N906HA

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 69,639 hrs · 78,850 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 2 IS INOPERATIVE. REMOVED LENS PANEL, R & R BULB. OPS CHECKED GOOD.

Part: WIRE — BROKEN (PUMP CONNECTOR) · airframe 69,519 hrs · 78,692 cycles

NR 1 HYDRAULIC STANDBY PUMP INOPERATIVE, ZERO PRESSURE. FOUND WIRE 10009B22 BROKEN AT P4 CONNECTOR PLUG. REPAIRED WIRE USING STD MTC PRACTICE. OPS CHECKED GOOD.

Part: PSEU — FAULTED (MLG) · airframe 68,576 hrs · 77,582 cycles

LEFT MLG AMBER DOOR LIGHT REMAINED ILLUMINATED AFTER MLG RETRACTION, CYCLED GEAR IAW CHECK LIST, ALL INDICATIONS ARE NORMAL. PERFORMED PSEU TEST FOUND CODE 54 CARD FAULT. R & R PSEU,CYCLED GEAR OPS CHECKED GOOD. ALSO CHECKED RIGGING OF DOOR SENSOR, NO DEFECTS NOTED.

Part: PITOT HEAD — FAILED · airframe 68,431 hrs · 77,423 cycles

CAPTAIN LOST AIRSPEED, HEADING DATA AND YAW DAMPER FAILED. REPLACED RUBBER PITOT HOSE BETWEEN CAPTS PITOT TUBE AND FLOOR V THROUGH. R & R CAPT'S PITOT TUBE. OPS CHECKED GOOD IAW MM 34-11-00.

Part: WARNING LIGHT — ILLUMINATED (DC GENERATOR) · airframe 68,197 hrs · 77,158 cycles

SUSPECTED LIGHTNING STRIKE, FOLLOWED BY ILLUMINATION OF NR 2 DC GEN CAUTION LIGHT. CAUTION LIGHT EXTINGUSHED AFTER CYCLING NR 2 DC GENERATOR. COMPLIED WITH LIGHTNING STRIKE INSPECTION IAW MM 05-50-31, PAGE 1 THROUGH 6. NO DEFECTS NOTED AT THIS TIME.

Part: ACTUATOR — OUT OF ADJUST (MLG DOOR) · airframe 67,330 hrs · 76,168 cycles

LT MAIN GEAR DOOR AMBER LIGHT ILLUMINATED AFTER GEAR RETRACTION. RECYCLED GEAR IAW CHECK LIST. AMBER LIGHT RE-ILLUMINATED. ADJUSTED FORWARD LT GEAR DOOR ACTUATOR AND INSTALLED NEW PROX SWITCH FOR GEAR DOOR IAW MM 32-10-36. SWUNG GEAR SEVERAL TIMES. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 66,528 hrs · 75,252 cycles

(1) OVERHEAD EMERGENCY LIGHT AT ROW 6 IS INOP. R & R BULB. OPS CHECKED GOOD.

Part: DRAG STRUT — INOPERATIVE (MLG) · airframe 66,503 hrs · 75,225 cycles

REJECTED TAKEOFF DUE TO NOSE GEAR UNSAFE LIGHT, GEAR SELECT HANDLE LIGHTS AND NOSE STEERING CAUTION LIGHT ILLUMINATED AT 75 KNOTS ON TAKEOFF ROLL. LIGHTS EXTINGUISHED AT TIME OF REJECTION. R & R DRAG STRUT AND DOWN LOCK PROX SWITCHES. IAW -8 MM 32-20-16. OPS CHECKED GOOD AT THIS TIME.

Part: WIRE HARNESS — MISWIRED (EMERGENCY LIGHTS) · airframe 66,379 hrs · 75,089 cycles

PANEL 143BZ (CTR FLOOR) EMERGENCY LIGHTS DO NOT COME ON AND DIM ALL OTHER EMERGENCY LIGHTS WHEN PLUGGED IN. R & R POWER SUPPLY BASE AND BATTERY, NO FIX. FOUND LIGHT HARNESS AT THIS LOCATION WIRED INCORRECTLY. REWIRED HARNESS. FLOOR EMERGENCY ESCAPE LIGHTS OPERATE NORMALLY.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,379 hrs · 75,089 cycles

RIB AT X240.5, STA. 31S HAS CORROSION. REMOVED RIB SECTION AT X240.5 BETWEEN STRINGER 32P AND STRINGER 28S. COMPLIED WITH HFEC IAW EO8-53-11-0289. NO DEFECTS NOTED. SPLICE FRAME AT X240.5 IAW EO8-53-11-0289.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,379 hrs · 75,089 cycles

RIB AT X222, STRINGER 30-31 HAS CORROSION. REMOVED VERTICAL FLOOR SUPPORT FRAME. REMOVED RIB SECTION AT X222 BETWEEN STRINGERS 32P AND 28S. COMPLIED WITH HFEC INSPECTION, NO DEFECTS NOTED. SPLICE FRAME AT X222 IAW EO8-53-11-0289.

