. PERFORMED TROUBLESHOOTING IAW FIM, 32-60-07, INTERROGATED PSEU, RECEIVED "S20 DOWN ARROW FAR". LT UPLOCK ASSY INSPECTED AND FOUND TARGET LOOSE, RESECURED AND RERIGGED UPLOCK TARGET IAW AMM 32-32-05, GEAR SWING AND OPS CK GOOD.

Part: ACTUATOR — FAILED (HYD SHUTOFF VALV) · airframe 21,952 hrs · 20,648 cycles

JUST PRIOR TO LANDING, RT ENGINE HYD SOV CB POPPED AND DETECTED AN ODOR OF ELECTRICAL SMOKE MOMENTARILY IN COCKPIT. CB REMAINS OPEN CBP NR 1 "S4". R & REPAIRED RT ENG HYD SHUTOFF VALVE ACTUATOR. OPS CHECKS GOOD IAW 29-11-36, NO SMELL NOTED.

Part: O-RING — LEAKING (APU FUEL) · airframe 21,393 hrs · 20,055 cycles

FUEL ODOR IN ACFT SEEMS TO BE COMING FROM PACKS, SEEMS TO BE ASSOCIATED WITH APU AIR. R & R O-RING UNDER UNION AT FUEL SOLENOID. OPS AND LEAK CHECK OK IAW AMM 49-30.

Part: FRAME — CORRODED (BS 349) · corrosion level 1 · airframe 24,637 hrs · 22,748 cycles

FRAME STATION 349, CORRODED ON FWD & AFT FACE 6 O`CLOCK POSITION SECTION. REMOVED CORROSION ON FWD AND AFT FACE OF FRAME AT FS 349 IAW SRM 51-21-06 AND REPAIRED FUSELAGE STRUCTURE FS 349 AND STR 26L IAW REO 601R-53-21-1200.

Part: TORQUE BOX — CRACKED (THRUST REVERSER) · airframe 24,637 hrs · 22,748 cycles

LT LOWER CORE COWL CHAFED FROM BLOCKER DOOR NEXT TO FWD LATCHES. BLENDED DAMAGE IAW REO 601R-71-12-232, REV D AND WAS FOUND TO BE WITHIN ALLOWABLE LIMITS DAMAGE MEASURES 4.00 LONG, 0.25 WIDE AND .007 DEEP TREATED AREA IAW CMM 200 AND SRM 51-25-06.

Part: SILL — CORRODED (BS 349) · airframe 24,637 hrs · 22,748 cycles

RT FLOOR SILL CORRODED AFT OF FS 349. REPAIRED RT FLOOR SILL BETWEEN FS 349 AND FS 379 AT WL 73.10 IAW REO 601R-53-21-326.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,637 hrs · 22,748 cycles

FLOOR CROSSBEAM AT FS 349.00 IS CORRODED ON RT SIDE. REPAIRED CROSSBEAM AT FS 349, RBL 40.0, WL 73.10 IAW REO 601R-53-21-1198 & REO 601R-53-21-1202.

Part: SEAT TRACK — CORRODED (BS 439) · corrosion level 2 · airframe 24,637 hrs · 22,748 cycles

LT SIDE SEAT RAILS HAVE CORROSION AT AFT END OF NR 4 AND FWD END OF NR 5 RAILS. R & R UNSERVICEABLE SEAT RAIL SECTIONS WITH SERVICEABLE BULK TRACK P/N N126-2075 IAW AMM 53-01-11 AND REO 601R-53-00-055.

Part: VANE — CHAFED (LT WING FLAP) · airframe 24,637 hrs · 22,748 cycles

LT INBD FLAP VANE HAS CHAFING DAMAGE IN 3 PLACES ON L/E. R & R NEW SERVICEABLE TITANIUM CAPS ON LT INBD FLAP VANE L/E IAW SB 601R-57-022, REV B.

Part: VANE — CHAFED (RT WING FLAP) · airframe 24,637 hrs · 22,748 cycles

RT INBD FLAP ON L/E HAS CHAFING DAMAGE IN 3 PLACES. REMOVED AND INSTALLED NEW SERVICEABLE TITANIUM CAPS ON RT INBD FLAP VANE L/E IAW SB 601R-57-022, REV B.

