N781CA

Part: SKIN — CORRODED (RT WING) · airframe 40,769 hrs · 37,860 cycles

LOWER WING PLANK SKIN CUTOUT RH BOOST PUMP HAS MULTIPLE INDICATIONS NOTED AROUND ENTIRE CIRCUMFERENCE ON HORIZ LANDING FOR PNL AND VERTICAL SURFACES 50% FSH FAILED NDT INSP. C/W CARD REO 601R-57-21-2884 BLENDED CORROSION.

Part: BUSHING — FAILED (LT ELEVATOR) · airframe 40,769 hrs · 37,860 cycles

REF:CO# 7312618 JOB#7731265A OP#9 L/H ELEVATOR FAILED BEARING BACKLASH SYSTEM NO.1 AT .230 AND SYSTEM NO.3 AT .232, MAX LIMIT IS .210. C/A REPAIRED L/H ELEVATOR IAW EXPRESSJET EC/TC RIL#0183 AND BOMBARDIER RIL# 0183 REV B, DATED 01/24/2014. REPLACED BUSHINGS AND BEARINGS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,769 hrs · 37,860 cycles

AFT CABIN FLOORBEAM HAS CORROSION ON UPPER SURFACE FS 559.00 RBL 9.0. COMPLIED WITH EC/TC REO 601R-53-41-2379 AND GENERIC REO 601R-53-41-2379 DATED: 10/29/2018.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,769 hrs · 37,860 cycles

DENT FOUND AT FS 409+16 ON STR 16L APPROX L=2", W=1.5, D=.012". REPAIRED DENT AT FS 409+16 AT STR 16L IAW EA 30-2018-231 AND ECTC EA 30-2018-231 REV 0.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,769 hrs · 37,860 cycles

DENT AT FS 582 STR 22L APPROX L 1.7" W 1.0" D .015". REPAIRED DENT AT FS 582 STR 22L IAW EA 32-2018-225 AND ECTC EA 32-2018-225 REV 0.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,769 hrs · 37,860 cycles

LBL 27 UPPER FLOORBEAM CAP FROM FS 574 TO FS 621 IS CORRODED. REPAIRED UPPER FLOORBEAM CAP IAW REO 601R-53-61-6743 REV -, ECTC REO 601R-53-61-6743 REV 0, REO 601R-53-61-3778, AND ECTC REO 601R-53-61-3778 REV C.

Part: SIDEWALL SUPPORT — CORRODED (BS 559) · airframe 40,769 hrs · 37,860 cycles

LEFT CARGO SIDEWALL SUPPORT HAD CORROSION BS 559+83, LBL 36. REPAIRED THE SIDEWALL SUPPORT IAW SNIEO 601R31133-S04, AND SNIEO CC601R31133 S04.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,769 hrs · 37,860 cycles

AFT CARGO AREA HAS CORROSION BELOW FLOOR, FS 605.00, LBL 6.0 LOWER FRAME FLANGE. REMOVED AND REPLACED FRAME IAW SRM 51-40-11, 51-42-06, CC 601R36026 S01 AND EC/TC CC 601R36026 S01.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 40,769 hrs · 37,860 cycles

CABIN LEFT SIDE FLOOR SUPPORT HAD SIGNS OF CORROSION, BS 409 - 409+16 AND 409+110. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-00-530, REV A, EC/TC 601R-53-00-530, REV A, REO 601R-53-00-708 REV --, AND EC/TC REO 601R-53-00-708 REV --.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 40,769 hrs · 37,860 cycles

FS 621 BULKHEAD FWD FACE HAS DAMAGE AROUND FASTENER HOLE AT LBL44, 18" ABOVE FLOOR LEVEL. REPAIRED FS 621 BULKHEAD FWD FACE IAW REO 601R-53-61-2155 REV -A, DATED 2013-08-13 AND EC/TC REO 601R-53-61-2155.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 40,769 hrs · 37,860 cycles

FS 621 BULKHEAD FWD FACE HAS 1 LIGHT GOUGE AT LBL 14, 3" ABOVE FLOOR LEVEL AND APPROX. .5" LONG. REPAIRED FS 621 BULKHEAD FWD FACE IAW REO 601R-53-61-2155 REV -A, DATED 2013-08-13 AND EC/TC REO 601R-53-61-2155.

Part: NOT REPORTED — WORN (RT ELEVATOR) · airframe 40,769 hrs · 37,860 cycles

RT ELEVATOR FAILED BEARING BACKLASH SYSTEM NR 3 AT .285. MAX LIMIT IS .210. REPAIRED RT ELEVATOR IAW EC/TC RIL 0183 AND RIL 0183 REV B, DATED 01/24/2014.

Part: SKIN — CRACKED (RT WING) · airframe 40,769 hrs · 37,860 cycles

REF: CO# 7312618 JOB# 7731265 OP# 26: LOWER WING PLANK ACCESS HOLE HAS MULTIPLE INDICATIONS NOTED IN THE LANDING FOR PANEL 640AB AT FWD AND AFT AREA, BOTH AREAS ARE 4" LONG BY 0.250" WIDE BY 50% SCREEN HEIGHT. FAILS NDT. C/A: REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV L, DATED 2014-02-05 AND EXPRESSJET EC/TC EO600-57-81.

Part: SKIN — CRACKED (RT WING) · airframe 40,769 hrs · 37,860 cycles

REF: CO# 7312618 JOB# 7731265 OP# 25: LOWER WING PLANK ACCESS HOLE HAS MULTIPLE INDICATIONS NOTED IN THE LANDING FOR PANEL 650D B AT FWD AND AFT AREA, BOTH AREAS ARE 4" LONG BY 0.250" WIDE BY 50% SCREEN HEIGHT. FAILS NDT.C/A: REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV L, DATED 2014-02-05 AND EXPRESSJET EC/TC EO600-57-81.

