N931HA

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,690 hrs · 75,902 cycles

CABIN FWD MOST FLOOR EMERGENCY LIGHT MODULE AT SEAT 1D-F1-RT EMERGENCY EXIT DOOR WILL NOT ILLIMINATE. REMOVED FLOOR LENS COVER, R & R LAMP IN LIGHT MODULE AND REINSTALLED AND SECURED LENS COVER, PN OL3071BPEGPL.

Part: BLEED AIR SYS — ODOR · airframe 67,258 hrs · 75,370 cycles

AFTER SELECTING ENGINE BLEEDS ON, CREW NOTICED FUEL ODOR IN CABIN AND FLIGHT COMPARTMENT AREA. SELECTED NR 2 BLEED OFF, SMELL DIMINISHED. GROUND RAN ACFT WITH BOTH NR 1 AND NR 2 BLEEDS SELECTED ON. NO ODOR NOTED. OK FOR SERVICE.

Part: ACTUATOR — WARNING LIGHT (NLG DOOR) · airframe 67,677 hrs · 75,150 cycles

NOSE GEAR DOOR AMBER LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. EXTENDED LANDING GEAR AND LIGHT REMAINED ON. R & R NOSE GEAR DOOR ACTUATOR IAW 32-20-26. SWUNG GEAR SEVERAL TIMES. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,820 hrs · 74,857 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,783 hrs · 74,813 cycles

RIGHT AFT EMERGENCY EGRESS LIGHT IS INOPERATIVE. R & R BULB FOR RT EMERGENCY EGRESS LIGHT. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,516 hrs · 74,483 cycles

RIGHT SIDE BOTTOM EXIT SIGN, ROW 4 EMERGENCY LIGHT INOPERATIVE. R & R THE BULB.

Part: SMOKE DETECTOR — NO TEST (CARGO BAY) · airframe 66,237 hrs · 74,130 cycles

CARGO SMOKE TEST 2 SWITCH WILL NOT TEST. R & R FORWARD SMOKE DETECTORT IAW AMM 26-12-01. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,132 hrs · 74,003 cycles

LEFT EMERGENCY LIGHT IS INOPERATIVE ON LEFT SIDE OF FUSELAGE. R & R EMERGENCY LIGHT BATTERY AT ROW 3AC. OPS CHECKED GOOD.

Part: LONGERON — DAMAGED (NR 2 NACELLE) · airframe 66,237 hrs · 74,130 cycles

OTBD AND MID HOLE IN NR 2 NACELLE LONGERON, AT POSITION 300 IS SHOWING MECHANICAL DAMAGE. PERFORM RD8-54-3294 ON BOTH HOLES. MOST OTBD HOLE FINAL DIAMETER IS .280. MID HOLE FINAL DIAMETER IS .250, EO8-54-15-0151 AND EO8-54-15-0152.

Part: STRUCTURE — DAMAGED (NACELLE) · airframe 66,237 hrs · 74,130 cycles

MOST OTBD HOLE SHOWING MECHANICAL DAMAGE LESS THEN 80 PERCENT. PERFORMED RD8-54-3292.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,218 hrs · 74,106 cycles

F/A'S EMERGENCY NORMAL GREEN LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,735 hrs · 73,539 cycles

4TH AFT RED FLOOR PATH EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED · airframe 65,688 hrs · 73,478 cycles

NR 2 ITT WENT TO ZERO IN FLIGHT. R & R T6 WIRING HARNESS FROM K FLANGE TO CONNECTOR AT FIREWALL IAW -8 POWER PLANT BUILD UP 71-00-02. OPS CHECKED GOOD IAW RUN UP MANUAL. OK FOR SERVICE.

Part: BRAKE — DAMAGED (MLG) · airframe 65,663 hrs · 73,446 cycles

DURING FINAL APPROACH, INBD ANTI-SKID. R & R NR 2 BRAKE ASSY IAW WC 32-42-11X. CREW PERFORMED ACFT TAXIING. OPS CHECKED GOOD. ANTI-SKID OPS CHECKED GOOD. NO CAUTION LIGHTS. OK FOR SERVICE.

Part: GROUND STUD — BROKEN (EMERGENCY LIGHT) · airframe 65,564 hrs · 73,323 cycles

FORWARD CEILING EMERGENCY LIGHT IS INOPERATIVE. REMOVED LIGHT LENS, FOUND GROUND TAB PUSH ON OUT. R & R HOUSING WITH RETAINED HARDWARE. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,486 hrs · 73,222 cycles

FLOOR EMERGENCY LIGHT AT ROW 4DF IS INOPERATIVE. R & R BULBS AT ROW 4DF EMERGENCY LIGHTS. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,215 hrs · 72,895 cycles

DURING EMERGENCY LIGHT SYS OPS CHECKED, FOUND RT FORWARD EGRESS LIGHT AND FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT POWER SUPPLY AT POSITION PS-2. OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (NR 2 GENERATOR) · airframe 65,215 hrs · 72,895 cycles

RIGHT AC BUSS CAUTION LIGHTS ILLUMINATED IN FLIGHT WITH ASSOCIATED CAUTION LIGHTS. CLEANED CONNECTOR ON NR 2 AC GENERATOR AND GCU. INSPECTED AC CONTACTOR BOX. GROUND RAN NR 2 ENGINE. OPERATED AC SYSTEMS, PROP HEAT AND WINDSHIELD HEAT. OPS CHECKED GOOD.

Part: CONTROL BOX — FAILED (EMERGENCY LIGHTS) · airframe 65,215 hrs · 72,895 cycles

EMERGENCY LIGHTS FLICKERING IN FLIGHT. R & R EMERGENCY LIGHT CONTROL BOX AND SECURED WITH RETAINING HARDWARE. INSPECTED CONTROL BOX CONNECTOR PLUG. NO DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,155 hrs · 72,823 cycles

AFT CEILING EMERGENCY LIGHT AND LT EGRESS LIGHT IS INOPERATIVE. R & R THE BATTERY PACK AT ROW 3AC. OPS CHECKED GOOD.