Part: ANGLE — GOUGED (BS 621) · airframe 24,637 hrs · 22,748 cycles

ANGLE ON AFT PRESSURE BULKHEAD 621.0 BETWEEN CARGO NET SUPPORT AND CONNECTOR PLUGS IS GOUGED. REPAIRED AND REINSTALLED ANGLE HORIZ FLANGE IAW REO AND 601R-53-61-109, REV NC.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 24,637 hrs · 22,748 cycles

PAX DOOR INNER AND OUTER CORNER ANGLES AT FS 347.25 CORRODED. REMOVED PAX DOOR INNER AND OUTER CORNER ANGLES AT FS 347.25 AND INSTALLED NEW SERVICEABLE ANGLE PN 601R319983-4 IAW SRM 51-42-06, 51-40-11.

Part: BULKHEAD — CHAFED (BS 280) · airframe 24,637 hrs · 22,748 cycles

RT AFT 280 BULKHEAD CHAFED FROM GALLEY DOOR. REMOVED CHAFING BY CUTTING OUT THE DAMAGED AREA ON RT AFT 280 BULKHEAD AND INSTALLING WEB DOUBLER, WEB FILLER IAW REO 601R-53-11-1727.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 24,637 hrs · 22,748 cycles

PAX DOOR INNER AND OUTER ANGLES CORRODED AT FS 311.75. REMOVED FWD INNER & OUTER CORNER ANGLES AT FS 311.75 AND INSTALLED NEW PN 601R319983-3.

Part: FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 24,637 hrs · 22,748 cycles

PAX DOOR LWR INNER CLEATS 4 EA CORRODED BEYOND LIMITS AT 320.10 AND 338.00. REMOVED CORRODED CLEATS AT FS 320.10 AND 338.00 4 EA AND INSTALLED NEW CLEATS IAW SRM 52-10-14, 51-42-06.

Part: BONDING — CORRODED (LT PYLON) · corrosion level 2 · airframe 24,637 hrs · 22,748 cycles

LT UPPER PYLON T/E HAS 2 EA BONDING PLATES PN 601-37012-33 CORRODED. R & R LT UPPER PYLON T/E BONDING PLATES PN 601-37012-33 SRM 51-22-00.

Part: PLATE — CORRODED (RT PYLON) · corrosion level 2 · airframe 24,637 hrs · 22,748 cycles

RT UPPER PYLON T/E HAS 2 EA BONDING PLATES (PN 601-37012-33) CORRODED. R & R RT UPPER PYLON T/E BONDING PLATES PN 601-37012-33 IAW SRM 51-22-00.

Part: SKIN — CHAFED (LT AILERON) · airframe 24,637 hrs · 22,748 cycles

UPPER AND LOWER L/E OF LT AILERONS IS CHAFED. BLENDED OUT LOWER SKIN WITH .040 MATERIAL REMAINING FOUND TO BE WITHIN LIMITS IAW REO 601R-57-60-020, REV NC. UPPER SKIN FOUND TO BE OUT OF LIMITS. DRILLED AND INSTALLED NEW SERVICEABLE UPPER SKIN IAW SRM 51-40-11, 51-42-06, 51-42-10.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 24,637 hrs · 22,748 cycles

LT INBD FLAP INNER SKIN AT CENTER FLAP VANE ACTUATOR CARRIAGE CHAFED FROM BONDING JUMPER. REPAIRED LT INBD INNER SKIN AT CENTER FLAP VANE ACTUATOR CARRIAGE IAW REO 601R-57-52-1665 REV, NC.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 24,637 hrs · 22,748 cycles

PAX DOOR AFT DRAG ANGLE CRACKED CUT OUT DAMAGED SECTION AND THEN SPLICED IN NEW SECTION WITH NEW SERVICEABLE ANGLE PN 601R31907 IAW REO 601R-52-11-513 REV A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,637 hrs · 22,748 cycles

FS559+80 FLOOR SEAT TRACKS AT LBL9, LBL27, RBL9 AND RBL27 ARE CORRODED. REMOVED UNSERVICEABLE FLOOR SEAT TRACKS (LBL9, LBL27, RBL9 AND RBL27) DUPLICATED FLOOR SEAT TRACKS FROM BULK STOCK PN N126-2075.