Part: HINGE — WORN (RUDDER) · airframe 40,769 hrs · 37,860 cycles

RUDDER BACKLASH FAILED. SYSTEM NR 1 PCU AT 0.312" AND SYSTEM NO.3 PCU AT 0.340". BEARING FAILED AT 0.170". REPAIRED RUDDER SYSTEM BACKLASH IAW RIL'S 0602, 0392 AND EC/TC 0602 AND 0392. RUDDER BACKLASH PERFORMED IAW AMM 27-21-00-220-810. BACKLASH CHECK PASSED.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 40,769 hrs · 37,860 cycles

REF: CO 7312618 JOB 7731268 OP 30: LT AFT CARGO DOOR SILL CORRODED. C/A: REPAIRED LT AFT CARGO DOOR SILL IAW REO 601R-53-00-526 REV— DATED 22 MAY 2013 AND ECTC REO 601R-53-00-526.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,769 hrs · 37,860 cycles

REF: CO 7312618 JOB 7731265 OP 7022: FROM MX TRANS 17250131 DENT UNDER CARGO DOOR. COMPLIED WITH REO 601R-53-61-6255. COMPLY WITH LPI WITHIN 50FH, AND REINSPECT EVERY 300FH. PERMANENT REPAIR DUE IN 2800 FH BY TAT42138.8. ACCOMPLISH PERMANENT REPAIR PER REO 601R-53-61-6255. REINSPECT DUE EVERY 300FH. C/A: REPAIRED FUSELAGE SKIN AT FS682.00 BETWEEN STR20L - STR21L IAW REO 601R-53-61-6721 REV -- DATED 2018-09-23 AND EC/TC REO 601R-53-61-6721.

Part: SKIN — CHAFED (ZONE 100) · airframe 40,769 hrs · 37,860 cycles

REF: CO 7312618 JOB 7731261 OP 79: CENTER WING LOWER PLANK IS CHAFED AT LBL45 & RBL45 FROM CONTACT WITH BELLY FAIRING 193AB. C/A: COMPLIED WITH EC/TC REO 601R-57-21-880 IN ACCORDANCE WITH REO 601R-57-21-880 REV. D, DATED: 03/06/2017 AS WRITTEN.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 40,769 hrs · 37,860 cycles

REF: CO 7312618 JOB 7731268 OP 22: RT CARGO FLOOR SIDE SILL 559.00+80 TO FS 578.00, RBL 36.0 HAS CORROSION AROUND NUTPLATES. C/A: COMPLIED WITH EC/TC REO 601R-53-00-526 01 AND GENERIC REO 601R-53-00-526 REV. --, DATED: 05/22/2013 AS WRITTEN.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 40,769 hrs · 37,960 cycles

MAIN AVIONICS DOOR SURROUND STRUCTURE HAS CORROSION AT TWO FWD INTERCOSTALS LBL 2.0, RBL 2.0 AND ONE AFT INTERCOSTAL RBL 2.0 FS 364 - 394. FRAME STATION 280.00 FWD J ANGLE IS CORRODED. REMOVED AND REPLACED ONE AFT INTERCOSTAL RBL 2.0 FS 364 - 394 IAW SRM 51-42-06 AND 51-40-11 TEMP REV 51-42. FWD TWO INTERCOSTALS WERE REPAIRED IAW STS EA 32-2018-179, EA 32-2018-180 AND ECTC EA 32-2018-179, EA 32-2018-180.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 40,769 hrs · 37,860 cycles

CARGO FLOOR TRACKS AT FS 559.00+112 HAVE CORROSION, LBL 9.00 AND RBL 9.00. REMOVED AND REPLACED TRACKS IAW EC/TC REO 601R-53-00-485 AND GENERIC REO 601R-53-00-485 REV D, DATED 01/29/2018.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 40,769 hrs · 37,860 cycles

CARGO TRACKS CORRODED FS 559.00+90, LBL 9.0, RBL 9.0 AND RBL 27.00. REMOVED AND REPLACED TRACKS IAW EC/TC REO 601R-53-00-485 AND GENERIC REO 601R-53-00-00485 REV D, DATED 01/29/2018.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 40,769 hrs · 37,860 cycles

FRAME STATION 280.00 FWD J ANGLE IS CORRODED. INSTALLED NEW SERVICEABLE FWD J ANGLE IAW SRM 51-42-21, 51-42-06, 51-44-06, 51-25-16.

Part: BRACKET — CORRODED (ZONE 200) · airframe 40,769 hrs · 37,860 cycles

REF: CO 7312618 JOB 7731268 OP 16: PAX DOOR BRACKET AND CLEAT CORRODED AT FS 343.00, LBL 33. C/A: REMOVED AND REPLACED BRACKET IAW SRM 51-42-06, 51-42-11 AND 51-42-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,769 hrs · 37,860 cycles

REF: CO 7312618 JOB 7731261 OP 204: WALL SEAT TRACK ON RT SIDE FROM FS 449 TO FS 500 CORRODED. C/A: REMOVE, FABBED AND REPLACED SEAT TRACK IAW REO 601R-53-00-485.

Part: STRAP — CORRODED (FLOOR PANEL) · airframe 40,769 hrs · 37,860 cycles

REF: CO 7312618 JOB 7731261 OP 158: CORROSION ON FLOOR PNL STRAP AT LT AFT EDGE OF PRESSURE BOX AT FS 559.0. C/A: FABBED AND REPLACED STRAP IAW SRM 53-41-43, 51-40-11, 51-25-01 AND 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,769 hrs · 37,860 cycles

REF: CO 7312618 JOB 7731261 OP 205: WALL SEAT TRACK ON RT SIDE FROM FS 500 TO FS 545 CORRODED. C/A: REMOVE, FABBED AND REPLACED SEAT TRACK IAW REO 601R-53-00-485.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,769 hrs · 37,860 cycles

RT 484 FRAME O/B CLIP IS CRACKED. REPAIRED IAW REO 601R-53-41-2376 REV - DATE 2018-10-19.

Part: FLOOR SUPPORT — CORRODED (BS 518-527) · airframe 37,061 hrs · 33,819 cycles

LEFT CABIN FLOOR SUPPORT AND ANGLE BETWEEN BS 518 AND 527. REPAIRED THE FLOOR SUPPORT AND ANGLE IAW REO.

