N418SW

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 40,813 hrs · 34,514 cycles

RECEIVED A RIGHT WINDSHIELD HEAT CAUTION - RIGHT WINDSHIELD CRACKED. RAN QRH AND MANUALLY CONTROLLED PRESSURIZATION, HOWEVER THE NUMBERS WERE TOO HIGH IN THE CABIN. DECLARED AN EMERGENCY AND DID A QUICK DESCENT AND DIVERTED. (FLT 4668) FO: 12/28/2017 CLOSED. REMOVED AND REPLACED WINDSHIELD IAW AMM.

Part: SKIN — CHAFED (BS 529-554) · airframe 37,606 hrs · 30,981 cycles

RIGHT APRON SKIN HAS CHAFING BETWEEN BS 529 - 554 AT WL 51-58. REPAIRED IAW REO.

Part: PANEL — CORRODED (PAX DOOR) · airframe 37,606 hrs · 30,981 cycles

DOOR PANEL 832BR HAS CORROSION AROUND THE FASTENER HOLES. REPLACED PAX DOOR PANEL 832BR IAW SRM.

Part: SKIN — DENTED (BS 640) · airframe 37,606 hrs · 30,981 cycles

SKIN DENTED LOCATED EIGHT INCHES AFT OF BS 640 BETWEEN STRINGERS 22 - 23R. PERFORMED PERMANENT REPAIR, SECTION 1 IAW EA.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 37,606 hrs · 30,981 cycles

RIGHT INBD FLAP VANE CHAFED AT CENTER L/E CAP. REPLACED RT INBD FLAP VANE CENTER CAP IAW SRM AND STS EA.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 37,606 hrs · 30,981 cycles

AFT 621 BULKHEAD ISOLATOR CRACKED. R & R THE ISOLATOR IAW SRM.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 37,606 hrs · 30,981 cycles

ISOLATOR CRACKED ON FWD SIDE OF FS 621. R & R THE ISOLATOR, AT FS 621, LBL 27 IAW SRM.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 37,606 hrs · 30,981 cycles

RIGHT TRU FLOOR CRACK AT FS 193.00. COMPLIED WITH PERMANENT REPAIR, TYPE II, OF RT TRU FLOOR IAW REO.

Part: FILTER — CONTAMINATED (LEFT) · airframe 37,522 hrs · 30,891 cycles

LT PACK HI TEMP FOLLOWED BY SMOKE TOILET MESSAGE. R & R LT PRSOV FILTER IAW CMM. OPS CHECK GOOD.

Part: FAN — SMOKE (LAVATORY) · airframe 37,441 hrs · 30,806 cycles

RETURN TO FIELD FOR SMOKE IN THE LAV. R & R LAVATORY EXHAUST FAN IAW AMM. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 35,454 hrs · 28,789 cycles

EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. CHARGED BATTERIES AND ALL EMERGENCY LIGHTS ILLUMINATE NORMALLY.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 34,928 hrs · 28,282 cycles

BOTTOM LEFT INTERIOR EMERGENCY LIGHT INOPERATIVE. REPAIRED A LOOSE CONNECTION.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 34,383 hrs · 27,764 cycles

RT OVERWING EMERGENCY LIGHT NR 6 INOPERATIVE. R & R RT OVERWING EMERGENCY LIGHT NR 6 IAW AMM.

Part: OVERHEAT SENSOR — FAILED (RT WING) · airframe 34,364 hrs · 27,745 cycles

DURING CLIMB OUT, RECEIVED A RT WING OVERHEAT MESSAGE. COMPLIED WITH QRH AND RETURNED TO DEPARTURE. R & R RT WING OVERHEAT SENSOR AND CONTROL SENSOR WITH SERVICEABLE UNITS IAW AMM.

Part: STRUCTURE — CRACKED (APU BAY) · airframe 34,108 hrs · 27,488 cycles

THE APU ENCLOSURE CRACKED ALONG SIDE THE WELD DURING INSTALLATION. C-CHECK, WELDED CRACK ON APU ENCLOSURE IAW REO.

Part: STRUCTURE — DELAMINATED · airframe 34,108 hrs · 27,488 cycles

L/E PANEL 630KL HAS SEPARATION OF THE SHROUD TO L/E SKIN. DELAMINATION. C-CHECK, REBONDED SEPARATION OF THE SHROUD TO L/E SKIN IAW REO.

