N272SK

Part: FITTING — CRACKED (ENGINE MOUNT) · airframe 34,973 hrs · 30,133 cycles

LEFT ENGINE LOWER FWD YOKE LINKAGE FITTING CRACKED. R & R LT ENGINE LOWER FWD YOKE LINKAGE FITTING IAW ETD2015-145-112035, REV A.

Part: ROD — NOT REPORTED (PAX DOOR) · airframe 34,728 hrs · 29,877 cycles

THE MAIN ENTRY DOOR AIRSTAIRS WOULD NOT RETRACT WHEN THE DOOR WAS CLOSED. MAINTENANCE R & R THE DOOR STEP ACTUATING ROD IAW AMM 52-10-03 AND ALL OPS CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,590 hrs · 29,740 cycles

DURING INSPECTION, THE EMERGENCY EXIT SIGNS OVER THE LT OVERWING EMERGENCY EXIT, FORWARD BULKHEAD, AND SERVICE DOOR WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 2, 3, AND 5 INVERTERS IAW AMM 33-50-11 AND ALL OPS CHECKS WERE GOOD; NO FURTHER DEFECTS HAVE BEEN NOTED.

Part: WINDSHIELD — FAULTY (COCKPIT) · airframe 33,992 hrs · 29,134 cycles

THE CREW REPORTED A BURNING ODOR IN FLIGHT WHEN THE WINDSHIELD 1 HEAT WAS IN OPERATION. THE ACFT LANDED AT ITS INTENDED DESTINATION WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED WINDSHIELD 1. OPS AND PRESSURIZATION CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 33,989 hrs · 29,131 cycles

THE CREW REPORTED THAT THEIR WAS A BURNING ODOR IN THE COCKPIT AND CABIN DURING FLIGHT. THE ACFT LANDED UNEVENTFULLY AT ITS INTENDED DESTINATION. MAINTENANCE INSPECTED THE ELECTRICAL DISTRIBUTION SYSTEM, THE CABIN AND COCKPIT LIGHTING, THE ELECTRIC HYDRAULIC PUMPS, AND THE ANTI-ICE SYS WITH NO DEFECTS. THEY ALSO RAN BOTH PACKS FROM BOTH THE ENGINE AND APU BLEED SYSTEMS WITH NO DEFECTS NOTED. THE ACFT WAS RETURNED TO SERVICE WITH NO ODORS OR SIGNS OF BURNING.

Part: FRAME — GOUGED (FRM 15) · airframe 33,522 hrs · 28,704 cycles

DURING INSPECTION, A GOUGE WAS FOUND ON FRAME 15 BETWEEN STRINGERS 1R AND 2R. THE FRAME REPAIRED IAW SRM 53-00-04, SRM 51-40-02, AND CPM 51-21-04.

Part: FRAME — CRACKED (FRM 10) · airframe 33,522 hrs · 28,704 cycles

DURING INSPECTION, FRAME 10 ON THE CAPTAIN`S SIDE WAS FOUND TO BE CRACKED UNDER THE DV WINDOW. THE FRAME SECTION WAS REPLACED IAW SRM 51-40-02.

Part: FRAME — CRACKED (FRM 10) · airframe 33,522 hrs · 28,704 cycles

DURING INSPECTION, FRAME 10 ON THE FIRST OFFICERS SIDE WAS FOUND TO BE CRACKED UNDER THE DV WINDOW. THE FRAME SECTION WAS REPLACED IAW SRM 51-40-02.

Part: FRAME — CRACKED (FRM 750 S2R) · airframe 33,522 hrs · 28,704 cycles

DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 AND STRINGER 2R. THE SKIN WAS REPAIRED IN ACCORDANCE WITH ETD 2015-145-00367

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 33,522 hrs · 28,704 cycles

DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO FLOOR SUPPORT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 24) · airframe 33,522 hrs · 28,704 cycles

DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM SILL AT FRAME 24. THE SILL WAS REPAIRED IAW ETD 2015-145-004502.

Part: STEP — CORRODED (PAX DOOR) · airframe 33,522 hrs · 28,704 cycles

DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER NUTPLATE FOR THE PASSENGER DOOR LOWER STEP. THE CENTER NUTPLATE STRIP FITTING WAS REPLACED IAW SRM 51-40-02.

