N408SW

Part: SKIN — CRACKED (WING) · airframe 45,005 hrs · 37,561 cycles

DURING WING SPLICE INSPECTION FOUND ONE CRACK ON WING SKIN, ORIGINATES FROM TRAILING EDGE OF RIVET AND IS PARALLEL TO WS 65.75. (SERVICE) WORK PERFORMED BY VENDOR IAW REO.

Part: CONNECTOR — OUT OF ADJUST (CABIN) · airframe 44,492 hrs · 37,060 cycles

EMERGENCY FLOOR LIGHTING AND LEFT OVERWING EXIT LIGHT IN CABIN IS OUT. (FLT 4833) ADJUSTED CONNECTOR ON NR 2 INVERTER IN REFERENCE TO CRJ 200 AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,282 hrs · 36,853 cycles

LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT IS OUT. (FLT 4810) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,226 hrs · 36,802 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4665) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,777 hrs · 36,353 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4660) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,667 hrs · 36,241 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4758) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,212 hrs · 35,805 cycles

NR 2 AND 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4737) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,819 hrs · 35,438 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4822) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,692 hrs · 35,322 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4495) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,545 hrs · 35,184 cycles

LEFT EXTERIOR FORWARD OVERWING EMERGENCY LIGHT IS OUT. (FLT 4666) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,468 hrs · 35,112 cycles

EMERGENCY EXIT LIGHT NEXT TO LEFT OVERWING DOOR IS OUT. (FLT 4515) RELAMPED EMERGENCY LIGHT.

Part: WIRE HARNESS — FAILED (CABIN) · airframe 42,408 hrs · 35,058 cycles

FLOOR LEVEL EMERGENCY LIGHTS ARE OUT. (FLT 4541) REPLACED FLOOR EMERGENCY LIGHT HARNESS AT ROW 7.

Part: INVERTER — FAILED (CABIN) · airframe 42,357 hrs · 35,016 cycles

OVERWING EMERGENCY LIGHT EXIT SIGNS AT SEAT LEVEL ARE OUT. (FLT 4764) INSTALLED A SERVICEABLE INVERTER FOR POWER PACK 3.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,357 hrs · 35,016 cycles

EMERGENCY FLOOR LEVEL LIGHTS ARE OUT FROM ROW 5 TO 8. (FLT 4645) REPLACED FLOOR EMERGENCY LIGHT CABLE AT ROW 8.

Part: WIRE — BROKEN (CABIN) · airframe 42,199 hrs · 34,883 cycles

LOWER EMERGENCY EXIT SIGN AT ROW 8 DOES NOT LIGHT UP. (FLT 4655) REPAIRED WIRE AT LOWER EMERGENCY EXIT SIGN NEAR ROW 8.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,002 hrs · 34,712 cycles

EMERGENCY EXIT LIGHT AT SERVICE DOOR HAS A BURNED OUT BULB. (FLT 4615) RELAMPED EMERGENCY LIGHT.

Part: WIRE — DAMAGED (CABIN) · airframe 41,821 hrs · 34,563 cycles

EMERGENCY LIGHT SUPPLY POWER CIRCUIT BREAKER POPPED AND WILL NOT RESET. (FLT 4706) FOUND DAMAGED WIRE INSULATION CAUSING SHORT. REPAIRED WIRE IN REFERENCE TO ESPM 20-11-00.

Part: FITTING — CRACKED (RT MLG TRUNNION) · airframe 41,789 hrs · 34,535 cycles

RIGHT MAIN LANDING GEAR TRUNNION FITTING IS CRACKED. (C-CHECK) REPLACE MLG TRUNNION FITTING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 41,789 hrs · 34,535 cycles

FS 621.0 BULKHEAD CRACKED AT LEFT SIDE WEB. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,008 hrs · 34,717 cycles

FS 559.0 PRESSURE BULKHEAD CRACKED AT LEFT SIDE. (C-CHECK) REPAIRED PER REO.

Part: CONNECTOR — LOOSE (CABIN) · airframe 41,781 hrs · 34,529 cycles

EMERGENCY FLOOR LIGHT STRIP FROM ROW 2 THRU 5 IS OUT. (SERVICE) RE-SECURED CONNECTOR UNDER FLOOR AT ROW 6.

Part: WIRE — DAMAGED (CABIN) · airframe 41,781 hrs · 34,529 cycles

LEFT SIDE EMERGENCY FLOOR LIGHT OUT AT ROW 8. (FLT 4642) REPAIRED WIRE FOR EMERGENCY EXIT LIGHT.

Part: LINK — CORRODED (ENGINE MOUNT) · airframe 40,852 hrs · 33,760 cycles

RIGHT ENGINE LINK ASSEMBLY CORRODED. (ENGINE CHANGE) INSTALLED SERVICEABLE LINK ASSEMBLY.

Part: CONNECTOR — BROKEN (CABIN) · airframe 40,223 hrs · 33,218 cycles

PASSENGER DOOR LOWER EMERGENCY LIGHT INOP. (F4813) REPLACED CONNECTOR.

Part: HANDLE — OUT OF ADJUST (CABIN DOOR) · airframe 38,964 hrs · 32,177 cycles

UNABLE TO OPEN MAIN CABIN DOOR FROM INSIDE. (FLT 4451) ADJUSTED DOOR HANDLE.

Part: ROLLER — BINDING (PAX DOOR) · airframe 38,916 hrs · 32,137 cycles

CABIN DOOR HARD TO OPEN. SERVICE CK, REPLACED ROLLER ASSEMBLY.

Part: BEARING — CORRODED (ENGINE MOUNT) · airframe 38,675 hrs · 31,945 cycles

LEFT ENGINE FORWARD YOKE BEARINGS AND LINK CORRODED. (ENG CHANGE) REPLACED YOKE AND LINK PER AMM.

Part: LINKAGE — OUT OF ADJUST (PAX DOOR) · airframe 37,653 hrs · 31,119 cycles

MAIN DOOR DOES NOT OPEN USING OUTER HANDLE. (FLT 4826) ADJUSTED DOOR LINKAGES FOR THE ROLLOVER CAMS AND THE BAYONETT PINS AND REALIGNED SPIGOT BRACKETS.

Part: HANDLE — DAMAGED (PAX DOOR) · airframe 37,628 hrs · 31,102 cycles

FLT 4747 - MAIN CABIN DOOR LATCH STICKS. REPLACED HANDLE AND HANDLE HOUSING, TWO DAMAGED PROX SENSORS, BENT PUSHROD, AND BEARING AND RIGGED DOOR.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 37,443 hrs · 30,961 cycles

C-CHECK, CLIPS AT FS 280 CRACKED. REPAIRED PER SRM.

Part: BULKHEAD — CRACKED (BS 621) · airframe 37,443 hrs · 30,961 cycles

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

Part: BULKHEAD — CRACKED (BS 621) · airframe 37,443 hrs · 30,961 cycles

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

Part: FRAME — CRACKED (PAX DOOR) · airframe 37,443 hrs · 30,961 cycles

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

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,443 hrs · 30,961 cycles

C-CHECK, SEAT TRACK CORRODED. REPLACED PER AMM.

Part: SKIN — CORRODED (PAX DOOR) · airframe 37,443 hrs · 30,961 cycles

C-CHECK, PASSENGER DOOR SKIN CORRODED. REPAIRED PER SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 37,443 hrs · 30,961 cycles

C-CHECK, TIE CLIPS AFT FUSELAGE CRACKED. REPLACED PER SRM.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 37,287 hrs · 30,836 cycles

FLT 4690 - NR 1 HYDRAULIC SYSTEM SHOWING 0 PERCENT QUANTITY. REPLACED NR 1 ENGINE DRIVEN PUMP.

