N940HA

Part: SENSOR — FAILED (NLG) · airframe 67,505 hrs · 75,809 cycles

DURING AND AFTER GEAR RETRACTION, NOSE GEAR REMAINED IN TRANSIENT AND MAIN GEAR DOOR AMBER LIGHTS REMAINED ILLUMINATED. INSPECTED AND FOUND DRAG STAY UPLOCK SENSOR BAD. R & R THE SENSOR. CYCLED GEAR SEVERAL TIMES. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,323 hrs · 75,597 cycles

EMERGENCY FLOOR LIGHT AT ROW 1 INOPERATIVE. REMOVED AND REPLACED THE BULB.

Part: TRANSCEIVER — INOPERATIVE (WEATHER RADAR) · airframe 67,160 hrs · 75,398 cycles

WEATHER RADAR INTERMITTENTLY DISPLAYS TX FLT AND WAS NOT PAINTING IN CRUISE FLT AT ABOUT 4K, DID START WORKING INTERMITTENTLY DURING RETURN TO FIELD. R & R WEATHER RADAR RT UNIT AND C/W OPS CHECK IAW BULLETIN 34-18. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,139 hrs · 75,723 cycles

4TH EMERGENCY FLOOR LIGHT FROM FRONT IS INOPERATIVE. R & R LIGHT BULB, RESECURED EMERGENCY LIGHT TRIM COVER.

Part: GCU — FAILED (AC GENERATOR) · airframe 65,727 hrs · 73,994 cycles

RIGHT AC BUSS CAUTION LIGHT ILLUMINATED IN FLIGHT WITH LOSS OF ASSOCIATED SYSTEMS. R & R ACFT GCU IAW 24-21-00 AND R & R AC GENERATOR IAW WC 24-20-11R.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,426 hrs · 74,504 cycles

REAR LEFT EMERGENCY LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK PS3. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 66,426 hrs · 74,504 cycles

CABIN EMERGENCY LIGHTS FLICKERED DURING FLIGHT WITH PROP HEAT ON AND OFF. CLEANED AND RE-SEATED CONNECTOR ON EMERGENCY LIGHTING CONTROL BOX. GROUND RAN ACFT, OPS CHECKED NORMAL AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,423 hrs · 74,498 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,423 hrs · 74,498 cycles

RED FLOOR EMERGENCY LIGHT IS INOPERATIVE AT ROW 1DF. R & R THE BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,310 hrs · 74,359 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,310 hrs · 74,359 cycles

EMERGENCY FLOOR LIGHT IS OUT AT ROW 2. R & R BULBS AT ROW 2. OPS CHECKED GOOD.

Part: CONTROL BOX — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 66,260 hrs · 74,301 cycles

PASSENGER EMERGENCY LIGHTS FLICKERED DIMLY DURING CLIMB OUT WITH PROP DEICE OFF, BUFFER LIGHT FLUCTUATING AT THE SAME TIME. R & R EMERGENCY LIGHT CONTROL BOX IAW MM 33-51-11. OPS CHECKED GOOD. OK FOR SERVICE.

Part: INVERTER — MALFUNCTIONED (PRIMARY) · airframe 65,126 hrs · 72,953 cycles

PRIMARY INVERTER CAUTION LIGHT ILLUMINATED. R & R PRIMARY INVERTER IAW MM24-22-00. OPS CHECKED GOOD. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN · airframe 64,942 hrs · 72,729 cycles

RUDDER TRAVEL TO LEFT INDICATION IS 8 DEGREES AT O FLAPS AND 11 DEGREES AT 5 DEGREES OF FLAPS. INSPECTED RUDDER TRAVEL IAW MM 27-05-16 AND INSPECTED PSEU OUTPUT VOLTAGE TO FDAU. FOUND NO FAULTS WITH RUDDER OPERATION O INDICATION IAW AMM BULLETIN NR 27-28.

Part: CONNECTOR — CONTAMINATED (AUTOFEATHER SYS) · airframe 64,429 hrs · 72,112 cycles

ABORTED TAKEOFF DUE TO AUTO FEATHER DID NOT ARM. AFTER ABORT, CREW TESTED A/F. TESTED NORMALLY. PUSHED POWER LEVERS UP, ARM LIGHT ILLUMINATED AT 76 PERCENT. INSPECTED POWER LEVER MICROSWITCHES 6121-S6, 7, 8 AND 9. NO DEFECTS NOTED. INSPECTED NR 1 AND NR 2 TSCU CONNECTOR PLUGS. NO DEFECTS NOTED. FOUND SMALL AMOUNT OF FLUID AND CLEANED CONNECTOR PLUGS. REINSTALLED NR 1 AND NR 2 CONNECTOR PLUGS. REMOVED AND REPLACED BOTH TSCU. OPS CHECKED GOOD. RUN UP MANUAL.

