N930HA

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,418 hrs · 77,460 cycles

CABIN EMERGENCY EXIT LIGHT AT AIR STAIR DOOR HAS NUMEROUS BULBS THAT WILL NOT ILLUMINATE. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,170 hrs · 77,174 cycles

ROW 6DF EMERGENCY LIGHT INOPERATIVE. R & R THE BULB.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,167 hrs · 77,168 cycles

EMERGENCY LIGHTS DISARM CAUTION LIGHT INOPERATIVE, REPLACED THE LAMP. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,997 hrs · 76,939 cycles

CEILING EMERGENCY LT AT ROW 2 INOPERATIVE. R & R THE BULB.

Part: ROD END — BROKEN (NR 1 MLG) · airframe 67,947 hrs · 76,905 cycles

LOUD BANG HEARD WHEN GEAR SELECTED DOWN FROM MAIN GEARS. MLG GEAR DOORS SLOW TO CLOSE. INDICATIONS NORMAL. FOUND NR 1 MLG RETRACTION ACTUATOR ROD END BROKEN. REMOVED AND REPLACED THE ROD END IAW CMM 32-30-01, AMM 32-30-11 STEP THREE. ATTACHED ROD END TO DRAG STRUT IAW AMM 32.30.11, STEP 3, REF TO HA 300, SEQ 20 FOR OPS CK.

Part: VALVE — INOPERATIVE (DE ICE BOOT) · airframe 67,114 hrs · 75,909 cycles

RT OUTER DEICE BOOT DOES NOT INDICATE INFLATION AND DOES NOT INFLATE IN MANUAL OR AUTO. NR 4 RT OTBD DISTRIBUTOR VALVE AND OTBD PRESSURE SWITCH IAW MM 30-10-16 AND PB 30-3. OPS CHECKED GOOD.

Part: SELECTOR SWITCH — INOPERATIVE (FEATHERING) · airframe 66,943 hrs · 75,694 cycles

DURING AUTOFEATHER TEST, NR 2 PROP WILL NOT FEATHER. RPM DROPS FROM 650 TO 590. ALL OTHER PARAMETERS OK. R & R RELAYS 6121-K4, K2 AND K10. SLAVED IN NR 2 TSEU, NO FIX. ORIGINAL TSEU REINSTALLED. R & R NR 2 PCU IAW 61-10-10R. NO FIX. R & R AUTOFEATHER SELECT SWITCH. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,933 hrs · 75,682 cycles

EMERGENCY LIGHT ON FORWARD RT SIDE OF FUSELAGE IS INOPERATIVE. R & R BULB FOR RT FORWARD EGRESS LIGHT IAW MM 33-51-05. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 66,904 hrs · 75,646 cycles

BULBS BURNED AT EMERGENCY EXIT OVERHEAD PANEL. R & R BULBS AT EMERGENCY OVERHEAD PANEL. OPS CHECKED GOOD.

Part: DOWNLOCK SENSOR — MALFUNCTIONED (NLG) · airframe 66,792 hrs · 75,516 cycles

ON FINAL WITH GEAR EXTENDED, APPROXIMATELY 500 FEET BEFORE TOUCHDOWN, PERFORMED ALTERNATE EXTENSION, ALL INDICATIONS NORMAL AFTER LANDING ROLL OUT. NLG RED LIGHT ILLUMINATED, THEN WHEN OUT. LOCKED NLG. NO FURTHER ISSUES. R & R NLG DOWNLOCK PROXIMITY SWITCH IAW MM 32-33-30. SYSTEM OPS CHECKED GOOD.

Part: SKIN — DELAMINATED (NLG DOOR) · airframe 66,741 hrs · 75,452 cycles

WOW CAUTION LIGHT AND NOSE DOOR OPEN LIGHT ILLUMINATED AFTER GEAR RETRACTION, CYCLED GEAR AND BOTH LIGHTS REMAINED ILLUMINATED. MAINTENANCE FOUND RT AFT NOSE DOOR DELAMINATED.

Part: WARNING LIGHT — FALSE ACTIVATION (ELEVATOR) · airframe 66,741 hrs · 75,452 cycles

ELEVATOR HORN HEAT CAUTION LIGHT ILLUMINATED ON ROTATION, WOW CAUTION LIGHT ILLUMINATED AFTER GEAR SELECTED UP, NOSE GEAR DOOR CAUTION LIGHT ILLUMINATED AFTER GEAR RETRACTED. SELF CLEARED AFTER CHECK LIST COMPLIED WITH.

Part: SWITCH — CONTAMINATED (GYRO PANEL) · airframe 66,726 hrs · 75,429 cycles

SMOKE EMANATED FROM THE SAHS SWITCH. FOUND GYRO NR 1 SWITCH ON GYRO PANEL SCORCHED 3420-SW1. CLEANED DEBRIS FROM OTHER SWITCHES ON PANEL.

Part: UNKNOWN — ODOR (CABIN) · airframe 66,517 hrs · 75,178 cycles

ODOR OF JET FUEL IN COCKPIT WITH APU RUNNING. PULLED AND COLLARED CIRCUIT BREAKER N-8 ON RT MAIN BUS, AUXILIARY POWER UNIT.

Part: PANEL — MALFUNCTIONED (FUEL PRESSURE) · airframe 66,459 hrs · 75,104 cycles

NR 1 ENGINE FUEL PRESSURE CAUTION LIGHT ILLUMINATED WHILE TAKING RUNWAY. REMAINED ON UNTIL ENGINE SHUTDOWN. R & R CAUTION LIGHT PANEL IAW 33-12-01. GROUND RAN AND TAXIIED WITH CREW. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,911 hrs · 74,424 cycles

F/A EMERGENCY LIGHT SWITCH GREEN LIGHT IS OUT. R & R BULB IN GREEN LIGHT SWITCH. OPS CHECKED GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 65,664 hrs · 74,129 cycles

RT FORWARD FUSELAGE EMERGENCY LIGHT DIM. R & R FORWARD FUSELAGE EMERGENCY LIGHT BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,512 hrs · 73,943 cycles

2ND FLOOR EMERGENCY LIGHT IS INOPERATIVE. R & R BULB FOR 2ND EMERGENCY FLOOR PATH LIGHT. OPS CHECKED GOOD.

Part: HANDLE — MALFUNCTIONED (MLG) · airframe 64,661 hrs · 72,933 cycles

DURING FERRY FLIGHT WITH GEAR DOWN, NOSE GEAR CYCLED UP/DOWN SEVERAL TIMES WITH INDICATIONS FOLLOWING GEAR POSITION. ALTERNATE EXTENSION WAS REQUIRED TO MAKE A LANDING. R & R GEAR HANDLE DUE TO UNCOMMANDED GEAR RETRACTION. SWUNG GEAR, OPS CHECKED GOOD. OK FOR SERVICE AT THIS TIME.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE) · airframe 64,576 hrs · 72,825 cycles

AT 1500 AGL, SWITCHED FROM TOP TO NORMAL, NR 2 ENGINE TORQUE DROPPED TO ZERO. PROPELLER RPM A 1000. ITT BETWEEN 500 TO 600 DEGREES. PERFORMED EMERGENCY PROCEDURES FOR ENGINE SHUTDOWN. R & R NR 2 HMU AND FUEL PUMP IAW 73-20-01R. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,399 hrs · 72,615 cycles

FLOOR LEVEL AND CABIN SIDEWALL EMERGENCY LIGHTS FLICKERING WITH COCKPIT SWITCH IN THE OFF AND F/A SWITCH IN NORMAL WITH ENGINES SHUTDOWN ON APU POWER DURING PASSENGER DEPLANE. R & R EMERGENCY LIGHT BATTERY AND POWER SUPPLY AT POSITION PS4 IAW MM 33-51-00. OPS CHECKED GOOD. OK FOR SERVICE AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,381 hrs · 72,594 cycles

TWO EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 7 AND 8. R & R BULBS. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 64,162 hrs · 72,321 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROW 6. R & R 1 PIN IN CONNECTOR IAW MM 20-45-09. OPS CHECKED GOOD.

Part: ACTUATOR — MALFUNCTIONED (NR 2) · airframe 64,144 hrs · 72,298 cycles

AFTER TAKE OFF, SELECTED GEAR UP, RT MLG RED UNSAFE LIGHT ILLUMINATED, AMBER LIGHT ILLUMINATED ON LT MLG AND NLG. R & R NR 2 RETRACT ACTUATOR AND FITTING IAW MM32-30-11. OPS AND LEAKED CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,114 hrs · 72,259 cycles

EMERGENCY PATH LIGHT 4TH FROM FRONT INOPERATIVE. REPLACED THE LAMP, OPS CHECKED GOOD, OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,954 hrs · 72,059 cycles

FIFTH CABIN EMERGENCY LIGHT FROM REAR IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: UNKNOWN — SMOKE (CABIN & COCKPIT) · airframe 63,390 hrs · 71,388 cycles

CABIN AND FLIGHT DECK HAD SMOKE WITH BLEEDS ON, DISIPATED WITH BLEEDS OFF. ACFT WAS DIVERTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,390 hrs · 71,388 cycles

ROW 2 EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT BULB AT ROW 2.

Part: UNKNOWN — ODOR (CABIN) · airframe 63,347 hrs · 71,337 cycles

CREW REPORTED PETROLEUM ODOR, STARTED WHEN ACFT WAS IN STEEP DESCENT AND CLEARED BEFORE LANDING. R & R CONDENSER MIXER, HEAT EXCHANGER, IAW ACM. GROUND RAN, OPS CHECKED GOOD.

Part: LIGHT — DIM (BETA) · airframe 63,340 hrs · 71,328 cycles

RIGHT AFT, RIGHT FORWARD, LEFT AFT BETA LIGHTS DIMMER THAN REFERENCE LIGHT. REMOVED & REPLACED 3 BETA LIGHTS.

Part: INDICATOR — FAILED (COCKPIT) · airframe 63,082 hrs · 71,004 cycles

GPU HAD 3 VOLTAGE SPIKES. CREW SHUTOFF GROUNDPOWER. CIRCUIT BREAKER P-6 AND CIRCUIT BREAKER C-1 ON LT ESS AND SEC BUSSES FOUND TRIPPED WITH AN ELECTRICAL ODOR. R & R CABIN PRESSURE INDICATOR. RESET P6. OPS CHECKED GOOD IAW MM 21-30-03, RESET G1 CIRCUIT BREAKER. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,061 hrs · 70,980 cycles

ONE EMERGENCY LIGHT IS INOP AT ROW 1DF SIDEWALL. R & R BULB FOR SIDEWALL EMERGENCY LIGHT AT ROW 1DF. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 62,925 hrs · 70,816 cycles

ODOR IN FLIGHT DECK DURING DECENT. SELECTED BLEEDS OFF. ODOR DISIPATED, INSPECTED ACM. NO DEFECTS NOTED. GROUND RAN BOTH ENGINES WITH BOTH BLEEDS ON AND THEN ONE AT A TIME. NO ODOR NOTICED BY CREW OR MAINTENANCE ON FLIGHT DECK.

Part: UNKNOWN — SMOKE (CABIN/COCKPIT) · airframe 62,916 hrs · 70,807 cycles

DURING FLIGHT, OIL ODOR ENTERED THE CABIN AND FLIGHT DECK WITH ASSOCIATED SMOKEY HAZE IN THE CABIN. SWITCHED THE BLEEDS OFF AND ODOR AND SMOKE DISIPATED. INSPECTED BOTH ENGINES, INTAKES AND OIL LEVELS. GROUND RAN ACFT WITH BOTH ENGINE BLEEDS AND APU BLEEDS. NO SMOKE ODOR OR OTHER DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: SMOKE DETECTOR — ACTIVATED (LAVATORY) · airframe 62,752 hrs · 70,615 cycles

LAVATORY SMOKE DETECTOR SOUNDED DURING TAXI OUT. SELECTED ENGINE BLEEDS OFF DURING RETURN TO GATE AND LAVATORY ALARM STOPPED. GROUND RAN BOTH ENGINES AND APU. OPERATED BLEEDS ON FOR 15 MINUTES. NO SMOKE OR ODORS DETECTED. NO SMOKE ALARM SOUNDED.

