N975HA

Part: DUCT — OVERTEMP · airframe 66,510 hrs · 74,642 cycles

DUCT TEMP RUNAWAY. FUMES IN CABIN. CABIN DUCT HOT, CAUTION LIGHT ILLUMINATED. GROUND RAN AIRCRAFT, CREW OPS CHECKED THE ECS IN MANUAL AND THEN IN AUTO. TAXI AIRCRAFT AND OPS CHECKED SYSTEM. OPS CHECKED GOOD.OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,422 hrs · 74,537 cycles

FIFTH EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,026 hrs · 74,080 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,887 hrs · 73,914 cycles

EMERGENCY LIGHT ON CEILING AT ROW 7 INOPERATIVE. R & R EMERGENCY LIGHT ON CEILING AT ROW 7.

Part: RADAR — ERRATIC (WX SYSTEM) · airframe 65,794 hrs · 73,808 cycles

WEATHER RADAR PAINTS ERRATIC WEATHER. APP.1 34-13. R & R WEATHER RADAR GRAPHICS UNIT IN REF TO -8 MM 34-02-02. OPS CK OF WEATHER RADAR GOOD IN REF TO -8 MM 34-41-04. CCN ON, SRL ON, CCN OFF, SRL OFF TAG POS, RSN SOS BOR 8340137, 1359, 8340137 P-1020 533440 -00, 02.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,895 hrs · 72,733 cycles

EMERGENCY FLOOR LIGHT IS INOPERATIVE AT ROW 2. REMOVED FLOOR TRIM, R & R BULBS. REINSTALLED TRIM, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,714 hrs · 72,524 cycles

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

Part: RADAR — INOPERATIVE (WX SYSTEM) · airframe 64,158 hrs · 71,864 cycles

WEATHER RADAR WILL NOT PAINT IN KNOWN WEATHER. R & R WEATHER RADAR R/T IAW MM 34-41-04. OPS CHECKED GOOD IAW PB 34-18. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,786 hrs · 71,413 cycles

AFT EMERGENCY EGRESS LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY AT ROW 3AC IAW MM 33-51-05. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,630 hrs · 71,226 cycles

RIGHT FORWARD EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. R & R BULB FOR RT FWD EXTERIOR EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,001 hrs · 70,451 cycles

F/A'S EMERGENCY LIGHT SWITCH BACK LIGHT IS INOPERATIVE. R & R BULB IN BACK LIGHT SWITCH. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,904 hrs · 70,407 cycles

EMERGENCY LIGHT INOP. R & R THE BULB. , OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,786 hrs · 70,200 cycles

F/A EMERGENCY LIGHT SWITCH BACK LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT SWITCH BULB. OPS CHECKED GOOD.

Part: GROUND STUD — LOOSE (NR 1 ENGINE) · airframe 62,570 hrs · 69,951 cycles

AT 18,000 FT, NR 1 OIL TEMP FLUXUATED BETWEEN 100 AND RED LINE AT LOWER ALTITUDE, NORMAL UNTIL DECENT, THEN FLUXUATES BETWEEN NORMAL TO THE TOP OF GREEN ARC AND RED LINE. INSPECTED NR 1 ENGINE, FOUND LOOSE GROUND AT JUNCTION, TIGHTENED AND CLEANED GROUND TERMINAL AND GROUND RAN ACFT. OPS CHECKED GOOD AT THIS TIME, OK FOR SERVICE.

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 62,472 hrs · 69,833 cycles

NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. REJECTED TAKEOFF. CHECKED NR 1 ENGINE OIL QTY. ADDED 2 QTS OF OIL. CLEANED AND INSPECTED OIL PRESSURE SWITCH AND TRANSMIT CONNECTORS. CREW GROUND RAN ACFT. NO WARNING LIGHTS ILLUMINATED. OK FOR SERVICE.

Part: PCU — MALFUNCTIONED (NR 2) · airframe 61,819 hrs · 69,026 cycles

AFTER ROTATION, NR 2 PROPELLER INDICATED 1236 FOR 5 SECONDS, TORQUE INDICATED 87-88 PERCENT. R & R NR 2 PCU IAW 61-10-10R AND WC 76-00-01Q. OPS CHECK AND LEAK CHECKED GOOD. OK FOR SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 61,002 hrs · 68,018 cycles

EMERGENCY FLOOR PATH LIGHTS AT POSITIONS 2 AND 3 ARE INOPERATIVE. R & R BULBS. OPS CHECKED GOOD.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 2) · airframe 60,623 hrs · 67,575 cycles

DURING GEAR RETRACTION, NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED. BOTH MAIN AND STANDBY PSI DROPPED TO 2000 PSI AND RUDDER FULL CAUTION LIGHT ILLUMINATED. AFTER THREE SECONDS, BOTH CAUTION LIGHTS EXTINGUISHED AND PRESSURE RETURNED TO NORMAL. ACFT JUST COMPLETED MAJOR HYDRAULIC SYSTEM COMPONENT R & R. SUSPECTED AIR IN HYDRAULIC SYSTEM. CHECKED BOTH SYSTEMS FOR EXCESS AIR IAW MM PROCEDURES 29-10-00. NO EXCESSIVE AIR NOTED AT THIS TIME.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 60,623 hrs · 67,577 cycles

