N941HA

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 67,190 hrs · 75,716 cycles

NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED IN FLIGHT. CREW SHUT DOWN NR 2 BLEED AD PER CHECKLIST, THEN NR 1 BLEED HO CAUTION LIGHT CAME ON, WAS SHUT OFF. RETURNED TO FIELD......GROUND RAN AND OPERATED BLEED SYSTEM NUMEROUS TIMES. NO DEFECTS NOTED. INSPECTED HP BLEED VALVES AND CONNECTORS FOR OBVIOUS DEFECTS. NONE NOTED. OK FOR SERVICE.

Part: ELEC CONNECTOR — DAMAGED (ROLL SPOILER) · airframe 66,895 hrs · 75,390 cycles

DURING CLIMBOUT, ROLL SPOILER INBOARD HYDRAULIC CAUTION LIGHT ILLUMINATED. REMOVED AND REPLACED THE CONNECTOR. OPS CHECKED GOOD. OK FOR SERVICE.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 66,876 hrs · 75,367 cycles

DURING CLIMB OUT AT ABOUT 11K, BOTH NR 1 HYDRAULIC ISO AND ROLL SPOILER INBOARD CAUTION LIGHTS ILLUMINATED WITH NR 1 HYDRAULIC QUANTITY RAPIDLY DROPPING TO .7 QUARTS. HYDRAULIC PRESSURE REMAINED AT 3000. NSPECTED AND FOUND PRESSURE FITTING ON NR 1 EDHP LOOSE AND LEAKING. REMOVED AND REPLACED THE O-RING AND INSPECTED CASE DRAIN HYDRAULIC FILTER. NO CONTAMINATION FOUND. SERVICED NR 1 HYDRAULIC QUANTITY . GROUND RAN GOOD. LEAKED CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,589 hrs · 75,013 cycles

SECOND FLOOR EMERGENCY FLOOR PATH LIGHT INOPERATIVE. R & R BULB AT SECOND FLOOR EMERGENCY FLOOR PATH LIGHT.

Part: INDICATOR — MALFUNCTIONED (WX RADAR) · airframe 66,324 hrs · 74,696 cycles

WEATHER RADAR WILL NOT PAINT KNOWN WEATHER OR AND/OR INTENSITY. CLEANED AND RESEATED WX RADAR INDICATOR. OPS GOOD, IAW 34-41-04.

Part: BATTERY — OVERTEMP (MASTER) · airframe 65,843 hrs · 74,131 cycles

AUXILIARY BATTERY TEMP AT 38 PRIOR TO T/O, IN CRUISE, SLOWLY ROSE TO 55 WITH A LOAD OF 25 PERCENT AND BOTH TEMP CAUTION LIGHT ILLUMINATING. BATTERY SELECTED OFF AND TEMP INCREASED TO 75 DEGREES PRIOR TO LANDING. MAINTENANCE NOTIFIED OF RT TRIP TO REPLACE AUXILIARY BATTERY.

Part: SEQUENCE VALVE — MALFUNCTIONED (MLG) · airframe 65,632 hrs · 73,870 cycles

ILLUMINATION OF 2 MLG DOOR LIGHTS AND ILLUMINATION OF RED GEAR. R & R PSEU AND NOSE GEAR SOLENOID SEQUENCE VALVE. OPS AND LEAKED CHECKED GOOD IAW 32-30-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 65,537 hrs · 73,756 cycles

FLOOR EMERGENCY LIGHTS IN CABIN 9TH FROM FRONT INOPERATIVE. R & R EMERGENCY LIGHT FLOOR PATH LIGHT BULB AND RESECURED LIGHT COVER.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 65,501 hrs · 73,710 cycles

DIM AT EMERGENCY LIGHT ON, LT OF FUSELAGE. R & R BULB. OPS CHECKED GOOD.

Part: INVERTER — ODOR · airframe 64,874 hrs · 72,962 cycles

AUX INVERTER CAUTION LIGHT ILLUMINATED IN FLIGHT. CIRCUIT BREAKER TRIPPED WITH ODOR AND SMOKE COMING FROM AUX INVERTER AREA. R & R AUX INVERTER IAW 24-22-00. OPS CHECKED GOOD. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN · airframe 64,849 hrs · 73 cycles

TROUBLESHOT UNCOMMANDED LT TURN WITH AUTOPILOT ENGAGED, NR 802 MESSAGE OR CAUTION LIGHTS NOTED. INSPECTED AILERON SERVO AND CABLE FOR PROPER INSTALLATION, NO DEFECT. PERFORMED OPS MAINTENANCE ST FOR 45 MINUTES. FLYING WITH LT AND RT AFCS MASTER AND FLYING WITH LT AND RT HSI SELECTED. NO DEFECTS. PERFORMED GROUND MAINTENANCE TEST. DID NOT REVEAL ANY FAULT, COULD NOT DUPLICATED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,659 hrs · 72,695 cycles

FLOOR EMERGENCY LIGHTS ARE INOPERATIVE AT ROW 1, FURTHER MOST FROM THE FRONT AND ROW 9. R & R THE EMERGENCY LIGHT BULBS. OPS CHECKED GOOD.

Part: LIGHT — UNKNOWN (CABIN) · airframe 64,189 hrs · 72,109 cycles

EMERGENCY LIGHTS FLICKERED DURING FLIGHT. GROUND RAN ACFT. OPERATED EMERGENCY LIGHTS. NO DEFECTS NOTED.

