N508LX

Part: PROXIMITY SENSOR — DEFECTIVE (L1 DOOR) · airframe 8,620 hrs · 8,496 cycles

AT APPROXIMATELY 16,000 FT, RECEIVED A WARNING LIGHT FOR L1 DOOR. PRESSURIZATION NORMAL AND F/A VERIFIED THE DOOR SECURE. RETURNED TO DEPARTURE. AN EMERGENCY WAS NOT DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE CLOSED DOOR SENSOR AND PERFORMED RIG OF DOOR AMM. DOOR OPS CHECKED GOOD AND ACFT IS GOOD FOR SERVICE.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 8,602 hrs · 8,484 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND CORROSION IN COUNTER SINK SCREW HOLES ON ACCESS PANEL 522AT ON LT WING. R & R ACCESS PANEL.

Part: SEAL — CUT (CARGO DOOR) · airframe 8,328 hrs · 8,215 cycles

CREW REPORTED THAT UPON REACHING FL 130, UNABLE TO PRESSURIZE CABIN. ALL DOORS INDICATED CLOSED AND LOCKED AND CREW ELECTED TO RETURN TO DEPARTURE. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND A 3 INCH GASH IN THE AFT CARGO DOOR SEAL. MAINTENANCE R & R THE AFT CARGO DOOR SEAL IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.

Part: SEAL — LEAKING (PAX DOOR) · airframe 8,278 hrs · 8,159 cycles

CREW REPORTED THE L1 DOOR SEAL IS LEAKING. R & R DOOR SEAL IAW AMM AND OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: PSU — DISLODGED (SEAT 16AB) · airframe 8,155 hrs · 8,026 cycles

CREW REPORTED THAT THE PSU OVER SEATS 16 AB IS FALLING DOWN. MX SECURED THE PSU PANEL IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 8,116 hrs · 7,980 cycles

CREW REPORTED THAT THE A F/A FLASHLIGHT BATTERIES INOPERATIVE. MX REPLACED BATTERIES IAW AMM AND OPS CHECKED GOOD.

Part: GAS CYLINDER — FAILED (PAX DOOR) · airframe 8,065 hrs · 7,926 cycles

F/A UNABLE TO CLOSE THE MAIN CABIN DOOR FROM INSIDE THE CABIN. MX R & R MAIN DOOR GAS SPRINGS IAW AMM AND OPS CHECKED GOOD. ACFT GOOD FOR SERVICE.

Part: PSU — UNSECURE (ROW 16AB) · airframe 7,553 hrs · 7,423 cycles

CREW REPORTED THAT THE PSU AT ROW 16 AB FELL DOWN. MX SECURED PSU IAW AMM AND OPS CHECKED GOOD.

Part: TIRE — SEPARATED (RT MLG) · airframe 7,064 hrs · 6,951 cycles

AFTER DEPARTURE ATC NOTIFIED CREW OF POSSIBLE TIRE DEBRIS ON RUNWAY. PASSENGER CONFIRMED RIGHT INBOARD TIRE DID BLOW OUT, CREW DECLARED AN EMERGENCY AND RETURNED TO DEN WITH EMERGENCY VEHICLES ROLLING AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND ENTIRE TREAD CAP SEPARATED AND GEAR DOOR DAMAGED. MAINTENANCE REPLACED BOTH RIGHT MAIN LANDING GEAR TIRE ASSEMBLIES AND RIGHT MAIN LANDING GEAR DOOR PER BOMBA AMM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 7,056 hrs · 6,945 cycles

WHILE A/C WAS IN FOR HEAVY MAINT. FOUND RT SIDE OUTBOARD RIB CRACKED ON HORIZ STAB AT FWD UPPER FLANGE RADIUS, 3/4" LONG. MX LOCATED AND DRILLED REPAIR ANGLE INSTALLED REPAIR ANGLE TO RIB P/N 85517473-102 IAW Q400 SRM 51-40-07, 55-10-10. A/C REMAINS IN TUS FOR COMPLETION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 7,056 hrs · 6,945 cycles

WHILE A/C WAS IN FOR HEAVY MAINT FOUND FRAME FLANGE CRACKED AT RADIUS ON FS 196 STR 13L. CRACK IS 3/4" IN LENGTH IN RADIUS. MX REMOVED AND REPLACED DAMAGED FRAME IAW Q400 SRM 51-42-05, 51-40-07. P/N 85328121-105. A/C REMAINS IN TUS FOR COMPLETION.

Part: SKIN — DENTED (RUDDER) · airframe 7,056 hrs · 6,945 cycles

MULTIPLE DENTS ON TRAILING RUDDER LEFT SIDE UPPER SKIN. BTAC MX REMOVED AND REPLACED THE RUDDER LEFT SIDE UPPER SKIN P/N 85547156-103 IAW DASH 8 Q400 SRM 51-42-45 ON BTAC JOB 8418215 OP 53. A/C REMAINS IN TUS FOR COMPLETION.

Part: SKIN — DENTED (HORIZ STAB) · airframe 7,056 hrs · 6,945 cycles

HAIL DENTS UPPER HORIZONTAL STABILIZER RIGHT SIDE. REMOVED AND REPLACED RIGHT SIDE HORIZONTAL UPPER SKIN PANEL REF BTAC CO 8418212 OP 5011, 5012 IAW Q400 SRM 51-42-15 AND 51-41-05, AND JOB 841815 SKIN P/N 85517100-106. A/C REMAINS IN TUS FOR COMPLETION.

