N416SW

Part: PUMP — FAILED (HYD SYSTEM) · airframe 40,604 hrs · 34,373 cycles

HYD 3A LOW PRESS CAUTION 1800 PSI. REQUIRED EMERGENCY GEAR EXTENSION. AFTER EXTENSION DOWN TO 1500 PSI QTY IN FLIGHT SHOWN 80 PERCENT BEFORE GEAR EXTENSION. ON GROUND WITH BOTH PUMPS ON QTY DOWN TO 5 PERCENT. FLUID AROUND RT MAIN GEAR. FO: REPLACED 3A PUMP, LEAK CHECK GOOD. PERFORMED GEAR SWINGS AND ALTERNATE EXTEND. ALL OPS CHECK GOOD. CLEANED RESIDUAL FLUID.

Part: PLACARD — CRACKED · airframe 39,265 hrs · 33,023 cycles

APU ECU "NO STEP" COVER IS CRACKED. REPAIRED APU ECU "NO STEP" COVER IAW EA.

Part: COVER — UNSERVICEABLE · airframe 39,265 hrs · 33,023 cycles

UPPER SHROUD FOR LT WINDSCREEN ON INBD SIDE IS UNSERVICEABLE. REPAIRED TURNBUCKLE COVER IAW EA.

Part: SKIN — DENTED (LT WING) · airframe 39,265 hrs · 33,023 cycles

LT INBD WING L/E PANEL HAS TWO DENTS AT APPROXIMATE WS92.0 AND WS124.5. DRESSED BACK THE DENTS IAW REO.

Part: SKIN — DENTED (LT WING) · airframe 39,265 hrs · 33,023 cycles

LEFT MIDDLE WING L/E 530JL HAS A DENT AT APPROXIMATE WS 200. HAND DRESSED THE DENT IAW REO.

Part: HAND RAIL — DAMAGED (PAX DOOR) · airframe 39,265 hrs · 33,023 cycles

PAX DOOR FWD HAND RAIL, DENTED FWD UPPER CORNER COVER AND DAMAGED ATTACH FASTENER. REPAIRED AND RESTORED FINISH IAW SRM AND REO.

Part: HAND RAIL — DAMAGED (PAX DOOR) · airframe 39,265 hrs · 33,023 cycles

PAX DOOR AFT HANDRAIL, DENTED AFT UPPER CORNER COVER AND DAMAGED ATTACH FASTENER. REPAIRED AND RESTORED FINISH IAW SRM AND REO.

Part: POST — CRACKED (BS 409) · airframe 39,265 hrs · 33,023 cycles

BS 409+128 BL 0, RT SIDE OF POST CRACKED AT TOP. INSTALLED POST ASSEMBLY IAW SRM AND REO.

Part: FLOOR SUPPORT — GOUGED (BS 435) · airframe 39,265 hrs · 33,023 cycles

FLOOR SUPPORT AT BS 435, LBL 43 IS DAMAGED OUT OF LIMITS. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EA.

Part: PICCOLO TUBE — GOUGED (LEFT WING) · airframe 39,265 hrs · 33,023 cycles

LEFT WING OTBD PICCOLO TUBE IS GOUGED AT THE OTBD END. REPAIRED LT WING OTBD PICCOLO TUBE IAW EA.

Part: FRAME — CRACKED (BS 559) · airframe 39,265 hrs · 33,023 cycles

LEFT INTERIOR FUSELAGE FRAME AT BS 559 + 32 AT STRINGER 6L IS CRACKED. INSTALLED REPAIR 6 IAW EA.

Part: DUCT — BROKEN (BS 953) · airframe 39,265 hrs · 33,023 cycles

RT PSU DUCT RISER AF BS 953 HAS A BROKEN DUCT ON THE AFT SIDE. : REPAIR COMPLETE IAW EA.

Part: FRAME — CRACKED (BS 409) · airframe 39,265 hrs · 33,023 cycles

FUSELAGE FRAME AT BS 409+80 IS CRACKED AT STRINGER 6L. REPAIRED THE FRAME IAW SRM AND STS EA.

Part: FLOOR SUPPORT — CORRODED (BS 409-473) · airframe 39,265 hrs · 33,023 cycles

LEFT FLOOR SUPPORT FROM BS 409.128 - 473.15 HAS CORROSION. REMOVED THE CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 409-473) · airframe 39,265 hrs · 33,023 cycles

RIGHT FLOOR SUPPORT BS 409.128 - 473.15 HAS CORROSION. CORROSION WAS BLENDED IAW REO.

Part: FLOOR PANEL — CORRODED (BS 409-559) · airframe 39,265 hrs · 33,023 cycles

LEFT FLOOR PANEL FROM BS 409.128 - 559 HAS CORROSION. BLENDED CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 473-513) · airframe 39,265 hrs · 33,023 cycles

RIGHT FLOOR SUPPORT ANGLE FROM BS 473.15 - 513 CORRODED. THE CORROSION WAS BLENDED IAW REO.

Part: FLOOR PANEL — CORRODED (BS 409-559) · airframe 39,265 hrs · 33,023 cycles

RIGHT FLOOR PANEL FROM BS 409.128 559 HAS CORROSION. REMOVED CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 513-559) · airframe 39,265 hrs · 33,023 cycles

RIGHT FLOOR SUPPORT ANGLE FROM BS 513 - 559 CORRODED. CORROSION WAS BLENDED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 473-513) · airframe 39,265 hrs · 33,023 cycles

LEFT FLOOR SUPPORT FROM BS 473.15 - 513 HAS CORROSION. THE CORROSION WAS BLENDED IAW REO.

Part: LOUVER — LOOSE (RAM AIR EXHAUST) · airframe 39,265 hrs · 33,023 cycles

RIGHT RAM AIR EXHAUST DUCT HAS LOOSE LOUVERS. REPAIRED RIGHT ACM RAM AIR EXHAUST DUCT LOUVERS IAW REO.

Part: POST — CRACKED (BS 409) · airframe 39,265 hrs · 33,023 cycles

BS 409+128 VERTICAL POST AT BL 0, CRACKED. INSTALLED A NEW POST ASSY IAW SRM AND REO.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 39,265 hrs · 33,023 cycles

BS 621 BULKHEAD WEB HAS ONE CRACK LOCATED AT LBL 18. INSTALLED A REPAIR IAW REO.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 39,265 hrs · 33,023 cycles

BS 621 BULKHEAD WEB HAS TWO CRACKS LOCATED AT BL 0. INSTALLED A REPAIR IAW REO.

Part: LINE — LOOSE (FUEL SYS) · airframe 39,265 hrs · 33,023 cycles

TWO MOTIVE FLOW LINES INSIDE THE FUEL PRESSURE BOX ARE LOOSE. REINFORCED THE FUEL LINES IN FUEL PRESSURE BOX IAW REO.

Part: POST — CRACKED (BS 409) · airframe 39,265 hrs · 33,023 cycles

BS 409+128 VERTICAL POST AT LBL 18 INBD RADIUS CRACKED. INSTALLED A NEW VERTICAL POST ASSEMBLY IAW REO AND SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 39,265 hrs · 33,023 cycles

FS 621 BULKHEAD WEB HAS ONE CRACK AT RBL 9.5. REPAIR DOUBLER, TRIPLER AND FILLER WERE FABRICATED AND INSTALLED IAW REO.

