N409SW

Part: STRUT — LOW (NLG) · airframe 46,308 hrs · 38,960 cycles

GEAR DISAGREE ON TAKEOFF. NOSE GEAR INDICATED DOWN WITH THE GEAR HANDLE IN THE UP POSITION. FLT#4811 JACKED AIRCRAFT & VISUALLY INSPECTED LANDING GEAR. FOUND NOSE GEAR NOT FULLY EXTENDING. PERFORMED FULL SERVICE OF NOSE GEAR STRUT IAW AMM.

Part: STRUT — LOW (NLG) · airframe 46,293 hrs · 38,948 cycles

RETURN TO FIELD WITH NOSE GEAR DISAGREE. GEAR REMAINED DOWN ON UP SELECTION. FLT#4811 FOUND NO CHROME SHOWING ON NOSE STRUT, SERVICED STRUT.

Part: CIRCUIT BREAKER — FAULTY (COCKPIT) · airframe 44,690 hrs · 37,363 cycles

ELECTRICAL BURNING SMELL IN COCKPIT. (FLT 4568) REPLACED CIRCUIT BREAKER AND NR 2 PITCH FEEL LINEAR ACTUATOR. P/N ON DL2428M4 S/N ON 2778 P/N OFF DL2428M4 S/N OFF AE0816

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,632 hrs · 37,297 cycles

NUMBER 2 OVERHEAD EMERGENCY LIGHTS BURNED OUT. (FLT 7769) RELAMPED EMERGENCY LIGHTS.

Part: SAFETY WIRE — OUT OF ADJUST (SELECTOR VALVE) · airframe 44,632 hrs · 37,297 cycles

GEAR DISAGREE WARNING. (FLT 4636) ADJUSTED SAFETY WIRE ON NOSE GEAR DOOR SELECTOR VALVE IN REFERENCE TO CRJ 200 AMM.

Part: RIB — CRACKED (RT WING) · airframe 44,488 hrs · 37,166 cycles

RIB ASSEMBLY FOUND TO BE CRACKED ON RIGHT WING. (C-CHECK) INSTALLED NEW FABRICATED DOUBLER PER REO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,488 hrs · 37,166 cycles

TWO EACH CRACKS ON FRAME AT FS 605.00 ABOVE AND BELOW LEFT STRINGER 9 ABOVE CARGO DOOR CUTOUT. (C-CHECK) INSTALLED NEW FRAME AT FS 605.00 LEFT BETWEEN STRINGER 6 TO 11 PER CRJ-200 SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 44,488 hrs · 37,166 cycles

FS 621 BULKHEAD HAS A CRACK. (C-CHECK) REPAIRED FS 621 BULKHEAD PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,362 hrs · 37,049 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4829) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,331 hrs · 37,021 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4606) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,849 hrs · 36,568 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4507) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,581 hrs · 36,309 cycles

FURTHEST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4520) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,262 hrs · 36,006 cycles

LEFT FORWARD EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 4460) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,886 hrs · 35,640 cycles

NR 1 AND 4 OVERHEAD EMERGENCY LIGHTS ARE BURNED OUT. (FLT 4584) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,749 hrs · 35,521 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4456) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,749 hrs · 35,521 cycles

NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 4799) RELAMPED EMERGENCY LIGHT.

Part: STRUT — LOW PRESSURE (MLG) · airframe 42,667 hrs · 35,428 cycles

GEAR UP DISAGREE. (FLT 4704) SERVICED MAIN LANDING GEAR STRUT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,406 hrs · 35,174 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4640) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,308 hrs · 35,084 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 13 IS OUT. (FLT 4553) RELAMPED EMERGENCY LIGHT.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 42,181 hrs · 34,971 cycles

WHEN LANDING GEAR WAS SELECTED DOWN A 'GEAR DISAGREE' AND A 'NOSE GEAR' WARNING MESSAGE. (FLT 4640) REPLACED NOSE LANDING GEAR PRIORITY VALVE.

Part: BUSHING — WORN (SERVICE DOOR) · airframe 42,036 hrs · 34,838 cycles

GALLEY SERVICE DOOR DIFFICULT TO OPEN. (FLT 4704) REPLACED HINGE FITTING BUSHINGS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,020 hrs · 34,825 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4527) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,851 hrs · 34,671 cycles

NR 2 CEILING EMERGENCY LIGHT IS OUT. (FLT 4513) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,851 hrs · 34,671 cycles

MIDDLE LEFT EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 4513) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,480 hrs · 34,367 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4616) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 41,170 hrs · 34,104 cycles

FS 621 BULKHEAD WEB IS CRACKED AT 5 PLACES. (C-CHECK) REPAIR PER REO.

Part: POST — CRACKED (FUSELAGE) · airframe 41,170 hrs · 34,104 cycles

FS 409.00+128 OUTBOARD VERTICAL POST CRACKED. (C-CHECK) REPAIR PER REO.

Part: WEB — CRACKED (FUSELAGE) · airframe 41,402 hrs · 34,303 cycles

FS 202 WEB CRACKED AT PARKING BRAKE. (C-CHECK) REPAIRED PER REO.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 38,918 hrs · 32,219 cycles

EMERGENCY LIGHTING LIGHT SWITCH INOP. (FLT 7652) RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,329 hrs · 31,748 cycles

CABIN CEILING EMERGENCY LIGHT INOP. (FLT 4889) RELAMPED EMERGENCY LIGHT.

Part: HINGE PIN — BINDING (PAX DOOR) · airframe 37,848 hrs · 31,375 cycles

FLT 4853 - MAIN CABIN DOOR OUTER LATCH IS DIFFICULT TO UNSTOW. CHANGED DOOR HINGE PIN.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 37,832 hrs · 31,361 cycles

FLT 4413 - THE CABIN DOOR WILL NOT OPEN FROM THE OUTSIDE. ADJUSTED HANDLE STOP AND TENSION.

Part: GAS CYLINDER — WEAK (PAX DOOR) · airframe 37,825 hrs · 31,355 cycles

FLT 4797 - FORWARD ENTRY DOOR DOES NOT OPEN FROM OUTSIDE. REPLACED AFT GAS SPRING.

Part: PIVOT — UNKNOWN (PAX DOOR) · airframe 37,787 hrs · 31,323 cycles

FLT 4542 - MAIN DOOR HARD TO OPEN. REINSTALLED INDICATOR PIVOT AND PUSHROD ASSEMBLY.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 37,772 hrs · 31,310 cycles

FLT 4619 - MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED DOOR MECHANISM.

Part: ANTENNA — CORRODED (ADF) · airframe 37,506 hrs · 31,103 cycles

C-CHECK, ADF ANTENNA FUSELAGE SURFACE CORRODED. REPAIRED PER REO.

Part: ANGLE — CRACKED (BS 621) · airframe 37,506 hrs · 31,103 cycles

C-CHECK, RT FS 621 LOWER ANGLE CRACKED AT RADIUS AT WL73.0. REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,506 hrs · 31,103 cycles

DURING C-HECK, AFT PRESSURE BULKHEAD CRACKED. REPAIRED PER REO.

Part: STRUCTURE — CORRODED (BS 409-559) · airframe 37,506 hrs · 31,103 cycles

C-CHECK, STRUCTURE AT WL73.0 FS 409 TO FS 559 CORRODED. REPAIRED PER REO.

Part: ATTACH FITTING — CRACKED (BULKHEAD) · airframe 37,506 hrs · 31,103 cycles

C-CHECK, AFT PRESSURE BULKHEAD LINTEL ATTACH FITTING CRACKED. REPAIRED PER REO.

Part: STRUCTURE — DAMAGED (PAX DOOR) · airframe 36,154 hrs · 30,052 cycles

CABIN DOOR FWD UPPER CORNER IS DAMAGED. (FLIGHT NR3983) REPLACED CORNER CAP ON PASSENGER DOOR IAW SRM 52-10-31.

Part: ROD END — CORRODED (EMERGENCY EXIT) · airframe 35,152 hrs · 29,296 cycles

RIGHT EMERGENCY EXIT ACTUATING HANDLE AT PIN ROD ENDS ARE CORRODED. REPLACED CLEVIS PINS AND LUBED IAW 52-21-02.

Part: ROD END — CORRODED (EMERGENCY EXIT) · airframe 35,152 hrs · 29,296 cycles

LEFT EMERGENCY EXIT ACTUATING HANDLE AT PIN ROD ENDS ARE CORRODED. REPLACED CLEVIS PINS IAW 52-21-02.

Part: SOLENOID — LEAKING (APU) · airframe 34,864 hrs · 29,067 cycles

FUEL COULD BE DETECTED IN THE CABIN WHEN APU AUTO SHUTDOWN, FLIGHT NR 3946. REPLACED APU FUEL SOLENOID IAW MM 49-31-00. OPS CHECKS GOOD.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 34,366 hrs · 28,705 cycles

FLT 3805 - RECEIVED A GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE AFTER SELECTING GEAR DOWN. ALTERNATE GEAR EXTENSION COMPLIED WITH. REPLACED MAIN LANDING GEAR DOOR SELECTOR VALVE IAW 32-22-00. OP AND LEAK CHECKS GOOD.

Part: WINDSCREEN — CRACKED (COCKPIT) · airframe 33,797 hrs · 28,270 cycles

CAPTAINS WINDSCREEN IS CRACKED. REPLACED THE CAPTAINS WINDSCREEN IAW MM 56-11-01 AND RII 56-220-1000, PN/OFF 139321-9, SN/OFF 01250H7456.

Part: RIB — DAMAGED (FUSELAGE) · airframe 33,797 hrs · 28,270 cycles

SECOND RIB JUST AFT OF RADOME IS DAMAGED. REPLACED SECOND RIB AFT OF RADOME IAW CRJ SRM 51-42-06.

Part: STRINGER — CRACKED (FUSLEAGE) · airframe 33,797 hrs · 28,270 cycles

CENTER STRINGER JUST AFT OF RADOME IS CRACKED AND NEEDS REPLACEMENT. REPLACED STRINGER AFT OF RADOME IAW CRJ SRM 51-42-06.

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 33,797 hrs · 28,270 cycles

RIGHT TRU DOOR SURROUND UPPER STIFFENER IS DAMAGED. REPLACED UPPER STIFFENER ABOVE TRU DOOR IAW CRJ SRM 51-42-06.

Part: BEAM — CRACKED (ENGINE ATTACH) · airframe 32,541 hrs · 27,310 cycles

FOUND LT UPPER OTBD BRACKET TOP WEB OF ENG BEAM TO FUSE SKIN. BRACKET CRACKED ON AFT RADIUS, DISCOVERED DURING C-CHECK INSPECTION. NEW ANGLE INSTALLED PER CRJ200 SRM 51-42-21.

Part: DOOR FRAME — CRACKED (BS 388) · airframe 32,541 hrs · 27,310 cycles

PAX DOOR FRAME FS388 HAS A CRACK ON INNER FLANGE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FRAME INSERT, SPLICES, SHIM AND NEW CLEAT PER REO 601R-52-11-402.

Part: STRINGER CLIP — CRACKED (BS 625 S14L) · airframe 32,541 hrs · 27,310 cycles

FOUND LT STR14 AT STATION 625 CLIP IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CRACKED CLIP AT LT STRINGER STA 625 AND WITH INTERCOSTAL PER CRJ200 SRM 51-42-06 PG 11,18.

Part: DOOR FRAME — CRACKED (BS 323) · airframe 32,541 hrs · 27,310 cycles

PAX DOOR FRAME FS 323.5 IS CRACKED ON INNER FLANGE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW FRAME PER CRJ200 SRM 31-42-06 AND SRM 51-42-21.

Part: DOOR FRAME — CRACKED (BS 321) · airframe 32,541 hrs · 27,310 cycles

PAX DOOR FRAME FS321.5 IS CRACKED ON INNER FLANGE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FRAME INSERT, SPLICES, SHIM AND CLEAT PER REO 601R-52-11-402.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,541 hrs · 27,310 cycles

FOUND RT GEAR WELL AILERON QUADRANT LOWER MOUNT HAS CRACK ON BULKHEAD, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR DOUBLER, SHIMS AND BUTT STRAP PER CRJ200 REO 601R-53-41-26 STEPS 7 AND 8.

Part: STRINGER CLIP — CRACKED (BS 625 S13R) · airframe 32,541 hrs · 27,310 cycles

FOUND CRACK IN RADIUS OF CLIP AT STA625.00 STR 13R, BL 50.000 REF DRAWING 601-35012, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP PN 601-35012-45 PO 75630 AT STA 625-00 STR13R, BL50.000 PER CRJ200 SRM 51-40-06 PG 12.

Part: STRINGER CLIP — CRACKED (BS 625 S14R) · airframe 32,541 hrs · 27,310 cycles

FOUND RT STRINTER 14 AT STATION 625 CLIP IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CRACKED CLIP AT RT STRINGER 14STD625 AND WITH INTERCOSTAL PER CRJ200 SRM 51-42-06 PG 11.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 32,541 hrs · 27,310 cycles

FOUND CLIP CRACKED AT RBL9 ON AFT SIDE OF STA 280 AT FLOOR LEVEL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP, AT FS 280 RBL 9 INBD AFT SIDE OF FLOORBEAM AS PER CRJ200 SRM 51-42-21 PG 1-19 AND SRM 51-42-06 PG 1-18.

Part: DOOR FRAME — CRACKED (BS 336) · airframe 32,541 hrs · 27,310 cycles

PAX DOOR FRAME FS336 HAS A CRACK ON INNER FLANGE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW FRAME PER CRJ200 SRM 51-42-06 AND SRM 51-42-21.

Part: SEAL — BINDING (SERVICE DOOR) · airframe 29,738 hrs · 25,218 cycles

SERVICE DOOR EXTREMELY HARD TO OPEN AND CLOSE. REPLACED DOOR SEAL IAW MM 52-41-07.

Part: WINDOW — CRACKED (COCKPIT) · airframe 29,082 hrs · 24,705 cycles

CAPTAIN'S SIDE WINDOW CRACKED. CAPT'S SIDE WINDOW INSTALLED IAW MM 56-11-00, 56-12-01, PN/OFF NP-139322-5 SN/OFF 01144H8545.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 28,660 hrs · 24,378 cycles

AFTER TAKEOFF, STALL FAIL CAUTION MSGS. REPLACED STALL PROTECTION COMPUTER. OPERATIONAL CHECK GOOD IAW MM 27-35-01, P/N ON 3995100208, S/N OFF 247.

Part: SLIDING SLEEVE — BINDING (PAX DOOR HANDLE) · airframe 28,328 hrs · 24,105 cycles

PAX - DOOR DIFFICULT TO STOW FROM THE INSIDE AND HARD TO OPEN FROM THE OUTSIDE. INSPECTED LINKAGE AND REINSTALLED OUTER HANDLE PUSH LATCH PIN. LUBED SLIDER. OPERATIONAL CHECK GOOD.

Part: PDU — MALFUNCTIONED (TE FLAPS) · airframe 28,278 hrs · 24,065 cycles

DURING TAXI, AFTER SELECTING FLAPS TO 8 DEGREES FLAPS HALFSPEED STATUS MESSAGE ILLUMINATED. REPLACED PDU IAW 27-52-00 AND FECU IAW 27-50-00. OPERATIONAL CHECK GOOD PN 865D100-7, SN/OFF 162 PN 860D100-18 SN/OFF 768.

Part: RIB — CRACKED (RT WING) · airframe 29,231 hrs · 24,827 cycles

RIGHT BAT RIB CRACKED ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR OF RIGHT BAT RIB IAW REO 601R-57-51-046 AND REO 601R-57-51-217.

Part: RIB — CRACKED (LT WING) · airframe 29,231 hrs · 24,827 cycles

LEFT BAT RIB CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR OF LEFT BAT RIB IAW REO 601R-57-51-046.

Part: ANGLE — CRACKED (BS 484) · airframe 29,231 hrs · 24,827 cycles

FOUND CRACKED ANGLE FS 484 LBL27, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW PART CLIP IAW 51-23-00; 51-42-06 AND 51-42-21 CRJ200 SRM AT FS 484 LBL 27.

Part: RIB — CRACKED (RT WING) · airframe 29,231 hrs · 24,827 cycles

RIGHT BAT RIB CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW RIB AT RIGHT BAT IAW SRM 51-42-21.

Part: RIB — CRACKED (LT WING) · airframe 29,231 hrs · 24,827 cycles

LEFT BAT RIB CRACKED, ITEM FOUND AT C-CHECK INSPECTION. RIB INSTALLED IAW CRJ200 SRM 51-42-21 AND 51-25-16.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 27,570 hrs · 23,524 cycles

FLIGHT SPOILERS FAULT AND INBOARD GROUND SPOILERS FAULT STATUS MESSAGES. REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD.

Part: PDU — MALFUNCTIONED (TE FLAPS) · airframe 27,047 hrs · 23,128 cycles

FLAP FAIL MESSAGE. REPLACED PDU IAW CRJ MM 27-52-01, OPERATIONAL CHECK GOOD. P/N 865D100-7, S/N OFF 179.

Part: RADOME — DAMAGED (NOSE) · airframe 26,505 hrs · 22,679 cycles

UPON ARRIVAL AT GATE, FIRST OFFICER NOTICED SMOKE COMING FROM NOSE (TRU) BAY. REPLACED RADOME ASSY.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 26,055 hrs · 22,326 cycles

ONE CEILING EMERGENCY LIGHT IS OUT. RELAMPED AFT CENTER CEILING EMERGENCY LIGHT WITH SERVICEABLE BULB. OPERATIONAL CHECK GOOD.

Part: KNOB — STUCK (RUDDER TRIM) · airframe 25,466 hrs · 21,864 cycles

RUDDER TRIM STICKS TO LEFT. CLEANED AND RE-ADJUSTED RUDDER TRIM KNOB. OPERATIONAL CHECK GOOD.

Part: TRANSMITTER — MALFUNCTIONED (TE FLAPS) · airframe 25,129 hrs · 21,604 cycles

RIGHT FLAP INDICATIONS FLUCTUATES BETWEEN 18 DEGREES TO 20 DEGREES WHEN FLAPS ARE SELECTED TO 20 DEGREES. REPLACED RIGHT FLAP POSITION TRANSMITTER PER AMM 29-55-01. OPS CHECK NORMAL.

Part: WIRE — BROKEN (T/E FLAP) · airframe 24,852 hrs · 21,380 cycles

FLAPS FAILED AT 17 DEGREES AFTER TAKEOFF AT SLC. RETURNED TO SLC. FOUND WIRE BROKEN AT PIN -K- ON CANNON PLUG 2P2CE TO RT BPSU AND CANNON PLUG SOCKETS CORRODED. REPLACED CANNON PLUG 2P2CE WITH A SERVICEABLE UNIT IAW CRJ WM 20-17-80. FLAPS SYSTEM OPERATES NORMALLY. P/N: D38999-26WC98SN.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 24,441 hrs · 21,070 cycles

FS 280 LT FLOORBEAM LBL 9.0 INBOARD ATTACH ANGLE CRACKED. REPLACED ANGLES IAW CRJ SRM 51-40-11 AND CRJ REO 601R-53-11-171 REV NC (RII 53-401). P/N: 601R311011-73SA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 24,441 hrs · 21,070 cycles

FS 280 PILOT'S BULKHEAD AFT FLOOR SUPPORT ANGLE LBL 9.0 CRACKED. REPAIR ANGLE IAW CRJ REO 601R-53-11-138 REV NC, RII 53-401. P/N: 7075T6 040, 600-34017-351.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 24,441 hrs · 21,070 cycles

FS 280 RT FLOORBEAM RBL 9.0 O/B ATTACH ANGLE CRACKED. REPLACED ANGLE IAW CRJ REO 601R-53-11-171 REV NC (RII 53-401). P/N: S6144-13.

Part: STRUCTURE — CRACKED (E/E BAY) · airframe 24,441 hrs · 21,070 cycles

FS 193 LHS ELECTRICAL BAY FLOOR CRACKED. INSTALLED REPAIR IAW REO 601R-53-11-081 REV NC AND SKYWEST RII 53-401.

Part: BEAM — CRACKED (FUSELAGE) · airframe 24,441 hrs · 21,070 cycles

FS 409 + 128 LT VERTICAL BEAM LBL 18 LWR O/B FLANGE CRACKED. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 REV NC & RII 53-401.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,465 hrs · 21,086 cycles

FS 625 LT INTERCOSTAL ANGLE CRACKED STR 14L. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 24,441 hrs · 21,070 cycles

FS 280 PILOT'S BULKHEAD AFT FLOOR SUPPORT ANGLE RBL 11 CRACKED. REPAIR ANGLE IAW CRJ REO 601R-53-11-137 REV NC (RII 53-401).

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,465 hrs · 21,086 cycles

FS 605 CARGO DOOR LANDING PLATE TRANSVERSE BEAM LBL 44 ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 & RII 53-401.

Part: STRUCTURE — CRACKED (E/E BAY) · airframe 24,441 hrs · 21,070 cycles

FS 193 RHS ELECTRICAL BAY FLOOR CRACKED. REPAIRED FLOOR IAW CRJ REO 601R-53-11-245 REV NC & RII 53-401.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,465 hrs · 21,086 cycles

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

Part: BEAM — CRACKED (FUSELAGE) · airframe 24,441 hrs · 21,070 cycles

FS 409 + 128 RT VERTICAL BEAM RBL 18 LWR O/B FLANGE CRACKED. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 REV NC & RII 53-401.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,441 hrs · 21,070 cycles

FS 484 RT INTERCOSTAL RBL 27 ANGLE CRACKED. ANGLE REPLACED IAW CRJ REO 601R-53-41-059 REV A. P/N: 601R31171-9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,441 hrs · 21,070 cycles

SEAT TRACKS FS 409 + 128 AND FS 559 LBL 9 AND RBL 9 CORRODED. RT SEAT TRACK REPLACED IAW CRJ SRM 51-40-11, 51-41-02, 51-42-04. INSTALLED NEW LT SEAT TRACK IAW SRM 51-41-02, 51-41-04. P/N: 601R31032-7.

Part: BEAM — CRACKED (FUSELAGE) · airframe 24,441 hrs · 21,070 cycles

FS 559 RT VERTICAL BEAM RBL 9 INBOARD & OUTBOARD LWR FLANGES CRACKED. BEAM REPAIRED IAW CRJ REO 601R-53-41-057 REV NC, RII 53-401.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,465 hrs · 21,086 cycles

FS 589 CARGO DOOR FLOOR LANDING PLATE TRANSVERSE BEAM ANGLE LBL 44 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11-11, 51-42-06, 51-42-21, 51-23-00 & RII 53-401.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,465 hrs · 21,086 cycles

FS 662 LT FIRE WALL SHUT-OFF INTERCOSTAL ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06.

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 24,441 hrs · 21,070 cycles

EXTERIOR HANDLE OF CREW ESCAPE HATCH HAS CORROSION DAMAGE. REPLACED CREW ESCAPE HATCH OUTER HANDLE WITH NEW ASSY. HANDLE OPS CHECKED OK. P/N: H3419-33.

Part: BEAM — CRACKED (FUSELAGE) · airframe 24,441 hrs · 21,070 cycles

FS 409 + 128 LT VERTICAL BEAM LBL 27 LWR INBOARD FLANGE CRACKED. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 REV NC & RII 53-401.

Part: BEAM — CRACKED (FUSELAGE) · airframe 24,441 hrs · 21,070 cycles

FS 559 LT VERTICAL BEAM LBL 9.0 INBOARD & OUTBOARD LWR FLANGES CRACKED. BEAM REPAIRED IAW CRJ REO 601R-53-41-057 REV NC, RII 53-401.

Part: BRACKET — CORRODED (PA X DOOR) · airframe 24,441 hrs · 21,070 cycles

PASSENGER DOOR CUTOUT LWR SILL AFT BRACKET ASSY FOR AIR STAIR HINGE ARM CORRODED. REPLACED BRACKET ASSY IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00.

Part: RIB — CRACKED (RT PYLON) · airframe 24,441 hrs · 21,070 cycles

FS 605 RT PYLON RIB CRACKED. REPLACED RIB IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 & RII 54-401. P/N: 601-37004-86.

Part: BEAM — CRACKED (FUSELAGE) · airframe 24,441 hrs · 21,070 cycles

FS 409 + 128 RT VERTICAL BEAM RBL 27 LWR INBOARD FLANGE CRACKED. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 REV NC & RII 53-401.

Part: HANDLE — MALFUNCTIONED (MLG) · airframe 23,934 hrs · 20,678 cycles

NOSE DOOR OPENED AT 20,000 FT. GEAR DISAGREE MESSAGE AND PROX SENSOR FAIL MESSAGE. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE. OPS CHECK GOOD IAW MM 32-31-01.

Part: CONTROL PANEL — MALFUNCTIONED (RUDDER TRIM) · airframe 23,459 hrs · 20,293 cycles

RUDDER TRIM TEST FAILED DURING ORIGINATING CHECK, TRIM WOULD NOT TRIM BACK TO LEFT. REMOVED AND REPLACED RUDDER/AILERON TRIM CONTROL PANEL. OPS CHECK GOOD. P/N: 601R51226-23.

Part: TIRE — BLOWN (NR 1 & 4) · airframe 21,888 hrs · 19,052 cycles

NR 1 AND 4 MAIN TIRES FAILED ON LANDING. REMOVED AND REPLACED NR 1 AND 4 MAIN WHEEL ASSY.

Part: SENSOR — MALFUNCTIONED (ANTI-ICE DUCT) · airframe 21,466 hrs · 18,724 cycles

DURING CRUISE CLIMB WE RECEIVED AN ''ANTI-ICE DUCT'' WARNING MESSAGE WHICH WOULD NOT EXTINGUISH WHILE ANTI-ICE WAS ON. ANTI-ICE SYNOPTIC PAGE SHOWED LEFT WING ANTI-ICE DUCT ILLUMINATED IN RED. REMOVED AND REPLACED SENSOR.IAW AMM 30-12-00. PERFORMED ENGINE RUNS FOR OPS CHECK. OPS CHECKS GOOD AT THIS TIME.

Part: SWITCH — OUT OF ADJUST (THRUST REVERSER) · airframe 21,099 hrs · 18,446 cycles

`L REV UNLOCKED` INFLIGHT CLIMBING THROUGH 18,000 FEET. A/C WAS STABLE AND CONTROLLED. A/C DID NOT BUFFET OR YAW. DIVERTED TO BZN. FOUND LEFT REVERSER STOW MICROSWITCH OUT OF ADJUSTMENT, ADJUSTED STOW SWITCH IAW MM 78-37-01. OPS CHECK GOOD.

Part: FITTING — CRACKED (SPOILERON) · airframe 20,390 hrs · 17,889 cycles

RIGHT SPOILERON INBOARD ANTI-ROTATION FITTING IS BENT AND CRACKED. RIGHT SPOILERON INBOARD ANTI-ROTATION FITTING REPLACED IAW CRJ MM 27-64-01-420-801.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 20,132 hrs · 17,680 cycles

DURING TAXI TO GATE, RECEIVED A SPOILERONS MESSAGE ON THE STATUS PAGE. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU WITH SERVICEABLE UNIT IAW MM 27-62-01. LEAK CHECK AND OPS CHECK GOOD.

Part: DAMPER — FAILED (AUTOPILOT SYS) · airframe 19,045 hrs · 16,822 cycles

NR 1 YAW DAMPER WILL NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPER IAW 22-20-00. OPS CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 18,611 hrs · 16,491 cycles

LEFT WINDSHIELD STARTED CRACKING DURING TAXI OUT. REMOVED & REPLACED LEFT WINDSHIELD PER MM 56-11-01 & RII56-401. OPS CHECK/LEAK CHECK GOOD. PN ON NP-139321-9 SN OFF 00151H8911.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 17,143 hrs · 15,282 cycles

AT APPROXIMATELY 500 FT AGL L STATIC HEAT CAUTION MESSAGE APPEARED. POWERED DOWN A/C. ALL PROBE HEAT FUNCTIONAL CHECK OK FOLLOWING POWER UP IAW GMPM VOL 1.

Part: SENSOR — MALFUNCTIONED (CABIN TEMP) · airframe 17,066 hrs · 15,213 cycles

DISPLAY COOL MESSAGE CAME ON CLIMBING THROUGH 12,000 FEET. TRIED FLT ALT AND STBY POSITIONS ON DISPLAY FAN. MESSAGE REMAINED FOR ABOUT 10 MINUTES. VERIFIED FAN OPERATION IN ALL POSITIONS AND AIR FLOW GOOD, NO LEAKS. REPLACED AIRFLOW SENSOR. OPS CHECK GOOD ON GROUND. P/N: 009519-04.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (AOA VANE) · airframe 17,066 hrs · 15,213 cycles

RIGHT AOA VANE CAUTION MESSAGE CAME ON IN FLIGHT. RETURNED TO SLC. CYCLED POWER. RAN 20 MINUTES. RIGHT AOA HEAT OPS CHECK GOOD.

Part: DOOR — LACK OF LUBE (PAX DOOR) · airframe 16,634 hrs · 14,833 cycles

DURING CLIMBOUT, PAX DOOR HANDLE OUT (CAUTION) MESSAGE CAME ON EICAS. QRH PROCEDURE CALLS FOR RE-STOWING THE DOOR HANDLE. WHEN THIS WAS DONE MASTER WARNING CAUTION DOOR MESSAGE CAME ON (RED). AS PER QRH AIRCRAFT WAS LANDED AT NEAREST SUITABLE AIRPORT. PAX DOOR AMBIENT NOISE WAS HIGH. INSPECTED DOOR, FOUND TO NEED LUBRICATION. LUBRICATED DOOR AND FUNCTIONAL CHECK THROUGH 20 CYCLES. CHECKS OK AT THIS TIME.

Part: SENSOR — FAILED (WINDOW HEAT) · airframe 16,392 hrs · 14,616 cycles

LEFT WINDOW HEAT MESSAGE. RETURNED TO SLC. SWITCHED LEFT WINDOW HEAT SENSOR TO SPARE HEAT SENSOR IAW MM 30-40-01. LEFT WINDOW HEAT OPS CHECKS GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 16,362 hrs · 14,592 cycles

CAPTAINS WINDSHIELD CRACKED AT FL 330. DIVERTED TO RAP. REMOVED AND REPLACED CAPTAINS WINDSHIELD WITH NEW WINDSHIELD IAW CRJ MM 56-11-01. LEAK CHECKS OK. P/N ON: PPG-NP-139321-5, S/N ON: 151H8911, SN/ OFF: 94173H8253.

Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 16,314 hrs · 14,553 cycles

AILERON TRIM WILL NOT TRIM TO THE RIGHT. REMOVED AND REPLACED AILERON/RUDDER TRIM PANEL IAW 27-12-10. OPS CHECKS GOOD. PN 601R51226-23/01 SN ON:1046147 PN AND SN OFF: ILLEGIBLE.

Part: SENSOR — OUT OF ADJ (PAX DOOR) · airframe 15,355 hrs · 13,690 cycles

CLIMBING THROUGH FL 180 GOT AMBER ''''PASSENGER DOOR HANDLE NOT STOWED''''. F/A CHECKED ALIGNMENT AND TRIED TO RESTOW HANDLE WITHOUT SUCCESS. RETURNED TO SLC. ADJUSTED PAX DOOR HANDLE PROXIMITY SENSOR IAW MM 52-70-00. OPS CHECKS GOOD AT THIS TIME.

