N925SW
Registered owner: CORPORATE FLIGHT MANAGEMENT INC DBA, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SKYWEST AIRLINES, INC. (SWIA) | Operator | 2010-05-23 – 2010-05-23 | Operator named in NTSB report |
| SKYWEST AIRLINES INC | Operator | 2010-05-23 – 2010-05-23 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AFTER TAKEOFF, FO CALLED FOR GEAR UP. AFTER GEAR SET UP WE RECEIVED THE NOSE GEAR DOOR WARNING MESSAGE ALONG WITH GEAR DISAGREE AND WOW INPUT CAUTION MESSAGE. THE NOSE GEAR WAS STILL IN THE DOWN POSITION AND THE MAIN GEARS WERE INDICATING UP. THERE WAS ALSO A WOW OUTPUT FAIL STATUS MESSAGE. WE RAN THE QRH WHICH REQUIRED 3B AND 2B SET IN ON WHICH DID NOT RESOLVE ANY ISSUES. THEN AS PER QRH PULLED THE MANUAL GEAR EXTENSION WHICH RELEASED THE MAIN GEAR DOWN. THEN AS PER THE QRH WE SET THE LANDING GEAR LEVER DOWN WHICH GAVE THE INDICATION OF ALL 3 GEAR DOWN AND GREEN. IN ADDITION, WE HAD A NOSE STEERING INOP CAUTION MESSAGE WHICH CLEARED AFTER I CYCLED THE N/W STEERING SWITCH OFF THEN ARMED. WE LANDED AND WERE ABLE TO TAXI BACK TO THE GATE WITH NO OTHER ISSUES. ( FLIGHT 5035 - FILED OPEN) VERIFIED THAT THERE WAS NO GEAR DISAGREE DISCREPANCIES IN THE EAML IN THE LAST 30 DAYS. PERFORMED A VISUAL INSPECTION OF THE NOSE LANDING GEAR HARNESS AND NOSE LANDING GEAR AND GEAR AREA IN REFERENCE TO CRJ 200 AMM 32-20-00. UPON INITIAL INSPECTION FOUND THE MOUNTING BRACKET FOR #2 WOW CENTERED HARNESS ASSY DAMAGED AND FOUND THE HARNESS PINCHED / CRUSHED BY THE DAMAGED BRACKET. REMOVED AND REPLACED THE WOW #2 AND CENTERED HARNESS ASSY IN REFERENCE TO CRJ 200 AMM 32-61-25. REMOVED AND REPLACED THE LOWER PROX SENSOR MOUNT BRACKET THAT WAS BENT IN REFERENCE TO CRJ 200 CMM 32-20-04. BOTH PROX SENSORS ON THE #2 WOW HARNESS ASSY REQUIRE SAFETIES AND ADJUSTMENTS - DUE TO HIGH WINDS UNABLE TO JACK AIRCRAFT AT THIS TIME. PLEASE REFERENCE AML 814507 FOR FDR DOWNLOAD. PLEASE REFERENCE AML 814510 FOR THE INTERROGATION OF THE PSEU. PLEASE REFERENCE AML 814589 FOR THE NOSE STEERING INOP CAUTION MESSAGE THAT CLEARED. PLEASE REFERENCE AML 814598 FOR THE SAFETYING AND FINAL ADJUSTMENT OF BOTH OF THE PROX SENSORS ON
PASSENGER DOOR CUTOUT UPPER FORWARD STOP FITTING IS CRACKED. FILED CLOSED. REMOVED AND REPLACED PASSENGER DOOR CUTOUT UPPER FORWARD STOP FITTING REFERENCING APPLICABLE STEPS OF CRJ200 SRM 51-42-20. PERFORMED OPERATIONAL CHECK OF THE DOOR STOP FITTING IAW CRJ200 AMM 52-11-00. OPS CHECK GOOD AT THIS TIME.
