N405SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,952 hrs · 38,576 cycles

NR 1 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 6498) RELAMPED EMERGENCY LIGHT.

Part: WINDOW — CRACKED (COCKPIT) · airframe 45,556 hrs · 38,252 cycles

FIRST OFFICERS SIDE WINDOW CRACKED. (FLT 4776) REPLACED RIGHT SIDE WINDOW IN REFERENCE TO CRJ 200 MM. P/N: NP-139322-12 S/N OFF: 93046H5242.

Part: WINDSHIELD — DAMAGED (COCKPIT) · airframe 45,556 hrs · 38,252 cycles

SMOKE IN THE COCKPIT. ISOLATED THE SMOKE TO THE PHENOLIC BLOCK ON THE FIRST OFFICER'S SIDE. (FLT 4762) REPLACED CO-PILOTS WINDSHIELD IN REFERENCE TO CRJ MM. P/N OFF: NP-139321-14 S/N OFF: 09156H2146

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,225 hrs · 37,944 cycles

EMERGENCY LIGHTS ARE OUT. (FLT 6299) CHARGED BATTERIES.

Part: SWITCHING UNIT — FAILED (THROTTLE QUAD) · airframe 45,165 hrs · 37,900 cycles

MULTIPLE GEAR INDICATION MESSAGES. (FLT 5492) REPLACED THROTTLE QUADRANT ADJUSTABLE CAM SWITCHING UNIT. PN: FE210-302, SN OFF: FR1008.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 45,110 hrs · 37,853 cycles

LEFT FUSELAGE SKIN AT STATION 411 BETWEEN STR 19 AND 20 LEFT IS DAMAGED. (FLT 4468) REPAIRED PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,048 hrs · 37,803 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4446) RELAMPED EMERGENCY LIGHT.

Part: COUNTERBALANCE — OUT OF RIG (CABIN DOOR) · airframe 44,937 hrs · 37,694 cycles

MAIN CABIN DOOR IS BINDING WHEN OPENING. (FLT 4623) ADJUSTED UPPER LATCH CAM ROD AND RIGGED DOOR COUNTER BALANCE FORWARD AND AFT IN REFERENCE TO AMM.

Part: RELAY — FAILED (ESSENTIAL BUS) · airframe 44,517 hrs · 37,337 cycles

EMERGENCY LIGHTS CAME ON IN FLIGHT, WERE ON WHENEVER LIGHTS WERE ARMED, WENT OFF WHEN SWITCH WAS OFF. (FLT 4665) REPLACED AC ESSENTIAL BUS RELAY IN REF TO AMM. P/N: V210D090BC

Part: ANGLE — CRACKED (LT WING LE) · airframe 44,309 hrs · 37,155 cycles

LEFT WING UPPER MID LEADING EDGE ANGLE CRACKED. REPLACED ANGLE AT LEFT WING UPPER MID AREA.

Part: ANGLE — CRACKED (RT WING LE) · airframe 44,309 hrs · 37,155 cycles

RIGHT WING UPPER MID LEADING EDGE ANGLE CRACKED. REPLACED RIGHT WING UPPER MID LEADING EDGE ANGLE.

Part: ATTACH BRACKET — CRACKED (LT WING LE) · airframe 44,309 hrs · 37,155 cycles

OUTBOARD SIDE ATTACH BRACKET OF LEFT INBOARD WING LEADING EDGE IS CRACKED. REPLACED OUTBOARD SIDE ATTACH BRACKET AT LEFT WING INBOARD LEADING EDGE.

Part: OIL SYSTEM — OVERSERVICED (LT ENGINE) · airframe 44,102 hrs · 36,970 cycles

RETURNED TO THE FIELD WITH LEFT ENGINE HIGH OIL TEMPERATURE. (FLT 6403) INSPECTED LEFT ENGINE OIL LEVEL FOUND TO BE OVERSERVICED, REMOVED 2 QTS OF OIL.

Part: HANDLE — DIRTY (CABIN DOOR) · airframe 44,078 hrs · 36,951 cycles

MAIN CABIN DOOR HARD TO OPEN FROM THE EXTERIOR. (FLT 5441) CLEANED AND LUBED EXTERIOR DOOR HANDLE.

Part: BRAKE — LOCKED (NR 2 MLG) · airframe 43,434 hrs · 36,397 cycles

NR 2 MLG BRAKE LOCKED UP AND NR 2 MLG TIRE IS FLAT. (FLT 5819) REPLACED BOTH NR 1 AND NR 2 MAIN LANDING GEAR WHEEL ASSEMBLIES AND REPLACED NR 2 BRAKE ASSEMBLY P/N: 5010571-1 S/N OFF: DEC836147 P/N: 5010571-1 S/N OFF: SEP110837 / P/N:5010520-1 S/N OFF: AUG00-2253.

Part: SHAFT — DEFECTIVE (CABIN DOOR) · airframe 43,191 hrs · 36,200 cycles

MCD IS DIFFICULT TO OPEN. (FLT 5819) REPLACED THE MAIN CABIN DOOR FORWARD COUNTER-BALANCE GUIDE SHAFT.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,406 hrs · 35,605 cycles

FLOOR INTERCOSTAL AT FS 484.0 CRACKED UNDER FLOOR. (C-CHECK) REPLACED FLOOR INTERCOSTAL AT FS 484.0 RIGHT OUTBOARD INTERCOSTAL.

Part: MOUNT — DAMAGED (RT ENGINE) · airframe 41,993 hrs · 35,256 cycles

RIGHT ENGINE FWD YOKE MOUNT UPPER END DAMAGED AND LOWER BUSHING PITTED. (ENGINE CHANGE) REMOVED AND REPLACED.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 41,960 hrs · 35,227 cycles

LEFT ENGINE FORWARD MOUNT LINK HAS PITTING CORROSION ON BUSHINGS. (C-CHECK) REPLACED BUSHINGS.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 41,960 hrs · 35,227 cycles

LEFT ENGINE FORWARD MOUNT LINK CLAMP-UP BUSHING HAS PITTING CORROSION. (ENGINE CHANGE) REPLACED BUSHING.

Part: DOOR — BINDING (CABIN) · airframe 41,941 hrs · 35,213 cycles

MAIN CABIN DOOR WAS DIFFICULT TO OPEN. (FLT 4761) REPOSITIONED AIRCRAFT TO LEVEL GROUND.

Part: ROLLER — OUT OF ADJUST (CABIN DOOR) · airframe 41,650 hrs · 34,979 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6518) ADJUSTED MAIN DOOR TOP SPIGOT ROLLERS AND ALL LATCH PINS PER AMM.

Part: CAM — OUT OF ADJUST (CABIN DOOR) · airframe 41,644 hrs · 34,974 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN FROM OUTSIDE. (FLT 4656) RIGGED LOWER CAM LOCK.

Part: HINGE — WORN (CABIN DOOR) · airframe 41,536 hrs · 34,887 cycles

OUTER DOOR HANDLE ON MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6900) REPLACED DOOR HINGE.