Part: APU — FIRE · airframe 64,396 hrs · 72,071 cycles

FUELER REPORTED FLAMES AND SMOKE COMING FROM APU EXHAUST, APU HUNG START. DISCHARGED APU FIRE BOTTLE. R & R APU FIRE BOTTLE IAW WC, 26-20-09X, 26-20-04F AND 26-21-01. RAN APU AND FOUND TO BE HUNG START. R & R FORWARD PURGER VALVE IAW HS 49-20M, THEN START NOZZLE AND IGNITER DUE TO COKING IAW WC 49-30-07C AND 49-40-41. OPS AND LEAKED CHECKED GOOD. OK FOR SERVICE.

Part: BRUSH BLOCK — FAILED (PROPELLER HEAT) · airframe 64,344 hrs · 72,007 cycles

RIGHT PROPELLER PHASE "B" CIRCUIT BREAKER TRIPPED IN FLIGHT. R & R NR 200 PROPELLER BRUSH BLOCK. FOUND HEATER LEADS AT 2 AND 3 BLADES CHAFED. R & R SAID LEADS IAW H/S MM61-10-00. OPS CHECKED GOOD. OK FOR SERVICE.

Part: PROPELLER — VIBRATION · airframe 64,146 hrs · 71,772 cycles

MODERATE PROPELLER VIBRATION AT 1050 N/P. OK AT 900N/P. R & R NR 2 PROPELLER ASSY IAW MM 61-10-06. PERFORMED -8 RUN UPS IAW START RUN TAXI MANUAL. NO PROPELLER VIBRATION NOTED AT THIS TIME.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,847 hrs · 71,416 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROW 7. R & R POWER SUPPLY AT ROW 3AC. OPS CHECKED GOOD.

Part: COVER — BURNED (COCKPIT) · airframe 63,912 hrs · 71,373 cycles

BURNING ODOR IN COCKPIT. INSPECTED AND FOUND CLOTH COVER OF OBSERVERS HEADREST STOWAGE TOUCHING DOME LIGHT. REPOSITION COVER AS REQUIRED. NO HIDDEN DAMAGE FOUND. OK FOR SERVICE.

Part: SPOILER SYS — MALFUNCTIONED · airframe 63,800 hrs · 71,358 cycles

OTBD ROLL SPOILER REMAINED RETRACTED WITH TAXI SWITCH SELECTED TO FLIGHT POSITION WITH ROLL SPOILER CAUTION LIGHT. ABORTED TAKEOFF. PULLED AND COLLARED CIRCUIT BREAKER C7 AND F6 IAW APPENDIX GROUND AND ROLL SPOILER GROUND MODE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,471 hrs · 70,956 cycles

CENTER AISLE EMERGENCY LIGHT IS INOPERATIVE AT ROW 2. R & R BULB. OPS CHECKED GOOD.

Part: FILLER — MISSING (EMERGENCY LIGHT) · airframe 63,411 hrs · 70,875 cycles

THE FLOOR EMERGENCY LIGHT STRIP FWD END AROUND ROW 1 FILLER MISSING AND WIRES EXPOSED. LIFTED EMERGENCY LIGHT STRIP FLOOR COVER INSTALLED THE FILLER OVER EXPOSED WIRE AND REINSTALLED EMERGENCY LIGHT STRIP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,467 hrs · 69,729 cycles

EMERGENCY LIGHTS WILL NOT TEST. R & R EMERGENCY LIGHT BATTERY IAW WC'S 33-50-03 AND 33-50-05. OPS CHECKED GOOD, OK FOR SERVICE.

Part: CONNECTOR — CONTAMINATED (PRESSURE SWITCH) · airframe 62,104 hrs · 69,284 cycles

ROLL SPOILER INBD HYD CAUTION LIGHT ILLUMINATED IN FLIGHT. SELECTED OFF IAW CHECK LIST. FOUND PRESSURE SWITCH ELECTRICAL CONNECTOR WET & DIRTY. CLEANED CONNECTOR, CONNECTION & CLEANED SURROUNDING HYD LINES AND SWITCH. PERFORMED OPS & LEAK CHECKS. NO DISCREPANCIES FOUND AT THIS TIME. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,045 hrs · 69,220 cycles

ROW 1 FLOOR EMERGENCY PATH LIGHT IS INOPERATIVE. REPLACED LAMP. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (ENGINE) · airframe 61,544 hrs · 68,623 cycles

BOTH ENGINES MANUAL CAUTION LIGHTS ILLUMINATED IN FLIGHT. NO ENGINE ROLL BACK MODE SWITCH LIGHTS REMAINED ON. INSPECTED ENGINE CONDITION PANEL. NO DEFECTS NOTED. CYCLED BETA LOCKOUT CIRCUIT BREAKER IN DC CONTACTOR BOX. CREW GROUND RAN ACFT. TESTING BOTH ECU'S. NO DEFECTS NOTED. CAUTION LIGHTS OPERATED NORMALLY. OK FOR SERVICE.

Part: DUCT — DIRTY (CABIN AIR) · airframe 61,361 hrs · 68,389 cycles

LIGHT ODOR NOTICED WITH ENGINE BLEEDS SELECTED ON. REMOVED ALL DUCTS FROM HEAT EXCHANGER, ACM AND CONDENSOR MIXER, CLEANED DUCTS. REINSTALLED ALL DUCTS AND SAFTIED WIGGENS FITTING. NO ODOR NOTED.

