N942HA

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,532 hrs · 75,916 cycles

FLOOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,475 hrs · 75,852 cycles

EMERGENCY LIGHT INOPERATIVE AT THIRD FROM THE FRONT. REMOVED AND REPLACED THE BULBS, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,475 hrs · 75,852 cycles

CEILING EMERGENCY LIGHT IS INOPERATIVE AT ROW 7. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.

Part: TAPE — LOOSE (NR 1 PROP BLADE) · airframe 67,203 hrs · 75,531 cycles

AFTER TAKEOFF, EROSION TAPE SEPARATED FROM THE NR 1 PROPELLER. NO VIBRATION NOTED. INSPECTED THE PROP ASSY. FOUND LOOSE EROSION TAPE ON NR 1 BLADE. REMOVED REMAINING TAPE, CLEANED AND RE-INSTALLED NEW TAPE. NO OTHER DEFECTS NOTED. GROUND RAN. NO DEFECTS NOTED. PROP HEAT OPS CHECKED GOOD. OK FOR SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 67,198 hrs · 75,520 cycles

EMERGENCY FLOOR LIGHT IS INOPERATIVE AT ROWS 3 AND 9. REMOVED TRIM. R & R BULBS, REINSTALLED TRIM AND FOUND BROKEN WIRE FOR EMERGENCY LIGHT AT ROW 9. REPAIRED WIRE IAW MM 20-45-07. OPS CHECKED GOOD.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 67,188 hrs · 75,509 cycles

RADAR DOES NOT PAINT, ANTENNA FAULT DISPLAYED. R & R RADAR RT IAW -8MM 34-41-04 AND OPS CK GOOD.

Part: LAMP — INOPERATIVE (BACK LIGHT) · airframe 67,081 hrs · 75,374 cycles

F/A EMERGENCY LIGHT SWITCH BACK LIGHT INOPERATIVE. REPLACED THE LAMP. OPS CHECKED GOOD. OK FOR SERVICE.

Part: COVER — MISSING (EXIT SIGN) · airframe 67,070 hrs · 75,359 cycles

LOWER EMERGENCY EXIT SIGN COVER MISSING AT ROW 4AC. INSTALLED LOWER EMERGENCY EXIT SIGN COVER AT ROW 4AC.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,976 hrs · 75,239 cycles

FWD FUSELAGE EMERGENCY EXIT LIGHT AND EMERGENCY EXIT LIGHT ABOVE PAX DOOR MOMENTARILY COMES ON AND THEN GOES OFF. R & R THE BATTERY PACK.

Part: CONTROL ROD — OUT OF ADJUST (LG DOOR) · airframe 66,728 hrs · 75,349 cycles

LEFT AMBER GEAR DOOR LIGHT ON AFTER GEAR RETRACTION. CYCLED GEAR IAW CHECK LIST. LIGHT EXTINGUISHED. ADJUSTED FWD GEAR DOOR AFT OPERATING ROD. PERFORMED 20-30 GEAR EXTENSION AND RETRACTION WITH NO AMBER GEAR DOOR INDICATION IAW AMM 32-10-21. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,743 hrs · 74,951 cycles

F/A EMERGENCY LIGHT SWITCH ON LIGHT INOPERATIVE. R & R BULB. OPS CHECK GOOD. OK FOR SERVICE.

Part: RELAY — INOPERATIVE (MLG) · airframe 66,675 hrs · 75,289 cycles

ON GEAR RETRACTION, LT AND RT DOOR AMBER LIGHTS REMAINED ILLUMINATED. DOORS STAYED OPEN ON RETRACTION. PERFORMED ALTERNATE GEAR EXTENSION IAW CHECK LIST. ACFT FERRY AFTER MAINTENANCE INSPECT HISTORY: ACFT. PICKUP MDT SPARE 975HA TO CONTINUE. R & R RELAYS 3261-K8, K9, K11, K13. R & R FWD RT GEAR DOOR ACT, REF 32-30-00. OPS OK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,303 hrs · 74,406 cycles

17 TH FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. R & R BULBS. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,191 hrs · 74,272 cycles

LIGHTNING STRIKE THROUGH CENTER OF CABIN. NO LOSS OF SYSTEMS OR ELECTRICAL COMPONENTS. DAMAGE FOUND DURING LIGHTNING STRIKE INSPECTION. PERFORMED WC 05-51-31I PRIOR TO FERRY FLIGHT.

Part: CONNECTOR — DAMAGED (RT AC BUSS) · airframe 65,454 hrs · 73,389 cycles

RIGHT AC BUSS CAUTION LIGHT ILLUMINATED WITH ASSOCIATED FAILURE CAUTION LIGHTS. R & R CONNECTOR 2421-P20 IAW STANDARD PRACTICE. OPS CHECKED GOOD.

Part: BUSS — WARNING LIGHT (RT AC GENERATOR) · airframe 65,318 hrs · 73,226 cycles

RIGHT AC BUSS FAIL WITH ASSOCIATED CAUTION LIGHTS, WOULD NOT RESET. NO LOAD ON NR 2 ON NR 2 AC GEN. R & R RT GCU AND NR 2 AC GENERATOR IAW 24-20-11. OPS CHECKED GOOD.

Part: INDICATOR — FAILED (RADAR) · airframe 64,775 hrs · 72,558 cycles

TERRAIN INOPERATIVE CAUTION LIGHT ILLUMINATED FOLLOWED BY ELECTRICAL ODOR AND FAILURE OF RADAR INDICATOR. R & R RADAR INDICATOR IAW 34-41-04. OPS CHECKED GOOD.

Part: OIL SYSTEM — LOW PRESSURE (NR 1 ENGINE) · airframe 64,731 hrs · 72,508 cycles

NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED ON TAKEOFF. SERVICE NR 1 ENGINE OIL TO PROPER LEVEL. GROUND RAN ACFT, OPS CHECKED GOOD.

Part: INVERTER — ODOR (COCKPIT) · airframe 64,595 hrs · 72,349 cycles

FISHY ODOR IN COCKPIT. ONCE RADAR WAS TURNED OFF, ODOR DISSIPATED. FOUND ODOR WAS COMING FROM AUX INVERTER.

Part: SENSOR — OUT OF ADJUST (RIGHT MLG) · airframe 64,465 hrs · 72,187 cycles

GEAR SLOWER THAN NORMAL TO RETRACT. DURING RETRACTION, RED LIGHTS REMAINED ON LONGER THAN NORMAL. GEAR RETRACTED, WOW CAUTION LIGHT ILLUMINATED. ON LANDING, WOW CAUTION LIGHT EXTINGUISHED. ADJUSTED RT INBD SENSOR. OPERATED GEAR SEVERAL TIMES. RETRACTION AND EXTENSION SPEEDS BOTH NORMAL. ALL INDICATION LIGHTS OPS CHECKED NORMAL. OK FOR SERVICE AT THIS TIME.