Part: CONTROLLER — FAILED (STABILIZER) · airframe 14,321 hrs · 12,738 cycles

STABILIZER CHANNEL NUMBER TWO WILL NOT ENGAGE. REMOVED AND REPLACED HSTA AND MCU IAW MM 274201, OPS CEHCKS GOOD CAT II OK HSTA (P/N 83963) ON, (S/N 125) ON, (S/N 876) OFF, MCU (P/N 70623) ON, (S/N 205) ON, (S/N 319) OFF.

Part: RVDT — FAILED (NLG)

NOSE WHEEL STEERING INOP MESSAGE CAME ON IN FLIGHT. RETURNED TO SLC. REMOVED AND REPLACED RIGHT RVDT AT NOSE GEAR, OPS CHECK GOOD.

Part: PUMP — FAILED (LEFT ENGINE)

NUMBER ONE HYDRAULIC QUANTITY DROPPED TO 35 PERCENT EN ROUTE. RETURNED TO SLC. INSTALLED SERVICEABLE HYDRAULIC PUMP ON LEFT ENGINE IAW MM 29-13-00. OPS AND LEAKS CHECK GOOD.

Part: WIRE — FAILED (WING ANTI-ICE)

AT 10,000 FEET ENCOUNTERED ICE. TURNED ON ANTI-ICE AND GOT ON ANTI-ICE DUCT MESSAGE. FOLLOWED QRH AND RETURNED TO SLC IN STANDBY POSITION. ANTI-ICE DUCT MSG WOULD CYCLE ON AND OFF. REPLACED NR S27WK LX WIRING LEADING EDGE THERMAL SWITCH.

Part: SWITCH — FAILED (LT WING ANTI-ICE)

WITH WING ANTI-ICE SELECTED ON ANTI-ICE DUCT MESSAGE CAME ON SHOWING LEFT WING RED, SAME IN BOTH NORMAL, STANDBY MODES. RETURNED TO SLC. REPLACED 3 THERMAL SWITCHES IN LEFT WING MID SECTION AND HEAT SHRINK INSTALLED ON LEFT WIRE ENDS. RAN AIRCRAFT AND TAXIED FOR 20 MINUTES. NO DISCREPANCIES NOTED. OPS CHECKS GOOD IN STANDBY AND ON POSITIONS.

Part: FLOORBEAM — CORRODED (BS 330)

AREA AROUND NUT PLATE LBL 27, FS 330 INBOARD SIDE HAS CORROSION OUT OF LIMITS. REPLACED AREA AROUND NUT PLATE IAW MM.

Part: FLOORBEAM — CORRODED (BS 335 & 345)

AREA NEXT TO INSERTS CENTER OF LBL 9, FS 335 AND 345 HAS LIGHT CORROSION. CUT OUT DAMAGED AREA, FABRICATED A L-ANGLE AND FILLERS AND INSTALLED ON LBL 9, FS 335 AND 345 IAW MM .

Part: RADOME — BIRD STRIKE (FWD FUSELAGE)

HIT A BIRD ON CLIMBOUT AND RETURNED FOR LANDING. PERFORMED BIRD STRIKE INSPECTION, FOUND NOSE RADOME RIGHT LOWER CORNER DAMAGED. REPLACED RADOME.

Part: BULKHEAD — CRACKED (FS 409+128)

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

Part: STAB TRIM — MALFUNCTIONED (HORIZ STAB)

STABILIZER TRIM FAILURE BOTH CHANNELS INFLIGHT. STABILIZER TRIM WOULD NOT RESET IN FLIGHT. PERFORMED SYSTEM TEST AT ASTCU, NO FAULTS SHOWN. RESET ASTCU, CHECKED MDC AND FOUND NO HSTCU LOADS. OPERATED STABILIZER TRIM WITH BOTH CHANNELS AND NO PROBLEMS. INSPECTED STABILIZER VISUALLY, FOUND OK.

Part: WINDSHIELD — FAILED (RT COCKPIT)

RT WINDSHIELD SHATTERED AT 33,000 FEET. REMOVED AND REPLACED CO-PILOT'S WINDSHIELD WITH NEW UNIT IAW MM 56-12-01 AND RT NR 56-10.

Part: IDG — FAILED (RT ENGINE)

NR 1 IDG CAUTION MESSAGE ILLUMINATED IN FLIGHT. IDG DISCONNECTED PER CHECKLIST. REMOVED AND REPLACED NR 2 IDG ON RIGHT HAND ENGINE. RAN ENGINE, OPS CHECK AND LEAK CHECK GOOD.

Part: FECU — FAILED (TE FLAPS)

FLAPS FAILED ON APPROACH. REMOVED AND REPLACED FECU. FLAP OPS CHECK OK. SEE FL 5129 FOR MECH SIGN OFF.