Part: ACM — ODOR · airframe 61,355 hrs · 68,381 cycles

DURING PUSH BACK, HEARD GRINDING NOISE ASSOCIATED WITH ODOR. SELECTED APU BLEED OFF, WHICH ELIMINATED NOISE AND ODOR. INSPECTED AND FOUND ACM SEIZED. R & R ACM IAW WC 21-50-03, STEPS 13 AND 25. OPS CHECKED GOOD. NO NOISE OR ODOR NOTICED.

Part: CONNECTOR — DIRTY (PRESSURE SWITCH) · airframe 60,765 hrs · 67,667 cycles

NR 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED DURING CLIMB WITH NO OTHER INDICATION OF OIL PRESSURE LOSS. LIGHT EXTINGUISHED AFTER LEVELING OUT. INSPECTED NR 2 ENGINE, OIL QTY WAS GOOD. CLEANED BOTH CONNECTORS ON THE PRESSURE SWITCH AND PRESSURE TRANSMITTER. CREW GROUND RAN ACFT TO TAKEOFF POWER. NO DEFECTS NOTED.

Part: BULB — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 58,865 hrs · 65,334 cycles

RIGHT FORWARD EMERGENCY LIGHT ON OUTSIDE OF FUSELAGE IS DIM. R & R BULB. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,865 hrs · 65,334 cycles

MID CABIN CEILING EMERGENCY LIGHT IS INOPERATIVE. R & R LIGHT BULB IAW 33-51-00. OPS CHECKED GOOD.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,387 hrs · 64,779 cycles

AIRSTAIR DOOR FLOOR THRESHOLD IS CORRODED. REMOVED CORROSION FLOOR THRESHOLD. INSTALLED NEW THRESHOLD ASSY AND RUBBING STRIP IAW 85321241.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 58,285 hrs · 64,661 cycles

BAG BAY SMOKE WARNING LIGHT ILLUMINATED ON APPROACH AND WENT OUT. NO SMOKE IN BAG BAY. R & R NR 2 BAG BAY SMOKE DETECTOR IAW MM 26-12-01. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,240 hrs · 48,064 cycles

EMERGENCY EXIT SIGN NEAR FLOOR BY AIRSTAIR DOOR HAS 1 BULB INOPERATIVE. R & R COVER PLATE. R & R BULB. OPS CHECKED GOOD. REINSTALLED COVER PLATE.

Part: SHUTOFF VALVE — INOPERATIVE (FUEL SYSTEM) · airframe 57,899 hrs · 64,247 cycles

WHEN PERFORMING FIRE PROTECTION TEST, PULLED NR 2 TEE HANDLE AND IT DID NOT ILLUMINATE FUEL OFF VALVE. LIGHT FILAMENT TESTS OK. R & R NR 2 ENGINE FUEL SHUTOFF VALVE ACTUATOR IAW MM 28-21-21. OPS CHECKED GOOD.

Part: DADC — FAILED (NR 1) · airframe 57,653 hrs · 63,974 cycles

ON ROTATION WITH HSI SELECTED TO NR 1, DADC INVALID MESSAGE APPEARED, LOST SAT, ALT PRE SELECT WENT BLANK AND CAPT ALTIMETER FLAGGED. ALL CLEARED WHEN NR 2 ADC WAS SELECTED. R & R NR 1 DADC. OPS CHECKED GOOD IAW 34-12-02.

Part: BRUSH BLOCK — MELTED (PROPELLER HEAT) · airframe 57,483 hrs · 63,783 cycles

EMERGENCY LIGHTS FLICKERED IN FLIGHT. MX INSPECTED AND FOUND NR 2 BRUSH BLOCK MELTED. R & R NR 2 ENGINE BRUSH BLOCK IAW 61-10-11. GROUND RAN ACFT. OPS CHECKED GOOD.

Part: BRACKET — FAILED (MLG DOOR) · airframe 56,414 hrs · 62,590 cycles

RIGHT DOOR AMBER LIGHT ILLUMINATED ON GEAR RETRACTION. CYCLED GEAR,ON EXTENSION, GEAR WENT OUT WHEN RETRACTED. LIGHT CAME BACK ON. INSTALLED NEW HOOK AND PROX SENSOR BRACKET ASSY IAW MM 32-10-21. PERFORMED SEVERAL GEAR SWINGS, ALSO PERFORMED EMERGENCY ALTERNATE RELEASE. ALL OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 55,968 hrs · 62,102 cycles

LT GEAR DOOR AMBER LIGHT REMAINED ON AFTER GEAR RETRACTION. CHECKED LT GEAR DOOR RIGGING AND BLED AIR AT PRESSURE LINES. CYCLED GEAR, OPS CHECKED GOOD PENDING SATISFACTORY LEVAL FLIGHT.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 55,555 hrs · 61,655 cycles

EMERGENCY FLOOR PATH LIGHT IS INOP AT ROW 1. R & R FLOOR PATH LIGHT LAMP AT ROW 1 AND CLOSED ACCESS PANEL.