Part: HANDLE — NICKED (GALLEY DOOR) · airframe 36,676 hrs · 30,386 cycles

FLT 4852 - GALLEY SERVICE DOOR HARD TO OPEN FROM OUTSIDE. REMOVED BURR FROM OUTER HANDLE DOOR ALIGNMENT PIN.

Part: SWITCH — FAILED (NLG) · airframe 35,834 hrs · 29,727 cycles

FLT 4112 - NOSE GEAR DID NOT INDICATE DOWN AND LOCKED WHEN SELECTING GEAR DOWN. REPLACED RIGHT NOSE DOOR OPEN MICROSWITCH PER AMM 32-61-15. OPS CHECK GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG DOOR) · airframe 35,806 hrs · 29,704 cycles

FLT NR 4042 - RECEIVED A GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE WHEN EXTENDING GEAR. ADJUSTED PROX SENSOR PS 17GA IAW AMM 32-61-05. ALL OPS CHECKS GOOD.

Part: LANDING GEAR — MALFUNCTIONED · airframe 35,702 hrs · 29,625 cycles

NOSE GEAR WOULD NOT EXTEND AND RECEIVED A GEAR DISAGREE MESSAGE. RECYCLED GEAR HANDLE AND THE NOSE GEAR EXTENDED CORRECTLY. (FLIGHT NR 4048) INSPECTED AND SWUNG GEAR SEVERAL TIMES IAW MM 32-30-00. NO DEFECTS NOTED AT THIS TIME.

Part: LIGHT — BROKEN (CABIN) · airframe 35,411 hrs · 29,399 cycles

FOUND EMERGENCY LIGHTS ARE INOP BETWEEN ROWS 6 AND 7. REPLACED THE POWER STRIP FOR THE EMERGENCY LIGHTING TRACK. OPS CHECKS GOOD.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 35,026 hrs · 29,111 cycles

FLT 3768 - DURING APPROACH MAIN GEAR DID NOT EXTEND. MANUAL EXTENSION REQUIRED TO EXTEND MAINS. REPLACED MLG SELECTOR VALVE IAW MM 32-32-10. OPS AND LEAK CHECK GOOD, PN 750005000, SN/OFF 0033.

Part: CONTROL ROD — BINDING (DOOR VENT) · airframe 34,162 hrs · 28,471 cycles

PAX DOOR OUTER HANDLE WILL NOT CLOSE FROM INSIDE AIRPLANE. (FLIGHT #3810) ADJUSTED PRESSURE VENT FLAP CONTROL ROD IAW 52-11-15. OPS CHECKS GOOD.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 33,675 hrs · 28,101 cycles

HYDRAULIC SYSTEM 2 RESERVOIR INDICATES EMPTY. FLIGHT NR 3995, REPLACED NR 2 EDP.

Part: WINDOW — CRACKED (COCKPIT) · airframe 33,675 hrs · 28,101 cycles

CAPTAINS SIDE WINDOW CRACKED WHILE AIRCRAFT WAS SITTING AT THE GATE. FLIGHT NR 3995, REPLACED LEFT SIDE WINDOW IAW MM 56-12-01.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 33,371 hrs · 27,878 cycles

FLT 3850 - EMERGENCY LIGHTS IN THE GALLEY DO NOT WORK. RESECURED LOOSE CONNECTIONS IN THE GALLEY CLOSET. OPS CHECK GOOD.

Part: PRIORITY VALVE — MALFUNCTIONED (MLG) · airframe 33,313 hrs · 27,836 cycles

FLT 3897 - GEAR DISAGREE WARNING WITH NOSE GEAR UP INDICATION ON FINAL. WHEN 3B WAS SELECTED, NOSE GEAR DOWN INDICATION GIVEN. REPLACED PRIORITY VALVE AND CYCLED GEAR UP AND DOWN SEVERAL TIMES. OPS CHECK GOOD AT THIS TIME.

Part: OXYGEN MASK — UNWANTED DEPLOY (LAVATORY) · airframe 33,153 hrs · 27,726 cycles

O2 MASK DEPLOYED IN LAVATORY. REPACKED LAVATORY OXYGEN MASKS IAW 35-21-09.

Part: PITOT SYSTEM — FALSE INDICATION · airframe 32,872 hrs · 27,524 cycles

EFIS COMP MON CAUTION MESSAGE ON DESCENT. CAPTAIN SIDE AIRSPEED IS INACCURATE. FOUND "DETECTABLE CURL' ON LEFT PITOT TUBE OPENING. REPLACED LEFT PITOT TUBE. REPLACED ADC NR 1, P/N: 822-0372-445 S/N ON: G77F S/N OFF: 12V9P

Part: FLOORBEAM — CRACKED (BS 484) · airframe 32,692 hrs · 27,388 cycles

FLOOR SUPPORT STRUCTURE AT FS 484 RBL 30 HAS A CRACKED ANGLE, DISCOVERED AT C-CHECK. REPLACED CLIP PN 601R31171-9 PER REO 601R-53-41-059.

Part: BOLT — CORRODED (SERVICE DOOR) · airframe 32,692 hrs · 27,388 cycles

SERVICE DOOR CUT OUT LOWER DOWN LOCK ROLLER GUIDE BOLTS CORRODED, DISCOVERED AT C-CHECK. REMOVED AND REPLACED 8 BOLTS, 8 WASHERS (P/N AN960JD416), 8 WASHERS (P/N NAS1149CO463R) AND 8 NUTS IAW CRJ200 AMM TASK 20-21-00-944-001.

Part: ANGLE — CRACKED (BS 625) · airframe 32,692 hrs · 27,388 cycles

AFT EQUIPMENT BAY FS 625 LBL40 ANGLE CRACKED, DISCOVERED AT C-CHECK. REPLACED ANGLE AT FS 625 LBL 210 NEW PN 601-35012-51 PO 71471 AS PER CRJ200 SRM REF 51-42-21 PG 1.

Part: SHROUD — CRACKED (RIGHT) · airframe 32,692 hrs · 27,388 cycles

RIGHT L/E OUTBOARD SECTION SHROUD CRACKED, DISCOVERED AT C-CHECK. INSTALLED NEW SHROUD PER CRJ200 SRM REF 57-41-29 AND CRJ200 SRM REF 51-25-00 PG 1.

Part: CLAMP — CRACKED · airframe 32,692 hrs · 27,388 cycles

LEFT WING PICCOLO TUBE CLAMPS CRACKED INSIDE ACCESS PANELS 530FZ, 530GZ, 530JZ, 530AZ AND 530BZ, DISCOVERED AT C-CHECK. REPLACED CLAMPS INSIDE ACCESS PANELS 530FZ AND 530GZ WITH P/N 601R80004-7, PANEL 530JZ WITH P/N 601R8004-9, AND PANELS 530AZ AND 530BZ WITH P/N 600-800G1-9 PER CRJ200 AMM 30-11-41-000-801.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 32,692 hrs · 27,388 cycles

FS 280 RBL 9 FLOOR SUPPORT UPPER ANGLE IS CRACKED, DISCOVERED AT C-CHECK. FABRICATED AND INSTALLED REPAIR PART -6, -4 SPLICE ANGLE AND -2 FILLER ANGLE IAW CRJ 200 SRM 51-42-10 AND REO 601R-53-11-137 REV NC.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 32,692 hrs · 27,388 cycles

ENGINE SUPPORT BEAM LOWER WEB AT LBL15 AND RBL15 IS CRACKED IN THREE LOCATIONS, DISCOVERED AT C-CHECK. FABRICATED P/N 601R53-61-2129-51-6 SHIMS AND SPLICE ANGLES P/N 601R 641-2129-1/-2 PER CRJ200 REO 601R 53-61-2129 STEPS FIG 1/2. INSTALLED ALL REPAIR PARTS ON LOWER AFT ENG WEB PER CRJ200 REO RE0 601R 53-61-2129 SB601R 53-068.