Part: FASTENER — BROKEN (ELEVATOR) · airframe 41,261 hrs · 34,655 cycles

WHEN DOING CONTROL CHECKS, THE LEFT ELEVATOR WILL NOT RETURN TO NEUTRAL. (FLT 4458) REPLACED HI-LOK PIN ON PCU/ELEVATOR INTERCONNECT BRACKET.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 41,142 hrs · 34,560 cycles

MAIN CABIN DOOR AND SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHTS INOP. (FLT 6311) OPERATIONAL CHECK NORMAL.

Part: HANDLE — OBSTRUCTED (CABIN DOOR) · airframe 40,922 hrs · 34,381 cycles

UNABLE TO OPEN MAIN CABIN DOOR FROM OUTSIDE. (FLT 3094) REMOVED DEBRIS AND CLEANED AROUND MAIN CABIN DOOR OUTER HANDLE.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 40,639 hrs · 34,129 cycles

FLT 5880 - EMERGENCY LIGHTS ILLUMINATED WITH SWITCH IN ARMED POSITION. RESET TRIPPED CIRCUIT BREAKER, OPERATION CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,948 hrs · 33,580 cycles

AFT RED ARROW ON EMERGENCY FLOOR STRIP IS NOT ILLUMINATED AT ROWS 9 AND 11. (FLT 5791) REPLACED FLOOR TRACK EMERGENCY LIGHT AT ROW 9 AND 11 IAW AMM 33-51-01.

Part: INVERTER — FAILED (CABIN) · airframe 39,880 hrs · 33,527 cycles

MAIN AND SERVICE DOOR EMERGENCY LIGHTS INOP. (FLT 6723) REPLACED NR 1 INVERTER.

Part: TORQUE SHAFT — OUT OF RIG (CABIN DOOR) · airframe 39,813 hrs · 33,471 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 4435) INSTALLED SHIMS ON INNER HANDLE TORQUE SHAFT.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 39,804 hrs · 33,464 cycles

MAIN DOOR HARD TO OPEN FROM OUTSIDE. (FLT 4530) LUBED LATCH PINS AND HANDLE.

Part: HANDLE — OUT OF POSITION (CABIN DOOR) · airframe 39,740 hrs · 33,408 cycles

MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. (FLT 6157) FOUND OUTER HANDLE IMPROPERLY STOWED. OPERATIONAL CHECKS NORMAL.

Part: DOOR — BINDING (CABIN) · airframe 39,583 hrs · 33,288 cycles

MAIN DOOR WILL NOT OPEN FROM OUTSIDE. (FLT 5800) OPERATIONAL CHECK NORMAL.

Part: LATCH — OUT OF RIG (CARGO DOOR) · airframe 39,035 hrs · 32,867 cycles

FLT 6015 - MCD OUTER HANDLE WOULD NOT OPEN. RIGGED LATCH CAM ASSEMBLY.

Part: DOOR — STIFF (MAIN PAX) · airframe 38,983 hrs · 32,824 cycles

FLT 4794 - MAIN CABIN DOOR VERY DIFFICULT TO OPEN. DOOR OPERATES NORMALLY.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 38,712 hrs · 32,628 cycles

C-CHECKM, SIDEWALL SEAT TRACK CORRODED. REPLACED TRACK SECTIONS PER SRM.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 38,712 hrs · 32,628 cycles

C-CHECK, RIGHT WINDSHIELD SIDE POST LOWER OUTBOARD CLIPS CRACKED. REPLACED PER SRM.

Part: BULKHEAD — CRACKED (BS 621) · airframe 38,712 hrs · 32,628 cycles

C-CHECK, FS 621 AFT PRESSURE BULKHEAD CRACKED. REPAIRED PER REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 38,712 hrs · 32,628 cycles

C-CHECK, FS 280 FORWARD FLOOR SUPPORT AT LBL9 AND RBL9 CRACKED. REPAIRED PER SRM.

Part: SKIN — CORRODED (PAX DOOR) · airframe 38,712 hrs · 32,628 cycles

C-CHECK, INNER SKIN OF PASSENGER DOOR CORRODED. REPAIRED PER REO.

Part: DOOR FRAME — CRACKED (BS 338) · airframe 38,712 hrs · 32,628 cycles

C-CHECK, PASSENGER DOOR FRAME AT FS 338 CRACKED. REPAIRED PER REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 38,712 hrs · 32,628 cycles

C-CHECK, FS 280 FLOOR SUPPORT BEAM CRACKED. REPAIRED PER REO.

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 38,712 hrs · 32,628 cycles

C-CHECK, AFT SIDE OF PRESSURE BULKHEAD HAS NUMEROUS CRACKS. REPAIRED PER REO.

Part: SKIN — DENTED (RT WING) · airframe 38,370 hrs · 32,372 cycles

FLT 1010 - TWO DENTS ON RIGHT LEADING EDGE AT WS 201.0 EXCEED LIMITS OF SRM. REPLACED LEADING EDGE SKIN PER SRM.

Part: ACCESS PANEL — CORRODED (PAX DOOR) · airframe 37,679 hrs · 31,775 cycles

PASSENGER DOOR SHOWS SIGNS OF CORROSION AROUND UPPER ACCESS PANELS. REPAIRED PAX DOOR PER REO 601R-52-11-1520.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 37,013 hrs · 31,237 cycles

FLT 6377 - WHEN EXTENDING GEAR ON APPROACH, RECEIVED A "GEAR DISAGREE" MESSAGE. MANUALLY EXTENDED THE GEAR. REPLACED MAIN GEAR SELECTOR VALVE IAW 32-32-10.

Part: O-RING — LEAKING (NLG STRUT) · airframe 36,079 hrs · 30,468 cycles

FLT 3920 - RECEIVED "GEAR DISAGREE" MESSAGE AFTER GEAR RETRACTION. REPLACED O-RINGS AND SEALS ON NOSE STRUT IAW AMM 32-21-30.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 36,049 hrs · 30,447 cycles

FLT 3835 - AFTER TAKEOFF RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN MESSAGE. REPLACED NOSE SELECTOR VALVE IAW MM 32-33-10. OPS CHECKS GOOD.

Part: SENSOR — MALFUNCTIONED (NLG CENTERING) · airframe 36,049 hrs · 30,447 cycles

FLT 3756 - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. INSPECTED NOSE GEAR AND ADJUSTED CENTERING SENSOR GAP IAW MM 32-61-05. OPS CHECKS GOOD.

Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 35,894 hrs · 30,329 cycles

FLT 6083 - NOSE GEAR DISAGREE SHORTLY AFTER GEAR RETRACTION. RETURNED TO FIELD. REPLACED NLG ACTUATOR IAW MM 32-33-01.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 35,804 hrs · 30,256 cycles

FLT 5889 - OXYGEN MASKS ABOVE SEATS 7A AND 7B DEPLOYED INADVERTANTLY ON LANDING. REPACKED OXYGEN MASKS IAW 35-21-09.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 35,753 hrs · 30,205 cycles

NOSE GEAR WILL NOT RETRACT, FLIGHT NR 3940. REPLACED NOSE LANDING GEAR SELECTOR VALVE AND PRIORITY VALVE IAW MM 32-33-15. NO DEFECTS NOTED, PN: 4622 SN ON: 440A SN OFF: 420.

