N912HA

Part: UNKNOWN — ODOR (COCKPIT) · airframe 69,540 hrs · 78,823 cycles

EXHAUST ODOR IN COCKPIT. RAN BOTH ENGINES AND BLEEDS. RAN ALL DEICE SYSTEMS. CHECKED ALL CIRCUIT BREAKERS. CHECKED ALL AVIONICS SYSTEMS. ALL CHECKED GOOD. NO EVIDENCE OF SMOKE OR EXHAUST ODOR. ALL COCKPIT LIGHTING CHECKED GOOD.

Part: CONTROL PANEL — FAILED (MLG) · airframe 68,733 hrs · 77,849 cycles

RT MLG DOOR AMBER LIGHT AFTER TAKE OFF (AFT DOOR). CYCLED GEAR IAW CHECKLIST, LIGHT EXTINGUISHED FOR A MOMENT AND THEN RETURNED. R & R GEAR DOOR ACTUATOR AND LANDING GEAR CONTROL PANEL. IAW MM 32-10-36 AND 32-30-05. OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE REF 32-30-00.

Part: CONTROL SWITCH — INOPERATIVE (WINDSHIELD HEAT) · airframe 68,575 hrs · 77,655 cycles

LT WINDSHIELD HEAT HOT CAUTION LIGHT CAME ON WHEN SELECTED TO NORM. NO LOAD. R & R WINDSHIELD HEAT CONTROL SWITCH IN COCKPIT 3041-S1. HEAT OPS CHECKED GOOD AT THIS TIME IAW MM 20-45-04.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 68,143 hrs · 77,144 cycles

SELECTED GEAR DOWN ON APPROACH. LT MAIN UNSAFE LIGHT ILLUMINATED AND PASSENGER REPORTED LT GEAR NOT EXTENDED. EXECUTED GO AROUND AND GEAR EXTENDED ON ITS OWN AFTER APPROX 5 MINUTES. R & R GEAR SELECTOR VALVE WC 32-30-41. NO FIX. R & R UPLOCK ACTUATOR AND SURGE DAMPER IN THE 1 GEAR WELL IAW MM 32-30-26. CYCLED GEAR MANY TIMES. OPS CHECKED GOOD.

Part: DUMP VALVE — MALFUNCTIONED (NR 2) · airframe 68,047 hrs · 77,032 cycles

CIRCUIT BREAKER G6 RT OTBD ROLL SPOILER INDICATION WILL NOT RESET. R & R NR1 SYSTEM, NR 2 ROLL LIFT DUMP VALVE IAW MM 27. OPS AND LEAK CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 67,995 hrs · 76,966 cycles

ROW 8, EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE. R & R BULB . OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,995 hrs · 76,966 cycles

ROW 4 EMERGENCY LIGHT BULBS ARE INOPERATIVE. R & R EMERGENCY LIGHTS. OPS CHECKED GOOD.

Part: CURRENT LIMITER — BLOWN (DC BUSS) · airframe 67,894 hrs · 76,841 cycles

DC BUSS CAUTION LIGHT CAME ON DURING TAKEOFF ROLL. REJECTED TAKEOFF. CLEARED RUNWAY. ATTEMPED TO RESET. WILL NOT RESET. MX FOUND CURRENT LIMITERS BLOWN. R & R CURRENT LIMITERS.

Part: LIGHT — MISSING (CABIN) · airframe 66,342 hrs · 74,946 cycles

ONE FLOOR EMERGENCY FLOOR PATH LIGHT IS MISSING. INSTALLED LIGHT IN CORRECT LOCATION.

Part: SEAT TRACK — CRACKED (BS 222) · airframe 66,342 hrs · 74,946 cycles

LEFT SEAT TRACK FLANGE IS CRACKED ON FWD END AT BS X222. REMOVED FLANGE. INSTALLED NEW FLANGE IAW DWG 85320079.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 66,342 hrs · 74,946 cycles

AREA OF CORROSION AT BS X488 AND STR 31S. REMOVED 2 RIVETS, CLEANED AREA AND REPAIRED IAW SRM 51-20-11 AND 51-20-36. INSTALLED NEW RIVETS.

