N933HA

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 68,482 hrs · 77,115 cycles

RED FLOOR EMERGENCY LIGHT IS INOPERATIVE. CYCLED SWITCH SEVERAL TIME, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,421 hrs · 77,043 cycles

SEVERAL EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED THE BATTERY IAW WORK CARD 33-50-05R. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,369 hrs · 39,000 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROW 6. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,369 hrs · 39,000 cycles

FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH PANEL IS INOPERATIVE. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,369 hrs · 39,000 cycles

THREE EMERGENCY CEILING LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,260 hrs · 76,870 cycles

RIGHT AFT OUTSIDE EMERGENCY EXIT EGRESS LIGHT IS INOPERATIVE. LOWERED PSU COVER AT ROW 7DF. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY. SECURED PSU COVER PANEL AT ROW 7DF. OPS CHECKED GOOD.

Part: GENERATOR — MALFUNCTIONED (NR 1 ENGINE) · airframe 67,767 hrs · 76,267 cycles

AIRCRAFT TOOK LIGHTNING STRIKE-NR 1 AND NR 2, DC GENERATORS WERE TAKEN OFF LINE, SUCCESSFULLY RESET BOTH DC GENERATORS. GEAR WAS RETRACTED. COMPLETE ALL STEPS OF WORK CARD 05-50-31I, INSPECTION FOR REPORTED LIGHTNING STRIKE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,552 hrs · 76,007 cycles

EMERGENCY FLOOR LIGHT ROW 7DF INOPERATIVE. PULLED UP EMERGENCY FLOOR LIGHT COVER REPLACED INOPERATIVE EMERGENCY FLOOR LIGHT BULB AT 7DF. RESECURED EMERGENCY FLOOR LIGHT COVER.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,251 hrs · 75,659 cycles

CABIN 2 AFT RED EMERGENCY LIGHTS WILL NOT ILLUMINATE AT RT FWD EXIT. R & R BULBS IN MODULE ASSY. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,064 hrs · 75,434 cycles

FORWARD EGRESS AND PASSENGER DOOR EMERGENCY LIGHTS ARE OUT. R & R EMERGENCY LIGHT BATTERY PS1 IAW MM 33-51-00. OPS CHECKED GOOD.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 67,043 hrs · 75,410 cycles

AUTOFEATHER WILL NOT ARM ON TAKEOFF ROLL. AUTO FEATHER SELECT SWITCH WENT BLANK. K5 CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER K5 ENGINE TORQUE CONDITION. CLEANED CONNECTOR ON NR 2 ENGINE TSCU. GROUND RAN ACFT. AUTOFEATHER TEST FAILED. NO FIX. SLAVED IN NEW TORQUE INDICATOR. NO FIX. REINSTALLED ORIGINAL NR 2 TORQUE INDICATOR IAW MM 77-10-00.

Part: CONTROL UNIT — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 67,037 hrs · 75,401 cycles

AUTOFEATHER WOULD NOT ARM DURING TAKEOFF ROLL. R & R NR 2 TSCU. RAN AIRCRAFT. OPS CHECKED GOOD IAW MM 72-01-10.

Part: CIRCUIT BREAKER — TRIPPED (NR 2 TORQUE IND) · airframe 67,037 hrs · 75,401 cycles

IN FLIGHT, NR 2 TORQUE INDICATOR CIRCUIT BREAKER TRIPPED. REMOVED CONNECTOR FROM NR 2 TSCU. CLEANED, INSPECTED AND REINSTALLED CONNECTOR . RESET CIRCUIT BREAKER K-5. GROUND RAN ACFT. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,549 hrs · 74,832 cycles

EMERGENCY AISLE LIGHT ABOVE ROW 4 INTERMITTENTLY. WILL NOT COME ON AS EXPECTED. R & R POWER SUPPLY FOR EMERGENCY LIGHTS AT ROWS 3AC AND 7DF IAW WC 33-50-05R AND 33-50-03Q. OPS CHECKED GOOD AT THIS TIME.