DURING GEAR RETRACTION, NR 2 HYDRAULIC PRESSURE DROPPED TO 2000 PSI WITH NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT. R & R NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND SHAFT IAW WC 29-00-00R, 72-00-04L AND MM 29-10-11, PAGE 201.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 60,560 hrs · 67,496 cycles

FLOOR LEVEL EMERGENCY LIGHTS WILL NOT ILLUMINATE DURING TEST. R & R ALL EMERGENCY LIGHT BATTERIES IAW WC 33-50-03Q. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 60,153 hrs · 66,971 cycles

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

Part: OIL SYSTEM — LOW (ENGINES) · airframe 60,104 hrs · 60,904 cycles

MASTER WARNING LIGHT ILLUMINATED AND SUSPECT NR 1 OR NR 2 ENGINE OIL PRESSURE LIGHT WAS ILLUMINATED DURING TAKEOFF ROLL. INSPECTED NR 1 AND NR 2 ENGINES. SERVICED NR 1 WITH 3 QUARTS AND NR 2 WITH 2 QUARTS OF OIL. GROUND RAN ACFT AT HIGH POWER. NO DEFECTS NOTED.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 60,067 hrs · 66,860 cycles

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

Part: ACM — ODOR · airframe 60,047 hrs · 66,836 cycles

OIL ODOR IN COCKPIT WITH BLEEDS ON AND POWER AT FLIGHT IDLE. NO ODOR WITH BLEEDS OFF. R & R ACM IAW MM 21-50-11. OPS CHECKED GOOD.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 59,925 hrs · 66,694 cycles

WEATHER RADAR FAILS WHEN ADJUSTING TILT. R & R RADAR R/T IAW MM 34-41-04. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 58,948 hrs · 65,493 cycles

SIDEWALL EMERGENCY LIGHT HAS 1 BULB INOP AT ROW 4DF. REMOVED LENS, REMOVED AND REPLACED BULB, AT SAID LOCATION. INSTALLED LENS. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 219-240) · airframe 58,877 hrs · 65,394 cycles

RT INBD SEAT TRACK IS CORRODED AT STA 219 TO X240. REPAIRED RT SEAT TRACK IAW RD8-53-3074 AND DWG 85320490. ALODINE AS REQUIRED.

Part: CHANNEL — CRACKED (BS 545) · airframe 58,877 hrs · 65,394 cycles

ANGLE FOUND CRACKED ON FRAME STA X545, STR 16 AND STR 22. REPLACED CHANNEL ASSY ON FRAME BETWEEN STRINGERS 16 AND 22, AT STA X545 IAW SRM 51-42-05

Part: ANGLE — CRACKED (RT NACELLE) · airframe 58,877 hrs · 65,394 cycles

RT NACELLE FINGERNAIL OTBD LOWER AFT HEAT SHIELD ANGLE IS CRACKED. R & R LOWER AFT ANGLE IAW SRM 51-42-05.

Part: ANGLE — CRACKED (NACELLE) · airframe 58,877 hrs · 65,394 cycles

LEFT INBD AND OTBD UPPER ANGLE IS CRACKED. REPAIRED BOTH LT AND RT UPPER ANGLES IAW SRM 51-42-45.

Part: BRACKET — CRACKED · airframe 68,877 hrs · 65,394 cycles

GENERATOR INTAKE COOLING BRACKET IS CRACKED ON RT ENGINE COWLING PANEL 424AR. REPAIRED INNER SKIN OF RT ENGINE COOLING DUCT BRACKET IAW EA16-2013-037 AND E08-71-13-0034.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,877 hrs · 65,394 cycles

CORROSION FOUND ON LT AND RT INBD SEAT TRACK DEFLECTOR BETWEEN STA X260 AND X387. REPAIRED DEFLECTOR FOR LT AND RT INBD SEAT TRACK IAW SRM 51-42-05

Part: HINGE — CRACKED (ACCESS PANEL) · airframe 58,877 hrs · 65,394 cycles

CARGO ARTICULATED PANEL HINGE IS CRACKED. R & R HINGE PANEL FOR CARGO ARTICULATED PANEL.

Part: RETAINER — CRACKED (EXHAUST) · airframe 58,877 hrs · 65,395 cycles

LT NACELLE EXHAUST SHROUD SEAL RETAINER IS CRACKED. REPAIRED SEAL RETAINER IAW DWG 85411375.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,877 hrs · 65,394 cycles

LEFT AND RIGHT INBD SEAT TRACK FROM STA X182 TO X526 HAVE LIGHT SURFACE CORROSION. REPAIRED LT SEAT RAIL, INBD FROM STA X182 TO X526 IAW RD8-53-1339. REPAIRED RT INBD SEAT TRACK IAW RD8-53-1339. HFEC INSPECTION WAS COMPLIED WITH. NO DEFECTS FOUND.