Part: SKIN — DAMAGED (DAMAGED) · airframe 35,189 hrs · 29,745 cycles

LEFT LOWER FUSELAGE IS DAMAGED DUE TO CONTACT WITH GROUND EQUIPMENT WHILE PARKED ON RAMP. REPAIRED LOWER FUSELAGE PER REO 601R-53-11-1230 AND REO 601R-53-11-1231.

Part: ROLLER — BINDING (SERVICE DOOR) · airframe 34,673 hrs · 29,320 cycles

SERVICE DOOR IS DIFFICULT TO OPEN. REPLACED CAM ROLLER ON SERVICE DOOR INNER HANDLE ROLLER LATCH IAW MM 52-41-00. OPS CHECK GOOD.

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 34,288 hrs · 29,005 cycles

EMERGENCY LIGHTS ILLUMINATE IMMEDIATELY WHEN ARMED. REPLACED AC ESSENTIAL BUSS SENSE RELAY KIXD PER CRJ MM 24-51-27.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 34,488 hrs · 29,169 cycles

PASSENGER DOOR HAS CRACKED BRACKET UNDER THE CLOSING PLATE, DISCOVERED AT C-CHECK. INSTALLED NEW SUPPORT BRACKET PER CRJ200 SRM 51-41-02 PG 5.

Part: ATTACH BRACKET — CRACKED (FLOORBEAM) · airframe 34,488 hrs · 29,169 cycles

CABIN FLOORBEAM CLIP CRACKED AT FS484 RBL27, DISCOVERED AT C-CHECK. INSTALLED NEW CLIP AT CABIN FLOORBEAM FS 484 RBL 27 PER REO 601R-53-41-059.

Part: SUPPORT ANGLE — CRACKED (BS 720) · airframe 34,488 hrs · 29,169 cycles

STRUCTURE AT FS 720 UNDER RT PACK IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED NEW SUPPORT ANGLE P/N 601R95159-25 AND CLIP P/N 601R95159-37 UNDER RIGHT PACK PER CRJ200 SRM 51-42-06.

Part: WEB — CRACKED (PAX DOOR) · airframe 34,488 hrs · 29,169 cycles

THE FORWARD WEB ON THE PAX DOOR IS CRACKED IN THE RADIUS BETWEEN THE SECOND AND THIRD STEPS, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS 601R-52-11-1223 -2,-3,-4 AT PAX DOOR FORWARD WEB PER REO 601R-52-11-1223 SHTS 1-3.

Part: CONNECTOR — LOOSE (CABIN) · airframe 34,049 hrs · 28,828 cycles

FOUND FLOOR LEVEL EMERGENCY LIGHTS AFT OF ROW 8 ARE INOP. SECURED CONNECTOR AT ROW 12. OPERATIONAL CHECKS GOOD..

Part: SWITCH — MALFUNCTIONED (THRUST REVERSER) · airframe 33,188 hrs · 28,177 cycles

RT REVERSE UNLOCK CAUTION IN FLIGHT. ENGINE SHUTDOWN. REPLACED THE RT ENGINE THRUST REVERSER STOW SWITCH AND RIGGED IAW CRJ 200 MM 78-37-01 AND 78-30-00. OPERATIONAL CHECKS GOOD, PN: 228-50741-115-88308

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 33,132 hrs · 28,135 cycles

FLOOR LEVEL EMERGENCY LIGHTING AT ROW 1 INOP. RECONNECTED FIRST SECTION OF EMERGENCY FLOOR TRACK LIGHTING IAW MM 33-51-01. OPERATIONAL CHECKS GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,903 hrs · 27,179 cycles

EXIT SIGN ABOVE RIGHT SIDE OF ROW 8 DOES NOT ILLUMINATE. REPLACED BATTERY ASSY AT NR 1, NR 2, NR 3 AND NR 4 POSITION IAW 33-50-02 AND REPLACED TERMINAL BLOCK 105. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 31,883 hrs · 27,164 cycles

FWD LOWER LIGHTS ARE INOP. REPLACED FWD EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-02, OPERATIONAL CHECK GOOD.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 31,810 hrs · 27,110 cycles

PAX DOOR OUTER HANDLE JAMS, HARD TO OPEN PAX DOOR. ADJUSTED FWD SPIGOT ROLLER IAW MM 52-11-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,531 hrs · 26,908 cycles

FOUND FWD EMERGENCY LIGHT STRIP INOP. REPLACED FORWARD EMERGENCY LIGHT STRIP, OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (YAW DAMPER) · airframe 31,191 hrs · 26,647 cycles

"YD2 INOP" STATUS MSG. REPLACED YD2 IAW MM 22-22-01. OPERATIONAL CHECK GOOD.

Part: BATTERY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 30,957 hrs · 26,470 cycles

SERVICE DOOR FLOOR EXIT SIGN, MAIN CABIN DOOR FLOOR EXIT SIGN NOT ILLUMINATING. FIRST SECTION OF FLOOR EMERGENCY LIGHTS NOT ILLUMINATED. REPLACED EMERGENCY BATTERY PACK, INDICATORS, AND A WIRE SEGMENT. OPERATIONAL CHECK GOOD.

Part: ANGLE — CRACKED (RT WING) · airframe 31,351 hrs · 26,773 cycles

RT BATT ANGLE CRACKED, ITEM FOUND AT C CHECK INSPECTION. INSTALLED ANGLE DOUBLER PER REO 601R-57-51-046 REV 'B STEPS 5-10 OF RT BAT ANGLE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,351 hrs · 26,773 cycles

RT FS 280 CRACKED AT TOP SIDE, ITEM FOUND AT C CHECK INSPECTION. INSTALLED ANGLE IAW DWG 601R-11436 AT FS 280.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,351 hrs · 26,773 cycles

CRACKED ANGLE FS 625 RBL33 WL90.0 AFT SIDE PRESSURE BULKHEAD AFT EQUIPMENT BAY, ITEM FOUND AT C CHECK INSPECTION. INSTALLED NEW ANGLE TO AFT SIDE OF PRESSURE BULKHEAD AT FS625 RBL33 WL90.0 IAW CRJ200 SRM 51-42-06 PG 11-12.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 29,950 hrs · 25,691 cycles

STAB TRIM CH 1 WILL NOT ENGAGE. REPLACED HSTA IAW MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 29,815 hrs · 25,587 cycles

PILOT SIDE WINDOW CRACKED. REPLACED PILOT SIDE WINDOW IAW MM56-12-01, P/N NP-139322-5, S/N OFF 03105R1941.

Part: CONVERTER — MALFUNCTIONED (CABIN) · airframe 29,350 hrs · 25,226 cycles

AFT SECTION OF FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE. REPLACED NR 4 ELBP CONVERTER IAW CRJ MM 33-51-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 29,359 hrs · 25,231 cycles

LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED LEFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: SWITCH — STICKING (STAB TRIM) · airframe 29,226 hrs · 25,130 cycles

FOS TRIM SWITCH IS STICKY. REPLACED FOS TRIM SWITCH, OPERATIONAL CHECK GOOD IAW MM 27-41-00.

Part: CONTROL CABLE — MISROUTED (PAX DOOR) · airframe 28,633 hrs · 24,664 cycles

CABIN DOOR DIFFICULT TO CLOSE. REROUTED DOOR CABLE AS REQUIRED. OPERATED PAX DOOR SEVERAL TIMES. OPERATIONAL CHECKS GOOD.