Part: SEAT TRACK — CORRODED (BS 615) · airframe 39,265 hrs · 33,023 cycles

LBL 9 SEAT TRACK AT FS 615 HAS CORROSION AROUND FASTENERS. REPLACED SEAT TRACK AT LBL 9, FS 615 IAW REO.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 39,265 hrs · 33,023 cycles

LBL9 SEAT TRACK AT BS 559+90 HAS CORROSION. REPLACED THE SEAT TRACK IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 39,265 hrs · 33,023 cycles

LBL 9 FLOOR SUPPORT UPPER CAP BETWEEN BS 574 - 621 HAS CORROSION AT NUTPLATE LOCATIONS. INSTALLED NEW FLOOR SUPPORT CAP IAW SRM AND REO.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 39,265 hrs · 33,023 cycles

LBL9 SEAT TRACK BETWEEN FS 559+112 AND FS 574 HAS CORROSION. C-CHECK, REPLACED SEAT TRACK AT LBL 9 FS 559+112 - FS574 IAW REO.

Part: LOUVER — LOOSE (RAM AIR EXHAUST) · airframe 39,265 hrs · 33,023 cycles

LEFT RAM AIR EXHAUST DUCT HAS LOOSE LOUVERS. REPAIRED THE LEFT ACM RAM AIR EXHAUST DUCT LOUVERS, IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 39,265 hrs · 33,023 cycles

LBL 27, FLOOR SUPPORT UPPER CAP BETWEEN BS 574 - 621 HAS CORROSION AT NUTPLATE LOCATIONS. INSTALLED NEW FLOOR SUPPORT CAP IAW SRM AND REO.

Part: STRIKER — DENTED (PAX DOOR) · airframe 39,265 hrs · 33,023 cycles

PAX DOOR SEAL STRIKER REPAIR IN AFT UPPER CORNER IS BENT/DENTED. C-CHECK, R & R EXISTING REPAIR STRIP ON PAX DOOR SEAL STRIKER IN AFT UPPER CORNER IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 39,265 hrs · 33,023 cycles

LT INBD FLAP VANE, OTBD OF CENTER ACTUATOR L/E SKIN CHAFED. BLENDED CHAFE ON LT INBD FLAP VANE, OTBD OF CENTER ACTUATOR L/E SKIN IAW REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 39,265 hrs · 33,023 cycles

LEFT INBD FLAP VANE, MIDWAY BETWEEN INBD AND CENTER ACTUATOR L/E SKIN CHAFED. BLENDED CHAFE ON LT INBD FLAP VANE, MIDWAY BETWEEN INBD AND CENTER ACTUATOR L/E SKIN IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 39,265 hrs · 33,023 cycles

LEFT INBD FLAP VANE, BETWEEN OTBD AND CENTER ACTUATOR L/E SKIN CHAFED. C-CHECK, BLENDED CHAFE ON LT INBD FLAP VANE, BETWEEN OTBD AND CENTER ACTUATOR L/E SKIN IAW REO.

Part: SHROUD — CHAFED (LT AILERON) · airframe 39,265 hrs · 33,023 cycles

LT LOWER AILERON SHROUD PANEL 599AB IS CHAFED., BLENDED CHAFE ON LT LOWER AILERON SHROUD PANEL 599AB IAW REO.

Part: SHROUD — CHAFED (LT AILERON) · airframe 39,265 hrs · 33,023 cycles

LEFT LOWER AILERON SHROUD PANEL 599BB IS CHAFED. BLENDED CHAFE ON LT LOWER AILERON SHROUD PANEL 599BB IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 39,265 hrs · 33,023 cycles

LEFT INBD FLAP VANE, OTBD OF OTBD ACTUATOR L/E SKIN CHAFED. BLENDED CHAFE IAW REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 39,265 hrs · 33,023 cycles

LT INBD FLAP VANE, INBD OF INBD ACTUATOR L/E SKIN CHAFED. BLENDED CHAFE ON LT INBD FLAP VANE, INBD OF INBD ACTUATOR L/E SKIN IAW REO.

Part: SHROUD — CHAFED (LT AILERON) · airframe 39,265 hrs · 33,023 cycles

LEFT LOWER AILERON SHROUD PANEL 599CB IS CHAFED. BLENDED CHAFE ON LT LOWER AILERON SHROUD PANEL 599CB IAW REO.

Part: PANEL — FAILED (HORIZONTAL STAB) · airframe 39,265 hrs · 33,023 cycles

HORIZONTAL STABILIZER VISOR PANEL 326BR RT LOWER. CONTOURED THE VISOR PANEL IAW REO.C.

Part: HOUSING — GOUGED (DOOR HANDLE) · airframe 39,265 hrs · 33,023 cycles

PAX DOOR EXTERIOR HANDLE HOUSING HAS A GOUGE. PAX DOOR EXTERIOR HANDLE HOUSING BLENDED OUT IAW EA.

Part: PANEL — FAILED (HORIZONTAL STAB) · airframe 39,265 hrs · 33,023 cycles

HORIZONTAL STABILIZER VISOR PANEL 326BL, LT LOWER. CONTOURED THE VISOR PANEL IAW REO.

Part: PANEL — FAILED (HORIZONTAL STAB) · airframe 39,265 hrs · 33,023 cycles

HORIZONTAL STABILIZER VISOR PANEL 326AR RT UPPER. CONTOURED THE VISOR PANEL IAW REO.

Part: SKIN — DENTED (BS 654-672) · airframe 39,265 hrs · 33,023 cycles

ONE DENT BS 654.5 - 672.2 S18-21L. COLDWORKED DENT TO ORIGINAL CONTOUR IAW EA.

Part: FRAME — CORRODED (BS 319) · airframe 39,265 hrs · 33,023 cycles

FUSELAGE FRAME CORRODED. PAINT LIFTING AND BUBBLED AT STA 319 AND STRINGER 26 LT. REPAIRED IAW REO AND SRM.

Part: BRACKET — LOOSE (BLEED DUCT) · airframe 38,399 hrs · 32,167 cycles

RT ENGINE HAS LOOSE 10TH STAGE BLEED DUCT ISOLATORS. C-CHECK, REPLACED ISOLATORS.

Part: WIRE — BROKEN (CABIN) · airframe 37,806 hrs · 31,636 cycles

LOWER EMERGENCY EXIT SIGN AT MAIN CABIN DOOR DOES NOT ILLUMINATE. FLT 7372 REPAIRED BROKEN WIRE.

Part: STRUT — LOW (NLG) · airframe 37,088 hrs · 30,925 cycles

ON TAKE OFF NOSE GEAR WOULD NOT RETRACT. FLT#4624 SERVICED THE NLG SHOCK STRUT IAW AMM. PERFORMED NUMEROUS GEAR SWINGS. OPERATIONS CHECKED GOOD.

Part: ROD — FAILED (CABIN DOOR) · airframe 36,928 hrs · 30,758 cycles

MAIN CABIN DOOR DOES NOT CLOSE FROM THE OUTSIDE. FLT#4542 REPLACED MCD OUTER PRESSURE RELIEF FLAPPER ROD. PN 601R38649-3

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,441 hrs · 30,279 cycles

GALLEY EMERGENCY LIGHT IS BURNED OUT. RELAMPED.

Part: TARGET — MISALIGNED (LT MLG) · airframe 36,270 hrs · 30,099 cycles

RECEIVED GEAR DISAGREE WARNING MESSAGE FOR LT MAIN GEAR. RAN QRH. GEAR DOWN & LOCKED. STRAIGHTENED AND REALIGNED LT UPLOCK SENSOR TARGET, TORQUED AND COTTER PINNED TARGET. PERFORMED EMERGENCY EXTENSION AND NORMAL RETRACTION/EXTENSIONS. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,175 hrs · 30,005 cycles

MAIN CABIN DOOR FLOOR FLOOD LIGHT IS BURNED OUT. (FLT 4727) RELAMPED FLOOR LIGHT.

Part: VANE — CHAFED (TE FLAP) · airframe 35,763 hrs · 29,546 cycles

RIGHT INBOARD FLAP VANE IS CHAFED BEYOND LIMITS AND REQUIRES REPLACEMENT. (C-CHECK) REMOVED AND REPLACED RIGHT INBOARD FLAP VANE LEADING EDGE IAW SRM.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 35,763 hrs · 29,546 cycles

LEFT LOWER WING PLANK WS 65.75 STR 14-15 DRAIN VALVE HOLE CRACK INDICATION NOTED. (C-CHECK) REPAIRED LEFT LOWER WING PLANK DRAIN VALVE HOLE AT WS 65.75 STR 14-15 IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,763 hrs · 29,546 cycles

AFT PRESSURE BULKHEAD HAS CRACK AT BL 0.0. (C-CHECK) REPAIRED AFT PRESSURE BULKHEAD AT FS 621 BL 0.0 IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,763 hrs · 29,546 cycles

AFT PRESSURE BULKHEAD AT LBL 18.0 HAS A CRACK. (C-CHECK) REPAIRED AFT PRESSURE BULKHEAD AT LBL 18.0 IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 35,763 hrs · 29,546 cycles

FS 409.0+128 LBL 18.00 OUTBOARD VERT POST CRACK INDICATION NOTED AT AFT RADIUS. (C-CHECK) REPLACED OUTBOARD VERTICAL POST AT FS 409.0+ 128 LBL 18.00 IAW REO AND SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 35,763 hrs · 29,546 cycles

FS 409.0+128 RBL 18.00 OUTBOARD VERT POST CRACK INDICATION NOTED AT AFT RADIUS. (C-CHECK) REPLACED OUTBOARD VERTICAL POST AT FS 409.0+ 128 RBL 18.00 IAW REO AND SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,355 hrs · 29,142 cycles

NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 4839) RELAMPED EMERGENCY LIGHT.

Part: SENSOR — FAILED (NLG) · airframe 34,933 hrs · 28,735 cycles

AFTER TAKEOFF GEAR RETRACTED NORMALLY THEN EN ROUTE WE HAD A NOSE GEAR DISAGREE. (FLT 7811) REPLACED NR 1 NLG DOWN LOCK SENSOR ASSEMBLY IN REFERENCE TO AMM.

Part: SENSOR — DAMAGED (NLG) · airframe 34,933 hrs · 28,735 cycles

RECEIVED NOSE GEAR AMBER DASHES MOMENTARILY AND NOSE GEAR DISAGREE. (FLT 4824) REPLACED DAMAGED WOW NR 2 AND CENTERED HARNESS ASSEMBLIES IN REFERENCE TO AMM.

Part: PLUNGER — LACK OF LUBE (PAX DOOR) · airframe 34,814 hrs · 28,615 cycles

PASSENGER DOOR IS HARD TO OPEN FROM THE OUTSIDE. (SERVICE) LUBRICATED PASSENGER DOOR OUTER HANDLE PLUNGER.

Part: SKIN — CRACKED (LT WING) · airframe 34,673 hrs · 28,474 cycles

CRACK ON LEADING EDGE OF LEFT WING ALONG RIVETS. (FLT 4605) REPLACED CRACKED SKIN ON LEFT WING MIDDLE LEADING EDGE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,673 hrs · 28,474 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4714) RELAMPED EMERGENCY LIGHT.

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG) · airframe 34,646 hrs · 28,448 cycles

GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF RIGHT MAIN WOULD NOT RETRACT. (FLT 4569) ADJUSTED RIGHT MLG UPLOCK PROXIMITRY SENSOR.

Part: LIGHT — SHORTED (CABIN) · airframe 34,055 hrs · 27,876 cycles

SMOKE REPORTED IN CABIN ABOVE ROW 4AB. (FLT 6466) REPLACED SIDEWALL LIGHT ASSEMBLIES AT ROW 4AB FOR A SHORT CIRCUIT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,710 hrs · 27,553 cycles

LEFT FORWARD AFT TWO OVERWING EMERGENCY LIGHT OUT OF SERVICE. (FLT 4762) RELAMPED EMERGENCY LIGHT.

Part: PANEL — MALFUNCTIONED (COCKPIT) · airframe 33,462 hrs · 27,323 cycles

MFD 2 & PFD 2 WENT BLANK DURING CLIMBOUT. (FLT 4841) REPLACED F/O'S INSTRUMENT LIGHTING PANEL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 33,437 hrs · 27,294 cycles

AFT SECTION OF EMERGENCY FLOOR LIGHT STRIP IS OUT. (FLT 4483) RECONNECTED EMERGENCY FLOOR STRIP LIGHT CONNECTION.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 32,400 hrs · 26,337 cycles

EMERGENCY EXIT SIGN ON LEFT OF GALLEY SERVICE DOOR DOES NOT ILLUMINATE. (FLT 4593) REPLACED EMERGENCY EXIT LIGHTED SIGN AT SERVICE DOOR.

Part: CONNECTOR — DIRTY (CABIN) · airframe 32,290 hrs · 26,245 cycles

LAST ROW OF FLOOR EMERGENCY LIGHTS ARE OUT. (FLT 4728) CLEANED CONNECTORS ON AFT FLOOR LEVEL EMERGENCY LIGHT STRIP.

Part: SKIN — CRACKED (RT WING) · airframe 32,261 hrs · 26,219 cycles

RIGHT WING DRAIN HOLE AT WS 85.50 IS CRACKED. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,266 hrs · 26,223 cycles

FS 202 BULKHEAD CRACKED AT PARKING BRAKE CABLE HOLE. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,375 hrs · 26,315 cycles

FS 202 PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE HOLE. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,154 hrs · 26,126 cycles

LEFT FORWARD EXTERIOR OVERWING EMERGENCY EXIT LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: HANDLE — DIRTY (CABIN) · airframe 29,963 hrs · 24,210 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 4443) CLEANED AND LUBRICATED DOOR HANDLE AND LATCH PINS.

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 29,861 hrs · 24,115 cycles

PASSENGER DOOR AND SERVICE DOOR EMERGENCY EXIT SIGNS INOP. (FLT 4488) CYCLED EMERGENCY LIGHT SWITCH SEVERAL TIMES.