Part: STRUCTURE — DELAMINATED · airframe 34,108 hrs · 27,488 cycles

L/E PANEL 630JL HAS SEPARATION OF THE SHROUD TO L/E SKIN, DELAMINATION. C-CHECK, REBONDED SEPARATION OF THE SHROUD TO L/E SKIN IAW REO.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 34,108 hrs · 27,488 cycles

LEFT INBD FLAP INSIDE PANEL 584CB GOUGE IN SKIN IN BETWEEN ACTUATOR FITTING. C-CHECK, BLENDED GOUGE SMOOTH IAW REO.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 34,108 hrs · 27,488 cycles

LEFT INBD FLAP INSIDE PANEL 584AB GOUGE IN SKIN IN BETWEEN ACTUATOR FITTING. C-CHECK, BLENDED GOUGE SMOOTH IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 34,108 hrs · 27,488 cycles

RIGHT INBD FLAP VANE L/E CENTER CAP CHAFED BEYOND PERMANENT LIMITS. C-CHECK, REPLACED RT INBD FLAP VANE L/E CENTER CAP IAW SRM.

Part: STIFFENER — CRACKED (BS 473.15) · airframe 34,108 hrs · 27,488 cycles

RT SIDE OUTER FUSELAGE VERTICAL STIFFENER HAS CRACK AT FS 473.15. C-CHECK, REMOVED AND INSTALLED NEW VERTICAL STIFFNER IAW SRM.

Part: STIFFENER — CRACKED (BS 461) · airframe 34,108 hrs · 27,488 cycles

OUTSIDE FUSELAGE VERTICAL STIFFENER HAS CRACK AT RADIUS AT BS 461, RT SIDE. C-CHECK, R & R VERTICAL STIFFENER IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 34,108 hrs · 27,488 cycles

RT WING INBD FLAP VANE CHAFED ON INBD L/E. C-CHECK, BLENDED RT WING INBD FLAP VANE CHAFE ON INBD L/E IAW REO.

Part: LEVER — CHAFED (PAX DOOR) · airframe 34,108 hrs · 27,488 cycles

PAX DOOR FORWARD PULL IN LEVER IS CHAFED. C-CHECK, REMOVED CHAFE ON PAX DOOR PULL IN LEVER IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 34,108 hrs · 27,488 cycles

LT AILERON HAS CHAFING ON UPPER L/E SHROUD IN VARIOUS AREAS. C-CHECK, CHAFED LT AILERON UPPER L/E WAS BLENDED IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 34,108 hrs · 27,488 cycles

RT WING INBD FLAP VANE CHAFED ON OTBD L/E. C-CHECK, R & R WITH NEW RT WING INBD FLAP VANE OTBD FLAP VANE SKIN IAW SRM.

Part: STRUCTURE — CHAFED (RT MLG DOOR) · airframe 34,108 hrs · 27,488 cycles

RT MLG DOOR, THE INBD FWD CORNER OF INNER DOOR BY THE BRUSH ASSY HAS CHAFING. C-CHECK, REPAIRED IAW REO AND SRM.

Part: BELLCRANK — CHAFED (RT MLG DOOR) · airframe 34,108 hrs · 27,488 cycles

RIGHT MLG DOOR, WING TO BELL CRANK ASSY LEVER/ARM, THE FWD ATTACH POINT HAS CHAFING. C-CHECK, BLENDED CHAFING ON RT MLG DOOR, WING TO DOOR BELLCRANK ASSY LEVER ARM, FWD ATTACH POINT IAW REO.

Part: STRUCTURE — CHAFED (LT MLG DOOR) · airframe 34,108 hrs · 27,488 cycles

LEFT MLG DOOR, THE INBD FWD INNER CORNER BY THE BRUSH ASSY HAS CHAFING. C-CHECK, REPAIRED IAW REO AND SRM.

Part: PANEL — CHAFED (UNKNOWN) · airframe 34,108 hrs · 27,488 cycles

CHAFE ON PANEL 599BB. C-CHECK, BLENDED CHAFED AREA ON PANEL 599BB IAW REO.

