N102QS

ATA 7321

Part: FUEL CONTROL — MALFUNCTIONED (NR 1 ENGINE) · airframe 3,959 hrs · 3,680 cycles

DURING TAXI, AFTER NORMAL ENGINE START, NR 1 ENGINE SHUTDOWN ON ITS OWN. BEFORE SECOND ENGINE START ATTEMPT, EXECUTED SHUTDOWN AND START CHECKLIST, BUT THE NR 1 ENGINE N2 NEVER WENT ABOVE 41 PERCENT. REMOVED DEFECTIVE LT FUEL CONTROL. INSTALLED REPAIRED LT FUEL CONTROL. PERFORMED LT FUEL CONTROL RIGGING PROCEDURES AND ENG RUNS. LEAK AND OPS CHECKS ARE GOOD. NO FURTHER DEFECTS NOTED. ALL WORK PERFORMED IAW MM 73-20-02.

ATA 5414

Part: SKIN — CRACKED (NACELLE) · airframe 3,935 hrs · 3,654 cycles

LT PYLON AFT UNDERSIDE SKIN IS CRACKED AT TOW RIVET LOCATIONS. COMPLIED WITH THE REMOVAL AND REPLACEMENT OF THE LT PYLON SKIN, PN 45A34420-049. PN OF THE RIVETS USED FOR THE R & R IS CR3242-4-02 BLIND RIVETS. WORK WAS PERFORMED IAW THE MODEL 400XP, SRM CHAPTERS 51-40-01; 51-41-00; 51-43-00 AND 51-43-01.

ATA 7830

Part: ANGLE — CRACKED (THRUST REVERSER) · airframe 3,935 hrs · 3,654 cycles

LT T/R, OTBD STANG FAIRING, UPPER ATTACH BRACKET IS CRACKED. R & R LEFT THRUST REVERSER OTBD UPPER STANG ANGLE. WORK WAS PERFORMED IN REF TO SRM 51-40-01.

ATA 2750

Part: CONTROL CABLE — OUT OF RIG (TE FLAPS) · airframe 3,187 hrs · 2,935 cycles

FLAP ASYMMETRY ANNUNCIATOR ILLUMINATED ON APPROACH, JUST AFTER FLAPS SELECTED TO 10 DEGREES. FLAPS EXTENDED A FEW DEGREES BEFORE FREEZING IN PLACE. FLAP HANDLE RETURNED TO ZERO DEGREES TO MATCH CONDITION OF INDICATOR WITH NO MOVEMENT OR RETRACTION NOTED. NO ASYMMETRY IN THE FLIGHT CONTROLS NOTED. FOUND FOWARD RT WING FLAP CABLE TENSIONS OUT OF LIMITS, AFT AT 346 LBS AND FWD LOW AT 155 LBS RT WING & INTERCONNECT IN LIMITS. ADJUSTED RT WING FLAP CABLE INTO LIMITS. OPS CHECKS GOOD FOR RT FLAP CABLE ADJUSTMENTS. PERFORMED 2ND FLAP ASYMMETRY TEST/OPERATION CHECK SATISFACTORY, FIND GROUND RUN AND OPS CHECKS GOOD FOR FLAPS AT THIS TIME MM 27-50-00.

ATA 5534

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 2,542 hrs · 2,312 cycles

FOUND DAMAGE ON VENTRAL FIN. POSSIBLE LIGHTNING STRIKE. LOCATED, DRILLED, AND INSTALLED REPLACEMENT VENTRAL FIN USING SCREWS AND RIVETS PER SRM 51-40-01 AND SERVICE MANUAL DEVIATION FORM NUMBER 1-18X37K.

ATA 3240

Part: VALVE — STICKING (BRAKE) · airframe 1,798 hrs · 1,605 cycles

ON LANDING AND ROLLOUT WHILE BRAKING LT, BRAKE DID NOT OPERATE FROM 3-4 SECONDS THEN GRABS AND PULLS LT SHARPLY. CONFIRMED DISCREPANCY, FOUND POWERBRAKE VALVE STICKING. GAINED ACCESS TO VALVE. REMOVED VALVE AND INSTALLED AN OVERHAULED VALVE. BLED SYSTEM, PERFORMED FUNCTIONAL TEST AND TAXI CHECKED TO 40KTS. LEAK AND OPS CHECKS GOOD AT THIS TIME. WORK DONE I/A/W HAWKER 400XP M/M 32-40-00. RESTORED ACCESS ITEMS.

ATA 3240

Part: CONTROL VALVE — INOPERATIVE (BRAKE SYS) · airframe 1,647 hrs · 1,447 cycles

NO BRAKES ON RIGHT SIDE. RIGHT BRAKE PEDAL P/CP GOES TO FLOOR. REMOVED AND REPLACED POWER BRAKE ANTI-SKID CONTROL VALVE IAW HAWKER 400 XP MM 32-40-00. OPS AND LEAK CHECK GOOD.

ATA 3100

Part: DISPLAY — BURNED OUT (COCKPIT) · airframe 1,356 hrs · 1,192 cycles

MFD WENT BLACK IN FLIGHT- DETECTED POSSIBLE SMOKE. REMOVED AND REPLACED MFD WITH OVERHAULED UNIT RECEIVED. ALL WORK PERFORMED IAW SRM NR 523-0775807. OPS CHECK GOOD. NO SMOKE ODOR NOTED AT THIS TIME.

ATA 3260

Part: INDICATOR — INOPERATIVE (MLG) · airframe 597 hrs · 489 cycles

LEFT GREEN LANDING GEAR DOWN INDICATOR LIGHT WOULD NOT ILLUMINATE WITH GEAR SELECTED . CYCLED GEAR 2 TIMES NO CHANGE, DID EMERGENCY GEAR RETRACTION (PNEUMATIC) AND LEFT LIGHT STILL DIDN'T ILLUMINATE . TURNED ON ALL INDICATOR LIGHTS AND LEFT GEAR WOULD NOT ILLUMINATE. - REPLACED LANDING GEAR INDICATOR LIGHT ASSEMBLY IAW HAWKER 400XP M/M, CHAPTER 32-60-00, OPS CHECK GOOD. POWERED LDG. GEAR HDYRAULIC SYSTEM AND SERVICED HYDRAULIC RESERVIOR I.A.W. 400XP M/M CHAPTER 32-30-00, OPS CHECK GOOD.