Part: POTENTIOMETER — OUT OF ADJUST (TE FLAPS) · airframe 27,661 hrs · 23,899 cycles

RIGHT FLAP INDICATES 22 DEGREES AT 20 DEGREE SETTING. ADJUSTED RIGHT FLAP POSITION POTENTIOMETER IAW MM 27-55-01. OPERATIONAL CHECK SATISFACTORY.

Part: POTENTIOMETER — INACCURATE (FLAP INDICATOR) · airframe 27,295 hrs · 23,610 cycles

DURING TAXI-OUT, RIGHT FLAP INDICATES 2 DEGREES MORE THAN LEFT FLAP. TAXI BACK TO GATE. ADJUSTED THE RIGHT FLAP INDICATOR POTENTIOMETER IAW AMM 27-55-01. OPERATIONAL CHECK GOOD.

Part: OVERHEAT LOOP — MALFUNCTIONED (LT ENGINE) · airframe 26,748 hrs · 23,176 cycles

LOOP-B ON LT JETPIPE HAS BEEN PRODUCING FAIL MESSAGES. REMOVED AND REPLACED ALL A & B EYELET CONNECTIONS AS REQUIRED. OPS CHECKS GOOD AT THIS TIME IAW MM 26-11-0.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILER) · airframe 26,748 hrs · 23,176 cycles

LARGE ROLLING MOMENT WHEN FLIGHT SPOILERS EXTENDED. INSTALLED SERVICEABLE PCU ON RIGHT SPOILER IAW 27-62-01. OPS CHECKS GOOD.

Part: OVERHEAT LOOP — FALSE ACTIVATION (LT ENGINE) · airframe 26,690 hrs · 23,133 cycles

LEFT JET OVERHEAT CAUTION MESSAGE. INSTALLED SERVICEABLE JET PIPE ON LT ENG. LT PIPE OVERHEAT TESTS GOOD LOOPS ''A & B''.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 26,690 hrs · 23,133 cycles

MACH TRIM WILL NOT ENGAGE. REMOVED AND REPLACED STALL PROTECTION COMPUTER. OPS CHECK SATISFACTORY IAW CRJ MM 27-35-01 AND WM 34-13-00.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

MAIN FUSELAGE; PRESSURE FLOOR WEB CRACKED; FS 469.00 LBL 9.0 TO RBL 9.0. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRED PRESSURE FLOOR CUTOUT IAW CRJ REO 601R-53-41-102 REV. NC.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

CARGO PIT FLOORBEAM ANGLE REPAIR ANGLE CRACKED AT FS 621.00 LBL 42.0. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED REPAIR ANGLE IAW CRJ REO 601R-53-61-117 REV. A AND RII53-401.

Part: ATTACH ANGLE — CRACKED (FLOORBEAM) · airframe 26,640 hrs · 23,091 cycles

FS 280 LEFT FLOORBEAM RBL 9 INBOARD ATTACH ANGLE CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-06, 51-42-21, 21-23-00, 51-25-00, 51-42-36 AND 51-21-11 AND RII 53-401.

Part: FLOORBEAM — DISTORTED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

CARGO PIT FLOORBEAM SIDE WEB BUCKLED AND DISTORTED; FS 589.00 - FS 605.00; LBL 27.0; OUTBOARD SIDE. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED WEB IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-25-16, AND REO 601R-53-61-989 REV., RII 53-401.

Part: BEAM — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

FS 409 AND 128 RIGHT VERTICAL POST RBL 27 LOWER INBOARD FLANGE CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) MADE REPAIR PART AND INSTALLED IAW CRJ REO 601R-53-41-056 REV. NC. REF. RII 53-401.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

FS621 BULKHEAD LEFT VERTICAL STIFFENER LBL 9.0 UPPER ATTACH CLIP CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-21, 51-23-00. REF. RII 53-401.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 26,640 hrs · 23,091 cycles

DISCOVERED DURING C-CHECK INSPECTION, FS 621 BULKHEAD VERTICAL STIFFENER BL 0 UPPER CLIP CRACKED. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-21, 51-23-00. REF. RII53-401.

Part: INTERCOSTAL — CHAFED (HYD SYSTEM) · airframe 26,640 hrs · 23,091 cycles

CHAFE IN NR 1 HYDRAULIC MANIFOLD ATTACH INTERCOSTAL AT FS 712.00 BEYOND LIMITS. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 26,640 hrs · 23,091 cycles

FS621 BULKHEAD RIGHT VERTICAL STIFFENER RBL 9.0 UPPER ATTACH CLIP CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-21, 51-23-00. REF. RII 53-401.

Part: ATTACH ANGLE — CRACKED (FLOORBEAM) · airframe 26,640 hrs · 23,091 cycles

FS 280 RIGHT FLOORBEAM RBL 9 OUTBOARD ATTACH ANGLE CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-40-13, 51-42-21, 51-23-00, 51-25-00, AND 51-24-36

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

RT FIREWALL SHUTOFF VALVE SUPPORT INTERCOSTAL AFT ANGLE IS CRACKED FS 654 ADJACENT STR 9. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED ANGLE IAW CRJ SRM 51-40-11, AND 51-42-06.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

FS 625 RIGHT INTERCOSTAL STR 14R IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) INTERCOSTAL REPLACED IAW CRJ SRM 51-40-11, 51-42-06.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

FS 364 STR 8R IS CRACKED FROM FASTENER HOLES ON UPPER AND LOWER FRAME TO SKIN FLANGE. (DISCOVERED DURING C-CHECK INSPECTION) FABRICATED, FIT, DRILLED AND INSTALLED ALL THE REPAIR PARTS IAW CRJ REO 601R-53-21-501 REV. NC.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

DISCOVERED DURING C-CHECK INSPECTION, CARGO PIT; FUSELAGE FRAME AT FS 589.00 HAS 1 CRACKED FLANGE THAT ATTACHES TO STR 18L LOWER SIDE. REPAIRED IAW CRJ REO 601R-53-61-999 REV. A. REPAIRED IAW CRJ REO 601R-53-61-999 REV. A.

Part: FITTING — CRACKED (FLOORBEAM) · airframe 26,640 hrs · 23,091 cycles

MAIN FUSELAGE; FS 460 RBL 9.0 OB FLOORBEAM FITTING CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED FITTING IAW CRJ SRM 51-40-11, 51-41-06, 51-23-00, 51-42-06, 51-23-00, 51-42-21, 51-21-11, 51-25-16, AND RII 53-401.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

FS 625 LEFT INTERCOSTAL STR 14L IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) INTERCOSTAL REPLACED AT FS625 STR 14LH IAW CRJ SRM 51-40-11, 51-42-06.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

FS621 BULKHEAD LEFT VERTICAL STIFFENER LBL 18 UPPER ATTACH CLIP CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-21, 51-23-00. REF. RII 53-401.