Part: BRACKET — CORRODED (LT AILERON PULLE) · airframe 32,692 hrs · 27,388 cycles

LEFT AILERON OUTBOARD PULLEY BRACKET HAS CORRODED HARDWARE, DISCOVERED AT C-CHECK. REPLACED CORRODED HARDWARE ON LEFT AILERON OUTBOARD PULLEY ATTACHING BRACKET PER CRJ200 SRM 51-41-02 PG 5, 6 AND 7.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 32,296 hrs · 27,092 cycles

FOUND LAST EMERGENCY OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED AFT MOST CEILING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,826 hrs · 25,986 cycles

EMERGENCY FLOOD LIGHT IN CABIN INOP (3RD FROM FRONT). RELAMPED 3RD OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 30,164 hrs · 25,493 cycles

O2 MASKS OVER SEATS 8CD DEPLOYED BY THEMSELVES DURING DESCENT THRU +OR - 15000 FEET CABIN PRESSURE AND ALL OTHER INDICATIONS WERE NORMAL. RESTOWED O2 MASKS AT 8CD AS REQUIRED. A/C OK FOR CONTINUED SERVICE.

Part: TRIM SWITCH — STICKING (COCKPIT) · airframe 30,086 hrs · 25,432 cycles

FO'S TRIM SWITCH STICKS. REPLACED F.O.'S TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD IAW MM 27-40-00.

Part: DETECTOR — MALFUNCTIONED (T/E FLAP) · airframe 29,075 hrs · 24,672 cycles

FLAPS DEGRADED MSG. REPLACED SKEW DETECTOR UNIT. OPERATIONAL CHECKS GOOD. IAW 27-51-15.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 29,069 hrs · 24,667 cycles

"FLAP FAIL" CAUTION MESSAGE WHEN MOVING FLAP SELECTOR FROM 0 TO 8. FLAPS FAILED AT 0. REPLACED ALL FLAP ACTUATORS ON LT AND RT WINGS IAW CRJ MM 27-53-01, 27-53-03. OPERATIONAL CHECK GOOD.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 28,746 hrs · 24,409 cycles

FUSELAGE, PULLEY INTERCOSTAL IS CRACKED ON O/B FLANGE, FS 484.00 - LBL 36.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED PULLEY INTERCOSTAL. REF. CRJ REO 601R-53-41-059 REV A, AMM 20-24-00, SRM 51-41-02.

Part: POST — CRACKED (BS 559) · airframe 28,746 hrs · 24,409 cycles

FUSELAGE, VERT POST IS CRACKED AT LOWER RIVET LOCATION, FS 559.00 - RBL 9.0, I/B AND O/B SIDES, ITEM FOUND AT C-CHECK INSPECTION. VERTICAL POST AT FS 559.00; RBL 9.0 REPLACED IAW CRJ REO 601R-53-41-260 REV "A".

Part: POST — CRACKED (BS 559) · airframe 28,746 hrs · 24,409 cycles

FUSELAGE, VERT POST IS CRACKED AT LOWER RIVET LOCATION, FS 559.00 - LBL 9.0, I/B AND O/B SIDES, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-057 REV NC.

Part: ATTACH FITTING — CRACKED (BS 625) · airframe 28,746 hrs · 24,409 cycles

AFT EQUIP COMP, 6 INTERCOSTAL TO STRINGER ATTACH CLIP ARE CRACKED FS 625.00, STR 11 RT, ITEM FOUND AT C-CHECK INSPECTION. REMOVED & REPLACED CLIPS IAW CRJ SRM 51-42-06, 51-40-11, 51-42-21, 51-23-00, 51-25-16.

Part: RIB — CRACKED (RT PYLON) · airframe 28,746 hrs · 24,409 cycles

RT PYLON, RIB CRACKED ON LOWER FLANGE AT FS605, ITEM FOUND AT C-CHECK INSPECTION. RIB REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 .

Part: DOOR FRAME — CRACKED (BS 320) · airframe 28,746 hrs · 24,409 cycles

PAX DOOR, DOOR FRAME IS CRACKED ON UPPER END, FS 320.10, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED FRAME IAW CRJ REO 601R-52-11-402 REV E.

Part: BULKHEAD — CRACKED (BS 559) · airframe 28,746 hrs · 24,409 cycles

RT MLG WHEEL BAY, PRESSURE BULKHEAD WEB IS CRACKED BEHIND AILERON QUADRANT, FS 559.00 - RBL 17.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-260 REV A & CRJ REO 601R-53-41-251 REV "A" & CRJ REO 601R-53-41-348.

Part: POST — CRACKED (BS 409) · airframe 28,746 hrs · 24,409 cycles

FUSELAGE, VERTICAL POST IS CRACKED AT LOWER RIVET LOCATION, FS409.0+128 - LBL36.0 - I/B SIDE, ITEM FOUND AT C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-53-41-189 REV NC

Part: FRAME — CRACKED (BS 605) · airframe 28,746 hrs · 24,409 cycles

CARGO COMP, FRAME FLANGE IS CRACKED, FS 605.00 - STRL 9L, LOWER SIDE ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DAMAGE FRAME FLANGE FS 605.00; STR 9L IAW CRJ REO 601R-53-61-1529

Part: DOOR — CORRODED (EMERGENCY EXIT) · airframe 28,746 hrs · 24,409 cycles

LT EMERG EXIT, LOWER CORNERS HAVE CORROSION ON INNER STRUCTURE ITEM FOUND AT C-CHECK INSPECTION. REMOVED CORROSION IAW CRJ SRM 52-00-00, FIG 102, 51-21-06, 51-45-00. .002 MAT LOSS WITHIN LIMITS IAW CRJ SRM 52-00-00, FIG. 102.

Part: POST — CRACKED (BS 409) · airframe 28,746 hrs · 24,409 cycles

FUSELAGE, VERTICAL POST IS CRACKED AT LOWER RIVET LOCATION, FS409.0+128 - LBL27.0 - I/B SIDE, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-056 REV C .

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 28,746 hrs · 24,409 cycles

CARGO DOOR, INTERCOSTAL IS CRACKED, LOWER AFT CORNER, ITEM FOUND AT C-CHECK INSPECTION. REPLACE INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-42-21, 51-25-16, 51-42-13.

Part: FITTING — CORRODED (PAX DOOR) · airframe 28,746 hrs · 24,409 cycles

PAX DOOR, LOWER CORNER FITTINGS ARE CORRODED, FS 312.00 AND FS 346.00, ITEM FOUND AT C-CHECK INSPECTION. REPLACED FITTINGS (FWD & AFT).

Part: CLIP — CRACKED (BS 280) · airframe 28,746 hrs · 24,409 cycles

MAIN FUSELAGE, FS 280 LBL 9.0, O/B AND I/B CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-6, 51-42-13, 51-23-00 (REF REO 601R-53-11-171 REV B DUE TO REPAIR IN SAME AREA).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,580 hrs · 25,052 cycles

CORROSION FOUND ON SEAT TRACK RBL 9 + STA 559 + 80 - STA 559 + 112, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW SEAT TRACK IAW CRJ SRM 51-41-02 AND 51-23-00.

Part: POST — CRACKED (BS 409) · airframe 28,746 hrs · 24,409 cycles

FUSELAGE, VERTICAL POST IS CRACKED AT LOWER RIVET LOCATION, FS409.0+128 - RBL27.0, I/B SIDE, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-056 REV C .

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,580 hrs · 25,052 cycles

FUSELAGE, FRAME STATION 265 STR 16 LT, FRAME FLANGE DAMAGED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-11-927.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,580 hrs · 25,052 cycles

CRACK ON FRAME FLANGE AT FS 640 RT STR 9R, ITEM FOUND AT C CHECK INSPECTION. REPAIRED CRACKED FRAME IAW CRJ REO 601R-53-61-1543 AND RII 53-401.