Part: SKIN — DENTED (RUDDER) · airframe 7,056 hrs · 6,945 cycles

HAIL DENTS LEFT SIDE FORE RUDDER, SKIN DENTED IN 9 PLACES. BTAS MX REMOVED AND REPLACED LEFT SIDE RUDDER SKIN PANELS P/N 85547102 REF BTAC JOB 8418215 OP 15. A/C REMAINS IN TUS FOR COMPLETION.

Part: SKIN — DENTED (RUDDER) · airframe 7,056 hrs · 6,945 cycles

DENTS FOUND ON FORE RUDDER LOWER SKIN PANEL P/N 85547101-105. BTAC MX REMOVED AND REPLACED THE FORE RUDDER LOWER SKIN PNL IAW Q400 SRM 51-42-05 ALL WORK DONE ON JOB 8418215 OP 5009. A/C REMAINS IN TUS FOR COMPLETION.

Part: SKIN — DENTED (RUDDER) · airframe 7,056 hrs · 6,945 cycles

FOUND SEVERAL DENTS IN THE AFT RUDDER LOWER SKIN PANEL P/N 85547155-101. BTAS MX REMOVED AND REPLACED THE AFT RUDDER LOWER SKIN PANEL IAW Q400 SRM 51-40-07, ALL WORK CARRIED OUT ON JOB 8418215 OP 5010. A/C REMAINS IN TUS FOR A/C COMPLETION.

Part: SKIN — DENTED (FUSELAGE) · airframe 7,056 hrs · 6,945 cycles

***MAJOR*** A/C HAS HAIL DAMAGE TO TOP SKIN THAT GOES UNDER WING, BETWEEN STR. X234.475 AND X301.00 BETWEEN STR 8S AND 8P. P/N 85360111-111. MX SPLICED SKIN AT X301.00 AND REMOVED AND REPLACED WITH NEW SKIN IAW BOMBARDIER RD 8/4-53-4633. DATED 5 JUL-12. A/C REMAINS IN TUS FOR A/C COMPLETION.

Part: SKIN — DENTED (HORIZ STAB) · airframe 7,056 hrs · 6,945 cycles

HAIL DENTS UPPER HORIZONTAL STABILIZER LEFT SKIN. BTAC MX REMOVED AND REPLACED THE LEFT SIDE HORIZONTAL UPPER SKIN PANEL REF BTAC JOB# 8418215 OP 5011 FOR ALL WORK PERFORMED. SKIN P/N 85517100-105. A/C REMAINS IN TUS FOR COMPLETION.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 6,589 hrs · 6,277 cycles

CREW REPORTED HYD NR 1 FAIL IN FLIGHT, AND DECLARED AN EMERGENCY INTO DEN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED VDP NR 1 PER BOMBDR AMM, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 6,583 hrs · 6,269 cycles

CREW REPORTED MID CABIN EMERGENCY LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY BATTERY PER BOMBDR AMM, OPS CHECK GOOD.

Part: COVER — OUT OF POSITION (CABIN) · airframe 6,354 hrs · 5,963 cycles

CREW REPORTED THE MAIN CABIN DOOR EMERGENCY LIGHT COVER FELL OFF DURING TAXI. MAINTENANCE RE-INSTALLED COVER PER BMB AMM, NO DEFECTS NOTED.

Part: STRUT — DEFECTIVE (PAX DOOR) · airframe 6,288 hrs · 5,872 cycles

CREW REPORTED PASSENGER DOOR WAS HEAVY TO CLOSE. MAINTENANCE REMOVED AND REPLACED PASSENGER DOOR GAS BALANCE STRUTS PER BOMBDR AMM, OPS CHECK GOOD.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 6,181 hrs · 5,726 cycles

CREW REPORTED THE F/A EMERGENCY LIGHT SWITCH WAS INOP. MAINTENANCE RELAMPED SWITCH PER BMB AMM, OPS CHECK GOOD.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 2) · airframe 4,276 hrs · 3,876 cycles

ALL GEAR DOOR AMBER LIGHTS REMAINED ILLUMINATED AFTER TAKEOFF. RAN QRH, PERFORMED ALTERNATE GEAR EXTENSION. AIRCRAFT NUMBER TWO ENGINE DRIVEN HYD PUMP HAD BEEN CHANGED AND BLED PRIOR TO TAKEOFF. SUSPECTED AIR IN SYSTEM. AIRCRAFT WAS REPOSITIONED AS A MAINTENANCE FERRY FLIGHT FROM FAR TO DEN. MAINTENANCE PERFORMED ADDITIONAL BLEEDING OF THE NUMBER 2 HYDRAULIC SYSTEM AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (MLG) · airframe 931 hrs · 765 cycles

RIGHT AFTER ROTATION WHEN GEAR WAS SELECTED UP, LT, NOSE AND RT GREEN GEAR LIGHTS INDICATIONS STAYED ILLUMINATED. UPON SELECTING GEAR UP, RED LIGHTS (LT, NOSE AND RT HANDLE ILLUMINATED. AMBER LIGHTS NEVER ILLUMINATED. RAN QRH, SPEED REMAINED BELOW 185KIAS, LANDING WEIGHT WAS NOT EXCEEDED. TROUBLESHOT NLG CENTERING PROX SENSOR. ADJUSTED PROX SENSOR IAW AMM 32-61-06-830. TORQUE WRENCH SN F9TAB1567C CAL DUE 3/09. OPS CHECK GOOD. NO DEFECTS AT THIS TIME. PERFORMED A FUNCTIONAL TEST OF THE LANDING GEAR PRIMARY EXTENSION AND RETRACTION IAW AMM 32-31-00-720-80. OPS CHECK GOOD.