Part: ARM — CHAFED (LT MLG DOOR) · airframe 34,108 hrs · 27,488 cycles

LEFT MLG DOOR, THE WING TO DOOR BELLCRANK LEVER/ARM HAS CHAFING ON LOWER AFT SECTION. C-CHECK, BLENDED CHAFING ON LT MLG DOOR, WING TO DOOR BELLCRANK LEVER ARM LOWER AFT SECTION IAW REO.

Part: RIB — CRACKED (LT WING) · airframe 34,108 hrs · 27,488 cycles

LT WING BATTERY RIB HAS CRACK AT UPPER EDGE. C-CHECK, TRIMMED OUT DAMAGE TO LEFT BATTERY RIB IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,521 hrs · 26,077 cycles

SERVICE DOOR EMERGENCY EXIT IS BURNED OUT. SERVICE RELAMPED.

Part: CONTROL UNIT — FAILED (NLG STEERING) · airframe 32,370 hrs · 25,973 cycles

LOST DIRECTIONAL CONTROL WITH NOSE WHEEL STEERING AND RUDDER IMPUTS. ACFT VEERED HARD TO THE RT. NO CAUTION MESSAGE WAS RECEIVED, AFTER STOPPING, NOSE WHEEL STEERING WOULD NOT REENGAGE WITH SWITCH AND STEERING INOP CAUTION MESSAGE APPEARED. REPLACED HCU DUE TO FAILURE OF CALIBRATION CHECK OF STEERING IAW AMM. PN ON/OFF 16650-101, SN ON DCL884/02, SN OFF DCL871/02.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 31,037 hrs · 24,912 cycles

LIGHT ON EXIT SIGN NEAR SERVICE DOOR BURNED OUT. (FLT 5649) RELAMPED EXIT SIGN.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,314 hrs · 24,321 cycles

DAMAGE FROM A BIRD STRIKE FOUND ON NOSE OF AIRCRAFT BETWEEN THE TRU ACCESS DOORS. (FLT 4566) REPLACED SKIN IN REFERENCE TO CRJ200 SRM.

Part: TIRE — BLOWN (MLG) · airframe 30,270 hrs · 24,278 cycles

RIGHT OUTBOARD MAIN TIRE WAS BLOWN AND FLAT. (FLT 6222) REPLACED NR 3 AND 4 MAIN LANDING GEAR WHEEL ASSEMBLIES AND NR 4 WHEEL SPEED TRANSDUCER. P/N: 5010571-1, S/N OFF: SEP04-6652, P/N: 5010571-1, S/N OFF: SEP11-0859.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,133 hrs · 24,180 cycles

OVERHEAD EMERGENCY LIGHT NEAR ROW 8 IS OUT. (FLT 5514) RELAMPED EMERGENCY LIGHT.

Part: SIGN — INOPERATIVE (CABIN) · airframe 30,014 hrs · 24,086 cycles

FLOOR LEVEL EMERGENCY EXIT SIGN AT SEAT 8A AND FLOOR LEVEL LIGHTING STRIP FROM ROWS 1-5 DOES NOT LIGHT UP. (FLT 7769) REPLACED EMERGENCY EXIT SIGN AT SEAT 8A, CLEANED CONNECTIONS, AND REPLACED 1ST FLOOR LEVEL LIGHT STRIP.

Part: TIRE — POPPED (RT MLG) · airframe 29,938 hrs · 24,017 cycles

RIGHT OUTBOARD MAIN TIRE SEEMED TO POP. (FLT 6242) REPLACED NR 3 AND NR 4 MLG WHEEL ASSEMBLIES REFERENCING AMM. P/N OFF: 5010571-1, S/N OFF: OCT99-2723, P/N OFF: 5010571-1, S/N OFF: MAY01-2939.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,811 hrs · 23,920 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6490) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,637 hrs · 23,787 cycles

NR 4 EXTERIOR EMERGENCY LIGHT ON LEFT SIDE IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: POST — CRACKED (FUSELAGE) · airframe 29,593 hrs · 23,747 cycles

(C-CHECK) FS 409.0 +128 CRACK AT RBL 18.00 OUTBOARD SIDE OF VERTICAL POST. REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,537 hrs · 23,702 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 5 IS OUT. (FLT 4614) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,321 hrs · 23,508 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4746) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,214 hrs · 23,415 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5463) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,068 hrs · 23,303 cycles