Part: BLOCKER DOOR — WORN (THRUST REVERSER) · airframe 24,637 hrs · 22,748 cycles

BLOCKER DOORS NR 3, 4, 5, 6, 7 AND 8 ON LT T/R ARE WORN FROM STOPS. REPAIRED LT T/R BLOCKER DOORS NR 3,5,6,7,8 IAW CMM 78-30-00-300-8720-A01. REPAIR NO SRS 100.

Part: PANEL — CHAFED (RT PYLON) · airframe 24,637 hrs · 22,748 cycles

PYLON PANEL 422DB SEPARATORS ARE KNIFE EDGE. R & INSTALLED PN 601R37138-26 AND PN 601R37138-28 IAW SRM 51-42-06.

Part: HINGE — GOUGED (FUSELAGE) · airframe 24,637 hrs · 22,748 cycles

PAX DOOR HINGE (ACFT SIDE) HAS 3 GOUGED LUGS. REMOVED 3EA GOUGES ON PAX DOOR HINGE (ACFT SIDE) LUGS IAW REO 601R-53-21-814, REV NC TREATED AREAS IAW SRM 51-21-16.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,637 hrs · 22,748 cycles

FS 559 + 112 FLOOR SEAT TRACKS AT LBL 9 AND RBL 9 ANR CORRODED. REMOVED UNSERVICEABLE SEAT TRACK LBL9 AND RBL9. DUPLICATED PARTS FROM BULK STOCK. N126-2075 AND INSTALLED SERVICEABLE SEAT TRACK AT LBL9 AND RBL9 FS559+112.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 24,637 hrs · 22,748 cycles

PAX DOOR FRAME AT FS 338.00 CRACKED ON UPPER END. REMOVED CRACKED SECTION AND SPLICED IN NEW SECTION FROM NEW SERVICEABLE PN 601R31902-5 IAW REO 601R-52-11-402, REV H, REPAIR I.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 24,637 hrs · 22,748 cycles

LWR AFT FRAME BRACKET SEAL STRIKER & SILL ANGLES ON SERVICE DOOR THRESHOLD HAVE CORROSION. EVALUATION CORROSION BRACKET FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06, EVL CORROSION ON SEAL STRIKER & SILL ANGLES IAW SRM 51-21-06. ORIG MATERIAL .063 REMOVED 004 FOUD IN LIMIT IAW SRM 51-21-06. CHECKED TOOL AAR 326 THICKNESS TEST.

Part: RIB — CRACKED (LT WING) · airframe 24,637 hrs · 22,748 cycles

LT BATT RIB CRACKED. REPAIRED BATT RIB WS 53.60 IAW REO 601-57-51-046, REV B, REPAIR NR 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,637 hrs · 22,748 cycles

INBD AND OTBD CLIPS ON LBL 9 ARE CRACKED AT FS 280. REMOVED INBD AND OTBD CLIPS ON LBL9 AND INSTALLED NEW SERVICEABLE CLIPS AT BOTH LOCATIONS IAW SRM 51-42-21, 51-42-06.

Part: SEAT TRACK — CORRODED (BS 378) · airframe 24,637 hrs · 22,748 cycles

NR 1 SEAT TRACKS ON RBL AND LBL 9 HAVE CORROSION. REMOVED OLD SEAT TRACKS IAW AMM 53-01-11. INSTALLED NEW SEAT TRACKS PN 126-2075 IAW AMM 53-01-11.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,637 hrs · 22,748 cycles

RT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED UNSERVICEABLE OBLIQUE ANGLE FROM RT FS 625 AND INSTALLED SERVICEABLE OBLIQUE ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-985, REV NC.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,637 hrs · 22,748 cycles

AT FS STA 484, LBL 27 CLIP PN 601R31171-17 ATTACHED TO INTERCOSTAL PN 601R31171-21 HAS A CRACK AT AFT LWR FACE .2500 INCH LONG. REMOVED CRACKED CLIP AND FABRICATED NEW CLIP AND INSTALLED NEW CLIP IAW REO 601R-53-41-059 AND SRM 51-04-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,637 hrs · 22,748 cycles

OTBD CLIP ON RBL9 IS CRACKED AT FS280. REMOVED OTBD CLIP ON RBL9 AND INSTALLED NEW SERVICEABLE CLIP ON RBL9 IAW SRM 51-42-21, 51-42-06.

