N591SW

Part: UPLOCK TARGET — OUT OF RIG (MLG) · airframe 32,899 hrs · 28,968 cycles

AFTER TAKEOFF FROM IAD RECEIVED A LANDING GEAR DISAGREE CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. ADJUSTED GAP TO THE LEFT MLG UPLOCK ASSEMBLY AND PERFORMED AN OPERATIONAL TEST OF THE PROX SENSOR SYSTEM AND FUNCTIONAL TEST OF THE EXTENSION AND RETRACTION SYSTEM. OPERATIONAL AND FUNCTIONAL TEST SATISFACTORY, NO DEFECTS NOTED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 31,362 hrs · 27,662 cycles

PRESSURE FLOOR SKIN IS CRACKED IN TWO PLACES, ONE ON EACH SIDE OF BL 0 AT FS 460.00. REMOVED DAMAGE AND APPLIED A TEMPORARY REPAIR PER CRJ REO 301R-53-41-103 REV (D).

Part: FLAP — FAILED (WING) · airframe 29,878 hrs · 26,389 cycles

FLIGHT 5200 - FLAPS FAIL CAUTION MESSAGE, LEFT FLAP AT 2 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY. COMPLIED WITH SI-2-2710001 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 17,783 hrs · 14,490 cycles

FLIGHT 4991 - CAPTAIN'S WINDSHIELD CRACKED IN FLIGHT. CONTINUED FLIGHT. LANDED LGA WITHOUT INCIDENT. REPLACED CAPTAIN'S WINDSHIELD. NO FURTHER DEFECTS.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 28,347 hrs · 25,203 cycles

DURING FS 409 INSPECTION FOUND CRACK AT LOWER END OF VERTICAL STIFFENER, FS 409, RBL 36, INBOARD SIDE. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW CRJ REO 601R-53-41-189.

Part: UPLOCK — FAULTY (RT MLG BAY) · airframe 27,237 hrs · 24,336 cycles

FLIGHT 4997 - ON APPROACH, AFTER SELECTING GEAR DOWN, RECEIVED GEAR DISAGREE WARNING AFTER 8 SECONDS WITH SLOW EXTENSION OF RIGHT MAIN GEAR. WARNING EXTINGUISHED AFTER 5 SECONDS WHEN ALL GEARS WERE DOWN AND LOCKED. MLG AND PRIORITY AND SELECTOR VALVE REPLACED, PROBLEM RECURRED ON JACKS, REPLACED RIGHT MLG UPLOCK ASSEMBLY. NO FURTHER DEFECTS.

Part: SELECTOR VALVE — FAULTY (NLG) · airframe 25,934 hrs · 23,301 cycles

FLIGHT 5350 - RECEIVED A STEERING INOPERATIVE CAUTION MESSAGE DURING LANDING AT ATL, A/C WAS TOWED TO GATE. REPLACED THE NOSE LANDING GEAR SELECTOR VALVE.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 25,432 hrs · 22,885 cycles

FLIGHT 5249 - ABORTED TAKEOFF AT DTW AT 60 KTS DUE TO A COMP MON IAS CAUTION MESSAGE. PURGED WATER FROM THE PITOT SYSTEM P2.

Part: IDG — LACK OF LUBE (NR 1) · airframe 25,258 hrs · 22,732 cycles

FLIGHT 5033 - NR 1 IDG CAUTION. SERVICED IDG OIL SYSTEM, NO DEFECTS FOUND.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,538 hrs · 22,182 cycles

FWD GALLEY EMERGENCY LIGHT INOP. REPLACED FWD EMERGENCY SIGN. OPERATIONAL CHECK GOOD.

Part: BUSHING — DAMAGED (HORIZONTAL STAB) · airframe 24,354 hrs · 22,039 cycles

DURING CLIMB-OUT AT 280KTS AT 25,500 FT, EXPERIENCED AC FLUTTER. REMOVED AND REPLACED HORIZ STABILIZER BUSHINGS IAW SB 601R-55-007.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 24,338 hrs · 22,024 cycles

STAB TRIM CH 2 WILL NOT ENGAGE. REPLACED THE HSTA ACTUATOR IAW MM 27-42-01 AND MCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 215.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 22,992 hrs · 20,970 cycles

GROUND LIFT DUMP FAILED TO DEPLOY AFTER TOUCHDOWN. REPLACED NR 1 SECU IAW MM 27-61-05, OPERATIONAL CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,661 hrs · 20,709 cycles

RIGHT HAND ABOVE WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 2 CHARGER/SUPPLY ASSY IAW 33-52-00, OPERATIONAL CHECK GOOD.

Part: SKIN — CORRODED (NACELLE) · airframe 22,587 hrs · 20,651 cycles

TWO METAL PLATES CORRODED ON TOP SKIN OF THE LEFT NACELLE/PYLON FS 736 AND 7 INCHES FWD OF T/E OF THE NACELLE/PYLON. ITEM FOUND AT C-CHECK INSPECTION. REPLACED METAL PLATES IAW CRJ SRM 51-31-00, 51-21-11, 51-24-36, 51-25-06, 51-25-01, 51-40-11, 51-42-13 & 51-22-46.

Part: SKIN — CORRODED (RT NACELLE) · airframe 22,587 hrs · 20,651 cycles

TWO METAL PLATES CORRODED ON TOP SKIN OF THE RIGHT NACELLE FS 736 AND 7 INCHES FWD OF T/E OF NACELLE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED METAL PLATES IAW CRJ SRM 51-31-00, 51-21-11, 51-24-36, 51-25-06, 51-25-01, 51-40-11, 51-42-13 & 51-22-46.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,587 hrs · 20,651 cycles

RIGHT SIDE SEAT RAIL FROM FS 544.00 TO 559+96 CORRODED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED SEAT RAIL IAW CRJ SRM 51-41-02 AT FS 544 TO 559+96 RBL 27.0.

Part: TORQUE TUBE — CORRODED (PAX DOOR) · airframe 22,587 hrs · 20,651 cycles

PAX DOOR PULL-IN LEVER TORQUE TUBE IS CORRODED AND INNER SHAFTS ARE SEIZED. ITEM FOUND AT C-CHECK INSPECTION. PULL IN LEVER TORQUE TUBE FWD AND AFT SECTIONS, FWD INNER SHAFT, AFT PULL IN LEVER AND HARDWARE REPLACED IAW CRJ MM 52-11-01-400-819.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 22,587 hrs · 20,651 cycles

PAX DOOR FLOOR BRACKET FS 343 CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BRACKET REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00.

Part: SILL — CORRODED (FUSELAGE) · airframe 22,587 hrs · 20,651 cycles

PAX DOOR SILL CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SILL IAW CRJ SRM 51-40-11.

Part: PRESSURE PANEL — CORRODED (FUSELAGE FLOOR) · airframe 22,587 hrs · 20,651 cycles

FUSELAGE PRESSURE FLOOR HAS SURFACE CORROSION FS 409+128 TO FS 559.0 RBL 36-43. ITEM FOUND AT C-CHECK INSPECTION. REMOVED CORROSION IAW CRJ SRM 51-21-06 REO 601R-53-41-272. MAP DAMAGE IAW CRJ SRM 51-13-01.

Part: PRESSURE PANEL — CORRODED (FUSELAGE FLOOR) · airframe 22,587 hrs · 20,651 cycles

FUSELAGE PRESSURE FLOOR HAS SURFACE CORROSION FS 409+128 TO FS 559.0 LBL 36-43. ITEM FOUND AT C-CHECK INSPECTION. REMOVED CORROSION IAW CRJ SRM 51-21-06. MAPPED DAMAGED AREA IAW CRJ SRM 51-13-01. REF REO 601R-53-41-272 REV A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,587 hrs · 20,651 cycles

LEFT SIDE SEAT RAIL FROM FS 449+85 TO 499.00 CORRODED. SEAT RAIL INSTALLED IAW CRJ SRM 51-41-02 AT 449+85 TO 499.00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,587 hrs · 20,651 cycles

FS 484 LEFT INTERCOSTAL INBOARD ANGLE LBL 27 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06.