Part: STRUCTURE — CORRODED (PRESSURE FLOOR) · airframe 28,746 hrs · 24,409 cycles

PRESSURE FLOOR SIDE BOX STRUCTURE, CORROSION ON UPPER DOUBLER, RT SIDE, FS 473.00, ITEM FOUND AT C-CHECK INSPECTION. CORROSION ON UPPER DOUBLER; R/H SIDE; FS 478.00 REMOVED IAW CRJ SRM 53-41-45. BLENDED AREA REPROTECTED IAW CRJ SRM 51-21-16 (CODE A023). MATERIAL REMOVED 0.005; MATERIAL REMAINING 0.075" AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW CRJ SRM 53-41-45.

Part: CLIP — CRACKED (BS 280) · airframe 28,746 hrs · 24,409 cycles

MAIN FUSELAGE, FS 280 RBL 9.0, O/B AND I/B CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-42-13, 51-23-00.

Part: CHANNEL — CORRODED (PAX DOOR) · airframe 28,746 hrs · 24,409 cycles

PAX DOOR, LWR CENTER CHANNEL HAS CORROSION ON INSIDE UNDER WATER DAM, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CHANNEL.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 28,746 hrs · 24,409 cycles

MAIN FUSELAGE, FS 280.00, LBL 9.0, UPPER FLANGE CRACKED ON FLOORBEAM, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED MAIN FUSELAGE FS 280.00, LBL 9.0 UPPER ANGLE ON TRANSVERSE BEAM IAW CRJ REO 601R-53-11-138 REV "NC".

Part: FRAME — CRACKED (PAX DOOR) · airframe 28,746 hrs · 24,409 cycles

PAX DOOR, DOOR FRAME IS CRACKED ON UPPER END, FS 338.90, ITEM FOUND AT C-CHECK INSPECTION. FRAME REPAIRED IAW REO 601R-52-11-402 REPAIR 2.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 28,746 hrs · 24,409 cycles

REAR PRESSURE BULKHEAD, AFT SIDE RBL - 36.0 - WL 73.50, CRACKED ON VERTICAL BEAM, FWD RADIUS, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO CRJ REO 601R-53-61-1532.

Part: FRAME — CRACKED (PAX DOOR) · airframe 28,746 hrs · 24,409 cycles

PAX DOOR, SUB FRAME IS CRACKED AT UPPER END, FS 335.70, ITEM FOUND AT C-CHECK INSPECTION. REPLACED SUB-FRAME.

Part: PITOT TUBE — OBSTRUCTED · airframe 28,716 hrs · 24,388 cycles

STALL FAIL, CAUTION MSG AFTER TAKEOFF RETURN TO SLC. REMOVED CONTAMINATION FROM CAPT PITOT TUBE. PURGED PITOT PROBE OF CONTAMINATION. OPERATIONAL CHECK GOOD IAW MM 27-35-05; 27-35-01 AND 34-11-00.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 28,155 hrs · 23,947 cycles

FLIGHT SPOILER FAULT MSG DURING TAXI. REPLACED LT INBOARD FLIGHT SPOILER PCU IAW 27-62-01. OPERATIONAL CHECK GOOD.

Part: BEARING — NOISY (AILERON TRQ TUBE) · airframe 27,700 hrs · 23,593 cycles

NOISES CAN BE HEARD AND FELT WHILE MAKING AILERON INPUTS WITH THE CAPTIAN'S YOKE. REPLACED LEFT AILERON TORQUE TUBE BRACKET BEARING IAW AMM 27-11-05. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN DOOR) · airframe 27,554 hrs · 23,485 cycles

EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT AT CABIN DOOR, OPERATIONAL CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 26,878 hrs · 22,946 cycles

DURING PREFLIGHT FOUND LARGE CRACK IN RIGHT WINDSHIELD. REPLACED RIGHT WINDSHIELD IAW CRJ MM 56-00-00, 56-11-01, 56-12-01.

Part: WINDSHIELD — BROKEN (COCKPIT) · airframe 26,259 hrs · 22,453 cycles

RIGHT WINDSHIELD SHATTERED. REMOVED AND REPLACED RIGHT WINDSHIELD ASSY IAW MM 56-11-01. P/N OFF NP-139321-10, S/N OFF 01208144243.

Part: ENGINE — POWER LOSS (LEFT) · airframe 26,109 hrs · 22,335 cycles

LEFT ENGINE QUIT AT 500 FT AGL ON APPROACH INTO SLC. N1 AND N2 ROLLED BACK AND ITT WENT RED. REMOVED AND REPLACED ENGINE ASSY IAW MM 71-00-00, OPERATIONAL CHECK GOOD.

Part: POSITION SENSOR — MALFUNCTIONED (BRAKE) · airframe 25,549 hrs · 21,897 cycles

ON APPROACH, SELECTED FLAPS TO 20 DEGREES AND RECEIVED FLAPS FAIL. REMOVED AND REPLACED LEFT HAND BPSU, RIGGED LEFT HAND AND RIGHT HAND BPSU. OPERATIONAL CHECKED GOOD.

Part: APU — FAILED (APU BAY) · airframe 25,468 hrs · 21,832 cycles

APU AUTO SHUTDOWN ON GROUND. STRONG ODOR OF ELECTRICAL SMOKE IN COCKPIT PRIOR TO APU SHUTDOWN. RECEIVED APU FIRE WARNING. COMPLIED WITH QRC AND QRH PROCEDURES. FERRIED TO SLC. REMOVED AND REPLACED APU ASSEMBLY IAW MM 49-10-00 AND RII 49-401. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 25,132 hrs · 21,567 cycles

NR 3 ACTUATOR ON LEFT WING HAS EXCESSIVE PLAY IN FLAP SIDE ATTACH POINT INBOARD BUSHING ON GIMBLE PIN ATTACH POINT. REMOVED AND REPLACED NR 3 ACTUATOR ON LT WING I/B GIMBLE ATTACH BUSHING BLOCK IAW CRJ MM 27-53-05 AND CMM 27-50-12. P/N

Part: POSITION SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 25,132 hrs · 21,567 cycles

RECEIVED A FLAPS FAIL CAUTION MESSAGE UPON ARRIVAL AT SLC. COULD NOT RAISE FLAPS FROM THE 45 DEGREE POSITION. REMOVED AND REPLACED RT BPSU IAW MM 27-51-10. RIGGED RT BPSU IAW CRJ MM 27-51-10 AND REINSTALLED FLEX DRIVE AND SAFETIED IAW CRJ MM 27-54-00. OPS CHECK GOOD.

Part: SILL — CORRODED (FUSELAGE)

LT FLOOR SILL PN 601R3114863 BETWEEN FS 364 AND FS 379 IS SEVERELY CORRODED. PROBABLE CAUSE: POSSIBLE WATER INTRUSION. (EA09200402076)

Part: ANGLE — CRACKED (LT WING)

LT WING STA 48.30 ANGLE PN 600-1020427 IS CRACKED 1 INCH IN RADIUS. PROBABLE CAUSE: STRESS. REMOVE AND REPLACE ANGLE IAW CRJ 200 SRM 51-42-21 AND 51-42-06.

Part: ANGLE — CRACKED (RT WING)

RT WING STA 48.30 ANGLE PN 600-1020428 IS CRACKED , 1 INCH IN RADIUS. PROBABLE CAUSE: STRESS. REMOVE AND REPLACE ANGLE IAW CRJ 200 SRM 51-42-21 AND 51-42-06.

Part: BULKHEAD — CRACKED (FUSELAGE)

BULKHEAD FS 202.75 LBL 24 BETWEEN STRINGERS 20L AND 21L IS CRACKED PROTRUDING FROM CUTOUT FOR PARKING BRAKE CONTROL ROD. VIBRATION AND STRESS FROM CABLE ARE THE PROBABLE CAUSE. INSTALL DOUBLER ON BULKHEAD.

Part: BUSHING — LACK OF LUBE (HORIZ STAB)

LT VERTICAL STABILIZER PIVOT FITTING FOR THE HORIZONTAL STABILIZER HAS BUSHING (PN 601R55310025) MIGRATED AT WL 235.00, LBL 4.10. PROBABLE CAUSE: PIVOT PIN LUBRICATION NOT ADEQUATE. (EA09200401997)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

ENGINE SUPPORT BEAM LEFT UPPER ATTACHMENT ANGLE (PN 6013500661) AT FS 640, WL 115, LBL 45, STRINGER 9 IS CRACKED. PROBABLE CAUSE: STRESS (EA09200401997)

Part: SKIN — CRACKED (FUSELAGE)

FUSELAGE SKIN IS CRACKED AT THE CORNERS OF THE NOSE LANDING GEAR CUT OUT AT FS 235, RBL 6 AND LBL 6, STINGERS 26 R AND 26L. PROBABLE CAUSE: STRESS (EA09200401997)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

FS 484 WATERLINE 73 RBL 27 OB INTERCOSTAL ATTACHMENT ANGLE PN 601R311719 IS CRACKED .2500 INCH. PROBABLE CAUSE: STRESS

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

FS 484 WATERLINE 73 RBL 9 OB INTERCOSTAL ATTACHMENT ANGLE PN 601R311719 IS CRACKED .2500 INCH. PROBABLE CAUSE: STRESS (EA09200401997)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

FS 484 WATERLINE 73 LBL 27 OB INTERCOSTAL ATTACHMENT ANGLE (PN 601R3117117) IS CRACKED .2500 INCH. PROBABLE CAUSE: STRESS (EA09200401997)

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,107 hrs · 21,550 cycles

FUSELAGE SKIN AT FS 235.0 LBL 6.0 AND RBL 6.0 (TRAILING EDGE OF NLG CUTOUT) POSSIBLE CRACKS. DISCOVERED DURING C-CHECK INSPECTION. FABRICATED AND INSTALLED REPAIR PANELS IAW REO 601R-53-11-010 REV. C.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 25,107 hrs · 21,550 cycles

FS 484 RBL 27 OUTBOARD INTERCOSTAL ANGLE CRACKED .25 INCH IN THE ANGLE RADIUS AT WL 73. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED CRACKED ANGLE WITH NEW ANGLE PN 601R31171-9 AT FS 484 RBL 27 INBD SIDE IAW CRJ 200 SRM 51-42-21, 51-42-06, 51-40-11, AND 51-21-11 AND EO #601R-53-4865 AND SKYWEST EA RJ240-53.

Part: SUPPORT BEAM — CRACKED (LT ENGINE) · airframe 25,107 hrs · 21,550 cycles

LEFT ENGINE SUPPORT BEAM UPPER ATTACHMENT ANGLE P/N 601-35006-61 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ATTACHMENT ANGLE LEFT TOP ENGINE SUPPORT BEAM AS REQUIRED IAW CRJ SRM 51-42-21.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 25,284 hrs · 21,689 cycles

FORWARD BULKHEAD TO STRINGER 21 LT, ATTACH CLIP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED CLIP IAW CRJ 200 SRM CH 51-42-06.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,107 hrs · 21,550 cycles

CRACK FOUND AT FS 202.75 BULKHEAD LBL 2A AT PARKING BRAKE CONTROL ROD CUTOUT. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACKED BULKHEAD AT FS 202.75 LBL 2A BETWEEN STRINGERS 20L AND 21L IAW REO 601R-53-11-767.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 25,107 hrs · 21,550 cycles

FS 484 WL 73 LBL 9 OUTBOARD INTERCOSTAL ATTACHMENT ANGLE IS CRACKED .25 INCH. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW ANGLE PN 601R31171-27 PER BRAS EO STEPS 1 AND SRM 51-42-21, AND SKYWEST EA NO. RJ240-53.

Part: SILL — CORRODED (PAX DOOR) · airframe 25,284 hrs · 21,689 cycles

U-CHANNELS ON FUSELAGE, PAX DOOR SILL CORRODED (UNDER PANEL 231CLF). DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CHANNEL P/N 601R31527-217 AT FOWARD AND AFT LOCATIONS IAW CRJ SRM 51-42-06 AND 51-42-11.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 25,107 hrs · 21,550 cycles

RIGHT SIDE 625 OBLIQUE ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED & REPLACED OBLIQUE ANGLE P/N 601-35012-52 IAW SRM 51-42-06.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 25,107 hrs · 21,550 cycles

FS 484 WL 73 LBL 27 OUTBOARD INTERCOSTAL ATTACHMENT ANGLE IS CRACKED .25 INCH. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED ANGLE PN 601R31171-17 AT FS 484 LBL 27 OUTBOARD SIDE IAW CRJ 200 SRM 51-42-21, 51-42-06, 51-40-11, 51-21-11 AND EO # 601R-53-4865 AND SKYWEST EA NO. RJ240-53.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 25,107 hrs · 21,550 cycles

FS 484 INTERCOSTAL ANGLE AT RBL 9 OUTBOARD IS CRACKED .5 INCH IN RADIUS OF ANGLE AT WL 73. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW ANGLE PN 601R31171-9 PER BRAS EO STEP 1 AND SRM 51-42-21 AND SKYWEST EA NO. RJ240-53.

Part: RIB — CRACKED (RT WING) · airframe 25,107 hrs · 21,550 cycles

RIGHT BATT RIB AT WS 53.60 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION.

Part: ANGLE — CRACKED (RT WING) · airframe 25,107 hrs · 21,550 cycles

RIGHT WING SECTION 48.30 ANGLE PART NUMBER 600-10204-28 IS CRACKED 1 INCH IN RADIUS. DISCOVERED DURING C-CHECK INSPECTION.

Part: STRUCTURE — CRACKED (LT WING) · airframe 25,107 hrs · 21,550 cycles

LEFT WING SECTION 48.30 PART NUMBER IS CRACKED 1 INCH IN RADIUS. DISCOVERED DURING C-CHECK INSPECTION.

Part: SILL — CORRODED (FUSELAGE) · airframe 25,107 hrs · 21,550 cycles

LEFT FLOOR SILL P/N 601R3114863 FS 364 AND FS 379 IS SEVERELY CORRODED. DISCOVERED DURING C-CHECK INSPECTION.

Part: RIB — CRACKED (LT WING) · airframe 25,107 hrs · 21,550 cycles

LEFT BATT RIB AT WS 53.60 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION.

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

FS 484 WATERLINE 73 LBL 9 OB INTERCOSTAL ATTACHMENT ANGLE PN 601R3117127 IS CRACKED .2500 INCH. PROBABLE CAUSE: STRESS (EA09200401997)

Part: CONTROL LEVER — MALFUNCTIONED (SPOILERS) · airframe 24,939 hrs · 21,419 cycles

ON TAXI OUT RECEIVED INBOARD GROUND SPOILER FAULT STATUS MESSAGES. REMOVED AND REPLACED FLIGHT SPOILER CONTROL LEVER IAW MM 27-61-01. OPS CHECK GOOD. P/N: 365-209D, S/N OFF: F0621A.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILER) · airframe 24,539 hrs · 21,112 cycles

SPOILERONS FAULT STATUS MESSAGE ON TAXI OUT. RIGHT SPOILERON PANEL DEPICTION WAS WHITE ON FLIGHT CONTROL PAGE. REMOVED AND REPLACED RIGHT INBOARD PCU ON SPOILERON. OPS AND LEAK CHECKS GOOD IAW MM 27-61-01.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 24,064 hrs · 20,744 cycles

ON DEPARTURE FROM BZN AT ABOUT 500 FT RUDDER TRIM DEFLECTED ALMOST FULL SCALE NR RUDDER TRIM SWITCH WAS ABLE TO BRING TRIM BACK TO LESS THAN 1/2 DEFLECTION. REMOVED AND REPLACED RUDDER/AILERON TRIM CONTROL PANEL. RUDDER TRIM SYSTEM OPS CHECK GOOD. P/N: 601R51226-23SW.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 23,517 hrs · 20,316 cycles

AFTER TAKE-OFF AND AFTER GEAR WAS SELECTED UP, RECEIVED ''NOSE DOOR OPEN'' MESSAGE. WAS UNABLE TO GET LIGHT OUT AND WE RETURNED TO FIELD. REMOVED AND REPLACED NLG DOOR SELECTOR VALVE IAW CRJ MM 32-22-20. OPS AND LEAK CHECK GOOD.