Part: SMOKE DETECTOR — SHORTED (CARGO BAY) · airframe 55,498 hrs · 61,589 cycles

BAG BAY SMOKE DETECTOR INTERMITTENTLY ILLUMINATED ON GROUND AND SYS TESTED GOOD. NO SMOKE SEEN. R & R NR 2 BAGGAGE SMOKE DETECTOR IAW 26-12-01. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 54,805 hrs · 60,828 cycles

APPROX 8 MINUTES AFTER TAKEOFF, (LEVEL AT 7000 FT) IN DRY ICING CONDITIONS, NO RAIN- LIGHT VERGA, RT AC BUSS CAUTION LIGHT ILLUMINATED WITH SUBSEQUENT CAUTION LIGHTS ASSOCIATED WITH THE BUSS, OCCURED SHORTLY AFTER PROP HEAT SELECTED. EMERGENCY LIGHTS FLASHING. INSPECTED AND FOUND EXPOSED WIRES AT LARGEST LOWER FWD CONNECTOR PLUG ON THE RT ACFT CONTACTOR BOX. REPAIRED WIRE COVERING AND GROUND RAN ACFT TO POWER WITH CREW, WITH BUSS LOADED. AND OPS CHECKED ALL ITEMS ON THAT BUSS, NO FURTHER DEFECTS FOUND, ACFT RETURNED TO SERVICE.

Part: O-RING — LEAKING (ENGINE OIL) · airframe 54,070 hrs · 60 cycles

IN FLIGHT CRUISE POWER AT 83 PERCENT TORQUE, NR 1 OIL PRESSURE FLUCTUATED IN TO YELLOW AT 50 PSI. NR 1 POWER LEVER MOVED TO FLIGHT IDLE, THEN OIL PRESSURE WENT INTO RED WITH WARNING LIGHT, THEN NR 1 ENGINE SHUTDOWN IAW CHECK LIST. FOUND OIL LEAKING FROM PCU ADAPTER, R & R ADAPTER AND TRANSFER TUBE O-RINGS IAW WORK CARD 61-10-10 AND RIG CHECKED IAW WORK CARD 76-00-01. OPS AND LEAKED GOOD.

Part: LANDING GEAR — MALFUNCTIONED · airframe 53,508 hrs · 59,317 cycles

TAKEOFF WARNING HORN SOUNDED ON TAKEOFF WITH RT GEAR RED UNSAFE LIGHT AND LT GEAR AMBER DOOR LIGHT ILLUMINATING. CHECKED OLD PSEC FOR FAULTS, FOUND CODES 6 AND 17. R & R PSEU IAW 32-61-50, OPS CHECKED GOOD ON THE GROUND. CREW PERFORMED TAKEOFF WARNING TEST, OPS NORMAL.

Part: SEQUENCE VALVE — MALFUNCTIONED (LT MLG DOOR) · airframe 59,267 hrs

LT GEAR DOOR ADVISORY LIGHT CAME TWICE AND VISUALLY NOTED FWD GEAR DOOR OPEN. R & R RELAY 3261 K-5 OPS CHECKED ON LANDING GEAR DOORS OK. REF-8 MM 32-30-00. LT GEAR DOOR ADVISORY LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION AND FWD DOOR REMAINED OPEN. R & R LT GEAR DOOR SEQUENCE VALVE IAW -8 MM 32-10-51, CYCLED GEAR 10 TIMES AND OPS CHECKED GOOD. LT MAIN GEAR ADVISORY LIGHT ILLUMINATED AFTER GEAR RETRACTION, FWD DOOR REMAINED OPEN. CYCLED GEAR AND FWD DOOR CLOSED, BUT AMBER LIGHT REMAINED ILLUMINATED, ( ON APPROACH, LANDING AND TAXI ALL INDICATIONS WHERE NORMAL. R & R PSEU IAW -8 MM 32-61-50. OPS CHECKED GOOD.

Part: CONTROL BOX — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 59,070 hrs · 66,604 cycles

EMERGENCY LIGHTS FLICKER ON AND OFF IN FLIGHT UNCOMMANDED. PERFORMED OPERATIONAL CHECK, COULD NOT DUPLICATE. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL BOX AS MAINTENANCE PRECAUTION. CHECKED GOOD IN ACCORDANCE WITH MM 33-51-00. OK FOR SERVICE.

Part: CONTROL BOX — INTERMITTENT (EMERGENCY LIGHTS) · airframe 53,124 hrs · 58,918 cycles

EMERGENCY LIGHTS FLICKERED ON AND OFF IN FLIGHT UNCOMMANDED. PERFORMED OPERATIONAL CHECK, COULD NOT DUPLICATE. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL BOX AS MAINTENANCE PRECAUTION. OPERATIONAL CHECKED GOOD IN ACCORDANCE WITH MM 33-51-00. OK FOR SERVICE AT THIS TIME.