Part: FRAME — CORRODED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

FRAME SECTOR AT FS 349 BETWEEN STR 24 LT AND 24 RT IS CORRODED BEYOND LIMITS. FRAME SECTOR REPLACED IAW CRJ SRM 51-40-11, 51-42-06 AND RII 53-401. (DISCOVERED DURING C-CHECK INSPECTION)

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

CARGO PIT; TRANSVERSE BEAM ATTACH ANGLES FOR DOOR STOP FITTINGS ARE CRACKED; FS 589.00 AND FS 605.00 LBL 42.0. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, AND 51-25-16 AND RII 53-401.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

FS 559 PRESSURE WEB AT RBL 10 AND 18 CRACKED AT AILERON BELLCRACK MOUNTING POINTS. (DISCOVERED DURING C-CHECK INSPECTION) WEB REPAIRED IAW CRJ REO 601R-53-41-207 REV. NC AND RII53-401.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 26,796 hrs · 23,208 cycles

FS 280 RIGHT FLOORBEAM ANGLE RBL 9.0 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPAIRED IAW CRJ REO 601R-53-11-136 REV NC AND RII 53-401.

Part: BEAM — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

FS 559 VERTICAL POST LBL 9.0 INBOARD AND OUTBOARD LOWER FLANGES CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRED POST IAW CRJ REO 601R-53-41-057 REV. NC. REF. SKYWEST RII 27-414 AND RII 53-401.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

DISCOVERED DURING C-CHECK INSPECTION, CARGO PIT; FUSELAGE FRAME AT FS 605.00 HAS 2 CRACKED FLANGES THAT ATTACH TO STR 18L.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

MAIN FUSELAGE; PULLEY INTERCOSTAL INBOARD REMOTE ANGLE IS CRACKED AT FS 484.00 LBL 27.0. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED ANGLE IAW CRJ REO 601R-53-41-059 REV. A AND RII 53-401.

Part: INTERCOSTAL — CRACKED (HYD MANIFOLD) · airframe 26,640 hrs · 23,091 cycles

CRACK IN NR 1 HYDRAULIC MANIFOLD ATTACH INTERCOSTAL AT FS 718.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,640 hrs · 23,091 cycles

FS 379 STR 8R IS CRACKED FROM FASTENER HOLE IN UPPER FRAME TO SKIN FLANGE. (DISCOVERED DURING C-CHECK INSPECTION) FABRICATED, FIT, DRILLED AND INSTALLED ALL THE REPAIR PARTS IAW CRJ REO 601R-53-21-501 REV. NC.

Part: BRACKET — CORRODED (DOOR SILL) · airframe 26,796 hrs · 23,208 cycles

PAX DOOR SILL BRACKETS AND CLEATS AT FS 316 AND FS 343 CORRODED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SILL BRACKETS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 26,796 hrs · 23,208 cycles

SERVICE DOOR; FRAME TO SILL ANGLE IS CORRODED AT FS 349.00. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED CORRODED ANGLE IAW CRJ SRM 51-42-21, 51-40-11, 51-23-00, 51-42-21, 20-21-00.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,796 hrs · 23,208 cycles

MAIN FUSELAGE; PRESSURE FLOOR/WING TIE BEAM FITTING IS DENTED AND CRACKED ALONG LOWER FLANGE; LBL 3.0 FS 460.00. DISCOVERED DURING C-CHECK INSPECTION. NEW TIE BEAM FIT, DRILLED AND INSTALLED IAW CRJ SRM 51-40-11.

Part: FLOORBEAM — CUT (FUSELAGE) · airframe 26,796 hrs · 23,208 cycles

MAIN FUSELAGE; FLOORBEAM CUT ALONG BOTTOM FLANGES, FS 467.0; LBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO-53-41-211.

Part: CONTROL LEVER — MALFUNCTIONED (FLIGHT SPOILER) · airframe 26,159 hrs · 22,729 cycles

IN FLIGHT, THE FLIGHT SPOILER FAULT MESSAGE CAME ON. REMOVED AND REPLACED FLIGHT SPOILER CONTROL LEVER IAW AMM 27-61-01. OPS CHECKS GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 25,889 hrs · 22,515 cycles

AUTOPILOT SELF-DISCONNECTED SEVERAL TIMES ON APPROACH. REMOVED AND REPLACED FCC NR 2 IAW MM 22-12-14. AUTOPILOT OPS CHECK GOOD IAW MM 22-11-00.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 25,544 hrs · 22,233 cycles

ON TAXI INTO SLC FLT SPOILER MESSAGE ON EICAS. REPLACED RIGHT INBOARD FLIGHT SPOILER PCU WITH SERVICEABLE UNIT IAW CRJ MM 27-62-01. LEAK AND OPS CHECKS OK. S/N OFF: 0038.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 25,435 hrs · 22,149 cycles

SPOILERONS FAULT MESSAGE AND FLIGHT SPOILERS FAULT - LEFT SPOILERON MESSAGE. REMOVED AND REPLACED NR 1 AND NR 2 SECU IAW 27-61-05. OPS CHECKS GOOD IAW 27-64-00. P/N OFF: 49-164-06, S/N OFF: 01397, S/N ON: 01455.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 25,344 hrs · 22,076 cycles

FLIGHT SPOILER FAULT STATUS MSG ON TAXI RESET CB'S 1N8, 1F3, 2N8, 2F3, 4A2, 4A3, 4A4, 4A5 IAW MX CONTROL. MESSAGE WENT AWAY. REMOVED AND REPLACED NR 1 SECU IAW MM 27-61-05. OPS CHECKS GOOD. S/N OFF 0273

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERONS) · airframe 25,264 hrs · 22,019 cycles

SPOILERON STATUS MSG WHEN RIGHT SPOILERON FULLY DEPLOYED. IF LEFT UP FOR SEVERAL SECONDS, INBOARD GROUND SPOILER FAULT FOLLOWS. ROLL DISCONNECT CREATES A SPOILERON CAUTION MSG WHEN RIGHT SPOILERON DEPLOYED.REMOVED AND REPLACED NR 2 SECU IAW MM 27-61-05. OPS CHECK GOOD.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 25,239 hrs · 22,001 cycles

FLIGHT SPOILER STATUS MESSAGE. RESET CB'S. REPLACED LEFT SPOILERON SYSTEM 1 ACTUATOR PER MM 27-62-01. LEAK AND OPS CHECK OK.

Part: PCU — FAILED (SPOILER) · airframe 24,909 hrs · 21,746 cycles

FLIGHT SPOILER FAULT MESSAGE DURING TAXI. RESET BREAKERS, FAULT DID NOT CLEAR. REMOVED AND REPLACED RIGHT OUTBOARD FLIGHT SPOILER PCU. OPS CHECK GOOD IAW 27-62-01. SN OFF: MAL 0278

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,765 hrs · 21,629 cycles

EMERGENCY EXIT LIGHT NEXT TO PAX DOOR INOP. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT ASSY. OPS CHECK GOOD. P/N: 36527-1

Part: MECHANISM — DAMAGED (NLG DOOR) · airframe 24,347 hrs · 21,292 cycles

HYDRAULIC SYSTEM NR 3 PRESSURE BLEEDS OFF ALLOWING THE NOSE DOOR TO OPEN IN FLIGHT. REMOVED AND REPLACED RIGHT NOSE LANDING GEAR ''DOOR OPERATION MECHANISM'' PIVOT BOLT FOR CAM ROLLER. ALSO CLEANED AND LUBED ASSOCIATED HARDWARE. OPERATIONAL CHECKS GOOD IAW 32-22-15. REMOVED AND REPLACED NOSE DOOR MANUAL BYPASS VALVE IAW CRJ MM 32-34-40. PERFORMED FUNCTIONAL CHECK OF LANDING GEAR IAW CRJ MM 32-34-00, 32-30-00. OPS CHECK GOOD AND LEAK CHECK GOOD.