RIGHT WING FORWARD EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 5630) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,068 hrs · 23,303 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5361) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,068 hrs · 23,303 cycles

LEFT AFT WING EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 6206) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,009 hrs · 23,255 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5228) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,009 hrs · 23,255 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT (FLT 6306) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,926 hrs · 23,199 cycles

NR 2 LEFT OVERWING AND NR 1 RIGHT OVERWING EXTERIOR EMERGENCY LIGHTS ARE OUT. (FLT 4830) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,884 hrs · 23,156 cycles

EMERGENCY LIGHT AT MAIN CABIN DOOR IS OUT. (FLT 4655) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,776 hrs · 23,045 cycles

THE 3RD OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 4472) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,723 hrs · 22,995 cycles

NR 1 OVERHEAD EMERGENCY LIGHT BURNED OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,390 hrs · 22,648 cycles

NR 1 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 5399) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,276 hrs · 22,560 cycles

RIGHT SIDE AFT EMERGENCY EXTERIOR LIGHT IS OUT. (FLT 5498) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,015 hrs · 22,363 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 10 IS OUT. (FLT 4476) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,459 hrs · 21,899 cycles

RIGHT SIDE EXTERIOR EMERGENCY EXIT LIGHT NEAR SERVICE DOOR IS BURNED OUT. (FLT 4491) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,230 hrs · 21,701 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4678) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,200 hrs · 21,677 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4762) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,986 hrs · 21,509 cycles

RIGHT EXTERIOR FORWARD EMERGENCY LIGHT IS OUT. (FLT 3047)RELAMPED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,986 hrs · 21,509 cycles

LEFT EXTERIOR AFT EMERGENCY LIGHT IS OUT. (FLT 3047)RELAMPED.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 26,753 hrs · 21,332 cycles

EXHAUST SMELL BLOWING OUT OF VENTS. (FLT 6338) CLEANED RIGHT PACK COALESCER SOCK. NO ABNORMAL ODORS NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,704 hrs · 21,288 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6719) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 26,408 hrs · 21,018 cycles

EMERGENCY EXIT LIGHT AT GALLEY SERVICE DOOR OUT. (FLT 6736) REPAIRED WIRING FOR EXIT SIGN AT GALLEY SERVICE DOOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,096 hrs · 20,748 cycles

NR 1 INTERIOR EMERGENCY LIGHT INOPERATIVE. (FLT 6138) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,473 hrs · 20,218 cycles

CEILING EMERGENCY LIGHT AT ROW 5 INOP. (FLT 4601) RELAMPED EMERGENCY LIGHT.

Part: ANGLE — CRACKED (BS 559 FLOORBEAM) · airframe 25,428 hrs · 20,176 cycles

CAP ANGLE AT FS 559.0 CRACKED. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,428 hrs · 20,176 cycles

FS 621 PRESSURE BULKHEAD CRACKED AT BL0.0. (C CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,639 hrs · 20,376 cycles

1 ½" CRACK NOTED ON FS 621 BULKHEAD. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,639 hrs · 20,376 cycles

CRACK FOUND ON FS 559.0 BULKHEAD WEB AND CRACK FOUND ON FS 559.0 GAP ANGLE BELOW VERTICAL POST. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,246 hrs · 20,032 cycles

NR 1 OVERHEAD AISLE EMERGENCY FLOOD LIGHT INOP. (FLT 4723) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,119 hrs · 19,930 cycles

NR 2 EMERGENCY CEILING LIGHT INOP. (FLT 6681) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,931 hrs · 19,782 cycles

NR 2 CEILING EMERGENCY LIGHT INOP. (FLT 4778) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,833 hrs · 19,707 cycles

NR 1 CEILING EMERGENCY LIGHT INOP. (FLT 6486) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,779 hrs · 19,664 cycles

CEILING EMERGENCY LIGHT NR 2 INOP. (FLT 6517) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,492 hrs · 19,439 cycles

NR 3 CEILING EMERGENCY LIGHT INOP. (FLT 6119) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 23,864 hrs · 18,924 cycles