Part: STIFFENER — CRACKED (RT NACELLE) · airframe 58,877 hrs · 65,394 cycles

TWO STIFFENERS AND ONE CHANNEL WAS FOUND CRACKED ON RT NACELLE HEAT SHIELD. REPAIRED STIFFENERS AND CHANNEL ON RT NACELLE HEAT SHIELD AD IAW RD8-54-1153 AND RD8-54-3195.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 58,877 hrs · 65,394 cycles

LT FORWARD CLOSING ANGLE IS CRACKED. R & R CLOSING ANGLE IAW SRM 51-40-10, SRM 51-42-45, SRM 51-42-05, RD8-51-0015 AND RD8-51-0102.

Part: BRACKET — CRACKED (INTAKE DUCT) · airframe 58,877 hrs · 65,394 cycles

RT ENGINE COWLING GEN COOLING INTAKE DUCT BRACKET IS CRACKED. REPAIRED RT ENGINE COWLING PANEL 424AR IAW EO8-71-13-0073, EA09-2013-019.

Part: BRACKET — CRACKED (BLEED DUCT) · airframe 58,877 hrs · 65,394 cycles

RT SHROUDED BLEED PIPE LOWER BRACKET IS CRACKED. REPAIRED RT LOWER BRACKET FOR BLEED PIPE SHROUD IAW SRM 51-42-05.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,877 hrs · 65,394 cycles

PAX DOOR THRESHOLD IS CORRODED ON TOP AND BOTTOM SURFACE. R & R PAX DOOR THRESHOLD ASSY IAW SRM 61-42-05.

Part: STRUCTURE — CRACKED (LT NACELLE) · airframe 58,877 hrs · 65,394 cycles

LEFT NACELLE FWD DOOR OPENING, OTBD CORNING IS CRACKED. STOP DRILLED AND TRIMMED AWAY CRACK, FILLED AND SEALED IAW RD8-54-119.

Part: DIAPHRAGM — CRACKED (NACELLE) · airframe 58,877 hrs · 65,394 cycles

DIAPHRAGM IS CRACKED ON RT FINGERNAIL AT STA XN215, OTBD LOWER CORNER. R & R DIAPHRAGM IAW STRUCTURAL REPAIR MANUAL 51-42-051.

Part: RELEASE CABLE — CHAFED (MLG) · airframe 58,877 hrs · 65,394 cycles

LEFT NACELLE MLG EMERGENCY RELEASE CABLE IS CHAFED AND CORRODED. R & R EMERGENCY RELEASE CABLE IN LT NACELLE IAW AMM32-35-00.

Part: DRAG ANGLE — CRACKED (LT NACELLE) · airframe 58,877 hrs · 65,394 cycles

LT NACELLE TO WING INBD DRAG ANGLE IS CRACKED. REPAIRED LT DRAG ANGLE IAW RD8-57-1053 AND RD8-51-0015. HIGH FREQUENCY EDDIE CURRENT WAS COMPLIED WITH IAW RD8-57-1053. NO DEFECTS NOTED.

Part: DRAG ANGLE — CRACKED (RT NACELLE) · airframe 58,877 hrs · 65,394 cycles

RT NACELLE TO WING OTBD DRAG ANGLE WAS FOUND TO BE CRACKED. REPAIRED DRAG ANGLE IAW EA 16-2013-042. HIGH FREQUENCY EDDIE CURRENT WAS COMPLIED WITH IAW EA 16-2013-042. NO DEFECTS FOUND.

Part: STRUCTURE — CRACKED (LT NACELLE) · airframe 58,875 hrs · 65,392 cycles

LEFT ENGINE COWL OPENING IS CRACKED, XN 125.50. HFEC INSPECTION WAS DONE IAW RD8-54-1315. NO DEFECTS NOTED.

Part: STIFFENER — CRACKED (HEAT SHIELD) · airframe 58,875 hrs · 65,392 cycles

TWO STIFFENERS AND ONE CHANNEL WAS FOUND CRACKED ON RT NACELLE SHIELD. FABRICATED HEAT SHIELD IAW RD 8-54-1153 AND RD8-54-3195.

Part: DRAG ANGLE — CRACKED (RT NACELLE) · airframe 58,875 hrs · 65,293 cycles

RT NACELLE TO WING OTBD DRAG ANGLE WAS FOUND CRACKED. DRAG ANGLE WAS REPAIRED IAW EA 16-2013-042. COMPLIED WITH HFEC INSPECTION. REINSTALLED ACCES SKIN PANEL IAW RD8-51-0015 AND SRM 51-42-05.

Part: STRUCTURE — CORRODED (NR 2 NACELLE) · airframe 58,875 hrs · 65,392 cycles

NR 2 NACELLE AFT ID CORRODED. REPAIRED RT AFT ID IAW RD8-54-020. NO DEFECTS NOTED.

Part: GAUGE — ERRATIC (FUEL TEMP) · airframe 58,873 hrs · 65,391 cycles

NR 1 ENGINE FUEL TEMP GAUGE IS ERRATIC. REPLACED GAUGE. DID NOT FIX. REINSTALLED ORIGINAL GAUGE. R & R NR 1 ENGINE FUEL TEMP BULB IAW AMM 71-00-02. RAN ACFT. OPS CHECKED GOOD AT THIS TIME. OK FOR SERVICE.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 58,819 hrs · 65,323 cycles

NOTICED NR 1 HYD FLUID QTY DECREASING IN FLIGHT. NR 1 HYD QTY AT 1.25 AFTER LANDING. FOUND B-NUTS ON NR 1 RESERVOIR LOOSE. VERIFIED ALL CONNECTIONS SECURE, IN NR 1 NAC. CLEANED TIRE, AND NAC OF RESIDUAL HYD FLUID. CKED EPA DRAINS FOR FLUID. NONE FOUND. CYCLED THROUGH ALL FLIGHT CONTROL FLAPS AND PERFORMED NUMEROUS GEAR SWINGS. ALL CKD GOOD. NO LEAKS NOTED.

Part: RELAY — FAILED (WINDSHIELD HEAT) · airframe 58,784 hrs · 65,277 cycles

LEFT FRONT WINDSHIELD HEAT IN NORM IS INOPERATIVE. OHMED WINDSHIELD, CHECKED GOOD. SLAVED IN CONTROLLER, NO FIX. REINSTALLED ORIGINAL. R & R RELAY 3041-K6, NO FIX. R & R RELAYS 3041-K4 AND K9. OPERATED WINDSHIELD HEAT. OPS CHECKED GOOD AT THIS TIME.

Part: COMBUSTION HEAD — ODOR (APU) · airframe 58,592 hrs · 65,028 cycles

AFTER STARTING APU, NOTICED STRONG FUEL ODOR FOLLOWED BY APU SHUTDOWN. INSPECTED, NO LEAKS FOUND, CONFIRMED PROBLEM WITH BLEEDS ON. R & R APU COMBUSTER IAW AMM 49-20-00. OPS AND LEAKED CHECKED GOOD. RAN APU WITH BLEEDS ON. NO FUEL ODOR NOTED. CLEARED MEL 49-4.

Part: APU — FUMES · airframe 58,554 hrs · 64,982 cycles

FUEL FUMES ENTERING CABIN WITH APU BLEEDS ENGAGED, FOLLOWED BY APU SHUTDOWN.

Part: GAUGE — FAILED (FUEL TEMP) · airframe 58,346 hrs · 64,736 cycles

NR 2 ENGINE FUEL TEMP INDICATOR RED LINED AFTER ENGINE START. R & R FUEL TEMP GAUGE, FUEL TEMP TRANSMITTER AND FUEL TEMP TRANSMITTER CONNECTOR PLUG. CHECKED ALL GROUNDS IAW 73-33-00 AND 71-00-02. OPS CHECKED GOOD. OK FOR SERVICE.

Part: INDICATOR — MALFUNCTIONED (WX RADAR SYS) · airframe 57,870 hrs · 64,157 cycles

WEATHER RADAR SHOWS TEST PATTERN WHEN SELECTED ON. R & R WEATHER RADAR INDICATOR, OPS CHECKED GOOD. OK OR SERVICE.

Part: WARNING HORN — FALSE ACTIVATION · airframe 57,107 hrs · 63,276 cycles

TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL AT APPROX 70 PERCENT TORQUE. CYCLED FLAPS, ELEVATOR TRIM. SYS OPS CHECKED GOOD.

Part: ACTUATOR — LEAKING (SPOILERS) · airframe 56,937 hrs · 63,071 cycles

NR 1 HYD QTY WENT TO 0.5 WITH HYD ISO AND INBD ROLL SPOILER CAUTION LIGHTS ILLUMINATED. R & R LT INBD SPOILER ACTUATOR IAW MM 27-14-05. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 56,905 hrs · 63,031 cycles

FLOOR EMERGENCY LIGHTS FROM ROW 1 TO ROW 4 BURNED OUT. R & R BULBS. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 56,851 hrs · 62,971 cycles

ROW 4AC LOWER WALL EMERGENCY EXIT LIGHT HAS BULB INOPERATIVE. R & R BULB IN ROW 4AC LOWER WALL EMERGENCY EXIT LIGHT AS REQUIRED. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 56,851 hrs · 62,971 cycles

ROW 1DF HAS 1 FLOOR EMERGENCY LIGHT INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — FAILED (CONTROL PANEL) · airframe 57,233 hrs · 63,836 cycles

BACKLIGHT IN EMERGENCY LIGHT BUTTON AT F/A PANEL IS INOPERATIVE. REMOVED SWITCH COVER, RELAMPED. REINSTALLED SWITCH COVER. OPS CHECKED GOOD.

Part: MODULE — MISINSTALLED (EMERGENCY LIGHTS) · airframe 56,442 hrs · 62,490 cycles

FLOOR LEVEL MID EXIT EMERGENCY LIGHT MODULE ARE POINTING IN WRONG DIRECTION. REALIGNED FLOOR LIGHT MODULE. OPS CHECKED GOOD. OK FOR SERVICE.

Part: ENGINE — OVERSPEED (NR 2) · airframe 56,295 hrs · 62,315 cycles

DURING APPROACH, BRINGING CONDITION LEVERS UP TO MAX, NR 2 NP WENT TO 1360 AND NR1 TO 1200. VERY LITTLE TQ INCREASE WHEN POWER LEVER ADVANCED, NP CONTINUED TO INCREASE. R & R NR 2 ENGINE IAW WORKCARD 71-00-01R AND 71-00-02R. OPS CHECKED AND LEAKED CHECKED GOOD.

Part: TRU — MALFUNCTIONED (RIGHT) · airframe 56,302 hrs · 62,324 cycles

RT AC BUSS CAUTION LIGHT ILLUMINATED INFLIGHT. PULLED CIRCUIT BREAKER FOR RT TRU. GROUND RAN ACFT. RT AC BUSS CAUTION LIGHT REMAINED EXTINGUISHED.

Part: LINE — FAILED (HYDRAULIC SYS) · airframe 55,972 hrs · 61,946 cycles

AFTER TAKEOFF, NR 2 HYD SYS WENT TO ISO, NR 2 HYD SYS DROPPED TO 1 QUART. RETURN TO FIELD. NR 2 QUANTY DOWN TO ZERO. R & R NOSE GEAR STAY ACTUATOR HYD LINE. BLED AND SERVICED NR 2 HYD SYS AND LEAKED CHECKED GOOD.

Part: FUEL CAP — UNSECURE (LT WING) · airframe 55,820 hrs · 61,777 cycles

AFTER LIFTOFF, CREW NOTICED WING FUEL CAP LIFTING UP. RETURN TO FIELD. INSPECTED LT WING FUEL CAP AND UPPER WING SURFACE. NO DEFECTS NOTED. R & R FUEL CAP AS PRECAUTION. CLEANED UP EXCESSIVE FUEL. OK FOR SERVICE.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 55,316 hrs · 61,194 cycles

LEFT AFT EMERGENCY EGRESS LIGHT IS INOP. FOUND AFT EMERGENCY CEILING LIGHT INOP. R & R EMERGENCY LIGHT BATTERY AT PS3 LOCATION. OPS CHECKED GOOD.

Part: BULB — WEAK (EMERGENCY LIGHT) · airframe 55,716 hrs · 60,543 cycles

DIM EMERGENCY LIGHT AT RT FUSELAGE AFT EXTERIOR. REMOVED LENS, R & R BULB AT SAID LOCATION, REINSTALLED LENS.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 54,255 hrs · 50,037 cycles

2 RED FLOOR EMERGENCY LIGHTS ARE INOP AT ROW 1. INSTALLED NEW BULBS, OPS CHECKED GOOD.

Part: PSU — SHORTED (ROW 4 DF) · airframe 53,231 hrs · 60,016 cycles

ELECTRICAL ODOR IN CABIN, RETURNED TO FIELD. ISOLATED ODOR TO DEFECTIVE PSU AT ROW 4DF. PERFORMED SURROUNDING AREA INSP. NO DEFECTS. R & R PSU. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,658 hrs · 59,371 cycles

THERE ARE ONLY 20 EMERGENCY FLOOR LIGHTS. INSPECTED EMERGENCY PATH, FOUND 1 LIGHT UNDER FLOOR AT ROW 6 AND 7. REPLACED BASE MATERIAL FROM ROW 6 BACK TO ROW 9.

Part: SOLENOID VALVE — INOPERATIVE (SPOILERS) · airframe 53,493 hrs · 59,177 cycles

ROLL SPOILER OTBD CAUTION LIGHT ILLUMINATED. ABORTED TAKEOFF AND RETURNED TO GATE. VERFIED SPOILERS INACTIVE, (SHUTOFF) REMOVED CONNECTOR FROM UNLOADING VALVE AND SPOILERS STILL SHUT OFF AND NO VOLTAGE TO SOLENOID WHEN SELECTED ON. SUSPECTED BAD UNLOADING VALVE. R & R UNLOAD SOLENOID VALVE NR2 IAW 27-14-21.

Part: SKIN — LOOSE (NACELLE) · airframe 53,465 hrs · 59,147 cycles

SEVERAL RIVETS IN NACELLE SIDE SKINS FROM STA. XN 134-XN138 AT LONGERON ATTACH POINT ARE LOOSE. REMOVED LOOSE RIVETS. REPAIRED IAW EO8-54-10-0406.

Part: SKIN — LOOSE (NACELLE) · airframe 53,466 hrs · 59,147 cycles

SEVERAL RIVETS ARE LOOSE ON NACELLE SIDE SKIN STA XN134, XN140 AT LOWER LONGERON ATTACH POINT. REPAIRED IAW EO8-54-20-0433.

Part: FITTING — CORRODED (BS 531 S31R) · airframe 53,465 hrs · 59,147 cycles

CORROSION AT TENSION FITTING STA 531 AND STR 31 RT SIDE. REMOVED FWD TENSION FITTING AT CORROSION AREA. COMPLIED WITH BOND TEST, NO DEFECTS NOTED. REPLACED TENSION FITTING IAW DWG 85330510. REMOVED CORRODED SECTION OF STR 31, RT SIDE BETWEEN FRAME X488 X531. REPAIRED STR.31 IAW EO8-53-10-0436.

Part: RIVET — LOOSE (NACELLE) · airframe 53,466 hrs · 59,147 cycles

SEVERAL RIVETS ARE WORKING ON LT NACELLE, INBD SIDE AT XN137.37. REMOVED LOOSE RIVETS. REPAIRED IAW EO8-54-0406.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,546 hrs · 58,074 cycles

EMERGENCY LIGHTS ROW 1DF ON SIDEWALL AND ONE EMERGENCY LIGHT AT CABIN ENTRANCE ON FLIGHT ATTENDANCE WALL HAS LIGHT INOP. RE-LAMPED CABIN SIDEWALL AND CABIN ENTRANCE LOCATIONS REFERENCE WDM 33-51-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,546 hrs · 58,074 cycles

ROW 1 RED EMERGENCY FLOOR PATH LIGHT IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT, LOCATION REFERENCE MM 33-53-02.

Part: LIGHT — NOT SEATED (CABIN) · airframe 52,531 hrs · 58,054 cycles

ROW 1 AND ROW 2 HAVE 2 EMERGENCY PATH FLOOR LIGHTS INOP AND ONE FLOOR LEVEL WHITE EMERGENCY LIGHT ROW 2 NOT WORKING. RESEATED LIGHT BULBS IN SOCK AT ROWS 1 AND 2, REMOVED AND REPLACED FLOOR MOUNTED EMERGENCY LIGHT BULB AT ROW 2. OPS CHECKED GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 51,115 hrs · 56,467 cycles

EMERGENCY EXIT SIGN AT EACH OF (3) EMERG EXIT DOORS, FWD CABIN EXIT LOCATOR AND MID CTR CEILING AISLE LT ARE ILLUMINATED AND C/N TURN OFF WHEN ACFT IS ON BATTERY POWER ONLY. T/S AND FOUND POWER SUPPLIES PS2 AND PS6 INOP. REMOVED AND REPLACED PS2 AND PS6. REF-8MM 33-51-00. OPS CHECK.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 50,720 hrs · 56,028 cycles

EMERGENCY FLOOR PATH LIGHT BURNED OUT. REMOVED AND REPLACE BULB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,304 hrs · 55,583 cycles

OVERHEAD EMERGENCY EXIT SIGN AT ROW 1 HAS SEVERAL LIGHT INOP. REMOVED AND REPLACED LIGHT BULB.

Part: UNKNOWN — ODOR (CABIN) · airframe 50,279 hrs · 55,555 cycles

ELECTRICAL BURNING SMELL WHEN APU BLEED IS ON AROUND MIDDLE CABIN AREA. INSPECTED OVERHEAD AND SIDEWALL LIGHTS NO BURNS OR ANY DEFECTS NOTED FROM MIDDLE TO AFT CABIN (SHORT SIGNED BY 9452). GROUND RAN AIRCRAFT OPERATED ENGINES AND AUXILIARY POWER UNIT BLEEDS, CHECKED AIR CYCLE MACHINE OIL LEVEL ALL CHECKED GOOD. SMELL DISSIPATED, OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,231 hrs · 55,499 cycles

CABIN FLOOR EMERGENCY LIGHT BULB AT ROW 4 RIGHT IS BURNT OUT. RELAMPED BULB IAW 33-52-00, OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,231 hrs · 55,499 cycles

CABIN EMERGENCY FLOOR PATH LIGHT IS INOP, MOST FWD. REMOVED AND REPLACED EMERGENCY FLOOR PATH LIGHT, MOST FWD.

Part: UNKNOWN — MALFUNCTIONED (NR 2 PROPELLER) · airframe 50,143 hrs · 55,397 cycles

NR 2 PROPELLER WENT TO 1232 RPM, TORQUE 90 PERCENT AFTER TAKEOFF APPROX 300 FT. PULLED BACK ON CONDITION LEVERS AND PROPELLER REACTED NORMALLY FOR THE REMAINDER OF FLIGHT. PERFORMED BETA LOCKOUT WITH PARKING BRAKE INHIBIT SYS, OPS CK GOOD. AT THIS TIME NO DEFECTS NOTED IN ACCORDANCE WITH AIRCRAFT MAINTENANCE OPS MANUAL.

Part: WINDSCREEN — CRACKED (COCKPIT) · airframe 49,552 hrs · 54,719 cycles

FIRST OFFICES FRONT WINDSCREEN CRACKED, ARCHING AT THE INNER HEATER ELEMENT. REMOVED AND REPLACED FIRST OFFICERS WINDSHIELD REF MM 56-10-11, OPS CHECK GOOD.

Part: WIRE — BROKEN (CABIN)

EMERGENCY LIGHT AT ROW 1F IS INOP. REPAIRED BROKEN WIRES AT RT FWD EMERGENCY DOOR LIGHT. OPS CHECK GOOD. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,834 hrs · 52,794 cycles

OVERHEAD CENTER AISLE E-EXIT SIGN ROW 4 INOP ON FORWARD SIDE. REMOVED AND REPLACED BATTERY PACK NR 6, OPS CHECK GOOD I.A.W. 33-51-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,834 hrs · 52,794 cycles

OVERHEAD CENTER AISLE E-EXIT SIGN ROW 4 INOP ON FORWARD SIDE. REMOVED AND REPLACED BATTERY PACK NR 6, OPS CHECK GOOD IAW 33-51-01.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,121 hrs · 52,038 cycles

FIRST RED LIGHT ON FLOOR INOP. REMOVED AND REPLACED THE MODULE, OPS CHECK GOOD.

Part: ODOR — DETECTED (CABIN LIGHTS) · airframe 43,785 hrs · 48,486 cycles

ELECTRICAL SMELL FROM APU BLEED. CABIN INTERIOR LIGHTING FOUND TO BE CAUSE OF SMELL. DEACTIVATED ROW 4A AND 5A LIGHTS.

Part: TAPE — PEELING (ZONE 400) · airframe 41,972 hrs · 46,533 cycles

RETURN TO FIELD DUE TO NOISE FROM LEFT PROP. FOUND EROSION TAPE PEELING OFF BLADE.

Part: MANIFOLD — BROKEN (NLG STEERING) · airframe 41,820 hrs · 46,374 cycles

STEERING MANIFOLD RETURN OUTLET AND COMPENSATOR ASSY PLATE HAS THREE SHEARED BOLTS. REMOVED AND REPLACED STEERING MANIFOLD.

Part: HEATER — INOPERATIVE (WINDSHIELD) · airframe 40,364 hrs · 44,805 cycles

LEFT WINDSHIELD HOT CAUTION LIGHT ILLUMINATED IN FLIGHT (COOL TO THE TOUCH). A/C DIVERTED TO MDT RATHER THAN LANDING ELM, BECAUSE IT WAS SNOWING THERE. REMOVED AND REPLACED WINDSCREEN HEAT CONTROLLER.

Part: DOOR — OUT OF ADJUST (NLG) · airframe 38,303 hrs · 42,519 cycles

NLG DOOR AMBER C/L ILLUMINATED AFTER GEAR RETRACTED, ADJUSTED NOSE GEAR DOOR PROXIMITY SWITCH IAW AC MM PERFORMED PSEU. GROUND OPS CHECK, OPS CHECK GOOD.

Part: CONTROL BOX — DEFECTIVE (EMERGENCY LIGHT) · airframe 36,575 hrs · 40,704 cycles

EMERGENCY LIGHTS COMES ON AND REMAINS ON IN FLIGHT. REPLACED EMERGENCY LIGHT CONTROL BOX.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,559 hrs · 40,688 cycles

DURING 40K INSPECTION FRAME LEG WAS FOUND WITH CORROSION AT STATION X510 AND BETWEEN STR 32S AND STR 31S. A NEW FRAME WAS SPLICED IN AS PER EO 8-53-03-0782.

Part: HARNESS — FAILED (CABIN)

FIRST THREE WHITE FLOOR EMERGENCY LIGHTS INOP. INSPECTED EMERGENCY LIGHT AND FOUND BROKEN WIRE AT LIGHT SOCKET. ALSO, FOUND LOOSE PIN AT 3352 P-1. RE-SECURED PIN, OPS CHECK GOOD.

Part: SIGN — FAILED (PAX DOOR)

PAX EXIT SIGN AND LEFT FWD EGRESS LT OUT. REMOVED AND REPLACED 3351-P1, OPS CHECK GOOD.

Part: RAIL — CORRODED (BS 215)

CORROSION ON RT CENTER FLOORBOARD RAIL AT FRAME 215.00 ON TOP FLANGE .025 DEEP, ON OUTER FLANGE .035 DEEP AND ON INBOARD SIDE OF OUTER FLANGE .016 DEEP. BLENDED CORROSION FROM RAILS.

Part: RIVETS — LOOSE (NR 2 NACELLE)

TWELVE WORKING RIVETS ON INBOARD WALL OF NR 2 NACELLE (ALL RIVETS ON STRAP) AT GROUND POWER CONNECTOR. REPLACED RIVETS.

Part: BATTERY — DISCHARGED (CABIN)

DURING PRE-FLIGHT INSPECTION FOR FLIGHT 3349 DCA - CRW RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK 3351-PS2. (M)

Part: BATTERY — DISCHARGED (CABIN)

PIT/LYH - FLT 3403 - EMERGENCY EXIT LIGHT OVERHEAD CABIN AT ROW 4, OVERHEAD MIDDLE, AND EXTERIOR RIGHT SIDE LIGHTS INOPERABLE. REMOVED AND REPLACED BATTERY 3351-PS4. (X)

Part: TSCU — FAILED (NR 1 ENGINE)

FLT 3050 - TPA-TLH - UPON POWER ADVANCE FOR TAKEOFF, THE NR 2 ENGINE PROPELLER AUTO FEATHERED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 AND NR 2 TORQUE SIGNAL CONDITIONING UNIT (TSCU). (M)

Part: TSCU — FAILED (NR 2 ENGINE)

FLT 3050 - TPA-TLH - UPON POWER ADVANCE FOR TAKEOFF, THE NR 2 ENGINE PROPELLER AUTO FEATHERED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 AND NR 2 TORQUE SIGNAL CONDITIONING UNIT (TSCU). REFERENCE HNAA9797552.

Part: ACTUATOR ROD — OUT OF ADJUST (LT MLG DOOR)

SBY/PHL - FLT 3081 - AFTER TAKEOFF, THE LEFT GEAR DOOR ADVISORY LIGHT REMAINED ON. THE AIRCRAFT RETURNED TO SBY AND LANDED WITHOUT INCIDENT. REMOVED ICE FROM THE GEAR DOOR AND THE GEAR DOOR PROXIMITY SENSOR BRACKET ASSEMBLY. EVALUATION FLIGHT FOUND UNSATISFACTORY. UPON RETURN, ADJUSTED LEFT FORWARD GEAR DOOR ACTUATOR ROD. GEAR SWING OPERATIONAL CHECK GOOD. (X)

Part: RETRACT MECH — OUT OF ADJUST (LANDING GEAR)

ORF\PHF - FLT 71 - AFTER TAKEOFF, LEFT REAR AND CENTER MLG DOORS WILL NOT CLOSE COMPLETELY FOLLOWING GEAR RETRACTION. THE AIRCRAFT CONTINUED ON TO PHF AND LANDED WITHOUT INCIDENT. FOUND GEAR DOORS OUT OF RIG, RIGGED AS REQUIRED. (X)

Part: EEL POWER SUPPLY — FAILED (CABIN)

EWN/CLT - FLT 3207 - DURING PRE-FLIGHT WALK-AROUND, FOUND MID-CABIN OVERHEAD EMERGENCY EXIT LIGHT OUT. REMOVED AND REPLACED 3351-PS4 EMERGENCY LIGHT BATTERY AND POWER SUPPLY. REFERENCE CONTROL NR 95ZZZX4236.

Part: EEL BATTERY — DISCHARGED (CABIN)

EWN/CLT - FLT 3207 - DURING PRE-FLIGHT WALK-AROUND, FOUND MID-CABIN OVERHEAD EMERGENCY EXIT LIGHT OUT. REMOVED AND REPLACED 3351-PS4 EMERGENCY LIGHT BATTERY AND POWER SUPPLY. REFERENCE CONTROL NR 95ZZZX4237.

Part: SELECTOR VALVE — FAILED (LANDING GEAR)

FLT NR 3111 - PHL-LYH - ON APPROACH TO LYH, SELECTED GEAR DOWN AND GEAR FAILED TO EXTEND. THREE UNSAFE LIGHTS WERE ILLUMINATED. THE CREW PERFORMED THE ALTERNATE EXTENSION AND LANDED IN LYH WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE.

Part: SEL VALVE — FAILED (NLG)

FLT 3434 - BWI-CHO - ON TAKEOFF, THE NOSE GEAR DID NOT RETRACT, THE DOORS REMAINED OPEN AND NOSE GEAR REMAINED UNSAFE FOR 20 SECONDS. THE AIRCRAFT CONTINUED ON TO CHO AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE AND THE PROXIMITY SENSOR FOR THE NOSE GEAR DRAG STRUT. (M)

Part: PROX SENSOR — FAILED (NLG)

FLT 3434 - BWI-CHO - ON TAKEOFF, THE NOSE GEAR DID NOT RETRACT, THE DOORS REMAINED OPEN AND NOSE GEAR REMAINED UNSAFE FOR 20 SECONDS. THE AIRCRAFT CONTINUED ON TO CHO AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE AND THE PROXIMITY SENSOR FOR THE NOSE GEAR DRAG STRUT. (M)

Part: PSEU — FAILED (CABIN)

FLT NR 3103 - BWI TO HPN - ON TAKEOFF, NOSE GEAR WOULD NOT RETRACT. CREW CYCLED THE GEAR DOWN, RETURNED TO BWI AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE PROXIMITY SENSING ELECTRONIC UNIT.