N713QS

ATA 5210

Part: TRIM PANEL — OUT OF ADJUST (ZONE 800) · airframe 96 hrs · 60 cycles

HEARD CLICKING NOISE DURING CLOSING OF MAIN CABIN DOOR IN THE VICINITY OF THE DOOR RETRACT MECHANISM. ON POST FLIGHT CHECKED THE EMERGENCY RETRACT HANDLE. PULLED IT SEVERAL TIMES AND DOOR DID NOT RETRACT. FOUND DECORATIVE TRIM PIECE HITTING THE AFT DOOR STRUT WHEN DOOR WAS CLOSING. ADJUSTED DECORITVE TRIM PIECE AND STRUT NO LONGER HITS TRIM PIECE, INSPECTED DOOR MECHANSIAM FOR ANY DISCREPANCIES OR DAMAGE. NO DISCREPANCIES OR DAMAGE FOUND. DOOR OPERATES FINE. / INFORMED MCC AND MCC OK TO SIGN OFF. WORK DONE IAW CL-350 AMM 25-00-00

ATA 7200

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 5,276 hrs · 4,013 cycles

LEFT ENG ROLLED BACK TO 91% N1 ON T/O ROLL (APROX 80 KNOTS). T/O ABORTED. INSP EEC FOR FAULTS NONE NOTED. RAN A/C AT ALL POWER SETTINGS IN AUTO & MANUAL MODES. NO ROLL BACK NOTED SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME ALL WORK DONE IAW CE 650 M/M 76-10-04 & HONEYWELL TFE731 M/M 76-00-00

ATA 2750

Part: GEARBOX — FROZEN (TE FLAPS) · airframe 4,872 hrs · 3,713 cycles

FLAPS INOP, WOULD NOT EXTEND. FLAP INOP LIGHT ILLUM, WOULD NOT RESET. CHK`D FLAP CONTROLLER. NONE FOUND GAINED ACCESS TO FLAP PDU. DISCONNECTED RT FLAP DRIVE CABLE FROM PDU. UPON REMOVAL, DRIVESHAFT OF FLEX CABLE REMAINED IN PDU & CABLE SEPARATED FROM PDU. REMOVED RT INBD FLAP FLEX DRIVE CABLE ASSY IAW MM. OK TO INSTALL. INSTALLED NEW RT FLAP FLEX CABLE BETWEEN PDU & GEAR BOX TURN A/C PWR ON & FLAP INOP ILLUM BITE CODE NR 5. DISCONNECTED FLEX CABLES AT PTU. ATTEMPTED TO MANUAL DRIVE FLAPS. RT FLAP WOULD NOT MOVE. REMOVED RT FLAP GBOX. FLAPS MANUAL MOVED FREELY. INSPECTED GBOX FOUND 1 BEARING SEIZED. R & R RT GBOX IN REF TO 650 MM. RE-INSTALLED FLEX CABLES TO PTU. T/S BITE NR 5 TO BLOWN FUSE LIMI

ATA 3260

Part: INDICATOR — INOPERATIVE (MLG) · airframe 4,491 hrs · 3,411 cycles

LT GEAR ANNUNCIATOR FAILED TO LIGHT DURING GEAR EXTENSION (OR ROTORY TEST) BLEW GEAR DOWN USING CHECK LIST PROCEDURE. DURING ROLL OUT (L) SIDE GEAR BEGAN SMOKING. FOUND LT LANDING GEAR INDICATOR PULLED LOOSE IN ITS SOCKET. RESET INDICATOR AND PERFORMED LANDING GEAR FUNCTIONAL TEST IAW CE-650 M/M 32-00-01. OPS CHECK GOOD. VISUALLY INSPECTED LT GEAR, WHEEL AND BRAKE FOR DAMAGE. NONE NOTED.

ATA 3241

Part: ANNUNCIATOR — ILLUMINATED (ANTI SKID SYS) · airframe 4,488 hrs · 3,408 cycles

DURING OCF TAKEOFF ROLL, AT 70 KIAS, THE ANTI-SKID ANNUNICATOR ILLUMINATED. ABORTED TAKEOFF. LIGHT WENT OUT AFTER WE EXCITED THE RUNWAY. TROUBLESHOT ANTI-SKID LIGHT ILLUMINATED. TROUBLESHOT TRANSDUCER. ALL VOLTAGES AND OHMS READ CORRECTLY. TROUBLESHOT WIRING AND CONNECTED ALL GOOD. TROUBLESHOT CONTROL BOX, BY SLAVING IN KNOWN GOOD CONTROL BOX. ANNUNCIATOR EXTINGUISHED, RECONNECTED OLD CONTROL BOX, LIGHT REMAINED EXTINGUISHED. ALL TEST GOOD, CLEANED ALL CONNECTORS, TAXIED AIRCRAFT AT LOW AND HIGH SPEED.

ATA 3241

Part: CONTROL BOX — DEFECTIVE (ANTI-SKID SYS) · airframe 4,485 hrs · 3,405 cycles

ANTI-SKID LIGHT ILLUMINATED DURING TAXI-OUT. AFTER TEST, LIGHT WENT OUT AFTER 6 SECONDS. AFTER RESET C/B, LIGHT WENT OUT AFTER 6 SEC, LIGHT RE-ILLUMINATED BOTH TIMES AFTER BRAKE APPLICATION, WITH LIGHT ILLUMINATED.; STEP ON RIGHT BRAKE ONLY LT GOES OUT, ON LEFT BRAKE LT STAYS ON. REMOVED AND REPLACED ANTI-SKID CONTROL BOX, OPS CHECK GOOD.

ATA 1430

Part: BOLT — BENT (ELEVATOR CONTROL)

DURING PHASE 5 INSP, NOTICED CORROSION ON PN 62610401, IDLER ASSY(ELEVATOR CONTROL SYS), THE -1 IDLER ASSY IS MADE OF STEEL AND HAS 2 EA ARM ASSY ATTACHED TO IT WHICH ARE ALUMINUM. THE ARMS HAD TO BE REMOVED FROM THE ASSY TO GAIN ACCESS TO AREA TO BE TREATED. THERE IS A TOTAL, 5 FASTENERS WHICH HOLED THE THREE PARTS TOGETHER, PN AN174-13A BOLTS. UPON DISASSEMBLY THE FASTENERS REMOVED WERE HI-LOKS PN HL64-8. MFG TECH SAID NO CALL OUT TO DEVIATE FROM THE AN174-13A BOLTS. ALL THE HI-LOKS REMOVED WERE BENT, COULD NOT DETERMINE IF BENT ON INSTALLATION OR STRESS DURING USE. INSTALLED WHAT THE IPC CALLED OUT AND TECH VERIFIED FROM THE BUILD PRINT. NOT PROBLEM WITH HOLE ALIGNMENT. PICTURES.

ATA 3233

Part: ACTUATOR — INOPERATIVE (MLG) · airframe 3,072 hrs · 2,357 cycles

ON APPROACH WHEN SELECTING GEAR DOWN, NO RT MAIN GEAR GREEN LIGHT ILLUMINATED NOSE AND LEFT MAIN NORMAL. TOWER STATED RIGHT GEAR COCKED AND GPWS ' TOO LOW GEAR' DURING FLYBY. ALL CB'S OK. AUX GEAR HANDLE PULLED AND WHEN A/C YAWED RT MAIN LIGHT ILLUMINATED. - REMOVED AND REPLACED RH MLG SIDE BRACE ACTUATOR IAW 650 MM CHAPTER 32-30-04. OPS CHECK AND LEAK CHECK GOOD.

ATA 2432

Part: CONNECTOR — DAMAGED (SENSOR)

CONNECTOR PINS RECESSES EXCESSIVELY INTO HOUSING OF CONNECTOR. FOUND DURING SCHEDULES INSPECTION OF BATTERY. PROBABLE CAUSE IS IMPROPER ASSEMBLY OF CONNECTOR DURING MANUFACTURE (BUILD-UP) OF SENSOR ASSEMBLY. RECOMMEND MANUFACTURER (SAFT) TIGHTEN THEIR QUALITY ASSURANCE PROCEDURES.

ATA 3242

Part: BRAKE — DAMAGED (MLG BRAKE)

DURING AN INSPECTION, FOUND A 3 INCH AND A 2 INCH SECTION OF FRICTION MATERIAL MISSING FROM THE SAME DISC. ALL OTHER DISCS WERE SERVICEABLE AND THE BRAKE ASSY HAD NORMAL WEAR. SUBMITTER RECOMMENDED BETTER MATERIALS OF PROCEDURES FOR BONDING OF FRICTION MATERIALS. (X)