Part: SENSOR — MALFUNCTIONED (NLG WOW) · airframe 65,006 hrs · 72,641 cycles

W.O.W CAUTION LIGHT ILLUMINATED INTERMITTENLY ON TAKE OFF. R & R RT NLG SENSOR AND HARNESS. OPS CHECKED GOOD. OK FOR SERVICE AT THIS TIME. PSEU SHOWED FAULT ON RT NLG WOW SENSOR UPON ARRIVAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,693 hrs · 72,259 cycles

LEFT REAR EGRESS LIGHT AND MOST REAR CEILING EMERGENCY LIGHTS ARE INOPERATIVE. R & R THE BATTERY. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,693 hrs · 72,259 cycles

EXIT EMERGENCY LIGHT IS INOPERATIVE AT ROW 4AC. R & R THE BULB, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,529 hrs · 72,063 cycles

ONE FLOOR EMERGENCY EXIT LIGHT IS INOPERATIVE A ROW 1DF. R & R BULB, OPS CHECKED GOOD.

Part: MODULE — FAILED (EMERGENCY LIGHTS) · airframe 64,076 hrs · 71,521 cycles

CABIN EMERGENCY LIGHTS 11TH FROM FRONT OF AIRCRAFT INOPERATIVE. R & R EMERGENCY LIGHT MODULE IAW PPS 9.09 AND AMM 33-51-11.

Part: DISPLAY — MALFUNCTIONED (WX RADAR) · airframe 63,933 hrs · 71,355 cycles

RADAR DISPLAYED TX FLT, WOULD NOT PAINT WEATHER, CYCLED OFF AND ON THREE TIMES. RADAR OPS NORMAL. R & R RADAR INDICATOR AND RT IAW 34-41-04, OPS CHECKED GOOD, OK FOR SERVICE. INSPECTED CONNECTORS NO DEFECTS NOTED.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 63,511 hrs · 70,836 cycles

SMOKE WARNING LIGHT ILLUMINATED WITH NO EVIDENCE OF SMOKE. R & R NR 2 BAG BAY SMOKE DETECTOR. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,046 hrs · 70,268 cycles

EMERGENCY EXIT SIGN AT ROW 4, AFT FACING IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY AT ROW 3. SECURED FILLER PANEL AND PSU WITH ATTACHED HARDWARE. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,046 hrs · 70,268 cycles

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

Part: CURRENT LIMITER — FAILED (PROP DE-ICE) · airframe 62,921 hrs · 70,116 cycles

NR 1 PROPELLER DE-ICE PHASE SHOWS NO LOAD. FOUND AND REPLACED "B" PHASE CURRENT LIMITER. OPS CHECKED GOOD IN HANGER. GROUND RAN ACFT AND CYCLED AC SYSTEM CURRENT LIMITER REMAINED INTACT AT THIS TIME.

Part: BLEED AIR SYS — HAZE (APU) · airframe 62,777 hrs · 69,938 cycles

LIGHT SMOKEY HAZE IN ACFT WITH APU BLEED SELECTED. GROUND RAN ACFT. CONFIRMED HAZE TO BE PRODUCT OF APU BLEED. ENGINE BLEEDS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,789 hrs · 69,950 cycles

CEILING EMERGENCY LIGHT IS INOPERATIVE AT ROW 8. R & R BULB. OPS CHECKED GOOD.

Part: BLEED AIR SYS — SMOKE (CABIN) · airframe 62,777 hrs · 69,938 cycles

LIGHT SMOKEY HAZE IN ACFT WITH APU BLEED SELECTED. GROUND RAN ACFT, CONFIRMED HAZE TO BE PRODUCT OF APU BLEED. ENGINE BLEEDS CHECKED GOOD.

Part: GCU — WARNING LIGHT (AC GENERATOR) · airframe 62,685 hrs · 69,832 cycles

NR 1 PROP DEICE A-PHASE SHOWS NO ADVISORY LIGHT OR LOAD. NR 1 AC GENERATOR A-PHASE SHOWS ONLY 86 VOLTS AND .06 LOAD WITH PROP HEAT SELECTED OFF AND 67 VOLTS WITH PROP HEAT SELECTED ON. R & R NR 1 AC GCU AND CURRENT LIMITER. GROUND RAN ACFT. OPS CHECKED GOOD. OK FOR SERVICE.

Part: PLATE — CRACKED (LT WING) · airframe 62,597 hrs · 69,724 cycles

LEFT WING LADDER PLATE IS CRACKED FOR ACCESS PANEL 522AT AT INBD FWD CORNER. REPAIRED LADDER PLATE IAW RD8-57-6203, RD8-57-2413 AND EO8-57-13-0616.

Part: SEAT TRACK — CORRODED (BS 262) · corrosion level 2 · airframe 62,597 hrs · 69,724 cycles

SEAT TRACK CORRODED. CUT AND SPLICED NEW SECTION OF SEAT TRACK AT BS 262 IAW RD8-53-3074. COMPLIED WITH HFEC INSPECTION. NO DEFECTS NOTED.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 62,597 hrs · 69,724 cycles

TOP SURFACE OF PAX DOOR THRESHOLD HAS CORROSION AROUND NUT PLACES. REMOVED PAX DOOR THRESHOLD AND REPLACED WITH NEW AND RUB STRIP IAW DWG 85321241.

Part: BRAKE ASSY — SMOKE (NR 2) · airframe 62,487 hrs · 69,588 cycles

NR 2 BRAKE SMOKED DURING TAXI IN. R & R NR 2 BRAKE ASSY IAW W/C 32-10-03I AND 32-41-11X.

Part: RADAR — MALFUNCTIONED (WX SYS) · airframe 61,989 hrs · 68,968 cycles

WEATHER RADAR SHOWING IN FLIGHT 6 MESSAGE. R & R WEATHER RADAR IAW -8 MM 34-41-04 AND SB 34-18. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 61,175 hrs · 67,972 cycles

EMERGENCY EXIT DOOR LIGHTS HAS ONE BULB OUT. REPLACED BULB IAW AMM 33-52-00.

Part: UNKNOWN — UNKNOWN · airframe 60,708 hrs · 67,394 cycles

NR 2 PROPELLER A PHASE CAUSES EMERGENCY LIGHTS TO FLICKER AT 1050. INSPECTED BRUSH BLOCK AND NR 2 PROP HEATER BLADE WIRING. GROUND RAN ACFT WITH NO DEFECTS NOTED AT THIS TIME.

Part: CONTROL BOX — INTERMITTENT (EMERGENCY LIGHTS) · airframe 60,635 hrs · 67,294 cycles

EMERGENCY LIGHTS FLICKERED ON /OFF IN FLIGHT OVERHEAD AND EXIT SIGNS. INSPECTED BOTH BRUSH BLOCKS. NO DEFECTS NOTED. R & R EMERGENCY LIGHT CONTROL BOX. OPS CHECKED GOOD IAW WC 33-50-03.

Part: HSI — MALFUNCTIONED · airframe 60,284 hrs · 66,866 cycles

NR 2 HSI PERIODICALLY DISPLAYS HDG FLAG WITH SAHS. R & R NR 2 HSI. OPS CHECKED GOOD IAW AMM 34-26-01.

Part: CONNECTOR — FAILED (SPOILERS) · airframe 60,240 hrs · 66,815 cycles

AFTER TAKEOFF, ROLL SPOILER INBD HYD CAUTION LIGHT ILLUMINATED INTERMITTENTLY, THEN CONTINOUS. R & R CONNECTOR 2761P1 AT INBD ROLL SPOILER HYD PRESSURE SWITCH. GROUND RAN AND CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,216 hrs · 66,782 cycles

AFT CENTER CEILING EMERGENCY LIGHT IS INOPERATIVE. FOUND ROW 3AC EMERGENCY LIGHT BATTERY INOPERATIVE. R & R EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD IAW WC 33-50-03.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 60,117 hrs · 66,666 cycles

TEXT FLIGHT MESSAGE DISPLAYED IN FLIGHT. RETURN TO FIELD. WEATHER RADAR SYSTEM. R & R RADAR IAW SP 34-18. OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 59,607 hrs · 66,076 cycles

TWO RED FLOOR LEVEL EMERGENCY LIGHTS NEXT TO EACH OTHER INOPERATIVE AT FWD SECTION. RESEATED BATTERY AND CONNECTOR AT PS2. OPS CHECK GOOD.

Part: SENSOR — MALFUNCTIONED (WOW) · airframe 59,444 hrs · 65,898 cycles

WOW CAUTION LIGHT ILLUMINATED INFLIGHT FOR APPROX 1 MINUTE, THEN SELF CLEARED. R & R WOW 1 NLG SENSOR AND WOW 2 SENSOR. TARGET TEST GOOD AT PSEU. OK FOR SERVICE. ADJUSTED IAW AMM 32-20-11.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 59,126 hrs · 65,525 cycles

FLOOR EMERGENCY LIGHT AT ROW 6 AND 7 ARE INOPERATIVE. RELAMPED EMERGENCY FLOOR PATH LIGHTS AT ROW 6 AND 7 AS REQUIRED. OPS CHECKED GOOD.

Part: CONTROL BOX — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 53,023 hrs · 65,409 cycles

EMERGENCY LIGHTS FLICKER IN FLIGHT WHEN NR2 PROP 'A' PHASE IS SELECTED. R & R NR 2 PROP BRUSH BLOCK ASSY IAW -8 MM. GROUND RAN ACFT. OPS CHECKED GOOD. EMERGENCY LIGHTS FLICKERED IN CRUISE. OPS CHECKED EMERGENCY LIGHTS IAW MM 33-51-00. OPS CHECKED GOOD. R & R EMERGENCY LIGHTS CONTROL BOX AS PRECAUTIONARY MEASURE. OK FOR SERVICE IAW MM 33-51-00.

Part: BULB — OUT OF POSITION (CABIN LIGHTS) · airframe 59,028 hrs · 65,415 cycles

BURNING ODOR WITH LOWER GALLEY LIGHTS ON (BUFFET LIGHTS), NO ODOR WITH LIGHTS OFF. INSPECTED LIGHT ASSY'S AND FOUND BULB TOUCHING LENS ON AFT POSITION. REPOSITIONED, OK FOR SERVICE. NO ODOR DETECTED WITH LIGHTS ON (NO DAMAGE TO LENS).

Part: CONTROL BOX — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 59,018 hrs · 65,403 cycles

EMERGENCY LIGHTS FLICKERED DURING CRUISE, IN CABIN. OPS CHECKED EMERGENCY LIGHTS IAW MM 33-51-00. OPS CHECKED GOOD. R & R EMERGENCY LIGHT CONTROL BOX AS PRECAUTIONARY MEASURE. IF CONDITION RE-OCCURES MORE INFORMATION ON ACFT SYS CONDITIONS REQUIRED. OK FOR CONTINUED SERVICE IAW MM 33-51-00.

Part: WIRE — CHAFED (MLG WOW) · airframe 58,974 hrs · 65,350 cycles

WOW CAUTION LIGHT ILLUMINATED IN CRUISE. FOUND CHAFED WIRE ON 3261-38C22 AT RT MLG DISCONNECT. REPAIRED WIRE IAW AMM 20-45-08. CHECKED PROX SENSOR TARGET GAP ON ALL LANDING GEAR. ADJUSTED AS REQUIRED. IAW AMM 32-10-11. PERFORMED GEAR SWINGS. OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,956 hrs · 65,327 cycles

EXIT SIGN AT EMERGENCY EXIT DOOR AT ROW 4AC IS INOPERATIVE. R & R BULB AS REQUIRED.

Part: SMOKE DETECTOR — ACTIVATED (LAVATORY) · airframe 58,843 hrs · 65,191 cycles

LAV SMOLE DETECTOR SOUNDED ON PUSHBACK WITH ENGINE BLEEDS ON. WENT OUT WHEN ENGINE BLEEDS TURNED OFF. CHECKED NR 2 ENGINE OIL LEVEL, GROUND RAN NR 2 ENGINE SELECTED BLEEDS ON AND OFF. SMOKE DETECTOR DID NOT SOUND. R & R NR 2 ENGINE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,782 hrs · 65,123 cycles

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

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,782 hrs · 65,123 cycles

EMERGENCY PATH LIGHT AT ROW 8 IS INOP. R & R BULB IN EMERGENCY PATH FLOOR LIGHT AT ROW 8. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 58,752 hrs · 65,081 cycles

OIL ODOR IN CABIN AND FLIGHT DECK, DURING FLIGHT WITH ENG BLEEDS ON. MX INSPECTED BOTH ENG INTAKES, NO EVIDENCE OF ANY OIL LEAKS. CHECKED BOTH ENG QTYS NO OIL REQUIRED. GROUND RAN BOTH ENGS, CONFIRMED BLEEDS OPERATE NORMALLY. RAN ENGS FOR SEVERAL MINS WITH BLEEDS ON, OPS NORMAL AT THIS TIME.

Part: PUMP — FAILED (ENGINE OIL) · airframe 58,727 hrs · 65,055 cycles

NR 2 ENGINE OIL PRESSURE FLUX IN FLIGHT. INDICATED IN YELLOW ON FINAL FOR LANDING. SHUTDOWN ENGINE WHEN OIL PRESSURE DROPPED BELOW YELLOW ON ROLL OUT. R & R PROP GOV AND PUMP IAW MM 72-01-50. OPS AND LEAKED CHECKED GOOD.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 58,247 hrs · 64,509 cycles

DURING TAXI OUT, BAG BAY SMOKE WARNING ILLUMINATED INTERMITTENTLY. F/A CONFIRMED NO SMOKE OR FUMES IN BAG BAY.( BOTH TEST NORMAL). R & R FORWRD NR 2 BAG BAY SMOKE DETECTOR IAW 26-12-01. OPS CHECKED GOOD. OK FOR SERVICE.

Part: ELECTRONIC UNIT — FAILED (PROP TORQUE) · airframe 57,835 hrs · 64,041 cycles

AUTOFEATHER ARM LIGHT REMAINED ILLUMINATED INFLIGHT UNTIL TORQUE REDUCED BELOW 80 PERCENT, NR 1 TORQUE INDICATOR ERRATIC AND STICKS. R & R TSEU USING RETAINED HARDWARE AND RESECURED ALL CONNECTOR PLUGS AND BONDING WIRE. GROUND RAN ACFT WITH OPS CHECKS. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (EMERGENCY EXIT) · airframe 57,189 hrs · 63,302 cycles

RT AFT EMERGENCY EXIT BETA LIGHT IS DIMMER THAN COMPARING LIGHT. R & R USING ATTACHED HARDWARE.

Part: LIGHT — MALFUNCTIONED (EMERGENCY EXIT) · airframe 57,189 hrs · 63,302 cycles

LT AFT EMERGENCY EXIT BETA LIGHT IS DIMMER THAN THE CAMPARING LIGHT. R & R LIGHT USING ATTACHING HARDWARE.

Part: LIGHT — MALFUNCTIONED (EMERGENCY EXIT) · airframe 57,189 hrs · 63,302 cycles

RT FWD EMERGENCY EXIT BETA LIGHT IS DIMMER THAN THE COMPARING LIGHT. R & R LIGHT USING ORIGINAL ATTACHED HARDWARE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 56,615 hrs · 62,656 cycles

ROW 7 CEILING EMERGENCY LIGHT INOP. RELAMPED ROW 7 CEILING EMERGENCY LIGHT, REF AMM 33-20-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,921 hrs · 61,871 cycles

EMERGENCY FLOOR LIGHT INOP. R & R FLOOR LIGHT BULB. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 55,497 hrs · 61,395 cycles

WHEN SELECTING EMERGENCY LIGHTS OFF, (EMERGENCY LIGHT DISARM LIGHT) LIGHT DOES NOT ILLUMINATE. AFTER GROUND POWER IS APPLIED TO ACFT WITH EMERGENCY LIGHTS OFF, CAUTION LIGHT ILLUMINATES. WITH JUST BATTERY POWER, DUE TO SECONDARY BUSS'S NOT BEING POWERED, THIS CONDITION IS NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,083 hrs · 60,919 cycles

ROW 6, FLOOR EMERGENCY LIGHT NOT WORKING. REMOVE CLEAR LENS, R & R BULB AT SAID LOCATION, REINSTALLED CLEAR LENS TO FLOOR.

Part: WIRE — BROKEN (FLAP SELECTOR) · airframe 54,733 hrs · 60,509 cycles

AFTER TAKEOFF FLAPS FAILED TO RETRACT. FOUND BROKEN WIRE ON FLAP SELECTOR LEVER SWITCH, RE-SOLDERED WIRE TO SWITCH. OPS CHECKED IN ACCORDANCE WITH -8 MM 27-51-05 AND 27-53-05 CHECKED GOOD.

Part: TIRE — FLAT (NLG) · airframe 54,390 hrs · 60,132 cycles

NOSE TIRES WENT FLAT DURING TAXI OUT. R & R NOSE WHEEL ASSY IAW -8 MM 32-41-16. OK FOR SERVICE.

Part: OVERHEAT SENSOR — MALFUNCTIONED (WINDSHEILD) · airframe 53,896 hrs · 59,602 cycles

RT WINDSHIELD HEAT HOT CAUTION LIGHT ILLUMINATED IN FLIGHT. FOUND OVERHEAT SENSOR ON F/O WINDSCREEN OPEN. SWAPPED TO SPARE SENSOR, OPERATIONAL CHECKED GOOD IAW 30-41-00

Part: RELAY — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 53,137 hrs · 58,763 cycles

ON 8/1/2009 AT PHL, AUTO FEATHER DID NOT ARM DURING TAKEOFF ROLL. TORQUE INDICATED 85 PERCENT. SBY MAINTENANCE FOUND MICRO SWITCH 6121-S13 TO WORK INTERMITTENTLY. REMOVED AND REPLACED SWITCH IAW AMM 76-10-13. GROUND RAN AIRCRAFT IAW SRT MANUAL NO FIX. ISOLATED PROBLEM TO NR 2 SIDE. REMOVED AND REPLACED RELAY 6121-K5, NO FIX. REPAIRED BAD WIRE SPLICES AT 6121-513.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 53,133 hrs · 58,757 cycles

DURING TAKEOFF ROLL, AUTOFEATHER DID NOT ARM. REJECTED TAKEOFF. SBY MAINTENANCE CLEANED AND INSPECTED THROTTLE LAY SHAFT MICRO SWITCHES, NO DEFECTS NOTED. GROUND RAN, PERFORMED AUTO FEATHER RUN IAW -8 RUN-UP MANUAL, OPS CHECK GOOD, NO DEFECTS.

Part: RELAY — FAILED (AUTOFEATHER SYS) · airframe 53,098 hrs · 58,719 cycles

AUTOFEATHER DID NOT ARM DURING TAKEOFF ROLL. ABORTED TAKEOFF. C/W AUTOFEATHER TEST, SYSTEM OPS NORMALLY. DNAA INFO PER MP&P LOGIC DIAGRAM STEP 1. INSPECTED P/L MICROSWITCHES FOR CORRECT OPERATION. NO DEFECTS NOTED. CLEANED C/P'S AT TSCU. REMOVED AND REPLACED RELAY 6121-K5. GROUND RAN A/C, OPS CHECK GOOD.

Part: TSCU — FAILED (NR 1) · airframe 53,098 hrs · 58,719 cycles

NR 1 TORQUE GAUGE WENT TO ZERO ON T/O ROLL. REMOVED AND REPLACED NR 1 TSCU. RUN-UP CHECK GOOD IAW -8 RUN UP MANUAL. EVALUATION FLIGHT SATISFACTORY.

Part: RELAY — FAILED (AUTOFEATHER SYS) · airframe 53,098 hrs · 58,719 cycles

DURING TAKEOFF RUN, AUTOFEATHER DID NOT ARM. INSPECTED P/L MICRO SWITCHES FOR CORRECT OPERATION. NO DEFECTS NOTED. CLEANED C/P'S AT TSCU. REMOVED AND REPLACED RELAY 6121-K5. GROUND RAN, A/C OPS CHECK GOOD.

Part: POWER SUPPLY — SHORTED (CABIN) · airframe 53,075 hrs · 58,697 cycles

EMERGENCY LIGHT INOP ON CEILING AT ROW 2, FLOOR ESCAPE PATH AT ROW 2, 4, 5, 8, 9. REMOVED AND REPLACED POWER SUPPLY BASE.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 53,081 hrs · 59,295 cycles

FLIGHT ATTENDANT REPORTS ELECTRICAL SMELL IN AREA OF FORWARD CABIN AND CALL BUTTON LIGHT IS VERY WARM TO THE TOUCH. INSPECTED CABIN AREA AND FOUND SIDEWALL LIGHT HAVE A BURNT BULB HOLDER AT FORWARD END OF FIXTURE. FOUND BALLAST BAD. REMOVED AND REPLACED LIGHT FIXTURE AND BALLAST ASSY.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 52,912 hrs · 58,505 cycles

EMERGENCY LIGHTS FLICKER IN FLIGHT. REMOVED AND REPLACED F/A PANEL EMERGENCY LIGHT SWITCH.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,123 hrs · 37,634 cycles

UPON LINE INSPECTION AT SBY AN EMERGENCY LIGHT AT ROW 1 WAS FOUND BURNT OUT. REMOVED AND REPLACED LIGHT BULB AND THE OPERATIONAL CHECK WAS GOOD.

Part: GYRO — FAULTY (COCKPIT) · airframe 52,117 hrs · 57,627 cycles

AFTER STARTUP FLIGHT CREW SMELLED FUMES AND DETERMINED IT TO BE A DIRECTIONAL GYRO CONTROLLER. REMOVED AND REPLACED SAHS CONTROLLER & OPERATION CHECKED GOOD. NO DEFECTS. IN REFERENCE TO AMM 34-20-50.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,080 hrs · 57,592 cycles

FLOOR EMERGENCY LIGHT OUT LOCATED AT ROW 1. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT BULB.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,916 hrs · 57,414 cycles

DURING RON MX THE FIRST 2 EMERGENCY EXIT FLOOR LIGHTS IN THE PASSENGER CABIN WERE FOUND TO BE INOPERATIVE. THE EMERGENCY BATTERY LOCATED AT 3352/PS2 WAS CHANGED OUT. SYSTEM OPS CHECKED GOOD.

Part: ROLLER — DAMAGED (SPOILER) · airframe 51,808 hrs · 57,292 cycles

DURING TAKEOFF ROLL, THE AILERONS BECAME VERY STIFF AND HARD TO MOVE. THE TAKEOFF WAS ABORTED. THE ACFT WAS INSPECTED AND A FERRY PERMIT ISSUED TO RELOCATE TO A MX BASE WITH MORE EXTENSIVE FACILITIES. UPON FURTHER INVESTIGATION, THE SPOILER CABLE GUIDE ROLLERS LOCATED ABOVE THE BAG BAY DOOR BEHIND THE LT WING WERE FOUND TO BE GRINDING. THE ROLLERS WERE THEN CHANGED. AN EVALUATION FLIGHT WAS SATISFACTORILY PERFORMED AND THE ACFT WAS THEN RELEASED FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (ENGINE) · airframe 51,715 hrs · 57,177 cycles

NR 2 ELECTRONIC CONTROL UNIT FAILED IN FLIGHT. RESET NR 2 ELECTRONIC CONTROL UNIT & BETA LOCKOUT CIRCUIT BREAKERS GROUND RUN AIRCRAFT, OPS CHECK GOOD OK FOR SERVICE.

Part: RECEIVER — FAILED (COCKPIT) · airframe 51,715 hrs · 57,177 cycles

NUMBER ONE NAVIGATION RADIO FAILED IN FLIGHT, CONTROL HEAD DISPLAY WENT BLANK AND NAVIGATION FLAG SHOWING. REMOVED AND REPLACED NUMBER 1 NAVIGATION RECEIVER, CHECKED WITH TIC BOX, OPS CK'D GOOD IN ACCORDANCE WITH 34-55-00.

Part: REPAIR — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,167 hrs · 56,595 cycles

UNRECORDED AND CORRODED REPAIR FOUND ON LT FLOORBEAM AT STATIONS 270.5 AND 240.5. REMOVED UNRECORDED REPAIR AND REPLACED WITH A REPAIR APPROVED BY EO8-53-08-3278. BRACKETS FABRICATED IN HOUSE IAW DRAWING NUMBER 85320044 AND INSTALLED IAW SRM 51-40-00.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 5,108 hrs · 56,528 cycles

PROTRUDING DENT ON LT FUSELAGE AT STATION X195 BETWEEN STRINGER 23P AND 24P. REPAIRED DAMAGED IAW RD8-53-2181.

Part: BELTFRAME — CORRODED (FUSELAGE)

FWD EMERGENCY DOOR AREA, BELTFRAME AT STA X254 FOUND CORRODED AND SURFACE CORROSION ON DOOR SILL. AT STA X259 BLENDED BELTFRAME IAW SRM 53-00-16. CLEAT, THRESHOLD, STRAP AND BRACKET LOCALLY FABRICATED IAW DRAWINGS 8532075, 85320594, 85321705, 853206070.

Part: THRESHOLD — CORRODED (FUSELAGE)

FWD EMERGENCY DOOR AREA, BELTFRAME AT STA X254 FOUND CORRODED AND SURFACE CORROSION ON DOOR SILL. AT STA X259 BLENDED BELTFRAME IAW SRM 53-00-16. CLEAT, THRESHOLD, STRAP AND BRACKET LOCALLY FABRICATED IAW DRAWINGS 8532075, 85320594, 85321705, 853206070.