Part: SKIN — DAMAGED (FRAME 14) · airframe 33,522 hrs · 28,704 cycles

DURING HEAVY, FOUND A LIGHTNING BURN. A REPAIR DOUBLER WAS INSTALLED AT FRAME 14 AND STRINGER 1R IAW ETD 2014-145-081088.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 32,987 hrs · 28,234 cycles

DURING INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AT FRAME 20. THE RAM ANGLE WAS REPLACED IAW SRM 51-40-02.

Part: PROFILE — CORRODED (FUSELAGE) · airframe 32,987 hrs · 28,234 cycles

DURING INSPECTION THE PROFILE FWD OF THE RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. THE PROFILE WAS REPAIRED IAW SRM 53-21-10.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 32,987 hrs · 28,234 cycles

DURING INSPECTION THE RT RAMP SUPPORT WAS FOUND TO BE CORRODED. THE RT RAMP ANGLE WAS REPLACED IAW SRM 51-40-02 & ETD 2014-145-08-1412.

Part: SWITCH — FAULTY (BLEED AIR SYS) · airframe 32,627 hrs · 27,895 cycles

CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 1 VLV FAIL MSG. THE ACFT WAS DIVERTED & LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE BLEED SYS 1 PUSH BUTTON SWITCH. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.

Part: FLAPPER VALVE — BROKEN (CABIN PRESSURE) · airframe 32,501 hrs · 27,786 cycles

CREW REPORTED THAT THE AUTO PRESSURIZATION SYS WAS INOPERATIVE DURING FLIGHT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX FOUND THE MANUAL PRESSURIZATION SYS TO BE WORKING & DEFERRED THE AUTO PRESSURIZATION. THE DEFERRAL WAS CLEARED ON 6/11/14 WHEN MX REPLACED THE GND AIR CONNECTION FLAPPER VLV.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,426 hrs · 27,715 cycles

DURING INSPECTION, THE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 31,902 hrs · 27,240 cycles

CREW REPORTED THAT DURING FLIGHT, PACK 1 HAS AN ODOR WHEN SELECTED ON. INSPECTED THE PACK AREA WITH NO DEFECTS. OPERATIONS CHECKED GOOD WITH NO DEFECTS OR ODORS NOTED.

Part: CONTROLLER — ERRATIC (CABIN PRESSURE) · airframe 31,558 hrs · 26,911 cycles

CREW REPORTED THAT THEY WERE UNABLE TO PRESSURIZE THE AIRCRAFT IN THE AUTO PRESSURIZATION MODE. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. THE AUTO PRESSURIZATION FUNCTION WAS DEFERRED. THE DEFERRAL WAS CLEARED ON 11/21/2013 WHEN MX REPLACED THE DIGITAL CONTROLLER. OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.

Part: ICU — FAULTY (NR 2) · airframe 31,519 hrs · 26,875 cycles

CREW REPORTED THAT AFTER TAKEOFF BOTH RADIO MANAGEMENT UNITS SHOWED DASHES IN THE TRANSPONDER AND TCAS FIELDS. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 INTEGRATED COMMUNICATIONS UNIT. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,463 hrs · 26,826 cycles

DURING INSPECTION, OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND ALL OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,463 hrs · 26,826 cycles

DURING INSPECTION, FORWARD WING TO FUSELAGE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND OPS CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 30,907 hrs · 26,295 cycles

MX REPORTED THAT THE MAIN ENTRY DOOR HANDRAIL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPAIRED WIRE W737-0034-20. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 30,016 hrs · 25,398 cycles

CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER ROTATION AND REPORTED THAT THE LANDING GEAR DID NOT RETRACT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS HARNESS. OPERATIONAL CHECKS AND LANDING GEAR SWINGS WERE GOOD WITH NO FURTHER DEFECTS NOTED.

Part: CONTROL UNIT — FAULTY (BRAKE SYSTEM) · airframe 29,940 hrs · 25,328 cycles

CREW REPORTED THAT ON LANDING THE CAPTAIN'S BRAKES SEEMED TO LOSE PRESSURE FOR APPROXIMATELY ONE SECOND AND THEN WOULD GRAB. THE AIRCRAFT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE BRAKE CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,285 hrs · 24,747 cycles

DURING INSPECTION, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 3 AND 12 WERE FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE OVERHEAD EMERGENCY LIGHTS AT ROWS 3 AND 12. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.

Part: DOOR FRAME — CORRODED (SERVICE DOOR) · airframe 29,283 hrs · 24,745 cycles

DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR STRUCTURE AROUND THE FASTENERS AT THE BOTTOM OF THE DOOR. THE SERVICE DOOR STRUCTURE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-013524.

Part: DOOR FRAME — CORRODED (SERVICE DOOR) · airframe 29,283 hrs · 24,745 cycles

DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR STRUCTURE AROUND THE FASTENERS AT THE BOTTOM OF THE DOOR. THE SERVICE DOOR STRUCTURE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-013524.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 29,283 hrs · 24,745 cycles

DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE WALL SEAT TRACK SUPPORT AT FRAME 50. THE SEAT TRACK SUPPORT AT FRAME 50 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 28,714 hrs · 24,205 cycles

CREW REPORTED AN ELECTRICAL ODOR FROM THE CEILING LIGHT AT SEAT 1A. REMOVED AND REPLACED CEILING LIGHT BALLAST. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 28,045 hrs · 23,608 cycles

CREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A LAVATORY SMOKE WARNING MESSAGE. FLIGHT ATTENDANT VERIFIED THAT THERE WAS NO SMOKE OR ODOR IN THE CABIN. DECLARED AN EMERGENCY AND RETURNED TO FIELD. MESSAGE CLEARED ON LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO EVIDENCE OF FIRE OR SMOKE IN THE LAVATORY. LAVATORY SMOKE DETECTOR REPLACED. OPS CHECKED GOOD WITH NO FURTHER DEFECT NOTED.

Part: ENGINE — LEAKING (LEFT) · airframe 27,143 hrs · 22,897 cycles

CREW REPORTED THAT DURING TAKEOFF THERE WAS SMOKE IN THE CABIN AND COCKPIT. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT-HAND ENGINE. ALL LEAK CHECKS AND OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 27,134 hrs · 22,889 cycles

CREW REPORTED THAT DURING CLIMB THERE WAS SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED TO KDTW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT ELECTRICAL SYSTEM, THE WINDSHIELD HEATING SYSTEM, OPERATED BOTH COOLING PACKS, AND PERFORMED ENGINE RUNS WITH NO DEFECTS NOTED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 26,330 hrs · 22,218 cycles

DURING INSPECTION, THE UPPER AFT ILLUMINATED PLACARD FOR THE RIGHT OVERWING ESCAPE HATCH WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 5 DC TO AC INVERTER. OPERATIONAL CHECKS OF THE UPPER AFT ILLUMINATED PLACARD FOR THE RIGHT OVERWING ESCAPE HATCH WERE GOOD WITH NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,539 hrs · 20,603 cycles

DURING INSPECTION, THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT SEAT 6A WAS INOP. MAINTENANCE REPLACED THE LIGHT STRIP.

Part: FIXTURE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,149 hrs · 19,423 cycles

DURING INSPECTION, MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT INOP. THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT ASSEMBLY WAS REPLACED WITH NO FURTHER DEFECTS NOTED.

Part: BLEED VALVE — CLOSED (NR 2 ENGINE) · airframe 22,313 hrs · 18,590 cycles

FLIGHT 6030 FROM CMH TO JFK. THE FLIGHT CREW RECEIVED A BLEED 2 VALVE CLOSED MESSAGE DURING FLIGHT. THE CREW CYCLED THE VALVE BUT THE MESSAGE REMAINED. THE AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 PRSOV AND THE BLEED SYSTEM OPERATED NORMALLY.

Part: CONNECTOR — UNSECURE (DOOR WARNING) · airframe 21,819 hrs · 18,066 cycles

FLIGHT 6033, CVG TO MSY. AFTER TAKE-OFF THE CREW RECEIVED A CABIN SERVICE DOOR WARNING ON EICAS AND RETURNED TO CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED THE SERVICE DOOR EICAS INDICATION AND RELEASED THE AIRCRAFT FOR SERVICE. THE DEFERRAL WAS CLEARED ON 4/8/2009 WHEN THE CONNECTOR FOR THE DOOR HARNESS WAS RE-SECURED AND THE DOOR INDICATION OPERATED NORMALLY.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 21,695 hrs · 17,928 cycles

FLIGHT 6042, CVG TO JAX - THE FLIGHT CREW REPORTED THAT DURING CLIMB AT FL230 THEY HEARD A POP FROM THE CAPTAIN'S WINDSCREEN AND THE OUTSIDE PANE WAS CRACKED. THE FLIGHT RETURNED TO CVG AND LANDED WITHOUT INCIDENT. THE CAPTAIN'S WINDSHIELD WAS REPLACED IAW AMM 56-10-01 WITH PRESSURE AND SECURITY CHECKS GOOD.

Part: CONTACTOR — FAULTY (EMERGENCY LIGHTS)

FLIGHT 6312, CVG TO FWA. WHILE CLIMBING THROUGH 1,000 FT, AN EMERGENCY LIGHTS NOT ARMED WAS DISPLAYED. THE EMERGENCY LIGHTS WERE RESET AND LIGHTS CAME BACK ON ALONG WITH AN ELECTRICAL EMERGENCY ABNORMAL MESSAGE. THE ELECTRICAL PAGE ON THE MFD SHOWED NORMAL LOADS AND VOLTAGE. THE QRH WAS COMPLIED WITH AND THE ACFT RETURNED TO CVG. MAINTENANCE FOUND NO MESSAGES ON THE CMC AND TROUBLESHOT THE FAULT TO THE ESSENTIAL BUSS CONTACTORS. BOTH K0079 AND K0080 WERE REPLACED. (S)

Part: ACTUATOR — OUT OF ADJUST (THRUST REVERSER) · airframe 19,784 hrs · 15,968 cycles

CMH TO CMH - DURING CLIMB-OUT FROM CMH, THE CREW RECEIVED AN E1 REVERSER DISAGREE MESSAGE ON EICAS. THE CREW LEVELED OFF, FOLLOWED THE APPROPRIATE QRH CHECKLISTS, AND E1 WAS SHUTDOWN. THE AIRCRAFT THEN LANDED AT CMH WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE E1 REVERSER AND FOUND THAT THE UPPER AND LOWER PIVOT DOOR ACTUATORS WERE OUT OF ADJUSTMENT. AFTER ADJUSTING THE ACTUATORS, THE THRUST REVERSER OPERATED NORMALLY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 16,923 hrs · 13,324 cycles

FOUND OVERWING EMERGENCY LIGHT ON RIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 30-50-04-4.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,885 hrs · 13,287 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED AFT EMERGENCY LIGHT BULB IAW MM 33-50-00. OPS CHECK GOOD.

Part: STARTER — SMOKE (ENGINE) · airframe 14,305 hrs · 11,106 cycles

ON PUSHBACK & ENG START, NORMAL UNTIL START OF NR 1 ENG, WHEN START/STOP SELECTOR ENGAGED RECEIVED NO INDICATION OF NORMAL START. NO ROTATION, NO OIL PRESSURE, NO FUEL FLOW, AND NO ITT RISE. ABORTED START, ATTEMPTED A CROSS BLEED START, SAME RESULTS. TAXIED TO GATE TO ATTEMPT A EXTERNAL AIR START. NOTIFIED BY GROUND PERSONNEL OF SMOKE COMING OUT OF ENGINE. BEGAN EMERGENCY EVACUATION MEMORY ITEM & CHECKLIST. CAPTAIN PULLED BOTH FIRE HANDLES. F/O NOTIFIED ATC & VISUALLY VERIFIED CHECKLIST ITEMS. VISUALLY INSPECTED NR 1 ENG & SAW SMOKE. BLEW -A- BOTTLE & WAITED, SMOKE STILL VISIBLE AS STRONG IF NOT STRONGER. BLEW B-BOTTLE AND SMOKE BEGAN TO CEASE. REMOVED & REPLACED TURBINE STARTER.

Part: BATTERY PACK — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 13,319 hrs · 10,356 cycles

ON INITIAL WALK OUT TO THE AIRCRAFT THE EMERGENCY LIGHTS WERE ALL ON. FOUND THE SWITCH IN THE COCKPIT TO BE IN THE OFF POSITION. INSPECTED AIRCRAFT AND FOUND IT TO BE SAFE FOR FERRY FLIGHT FROM TPA TP CMH. REMOVED AND REPLACED ALL FOUR EMERGENCY BATTERY PACKS. OPS CHECK GOOD IAW EMB 145 AMM 33-50-4.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,671 hrs · 9,922 cycles

EMERGENCY FLOOR PROXIMITY LIGHTING IS INOP AT SEATS 8 AND 9. REMOVED AND REPLACED FLOOR LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD.