N905SW

Part: WINDOW — CRACKED (COCKPIT) · airframe 49,826 hrs · 41,930 cycles

LEFT SIDE WINDOW INNER PLY CRACKED, REQUIRES REPLACEMENT, FLIGHT 5243. REMOVED AND REPLACED THE LT SIDE WINDOW IAW TASK CARD.

Part: WINDOW — CRACKED (LEFT) · airframe 49,825 hrs · 41,929 cycles

LEFT SIDE WINDOW INNER PLY CRACKED. FLIGHT 5243. REMOVED AND REPLACED LEFT SIDE WINDOW IAW TASK CARD CP 21268893-1 FOR PRESSURIZATION AND LEAK CHECK.

Part: CHECK VALVE — FAILED (RT RAM AIR) · airframe 48,593 hrs · 40,814 cycles

AFTER TAKE OFF, VISIBLE SMOKE IN THE CABIN AND FLIGHT DECK. ABOUT 1 MINUTE AFTER TAKE OFF SMOKE TOLIET CAUTION MESSAGE. FLT 5336 CLOSEDTROUBLESHOT VISIBLE SMOKE IN CABIN. FOUND RAM AIR INLET, BUTTERFLY VALVES AND DUCTING FROM RAM AIR INLET TO HEAT EXCHANGER TO HAVE COKING RESIDUE AND ANTI-ICE FLUID. ALL OTHER DUCTS TO AND FROM PACKS WERE CLEAN. REMOVED AND REPLACED RH PACK RAM AIR CHECK VALVE AND REINSTALLED LH RAM AIR CHECK VALVE IAW AMM. REMOVED, INSPECTED, CLEANED, AND REINSTALLED RAM AIR INLET DUCTS FROM RAM AIR INLET TO HEAT EXCHANGER IAW AMM. ALL GROUND OPS AND LEAK CHECKS OF ECS SYSTEM GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 47,563 hrs · 39,896 cycles

CORROSION ON LT LATCH PIN INTERCOSTAL @ STR 27, BETWEEN FS 349 - FS 364. (C-CHECK) RO: 05/07/2019 REMOVED AND INSTALLED NEW SERVICEABLE LATCH PIN INTERCOSTAL STR 27L BETWEEN FS349.00-FS364.00 IAW SRM. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 47,563 hrs · 39,896 cycles

CORROSION ON RT LATCH PIN INTERCOSTAL @ STR 27 BETWEEN FS 349 - FS 364. (C-CHECK) RO: 05/07/2019 REMOVED & INSTALLED NEW SERVICEABLE LATCH PIN INTERCOSTAL STR 27R BETWEEN FS349.00-FS364.00 IAW SRM. LEAK CHECK GOOD.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 47,563 hrs · 39,896 cycles

LT EMERGENCY EXIT DOOR, UPPER AFT CORNER AT AREA COMMON TO STOP FITTING HAS CORROSION ON THE INSIDE OF THE DOOR FRAME AT NUTPLATE LOCATION. (C-CHECK) RO: 05/07/2019 INSTALLED NEW LT OVER WING EMERGENCY DOOR P/N 601R30000-957 S/N SB/RJ/1335 IAW SRM. LK & OP CK GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 47,563 hrs · 39,896 cycles

LT CARGO DOOR, FLOOR SILL HAS CORROSION AROUND NUTPLATES AND AROUND DOOR STOPS FROM FS 559.00+118 - FS 621.00, LBL 46. (C-CHECK) RO: 05/07/2019 REPLACED LT CARGO FLOOR SILL FROM FS559+118 TO FS621 IAW SRM AND REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,563 hrs · 39,896 cycles

CORROSION ON FLOORBEAM INBOARD FLANGE AT NUTPLATE, LOCATED 2.0" AFT OF FS 409.00+16, RBL9. (C-CHECK) RO: 05/07/2019 PERFORMED SPLICE REPAIR OF FLOORBEAM IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 47,563 hrs · 39,896 cycles

PAX DOOR INTERCOSTAL P/N 601R31902-413 @ DD6 IS CORRODED. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED INTERCOSTAL PN 601R31902-413 IAW SRM. PRESSURE CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 47,563 hrs · 39,896 cycles

PAX DOOR INTERCOSTAL P/N 601R31902-322 @ DD4 IS CORRODED. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED PAX DOOR INTERCOSTAL P/N 601R31902-322 IAW SRM. LEAK CHECK GOOD.

Part: STRAP — CORRODED (FUSELAGE) · airframe 47,563 hrs · 39,896 cycles

FLOOR STRAP CORRODED FS559 LBL27 €“ LBL 43. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED LT FLOOR STRAP AT FS559 LBL27-LBL43 IAW SRM. LEAK CHECK GOOD.

Part: GUSSET — GOUGED (FUSELAGE) · airframe 47,563 hrs · 39,896 cycles

GOUGE ON GUSSET FOR FRAME FS319, APPROX STR-10R. (C-CHECK) RO: 05/07/2019 REPLACED DAMAGED GUSSET WITH NEW P/N: 601R38303-75, AT FRAME FS 319.00 AT APPROX STR-10R IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 47,563 hrs · 39,896 cycles

FRAME CORRODED AT FS 349 BETWEEN STR 25 LEFT AND STR 25 RIGHT. (C-CHECK) RO: 05/07/2019 REMOVED CORRODED FRAME SECTION AND INSTALLED NEW SERVICEABLE LOWER FRAME SECTOR AT FS349.00 BETWEEN STR 23L AND STR 23R IAW SRM. PRESSURE CK GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 47,563 hrs · 39,896 cycles