Part: WIRE — CHAFED (BRUSH BLOCK) · airframe 64,179 hrs · 72,097 cycles

EMERGENCY LIGHTS FLICKERED IN FLIGHT. REPAIRED CHAFED WIRE AT RT ENGINE BRUSH BLOCK WIRE HARNESS. R & R RT NR 3 BLADE PROP DEICE LEADS IAW MM 66-10-00 AND MM 20-45-10. GROUND RAN ACFT. OPS CHECKED GOOD AT THIS TIME.

Part: GCU — WARNING LIGHT (NR 1) · airframe 63,845 hrs · 71,700 cycles

DURING CLIMBOUT AT 13,000 FEET, NR 1 DC GENERATOR FAILED WITH CIRCUIT BREAKER E5 ADCI, E3 NAV SWITCH ANN, A3 O/H CONS AND B3 PLT FLT POP. BUSS DID TIE. R & R NR 1 DC GEN. IAW WC 24-30-02R, NR 1 DC GCU IAW MM 24-31-03, RESET CIRCUIT BREAKER AND GROUND RAN ACFT. OPS AND LEAKED CHECKED GOOD AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,840 hrs · 71,693 cycles

MOST FORWARD FLOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. R & R BULB A FWD FLOOR EMERGENCY EXIT LIGHT. OPS CHECKED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 63,774 hrs · 71,603 cycles

EMERGENCY LIGHTS WILL NOT TEST. R & R EMERGENCY LIGHT BATTERIES IAW WC 33-50-03Q. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,575 hrs · 71,368 cycles

EMERGENCY EXIT KNEE SIN IS INOPERATIVE AT ROWS 1DF AND 4DF. REMOVED LENS COVER, R & R BULBS. OPS CHECKED GOOD. REINSTALLED LENS COVER.

Part: SEAT TRACK — CORRODED (BS 206) · airframe 63,564 hrs · 71,360 cycles

RIGHT INBD SEAT TRACK HAS CORROSION BS 206. BLENDED, ALODINE AND PRIMED IAW RD8-53-4689. COMPLIED WITH HFEC INSPECTION. NO DEFECTS NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,343 hrs · 71,089 cycles

LEFT AND RT KNEE EMERGENCY EXIT SIGNS ARE DIM AT ROW 4. R & R BULBS. OPS CHECKED GOOD.

Part: SWITCH — MALFUNCTIONED (WARNING HORN) · airframe 63,108 hrs · 70,802 cycles

TAKEOFF WARNING HORN SOUNDED DURING POWER LEVER ADVANCEMENT. ACFT CONFIGURED CORRECTLY AND FLAPS INDICATING NORMAL. REMOVED THE SWITCH AND REPLACED ROLLER/ACTUATOR AND INSTALLED THE SWITCH. ADJUSTED AND RIGGED ROLLER IAW MM 76-10-00, SWITCH IAW MM 27-36-00. TESTED RT FLAP RVDT IAW PDT BULLETIN. TEST NORMAL

Part: INDICATOR — MALFUNCTIONED (TE FLAPS) · airframe 63,098 hrs · 70,792 cycles

TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF ROLL WHEN POWER LEVERS ADVANCED. TAKEOFF ABORTED. R & R FLAP POSITION INDICATOR AND PERFORMED OPS CHECK IAW MM 27-53-05. OPS CHECKED GOOD. PERFORMED TAKEOFF WARNING SYS CHECK, OPS CHECKED GOOD.

Part: WARNING HORN — FALSE ACTIVATION (TAKEOFF) · airframe 63,098 hrs · 70,792 cycles

TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF ROLL WHEN POWER LEVERS ADVANCED. TAKEOFF ABORTED. POWERED DOWN AND POWERED UP. CYCLED CIRCUIT BREAKER AND CONFIGURED ACFT. OPS CHECKED NORMAL AT THIS TIME. OK FOR SERVICE.

Part: WARNING HORN — FALSE ACTIVATION · airframe 63,083 hrs · 70,772 cycles

TAKEOFF WARNING HORN SOUNDED AS TAKEOFF POWER WAS APPLIED, CYCLED TRIM AND HORN SILENCED. COMPLIED WITH TAKEOFF WARNING WC 31-50-00. NO DEFECTS NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,805 hrs · 70,438 cycles

EMERGENCY LIGHT IS INOPERATIVE 3RD FROM THE FRONT. R & R BULB. OPS CHECKED GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 62,530 hrs · 70,083 cycles

EMERGENCY LIGHTS SELECTED, FUSELAGE LIGHTS MOMENTARILY CAME ON AND THEN WENT OFF. R & R EMERGENCY LIGHT POWER SUPPLIES IAW WC 33-50-05. OPS CHECKED GOOD.