Part: WIRE — DAMAGED (FLAP INDICATOR) · airframe 23,372 hrs · 20,554 cycles

FLAPS INDICATE DIFFERENT VALUES AT 20 DEGREE SETTING. RETURNED TO GATE. REINSTALLED WIRE AT PIN 40 P211, RE-POWERED AND INITIALIZED FLAP SYSTEM. PERFORMED EXTENSIVE OPS CHECK OF FLAPS. ALL INDICATION FOUND TO BE MATCHED AND NORMAL.

Part: DETECTOR — MALFUNCTIONED (LEFT) · airframe 23,185 hrs · 20,396 cycles

CAPTAIN'S HEADING 5-10 DEGREES OFF FROM COMPASS AND FIRST OFFICER'S. RECEIVED SEVERAL EFIS COMP MON CAUTION MESSAGES. PERFORMED QRH PROCEDURE AND RETURNED TO SLC. REMOVED AND REPLACED LT FLUX DETECTOR UNIT IAW MM 34-21-04. DEGAUSSED WINGS AND LANDING GEAR. OPS CHECK OF HEADING SYSTEM GOOD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 22,911 hrs · 20,194 cycles

FS 280.0 RBL AND LBL 9.0 FLOORBEAM INBOARD ANGLES CRACKED. FOUND DURING C CHECK INSPECTION, NEW ANGLES FITTED AND INSTALLED IAW CRJ SRM 51-40-11, 51-42-06 AND 51-42-20.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 22,911 hrs · 20,194 cycles

INTERCOSTAL AT FS 404.0 AND RBL 1.5 IN AVIONICS CRAWL WAY AFT OF MAIN AVIONICS DOOR HAS SURFACE CORROSION ON SIDE OF INTERCOSTAL, BEYOND LIMITS. FOUND DURING C-CHECK INSPECTION, NDT-ET CONDUCTIVITY CARRIED OUT AND FOUND MATERIAL TO BE 30.20 PERCENT IACS. INTERCOSTAL REMOVED AND REPLACED IAW CRJ SRM 51-23-00 AND 51-42-06 AND 51-40-11.

Part: WIRE — BROKEN (RUDDER TRIM) · airframe 22,644 hrs · 19,991 cycles

RUDDER TRIM WILL MOVE LEFT, BUT NOT RIGHT. SOLDERED BROKEN TERMINAL/WIRE CONTACT ON RUDDER TRIM CONTROL KNOB. OPS CHECK GOOD.

Part: RIB — CRACKED (LEFT PYLON) · airframe 22,911 hrs · 20,194 cycles

RIB AT AFT LOWER ATTACH SCREW OF LEFT PYLON LEADING EDGE PANEL IS CRACKED. FOUND DURING C CHECK INSPECTION. REPLACED RIB IAW CRJ SRM 51-42-06 & 51-23-11. P/N: 601-37004-85.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,911 hrs · 20,194 cycles

FUSE FRAME AT FS 640.0 IS CRACKED AT STR 9 CUTOUT. FOUND DURING C CHECK INSPECTION, HFEC INSPECTION CARRIED OUT ON CUTOUT EDGE AND AREA AS REQUIRED IAW REO 601R-53-61-532. NO CRACKS FOUND. REPAIRED FRAME IAW CRJ REO 601R-53-61-532 REV NC.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,911 hrs · 20,194 cycles

FUSE FRAME AT FS 718 CRACKED ON RIGHT SIDE AT STR 11. FOUND DURING C-CHECK INSPECTION, HFEC INSPECTION CARRIED OUT ON CUTOUT REPAIR EDGE AND AREA AS REQUESTED IAW RJ NDTM 51-20-01. NO CRACKS FOUND. REPAIRED FRAME IAW CRJ REO 601R-53-61-193 REV A ANGLE.

Part: SWITCH — DEFECTIVE (COCKPIT) · airframe 22,234 hrs · 19,673 cycles

YAW DAMPER CH 1 INTERMITTENT, WILL NOT STAY ENGAGED. RETURNED TO THE GATE. REMOVED AND REPLACED CAPTAIN'S STAB TRIM DISCONNECT SWITCH. YAW DAMPER SYSTEM, OPS CHECKS GOOD.

Part: BPSU — FAILED (T/E FLAP) · airframe 21,835 hrs · 19,355 cycles

FLAP FAIL MESSAGE ON CLIMBOUT. RECEIVED THE FAIL MESSAGE FROM FLAPS 8 DEGREES TO 0 DEGREES. UPON LANDING AND CHECKING THE FLAPS, FLAPS WERE AT 0 DEGREES OR FULLY UP. REMOVED AND REPLACED FLAP BRAKE POSITION SENSOR IAW MM 27-51-10. OPS CHECKED GOOD.

Part: BPSU — FAILED (T/E FLAP) · airframe 21,807 hrs · 19,330 cycles

FLAPS FAIL CAUTION MESSAGE ILLUMINATED. REPLACED RIGHT BPSU. OPS CHECKS GOOD.

Part: A/C PACK — MALFUNCTIONED (A/C BAY) · airframe 21,780 hrs · 19,311 cycles

AFTER TAKEOFF, SWITCHED BLEEDS PER SINGLE PACK OPERATIONS. RECEIVED A HIGH PACK PRESSURE CAUTION MESSAGE ON THE LEFT PACK. RESET BUT PACK HIGH PRESSURE CAUTION CAME BACK. RETURNED TO OAK. OPERATED THE AIRCRAFT AT TAKEOFF POWER AFTER REPAIRING THE RIGHT PACK. BOTH PACKS OPERATE NORMALLY WITH NO HIGH PRESSURE WARNINGS.

Part: CONTROLLER — MALFUNCTIONED (RUDDER) · airframe 21,465 hrs · 19,070 cycles

RUDDER TRIM SWITCH OPERATES RUDDER TRIM TO THE LEFT ONLY. REPLACED RUDDER AND AILERON TRIM CONTROL PER 27-12-10. OPS CHECK GOOD.

Part: BLADE — DAMAGED (LT ENGINE) · airframe 21,058 hrs · 18,762 cycles

ON TAKEOFF ROLL, LARGE VIBRATION/NOISE FELT THROUGHOUT AIRCRAFT FELT ON RUDDER PEDALS AND THRUST LEVERS. FOUND DAMAGE TO LEFT ENGINE NR 8 & 9 FAN BLADES. REMOVED AND REPLACED NR 8, 9, 22 & 23 LEFT ENGINE FAN BLADES WITH SERVICEABLE UNITS. PERFORMED RUN CHECKS. OPS CHECKS GOOD. NO VIBRATION NOTED. BLADE NR 8 P/N ON 6018T30P06, S/N OFF KGAJ0009. BLADE NR 9 P/N ON 6018T30P06, S/N OFF KGAR9905. BLADE NR 22 P/N ON 6018T3P06, S/N OFF KGAJ0051. BLADE NR 23 P/N ON 6018T3P06, S/N OFF KGAJ0384.