Part: OIL SYSTEM — LOW (NR 2 ENGINE) · airframe 64,273 hrs · 71,940 cycles

ON TAKEOFF, ROLL 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF AT APPROXIMATELY 90 KNOTS. INSPECTED NR 2 ENGINE, FOUND ENGINE OIL QTY 2 QUARTS LOW. SERVICE ENGINE WITH OIL. CREW PERFORMED TAKEOFF ROLL. LIGHT REMAINED EXTINGUISHED. OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 1 ENGINE OIL) · airframe 63,988 hrs · 71,606 cycles

NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. CHECKED OIL LEVEL, FOUND TO BE AT ACCEPTABLE LIMIT. INSPECTED, CLEANED AND RESEATED OIL PRESSURE SWITCH AND TRANSMITTER. PERFORMED SIMULATED TAKEOFF ROLL WITH CREW. NO DEFECTS NOTED AT THIS TIME.

Part: PRESSURE SWITCH — FAILED (ENGINE OIL) · airframe 63,988 hrs · 71,606 cycles

NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. R & R NR 1 ENGINE PRESSURE WARNING SWITCH IAW 71-00-02. LEAKED CHECKED GOOD.

Part: INDICATOR — INACCURATE (NR 2 TORQUE) · airframe 63,947 hrs · 71,558 cycles

WHEN APPLYING POWER ON TAKEOFF ROLL, NR 1 WENT TO 80 PERCENT. NR 2 WOULD NOT GO ABOVE 28 PERCENT. R & R NR 2 TORQUE INDICATOR IAW MM 77-10-00. ENGINE RUN IAW RUN UP MANUAL. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 63,905 hrs · 71,502 cycles

FAINT BURNED ODOR ON DESCENT, SELECTED ENGINE BLEEDS OFF AND ODOR DISSIPATED. GROUND RAN AIRCRAFT, SELECTED BOTH BLEEDS ONE AT A TIME FOR 10 MINUTES. NO BURNED ODORS. OK FOR SERVICE.

Part: INDICATOR — FAILED (WX RADAR SYS) · airframe 63,761 hrs · 71,309 cycles

RADAR DISPLAYS MULTICOLORED BANDS CONTINUOUSLY. R & R RADAR TRANSCEIVER AND RADAR INDICATOR IAW MM 34-41-04. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,638 hrs · 71,170 cycles

PAX DOOR EMERGENCY EXIT SIGN DOES NOT ILLUMINATE AND ROWS 1 AND 4 EXIT LIGHTS ONLY REMAIN ILLUMINATED FOR FIVE SECONDS. R & R EMERGENCY LIGHT BATTERIES IAW WC 33-50-05R. OPS CHECKED GOOD. OK FOR SERVICE AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,566 hrs · 71,086 cycles

EMERGENCY LIGHTS ARE INOPERATIVE. R & R BULBS IN EMERGENCY LIGHTS, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,260 hrs · 70,711 cycles

SECOND OVERHEAD EMERGENCY LIGHTING IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: TERMINAL — BURNED (COFFEEMAKER) · airframe 63,084 hrs · 70,501 cycles

BRIEF HOT ODOR NOTICED DURING FINAL. SELECTED COFFEEMAKER OFF AND ODOR WENT AWAY. FOUND ONE PIN SOCKET BURN. COMPLIED WITH WC 25-00-004N. R & R RECEPTACLE TO NR 1 HOT JUG AND INSTALLED 2 NEW RING TERMINALS. R & R NR 1 HOT JUG. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,054 hrs · 70,563 cycles

F/S EMERGENCY LIGHT SWITCH DOES NOT ILLUMINATED. R & R BULB. OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (MLG WOW) · airframe 62,786 hrs · 70,128 cycles

AFTER GEAR RETRACTION, WOW CAUTION LIGHT ILLUMINATED AND EXTINGUISHED TWO TIMES. NORMAL GEAR EXTENSION FOR LANDING. PSEU CODE 12, RT GEAR WOW CHECK. WIRING FROM 3261-P15 TO SENSOR FOUND INDUCTANCE AND RESISTANCE HIGH. R & R RT GEAR WOW 1 HARNESS. JACKED AND CYCLED GEAR. NO DEFECTS NOTED. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,752 hrs · 70,081 cycles

REAR EMERGENCY LIGHT ON LT FUSELAGE IS INOPERATIVE. R & R LIGHT BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,637 hrs · 69,937 cycles

LEFT AFT FUSELAGE EXTERIOR EMERGENCY LIGHT IS DIM. R & R BULB, AT LOCATION, OPS CHECKED GOOD.

Part: SPINNER — CRACKED (PROPELLER) · airframe 62,217 hrs · 69,431 cycles

IN CRUISE FLIGHT, ACFT EXPERIENCED MODERATE TURBULENCE WITH A 45 DEGREE LT BANK AND A 20 DEGREE PITCH UP ACCOMPANIED BY NUMEROUS ITEMS BEING DISLODGED FROM POSITION. YD AND AP BOTH DISENGAGED AND ACFT EXPERIENCED A 300 TO 400 FOOT LOSS IN ALTITUDE. COMPLIED WITH SEVERE TURBULENCE INSPECTION WC 05-50-21I. NR 1SPINNER IS CRACKED IN NUMEROUS PLACES EXTENDING FROM SCREW HOLES. R & R NR 1 PROP SPINNER USING RETAINED HARDWARE. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,958 hrs · 69,112 cycles

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

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 61,872 hrs · 69,004 cycles

NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF AND REDUCED POWER. LIGHT EXTINGUISHED AND PRESSURE APPEARED NORMAL BEFORE ENGINE SHUTDOWN. CHECKED NR 1 ENGINE OIL LEVEL AND SERVICED WITH 2 OUARTS. INSPECTED, CLEANED AND SECURED NR 1 ENGINE OIL PRESSURE SWITCH CONNECTOR. GROUND RAN AIRCRAFT. OPS CHECKED NORMAL AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,845 hrs · 68,970 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE THIRD FROM FRONT. R & R BULB, OPS CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 61,827 hrs · 68,948 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 8. FOUND BROKEN WIRES, SPLICED IN NEW LIGHT ASSEMBLY IAW AMM 20-45-06.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,790 hrs · 68,906 cycles

MOST AFT EMERGENCY CEILING LIGHT IS INOPERATIVE. R & R BULB AT MOST AFT CEILING LIGHT. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 61,663 hrs · 68,752 cycles

ELECTRICAL ODOR IN COCKPIT. RADAR CIRCUIT BREAKER FOUND TRIPPED WITH TERRAIN INOPERATIVE. CAUTION LIGHT AND MASTER CAUTION LIGHT ILLUMINATED. REMOVED RT NAV PANEL WITHOUT DISCONNECTING CONNECTOR, INSPECTED AREA. NO DEFECTS NOTED OR ODOR. REINSTALLED RT NAV PANEL. COLLARED RADAR CIRCUIT BREAKER.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,587 hrs · 68,662 cycles

AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: DISPLAY — FAILED (WX RADAR SYS) · airframe 61,510 hrs · 68,568 cycles

WEATHER RADAR FAILED ENROUTE. TEXT MESSAGE APPEARED IN LOWER RT CORNER. R & R RADAR RT AND INDICATOR IAW 34-41-04 AND BULLETIN 34-18. OPS CHECKED GOOD ON GROUND. OK FOR SERVICE.