Part: WIRE — BROKEN (BLEED AIR VALVE) · airframe 61,895 hrs · 69,295 cycles

DURING FLIGHT, ACFT WAS AT 5000 FT, CABIN ALTITUDE WAS ABOUT 2000 FT. CAPTAIN TURNED OFF BLEEDS, ACFT CONTINUED TO PRESSURIZE DOWN TO APPROXIMATELY 500 FT. CABIN ALTITUDE WITH BOTH BLEEDS REMAINING IN THE OFF POSITION. AFTER RETURN, FOUND BROKEN WIRE 2121-2F22 IN NR 1 NACELLE. ALSO, FOUND NR 2 PRSOV INOPERATIVE. R & R NR 2 PRSOV IAW MM 21-11-11. GROUND RAN ACFT. OPS CHECKED GOOD AT THIS TIME.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 61,093 hrs · 69,047 cycles

INFLIGHT, NR 2 HYD ISOLATION VALVE CAUTION LIGHT ILLUMINATED AND ASSOCIATED LOSS OF NR 2 HYD QTY, NR 2 SYSTEM .7 REMAINS. FOUND NR 2 SYSTEM PRESSURE LINE LEAKING IN FLAP WELL BETWEEN FUSELAGE AND NR 1 NACELLE. REMOVED RIDGED LINE AND INSTALLED TEMP FLEX LINE IAW SPEC PROCEDURE 20.1. LEAKED CHECKED GOOD AT THIS TIME.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 61,417 hrs · 68,721 cycles

NR 2 HYDRAULIC QTY SLOWLY DROPPED. ISOLATION LIGHT ILLUMINATED FOR APPROX 2 MINUTES, THEN EXTINGUISHED. ENGINE DRIVEN PUMP CAUTION LIGHT ILLUMINATED AND REMAINED ON. INSPECTED AND FOUND NR 2 ENGINE HYDRAULIC PUMP LEAKING. R & R PUMP IAW 72-00-04L. ALSO, R & R CASE DRAIN FILTER IAW 29-12-03R. SERVICED HYDRAULICS AND BLED SYSTEM. OPS AND LEAKED CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,145 hrs · 68,382 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,913 hrs · 68,106 cycles

EMERGENCY EXIT DOOR PATH LIGHT IS INOPERATIVE AT ROW 6DF. R & R LAMP AT EMERGENCY EXIT FLOOR PATH LIGHT. OPS CHECKED GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 60,832 hrs · 68,001 cycles

CABIN, EMERGENCY EXIT SIGN ON CENTER AISLE AT ROW 1 IS DIM. R & R EMERGENCY LIGHT THAT WERE DIM AT CENTER AISLE AT ROW 1. OPS CHECKED GOOD REINSTALLED COVER.

Part: ACTUATOR — OUT OF ADJUST (MLG DOOR) · airframe 60,457 hrs · 67,544 cycles

LEFT MAIN GEAR DOOR LIGHT ILLUMINATED DURING CRUISE FLIGHT. GEAR DOOR WAS VERFIED TO BE OPEN WITH GEAR UP AND LOCKED. R & R LT MAIN FORWARD GEAT DOOR ACTUATOR. FOUND BUSHING WORN IN ACTUATOR LEVER. RIGGED FWD DOOR ACTUATOR IAW AMM 32-10-36. OPS AND LEAKED CHECKED GOOD.

Part: ACTUATOR — INOPERATIVE (MLG DOOR) · airframe 60,141 hrs · 67,154 cycles

RIGHT AMBER GEAR DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW CYCLED GEAR IAW CHECKLIST. LIGHTS REMAINED ON WITH GEAR DOOR OPEN. REMOVED MAIN GEAR DOOR ACTUATOR IAW MM 32-10-36. INSTALLED NEW GEAR DOOR ACTUATOR IAW DASH 8 MM 32-10-36.

Part: BOLT — BROKEN (MLG ACTUATOR) · airframe 60,137 hrs · 67,147 cycles

AFTER TAKEOFF AND GEAR RETRACTION, RED UNSAFE LIGHT REMAINED ILLUMINATED FOR LT MAIN. PERFORMED ALTERNATE EXTENSION IAW ABNORMAL CHECK LIST, ALL GREEN FOR ALTERNATE INDICATION. FOUND UPPER BOLT BROKEN ON MLG RETRACT ACTUATOR FITTING. R & R FITTING AND ALL BOLTS IAW MM 32-30-11. FCD8-54-95-162A WAS ACCOMPLISHED FOR LT SIDE. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 59,959 hrs · 66,934 cycles

F/A EMERGENCY SWITCH "GREEN" LIGHT IS INOPERATIVE. R & R F/A EMERGENCY SWITCH GREEN LIGHT. RE-SECURED LENS, OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 59,881 hrs · 66,834 cycles

EMERGENCY FLOOR PATH LIGHT HAS VERY DIM LIGHT AT ROW 8. R & R BULB IAW MM 33-51-00.

Part: STRUT — DISCHARGED (NLG) · airframe 59,617 hrs · 66,505 cycles

ON GEAR RETRACTION, WW YELLOW CAUTION LIGHT AND NOSE GEAR ADVISORY LIGHT ILLUMINATED. ALSO A GRINDING NOISE FROM NOSE BAY HEARD. FOUND NLG SERVICING LOW. SERVICED ALL LANDING GEAR IAW MM 12-10-32. SWUNG GEARS. OPS CHECKED GOOD.

Part: STRUT — LOW PRESSURE (NLG) · airframe 59,616 hrs · 66,503 cycles

ON GEAR RETRACTION WOW CAUTION LIGHT AND NOSE GEAR YELLOW ADVISORY ILLUMINATED. A GRINDING NOISE FROM NOSE BAY HEARD. FOUND NLG SERVICING WAS LOW. SERVICED ALL LANDING GEAR IAW MM 12-10-32. GEAR SWINGS OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,616 hrs · 66,503 cycles

CENTER CEILING EMERGENCY LIGHT IS INOPERATIVE. INSTALLED NEW BATTERY. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 59,356 hrs · 66,190 cycles

ROW 5 CEILING EMERGENCY LIGHT IS INOPERATIVE. REMOVED LENS. R & R BULB, AT SAID LOCATION. REINSTALLED LENS.