Part: VALVE — FAILED (CABIN AIR) · airframe 62,621 hrs · 70,451 cycles

LIGHT SMOKE IN FLIGHT DECK, CABIN AND BAG BAY IN FLIGHT AT 19,000 FT COMPLIED WITH UNKNOWN SMOKE CHECKLIST, RECIRCULATION FAN AND BLEEDS SELECTED OFF. AFTER BLEEDS OFF, SMOKE DISSIPATED. R & R AIR SWITCHING VALVE IAW MM 72-30-00. GROUND RAN ACFT WITH BLEEDS ON. NO DEFECTS NOTED. NO SMOKE ODOR NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (NLG) · airframe 62,112 hrs · 69,830 cycles

ON ROLL OUT AFTER LANDING, NOSE GEAR INDICATED RED UNSAFE. ACFT WAS STOPPED ASAP AND RED INDICATION SELF CLEARED TO GREEN. DISCREPANCY WAS ASSOCIATED WITH WOW CAUTION LIGHT. CHECKED PSEU FOR FAULT CODES. NO CODES INVALID NOTED. CHECKED SENSOR GAP CLEARENCE. ALL CHECKED OK. INSPECTED NOSE LANDING GEAR WHEEL WELL STRUT AND ATTACHMENTS. NO DAMAGE NOTED. AS PRECAUTIONARY MEASURE, R & R PSEU. OPS CHECKED GOOD ON EXTENSION RETRACTION 6 CYCLES AND TAXI IAW 32-61-50.

Part: RADAR — FAILED (WX SYS) · airframe 61,856 hrs · 69,513 cycles

RADAR WILL NOT TEST OR PAINT GROUND. R & R WEATHER RADAR RT IAW MM 34-41-04 AND PB 34-18. OPS CHECKED GOOD.

Part: STRINGER — CORRODED (BS 240 S31R) · airframe 61,630 hrs · 69,229 cycles

STRINGER 31S HAS MINOR SURFACE CORROSION JUST AFT OF FRAME BS 240.50. BLENDED MINOR CORROSION IAW THE SRM 51-20-16,51-20-36.

Part: STRAP — CORRODED (BS 182) · airframe 61,630 hrs · 69,229 cycles

CORROSION ON FUSELAGE JOINT STRAP AT BS 182 BETWEEN STRINGERS 29 AND 30P. BLENDED AREA OF FUSELAGE STRAP. PERFORMED HFEC INSPECTION. NO DISCREPANCIES FOUND IAW EO8-53-13-0238.

Part: SEAT TRACK — CORRODED (BS 510) · airframe 61,630 hrs · 69,229 cycles

RIGHT OTBD SEAT TRACK HAS MINOR SURFACE CORROSION AFT OF BS 510. BLENDED MINOR SURFACE CORROSION AND FOUND IT TO BE WITHIN LIMITS IAW RD8-53-3644. ALODINED AND PRIMED BLENDED AREA.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 61,630 hrs · 69,229 cycles

PAX DOOR LOWER SILL HAS CORROSION ON TOP SURFACE AROUND FASTENER HOLES AND UNDER SURFACE NUT PLATES. R & R PAX DOOR LOWER SILL. CLEANED MINOR CORROSION FROM UNDER SILL. APPLIED ALODINE AND PRIMER TO ALL BARE METAL SURFACE IAW DWG NR 85321241.

Part: SEAT TRACK — CORRODED · airframe 61,630 hrs · 69,229 cycles

CENTER LT SEAT TRACK HAS AREA OF MINOR SURFACE PITTING THROUGH OUT THE LENGTH OF THE TRACK. BLENDED LIGHT CORROSION WITHIN LIMITS OF RD8-53-1339. PERFORMED HFEC ON THE AFFECTED AREA. NO DEFECTS FOUND. ALODINED AND PRIMED SEAT TRACK AS REQUIRED.

Part: SEAT TRACK — CORRODED (BS 253.4) · airframe 61,630 hrs · 69,229 cycles

CENTER RT SEAT TRACK HAS AREAS OF MINOR SURFACE PITTING THROUGH OUT THE LENGTH OF THE TRACK. BLENDED AREAS OF CORROSION ON INBD RT SEAT TRACK. CORROSION WAS FOUND TO BE WITHIN LIMITS IAW RD8-53-1339. NO CRACKS FOUND. APPLIED EPOXY PRIMER IAW RD8.53-1339.

Part: SEAT TRACK — CORRODED (BS 201-240) · airframe 61,630 hrs · 69,229 cycles

CENTER LT SEAT TRACK HAS SURFACE CORROSION THROUGHOUT BS 201.15 TO 240.50. BLENDED CORROSION AND FOUND TO BE WITHIN LIMITS IAW RD8-53-4698.

Part: DOOR — CORRODED (LAV SERVICE) · corrosion level 2 · airframe 61,629 hrs · 69,229 cycles

LAVATORY SERVICE DOOR CORRODED. R & R LAV SERVICE DOOR IAW DWG 85320983.

Part: SKIN — DEBONDED (FUSELAGE) · corrosion level 2 · airframe 61,629 hrs · 69,229 cycles

LOWER FUSELAGE SKIN PANEL IS DEBONDED AT STA X182.00, STR 29P TO 30P. UNRIVETED, DISBONDED AREA FOR FURTHER EVALUATION. CUT OUT DEBONDED SKIN AND WAFFLE DOUBLER. PERFORMED HFEC AND BOND TEST INSPECTION. NO DISCREPANCIES FOUND. REPAIRED IAW EO8-53-13-0248.

Part: HINGE — CORRODED (LAV SERVICE DOOR) · corrosion level 2 · airframe 61,629 hrs · 69,229 cycles

LAVATORY BOX SERVICE DOOR CUT OUT HAS SOME CORROSION AT DOOR HINGE AREA. FOUND SERVICE DOOR TO HAVE DEEP CORROSION AT HINGE AREA. R & R SERVICE DOOR AND HINGE IAW DWG 85320983.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 61,629 hrs · 69,229 cycles

CENTER RT SEAT TRACK HAS CORROSION THROUGHOUT STA X201.14 TO X252.30. PARTIALLY REMOVED SEAT TRACK. INSTALLED NEW SEAT TRACK AND SPLICE REPAIR. INSTALLED REMAINDER OF FASTENERS IAW RD8-53-3074.

Part: BEARING — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 61,630 hrs · 69,229 cycles

RT ELEVATOR ANCHOR SPRING BEARING CORRODED. REMOVED SOME CORROSION ON INBD SIDE . R & R INBD AND OTBD BEARING IN RT ELEVATOR ANCHOR SPRING ASSY IAW DWR 82760113.

Part: FLOOR SUPPORT — CORRODED (BS 600) · airframe 61,630 hrs · 69,229 cycles

LOWER CARGO BAY FLOOR SUPPORT ANGLE CORRODED. LT SIDE ANGLE OUT OF LIMITS. REMOVED LT AND RT ANGLES. BLENDED LIGHT CORROSION ON RT ANGLE, ALODINED AND PRIMED. REINSTALLED IAW DWG NR 85330112. INSTALLED NEW ANGLE ON LT SIDE IAW DWG 85330112.

Part: BULB — INOPERATIVE · airframe 61,567 hrs · 69,152 cycles

FOURTH EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,567 hrs · 69,152 cycles

SIDEWALL EMERGENCY LIGHT IS DIM AT ROW 1DF. R & R BULBS. OPS CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 61,567 hrs · 69,152 cycles

EMERGENCY EXIT SIGN AT FLOOR, FORWARD SIDE OF PAX DOOR IS BROKEN. R & R EMERGENCY LIGHT SUBASSEMBLY IAW WIRING PRACTICES. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 61,443 hrs · 69,003 cycles

EMERGENCY EXIT SIDEWALL LIGHT BY PAX DOOR IS DIM. R & R BURNED OUT BULB IN SIDEWALL EMERGENCE LIGHT BY PAX DOOR.

Part: CONTROL BOX — UNKNOWN (EMERGENCY LIGHTS) · airframe 60,994 hrs · 68,451 cycles

EMERGENCY LIGHTS ILLUMINATED ON GROUND, CYCLED SWITCH, LIGHTS WENT OUT. R & R EMERGENCY LIGHTS CONTROL BOX IAW WC 33-50-03Q. OPS CHECKED GOOD. CLEANED CONNECTOR PLUG ON EMERGENCY LIGHTS CONTROL BOX. OPS CHECKED GOOD. NO DEFECTS FOUND.

Part: GENERATOR — MALFUNCTIONED (NR 2) · airframe 60,392 hrs · 67,715 cycles

AC GENERATOR CAUTION LIGHT REMAINS ON, NO LOAD ON NR 2 AC GENERATOR. R & R NR 2 AC GENERATOR AND NR 2 GCU AS REQUIRED. GROUND RAN ACFT. OPS CHECKED GOOD IAW 24-21-01.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 59,600 hrs · 66,755 cycles

EMERGENCY CEILING LIGHT IS INOPERATIVE AT ROW 7. R & R BULB IAW AMM 33-51-00.

Part: SHROUD — CRACKED (EXHAUST) · airframe 59,588 hrs · 66,744 cycles

HOLE IN OTBD FWD SIDE OF NR 1 EXHAUST FINGER NAIL. R & R LT EXHAUSTS SHROUD WITH RETAINED FASTENERS.

Part: INDICATOR — FAILED (VERTICAL SPEED) · airframe 59,566 hrs · 66,716 cycles

SMOKE IN COCKPIT DURING FLIGHT. PERFORMED EMERGENCY CHECKLIST. SMOKE DID NOT DISSIPATE. DECLARED EMERGENCY. LANDED NORMALLY. FOUND CAPTAIN`S IVSI INOPERATIVE AND SCREEN BLANK. R & R IVSI. OK FOR SERVICE.

Part: DRAG STRUT — CRACKED (MLG) · airframe 59,361 hrs · 66,488 cycles

UPON GEAR RETRACTION, RED NOSE AND HANDLE LIGHT REMAINED ILLUMINATED FOR ABOUT 10 MINUTES AND THEN EXTINGUISHED. GEAR EXTENSION NORMAL FOR LANDING. R & R NLG DRAG STRUT ASSY IAW WORKCARD 32-20-11R. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 59,325 hrs · 66,447 cycles

SMOKE ALARM IN LAVATORY SOUNDED CONTINUOUSLY. STOPPED WHEN AIRSTAIR DOOR OPEN. INSPECTED LAV SMOKE DETECTOR. NO DEFECTS NOTED. CLOSED CABIN DOOR AND RAN APU WITH BLEED AIR ON.NO DEFECTS. RAN BOTH ENGINES BLEED AIR ON. NO DEFECTS. NO SMOKE OR ODOR PRESENT. LAV LIGHTS NO DEFECTS. OKAY FOR SERVICE. APU BLEED PLACED ON MEL AS PRECAUTION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,313 hrs · 66,432 cycles

SEAT LEVEL EMERGENCY EXIT SIGN IS INOPERATIVE. R & R SEAT LEVEL EMERGENCY EXIT SIGN AND SECURED LENS COVER.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 59,100 hrs · 66,190 cycles

AFT OVERHEAD EMERGENCY EXIT LIGHT IS INOPERATIVE. R & R OVERHEAD EMERGENCY LIGHT AS REQUIRED. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 59,076 hrs · 66,157 cycles

LEFT AFT EGRESS LIGHT IS DIM. R & R LEFT AFT EGRESS LIGHT. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 58,964 hrs · 66,030 cycles

LAVATORY SMOKE DETECTOR SOUNDED AFTER ROTATION. WOULD NOT GO OFF. RETURNED TO FIELD. TURNED OFF CABIN LIGHTS AND PSU. ALARM STOPPED. INSPECTED FWD CABIN AREA AND LAVATORY FOR HIDDEN DAMAGE IAW SPECIAL PROCEDURES 33.1. NO ODOR OR DAMAGE FOUND.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 58,453 hrs · 65,426 cycles

EMERGENCY EXIT LOWER LIGHTED EXIT SIGNS HAVE INOPERATIVE LAMPS. R & R LAMPS. OPS CHECKED GOOD.