GEAR DISAGREE AND NOSE GEAR DOOR WARNING MESSAGE ON DEPARTURE. RAN QRH, GEAR CAME UP AFTER TURNING ON HYDRAULIC 2 AND 3B PUMPS. FLIGHT 5069 - FILED CLOSED T/S: PSEU CODES: LEG 1: S23 FAR, S35 NEAR, S21 NEAR, S22 FAR, S30 FAR, S31 FAR, S32 FAR, DI15 ON, DI14 ON PLEASE REFERENCE AML 578744 FOR FURTHER MX ACTION
PAX DOOR INNER SKIN LIFTS UP AT THE CABLE PULLEY ATTACH AREA WHEN ASSIST MOTOR IS USED TO LIFT DOOR (C-CHECK) RO: 09/29/2019 PERFORMED PERMANENT REPAIR TO PAX DOOR INNER SKIN IAW REO. NO DEFECTS NOTED.
FRAME BS 589, STRINGER 17L - 22R CORRODED. BLENDED CORROSION IAW REO.
NOSE WHEEL WELL SKIN CRACKED AT LBL6 AND RBL6 FS235 (MARKED) (C-CHECK) RO: 09/29/2019 COMPLIED WITH THE REPAIR TO THE CRACKED NOSE WHEEL WELL SKIN AT FS235 LBL6 AND RBL6 IAW REO. PRESSURE CHECK GOOD.
RH MAIN LANDING GEAR DOOR PREVIOUS REPAIR ON LEADING EDGE CHAFED. NEW FILLER WAS FABRICATED AND INSTALLED IAW REO.
LH MAIN LANDING GEAR DOOR LEADING EDGE CHAFED BLENDED OUT IAW SRM. AND REPAIRED OUT OF LIMIT AREA IAW REO.
PANEL 699BB HAS SEVERAL CHAFFS. BLENDED OUT DAMAGES. REPLACED WITH NEW PANEL PN CC670-13056-4.
SERVICE DOOR ENTRY THRESHOLD CORRODED AROUND UPPER SCREW HOLES. LOCATED NEW PART AND INSTALLED NEW NUTPLATES WITH NEW RIVETS IAW SRM. RESTORED FINISH.
RH INBOARD FLAP VANE LEADING EDGE CHAFED APPROXIMATELY 7Ãâ¬? FROM OUTBOARD END. BLENDED OUT FLAP VANE OUT OF LIMITS, REMOVED AND REPLACED, INSTALLED NEW FLAP VANE AT RH INBD FLAP VANE LEADING EDGE OUTBOARD END IAW SRM.
RH INBOARD FLAP VANE LEADING EDGE CHAFED APPROXIMATELY 6Ãâ¬? FROM INBOARD END. BLENDED OUT FLAP VANE OUT. REMOVED AND REPLACED, INSTALLED NEW FLAP AT RH INBD FLAP VANE LEADING EDGE INBD END IAW SRM.
SMOKE AND SPARKS COMING FROM SIDEWALL LIGHT AT SEAT 5D. DECLARED EMERGENCY. DIVERTED. (FLT 5672) CLOSED INSPECTED SIDEWALL AND CEILING LIGHT AT SEAT 5D AND SURROUNDING AREA FOR FIRE DAMAGE. NO FIRE DAMAGE FOUND. REMOVED AND REPLACED SIDEWALL LIGHT 5D LUMINAIRE IAW AMM.
SERVICE DOOR LOWER DOOR THRESHOLD HAS CORROSION, BETWEEN BS 319 TO 349. REMOVED AND REPLACED SERVICE DOOR LOWER SILL ANGLE IAW SRM.
FRAME AT SERVICE DOOR THRESHOLD, AT FLOOR LEVEL HAS CORROSION AT APPROX BS 349 INSIDE FUSELAGE. REPAIRED THE FRAME IAW REO.
FOUND ADDITIONAL DENTS ON THE RT SIDE OF CENTER WING-BOX LOWER PLANK BETWEEN BL 0 AND RBL 45 AND FROM STRINGERS 17 TO 26R APPROX. AREA OF 21" X 32". ALL STEPS COMPLETED OF PERMANENT REPAIR IAW REO AND SRM.
RIGHT FORWARD SIDE OF CENTER WING PLANK HAS 9 SMALL DENTS IN AN AREA APROXIMATELY 6" X 8". ALL STEPS COMPLETED OF PERMANENT REPAIR IAW REO AND SRM.
LEFT INBD FLAP VANE, CENTER L/E CAP REQUIRES REPLACEMENT. R & R LT INBD FLAP VANE CENTER L/E CAP IAW SRM AND STS.
RIGHT ENGINE LOWER COWL DAMAGED. R & R RT ENGINE INLET COWL IAW AMM.
PAX DOOR AREA FLOOR EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM.
LEFT AFT EMERGENCY LIGHT IS BURNED OUT. REPLACED THE LAMP.
NR 3 EMERGENCY OVERHEAD FLOOD LIGHT IS BURNED OUT. FLT 6473 RELAMPED.
FLOOR LEVEL MAIN CABIN DECK & GALLEY SERVICE DOOR EMERGENCY LIGHTS INOPERATIVE. FLT 5256 FOUND FLOOR LEVEL & GALLEY SERVICE DOOR EMERGENCY LIGHT CONNECTORS TO BE HOOKED UP WRONG, RE-CONNECTED TO PROPER EMERGENCY LIGHTS, OPERATIONS CHECKED GOOD IAW AMM.
NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 6303 RELAMPED.
FS 200 RBL 11 ANGLE IS GOUGED. GOUGE MEASURES APPROXIMATELY .32 INCHES L X .100 INCHES W X .050 INCHES D. C-CHECK REPLACED ANGLE IAW SRM.
FOUND FS 409.0 + 128 VERTICAL POST RBL 18.0 INBD & OTBD SIDES HAVE INDICATIONS NOTED AT AFT FLANGE. RADIUS APPROXIMATELY 3 INCHES IN LENGTH 50 % FSH. C-CHECK REMOVED CRACKED POSTS AT FS 409.0 + 128 VERTICAL POST RBL 18.0 INBD & OTBD SIDES & INSTALLED NEW VERTICAL POSTS IAW SRM & REO.
FOUND FS 409.0 + 128 VERTICAL POST BL 0.0 LT & RT SIDES HAVE INDICATIONS NOTED AT AFT FLANGE RADIUS APPROXIMATELY .3 INCHES IN LENGTH 60% & 80% FSH. C-CHECK REMOVED LT & RT BL 0.0 VERTICAL POSTS AT FS 409.0 + 128 & INSTALLED NEW VERTICAL POSTS IAW REO & SRM.
FIRST OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT#6397 RELAMPED.
FLT 5642, RETURNED TO FIELD WITH PRESSURIZATION FLUCTUATION PROBLEM. OPS CHECKED GOOD AFTER FUNCTIONAL FLIGHT ADJUSTMENT TEST OF BOTH CABIN PRESSURE CONTROLLERS IAW AMM.
GALLEY SERVICE EXIT LIGHT BURNED OUT. FLT#5537 RELAMPED.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6360) RELAMPED EMERGENCY LIGHT.
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6452) RELAMPED EMERGENCY LIGHT.
PASSENGER DOOR FLOOR LEVEL EMERGENCY EXIT SIGN IS OUT. (FLT 5298) RELAMPED EMERGENCY EXIT SIGN.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5378) RELAMPED EMERGENCY LIGHT.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6258) RELAMPED EMERGENCY LIGHT.
CRACK ON FS 621 BULKHEAD WEB, FORWARD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING. (C-CHECK) REPAIR CRACK ON FS 621 BULKHEAD WEB, FORWARD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING PER REO.
CAPTAIN'S SIDE INBOARD SHOULDER HARNESS BINDS TOO EASILY. (FLT 5592) ADJUSTED CABLE ON HARNESS LOCKING MECHANISM.
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6234) RELAMPED EMERGENCY LIGHT.
SECOND AND THIRD FROM FRONT EXTERIOR EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5348) RELAMPED EMERGENCY LIGHT.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6218) RELAMPED EMERGENCY LIGHT.
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6267) RELAMPED EMERGENCY LIGHT.
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5463) RELAMPED EMERGENCY LIGHT.
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6247) RELAMPED EMERGENCY LIGHT.
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4599) RELAMPED EMERGENCY LIGHT.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6290) RELAMPED EMERGENCY LIGHT.
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5506) RELAMPED EMERGENCY LIGHT.
SHUT DOWN THE RIGHT ENGINE DUE TO OIL PRESSURE WARNING MESSAGE. (FLT 6396) REPLACED CARBON SEALS ON ACCESORY GEARBOX.
EMERGENCY LIGHT BY SERVICE DOOR AND LEFT FORWARD OVERWING EXTERIOR ARE OUT. (FLT 6217) RELAMPED EMERGENCY LIGHT.
FLOOR AND LEFT EXIT EMERGENCY LIGHTS INOPERATIVE. (SERVICE CHECK) REPLACED NR 2 EMERGENCY LIGHT INVERTER.
BOTH LEFT ENGINE FORWARD MOUNT PINS NEED REPLACED DUE TO PITTING. (ENGINE CHANGE) REPLACED BOTH LEFT ENGINE FORWARD MOUNT PINS PER AMM.
FS 621 BULKHEAD CRACKED AT LINTEL FITTING. (C CHECK) REPAIR PER REO.
CRACK INDICATION NOTED TO FS 559.0 PRESSURE BULKHEAD AT RT SIDE AS NOTED. (C-CHECK) REPAIRED PER REO.
NOSE GEAR FAILED TO EXTEND FOR LANDING. LANDED NLG RETRACTED. (FLT 6467) REPLACED NLG MANIFOLD, WOW HARNESS, NLG UPLOCK PROX SENSOR, NLG UPLOCK ASSEMBLY, AND NLG ELECTRIC HYDRO SERVO VALVE.
AFT FLOOR EMERGENCY LIGHT STRIP INOP. (FLT 6826) TIGHTENED LOOSE CONNECTION ON STRIP.
OVERHEAD EMERGENCY LIGHT NR 4 INOP. (FLT 6580) RELAMPED EMERGENCY LIGHT.
CEILING EMERGENCY LIGHT NR 2 INOP. (FLT 6450) RELAMPED EMERGENCY LIGHT.
FORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE ACTUATOR ARM ACCESS PORT. (SVC CHECK)REPAIRED PER REO.
MAIN CABIN DOOR WILL NOT CLOSE. (FLT 5935) ADJUSTED MAIN CABIN DOOR LOWER TORQUE TUBE LOCKING CAM.
NR 2 EMERGENCY CEILING LIGHT INOP. (FLT 6615) RELAMPED EMERGENCY LIGHT.
MAIN CABIN DOOR WILL NOT CLOSE. (FLT 6699) ADJUSTED MAIN CABIN DOOR UPPER OVER CENTER CAM.
FLT 5955 - NR 4 CABIN EMERGENCY LIGHT NR 4 INOP. RELAMPED.
FLT 6369 - CEILING EMERGENCY LIGHT AT ROW 2 INOP. RELAMPED.
FLT 6621 - EMERGENCY LIGHT, LEFT WING ROOT AREA NEAR LEADING EDGE INOP. RELAMPED.
DURING C-CHECK, LEFT ENGINE AFT THRUST MOUNT CORRODED. REPLACED.
DURING C-CHECK, RIGHT ENGINE AFT THRUST MOUNT CORRODED. REPLACED.
FLT 6656 - LAST TEN FEET OF EMERGENCY FLOOR LIGHTING INOP. REPLACED NR 4 INVERTER.
LEFT MLG AXLE REQUIRES REPLACEMENT DUE TO CORROSION. C-CHECK, INSTALLED LEFT MLG AXLE.
REMOVED RIGHT MLG AXLE DUE TO CORRSION. C-CHECK, REPLACED RIGHT MLG AXLE.
RIGHT MLG TRAILING ARM CORRODED. C-CHECK, REPLACED RIGHT MLG TRAILING ARM.
EMERGENCY LIGHTS INOP AFT OF ROW 8. FLT 6644, REPAIRED BROKEN WIRE.
EMERGENCY LIGHTS INOP AFT OF WINDOW EXIT (FLT 6703). FOUND LOOSE CONNECTION AT ROW 8, TIGHTENED CONNECTION.