Part: STRUCTURE — BENT (A/C DOOR) · airframe 37,061 hrs · 33,819 cycles

FWD AND AFT LANDS FOR THE GROUND AIR CONDITIONING DOOR BENT. REPAIRED FWD AND AFT LANDS FOR THE GROUND AIR CONDITIONING DOOR IAW EA.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 37,061 hrs · 33,819 cycles

FLOORBEAM AT BS 349 BETWEEN RBL 27 AND 38 HAS CORROSION BEYOND LIMITS. REPAIRED THE FLOORBEAM IAW EA.

Part: ANGLE — CORRODED (CARGO DOORWAY) · airframe 37,061 hrs · 33,819 cycles

CARGO DOOR AFT LOWER ANGLE BEHIND COMBING IS CORRODED. THE ANGLE WAS REMOVED AND NEW ANGLE P/N: 600-35011-45 INSTALLED IAW SRM.

Part: BRACKET — CORRODED (BS 319) · airframe 37,061 hrs · 33,819 cycles

CORROSION ON LOWER FRAME BRACKET AT BS 319 STRINGER 17R. REMOVED AND REPLACED LOWER FRAME BRACKET IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 37,061 hrs · 33,819 cycles

L/H INBOARD FLAP CENTER VANE CAP CHAFED. REMOVED AND REPLACED THE VANE CAP IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 37,061 hrs · 33,819 cycles

RT INBOARD FLAP CENTER VANE CAP CHAFED. REMOVED AND REPLACED THE VANE CAP IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 37,061 hrs · 33,819 cycles

RIGHT SIDE FUSELAGE INTERIOR FLOOR SUPPORT AT BS 349 HAS CORROSION. REPAIRED THE FLOOR SUPPORT IAW EA.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 37,061 hrs · 33,819 cycles

RIGHT INBOARD FLAP OUTBOARD VANE CAP IS CHAFED. VANE CAP WAS REMOVED AND REPLACED IAW SRM.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 37,061 hrs · 33,819 cycles

PAX DOOR ENTRY THRESHOLD HAS CORROSION AT FWD AND AFT CUPS. INSTALLED FWD AND AFT PAX DOOR ENTRY THRESHOLD CUP IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 37,061 hrs · 33,819 cycles

LEFT SIDE INSIDE FUSELAGE AT BS 349, CORROSION ON FLOOR SUPPORT. REPAIRED THE FLOOR SUPPORT IAW EA.

Part: ANGLE — CORRODED (BS 319) · airframe 37,061 hrs · 33,819 cycles

GALLEY SERVICE DOOR THRESHOLD AT BS 319, ANGLE HAS CORROSION. REMOVED AND REPLACED THE ANGLE IAW SRM.

Part: PANEL — FAILED (HORIZONTAL STAB) · airframe 37,061 hrs · 33,819 cycles

HORIZONTAL STABILIZER VISOR PANEL 326AR FAILED GAP CHECK. REMOVED AND REPLACED IAW SRM.

Part: HOUSING — GOUGED (CARGO DOOR HANDL) · airframe 37,061 hrs · 33,819 cycles

EXTERNAL CARGO DOOR HANDLE HOUSING IS GOUGED. A NEW EXTERNAL CARGO DOOR HANDLE INSTALLED IAW AMM AND SRM. OPERATIONAL TESTS GOOD.

Part: SKIN — DENTED (MLG DOOR) · airframe 37,061 hrs · 33,819 cycles

TWO DENTS ON THE RT LANDING GEAR DOOR. DRESSED THE DENTS IAW STS EA.

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 36,273 hrs · 32,988 cycles

GEAR DISAGREE ON GEAR RETRACTION. OPEN

Part: STRUCTURE — CRACKED (BS 640) · airframe 34,407 hrs · 31,142 cycles

FOUND CRACKED AT BS 640, S9R CUT-OUT. REPAIRED IAW REO.

Part: LOOP — FAILED (RT MLG WW) · airframe 34,092 hrs · 30,821 cycles

RETURNED TO THE FIELD WITH AN ANTI-ICE DUCT WARNING MESSAGE. CHANGED THE RT WHEEL BIN LOOP. OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (NLG DOOR) · airframe 33,502 hrs · 30,220 cycles

NOSE DOOR NOT OPERATING PROPERLY, DID NOT OPEN WITH HYDRAULIC 3A ON. DID OPEN WHEN HYDRAULIC 3A WAS OFF AND PRESSURE DECREASED IN SYSTEM 3. SECURED LOOSE CONNECTOR ON NLG DOOR SELECTOR VALVE. OPS CHECK OF NLG GEAR DOORS GOOD AT THIS TIME IAW AMM.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 33,369 hrs · 30,078 cycles

PAX DOOR LOWER INNER SKIN DAMAGED. REPAIRED PAX DOOR INNER SKIN IAW EA.

Part: HINGE — GOUGED (PAX DOOR) · airframe 33,369 hrs · 30,078 cycles

PAX DOOR HINGE, ACFT SIDE, AFT LUG LAND IS GOUGED. REPAIRED PAX DOOR HINGE IAW EA.

Part: FLOORBEAM — DAMAGED (BS 618) · airframe 33,369 hrs · 30,078 cycles

BS 618, LBL 9, FLOORBEAM DAMAGED, ELONGATED HOLES. REMOVED AND INSTALLED NEW FLOORBEAM WEB, WEB DOUBLER, , AND FLOORBEAM ANGLE, IAW SRM.

Part: STOP — GOUGED (SEAT TRACK) · airframe 33,369 hrs · 30,078 cycles

PILOTS LT SEAT TRACK, SEAT STOP GOUGED. FOUND TO BE WITHIN LIMITS IAW REO.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 33,369 hrs · 30,078 cycles

CORROSION ON SEAT TRACK AT LBL 9 BS 409+118 - 559+10. R & R SEAT TRACK IAW AMM.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · airframe 33,369 hrs · 30,078 cycles

SERVICE DOOR THRESHOLD HAS CORROSION ON LOWER SIDE AROUND SCREW MOUNT HOLES. THRESHOLD VISIBLY OUT OF LIMITS. REPAIRED IAW SRM.