Part: ECU — FAILED (NR 1) · airframe 58,017 hrs · 64,923 cycles

DURING SHUTDOWN WITH NR1 CONDITION LEVER IN START/FEATHER. NR 1 ENGING TORQUE SURGED TO 90 PERCENT AND PROPELLER RPM STAYED AT 600 FOR 7 SECONDS. ALL OTHER PARAMETERS NORMAL. R & R ECU. PERFORMED RUN UP OPS CHECK IAW MX RUN UP MANUAL FOR COMPONENT CHANGED. OPS CHECKED GOOD FOR SERVICE.

Part: LAMP — BURNED (EMERGENCY LIGHT) · airframe 57,758 hrs · 64,638 cycles

EMERGENCY FLOOR LAMP AT ROW 7DF IN INOP. R & R LIGHT BULB IAW 33-52-00.

Part: RESERVOIR — LEAKING (HYD SYSTEM) · airframe 57,691 hrs · 64,558 cycles

AFTER TAKEOFF NR 2 HYD QUANITY DROPPED AND NR 2 RUDDER ISO CAUTION LIGHT ILLUMINATED FOLLOWED BY NR2 HYD PUMP CAUTION LIGHT. QUANITY ON THE GROUND IS O. R & R NR 2 HYD RESERVOIR IAW MM 29-10-26. R & R NR2 ENGINE DRIVEN PUMP IAW MM 29-10-11. BLED AND SERVERED IAW MM 12-10-29. GROUND RAN ACFT, OPS AND LEAKED CHECKED GOOD. ALL INSP COMLPIED WITH IAW 05-50-33.

Part: WIRE — CROSSED (THERMOCOUPLES) · airframe 57,181 hrs · 63,976 cycles

ABORTED TAKEOFF DUE TO PEGGED NR 2 ITT GAGE WITH AMBER LIGHT AND NO OTHER UNUSUAL INDICATIONS. INSPECTED NR 2 ENGINE HOT SECTION, FOUND 3 THERMOCOUPLE WIRES CROSSED, REPOSITIONED WIRES, GROUND RAN NR2 ENGINE, OPS CHECKED GOOD.

Part: GENERATOR — INOPERATIVE (NR 2 AC) · airframe 56,697 hrs · 63,449 cycles

WHEN RETRACTING WHEELS, NR 2 A/C GENERATOR WENT OFF LINE WITH CAUTION LIGHT AND VOLTS BUT NO LOADS. RESET GENERATOR CAUTION, CAUTION LIGHT WENT OUT. EXTENDED LANDING GEAR, NR 2 A/C GENERATOR LIGHT ILLUMINATED AGAIN, (VOLTS BUT NO LOADS). DUE TO HISTORY OF GENERATOR, R & R A/C GENERATOR IAW WORK CARD 24-20-11R. ALSO, R & R GENERATOR SWITCH USING STANDARD MX PRACTICES. GROUND RAN ACFT, OPS CHECKED GOOD.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 56,118 hrs · 62,814 cycles

BOTTOM SIDE OF PAX DOOR FLOOR LEVEL HAS CORRODED NUTPLATES. REMOVED NUT PLATES, REMOVED CORROSION, REPLACED NUTPLATES, ALODINED AND PRIMED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 56,118 hrs · 62,814 cycles

AFT GALLEY SUPPORT ANGLE HAS NUTPLATE CORRODED ON BOTTOM SURFACE AT X242.200. REMOVED NUTPLATES, CLEANED ALODINED AND PRIMED. INSTALLED NUTPLATES WITH CCR RIVETS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,118 hrs · 62,814 cycles

BOTTOM ATTACH ANGLE FOR OTBD SEAT TRACK IS CORRODED AT BOTTOM SIDE AT RT FWD EMERGENCY EXIT DOOR SURROUND (FLOOR LEVEL-AFT END). REMOVED 2 RIVETS AND 2 HILOCS, CLEANED ANGLE, ALODINED, PRIMED. INSTALLED 2 UNIVERSAL AD5 RIVETS AND 2 HILOC 328-6 HILOCS.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 56,118 hrs · 62,814 cycles

RT FWD EMERGENCY EXIT DOOR SURROUND HAS CORROSION AT BOTTOM THRESHOLD AND AROUND DATAPLATE. REMOVED PLATE, CLEANED, ALODINED, PRIMED. REINSTALLED PLATE WITH 6 CCR RIVETS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,027 hrs · 61,465 cycles

FLOOR EMERGENCY EXIT LIGHTS NOT WORKING. REMOVED LIGHT TRIM, REMOVED RED LIGHT LENS, R & R BULBS, OPS CHECKED GOOD, INSTALLED RED LENS AND TRIM.

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 54,607 hrs · 60,994 cycles

EMERGENCY LIGHTS WILL NOT TURN OFF WHEN SELECTED OFF, WILL TURN OFF IN THE ARM POSITION. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BASE AT LOCATION 3352PS1 AND 3352PS2. OPERATIONAL CHECKED GOOD.