Part: BPSU — FAILED (T/E FLAP) · airframe 20,967 hrs · 18,694 cycles

PRIOR TO FAF AT IDA, WHEN F/O CALLED FLAPS 8 RECEIVED A (FLAP FAIL) AMBER MESSAGE. CONSULTED QRH. FLAPS WERE STUCK AT 8 DEGREES. RETURNED TO SLC. LEFT BPSU FAILED BRAKE CHECK. REMOVED AND REPLACED LEFT BPSU. PERFORMED OPERATIONAL CHECKS, NO FAULTS NOTED. REF MM 27-51-10.

Part: ACCESS PANEL — OPEN (NOSE DOOR) · airframe 20,187 hrs · 18,091 cycles

LOUD SQUEAL COMING FROM RIGHT SIDE OF NOSE ON TAKEOFF. DIVERTED TO SLC.INSPECTED FORWARD PORTION OF A/C. FOUND FORWARD RIGHT SIDE NOSE DOOR ACCESS PANEL OPEN. NO DAMAGE. CHECKS GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 19,754 hrs · 17,737 cycles

TAKEOFF ABORTED DUE TO HIGH ITT WARNING. OBSERVED 902 DEGREES CENT. BEFORE TRIPLE CHIME AND WARNING MESSAGE APPEARED. BTMS WENT TO 8 ON LEFT SIDE. OPERATED ENGINES AS REQUIRED IAW GE MM 72-00-00. ENGINE PARAMETERS WITHIN LIMITS. NO DISCREPANCIES NOTED AT THIS TIME.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 19,816 hrs · 17,788 cycles

AFTER TAKEOFF, HIGH SPEED CHECKER BOARD CAME DOWN TO 230 KIAS AND LATER FILLED ENTIRE SPEED TAPE. DUE TO FLAP SYSTEM DEFERRAL AIR DATA SYSTEM AND EICAS BELIEVED FLAPS WERE IN A POSITION OTHER THAN ZERO, THUS CAUSING HIGH SPEED TAPE TO BE LOWER. FLAP DEFERRAL HAS BEEN CLEARED AND HIGH SPEED TAPE INDICATION IS NOW NORMAL.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 4,368 hrs · 3,908 cycles

SMOKE CARGO MESSAGE AND ASSOCIATED AURAL WARNINGS SOUNDED MOMENTARILY AND THEN EXTINGUISHED. REMOVED AND REPLACED FORWARD AND AFT SMOKE DETECTORS. OPS CHECK GOOD ON BOTH. FWD S/N ON 2012, S/N OFF 2130, AFT S/N ON 2875, S/N OFF 0326.

Part: WINDOW — CRACKED (COCKPIT) · airframe 19,081 hrs · 17,165 cycles

ON LANDING THE RIGHT SIDE WINDOW CRACKED. REMOVED AND REPLACED RIGHT SIDE SIDE WINDOW IAW 56-12-01; RII 56-401. OPS CHECK GOOD. P/N ON PPG-NP-139322-6, S/N ON 00320H3690, S/N OFF 92016H6381.

Part: COUPLING — LOOSE (BLEED AIR) · airframe 18,854 hrs · 16,967 cycles

LEFT 14TH DUCT WARNING ILLUMINATED AFTER TAKEOFF. FOLLOWED QRH RETURNED TO AIRPORT FOR LANDING. RAN THE LEFT ENGINE AND FOUND THE LEFT 14TH STAGE PYLON SECTION BLEED AIR TUBE FORWARD CHECK BAND COUPLING LOOSE. TIGHTENED CLAMP RAN ENGINE IAW MM 21-00-00. BLEED AIR TUBE LEAK CHECKS GOOD IAW MM 30-20-01. RAN ENGINE FOR 30MINS WITH NO 14TH DUCT WARNING MESSAGE NOTED.

Part: RELAY — FAILED (APR SYSTEM) · airframe 17,874 hrs · 16,095 cycles

APR INOP ON TAKEOFF ROLL. ABORTED TAKEOFF FAT - DEFERRED APR. REMOVED AND REPLACED APR ARM RELAY (KIKL) IN JB5 MM 76-13-01. RAN BOTH ENGINES APR TESTS NR 1, 2, 3, FUNCTION NORMALLY.

Part: LATCH — LACK OF LUBE (CARGO DOOR) · airframe 17,659 hrs · 15,899 cycles

AFTER TAKEOFF, CARGO DOOR CAUTION MESSAGE CAME ON. RETURNED TO FIELD. LUBED CARGO DOOR LATCH AND CHECKED IAW MM 52-31-02. OPS CHECKS GOOD.

Part: PCU — FAILED (SPOILERS) · airframe 17,504 hrs · 15,761 cycles

ON TAKEOFF ROLL AT 120 KTS ''TO CONFIG SPOILERS'' ORAL AND RED MESSAGE. ABORTED TAKEOFF. AC FERRIED TO SLC. REMOVED AND REPLACED LEFT OUTBOARD SPOILERON PCU. OPS CHECKS GOOD.

Part: CONTROLLER — MALFUNCTIONED (SPOILERS) · airframe 17,489 hrs · 15,746 cycles

RED ''CONFIG SPOILER'' MESSAGE ON TAKEOFF. ABORT AT 70 KNOTS. INSPECT SPOILERS. CHECKED FOR FAULTS ON SECU''S AND CLEARED FAULTS PER 27-61-05. ALL CHECKS GOOD. (NO FAULTS FOUND).

Part: CONTROLLER — MALFUNCTIONED (SPOILER SYSTEM) · airframe 17,062 hrs · 15,352 cycles

CONFIG SPOILERS MESSAGE CAME ON DURING TAKEOFF ROLL AT 95 KIAS. ABORTED TAKEOFF AND RETURNED TO GATE. UPON GATE ARRIVAL STATUS MESSAGE FLT SPLRS FAULT WAS AND IS DISPLAYED. ON TAKEOFF ROLL TO CONFIG OK, MSG OK WAS PRESENT UNTIL THE NEED TO ABORT. POWERED DOWN AND RESET SPOILER SYSTEM, OPS CHECKS NORMAL.

Part: ADC — FAILED (NR 1) · airframe 15,922 hrs · 14,296 cycles

EFIS COMP MONITOR FLAGGED IAS AFTER TAKEOFF RIGHT AIRSPEED INDICATOR MATCHES STAND BY AIRSPEED. DIVERTED TO LAX. PURGED PITOT AND STATIC LINES IAW MM 341100. PERFORMED OPS CHECK OF ADC IAW MM 341301, OPS AND LEAK CHECK GOOD. REMOVED AND REPLACED NR 1 AIR DATA COMPUTER IAW CRJ MM 341301. PERFORMED PITOT STATIC CHECK OF AIR DATA SYSTEM IAW CRJ 341100, OPS AND LEAK CHECK GOOD. (P/N 8220372140) (S/N 1022) ON, (S/N 1102) OFF.

