N934HA

Part: LANDING GEAR — MALFUNCTIONED (LEFT) · airframe 61,671 hrs · 68,907 cycles

LT MAIN GEAR FAILED TO EXTEND WHEN SELECTED, ACFT PERFORMED EMERGENCY GEAR UP LANDING.

Part: SEAL — LEAKING (STARTER GEN) · airframe 61,513 hrs · 68,724 cycles

WITH APU RUNNING, WITHOUT GROUND POWER UNIT, ELECTRICAL BURNING ODOR AND SMOKE COMING FROM CARGO BAY / APU AREA. INSPECTED AND FOUND APU STARTEF GENERATOR TO BE THE CAUSE OF SMOKE AND FUMES. NO DAMAGE NOTED. REMOVED APU STARTER GENERATOR AND FOUND OIL SOAKED. SUSPECT OIL LEAKING PAST REDUCTION DRIVE ASSY END SEAL OUTPUT SIDE.

Part: CONNECTOR — CORRODED (WX RADAR) · airframe 61,484 hrs · 68,689 cycles

RADAR DOES NOT PAINT WEATHER OR GROUND. RADAR DISPLAY SPOKES, FOUND CORROSION IN CONNECTOR 3441-P1001. R & R CONNECTOR IAW MM 20-45-06

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 61,465 hrs · 68,665 cycles

ROW 7 EMERGENCY LIGHT INOPERATIVE. R & R BULB.

Part: INDICATOR — INOPERATIVE (TORQUE) · airframe 61,191 hrs · 68,333 cycles

NR 1 TORQUE GAUGE ANOLOG AND DIGITAL DID NOT GO ABOVE 10 PERCENT. CLEANED CONNECTOR ON TSCU. R & R NR 1 TORQUE INDICATOR. OPS CHECKED GOOD ON THE GROUND RUN, IAW MM 77-10-00.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 61,169 hrs · 68,301 cycles

SIDEWALL EMERGENCY LIGHTS ARE DIM AT ROWS 1DF AND 4AC. R & R BURNED BULB IN SIDEWALL EMERGENCY LIGHTS. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 61,169 hrs · 68,301 cycles

RT AFT FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. R & R BULB IN RT AFT FUSELAGE EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 61,156 hrs · 68,283 cycles

LOWER LEVEL EMERGENCY EXIT LIGHT IS INOPERATIVE AT ROW 2 AND ROW 4. R & R EMERGENCY LIGHT BULB IAW 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,123 hrs · 68,245 cycles

LAST CEILING EMERGENCY LIGHT IS INOPERATIVE. R & R EMERGENCY CEILING LIGHT, OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 61,123 hrs · 68,245 cycles

17TH AND 21ST FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. R & R BULBS IN FLOOR EMERGENCY LIGHTS. OPS CHECKED GOOD.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 60,985 hrs · 68,075 cycles

EMERGENCY FLOOR LIGHT MODULE IS OFF POSITION AT ROW 9. POSITIONED EMERGENCY FLOOR LIGHT MODULE AT ROW 9.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 60,599 hrs · 67,594 cycles

ROW TWO CEILING EMERGENCY LIGHT IS INOPERATIVE. R & R BULB.

Part: TORQUE SENSOR — FAILED (NR 2) · airframe 60,280 hrs · 67,188 cycles

DURING TAKEOFF, NR 2 TORQUE INDICATOR BOTH DIGITAL AND ANOLOG, DID NOT SHOW AN INCREASE. R & R NR 2 TORQUE INDICATOR IAW AMM 77-10-00. INSPECTED ASSOCIATED CONNECTOR PLUGS, NO DEFECTS NOTED. GROUND RAN ACFT. OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 59,707 hrs · 66,478 cycles

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

Part: ENGINE — SURGES (NR 1) · airframe 59,417 hrs · 66,141 cycles

NR 1 ENGINE TORQUE SURGED ON TAKEOFF ROLL UP TO 99 PERCENT. R & R NR 1 ENGINE HMU AND FUEL PUMP IAW 73-20-01. GROUND RAN ACFT IAW SRT MANUAL. OPS CHECKED GOOD.