Part: CIRCUIT BREAKER — DEFECTIVE (CABIN) · airframe 54,603 hrs · 60,988 cycles

EMERGENCY LIGHT CAUTION LIGHT DOES NOT ILLUMINATE WHEN SELECTING EMERGENCY LIGHTS OFF. SLAVED IN F/A'S SWITCH PANEL, NO FIX, CHECKED CONTINUITY OF FLIGHT DECK SWITCH 3312-P1 PIN17 TO 9811 P45 PIN AND 3351 P1 PIN R, NO DISCREPANCIES NOTED. FOUND ONLY 16 VOLTS AT 9811 TB 14 PIN 7A. REMOVED AND REPLACED C/B C3 ON RIGHT SECONDARY BUDD. OPS CHECKED GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 54,601 hrs · 60,986 cycles

UNABLE TO CANCEL EMERGENCY LIGHTS WITH ACFT POWER ( BATTERIES OR APU) CONNECTED GPU LIGHTS OPERATE NORMALLY WITH GPU CONNECTED AND WITHOUT GPU. DUPLICATE PROBLEM ONLY WITH SECONDARY BUSS. POWERED AND ONLY FLOOR LEVEL LIGHTING REMAINED ILLUMINATED. OPS CHECKED GOOD WITHOUT SECONDARY BUSS POWERED. R & R EMERGENCY LIGHT POWER SUPPLY BASE AT LOCATION 3352PS1 AND 3352PS2. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 54,280 hrs · 60,632 cycles

FWD MOST FLOOR EMERGENCY LIGHT IN FRONT OF SEAT 1DF WILL NOT ILLUMINATE. RAISED FLOOR STRIP, REPLACED BULB AND LOWERED AND SECURED FLOOR STRIP.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,713 hrs · 59,999 cycles

EMERGENCY LIGHT OUT AT NR 3 FROM FORWARD TO AFT (RED). REMOVED AND REPLACED LIGHT BULB. OPERATES CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 53,484 hrs · 59,739 cycles

DURING INSPECTION IN SBY TWO SIDEWALL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE BULBS WERE REMOVED AND REPLACE AND THE OPERATIONAL CHECK WAS GOOD

Part: COMPASS — SMOKE (COCKPIT) · airframe 53,065 hrs · 59,275 cycles

DC BUSS CAUTION LIGHT ILLUMINATED AFTER STARTING NR 1 ENG FOLLOWED BY SMOKE COMING FROM CTR CONSOLE COMPASS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,611 hrs · 58,777 cycles

ONE EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,276 hrs · 39,631 cycles

UPON LINE INSPECTION AT SBY, AN EMERGENCY EXIT LIGHT AT ROW 5 WAS FOUND INOPERATIVE. REMOVED AND REPLACED LIGHT BULB, OPERATIONAL TIME WAS GOOD.

Part: LINKAGE — BROKEN (NLG DOOR) · airframe 52,199 hrs · 58,324 cycles

AFTER TAKEOFF ON GEAR RETRACTION HAD RED NOSE GEAR LIGHT, AFTER APPROX 1 MIN ALL LIGHTS CLEARED FOLLOWED BY NOTICEABLE VIBRATION IN YOKE AND RUDDER. JACKED AND SWUNG GEAR REF MM 32-30-00. GEAR AND INDICATION ARE WORKING CORRECTLY. INSPECTED NOSE GEAR AREA, FOUND RIGHT AFT NOSE GEAR DOOR LINKAGE BROKEN. REMOVED AND REPLACED LINKAGE.

Part: GCU — INTERMITTENT (NR 2 ENGINE) · airframe 52,106 hrs · 58,218 cycles

EMERGENCY LIGHT CAME ON DURING FLIGHT. FOUND AC GENERATOR CONTROL UNIT BAD. REMOVED AND REPLACED AC GENERATOR CONTROL UNIT ON BOTH ENGINES. REMOVED AND REPLACED FUSES 2421 F8 AND F10, OPS CHECK GOOD.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 51,853 hrs · 57,930 cycles

WHILE ACFT WAS ON THE GROUND, THE EMERGENCY LIGHTS WERE OBSERVED TO FLICKER INTERMITTENTLY. ACFT WAS RUN ON GROUND AND EMERGENCY LIGHTS WERE OPERATED, BUT THE PROBLEM COULD NOT BE DUPLICATED. NO HISTORY OF SIMILAR PROBLEMS WAS FOUND. ACFT WAS THEN RELEASED FOR SERVICE.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 51,853 hrs · 57,930 cycles

EMERGENCY LIGHT FLICKER ON INTERMITENTLY ON GROUND. RAN ACFT OPERATED EMERGENCY LIGHTS ON/OFF WITH LIGHTS ARMED. DID NOT FLICKER, CANNOT DUPLICATE. NO HISTORY.

Part: BRAKE — SMOKE (LT MLG) · airframe 51,782 hrs · 57,848 cycles

LEFT MAIN BRAKE ASSEMBLY WET, SMOKES AFTER LANDING. REMOVED AND REPLACED NUMBER ONE BRAKE ASSY IN ACCORDANCE WITH 32-42-11, LEAK AND OPS GOOD.

Part: REGULATOR — FAILED (ZONE 300) · airframe 51,791 hrs · 57,859 cycles

RUDDER PRESSURE AND RUDDER FULL PRESSURE CAUTION LIGHT'S ILLUMINATED AFTER TAKEOFF. QUANTITY’S AND PRESSURE WERE NORMAL. RUDDER PRESSURE WENT OUT BELOW 140 KNOTS, RUDDER FULL PRESSURE WENT OUT AT 120 KNOTS. REMOVED AND REPLACED RUDDER DUAL PRESSURE REGULATOR IAW 27-20-38, OPS CHECK GOOD OK FOR SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY EXIT SIGN FWD RT INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY. OPS CHECK GOOD. (S)

Part: CONTROL BOX — MALFUNCTIONED (EMERGENCY LIGHTS)

CABIN EMERGENCY LIGHTS INTERMITTENT ILLUMINATION DURING TAXI AND FLIGHT. A/C FERRIED FOR REPLACEMENT OF LIGHTS CONTROL BOX. OPS CHECKED GOOD. (K)

Part: OIL SYSTEM — LEAKING (APU)

APU BLEED ON, VAPOR VISIBLE IN CABIN. INSPECTED AND FOUND APU HAS AN OIL LEAK, NO VAPOR VISIBLE OFF ENGINE BLEEDS. REMOVED AND REPLACED APU. (K)

Part: SPOILER SYS — FAILED (NR 2) · airframe 49,691 hrs · 55,535 cycles

DURING FLIGHT, NR 2 HYDRAULIC SYSTEM BEGAN LOOSING FLUID. AT 1/2 QT LOSS, SYSTEM ISOLATION VALVE CLOSED TO PREVENT FURTHER LOSS OF FLUID. LANDING GEAR WAS CYCLED DOWN BEFORE ISOLATION VALVE CLOSED AS A PRECAUTION. MAINTENANCE FOUND NR 2 ROLL SPOILER UNLOADING VALVE UNSERVICEABLE. REMOVED AND REPLACED VALVE. SERVICED HYDRAULIC SYSTEM AND OPS CHECKED AIRCRAFT IAW MAINTENANCE MANUAL PROCEDURES. CHECKS WERE GOOD.

Part: PUMP — BROKEN (HYDRAULIC SYS) · airframe 48,757 hrs · 54,512 cycles

IN FLT NR 1 HYD ISO VALVE, ROLL SPOILER INBOARD DYD, NR 1 RUD HYD CAUTION LIGHT ILLUMINATED FOLLOW BY LOSS OF NR 1 HYD QTY. REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP. NO CONTAMINATION IN CASE DRAIN FILTER, OPS & LEAK CHECK GOOD.

Part: SOCKET — ARCED (CABIN LIGHTS) · airframe 45,773 hrs · 51,261 cycles

ELECTRIC SMELL IN CABIN. FOUND BULB SOCKET BURNED AT SIDEWALL LIGHTING AT ROW 9 RT SIDE.

Part: BATTERY — SHORTED (AUX BATTERY) · airframe 45,634 hrs · 51,116 cycles

AUX BATTERY HOT WARINING LIGHT ILLUMINATED IN FLIGHT. REPLACED AUX BATTERY.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 43,188 hrs · 48,462 cycles

WOW CAUTION LIGHT ILLUMINATED UPON LDG EXTENSION CYCLED GEAR AND LIGHT WENT OUT, NO PROBLEMS ON LANDING. INSPECTED AND CLEANED ALL LANDING GEAR WOW SENSORS. PERFORMED PSEU MEMORY TEST, NO FAULTS CODES FOUND. PERFORMED SATISFACTORY EVALUATION FLIGHT. PROBLEM RETURNED LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE REPLACED THE PSEU, EVAL FLIGHT WAS UNSATISFACTORY. MAINTENANCE THEN REPLACED THE LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECK WAS GOOD.

Part: DIODE — SHORTED (LANDING GEAR) · airframe 42,441 hrs · 47,668 cycles

ON APPROACH TO DCA, ALL THREE LANDING GEAR DOORS OPENED AND CLOSED THEN OPENED AGAIN. FERRIED A/C TO SBY FOUND 2 BAD DIODES 3261-CR1 AND 3261-CR2 REMOVED AND REPLACED DIODES, OPS CHECK GOOD.

Part: SEALANT — DETACHED (WINDSHIELD) · airframe 40,938 hrs · 45,992 cycles

NOTED LOUD FLAPPING NOISE INFLT FROM CAPT WINDSHIELD AFTER T/O RETURN TO FIELD. FOUND LOOSE WINDSHIELD SEAL, EXCESS WAS REMOVED AND APPLIED SPEED TAPE. SEALED AT NEXT RON PER EO 8-56-04-0273

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,800 hrs · 44,782 cycles

MAJOR REPAIR; REPAIR FOR AFT LOWER FUSELAGE SKIN DAMAGE.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 39,800 hrs · 44,782 cycles

MAJOR REPAIR: SPLICE OF STR 31S IN AFT FUSELAGE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,800 hrs · 44,782 cycles

MAJOR REPAIR; X467 FRAME SECTION REPLACEMENT.

Part: SKIN — DENTED (ESCAPE HATCH) · airframe 39,800 hrs · 44,782 cycles

REPAIR FOR DENTED ROOF SKIN AFT OF COCKPIT ESCAPE HATCH.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 39,800 hrs · 44,782 cycles

MAJOR REPAIR; REPAIR FOR BELLY SKIN EXTERNAL CORROSION.

Part: SELECTOR VALVE — LEAKING (LANDING GEAR) · airframe 33,592 hrs · 38,144 cycles

ON GEAR DOWN SELECTION, 3 UNSAFE RED LIGHTS ILLUMINATED AND GEAR DID NOT COME DOWN. GEAR ALTERNATE RELEASE WAS PERFORMED.

Part: CONTROL UNIT — SMOKE (COCKPIT) · airframe 32,645 hrs · 37,120 cycles

WHEN GROUND POWER WAS APPLIED TO THE AIRCRAFT SMOKE AND SPARKS CAME FROM THE F/O'S SIDE OF THE CENTER CONSOLE. REPLACED THE NO. 2 COMM CONTROL HEAD.

Part: CONTROL UNIT — SMOKE (COCKPIT) · airframe 32,645 hrs · 37,120 cycles

WHEN GROUND POWER WAS APPLIED TO THE AIRCRAFT SMOKE AND SPARKS CAME FROM THE F/O'S SIDE OF THE CENTER CONSOLE. REPLACED THE NR 2 TRANSPONDER CONTROL HEAD.

Part: STRUT — BROKEN (PAX DOOR)

PAX DOOR HEAVY, ALREADY INFO''D. FOUND FWD STRUT SHEARED AND FOUND GAS STRUT UPPER ATTACH BRACKETS BENT. REMOVED AND REPLACED FORWARD AND AFT AIRSTAIR DOOR STRUT AND REMOVED AND REPLACED SLIDE ASSY.

Part: WINDSHIELD — SPARKS (COCKPIT) · airframe 30,349 hrs · 34,642 cycles

DURING TAKE OFF ROLL THE CREW SAW FLAME AND SPARKS COMING FROM THE F/O''S FRONT WINDSCREEN. TAKE OFF WAS ABORTED. REPLACED F/O''S WINDSCREEN.

Part: WINDSHIELD — SPARKS (COCKPIT) · airframe 30,349 hrs · 34,642 cycles

DURING TAKE OFF ROLL THE CREW SAW FLAME AND SPARKS COMING FROM THE F/O''S FRONT WINDSCREEN. TAKE OFF WAS ABORTED. REPLACED F/O''S WINDSCREEN.

