N895QS

ATA 2120

Part: CLAMP — UNSECURE (CABIN AIR DUCT) · airframe 8,299 hrs · 6,028 cycles

WHILE CLIMBING THROUGH FL 270, A MUFFLED THUMP WAS HEARD FROM THE AFT CABIN. RESULTED IN LOSS OF CABIN PRESS WITH A CABIN CLIMB RATE OF APPROX 2700 FEET PER MINUTE. CABIN MASKS WERE MANUALLY DEPLOYED. UPON INSPECTION ON THE GND, A SIGNIFICANT BLEED AIR LEAK WAS NOTICED IN THE FWD SECTION OF THE REAR BAY WITH APU RUNNING. INSPECTED REAR BAY CABIN AIR DUCTING & FOUND BAND CLAMP COMPLETELY BACKED OFF OF CABIN AIR SUPPLY DUCT ON OUTLET END OF WATER SEPARATOR, SECURED BAND CLAMP AS REQUIRED & PRESSURIZED ACFT TO MAX DIFFERENTIAL PRESS USING APU NO LEAKS NOTED, PRESSURIZATION SYSTEM OPS CHECK GOOD. RE-PACKED CABIN O2 MASKS AS REQUIRED. ALL DONE IAW MM 21-30-00-501 & 35-20-01.

ATA 7200

Part: ENGINE — FAILED (NR 1) · airframe 7,441 hrs · 5,390 cycles

NR 1 ENGINE FAILED INFLIGHT AT FL390 AT TOP OF CLIMB. HEARD A LOUD BANG, SLAM & HAD HIGH ITT. THE THRUST LEVER WAS REDUCED TO IDLE & THE ENG WAS SUBSEQUENTLY SECURED WITH THE INFLIGHT ENG SHUTDOWN QRC. REMOVED AND REPLACED THE ENGINE. WORK ACCOMPLISHED IAW PPBM 71-20-03-401, AMM 71-00-00, 71-00-01, 71-00-02, , 71-10-00, 71-20-00, 71-70-00 AND LMM 72-02-96.

ATA 2120

Part: CLAMP — LOOSE (AC BAY) · airframe 6,685 hrs · 4,842 cycles

IN CRUISE FLIGHT AT FL 350, WE HEARD A LOUD THUMP & BANG FROM REAR OF CABIN. EXPERIENCED A RAPID DECOMPRESSION AT THIS POINT, CABIN CLIMB OF 2000 FPM PLUS. FOLLOWED PROPER CHECKLIST PROCEDURES, MANUALLY DEPLOYED PASSENGER MASKS. TROUBLESHOOTING REVEALED A LOOSE RUBBER BOOT BETWEEN THE WATER SEPARATOR AND J-DUCT. THIS CAUSED A MAJOR LEAK AND PREVENTED THE AIRCRAFT FROM PRESSURIZING. TIGHTENED RUBBER BOOT CLAMP. PRESSURIZED AIRCRAFT, LEAK CHECKED CLAMP, LEAK CHECK GOOD IAW M/M CH 21-10-15.

ATA 2120

Part: DISPLAY — ODOR (COCKPIT) · airframe 6,548 hrs · 4,748 cycles

THERE WAS A STRONG ACRID ODOR COMING FROM THE LT SIDE OF THE COCKPIT. ODOR DID NOT DISSAPATE, NO SMOKE OR FIRE. POWERED UP AIRCRAFT AND FOUND PILOTS PFD INOPERATIVE. REMOVED PFD AND DETERMINED ODOR WAS FROM BURNED COMPONENTS INSIDE THE DISPLAY UNIT. REPLACED PFD. OPS CHECKED SATISFACTORY. WORK ACCOMPLISHED IAW MM 31-03-00.