Part: LEVER — OUT OF ADJUST (CONDITION) · airframe 59,356 hrs · 66,191 cycles

WITH BOTH CONDITION LEVERS SELECTED TO MAX ON LANDING WITH TORQUE SELECTED BETWEEN 20 TO 40 PERCENT MAX. NP WAS 1150 TO 1165. ENGINES RIGGED IAW WC 76-00-01. GROUND RAN ACFT TO MAX PROP AND WAS FOUND TO BE WITHIN LIMITS IAW SRT MANUAL.

Part: PULLEY — STIFF (CONTROL YOKE) · airframe 59,356 hrs · 66,191 cycles

IN FLIGHT, WITH MORE THAN 10 DEGREES RT DEFLECTION OF THE YOKE CONTROL, FORCE WAS HEAVY. INSPECTED AND FOUND 2 GUIDE PULLEYS STIFF FOR THE RT WING. REMOVED BOTH PULLEYS. YOKES MOVE FREELY. PULLEYS REMOVED WERE AT RT SIDE OF GUSTLOCK. RE-VERFIED CABLE TENSIONS ON BOTH CABLE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,356 hrs · 66,190 cycles

EMERGENCY EXIT LIGHT ABOVE ROW 1 EMERGENCY EXIT HAS NUMEROUS BULBS THAT ARE INOP. REMOVED EXIT LIGHT LENS. SOLDERED SEVERAL LIGHT SOCKETS FOR INDIVIDUAL BULBS THAT WERE MISSING. REINSTALLED LIGHT ASSY AND LIGHT LENS COVER.

Part: WARNING LIGHT — FALSE ACTIVATION (NLG) · airframe 59,356 hrs · 66,191 cycles

UPON GEAR RETRACTION, WOW CAUTION LIGHT, NOSE GEAR UNSAFE AND LT AND RT AMBER GEAR DOOR LIGHTS ILLUMINATED. RACKED PSEU. CYCLED GEAR NUMEROUS TIMES. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,356 hrs · 66,190 cycles

FORWARD RT EMERGENCY LIGHT INOPERATIVE. REINSTALLED FORWARD RT EXIT.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,356 hrs · 66,190 cycles

CORROSION AT LAVATORY, BELOW ORANGE TUBE AT LAV BOX. REMOVED CORRODED MACHINED FITTING. DRILLED NEW FITTING AND INSTALLED IAW DWG 85320983.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,356 hrs · 66,190 cycles

PAX DOOR THRESHOLD HAS SEVERAL AREAS OF CORROSION. R & R THRESHOLD ASSY IAW DWG 85321241.

Part: BULB — FAILED (BACK LIGHT) · airframe 59,277 hrs · 66,091 cycles

F/A PANEL EMERGENCY SWITCH BACKLIGHTING IS INOPERATIVE. R & R BULB.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,226 hrs · 66,025 cycles

LEFT AFT EMERGENCY EXIT, FORWARD ROW 4 AND 7 OVERHEAD LIGHTS ARE INOPERATIVE. R & R EMERGENCY LIGHT BATTERY IAW WC 33-50-05R. OPS CHECKED GOOD.

Part: INVERTER — ODIFEROUS (COCKPIT) · airframe 59,097 hrs · 65,868 cycles

STRONG FISHY ODOR IN COCKPIT. R & R AUX INVERTER REF 24-22-00, OPS CHECKED GOOD, NO ODOR FOUND. OK FOR SERVICE.

Part: CONTROLLER — FAILED (AFCS) · airframe 58,898 hrs · 65,626 cycles

IN FLIGHT, ACFT LOST BOTH YAW DAMPER CARROTS, RT AUTO-PILOT CARROT, F/O FLIGHT DIRECTOR FLAGGED AND ALTITUDE SELECT INOPERATIVE ON CAPTAINS SIDE. FLIGHT DATA INVALID MESSAGE ON CAPTAINS SIDE. R & R AFCS CONTROLLER. OPS CHECKED GOOD IAW SPZ8000. GROUND MX TEST.

Part: UNKNOWN — ODOR (CABIN) · airframe 58,826 hrs · 65,531 cycles

STRONG ELECTRICAL ODOR NEAR PASSENGER DOOR AREA. INSPECTED ACFT FOR POTENTIAL ELECTRICAL FIRE. NO DEFECTS FOUND. OK FOR SERVICE AT THIS TIME.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,252 hrs · 64,812 cycles

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

Part: OIL SYSTEM — LOW (NR 2 ENGINE) · airframe 58,224 hrs · 64,781 cycles

NR 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED AT 95 KNOTS. INSPECTED NR 2 ENGINE AND NO LEAKS NOTED. SERVICED NR 2 ENGINE WITH 3 QTS OF OIL. CHECKED NR 1 ENGINE AND SERVICED WITH 2 QTS OF OIL. CREW GROUND RAN ACFT. NO WARNING LIGHTS NOTED.