Part: INDICATOR — FLUCTUATES (TORQUE) · airframe 59,289 hrs · 65,994 cycles

ABORTED TAKEOFF DUE TO NR 1 ENGINE TORQUE FLUX 20-40-PERCENT. OTHER PARAMETERS NORMAL. R & R NR 1 TORQUE INDICATOR IAW MM 77-10-00. GROUND RAN ACFT. OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 59,154 hrs · 65,836 cycles

RT FWD EMERGENCY EXIT SIGN HAS BULB INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: CHECK VALVE — FAILED (DE ICE SYSTEM) · airframe 59,011 hrs · 65,686 cycles

WITH BOTH ENGINES SHUTDOWN AND APU BLEEDS OFF. DEICE PRESSURE SHOWS 24 PSI AND BOOTS STILL INFLATED. R & R APU LINK UP PRESSURIZATION CHECK VALVE. RAN APU DEICE PRESSURE WAS NORMAL, BOOTS PARTIALLY INFLATED WITH OUT LIGHTS ILLUMINATING. NORMAL 8 OPERATION.

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 58,188 hrs · 64,725 cycles

NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. LIGHT EXTINGUISHED AFTER ABORTED TAKEOFF. CLEANED OIL PRESSURE SWITCH AND TRANSDUCER. FOUND ENGINE 4 QUARTS LOW ON OIL. SERVICED ENGINE. GROUND RAN ACFT AT FULL POWER. OPS CHECK GOOD. OK FOR SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 57,901 hrs · 64,394 cycles

LT AFT EMERGENCY LIGHT DIM. R & R BULB.

Part: SELECTOR PANEL — FAILED (CABIN PRESSURE) · airframe 57,894 hrs · 64,384 cycles

PRESSURIZATION FAULT LIGHT ON. WILL NOT GO OUT. R & R CABIN PRESSURE SELECTOR PANEL. OPS CHECKED GOOD IAW MM 21-30-07. CLEARED MEL. REVERSED SP21-1 OUTFLOW RETURNED TO ORIGINAL CONFIGURATION.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 57,477 hrs · 63,932 cycles

ACFT DID NOT PRESSURIZE DURING CLIMBOUT AND NR 1 TRANSPONDER, F/O ALT, F/O IVSI FAILED. MX R & R NR 2 BLEED OVERTEMP SWITCH AND CABIN PRESSURE CONTROLLER AND NR 2 FGC, ALL SYS OPS CHECKED GOOD DURING GROUND RUN UPS AND LEAK CHECKED GOOD WITH TEST SET PROCEDURES.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 57,400 hrs · 63,840 cycles

EMERGENCY FLOOR PATH LIGHTS AT ROWS 5 AND 6. THE ARROWS ARE FACING THE WRONG DIRECTION. REPOSITIONED EMERGENCY FLOOR PATH LIGHTSAT ROWS 5 AND 6 TO FACE PROPER DIRECTION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,400 hrs · 63,840 cycles

AFT EMERGENCY FLOOR PATH LIGHT IS TOO FAR BACK AND VERY DIM. R & R BULB. REPOSITIONED PATH LIGHT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,362 hrs · 62,700 cycles

2ND RED FLOOR LIGHT IS INOP. RELAMP, OPS CHECKED GOOD IAW MM 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,305 hrs · 62,640 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 5 IS OUT. REMOVED LENS, R & R BULB, OPS CHECKED GOOD, INSTALLED LENS WITH ATTACHED HARDWARE.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 56,305 hrs · 62,640 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 5 IS OUT. REMOVED LENS, R & R BULB, OPS CHECKED GOOD. INSTALLED LENS WITH ATTACHED HARDWARE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,258 hrs · 62,580 cycles

PAX DOOR OVERHEAD EMERGENCY SIGN AND LT FUSELAGE FWD EMERGENCY LIGHT INOP. R & R EMERGENCY LIGHT BATTERY ON PSI IAW WORDCARD 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,009 hrs · 60,035 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 5 IS INOPERATIVE. R & R LIGHT LENS, R & R LIGHT BULB, OPS CHECKED GOOD. INSTALLED LIGHT LENS WITH ATTACHED HARDWARE.

Part: ACTUATOR — LEAKING (SPOILERS) · airframe 53,681 hrs · 59,662 cycles

DURING TAXI, NR 1 HYD RUDDER ISO CAUTION LIGHT AND ROLL SPOILER INBD CAUTION LIGHT ILLUMINATED. NR1 HYD QUANTITY DROPPED TO .6 QUARTS. REMOVED AND REPLACED INBD SPOILER ACTUATOR, REF 8 27-14-05. RECONNECTED HYD LINES AND OPS CHECKED GOOD.