Part: FLAP — OUT OF RIG (WING) · airframe 29,714 hrs · 23,977 cycles

WHEN FLAPS ARE SELECTED TO 45°, AIRCRAFT ROLLS RIGHT. (FLT 1001) RIGGED FLAPS.

Part: PANEL — DEFECTIVE (TE FLAP) · airframe 29,702 hrs · 23,963 cycles

UNCOMMANDED ROLL WITH FLAPS EXTENDED TO 45°. (FLT 1002) REPLACED FLAP PANEL.

Part: AILERON — OUT OF RIG (WING) · airframe 29,701 hrs · 23,961 cycles

SELECTING FLAPS 45°, AIRCRAFT ROLLED TO THE RIGHT. (FLT 4493) REMOVED EXCESSIVE SEALANT AND PAINT RIDGE, RIGGED RIGHT AILERON.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 29,676 hrs · 23,941 cycles

UNCOMMANDED ROLL TO THE RIGHT ON FINAL WHEN SELECTING FLAPS. (FLT 4648) INSPECTION AND SYSTEM OPERATIONAL CHECKS NORMAL.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 28,796 hrs · 23,240 cycles

MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. (FLT 4611) OPERATIONAL CHECKS NORMAL.

Part: PULLEY — BINDING (CABIN DOOR) · airframe 28,545 hrs · 23,046 cycles

MAIN CABIN DOOR NOT OPENING. (FLT 4481) REPLACED FORWARD COUNTER BALANCE PULLEY.

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 28,135 hrs · 22,747 cycles

FLT 4760 - PASSENGER CABIN DOOR WOULD NOT OPEN FROM OUTSIDE. NO DEFECTS FOUND.

Part: BEAM — GOUGED (FUSELAGE) · airframe 28,448 hrs · 22,972 cycles

FS280 BEAM GOUGED. (C CHECK)REPAIRED PER REO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 28,448 hrs · 22,972 cycles

FS625 STRINGER 14 CLIPS CRACKED. (C CHECK)REPLACED PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 28,448 hrs · 22,972 cycles

AFT PRESSURE BULKHEAD CRACKED. (C CHECK)REPAIRED PER REO.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 28,448 hrs · 22,972 cycles

CRACKS AT FS559. (C CHECK)REPAIRED PER REO.

Part: WINDOW — BROKEN (COCKPIT) · airframe 26,133 hrs · 21,227 cycles

FLT 1001 - FIRST OFFICERS WINDOW IS BROKEN. REPLACED RIGHT WINDOW IAW MM 56-12-01. OPS AND LEAK CHECK GOOD, PN NP139322-6, S/N OFF 01047H1052.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 24,794 hrs · 20,204 cycles

FLT 3826 - ON TAXI OUT, HYDRAULIC PAGE SHOWED 0 PERCENT QUANTITY ON NR 2 SYSTEM. REPLACED PRESSURE LINE IN RIGHT PYLON. LEAK AND OPS CHECK GOOD.

Part: BEACON — SHORTED · airframe 24,747 hrs · 20,167 cycles

FLT 3948 - ELECTRICAL ARCING IN CEILING AREA ABOVE ROW 3. REPLACED UPPER BEACON IAW MM 33-41-00. OPS CHECKED GOOD, P/N 2LA002760-70, S/N OFF 361847.

Part: HANDLE — MALFUNCTIONED (PAX DOOR) · airframe 24,482 hrs · 19,960 cycles

FLT 3945 - OUTER HANDLE ON PAX DOOR WILL NOT STOW. REPLACED DAMAGED BOLT IN HANDLE MECHANISM IAW CMM 52-43-03. OPS CHECK GOOD.

Part: TERMINAL BLOCK — SHORTED (COCKPIT) · airframe 24,018 hrs · 19,611 cycles

ELECTRICAL SMOKE FROM THE FIRST OFFICER'S CB PANEL DURING DESCENT INTO SLC. FLIGHT NR 3922, REPLACED TERMINAL BLOCK NR 12 AND TERMINAL ENDS IAW AMM 20-00-00.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 23,445 hrs · 19,185 cycles

OXYGEN MASKS FROM PANEL OVER SEATS 12A AND 12B DEPLOYED DURING CLIMB-OUT. RETURNED TO FIELD. INSPECTED AND RESTOWED O2 MASKS.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 23,379 hrs · 19,133 cycles

CABIN FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 484 AND RBL27, DISCOVERED AT C-CHECK. INSTALLED NEW CLIP PER CRJ200 SRM 51-42-21 PG 17 AND REO 601R-53-41-059.

Part: DOOR FRAME — CRACKED (BS 338) · airframe 23,379 hrs · 19,133 cycles

CRACK FOUND AT FS 338.00 FRAME MEMBER ON PAX DOOR, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS AT FS 338.00 ON PAX DOOR PER REO 601R-52-11-402 REV G.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 23,379 hrs · 19,133 cycles

CABIN FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 484 AND RBL36, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE PER REO 601R-53-41-059 AND CRJ200 SRM 51-42-21.

Part: CLEVIS PIN — CORRODED (EMERGENCY EXIT) · airframe 23,379 hrs · 19,133 cycles

LEFT EMERGENCY EXIT FORWARD HINGE FITTING CLEVIS PIN IS CORRODED AND FROZEN, DISCOVERED AT C-CHECK. REPLACED PIN IAW CRJ200 AMM 52-21-00-820-801.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 23,379 hrs · 19,133 cycles

FOUND FLOORBEAM ANGLE AT FS 280 RBL 9 TO BE CORRODED BEYOND REPAIR, DISCOVERD AT C-CHECK. INSTALLED REPAIR FILLER ANGLE AND SPLICE ANGLES PER CRJ REO 601R-53-11-116.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,379 hrs · 19,133 cycles

FLOORBEAM AT FS 280 AND LBL9.0 IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE AT FS 280 LBL 9.0 IAW CRJ200 REO 601R-53-11-171.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 23,379 hrs · 19,133 cycles

CABIN FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 484 AND LBL27, DISCOVERED AT C-CHECK. INSTALLED NEW CLIP AT FS 484 AND LBL27 IAW REO 601R-52-4-059.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,379 hrs · 19,133 cycles

CRACK FOUND ON SKIN AFT OF RIGHT NOSE GEAR CUT-OUT, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS AS PER REO 601R-53-11-048.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 23,379 hrs · 19,133 cycles

CABIN FLOORBEAM STRUCTURE IS CRACKED AT FS 484 AND LBL36, DISCOVERED AT C-CHECK. INSTALLED NEW CLIP AT FS 484 AND LBL36 IAW REO 601R-52-4-059.

Part: BEAM — CRACKED (ENGINE) · airframe 23,379 hrs · 19,133 cycles

UPPER ENGINE BEAM ANGLE IS CRACKED AT FS 640 AND STR 10, DISCOVERED AT C-CHECK. REPLACED ANGLE P/N 601-35006-61 PER CRJ200 SRM 51-42-21 PGS 1-20.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 22,852 hrs · 18,722 cycles

FOUND LEFT WINDSHIELD CRACKED. REPLACED LEFT WINDSHIELD IAW RII 56-220-1000. OPERATIONAL CHECKS GOOD.

Part: LATCH — MALFUNCTIONED (E/E BAY DOOR) · airframe 22,262 hrs · 18,255 cycles

CANT OPEN MAIN CABIN DOOR FROM OUTSIDE. REPLACED OUTER DOOR HANDLE ASSEMBLY. OPERATIONAL CHECKS GOOD IAW 52-11-03, PN OFF H3414-39.

Part: DOOR — STICKS (PAX DOOR) · airframe 22,149 hrs · 18,160 cycles

COULD NOT OPEN MAN CABIN DOOR FROM OUTSIDE. OPENED AND CLOSED MAIN CABIN DOOR SEVERAL TIMES FROM OUTSIDE. DOOR OPERATES NORMALLY.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 21,989 hrs · 18,048 cycles

3 ROWS OF EMERGENCY LIGHTS INOP ALONG FLOOR LEADING TO EXIT ROW INCLUDING EXIT ROW. REPLACED EMERGENCY BATTERY INVERTER NR 3. OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 20,688 hrs · 17,090 cycles

EMERG LIGHTS INOP. REPLACED NR 1, 2, 3, 4 ELBPS WITH SERVICEABLE PACKS IAW 33-50-02, PN ON #1 2013-1A SN OFF 83074; 57129; 80677; 53657.

Part: CONTROL UNIT — BINDING (ELEVATOR) · airframe 20,378 hrs · 16,848 cycles

DURING FFOD ELEVATOR/AILERON CHECK, NR 3 HYD PUMP ELEVATOR BINDING. REMOVED AND REPLACED NR 3 HYD PCU ON RT ELEVATOR IAW CRJ MM 27-33-01. ALL CHECKS SMOOTH.

Part: HANDLE — MALFUNCTIONED (PAX DOOR) · airframe 20,049 hrs · 16,603 cycles

PAX DOOR WILL NOT OPEN FROM INSIDE CABIN. REPLACED OUTER HANDLE LATCH TRIGGER LIFT ASSY. OPERATIONAL CHECK GOOD IAW CMM 52-11-03.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 19,689 hrs · 16,320 cycles

SPOILERONS FAULT STATUS. REPLACED NR 1 SECU IAW 27-61-05. OPERATIONAL CHECK OK.

Part: SPAR — CRACKED (WS 148) · airframe 19,689 hrs · 16,320 cycles

RT WING; LOWER WING PLANK; REAR SPAR LOWER FLANGE IS CRACKED, WS 148.00, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-57-21-130 REV G & REO 601R-57-21-131 REV NC & RII 57-401.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 20,232 hrs · 16,736 cycles

AFT EQUIPMENT COMPARTMENT FS 625 STR 14L LT INTERCOSTAL CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ REO 601R-53-61-100, 601R-53-61-422.

Part: INTERCOSTAL — CRACKED (BS 654) · airframe 19,689 hrs · 16,320 cycles

INTERCOSTAL CRACKED AT FS 654.50 AT STR 4L, ITEM FOUND AT C-CHECK INSPECTION. INTERCOSTAL REPAIRED IAW CRJ SRM 51-71-12 FIG 4 & 51-31-00, 51-25-06, 51-23-00 & 51-25-16.

Part: POSITION SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 19,539 hrs · 16,204 cycles

FLAPS FAIL CAUTION MESSAGE EN ROUTE. REPLACED LT WING FLAP BPSU IAW MM 27-51-01. OPERATIONAL CHECK GOOD.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 19,428 hrs · 16,112 cycles

FLAPS FAIL CAUTION MESSAGE WITH OVERSPEED CLACKER FLAPS WERE IN THE 0 DEGREE DETENT POSITION. REPLACED FECU IAW MM 27-51-05, OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 18,790 hrs · 15,614 cycles

FLAPS HALFSPEED STATUS MSG IN FLIGHT. REPLACED FECU IAW CRJ 200 MM 27-50-00. OPERATIONAL CHECK GOOD, PN 860D100-18 SNOFF 251.

Part: SENSOR — MALFUNCTIONED (BRAKE POSITION) · airframe 18,688 hrs · 15,529 cycles

FLAPS FAIL .17 DEGREES ON APPROACH INTO SLC. REMOVED AND REPLACED NR 1 BPSU AND RIGGED LEFT AND RIGHT BPSU IAW CRJ 27-51-10. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 18,297 hrs · 15,214 cycles

SPOILERONS FAULT STATUS MESSAGE ILLUMINATED. REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD.

Part: LANDING GEAR — ICED (NOSE) · airframe 17,722 hrs · 14,770 cycles

WHEN RETRACTING LANDING GEAR, GOT RED MASTER WARNING, GEAR UP DISAGREE AND NOSE DOOR OPEN. FOUND NOSE GEAR COVERED IN ICE. THAWED NOSE GEAR AND SWUNG NOSE GEAR SEVERAL TIMES. OPERATIONAL CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 17,046 hrs · 14,246 cycles

PILOTS SIDE WINDOW CRACKED IN LOWER AFT CORNER. REPLACED LEFT SIDE WINDOW IAW 56-12-01, PN OFF 601R3033-3, SN OFF 9517349897.

Part: LINKAGE — DEFECTIVE (LT ELEVATOR) · airframe 16,987 hrs · 14,200 cycles

UNUSUAL FLUTTERING EXPERIENCED INFLIGHT, REDUCED SPEED, FLUTTER STOPPED. REPLACED LEFT ELEVATOR NR 1-3 PCU BOLTS AND BUSHINGS, NR 2, NR 3 LINKAGE. REPLACED RIGHT PCU LINKAGE AND HARDWARE FOR SYSTEMS 1-3 IAW MM CH 27-33-01. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 16,987 hrs · 14,200 cycles

ON DESCENT, RECEIVED STATUS "FLT SPOILER FAULT" MESSAGE ON THE RIGHT SIDE. REMOVED AND REPLACED RIGHT OUTBOARD FLIGHT SPOILER PCU IAW CRJ 200 MM 27-62-05. OPERATIONAL CHECK GOOD.

Part: SENSOR — MALFUNCTIONED (AOA VANE) · airframe 16,671 hrs · 13,949 cycles

CAPTAINS 1.27 STALL GREEN LINE SHOWS 280 KTS AT FLIGHT LEVEL 290 WHEN CO-PILOT'S IS NOT EVEN VISIBLE. NO STALL TAPE INDICATION. REMOVED AND REPLACED BOTH LT AND RT AOA VANES IAW MM 27-35-05. OPERATIONAL CHECK GOOD IAW AMM 27-35-01. PN 45150340 SN OFF 338 AND SN OFF 332.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 16,624 hrs · 13,908 cycles

REAR CARGO SMOKE DETECTOR INOPERATIVE. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR IAW MM 26-15-01. OPERATIONAL CHECK GOOD.

Part: ENGINE — FAILED (LEFT) · airframe 16,822 hrs · 14,068 cycles

LT ENGINE CHANGE REQUIRED DUE TO FAILED BOROSCOPE INSPECTION. REMOVED AND REPLACED LEFT ENGINE IAW MM 71-00-00. OPERATIONAL CHECK GOOD.

