N590SW

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 30,719 hrs · 27,024 cycles

EN ROUTE FROM LGA TO CHS RECEIVED LEFT REV UNLOCK MSG. ACFT DIVERTED TO JFK AND LANDED SAFELY. INSPECTED LT ENG T/R SYSTEM. NO DEFECTS FOUND. PERFORMED OPS CHECKS OF T/R SYSTEM. ALL CHECKS GOOD. COULD NOT DUPLICATE MSG ON GROUND. (S)

Part: BPSU — FAULTY (T/E FLAP) · airframe 30,389 hrs · 26,771 cycles

FLIGHT 5018 - RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RIGHT BPSU. ALSO PERFORMED SE-27I001. NO FURTHER DEFECTS.

Part: CONNECTOR — WORN (ANTI-ICE SYSTEM) · airframe 29,609 hrs · 26,158 cycles

FLIGHT 5449 - ON CLIMBOUT FROM CVG TO DTW ANTI-ICE DUCT WARNING MESSAGE CAME ON WITH BOTH, WING AND COWLING ANTI-ICE SELECTED ON IN ICING CONDITIONS. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. REMOVED AND REPLACED FENWAL LOOP CONNECTOR AT FS 628 RIGHT SIDE.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 26,204 hrs · 23,409 cycles

FLIGHT 5251 - CREW REPORTED 3A PUMP CAUTION INFLIGHT, THEN ON LANDING, HAD A MOMENTARY GEAR DISAGREE. CREW PERFORMED A GO-AROUND WITH NO FURTHER EVENTS. DEFERRED 3A PUMP PER MEL 29-12-01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,490 hrs · 22,011 cycles

3RD CABIN POD EMERGENCY LIGHT INOP. REPLACED LAMP. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,176 hrs · 21,773 cycles

PAX MAIN CABIN DOOR EMERGENCY FLOOD LIGHT HAS A BURNED OUT LIGHT BULB. RELAMPED PAX MAIN CABIN DOOR EMERGENCY FLOOD LIGHT. OPERATIONAL CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 23,944 hrs · 21,592 cycles

DESCENDING THROUGH APPROX 27000' HEARD A LOUD POP. REPLACED RIGHT WINDSHIELD IAW CRJ 200 MM 56-11-01, PN/OFF 601R33033-2 , SN/OFF 951038635T.

Part: COUNTERBALANCE — OUT OF RIG (PAX DOOR) · airframe 23,849 hrs · 21,526 cycles

PAX DOOR SLOW TO OPEN. ADJUSTED AND RIGGED PAX DOOR COUNTER BALANCE SYSTEM IAW MM 52-11-17. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 22,971 hrs · 20,849 cycles

SPOILERONS STATUS MESSAGE. REPLACED RIGHT OUTBOARD SPOILERON PCU IAW CRJ MM27-62-01. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 22,859 hrs · 20,758 cycles

SPOILERON FAULT STATUS MESSSAGE. REPLACED RIGHT WING SPOILERON (OUTBOARD) PCU IAW MM 27-64-01. OPERATIONAL CHECK GOOD.

Part: ATTACH FITTING — DAMAGED (WING) · airframe 22,813 hrs · 20,718 cycles

FORWARD WING ATTACH FITTING, FORWARD SIDE, FLANGED BUSHING HAS COMPLETE SEPARATION OF FLANGE FROM BUSHING SLEEVE. ITEM FOUND AT C-CHECK INSPECTION. RT WING FITTING/BUSHING REPAIRED IAW REO 601R-57-21-564 155.2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,466 hrs · 21,221 cycles

LT SIDE SEAT RAIL BETWEEN FS 409.00 + 112 AND FS 449.85 IS CORRODED ITEM FOUND AT C-CHECK INSPECTION. INSTALLED LT SIDE SEAT RAIL BETWEEN FS 409.00 + 112 ANS FS 449.85 IAW CRJ 200 SRM 51-41-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,466 hrs · 21,221 cycles

LT SIDE SEAT RAIL BETWEEN FS 409.00 + 16 - FS 409.00 + 112 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-40-11, 51-41-02, 51-41-04 AND 51-25-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,466 hrs · 21,221 cycles

LT SIDE SEAT RAIL BETWEEN FS 364 - 409 + 16 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED LT SIDE SEAT RAIL B/W FS 364-409 + 16 IAW CRJ SRM 51-41-02 PART 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,466 hrs · 21,221 cycles

LT SIDE SEAT RAIL BETWEEN FS 449.85 - 449.00 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-04-11, 51-41-02, 51-25-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,466 hrs · 21,221 cycles

CRACKED FRAME FLANGE AT FS 605 AND STRINGER 9 LT SIDE ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-1305.

Part: SILL — CORRODED (FUSELAGE) · airframe 23,466 hrs · 21,221 cycles

CARGO COMPT RT FLOOR SILL PLATE RBL 41.0 BETWEEN FS 610.0 AND FS 621.0 CORRODED ON UPPER PLATE, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED PARTS INSTALLED IAW REO 601R-53-61-1301.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,466 hrs · 21,221 cycles

RT SIDE SEAT RAIL BETWEEN FS 409.00 + 16 - FS 409.00 + 112 IS CORRODED ITEM FOUND AT C-CHECK INSPECTION. INSTALLED RT SIDE SEAT RAIL BETWEEN FS 409.00 + 16 - FS 409.00 + 112 IAW CRJ 200 AND MM 20-21-00-910-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,466 hrs · 21,221 cycles

RT SIDE SEAT RAIL BETWEEN FS 364.00 - FS 409.00 + 16 IS CORRODED ITEM FOUND AT C-CHECK INSPECTION. REPLACED RT SIDE SEAT RAIL BETWEEN FS 364.00 - FS 409 + 16 IAW CRJ SRM 51-40-11, 51-41-02, 51-41-04, 51-25-16.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 23,466 hrs · 21,221 cycles

PAX CABIN UNDER FLOOR AT FS 559 VERTICAL POST RBL 27.0 INBD FLANGE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-280.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 22,813 hrs · 20,718 cycles

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

Part: FRAME — CRACKED (PAX DOOR) · airframe 22,813 hrs · 20,718 cycles

PAX DOOR INNER DOOR SUB-FRAME IS CRACKED; FS 335.70 UPPER END OF DOOR. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SUB-FRAME IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-25-16.

Part: CLIP — CRACKED (FLOORBEAM) · airframe 22,813 hrs · 20,718 cycles

FS 280 RIGHT FLOORBEAM AT RBL 9.0 OUTBOARD ATTACH CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00.

Part: SILL — CORRODED (FUSELAGE) · airframe 22,813 hrs · 20,718 cycles

CABIN BELOW FLOOR, CORROSION UNDER FLOOR SILL AT FS 394.0 LBL 48.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ SRM 51-21-06, 53-00-00 FIG 102 AND 51-25-06.

Part: ANGLE — DAMAGED (PAX DOOR) · airframe 22,813 hrs · 20,718 cycles

PASSENGER DOOR INTERNAL STRUCTURE ANGLE IS DAMAGED AT DOOR DATUM 6; FS 331.13. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-42-06, 51-42-21, 51-23-00 AND 51-25-16.

Part: CLIP — CRACKED (FLOORBEAM) · airframe 22,813 hrs · 20,718 cycles

FS 280 LEFT FLOORBEAM AT LBL 9.0 INBOARD AND OUTBOARD ATTACH CLIPS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00.

Part: FRAME — CRACKED (PAX DOOR) · airframe 22,813 hrs · 20,718 cycles

PAX DOOR INNER FRAME IS CRACKED; FS 320.10 UPPER END OF DOOR. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DOOR FRAME FS 320.10 UPPER END IAW CRJ REO 601R-52-11-402 REV "B".

Part: FRAME — CRACKED (PAX DOOR) · airframe 22,813 hrs · 20,718 cycles

PAX DOOR INNER DOOR SUB-FRAME IS CRACKED; 323.30 UPPER END OF DOOR. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SUB-FRAME IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-25-16.

Part: FRAME — CRACKED (PAX DOOR) · airframe 22,813 hrs · 20,718 cycles

PAX DOOR INNER DOOR FRAME IS CRACKED; FS 338.90 UPPER END OF DOOR. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DOOR FRAME FS 338.90 UPPER END IAW CRJ REO 601R-52-11-402 REV B.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,813 hrs · 20,718 cycles

FUSELAGE FRAME FS 364 STR 8R FLANGE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FRAME IAW CRJ REO 601R-53-21-561.

Part: FITTING — CORRODED (PAX DOOR) · airframe 22,813 hrs · 20,718 cycles

PAX DOOR LOWER CORNER FITTINGS CORRODED; FS 312.00 + FS 346.00. ITEM FOUND AT C-CHECK INSPECTION. REPLACED FITTINGS IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-25-16 MOD SUM TC601R16637 REV A, TC601R16876 REV "A".

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,813 hrs · 20,718 cycles

FUSELAGE PULLEY INTERCOSTAL HAS CRACKED OUTBOARD REMOTE ANGLE FS 484.00 RBL-36.0. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE CRJ SRM 51-40-11, 51-25-06, 51-25-16, 51-42-06, 51-42-21, 51-23-00, 51-21-11.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,147 hrs · 20,199 cycles

AFT MOST EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED THE LAMP IN THE LIGHT ASSY, OPERATIONAL CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (AILERONS) · airframe 21,303 hrs · 19,542 cycles

AILERON TRIM WILL SOMETIMES NOT MOVE TO THE RIGHT. REMOVED AND REPLACED AILERON/RUDDER TRIM PANEL IAW MM 27-12-10, OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 20,879 hrs · 19,223 cycles

STAB CH 1 STATUS MESSAGE, CANNOT RESET. REMOVED AND REPLACED HORIZONTAL STAB ACTUATOR AND MCU IAW MM 27-42-01. OPS CHECKED GOOD. MCU P/N: 7062-3, S/N OFF: 602.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 20,580 hrs · 18,986 cycles

GEAR/FLAP ANNUNCIATED AT FL330. WHITE BAR WENT FROM FLAPS 2 DEGREES - 3 DEGREES - 6 DEGREES - 8 DEGREES. FLIGHT CONTROL PAGE SHOWS FLAPS 10 DEGREES LEFT, 0 DEGREES RIGHT - NO ADVERSE HANDING CHARACTERISTICS. REMOVED AND REPLACED FLAP POSITION INDICATOR AS REQ. OPS CHECK GOOD IAW MM 27-55-01.

Part: SWITCH — FAILED (TRIM DISCONNECT) · airframe 19,526 hrs · 18,180 cycles

STAB TRIM AND MACH TRIM FAILED SHORTLY AFTER TAKEOFF AND WOULD NOT RESET. RETURNED TO FIELD. REMOVED AND REPLACED COPILOT'S STAB TRIM DISCONNECT SWITCH IAW MM 27-41-30. OPS CHECK GOOD. P/N ON & OFF 996-0013.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 19,001 hrs · 17,784 cycles

''FLAPS FAIL'' CAUTION MESSAGE IN FLIGHT WITH FLAPS 0. (OCCURED ON DESCENT WITHOUT FLAP HANDLE BEING MOVED.)REMOVED AND REPLACED LEFT BPSU, REF MM 27-51-10. OPS CHECKS GOOD.

Part: BPSU — MALFUNCTIONED (T/E FLAP) · airframe 18,949 hrs · 17,749 cycles

FLAPS FAIL CAUTION DURING INITIAL DESCENT INTO SLC. NO FLAP LANDING. REMOVED AND REPLACED LEFT BPSU IAW MM 27-51-10. OPS CHECK GOOD. P/N: 955D100-9, S/N OFF: 206B.

Part: ECU — MALFUNCTIONED (T/E FLAP) · airframe 18,854 hrs · 17,672 cycles

AFTER LANDING IN SLC, WHEN FLAP SELECTED UP, 'FLAP FAIL' MSG AND FLAPS FAILED TO RETRACT. REMOVED AND REPLACED THE FECU WITH A SERVICEABLE UNIT IAW AMM 27-51-5. SYSTEM CHECKS GOOD. SN OFF 658.

Part: SKIN — CRACKED (RT WING) · airframe 18,873 hrs · 17,686 cycles

RT LWR WING PLANK WS 148 CRACKED. DISCOVERED DURING C-CHECK, REPAIRED DAMAGED AREA IAW CRJ REO 601R-57-21-130 REV 'D'.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,873 hrs · 17,686 cycles

FS 280 PILOT'S BULKHEAD RT VERTICAL ANGLE RBL 12 CRACKED. DISCOVERED DURING C-CHECK, REPLACED ANGLE IAW CRJ REO 601R-53-11-034 REV 'A'. P/N: 600-34017-724

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,895 hrs · 17,704 cycles

LT FIRE WALL SHUTOFF VALVE FS 665 ANGLE CRACKED. DISCOVERED DURING C-CHECK, REPAIRED ANGLE IAW CRJ SRM 51-40-11. P/N: S6144-13

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 18,873 hrs · 17,686 cycles

CARGO DOOR COAMING FS 580 CRACKED. DISCOVERED DURING C-CHECK, REPLACED COAMING IAW CRJ SRM 51-40-11. P/N: 600-35160-11

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 18,873 hrs · 17,686 cycles

FS 280 RT FLOORBEAM RBL 9.0 ATTACH ANGLES IB & OB CRACKED. DISCOVERED DURING C-CHECK, REPLACED ANGLES IAW CRJ SRM 51-40-11.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 18,895 hrs · 17,704 cycles