Part: GARLOCK SEAL — LEAKING (NR 1 ENGINE) · airframe 53,129 hrs · 59,064 cycles

IN CRUISE FLIGHT NR 1 ENGINE OIL PRESSURE INDICATOR FLUXED FOLLOWED BY NR 1 ENGINE WARNING LIGHT ILLUMINATED. FOLLOWED CHECK LIST AND SHUT NR 1 ENGINE. REMOVED AND REPLACE GARLOCK SEAL I/A/W 72-20-00. FOUND TEMP BULB LOOSE. REMOVED TEMP BULB REPLACE O-RING REINSTALLED TEMP BULB. NO LEAK NOTED

Part: DISPLAY — BURNED (ZONE 100) · airframe 52,752 hrs · 58,650 cycles

ELECTRICAL BURNED ODOR IN FLIGHT, FOUND NR 2 TRANSPONDER DISPLAY SCREEN BLANK AND THE COMPONENT WAS HOT. PULLED ATC2 CIRCUIT BREAKER AND ODOR WENT AWAY AND COMPONENT COOLED DOWN.

Part: O-RING — LEAKING (FUEL HEATER) · airframe 52,448 hrs · 58,322 cycles

NUMBER 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. REMOVED AND REPLACED O-RING AT FUEL HEATER REDUCTION GEAR BOX OUT PRESS LINE. LEAK AND OPS GOOD.

Part: FUEL HEATER — BROKEN (FUEL SYSTEM) · airframe 52,436 hrs · 58,311 cycles

IN FLIGHT THE NR 2 FUEL TANK TEMPERATURE WAS ABOVE RED LINE ON THE GAUGE. THE TEMPERATURE DROPPED WHEN PULLING POWER BACK OR SELECTING AUXILIARY PUMP. THERE WAS A REPORT OF SMELLING BURNT POPCORN IN THE CABIN AREA. WHEN 934HA WAS IN ROA THE FUEL/OIL WAS REMOVED AND REPLACED FIXING THE HIGH TEMPERATURE PROBLEM. ALSO THE RIGHT HAND BLEED PIPE ASSEMBLY WAS REPLACED WITH NO FURTHER SMELLS OF BURNT POPCORN.

Part: PSEU — FAULTY (NLG) · airframe 50,923 hrs · 56,734 cycles

UPON GEAR RETRACTION NOSE GEAR DOOR AMBER LIGHT ILLUMINATED CYCLED GEAR PER EMERGENCY CHECKLIST AND RED UNSAFE LIGHT ILLUMINATED WITH NO ALTERNATE INDICATION, PERFORMED ALTERNATE EXTENSION ALL INDICATIONS NORMAL. INSPECTED AND FOUND DRAG STAY PROX SWITCH FOR NOSE LANDING GEAR ROUTED INCORRECTLY. RE-ROUTED SWITCH CABLE IN ACCORDANCE WITH MAINTENANCE MANUAL CHAPTER 32-20-00.

Part: PSEU — FALSE INDICATION (NLG) · airframe 52,312 hrs · 58,181 cycles

UPON GEAR RETRACTION NOSE GEAR DOOR AMBER LIGHT ILLUMINATED. CYCLED GEAR PER EMERGENCY CHECKLIST AND RED UNSAFE LIGHT ILLUMINATED WITH NO ALTERNATE INDICATION. PERFORMED ALTERNATE EXTENSION ALL INDICATIONS NORMAL. FOUND PSEU TO HAVE NUMEROUS CODES TARGET 17, 14, 06, 10, 09, 14 SENSOR 14, 10, 09 AND CARD 40. REMOVED AND REPLACED PROXIMITY SYSTEM ELECTRONIC UNIT IN ACCORDANCE WITH MAINTENANCE MANUAL 32-61-50, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,088 hrs · 57,942 cycles

UPON INSPECTION AT SBY, IT WAS NOTICED THAT AN EMERGENCY LIGHT AT ROW 1 WAS INOPERATIONAL. REPLACED THE LIGHT BULB AND THE OPERATIONAL CHECK WAS GOOD.

Part: LIFT STRUT — WORN (PAX DOOR) · airframe 50,020 hrs · 55,581 cycles

PAX DOOR UNLATCHED ITSELF (HANDLE POPPED TO THE FIRST DETENT) FOLLOWED BY PAX DOOR WARNING LIGHT IN FLIGHT COMPARTMENT. F/A LATCHED DOOR AND DOOR REMAINED LATCHED FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED AIRSTAIR DOOR LIFT MECHANISM GAS SPRING AND ADJUSTED DOOR PRESSURE STOPS.