Part: SELECTOR PANEL — MALFUNCTIONED (MLG) · airframe 61,277 hrs · 68,282 cycles

AT APPROX. 300 FT. ALL GEAR SHOWED RED UNSAFE, WARNING HORN SOUNDED AND CREW FELT NLG CLUNKING FOR APPROX 1 MINUTE. R & R LANDING GEAR SELECTOR PANEL IAW AMM 32-30-05. R & R LANDING GEAR SELECTOR VALVE IAW WC 32-30-41R. OPS AND LEAKED CHECKED GOOD AT THIS TIME. SWUNG GEAR SEVERAL TIMES.

Part: ENGINE — POWER LOSS · airframe 61,015 hrs · 67,966 cycles

AFTER TAKEOFF, SHORTLY AFTER GEAR RETRACTION, NR 1 ENGINE MADE A LOUD SOUND, THEN NOTICED NR 1 PROP AT APPROX 400 RPM AND TORQUE 125, PLUS FOR APPROX 30-60 SECONDS BEFORE CREW SHUTDOWN ENGINE, AUTOFEATHER SELECTED AND ARMED. NO UPTRIM INITIATED. INSPECTED NR 1 ENGINE AND PROP, NO DEFECTS NOTED. OIL QUANTITY GOOD. NO LEAKS NOTED. CREW DRY MOTORED ENGINE, NO OBVIOUS DEFECTS HEARD. CREW GROUND RAN ACFT WITH MX MONITORING, ALL TEST COMPLETE. ALL SYS OPS CHECKED NORMAL PERFORMED NR 1 PROP SPINNER OFF CHECKS IAW MM 61-10-00. NO DEFECTS NOTED. OIL LEVEL GOOD. PERFORMED NR 1 RGB SCAVENGE FILTER AND CHIP DETECTOR INSPECTION, NO CONTAMINATION FOUND. LEAKED CHECKED GOOD IAW MM 72-01-50. ENGINE WILL BE R & R.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 60,833 hrs · 67,758 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 5. R & R BULB AT EMERGENCY FLOOR PATH LIGHT IN ROW 5. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 60,084 hrs · 66,858 cycles

EMERGENCY SIDEWALL LIGHTS ARE DIM AT ROWS 1DF AND 4DF.....REMOVED AND REPLACED BURNED OUT BULBS IN EMERGENCY SIDEWALL LIGHTS AT ROWS 1DF AND 4DF. OPS CHECKED GOOD.

Part: BULB — FAILED (CAUTION LIGHT) · airframe 59,929 hrs · 66,674 cycles

TERRAIN CAUTION LIGHT FOR DISARM LIGHT IS INOPERATIVE. R & R CAUTION LIGHT. RESECURED LENS. OPS CHECKED GOOD.

Part: SENSOR — OUT OF ADJUST (MLG DOOR) · airframe 59,901 hrs · 66,640 cycles

LT FWD GEAR DOOR REMAINED OPEN, AFTER GEAR RETRACTION AND ADVISORY LIGHT REMAINED ILLUMINATED, UNTIL GEAR SELECTED DOWN. ADJUSTED SENSOR GAP. R & R ACTUATOR HOOK LINK AND HARDWARE. R & R BUSHINGS AND HARDWARE AT DOOR CONNECTING ROD TO LEVER. SWUNG GEAR SEVERAL TIMES IAW 32-10-36. OPS CHECKED GOOD.

Part: SWITCH — BROKEN (COCKPIT) · airframe 59,546 hrs · 66,202 cycles

COCKPIT EMERGENCY LIGHT SWITCH BROKEN. R & R SWITCH. OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (NR 1 DC GEN) · airframe 59,545 hrs · 66,200 cycles

NR 1 DC GENERATOR FAILED IN FLIGHT. CREW FOLLOWED CHECKLIST AND GENERATOR FAILED AGAIN. CLEANED WING ROOT CONNECTION, 2431-TB3. CLEANED GROUND AT T.1 CURRENT TRANSFORMER AND CONNECTORS AT AUX AND MAIN BATTERIES USING STANDARD MAINTENANCE PRACTICES. OPS CHECKED GOOD DURING GROUND OPERATIONS.

Part: ACM — SMOKE · airframe 59,523 hrs · 66,172 cycles

WHILE ENROUTE, AT 16K, ENCOUNTERED ELECTRICAL ODOR IN FLIGHT DECK WITH F/A REPORTS ODOR IN CABIN TOO, WITH HAZE NOTED NEAR CEILING. INSPECTED ACFT. FOUND ACM AT FAULT. R & R ACM IAW WC 21-50-03I. OPS AND LEAKED CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,901 hrs · 65,397 cycles

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

Part: TERMINAL BLOCK — MISINSTALLED (COCKPIT) · airframe 58,765 hrs · 65,225 cycles

F/O OBSERVED PUFF OF SMOKE FROM FORWARD WINDSCREEN WHILE OPERATING. FOUND HARDWARE FOR POWER TERMINAL ON WINDSCREEN TERMINAL BLOCK INCORRECTLY INSTALLED. R & R SCREWS. RAN ACFT IAW SRT MANUAL. OPS CHECKED GOOD. CLEARED MEL.

Part: STRINGER — CORRODED (BS 222-270 S31R) · corrosion level 2 · airframe 58,719 hrs · 65,164 cycles

STRINGER 31S IS CORRODED AT BS 222,252 AND 270. CUT AND SPLICE STRINGER 31S IAW RD8-53-24-99 AND EO8-53-12-0308.

Part: SEAT TRACK — CORRODED (BS 268) · corrosion level 2 · airframe 58,719 hrs · 65,164 cycles

LEFT HAND INBD SEAT TRACK HAS AREAS OF CORROSION AT BS 268. BLENDED CORROSION AS PER RD8-53-1339. FOUND BLENDED AREA TO BE OUT OF LIMITS. REMOVED FASTENERS AND RIVETS FROM BS 291 FORWARD OF BS 182. CUT AND SPLICE SEAT RAIL IAW RD8-53-3074.

Part: SKIN — CORRODED (BS 389) · airframe 58,719 hrs · 65,164 cycles

TWO AREAS CORRODED ON SKIN AT BS 389 BETWEEN STR30P AND 30S. FOUND TO BE LIGHT CORROSION. CLEANED AREA IAW CHAPTER 4, SECTION 8 OF CORROSION PREVENTION AND CONTROL MANUAL. ALODINE AND PRIMED AREA.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 58,719 hrs · 65,164 cycles

RT INBD SEAT TRACK HAS SEVERAL SPOTS OF CORROSION WHERE LAV/GALLEY ATTACHES. BLENDED CORROSION AT SEVERAL SPOTS, BLENDING FOUND TO BE WITHIN LIMITS IAW RD8-53-1339. ALODINE BLENDED SPOTS IAW SRM 51-20-16. EDDY CURRENT COMPLIED WITH, NO DEFECTS NOTED.

Part: WEB — CORRODED (BS 225-235) · corrosion level 1 · airframe 58,718 hrs · 65,164 cycles

SPOTS OF CORROSION ON WEB FLANGE AT STA X225 TO X235 AND STR 25P. CLEANED LIGHT SURFACE CORROSION, ALODINED, PRIMED AND REAPPLIED AV30 RUST INHIBITOR.

Part: SEAT TRACK — CORRODED (BS 598) · airframe 58,718 hrs · 65,164 cycles

LIGHT CORROSION FOUND IN SEAT TRACK SECTION AT STA 598. LIGHTLY BLENDED SEAT TRACK. INSPECTED SEAT TRACK AND FOUND THEM TO BE OUT OF LIMITS IAW RD8-53-4936.

Part: BOLT — CORRODED (VERTICAL STAB) · airframe 58,718 hrs · 65,164 cycles

LOCK BOLTS ARE CORRODED INSIDE OF VERTICAL STAB, FORWARD TUNNEL, AT RIB 4. CLEANED OFF LIGHT SURFACE CORROSION ON LOCK BOLTS, INSIDE VERTICAL STAB, FORWARD TUNNEL AT RIB 4.

Part: FRAME — CORRODED (BS 222 S30-31R) · corrosion level 1 · airframe 58,719 hrs · 65,164 cycles

FRAME LEG HAS CORROSION AT STA.X222 BETWEEN STR.31S AND 30S. LIGHTLY BLENDED CORROSION FROM FRAME LEG, ALODINED AND PRIMED AREA IAW SRM 51-20-16 AND 51-20-36.

Part: STRINGER SPLICE — CORRODED (BS 639 S32R) · airframe 58,718 hrs · 65,164 cycles

STRINGER SPLICE AT STA X639, STR 32S HAS SEVERAL SPOTS OF LIGHT CORROSION. CLEANED AREA, REMOVED 3 RIVETS, LIGHTLY BLENDED STRINGER 32S TO REMOVED LIGHT CORROSION. ALODINE AND PRIMED AREA IAW SRM 51-20-36.

Part: FRAME — CORRODED (BS 312 S30-31R) · airframe 58,719 hrs · 65,164 cycles

FRAME LEG HAS CORROSION AT STA X312, BETWEEN STR 31S AND 30S. FRAME LEG HAD DIRT ACCUMULATION, CLEANED FRAME LEG AND FOUND NO CORROSION. ALODINE AND PRIMED AREA IAW SRM 51-20-16 AND 51-20-36.

Part: FRAME — CORRODED (BS 352 S30-31R) · corrosion level 1 · airframe 58,719 hrs · 65,164 cycles

FRAME LEG HAS CORROSION AT STA X252 BETWEEN STR 31S AND 30S. LIGHTLY BLENDED AROUND 1 RIVET HOLE. REMOVING MINOR CORROSION, ALODINE AND PRIMED AREA IAW SRM 51-20-16 AND 51-20-36.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,711 hrs · 65,152 cycles

ONE EMERGENCY LIGHT IS INOPERATIVE ON BASE OF F/A'S WALL. R & R BULB. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,365 hrs · 64,750 cycles

EMERGENCY PATHWAY FLOOR LIGHT AT SEAT ROW 6DF IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: WINDSCREEN — FAILED (COCKPIT) · airframe 58,270 hrs · 64,641 cycles

INFLIGHT, CREW NOTICED ELECTRICAL ODOR FROM F/O FRONT WINDOW. SELECTED HEAT TO WARM UP. ODOR DISSIPATED. NO CAUTION LIGHTS. CREW GROUND RAN ACFT. PERFORMED WINDSHIELD HEAT OPS CHECK. RT WINDSHIELD LOAD .06. LT WINDSHIELD NORMAL. REF SEQ NR 2. R & R F/O WINDSHIELD HEAT CONTROLLER. OPS CHECK FAILED. R & R F/O WINDSCREEN IAW WC 56-00-00. OPS CHECKED, LEAKED CHECKED, GOOD.

Part: TERMINAL — BURNED (WINDSHIELD HEAT) · airframe 58,242 hrs · 64,611 cycles

STRONG TO VERY STRONG BURNING ODOR NOTICED ONLY IN COCKPIT DURING THE LAST 100 MILES OF FLIGHT AND 5 TO 7 MINUTES THRU TAXI. FOUND F/O WINDSHIELD HEAT POWER LEAD RING TERMINAL HEAT DAMAGED. NO DAMAGE TO WINDSHIELD. R & R TERMINAL SCREW AND WASHER. GROUND RAN WINDSHIELD HEAT. NO ORDER NOTED. OPS CHECKED GOOD IAW MM 56-10-11.

Part: UNKNOWN — VAPOR (BRAKE) · airframe 57,906 hrs · 64,227 cycles

VAPOR PRESENT AT LT OTBD MLG WHEEL ASSY DISSIPATED AFTER 15 MINUTES. INSPECTED NR 1 MLG WHEELS AND BRAKES FOR SIGNS OF OVERHEATING OR LEAKAGE. NONE FOUND. TAXIED ACFT, BRAKING NORMAL AND NO SIGN OF SMOKE OR VAPORS. OK FOR SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 57,593 hrs · 63,879 cycles

1 FORWARD RED EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: WIRE — BROKEN (TE FLAPS) · airframe 56,772 hrs · 62,941 cycles

ON TAKEOFF, FLAP HANDLE SELECTED TO ZERO. WOULD NOT RETRACT. STUCK AT 5. FOUND BROKEN WIRE ON FLAP HANDLE ARMING SWITCH, RESOLDERED SAID WIRE IAW AMM 20-45-04. OPS CHECKED GOOD AT THIS TIME.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 56,722 hrs · 62,880 cycles

EMERGENCY EXIT BETA LIGHTS VERY DIM. R & R LIGHT ON EMERGENCY EXIT USING RETAINING CLIPS.

Part: CURRENT LIMITER — INOPERATIVE · airframe 56,659 hrs · 62,805 cycles

LEFT SECONDARY BUSS INDICATES LOW VOLTAGE AND VOLTAGE REDUCES WHEN ITEMS ARE TURNED ON. OK WITH APU POWER. R & R CURRENT LIMITER F1, GROUND RUN, CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 56,399 hrs · 62,516 cycles

IN FLIGHT, LANDING GEAR INOPERATIVE CAUTION LIGHT ILLUMINATED TWICE AND EXTINGUISHED. PERFORMED ALTERNATE EXTENSION. NO INCIDENT ON LANDING. ENTIRE FLIGHT HAS GOOD HYD PRESSURE AND QTY. COULD NOT DUPLICATE IN HANGER, R & R PSEU AND RELAYS 3261-K5, K6 AND K7 AS PRECAUTION. COMPLIED WITH NUMEROUS GEAR SWINGS. NO DEFECTS AT THIS TIME.

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE) · airframe 56,087 hrs · 62,289 cycles

REJECTED TAKEOFF DUE TO NR 2 OIL PRESSURE WARNING LIGHT ILLUMINATED. CLEANED AND INSPECTED ENGINE FOR LEAKS, FOUND NR 2 ENGINE, 2 QUARTS LOW ON OIL. ADDED OIL AS REQUIRED. GROUND RAN, OPS CHECKED GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 56,171 hrs · 62,253 cycles

LT EMERGENCY EXIT SIGN AND LT FWD EMERGENCY EGRESS LIGHT INOP. R & R EMERGENCY LIGHT BATTERY AT PS1 LOCATION. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 56,139 hrs · 62,219 cycles

OVERHEAD EMERGENCY LIGHT INOP AT ROW 5. R & R BULB. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 56,139 hrs · 62,219 cycles

FLOOR EMERGENCY LIGHT INOPERATIVE AT ROW 7. R & R BULB IN THE EMERGENCY FLOOR LIGHT AT ROW 7. OPS CHECKED GOOD.

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 56,139 hrs · 62,219 cycles

FIRST FLOOR EMERGENCY LIGHT LENS IS WRONG COLOR. INSTALLED CORRECT COLORED LENS AS REQUIRED.

Part: WIRE — BROKEN (TE FLAPS) · airframe 56,060 hrs · 62,121 cycles

DURING RETURN TO FIELD, FLAPS WOULD NOT EXTEND, FOUND C/B L7 ON LT ESSENTIAL POPPED. FOUND WIRE BROKEN AT FLAP ARMING SWITCH, WILL SOLDER AND OPS CHECKED FLAP. NO FIX. REMOVED RELAY 2752 K1 CIRCUIT BREAKER STILL POPS, REINSTALLED RELAY.

Part: WIRE — BROKEN (CONTROL HANDLE) · airframe 55,495 hrs · 61,503 cycles

FLAPS WILL NOT GO TO 35 DEGREES. REMOVED 2 PANELS AT CTR CONSOLE. INSPECTED AND CLEANED FLAP TRIGGER MICRO SWITCH. GROUND RAN ACFT, OPERATED FLAPS THROUGH FULL TRAVEL, OPS CHECKED GOOD IAW -8 MM 27-51-00. REINSTALLED PANELS, OK FOR SERVICE. ON TAKEOFF, FLAPS WOULD NOT GO FROM 5 TO ZERO DEGREES. INSPECTED AND FOUND BROKEN WIRE AT FLAP CONTROL HANDLE, REPAIRED BROKEN WIRE, RAN FLAPS, OPS CHECKED NORMAL, OK FOR SERVICE.

Part: BLEED AIR SYS — ODOR (APU) · airframe 54,583 hrs · 60,490 cycles

STRONG ELECTRICAL ODOR IN CABIN. FOUND ODOR TO BE FROM APU BLEED. ENGINE BLEEDS NORMAL. SEQUENCE 2 FOR APU MEL. ACFT OK FOR SERVICE.

Part: BATTERY — DISCONNECTED (EMERGENCY LIGHTS) · airframe 54,113 hrs · 59,949 cycles

YELLOW EMERGENCY LIGHT ON BUTTON DOES NOT ILLUMINATE WHEN BUTTON DEPRESSED. UPON FURTHER INVESTIGATION FOUND FOUND THAT MAIN BATTERIES WERE DISCONNECTED, HENCE LIGHT DID NOT WORK.

Part: BOLT — SHEARED (NLG) · airframe 53,809 hrs · 59,603 cycles

UPON GEAR RETRACTION, NOSE AND LT AMBER LIGHT REMAINED ILLUMINATED. RED UNSAFE LIGHT ILLUMINATED. CREW CYCLED GEAR, NO CHANGE IN INDICATIONS. DURING GEAR INSPECTIONS, FOUND RETRACTION ACTUATOR FITTING UPPER BOLT SHEARED ON RT GEAR. R & R RETRACTION ACTUATOR AND ACTUATOR FITTING IAW AMM 32-30-11 AND WORK CARD 54-91-28. OPS CHECKED GOOD.

Part: RELAY — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 53,389 hrs · 59,114 cycles

NR 1 FUEL FILTER BYPASS CAUTION LIGHT ILLUMINATED IN FLIGHT. R & R RELAY 6121-K5 (AUTOFEATHER ARM CONTROL RELAY) GROUND RUN ACFT IAW DASH 8 RUN UP MANUAL. OPS GOOD AT THIS TIME.

Part: TERMINAL — BURNED (WINDSHIELD HEAT) · airframe 53,414 hrs · 59,140 cycles

IN FLIGHT, ELECTRICAL SMELL NOTED IN COCKPIT FOLLOWED BY SMOKE COMING FROM CAPTAINS WINDSHIELD WIRE TERMINAL AREA. INSPECTED CAPTAIN'S FRONT WINDSHIELD TERMINALS L1. FOUND TERMINAL END BURNED WITH MINOR DISCOLORATION ON TERMINAL BUSS L2. NO DEFECTS FOUND. R & R L1 TERMINAL WITH NEW AND INSPECTED WINDHIELD TERMINAL BLOCK AND FOUND TO BE WITHIN LIMITS IAW CMM 56-10-01.

Part: WIRE — WRONG PART (EMERGENCY LIGHT) · airframe 53,390 hrs · 59,114 cycles

LAST (2) FLOOR LEVEL EMERGENCY LIGHTS IN OP. FOUND 3352, CR5 TO BE THE WRONG PN AND MISWIRED. INSTALLED CORRECT DIODE AND WIRED IT CORRECTLY IAW 33-53-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,565 hrs · 59,312 cycles

LAST 2 FLOOR LEVEL EMERGENCY LIGHTS ARE NOT WORKING. FOUND 3352CR5 TO BE THE WRONG PN DIODE AND MISSED WIRED. INSTALLED CORRECT DIODED AND WIRED IT CORRECTLY IAW 33-53-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,389 hrs · 59,114 cycles

SEAT TRACK RAIL IS CORRODED IN FRONT OF GALLEY, LAV FWD ATTACH POINT. REMOVED PORTION OF SEAT TRACK FWD OF SPLICE AT APPROX X277. INSTALLED NEW SECTION OF SEAT RAIL IAW EO8-53-10-0120.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 53,051 hrs · 58,736 cycles

ROW 4 FLOOR PATH EMERGENCY LIGHT RED IS NOT WORKING. R & R FLOOR LIGHT BULB IAW 33-51-00.

Part: SELECTOR PANEL — MALFUNCTIONED (MLG) · airframe 52,529 hrs · 58,138 cycles

NOSE GEAR DID NOT RETRACT AFTER TAKEOFF CYCLED GEAR, OPERATES NORMAL. REMOVED AND REPLACED GEAR SELECTOR PANEL, GROUND TESTED GOOD IAW 32-20-05.

Part: PSEU — MALFUNCTIONED (NLG)

AFTER GEAR EXTENSION NOSE GEAR RETRACTED UN-COMMANDED THEN EXTENDED UN-COMMANDED AFTER UN-COMMANDED EXTENSION NOSE GEAR STAYED DOWN AND LOCKED WITH NO OTHER ABNORMAL INDICATIONS. FOUND PSEU WITH CARD FAIL FAULT LIT RESET UNIT JACKED AND SWUNG GEAR CARD FAIL FAULT RETURNED R&R PSEU AND SWUNG GEAR SEVERAL TIMES, NO CARD FAIL FAULT NOTED. OPS AND INDICATION DURING GROUND OPS CHECK OK AT THIS TIME IN REF TO MM 32-30-00 AND MM 32-61-50. ACFT RELEASED FOR EVALUATION FLT DUE TO UN-COMMANDED GEAR EXTENSION AND RETRACTION DURING EXTENSION CYCLE AND REPLACEMENT OF THE PSEU ALL GROUND OPS AND INDICATION CHECKS GOOD MAINTENANCE ACTION COMPLETE SUBJECT TO SAT EVAL FLT REF LP 28720 SEQ3. ACFT DOWN FROM LAST NIGHT, AFTER GEAR EXTENSION NOSE GEAR RETRACTED UN-COMMANDED THEN EXTENDED NOSE GEAR STAYED DOWN AND LOCKED WITH NO OTHER ABNORMAL INDICATIONS.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 51,938 hrs · 57,461 cycles

FLOOR LEVEL EMERGENCY LIGHT AT ROW 6 INOP. REMOVED AND REPLACED BULB IN ACCORDANCE WITH MAINTENANCE MANUAL 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,938 hrs · 57,461 cycles

THE 3RD FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE. INSTALL NEW LAMP MODULE IN ACCORDANCE WITH MAINTENANCE MANUAL 20-45-07.

Part: ACTUATOR — BYPASSING (LT MLG) · airframe 51,716 hrs · 57,203 cycles

LT MAIN AMBER GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR IAW CHECKLIST, GEAR RETRACTED AND LIGHT EXTINGUISHED. ACFT DIVERTED DURING FERRY FLIGHT. MECH WORKED ISSUE AND COULDN'T FIND PROBLEM. FERRY TO OTHER FACILITY. MX FOUND FWD GEAR DOOR ACTUATOR TO BE BYPASSING. REMOVED AND REPLACED ACTUATOR. PERFORMED GEAR SWINGS, ALTERNATE GEAR EXTENSION CHECKS AND INSP FOR LEAKS IAW MM 32-10-36. OPS CHECK GOOD PENDING EVAL FLIGHT.

Part: WARNING HORN — FALSE ACTIVATION · airframe 50,655 hrs · 56,052 cycles

DURING TAKEOFF ROLL, THE TAKEOFF WARNING HORN BEGAN TO SOUND. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO GATE. MX POWERED DOWN THEN POWERED UP THE ACFT AND GROUND RAN THE ACFT TWICE. NO DEFECTS WERE NOTED AND THE ACFT WAS THEN RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,555 hrs · 55,947 cycles

FLOOR EMERGENCY LIGHT INOPERATIVE AT 11TH 1 FROM THE FRONT. R&R RED LAMP MODULE, IAW MX MANUAL 20-45-07. OPS CHECK GOOD.

Part: LIGHT — DEFECTIVE (EXTERIOR) · airframe 50,425 hrs · 55,806 cycles

DURING RON MAINTENANCE, THE LEFT FORWARD EMERGENCY EGRESS LIGHT WAS FOUND TO BE DIM. THE BULB WAS REPLACED AND LIGHTING, OPS CHECKED GOOD.

Part: SWITCH — BROKEN (BLEED AIR SYS)

NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED IN FLIGHT. R&R NR 2 ENGINE HIGH PRESSURE BLEED SWITCH. REFERENCE MM 21-11-21. GROUND RUN OPS CHECK GOOD.

Part: CONTROL UNIT — FAULTED (NR1 PROPELLER)

NR 1 ENG PROP SPEED WENT TO 1217 ON TO ROLL ABORTED TAKEOFF. ABORTED T/O RETURNED TO GATE. MAINTENANCE REPLACED NR 1 PROP CONTROL UNIT AND TRANSFER TUBE OPS AND LEAK CHECK GOOD FLIGHT 4436. (S)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

REJECTED TO AT 45 KNOTS DUE TO SECONDARY INVERTER CAUTION LIGHT COMING ON DURING ROLL. GOT OFF THE RUNWAY AND CALLED MX CONTROL. DID NOT RETURN TO GATE, MEL WAS ISSUED. (K)

Part: CABLE — BURNED (NR 2 ENGINE) · airframe 49,099 hrs · 54,343 cycles

NR 2 ENG WOULD NOT START, NO ROTATION. MT INSPECTED AND FOUND LEAD CABLE FROM GEN TO BULKHEAD BURNED. REMOVED AND REPLACED LEAD CABLE, GROUND RAN AC AND OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,089 hrs · 54,328 cycles

EMERGENCY EXIT SIGN OVER MAIN CABIN DOOR HAS SEVERAL LAMPS INOP. REMOVED INOP LAMPS AND REPLACED WITH NEW. OPS CHECK GOOD.

Part: BRAKE — SMOKE (NR 1) · airframe 48,906 hrs · 54,134 cycles

AFTER LANDING AND TAXI, SMOKE COMING FROM NR 1 BRAKE ASSEMBLY. INSPECTED NR 1 BRAKE ASSEMBLY, NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: PROPELLER — OUT OF BALANCE (NR 2 ENGINE) · airframe 48,746 hrs · 53,963 cycles

AIRCRAFT WAS EN ROUTE FROM LGA TO ORF, THE CAPTAIN NOTIFIED DISPATCH NORTH OF SBY THAT THE AIRCRAFT WAS ENCOUNTERING A MODERATE TO HEAVY PROPELLER VIBRATION AT ALL RPM SETTINGS. THE AIRCRAFT WAS DIVERTED TO SBY. IT WAS DETERMINED THAT NR 2 PROPELLER WAS CAUSING THE VIBRATION. THE PROPELLER WAS REMOVED, STATIC BALANCED AND RE-INSTALLED, GROUND RUN WAS SATISFACTORY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,375 hrs · 53,552 cycles

INTERIOR EMERGENCY LIGHT INOP 2ND CEILING LIGHT AFT. REMOVED AND REPLACED BULB LIGHT OPS CHECK GOOD IAW M/M 33-51-00.

Part: MOUNT — BROKEN (NR 2 ENGINE) · airframe 47,480 hrs · 52,577 cycles

ENGINE REMOVED FROM A/C 942 HA IN MDT ON 7-3-07 RECEIVED AT SBY MAINTANCE SHOP. FOUND TORQUE MOUNT END BROKEN OFF. ENG S/N 12-42.

Part: MOUNT — BROKEN (NR 2 ENGINE) · airframe 47,480 hrs · 52,577 cycles

ENGINE WAS REMOVED FROM A/C IN MDT ON 7-3-07. RECEIVED IN SBY MAINTENANCE SHOP FOUND TORQUE MOUNT END BROKE OFF. ENGINE S/N 120042.

Part: SWITCH — DIRTY (T/E FLAP) · airframe 47,316 hrs · 52,413 cycles

CREW RETURNED TO THE FIELD IN MDT AFTER THE FLAPS WOULD NOT RETRACT. NO EMERGENCY DECLARED. CLEANED AND LUB MICROSWITCH AND LINKAGE ON FLAP CONSOLE. OPS CHECK OF FLAPS GOOD.

Part: PSU — BURNED · airframe 46,326 hrs · 51,371 cycles

FLIGHT ATTENDANT NOTICED SMOKE COMING FROM AROUND PSU AT 2AC. FOUND CIRCUIT CARD BURNED, REMOVED AND REPLACED PSU AT 2AC.

Part: PUMP — LOOSE (HYD SYSTEM) · airframe 45,330 hrs · 50,282 cycles

NR 1 STBY HYD PUMP FAILED ON SINGLE ENGINE TAXI OUT, LOST NORMAL BRAKES FOUND RUBBER BOOT ON C/P TO STBY HYD PUMP LOOSE AND FLUID IN IT. CLEANED AND RESEALED C/P.

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG) · airframe 44,569 hrs · 49,461 cycles

RIGHT AMBER LIGHT STAYED ILLUMINATED AFTER GEAR WAS SELECTED UP. LIGHT REMAINED ON AFTER ADDITIONAL CYCLE OF THE GEAR. VERIFIED CODE 18 ON PSEU, RT FORWARD GEAR DOOR. DISCONNECTED FWD GEAR DOOR AFT ATTACH POINT ROD AND CHECKED SENSOR GAP. FOUND TO BE OUT OF LIMITS. RIGGED DOOR SENSOR AND RIGGED FORWARD GEAR DOOR.

Part: RADAR — INOPERATIVE (WX SYSTEM) · airframe 42,951 hrs · 47,738 cycles

WEATHER RADAR SPOKING, WILL NOT RETURN KNOWN WEATHER. REPLACED RADAR R/T ANTENNA. MORE TO FOLLOW (P/N'S AND S/N'S)

Part: SKIN PANEL — DEBONDED (BS 424-445) · airframe 42,738 hrs · 47,524 cycles

SKIN WAS FOUND DISBONDED BETWEEN FRAMES AT STATIONS 424 AND 445 ON STRINGERS 24S, 27S, AND 28S. THE SKIN PANEL WAS REPLACED.

Part: GARLOCK SEAL — LEAKING (NR 2 ENGINE) · airframe 42,503 hrs · 47,279 cycles

NR 2 ENGINE OIL PRESSURE FLUCTUATED IN FLIGHT STAYED BETWEEN 40-55 PSI OVER 3 MINUTES. REMOVED AND REPLACED HYDRAULIC PUMP GARLOCK SEAL.

Part: VALVE — STICKING (NR 2 ENGINE) · airframe 42,305 hrs · 47,068 cycles

NR 2 ENGINE OIL TEMP WENT TO REDLINE, DECREASED POWER TO FLIGHT IDLE AND OIL TEMP DROPPED TO TOP OF GREEN ARC. REMOVED AND REPLACED NR 2 DIVERTER VALVE.

Part: SENSOR — INOPERATIVE (CARGO DOOR) · airframe 40,264 hrs · 44,821 cycles

DURING CLIMBOUT BAG BAY DOOR WARNING LIGHT ILLUMINATED. CREW INSPECTED DOOR, NO DEFECTS NOTED. CREW IS C/W APPENDIX 5 TO MEL WARNING LIGHT. REMOVED AND REPLACED FWD BAG DOOR SENSOR, OPS CHECK GOOD.

Part: PIN — LOOSE (STORAGE BOX) · airframe 39,834 hrs · 44,336 cycles

NOISE NOTED AT AIRSTAIR DOOR EXTERIOR AFTER T/O AIR TURNBACK, FOUND PROP TIE STREAMER HANGING FROM AIRSTAIR DOOR PROP TIE STORAGE AREA. INSPECTION OF ACFT FOUND NO DAMAGE.

Part: BALLAST — BURNED (CABIN LIGHTS) · airframe 39,374 hrs · 43,820 cycles

BURNING SMELL IN CABIN. MX FOUND SIDEWALL LIGHT BALLAST AT 4DF SMOKING. DISCONNECTED AND SECURED POWER WIRE TO BALLAST IAW EO 8-33-04-0156. INSPECTED FOR HIDDEN DAMAGE, NO DEFECTS NOTED.

Part: TURNBUCKLE — BENT (NLG) · airframe 39,300 hrs · 43,734 cycles

NOSE LANDING GEAR WOULD NOT RELEASE HAD TO BE MANUALLY RELEASED. WHEN GEAR HANDLE SELECTED DOWN NOSE UNSAFE LIGHT D/N ILLUMINATE, TRIED MANUAL EXTENSION, DID NOT WORK, TRIED AGAIN AND GEAR UNLOCKED. FOUND TURNBUCKLE BENT. REMOVED AND REPLACED TURNBUCKLE, OPS CHECK GOOD.

Part: SWITCH — SHORTED (ZONE 200) · airframe 37,357 hrs · 41,678 cycles

DURING NR 1 ENGINE START THE FLIGHT/TAXI SWITCH POPPED TO THE FLIGHT POSTION, FOLLOWED BY A DC BUS FAULT AND SMOKE COMING FROM THE FLIGHT TAXI SWITCH. REPLACED THE FLIGHT TAXI SWITCH.

Part: AILERON — MALFUNCTIONED (WING) · airframe 33,265 hrs · 37,301 cycles

JUST BEFORE LANDING, ROLL CONTROL SYSTEM DISCONNECTED. INSPECTED DISCONNECT, ROLLED AILERONS SEVERAL TIMES, INSPECTED VISUALLY AILERON CONTROL CABLES. COULD NOT DUPLICATE PROBLEM ON GROUND. PERFORMED EVALUATION FLIGHT WITH SATISFACTORY RESULTS.

Part: CABLE — DAMAGED (PAX DOOR) · airframe 29,515 hrs · 33,249 cycles

CREW WAS UNABLE TO OPEN THE PASSENGER DOOR. FOUND OUTER COUNTERBALANCE CABLE OF THE CABLE DRUM DAMAGED. REPLACED THE OUTER CABLE, COUNTERBALANCE GAS STRUTS AND INSTALLED MODIFIED CABLE GUARD.

Part: COVER — MISSING (ROW 4)

LOW BULKHEAD EMER LIGHT COVER MISSING RT SIDE ROW 4. REMOVED AND REPLACED EMERGENCY LIGHT ASSY.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SBY - FLT 3081 - AFT OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED THE POWER SUPPLY AND BASE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

DURING C-CHECK INSPECTION, THE SEAT TRACKS WERE FOUND CORRODED BEYOND THE DEHAVILLAND LIMITS. THE SEAT TRACKS WERE REPAIRED IAW E08-98-817. (M)

Part: SEAT TRACK — CORRODED (CABIN)

DURING C-CHECK INSPECTION, THE SEAT TRACKS WERE FOUND CORRODED BEYOND THE DEHAVILLAND LIMITS. THE SEAT TRACKS WERE REPAIRED IAW EO8-98-817. (M)

Part: SEAT TRACKS — CORRODED (CABIN)

DURING C-CHECK INSPECTION, THE SEAT TRACKS WERE FOUND CORRODED BEYOND THE DEHAVILLAND LIMITS. THE SEAT TRACKS WERE REPAIRED IAW EO8-53-98-817. (M)

Part: SEAT TRACKS — CORRODED (CABIN)

DURING C-CHECK INSPECTION, THE SEAT TRACKS WERE FOUND CORRODED BEYOND THE DEHAVILLAND LIMITS. THE SEAT TRACKS WERE REPAIRED IAW EO8-53-98-917. (M)

Part: SKIN — DENTED (FUSELAGE)

DURING C-CHECK INSPECTION, A DENT WAS BELOW THE ICE SHIELD ON STRINGER 235 WITH A MAX DEPTH OF .040 INCH, 1.6 INCH LONG AND .8 WIDE OUT OF THE LIMITS OF THE DEHAVILLAND SRM 53-00-16. THE DENT WAS PLACED ON A 250 HOUR REINSPECT FOR CRACKING IAW EO8-53-98-815. (M)

Part: SEAT TRACKS — CORRODED (CABIN)

DURING C-CHECK INSPECTION, THE SEAT TRACKS WERE FOUND CORRODED BEYOND THE DEHAVILLAND LIMITS. SEAT TRACKS WERE REPAIRED IAW EO8-53-98-335. (M)

Part: DOOR STRUT — BROKEN (AIRSTAIR DOOR)

FLT 3040 - FLL-TPA - UPON ARRIVAL AT THE AIRCRAFT, THE PAX DOOR WOULD NOT OPEN. FOUND BOTH UPPER HANDRAIL STRUTS BROKEN. REMOVED AND REPLACED THE FORWARD AND AFT UPPER DOOR STRUTS. (M)

Part: TRIM SW — FAILED (RUDDER)

FLT NR 3064 - PBI-TPA - DURING FLIGHT, THE RUDDER TRIM MADE AN UNCOMMANDED RIGHT TRIM. THE PILOT RETURNED THE SWITCH TO CENTER MANUALLY AND CONTINUED ON TO TPA WITHOUT INCIDENT. REMOVED AND REPLACED THE RUDDER TRIM SWITCH. (M)

Part: GEAR DOOR — CRACKED (RT MLG)

FLT NR 3079 - MIA-JAX - ON APPROACH INTO TPA, THE RIGHT GEAR AFT DOORS WAS BINDING AND WILL NOT MANUALLY EXTEND. THE AIRCRAFT LANDED IN TPA WITHOUT INCIDENT. FOUND TO BE CRACKED IN TWO LOCATIONS. REPAIRED IAW RD8-54-068. (M)

Part: DN/UPLOCK SENSOR — FAILED (NLG)

FLT 3465 - MIA-MCO - ON FINAL APPROACH WITH GEAR SELECTED DOWN AND THREE GREEN, THE NOSE GEAR DOORS BEGAN TO CYCLE OPEN AND CLOSED WITH ACCOMPANYING INDICATIONS ON FLIGHT DECK. AIRCRAFT LANDED IN MCO WITHOUT INCIDENT. REMOVED AND REPLACED THE NOSE LANDING GEAR DRAG STRUT DOWN/UPLOCK SENSOR. (M)

Part: SENSOR — FAILED (NLG)

CRW/DCA - FLT 3075 - THE NOSE LANDING GEAR CYCLES WHEN THE GEAR HANDLE IS SELECTED DOWN. ALTERNATE EXTENSION PROCEDURES WERE FOLLOWED. THE AIRCRAFT LANDED IN DCA WITHOUT INCIDENT. REMOVED AND REPLACED THE NOSE GEAR DOWNLOCK PROXIMITY SENSOR.

Part: BYPASS SWITCH — FAILED (NR 2 FUEL PUMP)

FLT 3398 - BWI-YYZ - NR 2 FUEL FILTER BYPASS CAUTION LIGHT ILLUMINATED ON TAKEOFF. THE CREW ABORTED THE TAKEOFF WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 FUEL FILTER BYPASS SWITCH. (W)