CARGO PIT HAS FLOORBEAM WITH BUCKLED WEB & CRACKED AT FS 589.0 - FS 605.0; LBL 27 INBOARD SIDE. DISCOVERED DURING C-CHECK, REPAIRED IAW CRJ SRM 51-24-36.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,873 hrs · 17,686 cycles

FS 484 LT INTERCOSTAL OB FLANGE LBL 36 AND IB CLIP LBL 27 CRACKED. DISCOVERED DURING C-CHECK, INTERCOSTALS REPAIRED IAW CRJ REO 601R-53-41-059 REV 'A'.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,873 hrs · 17,686 cycles

PILOT'S BULKHEAD AFT FLOOR ANGLE RBL 11.0 CRACKED. DISCOVERED DURING C-CHECK, REPAIRED ANGLE IAW CRJ REO 601R-53-11-137 REV 'NC'.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,873 hrs · 17,686 cycles

FS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. DISCOVERED DURING C-CHECK, REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06. P/N: 601-35012-51

Part: RIB — CRACKED (LT PYLON) · airframe 18,873 hrs · 17,686 cycles

LT PYLON HAS CRACK IN RIB AT FS 605.00. DISCOVERED DURING C-CHECK, REPLACED RIB IAW CRJ SRM 51-40-11.

Part: SKIN — CRACKED (LT WING) · airframe 18,873 hrs · 17,686 cycles

LT LWR WING PLANK WS 148 CRACKED. DISCOVERED DURING C-CHECK, DAMAGED AREA REPAIRED IAW CRJ REO 601R-57-21-130 REV 'D' & 601R-57-21-131 REV 'NC'.

Part: RIB — CRACKED (RT PYLON) · airframe 18,873 hrs · 17,686 cycles

RT PYLON RIB FS 605 CRACKED. DISCOVERED DURING C-CHECK, REPLACED RIB IAW CRJ SRM 51-40-11.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 18,895 hrs · 17,704 cycles

FS 589 + 605 TRANVERSE BEAM ANGLES LBL 42 CRACKED. DISCOVERED DURING C-CHECK, REPLACED ANGLES IAW CRJ SRM 51-40-11. P/N: 601R-35011-13

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,873 hrs · 17,686 cycles

FS 280 PILOT'S BULKHEAD LT VERTICAL ANGLE LBL 12 CRACKED. DISCOVERED DURING C-CHECK, REPLACED ANGLE IAW CRJ REO 601R-53-11-034 REV ''A''. P/N: 600-34017-723

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,873 hrs · 17,686 cycles

FS 625 RT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK, REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06. P/N: 601-35012-52

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 18,589 hrs · 17,467 cycles

FLIGHT TO SLC FLAPS FAIL CAUTION. FLAPS UP, CONTINUED TO SLC. REPLACED LEFT BRAKE POSITION SENSOR UNIT. OPS CHECK GOOD IAW 27-51-10. P/N OFF/ON 855D100-9, S/N OFF 593A.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 18,443 hrs · 17,357 cycles

STAB TRIM CHANNEL 2 WILL NOT REMAIN ENGAGED DURING TEST. REMOVED AND REPLACED HSTA AND MCU WITH A SERVICEABLE UNITS. OPS CHECK GOOD AT THIS TIME. P/N ON 7062-3 OFF 814.

Part: TRIM SWITCH — INOPERATIVE (COCKPIT) · airframe 17,694 hrs · 16,786 cycles

FIRST OFFICER'S STAB TRIM SWITCH IS INOP. REPLACED FIRST OFFICER'S TRIM SWITCH IAW CRJ MM 27-41-05. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (NR 1 AIR DATA) · airframe 17,530 hrs · 16,657 cycles

OVERSPEED CLACKER WHEN FLAPS EXTENDED FROM 20 DEGREE POSITION THROUGH 30 DEGREE AND 45 DEGREE POSITION. CONTINUED UNTIL FLAPS RETRACTED AFTER LANDING TO THE 20 DEGREE POSITION. REMOVED AND REPLACED NR 1 AIR DATA COMPUTER (ADC 850A) IAW MM 34-13-01. PERFORMED OPERATIONAL CHECK OF AIR DATA COMPUTER WITH PITOT STATIC EQUIPMENT IAW MM 34-11-00.

Part: WARNING LIGHT — ILLUMINATED (NLG STEERING) · airframe 16,999 hrs · 16,246 cycles

UPON DEPARTURE WHEN RETRACTING GEAR, WE RECEIVED NOSE STEERING INOP, GEAR DISAGREE, AND NOSE DOOR MESSAGES. FOLLOWED QRH, RETURNED TO SLC. INSPECTED AND SERVICED NOSE GEAR IAW CRJ MM 12-12-32. PERFORMED GEAR SWING IAW CRJ MM 32-30-00. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 16,127 hrs · 15,577 cycles

STAB CH 2 INOP STATUS MESSAGE IN FLIGHT, WOULD NOT RE-ENGAGE. REMOVED AND REPLACED THE HSTA AND MOTOR CONTROL UNIT WITH SERVICEABLE HSTA AND MOTOR CONTROL UNIT. OPS AND FUNCTION CHECK GOOD IAW CRJ MM 27-40-00, 27-42-00 & 27-42-05.

Part: SEAL — DIRTY (GALLEY DOOR) · airframe 15,976 hrs · 15,465 cycles

CLIMBING THROUGH 25,000 FEET, WITH A CABIN ALTITUDE OF 7.0, A VIBRATION STARTED THAT SEEMED TO BE COMING FROM THE FORWARD GALLEY DOOR. THE FLIGHT ATTENDANT ALSO REPORTED LOUD NOISE AND VIBRATION COMING FROM GALLEY DOOR.REPLACED DOOR SEAL IAW MM 52-41-07. FOUND CENTER PLUNGER ASSEMBLY FORK BENT. REMOVED AND REPLACED SERVICE DOOR CENTER PLUNGER ASEEMBLY WITH NEW PLUNGER ASSEMBLY IAW 52-41-00. OPS CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (COCKPIT) · airframe 15,542 hrs · 15,124 cycles

AFTER TAKEOFF AT 1000 FT AGL, BOTH STAB TRIM CH 1 & CH 2 AND MACH TRIM DISCONNECTED. BOTH STAB TRIMS WOULD NOT RE-ENGAGE. RETURNED TO SLC. REMOVED AND REPLACED FIRST OFFICER'S STAB TRIM DISCONNECT SWITCH IAW 27-41-30. OPS CHECKS GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 15,096 hrs · 14,764 cycles

CLIMBING THROUGH FL 240, THE RIGHT COCKPIT WINDOW SHATTERED. RETURNED TO ABQ. REMOVED AND REPLACED RIGHT SIDE WINDOW WITH SERVICEABLE UNIT IAW MM 56-12-01. OPS CHECK GOOD.

Part: BLADE — BENT (NR 2 ENGINE) · airframe 14,994 hrs · 14,686 cycles

WHILE INFLIGHT AT 35,000 FT FELT A THUMP, FOLLOWED BY A SLIGHT VIBRATION. ALL INDICATIONS NORMAL AND WITHIN PARAMETERS. ON DESCENT INTO SLC RIGHT NR 2 ENGINE VIBRATION INDICATION GRADUALLY INCREASED UP TO 2.5 BUT STILL WITHIN GREEN BAND ON GAUGE. ALL OTHER INDICATIONS NORMAL. ALL FAN BLADES ON RIGHT ENGINE REMOVED. FOUND SEVERAL FAN BLADES BENT ON RIGHT ENGINE. REINSTALLED ALL FAN BLADES IAW MM 72-00-00.

Part: SENSOR — MALFUNCTIONED (RT WING) · airframe 14,603 hrs · 14,367 cycles

DUCT FAIL LIGHT AND MESSAGE RIGHT SIDE WITH WING ANTI-ICE ON. REMOVED ALL RIGHT LEADING EDGES AND INSPECTED PICCOLO TUBES FOR CRACKS, NONE NOTED. REMOVED AND REPLACED RIGHT WING DUCT LEAK SENSORS IAW 30-11-41. COMPLIED WITH OPS CHECK OF WING ANTI-ICE SYSTEM IAW 30-11-41. OPS CHECK GOOD. P/N: 601R59320-1.

Part: WIRE — CHAFED (ANTI-ICE SYS) · airframe 14,684 hrs · 14,435 cycles

ANTI-ICE DUCT MESSAGE INFLIGHT (RIGHT SIDE). RETURNED TO SLC. REMOVED RIGHT O/B LEADING EDGE. FOUND A CHAFED WIRE AT DUCT LEAK SENSOR. REPAIRED CHAFE. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,603 hrs · 14,367 cycles

EMERGENCY TRACK AND RIGHT EXIT OVERWING INTERIOR LIGHTING INOP. PLACED EMERGENCY LIGHT SWITCH IN ARM POSITION FOR 30 MIN. EMERGENCY LIGHTS OPS CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 14,532 hrs · 14,316 cycles

PILOT'S LEFT SIDE WINDOW SHATTERED. REMOVED AND REPLACED LEFT SIDE WINDOW WITH SERVICEABLE UNIT IAW 56-12-01. P/N ON NP-139322-5, S/N OFF 99139H7837.