Part: LIGHT — UNKNOWN (CABIN) · airframe 66,542 hrs · 74,824 cycles

ROW 4 EMERGENCY LIGHTS WILL NOT EXTINGUISH AS EXPECTED, REQUIRES APU ON GROUND POWER TO TURN OFF. CHECKED EMERGENCY LIGHT SYS IAW WC 33-50-03Q. NO FAULT NOTED. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,151 hrs · 74,350 cycles

SMALL EXIT SIGN NEST TOO ROW 1DF HAS BULB OUT. R & R BULB. OPS CHECKED GOOD.

Part: WIRE — CHAFED (MLG) · airframe 65,701 hrs · 73,798 cycles

ADVANCED POWER LEVERS FOR TAKEOFF, DURING FERRY FLIGHT AND LT MLG UNSAFE RED LIGHT AND GEAR HANDLE LIGHT ILLUMINATED. FOUND MULTIPLE CHAFED WIRES. HA300, SEQ 20, 18 AND 17. OPS CHECKED GOOD.

Part: WIRE — CHAFED (MLG) · airframe 65,701 hrs · 73,798 cycles

LEFT MAIN GEAR UNSAFE LIGHT AND GEAR HANDLE LIGHT AND WARNING HORN ILLUMINATED, SOUNDED. TAKEOFF REJECTED. FOUND MULTIPLE CHAFED WIRES. HA 300, SEQ 20,18 AND 17 FOR C/A. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,368 hrs · 73,406 cycles

ROW 1 EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. R & R BULB IN FLOOR PATH LIGHT. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,368 hrs · 73,406 cycles

EMERGENCY SIDEWALL LIGHTS ARE INOPERATIVE AT ROWS 1DF AND 4DF. R & R BULBS IN EMERGENCY SIDEWALL LIGHTS AT ROW 1DF AND 4DF. OPS CHECKED GOOD.

Part: TIMER — FAILED (PROPELLER HEAT) · airframe 64,816 hrs · 72,744 cycles

WITH NR 1 PROPELLER TIMER SELECTED, BLADES 1 AND 3 CONTINUED TO HEAT. WOULD NOT CYCLE. DURING GROUND RUN, OPS CHECKED OF NR 2 PROPELLER TIMER. R & R NR 2 PROPELLER TIMER. OPS CHECKED GOOD IAW MM 30-61-00. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,713 hrs · 72,622 cycles

EMERGENCY LIGHT IS INOPERATIVE. R & R THE BULB, OPS CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED (HORN HEAT) · airframe 64,494 hrs · 72,368 cycles

ELEVATOR HORN HEAT CAUTION LIGHT ILLUMINATED IN FLIGHT. SELECTED ELEVATOR LT HORN HEAT TO ALTERNATE POSITION. GROUND RAN ACFT WITH CREW, SYSTEM OPS CHECKED GOOD IAW MM 30-16-00. OK FOR SERVICE.

Part: PROPELLER — MALFUNCTIONED (NR 2) · airframe 64,242 hrs · 72,079 cycles

NR 2 PROPELLER RPM WAS 1185 TO 1187 DURING TAKEOFF ROLL. ABORTED TAKEOFF. ALL OTHER ENGINE PARAMETERS NORMAL. RAN ENGINES BEFORE RETURNING TO GATE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,415 hrs · 71,061 cycles

ONE BURNED RIVET ON LT FUSELAGE SKIN 6.0" AFT OF VERTICAL FRONT BETWEEN STR 25A-26A. REMOVED RIVET AND BLENDED AREA. REMAINING .35" DEEP. REPAIRED IAW EO8-53-14-0224, EA 25-2014-150, REV A.

Part: STATIC WICK — BURNED (LT ELEVATOR) · airframe 63,415 hrs · 71,061 cycles

LEFT ELEVATOR OTBD STATIC WICK BURNED OFF AND MOUNTING PLATE DAMAGED. REMOVED OTBD END CAP, INSTALLED NEW END CAP, STATIC WICK AND MOUNTING PLATE IAW DWG 85520002 AND PREVIOUS REPAIR EA01-09126.