Part: INTAKE — OBSTRUCTED (NR 1 ENGINE) · airframe 53,112 hrs · 58,905 cycles

NR 1 ENGINE WOULD NOT PRODUCE MORE THAN 38 PERCENT DURING TAKEOFF ROLL. REJECTED TAKEOFF. FOUND INTAKE PLUG LODGED INTO NR 1 ENGINE INTAKE, FWD OF IMPELLER. REMOVED PLUG, INSPECTED LP AND HP IMPELLERS. NO EVIDENCE OF DAMAGE OR SOFT MATERIAL INGESTION. REF MM 05-50-00 AND 72-00-00. PERFORMED POWER ASSURANCE RUN IAW WC 72-00-10.NP 6, NL3 NH2.5,T6 23 TQ 90,WF 27.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 53,112 hrs · 58,905 cycles

BURNING ODOR WITH SMOKE FROM COCKPIT DASH WITH APU RUNNING. REMOVED LT GLARESHIELD PANEL, INSPECTED GLARESHIELD WIRING BEHIND PANEL. NO DEFECTS NOTED. INSPECTED CAPTAINS FLIGHT INSTRUMENT PANEL. NO DEFECTS. ALL INSTRUMENTS AND COMPONENTS WORK NORMALLY. STARTED APU 3 TIMES WITH BLEED. NO DEFECTS NOTED.

Part: GCU — MALFUNCTIONED (NR 2) · airframe 53,093 hrs · 58,881 cycles

RT AC BUSS FAULT ASSOCIATED WITH RT TRU, RT ELEVATOR HORN HEAT AND RT STALL CAUTION LIGHT. R & R NR 2 AC GCU AND OPS CHECKED GOOD WITH DOUBLE ENGINE RUN.

Part: LIGHT — DAMAGED (CABIN) · airframe 52,027 hrs · 57,676 cycles

UPON INSPECTION IN SBY IT WAS FOUND THAT AN EMERGENCY FLOOR PATH BASE WAS DAMAGED BETWEEN ROW 1 AND 5. REMOVED AND REPLACED FLOOR PATH BASE AND SECURED WITH RETAINING HARDWARE. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 51,943 hrs · 57,572 cycles

ON JULY 27, CREW REPORTED RUDDER TRIM WOULD NOT WORK IN SLOW MODE. PHL MAINTENANCE COULD NOT DUPLICATE PROBLEM, RUDDER TRIM OPS CHECK GOOD. ON JULY 28, CREW REPORTED RUDDER TRIM WOULD NOT WORK IN SLOW MODE. PHL MAINTENANCE REMOVED AND REPLACED TRIM PANEL IAW AMM 27-22-11, RUDDER TRIM OPS CHECKED GOOD. CREW REPORTED RUDDER TRIM WOULD NOT WORK IN SLOW MODE. SBY MAINTENANCE REMOVED AND REPLACED RUDDER TRIM ACTUATOR PER PIEDMONT BULLETIN 27-20-37. COMMENT: SUBMITTER BELIEVES PREVIOUS REFERENCE ENTERED IN PIEDMONT SYSTEM IN ERROR AND CORRECT REFERENCES ARE AMM 27-20-37 AND PIEDMONT BULLETIN 27-9.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,106 hrs · 48,641 cycles

EMERGENCY PATH FLOOR LIGHT INOPERATIVE AT SEAT 3 DF. REMOVED AND REPLACED LIGHT BULB. OPS GOOD.

Part: BATTERY — DISCHARGED (CABIN)

CREW REPORTED EMERGENCY LIGHT ABOVE PASSENGER AIRSTAIR DOOR INOPERATIVE. MAINTENANCE FOUND AN EXTERIOR EMERGENCY LIGHT INOPERATIVE AS WELL. MAINTENANCE TROUBLESHOT THE SYSTEM, FOUND BOTH A BATTERY AND IT'S ASSOCIATED POWER SUPPLY INOPERATIVE. REMOVED AND REPLACED BOTH BATTERY AT LOCATION 3351-PS1 AND POWER SUPPLY AT LOCATION 3351-PS1. OPERATION CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,869 hrs · 56,400 cycles

THIRD RED FLOOR EMERGENCY LIGHT INOP. RELAMPED THIRD RED FLOOR EMERGENCY LIGHT IAW AMM 33-54-00. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,403 hrs · 55,875 cycles

LEFT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT ROW 3AC LOCATION IN ACCORDANCE WITH 33-51-00.

Part: DOOR — OUT OF ADJUST (AIRSTAIR)

AIRSTAIR DOOR INSIDE HANDLE IS HARD TO OPEN. DFRL 05JUN08 14:27 AVP MT LUBED DOOR STOPS NO FIX. FERRY ACFT TO MDT FOUND DOOR TO BE HANGING UP AT THE SILL AREA. ADJUSTED DOOR IAW 8M/M 52-10-00. OPS CHECK OK. (S)