Part: OIL SYS — REQD SERVICE (APU)

EN ROUTE TO HLN CLIMBING THROUGH 28,000 FT, RECEIVED AN APU LOW OIL PRESSURE LIGHT ON EICAS ONE. RETURNED TO SLC. SERVICED APU OIL TO CORRECT LEVEL. INSPECTED APU AND OBSERVED NO LEAKS OR OTHER ABNORMALITIES. OPS CHECKS GOOD AT THIS TIME.

Part: SERVICE DOOR — NOT CLOSED (OXYGEN COMPT)

AFTER TAKEOFF, A VERY LOUD SQUEAL WAS HEARD ALONG WITH IAS STALL FAIL, MACH TRIM AND EFIS COMP. RETURNED TO SLC. SECURED OXYGEN SERVICE DOOR IN FRONT OF RIGHT PITOT TUBE. ALL SYSTEMS FUNCTION NORMAL.

Part: HEAT MESSAGE — ACTIVATED (RT AOA)

RIGHT AOA HEAT MESSAGE CAME ON AFTER TAKEOFF. RETURNED TO SLC. POWERED SYSTEM DOWN AND BACK UP. OPS CHECK GOOD. COULDN'T DUPLICATE PROBLEM.

Part: UPLOCK ACTUATOR — FAILED (NLG)

GEAR DISAGREE ON TAKEOFF RETRACTION. RETURNED TO SLC. REMOVED AND REPLACED UPLOCK ACTUATOR IAW MM 32-33-01 AND 32-33-05. OPS CHECK AND LEAK CHECK GOOD. REMOVED AND REPLACED NLG RETRACTION ACTUATOR.

Part: PITOT SYST — NOISE (COCKPIT)

IMMEDIATELY AFTER TAKEOFF FROM SLC, LEFT AND RIGHT IAS MESSAGES APPEARED FOLLOWED BY STALL FAIL, MACH TRIM ALSO HIGH PITCH NOISE FOLLOWED BY VERY UNRELIABLE AIRSPEED INDICATION FROM CO-PILOTS AIRSPEED INDICATOR. AS AIRCRAFT SLOWED DOWN, LOUD NOISE WENT AWAY. RETURNED TO SLC. PITOT STATIC OPS CHECKS PITOT STATIC SYSTEM IAW MM 34-11-00. VERIFIED PITOT STATIC DRAINS CONTAINED NO WATER. UNABLE TO DUPLICATE SYSTEM FAILURE OR HAVE ANY HIGH PITCHED NOISES.

Part: WINDOW — CRACKED (RT COCKPIT)

CO-PILOTS SIDE WINDOW CRACKED ON DESCENT INTO PDX. REMOVED AND REPLACED RIGHT SIDE WINDOW IAW MM 56-12-01. OPS CHECKS GOOD.

Part: SERVICE DOOR — NOT CLOSED (CABIN)

CABIN DOOR WAS WHISTLING BADLY AND CABIN WOULDN'T PRESSURIZE ABOVE 6.2 PSI. RAMPERS LEFT THE SIDE SERVICE DOOR OPEN. RETURNED TO SLC. CHECKED PRESSURIZATION IAW MM 21-31-00. ALL CHECKS GOOD. CLEANED AND INSPECTED PASSENGER AND SERVICE DOOR SEALS WITH NO DEFECTS NOTED. PRESSURIZED AIRCRAFT, ALL CHECKS GOOD AND NO SQUEALS NOTED.

Part: BULKHEAD — CRACKED (BS 409)

DISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128.

Part: ANGLE — CORRODED (CABIN)

LEFT SUPPORT ANGLE IN FRONT OF PASSENGER DOOR HAS CORROSION. REMOVED, FABRICATED NEW ANGLE FROM S3992 MATERIAL AND INSTALLED ON LOWER PASSENGER DOOR ENTRY WAY, IAW SRM 51-24-36.

Part: ANGLE — CORRODED (CABIN)

RIGHT SUPPORT ANGLE IN FRONT OF SERVICE DOOR HAS CORROSION. REMOVED, FABRICATED NEW ANGLE FROM S3992 MATERIAL AND INSTALLED ON LOWER SERVICE DOOR ENTRY WAY IAW SRM 51-24-36.

Part: AHARS — INOPERATIVE (LT COCKPIT)

CAPT AHARS INOP. NO HDG/ATT AFTER TAKEOFF. RETURNED TO SLC. INITIALIZED NR 1 AHARS, OPS CHECKS GOOD AT THIS TIME.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR)

CARGO DOOR CAUTION CAME ON CLIMBING OUT OF APPROXIMATELY 16,000 FEET AND STAYED ON UNTIL DESCENDING OUT OF 14,300 FEET. RETURNED TO SLC. FOUND CARGO DOOR PROXIMITY SWITCH TO BE OUT OF THE .50 INCH GAP. READJUSTED CARGO DOOR HANDLE PROXIMITY SWITCH IAW MM 52-70-02. OPS CHECK OF CARGO DOOR WARNING MESSAGE CHECKS GOOD.

Part: CABLES — MALFUNCTIONED (TE FLAPS)

FLAPS FAIL CAUTION MESSAGE DURING APPROACH. REMOVED AND REPLACED FLEX DRIVE CABLES, RAN FLAPS AND OPS CHECKS GOOD.

Part: WIRE — LOOSE (TE FLAPS)

WHEN FLAPS ARE SELECTED FROM ZERO DEGREES TO 8 DEGREES, OR 20 DEGREES DOWN, FLAP FAIL MESSAGE COMES ON AND THE FLAP WILL NOT MOVE OUT OF ZERO DEGREES. EN ROUTE TO BILLINGS BUT RETURNED TO SLC. REPAIRED A WIRE AT THE LEFT BPSU CANNON PLUG. RAN FLAPS SEVERAL TIMES. OPS CHECKS GOOD.

Part: SENSOR — CHAFED (BLEED AIR)

RIGHT 14TH DUCT RED EICAS MESSAGE DURING CLIMB. MESSAGE OUT WITHIN 2 MINUTES OF POWER REDUCTION TO IDLE. MESSAGE RETURNED AT CLIMB POWER EVEN WITH 14TH STAGE VALUE CLOSED. AFTER POWER REDUCTION TO IDLE AGAIN, LIGHT OUT. WARNING RETURNED AND STAYED ON AFTER LANDING AND ENGINE WAS SHUTDOWN. FOUND CHAFED 14TH STAGE BLEED AIR SENSOR ELEMENT. REMOVED AND REPLACED ELEMENT IAW MM 36-21-00, DUCT OPS TEST GOOD.

Part: SKIN — DENTED (LT TE FLAP)

ABORTED TAKEOFF IN FSD. AIRCRAFT RETURNED TO GATE. INSPECTED AIRCRAFT AND FOUND DENT IN LEFT INBOARD FLAP ACTUATOR PYLON. INSPECTED LEFT INBOARD FLAP ACTUATOR PYLON. POPPED OUT DENT. DETERMINED AIRCRAFT TO BE AIRWORTHY AND OK FOR RETURN TO SERVICE. REINSPECTED BY SKYWEST MAINTENANCE IN SLC.