Part: CABLE — DISPLACED (PAX DOOR)

BEFORE THE FIRST FLIGHT OF THE MORNING THE CREW COULD NOT OPEN THE PAX DOOR MORE THAN APPROX 1 FOOT. THE COUNTERBALANCE CABLE WAS FOUND TO BE OFF THE CABLE DRUM. THE CABLE AND COUNTERBALANCE GAS STRUTS WERE REPLACED.

Part: DOOR — OUT OF ADJUST (MLG DOOR)

NR 1 GEAR DOOR (AFT) OPENED IN FLT AND WILL NOT CLOSE. ADJUSTED GEAR DOOR AND AND NR 1 PROX SENSOR.

Part: SKIN — CRACKED (FUSELAGE)

AFT FUSELAGE, SMALL CRACK IN SKIN APPROX 5 IN FWD OF FRAME 3 AT STR 33. TEMP REPAIRED IAW RD8-53-2181. TEMP REPAIRED PER ENGINEERING. FWD TO ENGINEERING FOR PERM REPAIR. DEFERED FOR 240HRS. ON 8/20/99, THIS DMT WAS CLEARED PER EO8-53-99-290.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FORWARD LEFT HAND INTERIOR FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY.

Part: PBE — UNSERVICEABLE (CABIN)

PERSONAL BREATHING EQUIPMENT (PBE) IN FLIGHT ATTENDANT'S CLOSET RED INDICATOR PROTRUDING PAST FACE OF CONTAINER. REPLACED PBE.

Part: STOP — OUT OF ADJUST (PASSENGER DOOR)

DCA - FLT 3159 - UNABLE TO OPEN PASSENGER DOOR FROM INSIDE. FOUND LOWER DOOR SKIN RUBBING. ADDED SHIMS AND ADJUSTED ALL DOOR STOPS. PRESSURIZED AIRCRAFT. OPERATIONAL AND LEAK CHECK GOOD. (M)

Part: ENGINE — FAILED (NR 2)

FLT NR 3249 - HPN-BWI - DURING FLIGHT, NR 2 ENGINE TORQUE BEGAN TO FLUCTUATE AND WAS FOLLOWED BY A LOUD BANG. THE CREW SHUT THE ENGINE DOWN IN FLIGHT AND LANDED IN BWI WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 2 ENGINE. (M)

Part: ARM — FAILED (NLG)

LYN/PHL - FLT 3230 - AFTER TAKEOFF, UPON GEAR RETRACTION, THE WOW CAUTION LIGHT ILLUMINATED AND THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND BOTH LIGHTS EXTINGUISHED. THE AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. AFTER FERRYING TO SBY, THE NOSE LANDING GEAR LOWER BEARING WAS FOUND TO BE BINDING AND STICKING. REMOVED AND REPLACED THE NLG INNER CYLINDER, TRAIL ARM, PISTON, AXLE, UPPER AND LOWER BEARINGS, AND ASSOCIATED SEALS.

Part: INNER CYLINDER — FAILED (NLG)

LYN/PHL - FLT 3230 - AFTER TAKEOFF, UPON GEAR RETRACTION, THE WOW CAUTION LIGHT ILLUMINATED AND THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND BOTH LIGHTS EXTINGUISHED. THE AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. AFTER FERRYING TO SBY, THE NOSE LANDING GEAR LOWER BEARING WAS FOUND TO BE BINDING AND STICKING. REMOVED AND REPLACED THE NLG INNER CYLINDER, TRAIL ARM, PISTON, AXLE, UPPER AND LOWER BEARINGS, AND ASSOCIATED SEALS.

Part: LWR BEARINGS — FAILED (NLG)

LYN/PHL - FLT 3230 - AFTER TAKEOFF, UPON GEAR RETRACTION, THE WOW CAUTION LIGHT ILLUMINATED AND THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND BOTH LIGHTS EXTINGUISHED. THE AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. AFTER FERRYING TO SBY, THE NOSE LANDING GEAR LOWER BEARING WAS FOUND TO BE BINDING AND STICKING. REMOVED AND REPLACED THE NLG INNER CYLINDER, TRAIL ARM, PISTON, AXLE, UPPER AND LOWER BEARINGS, AND ASSOCIATED SEALS.

Part: AXLE — FAILED (NLG)

LYN/PHL - FLT 3230 - AFTER TAKEOFF, UPON GEAR RETRACTION, THE WOW CAUTION LIGHT ILLUMINATED AND THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND BOTH LIGHTS EXTINGUISHED. THE AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. AFTER FERRYING TO SBY, THE NOSE LANDING GEAR LOWER BEARING WAS FOUND TO BE BINDING AND STICKING. REMOVED AND REPLACED THE NLG INNER CYLINDER, TRAIL ARM, PISTON, AXLE, UPPER AND LOWER BEARINGS, AND ASSOCIATED SEALS.

Part: PISTON — FAILED (NLG)

LYN/PHL - FLT 3230 - AFTER TAKEOFF, UPON GEAR RETRACTION, THE WOW CAUTION LIGHT ILLUMINATED AND THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND BOTH LIGHTS EXTINGUISHED. THE AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. AFTER FERRYING TO SBY, THE NOSE LANDING GEAR LOWER BEARING WAS FOUND TO BE BINDING AND STICKING. REMOVED AND REPLACED THE NLG INNER CYLINDER, TRAIL ARM, PISTON, AXLE, UPPER AND LOWER BEARINGS, AND ASSOCIATED SEALS.

Part: UPPER BEARINGS — FAILED (NLG)

LYN/PHL - FLT 3230 - AFTER TAKEOFF, UPON GEAR RETRACTION, THE WOW CAUTION LIGHT ILLUMINATED AND THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND BOTH LIGHTS EXTINGUISHED. THE AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. AFTER FERRYING TO SBY, THE NOSE LANDING GEAR LOWER BEARING WAS FOUND TO BE BINDING AND STICKING. REMOVED AND REPLACED THE NLG INNER CYLINDER, TRAIL ARM, PISTON, AXLE, UPPER AND LOWER BEARINGS, AND ASSOCIATED SEALS.