Part: FLAP TRACK — CORRODED (RT WING TE FLAP) · airframe 66,379 hrs · 75,089 cycles

RT NR 2 FLAP TRACK HAS PITTING AND CORROSION ON MATING SURFACE AND HEAVY WEAR AND PITTING ON ROLLER SURFACE. R & R FLAP TRACK WITH NEW HARDWARE IAW AMM57-50-26.

Part: FITTING — CORRODED (RT FLAP TRACK) · airframe 66,379 hrs · 75,089 cycles

RT NR1 FLAP TRACK THROUGH BOLT FITTING IS CORRODED. R & R NECESSARY HARDWARE WITH NEW HARDWARE.

Part: FLOOR SUPPORT — CORRODED (LAVATORY) · airframe 66,379 hrs · 75,089 cycles

LAV FLOOR ANGLE BRACKET IS CORRODED. REMOVED LOWER AND UPPER ANGLE. FABRICATED NEW ANGLES FROM 2024-T3 .040 ALUMINUM, ALODINED, PRIMED AND INSTALLED IAW DWG 82540006 WITH NEW HARDWARD AND BONDED.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 66,379 hrs · 75,089 cycles

INTERNAL STRUCTURE HAS SMALL CRACKS EMINATING FROM A RIVET AT LOWER AFT CORNER ON LT MID EMERGENCY EXIT. FURTHER INSP FOUND STRUCTURE AT HOLE BOWED OUT, CAUSING EDGE CRACKS. COLD WORKED METAL BACK INTO SHAPE, UPSIZED HOLE 1 STANDARD SIZE, WHICH CLEANED UP DAMAGE AND INSTALLED NEW RIVET IN HOLE.

Part: SKIN — CORRODED (PAX DOOR) · airframe 66,379 hrs · 75,089 cycles

SEVERAL AREAS OF CORROSION AT UPPER END OF PAX DOOR SKIN. R & R PAX DOOR SKIN.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 66,379 hrs · 75,089 cycles

PAX DOOR THRESHOLD IS CORRODED. R & R THRESHOLD ASSY, INSTALLED THRESHOLD ASSY IAW ENG DRAWING 85321241.

Part: FLAP TRACK — CORRODED (RT WING TE FLAP) · airframe 66,379 hrs · 75,089 cycles

RT NR 1 FLAP TRACK HAS CORROSION ON THE MATING SURFACE AND HEAVY WEAR AND PITTING ON THE ROLLER SURFACE. R & R FLAP TRACK WITH NEW HARDWARE IAW AMM 57-50-11.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,302 hrs · 74,994 cycles

EMERGENCY FLOOR PATH LIGHT IS INOP AT ROW 7. R & R LIGHT MODULE AS REQUIRED. OPS CHECKED GOOD.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 65,999 hrs · 74,655 cycles

FIRST RED EMERGENCY FLOOR LIGHT INOP. .RESEATED EMERGENCY LIGHT IN SOCKET. OPS CHECKED GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (HYD SYSTEM) · airframe 47,364 hrs · 53,419 cycles

ROLL SPOILER OTBD HYD CAUTION LIGHT ILLUMINATED ON CLIMB OUT AT 9000 FT AT 140 KNOTS. R & R PRESSURE SWITCH, GROUND RAN, OPS CHECKED GOOD. INSP, FOUND HYD QTY'S NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,529 hrs · 74,150 cycles

EMERGENCY FLOOR PATH LIGHT IS INOP AT SEAT 5DF. R & R BULB IN EMERGENCY FLOOR PATH LIGHT AT ROW 5. OPS CKD GOOD.

Part: COMPUTER — MALFUNCTIONED (STICK SHAKER) · airframe 65,344 hrs · 73,946 cycles

ON ROTATION, STICK SHAKER ACTIVATED FOR REMAINDER OF FLIGHT. R & R NR 1 COMPUTER AND CALIBRATED IAW MM 27-33-00. RECONNECTED SHAKERS, OPS CHECKED GOOD.