Part: BRACKET — CORRODED (FUSELAGE)

FWD EMERGENCY DOOR AREA, BELTFRAME AT STA X254 FOUND CORRODED AND SURFACE CORROSION ON DOOR SILL. AT STA X259 BLENDED BELTFRAME IAW SRM 53-00-16. CLEAT, THRESHOLD, STRAP AND BRACKET LOCALLY FABRICATED IAW DRAWINGS 8532075, 85320594, 85321705, 853206070.

Part: SKIN — CORRODED (FUSELAGE)

CORROSION FOUND ON BOTTOM SKIN OF COCKPIT STA X123, LT STRINGER 31. REPAIRED CORROSION ON BOTTOM SKIN IAW SRM 53-20-21.

Part: STRAP — CORRODED (FUSELAGE)

FWD EMERGENCY DOOR AREA, BELTFRAME AT STA X254 FOUND CORRODED AND SURFACE CORROSION ON DOOR SILL. AT STA X259 BLENDED BELTFRAME IAW SRM 53-00-16. CLEAT, THRESHOLD, STRAP AND BRACKET LOCALLY FABRICATED IAW DRAWINGS 8532075, 85320594, 85321705, 853206070.

Part: FITTING — CORRODED (FUSELAGE)

FWD EMERGENCY DOOR AREA, BELTFRAME AT STA X254 FOUND CORRODED AND SURFACE CORROSION ON DOOR SILL. AT STA X259 BLENDED BELTFRAME IAW SRM 53-00-16. CLEAT, THRESHOLD, STRAP AND BRACKET LOCALLY FABRICATED IAW DRAWINGS 8532075, 85320594, 85321705, 853206070.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,109 hrs · 56,528 cycles

DURING 'C' CHECK INSPECTIONS, AN UNRECORDED REPAIR AND CORROSION WAS DISCOVERED ON THE LT SIDE OF THE FLOOR BEAM LOCATED AT X270.5 AND Y9.25 UNDER THE SEAT RAIL. THE CORRODED FLOOR BEAM SECTION WAS REMOVED, REPAIR ANGLES AND A PACKER FABRICATED AND INSTALLED IAW EO8-53-3278.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 51,108 hrs · 56,528 cycles

UPPER AFT ANGLE OF INSIDE AIRSTAIR DOOR FOUND CORRODED. R&R PAX DOOR AFT ANGLE AND SHIMS IAW 52-10-00.

Part: THRESHOLD — CORRODED (FUSELAGE)

PAX DOOR THRESHOLD CORRODED. REPLACED PAX DOOR THRESHOLD IAW SRM 51-40-00.

Part: SEAT TRACK — CORRODED (FUSELAGE)

SEVERAL SPOTS OF MINOR CORROSION FOUND ON RT INBD SEAT TRACK FROM STA X259 TO X597. REMOVED CORROSION IAW RD8-53-1339 FROM X426 TO X526, R&R SEAT RAIL FROM X182 TO X425 AND X526 IAW SRM 51-40-00.

Part: SEAT TRACK — CORRODED (FUSELAGE)

SEVERAL SPOTS OF MINOR CORROSION FOUND ON RT INBD SEAT TRACK FROM STA X259 TO X597. REMOVED CORROSION IAW RD8-53-1339 FROM X426 TO X526, R&R SEAT RAIL FROM X182 TO X425 AND X526 IAW SRM 51-40-00.

Part: STRUCTURE — DENTED (FUSELAGE)

PROTRUDING DENT FOUND AT STATION X183.35 BETWEEN 24P AND 26P. REPAIRED DENT IAW RD 8-53-2181, HIGH FREQ EDDY CURRENT PERFORMED, NO DEFECT NOTED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 511 hrs · 56,528 cycles

FORWARD CARGO FLOOR AFT SUPPORT ANGLE CORRODED ON RT. R&R FORWARD CARGO FLOOR AFT SUPPORT ANGLE WITH SOLID RIVET AS PER STRUCTURAL REPAIR MANUAL 51-40-00.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 5,108 hrs · 56,528 cycles

PROTRUDING DENT FOUND AT STATION 183.350 BETWEEN 24P-25P. REPAIRED DAMAGE IAW RD8-53-2181.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,108 hrs · 56,528 cycles

SEVERAL SPOT OF MINOR CORROSION FOUND ON RT INBD SEAT TRACK FROM STA X259 TO 597. R&R SEAT TRACK IAW STRUCTURAL REPAIR MANUAL 51-40-00.

Part: SKIN — DENTED (ZONE 100) · airframe 51,108 hrs · 56,528 cycles

PROTRUDING DENT FOUND AT STATION X178.200 BETWEEN STRINGER 30S AND 31S. REPAIRED DAMAGE IAW RD8-53-2181.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

7TH FLOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPS CHECK GOOD. (K)

Part: RECEPTACLE — BURNED (GALLEY)

WARMER NR 1 SOCKET ON AIRCRAFT LOOKS DAMAGED AND DOES NOT WORK. WARMER NR 2 OPERATES NORMALLY. WARMER NR 2 HAS SMOKE ODOR WHEN SELECTED ON. INSPECTED FOR DAMAGE FOUND BOTH AIRCRAFT SOCKETS TO BE DAMAGED DURING HIDDEN DAMAGE INSPECTION, REF LOG BOOK PG 269250-1 BOTH RECEPTACLES WERE REPLACED, OPS CHECK GOOD. (A)

Part: DADC — FAULTY · airframe 50,515 hrs · 55,843 cycles

TWO MINUTES AFTER ROTATION, BOTH YAW DAMPERS DISENGAGED AND RECEIVED AHARS DATA INVALID MESSAGE. BOTH 802 PANELS WENT BLANK AND ALTITUDE PRE-SELECT WENT TO ALL DASHES. BOTH FLIGHT DIRECTORS FAILED MULTIPLE TIMES.

Part: UNKNOWN — ODOR (CABIN) · airframe 50,168 hrs · 55,491 cycles

SMOKEY LIKE SMELL IN REAR CABIN DURING CRUISE. RAN AIRCRAFT ON GROUND WITH APU OFF, ENGINE BLEEDS ON, ONE AT A TIME AND BOTH TOGETHER AND OFF, NO SMELL NOTICED INSIDE AIRCRAFT. OK FOR SERVICE.

Part: CONTROL BOX — INTERMITTENT (CABIN) · airframe 49,691 hrs · 54,963 cycles

DURING FLIGHT, THE CABIN EMERGENCY LIGHTING CYCLED ON AND OFF. CREW NOTED THAT THE PROP DEICE SYSTEM WAS NOT SELECTED ON. MAINTENANCE CHANGED THE EMERGENCY LIGHTS SYSTEM CONTROL BOX AND CHECKED OPERATIONS IAW PIEDMONT WORKCARD PROCEDURES. SYSTEM CHECKED GOOD AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CABLE — BROKEN (COCKPIT) · airframe 49,566 hrs · 54,828 cycles

MAIN LANDING ALTERNATE RELEASE CABLE BROKE IN FLIGHT DECK AT T-HANDLE. REMOVED AND REPLACED THE CABLE, OPERATIONAL CHECK GOOD.

Part: CONTACTOR — SMOKE (STARTER) · airframe 49,286 hrs · 54,540 cycles

THE CREW REPORTED NUMBER 2 ENGINE ROTATES AND SMOKE COMING FROM THE STARTER GENERATOR WHEN GROUND POWER IS APPLIED TO THE AIRCRAFT. THE NUMBER 2 STARTER GENERATOR AND START CONTACTOR WERE REMOVED AND REPLACED.

Part: TSCU — INOPERATIVE (AUTOFEATHER SYS) · airframe 48,823 hrs · 54,040 cycles

AUTOFEATHER ARM LIGHT REMAIN ILLUMINATED AFTER AUTOFEATHER SWITCH SELECTED OFF. DIVERTED TO MDT. REMOVED AND REPLACED TSCU AND REMOTE C/B 2431-CB4. OPS CHECKS GOOD.

Part: HYDRAULIC SYSTEM — LEAKING (NR 1) · airframe 44,875 hrs · 49,792 cycles

NR 1 HYDRAULIC QUANTITY DROPPED TO .5 QTS ON FINAL. REMOVED AND REPLACED HYDRAULIC TUBE AT CASE DRAIN MANIFOLD.

Part: SENSOR — FAILED (MLG) · airframe 44,250 hrs · 49,114 cycles

AFTER SELECTING GEAR UP BOTH MAIN GEAR DOOR AMBER LIGHTS, NOSE GEAR RED IN TRANSIT LIGHT AND GEAR SELECTOR HANDLE AMBER LIGHTS REMAINED ON. CYCLED GEAR NO FIX. REMOVED AND REPLACED THE DRAG STRUT SENSOR.

Part: HINGE — MISSING (LT MLG DOOR) · airframe 43,443 hrs · 48,224 cycles

LT MAIN FORWARD GEAR DOOR REMAINED DOWN AFTER GEAR RETRACTION. REPLACED LT MAIN FORWARD GEAR DOOR AND MISSING HARDWARE ON AFT HINGE. REPLACED DAMAGED FRAME ASSY. ADJUSTED DOOR AND SWUNG GEAR.

Part: CONTROL HEAD — SMOKE (COCKPIT) · airframe 41,516 hrs · 46,184 cycles

CREW NOTICED SMOKE AND SMELLED ODOR COMING FROM KNS 660, CREW TURNED OFF KNS 660 SMOKE AND ODOR WENT AWAY. KNS 660 REMOVED FOR INSPECTION FOUND NO DEFECTS, ALSO REMOVED RADAR DISPLAY UNIT, NO DEFECTS NOTED. PLACED KNS 660 ON MEL.

Part: MOUNT — CRACKED (NR 1 ENGINE) · airframe 40,997 hrs · 45,629 cycles

NR 1 ENGINE INBOARD AFT ENGINE MOUNT STRUT IS CRACKED AT UPPER WELD AREA. REMOVED AND REPLACED STRUT.

Part: TRANSMITTER — DEFECTIVE (TE FLAPS) · airframe 40,857 hrs · 45,480 cycles

TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL, ABORTED TAKE-OFF R&R RT RVDT

Part: CONTROL UNIT — INOPERATIVE (PROPELLER) · airframe 40,514 hrs · 45,116 cycles

DURING CLIMB PROP AT 1050 PROP JUMPED BETWEEN 1020 & 1080 AIRCRAFT RETURNED TO FIELD, CAPT REPORTED THE PROP SYNC WAS ON AT THE TIME AND THEY DID NOT TURN IT OFF. R & R NR 2 PCU.

Part: BEAM — CRACKED (FUSELAGE) · airframe 40,438 hrs · 45,030 cycles

TRANSVERSE BEAM HAS A CRACK WHERE THE ALTERNATE RELEASE CABLE GOES THROUGH, ABOUT .4 INCHES LONG. REPAIRED PER EO 8-53-04-0148.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,145 hrs · 44,730 cycles

R/S UNDERFLOOR STR 27 BETWEEN REAR SPAR FRAME AND X467 WAFFLE DOUBLER IS DEPARTING SKIN PANEL.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 38,815 hrs · 43,364 cycles

THREE EACH EMERGENCY LIGHTS ILLUMINATE WHEN SELECTED OFF AND AIRCRAFT BATTERIES ARE ON. RIGHT EMERGENCY EXIT ROW 1 AND EXIT CENTER AISLE AND CEILING LIGHT FORWARD. REPLACED BATTERY BASE AND POWER SUPPLY.

Part: CONE — BROKEN (NR 1 NACELLE) · airframe 38,187 hrs · 42,682 cycles

CREW REPORTED A WHISTLE SOUND FROM NR 1 ENGINE WHENEVER POWER WAS APPLIED. FOUND A PIECE OF THE NR 1 LOWER COWL AFT CONE HAD BROKEN OFF CAUSING FOD DAMAGE TO NR 1 ENGINE. REPLACED ENGINE AND LOWER COWL.

Part: SWITCH — INTERMITTENT (CABIN) · airframe 37,486 hrs · 41,926 cycles

FORWARD RIGHT EMERGENCY EXIT DOOR SIGN INTERMITANT. REPLACED FLIGHT ATTENDANT PANEL NORMAL ON SWITCH, OPERATIONAL CHECK GOOD.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM) · airframe 36,312 hrs · 40,649 cycles

CREW REPORTED LOSS OF HYDRAULIC FLUID FROM NR 2 HYD SYSTEM AND SUBSEQUENT ILLUMINATION OF ISO VALVE CAUTION LIGHT. CREW DECLARED AN EMERGENCY AND RETURNED TO MIA. FOUND 2 HYDRAULIC LINES AT NR 1 MLG FWD DOOR ACTUATOR WITH PIN HOLES. INSTALLED TEMPORARY FLEX LINES IAW SPECIAL PROCEDURE 20.1.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM) · airframe 36,312 hrs · 40,649 cycles

CREW REPORTED LOSS OF HYDRAULIC FLUID FROM NR 2 HYD SYSTEM AND SUBSEQUENT ILLUMINATION OF ISO VALVE CAUTION LIGHT. CREW DECLARED AN EMERGENCY AND RETURNED TO MIA. FOUND 2 HYDRAULIC LINES (P/N'S 82970010-399 & 82970010-401) AT NR 1 MLG FWD DOOR ACTUATOR WITH PIN HOLES. INSTALLED TEMPORARY FLEX LINES IAW SPECIAL PROCEDURE 20.1.

Part: BULB — FAILED (NR 2 ENGINE)

NR 2 OIL TEMP FLUCTUATED TO BETWEEN 100 DEGREES AND 115 DEGREES THEN REPEATED TWICE. INSPECTED ENGINE, REMOVED AND REPLACED ENGINE OIL TEMP INDICATOR, NO FIX. REMOVED AND REPLACED ENGINE OIL TEMP BULB, LEAK AND OPERATIONAL CHECK GOOD. SERVICED ENGINE WITH 2 QUARTS OF OIL.

Part: UNKNOWN — ODOR (CABIN) · airframe 31,426 hrs · 35,482 cycles

IN FLIGHT THE THE CREW REPORTED A PLASTIC BURN SMELL COMING FROM THE GASPERS. THE F/A REPORTED THAT THE SMELL WAS ORIGINATING IN THE AREA OF THE COAT CLOSET. MAINTENANCE INSPECTED ELECTRICAL EQUIPMENT BAY, AVIONICS RACK AND THE UNDER FLOOR AREA ADJACENT TO COAT CLOSET. ALSO, RAN UP AIRCRAFT WITH HIGH ELECTRICAL LOAD ITEMS TURNED ON. NO DISCREPANCIES WERE FOUND.

Part: PROP — DAMAGED (NR 1 ENGINE)

WHEN DEPARTING DCA, ACFT VIBRATED BAD. NR 1 PROP, NR 2 BLADE DAMAGED. NR 1 ENG REQUIRES VISUAL INSP OF 1ST STAGE IMPELLER FOR EVIDENCE OF SOFT OR HARD MATERIAL INGESTION. NR 1 PROP NR 2 BLADE REQUIRES SB14SF-61-118 PERFORMED BEFORE REVENUE FLIGHT. INSPECTED AND FOUND NICKLE SHEATH MISSING FROM NR 1 PROP NR 4 BLADE. REMOVED AND REPLACED NR 1 PROP NR 2 BLADE, OPS CHECK AND LEAK CHECK GOOD. INSPECTION COMPLETE, NO DEFECTS NOTED. ACFT FERRIED.

Part: MECHANISM — OUT OF ADJUST (LT MLG DOOR)

AFTER GEAR RETRACTION LEFT GEAR DOOR LIGHT AND DOOR OPEN LIGHT. CYCLED GEAR AND LIGHT STILL ON BUT DOOR CLOSED, SLOWLY FELL OPEN AGAIN. ADJUSTED LEFT HAND MAIN LANDING GEAR FORWARD DOOR ROD.

Part: MECHANISM — OUT OF ADJUST (RT MLG DOOR)

RIGHT HAND MAIN LANDING GEAR DOORS WOULD NOT OPEN. ADJUSTED CABLE AT NR 2 NACELLE FOR AFT DOORS. CYCLED DOOR SERVERAL TIMES OPENING DOORS WITH RELEASE HANDLE. OPERATIONAL CHECK GOOD.

Part: SKIN — DENTED (BS 202)

DENT ON RIGHT FUSELAGE FROM LAVATORY CAP HANDLE, LOCATED .5 INCHES BELOW STRINGER 265 RIVET ROW 2 INCHES FORWARD OF FRAME X202. DENT IS .020 INCHES DEEP, 1.2 INCHES LONG AND .4 INCHES WIDE. INSPECTED DENT AND DEFERRED.

Part: BRACKET — CRACKED (LT WING)

LEFT WING FLAP WELL PANEL MOUNT BRACKET (SECONDARY STRUCTURE) UNDER OUTBOARD ROLL SPOILER ACTUATING HINGE CRACKED ON FORWARD OUTBOARD EDGE OF OUTBOARD LIGHTENING HOLE. REPAIRED CRACK.

Part: DOOR — SEPARATED (NR 2 NACELLE)

FLT 3293 - CHO-PIT - SPR ACCESS DOOR CAME OFF. REMOVED DOOR HINGES AND INSPECTED AREA, ENTERED ON CDC. ON SEPT 18, REINSTALLED DOOR AND HINGES. CLEARED CDC ITEM. (M)

Part: STOP — SEPARATED (HORIZ STAB)

FLT 3264 - EWN-CLT, FULL NOSE DOWN ELEVATOR TRIM REQUIRED FOR STRAIGHT AND LEVEL FLIGHT. DISCOVERED RIGHT ELEVATOR TOP STOP BUMPER BROKEN OFF ALLOWING ELEVATOR TO STRIKE RUDDER DURING RON IN EWN. REMOVED AND REPLACED ELEVATOR BUMPER AND REPAIRED ELEVATOR AND TRIM TAB. (M)

Part: HYD LINE — FAILED (NR 1 ENGINE)

FLT 3270 - CLT-CRW - AFTER TAKEOFF, THE NR 1 HYDRAULIC SYSTEM BEGAN RAPIDLY LOOSING QUANTITY. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED AND LANDED AT CLT WITHOUT INCIDENT. INSTALLED TEMP FLEX LINE ON NR 1 ENGINE BETWEEN NR 1 AND NR 2 FLIGHT SPOILER DUMP VALVE. (M)

Part: VALVE — MALFUNCTIONED (CABIN DOOR)

FLT 3451 - TPA-JAX - THE PASSENGER DOOR WOULD NOT CLOSE AT DEPARTURE TIME. FREED DOOR SEAL PRESSURIZATION VALVE. WHEN AIRCRAFT ARRIVED IN JAX, THE DOOR WAS DIFFICULT TO OPEN. REMOVED AND REPLACED THE AIRSTAIR DOOR SEAL PRESSURIZATION VALVE. (M)