Part: STRUCTURE — CORRODED (BS 510) · airframe 66,342 hrs · 74,946 cycles

AREA OF CORROSION AT STA X510 AND STR 31S. R & R 3 RIVETS, CLEANED AREA AND REPAIRED IAW SRM 51-20-11 AND 51-20-36. INSTALLED NEW RIVETS.

Part: STRINGER FITTING — CORRODED (BS 222) · corrosion level 2 · airframe 66,343 hrs · 74,946 cycles

AREA OF HEAVY CORROSION AT STA X222 AND STR 26S. FOUND STRINGER END CLEAT CORRODED. REMOVED CLEAT. INSTALLED NEW CLEAT IAW DWG 85320983.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,343 hrs · 74,946 cycles

POSSIBLE CORROSION BUILDUP UNDER BOTH RADIO ALTIMETER ANTENNA. REMOVED MINOR CORROSION FROM SKIN SURFACE AT BOTH FORWARD AND AFT ALTIMETER ANTENNA AREA IAW CORROSION AND PREVENTION CONTROL MANUAL, SECTION 9, CHAPTER 4.

Part: STRINGER FITTING — CORRODED (BS 222) · airframe 66,343 hrs · 74,946 cycles

AREA OF HEAVY CORROSION AT STR 26S AND FRAME X222. FOUND STRINGER END CLEAT CORRODED. REMOVED CLEAT. INSTALLED NEW CLEAT IAW DWG 85320983.

Part: BATTERY — WEAK (EMERGENCY LGIHT) · airframe 66,338 hrs · 74,940 cycles

RT EXIT SIGN (TOP) & FWD CENTER EXIT SIGN INOP. T/S FOUND BAD BATTERY IN BOTTOM COAT CLOSET LOCATION R & R BATTERY. OPS CK GOOD IAW AMM 33-52-00 & W/C 33-50-03Q.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 66,161 hrs · 74,734 cycles

EMERGENCY FLOOR PATH LIGHTS ARE INOPERATIVE AT ROW 1. R & R EMERGENCY FLOOR PATH LIGHT LAMPS AT ROW 1 AND CLOSED ACCESS PANEL.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 66,072 hrs · 74,632 cycles

EMERGENCY OVERHEAD LIGHT IS INOPERATIVE AT ROW 7. REMOVED LENS, R & R BULB AT SAID LOCATION, REINSTALLED LENS.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 65,742 hrs · 74,244 cycles

ONE RED FLOOR EMERGENCY LIGHT AT ROW 4 IS INOP. MX FOUND WIRES BROKEN. ROA VERIFIED DISCREPANCY REPAIRED BROKEN WIRE, OPS CHECKS.

Part: LIGHT — DAMAGED (CABIN) · airframe 65,445 hrs · 73,885 cycles

MISSING EMERGENCY LIGHT ARROW ON LOWER LIGHT. R & R LIGHT MODULE WITH NEW. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 64,927 hrs · 73,296 cycles

SECOND FLOOR PATH LIGHT IS INOPERATIVE. R & R LAMP IAW 33-51-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 64,707 hrs · 73,057 cycles

EMERGENCY PATH LIGHTING AT ROWS 4DF AND 7DF NOT WORKING. R & R EMERGENCY LOWER LEVEL FLOOR LIGHT BULBS IN ROWS 4DF AND 7DF.

Part: TRU — FAILED (RIGHT) · airframe 63,938 hrs · 72,181 cycles

RIGHT AC BUSS CAUTION LIGHT ILLUMINATED INFLIGHT ASSOCIATED WITH OTHER CAUTION LIGHTS. REMOVED AND REPLACED RT TRU IAW 24-31-00, OPS CHECKED GOOD.

Part: BRUSH BLOCK — BURNED (NR 1 PROPELLER) · airframe 63,559 hrs · 71,763 cycles

ON APPROACH, NR 1 ENG WAS SPARKING FROM PROP SPINNER WITH PROP HEAT ON AND NR 1 AC GENERATOR "A" PHASE AT 85 VOLTS. SELECTED PROP HEAT OFF AND SPARKS STOPPED. ON GROUND NR 1 "A" PHASE WAS 103 VOLTS. R & R NR 1 BRUSH BLOCK ASSY. REFERENCE IAW 30-61-00. R & R ONE CURRENT LIMITER IN LT AC CONTACTOR BOX. GROUND RAN ACFT, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,513 hrs · 71,713 cycles