Part: INVERTER — FAILED · airframe 63,150 hrs · 70,732 cycles

STRONG FISH ODOR IN COCKPIT. INSPECTED PRIMARY, SECONDARY AND AUX INVERTER. NO DEFECTS NOTED. OPS CHCKED INVERTERS. NO ODOR, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,958 hrs · 70,501 cycles

EMERGENCY LIGHT INOPERATIVE. R & R BULB.

Part: ECU — FAILED (NR 2) · airframe 62,793 hrs · 70,293 cycles

NR 2 ECU FAILED AFTER TAKEOFF. ACFT RETURNED TO, NR 2 ECU FAILED AND WEATHER CONDITIONS TO BAD TO CONTINUE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,759 hrs · 70,249 cycles

FLOOR EMERGENCY PATH LIGHT IS INOPERATIVE AT ROWS 5DF. CHANGED BULBS. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 62,638 hrs · 70,096 cycles

DURING TAXI OUT WITH ENGINE BLEEDS SELECTED ON, A BURNING OIL ODOR IN FLIGHT DECK AND CABIN. WHEN BLEEDS WERE SELECTED OFF, ODOR STARTED TO DIMISHED. GROUND RAN BOTH ENGINES AND APU FOR ABOUT 20 MINUTES. WITH BLEEDS SELECTED ON AND OFF MULTIPLE TIMES, CHANGING TEMP CONTROL SETTING. NO ODORS DETECTED. OK FOR SERVICE.

Part: CONTROLLER — FAILED (WINDSHIELD HEAT) · airframe 62,513 hrs · 69,954 cycles

LEFT WINDSHIELD HOT CAUTION LIGHT ILLUMINATED IN FLIGHT. R & R CAPTAIN'S WINDSHIELD HEAT CONTROLLER. OPS CHECKED GOOD ON GROUND RUN IAW MM 30-41-00.

Part: BLADE — VIBRATION (NR 2 PROPELLER) · airframe 62,468 hrs · 69,895 cycles

NR 2 PROPELLER HAS EXCESSIVE VIBRATION IN FLIGHT. SHIMMED NR 3 AND NR 4 BLADES IAW MM 61-10-00. OPS CHECKED GOOD.

Part: TRANSMITTER — DAMAGED (SPOILER) · airframe 62,071 hrs · 69,389 cycles

ON TAKEOFF ROLL, RT SPOILER INDICATED DEPLOYED AND AGAIN IN TAXI MODE. INSPECTED RT INBD ROLL SPOILER, FOUND SYNCRO TRANSMITTER ARM OVER CENTER. REPOSITIONED TO CORRECT POSITION. GROUND RAN ACFT, OPS CHECKED SPOILERS. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: RADAR — FAULTED · airframe 61,921 hrs · 69,201 cycles

POSSIBLE LIGHTNING STRIKE. ACFT WAS DIVERTED, DUE TO POSSIBLE RADAR FAULT.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 61,527 hrs · 68,716 cycles

PASSENGER DOOR WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. ENTRY DOOR INDICATION WITH MOD APPENDIX 5 COMPLIED WITH.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 61,484 hrs · 68,660 cycles

OVERHEAD EMERGENCY LIGHT IS INOP AT ROW 7. R & R BULB. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,078 hrs · 68,166 cycles

EMERGENCY LIGHTS GO DIM THEN OFF AFTER 30 SECONDS. R & R ALL EMERGENCY LIGHT BATTERIES IAW WC 33-50-05R AND WC 33-50-03Q FOR OPS CHECK

Part: GENERATOR — FAILED (RIGHT) · airframe 59,515 hrs · 66,210 cycles

RIGHT AC BUSS CAUTION LIGHT ILLUMINATED IN FLIGHT WITH ASSOCIATED CAUTION LIGHTS. COULD NOT DUPLICTE ON GROUND RUN. FOUND PROP HEAT SELECTED ON AT THE TIME. INSPECTED WIRING AND CURRENT LIMITERS IN RT AC CONTACTOR BOX. NO DEFECTS NOTED. R & R NR 2 AC GENERATOR AND GCU IAW WORKCARD 24-20-011R. OPS AND LEAK CHECKED GOOD.