Part: SKIN — CORRODED (FUSELAGE) · airframe 22,587 hrs · 20,651 cycles

CORROSION FOUND BETWEEN FS 364 AND FS 349, STR 25R TO STRINGER 25L. ITEM FOUND AT C-CHECK INSPECTION. REMOVED CORROSION IAW CRJ SRM 51-21-06 & 53-00-00 MAT. LOSS MEASURED .002". REPROTECTED AREA IAW CRJ SRM 51-21-11, 51-25-06, 51-25-16.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 23,046 hrs · 21,012 cycles

PAX DOOR FRAMES P/N 601R31902-5, -25, -26 TO -455 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FRAMES PART IAW REO 601R52-11-402, REV B.

Part: POST — CRACKED (FUSELAGE) · airframe 22,587 hrs · 20,651 cycles

FS 409+128 VERTICAL POST OUTBOARD LOWER FLANGE RBL 18 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED VERTICAL POST IAW CRJ REO 60R-53-41-056 REV "NC".

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 22,587 hrs · 20,651 cycles

LEFT FUSELAGE INTERCOSTAL FS 349-364 STR 11L DAMAGED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL.

Part: ATTACH ANGLE — CRACKED (FLOORBEAM) · airframe 22,587 hrs · 20,651 cycles

FS 280 RIGHT FLOORBEAM RBL 9.0 OUTBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-13, 51-23-00, 51-21-11 & 51-42-21.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 22,587 hrs · 20,651 cycles

PAX DOOR FORWARD AND AFT BOTTOM DOOR CORNERS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DOOR IAW REO 601R-52-11-632.

Part: SKIN — CORRODED (FUSELAGE) · airframe 22,587 hrs · 20,651 cycles

RIGHT FUSELAGE SKIN BETWEEN FS 559+80 AND 559+96 STR 22, 23, 24 CORRODED. ITEM FOUND AT C-CHECK INSPECTION. DAMAGE REPAIRED, BLENDED AND ASSESSED, FOUND TO BE W/IN LIMITS IAW CRJ SRM 53-51-31, 53-00-31.

Part: POST — CRACKED (FUSELAGE) · airframe 22,587 hrs · 20,651 cycles

FS 559 VERTICAL POST LBL 9.0 INBOARD LOWER FLANGE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. VERTICAL POST REPAIRED IAW CRJ REO 601R-53-41-057.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,046 hrs · 21,012 cycles

LT SEAT RAIL FROM FS 364.00 TO 409+16 CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) SEAT REPAIRED IAW CRJ SRM 51-41-02 AT FS364.0 TO 409+16.

Part: RIB — CRACKED (RT PYLON) · airframe 22,587 hrs · 20,651 cycles

RIGHT PYLON RIB FS 605 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED RIB IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,587 hrs · 20,651 cycles

FS 202 LBL 23 PRESSURE BULKHEAD WL 59 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED BULKHEAD IAW CRJ REO 601R-53-11-563.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,587 hrs · 20,651 cycles

MAIN CABIN SEAT TRACK HAS NUMEROUS AREAS OF CORROSION; FS 559.0 TO FS 559.0+80 LBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. REMOVED CORROSION AND TREATED IAW CRJ SRM 51-21-06 & 51-21-11 AREAS BLENDED WITHIN LIMITS IAW CRJ SRM 53-51-49 & 53-21-49.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,587 hrs · 20,651 cycles

FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,587 hrs · 20,651 cycles

MAIN CABIN SEAT TRACK HAS NUMEROUS AREAS OF CORROSION; FS 559.0 TO FS 559.0+80 RBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW SEAT TRACK IAW CRJ SRM 51-40-11, 51-23-00, 51-41-04 AT F.S 559.0 TO 559.01-80, RBL 9.0.

Part: SEAT TRACK — CORRODED (FUSLEAGE) · airframe 23,046 hrs · 21,012 cycles

LEFT SIDE SEAT RAIL FROM FS 409+16 TO 409+112 CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) SEAT RAIL REPLACED IAW CRJ SRM 51-41-02 AT FS 409+16 TO 409+112.