Part: BULKHEAD — CHAFED (AFT) · airframe 33,369 hrs · 30,078 cycles

AFT PRESSURE BULKHEAD REAR SIDE, VERTICAL STIFFENER AT BL 0 HAS CHAFE DAMAGE ON AFT FACE 12" FROM TOP. REPAIRED CHAFE DAMAGE IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,369 hrs · 30,078 cycles

RT INBD FLAP VANE L/E IS CHAFED IN THE OTBD AREA. BLENDED CHAFE AREA IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 33,369 hrs · 30,078 cycles

CORROSION RT FLOOR SUPPORT LBL 45 BS 559+1 5- 559+20. BLENDED AND TREATED CORROSION IAW REO.

Part: SKIN — DENTED (LT WING SPOILER) · airframe 33,369 hrs · 30,078 cycles

LT WING INBD GROUND SPOILER HAS A DENT ON LOWER SURFACE. DENT IS WITHIN LIMITS IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,369 hrs · 30,078 cycles

LT FLAP VANE IS CHAFED ON THE OTBD SIDE OF THE L/E. BLENDED CHAFE AREA IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,373 hrs · 30,083 cycles

LT INBD FLAP VANE CENTER AREA OF L/E CHAFED. C-CHECK RO: 06/22/2014, R & R LT INBD FLAP VANE CENTER L/E, PN 601R14303-51 IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 574) · airframe 33,369 hrs · 30,078 cycles

BS 574, LBL 45 FLOOR SUPPORT HAS CORROSION AT NUTPLATE LOCATIONS. BLENDED AND TREATED IAW REO.

Part: FITTING — CORRODED (BS 621 BULKHEAD) · airframe 33,369 hrs · 30,078 cycles

FS 621, LBL 9 BULKHEAD FITTING HAS CORROSION. R & R FITTING IAW SRM.

Part: SEAT TRACK — DAMAGED (BS 559) · airframe 33,369 hrs · 30,078 cycles

LBL 9 SEAT TRACK BETWEEN BS 559+10-559+80 HAS CORROSION. REMOVED AND INSTALLED DAMAGED SEAT TRACK IAW SRM.

Part: FLOORBEAM — CORRODED (BS 615) · airframe 33,369 hrs · 30,078 cycles

FS 615, RBL 9 FLOORBEAM UPPER CAP HAS CORROSION AT NUTPLATE LOCATIONS. REPAIRED FLOORBEAM IAW EA.

Part: FLOOR SUPPORT — CORRODED (BS 590) · airframe 33,369 hrs · 30,078 cycles

FLOOR SUPPORT CARGO ENTRY AREA, AT APPROXIMATE BS 590, LBL 45 HAS LIGHT SURFACE CORROSION BETWEEN NUTPLATES. FLOOR SUPPORT REPAIRED IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,369 hrs · 30,078 cycles

RT INBD FLAP VANE CENTER AREA OF L/E CHAFED IN CENTER AREA. R & R RT INBD FLAP VANE CENTER AREA OF L/E IAW SRM.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 33,369 hrs · 30,078 cycles

RBL 9, SEAT TRACK BETWEEN BS 559+10 - 559+80 CORRODED. REMOVED AND INSTALLED NEW SEAT TRACK IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,373 hrs · 30,083 cycles

LT INBD FLAP VANE, INBD SIDE CHAFED. BLENDED CHAFE AREA IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,369 hrs · 30,078 cycles

RT INBD FLAP VANE INBD L/E CHAFED. R & R RT INBD FLAP VANE L/E SKIN IAW SRM.

Part: FITTING — CORRODED (BS 621 BULKHEAD) · airframe 33,369 hrs · 30,078 cycles

FS 621, LBL 27 BULKHEAD FITTING HAS CORROSION. INSTALLED NEW FITTING IAW REO.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 33,373 hrs · 30,083 cycles

RT SEAT TRACK AT RBL 9, BS 409 - 409 + 120 HAS CORROSION. R & R SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 33,373 hrs · 30,083 cycles

LT SEAT TRACK AT LBL 9, BS 409 - 409+118 HAS CORROSION AT FASTENER LOCATIONS. C-CHECK, R & R SEAT TRACK IAW SRM.

Part: BRACKET — CRACKED (BS 484) · airframe 33,373 hrs · 30,083 cycles

BS 484, BRACKET CRACKED AT LBL 36. C-CHECK, R & R BRACKET IAW REO.

Part: BULKHEAD — CRACKED (BS 621) · airframe 33,373 hrs · 30,083 cycles

FS 621, BULKHEAD CRACKED AT LBL 36. C-CHECK, REPAIRED BULKHEAD IAW REO.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 33,373 hrs · 30,083 cycles

BS 621 BULKHEAD WEB HAS CRACK AT RBL 36. C-CHECK, REPAIRED BULKHEAD WEB IAW REO.

Part: BULKHEAD — CRACKED (BS 621) · airframe 33,373 hrs · 30,083 cycles

BS 621, BULKHEAD CRACKED RBL 18. C-CHECK, REPAIRED BULKHEAD IAW REO.

Part: ANGLE — CORRODED (BS 559) · airframe 33,373 hrs · 30,083 cycles

CORROSION ON SILL ANGLE AT BS 559, LBL45. BLENDED AND TREATED IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 33,373 hrs · 30,083 cycles

RT AILERON UPPER L/E FOUND CHAFED BEYOND LIMITS. R & R RT AILERON UPPER L/E SKIN IAW SRM.

Part: STRUCTURE — CHAFED (RT AILERON) · airframe 33,373 hrs · 30,083 cycles

RT AILERON UPPER L/E CHAFED. C-CHECK, RT AILERON LE REPLACED IAW SRM.

Part: HINGE — GOUGED (PAX DOOR) · airframe 33,373 hrs · 30,083 cycles

PASSENGER DOOR PIANO HINGE ON FUSELAGE SIDE, THIRD LUG FROM FRONT GOUGED. C-CHECK, BLENDED GOUGE IAW REO.

Part: STIFFENER — CRACKED (BS 409) · airframe 33,373 hrs · 30,083 cycles

BS 409 +128, VERTICAL POST AT LBL 18 ON INBD SIDE CRACKED. C-CHECK, REPLACED VERTICAL POST IAW SRM.

Part: STIFFENER — CRACKED (BS 409) · airframe 33,373 hrs · 30,083 cycles

BS 409+128, VERTICAL POST AT RBL 18 OTBD SIDE CRACKED. C-CHECK, REPLACED VERTICAL POST IAW SRM.

Part: SKIN — DENTED (BS 409) · airframe 33,373 hrs · 30,083 cycles

DENT FOUND ON LT FUSELAGE, BS 409.13, WL 78.5. C-CHECK, REPAIRED SKIN IAW EA.

Part: THRUST REVERSER — OBSTRUCTED (RIGHT) · airframe 32,959 hrs · 29,679 cycles

RIGHT THRUST LEVER STUCK AT 81 PERCENT N1 IN CRUISE FLIGHT. T/L CAN BE PUSHED HIGHER BUT NOT LOWER. HAD TO SHUT DOWN RT ENG INFLIGHT TO LAND THE ACFT USING FIRE PUSH SWITCH. T/L STUCK AT 12 O'CLOCK POSITION. FOUND TOOL JAMMED BETWEEN FCU INPUT LEVER AND OIL LINE. REMOVED TOOL.

Part: BRACKET — BENT (NLG) · airframe 32,680 hrs · 29,400 cycles

NOSE DOOR OPEN WARNING FOLLOWED BY GEAR DISAGREE WARNING. COMPLIED WITH QRH, LG RETURNED DOWN. FLT 4548 REPLACED BENT NLG PROX SENSOR BRACKET PN 16215-105, PERFORMED NLG SWINGS. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 31,769 hrs · 28,468 cycles

STRONG FUEL OR EXHAUST SMELL COMING THROUGH THE GASPERS & PACK WHILE ON ENGINE BLEEDS & WORSE DURING DESCENT. FLT#4498 R&R BOTH ACMS IAW AMM. PN ON/OFF 782790-15, SN ON 200312046, SN OFF 200009183, PN ON/OFF 782790-15, SN ON 200012116 & SN OFF 200402113.

Part: O-RING — DAMAGED (HYDRULIC SYS) · airframe 31,470 hrs · 28,170 cycles

HYDRAULIC 2, LOW PRESS CAUTION. QTY INDICATED 5 PERCENT, HYD PUMP 2B CAUTION AND EDP 2A CAUTION FOLLOWED. REPLACED O-RINGS ON NR 2 ACMP LINE, LEAK CHECKED OK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,828 hrs · 27,524 cycles

EMERGENCY OVERHEAD LIGHT ROW 2 BURNED OUT. (FLT 4848) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,738 hrs · 27,428 cycles

OVERHEAD EMERGENCY LIGHT ABOVE F/A JUMPSEAT IS BURNED OUT. (FLT 4830) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,178 hrs · 26,874 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4803) RELAMPED EMERGENCY LIGHT.

Part: STRAP — CORRODED (FUSELAGE) · airframe 29,976 hrs · 26,684 cycles

CROSS SECTIONAL FLOOR STRAP AT FS 559 FROM RBL 27 TO RBL 45 HAS CORROSION. (C-CHECK) REPLACED STRAP AT FS 559.0 FROM RBL 27 TO RBL 45 IN REFERENCE TO CRJ 200 SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,976 hrs · 26,684 cycles

FRAME FS 310.00 HAS CORROSION FORWARD SIDE OF FRAME AND LEG AT SKIN ATTACH AREA STRINGER 27 TO 26L. (C-CHECK) REPLACED THE FRAME AT FS 310.00 AT STRINGERS 26L & 27L AS PER REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,976 hrs · 26,684 cycles

FLOORBEAM CORRODED UNDER FLOORBOARD AT FS 349.00 STRINGER 17L. (C-CHECK) REPAIRED FLOORBEAM IN ACCORDANCE WITH REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,976 hrs · 26,684 cycles

FRAME FS 319.70 IN AVIONICS BAY HAS CORROSION FORWARD SIDE OF FRAME AND LEG AT SKIN ATTACH AREA STRINGER 27 TO 26L. (C-CHECK) REPLACED FRAME AT APPROXIMATELY FS 319.7 STRINGER 27 TO 26L IN REFERENCE TO CRJ 200 SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 29,976 hrs · 26,684 cycles

CRACK ON FS 409.0+128 VERTICAL POST INBOARD AFT RADIUS AT RBL 18.00 WL 69.00. (C-CHECK) REPLACED VERTICAL POST AT FS 409.0+128.0 RBL 18.0 INBOARD PER REO.

Part: POST — CRACKED (FUSELAGE) · airframe 29,976 hrs · 26,684 cycles

CRACK ON FS 409.0+128 VERTICAL POST OUTBOARD AFT RADIUS AT LBL 18.00 WL 69.00. (C-CHECK) REPLACED OUTBOARD POST AT FS 409.0 +128 PER CRJ 200 REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,940 hrs · 26,648 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4846) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,822 hrs · 26,532 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4604) RELAMPED EMERGENCY LIGHT.