Part: TRACK — CRACKED (THRUST REVERSER) · airframe 24,637 hrs · 22,748 cycles

LT LOWER OTBD TR TRACK CRACKED. R & R LT OTBD T/R TRACK IAW SRM 51-42-02, 51-45-00 AND AMM 20-26-00, 78-34-11.

Part: MOUNT BRACKET — CRACKED (GROUND POWER) · airframe 24,637 hrs · 22,748 cycles

ACFT GROUND POWER RECEPTICLE MOUNT BRACKET IS CRACKED IN 1 PLACES. REMOVED AND REPLACED GROUND POWER RECEPTICLE MOUNTING BRACKET IAW SRM 51-42-06, 51-42-21 AND REO 601R-53-11-569, REV A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,637 hrs · 22,748 cycles

LT FS625 OBLIQUE ANGLE IS CRACKED. REMOVED UNSERVICEABLE OBLIQUE ANGLE FROM LT FS625 AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-985.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 24,637 hrs · 22,748 cycles

RT SIDE SEAT RAIL NR3 HAS CORROSION. REMOVED UNSERVICEABLE RT SEAT TRACK RAIL NR3 SIDE DUPLICATED SERVICEABLE SIDE SEAT TRACK FROM BULK STOCK AND INSTALLED SERVICEABLE RT SIDE SEAT RAIL NR3.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 24,637 hrs · 22,748 cycles

PAX DOOR AFT CLEAT CORRODED. R & R PAX DOOR AFT CLEAT IAW SRM 51-42-06.

Part: DOOR TRACK — GOUGED (CARGO BAY) · airframe 24,637 hrs · 22,748 cycles

CARGO DOOR FWD TRACK IS GOUGED IN 2EA AREAS. REPAIRED CARGO DOOR FWD TRACK IAW REO 601R-53-62-024.

Part: DOOR TRACK — GOUGED (CARGO BAY) · corrosion level 1 · airframe 24,637 hrs · 22,748 cycles

CARGO DOOR AFT TRACK IS GOUGED IN 2 EA AREAS. REPAIRED CARGO DOOR AFT TRACK IAW REO 601R-53-62-004.

Part: FITTING — CRACKED (LT COWLING) · airframe 24,637 hrs · 22,748 cycles

LT NOSE COWL HAS 1 CRACKED CLIP ON ATTACH FLANGE AT 9:00 POSITION. REMOVED UNSERVICEABLE CLIP & REPLACED BY SERVICEABLE CLIP ON LT NOSE COWL AT 9:00 POSITION IAW REO 601R-11-61-3941, REV A.

Part: HINGE — GOUGED (PAX DOOR) · airframe 24,637 hrs · 22,748 cycles

PAX DOOR HINGE (DOOR SIDE) HAS 3 GOUGED LUGS. REMOVED THE 3 GOUGES ON PAX DOOR HINGE ( DOOR SIDE LUGS IAW REO 601R-521-11-1347 REV NC, TREATED AREAS IAW SRM 51-21-16.

Part: SKIN — CHAFED (AILERON) · airframe 24,637 hrs · 22,748 cycles

UPPER & LOWER OF RT AILERON IS CHAFED. BLENDED OUT CHAFING AREA ON UPPER & LOWER L/E OF RT AILERON IAW REO 601R-57-60-020.

Part: BRACKET — BROKEN (BS 529) · airframe 24,637 hrs · 22,748 cycles

STAB FAIRING BRACKET LT SIDE BROKEN. INSTALLED SERVICEABLE BRACKET ATTACH FITTING ON LT SIDE IAW SRM 51-42-21.

Part: FRAME — CRACKED (BS 559) · airframe 22,639 hrs · 20,645 cycles

FOUND INDICATION OF CRACK RT 559 FRAME AT RBL 9. REPAIR USING REO 601R-53-41-260.