Part: LEVER — MALFUNCTIONED (TE FLAPS) · airframe 16,439 hrs · 13,761 cycles

(FLAPS FAIL) CAUTION MSG ON APPROACH TO SLC. REMOVED AND REPLACED FLAP HANDLE IAW MM 27-51-01, OPERATIONAL CHECK GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (EMERGENCY DOOR) · airframe 15,728 hrs · 13,194 cycles

LEFT EMERGENCY DOOR (OVERWING) MESSAGE CAME ON AFTER LANDING. ADJUSTED PROX SENSOR TARGET. OPS CHECK GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 15,616 hrs · 13,110 cycles

INTERCOSTAL BETWEEN FS 621 AND 625 ADJACENT STR 14 RIGHT IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INTERCOSTAL REPLACED IAW CRJ SRM 51-40-11, 51-40-06.

Part: PANEL — CRACKED (LT WING) · airframe 15,597 hrs · 13,095 cycles

LEFT WING LWR WING PLANK IS CRACKED WS 148.019. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-57-21-130 REV. E AND REO 601R-57-21-131 REV. NC.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 15,597 hrs · 13,095 cycles

FUSELAGE INTERCOSTAL FITTING CRACKED AT FS 461 RBL 9 O/B. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21.

Part: FLANGE — CRACKED (BEAM) · airframe 15,597 hrs · 13,095 cycles

FUSELAGE VERTICAL BEAM LWR I/B FLANGE CRACKED AT FS 559 RBL 9. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED BEAM IAW CRJ REO 601R-53-41-057 REV. NC.

Part: BEAM — CRACKED (FUSELAGE) · airframe 15,597 hrs · 13,095 cycles

FUSELAGE VERTICAL BEAM LWR I/B AND O/B FLANGE CRACKED AT FS 559 LBL 9. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED BEAM IAW CRJ REO 601R-53-41-057 REV. NC.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 15,616 hrs · 13,110 cycles

CARGO PIT FS 621 FLOOR SUPPORT ANGLE REPAIR CRACKED AT LBL 42. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV. A AND RII53-401.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,597 hrs · 13,095 cycles

FUSELAGE PULLEY INTERCOSTAL CLIP ANGLE CRACKED FS 484.00 LBL 27 O/B. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059.

Part: FLANGE — CRACKED (BEAM) · airframe 15,597 hrs · 13,095 cycles

FUSELAGE VERTICAL BEAM LWR I/B FLANGE CRACKED AT FS 409+128 LBL 27. DISCOVERED DURING C-CHECK INSPECTION. CARRIED OUT REPAIR IAW CRJ REO 601R-53-41-056 REV. C.

Part: FLANGE — CRACKED (BEAM) · airframe 15,597 hrs · 13,095 cycles

FUSELAGE VERTICAL BEAM LWR O/B FLANGE CRACKED AT FS 409+128 LBL 9. DISCOVERED DURING C-CHECK INSPECTION. CARRIED OUT REPAIR IAW CRJ REO 601R-53-41-056 REV. C.

Part: BEAM — CRACKED (FUSELAGE) · airframe 15,597 hrs · 13,095 cycles

FUSELAGE FS 280 RBL 9 LWR FLANGE CRACKED ON TRANSVERSE. DISCOVERED DURING C-CHECK INSPECTION. REPAIR BEAM IAW CRJ REO 601R-53-11-171 REV. NC.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,597 hrs · 13,095 cycles

FUSELAGE PULLEY INTERCOSTAL CLIP ANGLE CRACKED FS 484.00 RBL 27 O/B. DISCOVERED DURING C-CHECK INSPECTION. INTERCOSTAL CLIP REPLACED IAW CRJ REO 601R-53-41-059.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 15,597 hrs · 13,095 cycles

BRACKET CRACKED AT FS 202.75, 8:00 POSITION IN NOSE HYDRAULIC BAY COMPARTMENT. DISCOVERED DURING C-CHECK INSPECTION. CLIP REPAIRED IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-24-16, 51-24-36, 51-25-06, AND 51-25-16.

Part: SIGN — INOPERATIVE (CABIN) · airframe 15,513 hrs · 13,034 cycles

EXIT SIGN AT FORWARD WARDROBE INOP. REMOVED AND REPLACED EXIT SIGN AT FORWARD WARDROBE. OPS CHECKS GOOD. P/N: 6020-6.

Part: COMPUTER — MALFUNCTIONED (AHRS) · airframe 14,736 hrs · 12,426 cycles

WITH THE AUTOPILOT ON, THE CONTROL YOKE JERKS FORWARD SHARPLY. THE JERK IS MILD DURING CRUISE INTERMITTENTLY. THE JERK IS MORE PRONOUNCED DURING THE DESCENT AND LEVEL OFF AT LOW ALTITUDE FOR THE APPROACH. REMOVED AND REPLACED NR 2 AHC COMPUTER. OPS CHECKS GOOD IAW 34-21-01.

Part: COMPUTER — MALFUNCTIONED (FLIGHT CONTROL) · airframe 14,692 hrs · 12,390 cycles

ON DESCENT AND DURING APPROACH, THE CONTROL WHEEL WOULD INTERMITTENTLY JERK, BUT THE AUTOPILOT DID NOT DISCONNECT. REMOVED AND REPLACED FCC NR 2 CARD AND ELEVATOR SERVO IAW MM 27-12-14, MM 22-11-24. OPS CHECKS GOOD. SERVO P/N: 622-5027-001, S/N OFF: 2935.

Part: CARBON SEAL — DEFECTIVE (RT ENGINE) · airframe 11,030 hrs · 9,584 cycles

CLIMBING THROUGH FL240, 250 KTS, APPROX 5 DEGREES PITCH, CLIMB-THRUST, RIGHT ENGINE OIL LOW PRESS WARNING ILLUMINATED. QRH LED TO INFLIGHT SHUTDOWN. OIL PRESS APPROX 23-26 PSI AT 89.0 PERCENT N1. INSTALLED OVERHAULED NR 6 & NR 7 CARBON SEALS AND EXHAUST FRAME. RAN ENG FOR 10 MINUTES AT 85 PERCENT N2. NO LEAKS FOUND.

Part: TRIM SWITCH — DIRTY (COCKPIT) · airframe 10,989 hrs · 9,551 cycles

PILOT'S TRIM SWITCH STICKS WHEN TRIMMING NOSE UP, WON'T TRIM. CLEANED TRIM SWITCH, OPS CHECK GOOD THROUGH SEVERAL CYCLES.

Part: SELECTOR VALVE — FAULTY (MLG) · airframe 10,940 hrs · 9,514 cycles

AFTER TAKEOFF, UPON GEAR RETRACTION, RECEIVED A GEAR DISAGREE WARNING WITH A LIGHT AERODYNAMIC BUFFET. RETURNED TO SLC. FOUND MLG NOT UPLOCKING ON UPLOCK HOOKS. REMOVED AND REPLACED MLG SELECTOR VALVE IAW MM 32-32-00. SWUNG GEAR. OPS CHECKS GOOD & LEAK CHECKS GOOD.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 10,887 hrs · 9,469 cycles

AFTER TAKEOFF AND UPON RETRACTING LANDING GEAR, RECEIVED A NOSE GEAR UP DISAGREE WARNING. EXTENDED THE LANDING GEAR AND THE WARNING DID NOT PERSIST. ATTEMPTED TO RETRACT GEAR AGAIN. WARNING RETURNED. RETURNED TO BIL. REMOVED AND REPLACED THE NOSE LANDING GEAR SOLENOID VALVE IAW CRJ MM 32-33-10. PERFORMED SEVERAL GEAR SWINGS. OPS CHECKS GOOD.