Part: ACTUATOR — SLOW (LT MLG) · airframe 58,058 hrs · 64,592 cycles

LT MAIN GEAR DOOR SLOW TO CLOSE. R & R MAIN GEAR FORWARD DOOR ACUATOR IAW -8 MM 32-10-36. SWUNG GEAR WITH OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (MLG DOORS) · airframe 57,481 hrs · 63,904 cycles

RT GEAR DOOR REMAINED OPEN AFTER GEAR RETRACTION. CYCLED GEAR IAW CHECKLIST. DOOR CLOSED, BUT OPENED AGAIN. INBD CREW REPORTS NO DEFECTS NOTED. SWUNG GEAR MANY TIMES. NO DEFECTS NOTED. OK FOR SERVICE AT THIS TIME. ALSO CLEANED AND LUBED FORWARD DOOR UPLOCK ROLLERS. OPS CHECKED ON GEAR SWINGS.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 57,329 hrs · 63,744 cycles

EMERGENCY OVERHEAD LIGHT IN ROW 7 IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: WIRE — BURNED (DETECTION SWITCH) · airframe 57,227 hrs · 63,627 cycles

TESTED CAPTAINS ICE DETECTION LIGHT SWITCH. SWITCH WAS STICKING AND ELECTRICAL ODOR DETECTED AFTER PRESSING SWITCH. SMALL TRACE OF SMOKE OBSERVED IN COCKPIT. ICE DETECTOR LIGHTS DAY OPS PERFORMED HIDDEN DAMAGE INSPECTION. NO DEFECTS FOUND. CAPPED AND STOWED LIGHT WIRES SB 20-9. R & R CAPTAINS ICE DETECTION LIGHT SWITCH AS REQUIRED. RECONNECTED LIGHT WIRES. OPS CHECKED GOOD.

Part: CAUTION PANEL — FAILED (MASTER) · airframe 57,304 hrs · 63,711 cycles

NR 1 AC GENERATOR FAILED. RESET THEN FAILED AGAIN. R & R AC GCU IAW 24-21-02 AND AC GENERATOR IAW WORKCARD 24-20-11R. OPS AND LEAKED CHECKED GOOD. NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED IN FLIGHT 2 TIMES LASTING 3 SECONDS EACH WITH NO MASTER CAUTION LIGHT. R & R MASTER CAUTION PANEL. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 57,217 hrs · 63,616 cycles

2ND EMERGENCY EGRESS LIGHT ON FLOOR IS INOP. R & R BULB. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 56,487 hrs · 62,747 cycles

F/A EMERGENCY LIGHT SWITCH IS NOT BACK LIGHT. RELAMPED, OPS CHECKED GOOD. OK FOR SERVICE.

Part: OIL SYSTEM — LOW (NR 2 ENGINE) · airframe 56,181 hrs · 62,398 cycles

REJECTED TAKEOFF AT 70 KNOTS. MASTER WARNING LIGHT ILLUMINATED AND NR 2 ENGINE OIL PRESSURE WARNING LIGHT. INSPECTED NR 2 ENGINE FOR EVIDENCE OF OIL LEAKS. NONE FOUND. INSPECTED CONNECTOR PLUG, NR 2 OIL PRESSURE SWITCH. NO DEFECTS NOTED. FOUND NR 2 OIL QTY LOW, SERVICED WITH 4.5 QTS. GROUND RAN ACFT, OPS AND LEAKED CHECKED GOOD. OK FOR SERVICE.

Part: CONTROL PANEL — FAILED (MASTER CAUTION) · airframe 55,853 hrs · 62,020 cycles

MULTIPLE CAUTION LIGHTS CAME ON DURING TAKEOFF ROLL AND TAXI. R & R MASTER CAUTION PANEL IAW -8, MM 33-12-01. GROUND RAN ACFT. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR SYS) · airframe 55,150 hrs · 61,213 cycles

WEATHER RADAR SHOWS IN FLIGHT 6 MESSAGES AND DOES NOT PAINT WEATHER. R & R RADAR ATTENNA R/T. SYS CHECKED GOOD IAW 34-41-04 AND PMB 34-18. SYS HAS HISTORY, INSPECTED AND CLEANED CONNECTOR 3441-P1001 AND 3441-P1 AND 3441-J1 AS PRECAUTIONARY MEASURE. ALL WIRING AND CONNECTOR PINS ARE IN GOOD CONDITION. CONTINUITY CHECKS GOOD ON 453 DATA BUS.

Part: OIL SYSTEM — LOW (NR 2 ENGINE) · airframe 53,950 hrs · 59,904 cycles

NR2 ENGINE OIL PRESSURE DROPPED AND WARNING LIGHT ILLUMINATED WITH ADVANCING POWER LEVERS. SERVICED NR1 AND NR2 ENGINE OIL WITH 2.5 QTS EA IAW 12-20-79. GROUND RAN ACFT. NO DEFECTS NOTED AT THIS TIME.

Part: STUD — LOOSE (RT AILERON) · airframe 53,656 hrs · 59,568 cycles

RIGHT AILERON INBD BONDING STUD SPINS. REPAIRED BONDING STUD IAW EO8-57-10-0263.

Part: SKIN — DAMAGED (NR 2 NACELLE) · airframe 53,656 hrs · 59,568 cycles

ABOUT 10 RIVETS ARE WORKING ON OTBD SIDE OF NR2 NACELLE AT XN134.68 TO ZN 24.60 (BELOW AND AFT OF OTBD IGNITER BAY DOOR). REPAIRED IAW EO8-54-10-0275.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,593 hrs · 59,490 cycles

RT AFT EXTERIOR EMERGENCY LIGHT NOT WORKING. R & R BULB, REINSTALLED LENS.

Part: RELAY — FAILED (AUTOFEATHER SYS) · airframe 53,548 hrs · 59,432 cycles

DURING TAKEOFF ROLL, AUTOFEATHER ARM LIGHT DID NOT ILLUMINATED. R & R RELAY 6121-K5 (AUTOFEATHER ARM CONTROL RELAY). GROUND RAN ACFT IAW DASH 8 RUN UP MANUAL.OPS GOOD AT THIS TIME.

Part: AHRS — MALFUNCTIONED (NR 1) · airframe 53,422 hrs · 59,289 cycles

IN FLIGHT HOLDING AND IN TURBULENCE, NR 1 AHRS FAILED, BOTH CHANNELS OF YAW DAMPER AND FLIGHT DIRECTOR FAILED. SAHS CORRECTED AHRS. ACFT RETURNED TO FIELD DUE TO WEATHER. POWER DOWN AND POWER UP ACFT AND ALL SAID SYS WORKED NORMAL.

Part: SWITCH — STUCK (AUTOFEATHER SYS) · airframe 53,164 hrs · 58,993 cycles

AUTO FEATHER FILED TO ARM ON TAKEOFF. R & R NR1 AND NR2 TSEU AND NO FIX. FOUND MICRO SWITCH 6121S9 STUCK, R & R SWITCH, OPS CHECKED GOOD IAW MM 76-10-13.

Part: SWITCH — MALFUNCTIONED (AUTOFEATHER) · airframe 52,180 hrs · 57,886 cycles

AUTO FEATHER SYS FAILED TO ARM AT APPROX 60 KNOTS. AC ABORTED TAKEOFF AND RETURNED TO BLOCKS. REMOVED AND REPLACED MICRO-SWITCHES, 6121-S12, AND 6121-S13. OPS CK GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 52,047 hrs · 57,730 cycles

MOST AFT CEILING EMERGENCY BULB INOP. REMOVED AND REPLACE BATTERY IN ACCORDANCE WITH 33-30-00

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 52,047 hrs · 57,730 cycles

MOST AFT CEILING EMERGENCY BULB INOP. REMOVED AND REPLACE BATTERY IN ACCORDANCE WITH 33-30-00

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 52,047 hrs · 57,730 cycles

NR 2 EMERGENCY FLOOR LIGHT LAMPS INOP AT ROW ONE AND TWO. REMOVED AND REPLACED EMERGENCY BATTERY AT PS4 IN ACCORDANCE WITH 33-30-00

Part: UNKNOWN — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 51,810 hrs · 57,464 cycles

THE AUTOFEATHER WOULD NOT ARM ON TAKEOFF ON AIRCRAFT 941HA. MAINTENANCE COULD NOT DUPLICATE WITH GROUND RUN IAW DASH 8 MM 71-00-00. NOTED: AUTOFEATHER / POWER UPTRIM OPERATES NORMALLY. CLEANED AND LUBED LAYSHAFT MICRO SWITCHES AS PRECAUTION, CHECKED PSEC, NO FAULTS NOTED. AUTOFEATHER SYSTEM OPERATES NORMALLY AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,570 hrs · 57,191 cycles

UPON INSPECTION IN SBY THERE WAS AN EMERGENCY LIGHT INOPERATIVE. THE BULB WAS REMOVED AND REPLACED, OPERATIONAL CHECK WAS GOOD.

Part: SEQUENCE VALVE — MALFUNCTIONED (LT MLG DOOR) · airframe 51,505 hrs · 57,119 cycles

LANDING GEAR INOPERATIVE CAUTION LIGHT ILLUMINATED INTERMITTENTLY IN CRUISE FLIGHT (GEAR UP DOORS CLOSED). CREW PERFORMED ALTERNATE GEAR EXTENSION. COULD NOT DUPLICATE DURING RON MAINTENANCE. CHANGED RELAYS 3261-K8 AND RELAY 3261-K6 FOR POSITIVE MAINTENANCE ACTION. OPS CHECK GOOD IN ACCORDANCE WITH MAINTENANCE MANUAL 32-30-00. REMOVED AND REPLACED NR 2 MLG DOOR SOLENOID SEQUENCE VALVE, OPS CHECK GOOD REFERENCE MAINTENANCE MANUAL 32-10-51.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 51,211 hrs · 56,795 cycles

EMERGENCY FLOOR ESCAPE PATH HAS 2 LAMPS INOP, CEILING EMERGENCY LIGHT IS VERY DIM ROW 5. REMOVED AND REPLACED LIGHT BULB.

Part: PANEL — MALFUNCTIONED (AUTOPILOT SYS) · airframe 51,018 hrs · 56,591 cycles

SMOKE, ELECTRICAL FIRE FROM UNDER GLARE SHIELD AFTER GROUND POWER APPLIED. REMOVED & REPLACED CAPTAIN'S AUTO PILOT DISENGAGE ANNUNCIATOR PANEL ASSEMBLY DUE TO A BURNT RESISTOR. INSPECT AREA IN THE VICINITY FOR OTHER DAMAGE NONE FOUND. OP'S CHECK GOOD. IN ACCORDANCE WITH 22-10-01 PAR E AND 34-61-02.

Part: BULB — BURNED (EMERGENCY LIGHT) · airframe 50,530 hrs · 56,062 cycles

EMERGENCY CEILING LIGHT AT ROW 2 INOPERATIVE. R&R BULB, OPS CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 50,452 hrs

2ND FLOOR LEVEL EMERGENCY LIGHT INOP. R&R BULB IAW AMM 33-20-00. OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 50,452 hrs

EMERGENCY LIGHTING "NORM" BACK LIGHT INOP. INSTALLED NEW BULB IAW AMM 33-20-00. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,299 hrs · 55,799 cycles

EMERGENCY FLOOR PATH LIGHT INOPERATIVE AT ROW 4 AFT. R&R EMERGENCY FLOOR PATH LIGHT AT ROW 4 AFT.