Part: AUTOPILOT SYS — MALFUNCTIONED

WHEN AUTO PILOT SELECTED OFF F/O REPORTED POSSIBLE PITCH JAM, F/O REQUESTED HELP. CAPTAIN TOOK CONTROL, FELT NO JAM, NOTED ACFT FLEW NORMALLY. RIGGED ELEVATOR CONTROL CABLES IAW DASH 8 MM 27-32-00. MEL 30MAY08 16:52 ABE B15119 22-1 AUTOPILOT DFRL 30MAY08 16:54 ABE. MX INSPECTED ELEVATOR CONTROL CABLES AND AUTOPILOT SERVO IN APU HOLE, NO DEFECTS NOTED. CYCLED ELEVATOR FULL TRAVEL SEVERAL TIMES, NO DEFECTS NOTED. RAN GMT ON ELEVATOR SERVO AND ENGAGED AND DISENGAGED A/P SEVERAL TIMES WITH NO FAULTS. REF 8 M/M 2 2-10-01. TRANSCRIBED TO HA 300 30MAY 08 SEQ 2 FOR FURTHER ACTION 940 22-00 2659021 30MAY08 ABE CLOSE POSSIBLE PITCH JAM. MAINTENANCE ACTION COMPLETE SUBJECT TO SATISFACTORY EVAL FLIGHT. 67360 00 RWM FACT 30MAY08 17:31 ABE EVAL FLIGHT SAT. (S)

Part: RELAY — DEFECTIVE (LANDING GEAR) · airframe 49,049 hrs · 54,346 cycles

ON FOLLOW UP INOP FOR LOG BOOK WRITE UP 267083 ITEM 1 LEFT MAIN FWD GEAR DOOR AMBER LIGHT CAME ON AFTER GEAR SELECTED UP. CHECKED FUNCTION OF LEFT FWD MAIN GEAR DOOR ACTUATOR, CHECKED FOR LEAKES, CYCLED GEAR MULTIPLE TIMES, C/N/D. CHANGED 6121-K5 AS PRECAUTIONARY MEASURE. CYCLED GEAR MULTIPLE TIMES. GEAR OPS CHECK GOOD REF 32-30.

Part: LINE — CHAFED (HYDRAULIC SYS) · airframe 48,883 hrs · 54,167 cycles

DURING TAXI, NR 1 HYDRAULIC CONTENTS LEAKED, MAKING BRAKES UNUSABLE. INSP AIRCRAFT, FOUND HYDRAULIC FLUID LEAKING FROM NR 1 RUDDER FULL PRESSURE LINE. INSTALLED TFL, SERVICED HYDRAULICS, GROUND RAN AIRCRAFT, OPS CHECK AND LEAK CHECK GOOD. ASSIGNED 70 HOUR DMT.

Part: STARTER GEN — DEFECTIVE (NR 2) · airframe 48,778 hrs · 54,050 cycles

IN FLIGHT ON CLIMBOUT NR 2 DC BUSS FAULTED, RESET BUSS AND RETURNED TO FIELD. REMOVED AND REPLACED NR 2 STARTER GEN PER WC 24-30-02.

Part: AHRS — FAILED (COCKPIT) · airframe 48,751 hrs · 54,022 cycles

DURING FLIGHT, THE CAPTAINS AHRS FAILED CAUSING THE ADI AND HSI TO TUMBLE. BOTH F/DS BECAME INOPERATIVE. SAHS WAS SELECTED AND A SLIGHT MISMATCH WAS NOTED. AN AIR TURNBACK WAS PERFORMED BUT NO EMERGENCY WAS DECLARED. UPON RETURN TO FIELD, MAINTENANCE REPLACED THE NR 1 AHRS COMPUTER. OPS CHECKS WERE GOOD AT THAT TIME AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: AHRS — MALFUNCTIONED (NR 2) · airframe 48,710 hrs · 53,971 cycles

DURING FLIGHT, IT WAS NOTED THAT THE NR 2 AHRS WAS 10 DEGREES OFF FROM WHAT THE STANDBY HEADING SYSTEM AND THE WET COMPASS WERE READING. AIRCRAFT WAS RETURNED TO DEPARTURE POINT. MAINTENANCE COULD NOT DUPLICATE PROBLEM ON GROUND. NR 2 AHRS COMPUTER WAS RE-RACKED AND OPS CHECKS WERE GOOD. AIRCRAFT WAS THEN RETURNED TO SERVICE WITH NO FURTHER DIFFICULTIES NOTED.

Part: PROXIMITY SENSOR — MALFUNCTIONED (RT MLG) · airframe 47,757 hrs · 52,916 cycles

WEIGHT ON WHEELS CAUTION LIGHT ILLUMINATED ON GEAR RETRACTION & EXTINGUISHED ON GEAR EXTENSION. COMPLIED WITH PSEU TEST AND FOUND LEFT HAND OUTBOARD SENSOR FAULT AND NOSE LANDING GEAR RIGHT HAND TARGET FAULT. REMOVED AND REPLACED OUTBOARD PROX SENSOR & ADJUSTED LEFT AND RIGHT HAND NOSE LANDING GEAR WOW SENSORS IAW 32-61-00.

Part: CLAMP — CORRODED (WINDSHIELD) · airframe 47,578 hrs · 52,713 cycles

CORROSION FOUND ON LOWER CLAMP PLATE OF RIGHT WINDSHIELD. LOWER CLAMP PLATE OF RIGHT WINDSHIELD REPLACED IAW 56-10-11.