CEILING EMERGENCY LIGHT ROW 5 INOP. RELAMPED.
LEFT FUSELAGE AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LT SIDE EMERGENCY LIGHT.
FLT 6053 - FOUND DENT ON RIGHT SIDE OF FUSELAGE. REPAIRED RIGHT SIDE OF FUSELAGE BETWEEN STR15R AND STR 16R AND FS 394 AND FS 409 + 16 PER REO 601R-53-00-251.
FLT 6456 - EMERGENCY LIGHT ADJACENT TO CABIN DOOR IS INOP. REPAIRED WIRE AS REQUIRED. OPS CHECK GOOD.
FLT 1001 - RECEIVED "GEAR DISAGREE" WARNING MESSAGE AFTER TAKEOFF. SERVICED NOSE GEAR SHOCK STRUT WITH OIL AND NITROGEN IAW MM 12-12-32.
RECEIVED "GEAR DISAGREE" WARNING MESSAGE AFTER TAKEOFF, FLIGHT NR 1001. REPLACED PACKING ON STEERING SELECTOR VALVE FITTING IAW 32-51-25 CMM. OPS CHECK GOOD.
FLT 6729 - SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE. LUBED SERVICE DOOR OUTER HANDLE. OPS CHECKS GOOD.
EMERGENCY LIGHT POD INOP. RELAMPED EMERGENCY LIGHT IAW MM CHAPTER 33-50-00.
CRACK AT PAX DOOR STRUCTURE ANGLE INSIDE 832AR CUT OUT, DISCOVERED AT C-CHECK. INSTALLED NEW DOUBLER ANGLE P/N 601R-318094-2 AS PER CRJ200 SRM 51-42-06 PG 5-19 AND CRJ200 SRM 51-42-21 PG 15-19.
ENGINE SUPPORT BEAM CRACKED AT RIGHT LOWER WEB ON FORWARD INBOARD CORNER, DISCOVERED AT C-CHECK. INSTALLED ALL REPAIR PARTS FOR RIGHT LOWER ENGINE SUPPORT BEAM PER REO 601R-53-61-358 REV A.
FLOORBEAM IS CRACKED AT LBL11 DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE AND FILLER AT LBL9 PER CRJ200 REO 601R 53-11-171 REV 'D' AND CLIPS AND FILLER AT LBL9 PER REO 601R 53-11-171 REV 'D'.
PAX DOOR FWD WEB CRACKED AT STEPS 3 AND 4, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES, SHIM AND DOUBLER PER CRJ200 REO 601R-52-11-702 REV A.
FLOORBEAM IS CRACKED AT LBL11, DISCOVERED AT C-CHECK. INSTALLED FILLER ANGLE AND SPLICE ANGLES IAW CRJ200 REO 601R-53-11-138.
FLOORBEAM IS CRACKED AT RBL11 AND BOTH INBOARD AND OUTBOARD CLIPS ARE CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE, CLIP, FILLER, ANGLE FILLER, SHIM P/N 601R-53-11-1169-1 AND CLIP P/N 601R31113-58 IAW CRJ200 REO 601R-53-11-171, REV D AND REO 601R-53-11-1169.
PILOT SEAT RIGHT BACK SUPPORT CRACKED, DISCOVERED AT C-CHECK, INSTALLED NEW SUPPORT P/N 1C3076-2AJT IAW CMM 25-14-10.
CRACK AT PAX DOOR ASSIST MOTOR MOUNT STRUCTURE AFT RADIUS, DISCOVERED AT C-CHECK. INSTALLED NEW STIFFENER P/N 601R 317745-7 P/O 27867 PER CRJ200 SRM 51-42-06 PG 4 AND 18.
FOUND FLOOR EMERGENCY LIGHT AT ROW 5 INOP. REPLACED LIGHT STRIP AT ROW 5. OPERATIONAL CHECKS GOOD.
FOUND LEFT EMERGENCY EXIT LOWER EXIT SIGN DOES NOT ILLUMINATE. REPLACED LEFT OVERWING LOWER EXIT LIGHTED SIGN AS REQUIRED. OPERATIONAL CHECKS GOOD.