FRAME CORRODED AT FS 364 FORWARD SIDE BETWEEN STR 25 LEFT AND STR 25 RIGHT. (C-CHECK) RO: 05/07/2019 REMOVED CORRODED FRAME SECTION & INSTALLED NEW SERVICEABLE LOWER FRAME SECTOR P/N# 601R32007-11 AT FS364.00 BETWEEN STR 23L AND STR 23R IAW SRM. PRESSURE CK GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 47,563 hrs · 39,896 cycles

RT FLOOR SILL RBL43 CORRODED FS559 €“ 559+16. (C-CHECK) RO: 05/07/2019 REMOVED CORROSION AT RT FLOOR SILL RBL43 FS559 - FS 559.00+16 IAW REO.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 47,563 hrs · 39,896 cycles

RT AFT CARGO FLOOR SILL HAS MULTIPLE CORROSION AROUND FASTENER HOLES BETWEEN FS559.00+112 TO FS621.00. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED RT CARGO FLOOR SILL FROM FS559.00+12 TO FS621.00 IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 47,563 hrs · 39,896 cycles

RIGHT INBD FLAP VANE SKIN LEADING EDGE CHAFED IN THREE SPOTS. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED CHAFED RT INBD FLAP VANE SKIN L/E WITH NEW SKIN IAW SRM AND REO.

Part: VANE — CHAFED (TE FLAP) · airframe 47,563 hrs · 39,896 cycles

INBOARD FLAP VANE LT WING (OUT BOARD SIDE) HAS CHAFE. (C-CHECK) RO: 05/07/2019 INSTALLED NEW LT INBOARD FLAP ASSEMBLY, P/N 601R14002-1 IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 47,563 hrs · 39,896 cycles

LT FLOOR SILL PANEL FS409+128 THRU FS559 BETWEEN APPROX BL36 AND BL45 CORRODED. (C-CHECK) RO: 05/07/2019 REPAIRED AREAS OF CORROSION ON THE LT FLOOR SILL PANEL BETWEEN FS409+128 THRU FS559.00 AT LBL 36 AND LBL 45 IAW REO.

Part: PLATE — CORRODED (SERVICE DOOR) · airframe 47,563 hrs · 39,896 cycles

SERVICE DOOR PROTECTOR PLATE HAS CORROSION ON BACK SIDE. (C-CHECK) RO: 05/07/2019 LOCATED AND INSTALLED NEW SERVICE DOOR PROTECTOR PLATE P/N: 601R38957-31 IAW SRM.

Part: PANEL — DENTED (RT WING) · airframe 47,563 hrs · 39,896 cycles

SEVERAL DENTS RIGHT WING OUTBOARD LEADING EDGE PANEL. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED THE OUTBD SKIN OF THE RT WING OUTBD LE ASSY IAW SRM.

Part: HINGE — WORN (LAV SERVICE) · airframe 47,563 hrs · 39,896 cycles

LAV SERVICE DOOR HINGE WORN. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED WORN LAV SERVICE DOOR HINGE WITH NEW HINGE AND HARDWARE IAW SRM.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 47,563 hrs · 39,896 cycles

ENROUTE SMOKE TOILET CAUTION MSG. (FLT 1357) CLOSED INSPECTED AIRCRAFT FOR SIGNS OF ELECTRICAL ARCING, OR ODOR. NO ISSUES FOUND. RAN AIRCRAFT ENGINES AND AC PACKS. NO SMOKE FOUND IN THE CABIN. PERFORMED OPERATIONAL TEST OF LAV SMOKE DET IAW AMM. SYSTEM OPERATES NORMAL. AIRCRAFT IS OK FOR SERVICE

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 46,433 hrs · 38,858 cycles

GEAR DISAGREE ON TAKE OFF. RETURN TO FIELD. NORMAL OPS FOR REMAINDER OF FLIGHT. (FLT 5251) FO: 09/07/2018 CLOSED DEFERRED LANDING GEAR RETRACTION SYSTEM IAW MEL.

Part: PSEU — FAILED (LANDING GEAR) · airframe 46,427 hrs · 38,851 cycles

GEAR DISAGREE WARNING MESSAGE AFTER DEPARTURE. UPON LANDING GEAR EXTENDED NORMALLY. EMERGENCY DECLARED. (FLT 5151) REMOVED AND REPLACED PSEU IAW AMM. PERFORMED PSEU OPS CHECKS AND OPS CHECK GOOD. PERFORMED NLG SWINGS AND OPS CHECK GOOD. CHECKED GAPS OF NLG PROX SENSORS AND OPS CHECK GOOD. HYD SYSTEM NR 3 PRESSURE, QTY, AND TEMP READ NORMAL.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 42,962 hrs · 35,671 cycles

RIGHT FLOOR SUPPORT CORRODED AT BS 319, RBL 43. INSTALLED A NEW FLOOR SUPPORT FROM BS 310 TO 319 IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 42,962 hrs · 35,671 cycles

FLOOR SUPPORT AT LBL 9 HAS CORROSION AROUND THE NUT PLATE HOLES BETWEEN BS 589 AND 621 OTBD SIDE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM AND REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 42,962 hrs · 35,671 cycles

LEFT IBD FLAP VANE LEADING EDGE CHAFED APPROXIMATELY 6 INCHES FROM FROM THE IBD EDGE. REMOVED AND REPLACED THE VANE LEADING EDG IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 42,962 hrs · 35,671 cycles

LEFT INBOARD FLAP VANE CHAFED APPROXIMATELY 43.5 INCHES FROM FROM THE OTBD EDGE. REMOVED AND REPLACED THE THE VANE LEADING EDGE IAW SRM.

Part: BRACKET — BENT (NLG SENSOR) · airframe 41,132 hrs · 34,062 cycles

FUNCTIONAL FLIGHT RETURNED TO DEPARTURE DUE TO A GEAR DISAGREE. R & R NLG OLEO CENTERING, EXTEND SENSOR BRACKET IAW AMM AND C/W SENSOR ADJUSTMENT IAW AMM, ALL OPS GOOD.