Part: TRIM MOTOR — MALFUNCTIONED (STAB) · airframe 21,480 hrs · 19,779 cycles

STABILIZER TRIM FAILED IN FLIGHT, WOULD NOT RESET. STABILIZER TRIM AND MACH TRIM CAUTION MSGS. POWERED DOWN AIRCRAFT. PERFORMED SELF-TEST OF HSTCU. MOTORED STABILIZER TRIM BOTH CHANNELS AND SINGLE CHANNEL FULL TRAVEL 4 TIMES IAW MM 27-40-00. OPERATIONAL CHECK GOOD.

Part: BALLAST — MALFUNCTIONED (GALLEY LIGHT) · airframe 21,092 hrs · 19,461 cycles

STRONG ELECTRICAL ODOR IN COCKPIT DURING AND RIGHT BEFORE ENGINE START. ODOR GOT STRONGER AFTER TAKEOFF, THEN ALMOST WENT AWAY, THEN ON TAXI-IN THE ODOR WAS STRONGEST. REMOVED AND REPLACED GALLEY LIGHT BALLAST AND GALLEY EXHAUST FAN.

Part: WIRE — LOOSE (TRIM SWITCH) · airframe 19,610 hrs · 18,346 cycles

CAPTAIN'S TRIM SWITCH WILL NOT TRIM DOWN. SOLDERED WIRE ON TRIM SWITCH. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 19,319 hrs · 18,128 cycles

STAB TRIM & MACH TRIM FAILED INFLIGHT GOING THROUGH APPROX 17,000. RETURNED TO SLC. REMOVED AND REPLACED HSTCU. OPS CHECK GOOD.

Part: O-RING — WORN (HYD SYSTEM) · airframe 18,721 hrs · 17,658 cycles

AFTER DEPARTURE HYD 2 LOW PRESS CAUTION MSG FLUID QUANTITY INDICATED ZERO. RETURNED FOR LANDING AT SLC. FOUND PLUG ON NR 2 FILTER MANIFOLD LEAKING. REMOVED AND REPLACED O-RING ON PLUG. NO LEAKS NOTED AT THIS TIME.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 18,620 hrs · 17,582 cycles

INTERMITTENT UNCOMMANDED RIGHT RUDDER INPUTS IN CLIMB, CRUISE, WITH OR WITHOUT AP ON. MUST HOLD + 5 DEGREES RIGHT RUDDER FOR COORDINATED FLIGHT. REMOVED AND REPLACED NR 1 YAW DAMPER ACTUATOR IAW CL600 MM 22-22-01. OPS CHECK GOOD.

Part: RIB — CRACKED (LT PYLON) · airframe 18,410 hrs · 17,407 cycles

FS 605 LT PYLON RIB CRACKED. (DISCOVERED DURING C-CHECK) REPLACED RIB IAW CRJ SRM 51-40-11 P/N: 601-37004-85

Part: INTERCOSTAL — CRACKED (ANGLE) · airframe 18,410 hrs · 17,407 cycles

FS 625 STR 14L LT INTERCOSTAL ANGLE CRACKED. (DISCOVERED DURING C-CHECK) REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 600-35012-51

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 18,637 hrs · 17,596 cycles

FS 559 BULKHEAD VERTICAL POST RBL 9.0 INBOARD LOWER FLANGE CRACKED. (DISCOVERED DURING C-CHECK)REPAIRED POST IAW CRJ REO 601R-53-41-057 REV ''NC''.

Part: FLOORBEAM — CRACKED (ANGLE) · airframe 18,410 hrs · 17,407 cycles

FS 280 LBL 9.0 FLOORBEAM INBOARD ATTACH ANGLE CRACKED. (DISCOVERED DURING C-CHECK) ANGLE REPLACED IAW CRJ SRM 51-40-11. P/N: 601R311011-73SA

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 18,637 hrs · 17,596 cycles

FS193 ELECTRICAL BAY FLOOR LT CRACKED. (DISCOVERED DURING C-CHECK) REPAIRED DAMAGED FLOOR IAW CRJ REO 601R-53-11-081 REV. ''NC''.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 18,637 hrs · 17,596 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,637 hrs · 17,596 cycles

ANGLE AT FS 621 TO 625 AT STR 15S IS CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11 PARA 4. P/N: 601-35012-41.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,637 hrs · 17,596 cycles

FS 664 STR 9L FIREWALL SHUTOFF VALVE INTERCOSTAL SUPPORT AND ANGLE CRACKED. (DISCOVERED DURING C-CHECK) REPAIR INTERCOSTAL AND ANGLE FABRICATED AND INSTALLED IAW CRJ SRM 51-31-00.

Part: ANGLE — CRACKED (FUSELA EMERGENGE) · airframe 18,637 hrs · 17,596 cycles

ANGLES AT FS 589 & FS 605 LT O/B END CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLES IAW CRJ SRM 51-40-11. P/N: 601R35011-11.

Part: FUEL CONTROL — FIRE (APU) · airframe 18,010 hrs · 17,089 cycles

ON POSTFLIGHT, NOTICED SMOKE COMING FROM APU VENT. POWERED UP AIRPLANE AND APU FIRE BELL WITH LIGHT CAME ON FOR ABOUT FIVE SECONDS. POWER FUEL SWITCH WAS IN; I PRESSED OUT THE SWITCH. BOTTLE FIRED WHEN A/C WAS ADDED. REMOVED APU, INSPECTED FUEL MANIFOLD. REPLACED BOTH IGNITERS. PERFORMED LEAK CHECK WITH AIR OF FUEL SYSTEM. NO DEFECTS NOTED ON FUEL FEED SYSTEM. REINSTALLED APU PER CRJ MM 49-10-00.

Part: CONTROLLER — MALFUNCTIONED (HORIZONTAL STAB) · airframe 17,911 hrs · 17,008 cycles

AFTER LIFT OFF STAB TRIM CH 1 AND 2 FAILED AND MACH TRIM FAILED. UNABLE TO RESET IN FLIGHT. ABLE TO RESET AFTER LANDING. RETURNED TO PHX. PERFORMED ADJ/TEST OF HORIZONTAL STABILIZER CONTROL SYSTEM PER CANADAIR REGIONAL JET MM REF 27-41-00. NO DISCREPANCIES NOTED AT THIS TIME.

Part: WARNING LIGHT — ILLUMINATED (NLG) · airframe 17,678 hrs · 16,834 cycles

GEAR DISAGREE (NOSE WHEEL WOULD NOT COME UP). RECYCLED 4 TIMES, NO GOOD. RETURNED TO FIELD. SERVICE NOSE STRUT. PERFORMED GEAR SWING 8 TIMES. OPS CHECK GOOD AT THIS TIME.

Part: CONTROL PANEL — INOPERATIVE (NR 1 YAW DAMPER) · airframe 17,678 hrs · 16,834 cycles

NR 1 YAW DAMPER WILL NOT ENGAGE. FERRIED TO SLC. REMOVED AND REPLACED FLIGHT CONTROL PANEL. PERFORMED OPS CHECK OF YAW DAMPERS. OPS CHECKS GOOD.

Part: ENGINE — FLAMED OUT (RIGHT) · airframe 17,500 hrs · 16,694 cycles

RT ENGINE EXPERIENCED FLAME-OUT DURING LANDING ROLLOUT AT PNS. PERFORMED FULL ENGINE RUN WITH CREW. TAKEOFF POWER, THEN REDUCED TO IDLE AND REVERSE POWER UP. CHECKED NORMAL OK FOR CONTINUED SERVICE. PERFORMED INSPECTION AND RUN UP PER MM 76-10-00 AND 71-00-00.

Part: COMPUTER — MALFUNCTIONED (NR 1 AHRS) · airframe 17,382 hrs · 16,594 cycles

PHX: YAW DAMPER ONE WON'T ENGAGE. POWERED DOWN A/C AND DID NOT CLEAR PROBLEM. FERRIED TO SLC. SLC: CAPTAIN'S AHRS FAILURE. RED FD, ATT & MAG MESSAGE ON PFD. RED MAG MESSAGE ON MFD. REMOVED AND REPLACED NR 1 AHRS PER CRJ MM 34-21-01. OPS CHECK GOOD. FCC DIAGNOSTICS AND MDC INDICATE NR 1 AHRS OPS CHECK GOOD. NO FAULTS NOTED.