Part: OIL COOLER — LEAKING (NR 1 ENGINE) · airframe 64,229 hrs · 72,651 cycles

IN FLIGHT, NR 1 ENGINE OIL PRESSURE DROPPED TO 40PSI FOR 3 MINUTES. SHUT NR1 ENGINE DOWN IAW CHECK LIST, LANDED NORMALLY WITH 1 ENGINE. INVESTIGATED, FOUND HELICOIL BACKING OUT ON INPUT SIDE OF THE OIL COOLER. FOUND O-RING ON OUTPUT SIDE SLICED. R & R OIL COOLER AND O-RINGS IAW MM 79-20-11, OPS AND LEAKED CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,937 hrs · 72,316 cycles

EMERGENCY LIGHT 8 BULBS IN OP LOCATED AT ROW 1 CEILING. R & R BULB IAW 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,937 hrs · 72,316 cycles

EMERGENCY LIGHT BULB IN OP AT ROW 4AC ON SIDEWALL. R & R BULB IAW 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,937 hrs · 72,316 cycles

EMERGENCY LIGHT, ONE BULB IN OP LOCATED AT ROW 1 FLOOR. R & R BULB IAW 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,937 hrs · 72,316 cycles

EMERGENCY LIGHT 26 BULBS INOP LOCATED AT CEILING ROW 4. R & R BULBS IAW 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,937 hrs · 72,316 cycles

EMERGENCY LIGHT 12 BULBS IN OP ON ROW 1AC ON TOP OF PAX DOOR. R & R BULBS IAW 33-51-00.

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 62,596 hrs · 70,829 cycles

EMERGENCY FLOOR PATH TRANSPARENT COVER IS MISSING. FORWARD MOST COVER. REMOVED AND REPLACED EMERGENCY FLOOR LIGHTING TRIM COVER AS REQUIRED. OPERATIONAL CHECK GOOD.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 62,596 hrs · 70,829 cycles

EMERGENCY FLOOR PATH TRANSPARENT COVER IS MISSING, FWD MOST COVER. REMOVED AND REPLACED FLOOR LIGHT TRIM COVER AS REQUIRED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 62,459 hrs · 70,677 cycles

RIGHT AFT EMERGENCY DITCHING LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT LOCATION/IDENT ROW 7DF (RIGHT SIDE)/ PS6, BATTERY REFERENCE DESIGNATION 3351-PS4. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 59,995 hrs

UNKNOWN ELECTRICAL ODOR ACCOMPANIED BY LIGHT SMOKE. MAINT WAS ON AC FOR APPROX 2.5 HOURS, SUSPECT WATER GOT ON TOP OF ADVISORY DISPLAY PANEL WHICH WAS CURRENTLY MEL`D. (K)

Part: HYDRAULIC LINE — CRACKED (LT WING) · airframe 59,393 hrs · 67,275 cycles

ON TAXI OUT LOST HYDRAULIC QTY ON NR 2 SYSTEM WENT DOWN TO .6 QTS. RETURNED TO GATE. UPON INVESTIGATION FOUND LEFT OUTBOARD SPOILER ACTUATOR LINE LEAKING, MECHANICS INSTALLED A TEMP FLEX LINE. GROUND RAN AIRCRAFT, LEAK CHECK GOOD. SERVICED NR 2 HYDRAULIC SYSTEM AS REQUIRED.

Part: TSCU — MALFUNCTIONED (NR 2) · airframe 59,149 hrs · 67,017 cycles

ON TAKEOFF ROLE NR 2 PROP FEATHERED AT 30% TORQUE. ARM LIGHT WAS NOT ILLUMINATED. ABORTED TAKEOFF. UNABLE TO DUPLICATE PROBLEM. REPLACED NR 2 TSCU.

Part: CONTROL MODULE — FAILED (FIRE HANDLE) · airframe 59,070 hrs · 66,933 cycles

WHEN TESTED, THE NR 1 ENGINE FIRE EXTINGUISHER 'T' HANDLE WOULD NOT ILLUMINATE. MAINTENANCE CLEANED THE ELECTRICAL CONNECTOR BETWEEN THE 'T' HANDLE AND SHAFT, THEN REPLACED THE NR 1 FIRE DETECTION CONTROL MODULE. SYSTEM WAS CHECKED IAW MM PROCEDURES AND OPS CHECKED GOOD. AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: SWITCH — FAILED (AUTOFEATHER SYS) · airframe 59,026 hrs · 66,883 cycles