ATA 4997

Part: GROUND STUD — FAILED (APU GENERATOR) · airframe 6,273 hrs · 4,528 cycles

APU WOULD NOT START. TESTED APPROPRIATELY, ALL LIGHTS WORKING, BUT WHEN THE MASTER SWITCH WAS POSITIONED TO "START," NOTHING HAPPENED. IMMEDIATELY AFTERWARDS, THERE WAS A STRONG ELECTRICAL ODOR IN THE APU COMPARTMENT. FOUND APU GENERATOR GROUNDING CABLE ON AIRFRAME SIDE WELDED. REMOVED & REPLACED GROUND STUD, CRIMPED NEW TERMINAL. CONNECTED NEW TERMINAL TO GROUND STUD. OPS CHECK APU / GENERATOR. OPS CHECKED GOOD. DRAWING 2855, & 321868. MM 49-11-00.

ATA 5730

Part: SKIN — CORRODED (RT WING) · airframe 6,218 hrs · 4,486 cycles

TOP OF RT WING SKIN HAS CORROSION AND CORROSION ALL AROUND FUEL FILLER WING SKIN. REMOVED NON-MEASURABLE CORROSION FROM FASTENERS AND AROUND THE FUEL FILLER CAP AND REPLACED CORRODED FASTENERS ON THE WING FUEL PANELS W219, W206, W208 & W212 IAW SRM 51-73-00 AND MM 28-10-26-401. ALL CORROSION REMOVED AREAS ARE WITHIN LIMITS.

ATA 3097

Part: TERMINAL BLOCK — FAILED (WINDOW) · airframe 4,789 hrs · 3,447 cycles

BOTTOM LT CIRCUIT BREAKER ON THE SCREEN OVERHEAT TEST PANEL POPPED ALONG WITH BURNING SMELL. REMOVED LT WINDSCREEN FILTER AND REPLACED WITH NEW UNIT. R & R TERMINAL BLOCK PKA. PERFORMED WINDSCREEN OVERHEAT OPS CHECK OPS CEHCK GOOD. WORK IAW MM 30-41-00. TERMINAL BLOCK PN: 72441-225-0AV2.

ATA 3230

Part: LANDING GEAR — OUT OF ADJUST (LEFT) · airframe 4,615 hrs · 3,306 cycles

AFTER TAKEOFF, LT MAIN GEAR FAILED TO RETRACT. ADJUSTED LT MLG SIDE-STAY CLEARENCES IAW AMM 32-10-25. OPS CHECK GOOD.

ATA 3420

Part: COMPUTER — FAULTY · airframe 3,576 hrs · 2,535 cycles

ON TAKEOFF AT APPROXIMATELY 60KTS, THE STALL IDENT 3 ANN LIGHTS ILLUMINATED. TAKEOFF ABORTED, LIGHT EXTINGUISHED. REMOVED FAULTY THIRD CHANNEL IDENT STALL CAN P/N - 10201-1 S/N F469 INSTALLED REPAIRED STALL CAN P/N - 10201-1 S/N F415. SYSTEM OPS CHECKS FUNCTIONS PROPERLY. FOR DETAILS REFERENCE FAS W/O 07-2994 & DUNCAN W/O YFY7A. DONE IAW HAWKER 800XP MM CHAP 27-33--14-501

ATA 2730

Part: FUSE — OPEN (AFT SERVICE BAY) · airframe 3,497 hrs · 2,476 cycles

ELECTRIC ELEVATOR TRIM FAILED IN FLIGHT. REMOVED AND REPLACED ELEVATOR E-TRIM SERVO FUSE ZL-F24 PN:622-3260 SN:1CKYC AND PN: 5920-99-012-0075. PERFORMED SYSTEM FUNCTIONAL CHECK IAW AMM 27-30-00.

ATA 7200

Part: ENGINE — UNKNOWN (RIGHT) · airframe 3,021 hrs · 2,136 cycles

ABORTED TAKEOFF AT APPROXIMATLEY 40 KTS, DUE TO RED FLASHING INDICATOR WITH 105 PERCENT N1 ON RT ENGINE MAX KIAS INDICATED 60 KNTS DURING ABORT TAKEOFF TAXIED TO FBO. DOWNLOADED DEEC'S & FORWARDED TO HONEYWELL, RECORDED LIVE ENGINE DATA & FWD TO HONEYWELL, NO DEFECTS NOTED. OHMED OUT N1 MONOPOLE, NO DEFECTS NOTED. NO DEFECTS NOTED IAW HAWKER 800XP MM 31-41-05.