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

Part: CONNECTOR — SHORTED (WINDSHIELD HEAT) · airframe 63,462 hrs · 71,649 cycles

NOTICE TRACE OF SMOKE IN FLIGHT DECK, DISCOVERED CAPT'S WINDSHIELD ELECTRICAL CONNECTION WITH SMALL TRACE OF SMOKE. SELECTED WINDSHIELD HEAT OFF AND SMOKE DISSIPATED. REPLACED LT WINDSCREEN IAW WORK CARD 56-00-00R, LOWERED COCKPIT OVERHEAD PANELS AND SPLICED IN 8 INCHED OF WIRE 3041-53A12C2-2 AND RESECURED PANEL. OPS AND PRESSURED CHECKED GOOD IAW WORK CARD 56-00-00R.

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR SYS) · airframe 63,438 hrs · 71,622 cycles

RADAR HAS STAB OFF MESSAGE AND WILL NOT PAINT KNOWN WEATHER. R & R RADAR RT IAW 34-41-02.OPS CHECKED GOOD. OK FOR SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 63,262 hrs · 71,426 cycles

1 EMERGENCY FLOOR PATH LIGHT IS MISSING. FOUND MISSING EMERGENCY LIGHT UNDER CENTER FLOOR PANEL AND PLACED IN IT'S PROPER POSITION, OPS CHECKED GOOD.

Part: WARNING HORN — FALSE ACTIVATION · airframe 63,246 hrs · 71,407 cycles

TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL, ABORTED TAKEOFF, CYCLED FLAPS AND CHECKED ACFT CONFIGURATION. CHECKED GOOD. PERFORMED TAKEOFF WARNING HORN OPS CHECKED GOOD. NO DISCREPANCY FOUND. ACFT OK FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 63,207 hrs · 71,362 cycles

ELECTRICAL ODOR EMINATING IN CABIN AT ROW 2 AND 3. INSPECTED CABIN LIGHTS AND ASSOCIATED AREAS WITH NO OBVIOUS DEFECTS OR ODOR NOTED.

Part: WINDSCREEN — SMOKE (COCKPIT) · airframe 62,799 hrs · 70,901 cycles

POPPING SOUND AND LIGHT SMOKE FROM LOWER PORTION OF CAPTAIN'S WINDSCREEN FOLLOWED BY BURNING RUBBER AND ELECTRICAL ODOR. R & R F/O'S RT WINDSCREEN IAW WC 56-00-00R.

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 62,797 hrs · 70,899 cycles

INTERMITTENT STRONG ODOR IN FRONT CABIN AND FLIGHT DECK. IN FLIGHT AND GROUND, STRONG SOUR BURNED TOAST ODOR MORE PREVALENT WITH ENGINE BLEEDS. OPERATED BLEED, FOUND ODOR FROM NR 2 ENGINE AND BLEED NOT OPERATING NORMAL, SUSPECT SOLNOID ON HP VALVE BAD. R & R HP BLEED VALVE, OPERATED BLEEDS, OPS CHECKED GOOD. NO ODOR.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 62,175 hrs · 70,179 cycles

ROW 13 EMERGENCY FLOOR PATH LIGHT INOP, WITH BROKEN WIRE. SPLICE WIRE AT ROW 13 RED EMERGENCY FLOOR LIGHT IAW AMM 20-45-07.

Part: WIRE — LOOSE (YOKE) · airframe 61,341 hrs · 69,207 cycles

LOOSE WIRE FOUND AT LT HANDHOLD ON CAPTAINS YOKE CAUSED SMOKE AND SPARKS WHEN TOUCHED. AUTOPILOT DISENGAGED ON CAPTAINS YOKE. DISABLED IAW EO8-22-10-10-0141. NEEDS TO BE REPAIRED OR REPLACED IN 70 FLIGHT HOURS. NO ADDITIONAL DAMAGE FOUND.

Part: TRIM SYSTEM — OUT OF ADJUST (NR 2 ENGINE) · airframe 61,271 hrs · 69,126 cycles

TAKEOFF WAS ABORTED DUE TO NP REACHING 1215 ON NR 2 ENGINE. ADJUSTED RIGHT ENGINE SPEED TRIM SCREW IN ACCORDANCE WITH HAMILTON STD MM 61-22-00. OPERATIONAL CHECKED GOOD, OK FOR SERVICE.