EXIT LIGHT ON WALL AT 1AB INOP. (FLT 4782) RE-SECURED CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,494 hrs · 18,623 cycles

FURTHEST AFT EMERGENCY LIGHT IN CEILING INOP. (FLT 6717) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,269 hrs · 18,450 cycles

AFT EMERGENCY LIGHT INOP. (FLT 4752) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,213 hrs · 18,406 cycles

NR 2 EMERGENCY CEILING FLOOD LIGHT INOP. (FLT 4514) RELAMPED EMERGENCY FLOODLIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,038 hrs · 18,273 cycles

EMERGENCY EXIT SIGN ON OVERHEAD PANEL HAS INOP LIGHTS. (FLT 2222) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,994 hrs · 18,221 cycles

NR 3 OVERHEAD EMERGENCY LIGHT INOP. (FLT 2680) RELAMPED EMERGENCY LIGHT.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 22,750 hrs · 17,946 cycles

FLT 2075 - GEAR DISAGREE MESSAGE DISPLAYED. REPLACED 3A ACMP.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 22,692 hrs · 17,882 cycles

FLT 2526 - ESCAPE PATH LIGHTING INOP. RESECURED ELECTRICAL CONNECTION.

Part: CONTROL PANEL — MALFUNCTIONED · airframe 21,533 hrs · 16,962 cycles

FLT 4128 - GEAR WOULD NOT COME UP AFTER TAKEOFF. REPLACED GEAR LEVER PANEL ASSEMBLY.

Part: LIGHT — BROKEN (CABIN) · airframe 20,075 hrs · 15,710 cycles

FLT 6433 - MAIN CABIN DOOR FLOOR LEVEL EMERGENCY LIGHT IS BROKEN. REPLACED LIGHT ASSEMBLY PER CRJ 200 MM 33-57-19.

Part: CONNECTOR — ARCED (LIGHTS) · airframe 19,878 hrs · 15,554 cycles

CONNECTOR PINS IN P167/J167 SHOW SIGNS OF ARCING. REPLACED P167 AND J167 CONNECTOR IAW MM 25-28-00. OPS CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 17,324 hrs · 13,600 cycles

AT FL330, CO-PILOTS WINDOW SHATTERED. REPLACED RIGHT SIDE WINDOW IAW RII 56-220-1000 AND MM 56-12-01. OPERATIONAL CHECKS GOOD.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 16,758 hrs · 13,178 cycles

CRACKED CLIP AT FS484 RBL 9 FLOOR SUPPORT, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PER CRJ200 SRM 51-42-06 & 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 16,758 hrs · 13,178 cycles

FS 280 FWD FLOOR SUPPORT ANGLE CRACKED AT RADIUS RBL 9 BELOW COCKPIT FLOOR, DISCOVERED DURING C-CHECK INSPECTION. FWD FLOOR SUPPORT ANGLE PER CRJ200 SRM 51-42-06 PG.4 P/N 600-34017-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,400 hrs · 12,205 cycles

CABIN OVERHEAD EMERGENCY LIGHTING POD INOP. RELAMPED CABIN OVERHEAD LIGHT. OPERATIONAL CHECKS GOOD, PN 1317.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 14,755 hrs · 11,721 cycles

FLAP FAULTS WITH THE INBOARD GROUND SPOILERS. REPLACED THE NR 2 SECU IAW CRJ AMM 27-61-05. OPERATIONAL CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (FLIGHT CONTROL) · airframe 14,679 hrs · 11,662 cycles

"YD 1 INOP" STATUS MESSAGE DURING CRUISE. REPLACED FCC CARD IAW MM 21-12-14. OPERATIONAL CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 14,164 hrs · 11,276 cycles

STAB TRIM MACH TRIM DISENGAGED REPEATEDLY ON TAXI OUT RETURNED TO GATE. REPLACED CAPT TRIM DISCONNECT SWITCH IAW CL 600 MM 27-41-05. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 13,728 hrs · 10,946 cycles

STAB TRIM CH 1 INOP MESSAGE ON TAXI OUT. REPLACED THE HSTA IAW MM 27-12-01 AND MCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD. P/N 8396-3; S/N OFF 643.