Part: LANDING GEAR — NO TEST · airframe 40,520 hrs · 33,482 cycles

FAILED FUNCTIONAL FLIGHT FOR GEAR RETRACTION/EXTENSION.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 40,520 hrs · 33,481 cycles

LANDING GEAR DISAGREE. NLG NEVER RETRACTED AND MANUAL EXTENSION WAS REQUIRED.

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 40,519 hrs · 33,480 cycles

GEAR DISAGREE ON GEAR RETRACTION, NLG. RETURNED TO THE FIELD. OPEN

Part: PRIORITY VALVE — FAILED (NLG) · airframe 40,518 hrs · 33,479 cycles

AIRCRAFT RETURNED TO THE FIELD DUE TO A GEAR DISAGREE. R & R NLG PRIORITY VALVE, SWUNG GEAR MULTIPLE TIMES, OPS CHECK GOOD.

Part: SKIN — DENTED (LT AILERON) · airframe 38,662 hrs · 31,829 cycles

AILERON UPPER SKIN DENTED AT A/STA 304, STS EA, C-CHECK RO 3/27/15, COMPLIED WITH REPAIR OF LT AILERON UPPER SKIN DENT AT WS 304 IAW STS EA. COMPLIED WITH ST 51-900-1003.

Part: SKIN — DENTED (BS 652-672) · airframe 38,662 hrs · 31,829 cycles

COMPLY WITH FUSELAGE DENT REPAIR BETWEEN FS652.56- FS672.20 BETWEEN S17L AND S18L IDENTIFIED AS DENT NR 2 ON CAMP MX TRANS 11921491, C-CHECK, RO 3/27/15, COMPLIED WITH PERMANENT REPAIR OF FUSELAGE DENT BETWEEN FS652.56-FS672.20 BETWEEN S17L AND S18L IAW STS EA.

Part: STRUCTURE — CHAFED (LT APRON) · airframe 38,662 hrs · 31,829 cycles

LEFT APRON SKIN HAS CHAFED DAMAGE CAUSED BY UPPER WING PLANK SEAL. C-CHECK, RO 3/27/15, BLENDED OUT, CHECKED AND FOUND LT APRON SKIN OUT OF LIMIT REF REO AND REPLACED WITH NEW APRON SKIN REF STS EA.

Part: TRUNNION — CRACKED (LT WING) · airframe 38,662 hrs · 31,829 cycles

FOUND 3 EA CRACKED HOLES ON L/WING WHILE PERFORMING SB, C-CHECK RO 3/27/15. REPAIRED 3EA CRACKED HOLES ON LT TRUNNION AT L/WING REF REO.

Part: STRUCTURE — CORRODED (DOOR HANDRAIL) · airframe 38,662 hrs · 31,829 cycles

LT FS 349 CUP FOR PAX DOOR AFT HANDRAIL, CORRODED BEYOND LIMITS. C-CHECK, RO 3/27/15. R & R 1 EA. BRACKET AND 1 EA CLEAT TO PAX DOOR LOWER STRUCTURE AT LT FS.349, REF CRJ 200 SRM .

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 38,662 hrs · 31,829 cycles

LT INBD FLAP VANE L/E HAS CHAFE OTBD OF OTBD ACTUATOR, C-CHECK, RO 3/27/15. REMOVED CHAFE FROM LT FLAP VANE OTBD L/E CAP, ORIGINAL THICKNESS 0.050", REMAINING THICKNESS 0.029" MATERIAL REMOVED 0.021" MAX MATERIAL ALLOWED TO BE REMOVED IS 0.020", BEYOND LIMITS REF REO. REPLACED LT INBD FLAP VANE, OTBD L/E CAP REF SRM.

Part: SKIN — CORRODED (PAX DOOR) · airframe 38,662 hrs · 31,829 cycles

PAX DOOR INNER SKIN HAS CORROSION IN BETWEEN NUTPLATE AND INNER SKIN AT ACCESS PANEL LOCATION 832BR. BLENDED CORROSION AND REPLACED NUTPLATES ON PAX DOOR INNER SKIN AT ACCESS PANEL 823BR IAW; SRM. ORIGINAL MATERIAL THICKNESS WAS 0.040" REF SRM, REMOVED 0.008", REMAINING MATERIAL THICKNESS IS 0.032", MEASURED WITH TOOL, TUC7197 DUE 31AUG2015. FOUND TO BE OUT OF LIMITS REF SRM MAX ALLOWED 0.004", 10 PERCENT. RECEIVED AND COMPLIED WITH EA.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 38,662 hrs · 31,829 cycles

FORWARD EQUIPMENT COMPARTMENT FLOOR HAS A CRACK AT LT SIDE FS193.00, MARKED, C-CHECK, RO 3/27/15, REPAIRED CRACK AT THE LT SIDE OF THE FORWARD EQUIPMENT, TRU BAY, FLOOR AT FS 193.00 REF REO.

Part: SKIN — DAMAGED (BS 621) · airframe 38,662 hrs · 31,829 cycles

AFT CARGO DOOR CUTOUT OUTER SKIN HAS SLIGHT DAMAGE AT AFT EDGE OF SKIN APPROXIMATELY FS 621.00. C-CHECK RO 3/27/15, REPAIRED AFT CARGO DOOR CUTOUT OUTER SKIN AFT EDGE OF SKIN APPROXIMATELY FS 621.00, REF STS EA 10. FUNCTIONAL & LEAK CHECKS GOOD, ORIGINAL MATERIAL THICKNESS IS 0.063", MATERIAL REMOVED IS 0.030" DEEP X 2.20" LONG, REMAINING MATERIAL IS 0.033", ALLOWABLE MATERIAL REMOVED IS 0.030" BLEND IS WITH IN LIMITS IAW STS EA.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 38,662 hrs · 31,829 cycles

FORWARD EQUIPMENT COMPARTMENT FLOOR HAS A CRACK AT RT SIDE FS193.00, MARKED, C-CHECK, RO 3/27/15. REPAIRED FORWARD EQUIPMENT COMPARTMENT FLOOR AT RT SIDE FS 193.00 IAW REO.