Part: GENERATOR — MALFUNCTIONED · airframe 61,214 hrs · 69,064 cycles

FLIGHT DECK REPORTS AC BUS CAUTION LIGHT ILLUMINATED IN FLIGHT WITH OTHER ASSOCIATED CAUTION LIGHTS. REMOVED AND REPLACED GENERATOR IN ACCORDANCE WITH WORK CARD 24-21-01, RANG WIRES FROM CONNECTOR P/N 2 GENERATOR PINS ABC TO RIGHT BUS CONTACTOR K2 PORTS ABC, ALL CHECKED GOOD.

Part: CONNECTOR — CONTAMINATED (ELECTRICAL SYS) · airframe 61,214 hrs · 69,064 cycles

RIGHT AC BUS CAUTION LIGHT ILLUMINATED IN FLIGHT FOLLOWED BY RIGHT TRU/STALL WARNING/ELEVATOR HORN HEAT CAUTION LIGHT. REMOVED AND REPLACED AC CONTACTOR K-2 IN ACCORDANCE WITH PMM WORK CARD 24-21-01. CLEANED OIL FROM CONNECTOR P1, PS,J1 AND J2 AS PRECAUTIONARY MEASURES, SYSTEM CHECKS GOOD IN ACCORDANCE WITH 24-21-01. OPERATIONAL CHECKED GOOD IN ACCORDANCE WITH SRT MANUAL, OKAY FOR SERVICE.

Part: LONGERON — CRACKED (NACELLE) · airframe 60,813 hrs

INBD UPPER LONGERON IS CRACKED AT THE FWD END. CRACK IS 1.3 INCH LONG AND IS IN THE INBD RADIUS. IT TRAVELS FROM THE FWD END, BELOW THE FIRST RIVET AND TO THE SECOND RIVET. INSTALLED RIVETS THRU VERTICAL LEG OF REPAIR ANGLE. REPAIRED IAW EO8-54 10-0007.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,511 hrs · 68,301 cycles

FLOOR EMERGENCY LIGHTS 3 AND 4 FROM FRONT NOT OPERATING. REMOVED AND REPLACED EMERGENCY LIGHT BULBS IN ACCORDANCE WITH AMM 33-52-00

Part: TRANSFER TUBE — OUT OF POSITION (NR 2 PROPELLER) · airframe 59,974 hrs · 67,710 cycles

ON TAKEOFF NR 2 PROPELLER INCREASED TO 1224 RPM WITH SUBSEQUENT PROPELLER FLUX AND TORQUE FLUX OF 5 TO 10 PERCENT. CAPTAIN WAS ABLE TO STABILIZE BY REDUCING POWER AND PROP RPM. FLIGHT DIVERTED TO MDT. MECHANIC'S PERFORMED RIGGING WORK CARD (76-00-01), NO DEFECTS NOTED. CHECKED TRANSFER TUBE, FOUND NOT INDEXED CORRECTLY. MAINTENANCE INDEXED TRANSFER TUBE IAW DASH 8 MM 61-10-00. GROUND RAN AIRCRAFT, OPS AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: BRAKE — MALFUNCTIONED (MLG) · airframe 59,047 hrs · 66,683 cycles

SMOKE COMING FROM RIGHT BRAKES. REMOVED AND REPLACED NR 4 BRAKE ASSY IN ACCORDANCE WITH MAINTENANCE MANUAL 32-42-11, LEAK AND OPS CHECKED GOOD.

Part: PRESSURE SWITCH — DEFECTIVE (ZONE 300) · airframe 58,917 hrs · 66,544 cycles

AFTER TAKEOFF RIGHT INBOARD TAIL DEICE BOOT DID NOT ILLUMINATE, LIGHT DOES TEST. REMOVED AND REPLACED TAIL DEICE BOOT PRESS SWITCH. GROUND RAN BOTH ENGINES, OPS CHECK GOOD. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,428 hrs · 65,984 cycles

FIRST FLOOR EMERGENCY LIGHT INOP. RELAMPED 1ST EMERGENCY LIGHT BULB.