Part: CONTROL SYSTEM — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 13,703 hrs · 10,927 cycles

STAB CH1 INOP STATUS MSG. ON ED2 CAME UP TWICE DURING CRUISE FLIGHT. REPLACED HSTCU, NR 1 SLATS ENGAGE SWITCH AND STAB TRIM CONTROL PANEL REF AMM 27-41-01. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 13,069 hrs · 10,430 cycles

SECOND OVERHEAD EMERGENCY LIGHT INOP. REPLACED LAMP. OPERATIONAL CHECK GOOD.

Part: CONTROL CABLE — TIGHT (PITCH DISCONNECT) · airframe 12,309 hrs · 9,820 cycles

PITCH DISCONNECT HANDLE CABLE IS TIGHT. ITEM FOUND AT C-CHECK INSPECTION. PITCH, ELEVATOR DISCONNECT SYSTEM RIGGED IAW CRJ MM 27-32-00-830-801.

Part: FLANGE — CRACKED (FUSELAGE) · airframe 12,309 hrs · 9,820 cycles

FUSELAGE STA 409.00 PLUS 128, LBL 27.0 INBOARD FLANGE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED CRACKED FLANGE IAW CRJ REO 601R-53-41-056 REV "C".

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,309 hrs · 9,820 cycles

FUSELAGE FLOORBEAM FITTING IS CRACKED; FS 460.00 RBL. ITEM FOUND AT C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11, 51-23-00, 51-42-21, 51-42-06, 51-25-16, AND 51-21-11.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,309 hrs · 9,820 cycles

FUSELAGE FS 280.00 RBL 9.0 LOWER FLANGE CRACKED ON TRANSVERSE BEAM. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FS 280, FBL 9, LOWER FLANGE ON TRANSVERSE BEAM IAW CRJ REO 601R-53-11-171 REV B.

Part: CLIP — CRACKED (FUSELAGE) · airframe 12,309 hrs · 9,820 cycles

AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED FS 625.00 STR 14L. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ REO 601R-53-61-100 REV "NC".

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 12,309 hrs · 9,820 cycles

RIGHT ELECTRICAL BAY FLOOR AT FS 193, RBL 30 IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CRACK REPAIRED IAW CRJ REO 601R-53-11-245 REV "A".

Part: CLIP — CRACKED (FUSELAGE) · airframe 12,309 hrs · 9,820 cycles

AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED FS 625.00 STR 14R. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ REO 601R-53-61-100 REV "NC".

Part: SERVO — MALFUNCTIONED (ELEVATOR) · airframe 11,980 hrs · 9,562 cycles

DURING CRUISE FLIGHT AT FL290 A/C STARTED AN UNCONTROLLED DESCENT. THE AUTOPILOT DISENGAGED AND RECEIVED A AP NOSE DOWN MESSAGE. REPLACED BOTH CAPT'S AND F/O STAB TRIM SWITCHES. REPLACED ELEVATOR SERVO IAW MM 22-11-04. REPLACED ELEVATOR SERVO MOUNT IAW MM 22-11-14. COMPLIED WITH DETAILED INSPECTION OF HORIZONTAL STAB TRIM ACTUATOR IAW AMM TASK 27-42-01-220-801. NO DEFECTS NOTED. ALL SYSTEMS OPERATIONAL CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL PROTECTION) · airframe 11,277 hrs · 9,006 cycles

SHORTLY AFTER ROTATION, RECIEVED "WINDSHEAR FAIL" AND "CONT IGNITION" STATUS MESSAGES, ALSO HAD INTERMITTENT STICK SHAKER. REPLACED STALL PROTECTIVE COMPUTER. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 11,069 hrs · 8,847 cycles

STAB CHANNEL 1 WON`T ENGAGE. REMOVED AND REPLACED CB PANEL CB F5 AND HSTCU COMPUTER. OPERATIONAL CHECKS GOOD IAW 27-41-01. P/N OFF 7060-8, S/N OFF 959.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 9,917 hrs · 7,955 cycles

CAPTAINS WINDSHIELD CRACKED ON TAXI IN. REMOVED AND REPLACED THE PILOT'S WINDSHIELD IAW CRJ 200 MM 56-00-00, 56-11-01, 56-12-01. P/N OFF NP-139321-1, S/N OFF 97007H5138.