Part: PROXIMITY SENSOR — INTERMITTENT (LT MLG) · airframe 49,645 hrs · 55,172 cycles

GEAR SELECTED DOWN, LEFT MAIN GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED, ALT GEAR IND HAD THREE GREEN. CREW VERIFIED GEAR WAS DOWN.

Part: BRAKE ASSY — DEFECTIVE (MLG) · airframe 49,559 hrs · 55,078 cycles

WHILE TAXING TO RUNWAY 36L, ANOTHER AIRCRAFT CREW SAID THE LEFT BREAKS WERE GLOWING RED. PULLED AIRCRAFT OFF TAXIWAY TO INSPECT. THE FIRST OFFICER NOTED SMOKE COMING FROM WHEEL ASSEMBLY, EVACUATED AIRCRAFT. REMOVED NR 1 AND NR 2 WHEEL AND BRAKE ASSEMBLIES. INSPECED SRUT AND AXLE, NO DEFECTS NOTED. INSTALLED NEW BRAKE, WHEEL ASSEMBLIES AND FLEXIBLE BRAKE LINES. LEAK AND OPERATIONAL CHECK GOOD.

Part: ROD — OUT OF ADJUST (MLG) · airframe 47,633 hrs · 52,988 cycles

FLIGHT ATTENDANT REPORTS FORWARD MAIN LANDING GEAR DOOR SHAKING AND WHEN CLOSED DOOR IS GAPPED. FLIGHT RETURNED TO FIELD, NO EMERGENCY WAS DECLARED BUT RESCUE VEHICLES WERE DISPATCHED TO ESCORT AIRCRAFT TO GATE. ADJUSTED LEFT HAND FORWARD GEAR DOOR ACTUATOR ATTACH ROD.

Part: FUEL FILTER — DIRTY (NR 2 ENGINE) · airframe 47,608 hrs · 52,951 cycles

NR 2 FUEL FILTER BYPASS CAUTION LIGHT ILLUMINATED AFTER TAKEOFF. INSPECTED WIRE HARNESS NO DEFECT NOTED. INSPECTED AND REPLACED THE HP FUEL FILTER. INSPECTED AND CLEANED THE L/P FUEL FILTER. RAN AIRCRAFT AT POWER SETTINGS, NO DEFECT NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,479 hrs · 52,819 cycles

CABIN AISLE ESCAPE PATH LIGHTING IS INOP. RELAMPED LIGHTING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,479 hrs · 52,819 cycles

EMERGENCY LIGHTING AIRSTAIR DOOR EMERGENCY EXIT SIGN CENTER LAMP IS INOP. RELAMPED LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,479 hrs · 52,819 cycles

CABIN AISLE ESCAPE PATH LIGHTING LIGHT NR 21 IS INOP. RELAMPED LIGHT.

Part: PROPELLER — UNKNOWN (NR 2) · airframe 46,553 hrs · 51,790 cycles

DURING CLIMB AND STRAIGHT AND LEVEL FLIGHT THE NR 2 PROP RPM WOULD NOT STABILIZE, FLUXED FROM 940 TO 1050. RAN TEMPORARY WIRE (10008C22) FROM WING ROOT CONNECTOR 6121P7-C TO 9811TB 159-1G.

Part: SWITCH — INTERMITTENT (EMERGENCY LIGHTS) · airframe 45,472 hrs · 50,611 cycles

EMERGENCY LIGHTS INTERMITTANTLY FLASH IN FLIGHT. REPLACED FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH.

Part: PSEU — FAULTY (MLG INDICATOR) · airframe 43,375 hrs · 48,323 cycles

NOSE GEAR LIGHT WILL NOT EXTINGUISH AFTER TAKEOFF. CYCLED GEAR AND LIGHT REMAINED ON. REMOVED AND REPLACED THE PSEU.

Part: TAPE — DEBONDED (LEADING EDGE) · airframe 40,406 hrs · 45,022 cycles

LEFT I/B BOOT LOOSE. PHL WILL SECURE WITH SPEED TAPE WE'LL MEL A/F DEICE AND FLY REVENUE TO SBY. SCURED LOOSE DEICE BOOT WITH SPEED TAPE I/A/W SPECIAL PROCEDURE 20.2 AND PLACED AIRFRAME DEICE ON MEL. R&R LEFT INBOARD DEICE BOOT LEADING EDGE.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,280 hrs · 44,883 cycles

MAJOR REPAIR DENTS AFT OF DITCHING HATCH .012 INCH DEEPEST DENT, WITH SKIN CUPPED .020 INCH.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,280 hrs · 44,883 cycles

CORROSION ON STRINGER.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,280 hrs · 44,883 cycles

CORROSION FRAME LEG X252 AND STRINGER 31S. REMOVED STRINGER.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 40,280 hrs · 77,883 cycles

MAJOR REPAIR FRAME SPLICE AT X 240 AND STRINGER 28S.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,280 hrs · 44,883 cycles

CORROSION, RT SEAT RAIL FLOOR FLANGE FOR RT LOWER FLOOR PANEL IS CORRODED FROM X560 TO X600 WITH PREVIOUS BLENDING.