AS THE POWER LEVERS WERE BEING ADVANCED TO START THE TAKEOFF ROLL, THE AUTOFEATHER SYSTEM DID NOT ACTIVATE AND THE NR 2 ENGINE TORQUE INDICATION WENT TO 105% FOR AT 3 SECONDS. MAINTENANCE PERFORMED THE BETA LOCKOUT GROUND LOGIC OPS CHECK WORKCARD. MICRO SWITCH 6121-S10 AND WIRES 6121-16D22 & 6121-17A22 RUNNING FROM THE -S10 SWITCH TO CONNECTOR 9811-P38 WERE REPLACED. GROUND CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — CONTAMINATED (WING ROOT) · airframe 59,021 hrs · 66,876 cycles

WHEN PILOT ADVANCED POWER FOR TAKEOFF, THE NR 2 PROPELLER WENT INTO FEATHER UNCOMMANDED. THE PROP SPEED WAS APPROXIMATELY 1200 RPM AND REACHED A TORQUE OF 100-105% FOR ABOUT 3 SECONDS. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT WAS RETURNED TO THE MAINTENANCE FACILITY. PLA SWITCHES 6121-S8, S9, S12 AND S13 WERE INSPECTED ALONG WITH NR 1 NAD AND NR 2 TSCU CONNECTORS, AND STRUT HARNESS, WITH NO DEFECTS NOTED. INSPECTION OF THE NR 1 AND NR 2 WING ROOT CONNECTORS, 9811-P13 & P14, FOUND WATER IN THE P14 CONNECTOR, WHICH WAS REMOVED. THE NR 2 STRUT HARNESS AND NR 2 PROP ASSEMBLY WERE THEN CHANGED. ALL OPS CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LEVER — WORN (AILERON TABS) · airframe 58,896 hrs · 66,733 cycles

IN FLIGHT AIRCRAFT IS DIFFICULT TO TURN LEFT AND SPOILER NR 1 PUSH OFF LIGHT ILLUMINATES WHEN MAKING RIGHT TURNS. FOUND WIRES ON RIGHT HAND SPOILER CLUTCH UPPER MICRO SWITCH, REPAIRED WIRES AND RIGGED MICRO SWITCH. INSPECTED LEFT AND RIGHT AILERONS AND SPRING TABS, FOUND SPRING TAB SPRINGS WORN. REPLACED AND RIGGED SPRING LEVER ASSEMBLIES FOR LEFT AND RIGHT AILERON TABS. EVALUATION FLIGHT SATISFACTORY.

Part: WINDSHIELD — DAMAGED (COCKPIT) · airframe 57,967 hrs · 65,744 cycles

THERE WAS A BIRD STRIKE NEAR THE F/O WINDSHIELD ON CLIMBOUT. THE FLIGHT WAS 20 MINUTES OUT OF CLT. THE FLIGHT CREW WAS HEARING A NOISE AND THEN IT WENT AWAY. FLIGHT DIVERTED TO ROA. AFTER LANDING IN ROA THE CAPTAIN REPORTED THERE WAS A LOSS OF PRESSURE. MAINTENANCE REMOVED BIRD DEBRIS RT WING INBOARD AFT SIDE. SEALED AROUND INSIDE AND OUTSIDE OF F/O WINDSCREEN, PRESSURIZED AIRCRAFT TO 5.25 DIFF IAW OUTSIDE SEAL REPAIR ESR 8-56-04-009. INSIDE REPAIR IAW SPECIAL PROCEDURE 56-1. NO DEFECTS NOTED, OK FOR SERVICE.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 57,938 hrs · 65,714 cycles

HYD LEAK IN NR 2 GEAR WELL LEFT SIDE ABOVE JET PIPE. ROA MX CANNOT REACH LEAK, CREW WILL TAKE A/C TO HANGAR, LOOKING TO TAKE A/C 980 AS A SPARE WILL HAVE TO USE LOWER COWL FOR 980. SWAP 980 AND TAKING LOWER COWL OFF OF 906. FOUND RIGHT LIFT DUMP SPOILER HYD LINE LEAKING. INSTALLED TEMP FLEX LINE. LEAK CHECK GOOD.

Part: TRANSDUCER — MALFUNCTIONED (STALL WARNING) · airframe 57,776 hrs · 65,539 cycles

JUST AFTER ROTATION FROM LGA, THE STICK SHAKER WENT OFF. CAPTAIN QUICKLY RETURNED TO THE FIELD. CAPTAIN'S STALL WARNING HAS A PROBLEM. REMOVED AND REPLACED NR 1 STALL WARNING TRANSDUCER. OPS CHECK GOOD.

