N410SW

Part: SWITCH — DEFECTIVE (AC BAY) · airframe 44,676 hrs · 37,226 cycles

LEFT PACK OVERHEATING, MAKING LOUD NOISE AND SMELLS LIKE SMOKE. (FLT 5647) REPLACED LEFT ACM TEMP SWITCH, REPLACED CONNECTOR TO LEFT ACM TEMP SWITCH AND REPLACED LEFT ACM IAW AMM. P/N ON/OFF: 782790-15 S/N ON: 200210170 S/N OFF: 200011034

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,144 hrs · 36,820 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4820) RELAMPED EMERGENCY LIGHT.

Part: RELAY — FAILED (EMERGENCY LIGHTS) · airframe 43,718 hrs · 36,412 cycles

EMERGENCY LIGHT IS ON WHEN IN THE ARMED POSITION. (FLT 4844) REPLACED K1XD RELAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,718 hrs · 36,412 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4844) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,509 hrs · 36,211 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4511) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,383 hrs · 36,086 cycles

RIGHT SIDE FORWARD EMERGENCY LIGHT IS OUT. (FLT 7766) RELAMPED EMERGENCY LIGHT.

Part: RESTRICTOR — DIRTY (SELECTOR VALVE) · airframe 43,325 hrs · 36,034 cycles

HYDRAULIC 3 LOW PRESSURE CAUTION UPON SELECTION OF LANDING GEAR TO THE DOWN POSITION AND LANDING GEAR SEEMED SLOW TO EXTEND. (FLT 4543) PURGED AIR FROM HYDRAULIC SYSTEM NR 3. REPLACED THE CHECK VALVE OF THE NLG SELCTOR VALVE AND CLEANED THE TWO WAY RESTRICTOR ON THE NLG SELECTOR VALVE IN REFERENCE TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,899 hrs · 35,632 cycles

EMERGENCY LIGHTS IN CABIN AT ROW 8 ARE OUT. (FLT 4666) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,809 hrs · 35,548 cycles

NR 1 MAIN CABIN DOOR EXTERNAL EMERGENCY LIGHT IS OUT. (FLT 4575) RELAMPED EMERGENCY LIGHT.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 42,621 hrs · 35,377 cycles

LEFT AND RIGHT FS 409+128 VERTICAL POSTS OUTBOARD C-CHANNELS ARE CRACKED. (C-CHECK) REPAIR PER REO.

Part: ACTUATOR — FAILED (NLG) · airframe 42,514 hrs · 35,273 cycles

HYD 3 LOW PRESS CAUTION MESSAGE. ON GEARS RETRACTION RECEIVED NOSE GEAR DISAGREE WARN FOR ABOUT 30 SEC. (FLT 4571) REPLACED NLG RETRACT ACTUATOR. P/N OFF 16520-101 S/N OFF: DH-0157-99

Part: PRIORITY VALVE — FAILED (NLG) · airframe 42,348 hrs · 35,117 cycles

GEAR DISAGREE WARNING MESSAGE ON GEAR RETRACTION. (FLT 4522) REMOVED AND REPLACED NR 3A ACMP AND NOSE LANDING GEAR PRIORITY VALVE. P/N ON 848847, S/N OFF Y20521, P/N ON 4622, S/N OFF 2153A.

Part: PIN — LACK OF LUBE (CABIN DOOR) · airframe 41,740 hrs · 34,558 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 4656) LUBED DOOR LATCH PINS.

Part: PIN — BENT (CABIN DOOR) · airframe 41,195 hrs · 34,083 cycles

MAIN CABIN DOOR PLUNGER HARD TO OPERATE. (FLT 4684) STRAIGHTENED ICE BREAK DOOR PLUNGER PIN.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,067 hrs · 33,968 cycles

LEFT FORWARD EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 4558) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,406 hrs · 32,500 cycles

AFT CEILING EMERGENCY FLOODLIGHT INOP. (FLT 4725) RELAMPED EMERGENCY LIGHT.

Part: FLOORBEAM — CHAFED (BS 280) · airframe 38,501 hrs · 31,742 cycles

C-CHECK, LANDING GEAR ALTERNATE RELEASE CABLE PULLEY CHAFING ON FS 280 BEAM. REPAIRED PER REO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,502 hrs · 31,743 cycles

LBL 18 CAP ANGLE RADIUS CRACKED. (C CHECK) REPAIRED PER REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 38,501 hrs · 31,742 cycles

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

Part: ANGLE — CRACKED (LT WING) · airframe 38,501 hrs · 31,742 cycles

LEFT WING BATT ANGLE AT WS 53 AND WS 48 CRACKED. (C CHECK) REPAIRED PER REO.

Part: VERTICAL BEAM — CRACKED (FUSELAGE) · airframe 38,501 hrs · 31,742 cycles

C-CHECK, AFT TOP RIGHT VERTICAL BEAM CRACKED AT FASTENER. REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,910 hrs · 32,086 cycles

FS 621 BULKHEAD CRACKED BELOW SPLICE STRAP. (C CHECK) REPAIRED PER REO.

Part: FRAME — CRACKED (CARGO BAY) · airframe 38,910 hrs · 32,086 cycles

FUSELAGE FRAME AT FS 605 ABOVE CARGO DOOR CRACKED. (C CHECK) REPAIRED PER REO.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 38,148 hrs · 31,449 cycles

NOSE GEAR DID NOT RETRACT. (FLT 4780) REPLACED NOSE GEAR SELECTOR VALVE. P/N: 750006000, S/N ON: 1731, S/N OFF: 1902.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,041 hrs · 31,361 cycles

EMERGENCY LIGHT AT SERVICE DOOR INOP. (FLT 4865) REPLACED LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,014 hrs · 31,339 cycles

OVERHEAD LIGHT POD NR 2 NOT WORKING. (FLT 4451) REPLACED NR 2 OVERHEAD EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,996 hrs · 31,324 cycles

RIGHT OVERWING EMERGENCY FORWARD LIGHT INOP. (FLT 4726) RELAMPED RIGHT OVERWING EXTERIOR EMERGENCY LIGHT (FWD).

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,996 hrs · 31,324 cycles

MAIN CABIN DOOR EMERGENCY EXIT LIGHT INOP. (FLT 4726) RELAMPED EMERGENCY LIGHT NEAR MCD EXTERIOR.

Part: DOOR — BINDS (CABIN) · airframe 37,716 hrs · 31,096 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 4731) OPERATIONAL CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,660 hrs · 31,055 cycles

LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOP. (FLT 4722) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — BROKEN (CABIN) · airframe 36,461 hrs · 30,115 cycles

FLT 4717 - PASSENGER DOOR EMERGENCY FLOOD LIGHT BROKEN INTO PIECES. REPLACED FLOOD LIGHT ASSEMBLY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 35,620 hrs · 29,485 cycles

EMERGENCY LIGHT BULB IN CEILING ROW 3 IS INOP. RELAMPED.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 35,570 hrs · 29,447 cycles

CRACK INDICATIONS NOTED AT AFT PRESSURE BULKHEAD LINTEL ATTACHMENT FITTING UPPER AND LOWER CORNER AREA. FOUND AT C-CHECK. REPAIRED PER REO 601R-53-61-1230 REV C.

Part: SUPPORT ANGLE — CRACKED (BS 621) · airframe 35,570 hrs · 29,447 cycles

STA 621 LT - SUPPORT ANGLE FROM PRESS BLKHEAD TO FLOOR CRACKED AT OUTBOARD END. FOUND AT C-CHECK. REPAIRED PER REO 601R-53-61-117.

Part: SKIN — CRACKED (LT AILERON) · airframe 35,570 hrs · 29,447 cycles

FS 559 UNDER RT SIDE LT AILERON HAS CRACKS IN WEB FOUND AT C-CHECK. REPAIRED PER REO 601R-53-41-260 STEP 13 A-E STEP 14 C,C REV "B".

Part: FLOOR SUPPORT — CORRODED (BS 424-559) · airframe 35,570 hrs · 29,447 cycles

RT AND LT CABIN FLOOR LINE STRUCTURE CORRODED FROM STA 424RT - 559RT. FOUND AT C-CHECK. REPAIRED PER REO 601R-53-41-724.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,570 hrs · 29,447 cycles

CRACK INDICATION NOTED ON AFT PRESSURE BULKHEAD LBL 36.20 JUST ABOVE LOWER LINER ATTACH CLIP. FOUND AT C-CHECK. REPAIRED PER REO 601R-53-61-1285 SHEET 11.

Part: HANDLE — WORN (PAX DOOR) · airframe 34,549 hrs · 28,661 cycles

FLT 3858 - PASSENGER DOOR HANDLE WILL NOT STOW. REPLACED PAX DOOR OUTER HANDLE ASSEMBLY IAW AMM 52-11-03. OPS CHECK GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 33,024 hrs · 27,513 cycles

HYDRAULIC SYSTEM NR 3 FLUID LEVEL IS 0%, FLIGHT NR 3763. REPLACED NOSE GEAR ACTUATOR AND PUMP 3B PRESSURE FLEXLINES IAW 32-33-01 AND 29-12-03. SERVICED NR 3 HYD SYSTEM.

Part: STRUT — BINDING (PAX DOOR) · airframe 32,900 hrs · 27,425 cycles

FLT 3865 - MAIN CABIN DOOR DOES NOT OPEN FREELY. REPLACED AFT PAX DOOR STRUT IAW AMM 52-11-17, PN: 601R31911-9.

Part: WIRE — BURNED (PFD) · airframe 32,157 hrs · 26,873 cycles

RECEIVED MULTIPLE CAUTION MESSAGES. THE NR 2 MFD, PFD AND THE RTU WENT DARK. REPLACED BURNED WIRES AND TERMINALS FROM CBP2 TO JB1 IAW WM 20-12-00. OPERATIONAL CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 31,805 hrs · 26,614 cycles

CAPTAIN'S WINDSHIELD CRACKED CLIMBING THROUGH FL 260. CAPTAIN’S WINDSHIELD INSTALLED IAW RII 56-220-1000 AND AMM 56-11-01. OPERATIONAL AND LEAK CHECKS GOOD.

Part: WINDSCREEN — CRACKED (COCKPIT) · airframe 31,805 hrs · 26,614 cycles

FIRST OFFICER'S WINDSCREEN SHATTERED ON PUSH BACK. REPLACED FIRST OFFICER'S WINDSCREEN IAW AMM 56-11-01 AND RII 56-220-1000, PN OFF: NP-139321-6, SN OFF: NSN.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 31,782 hrs · 26,598 cycles

AFT EMERGENCY CEILING LIGHT INOP. REPLACED LAMP IN AFT CEILING EMERGENCY LIGHT AS NEEDED. OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,686 hrs · 25,798 cycles

LOWER EXIT SIGN/LIGHT AT SERVICE DOOR INOP. REPLACED LOWER SERVICE DOOR LIGHT. OPERATIONAL CHECKS GOOD, PN: 6020-5.