Part: FITTING — LEAKING (APU) · airframe 9,339 hrs · 7,500 cycles

FUEL SMELL IN AIRCRAFT CABIN, ALSO FUEL LEAK FROM REAR OF AIRCRAFT. REPLACE FITTING AT APU FUEL CONTROL TO FUEL SHUTOFF VALVE. RAN APU, OPS CHECK AND LEAK CHECK GOOD. P/N: AP258S04.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,323 hrs · 6,739 cycles

FS 280 RIGHT FLOORBOARD RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11 & RII 53-401.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,323 hrs · 6,739 cycles

FS 484 RIGHT INTERCOSTAL OUTBOARD FLANGE RBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV ''A'' & RII 53-401.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,323 hrs · 6,739 cycles

FS 280 LEFT FLOORBOARD LBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11 & RII 53-401.

Part: SWITCH — FAILED (STAB TRIM) · airframe 8,193 hrs · 6,642 cycles

ON CLIMBOUT OF SLC (35 NM), BOTH STAB TRIMS AND MACH TRIM DISENGAGED. TRIMS WOULD NOT RESET AS PER QRH. RETURN TO SLC. REMOVED AND REPLACED STAB TRIM DISCONNECT SWITCH IAW 27-41-30. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 6,755 hrs · 5,481 cycles

RECEIVED FLAP FAIL CAUTION MESSAGE AT 11,000 FT. ON DOWNWIND, FLAPS FAILED AT 0 DEGREES. INTERROGATED FECU UPON ARRIVAL AT GATE. NO FAILURES LISTED. PERFORMED VISUAL INSPECTION OF FLAPS AND BPSU RIG CHECK AND SYSTEM CHECKS IAW CL600 MM 27-51-00 & 27-51-05. ALL SYSTEMS PASS CHECKS. FLAP OPERATION AND INDICATION CHECK GOOD.

Part: PCU — MALFUNCTIONED (RT SPOILERON) · airframe 6,635 hrs · 5,381 cycles

AT LIFTOFF RECEIVED A WHITE STATUS SPOILERON FAULT MESSAGE ON BOTH RIGHT AND LEFT SIDES. REPLACED BAD SPOILERON PCU IAW MM CH 27-62-01. LEAK CHECK GOOD. OPS CHECK GOOD.

Part: PIN — BENT (RT MLG CONNECTOR) · airframe 6,635 hrs · 5,381 cycles

GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOLLOWED AND COMPLETED QRH PROCEDURE, RETURNED TO HELENA. FOUND PUSHED PIN ON RIGHT GEAR SIDE STAY ACTUATOR CONNECTOR (P110 PIN-E). RE-SECURED PIN. SWUNG GEAR. OPS CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 5,206 hrs · 4,273 cycles

F/O'S WINDOW SHATTERED ON DESCENT INTO SLC. REMOVED AND REPLACED F/O'S SIDE WINDOW IAW RII 56-402.

Part: A/C PACK — SMOKE (A/C BAY) · airframe 5,066 hrs · 4,164 cycles

DURING CLIMBOUT, NOTICED VISIBLE SMOKE IN COCKPIT AND CABIN. APU BLEED IN USE. RIGHT AC PACK BLOWING SMOKE. RETURNED TO FIELD. FOUND RT PACK BLOWING SMOKE. CHECKED WATER SOCK AND WAS CLEAN. REINSTALLED WATER SOCK. RAN RIGHT AC PACK WITH ENG BLEEDS AND APU BLEEDS. NO SMOKE NOTED FROM THE RIGHT AC PACK SYSTEM. OPS CHECKED GOOD.

Part: ANGLE — CRACKED (FLOOR SUPPORT) · airframe 4,536 hrs · 3,731 cycles

FUSELAGE STA 621 RIGHT FLOOR SUPPORT ANGLE CRACKED AT RBL 42. REPAIRED ANGLE IAW REO 601R-53-61-117, REV. A.

Part: ANGLE — CRACKED · airframe 4,536 hrs · 3,731 cycles

FUSELAGE STA 625 STR 15L ANGLE FOUND CRACKED.REPLACED ANGLE IAW CRJ SRM 51-42-06. P/N: 601R-35012-51.