Part: CONTROL HEAD — CONTAMINATED (NR 2 TRANSPONDER) · airframe 57,250 hrs · 64,978 cycles

NR 2 TRANSPONDER SMOKED THEN MADE POPPING NOISE THEN FAIL TO OPERATE, SUSPECT WATER IN NR 2 TRANSPONDER. REMOVED NR 2 TRANSPONDER CONTROLLER C/P. REMOVED AND REPLACED NR 2 TRANSPONDER R/T, CONTROL HEAD, OPS CHECK GOOD IAW 34-52-00. CORR CHECK GOOD IAW W/C 34-53-01F. EXCESSIVE WATER FOUND IN COCKPIT COMING FROM DITCHING HATCH AND F/O'S SIDE PANEL. INSPECTED DITCH HATCH AND SEALED F/O'S SIDE WINDOW IAW SP&P 56.1.1, PRESSURIZED A/C, NO LEAKS NOTED AT THIS TIME.

Part: VHF COMM — CONTAMINATED (COCKPIT) · airframe 57,250 hrs · 64,978 cycles

16APR07 - EXPERIENCE SMOKE IN COCKPIT, SMOKE COMING FROM NR 2 COMM DURING RUN UP, SUSPECT WATER IN NR 2 COMM. 17APR07 - REMOVED AND REPLACED NR 2 COM R/T, CONTROL HEAD, ACP OPS CHECK GOOD IAW 8 M/M 23-21-00, 23-50-00. EXCESSIVE WATER FOUND IN COCKPIT COMING FROM DITCHING HATCH AND F/O'S SIDE PANEL. INSPECTED DITCH HATCH AND SEALED F/O'S SIDE WINDOW IAW SP&P 56.1.1, PRESSURIZED A/C NO LEAKS NOTED AT THIS TIME.

Part: TRANSDUCER — FAILED (STICK SHAKER) · airframe 55,599 hrs · 63,211 cycles

BOTH STICK SHAKERS ACTIVATED ON ROTATION AND STAYED ON UNTIL RETURN TO FIELD. REMOVED AND REPLACED LT TRANSDUCER. PART INFO TO FOLLOW

Part: STICK SHAKER — ACTIVATED (STALL WARNING) · airframe 55,469 hrs · 63,067 cycles

STICK SHAKER ACTIVATED ON TAKEOFF WITH OUT ASSOCIATED CAUTION LIGHTS. SYSTEM PLACED ON MEL....MORE TO FOLLOW.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 55,022 hrs · 62,561 cycles

DURING HEAVY CHECK INSPECTIONS IT WAS NOTED THE DOOR GAS STRUT CHASSIS WAS CRACKED. REPLACED CHASSIS.

Part: OIL COOLER — LEAKING (NR 1 ENGINE) · airframe 52,288 hrs · 59,638 cycles

NR 1 ENGINE OIL PRESSURE WARNING LT ILLUMINATED ON CLIMB-OUT. POWER REDUCED AND ENGINE S/D AT 40 PSI. REMOVED AND REPLACED ENGINE OIL COOLER. FERRIED TO MDT FOR ENGINE REMOVED AND REPLACED.

Part: SKIN — GOUGED (TE FLAPS) · airframe 50,953 hrs · 58,168 cycles

DURING 20,000 HOUR INSPECTION RIGHT OUTBOARD FLAP - UPPER INBOARD SURFACE CHAFED AND GOUGED. REPAIRED PER EO 8-57-04-0476 AS A MAJOR REPAIR. DUE TO PRIOR BLENDING REPAIRS AND INABILITY TO DETERMINE REMAINING THICKNESS OF SKIN, THIS EO TRIMS OUT DAMAGE AND INSTALLS AN EXTERNAL REPAIR DOUBLER. ADDITIONALLY, THE YW 171 FLAP SHROUD FRAME IS TRIMMED OUT PER RD8-57-1549 REV A ADDRESSES DAMAGE TO STR 2 INCURRED DURING INCORPORATION OF ORIGINAL ISSUE OF THIS REPAIR. CUTOUTS ENLARGED TO ALLOW ACCESS FOR STR REWORK AND LARGER DOUBLER INSTALLED.

Part: FITTING — CRACKED (FLAP TRACK) · airframe 50,953 hrs · 58,168 cycles

OUTBOARD FLAP NR 3 FLAP TRACK ROLLER FITTING (AFT) IS BROKEN/CRACKED. UPPER ROLLER BROKEN OFF. REMOVED AND REPLACED FLAP TRACK ROLLER ASSEMBLY.