FORWARD OVERHEAD EMERGENCY LIGHT INOP, RELAMPED CABIN FORWARD OVERHEAD EMERGENCY LIGHT IAW MM 33-51-00. OPERATIONAL CHECKS GOOD.
3RD EMERG OVERHEAD LIGHT IS INOP. REPLACED LIGHT BULB IN 3RD EMERGENCY LIGHT IAW MM 33-51-00.
CAPT SIDE TRIM STICKS. REPLACED CAPT SIDE PITCH TRIM SWITCH PER CRJ MM 27-41-05. OPERATIONAL CHECK GOOD.
MAIN CABIN DOOR OUTER HANDLE BROKE OFF AT LOWER NECK. REPLACED OUTER PAX DOOR HANDLE IAW 52-11-03. OPERATIONAL CHECK GOOD.
RUDDER TRIM SWITCH STICKS, GOES RIGHT WON`T GO LEFT. REPLACED RUDDER /AILERON TRIM SWITCH PANEL. OPERATIONAL CHECK GOOD.
SECU NR 1 SHOWS FAULT CODE (D7) RT FLIGHT SPOILER IB PCU SPOOL FAIL. REPLACED RT IB PCU 27-62-01. OPERATIONAL CHECK GOOD.
OVERHEAD EMERGENCY LIGHT INOPERATIVE. RELAMPED AS REQUIRED. OPERATIONAL CHECK GOOD.
RIGHT WINDOW CRACKED UP. REPLACED F/O'S SIDE WINDOW IAW MM 56-21-01. PN/OFF 601R33033-12, SN/OFF 02053H9219.
OTBD ANGLE CRACKED AT FS 280 LBL9 ITEM FOUND AT C CHECK INSPECTION. INSTALLED NEW OB CLIP AT FS 280 LBL 9 IAW REO 601R-53-11-136 CRJ200 SRM 51-42-06 PG 1-21; 51-42-21 PG 1-21; CW REO 601R-53-11-136.
OTBD ANGLE CRACKED AT FS 280 RBL9, ITEM FOUND AT C CHECK INSPECTION. INSTALLED OB BRACKET IAW CRJ200 SRM 51-40-11 AND REO 601R-53-11-136.
INBD AND OTBD ANGLES CRACKED AT FS 280 RBL 9.0, ITEM FOUND AT C CHECK INSPECTION. INSTALLED IB BRACKET IAW CRJ200 SRM 51-40-11 AND REO 601R-53-11-136.
INBD AND OTBD ANGLES CRACKED AT FS 280 LBL 9, ITEM FOUND AT C CHECK INSPECTION. INSTALLED NEW CLIPS AT FS 280 LBL 9 IAW REO 601R-53-11-136 CRJ200 SRM 51-42-06; PG 1-21; 51-42-21 PG 1-21; CW REO 601R-53-11-136.
LEFT RUDDER BINDS. REMOVED DEBRIS FROM AFT LEFT RUDDER PULLEY, OPERATIONAL CHECK GOOD IAW 27-21-00.
STAB TRIM CHANNEL NR 1 WILL NOT ENGAGE. INSTALLED SERVICEABLE MOTOR CONTROL UNIT REF AMM 27-42-05. OPERATIONAL CHECK GOOD.
DURING CLIMB, RECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGES. REPLACED F/O'S TRIM SWITCH IAW MM 27-41-07. OPERATIONAL CHECK GOOD.
STAB CH NR 1 STATUS MESSAGE. REPLACED HSTCU IAW MM 27-40-00. OPS CHECK GOOD.
SPOILERON FAULT AND GROUND SPOILER FAULT. REMOVED AND REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD.
WHILE PAX BOARDING AND BAGGAGE LOADING, RECEIVED A SMOKE CARGO WARNING WITH ASSOCIATED WARNINGS. CARGO COMPARTMENT WAS CHECKED, AND NO FIRE OR SMOKE NOTED. REPLACED FORWARD CARGO SMOKE DETECTOR. OPERATIONAL CHECK GOOD. REF CRJ MM CHAP 26-15-00.