Part: COMPUTER — FAILED (AUTOPILOT SYS) · airframe 29,614 hrs · 26,261 cycles

RECEIVED AP TRIM IS RWD CAUTION MESSAGE AND AIRPLANE MADE AN ABRUPT TURN. (FLT 4829) REPLACED FCC NR 1, FCC NR 2, AHRS NR 1, AND AHRS NR 2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,549 hrs · 26,193 cycles

RIGHT FORWARD OVERWING EMERGENCY LIGHT IS OUT. (FLT 4531) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,549 hrs · 26,193 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4732) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,168 hrs · 25,831 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4534) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,777 hrs · 25,434 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4619) RELAMPED EMERGENCY LIGHT.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 28,656 hrs · 25,308 cycles

ANGLE BRACKET IS CRACKED ON FORWARD FACE OF FS 621 PRESSURE BULKHEAD JUST BELOW THE DOOR TRACK SUPPORT BEAM. (SERVICE) REPLACED BRACKET ON FORWARD FACE OF FS 621 PRESSURE BULKHEAD JUST BELOW THE CARGO DOOR SUPPORT BEAM PER SRM.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 27,048 hrs · 23,761 cycles

ON APPROACH INTO XNA RECEIVED GEAR DISAGREE WARNING MSG. BOTH MLG INDICATED UP, NLG INDICATED DOWN. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED MLG SELECTOR VALVE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,631 hrs · 23,369 cycles

CARGO FLOOR SUPPORT AT LBL 27 FROM FS 570-621 CORRODED BEYOND LIMITS. REMOVED AND REPLACED CARGO FLOOR SUPPORT LBL 27 JUST FWD OF THE AFT BULKHEAD IAW SRM 51-42-21 AND BOMBARDIER REO 601R-57-61-3815.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,632 hrs · 23,370 cycles

FS 559 CAP ANGLE CRACKED AT RBL 18. CUT OUT DAMAGED AREA AND INSTALLED NEW CAP ANGLE SECTION IAW TASK CARD, REO 601R-53-41-260 RT REP.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,631 hrs · 23,369 cycles

AT FS 621.00 (FWD SIDE OF REAR PRESSURE BULKHEAD), THERE ARE THREE AREAS AROUND THE LINTEL FITTING THAT ARE CRACKED. REPAIRED FS 621.00 PRESSURE BULKHEAD AT THE LINTEL FITTING IAW BOMBARDIER REO 601R-53-61-1230 REV D, DATED JULY 19-2006.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,632 hrs · 23,370 cycles

FORWARD PRESSURE BULKHEAD IS CRACKED AT THE PARKING BRAKE CABLE FITTING. REPAIRED IAW REO 601R-53-11-563 AND REO 601R-53-11-1968.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,632 hrs · 23,370 cycles

CRACK ON FORWARD SIDE OF AFT PRESSURE BULKHEAD AT FS 621.00 ON LBL 27.50 JUST ABOVE WL 120.43 AND JUST BELOW THE CARGO DOOR TRACK. REPAIRED AFT PRESSURE BULKHEAD IAW REO 601R-53-61-1541.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,632 hrs · 23,370 cycles

CRACK ON FORWARD SIDE OF AFT PRESSURE BULKHEAD AT FS 621.00 ON LBL 27.50 AT THE TOP END OF THE CARGO DOOR TRACK. REPAIRED AFT PRESSURE BULKHEAD IAW REO 601R-53-61-154.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,632 hrs · 23,370 cycles

CRACK ON LEFT FRAME CAP ANGLE AT FS 559.00 LBL 18.00. REPAIRED FS 559 CAP ANGLE IAW REO 601R-53-41-260 LT REPAIR.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,631 hrs · 23,369 cycles

BULKHEAD WEB CRACKED AROUND LINTEL ATTACH FITTING AT FS 621, LBL 36.2. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1230 REV D.

Part: A/C PACK — SMOKE (LEFT) · airframe 26,329 hrs · 23,094 cycles

ON CLIMBOUT FROM MKE SMOKE IN COCKPIT AND CABIN COMING FROM PAC'S, (DETERMINED TO BE LEFT PAC). EMERGENCY DECLARED, A/C RETURNED TO MKE AND LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 21-51-01-2.

Part: SELECTOR VALVE — FAULTY (NLG) · airframe 24,471 hrs · 21,550 cycles

RECEIVED NOSE GEAR DISAGREE WARNING MSG ON APPROACH INTO BOS. EMERGENCY DECLARED, PERFORMED QRH A/C LANDED SAFELY. REMOVED AND REPLACED NLG SELECTOR VALVE.

Part: SKIN — DAMAGED (LT WING) · airframe 23,388 hrs · 20,640 cycles

FUEL DRAIN INSIDE FUEL ACCESS PANELS 510AB FWD AND AFT DRAIN ATTACH HOLES ARE DAMAGED. REAMED AND INSTALLED SERVICEABLE FREEZE PLUGS AT FUEL DRAIN FWD AND AFT ATTACH HOLES PER COMAIR EA 10-5721-02382.

Part: FRAME — CRACKED (FS 640) · airframe 23,388 hrs · 20,640 cycles

LT FS 640 FRAME DOUBLER AND BONDED SKIN DOUBLER ARE CRACKED. REMOVED DAMAGED PARTS AND COMPLIED WITH MODIFICATION K601R36009-3 ON LT FS 640 FRAME AND DOUBLER PER S/B601R-53-061 KIT DRWG. K601R36009 REV B, 601R-53-61-506 REV C AMD 601R53-61-569.

Part: SKIN — DAMAGED (RT WING) · airframe 23,388 hrs · 20,640 cycles

FUEL DRAIN FWD OF ACCESS PANELS 640AB AFT DRAIN ATTACH HOLE IS DAMAGED. REAMED AND INSTALLED FREEZE PLUG AT FUEL DRAIN AFT ATTACH HOLE PER COMAIR EA NR 10-5721-02382.

Part: SKIN PANEL — CRACKED (FS 559 RBL 9-18) · airframe 23,388 hrs · 20,640 cycles

FS 559 WEB RT SIDE IS CRACKED BY AILERON BELLCRANK UPPER O/B BOLT HOLE. REMOVED DAMAGE AND INSTALLED A PERMANENT REPAIR DOUBLER ON FS559 BULKHEAD WEB BETWEEN RBL9 AND RBL18.

Part: FLOORBEAM — CRACKED (FS 280) · airframe 23,388 hrs · 20,640 cycles

FS 280 FLOOR ANGLE 600-34017-595 IS CRACKED AT LBL9 IN THE LWR FLANGE. CUT OUT DAMAGE AND INSTALLED PERMANENT REPAIR DOUBLER PER REO 601R-53-11-171.

Part: SKIN — DAMAGED (RT WING) · airframe 23,388 hrs · 20,640 cycles

FUEL DRAIN FWD OF ACCESS PANELS 640AB AFT DRAIN ATTACH HOLE IS DAMAGED. REAMED AND INSTALLED FREEZE PLUG AT FUEL DRAIN AFT ATTACH HOLE PER COMAIR EA NR 10-5721-02382.

Part: SKIN — DAMAGED (RT WING) · airframe 23,388 hrs · 20,640 cycles

FUEL DRAIN FWD OF ACCESS PANELS 610AB FWD AND AFT DRAIN ATTACH HOLES ARE DAMAGED. REAMED AND INSTALLED FREEZE PLUGS AT FUEL DRAIN FWD AND AFT ATTACH HOLES PER COMAIR EA NR 10-5721-02382.

Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 21,833 hrs · 19,416 cycles

FLIGHT 5676 - DURING CLIMBOUT, LANDING GEAR HANDLE WOULD NOT MOVE TO RAISE THE GEAR. AIRCRAFT RETURNED BACK TO DCA AND LANDED SAFELY. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 21,196 hrs · 18,915 cycles

FLIGHT 5670 - FLAPS FAIL MESSAGE WHEN SELECTING 8 TO 20 DEGREE FLAPS. AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 19,830 hrs · 17,828 cycles

FLIGHT 5374 - LEFT WINDSHIELD CRACKED AND ARCED. RETURNED TO AIRPORT. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED LEFT WINDSHIELD.

Part: WARNING SYSTEM — MALFUNCTIONED (PAX DOOR) · airframe 19,550 hrs · 17,601 cycles

FLIGHT 5460 - PAX DOOR LATCH CAUTION MESSAGE RECEIVED AT 6000 FT. RAN QRH PRESS NORMAL. CONTINUED PER QRH RECEIVED PAX DOOR WARNING AT 10,500 FT. AIRCRAFT RETURNED BACK TO DSM AND LANDED SAFELY. INSPECTED AND PERFORMED OPS CHECK OF PAX DOOR AND WARNING SYSTEM, NO DEFECTS NOTED.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 18,995 hrs · 17,156 cycles

FLIGHT 4943 - EMERGENCY LIGHTS ZONE NR 2 INOP. REMOVED AND REPLACED BATTERY PACK.

Part: WINDOW — CRACKED (COCKPIT) · airframe 18,855 hrs · 17,051 cycles

FLIGHT 9484 - EN ROUTE CVG-CXO THE RIGHT SIDE WINDOW CRACKED, FLIGHT RETURNED TO CVG. REPLACED THE RIGHT SIDE WINDOW.

Part: COALESCER BAG — DIRTY (CABIN AIR) · airframe 18,083 hrs · 16,454 cycles

FLIGHT 4959 - DURING CLIMB-OUT OF CVG, THE CABIN AND COCKPIT HAD A STRONG ODOR ASSOCIATED WITH HAZE IN CABIN, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT AND RIGHT COALESCER SOCKS.

Part: FLAP — MALFUNCTIONED (WING) · airframe 17,591 hrs · 16,030 cycles

FLIGHT 5331 - DURING START UP AT MSP RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: WARNING LIGHT — FALSE ACTIVATION (COOLING FAN) · airframe 17,193 hrs · 15,701 cycles

FLIGHT 5007 - DISPLAY COOL CAUTION. INSPECTED AND FOUND NO DEFECTS. SYSTEM OPERATION CHECK SATISFACTORY.

Part: CONTROLLER — MALFUNCTIONED (DETECTION SYS) · airframe 15,818 hrs · 14,542 cycles

RT JET PIPE OVERHEAT AND APU FIRE FAIL CAUTION. CREW DECLARED EMERGENCY AND SHUTDOWN RT ENGINE. ACFT LANDED WITHOUT INCIDENT. REPLACED FIRE OVERHEAT CONTROLLER.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 13,716 hrs · 12,695 cycles

FLIGHT 5908 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 13,692 hrs · 12,679 cycles

FLIGHT 5890 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT. IAW AD 98-20-01.

Part: SERVICE DOOR — OPEN (OXYGEN SYS) · airframe 12,444 hrs · 11,727 cycles

FLIGHT 5609 STALL FAIL WARNING AND LOUD WHINING NOISE. THE 02 SERVICE DOOR WAS OPEN, REPAIRED DOOR AND SECURED CLOSED.

Part: COWLING — SEPARATED (RT ENGINE) · airframe 12,174 hrs · 11,510 cycles

FLIGHT 5892 RT ENGINE COWLING SEPARATED FROM AIRCRAFT AFTER T/O. REPAIRED AND REPLACED ENGINE COWLING.

Part: WARNING LIGHT — ILLUMINATED (ANTI SKID SYS) · airframe 11,904 hrs · 11,309 cycles

FLIGHT 5049 ANTI SKID MESSAGE DURING T/O. DEFERRED MAINTENANCE ON ANTI SKID IAW MEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,180 hrs · 10,724 cycles

FLIGHT 5215 CEILING EMERGENCY LIGHT, 2ND FROM FRONT IS INOPERATIVE. DEFERRED INOPERATIVE EMERGENCY LIGHT PER MEL 33-51-01.

Part: FIRE BOTTLE — DISCHARGED (CARGO BAY) · airframe 11,113 hrs · 10,664 cycles

FLIGHT 5133 CARGO FIRE BOTTLE LOW MESSAGE. REPLACED THE RT CARGO FIRE BOTTLE.

Part: PRESSURE SWITCH — MALFUNCTIONED (APU) · airframe 10,395 hrs · 10,073 cycles

FLIGHT 5254 APU LOW OIL PRESSURE CAUTION MESSAGE. REPLACED THE APU LOW OIL PRESSURE SWITCH.

Part: FRAME — CRACKED (FUSELAGE) · airframe 10,235 hrs · 9,951 cycles

FRAME ANGLE AT FS 718 CRACKED. COMPLIED WITH EA 10-5320-00236 AND S/B 601R-53-055 PART C.

Part: FRAME — CRACKED (FUSELAGE) · airframe 10,235 hrs · 9,951 cycles

FRAME ANGLE AT FS 718 CRACKED. COMPLIED WITH EA 10-5320-00236 AND S/B 601R-53-055 PART B.

Part: VALVE — DEFECTIVE (LEFT ENGINE) · airframe 9,653 hrs · 9,470 cycles

FLIGHT 5485 RECEIVED A LEFT ENGINE COWL ANTI-ICE CAUTION DURING TAKE OFF ROLL, AIRCRAFT RETURNED TO THE GATE. REPLACED THE LEFT ENGINE ANTI-ICE VALVE.

Part: PSEU — MALFUNCTIONED (AVIONICS) · airframe 9,159 hrs · 9,044 cycles

FLIGHT 5761 GEAR DISAGREE WARNING, NLG FAILED TO EXTEND.REPLACED THE PSEU.

Part: PRIORITY VALVE — MALFUNCTIONED (MLG) · airframe 9,153 hrs · 9,040 cycles

FLIGHT 5662 GEAR DISAGREE WARNING, "NLG" DID NOT EXTEND.REPALCED THE "MLG" PRIORITY VALVE.

Part: DEBRIS MONITOR · airframe 8,796 hrs · 8,720 cycles

FLIGHT 5376 STAB TRIM AND MACH TRIM CAUTION MESSAGE.CLEANED DEBRIS FROM STAB TRIM ENGAGE SWITCH.

Part: BATTERY — DISCHARGED (CABIN) · airframe 8,700 hrs · 8,643 cycles

FLIGHT 5203 R/H EMERGENCY WING LIGHT IS INOP.REPLACED THE #2 EMERGENCY BATTERY.

Part: ACTUATOR — MALFUNCTIONED (IMBOARD FLAP) · airframe 7,872 hrs · 7,913 cycles

FLAPS FAILED AT 36 DEGREES.REPLACED ALL FOUR INBOARD FLAP ACTUATORS.

Part: BPSU — MALFUNCTIONED (T/E FLAP) · airframe 7,870 hrs · 7,911 cycles

FLAPS FAILED AT 40 DEGREES. REPLACED THE RIGHT BRAKE AND POSITION SENSOR UNIT.

Part: BPSU — FAILED (T/E FLAP) · airframe 7,866 hrs · 7,906 cycles

FLAPS FAILED AT 30 DEGREES. REPLACED THE RIGHT BRAKE AND POSITION SENSOR UNIT.

Part: BPSU — FAILED (T/E FLAP) · airframe 7,866 hrs · 7,906 cycles

FLAPS FAILED AT 30 DEGREES. REPLACED THE RIGHT BRAKE POSITION UNIT.

Part: BPSU — FAILED (L/H) · airframe 7,858 hrs · 7,900 cycles

FLIGHT 5237 FLAPS FIALED AT 41 DEGREES.REPLACED THE L/H BPSU.

Part: FLAP · airframe 7,856 hrs · 7,898 cycles

FLIGHT 5962 - FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.

Part: LAMP — BURNED OUT (WING) · airframe 5,424 hrs · 5,520 cycles

FLIGHT #5324 L/H FWD OVERWING EMERGENCY LIGHT IS INOP.REPLACED LIGHT BULB.

Part: COMPUTER — MALFUNCTIONED (AVIONICS) · airframe 5,373 hrs · 5,466 cycles

FLIGHT #5559 CONFIG AILERON WARNING, T/O ABORTED.REPLACED THE #2 DCU.

Part: CONTROL UNIT · airframe 4,838 hrs · 4,914 cycles

DURING TAKE OFF CONFIG SPOILERS MESSAGE ACTIVATED AT 40 KNOTS, ABORTED TAKE OFF AND RETURNED TO GATE.PERFORMED RESET OF THE SPOILER ELECTRONIC CONTROL UNIT.

Part: WARNING SYSTEM — FALSE ACTIVATION (AILERONS) · airframe 3,448 hrs · 3,533 cycles

AILERON CONFIG WARNING DURING T/O. INSPECTED AILERONS AND TRIM SYSTEM, NO DEFECTS FOUND.

Part: AFCS — MALFUNCTIONED (FLIGHT CONTROLS) · airframe 3,377 hrs · 3,452 cycles

UNCOMMANDED YAW DURING FLIGHT, A/P ON OR OFF. COULD NOT DUPLICATE. INSPECTED FLIGHT CONTROLS. NO FAULTS FOUND.

Part: WHEEL — CRACKED (MLG) · airframe 2,297 hrs · 2,398 cycles

MECHANIC REMOVED WHEEL ASSEMBLY FROM AIRCRAFT DUE TO TIME CHANGE. DURING CLEANING OF THE WHEEL AT CVG FOUND SPOKE WAS CRACKED APPROXIMATELY 3 INCHES LONG. THIS WHEEL ASSY HAS BEEN REMOVED FROM SERVICE. 27 TOTAL TIRE CHANGES 4248 TOTAL LANDINGS.

Part: UNKNOWN — ODOR (CABIN)

STRONG FUEL ODOR IN AIRCRAFT. INSPECTED FOR FUEL LEAKS, NON FOUND. COULD NOT DUPLCIATE.

Part: LINK — DISCONNECTED (NLG)

LANDING GEAR DISAGREE WARNING. NLG TORQUE LINKS NOT CONNECTED. CONNECTED TORQUE LINKS AND RETRACT CHECKS NORMAL.

Part: PIN — SHEARED (PAX DOOR)

CREW REPORTED MAIN CABIN DOOR IS VERY HARD TO OPEN AND THAT DOOR HANDLE SEEMS TO GET STUCK WHEN PULLING UPWARD ON HANDLE. WHILE TROUBLESHOOTING THE DOOR HANDLE (P/N 600-31887-11 ITEM NR 5 PAGE 1 FIG 1 RJ IPC CH 52-11-02) FOUND THE PIN (HSP 115BO94-900 ITEM NR 185 IN THE RJ CMM PG 1010 CHAP 52-11-03) FOR THE FLUSH HANDLE LATCH ASSEMBLY TO BE SHEARED, CAUSING THE HANDLE ASSEMBLY TO BIND UP.