Part: ANGLE — CRACKED (FLOOR BEAM ATTAC) · airframe 4,536 hrs · 3,731 cycles

FUSELAGE STA 280 FLOOR BEAM ATTACH ANGLE CRACKED AT RBL 9 OUTBOARD. REPLACED CRACKED ANGLE IAW CRJ SRM 51-42-13 & 51-42-21. P/N: 601R31113-58.

Part: ANGLE — CRACKED · airframe 4,536 hrs · 3,731 cycles

FOUND FUSELAGE STA 625 STR 15R ANGLE CRACKED. REPLACED ANGLE IAW CRJ SRM 51-42-06. P/N: 601R-35012-52.

Part: ACCESS DOOR — OPEN (EXT POWER) · airframe 4,104 hrs · 3,389 cycles

RETURNED TO AIRPORT AFTER TAKEOFF DUE TO EXT POWER ACCESS PANEL LEFT OPEN BY COS RAMPERS. INSPECTED EXT POWER ACCESS DOOR. NO DEFECTS NOTED.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 3,348 hrs · 2,817 cycles

SPOILERONS FAULT MESSAGE WILL NOT GO OUT AFTER FLIGHT CONTROL CHECK PER MEL OPS PROCEDURE. ALSO EXCESSIVE LEFT AILERON TRIM REQUIRED TO MAINTAIN LEVEL FLIGHT PREVIOUS LEG. RIGHT SPOILERON ARROW MOMENTARILY POINTS UP AFTER ENGINE STARTS WITH CONTROL COLUMN NEUTRAL. REMOVED AND REPLACED RT SPOILERON I/B PCU IAW CRJ MM 27-62-01. OPS CHECK GOOD, LEAK CHECK GOOD. S/N OFF: 3795.

Part: PCU — MALFUNCTIONED (LT SPOILER) · airframe 3,380 hrs · 2,841 cycles

LEFT SPOILERON FAULT CAUTION MESSAGE. REPLACED LEFT SPOILER OUTBOARD PCU IAW CL600 MM 27-62-01. SPOILERON OPS CHECK GOOD. PCU LEAK CHECK GOOD. S/N OFF: 9779.

Part: SENSOR · airframe 2,083 hrs · 1,832 cycles

ARINC COOL CAUTION MESSAGE, ALL PHASES OF FLIGHT AND GROUND. REPLACED ARINC COOL FLOW SENSOR. MOUNT BOLTS AND CONNECTOR SECURE. OPS CHECK OK. P/N: 009519-05 S/N OFF: 0531

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (PITOT SYS) · airframe 1,192 hrs · 1,082 cycles

AFTER TAKEOFF RIGHT STATIC HEAT, RIGHT PITOT HEAT, TAT PROBE HEAT AND RIGHT AOA HEAT WARNINGS ILLUMINATED. RETURNED TO SLC. RESET HEAT SYSTEM FOR RIGHT PITOT STATIC, TAT PROBES, AND AOA SYSTEM. OPS CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 1,136 hrs · 1,030 cycles

FIRST OFFICER''S WINDSHIELD SHATTERED INFLIGHT AT FL250. INSIDE LAYER DID NOT DELAMINATE. NO CABIN PRESSURE LOSS. REMOVED AND REPLACED COPILOT''S WINDSHIELD IAW MM 56-11-01, CHECKS GOOD. P/N: NP-139321-10, S/N ON: 0107343239, S/N OFF: 0013047097.

Part: STALL WARNING — MALFUNCTIONED (PROTECTION UNIT) · airframe 257 hrs · 222 cycles

ON TAKEOFF ROLL, STALL FAIL CAUTION MESSAGE ON EICAS. ABORTED TAKEOFF. REMOVED AND REPLACED STALL PROTECTION UNIT. OPS CHECKS GOOD IAW MM 27-35-01. P/N ON: 3995100208, S/N ON: 249, S/N OFF: 608.

Part: ACTUATOR — FAILED (RUDDER TRIM) · airframe 47 hrs · 40 cycles

ON AFTER LANDING CHECK, RUDDER TRIM FAILED TO OPERATE. REPLACED RUDDER TRIM ACTUATOR PER MM 27-22-01 P/N AL00101, S/N ON 9862, S/N OFF 4411, OPS CHECK GOOD.