CONFIG SPOILERS WARNING ON T/O ROLL. ABORTED TAKEOFF. REPLACED RIGHT SPOILERON INBOARD PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD.
RUDDER TRIM RANAWAY TO THE LT WHILE TRYING TO TRIM AIRCRAFT IN THE CLIMB. RETURNED TO AIRPORT. REMOVED AND REPLACED RUDDER TRIM/AIL TRIM PANEL ASSY. OPERATIONAL CHECK GOOD. PN OFF 601R51227-13
SPOILERON FAULT ON RUNWAY. REMOVED AND REPLACED NR 1 SECU AND LEFT OUTBOARD PCU IN REF TO AMM 27-61-00 AND 27-62-1. OPS CHECK GOOD. SECU S/N OFF: 03059, PCU P/N: 27000-7, S/N OFF: MAL-5776.
MAIN FUSELAGE PULLEY INTECOSTAL HAS OB FLANGE CRACKED FS 484.00 RBL 36.0. (FOUND DURING C-CHECK INSPECTION). MANUFACTURED AND INSTALLED ANGLE AS REQUIRED IAW REO 601R-53-41-059.
MAIN FUSELAGE IB AND OB BEAM CLIPS CRACKED FS280.00 RBL 9.0. (FOUND DURING C-CHECK INSPECTION). REPLACED CLIPS IAW CRJ SRM 51-42-06, 51-40-11, 51-23-00, 51-42-21 AND RII53-401.
CARGO PIT FLOOR SUPPORT ANGLE IS CRACKED FS 621.00 LBL 42.0. (FOUND DURING C-CHECK INSPECTION). REPAIRED CARGO PIT, FLOOR SUPPORT ANGLE AT FS 621.00 IAW CRJ REO 601R-53-61-117 REV. A AND RII53-401.
CARGO PIT FLOOR SUPPORT ANGLE IS CRACKED FS 621.00 RBL 42.0. (FOUND DURING C-CHECK INSPECTION). ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV. A, RII53-401.
CARGO BOTTLE LOW CAUTION MESSAGE ON EICAS FOR APPROXIMATELY 5 MINUTES THEN WENT AWAY. RAN QRH. BOTTLES DID NOT PASS TEST IN FLIGHT. INSTALLED NEW CARGO BOTTLE. OPS CHECK GOOD.
CAPT SIDE ELEVATOR TRIM DOES NOT WORK IN THE UP OR DOWN DIRECTION. REMOVED CAPTAIN'S PITCH TRIM SWITCH AND INSTALLED NEW PITCH TRIM SWITCH IAW CRJ MM 27-41-05. OPS CHECK GOOD.
SPOILERON FAULT MESSAGE. RIGHT SPOILERON ILLUMINATED WHITE DURING TAXI. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU IAW CRJ MM 27-61-05. LEAK CHECK GOOD. REMOVED AND REPLACED NR 1 SECU UNIT WITH SERVICEABLE UNIT. (SECU) P/N OFF: 49-164-6, S/N OFF: 01656, OPS CHECKS GOOD.
ON FINAL TO DEN, SPOILERONS FAULT AND INBOARD GROUND SPOILER FAULT MESSAGES CAME ON. INSTALLED SERVICEABLE NR 2 SECU IAW CRJ MM 27-61-05. OPS CHECK GOOD.
''CARGO BOTTLE LOW MSG'' DURING FLIGHT. FOLLOWED QRH AND LANDED AT NEAREST SUITABLE AIRPORT. REMOVED AND CLEANED SWITCHES ON FIRE PANEL. SYSTEM CHECKS GOOD.
RT COWL ANTI-ICE MESSAGE WHEN SELECTED ON. RETURNED TO FAT. REMOVED AND REPLACED RIGHT COWL ANTI-ICE VALVE IAW CRJ MM 30-22-01. OPS CHECK GOOD.
AT THE GATE, THE APU AUTO SHUTDOWN, TWICE, WITH AN EGT SPIKE OF 990 DEGREES THE SECOND TIME. REMOVED AND REPLACED APU ASSEMBLY IAW RII 49-401 AND MM 49-10-00. OPS CHECK GOOD.