Part: WIRE — BROKEN (AUTOFEATHER SYS)

ABORTED TAKEOFF DUE TO AUTOFEATHER ARM LIGHT DID NOT ILLUMINATE. FERRIED TO SBY. MAINTENANCE REPAIRED WIRE AT POWER LEVER MICROSWITCH 6121S13. OPS CHECK GOOD. (S)

Part: PSEU — MALFUNCTIONED (NLG) · airframe 56,498 hrs · 63,841 cycles

AT 10,000 FT AND 210 KNOTS NOSE GEAR EXTENDED UNCOMMANDED FOR APPROXIMATELY 5 SECONDS THEN RETRACTED. THEN NOSE GEAR CYCLED DOWN AND UP BRIEFLY WITH MAIN GEAR DOORS OPENING THEN CLOSING. GEAR EXTENDED NORMALLY ON APPROACH. REPLACED PSEU.

Part: MASTER CAUTION — SPARKS (COCKPIT) · airframe 56,104 hrs · 63,414 cycles

MASTER CAUTION PUSH TO RESET SPARKED WHEN PUSHED AND WILL NOT TEST. REPLACED MASTER CAUTION SWITCH AND CAUTION PANEL.

Part: SWITCH — LOOSE (COCKPIT) · airframe 56,027 hrs · 63,334 cycles

WHEN THE GEAR WAS SELECTED DOWN, THE CREW GOT THREE RED LIGHTS. PERFORMED EMERGENCY EXTENSION AND GOT THREE GREEN LIGHTS. THE LANDING GEAR SELECTOR VALVE WAS REPLACED. ON 1 DECEMBER WHEN THE GEAR WAS SELECTED DOWN, THE CREW GOT THREE RED LIGHTS, AFTER LEVELING OFF, THE GEAR EXTENDED. FOUND RING TERMINAL ON THE LANDING GEAR INHIBIT SWITCH VERY LOOSE. TIGHTENED SCREWS, SWUNG THE GEAR SEVERAL TIMES, OPERATIONAL CHECK GOOD.

Part: CLAMP — DAMAGED (FUEL BOOST PUMP) · airframe 55,060 hrs · 62,266 cycles

RIGHT WING AUX FUEL BOOST PUMP CLAMP RING FOUND DAMAGED AND CORRODED. RIGHT WING AUX FUEL BOOST PUMP CLAMP RING REPLACED AS PER S/B 8-57-28, LEAK CHECK REF SEQ 23.

Part: DOUBLER — CORRODED (LT WING) · airframe 55,060 hrs · 62,266 cycles

LEFT AUX BOOST PUMP (FUEL) WING DOUBLER FOUND CORRODED INSIDE AND OUTSIDE FUEL TANK. LEFT AUX BOOST PUMP (FUEL) WING DOUBLER INSIDE AND OUTSIDE OF FUEL TANK CORROSION REMOVED IAW RD8-57-3679 (MATERIAL REMAINING .415") S/B 8-57-28 PREVIOUSLY COMPLIED WITH. HFEC AND DISBOND C/O NO DEFECTS FOUND.

Part: DOUBLER — CORRODED (LT WING) · airframe 55,060 hrs · 62,266 cycles

LEFT AUX BOOST PUMP (FUEL) WING DOUBLER FOUND CORRODED INSIDE AND OUTSIDE FUEL TANK. LEFT AUX BOOST PUMP (FUEL) WING DOUBLER INSIDE AND OUTSIDE OF FUEL TANK CORROSION REMOVED IAW RD8-57-3679 (MATERIAL REMAINING .415") S/B 8-57-28 PREVIOUSLY COMPLIED WITH. HFEC AND DISBOND C/O, NO DEFECTS FOUND.

Part: SKIN — CORRODED (RUDDER) · airframe 55,060 hrs · 62,266 cycles

SIX BLIND FASTENERS FOUND CORRODED ON RIGHT SIDE OF SKIN OF FORE RUDDER NEXT TO LOWER ACTUATOR FITTING. RIGHT SIDE OF SKIN OF FORE RUDDER NEXT TO ACTUATOR FITTING 6 BLIND FASTENERS REPLACED IAW RD8-55-024.

Part: PANEL — CORRODED (FUSELAGE) · airframe 55,060 hrs · 62,266 cycles

CORROSION FOUND IN VARIOUS PLACES IN LAV SERVICE PANEL. LAVATORY MACHINED SERVICE DOOR DOUBLER REPAIRED AS PER 8-53-07-3235 AND INSTALLED WITH SOLID RIVETS AS PER SRM 51-40-00 HFEC CUTOUT NO CRACKS.

Part: DOUBLER — DAMAGED (LAVATORY SERVICE) · airframe 55,060 hrs · 62,266 cycles

CORROSION FOUND IN VARIOUS PLACES IN LAV SERVICE PANEL. LAVATORY MACHINED SERVICE DOOR DOUBLER REPAIRED AS PER 8-53-07-3235 AND INSTALLED WITH SOLID RIVETS AS PER SRM 51-40-00, HFEC CUT OUT NO CRACKS.

Part: PANEL — CORRODED (WING) · airframe 55,060 hrs · 62,266 cycles

ELEVEN CORRODED HOLES ON STRESS PANEL 521AT. ELEVEN BUSHINGS FABRICATED LOCALLY IAW WITH RD 8-53-2674 ACCESS PANEL 521AT REPLACED ON SEQ 5042.

Part: SKIN — CORRODED (RT WING) · airframe 55,060 hrs · 62,266 cycles

RIGHT WING AUX FUEL BOOST PUMP SKIN DOUBLER CORROSION SUSPECTED ON PREVIOUS BLENDED AREA (INSIDE TANK). RIGHT WING AUX FUEL PUMP WING BLENDED AS PER RD 8-57-1907 (.45 MIN REMAINING) SB 8-57-28 FOUND PREVIOUSLY COMPLIED WITH. HFEC & DISBOND C/O IAW RD 8-57-1907, NO DEFECTS.

Part: FAILSAFE — CORRODED (RT ELEVATOR) · corrosion level 2

RIGHT ELEV O/B HINGE FAIL SAFE CORRODED.

Part: DRAIN LINE — CORRODED · airframe 55,060 hrs · 62,267 cycles

CORROSION FOUND ON LAV DRAIN TUBE FLANGE.

Part: SKIN PANEL — DEBONDED (FUSELAGE) · corrosion level 2 · airframe 55,060 hrs · 62,267 cycles

DISBOND DETECTED ON LEFT FUSELAGE SKIN PANEL BETWEEN FUSELAGE STA 488.50 AND STA 510.00 AND BETWEEN STR 23 AND STR 24.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,604 hrs · 61,809 cycles

EMERGENCY LIGHT SWITCH ON FLIGHT ATTENDANTS PANEL IS NOT ILLUMINATED. RELAMPED SWITCH.

Part: UNKNOWN — ODOR (CABIN) · airframe 54,090 hrs · 61,276 cycles

ELECTRICAL BURNING ODOR LT CABIN BETWEEN ROWS 1 AND 2. AFTER SELECTING OVERHEAD LIGHTS OFF ODOR DISSIPATED, ISSUED MEL. MORE TO FOLLOW.

Part: COFFEEMAKER — OVERHEATED · airframe 53,258 hrs · 60,396 cycles

BURNING ODOR IN CABIN AND COCKPIT. FOUND SEAL ON HOT JUG BURNING DUE TO NO LIQUID INSIDE REMOVED AND REPLACED HOT JUG.

Part: DOOR — OUT OF RIG (NLG) · airframe 52,593 hrs · 59,670 cycles

NOSE GEAR DOOR AMBER LIGHT REMAINED ON AFTER TAKEOFF. RIGGED NOSE GEAR DOOR SYSTEM.

Part: SELECTOR VALVE — FAULTY (LANDING GEAR) · airframe 51,200 hrs · 58,177 cycles

LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. CREW PERFORMED ALTERNATE EXTENSION AND ALL GEAR EXTENDED NORMALLY. AN EMERGENCY WAS DECLARED. THE LANDING GEAR SELECTOR VALVE WAS REPLACED.

Part: CONNECTOR — DIRTY (NR 2 GENERATOR) · airframe 52,233 hrs · 59,265 cycles

DURING CLIMBOUT RIGHT A/C BUSS FELL OFF LINE WITH ASSOCIATED TRU CAUTION LIGHT. CLEANED NR 2 AC GEN CONNECTOR.