Part: BRUSH BLOCK — MALFUNCTIONED (PROPELLER) · airframe 59,191 hrs · 65,848 cycles

EMERGENCY LIGHTS FLICKER IN FLIGHT WITH PROP HEAT ON. INSPECTED NR 2 BRUSH BLOCK. NO DEFECT NOTED. REMOVED BOTH SPINNER AND INSPECTED HEATER LEADS. NO DEFECTS NOTED. REMOVED NR 1 BRUSH BLOCK AND R & R EMERGENCY LIGHT CONTROL BOX. GROUND RUN ACFT. OPS CHECKED GOOD. EMERGENCY LIGHTS FLICKER IN FLIGHT WITH PROP HEAT ON. R & R NR 2 CIRCUIT BREAKER IN AC CONTACTOR BOX. C/B 2421-CB10. PN 2TC12-5. CLEANED GROUND STUD 9811-GS12 BEHIND L/E 612AR. R & R NR 2 BRUSH BLOCK. R & R FUSE 2421-F12 INSIDE OF NR 2 ACFT CONTACTOR BOX. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 59,119 hrs · 65,771 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 6. R & R EMERGENCY FLOOR PATH LIGHT BULB AT ROW 6. REINSTALLED FLOOR STRIP. OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 59,069 hrs · 65,709 cycles

UPON GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED EMERGENCY EXTENSION. GOT GEAR DOWN AND LOCKED INDICATION. R & R NOSE GEAR DRAG STAY/UPLOCK PROX SENSOR AND ADJUSTED AS REQUIRED. CYCLED GEAR 20 TIMES. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: STARTER GEN — FAILED (NR 1) · airframe 59,023 hrs · 65,660 cycles

NR 1 ENGINE START ASSOCIATED WITH BUSS FAULT. R & R NR 1 START GENERATOR IAW WC 24-30-02R. LEAKED AND OPS CHECKED GOOD.

Part: BRUSH BLOCK — INTERMITTENT (PROPELLERS) · airframe 59,022 hrs · 65,658 cycles

EMERGENCY LIGHTS FLICKERED INTERMITTENTLY. R & R BOTH PROP BRUSH BLOCKS IAW 61-10-00.

Part: CONTROL BOX — INTERMITTENT (EMERGENCY LIGHT) · airframe 58,886 hrs · 65,507 cycles

ALL EMERGENCY LIGHTS FLICKERED IN FLIGHT. R & R EMERGENCY LIGHT CONTROL BOX. OPS CHECKED GOOD IAW -8 MM 33-51-00.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,789 hrs · 65,402 cycles

ROW 5 CEILING EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,672 hrs · 65,276 cycles

CEILING EMERGENCY LIGHT IS INOPERATIVE AT ROW 2. R & R EMERGENCY LIGHT BULB ON CEILING AT ROW 2. OPS CHECKED GOOD.

Part: RELAY — MALFUNCTIONED (MLG) · airframe 58,676 hrs · 65,281 cycles

AFTER GEAR RETRACTION, NLG RED UNSAFE AND AMBER INTRANSIT LIGHT REMAINED ILLUMINATED. AFTER 1 MINUTE, LIGHTS EXTINGUSHED. CYCLED GEAR DOWN GREEN LIGHTS ILLUMINATED. REPLACED RELAYS 3261-K5, K6, K7 AND K8. OPS CHECKED GOOD. PSEU TEST WITH NO FAULTS AND NO MEMORY.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 58,628 hrs · 65,228 cycles

ONE EMERGENCY FLOOR LIGHT OUT AT ROW 6DF AND 2 OUT AT ROW 8DF. RELAMPED FLOOR PATH LIGHTS AT ROW 6DF AND ROW 8DF AS REQUIRED. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,374 hrs · 64,914 cycles

EMERGENCY CEILING LIGHT AT ROW 7 IS INOPERATIVE. R & R BULB IN EMERGENCY CEILING LIGHT AT ROW 7 AS REQUIRED. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,272 hrs · 64,816 cycles