Part: DOUBLER — CORRODED (WING) · corrosion level 2 · airframe 47,578 hrs · 52,713 cycles

CORROSION FOUND ON LT FUEL PUMP CUTOUT DOUBLER IN THE FUEL TANK. HFECC NO DEFECTS NOTED. CORROSION REMOVED IAW RD8-57-3701 AND RD8-57-1907.

Part: SEAT TRACK — CORRODED (BS 222-242) · corrosion level 2 · airframe 47,578 hrs · 52,713 cycles

RIGHT SEAT TRACK AT STA 222.7000 AND 242.200 SURFACE CORROSION. RIGHT SEAT TRACK REPLACED BY NEW PART AND INSTALLED WITH SOLID RIVETS AS PER SRM 51-40-00 AND DEFLECTOR REPLACED BY NEW PART AND INSTALLED WITH SOLID RIVETS IAW SRM 51-40-00.

Part: BUSHING — CORRODED (FLAP TRACK) · corrosion level 2 · airframe 47,578 hrs · 52,713 cycles

RIGHT FLAP TRACK NR 4 FOUND ALL FOUR BUSHING AT FLAP TRACK ATTACHMENT CORRODED. RIGHT FLAP TRACK CARRIAGE NR 4, FOUR BUSHING INSTALLED AS PER 20-19-02.

Part: SKIN — CORRODED (WING) · airframe 47,578 hrs · 52,713 cycles

CORROSION FOUND ON PANEL 623AT, 622AT, 521AT, 522AT, CORROSION LOCATED ON COUNTER SINKS. RD8-57-1420 COMPLETED ON PANEL 623AT, 523AT, 521AT. PANEL 522AT AND 622AT REPLACE INSTALLATION OF ALL PANELS W/C 05-00-21I MORE TO FOLLOW.

Part: ANGLE — CORRODED (LAV SERV DOOR) · corrosion level 2 · airframe 47,578 hrs · 52,713 cycles

TOILET SERVICE PANEL DOOR ANGLE FOUND HEAVY CORRODED. REPLACED SERVICE DOOR AS PER SRM 51-40-00.

Part: THRESHOLD — CORRODED (CABIN) · corrosion level 2 · airframe 47,578 hrs · 52,713 cycles

PASSENGER DOOR THRESHOLD WAS FOUND CORRODED. PASSENGER DOOR THRESHOLD WAS REPLACED WITH NEW PART IAW 51-40-00.

Part: RIB — CRACKED (RT AILERON) · corrosion level 2 · airframe 47,578 hrs · 47,578 cycles

RIB CRACKED INSIDE RIGHT AILERON APPROX YW 444. RIGHT AILERON RIB AT STA YW 4444 (APPROX) REPLACED AND INSTALLED WITH BLIND RIVETS AS PER THE SRM 51-40-00. REPAIRED SKIN PER SRM 57-60-21.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,244 hrs · 51,271 cycles

ELECTRICAL ODOR IN CABIN. ITEM PREVIOUSLY DEFERRED RESET C/B'S, SIDEWALL LTS OPS NORMAL, MEL CLEARED. NO ELECTRICAL ODOR NOTED, PERFORMED VISUAL INSP OF SIDEWALL LTS, NO DISCREPANCIES NOTED.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 45,130 hrs · 50,094 cycles

ON CLIMBOUT LOSS OF NR 2 HYDRAULIC PRESSURE HYDRAULIC QUANTITY DROPPED TO .5 QTS ASSOCIATED WITH NR 2 ISO VALVE CAUTION LIGHT AND RUDD PRESS HYDRAULIC AND RUD FULL PRESS LIGHT. REPLACED PRESSURE MANIFOLD UNION AND LINE.

Part: INDICATOR — BURNED (COCKPIT) · airframe 44,799 hrs · 49,744 cycles

CAPTAIN REPORTED WX RADAR UNIT BURNED UP IN FLIGHT, SMOKE IN COCKPIT. PERFORMED HIDDEN DAMAGE REPORT, NO FURTHER DEFECTS NOTED. REPLACED WEATHER RADAR INDICATOR.

Part: WIRE — SHORTED (OIL PRESS IND) · airframe 43,934 hrs · 48,815 cycles

NR 1 ENGINE OIL PRESSURE INDICATION WENT TO ZERO WITH NO LOW OIL PRESSURE LIGHT. ALL OTHER INDICATIONS NORMAL. FOUND WIRE -J- SHORTED TO -F- FROM INDICATOR TO WING ROOT. INSTALLED TEMPORARY WIRE.

Part: LINE — LEAKING (HYD SYS) · airframe 42,387 hrs · 47,185 cycles

ON APPROACH, CREW NOTICED NR 2 HYDRAULIC QTY AT 0 PSI. AFTER NORMAL SELECTION OF GEAR DOWN NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED. ENGINE HYDRAULIC PUMP RAN FOR 10 MINS AT 0 QTY FOUND DOWN LINE FOR NOSE LANDING GEAR DOORS LEAKING. INSTALLED TEMP FLEX LINE. PEFORMED LEAK CHECKS.