Part: TRANSMITTER — MALFUNCTIONED (NR 1 ENG OIL SYS)

AIR RETURN NR 1 OIL PRESS GAUGE FLUXED FROM 50 TO 0 THEN BACK TO 40. W/NO OIL WARNING LIGHT SO ENGINE WAS NOT SHUT DOWN. REMOVED AND REPLACED OIL PRESS XMITTER OPS AND LEAK CHECK GOOD. DEPARTURE AIR READINGS NORMAL. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE SWITCH P/N 8D1437 OPS AND LEAK CHECK GOOD. (A)

Part: HYDRAULIC LINE — CRACKED (NR 1 NACELLE) · airframe 48,422 hrs · 53,689 cycles

EN ROUTE HYDRAULIC QUANTITY DROPPED, QTY REMAINED AT .7 QT. UPON LANDING FOUND LEAK FROM NUMBER ONE NACELLE. CREW DID NOT DECLARE AN EMERGENCY, TRUCKS DID RESPOND. INSTALLED TEMP FLEX LINE FROM NUMBER ONE MLG DOOR SEQUENCE SOLENOID, PORT C2, TO UNION. GROUND RAN, OPS AND LEAK CHECKS GOOD.

Part: LENS — FADED (CABIN) · airframe 48,259 hrs · 53,508 cycles

FOUND TWO OF THE FOUR FLOOR LEVEL EMERGENCY EXIT MARKER LIGHTS AT ROW 1 WERE NO LONGER RED. REPLACED LENSES.

Part: ACM — MALFUNCTIONED (A/C BAY) · airframe 48,227 hrs · 53,472 cycles

ACM MAKING LOUD NOISES AND EMITTING BURNT OIL SMELL IN CABIN & FLIGHT DECK.

Part: SENSOR — FAILED (CARGO DOOR) · airframe 47,919 hrs · 53,143 cycles

BAG DOOR WARNING LIGHT ILLUMINATED AFTER TAKEOFF, WENT OUT AT 6000 FEET AND CAME BACK ON AT 7500 FEET AND THEN BACK OFF AT 6000 FEET. MAINTENANCE CONFIRMED THAT THE FORWARD BAG DOOR SENSOR IS BAD AND NEEDS TO BE REPLACED. SENSOR WAS REPLACED, OPERATIONAL CHECK GOOD.

Part: RADAR — FAILED (WX SYSTEM) · airframe 47,488 hrs · 52,653 cycles

WHILE EN ROUTE GSO-DCA WEATHER RADAR STOPPED PAINTING WEATHER. CREW SHUT THE WX RADAR DOWN FOR 5 MINUTES THEN RESTARTED AND THAT DID NOT FIX IT. WITH THUNDERSTORMS AHEAD THE CREW CALLED DISPATCHER AND THEY BOTH DECIDED TO DIVERT TO ROA AWAY FROM THE THUNDERSTORMS TO A MAINTENANCE BASE. TO GET THE AIRCRAFT REPAIRED.

Part: WIRE — BROKEN (LANDING GEAR) · airframe 45,103 hrs · 50,076 cycles

NOSE GEAR INDICATOR FAILED TO SHOW PROPER INDICATION ON NORMAL GEAR EXTENSION. GEAR WARNING HORN SOUNDED CONTINUOUSLY. CREW PERFORMED MISSED APPROACH, RETURNED TO MDT. FOUND AND REPAIRED BROKEN WIRE IDENT 11A00BLU.

Part: STRUT — LEAKING (PAX DOOR) · airframe 42,944 hrs · 47,731 cycles

PAX DOOR WARNING LIGHT ILLUMINATED AT 8000FT. REMOVED AND REPLACED GAS STRUT (SHORT).

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 35,604 hrs · 39,413 cycles

WHEN GEAR WAS SELECTED UP THE NOSEGEAR REMAINED UNSAFE AND AMBER MAIN GEAR DOOR LIGHTS ILLUMINATED. SELECTED GEAR DOWN ALL INDICATIONS NORMAL. REMOVED AND REPLACED NLG DRAGSTRUT PROXIMITY SENSOR.

Part: AMPLIFIER — INOPERATIVE (SMOKE DETECTORS) · airframe 40,490 hrs · 45,050 cycles

AT ABOUT 1500 FEET SMOKE WARNING ILLUMINATED ALONG WITH MASTER WARNING LIGHT. REMOVED AND REPLACED FWD AFT SMOKE DETECTORS P/N OFF 473054, S/N OFF 0772, FWD P/N ON 473054, S/N ON 1568. AFT SMOKE DETECTOR P/N ON AND OFF 30-231-3. S/N ON 31572, S/N OFF 31820. REMOVED AND REPLACED AMPLIFIER GROUND, OPS CHECK GOOD.

Part: VALVE — FAILED (NR 2 ENGINE) · airframe 40,328 hrs · 46,492 cycles

OIL SMELL IN CABIN AND FLIGHT DECK IN FLIGHT WITH POWER BELOW 30 PERCENT TORQUE SETTING. TURNED NR 2 BLEED OFF AND SMELL WENT AWAY. REPLACED NR 2 AIR SWITCHING VALVE.