Part: ACCESS PANEL — CORRODED (PAX DOOR) · airframe 38,662 hrs · 31,829 cycles

PAX DOOR FWD ACCESS PANEL AREA HAS CORROSION BETWEEN NUTPLATE AND INNER SKIN. AT 832AL LOCATION, C-CHECK, RO 3/27/15, BLENDED CORRODED AREAS REF SRM ORIGINAL MATERIAL THICKNESS WAS 0.040" REF SRM, REMOVED 0.006" MATERIAL, REMAINING MATERIAL THICKNESS IS 0.034", MEASURED WITH TOOL, TUC7197 DUE 31AUG2015, FOUND TO BE OUT OF LIMITS REF SRM MAX ALLOWED 0.004", 10 PERCENT. INSTALLED 5EA NEW NUTPLATES UNDER PAX DOOR ACCESS PANEL 832AL. RECEIVED STS EA.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,662 hrs · 31,829 cycles

DENT APPROXIMATELY 3 INCH AFT OF GROUND AIR SUPPLY DOOR SKIN CUTOUT. REPAIRED DENT APPROXIMATELY 3" AFT OF GROUND AIR SUPPLY DOOR SKIN CUTOUT REF STS EA.

Part: SKIN — GOUGED (PAX DOOR) · airframe 38,662 hrs · 31,829 cycles

PAX DOOR HAS GOUGES COMMON TO SKIN AND HANDLE HOUSING, MARKED, C-CHECK, RO 3/27/15. COMPLIED WITH PERMANT REPAIR I, STEPS 1-6, REF STS EA.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,806 hrs · 30,324 cycles

MULTIPLE INOPERATIVE BULBS IN THE LT AND RT EMERGENCY EXIT DOORS LIGHTED EXIT SIGNS. R & R THE BULBS IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,522 hrs · 30,129 cycles

FRONT LT OTBD EMERGENCY LIGHT INOPERATIVE, REPLACED THE LAMP.

Part: SHUTOFF VALVE — UNKNOWN (APU FUEL) · airframe 36,102 hrs · 29,839 cycles

NOXIOUS FUEL ODOR IN THE COCKPIT, DONNED O2 MASKS. RAN LT AND RT PACKS OFF OF APU BLEED AND ENGINE BLEEDS. CONFIRMED AN ODOR WITH APU AND ENGINE BLEEDS. NO ODOR NOTICED IN CABIN. INSPECTED APU, FOUND NO SIGNS OF SMOKE OR OIL LEAKS. APU OIL LEVEL WAS GOOD. REPLACED APU FUEL SOLENOID SHUTOFF VALVE AND LT PACK WATER SEPERATOR COALESCER IAW AMM. PERFORMED OPS CHECK OF LT PACK WITH ENGINE BLEED IN HOT AND COLD AND APU BLEED IN HOT AND COLD NO ODOR NOTED AT THIS TIME. OPS CHECK GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,984 hrs · 29,748 cycles

NR 4 EMERGENCY OVERHEAD FLOOD LIGHT IS BURNED OUT. FLT 5236 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,574 hrs · 28,675 cycles

MINI LIGHT IS BURNED OUT ON THE ENTRY FLOOR LEVEL EMERGENCY POD LIGHT. FLT#6290 RELAMPED.

Part: SKIN — DAMAGED (LT AILERON) · airframe 34,500 hrs · 28,615 cycles

LT AILERON UPPER LE SKIN DAMAGED. C-CHECK REPLACED LT AILERON UPPER LE SKIN WITH NEW PART NUMBER 601R13031-165 IAW SRM.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 34,500 hrs · 28,615 cycles

LT MLG DOOR HAS CHAFE ON INNER SKIN FORWARD EDGE. C-CHECK REPAIRED MLG DOOR FORWARD EDGE CHAFING IAW REO.

Part: SILL — CORRODED (FUSELAGE) · airframe 34,500 hrs · 28,615 cycles

AFT BAG BIN LT SIDE LOWER DOOR SILL HAS CORROSION. C-CHECK REPAIRED LIGHT CORROSION ON CARGO DOOR SILL IAW SRM & REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 34,500 hrs · 28,615 cycles

LT INBD FLAP VANE LE SKIN CHAFED AT OTBD VANE ACTUATOR. C-CHECK REPAIRED CHAFE BY BLENDING ON LT INBD FLAP VANE LE SKIN AT OTBD VANE ACTUATOR IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 34,500 hrs · 28,615 cycles

LT INBD FLAP VANE LE SKIN CHAFED AT CENTER VANE ACTUATOR. C-CHECK REPAIRED CHAFE BY BLENDING ON LT INBD FLAP VANE LE SKIN AT CENTER VANE ACTUATOR IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 34,500 hrs · 28,615 cycles

RT AILERON UPPER LE BETWEEN CENTER HINGES CHAFED. C-CHECK RT AILERON UPPER LEADING SKIN CHAFE REMOVED IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 34,500 hrs · 28,615 cycles

LT INBD FLAP VANE LE SKIN CHAFED AT INBD VANE ACTUATOR. C-CHECK REPAIRED CHAFE BY BLENDING ON LT INBD FLAP VANE LE SKIN AT INBD VANE ACTUATOR IAW REO.

Part: HINGE FITTING — GOUGED (TE FLAP) · airframe 34,500 hrs · 28,615 cycles

LT WING OTBD FLAP INBD FWD HINGE FITTING AFT SIDE HAS A GOUGE. C-CHECK BLENDED GOUGE ON LT WS178.00 FLAP HINGE BOX OTBD AFT SIDE OF AFT HINGE FITTING IAW STS.

Part: LENS — LOOSE (EXTERIOR) · airframe 33,238 hrs · 27,658 cycles

EXTERIOR EMERGENCY LIGHT NEXT TO MAIN CABIN DOOR HAD LOOSE LENS. (FLT 6441) REPLACED EXTERIOR EMERGENCY EXIT LIGHT LENS NEXT TO MAIN CABIN DOOR.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,218 hrs · 27,644 cycles

MAIN CABIN DOOR EXTERIOR EMERGENCY EXIT LIGHT BURNED OUT. (FLT 5652) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,123 hrs · 27,570 cycles

ONE EMERGENCY LIGHT BY MAIN CABIN DOOR IS BURNED OUT. (FLT 5556) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,637 hrs · 26,432 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5439) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,440 hrs · 26,281 cycles

MULTIPLE OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6386) REPLACED NR 2 AND NR 3 EMERGENCY BATTERY PACKS. P/N: AD-2013-1A, S/N: 35485, S/N OFF: 79464.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,234 hrs · 26,096 cycles

EXTERNAL LEFT WING EMERGENCY LIGHT IS OUT. (FLT 5318) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 30,305 hrs · 25,365 cycles

FLT 5264, NR 3 OVERHEAD EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT.

Part: SERVO — BINDING (AILERON) · airframe 29,991 hrs · 25,107 cycles

AILERONS FEEL JAMMED FOR 2 TO 3 SECONDS AFTER AUTO-PILOT IS DISCONNECTED IN-FLIGHT. (FLT 5552) REPLACED THE AILERON SERVO. P/N 622-4404-101, S/N OFF 46YG.

Part: VANE — CHAFED (TE FLAP) · airframe 31,579 hrs · 26,384 cycles

LEFT INBOARD FLAP VANE IS CHAFED AT INBOARD LEADING EDGE. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,579 hrs · 26,384 cycles

FS 621 BULKHEAD HAS A CRACK AT AFT CARGO DOOR TRACK ON WEB. (C-CHECK) REPAIRED PER CRJ200 SRM.

Part: STRUCTURE — CORRODED (L1 DOOR) · airframe 31,579 hrs · 26,384 cycles

PAX DOOR HAS CORROSION ON FORWARD CORNER, LOWER PORTION. (C-CHECK) REPAIRED PER CRJ200 SRM.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 31,579 hrs · 26,384 cycles

LEFT SIDE FS 559.0 PRESSURE BULKHEAD IS DAMAGED. (C-CHECK) REPAIRED PER REO.

Part: POST — CRACKED (FUSELAGE) · airframe 31,498 hrs · 26,330 cycles

CRACK ON VERTICAL POST BL0.0 AND FS 409 +128 LEFT C-CHANNEL IN AFT RADIUS. (C-CHECK) REPAIRED PER CRJ 200 SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 31,579 hrs · 26,384 cycles

LEFT INBOARD FLAP VANE IS CHAFED AT CENTER LEADING EDGE. (C-CHECK) REPAIRED PER REO.

Part: VANE — CHAFED (TE FLAP) · airframe 31,579 hrs · 26,384 cycles

LEFT INBOARD FLAP VANE IS CHAFED OUTBOARD LEADING EDGE. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,672 hrs · 24,847 cycles

NR 3 AFT LEFT EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,607 hrs · 24,787 cycles

RIGHT SIDE MIDDLE EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6390) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,607 hrs · 24,787 cycles

LEFT FORWARD EXTERIOR LIGHT EMERGENCY IS OUT. (FLT 6390) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,492 hrs · 24,695 cycles

LEFT SIDE AFT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5336) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,492 hrs · 24,695 cycles

RIGHT SIDE OVERWING MIDDLE EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5336) RELAMPED EMERGENCY LIGHT.

Part: HYDRAULIC LINE — CHAFED (HYDRAULIC SYS) · airframe 28,829 hrs · 24,183 cycles

HYDRAULIC 2 LO PRESS CAUTION. (FLT 5496) FOUND EDP2 CASE DRAIN LINE IN AFT EQUIPMENT BAY CHAFED THROUGH. PERFORMED REPAIR TO HYDRAULIC LINE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,906 hrs · 23,434 cycles

FORWARD EXTERIOR EMERGENCY EXIT LIGHT ON LEFT SIDE BURNT OUT. (FLT 6982) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,864 hrs · 23,398 cycles

EXTERIOR EMERGENCY LIGHT AT MAIN CABIN DOOR IS OUT. (FLT 6938) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,606 hrs · 21,477 cycles

RIGHT BULKHEAD WEB AT FS 559 CRACKED. (C CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,857 hrs · 21,692 cycles

FS 202 BULKHEAD CRACKED. (C-CHECK) REPAIRED PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,141 hrs · 21,083 cycles

LEFT EXTERIOR EMERGENCY LIGHT INOP. (FLT 6762) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,729 hrs · 19,130 cycles

FLT 6143 - AFT EMERGENCY LIGHT INOP. RELAMPED.

Part: WINDOW — CRACKED (COCKPIT) · airframe 22,644 hrs · 19,067 cycles

FLT 5868 - CAPTAIN'S SIDE WINDOW CRACKED. REPLACED WINDOW.

Part: HANDLE — OUT OF POSITION (PAX DOOR) · airframe 22,603 hrs · 19,031 cycles

FLT 6577 - CREW REPORTS MAIN DOOR OUTER HANDLE WON'T OPEN. DOOR HANDLE OUT OF POSITION, REPOSITIONED.

Part: MECHANISM — OUT OF ADJUST (PAX DOOR) · airframe 22,489 hrs · 18,933 cycles

FLT 5947 - PASSENGER DOOR WILL NOT OPEN. ADJUSTED THE HANDLE RETENTION BOLT MECHANISM ON THE INNER DOOR HANDLE.

Part: CIRCUIT BREAKER — TRIPPED (BRAKE PRESSURE) · airframe 22,406 hrs · 18,858 cycles

FLT 6546 - BRAKE PRESSURE INDICATION CAUTION MESSAGE IN CRUISE. RESET TRIPPED CIRCUIT BREAKER.

Part: TIRE — FAILED (MLG) · airframe 21,888 hrs · 18,460 cycles

FLT 6543 - BLEW RIGHT OUTBOARD MAIN TIRE ON ROTATION. REPLACED NR 3 AND NR 4 TIRE/WHEEL ASSEMBLIES AND RIGHT FLAP.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,439 hrs · 18,102 cycles

DURING C-CHECK, LOWER INBOARD CORNER OF LINTEL FITTING, REAR PRESSURE BULKHEAD, CRACKED. REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,439 hrs · 18,102 cycles

DURING C-CHECK, FS 280 RBL9 OUTBOARD CLIP CRACKED. REPLACED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,439 hrs · 18,102 cycles

DURING C-CHECK, FS 280 LBL9 INBOARD AND OUTBOARD CLIPS CRACKED. REPLACED PER REO.

Part: LINE — LEAKING (FUEL MANIFOLD) · airframe 20,957 hrs · 17,706 cycles

STRONG JET FUEL ODOR IN COCKPIT AND CABIN WHEN APU BLEEDS ARE USED. FLIGHT 6099. REPLACED THE PRIMARY AND SECONDARY FUEL MANIFOLD LINES PER AMM 49-31-09.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 18,872 hrs · 15,903 cycles

FLT 5872 - EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPAIRED WIRING ON AFT EMERGENCY LIGHT AS REQUIRED. OPS CHECKS GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 17,489 hrs · 14,661 cycles

GALLEY EMERGENCY EXIT LIGHT IS INOP. RELAMPED EMERGENCY EXIT LIGHT. OPS CHECK GOOD.

Part: BUSHING — NOISY (LT AILERON) · airframe 17,304 hrs · 14,502 cycles

SIGNIFICANT SQUEAKING NOISE FROM LEFT AILERON IN BOTH DIRECTIONS. REPLACED LEFT AILERON HINGE BUSHINGS AND HARDWARE IAW MM 27-14-15.

Part: SERVO — MALFUNCTIONED (ELEVATOR) · airframe 16,114 hrs · 13,494 cycles

AUTO PILOT KICKS OFF WITH FLAPS 20 DEGREES WHEN A TURN IS INITIATED. REPLACED ELEVATOR SERVO IAW MM 22-11-24. OPERATIONAL CHECKS GOOD.

Part: BRACKET — CRACKED (E/E BAY) · airframe 16,187 hrs · 13,558 cycles

AFT EQUIPMENT BAY BRACKET CRACKED APPROX 18" ABOVE APU EXHAUST BELLOWS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 601R75287-7 ANGLE IAW CRJ200 SRM 51-42-00.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 16,187 hrs · 13,558 cycles

FS 484 INTERCOSTAL CLIP CRACKED AT LBL27, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP PER BOMBARDIER REO 601R-53-41-059, CRJ 200 SRM 51-42-06, 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 16,187 hrs · 13,558 cycles

FS484 INTERCOSTAL CLIPS CRACKED AT RBL 27 AND 36, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 2 CLIPS IAW REO 601R-53-41-059, SRM 51-42-06 AND 51-42-21.

Part: BULKHEAD — CRACKED (BS 625) · airframe 16,187 hrs · 13,558 cycles

CRACK IN CLIP ON AFT SIDE OF REAR PRESSURE BULKHEAD AT FS 625.0 LT STRINGER 15, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP PANEL 601-35012-51 P/O 71471 AT FS 625.0 LT STRINGER 15 IAW CRJ200 REO 601R-53-61-422.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 16,187 hrs · 13,558 cycles

RT FS280 BEAM AT RBL10 LWR CRACKED BOTH OF THE 280 CLIPS ARE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED REPAIR PARTS PER CRJ200 SRM 51-42-13 PG 2.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 16,187 hrs · 13,558 cycles

FS 280 FLOORBEAM ANGLE AT LBL10 CRACKED AND BOTH OF 280 CLIPS ARE CRACKED LBL10, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED REPAIR PARTS AND ANGLE AT STA 280 LBL10 PER CRJ200 REO 601R 53-11-138.

Part: COMPUTER — MALFUNCTIONED (TE FLAPS) · airframe 15,891 hrs · 13,298 cycles

FLAPS FAIL CAUTION ON DEPARTURE. RETURNED TO BASE. RESET FLAP COMPUTER AND PERFORMED SYSTEM TEST ON FECU AND COULD NOT DUPLICATE. OPERATIONAL CHECKS GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 15,747 hrs · 13,181 cycles

FO'S SIDE WINDOW HAS CRACK IN CENTER PLY. REPLACED RIGHT SIDE WINDOW IAW CRJ MM 56-12-01 AND RII 56-220-1000, PN: NP139322-2, SN: 00126H6887.

Part: LIGHT — CONTAMINATED (CABIN) · airframe 15,329 hrs · 12,806 cycles

FLOOR LEVEL EMERGENCY LIGHTS ROW 2 THROUGH 5 INOP. CLEANED MOISTURE FROM FLOOR AND EMERGENCY LIGHTS ROW 2-5. OPERATIONAL CHECKS GOOD.

Part: PUMP — LEAKING (HYDRAULIC) · airframe 14,402 hrs · 11,973 cycles

LEVEL AT 29,000 RECEIVED -HYD 2 LOW PRESS- CAUTION MSG. REPLACED CASE DRAIN LINE IN AFT EQUIPMENT BAY AND NR 2 EDP HYD PUMP. OPERATIONAL AND LEAK CHECK GOOD.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 13,840 hrs · 11,476 cycles

AFT SECTION OF FLOOR EMERG LIGHTS INOP. RECONNECTED AFT LIGHT STRIP. OPERATIONAL CHECK GOOD AT THIS TIME IAW CRJ AMM 33-51-00.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 13,365 hrs · 11,053 cycles

CREW REPORTS RT OUTBOARD SPOILERON FAULT. REPLACED RT OUTBOARD SPOILERON INBOARD PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD, P/N: 27000-7 S/N OFF: MAL3774.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,570 hrs · 10,324 cycles

EMERGENCY FLOOR LIGHTING AFT OF OVERWING EXITS INOP. INSTALLED SERVICEABLE CONNECTOR ON AFT EMERGENCY FLOOR LIGHTING. OPERATIONAL CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,170 hrs · 10,002 cycles

EXIT EMERGENCY LIGHT BY STAIRS AND CABIN OVERHEAD EXIT LIGHT IS INOPERATIVE. REPLACED NR 2 BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD.

Part: CONNECTOR — INOPERATIVE (FLAP SCEW) · airframe 12,088 hrs · 9,936 cycles

FLAP SKEW DETECTION SYSTEM INOPERATIVE. REPLACED CONNECTOR 1J9CE IAW WDM 27-51-00. OPERATIONAL CHECK GOOD IAW MM 27-51-00.

Part: CLIP — CRACKED (BS 625) · airframe 13,164 hrs · 10,860 cycles

LEFT SIDE FS 625 CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALL CLIP IAW CRJ200 SRM 51-42-06.

Part: RIB — CRACKED (LT WING) · airframe 13,164 hrs · 10,860 cycles

LEFT MLG WHEEL WELL BATTERY RIB CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED DOUBLER IAW CRJ200 REO 601R-57-51-046 TYPE 1 REPAIR.

Part: RIB — CRACKED (RT WING) · airframe 13,164 hrs · 10,860 cycles

RIGHT MLG WHEEL WELL BATTERY RIB CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R-57-51-046.

Part: CLIP — CRACKED (BS 280) · airframe 13,164 hrs · 10,860 cycles

FRAME 280 AND BL-9 LT SIDE CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ200 SRM 51-10-06 PG 3, PARAGRAPH D.

Part: TRIM SWITCH — STICKS (COCKPIT) · airframe 11,754 hrs · 9,628 cycles

TRIM SWITCH ON PILOT SIDE STICKS. REPLACED THE CAPTAIN'S SIDE STAB TRIM SWITCH. OPERATIONAL CHECK GOOD IAW MM 27-41-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,369 hrs · 9,250 cycles

EMERGENCY LIGHT BY LAVATORY INOPERATIVE. REPLACED EMERGENCY LIGHT BY LAVATORY. OPERATIONAL CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,206 hrs · 8,261 cycles

EMERGENCY EXIT SIGN OVERHEAD OF CABIN AT ROW 8 INOPERATIVE. REMOVED AND REPLACED NR 1 AND NR 2 ELBP IAW MM 33-51-04 AND REPLACED NR 2 ELBP CHARGER. OPERATIONAL CHECK GOOD. P/N 2013-1A, S/N OFF 83335.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM MOTOR) · airframe 10,149 hrs · 8,211 cycles

STAB TRIM CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW MM 27-42-05. OPERATIONAL CHECKED GOOD.

Part: INTERCOSTAL — CRACKED (CRACKED) · airframe 8,199 hrs · 6,487 cycles

FS 484 RT INTERCOSTAL OB FLANGE RBL 36 CRACKED. DISCOVERED DURING C-CHECK. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV (A) RII 53-401.

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 8,199 hrs · 6,487 cycles

OVERHEAD CREW ESCAPE HATCH OUTER HANDLE SHAFT CORRODED. (DISCOVERED DURING C-CHECK)REMOVED AND REPLACED CREW ESCAPE HATCH OUTER HANDLE IAW HARTWELL CORP. CMM 52-22-03.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,199 hrs · 6,487 cycles

CARGO FLOOR SUPPORT ANGLE IS CRACKED AT FS 621.0; RBL 43.0. DISCOVERED DURING C-CHECK. DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117 REV A AND RII 53-401. P/N: 601R53-61-117-2.

Part: WARNING SYSTEM — ACTIVATED (T/E FLAP) · airframe 7,704 hrs · 6,002 cycles

AFTER TAKEOFF, DURING FLAP RETRACTION FROM 20 DEGREES TO 8 DEGREES, 'FLAPS FAIL' CAUTION MESSAGE DISPLAYED. RETURNED TO SMF. PERFORMED POWER DOWN PROCEDURE. OPS CHECKS GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 7,548 hrs · 5,864 cycles

STAB CHANNEL 1 INOPERATIVE. CHANGED HSTCA & MCU IAW 27-41-00. P/N 7062-3 S/N OFF 926.

Part: CIRCUIT CARD — FAILED (AUTOFLIGHT) · airframe 6,836 hrs · 5,237 cycles

ON DESCENT TO FINAL APPROACH RECEIVED AN AP PITCH TRIM CAUTION MESSAGE. RAN QRH, HEAVY NOSE DOWN WHEN DISCONNECTED. REENGAGED, AP MESSAGE WENT AWAY AFTER RE-TRIMMING. MESSAGE CAME BACK ON SHORT FINAL. REINITIALIZED FCC CARD NR 1 AND FCC CARD NR 2. OPS CHECKED NORMAL. PERFORMED OPERATIONAL CHECK OF AUTOPILOT TRIM SYSTEM. CHECKED NORMAL.