Part: SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 17,038 hrs · 16,340 cycles

ON DEPARTURE FROM DFW THE CAPTAIN'S STAB TRIM WOULD NOT TRIM NOSE UP. NO ASSOCIATED STAB TRIM MESSAGES NOTED. REMOVED AND REPLACED CAPTAIN'S PITCH TRIM SWITCH WITH SERVICEABLE UNIT IAW MM 27-41-05. OPS CHECK GOOD AT THIS TIME.

Part: WARNING SYSTEM — ACTIVATED (SPOILERS) · airframe 16,926 hrs · 16,258 cycles

RECEIVED INBOARD AND OUTBOARD GROUND SPOILERS FAULT MESSAGES AIRBORNE. RAN QRH AND RETURNED TO SLC. RESET CBP1 N8, 2-N8 & 4 A2 & 3 PER FAULT ISOLATION MANUAL. SYSTEM CHECKS OK.

Part: SENSOR — MALFUNCTIONED (LT AOA) · airframe 16,920 hrs · 16,254 cycles

''STALL FAIL'' CAUTION MESSAGE DURING CLIMB. RETURNED TO SLC. INBOARD GROUND SPOILERS CAUTION MESSAGE AFTER LANDING. REMOVED AND REPLACED LEFT AOA. OPS CHECKS GOOD. PN OFF 4515034 SN OFF 404.

Part: WINDSHIELD — CRACKED (CAPTAIN'S) · airframe 16,825 hrs · 16,180 cycles

CAPTAIN'S SIDE WINDSHIELD CRACKED DESCENDING INTO BNA. APPEARED TO BE AN ELECTRICAL SHORT LOW IN THE WINDSHIELD AT THE CENTER PRIOR TO THE CRACK. REMOVED AND REPLACED LEFT WINDSHIELD WITH SERVICEABLE UNIT IAW MM 56-11-01 OPS CHECK & LEAK CHECK GOOD. PN OFF/ON NP-139321-9 SN OFF 85 114H6827.

Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 16,667 hrs · 16,054 cycles

LEFT SIDE CABIN EMERGENCY EXIT DOOR IS STUCK. FA UNABLE TO OPEN. ADJUSTED THE EMERGENCY DOOR AND LUBED THE LATCH. DOOR CHECKS GOOD.

Part: BUSHING — WORN (ELEVATOR) · airframe 16,591 hrs · 15,991 cycles

PILOT REPORTS OSCILLATIONS ON CLIMB AND IN THE PITCH AT AIR SPEED OF 284 KTS TO 290 KTS. REMOVED & REPLACED HARDWARE & BUSHINGS ON ALL 6 ELEVATOR PCU'S ROD END SIDE. OPS CHECK GOOD.

Part: DAMPENER — DEFECTIVE (ELEVATOR) · airframe 15,981 hrs · 15,508 cycles

DURING STABLE FLIGHT, AIRPLANE EXPERIENCED FLUTTER. WHEN PUTTING LOADS ON ELEVATOR, FLUTTER WENT AWAY. RETURNED IN STEADY, STABLE FLIGHT. GREATER FLUTTER AT HIGHER SPEEDS, HAPPENED AT ALL ALTITUDES. RETURNED TO SLC. REMOVED AND REPLACED LT ELEVATOR FLUTTER DAMPERS WITH SERVICEABLE UNITS IAW MM 27-34-05.

Part: SCREW — BROKEN (PAX DOOR) · airframe 15,841 hrs · 15,395 cycles

PASSENGER STOW HANDLE MESSAGE ON EICAS. UNABLE TO CLOSE AND LATCH PASSENGER DOOR. FOUND BROKEN SCREW IN LATCHING MECHANISM. REPLACED SCREW IAW A/C MM 51-11-02. OPS CHECK GOOD.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 15,147 hrs · 14,842 cycles

DURING TAXI IN, RUDDER TRIM WENT FULL NOSE RIGHT. UNABLE TO RETURN TRIM TO TAKEOFF POSITION. INSTALLED SERVICEABLE RUDDER/AILERON TRIM PANEL. RUDDER TRIM CHECKS GOOD IAW 27-22-01.