1 RED FLOOR EXIT LIGHT AT ROW 1 IS INOPERATIVE. R & R 1 RED FLOOR EXIT LIGHT BULB AT ROW 1.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 57,749 hrs · 64,205 cycles

ROW 2 CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED LENS, R & R BULB AT SAID LOCATION. REINSTALLED LENS.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 57,701 hrs · 64,149 cycles

1 AFT AND 1 FORWARD EMERGENCY FLOOR LIGHT IS NOT WORKING. R & R LAMP.

Part: FLOOR SUPPORT — CORRODED · airframe 57,629 hrs · 64,057 cycles

SLIGHT CORROSION ON STRINGER 23 (FLOOR LEVEL) AT ROW 5DF. POLISHED CORRODED AREA, INSPECTED AND FOUND NO FURTHER DEFECTS. CLEANED, ALODINED AND PRIMED IAW 61-25-03.

Part: FLOOR SUPPORT — CORRODED · airframe 57,629 hrs · 64,057 cycles

AREA OF CORROSION AT STRINGER 23 FLOOR LEVEL FROM ROW 7DF TO ROW 9DF, X456.500 TO X531.500. POLISHED CORRODED AREA, INSPECTED AND FOUND NO FURTHER DEFECTS. CLEANED, ALODINED AND PRIMED AREA IAW AMM 51-25-03.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 57,315 hrs · 63,704 cycles

NR 1 HYD SYS LOST CONTENTS AFTER TAKEOFF. RETURNED TO FIELD. NR1 ENGINE MANUALLY SHUTDOWN NO MORE THAN 8 MINUTES AFTER LOSS. FOUND NR 1 EDP PRESSURE LINE "B" NUT LOOSE UNDER PANEL 412DT. RETORQUE "B" NUT, SERVICED NR 1 HYD, SYS CHECKED GOOD. REINSTALLED PANEL 412DT, SEALED AND RII COMPLIED WITH. CASE DRAIN FILTER INSP REVEALED NO METAL PARTICLES IAW -8, MM 05-50-53.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,161 hrs · 62,444 cycles

EMERGENCY LIGHTS INOP. R & R EMERGENCY LIGHT BATTERIES IAW 33-50-03Q. AFT EGRESS LIGHT ON RT EMERGENCY EXIT INOP, R & R POWER SUPPLY PS6, OPS CHECKED GOOD IAW WORKCARD 33-50-05R AND 33-50-03Q.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 53,000 hrs · 58,844 cycles

6 MILES OUT, BAG BAY SMOKE WARNING LIGHT FLICKERED ABOUT 5 TIMES. UPON OPENING BAG BAY DOOR STRONG ELECTRICAL ODOR WAS NOTED. INSPECTED BAG BAY FOR ELECTRICAL DAMAGE AND NONE FOUND. REMOVED AND REPLACE FWD AND AFT SMOKE DETECTOR IAW 26-10-00 OPS GOOD. MFG PN FOR SMOKE DETECTOR IS PU90-461S.

Part: VALVE — MALFUNCTIONED (DE ICE SYSTEM) · airframe 52,985 hrs · 58,829 cycles

DEICE BOOT'S IN AUTO AND FAST MODE, LT OTBD AND RT INBD BOOTS WILL NOT ILLUMINATE OR INFLATE, TAIL BOOTS ADVISORY LIGHTS LT OTBD AND RT INBD AND OTBD ILLUMINATES SIMULTANEOUSLY. GROUND RAN ACFT UNABLE TO DUPLICATE PROBLEM CONNECTED SHOP AIR TO ACFT RT WING EJECTOR AND LWR TAIL EJECTOR PLUGGED CYCLED EJECTORS. CHECKS GOOD. REPLACED RT WING INBD LT WING INBD AND UPPER TAILS DISTRIBUTOR VALVES IAW 30-10-16 AND BULLETIN 30-3. GROUND RUN AFTER. OPS CHECK GOOD.

Part: DISPLAY — DEFECTIVE (COCKPIT) · airframe 52,323 hrs · 58,094 cycles

DURING FLIGHT FROM SCE TO PHL, THE FLIGHT CREW SAW SMOKE AND SMELLED STRONG ODOR IN THE COCKPIT. DECLARED AN EMERGENCY THROUGH ATC AND LANDED IN INTENDED DESTINATION IN PHL. AN EMERGENCY EVACUATION WAS ORDERED THROUGH ONLY THE PAX DOOR. UPON INSPECTION THE GRAPHIC'S UNIT WAS FOUND BURNED AND INOPERATIVE. REMOVED AND REPLACED GRAPHICS UNIT AND THE OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 51,634 hrs · 57,359 cycles

ROW ONE DF SIDE WALL EMERGENCY EXIT LIGHT DIM. REMOVED AND REPLACED LIGHT BULBS IN ACCORDANCE WITH MAINTENANCE MANUAL 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,634 hrs · 57,359 cycles

FLOOR EMERGENCY LIGHT ROW 1 INOPERATIVE. REMOVED AND REPLACED LIGHT BULB IN ACCORDANCE WITH MAINTENANCE MANUAL 33-51-00.

Part: FILTER ELEMENT — SLOW (NR 1 ENGINE) · airframe 50,932 hrs · 56,609 cycles

NR 1 OIL PRESSURE LIGHT ILLUMINATED ON TAKEOFF ROLL WITH FLUCTUATION ON PRESSURE GAUGE. REJECTED TAKEOFF, LIGHT EXTINGUISHED REMAINED NORMAL. CONTRACT MAINTENANCE REPORTS SAFETY ON TRANSMITTER BROKEN AND CONNECTOR OIL SOAKED. CLEANED AND SERVICED ENGINE WITH 2 QTS OF OIL. PERFORMED HIGH POWER AND HIGH SPEED TAXI ALL INDICATIONS REMAIN NORMAL THROUGH ALL ABOVE STEPS. PLANE RELEASED FOR FERRY FLIGHT FROM ROC TO MDT. C/W LOW OIL PRESS IN PWMM 05-50-00. NO DEBRIS FOUND. INSTALLED NEW OIL FILTERS, NO EXTERNAL LEAKS FOUND ON ENGINE AFTER GROUND RUN. OPS AND LEAK CHECK GOOD.

Part: B-NUT — LOOSE (HYDRAULIC SYS) · airframe 50,749 hrs · 56,411 cycles

AIRCRAFT EN ROUTE FROM LGA TO ROA, THEN DIVERTED INTO LYH DUE TO WEATHER. IN LYH CREW FOUND FLUID DRIPPING FROM NR 2 NACELLE. MAINT CLEANED SUSPECTED AREA, GROUND RAN AIRCRAFT OPERATED FLAPS, SPOILERS, AND BRAKES. NO LEAKS NOTED AT THIS TIME. 10/10/2008 AIRCRAFT DUE INTO RON AT ROA TO UNDER GO MORE INVESTIGATION OF POSSIBLE LEAK. ROA MAINT FOUND LOOSE B-NUTS ON THE STANDBY PUMP. TIGHTED B-NUTS AS REQUIRED, OPERATED HYD SYSTEM, OPS/LEAK CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,419 hrs · 54,917 cycles

THE 3RD EMERGENCY FLOOR PATH LIGHT INOP. REMOVED AND REPLACED LAMP, OPS CHECKED GOOD.

Part: RELAY — SLOW (LANDING GEAR) · airframe 48,968 hrs · 54,431 cycles

WHILE CLIMBING THROUGH 11,000 FOOT ALTITUDE, THE AIRCRAFT CREW ELECTED TO TEST THE LANDING GEAR SYSTEM. ON EXTENSION, IT WAS NOTED THAT THE GEAR DOORS WERE TAKING A LONGER THAN NORMAL TIME TO CLOSE. MAINTENANCE WAS CONTACTED AND THE DECISION WAS MADE TO RETURN TO A MAINTENANCE BASE. MAINTENANCE CHANGED OUT THE TIME DELAY RELAY, 3261-K9, AND PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM. CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUT — LEAKING (OVERHEAD BIN) · airframe 48,387 hrs · 53,820 cycles

HYD/OIL LEAKING FROM PSU AREA ROW 4/5 RIGHT SIDE. CAPT RETURNED TO FIELD WITHOUT CONTACTING MX OR DISPATCH. HISTORY FROM PREVIOUS DAY, SAME DISCREPANCY OVERHEAD BIN WAS MEL'D DUE TO STRUT LEAKING. FLUID FOUND LEAKING FROM ROW 5 OVERHEAD BIN FWD GAS STRUT. OVERHEAD BIN PREVIOUSLY MEL'D. CLEANED AREA PLACARD BIN NOT TO BE USED. SBY MAINTENANCE REMOVED SIDEWALL PANEL AND EXAMINED HYDRAULIC LINES FROM OVERHEAD TO WAIST LVL. NO LEAKS NOTED. REMOVED AND REPLACED BOTH SNUBBERS FOR OVERHEAD BIN 5F.

Part: VALVE — MALFUNCTIONED (HYD SYSTEM) · airframe 47,861 hrs · 53,250 cycles

AT 20 MILES OUT OF MHT, THE FLIGHT CREW SAW THE NUMBER TWO HYDRAULIC QUANTITY DROP TO TWO QUARTS. ALSO, NOTICED THE NUMBER ONE HYDRAULIC QUANTITY DROP TO ONE AND ONE HALF QUARTS. THE NUMBER TWO HYDRAULIC QUANTITIES THEN STARTED DROPPING BELOW TWO QUARTS AMOUNT. THE CREW SLOWED THE AIRCRAFT DOWN AND LOWERED THE LANDINTG GEAR AND FLAPS. AN EMERGENCY WAS DECLARED AND DIVERTED IN TO BDL. THE FLIGHT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED UNLOADING VALVE FOR OUTBOARD RIGHT. SPOILER OPS AND LEAK CHECK GOOD.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 46,700 hrs · 52,002 cycles

CORROSION FOUND ON PAX DOOR THRESHOLD AROUND ANCHOR NUT. REPLACED PAX DOOR THRESHOLD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 46,711 hrs · 52,002 cycles

CORROSION FOUND AT INTERCOSTAL AT PAX DOOR ENTRANCE. REPLACED INTERCOSTAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,711 hrs · 52,002 cycles

FRAME ON DOUBLER IS CRACKED AT X129.00 AND X136.800. REPAIRED PER ED8-53-3541.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 46,711 hrs · 52,002 cycles

SURFACE CORROSION FOUND IN PAX DOOR AFT GOOSENECK DRAIN PAN. REPLACED BRACKET.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 46,252 hrs · 51,415 cycles

FIRST 3 RED EMERGENCY FLOOR LIGHTS ARE INOPERATIVE. ALSO 1 WHITE FLOOR LIGHT IS INOP. FOUND BROKEN WIRE ON FLOOR LIGHTING. REPAIRED WIRE.

Part: PROPELLER — MALFUNCTIONED (NR 1 ENGINE) · airframe 42,790 hrs · 47,730 cycles

AFTER TAKEOFF AT APPROX 100 AGL THE NR 1 ENGINE CYCLED 10 PERCENT TQ ALONG WITH POWER UPTRIM LIGHT CYCLING ON AND OFF WITH BOTH PROP RPM'S AT 1200.

Part: ANTENNA — FAILED (WX RADAR SYS) · airframe 42,365 hrs · 47,244 cycles

RADAR ANTENNA FAULT. REMOVED AND REPLACED RADAR RT, OPS CHECK GOOD.

Part: ANTENNA — FAILED (WX RADAR SYS) · airframe 42,365 hrs · 47,244 cycles

RADAR ANTENNA FAULT. REMOVED AND REPLACED RADAR RT, OPS CHECK GOOD.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,557 hrs · 45,260 cycles

DURING C CHECK, FOUND CORROSION OF AFT CAP ANGLE OF THE FPB AT STR 31 STARBOARD AND STR 31 PORT. REPAIRED IAW EO8-53-04-0423 BY PERFORMING ANGLE SPLICE IAW INTENT OF PREVIOUSLY APPROVED RD8-53-1395. NOTE THAT THE 85310026 SKIN IS CUT FOR ACCESS AND IS SPLICED BACK IN.