Part: VANE — MALFUNCTIONED (STALL WARNING) · airframe 23,376 hrs · 20,200 cycles

STALL FAIL MSG APPEARS JUST A FEW SECONDS AFTER TAKEOFF. REMOVED AND REPLACED LEFT AOA IAW MM 22-35-05. OPS CHECKS GOOD. P/N ON 45150340, SN OFF 229.

Part: CONNECTING ROD — LOOSE (EMERGENCY LIGHT) · airframe 22,802 hrs · 19,765 cycles

FIRST ROW OF ORANGE EMERGENCY LIGHTS IN CABIN NOT ILLUMINATING. SECURED LOOSE CONNECTOR AT ROW 1-C. OPS CHECK GOOD.

Part: GATE — MALFUNCTIONED (PAX DOOR) · airframe 21,371 hrs · 18,659 cycles

CABIN CLIMBED UNCONTROLLABLY IN AUTO AND MANUAL MODES. RETURNED TO BIL. REPAIRED AND RIGGED THE PASSENGER DOOR GATE IAW CRJ MM TASK 52-11-15-820-801. OPERATIONAL CHECK OF PRESSURE SYSTEM IAW 21-32-00 GOOD. OPS CHECK OF PRESSURE CONTROL SYSTEM IAW CRJ MM TASK 21-31-00-710-801 GOOD.

Part: CONTROLLER — MALFUNCTIONED (NR GND SPOILER) · airframe 21,371 hrs · 18,659 cycles

AFTER PUSHBACK RECEIVED AN INBOARD & OUTBOARD GROUND SPOILER FAULT MESSAGE. REMOVED AND REPLACED NR 2 SECU IAW MM 27-61-04. OPS CHECK GOOD.

Part: WEB — CRACKED (FUSELAGE) · airframe 21,049 hrs · 18,404 cycles

FOUND CRACK ON RIGHT AND LEFT SIDES OF FLOOR IN THE FORWARD EQUIPMENT COMPARTMENT AT FS 193.00, WL 79.50. FOUND DURING C CHECK INSPECTION. HDT-HFEC CARRIED OUT IAW CLIENT REQUEST AND NDTM PART 1, 51-20-01. NO CRACKS NOTED. DAMAGE REPAIRED IAW REO 601R-53-11-334.

Part: FRAME — CRACKED (FUSELAGE) · airframe 21,059 hrs · 18,410 cycles

FOUND RIGHT FRAME FS 640.0 STR 9R CRACK AT STR CUTOUT DURING C CHECK INSPECTION. REPAIRED DAMAGE AREA OF FRAME IAW CRJ REO 601R-53-61-532. NDT-HFEC CARRIED OUT IAW REO 601R-53-61-532. NO CRACKS NOTED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 21,049 hrs · 18,404 cycles

FOUND FS 484 RIGHT INTERCOSTAL RBL 27 ANGLE CRACKED. FOUND DURING C CHECK INSPECTION. NEW ANGLES FIT AND INSTALLED IAW CRJ REO 601R-53-41-059.

Part: PYLON — CRACKED (LEFT, FS 605) · airframe 21,049 hrs · 18,404 cycles

LEFT PYLON AT FS 605 IS CRACKED AT THE BOTTOM SIDE. FOUND DURING A C CHECK INSPECTION. REMOVED BLEED AIR LINES AND WIRING. FIT AND INSTALLED RIB IAW CRJ SRM 51-40-11, 51-42-06 & SRM 51-23-00. REINSTALL BLEED AIR DUCT IAW CRJ MM 30-21-01.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 21,049 hrs · 18,404 cycles

FOUND FS 280.0 RBL 9.0 FLOORBEAM INBOARD ANGLE CRACKED. FOUND DURING C CHECK INSPECTION. FIT AND INSTALLED NEW ANGLE IAW CRJ SRM 51-40-11, 51-42-13, 51-42-21.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 21,049 hrs · 18,404 cycles

FOUND FS 280.0 LBL 9.0 FLOORBEAM INBOARD AND OUTBOARD ANGLES CRACKED. FOUND DURING C CHECK INSPECTION. FIT AND INSTALLED NEW ANGLES IAW CRJ SRM 51-40-11, 51-42-13, 51-42-21 & FABRICATED ANGLES IAW REO 601R-53-11-171.

Part: BPSU — FAILED (T/E FLAP) · airframe 20,800 hrs · 18,217 cycles

FLAP FAIL MESSAGE DURING PREFLIGHT. REMOVED AND REPLACED LEFT BPSU IAW 27-51-10. OPS CHECK GOOD.

Part: ROD — MALFUNCTIONED (CABIN DOOR) · airframe 20,728 hrs · 18,160 cycles

AFTER DEPARTURE, AC WOULD NOT PRESSURIZE. F/A REPORTED CABIN DOOR VERY LOUD. RETURNED TO FIELD. REINSTALLED ROD ON DOOR PRESSURE VALVE IAW 52-11-15. OPS CHECK GOOD AT THIS TIME.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 19,415 hrs · 17,163 cycles

ON TAKEOFF AT ABOUT 50 KTS, EXPERIENCED AN ACCESS BUS CAUTION MESSAGE AND ABORTED THE TAKEOFF. AFTER PULLING OFF THE RUNWAY, ALL SYSTEMS APPEARED NORMAL EXCEPT LEFT AND RIGHT AOA HEAT. POWERED DOWN AND POWERED UP AIRCRAFT AND ALL SYSTEMS SEEM NORMAL. DEPOWERED PLANE AND RESET. COULD NOT DUPLICATE PROBLEM.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 19,270 hrs · 17,052 cycles

TAKEOFF OUT OF SLC NOSE GEAR FAILED TO COME UP AND HAD GEAR DISAGREE MESSAGE. GEAR DOWN PER QRH. GEAR DISAGREE MESSAGE DISAPPEARED. RETURNED TO SLC. REPLACED NOSE LANDING GEAR DOOR SELECTOR VALVE AND A NLG SELECTOR VALVE IAW MM 32-22-20 & 32-33-10. LANDING GEAR FUNCTION CHECK & NWS CHECK GOOD. NO LEAKS NOTED.

Part: ADC — MALFUNCTIONED (NR 2) · airframe 19,075 hrs · 16,896 cycles

AFTER DEPARTURE FO PFD LOST ALTITUDE TAPE AND ALTIMETER SETTING AND VSI INDICATION. RED BOXES ALT AND VSI DISPLAYED. UNABLE TO RESET. SWITCHED TO ADC 1 TO REGAIN INDICATIONS. RETURNED TO SLC. PERFORMED AIR DATA SYSTEM FUNCTIONAL TEST. NO FAULTS FOUND ON NR 2 ADC.

Part: WINDSHIELD — BROKEN (RIGHT) · airframe 18,963 hrs · 16,803 cycles

RIGHT WINDSHIELD BROKEN DURING TAXI BEHIND A B737.REMOVED AND REPLACED RIGHT WINDSHIELD IAW CRJ MM 56-11-01. P/N: NP-139321-10 S/N ON: 01208H4243

Part: PROXIMITY SENSOR — OUT OF ADJ (NLG) · airframe 18,656 hrs · 16,563 cycles

AFTER TAKEOFF AND SELECTING GEAR LEVER UP GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES ILLUMINATED IN EICAS. CONSULTED QRH AND RETURNED TO AIRPORT. ADJUSTED GAP ON OLEO STRUT - CENTERED PROXIMITY SENSOR PER 32-61-05. JACKED AIRCRAFT AND CYCLED GEAR. OPS CHECK GOOD.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 4,535 hrs · 4,030 cycles

HYDRAULIC EDP 1A CAUTION MESSAGE ON EICAS , NO HYDRAULIC FLUID QUANTITY IN SYSTEM NR 1. FOUND LEAKING HYDRAULIC LINE IN PYLON, REMOVED AND REPLACED HYDRAULIC LINE AND ENGINE DRAIN PUMP IAW MM 29-11-01. OPS CHECK GOOD. LEAK CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (STALL WARNING) · airframe 4,382 hrs · 3,904 cycles

30 SECONDS AFTER T/O, ''STALL WARNING'' CAUTION MESSAGE. COMPLIED WITH QRH & RETURNED TO SLC.REPLACED STALL PROTECTION UNIT. STALL PROBLEM OPS CHECKS GOOD IAW MM 27-35-01.

Part: STALL WARNING — FALSE ACTIVATION (COCKPIT) · airframe 17,204 hrs · 15,379 cycles

STALL FAIL CAUTION MESSAGE ON EICAS DURING CLIMBOUT. FOLLOWED QRH PROCEDURES. RETURNED TO SLC. RESET CIRCUIT BREAKERS CBP1, Q2 AND CBP4, C7. STALL FAIL MESSAGE WENT AWAY. OPS CHECK GOOD.

Part: HYDRAULIC LINE — LEAKING (ENGINE) · airframe 16,827 hrs · 15,054 cycles

DURING CLIMBOUT, LOST HYDRAULIC SYSTEM ONE PRESSURE AND QUANTITY. RETURNED TO SLC. FOUND HYDRAULIC LINE FOR ENGINE DRIVEN HYDRAULIC PUMP PSI LINE IN PYLON TO BE LEAKING. REMOVED AND REPLACED LINE. OPS CHECK AND LEAK CHECKED GOOD.

Part: ACTUATOR — MALFUNCTIONED (THRUST REVERSER) · airframe 16,664 hrs · 14,913 cycles

ON TAKEOFF ROLL RIGHT REVERSER UNLOCKED AND EICAS MESSAGE DISPLAYED. ABORTED TAKEOFF. UNABLE TO DEPLOY OR STOW RIGHT REVERSER. RIGHT THRUST REVERSER IS DEACTIVATED AND DEFERRED. CLEANED AND LUBRICATED THE 4 BALL SCREW ACTUATORS ON THE THRUST REVERSER ASSEMBLY. OPERATED THE REVERSER SEVERAL TIMES WITH NO PROBLEMS NOTED. RIGHT REVERSER OPS CHECKS GOOD.

Part: APU — FAILED (APU BAY) · airframe 16,531 hrs · 14,796 cycles

LAVATORY SMOKE DETECTOR MESSAGE. FLIGHT ATTENDANT REPORTS SMOKE IN CABIN. SMOKE DISSIPATED AND SMELLS LIKE OIL OR PACK SOURCE. INSPECTED AIRCRAFT AND FOUND APU SUSPECTED TO BE INOPERATIVE. DEFERRED THE APU.

Part: PCU — FAILED (SPOILER) · airframe 16,397 hrs · 14,682 cycles

SPOILERONS FAULT MESSAGE CAME ON INFLIGHT. REMOVED AND REPLACED LEFT INBOARD PCU ON LEFT SPOILERON IAW MM 27-26-01. OPS CHECK LEAK CHECK GOOD AT THIS TIME. PN ON 2700-7 SN ON MAL0581 SN OFF MAL0474

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 16,361 hrs · 14,653 cycles

N2 VIB AT ROTATION. CONTINUED. DID QRH AT SAFE ALTITUDE. N2. VIB WOULD GO OUT AT 81-82 PERCENT AND BACK ON AT 83-84 PERCENT HIGHER. ENGINE SOUNDED DIFFERENT AS WELL. RETURNED TO RAP. REMOVED AND REPLACED RIGHT ENGINE SUM TRANSDUCER IAW CRJ MM 77-31-01. PN 6233M30A SN ON BP28 SN OFF 088 BE78. OPS CHECK GOOD.

Part: BPSU — FAILED (TE FLAPS) · airframe 15,851 hrs · 14,198 cycles

FLAP FAIL MESSAGE ILLUMINATED EN ROUTE RAP. REMOVED AND REPLACED RIGHT PBSU AND FLAP CONTROL UNIT IAW MM 27-51-10 AND 27-51-05. OPS CHECKS GOOD AT THIS TIME. P/N ON: 860D100-18, S/N ON: 754, S/N OFF: 222.

Part: BPSU — OUT OF RIG (TE FLAPS) · airframe 15,851 hrs · 14,198 cycles

FLAP FAIL MESSAGE EN ROUTE AT FL33. MESSAGE WENT OUT DESCENDING THROUGH APPROXIMATELY 9000 FT. INSPECTED FLAPS, FOUND RIGHT BPSU OUT OF RIG AND REPLACED FLAP IAW 27-51-10. OPS CHECK GOOD.

Part: CONTROLLER — FAILED (WINDOW HEAT) · airframe 14,289 hrs · 12,764 cycles

AFTER LIFT OFF LEFT WINDOW HEAT MESSAGE CAME ON. RETURNED TO SLC. REMOVED AND REPLACED WINDSHIELD TEMPERATURE CONTROLLER (P/N 16591) (S/N 520) OFF, (S/N 418) ON, OPS CHECK GOOD IAW MM 304101. SW 301 AND 418 WERE SWAPPED FOR TROUBLESHOOTING WINDSHIELD CONTROLLER (S/N 418) WINDOW CONTROLLER OPERATIONAL CHECKS WERE GOOD.

Part: SENSOR — FAILED (WINDOW HEAT) · airframe 14,289 hrs · 12,764 cycles

AFTER LIFT OFF LEFT WINDOW HEAT MESSAGE CAME ON. RETURNED TO SLC. CONNECTED SPARE SENSOR ON LEFT WINDOW HEAT IAW 304106.

Part: SEAL — FAILED (PASSENGER DOOR)

AFTER DEPARTURE AIRCRAFT MAIN DOOR HAD LOUD SQUEAL AND AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO SLC. REMOVED AND REPLACED CABIN DOOR SEAL IAW SB 601R-52-067. PRESSURIZED AIRCRAFT AND ALL CHECKS GOOD.

Part: WIRE — CHAFED (LT ENGINE)

LEFT ENGINE JET PIPE OVERHEAT FAILED IN FLIGHT. SHUT ENGINE DOWN. FOUND LEFT ENGINE JET PIPE WIRES CHAFED TO GROUND. REPAIRED AND REPOSITIONED WIRES. TESTED JET PIPE SYSTEM, LEFT SIDE CHECKS GOOD.

Part: YAW DAMPER — INOP (NR 1)

YAW DAMPER 1 IS INOP. RETURNED TO FIELD. REMOVED AND REPLACED R1 YAW DAMPENER LINEAR ACTUATOR. REPLACED FLIGHT CONTROL PANEL, OPS CHECK OK FOR CAT II OPERATION.