Part: STRUT — LOW (NLG) · airframe 30,329 hrs · 25,518 cycles

AFTER TAKEOFF GOT GEAR UP DISAGREE AND THE NOSE GEAR WAS STILL DOWN. RETURNED TO FIELD. PERFORMED NOSE SHOCK STRUT SERVICE IAW ST 12-710-002. OPERATIONAL CHECKS GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,538 hrs · 25,683 cycles

ANGLE CRACKED AT STA 624 (AFT SIDE OF PRESSURE BULKHEAD) WL79 RBL40, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW ANGLE P/N 601R-35012-52 PO 64041 AS PER SRM 51-42-20 PG 23.

Part: CHANNEL — CRACKED (WING) · airframe 30,538 hrs · 25,683 cycles

'C' CHANNEL CRACKED AT WING STATION 75.5 UNDER LT I/B GROUND SPOILER, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW 'C' CHANNEL P/N 601R-10224-13 PO 67750 AS PER CRJ200 SRM REF 51-42-06 PG 11.

Part: PIN — CORRODED (EMERGENCY EXIT) · airframe 30,538 hrs · 25,683 cycles

LEFT OVERWING EMERGENCY EXIT BOTH HOOK FITTING PINS CORRODED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED LT OVERWING EMERGENCY EXIT HOOK FITTING PINS PER CRJ200 AMM TASK 52-21-00-820-001 PG 504 ITEM 8.

Part: PLATE — CRACKED (PAX DOOR) · airframe 30,538 hrs · 25,683 cycles

HANDLE MOUNT PLATE IS CRACKED ON 2ND STEP OF PAX DOOR, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW MOUNTING PLATE AND REINSTALLED 'T' KNOB PER CRJ200 AMM 52-11-03-400-803 STEPS 3.A.(3) THRU 3.A.(5).

Part: PIN — CORRODED (EMERGENCY EXIT) · airframe 30,538 hrs · 25,683 cycles

RT OVERWING EMERGENCY EXIT BOTH HOOK FITTING PINS CORRODED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED RT OVERWING EMERGENCY EXIT HOOK FITTING PINS PER CRJ200 AMM SUBTACK 52-21-00-820-001 PG 504 ITEM 8.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 30,538 hrs · 25,683 cycles

FLOOR SUPPORT BRACKET CORRODED UNDER CABIN FLOOR PNL 251CLF LOCATED NEAR AFT DOOR SILL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW BRACKET P/N 601R-31527-217 PO 39002 AND 601R31527-137 PO 39002 ON AFT DOOR SILL UNDER FLOOR PANEL 231CLF AS PER CRJ200 SRM REFERENCE 51-42-06 PG 11.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 30,538 hrs · 25,683 cycles

TWO CRACKS IN AFT DRAG ANGLE ON PAX DOOR, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE SECTION AND SPLICE ANGLES ON PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513 REV 'A'.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,189 hrs · 25,413 cycles

SECOND CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. REPLACED SECOND CEILING EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD, PN 1317.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 29,052 hrs · 24,563 cycles

ON TAXI IN AT SLC, SPOILERON FAULT STATUS MSG. REPLACED LEFT OUTBD SPOILERON PCU IAW CRJ 200 MM 27-62-01. OPERATIONAL CHECK OK, PN 27000-7 SN OFF MAL 437.

Part: CONTROL UNIT — MALFUNCTIONED (MOTOR) · airframe 27,659 hrs · 23,505 cycles

FFOD CHECKS STAB TRIM CH 1 INOPERATIVE. REPLACED HSTA AND MCU IAW 33-27-415 AND MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD, PN 8396-3 SN OFF 1087.

Part: TRIM SWITCH — STICKS (COCKPIT) · airframe 27,272 hrs · 23,194 cycles

CAPT YOKE STAB TRIM SWITCH STICKS. REPLACE TRIM SWITCH IAW MM 27-44-03. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 26,928 hrs · 22,921 cycles

STAB TRIM CHANNEL TWO WOULD NOT ENGAGE. REPLACED HSTCA IAW 27-42-01 AND MCU IAW 27-42-05. OPERATIONAL CHECK GOOD.

Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 26,928 hrs · 22,921 cycles

STAB TRIM CH 2 INOP. REPLACED CAPT'S STAB DISCONNECT SWITCH IAW CRJ MM 27-41-30, OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 26,911 hrs · 22,908 cycles

STAB TRIM CH 2 INOPERATIVE. REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW 27-42-01. OPERATIONAL CHECK GOOD, PN: 8396-3 SN OFF: 843.

Part: DOOR FRAME — CORRODED (PAX DOOR) · airframe 25,725 hrs · 21,983 cycles

PAX DOOR FORWARD AND AFT LOWER CORNERS FRAMES CORRODED, ITEM FOUND AT C-CHECK INSPECTION. CORNER FITTINGS REPLACED IAW CRJ REO 601R52-11-0600, REO 601R-52-11-583.

Part: BEAM — CRACKED (FUSELAGE) · airframe 25,725 hrs · 21,983 cycles

VERTICAL BEAM AT FS 409+128 LBL 27 INBOARD SIDE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-056 REV "C.

Part: CLIP — CRACKED (FUSELAGE) · airframe 25,725 hrs · 21,983 cycles

AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14R, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-25-16.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 25,725 hrs · 21,983 cycles

MAIN AVIONICS COMPARTMENT INTERCOSTAL STR 26L BETWEEN FS 349 AND FS 364 CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) CORRODED SECTION OF INTERCOSTAL BLENDED OUT IAW CRJ SRM 53-00-00 MATERIAL LOSS OF .004' WITHIN LIMITS. REINSTALLED INTERCOSTAL IAW CRJ SRM 51-42-21, 51-42-06, 51-23-00, 51-25-06, 51-25-16.