Part: ATTACH FITTING — CORRODED (LAVATORY) · corrosion level 2 · airframe 40,557 hrs · 45,260 cycles

LAV ADAPTER IS CORRODED. REPLACED LAV ADAPTER MOUNTING FLANGE.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,557 hrs · 45,260 cycles

AIRSTAIR DOOR THRESHOLD IS CORRODED. REMOVED AND REPLACED THRESHOLD.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,557 hrs · 45,260 cycles

AIRSTAIR DOOR THRESHOLD IS CORRODED. REMOVED AND REPLACED THRESHOLD.

Part: ADAPTER — CORRODED (LAVATORY) · corrosion level 2 · airframe 40,577 hrs · 45,260 cycles

FOUND LEVEL 2 CORROSION ON LAV ADAPTER MOUNTING FLANGE.

Part: COMPUTER — FAILED (ADC NR 1) · airframe 40,163 hrs · 44,839 cycles

AFTER TAKEOFF ADC 1 FAILED. NR 1 ALTIMETER AND IVSI FLAGGED, TRANSPONDER FAILED, OVERSPEED WARNING HORN SOUNDED AND GPWS C.L. OVERSPEED WARNING HORN SILENCED WHEN ADC 1 CB PULLED. REMOVED AND REPLACED DADC, SELF TEST GOOD.

Part: SEAT TRACK — CORRODED · airframe 34,699 hrs · 39,101 cycles

During 40K inspection the right hand inboard seat rail was found to be corroded at fastener holes for the lav. and galley. The damaged portion of the seat track was removed and a new section spliced in per RD8-53-3074.

Part: STRINGER — CORRODED · airframe 34,699 hrs · 39,101 cycles

During 40K inspection corrosion was found along the length of stringer 31S. The stringer was changed along with several tension fittings and frame legs along the length of stringer 31S.

Part: SKIN — CORRODED · airframe 34,699 hrs · 39,101 cycles

During 40K inspection corrosion was found on the interior of the A/C in the center of a bay between frames 202 and 222 and between stringers 32 left and right. The corroded area was cut out and a doubler installed per EO8-53-02-0228.

Part: FITTING — CRACKED (NR 1 NACELLE) · airframe 34,699 hrs · 39,101 cycles

DURING REPAIR OF THE NR 1 NACELLE HORSE COLLAR THE INTERNAL TOP MOUNT FITTING WAS FOUND CRACKED AT THE TOP AFT CORNER FROM THE RADIUS TO THE EDGE OF THE ATTACH FLANGE. THE CRACK ENCIRCLES THE TOP RIVET OF THE AFT ATTACH FLANGE. REMOVED AND REPLACED THE FITTING.

Part: HYD LINE — CHAFED (NR 1 HYD SYS)

NR 1 HYD SYS QUANTITY LOSS INFIGHT HAD TO DECLARE EMERGENCY LANDING. REMOVED AND REPLACED CHAFED LINE ANTI-SKID VALVE AND INSTALLED TFL. SERVICED 6 QTS IN NR 1 SYS, LEAK AND OPS CHECK GOOD.

Part: BOLT — OUT OF POSITION (AIRSTAIR)

FLT 3147 - DCA-BWI - UPON LANDING IN BWI, THE AIRSTAIR DOOR WOULD NOT OPEN FROM THE INSIDE. FOUND BOLT FELL FROM AIRSTAIR HANDRAIL. SECURED HARDWARE FOR FORWARD DOOR SUPPORT. (M)

Part: SELECTOR VALVE — FAILED (LANDING GEAR)

FLT NR 3166 - MCO-TCB - THE LANDING GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. PERFORMED ALTERNATE GEAR EXTENSION AND LANDED IN TCB WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE. (M)