Part: BRACKET — CRACKED (SPOILER) · airframe 42,296 hrs · 47,078 cycles

DURING C-CHECK INSPECTION THE OUTBOARD ROLL SPOILER MOUNTING BRACKET WAS FOUND TO BE CRACKED ON BOTTOM INBOARD SIDE. REMOVED AND REPLACED SPOILER BRACKET.

Part: SELECTOR PANEL — FAILED (MLG) · airframe 40,674 hrs · 45,303 cycles

NOSE WHEEL GEAR INDICATION WAS BLANK AFTER GEAR SELECTION WAS MADE. SMOKE CAME FROM NOSE WHEEL GREEN CAUTION LIGHT AREA. REMOVED AND REPLACED LANDING GEAR SELECTOR PANEL, OPS GOOD IAW 32-30-05 AND INPECTED FOR SECONDARY DAMAGE C/W NO DEFECTS NOTED.

Part: AHRS — FAILED (COCKPIT) · airframe 40,515 hrs · 45,128 cycles

WX RADAR FAILED IN FLIGHT DURING TURBULENCE. CND WX RADAR. PROBLEM OCCURRED AFTER LOSS OF THE NR 1 AHRS. REMOVED AND REPLACED NR 1 AHRU. WX RADAR AND AHRS OPS CHECK GOOD.

Part: RADAR — INOPERATIVE (WX SYSTEM) · airframe 10,036 hrs · 44,598 cycles

WX RADAR INOP, AIR TURNBACK FROM 20 MILES OUT, DISPATCH DETERMINED MUST HAVE FOR CVG FLT. REMOVED AND REPLACED RT, OPS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,580 hrs · 43,065 cycles

EMERGENCY FLOOR LIGHT OUT ON ROW 1.

Part: FRAME — CORRODED · corrosion level 2 · airframe 35,617 hrs · 39,912 cycles

During 40k insp. corrosion was found on frame leg at station X312 between stringers 31s and 32s. A new section of frame was spliced in as per EO8-53-02-0943.

Part: FRAME — CORRODED · corrosion level 2 · airframe 35,617 hrs · 39,912 cycles

During 40k insp. corrosion was found on frame leg at station X242 between stringers 31s and 30s. A new section of frame leg was spliced in as per EO8-53-02-0943

Part: FRAME — CORRODED · corrosion level 2 · airframe 34,617 hrs · 39,912 cycles

During 40k insp. corrosion was found on frame leg at station X312 between stringer 31s and 30s. A new frame section was spliced in as per. EO8-53-02-0943.

Part: FRAME — CORRODED · corrosion level 2 · airframe 35,617 hrs · 39,912 cycles

During 40k insp. frame leg was found with corrosion at station X370 between stringers 31s and 32s. A new frame section was spliced in as per EO8-53-02-943.

Part: FASTENER — MISSING (RT SPOILER) · airframe 32,138 hrs · 36,123 cycles

OUTBOARD ROLL SPOILER DOES NOT COME UP WHEN TURNING CONTROL WHEEL TO THE RIGHT. (NO INDICATION ON PFCS) MAINTENANCE FOUND HARDWARE MISSING WT THE CENTER HINGE POINT OF RIGHT HAND OUTBOARD SPOILER. REPLACED HARDWARE AND REPAIRED DAMAGE TO BRACKET.

Part: MOUNT — BROKEN (NR 1 ENGINE) · airframe 31,234 hrs · 35,146 cycles

DURING NUMBER 1 ENGINE CHANGE, THE AFT OUTBORD VERTICLE MOUNT STRUT WAS FOUND BROKEN.

Part: SEAT — OUT OF POSITION (ROW 9)

UNABLE TO REMOVE RIGHT HAND AFT FIRE BOTTLE FROM BULKHEAD. REPOSITIONED ROW 9 SEAT.

Part: ANGLE — CRACKED (NLG WW)

FOUND DURING PAHSE CHECK, THE UPPER RIGHT SIDEWALL OF THE NOSE LANDING GEAR WHEEL WELL HAS A CRACKED STIFFENER ANGLE. THE CORRECTIVE ACTION WAS TO REPAIR IAW ESR8-53-93-11. (M)

Part: ENGINE — FAILED (NR 2)

FLT 3156 - CHO-CLT - IN FLIGHT, AT 12,000 FEET, THE NR 2 ENGINE SURGED AT 100 PERCENT TORQUE THEN SHUTDOWN. NO INDICATIONS PRIOR TO SHUTDOWN, ALL OTHER PARAMETERS NORMAL. THE AIRCRAFT DIVERTED TO GSO AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 2 ENGINE. (M)

Part: HEAT CONTROLLER — FAILED (LT WINDSHIELD)

CLT-HHH - FLT 3377 - DURING TAKEOFF ROLL, LT WINDSHIELD HOT CAUTION LIGHT ILLUMINATED. ACFT ABORTED TAKEOFF WITHOUT INCIDENT. REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER.