N682QS
Registered owner: NETJETS SALES INC, OK (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| NETJETS AVIATION, INC. (DXTA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
CABIN NOT PRESSURIZING. ON TAKEOFF, WHEN TAKEOFF POWER WAS APPLIED, CREW NOTICED A DEMONSTRATABLE BUMP IN PRESSURIZATION. IN THE CLIMB, CREW NOTICED CABIN PRESSURIZATION WAS CLIMBING OFF SCHEDULE. CABIN ALTITUDE CLIMBED AS AIRCRAFT DID. CREW STOPPED CABIN ALTITUDE FROM CLIMBING ABOVE 10,000 FEET. MASKS NEVER DEPLOYED. EMERGENCY WAS NOT DECLARED. WE DID NOT LAND OVERWEIGHT. CORRECTIVE ACTION: FOUND DUCTING IN TAIL CONE AREA LOOSE. SECURED PER CITATION 560XL AMM 21-21-00, / LEAK CHECK AND FUNCTIONAL CHECK GOOD.
UPON RAISING THE LANDING GEAR, THE RED UNLOCK LIGHT STAYED ILLUMINATED AND THE HYD PRESS LIGHT STAYED ILLUMINATED. LOWERED THE GEAR, ALL THREE GREEN LIGHTS ILLUMINATED. LANDED SAFELY. CORRECTIVE ACTION: REMOVED ICE FROM MAIN UNLOCK ROLLERS. OPS CHECK GOOD. IAW CE560XL AMM 32-01-00
MAIN DOOR: MAIN ENTRANCE DOOR IS HARD TO CLOSE. TOP SECTION OF THE DOOR HITS THE AIRFRAME WHEN CLOSING. FROM OUTSIDE WHEN DOOR IS CLOSED AND LATCHED, THERE IS NO GAP ON THE FORWARD SIDE OF THE DOOR, IT'S METAL TO METAL. THE AFT SIDE OF THE DOOR HAS A NICE GAP. CORRECTIVE ACTION: OPS CHECK GOOD. NO DEFECTS NOTED. IAW CE560XL AMM 52-10-00
EMERG EXIT SIGN/LIGHT: THE INTERIOR EMERGENCY LIGHTS CHECK NORMAL WITH BATTERY SWITCH ON. WHEN TURNING THE BATTERY SWITCH TO OFF AND EMER LIGHT SWITCH STILL ON, THE AFT EXIT SIGNS ARE EXTREMELY DIM. CORRECTIVE ACTION; REPLACED DEFECTIVE AFT EMERGENCY BATTERY PACK REF. CE-560XLS AMM 33-50-01. OPS CHECK GOOD.
EMERG EXIT SIGN/LIGHT: WITH THE BATTERY SWITCH ON AND EMERGENCY LIGHT SWITCH TO ON, ALL INTERIOR EMERGENCY LIGHTS CHECK NORMAL. WHEN TURNING THE BATTERY SWITCH TO OFF AND EMERGENCY LIGHT SWITCH STILL ON, THE 3 AFT EXIT SIGNS DO NOT ILLUMINATE. CORRECTIVE ACTION: CHARGED BATTERIES WITH DC POWER FOR 2 HOURS. PERFORMED EMERGENCY LIGHT SYSYEM OPERATION CHECK AND FOUND ALL LIGHT TO BE WORKING AS STATED IN THE AMM, WORK DONE IAW CE560 AMM 33-50-00,
CABIN EMERG LIGHT: SEAT 10 EMER LIGHT INOP. FOUND SEAT 10 EMERGENCY - READING LIGHT LAMP LOOSE IN SOCKET. REINSTALLED LAMP, OPS CHECK GOOD IAW CE560XL AMM 33-50-03, AS REQUIRED.
NLG INDICATOR LIGHT: ON TAKE OFF NOSE GEAR WOULD NOT RETRACT. QRH DONE. NOISE LEVELS CONFIRMED NOT RETRACTED. LANDING UNDER WEIGHT. JACKED AIRCRAFT AND PERFORMED SEVERAL CYCLES WITH NO ISSUES. VERIFIED THE NLG UP LOCK SWITCH PLUNGER IS MAKING CONTACT AND OVER TRAVEL MEASUREMENT IS GOOD. COOLED SWITCH AND UPLOCK ACTUATOR SEPARATELY WITH NO ISSUES, RETRACTED THE GEAR AND DID THE FREE FALL OF THE NLG ONLY AND NLG RETRACTED LIKE NORMAL WHEN HYDRAULICS WERE TURNED BACK ON. CHECKED CONTINUITY OF NOSE GEAR UPLOCK SWITCH FROM WHEEL WELL CONNECTOR PN001 WHILE TAPPING ON SWITCH AND FLEXING WIRE BUNDLE. NO FAULTS FOUND. NOSE GEAR PARALLEL CIRCUIT CHECKED GOOD. UPLOCK SWITCH RIG CHECKED GOOD WITH 0.095" OVER TRAVEL. PERFORMED SEVERAL MORE GEAR CYCLES WITH NO ISSUES, VERIFIED NLG STRUT EXTENSION IS WITH LIMITS, VERIFIED BOTH RT & LT MLG UP LOCK SWITCHES OVER TRAVEL IN MORE THAN 0.03". BROKE OUT EACH GEAR INDIVIDUALLY WITH NO ISSUES NOTED. OPS CHECKS GOOD OF WORK PERFORMED. NO ISSUES NOTED WHILE CYCLING GEAR, NO FURTHER ACTION REQUIRED. WORK IAW 32-30-05. VERIFIED GEAR OPS AND FREE FALL CHECK, OPS CHECK GOOD. REMOVED NLG UP LOCK ACTUATOR, TRANSFERRED UNIONS AND ELBOW FIITINGS WITH NEW ORINGS TO THE NEW ACTUATOR. DISASSEMBLED ACTUATOR AND INSTALLED NEW SPRING & PIN ONTO NEW ACTUATOR. INSTALLED ACTUATOR. VERIFIED GEAR OPS AND FREE FALL CHECK, OPS CHECK GOOD. UPLOCK ACTUATOR OPS CHECKS GOOD. SAFETIED AS REQUIRED. DOWN JACKED AIRCRAFT AND CLOSED JACK ACCESS PANEL. WORK IAW 32-30-05. ORIGINAL SUBMISSION DATE: 11-27-2023.
IN CLIMB THROUGH 10,000 RECEIVED RIGHT IN CLIMB THROUGH 10,000 RECEIVED RIGHT ENGINE FIRE LIGHT, UPON PULLING POWER BACK OUT OF CLIMB DETENT TO CRUISE FIRE LIGHT EXTINGUISHED. AFTER APPLYING CLIMB POWER AGAIN, RT ENGINE FIRE LIGHT CAME BACK ON. ACCOMPLISHED INFLT ENGINE FIRE QRC & LIGHT EXTINGUISHED AFTER PULLING BACK POWER ON RT ENGINE. FIRE LIGHT, UPON PULLING POWER BACK OUT OF CLIMB DETENT TO CRUISE LIGHT EXTINGUISHED. REMOVED DAMAGE BLEED AIR TUBE SEALS & INSTALLED CUSTOMER SUPPLIED NEW SEALS PN W932-24F NSN ON RH BLEED AIR TUBE. IAW CE-560XL AMM 36-11-00. PERFOREMD ENGINE RUN ON RH ENGINE FOR LEAK CHECK. OPS CHECK IS GOOD 2 TECHS REQUIRED. IAW AMM 71-00-00. 36-11-00. NO DEFECTS NOTED
LEFT ENGINE N1 INDICATION: SHORTLY AFTER ROTATION, THE LEFT ENGINE ITT WENT INTO THE RED. I HAD TO PULL POWER BACK LESS THAN CRUISE TO GET IT OUT OF THE RED DURING CLIMB OUT. MOVED THE POWER LEVER BACK UP TO CLIMB POWER AND THE ITT WENT BACK INTO THE RED SHOWING 747° FOR A FEW SECONDS BEFORE I PULL THE POWER BACK. ABOUT A MINUTE AFTER THAT, THE LEFT EEC MANUAL ANNUNCIATOR CAME ON. FOLLOWED THE CHECKLIST AND LIGHT WENT OUT AND SEEM NORMAL FOR A FEW MINUTES. THEN THE LT ENGINE POWER DID AN UNCOMMANDED REDUCTION, AND THEN AN UNCOMMANDED ACCELERATION BACK UP TO THE POWER SETTING HAD IT AT. BOTH ECS FAULT LIGHTS IN THE HELLHOLE ARE TRIGGERED. LNSTALLED OVERHAULED LT ENG ON AIRCRAFT. INSTALLED TIMES: TSN: 12,482.7, CSN: 9,559, TSO: 0.0, CSO: 0. MM 71â¢00-03. LNSTALLED STARTER GENR, REF. MM 80-10-00. LNSTALLED AC ALTERNATOR, MM 24-20-0 I. DRAIN LINES. CONNECTED MAIN AND MOTIVE FLOW FUEL LINES. CONNECTED & SUPPLY & RDLLM HYD LINES. CONNECTED & RIGGED THROTTLE CABLE. CONNECTED PYLON ELEC CONNECTIONS. CONNECTED HP & LP BLEED LINES USING NEW SEALS. REF. MM 71--00-02 & 71--00-01. REPLACED ENG OIL FILTER. SERVICED LT ENGINE. CONNECTED BATTERY, CLEARED INLETS & EXHAUST, REMOVED RED GEAR. APPLIED PRIOR TO AIRCRAFT VIA APU. OPENED FIREWALL SHUTOFF VALVES. C/W ENG DEPRESERVATION. REF. EMM 72-00-00. C/W MOTORING OF THE LT ENGINE. SERVICED ENGINE C/W LT ENG GROUND NM. NO DEFECTS NOTED. MAX JTT DURING START 542 C. C/W SATISFACTORY FUEL & OIL LEAK CHECK, NO LEAKS NOTED. C/W BLEED AIR LEAK CHECK, NO LEAKS NOTED C/W SATISFACTORY ENGINE PERFORMANCE RUNS, NO DEFECTS NOTED. MINIMUM NI OF THE DAY 89.8. T/O NI FOR LH ENGINE 91.0. C/W SATISFACTORY LH STARTER DISENGAGE CHECK. C/W SATISFACTORY LT ENG LIMITATIONS CHECK. C/W SATISFACTORY LT ENG ACCELERATION CHECKS- FLIGHT IDLE & GROUND IDLE. C/W SATISFACTORY DECELERATION CHECKS. C/W SATISFACTORY LT ENG ELECTRICAL GENERATION CHECKS. REF. MM 71--00-04. ORIG SUBMISSION DATE: 9/5/2023.
DURING INSPECTION FOUND THE CARGO DOOR FWD HINGE AND U CHANNEL CRACKED.
MAIN DOOR: AFTER LANDING THE MAIN CABIN DOOR WOULD NOT OPEN, WE SHUT THE APU AIR OFF AND STILL WOULD NOT OPEN. AFTER SEVERAL TRIES ,WHEN CLOSING THE DOOR WE GET A VENT DOOR AND DOOR HANDLE LIGHT ON THE SIX PACK LIGHTS BY THE DOOR. DOOR SEAL DOESN'T WANT TO DEFLATE. REMOVED ACOUSTIC DOOR SEAL SOLENOID VALVE P/N 5035-00-1 S/N 10741, REPLACED WITH NEW PART. PERFORMED OPERATIONAL C:HEDCS WITH NO DISCREPANCIES NOTED. ALL WORK DONE WITH REFERENCE TO AMM-52-10-04. RETURNED AIRCRAFT BACK ID ORIGINAL CONFIGURATION
FLOOR EMERG EXIT LIGHT: LEFT FORWARD DROP DOWN AISLE LIGHTS FROM SEAT 5 TO MAIN CABIN DOOR OUT .THESE ARE EMERGENCY LIGHTS // SIGNOFF/ REMOVED AND REPLACED LEFT FWD DROP DOWN ALSLE LED STRIP IA W CE-560XL MM 33-50-00. NO FURTHER DEFECTS NOTED.
MAIN DOOR: MAIN DOOR IS VERY DIFFICULT TO CLOSE. THE PINS SEEM MISALIGNED AND IT IS VERY DIFFICULT TO MOVE THE HANDLE TOWARDS TO THE CLOSED POSITION. //SIGNOFF// ADJUSTED MAIN ENTRY DOOR AS REQUIRED IA W 560XLS AMM 52-10-00. PERFORMED CABIN DOOR ASSEMBLY DETAILED INSPECTION REF: 560XLS AMM TASK 52-10-00-2200. PERFORMED CABIN DOOR SEAL GVI REF: 560XLS TASK 52-10-00-2100 OPS CHECK GOOD, NO DEFECTS NOTED. DOOR LOCKS AND UNLOCKS SMOOTHLY FROM INSIDE OR OUTSIDE THE AIRCRAFT.
LEFT ENGINE ENGINE LOW POWER: CLIMBING THROUGH APPROXIMATELY FL 190 WITH THROTTLES IN CLIMB DETENTS (ABOUT 92% N1), THE LEFT ENGINE POWER SUDDENLY DROPPED TO ABOUT 80% N1. (THE DECELERATION RATE WAS AS IF THE THROTTLE HAD BEEN QUICKLY BROUGHT TO IDLE). AFTER ABOUT ONE SECOND, POWER ROSE BACK WHERE IT HAD BEEN BEFORE. HOWEVER, THE N1 FLUCTUATED ABOUT 2% UP AND DOWN FOR SEVERAL SECONDS. OTHER ENGINE INDICATIONS WERE NOT OBSERVED AS WE WERE FOCUSED ON THE N1. NO ANNUNCIATORS ILLUMINATED. ENG DATA SCAN BUTTON WAS PRESSED APPROXIMATELY 5 MINUTES AFTER EVENT. WE DIVERTED AND ENGINE APPEARED TO OPERATE NORMALLY THROUGHOUT REMAINDER OF FLIGHT. // SIGNOFF// ACCOMPLISHED THE DCU DOWNLOAD OF THE LH AND RH ENGINES AND SUBMITTED AS REQUIRED. GAINED ACCESS AND PERFORMED AN INSPECTION OF THE TO, TL/FCU, AND TL SENSORS WITH NO DEFECTED NOTED. INTERROGATED THE DOWNLOAD WITH NO CURRENT FAULTS NOTED. ALSO NOTED NO FAULT INDICATIONS WITHIN THE DOLLS EYES, CLOSED ACCESS AS REQUIRED. PREPPED AND ACCOMPLISHED REQUESTED LEFT HAND ENGINE RUNS AT VARIOUS POWER SETTINGS AND LENGTHS OF TIME WITH NO DUPLICATION OF POWER LOSS. ACCOMPLISHED AN ADD LTLONAL DOWNLOAD WITH NO ADDITIONAL EVENTS NOTED. VISUALLY INSPECTED DOLLS EYES WITH NO TRIPPED INDICATORS. PWC ADVISED NO ADDITIONAL RECOMMENDATIONS UP TO REPLACEMENT OF THE RIGHT HAND ENGINE EEC. REMOVED THE UNSERVICEABLE LH ENGINE EEC (P/N: 1004855-1-002 / 30J2659-02 5/N: 04127489) AND INSTALLED AN OVERHAULED SERVICEABLE LH ENGINE EEC (P/N: 1004855-2-002 / 30J2659-03 S/N: 07043676). PERFORMED FOLLOW ON CHECKS WITH SATISFACTORY RESULTS. MAINTENANCE ACCOMPLISHED IAW PW545B EMM CH. 73-20-03 , 77-40-01, 77-20-01, AND 73-20-01 AND 71-00-00.
AFTER TAKE OFF AND DURING CLIMB OUT AFTER GEAR AND FLAP RETRACTION THE HYD PRESS ANNUNCIATOR ILLUMINARED. AS PIC AFTER IDENTIFYING THE ISSUE AND CANCELLING THE CAUTION LIGHT, I CALLED FOR THE APPROPRIATE CHECKLIST. I THEN TRANFERRED THE CONTROLS TO THE F/O AND REFERENCED THE HYD PRESS ANNUNCIATOR ILLUMINATION IN FLIGHT CHECKLIST AND AS PART OF THE CHECKLIST THE HYDRAULIC CONTROL CIRCUIT BREAKER WAS PULLED AND THE HYD PRESS ANNUNCIATION EXTINGUISHED. AS PER THE CHECKLIST WE RESET THE HYDRAULIC CONTROL CIRCUIT BREAKER AND THE HYD PRESS ANNUNCIATOR RE-ILLUMINATED IMMEDIATELY PRIOR TO EXECUTING THE APPROACH IN PHL. AFTER TRANSFERRING THE CONTROLS BACK TO ME PRIOR TO THE APPROACH, WE CONFIGURED FOR LANDING AND THE HYD PRESS ANNUNCIATIOR EXTINGUISHED PRIOR TO LANDING. ALL HYDRAULIC DEPENDENT SUBSYSTEMS OPERATED NORMAL DURING THE FLIGHT. AFTER LANDUNG THE HYD PRESS ANNUNCITOR DID NOT RE-ILLUMINATE. REPOSITIONED AIRCRAFT INTO HANGER, CONNECTED HYDRAULIC MULE. PERFORMED OPERATIONAL CHECKS OF FLAPS, SPEED BRAKES AND HORIZONTAL STAB, NO DEFECTS NOTED. CONTACTED MCC WITH FINDINGS, WITH NO PRIOR HISTORY THEY ELECTED TO HAVE US REPLACE HYDRAULIC PRESSURE SWITCH. REMOVED AND REPLACED HYDRAULIC PRESSURE SWITCH. PLACED AIRCRAFT ON JACKS AND PERFORMED SEVERAL GEAR SWINGS WITH NO FAULTS. DOWN JACKED AIRCRAFT. ALL WORK DONE, IAW CE-560XL M/M 29-11-06. OPERATIONS AND LEAK CHECK GOOD.
MAIN CABIN DOOR STICKS AND IS DIFFICULT TO OPEN FROM BOTH INSIDE AND OUTSIDE THE CABIN. THE DOOR REQUIRES EXCESSIVE FORCE TO OPEN AFTER BEING UNLOCKED. SEEMS TO BE OUT OF ALLIGNMENT AND PINCHING ALONG THE OUTER FRAME. INSPECTED DOOR HINGE WITH NO DEFECTS FOUND. POWERED UP AIRCRAFT AND STARTED APU. OPERATED MED AND FOUND DOOR SEAL NO DEFLATING CORRECTLY. INSPECTED DEFLATION VALVE AND FOUND TO BE STICKING. REPLACED MED SEAL VALVE WITH A NEW UNIT, IAW CE560XL AMM 52-10-04. OPERATIONS AND LEAK CHECKS GOOD.
PASSENGER DOOR WILL NOT OPEN MOVE THE HANDLE TO THE DOWN OPEN POSITION IN THE DOOR WOULD STILL NOT OPEN. THEN MOVE THE HANDLE TO THE FULL UP POSITION THEN ALL THE WAY BACK DOWN TO THE OPEN POSITION AND THE DOOR STILL WOULDN'T OPEN. THEN PUSH THE PRE-CATCH BUTTON AND THEN WAS ABLE TO OPEN THE DOOR THEN PUSH THE PRE-CATCH BUTTON OUT AND LOCK THE DOOR AND TRIED TO RE-OPEN THE DOOR BUT IT WOULDN'T OPEN AGAIN AFTER TRYING THE SAME PROCEDURE I TRIED THE FIRST TIME TO OPEN THE DOOR. FOUND ON PRE-FLIGHT. CLEANED/LUBRICATED/CHECK/ADJUSTED AIRCRAFT MED, IAW TEXTRON AVIATION INC. MODEL 560XL MAINTENANCE MANUAL (REV 46) 52-10-01 (REV 44) DOOR HANDLE AND LINKAGES MAINTENANCE PRACTICES. PERFORMED SEVERAL CLOSING/OPENING OPERATIONAL CHECKS OF AIRCRAFT MED SATISFACTORY.
MAIN CABIN DOOR WILL NOT OPEN NORMALLY. AFTER UNLOCKING, ATTEMPTED TO OPEN THE DOOR BUT WHEN HANDLE WAS AT 6 O`CLOCK POSITION AND PULLED, THE DOOR WOULD NOT OPEN. ATTEMPTED SEVERAL TIMES WITH SAME RESULT. THE DOOR HANDLE IS STIFF BOTH CLOSING AND OPENING, INSIDE AND OUT. THE DOOR DID OPEN USING THE PRECATCH. CORRECTIVE ACTION: OPERATED CABIN DOOR MULTIPLE TIMES AND VERIFIED SQUAWK. MEASURED PRECATCH PLUNGER RETRACTION INTO HOUSING AND VERIFIED PLUNGER IS FLUSH WITH HOUSING WITH PRECATCH BUTTON PUSHED IN, IAW 560XL MM 52-10-00. NOTICED WITH CLOSING CABIN DOOR, DOOR HAD EXCESSIVE TENSION CAUSING DOOR TO RETRACT HALFWAY AUTOMATICALLY WHEN INITIALLY CLOSING THE DOOR. DOOR STEPS AND OPERATED DOOR. DOOR OPERATED CORRECTLY AND PRECATCH WORKS GOOD. WORK DONE IAW 560XL MM52-10-03.
MAIN CABIN DOOR HANDLE IS VERY HARD TO OPEN AND CLOSE. PERFORMED OPERATION OF THE MAIN CABIN DOOR HANDLE AND VERIFIED IT IS VERY HARD TO OPEN AND CLOSE. INSPECTED MAIN DOOR HANDLE FROM THE INSIDE AND OUTSIDE FOR DAMAGE. NO DAMAGE FOUND. REMOVED MAIN CABIN DOOR TOP FOLDING STEPS. REMOVED MAIN CABIN DOOR FIX STEPS ASSEMBLY. INSPECTED MAIN CABIN DOOR HANDLE AND LINAGES. CLEANED AND LUBED DOOR HANDLE AND LINKAGES. INSPECTED ALL MAIN CABIN DOOR GUIDE BLOCKS, LATCHING PINS AND PIN SOCKETS. PERFORMED ADJUSTMENT OF THE FWD MIDDLE AND AFT MIDDLE PIC SOCKETS SEVERAL TIMES. REINSTALLED MAIN CABIN DOOR FIX STEPS ASSEMBLY AND TOP FOLDING STEPS. ALL WORK PERFORMED IAW CE-560XLS MM 52-10-01.
REPAIR CRACKED FRAMES IN MAIN ENTRY DOOR. ROUTED OUT CRACKED AREAS OF THE MAIN ENTRY DOOR FWD AND AFT FRAME. INSTALLED FILLER AND DOUBLER ON THE FWD AND AFT FRAMES IAW AQRD ERO-966156 REV IR DATED MAR 26 2020.
NLG INDICATOR LIGHT BURNT OUT - DURING APPROACH WITH GEAR HANDLE DOWN WE NOTICED WE DIDN'T HAVE GREEN NOSE GEAR DOWN AND LOCKED INDICATION. WE INITIATED A GO AROUND, COMPLETED LANDING GEAR WILL NOT EXTEND QRH EMERGENCY CHECKLIST AND USED GEAR BLOW DOWN PROCEDURES. STILL NOT GETTING GREEN INDICATIONS. USING LDG GEAR ROTARY TEST WE GET HORN, RED UNLOCK LIGHTS, GREEN LH AND RH MLGS GREEN LIGHTS BUT NO NOSE GEAR LIGHTS. REMOVED AND REPLACED LANDING GEAR CONTROL LH,RH,NOSE AND UNLOCK INDICTOR LAMPS WITH NEW IAW AMM 31-13-00. RESET/SERVICED BLOW DOWN BOTTLE AND PERFORMED SEVERAL GEAR SWINGS INCLUDING HYDRAULIC SYSTEM BLEED IAW AMM 32-01-00.
ENGINE FIRE INDICATION ON RIGHT ENGINE WHILE CLIMBING OUT OF APPROXIMATELY FL190. WHEN THROTTLE WAS BROUGHT TO IDLE, THE FIRE LIGHT EXTINGUISHED IN ABOUT 3 SECONDS. AFTER LANDING, CFR CREWS COULD NOT IDENTIFY ANY HOT SPOTS WITH FLIR EQUIPMENT. COWLING FELT COOL TO THE TOUCH. THERE WERE NO OTHER PHYSICAL SIGNS OF FIRE ANYWHERE ON THE ENGINE COWLING, EXHAUST OR PYLON. ****CORRECTIVE ACTION**** ARRIVED AT AIRCRAFT INSPECTED COWLING NO SIGNS OF HEAT DAMAGE. OPENED COWLING INSPECTED LOWER FIRE LOOP NO DEFECTS NOTED INSPECTED ALTERNATOR NO DEFECT NOTED. REMOVED UPPER COWL AND FOUND WIGGINS FITTING SEAL JUST ABOVE PYLON DEFORMED AND SLIGHT DESCOLORATION ON COWLING. RAN ENGINE AND FOUND SIGNIFICANT LEAK FROM FITTING. REMOVED BLEED LINE AND REPLACED SEALS AS REQUIRED REF AMM CH36-11-00 C/W LEAK CHECKS NOTED NOTED. REINSTALLED UPPER AND LOWER COWLS AS REQUIRED.
DURING INSPECTION, FOUND LEFT AND RIGHT ELEVATOR TORQUE TUBES CORRODED. REMOVED ELEVATORS AND REPLACED TORQUE TUBES. PAINTED AND BALANCE ELEVATORS. REINSTALLED ELEVATORS ON AIRCRAFT.
LANDING GEAR WOULD NOT RETRACT. GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. RAN APPROPRIATE CHECKLIST & RETURNED FOR LANDING.
LANDING GEAR WOULD NOT RETRACT. GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. RAN APPROPRIATE CHECKLIST & RETURNED FOR LANDING. REMOVED NON-FUNCTIONING LG CONTROL HANDLE, PN 9912550-1 SN 025 & INSTALLED A OVERHAULED LG CONTROL HANDLE, PN 049801-001 SN H5464. CONDUCTED TEN COMPLETE GEAR SWINGS WITH NO FAULTS NOTED. LOWERED ACFT OFF JACKS & SERVICED HYD AS NEEDED. ALL WORK CONDUCTED IAW THE AMM 32-30-00, 32-30-01 & 12-12-01.
LT INBD FLAP INBD RIB CRACKED AT WS 64.073. COMPLETED REPAIR OF WING T/E RIB CRACKS IAW SRM 57-60-00 FOR LT INBD FLAP WELL RIB T/E.
RT WING INBD FLAP, INBD T/E RIB IS CRACKED AT WS 64.073. COMPLIED WITH WING T/E RIB CRACK REPAIR IAW SRM 57-60-00 FOR RT INBD FLAP WELL RIB T/E.
MAIN CABIN DOOR STRUCTURE CRACKED UNDER INTERIOR DOOR HANDLE. REMOVED IDENTIFIED DAMAGED AREA AND COMPLETED WEB REPAIR IAW SRM 52-10-00.
DURING A SCHEDULED INSPECTION, FOUND THE MAIN CABIN DOOR HINGE (FUSELAGE SIDE) TO BE CORRODED BEYOND LIMITS FROM THE EDGE OF THE PART TO THE FIRST FASTENER ATTACH HOLE. THIS CONDITION HAS ALSO BEEN REPORTED TO UNDER SCR 624006.
AFTER TAKEOFF NLG DID NOT LOCK IN UP POSITION . FOLLOWED BY ASSOCIATED FLASHING HYD PRESS & STAB MISCOMP ANNUNCIATORS. INSPECTED ALL 3 MLG UPLOCK SWITCHES. FOUND LT MLG UPLOCK SWITCH BROKEN. WITH MLG UP, TECH PUSH ON SWITCH & UNLOCK LIGHT & OTHER INDICATIONS WENT TO NORMAL. REMOVED INOP LT MLG UPLOCK SWITCH. INSTALLED NEW LT MLG UPLOCK SWITCH. ADJUSTED LT MLG UPLOCK SWITCH AS REQUIRED. PERFORMED SEVERAL MLG CYCLES. OPS CHECKED GOOD. PER AMM 32-30-05. REMOVED NLG ACTUATOR. INSTALLED INSPECTED NLG ACTUATOR. PERFORMED NLG FUNCTIONAL TEST & CHECKED EXTENSTION & RETRACTION NO DEFECTS NOTED. PERFORMED NLG FREEFALL TEST, NO DEFECTS NOTED. OPERATED MLG SEVERAL CYCLES. NO DEFECTS NOTED. WORK DONE PER AMM 32-01-00.