N220MJ

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 45,484 hrs · 43,813 cycles

AT 11800 FT, 20NM SOUTH OF DESTINATION CREW REPORTED AIRCRAFT LOST CABIN PRESSURE DURING DESCENT. CREW RAN THE CHECKLIST AND CONTINUED TO DESTINATION. A/C LANDED WITHOUT FURTHER INCIDENT. NO INJURIES WERE REPORTED. MX SECURED OUTFLOW VALVE OPEN AND MEL'D.

Part: POWER LEVER — OUT OF ADJUST · airframe 45,401 hrs · 43,697 cycles

ABORTED TAKEOFF AT 70KT DUE TO LT CTOT/APR NOT ENGAGING. MAINTENANCE ADJUSTED LT POWER LEVER. PERFORMED OP'S CHECKS. ALL CHECKED GOOD.

Part: SKIN — GOUGED (FUSELAGE) · airframe 45,061 hrs · 43,218 cycles

PERFORMED DOUBLER REPAIR FOR LARGE GOUGE ON THE LT FWD FUSELAGE IAW SAAB STATEMENT (SDS 023412). TD 340-53-12-02 CREATED FOR MAJOR REPAIR DOCUMENTATION. REF CONTROL # 220-40.

Part: CONNECTOR — LOOSE (MLG) · airframe 44,434 hrs · 42,323 cycles

FLIGHT 3870 JST-IAD DECLARED AN EMERGENCY DUE TO RIGHT MAIN GEAR INDICATION. CREW EXECUTED A GO AROUND RAN QRH CYCLED GEAR AND CHECKED THE LIGHT BULBS. CREW THEN EXECUTED A FLY BY THE TOWER, THE TOWER REPORTED THAT THE GEAR APPEARS TO BE DOWN, ALSO THERE WAS A UA CAPTAIN IN THE BACK OF THE AIRCRAFT AND REPORTED TO THE CREW THAT THE GEAR WAS DOWN. THE CABIN WAS PREPPED AND BRACED FOR AN UNSAFE LANDING. FLIGHT LANDED ON RUNWAY 1R WITHOUT INCIDENT AND WAS ABLE TO TAXI TO THE GATE A6E UNDER ITS OWN POWER. RESECURED MLG CONNECTOR. ALL OPS CHECKS GOOD, SWING CHECKS GOOD.

Part: DUCT — DEFECTIVE (RT ENGINE) · airframe 44,113 hrs · 41,858 cycles

ON INITIAL CLIMB AT APPROX 500 FT RIGHT ENGINE ITT INCREASED FROM 910 TO 980 DEGREES/POWER REDUCED TO 40 PERCENT TORQUE WHICH REDUCED TEMP. DECLARED EMERGENCY AND RETURNED TO FIELD IN IAD WITHOUT INCIDENT. REPLACED P3 DUCT, PERFOMED BORESCOPE FOR HIGHT ITT, OPS CHECKED GOOD.

Part: SWIVEL — DAMAGED (RT MLG) · airframe 43,996 hrs · 41,691 cycles

LOG PAGE "HYD FLUID QTY LOSS & MAIN HYD ACCUM FAILURE. HYD LEAK IN RIGHT MAIN GEAR WELL. REMOVED AND REPLACED RT MLG DOWNLOCK SWIVEL REF SAAB AMM 32-33-10-02. LANDING GEAR EXTENSION & RETRACTION REQUIRED OPS CHECKED OF LG EXT & RET GOOD REF SAMM 32-30-00-05.

Part: PANEL — FAULTY (COCKPIT) · airframe 43,841 hrs · 41,462 cycles

ABORTED TAKEOFF AT 75 KTS. AUTO COURSE HIGH LIGHT FAILED TO ILLUMINATE. L/R APR LIGHTS FAILED TO ILLUMINATE. CLEANED 64 DEG SWITCHES AS REQUIRED, REMOVED AND REPLACED CONSTANT TORQUE PANEL IAW 76-10-50. OPS CHECKED IAW 76-10-00 AND AMM 71-00-00 OPS CHECKED GOOD.

Part: GENERATOR — FAILED (AC) · airframe 42,186 hrs · 47,560 cycles

ON CLIMBOUT RECEIVED RIGHT AC GEN CAUTION LIGHT, AND RETURNED TO BGM. REPLACED RIGHT AC GEN, OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 43,625 hrs · 41,158 cycles

A REPOSITION FLIGHT ON CLIMB OUT CREW RESET THE RIGHT HAND BLEED THAT'S WHEN THEY GOT A BURNING SMELL IN THE FLIGHT DECK. CREW FOLLOWED THE QRH CHECKLIST AND DECLARED THE EMERGENCY AND RETURNED TO IAH. RAN AIRCRAFT OPS CHECKED GOOD IAW 71-00-00 & 21-60-00.

Part: DPU — MALFUNCTIONED (COCKPIT) · airframe 43,250 hrs · 40,571 cycles

LT EADI FAILED IN FLIGHT. SLIGHT ELECTRICAL BURNING SMELL, PULLED CB G18 LT EADI SCREEN BLACKED OUT. REPLACED LT EADI SCREEN IAW SAAB AMM 34-24-10, REPLACED LT DPU IAW SAAB AMM 34-24-20.

Part: FIRE WARNING — INTERMITTENT (NR 2 ENGINE) · airframe 42,844 hrs · 40 cycles

NR 2 ENGINE FIRE WARNING INTERMITTENT. CORRECTIVE ACTION STILL IN WORK.

Part: CLAMP — BROKEN (RT ENGINE) · airframe 42,838 hrs · 39,990 cycles

DURING GEAR RETRACTION, ENGINE FIRE (RT ENG) FIRE BELL AURAL ALERT ILLUMINATED AND WENT OUT. ENGINE FIRE CWP ONLY, HANDLE WAS NOT ILLUMINATED. DURING FLAP EXTENSION, AND GEAR EXTENSION, EXPERIENCED THE SAME PHENOMENON. INSTALLED WEU P/N 004W500, S/N 1116 AND OPS CHECKED PER AMM 26-11-00-05. INSTALLED FDCU P/N 899052-02, S/N ON 749, PERFORMED OPS CHECKS PER 26-11-00-05, OPS CHECKS GOOD. SWUNG GEAR SEVERAL TIME OPS CHECKS GOOD. DURING GEAR SWING FOUND RT ENG AFT FIRE LOOP CLAMP BROKEN, REMOVED AND REPLACED CLAMP P/N 245857 PER SRM 51-40-21, OPS CHECKS GOOD.

Part: CONTROL LEVER — MALFUNCTIONED (COCKPIT) · airframe 42,303 hrs · 39,245 cycles

ABORTED TAKEOFF DUE TO CONFIGURATION WARNING. CREW RESET CONDITION LEVERS. FLIGHT CONTINUE TO IAD.

Part: STRUCTURE — DAMAGED (NACELLE) · airframe 41,996 hrs · 38,807 cycles

ACFT REQUIRES MAJOR REPAIR FOR PER REPAIR FOR MISC RIVET DEVIATION ON RT INBOARD NACELLE IAW TD 340-54-10-02.

Part: CTOT PANEL — UNSERVICEABLE (COCKPIT) · airframe 41,740 hrs · 38,472 cycles

ABORTED TAKEOFF DUE TO CTOT AND APR INOP. REMOVED AND REPLACED THE CTOT PANEL, P/N 7239060-503.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,655 hrs · 38,355 cycles

AIRCRAFT REQUIRES MAJOR REPAIR DUE TO PERMANENT REPAIR OF FOUR DENTS BEHIND CARGO DOOR IAW SDS 018970 - TD 340-53-09-80 AND TRACKED BY DMI ID 12694.

Part: LIGHT — FAILED (CABIN) · airframe 40,231 hrs · 36,374 cycles

ODOR OF ELECTRICAL BURNING BY OVERHEAD COMPARTMENT AT ROW 2 AND 3. VISUAL INSPECTION OF WIRING AND LIGHTING AT SEAT 3A. FOUND BULB AND SOCKET CHARRED. REMOVED BULB AND DEFERRED IAW MEL 33-20-1-1.

Part: INDICATOR — FAILED (AIRSPEED) · airframe 37,397 hrs · 32,772 cycles

CAPT AIRSPEED INDICATOR FAILED, ABORTED AT APPROX 3040KTS. REMOVED AND REPLACED CAPT AIRSPEED INDICATOR IAW SMM 34-12-15, PN ON /OFF 622-5353-011 SN ON 285, SN OFF 20, OPS CHK GOOD.