Part: PRIORITY VALVE — MALFUNCTIONED (MLG) · airframe 10,906 hrs · 9,483 cycles

AFTER TAKEOFF ON GEAR UP RECEIVED GEAR DISAGREE AURAL AND AIRCRAFT BUFFETING. RAN QRH, AND PROBLEM REMAINED. AT SAME TIME NOTICED THE NR 1 BTMS INDICATION INOP. RETURNED TO SLC. REMOVED AND REPLACED MLG PRIORITY VALVE PER CRJ MM 32-32-15. OPERATIONAL CHECK GOOD. LEAK CHECK GOOD. REMOVED AND REPLACED NR 1 BTM SENSOR. OPS CHECK GOOD.

Part: SEAL — DIRTY (EXIT DOOR) · airframe 10,255 hrs · 8,975 cycles

PRESSURIZATION SQUEAL BY RIGHT OVER-WING EXIT DOOR PRESENT AT DELTA P OF 4.5 PSI AND GREATER. CLEANED EXIT SEAL. OPS CHECK GOOD.

Part: WIRE HARNESS — FAULTY (PAX DOOR) · airframe 9,938 hrs · 8,749 cycles

RECEIVED PASSENGER DOOR WARNING MESSAGE ON CLIMBOUT. RAN QRH AND RETURNED SLC. REMOVED AND REPLACED DOOR WARNING WIRING HARNESS, REF SB 601R-52-099 AND TESTED IAW MM 52-11-04. OPS GOOD.

Part: PROXIMITY SWITCH — OUT OF ADJ (AFT PAX DOOR CAM) · airframe 9,071 hrs · 8,082 cycles

RED PASSENGER DOOR MESSAGE APPEARED AFTER TAKEOFF OUT OF SLC. RETURNED TO THE FIELD. ADJUSTED AFT PASSENGER DOOR CAM PROXIMITY SWITCH IAW CRJ MM 52-11-02. OPS CHECK GOOD AT THIS TIME.

Part: OUTFLOW VALVE — FOD (PRIMARY) · airframe 9,071 hrs · 8,082 cycles

AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO SLC. REMOVED FOD FROM PRIMARY OUTFLOW VALVE. PERFORMED OPS CHECK PER MM 21-31-00. OPS CHECKS GOOD.

Part: STRAP — BROKEN (PAX DOOR) · airframe 8,945 hrs · 7,982 cycles

CLIMBING THROUGH 27,000 FEET CABIN DOOR LATCH CAUTION. FOLLOWED QRH. AT 30,000 FT PASSENGER DOOR WARNING. INITIATED DESCENT AND RETURNED TO SLC. REPLACED DOOR BONDING STRAP AND OPS CHECKED DOOR WARNING SYSTEM IAW CRJ MM 52-70-04. OPS CHECK GOOD.

Part: PROXIMITY SWITCH — OUT OF ADJ (PASSENGER DOOR) · airframe 8,945 hrs · 7,982 cycles

CLIMBING THRU 20,000', WE GOT A DOOR LATCH CAUTION MESSAGE. CLIMBING THRU 23,000', WE GOT A PASSENGER DOOR WARNING. THE WARNING WENT OUT DESCENDING THRU 14,000'. LATCH CAUTION CAME BACK ON, CAUTION WENT OUT AT 10,000'. ACCOMPLISHED PAX DOOR WARNING ADJUSTMENT TEST IAW 52-70-04. FOUND PROXIMITY SENSOR PS9MB OUT OF ADJUSTMENT. ADJUSTED SENSOR AND TESTED PASSENGER DOOR WARNING SYSTEM IAW CRJ MM 52-70-04. OPS CHECKS GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 8,911 hrs · 7,954 cycles

ON TAKEOFF PRIOR TO V1 RECEIVED A WING OVERHEAT MESSAGE AND ABORTED THE TAKEOFF. MESSAGE DISAPPEARED WITH THE POWER REDUCTION. PERFORMED AN OPERATIONAL TEST OF THE WING ANTI-ICE SYSTEM. OPS CHECK GOOD AT HIGH AND LOWER POWER SETTINGS IAW CRJ MM 30-12-00.

Part: ANALYZER — MALFUNCTIONED (ENGINE) · airframe 8,450 hrs · 7,592 cycles

N1 VIB AND ITT 899 DEGREES SHORTLY AFTER DEPARTURE (RIGHT SIDE). HAD TO CONTINUE AND REDUCE RIGHT POWER TO MAINTAIN CONTROL OF POWER SETTING. VIB ON LEFT .6, RIGHT WAS 1.6. RETURNED TO FIELD.MM 71-00-00 FIGURE 505 PAGE 521, ITT C DEGREE TABLE INDICATED NO MAINTENANCE ACTION REQUIRED FOR N1 VIB & 899 DEGREES ITT. GE OPERATION LIMITS TABLE 3-1 SHOWS WITHIN LIMITS.

Part: WINDOW — FAULTY (COCKPIT) · airframe 4,551 hrs · 4,121 cycles

RT WINDOW HEAT CAUTION MESSAGE 30 SECONDS AFTER TAKE OFF. REMOVED AND REPLACED RT SIDE WINDOW WITH SERVICEABLE WINDOW IAW CRJ MM 56-12-01. PN ON 328

Part: SWITCH — FAULTY (COCKPIT) · airframe 7,332 hrs · 6,640 cycles

STABILIZER TRIM AND MACH TRIM CAUTION MESSAGE CAME ON AFTER TAKEOFF. FOLLOWED QRH, WOULD NOT RE-ENGAGE. AIRCRAFT RETURNED TO THE FIELD. CAT II. REMOVED AND REPLACED FIRST OFFICER''S PITCH TRIM DISCONNECT SWITCH IAW MM 27-41-30. PERFORMED STABILIZER TRIM OPS AND FUNCTIONAL CHECKS IAW MM 27-40-00-710-801. OPS CHECKS GOOD, NO DEFECTS NOTED.

Part: CONTROL CABLE — OUT OF ADJ (RT ENGINE) · airframe 7,332 hrs · 6,640 cycles

AT TAKEOFF N1 SETTING NOTICED HIGHER THAN NORMAL ITT TEMPS ON RIGHT ENGINE. ALSO AT GROUND IDLE, NOTICED HIGHER THAN NORMAL N1 SPEEDS AT 28 PERCENT. ADJUSTED RIGHT ENGINE VG ACTUATOR FEED BACK CABLE IAW 72-00-00 SPECIAL PROCEDURE 07. RAN CHECK A/C, ALL RAN NORMAL.

Part: WIRE — DAMAGED (CABIN) · airframe 7,293 hrs · 6,606 cycles

EMERGENCY LIGHTS OUT FROM ROW 5 TO 8. REPAIRED WIRES AT ROW 8, DEFERRED ROW 6. REMOVED LIGHT STRIP AT ROW 6, PLUGGED IN RIGHT DIRECTION. OPS CHECK SATISFACTORY.

Part: ADC — FAILED (COCKPIT) · airframe 7,011 hrs · 6,368 cycles

CLIMBING THROUGH FL250 OFF BZN STAB TRIM CH2 AND MACH TRIM FAILED. RAN THE QRH AND DID NOT FIX THE PROBLEM. TROUBLESHOT SYSTEM. REPLACED ADC IAW 34-13-01. SYSTEM OPS CHECK AND STATIC LEAK CHECK OK. P/N ON 822-0371-140, S/N ON 5VYN, S/N OFF 2145.

Part: HEATER — INOPERATIVE (PITOT STATIC) · airframe 6,863 hrs · 6,248 cycles

AT 1500 FEET AFTER TAKEOFF PITOT BASE HEAT, LAOA HEAT, L STATIC HEAT, AND L PITOT HEAT MESSAGES ON EICAS WOULDN''T EXTINGUISH. RETURNED TO SLC. CYCLED POWER TO AC LEFT PITOT HEAT. MESSAGES OPS CHECK GOOD AT THIS TIME.

Part: CONTROLLER — FAILED (AD SENSOR HEAT) · airframe 6,802 hrs · 6,203 cycles

L AOA HEAT CAUTION MESSAGE ILLUMINATED SHORTLY AFTER TAKEOFF. RETURNED TO SLC. REPLACED NUMBER ONE AIR DATA SENSOR HEAT CONTROLLER IAW MM 30-31-15. LEFT AOA OPS CHECK GOOD. P/N 785-806-2, S/N ON 218, S/N OFF 169.

Part: TRIM SWITCH — MALFUNCTIONED (HORIZONTAL STAB) · airframe 6,609 hrs · 6,035 cycles

INFLIGHT THE STAB TRIM AND MACH TRIM DISCONNECTED AND WOULD RESET ONLY AFTER THE F/O TRIM DISCONNECT WAS CYCLED 4 OR 5 TIMES. POWER DOWN AIRCRAFT. OPERATIONAL CHECK OF HSTCU. OPS CHECKS GOOD IAW MM 27-41-01. RAN HORIZONTAL STABILIZER IAW MM 27-40-00 STAB TRIM AND MACH TRIM OPS CHECKS GOOD. UNABLE TO DUPLICATE DISCREPANCY.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 6,076 hrs · 5,556 cycles

AFTER ROTATION ON TAKEOFF, GOT STALL SHAKER WITH CONTINUOUS IGNITION, EVEN THOUGH SPEEDS WERE ABOVE VR AND V2 AND CLIMBING ON THE NORMAL PROFILE. WINDSHEAR FAIL, ALSO STATUS MESSAGE. RETURNED TO SLC. PERFORMED STALL PROTECTION PREFLIGHT AND MDC BITE OPERATIONAL CHECKS IAW MM 27-35-01. OPS CHECKS GOOD.

Part: SENSOR — FAILED (AIR DISTRIBUTION) · airframe 6,059 hrs · 5,538 cycles

INFLIGHT DISPLAY COOL MESSAGE CAME ON. COMPLIED WITH QRH AND MESSAGE WENT OUT ONLY IN STANDBY POSITION. RETURNED TO FIELD. REMOVED AND REPLACED DISPLAY COOL SENSOR AND FILTER. CHECKED DUCTS. OPS CHECKS GOOD. S/N: 0017, S/N OFF: 00155.

Part: COMPUTER — FAILED (AIR DATA) · airframe 6,019 hrs · 5,501 cycles

ADC NUMBER ONE FAILURE CLIMBING OUT OF SLC. RETURNED TO SLC. FOUND FAULT INDICATOR ON NUMBER ONE ADC ILLUMINATED. REPLACED NUMBER ONE ADC IAW CL600 34-13-01. AIR DATA OPS CHECKS AND PITOT STATIC CHECK GOOD. P/N ON: 822-0372-140, S/N ON: 3112, S/N OFF: 2044.

Part: CONTROLLER — MALFUNCTIONED (STAB TRIM) · airframe 5,416 hrs · 4,935 cycles

AP PITCH TRIM MESSAGE IN CRUISE. COULDN''''T GET ANYMORE THAN 4 DEGREES NOSE DOWN TRIM, BOTTOM OF GREEN, ON DESCENT INTO IDA. TRIM STOPS MOVING AT 4 DEGREES NOSE DOWN IN THE AIR AND 5 DEGREES NOSE DOWN ON THE GROUND. REMOVED AND REPLACED HSTA. OPS CHECKS GOOD IAW MM 27-42-01. P/N ON: 8396-3, S/N OFF: 196, S/N ON: 278. REMOVED AND REPLACED MCU FOR FAILURE OF HSTA. OPS CHECKS GOOD IAW MM 27-42-05. P/N ON: 7062-3, S/N OFF: 215, S/N ON: 205. OK FOR CAT II.

Part: TARGET — LOOSE (MLG UPLOCK)

AFTER GEAR RETRACTION GEAR DISAGREE WARNING ON LEFT MAIN GEAR. RETURNED TO SLC. NOTED FAULT IN PSEU FOR LEFT GEAR UPLOCK, (FAR). TIGHTENED UPLOCK TARGET AND CHECKED GAP PER MM 32-32-05. CYCLED GEAR NORMALLY AND PEFORMED FREE FALL CHECK. GEAR INDICATIONS CHECKS GOOD. CLEARED PSEU MEMORY.

Part: DE-ICE SYS — MALFUNCTIONED (LT WING)

ANTI-ICE DUCT MESSAGE WITH -A/I+ ON LEFT WING LEADING EDGE RED ON ANTI-ICE SYNOPTIC PAGE. RETURNED TO SLC. LEFT WING SUFFICIENT OVERHEAT SENSOR CHANGED. OPS CHECK GOOD.

Part: PIN — NOT REMOVED (LANDING GEAR)

GEAR DISAGREE ON DEPARTURE FROM SLC. BURNED FUEL DOWN TO LANDING WEIGHT AND RETURNED TO SLC. FOUND GEAR PIN IN NOSE GEAR. REMOVED PIN.

Part: MECHANISM — OUT OF ADJUST (PAX DOOR)

PASSENGER DOOR LATCH RED MESSAGE CAME ON INFLIGHT. RETURNED TO OMA, ADJUSTED ROD END TO ROD THAT ROTATES UPPER TWO CAMS IAW MM 52-11-02. OPS CHECKS GOOD.

Part: WARNING — ILLUMINATED (PAX DOOR)

CLIMBING THROUGH 16,000 AN EICAS MESSAGE PAX DOOR LATCH WAS OBSERVED. FOLLOWED QRH AND AT 22,000 AN EICAS RED MESSAGE PAX DOOR CAME ON. FOLLOWED QRH AND DIVERTED TO IDA. CHECKED AIRCRAFT PSEU AND FOUND IN MEMORY S46 FAR IN MEMORY. HAD SLC MAINTENANCE FAX THE MM TO IDA FOR REFERENCE. USED MM 52-70-04. GROUND CHECKS GOOD.