Part: ACTUATOR — MALFUNCTIONED (MLG DOOR) · airframe 39,719 hrs · 44,273 cycles

AFTER TAKEOFF LEFT GEAR DOOR AMBER LT REMAINED ON, CREW CONFIRMED ALL GEAR DOORS CLOSED.

Part: SPRING — BROKEN (MLG DOOR) · airframe 47,721 hrs · 54,745 cycles

NR 2 MLG AFT INBOARD GEAR DOOR CAME OPEN IN FLIGHT. FOUND DOOR ACTUATOR ROD AND ALT EXTENSION SPRING BROKEN. REPLACED ROD AND SPRING.

Part: SPRING — BROKEN (ACTUATOR ROD) · airframe 47,721 hrs · 54,745 cycles

NR 2 MLG AFT INBOARD GEAR DOOR CAME OPEN IN FLIGHT. FOUND DOOR ACTUATOR ROD AND ALT EXTENSION SPRING BROKEN. REPLACED ROD AND SPRING.

Part: TRACK — CORRODED · airframe 34,184 hrs · 38,319 cycles

L/H WING #3 FLAP TRACK HAS AREA OF CORROSION ON BACK FACE OF TRACK. BLENDED CORROSION IAW EO8-57-01-396.

Part: STRAP — CORRODED · airframe 34,184 hrs · 38,319 cycles

SKIN JOINT STRAP BETWEEN STRINGERS 20S AND 22S AT STATION X370.80 IS CORRODED. REPAIRED STRAP IAW EO8-53-01-399.

Part: TRACK — CORRODED · airframe 34,184 hrs · 38,319 cycles

R/H WING #3 FLAP TRACK HAS CORROSION ON BACK SURFACE. BLECDED CORROSION IAW EO8-57-01-396.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 34,184 hrs · 38,319 cycles

STRINGER 31S CORRODED AT STATION X207. BLENDED CORROSION ON STRINGER.

Part: ANGLE — CRACKED · airframe 34,184 hrs · 38,319 cycles

WING FRONT SPAR TO FUSELAGE L/H CLOSING ANGLE CRACKED. REPLACED CLOSING ANGLE.

Part: ANGLE — CRACKED · airframe 34,184 hrs · 38,319 cycles

L/H NACALLE HORSECOLLAR AFT FLANGE ANGLE CRACKED. REPLACED ANGLE.

Part: ANGLE — CRACKED · airframe 34,184 hrs · 38,319 cycles

R/H NACELLE HORSECOLLAR FRAME AFT FLANGE ANGLE CRACKED. REPLACED ANGLE.

Part: CONTROL CABLE — OUT OF RIG (MLG DOOR) · airframe 33,416 hrs · 37,528 cycles

LEFT MLG FWD DOOR OPENED IN FLIGHT AFTER GEAR RETRACTION SEQUENCE WAS COMPLETE. RERIGGED ALTERNATE EXTENSION CABLES FOR LT FWD DOOR ACTUATOR.

Part: OIL COOLER — LEAKING (NR 2 ENGINE) · airframe 33,088 hrs · 37,200 cycles

NR 2 ENGINE LOST OIL PRESSURE. SHUT DOWN ENGINE IN FLIGHT AND RETURNED TO PHL. REMOVED AND REPLACED NR 2 OIL COOLER.

Part: BRACKET — CRACKED (SPOILER ACTUATOR) · airframe 31,122 hrs · 35,055 cycles

THE LT WING OUTBOARD ROLL SPOILER ACTUATOR MOUNTING BRACKET ON REAR SPAR WAS CRACKED. REPLACED MOUNTING BRACKET.

Part: BATTERY — DISCHARGED (CABIN)

FLO - FLT 3252 - EMERGENCY EXIT SIGN ABOVE PASSENGER DOOR WILL NOT ILLUMINATE. REPLACED EMERGENCY BATTERY BASE PS1 IN WARDROBE CLOSET. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

FLT 3341 - CHO-PIT - DURING PREFLIGHT CHECKS, A STRONG ACID SMELL IN THE COCKPIT, FOLLOWED BY SMOKE COMING FROM LEFT WINDSHIELD HEAT TERMINAL CONNECTOR. REMOVED AND REPLACED CAPTAINS WINDSHIELD AND HEAT CONTROLLER. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

FLT 3341 - CHO-PIT - DURING PREFLIGHT CHECKS, A STRONG ACID SMELL IN THE COCKPIT, FOLLOWED BY SMOKE COMING FROM LEFT WINDSHIELD HEAT TERMINAL CONNECTOR. REMOVED AND REPLACED CAPTAINS WINDSHIELD AND HEAT CONTROLLER. (M)

Part: LUMINAIRE — BURN DAMAGE (CABIN)

PIEDMONT AIRLINES RETURNED LIGHTING UNIT FOR ARCING AND BURN DAMAGE AT LAMP HOLDER.

Part: CONTROL BOX — FAILED (CABIN)

FLT 3204 - CLT-CHA - THE FLIGHT ATTENDANT REPORTED THE EMERGENCY LIGHTS WERE FLICKERING WHILE TAXIING. THE AIRCRAFT RETURNED TO THE GATE. REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL BOX. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FLT 3451 - TPA-JAX - DURING PREFLIGHT CHECKS, FOUND THE CENTER AISLE AFT EMERGENCY FLOOR LIGHT INOP. REMOVED AND REPLACED THE BULB, NO FIX. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY 3351-PS3. (M)

Part: HYDRO MECH UNIT — MALFUNCTIONED (NR 2 ENG)

FLT 7106 - PHF-ROA - AFTER TAKEOFF, THE NR 2 ENGINE HAD A SEVERE REDUCTION IN POWER. THE PILOT FEATHERED THE ENGINE. THE AIRCRAFT RETURNED TO PHF AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND MOISTURE IN THE ELECTRICAL CONTROL UNIT CONNECTORS. REMOVED AND REPLACED THE NR 2 ELECTRICAL CONTROL UNIT. ALSO, REMOVED AND REPLACED THE NR 2 HYDRO MECHANICAL UNIT AS A PRECAUTION. (M)

Part: ELEC CONTROL UNI — FAILED (NR 2 ENG)

FLT 7106 - PHF-ROA - AFTER TAKEOFF, THE NR 2 ENGINE HAD A SEVERE REDUCTION IN POWER. THE PILOT FEATHERED THE ENGINE. THE AIRCRAFT RETURNED TO PHF AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND MOISTURE IN THE ELECTRICAL CONTROL UNIT CONNECTORS. REMOVED AND REPLACED THE NR 2 ELECTRICAL CONTROL UNIT. ALSO, REMOVED AND REPLACED THE NR 2 HYDRO MECHANICAL UNIT AS A PRECAUTION. (M)

Part: UPPER STRUT — FAILED (PAX DOOR)

FLT NR 3473 - RDU-BWI - UPON ARRIVAL IN BWI, THE PASSENGER DOOR WOULD NOT OPEN WITHOUT OUTSIDE ASSISTANCE. FOUND THE LEFT FORWARD UPPER STRUT CRACKED. REMOVED AND REPLACED THE LEFT FORWARD UPPER STRUT. (M)

Part: BRAKE ASSY — FAILED (MLG)

FLT 3074 - MCO-MIA - THE LEFT BRAKES WERE GRABBING EXCESSIVELY DURING TAXI OUT. RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 AND NR 2 BRAKE ASSEMBLIES. ALSO, REMOVED AND REPLACED ALL THREE HYDRAULIC FILTERS AS A PRECAUTION. (W)

Part: BRAKE ASSY — FAILED (MLG)

FLT 3074 - MCO-MIA - THE LEFT BRAKES WERE GRABBING EXCESSIVELY DURING TAXI OUT. RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 AND NR 2 BRAKE ASSEMBLIES. ALSO, REMOVED AND REPLACED ALL THREE HYDRAULIC FILTERS AS A PRECAUTION. (W)

Part: BULB — FAILED (CABIN)

FLT NR 3460 - MCO-MIA - DURING MORNING WALKAROUND, FOUND AFT CABIN CENTER AISLE OVERHEAD EMERGENCY WHITE DOWN LIGHT INOP. REMOVED AND REPLACED BULB. (W)