Part: FAN — FAILED (GALLEY) · airframe 20,764 hrs · 18,816 cycles

GALLEY/LAV FAN CIRCUIT BREAKER POPPED, NOTICED SLIGHT ODOR PRIOR TO FINDING CB POPPED. SUSPECT GALLEY FAN. REPLACED GALLEY FAN OPS TEST GOOD REMOVE FROM MEL. (K)

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 16,371 hrs · 14,949 cycles

RT WINDOW HEAT CASS MESSAGE DISPLAYED IN FLIGHT COMPLIED WITH QRH MESSAGE DID NOT CLEAR. IAW FIM, SWAPPED O/H SENSORS S1 AND S2 WITH SPARE SENSORS S5 AND S6. PERFORMED PRESSURIZATION CHECK, OPS CHECKED AND RT WINDOW HEAT SYS CHECKS NORMAL IAW AMM 30-41-01. (K)

Part: BULKHEAD — CRACKED (BS 202) · airframe 20,567 hrs · 18,625 cycles

CRACK FOUND ON FWD PRESSURE BLKHD AT FS 202.75, LBL 23.71 AROUND THE PARKING BRAKE CABLE FWD PRESSURE BLKHD REPAIRED IAW REO 601R-53-11-563. (K)

Part: ANTI-ICE VALVE — FAULTY (RT ENGINE) · airframe 20,245 hrs · 18,326 cycles

LOG 186570/2 RT COWL ANTI-ICE MSG IN FLIGHT WITH ANTI-ICE SELECTED ON. COMPLIED WITH QRH, MST PERSISTED, DIVERTED. REMOVED AND REPLACED RT COWL ANTI-ICE VALVE REF AMM 30-20. OPS AND LEAK CHECK GOOD.

Part: FITTING — CRACKED (BULKHEAD) · airframe 20,194 hrs · 18,275 cycles

MWC 18 FS 621 PRESSURE BULKHEAD WEB THAT SURROUNDS THE ATTACHMENT FITTING IS CRACKED. PERFORMED A REPAIR BY CUTTING OUT SECTION OF WEB, FABRICATING AND INSTALLING REPAIR PARTS IAW REO 601R-53-61-1230 REV D.

Part: HANDLE — DAMAGED (SERVICE DOOR) · airframe 19,240 hrs · 17,397 cycles

SERVICE DOOR OUTER HANDLE PLUNGER BROKE OFF. RESECURED HANDLE PLUNGER IAW AMM 52-40. (A)

Part: FLAP SYSTEM — FAILED (TE FLAPS)

FLAPS FAILED OCCURRED ON APPROACH TO PHL, FLAPS FAILED AT 20 DEGREES, QRH PROCEDURE COMPLIED WITH OPS CHECK GOOD. COMPLIED WITH RESET PER SUPP 98-018B, OPS CHECK GOOD. (M)

Part: HANDLE — STUCK (PAX DOOR)

FLIGHT CREW REPORTS PAX DOOR OUTER HANDLE DOES NOT RELEASE WHEN THE TRIGGER IS PRESSED. (K)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 18,204 hrs · 16,419 cycles

FLAPS FAIL INDICATION ON APPROACH, DIVERTED TO ORD, FLAPS AT 5 DEGREES. COMPLIED WITH RESET PROCEDURES, IAW AWAC SUPP 98-018B, STEPS 1.3 AND 1.4, FLAPS SYSTEM RESET OK. (M)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 13,982 hrs · 12,712 cycles

FLAPS FAIL INDICATION ON APPROACH DIVERTED TO ORD, FLAPS AT 5 DEGREES. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4. FLAPS SYSTEM RESET OK. (M)

Part: DRIVE SHAFT — FAILED (TE FLAPS) · airframe 18,130 hrs · 16,353 cycles

FLAPS FAIL AT ZERO DEGREE, WHEN MOVING TO FLAPS 8 DEGREE ON DESCENT. COMPLIED WITH RESET PROCEDURE IWA AWAC SUPP 98-018B STEPS 1.3 AND 1.4. FLAP SYS RESET OK. (K) FOUND LT DRIVE SHAFT NR 5 UNSEREVICEABLE. REMOVED AND REPLACED PER AMM 27-53-10, OPS CHECK GOOD. SYSTEM OPS CHECK GOOD. (M)

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS)

FLAPS FAIL AT 20 DEGREES AND FLAPS WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED FECU S/N 895, TSN 10680, CSN 9539. (M)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 15,865 hrs · 14,182 cycles

UPON FLAP SELECTION, FLAP FAIL MESSAGE APPEARED 8 DEGREES FLAP NOTED. (K) [06-13-07] REMOVED/REPLACED FLEX DRIVESHAFT SER NR 12973 TSN 25 CSN 23. REMOVED AND REPLACED FECU SER NR 1354 TSN 6945 CSN 6437. (M)

Part: DRIVE SHAFT — LACK OF LUBE (T/E FLAP) · airframe 15,832 hrs · 14,125 cycles

FLAPS FAILED AT 20 AFTER DEPARTURE. CLEANED AND LUBRICATED ALL RT FLAP DRIVE SHAFTS. OPS CHECK GOOD. (K)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS)

FLAPS FAIL CAUTION MESSAGE FLAPS FAILED ZERO. INSPECTED FLAPS FOUND NO EVIDENCE OF TWISTING SKEWING, OR ABNORMAL DEFORMATION, NO FAULTS FOUND, SYSTEM RESET AND SYSLED FLAPS IAW SUPPLEMENTAL 98-018A. (K)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 15,703 hrs · 14,028 cycles

CARGO DOOR SUPPORT BEAM ANGLE THAT ATTACHES TO REAR PRESSURE BULKHEAD FS 621. CRACKED APPROX 1 INCH LONG (ANGLE PN 601R35050-109). MAINTENANCE DRILLED OFF, REMOVED CRACKED BRACKET, INSTALLED NEW SUPPORT ANGLE PN 601R35050-109 USING HST10AG-6 AND HST110AG-6 HILITES IAW SRM 51-40-11 AND 51-42-21. (K)

Part: RIB — CRACKED (LT WING) · airframe 15,703 hrs · 14,028 cycles

LT MLG BATT RIB CRACKED 1 INCH LONG UPPER AFT CORNER MAINTENANCE REPAIRED BATT RIB IWA REO 601R-57-51-046. (K)

Part: RIB — CRACKED (RT WING) · airframe 15,703 hrs · 14,028 cycles

RT MLG BATT RIB CRACKED 1 INCH LONG AT UPPER AFT CORNER.. MAINTENANCE REPAIRED BATT RIB IAW REO 601R-57-51-046. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 15,703 hrs · 14,028 cycles

FS 484.0 INTERCOSTAL CRACKED AT RBL 36 APPROX .4 INCH IN UPPER RADIUS. MAINTENANCE REPAIRED INTERCOSTAL IAW REO 601R-53-41-059 REV (A) AND BSC STANDARD REPAIR 601R-53-0030A. (K)

Part: BEAM — CRACKED (FUSELAGE) · airframe 15,703 hrs · 14,028 cycles

VERTICLE BEAM AT FS 559.0, RBL 9 CRACKED APPROX .300 INCH LONG AT LOWER OB FLANGE. MAINTENANCE REPAIRED FS 559.0 BULKHEAD POST AT RBL 9, LOWER OB FLANGE IAW REO 601R53-41-057 (A). (K)

Part: SKIN — CORRODED (RT WING) · corrosion level 1 · airframe 15,703 hrs · 14,028 cycles

RT WING LOWER PLANK FUEL ACCESS PANEL 640AB HOLE NR 4 AT WS 54.681 HAS MINOR CORROSION ON AFT FLANGE APPROX .003 INCH DEEP AND 3 INCHES LONG IN CRITICAL AREA. MAINTENANCE REPAIRED FUEL WING PLANK CUTOUT HOLE NR 4 (640AB) IAW REO 601R-57-21-030 REV (F).