Part: LIGHT — SHORTED (CABIN) · airframe 6,318 hrs · 4,889 cycles

FORWARD ORANGE EMERGENCY LIGHT STRIP, FLOOR LEVEL FORWARD PASSENGER DOOR EMERGENCY EXIT SIGN, AND MID-LEVEL SERVICE DOOR EMERGENCY EXIT SIGN DO NOT ILLUMINATE. REPLACED TRACK LIGHT FLOOR STRIP NR 1. OPS TEST EMERGENCY LIGHTS GOOD. ORANGE STRIP FLOOR LEVEL PASS AND SERVICE DOOR LIGHTS CHECK GOOD. P/N: 36491-1.

Part: CONTROL VALVE — MALFUNCTIONED (APU) · airframe 5,595 hrs · 4,285 cycles

APU LOAD CONTROL VALVE WOULD NOT CLOSE AFTER TAKEOFF. RETURNED TO FAT. REMOVED AND REPLACED APU LCV IAW CRJ MM 49-51-01. OPERATIONAL CHECK GOOD AT THIS TIME.

Part: WIRE — DAMAGED (RUDDER TRIM) · airframe 5,286 hrs · 4,019 cycles

RUDDER TRIM INOP. INSPECTED RUDDER TRIM CONTROL SWITCH PANEL. REPAIRED WIRE CONNECTION. OPS CHECK GOOD.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 5,292 hrs · 4,027 cycles

RUDDER TRIM SWITCH STICKS NOSE RIGHT OR NOSE LEFT, DOES NOT SPRING BACK TO NEUTRAL. REMOVED AND REPLACED AILERON AND RUDDER CONTROL PANEL. OPS CHECKS GOOD.

Part: IDG — MALFUNCTIONED (NR 1 ENGINE) · airframe 5,123 hrs · 3,888 cycles

GENERATOR NR 1, LEFT WINDSHIELD HEAT AND LEFT WINDOW HEAT CAUTION MESSAGES ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF AND COMPLIED WITH QRH. COULD NOT RESET GENERATOR NR 1. REMOVED AND REPLACED LEFT IDG IAW CRJ MM 24-11-01. OPS CHECK GOOD.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 3,793 hrs · 2,734 cycles

MAIN GEAR WARNING ON LANDING. FOLLOWED EMERGENCY PROCEDURE AND MAIN GEAR DID NOT EXTEND. MANUALLY EXTENDED GEAR ON THIRD ATTEMPT. REMOVED AND REPLACED MAIN GEAR SELECTORS VALVE. GEAR SWINGS SATISFACTORY. LEAK CHECK GOOD.

Part: ARM — LACK OF LUBE (PAX DOOR) · airframe 3,557 hrs · 2,514 cycles

UNABLE TO OPEN MAIN CABIN DOOR FROM OUTSIDE. DISASSEMBLED LOWER PIVOTING ARM ASSEMBLY. CLEANED AND LUBED AS REQUIRED IAW 52-11-02.

Part: FLAP — MALFUNCTIONED (WING) · airframe 3,361 hrs · 2,314 cycles

AFTER T/O AT 400 FT RECEIVED FLAP FAIL CAUTION MESSAGE WHEN RETRACTING FLAPS. RAN QRH AND RETURNED TO THE FIELD. COMPLIED WITH AD 98-20-01. CYCLED FLAPS UP AND DOWN. OPS CHECK GOOD AT THIS TIME.

Part: CASE — CRACKED (APU) · airframe 2,934 hrs · 1,897 cycles

SMOKE APPEARED IN CABIN, PACKS WERE TURNED OFF. FIRST OFFICER NOTICED FLUID DRAINING THROUGH APU DRAIN VENTS, THEN APU AUTO SHUT DOWN. FOUND OIL LEAKING FROM APU. FOUND APU OIL CASE CRACKED. REMOVED AND REPLACED APU IAW CRJ MM 49-10-00. ALL OPS AND LEAK CHECKS GOOD. P/N ON: 3800488-3 S/N ON: P279C P/N OFF: 3800488-2 S/N OFF: P615

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 829 hrs · 548 cycles

ON PREFLIGHT INSPECTION, NOTICED CAPTAINS SIDE WINDSHIELD CRACKED REPLACED CAPTAINS WINDSCREEN IAW 56-11-04. P/N ON NP-139321-5, S/N ON 9927H9235, S/N OFF 00133H7393.

Part: DAMPER — FAILED (NR 2 YAW) · airframe 818 hrs · 542 cycles

UNABLE TO ENGAGE YAW DAMPER NUMBER TWO PRIOR TO FLIGHT. POWERED AIRCRAFT DOWN AND BACK UP. CYCLED YAW DAMPER SEVERAL TIMES. BOTH YAW DAMPER ONE AND TWO OPS CHECK GOOD.

Part: SHUTOFF VALVE — FAILED (LEFT) · airframe 777 hrs · 517 cycles

LEFT 10TH SOV FAILED TO OPEN. RECEIVED STATUS MESSAGE L 10TH ARMED OPEN. RETURNED TO DEN. POWERED DOWN AIRCRAFT AND RE-POWERED. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (STAB TRIM) · airframe 409 hrs · 271 cycles

STAB TRIM CH 1 INOP STATUS MESSAGE DURING FLIGHT. WOULD NOT ENGAGE. REMOVED AND REPLACED STAB TRIM ACTUATOR AND CONTROL BOX IAW CANADAIR RJ MM 27-41-00. OPS CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 229 hrs · 152 cycles

FIRST OFFICERS FRONT WINDSHIELD HAS SEVERAL LARGE CRACKS. REMOVED AND REPLACED RIGHT FRONT WINDSHIELD IAW 56-11-01, P/N 601R33033-2, S/N ON 97154H7754, S/N OFF 00224H5235.