Part: SHIM — OUT OF ADJUST (ENGINE) · airframe 51,465 hrs · 54,851 cycles

AIRCRAFT RETURNED TO FIELD DUE TO OIL PRESSURE RISING TO 70 PSI ON CLIMBOUT. REMOVED TWO SHIMS AT OIL PRESSURE REGULATOR.

Part: SWITCH — LACK OF LUBE (BETA SYSTEM) · airframe 51,416 hrs · 58,395 cycles

DURING CLIMBOUT AT ABOUT 200 TO 300 FEET NR 2 PROP CYCLED ABOUT 150 TO 200 RPM AND TQ CYCLED 85 TO 115 PERCENT FOR ABOUT 90 SECONDS. LUBED BETA BACK UP POWER LEVER SWITCHES, REINSTATED BETA LOCKOUT SWITCHES AND C/W BETA GROUND LOGIC WORK CARD.

Part: CHECK VALVE — CRACKED (HYD SYSTEM) · airframe 50,814 hrs · 57,759 cycles

AT GEAR RETRACTION NR 2 ISOV CAUTION LIGHT ILLUMINATED FOLLOWED BY ROLL SPOILER HYD. CAUTION LIGHT NR 2 QUANTITY DROPPED TO 1/2 QT. SYSTEM PRESSURE REMAINED NORMAL. REPLACED CHECK VALVE.

Part: PROXIMITY SENSOR — BROKEN (LANDING GEAR) · airframe 50,091 hrs · 56,960 cycles

LEFT AMBER GEAR DOOR LIGHT ON DURING GEAR RETRACTION. REPLACED PROXIMITY SENSOR. (M)

Part: CONNECTOR — NOT SEATED (NLG) · airframe 49,403 hrs · 56,228 cycles

AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT AND LT/RT GEAR DOORS REMAINED OPEN, NOSE GEAR RED TRANSIT LIGHT STAYED ILLUMINATED. LT AND RT MAINS RETRACTED NORMALLY. REROUTED ELECTRICAL HARNESS AND SEATED CONNECTOR OPS CHECK GOOD.

Part: WIRE HARNESS — MISROUTED (MLG) · airframe 49,403 hrs · 56,228 cycles

AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT AND LT & RT GEAR DOORS REMAINED OPEN, NOSE GEAR RED TRANSIT LIGHT STAYED ILLUMINATED. LT AND RT MAINS RETRACTED NORMALLY. REROUTED ELECTRICAL HARNESS AND SEATED CONNECTORS, OPS CHECK GOOD.

Part: DOOR — OUT OF ADJUST (LT MLG) · airframe 489,327 hrs · 55,685 cycles

AFTER GEAR RETRACTION LEFT MAIN GEAR DOOR LT CAME ON AND VISUALLY CONFIRMED DOOR OPEN. DUE TO THE AIRSPEED RESTRICTION, A/C RETURNED TO PHL. A/C WILL FERRY TO SBY FOR REPAIRS. ADJUSTED LEFT FWD GEAR DOOR. GEAR SWINGS, OP'S CHECK GOOD.

Part: ACM — SEIZED (CABIN COOLING) · airframe 47,628 hrs · 54,278 cycles

ACM SEIZES UP AND SMOKED UP CABIN

Part: BOOT — CONTAMINATED (RT WING) · airframe 43,894 hrs · 50,375 cycles

ON CLIMBOUT DEICE PRESSURE DROPPED TO 10 PSI FOLLOWED BY ILLUMINATION OF THE DEICE PRESSURE CAUTION LIGHT. RT WING SECOND BOOT FROM TIP AND ALL TAIL BOOTS WOULD NOT SHOW INFLATION. AIRCRAFT RETURNED TO FIELD. MAINTENANCE PURGED WATER FROM SYSTEM. GROUND CHECK GOOD.

Part: POTENTIOMETER — INOPERATIVE (R/H WING) · airframe 43,075 hrs · 49,536 cycles

UNCOMMANDED LEFT WING DOWN TRIM IN FLIGHT, RECENTERED TRIM WITH AILERON TRIM SWITCH. REPLACED AILERON TRIM TAB POTENTIOMETER.

Part: HYDRAULIC LINE — LEAKING · airframe 41,442 hrs · 47,791 cycles

#2 HYDRAILIC SYSTEM FLUID LOSS DOWN TO ISOLATION VALVE ACTUATION. PRESSURE REMAINED NORMAL WITH APPROX. 1/2 QT. INDICATED RESERVOIR QUANTITY. AIRCRAFT DIVERTED TO SAV. FOUND FLEX LINE TO NLG DRAG STRUT ACTUATOR LEAKING. REPLACED FLEX LINE.

Part: INDICATOR — DEFECTIVE (COCKPIT) · airframe 39,696 hrs · 45,962 cycles

WHILE PARKING THE AIRCRAFT CREW NOTICED RADAR INDICATOR CRT WAS COVERED WITH GREEN LINES AND A BURNING SMELL COMING FROM THE INDICATOR. REPLACED RADAR INDICATOR.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 3 · airframe 37,933 hrs · 44,068 cycles

FRAME LEG AT STA 240.5 OUTBOARD OF STRINGER 31 CORRODED AT WATERWAY PASSAGE. REPAIRED IAW SRM 53-20-21.

Part: RETRACT MECH — MALFUNCTIONED (RT MLG)

RT MAIN LANDING GEAR DOOR DID NOT CLOSE AFTER RETRACTION. CYCLED GEAR AND OK.

Part: ACTUATOR — LEAKING (NR 2 MLG DOOR)

UPON GEAR RETRACTION THE RT MLG DOOR REMAINED OPEN. CYCLED GEAR, DOOR CLOSED NORMALLY. REMOVED AND REPLACED NR 2 MLG DOOR ACTUATOR.

Part: BATTERY — DISCHARGED (CABIN)

PHL/SBY - FLT 3221 - AFT CEILING EMERGENCY DOWN LIGHT INOPERABLE. LEFT EMERGENCY EGRESS EXIT SIGN AND LOCATOR LIGHTS INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY PACK 3351-PS3.

Part: CONTROL UNIT — FAILED (NR 2 ENGINE)

CHO/CLT - FLT 3156 - DURING PRE-FLIGHT CHECKS, THE AUTOFEATHER TEST WAS FOUND INOPERATIVE. COULD NOT DUPLICATE. REMOVED AND REPLACED THE NR 1 AND NR 2 TORQUE SENSOR CONTROL UNITS. REFERENCE CONTROL NR 96ZZZX323. (X)

Part: CONTROL UNIT — FAILED (NR 1 ENGINE)

CHO/CLT - FLT 3156 - DURING PRE-FLIGHT CHECKS, THE AUTOFEATHER TEST WAS FOUND INOPERATIVE. COULD NOT DUPLICATE. REMOVED AND REPLACED THE NR 1 AND NR 2 TORQUE SENSOR CONTROL UNITS. REFERENCE CONTROL NR HNAA9591231.

Part: TSEU — MALFUNCTION (NR 1 ENGINE)

FLT 3409 - FLL-TPA - WHILE ATTEMPTING TO SET TAKEOFF POWER, NR 1 ENGINE TORQUE DID NOT COME UP AND PROPELLER WENT INTO FEATHER. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 TORQUE SENSOR ELECTRONIC CONTROL AND THE NR 1 ENGINE T1.8 SENSOR.

Part: SENSOR — MALFUNCTION (NR 1 ENG T1.8)

FLT 3409 - FLL-TPA - WHILE ATTEMPTING TO SET TAKEOFF POWER, NR 1 ENGINE TORQUE DID NOT COME UP AND PROPELLER WENT INTO FEATHER. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 TORQUE SENSOR ELECTRONIC CONTROL AND THE NR 1 ENGINE T1.8 SENSOR.

Part: ECU — FAILED (NR 1 ENGINE)

CHO/BWI - FLT 3201 - ON CLIMB-OUT, NR 1 ENGINE TORQUE UPTRIMMED TO 125 PERCENT. AT FLIGHT IDLE, STILL AT 110 PERCENT. CAPTAIN SHUT ENGINE DOWN IN-FLIGHT. AIRCRAFT DIVERTED TO RIC AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE ELECTRONIC CONTROL UNIT.

Part: EEL CONNECTOR — LOOSE (CABIN)

FLT NR 3427 - HPN-PHL - DURING PREFLIGHT WALKAROUND, TWO RED EMERGENCY FLOOR LIGHTS WERE FOUND INOP AT ROW 1. SECURED THE CONNECTOR UNDER THE FLOOR AT ROW 1.