Part: FRAME — CRACKED (PAX DOOR) · airframe 25,725 hrs · 21,983 cycles

PAX DOOR 7 INCHES ABOVE DATUM 1 AT FS 320.1 AND 338.9 FORMERS ARE CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) REPAIRED IAW CRJ REO 601R-52-11-609.

Part: VERTICAL BEAM — CRACKED (FUSELAGE) · airframe 25,725 hrs · 21,983 cycles

VERTICAL BEAM AT FS 409+128 RBL 27 INBOARD SIDE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-056 REV. "C".

Part: RISER — CORRODED (PAX DOOR) · airframe 25,725 hrs · 21,983 cycles

PAX DOOR SILL RISER CORRODED IN SEVERAL LOCATIONS. (ITEM FOUND AT C-CHECK INSPECTION.) AFFECTED AREAS REPAIRED IAW CRJ SRM 53-21-23

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,725 hrs · 21,983 cycles

AFT EQUIPMENT COMPARTMENT FRAME IS CRACKED; FS 640.00 STR 9L, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-557 REV "NC"

Part: CLIP — CRACKED (FUSELAGE) · airframe 25,725 hrs · 21,983 cycles

AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14L, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP CRJ SRM 51-40-11, 51-42-06, 51-25-16.

Part: PLATE — CORRODED (FUSELAGE) · airframe 25,725 hrs · 21,983 cycles

CARGO PIT; CARGO DOOR ENTRY LANDING PLATE HAS CORROSION AROUND A/NUT LOCATIONS, UPPER AND LOWER SURFACES AT FS 574.0 TO 621.0 LBL 42, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ SRM 53-61-23 & 53-00-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,725 hrs · 21,983 cycles

AFT EQUIPMENT COMPARTMENT FRAME IS CRACKED; FS 640.00 STR 9R, ITEM FOUND AT C-CHECK INSPECTION. FRAME REPAIRED IAW REO 601R-53-61-557 REV NC.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,725 hrs · 21,983 cycles

CORROSION ON FRAME 349.0 STR 26L AND ON FRAME 364.0 STR 26L IN AVIONICS CRAWL WAY. (ITEM FOUND AT C-CHECK INSPECTION.) AFFECTED AREAS REPAIRED IAW CRJ SRM 53-21-15.

Part: WEB — CRACKED (HORIZ STAB) · airframe 25,725 hrs · 21,983 cycles

LEFT HORIZONTAL STAB WEB CRACKED FROM LIGHTNING HOLE AT LBL 58.92 AND STRINGER NR 2, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED LT HORIZONTAL STAB, WEB AT LBL 58.92 AND STRINGER NR 2, IAW CRJ REO 601R-55-11-136.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 25,725 hrs · 21,983 cycles

HORIZONTAL STAB ANTI-ROTATION FITTING CORRODED, ITEM FOUND AT C-CHECK INSPECTION. HORIZONTAL STAB ANTI-ROTATION FITTING REPLACED IAW SB 601R-55-007.

Part: RIB — CRACKED (LT PYLON) · airframe 25,725 hrs · 21,983 cycles

LEFT PYLON AFT RIB IS CRACKED; FS 605.00, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED RIB IAW SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 25,725 hrs · 21,983 cycles

CARGO PIT FLOOR SUPPORT LBL 27.0 CRACKED AT 3 LOCATIONS INBOARD SIDE BETWEEN FS 574.0 TO 621.0, INBOARD WEB BUCKLED BETWEEN FS 574.0 TO FS 589.0. ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-42-06, 51-42-10, 51-42-21.

Part: WEB — CRACKED (PAX DOOR STEP) · airframe 25,725 hrs · 21,983 cycles

PAX DOOR BOTTOM STEP LOWER WEB CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ SRM 51-71-59.

Part: BEAM — CRACKED (FUSELAGE) · airframe 25,725 hrs · 21,983 cycles

FUSELAGE UPPER FLANGE ON TRANSVERSE BEAM IS CRACKED; FS 280.00, RBL 9.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 60R53-11-13 REV "NC" RII 53-401.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 25,725 hrs · 21,983 cycles

FUSELAGE; PULLEY INTERTCOSTAL HAS A CRACKED REMOTE ANGLE FS 484.00; LBL-27.0, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ REO 601R53-41-059 REV "A" .

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 25,610 hrs · 21,896 cycles

THIRD AFT EMERGENCY CEILING LIGHT INOPERATIVE. REMOVED AND REPLACED 3RD AFT CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECK GOOD IAW MM 33-00-00.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 25,348 hrs · 21,690 cycles

FLAP FAIL MESSAGE DURING FLAP RETRACTION OUT OF SLC. RETURN TO FIELD. REPLACED FECU IAW MM 27-51-05 AND LEFT NR 5 FLAP FLEX SHAFT IAW CRJ 200 MM 27-53-10. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 25,125 hrs · 21,512 cycles

FIRST FLIGHT OF DAY TRIM CHECK, STAB TRIM 2 FAILED. REMOVED AND REPLACED BOTH HST AND MOTOR CONTROL UNIT IAW MM 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 597.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 24,976 hrs · 21,387 cycles

ON SHORT FINAL WHILE RUNNING STAB TRIM, STAB AND MACH TRIM CAUTION MESSAGE DISPLAYED. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 24,816 hrs · 21,249 cycles

STABILIZER TRIM (BOTH CHANNELS) DISENGAGED DURING CLIMB. REMOVED AND REPLACED F/O'S TRIM SWITCH. OPERATIONAL CHECK GOOD IAW MM 27-41-05 AND 27-40-00.

Part: LOOP — MALFUNCTIONED (LT NACELLE) · airframe 24,489 hrs · 20,999 cycles

INFLIGHT FROM OAK TO SLC LEFT 14TH DUCT MSG POSTED, SHUTDOWN LEFT ENGINE. REMOVED AND REPLACED LEFT 14TH STAGE PYLON LOOP WITH SERVICEABLE UNIT IAW MM 36-21-04. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 24,197 hrs · 20,775 cycles

ON DESCENT INTO SLC THE A/C PITCHED UP AND GAVE A AP PITCH TRIM & NOSE UP TRIM CAUTION. STAB TRIM AND MACH TRIM DROPPED OFF 3 TIMES. NOTE: WITH AUTO PILOT OFF THE TRIM WAS NOT MOVING AND THE STAB TRIM KICKED OFF. REMOVED AND REPLACED THE HSTCU IAW MM 27-41-01. OPERATION CHECKS SATISFACTORY AT THIS TIME. NO DEFECTS NOTED. S/N OFF: 175.

Part: ACTUATOR — MALFUNCTIONED (RUDDER TRIM) · airframe 24,034 hrs · 20,657 cycles

RUDDER TRIM CB 2F6 POPPED. REMOVED AND REPLACED RUDDER TRIM ACTUATOR IAW MM 27-22-01. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 23,676 hrs · 20,387 cycles

F/O TRIM DISCONNECTS BOTH STABS AND MACH TRIMS. REMOVED AND REPLACED HSTA. FUNCTION CHECK SATISFACTORY IAW CRJ MM 27-42-01.

Part: COMPUTER — MALFUNCTIONED (FLIGHT CONTROL) · airframe 23,218 hrs · 20,039 cycles

AP PITCH TRIM CAUTION MESSAGE AT 6500 FEET MSL (2300 AGL) ON FINAL. REMOVED AND REPLACED FCC 4000 CARDS 1A & 2A IAW MM 22-12-14. OPS CHECK GOOD. P/N: 622-9815-704, S/N OFF: 854.

Part: SKIN — CRACKED (FUSELAGE) · airframe 21,721 hrs · 18,853 cycles

FS 235 FUSELAGE SKIN RBL 6.0 NLG CUTOUT CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-11-048 REV B.

Part: SKIN — CRACKED (FUSELAGE) · airframe 21,721 hrs · 18,853 cycles

FS 235 FUSELAGE SKIN LBL 6.0 NLG CUTOUT CRACKED. DISCOVERED DURING C-CHECK. DAMAGE REPAIRED IAW CRJ REO 601R-3-11-048 REV B.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 21,721 hrs · 18,853 cycles

FS 484 RT INTERCOSTAL O/B FLG RBL 3G CRACKED. DISCOVERED DURING C-CHECK. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-11-059.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,721 hrs · 18,853 cycles

SERVICE DOOR SILL PLATE CORRODED. DISCOVERED DURING C-CHECK. DAMAGE FOUND TO BE OUT OF LIMITS. REPLACED SERVICE DOOR SILL PLATE WITH NEW PART IAW CRJ SRM 51-40-11.

Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 21,721 hrs · 18,853 cycles

FS 280 PILOT'S BULKHEAD LBL 90 AFT FLOOR ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-11-138 NC.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 21,721 hrs · 18,853 cycles

FS 193 ELECTRICAL BAY RT FLOOR CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGE IAW CRJ REO 601R-53-11-245 REV NC.

Part: CONTROLLER — MALFUNCTIONED (RT ADC) · airframe 20,388 hrs · 17,809 cycles

AFTER TAKEOFF WE RECEIVED RIGHT AOA HEAT, R STATIC HEAT, R PITOT HEAT AND TAT PROBE HEAT CAUTION MESSAGES. RETURNED TO SLC. REMOVED AND REPLACED THE RIGHT SIDE AIR DATA SENSOR CONTROLLER. SYSTEM OPS CHECKS GOOD.

Part: FIRE LOOP — CHAFED (RT ENGINE) · airframe 19,136 hrs · 16,829 cycles

RECEIVED RIGHT 14TH STAGE DUCT LEAK WARNING CLIMBING THROUGH 7000 FT. AS PER QRH, RETARDED RIGHT ENGINE THRUST TO IDLE. AFTER 40 SECONDS STILL HAD THE WARNING. CLOSED THE RIGHT 14TH STAGE BLEED AND WARNING CLEARED. RETURNED TO OMA. FOUND 14TH STAGE LOOP TO BE CHAFED IN RIGHT ENGINE PYLON. REMOVED AND REPLACED CHAFED SECTION. OPS CHECK GOOD.

Part: CHECK VALVE — MALFUNCTIONED (LEFT PACK HEAT E) · airframe 19,068 hrs · 16,774 cycles

LEFT PACK FAILED INFLIGHT. RIGHT PACK DEFERRED. PERFORMED EMERGENCY DESCENT PROCEDURE PER QRH. LEFT PACK HEAT EXCHANGER CHECK VALVE HINGE AND SPRING WORN. REMOVED AND REPLACED CHECK VALVE (FAN BYPASS) PER MM 21-52-07. LEFT PACK OPS OK. P/N: 350023000.

Part: FILTER — DIRTY (DISPLAY COOLING) · airframe 18,753 hrs · 16,528 cycles

''DISPLAY COOL'' CAUTION MESSAGE DURING FLIGHT. MESSAGE PERSISTED AFTER 1ST STEP PER QRH. MESSAGE WENT AWAY AFTER SWITCHING TO STBY. RETURNED TO SLC. REMOVED AND REPLACED THE DISPLAY FILTER AS REQUIRED. OPS CHECK GOOD. PN 196305.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 18,288 hrs · 16,167 cycles

GEAR DISAGREE ON TAKEOFF. NOSE GEAR WOULD NOT COME UP. INSPECTED NOSE GEAR TORQUE LINKS, PROX SWITCHES AND STEERING. NO DEFECTS NOTED. JACKED A/C NOSE, SWUNG NOSE LANDING GEAR WITH NO DEFECTS NOTED. GEAR OPS CHECK GOOD.

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 18,231 hrs · 16,123 cycles

NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. CREW NOTED CHUNK OF ICE FELL FROM GEAR WHEN DOORS OPENED. PERFORMED NOSE GEAR RETRACTION TEST PER MM 32-30-00. NO DISCREPANCIES NOTED.

Part: POWER CABLE — CONTAMINATED (CABIN) · airframe 17,818 hrs · 15,813 cycles

CABIN FLOOR EMERGENCY LIGHT FWD SECTION INOP. FOUND ONE LAMP SECTION BAD. REPLACED LAMP. FOUND POWER CABLE FOR FLOOR LIGHT WET AND SHORTING. DRIED FLOOR. DRIED POWER CABLE. OPS CHECKED GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 17,757 hrs · 15,770 cycles

AFTER TAKEOFF DURING GEAR RETRACTION NOSE GEAR FAILED TO RETRACT AND WAS ACCOMPANIED BY GEAR DISAGREE AND NOSE DOOR OPEN MESSAGES WITH GEAR INDICATION SHOWING BOTH MAINS WHITE AND THE NOSE YELLOW. RETURNED TO THE AIRPORT. PERFORMED LANDING GEAR OPERATIONAL CHECKS. SWUNG GEAR 15 CYCLES WITH NO DEFECTS NOTED AT THIS TIME. OPERATIONAL CHECKS SATISFACTORY.

Part: SOCKET — FAULTY (CABIN) · airframe 17,750 hrs · 15,763 cycles

EMERGENCY LIGHTS ARE ON WITH THE SWITCH IN ARMED POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT REFLECTOR AND SOCKET ASSEMBLY AFT OF RT OVERWING EMERGENCY EXIT DUE TO FAULTY CONTACTOR IAW MM 33-51-21. EMERGENCY EXIT LIGHTING SYSTEM OPERATIONAL AND FUNCTIONAL CHECKS GOOD IAW MM 33-51-00. REFLECTOR (P/N BM5-0017-901), SOCKET (P/N BB1-0001-013).

Part: BEAM — CRACKED (ENGINE PYLON) · airframe 17,638 hrs · 15,682 cycles

ENGINE PYLON BOX BEAM LOWER WEB CRACKING FROM ANCHOR NUTS AT STRESS PANEL FS 640 LEFT AND RIGHT SIDES. REPAIRS ACCOMPLISHED IAW REO 601R-53-61-366, LEFT AND RIGHT SIDES OF BOX BEAM. HFEC INSPECTION CARRIED OUT IAW REO 53-61-366. NO CRACKS FOUND.

Part: BOLT — CORRODED (RT WING) · airframe 17,638 hrs · 15,682 cycles

RIGHT WING TRAILING EDGE NEAR AILERON POSITIONING TRANSMITTER HAS 3 CORRODED BOLTS. NEW HARDWARE INSTALLED IAW CRJ MM 27-15-01.

Part: BEAM — CRACKED (ENGNE PYLON) · airframe 17,638 hrs · 15,682 cycles

ENGINE PYLON BOX BEAM UPPER WEB HAS 2 CRACKS AT LBL 8.0 AND RBL 7.5, RADIATING FWD FROM TRAILING EDGE OF BEAM. CARRY OUT REPAIRS TO LOWER BOX BEAM WEB IAW REO 601R-53-61-345 AND 601R-53-61-368. CARRY OUT REPAIRS TO UPPER BOX BEAM WEB IAW REO 601R-53-61-442. NDT HFEC CARRIED OUT IAW REO'S 601R-53-61-345 AND 601R-53-61-442.

Part: PROXIMITY SWITCH — OUT OF ADJ (CARGO DOOR) · airframe 17,492 hrs · 15,567 cycles

ON TAKEOFF, HAD A CARGO DOOR CAUTION MESSAGE. PERFORMED ADJUSTMENT/TEST OF CARGO DOOR PROX SWITCHES PER CRJ MM 52-70-02. OPS CHECK FOUND GOOD.

Part: SWITCH — FAILED (COCKPIT) · airframe 16,760 hrs · 14,980 cycles

STAB TRIM CH NR 1 & 2 AND MACH TRIM ALL DISENGAGED SHORTLY AFTER TAKE OFF, RETURNED FOR LANDING. INSTALLED NEW STAB TRIM DISCONNECT SWITCH ON FIRST OFFICER'S SIDE. PN 996-0013. OPS CHECK GOOD, OK FOR CAT II OPERATIONS.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 16,621 hrs · 14,869 cycles

ON TAKEOFF ROLL ABOVE APPROXIMATELY 90 PERCENT N1, HAD A RED WARNING MESSAGE CONFIG AILERON AND CONFIG TRIM WITH AURAL WARNING. TRIM WAS IN THE GREEN. ABORTED TAKEOFF. PERFORMED OPS CHECK IAW AMM 31-41-00. RAN ENGINES ABOVE 70 PERCENT N1 AND HAD (T/O CONFIGURATION OK). COULD NOT DUPLICATE. OPS CHECK OF SYSTEM OK.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 16,519 hrs · 14,781 cycles

LEFT WINDSHIELD CRACKED. REMOVED AND REPLACED LT SIDE WINDOW (WINDSHIELD) IAW CRJ MM 56-12-01. PRESSURIZED AIRCRAFT TO 3.0 PSI. OPS LEAK CHECK OF WINDOW CHECKS GOOD. P/N ON 601R33033-11, S/N ON 0145H9919, S/N OFF 601R33033-3, S/N OFF 95039H2892 NP-139322-5-6.

Part: CONTROL UNIT — CONTAMINATED (HORIZ STAB) · airframe 16,395 hrs · 14,668 cycles

STAB TRIM CHANNEL 2 WILL NOT ENGAGE. WITH STAB TRIM CHANNEL 1 ENGAGED, THE MACH TRIM WILL NOT ENGAGE. REMOVE AND REPLACE MOTOR CONTROL UNIT (MCU) HORIZONTAL STABILIZER TRIM ACTUATOR IAW 27-42-01. FOUND HORIZONTAL STABILIZER CONTROL UNIT (HSTCU) WET WITH WATER. REMOVE AND REPLACE HSTCU IAW 27-41-01. OPS CHECK GOOD. COMPLIED WITH OPS CHECK OF MACH TRIM IAW 27-35-25. OPS CHECK GOOD AT THIS TIME. MCU: P/N ON 7026-2, S/N ON 218, S/N OFF 328, HSTA: P/N ON 8396-3, S/N ON 281, S/N OFF 910, HSTCU: P/N ON 7060-8, P/N OFF 7060-7, S/N ON 174, S/N OFF 350.

Part: ADC — FAILED (COCKPIT) · airframe 16,377 hrs · 14,656 cycles

ADC1 FAILURE, MAC TRIM FAILURE, IAS 1 FAIL, FD FAILURE - CAT II. REMOVED AND REPLACED NR 1 ADC 850A AND NR 1 ADC DRAIN ASSEMBLY. OPS CHECK GOOD IAW 34-13-01. CAT II OK FOR CAT II. P/N: 822-0372-140, S/N ON: 2145, S/N OFF: 1102.

Part: RESERVOIR — FAILED (HYD SYSTEM) · airframe 16,202 hrs · 14,502 cycles

AFTER TAKEOFF SELECTED GEAR UP AND HYDRAULIC NUMBER THREE LOW PRESSURE CAUTION CAME ON, FOLLOWED BY GEAR UP DISAGREE (BOTH MAIN GEAR). ALSO, NOSE DOOR OPEN WARNING MESSAGE CAME ON. NOTED NUMBER THREE HYDRAULIC SYSTEM FAILURE (3A & 3B PUMP PSI 0). RETURNED TO PSC. REPLACED HYDRAULIC NUMBER THREE RESERVOIR AND BOTH HYDRAULIC PUMPS. CHANGED FILTERS AND LEAK CHECK SYSTEM IAW 29-12-00. JACKED AIRCRAFT AND PERFORMED LANDING GEAR CHECK. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 14,810 hrs · 13,266 cycles

SETTING FLAPS FROM 0 DEGREES TO 8 DEGREES FLAPS FAILED AT 0 DEGREES WITH ATTENDING FLAP FAIL CAUTION MESSAGE. PERFORMED A ''''NO FLAP'''' LANDING. FOUND RIGHT HAND FLAP NUMBER 4 FLEX SHAFT SHEARED AND NUMBER 4 FLAP ACTUATOR BAD ON THE RIGHT SIDE. REPLACED DUE TO AD 98-20-01. REMOVED AND REPLACED NUMBER 4 FLEX SHAFT IAW AMM 27-53-10 AND REPLACED NUMBER 4 ACTUATOR IAW AMM 27-53-05. OPS CHECK GOOD.

Part: DRAG BRACE — DAMAGED (NLG) · airframe 14,184 hrs · 12,701 cycles

NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO FIELD. REMOVED AND REPLACED NOSE LANDING GEAR DRAG BRACE IAW MM 322105. OPS AND LEAK CHECKS GOOD. P/N ON: 16400105, SN: PCL07094, SN OFF: DCLO7494.

Part: SENSOR — MALFUNCTIONED (AIR DATA)

PITOT BASE OVERHEAT WARNING ILLUMINATED AFTER TAKEOFF. RETURNED TO FIELD. POWERED AIRCRAFT DOWN AND BACK UP. NO DEFECTS NOTED AT THIS TIME. AIRCRAFT GOOD FOR CONTINUED SERVICE. REMOVED AND REPLACED AIR DATA SENSOR CONTROLLER AFTER ARRIVAL IN SLC. OPS CHECKS GOOD IN OVERWEIGHT ON WHEELS CONFIGURATION.

Part: OVERHEAT MESSAGE — MALFUNCTION (RT 14 STG DUCT)

RIGHT 14TH STAGE DUCT OVERHEAT MESSAGE EN ROUTE. QUICK REFERENCE HANDBOOK PERFORMED AND MESSAGE PERSISTS. SINGLE ENGINE PROCEDURE PERFORMED AND DUCT MESSAGE PERSISTS. LEFT BECAME INTERMITTENT JUST PRIOR TO LANDING. FIRE CREWS REPORTED NO SIGN OF FIRE. REMOVED AND REPLACED RIGHT PYLON 14TH STAGE DUCT ELEMENT PER MM 36-11-05. RAN ENGINES AND INSPECTED 14TH STAGE DUCT AND COWLING ANTI ICE DUCTING FOR LEAKS. NONE NOTED. OPERATIONALLY RAN RIGHT ENGINE FOR 20 MINUTES WITH NO 14TH STAGE DUCT MESSAGE DUCT. MONITOR TEST GOOD.

Part: FECU — FAILED (TE FLAPS)

FLAP FAIL MSESSAGE DURING FLAP RETRACTION ON CLIMB-OUT. RETURNED FOR LANDING. REMOVED FLAP PDU AND FECU AND REPLACED WITH SERVICEABLE UNITS IAW MM 27-52-01. ALL CHECKS GOOD.

Part: ADC — FAILED (NR 1)

ON APPROACH TO EUG PFD NR 1 LOST ALL AIR DATA (AIRSPEED, ALTITUDE, ATTITUDE, VSI) ALSO MACH TRIM. REMOVED AND REPLACED IDC 4000 CONVERTER. ALL SYSTEMS CHECKS NORMAL.

Part: FIRE LOOP — MALFUNCTIONED (LT ENGINE)

LEFT JET PIPE LOOP A FAILED. MEL 26-11-2, INSPECTED LEFT EXHAUST NOZZLE FAIRING FOUND LOOSE HARDWARE. REMOVED AND INSTALLED SERVICEABLE HARDWARE AND SECURED IAW MM 78-11-01. OPS CHECKS OF ENGINE FIRE/OVERHEAT DETECTION GOOD AT THIS TIME IAW MM 26-11-00-710.

Part: WEB — TORN (RUDDER)

ON CLIMBOUT, HEARD A VERY LOUD LOW FREQUENCY VIBRATION. OCCURRED 2 TIMES AND SUBSIDED BOTH TIMES WITHOUT ANY CHANGES BY CREW TO CONFIGURATION. RETURNED TO TUC FOR PRECAUTIONARY LANDING. INSPECTED ENTIRE AIRCRAFT EXTERNALLY. INSPECTED INTERIOR OF BELLY AND ALL AIRCRAFT DUCTS. FOUND LIGHTING HOLES IN BOTTOM OF RUDDER TORN AND MADE INTERIM REPAIR IAW MM. NO OTHER DISCREPANCIES NOTED.

Part: AHRS — MALFUNCTIONED (LEFT)

AFTER TAKEOFF ATTITUDE AND HEADING BECAME INOP, YAW DAMPER 1 BECAME INOP AND AUTO PILOT INOP. RETURNED TO SLC. REPLACED CAPTAINS AHRS COMPUTER. OPS CHECKS GOOD IAW MM 34-21-01. THIS AIRCRAFT IS CATEGORY II.

Part: ANGLE — CORRODED (CABIN)

FLOOR SUPPORT ANGLE IN PASSENGER DOOR OPENING HAS CORROSION. REMOVED LOWER FLOOR BOARD SUPPORT ANGLE IN ENTRANCE WAY OF CABIN DOOR AND FABRICATED NEW ANGLE FROM S3992 MATERIAL AND INSTALLED IAW SRM 51-24-16.

Part: DOWNLOCK PIN — DIRTY (LANDING GEAR)

AIRCRAFT FERRIED TO PSP DUE TO NOSE LANDING GEAR NOT COMING UP AT SFO. RETURNED TO FIELD FOR LANDING. JACKED AIRCRAFT UP AND FOUND DIRT IN GEAR DOWNLOCK PIN. CLEANED AND OPERATED GEAR PER MM 32-30-00, OPS CHECKS GOOD.

Part: DRAG BRACE — FAILED (NLG)

TAKEOFF BUR, NOSE GEAR WOULD NOT RETRACT. NOSE GEAR REMAINED DOWN WITH NO TRANSIT INDICATION. CYCLED FOUR TIMES TO GET NOSE GEAR UP. REPLACED NOSE GEAR DRAG BRACE IAW CRJ MM 32-21-05 AND SWA RII 32-402.

Part: PRIORITY VALVE — MALFUNCTIONED (MLG)

AFTER DEPARTURE, NOSE GEAR FAILED TO RETRACT. PERFORMED QRH CHECKLIST. RETURNED TO PDX WITH A NORMAL LANDING. REMOVED AND REPLACED MAIN LANDING GEAR PRIORITY VALVE IAW MM 32-32-15, OPS AND LEAK CHECK GOOD.

Part: RETRACT MECH — MALFUNCTIONED (NLG)

NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. ATTEMPTED QRH PROCEDURES WITH NO CHANGE. RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN MESSAGE A FEW SECONDS LATER. INSPECTED NOSE GEAR AND COMPONENT, ADJUSTED DOOR PROX SENSOR, SWUNG GEAR PER RJ MM. PERFORMED FUNCTIONAL CHECK OF LANDING GEAR EXTENSION AND RETRACTION, OPS CHECK GOOD.

Part: FAIL MESSAGE — ACTIVATED (TE FLAPS)

FLAP FAIL MESSAGE AFTER TAKEOFF. ALSO, FLAP OVERSPEED AURAL WARNING AT 230 KTS. REVIEWED FLAP FAULTS AT FECU AND RESET FECU. OP CK FLAPS, OP CK GOOD.

Part: FECU — MALFUNCTIONED (TE FLAPS)

FLAP FAIL MESSAGE AT FLAP RETRACTION AFTER TAKEOFF, FLAPS INOP, COMPLETED FLAPS UP LANDING. RESET FECU ON FLAP CON CHAN 1 AND CHAN 2, OPS CKS NORMAL.

Part: CONTL MECH — MALFUNCTIONED (TE FLAPS)

FLAPS FAIL MESSAGE, FLAP FAILED AT 18 DEGREES. CONTACTED SGU MAIN CONTROL. DIVERTED TO MSO. RESET FECU CIRCUIT BREAKER FLAPS FAIL MESSAGE, CLEANED FLAPS, OPS CKS NORMAL.