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 15,703 hrs · 14,028 cycles

LT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REMOVED AND REPLACED INTERCOSTAL PN 6013501251 IAW SRM 51-42-06. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 15,703 hrs · 14,028 cycles

RT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REMOVED AND REPLACED INTERCOSTAL PN 601-35012-52 IAW SRM 51-42-06. (K)

Part: SWITCH — FAILED (PITCH SYS)

STAB AND MACH TRIM CAS MESSAGE IN FLIGHT. COMPLIED WITH QRH, MESSAGE CLEARED AFTER SECOND ATTEMPT, AIR RETURN. FOUND BAD PITCH DISCONNECT SWITCH DURING TROUBLESHOOTING. REMOVED AND REPLACED PILOTS SWITCH IAW AMM 27-41-30, OPS CHECK GOOD. (M)

Part: TRIGGER — DAMAGED (PAX DOOR)

PAX DOOR WON`T OPEN FROM INSIDE. REMOVED AND REPLACED PASSENGER DOOR TRIGGER AND PINS IAW AMM 52-1-03. (M)

Part: SMOKE DETECTOR — FAULTY (LAVATORY)

SMOKE TOILET CAS MESSAGE COMES ON INTERMITTENTLY FOR FEW SECONDS IN FLIGHT. STAGE OF FLIGHT WAS DESCENT, LANDING. REMOVED AND REPLACED SMOKE DETECTOR, OPS CHECK GOOD. (M)

Part: FUEL CAP — MISINSTALLED (LT WING) · airframe 12,054 hrs · 10,445 cycles

FUEL VENTED OUT L-WING ON TAKEOFF AFTER MANUAL OVERWING FUELING LANDED AT 48000 ORD MLW 47. LT FUEL CAP FOUND TO BE INSTALLED IMPROPERLY. INSTALLED LT WING FUEL CAP PROPERLY COMPLIED WITH OVERWEIGHT INSPECTION . NO DEFECTS NOTED. (K)

Part: PBE — DAMAGED (CABIN)

GALLEY PBE FALLING APART. REMOVED AND REPLACED FLIGHT ATTENDANT PBE WHOLE ASSEMBLY IAW 35-30-00. (M)

Part: GUIDE — WORN (TE FLAPS)

LEFT OUTBOARD FLAP MID BUTTE DOOR ROLLER GUIDE IS WORN, WS 235.843. S/D - REPAIRED LEFT OUTBOARD FLAP MID BUTE DOOR ROLLER GUIDE IAW BOMBARDIER INC REO 601R-57-53-019 REV NC.(M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND FS 280 LBL 9 OUTBOARD ANGLE CRACKED APPROX .9 INCH LONG IN RADIUS. REPLACED ANGLE IAW CRJ SRM 51-42-21 AND BRAS EO 601R-535992. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND FS 484 LBL 27 ANGLE CRACKED APPROX .30 IN RADIUS. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FS 484 LBL 36 INTERCOSTAL CRACKED APPROX .30 INCH RADIUS. REPLACED INTERCOSTAL IAW BOMBARDIER, IAW REO 601R-53-41-059 REV A AND BRAS STANDARD REPAIR 601R-53-00-30. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND FS 280 RBL 9 INBOARD ANGLE CRACKED APPROX .7 INCHES LONG IN RADIUS. REPLACED ANGLE IAW CRJ SRM 51-42-06 AND 51-42-21. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FS 280 LBL 9 INBOARD ANGLE CRACKED APPROX 1 INCH LONG IN RADIUS. REPLACED ANGLE IAW CRJ SRM 51-42-06 AND 51-42-21. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND FS 484 LBL 9 ANGLE CRACKED APPROX .40 INCH RADIUS. REPLACED ANGLE IAW BRAS EO 601R-53-5983. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUD FS 280 RBL 9 OUTBOARD ANGLE CRACKED APPROX .8 INCH LONG IN RADIUS. REPLACED ANGLE IAW CRJ SRM 51-42-21 AND BRAS EO 601R-53-8992. (M)

Part: SKIN — DENTED (TE FLAP)

RIGHT INBOARD FLAP OUTBOARD LOWER CORNER HAS A DENT .5 INCH BY 3 INCHES BY .080 INCHES. S/D REMOVED DAMAGED SECTION OF SKIN, FABRICATED REPAIR PARTS FROM 2024.T3.050, (WVAX PO NR 40777) 2024-T3.063 (WVAC PO NR 36153) AND 2024-T3.012 (WVAC PO NR 24116). INSTALLED REPAIR PARTS IAW CRJ 200 SRM 57-52-00 REPAIR 2. (M)

Part: ANGLE — CRACKED (FUSELAGE)