Part: WARNING LIGHT — MALFUNCTIONED (MLG) · airframe 50,190 hrs · 57,360 cycles

AFTER TAKEOFF NLG RED LIGHT TOOK LONGER TO EXTINGUISH THAN NORMAL. THEN CYCLED ON AND OFF SEVERAL TIMES WITH ASSOCIATED THUMP FROM NLG AREA. DOOR LITES DID NOT ILLUMINATE. CHECKED PSEU FOR FAULTS NONE FOUND CHECKED UPLOCK SENSOR NO FAULTS RERACKED PSEU AND PERFORMED SYSTEM TEST CHECKS GOOD. PERFORMED FLIGHT TEST OPS CHECK GOOD.

Part: ANTENNA — INOPERATIVE (RADAR) · airframe 49,179 hrs · 56,278 cycles

LOST RADAR SHORTLY AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD, WITHOUT TALKING TO MAINTENANCE. PILOT REPORTED RADAR STAB INOP, PLUS OTHER FAULTS. CREW TURNED RADAR OFF AND BACK ON, NO FIX. REPLACED RADAR RT.

Part: SKIN — DENTED (ZONE 200) · airframe 48,768 hrs · 55,863 cycles

AIRCRAFT SUSTAINED DAMAGE FROM GROUND EQUIPMENT CAUSING MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 48,768 hrs · 55,863 cycles

DURING C CHECK, CONTACT FROM PERSONNEL LIFT CAUSED GOUGE AND DENT.

Part: HYDRAULIC SYSTEM — MALFUNCTIONED (NR 1 ENGINE) · airframe 47,937 hrs · 54,984 cycles

AFTER LANDING WHEN NR 1 PROP WAS FEATHERED, CREW REPORTED LOSING NOSE WHEEL STEERING AND THE NORMAL BEAKES. CREW USED PARK BRAKE TO STOP AIRCRAFT. CREW OBSERVED MAIN AND STANDBY HYDRAULIC PRESSURE AT LESS THAN 1800 PSI FOLLOWED BY NR 1 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATING. AFTER 10 SECONDS ALL INDICATIONS RETURNED TO NORMAL. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY.

Part: MONITOR — INOPERATIVE · airframe 45,665 hrs · 52,561 cycles

MAIN AND AUX BATTERY HOT LIGHTS ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO TPA. REPLACED BATTERY TEMP MONITOR.

Part: ACTUATOR — BROKEN (#2 NACELLE)

AFTER TAKE OFF, THE RIGHT MAIN GEAR AND NOSE GEAR DID NOT INDICATE RETRACTED, GEAR DOORS STAYED OPEN. FOUND THE ROD END BROKEN OFF OF THE RIGHT MAIN GEAR RETRACTION ACTUATOR. REPLACED RETRACTION ACTUATOR.

Part: ANGLE — CRACKED · airframe 44,730 hrs · 51,534 cycles

#1 NACELLE HORSECOLLAR FRAME FWD ANGLE CRACKED. REPAIRED ANGLE I.A.W. EO8-54-02-0177.

Part: FRAME — CORRODED · airframe 43,437 hrs · 50,161 cycles

FRAME AT STATION 201 IS CORRODED AT STRINGER 31S. REPAIRED PER EO8-53-01-325.

Part: SKIN — CORRODED · airframe 43,437 hrs · 50,161 cycles

FUSELAGE SKIN CORRODED ON STRINGER 31P BETWEEN STATIONS 202 AND 240. REPAIRED PER EO8-53-01-312.

Part: STRAP — CORRODED · airframe 43,437 hrs · 50,161 cycles

THRESHOLD STRAP AT AIRSTAIR DOOR CUTOUT HAS CORROSION .020" DEEP IN SEVERAL AREAS. REPLACED STRAP.

Part: DOOR — SEPARATED (NR 2 NACELLE) · airframe 42,349 hrs · 48,995 cycles

NR 2 MLG FWD DOOR CAME OFF IN FLIGHT, DAMAGING SURROUNDING NACELLE STRUCTURE. REPLACED GEAR DOOR AND REPAIRED NACELLE STRUCTURE PER EO8-54-01-061.