Part: STRAP — CORRODED (BS 280-400)

THERE IS CORROSION IN A NUMBER OF PLACES IN BUTT STRAPS RBL 9, RBL 27, LBL 27 FROM STATION 280, STATION 400. REMOVED AND REPLACED BUTT STRAP, REMOVED CORROSION ON OTHER AREAS, IAW SRM 51-10-00.

Part: COMPUTER — FAILED (STALL WARNING)

STALL FAIL MESSAGE CAME ON DURING INITIAL CLIMB OUT. RETURNED TO SLC. REPLACED STALL WARNING COMPUTOR. OPS CHECKS GOOD.

Part: VALVE — FAILED (NLG)

NOSE GEAR DISAGREE AND WOULD NOT EXTEND. USED EMERGENCY GEAR EXTENSION. UPON LANDING, NO NOSE WHEEL STEERING. SYSTEM NR 3 HYDRAULIC PRESSURE 2400 PSI MAXIMUM. REPLACED NOSE LANDING GEAR SELECTOR VALVE IAW MM 32-31-00. CYCLED GEAR AND TAXIED AIRCRAFT. OPS CHECKS GOOD.

Part: PSEU — MALFUNCTIONED (E/E COMPT)

AFTER DEPARTURE THE FOLLOWING CAUTION MESSAGES APPEARED: L AOA HEAT, L STATIC, L PITOT, PITOT BASE HEAT, FOLLOWED QRH ELECTED TO RETURN TO SLC AIRPORT. REMOVED AND REPLACED PSEU. OPS CHECKS GOOD IAW MM 33-00-00.

Part: YAW DAMPER — FAILED (NR 2)

YAW DAMPER 2 FAILS INFLIGHT, BUT WOULD RESET AFTER SEVERAL SECONDS. RETURNED TO SLC. REPLACED NR 2 FCC 4000 IAW MM 22. OPS CHECKS GOOD FOR CATII.

Part: OIL SYST — REQD SERVICE (APU)

AT 57 MIN TO GO TO EUG, WE RECEIVED AND APU OIL TEMPERATURE MESSAGE. QRH CALLED FOR A DIVERSION TO NEAREST SUITABLE AIRPORT. SINCE EUG WAS IFR, THE SHUT DOWN OF APU WAS NOT AN OPTION. DIVERTED TO BOI. SERVICED APU OIL QUANTITY TO FULL, OPS CHECKS APU NORMAL PER MM 12-13-00.

Part: THERMO SWITCH — FAILED (RT BLEED)

BLEED AIR DUCT RED MESSAGE. RETURNED TO SLC. REMOVED AND REPLACED THERMO SWITCH AT 56 WK AND 58SF IAW MM 36-12-00, OPS CHECKS GOOD.

Part: HYD LINE — FAILED (NR 2 HYD SYST)

AFTER DEPARTURE APPROXIMATELY 80 MILES OUT OF BIL, NR 2 HYDRAULIC LOW PRESSURE ANNUNCIATOR LIGHT CAME ON. HYDRAUYLIC PAGE SHOWED NR 2 RESERVOIR AT 0 QUANTITY. RETURNED AND LANDED AT BIL. REMOVED AND REPLACED HYDRAULIC PRESSURE LINE ON RIGHT ENGINE PYLON. SERVICED RIGHT HYDRAULIC RESERVOIR TO 70 PERCENT. RAN ENGINE. OPS CHECKS AND LEAK CHECKS GOOD IAW MM 29-00-00.

Part: DE-ICE SYST — MALFUNCTIONED (AOA/TAT PROB)

RIGHT AOA HEAT AND TAT PROBE HEAT CAME ON DURING FLIGHT. RETURNED TO SLC. RECYCLED AIRCRAFT POWER. EICAS MESSAGE NOT DISPLAYED ON TAT PROBE HEAT. OPS CHECKS NORMAL AT THIS TIME.

Part: FLOORBEAM — CORRODED (BS 348)

ON FLOORBEAM LBL 9-00 AT FS 348 CORROSION AT INBOARD NUT PLATE. FABRICATED AND INSTALLED BACK UP ANGLE ON FLOORBEAM LBL 9-00 AT FS 348 IAW MM SRM 51-40-02.

Part: CROSSBEAM — CORRODED (CABIN)

AFT FS 349 CROSSBEAM CAPS BETWEEN LBL 9.00 AND LBL 27.00 AND BETWEEN LBL 27.00 AND FUSELAGE SIDE ARE REMOVED DUE TO DEEP CORROSION. REPLACED TWO WINDSCREEN SUPPORT LOCATED ON FS 349, BETWEEN LBL 9.00 AND FUSELAGE WALL IAW SRM 51-40-00.

Part: FLOORBEAM — CORRODED (BS 345)

ON FLOORBEAM RBL 9-00 AT FS 345 HAS CORROSION AT INBOARD NUT PLATE. FABRICATED AND INSTALLED DOUBLER REPAIR ON THE FLOORBEAM RBL 9-00 AT 345 IAW.

Part: FLOORBEAM — CORRODED (BS 336)

ON FLOORBEAM RBL 27-00 AT FS 336 CORROSION AT OUTBOARD NUT PLATE. FABRICATED AND INSTALLED A DOUBLER REPAIR ON THE FLOORBEAM IAW MM.

Part: FLOORBEAM — CORRODED (BS 345)

ON FLOORBEAM LBL 27-00 AT FS 345 ON OUTBOARD WING OF BEAM, CORROSION AT RIVETS. FABRICATED AND INSTALLED A DOUBLER REPAIR ON FLOORBEAM LBL 27 AT FS 345.

Part: STALL COMPUTER — MALFUNCTIONED (E/E COMPT)

STALL FAIL MESSAGE CAUTION CAME ON DURING DEPARTURE AND STAYED ON. REMOVED AND REPLACED STALL COMPUTER, OPS CHECKS GOOD.

Part: FLOOR BEAM — CORRODED (BS 295-349)

FLOOR BEAM RIGHT O/B RBL 27.00 WL 73.5 STA .295 TO 349, CORROSION FOUND ON TOP SURFACE. REMOVAL OF CORROSION IS BEYOND LIMITS OF REO 601R-53-00-005. FLOOR BEAM REPAIRED IAW 601R-53-21-058.

Part: FLOOR BEAM — CORRODED (BS 310-349)

FLOOR BEAM RT RBL 9.0 WL 73.50 STA 310 TO 349, CORROSION FOUND ON UPPER SURFACE. CORROSION BEYOND LIMITS OF REO 601R-53-00-00 SHT 3 FIG 1 .003 STN 319.0. FLOOR BEAM REPAIRED IAW REO 601R-53-21-058.

Part: SEAL — FAILED (CABIN DOOR)

MAIN CABIN DOOR SEAL LEAKS. VERY LOUD SQUEAL AND LOSS OF CABIN PRESSURE. REPLACED CABIN DOOR SEAL WITH A NEW UNIT. OPERATION AND LEAK CHECK GOOD.

Part: DE-ICE TUBE — FAILED (LT WING)

LT ANTI-ICE DUCT WARNING WING ANTI-ICE SWITCH NORMAL OR STANDBY POSITION. REMOVED LT OUTBD WING LEADING EDGE, REMOVED PICCALO TUBE, INSTALLED LEADING EDGE, IAW MM 57-41-01, GROUND RAN A/C OPS CKS GOOD, SEE F/L 2536.

Part: BPSU — FAILED (RT TE FLAPS)

FLAP FAIL CAUTION MESSAGE ILLUMINATED DURING LANDING. FLAPS WERE AT 45 DEGREES. REMOVED AND REPLACED RIGHT FLAP BPSU (BRAKE POSITION SENSING UNIT) IN ACCORDAMCE WITH MM 22-51-00. OPERATIONALLY CHECKS GOOD.