Part: LOCK — UNSECURE (NLG) · airframe 30,202 hrs · 34,101 cycles

AFTER TAKEOFF, THE NOSE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE FIELD. FOUND THE NOSE GEAR GROUND LOCK NOT STOWED. STOWED GROUND LOCK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

AFT OVERHEAD DOWN, MID CABIN EXIT AND EXTERIOR AFT LT EGRESS EMERGENCY LTS INOP. REMOVED AND REPLACED POWER SUPPLY.

Part: VALVE — DAMAGED (NR 1 MLG)

AFTER GEAR RETRACTION, NR 2 ENGINE DRIVEN HYD PUMP CAUTION LIGHTS ILLUMINATED. SERVICED AND BLED NR 2 HYD SYSTEM. REMOVED AND REPLACED THREE LANDING GEAR DOOR SEQUENCER VALVE ON RON FOR FCD 8-32-94-351. NR 2 HYD SYSTEM WAS NOT BLED PROPERLY. (M)

Part: VALVE — DAMAGED (NR 2 MLG)

AFTER GEAR RETRACTION, NR 2 ENGINE DRIVEN HYD PUMP CAUTION LIGHTS ILLUMINATED. SERVICED AND BLED NR 2 HYD SYSTEM. REMOVED AND REPLACED THREE LANDING GEAR DOOR SEQUENCER VALVE ON RON FOR FCD 8-32-94-351. NR 2 HYD SYSTEM WAS NOT BLED PROPERLY. (M)

Part: VALVE — DAMAGED (NLG)

AFTER GEAR RETRACTION, NR 2 ENGINE DRIVEN HYD PUMP CAUTION LIGHTS ILLUMINATED. SERVICED AND BLED NR 2 HYD SYSTEM. REMOVED AND REPLACED THREE LANDING GEAR DOOR SEQUENCER VALVE ON RON FOR FCD 8-32-94-351. NR 2 HYD SYSTEM WAS NOT BLED PROPERLY. (M)

Part: ROD ASSY — OUT OF ADJUST (LT MLG)

ON GER RETRACTION, LEFT FORWARD MAIN LANDING GEAR DOOR HANGS DOWN APPROX .5 INCH WITH GEAR UP AND LOCKED. NO ADVISORY LIGHT INDICATED. RIGGED AND ADJUSTED FORWARD DOOR. (M)

Part: SKIN — DENTED (CARGO DOOR)

DURING RON MAINTENANCE A DENT WAS FOUND IN THE BAGGAGE DOOR 1 INCH AFT OF FRAME INCHES, 1.1 INCH IN LENGTH AND .8 INCH WIDE OUT OF THE LIMITS OF THE SRM. THE DENT WAS DEFERRED FOR REPAIR WITHIN 500 HOURS BY AN ENGINEERING DISPOSITION. (M)

Part: BATTERY — DISHCARGED (CABIN)

SBY/PHL - FLT 3184 - NR 1 AND NR 2 RED FLOOR ESCAPE PATH LIGHTS INOPERABLE. REMOVED AND REPLACED BATTERY AND BASE ASSEMBLIES. (X)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

HPN/BWI - FLT 3260 - DURING PRE-FLIGHT WALK-AROUNDS, FOUND FIRST TWO RED EMERGENCY FLOOR LIGHTS INOPERABLE. REMOVED AND REPLACED THE 3352-PS2 POWER SUPPLY. (X)

Part: SENSOR — FAILED (NLG DOOR)

FLT 3393 - YYZ-BWI - NOSE GEAR DOOR INDICATOR LIGHT ILLUMINATES IN FLIGHT. STAYED ILLUMINATED AFTER GEAR SELECTED DOWN AND LOCKED. REMOVED AND REPLACED NOSE LANDING GEAR FORWARD DOOR SENSOR. (M)

Part: SENSOR — FAILED (NLG)

FLT NR 3481 - EYW-MIA - AFTER TAKEOFF, THE NOSE GEAR RED AND HANDLE LIGHT CYCLED ON AND OFF. THE AIRCRAFT CONTINUED ON TO MIA AND LANDED WITHOUT INCIDENT. ADJUSTED THE DRAG STRUT SENSOR AS REQUIRED AND GROUND CHECK WAS GOOD. LATER AT THE RON, THE SENSOR AT THE NOSE LANDING GEAR DRAG STRUT WS REPLACED. (M)

Part: ACTUATOR — BROKEN (COCKPIT)

AVL/CLT - FLT 3304 - DURING PRE-FLIGHT CHECKS, FOUND THE AUTOFEATHER SYSTEM WOULD NOT ARM. REMOVED AND REPLACED THE ACTUATOR ON POWER LEVER MICROSWITCH 6121-S9.

Part: EEL CONNECTOR — BENT (CABIN)

EWR-BWI - FLT 3266 - DURING FLIGHT CREW PREFLIGHT, FOUND FIRST TWO EMERGENCY FLOOR LIGHTS INOP. REPLACED PIN 6 ON PS2 BATTERY POWER SUPPLY CONNECTOR.

Part: SWITCH — DIRTY (AUTOFEATHER SYS)

CHO-SBY - FLT 3354 - ON TAKEOFF ROLL, AUTOFEATHER WOULD NOT ARM. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT. CLEANED AUTOFEATHER MICROSWITCH CONTACTS. OPERATIONAL CHECK GOOD.