Part: CONTROL VALVE — FAILED (ANTI-SKID SYSTEM) · airframe 40,304 hrs · 46,801 cycles

AFTER LANDING AND CLEARING THE RUNWAY IN FLO ON REPOSITIONING FLIGHT, THE A/C HAD AN UNCOMMANDED AND UNCONTOLLABLE TURN TO THE LEFT. NORMAL BRAKES WOULD NOT FUNCTION. CREW STOPPED THE AIRCRAFT USING THE PARKING BRAKE. AFTER ENGINE SHUTDOWN NR 4 TIRE WAS FOUND TO BE FLAT. REPLACED NR 4 MAIN WHEEL ASSEMBLY. REPLACED NR 4 BRAKE ASSEMBLY AS A PRECAUTION. INSPECTED AND OPS CHECKED ALL ASSOCIATED SYSTEMS, NO PROBLEMS FOUND. PERFOMED TAXI TEST AND EVALUATION FLIGHT, NO PROBLEMS FOUND. ANTI-SKID SYSTEM PLACED ON MEL FOR FUNCTION CHECK. ANTI-SKID FUNCTION CHECK FOUND NR 3 BRAKE WITH LOW PRESSURE. REPLACED THE ANTI-SKID DUAL CONTROL VALVE.

Part: BRAKE — SEIZED (MLG)

ON TAXI OUT, THE NR 4 BRAKE LOCKED UP. AIRCRAFT RETURNED TO THE GATE. REPLACED NR 4 BRAKE.

Part: BRAKE — SEIZED (MLG)

ON TAXI OUT, THE NR 4 BRAKE LOCKED UP. AIRCRAFT RETURNED TO THE GATE. REPLACED NR 4 BRAKE.

Part: INTERCOSTAL — CRACKED (NR 2 OIL COOLER)

NR 2 ENGINE OIL COOLER DOOR I/B INTERCOSTAL CRACKED FROM LARGE RIVET JUST FWD OF HINGE POINT RUNNING AFT TO HINGE POINT HOLE. DEFERED PER ESR8-54-91-11. REPLACE WITH POST MOD 8/1619 INTERCOSTAL WITHIN 500 HRS. REMOVED AND REPLACED OIL COOLER DOOR I/B INTERCOSTAL .

Part: SKIN — DENTED (FUSELAGE)

DENT LOCATED BETWEEN STRINGER 17 AND 18, 4 INCHES AFT OF ICE SHIELD, .044 DEEP .6 BY .1. C/W EO8-53-99-338 AS REQUIRED.

Part: SKIN — CHAFED (FUSELAGE)

WHEEL WELL CUT-OUT RADIUS CHAFED IN AFT RT SIDE APPROX .031 DEEP. DISPOSITION: BLEND OUT CHAFE AT 20:1 BLEND RATIO. EDDY CURRENT TO VERIFY NO CRACKS. TOUCH-UP W/ALODINE PER SRM 51-20-16 AND EPOXY PRIME PER SRM 51-20-36. COMPLIED WITH STATED DISPOSITION.

Part: TRUNNION — CORRODED (RT NLG WW)

RT NLG SHOCK STRUT TRUNNION CORRODED. FWD SIDE MATING SURFACE FOR TRUNNION CAP, APPROX .016 DEEP. REPAIRD IAW RD8-53-4535. PLACED ON A 1000 HR DEFERAL FOR PERM REPAIR.

Part: INTERCOSTAL — CRACKED (NR 1 NACELLE)

NR 1 NACELLE DOOR OUTBOARD INTERCOSTAL CRACKED AT FORWARD HINGE BRACKET. REPAIRED INTERCOSTAL.

Part: MAT — OUT OF POSITION (COCKPIT FLOOR)

NOSE GEAR DID NOT RETRACT WHEN SELECTED UP. FOUND ALTERNATE EXTENSION DOOR AJAR. SEATED DOOR AND CYCLED GEAR. OPERATION NORMAL. ON FOLLOWUP, TRIMMED RUBBER FLOOR MAT AWAY FROM DOOR. DOOR SEATS NORMALLY.

Part: TERMINAL — FAILED (E/E COMPT)

PHL - FLT 3455 - ODOR EVIDENT AT AFT CABIN AND FLIGHT DECK. REPLACED BURNED EXTERNAL LIGHTING RING TERMINAL AND CHAFED WIRE TO TERMINAL X1 OF RELAY 3341-K1. (M)

Part: SPRING PIN — FAILED (AILERON CONTROL)

FLT 3315 - PIT-CHO - ON LANDING, IN TURBULENCE, AILERON CHANNEL DISCONNECTED AND RECONNECTED WITH NORMAL YOKE MOVEMENT. NO ASSOCIATED CAUTION LIGHTS ILLUMINATED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE LEVER AND CLUTCH PLATE, SPROCKET AND CLUTCH PLATES, AND THE SPRING PIN. (M)

Part: CLUTCH PLATE — FAILED (AILERON CONTROLS)

FLT 3315 - PIT-CHO - ON LANDING, IN TURBULENCE, AILERON CHANNEL DISCONNECTED AND RECONNECTED WITH NORMAL YOKE MOVEMENT. NO ASSOCIATED CAUTION LIGHTS ILLUMINATED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE LEVER AND CLUTCH PLATE, SPROCKET AND CLUTCH PLATES, AND THE SPRING PIN. (M)

Part: SPROCKET — FAILED (AILERON CONTROLS)

FLT 3315 - PIT-CHO - ON LANDING, IN TURBULENCE, AILERON CHANNEL DISCONNECTED AND RECONNECTED WITH NORMAL YOKE MOVEMENT. NO ASSOCIATED CAUTION LIGHTS ILLUMINATED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE LEVER AND CLUTCH PLATE, SPROCKET AND CLUTCH PLATES, AND THE SPRING PIN. (M)

Part: SMOKE DETECTOR — OUT OF ADJUST (LAVATORY)

FLT 3394 - RIC-BWI - THE LAVATORY SMOKE DETECTOR WENT OFF IN FLIGHT. THE TEST SWITCH WAS MOVING TO TEST POSITION CAUSING IT TO ALARM. ADJUSTED THE TEST SWITCH. OPS CHECK GOOD. (M)

Part: CABLE — BROKEN (AIRSTAIR DOOR)

FLT 3177 - DCA-PHF - THE AIRSTAIR DOOR WOULD NOT FULLY OPEN. THE OUTER CABLE JAMMED ON PULLEY AND BROKE. REMOVED AND REPLACED THE OUTER AIRSTAIR DOR CABLE. (M)

Part: CARBON SEAL — DAMAGED (NR 1 ENGINE)

FLT 3221 - PHL-SBY - AT 1000 FEET ON CLIMB-OUT, THE NR 1 ENGINE OIL PRESSURE WARNING LIGHT CAME ON, OIL PRESSURE AT 20 PSI ON GAUGE. THE CREW SHUTDOWN THE NR 1 ENGINE AND RETURNED TO PHL AND LANDED WITHOUT INCIDENT. INSPECTED THE NR 1 ENGINE, NO METAL CONTAMINATION FOUND IN MAIN OR RGB FILTERS AND CHIP DETECTORS. SERVICED WITH 7 QUARTS OF OIL. LATER AT RON MAINTENANCE, PERFORMED ENGINE OIL FILTER REMOVED AND REPLACED AND REPLACED FORWARD CENTRIFUGAL CARBON SEAL AS A PRECAUTION. (M)

Part: RETRACT MECH — MALFUNCTIONED (NLG)

FLT 3089 - JAX-TPA - AFTER GEAR RETRACTION ON DEPARTURE, THE MAIN GEAR RETRACTED BUT THE GEAR DOORS REMAINED OPEN. THE LT AND RT GEAR DOOR AMBER LIGHTS ILLUMINATED. THE NOSE GEAR ALSO SHOWED UNSAFE AND A GRINDING NOISE WAS HEARD FROM THE NOSE AREA. THE AIRCRAFT TURNED BACK TO JAX AND LANDED WITHOUT INCIDENT. INSPECTED THE NOSE GEAR AREA AND FOUND HALF OF TOWING LUG MISSING. SUBMITTER STATES, SUSPECT THAT THE WOW SENSOR COVER JAMMED THE NOSE GEAR FROM FULLY COMING UP. REMOVED THE SENSOR COVER AND PLACED ON 70 HR DMT. THE NOSE LANDING GEAR WOW SENSOR COVER AND THE TOWING SPOOLS WERE REINSTALLED AT RON. (M)

Part: SELECTOR VALVE — FAILED (LANDING GEAR)

TPA/TLH - FLT 3040 - THE LANDING GEAR WOULD NOT EXTEND AFTER SELECTED DOWN UPON APPROACH. THREE RED UNSAFE LIGHTS ILLUMINATED. THE CREW PERFORMED ALTERNATE GEAR EXTENSION AND LANDED IN TLH WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE.

Part: VALVE — LACK OF LUBE (AIRSTAIR DOOR)

TLH/TPA - FLT 3087 - DURING PRE-FLIGHT WALK-AROUND, FLIGHT ATTENDANT COULD NOT OPEN MAIN EXIT DOOR. LUBED AIRSTAIR DOOR SEAL PRESSURE VALVE.