OBLIQUE ANGLE AT FS 625 IS CRACKED .25 INCH LONG, LEFT SIDE. REMOVED CRACKED OBLIQUE ANGLE AND INSTALLED NEW SERVICEABLE ANGLE IAW CRJ200SRM 51-42-06, P/N 601-35012-51. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND ANGLE CRACKED FS 484 AT RBL 27. REMOVED AND REPLACED ANGLE CLIP, IAW BOMBARDIER REO 601R-53-41-059. (M)

Part: ANGLE — CRACKED (FS)

FS 484 AT RBL 27 HAS A CRACKED ANGLE. REMOVED AND REPLACED ANGLE IAW BOMBARDIER REO 601R-53-41-059. (M)

Part: TRUNNION — CORRODED (MLG)

FOUND RIGHT MAIN LANDING GEAR, FORWARD TRUNNION, AFT BUSHING HAS PITTING ON FACE OF BUSHING. PERFORMED A MAJOR REPAIR TO PITTED RIGHT MAIN LANDING GEAR FORWARD TRUNNION AFT BUSHING BY REMOVING BUSHING AND INSTALLING 1ST OVERSIZE BUSHING P/N 601R-57-21-2003-41 IAW BOMBARDIER REO 601R-57-21-003 REV B. (M)

Part: BUSHING — CORRODED (LT MLG TRUNNION)

LEFT MAIN LANDING GEAR, FORWARD TRUNNION, AFT BUSHING HAS PITTING ON FACE OF BUSHING. PERFORMED A MAJOR REPAIR TO PITTED LEFT MAIN LANDING GEAR FORWARD TRUNNION AFT BUSHING BY REMOVING BUSHINGS AND INSTALLING 1ST OVERSIZE BUSHING P/N 601R-57-21-003-41, IAW BOMBARDIER INC REO 601R-27-21-003 REV B. (M)

Part: GEARBOX — DAMAGED (LT ENG THROTTLE) · airframe 9,285 hrs · 8,037 cycles

LT THRUST LEVER WHEN MOVED TO IDLE STOP SHUT OFF FUEL TO ENGINE. 2 INCH PLAY IN THRUST LEVER WITH NO ENGINE RESPONSE. REMOVED AND REPLACED THROTTLE CONTROL GEARBOX. OPS CHECK GOOD. IWA ENG SHOP MANAGER, REMOVED AND REPLACED NR 1 ENGINE THROTTLE GEARBOX IAW 76-11-17-400-801 C/W RIGGING AND SAFETIED T/R CABLE RIGGING REF 118912 NR 2.

Part: SKIN — DENTED (TE FLAP)

LEFT OUTBOARD FLAP HAS A DENT ON THE INBOARD SIDE OF THE FLAP VANE. REMOVED AND REPLACED DAMAGED LEFT OUTBOARD FLAP VANE, P/N 601R14571-7 IAW CRJ 200 SRM 51-42-11, 51-23-00, 51-25-16, 51-42-21 AND WVAC EO 601R-57-4088. (M)

Part: VANE — DENTED (TE FLAPS)

LT OUTBOARD FLAP HAS A DENT ON THE INBOARD SIDE OF THE FLAP VANE. REMOVED AND REPLACED DAMAGED LEFT OUTBOARD FLAP VANE P/N 601R14571-7 IAW 200 SRM 51-42-11, 51-23-00, 51-25-16, 51-42-21, AND WVAC EO 601R-57-4088. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

RIGHT SIDE UNDER FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 621 RBL 33, WL 73 DAMAGED STRUCTURE WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW REO 601R-53-61-004 REV B. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

RIGHT SIDE UNDER FLOORBEAM STRUCTURE IS CRACKED AT FS 621 RBL 33, WL 73 DAMAGED STRUCTURE WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW REO 601R-53-61-004 REV B. (M)

Part: WARNING LIGHT — FALSE INDICATION (PAX DOOR)

PAX DOOR WARNING AFTER TAKEOFF PLACARDED AND PLACED ON MEL 52-70-011. MAINTENANCE VERIFIED DOOR CLOSED AND LOCKED PROPERLY.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS)

FLAPS FAIL AT 14 DEGREES IN FLIGHT, COMPLIED WITH QRH AFTER LANDING, LEFT OUTBOARD FLAP IS TWISTED. REMOVED AND REPLACED NR 3 LEFT FLAP ACTUATOR. (M)