N337EN

Part: UNKNOWN — ODOR (CABIN) · airframe 54,380 hrs · 65,596 cycles

ACRID ODOR PRESENT IN CABIN. SEEMS TO BE FROM FORWARD OVERHEAD AIR VENT. INSPECTED THE CENTER CEILING AREA FOR SIGNS OF OVERHEAT. GROUND RAN THE ACFT AND OPERATED THE BLEED SYSTEM AND CYCLED THE INVERTERS. NO DEFECTS OR ODORS PRESENT. OKAY FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,734 hrs · 64,733 cycles

ONE WHITE EMERGENCY FLOOR LIGHT AT ROW 4 IS INOPERATIVE. R & R THE EMERGENCY LIGHT. OPS CHECKED GOOD. OK FOR SERVICE.

Part: COMPUTER — FAILED (NR 2 AHRS) · airframe 53,694 hrs · 64,679 cycles

NR 2 AHRS FAILED INFLIGHT. CREW REPORTED ASSOCIATED SYSTEM FAILURES AS WELL. R & R THE NR 2 AHRS COMPUTER IAW MM 34-20-01. OPS CHECKED GOOD.

Part: ELECTRONIC UNIT — FAILED (PA SYSTEM) · airframe 53,641 hrs · 64,611 cycles

BURNING ODOR IN CABIN AND FLIGHT DECK WITH LOSS OF INTERPHONE. CAPTAIN PULLED THE CIRCUIT BREAKER M1 AS A PRECAUTION. RESET CIRCUIT BREAKERS M1 & J1, AND FOUND ALL PA INTERPHONE LIGHTS ILLUMINATED WITH AN AUDIO POP SOUND OVER ALL SPEAKERS. INSPECTED WIRING AT BOTH F/A STATIONS, PA AMPLIFIER & PA ELECTRICAL UNIT WITH NO DEFECTS NOTED. FOUND BURNED ODOR COMING FROM PA ELECTRICAL UNIT. R & R THE PA ELECTRICAL UNIT, OPS CHECKED GOOD IAW 23-30-02. OK FOR SERVICE.

Part: INDICATOR — INOPERATIVE (HYD PRESSURE) · airframe 53,541 hrs · 64,480 cycles

NR 1 MAIN HYD PRESSURE INDICATOR READS 0 WITH NO ASSOCIATED ADVISORY LIGHTS ILLUMINATED. R & R THE NR 1 HYD PRESSURE INDICATOR, GROUND RAN THE ACFT. OPS CHECKED GOOD. OK FOR SERVICE.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,513 hrs · 64,440 cycles

RED FLOOR EMERGENCY LIGHT FROM FRONT IS INOPERATIVE. INSTALLED A NEW EMERGENCY LIGHT. IAW AMM 20-45-07. OPS CHECKED GOOD.

Part: PROPELLER — MALFUNCTIONED

WHEN PROPELLER LEVERS AT MAX FOR LANDING, RPM SPLIT MORE THAN 30 RPM. NR 1 ENGINE 1175 AND NR 2 AT 1120 RPM. GROUND RAN AIRCRAFT IAW GROUND RUN UP MANUAL AT MIN AND MAX POWER ALL PARAMETERS WITHIN LIMITS, OPS CHECKED GOOD, OK FOR SERVICE.

Part: TORQUE SENSOR — MALFUNCTIONED (TE FLAP SYS) · airframe 53,178 hrs · 63,999 cycles

FLAP DRIVE CAUTION LIGHT ILLUMINATED DURING TAXI. R & R THE FLAP DRIVE TORQUE SENSOR IAW W/C 27-50-11Q AND OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,103 hrs · 63,899 cycles

EMERGENCY CEILING LIGHT AT ROW 4 INOPERATIVE. R & R THE EMERGENCY LIGHT.

Part: HOLDER — BURNED (OVERHEAD LIGHT) · airframe 52,776 hrs · 63,486 cycles

SEAT 13AC OVERHEAD BIN LIGHT SMOKE. CABIN OVERHEAD LIGHTS AND CIRCUIT BREAKERS S1,S2 AND R2 DEACTIVATED.COLLARD CIRCUIT BREAKERS. LOWERED BINS AT 12 AND 11AC. REMOVED AND REPLACED BALLAST AND LAMP HOLDER. SPLICED WIRES IAW MM 20-45-07. SECURED BINS, RESET CIRCUIT BREAKERS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,787 hrs · 63,500 cycles

CABIN FLOOR EMERGENCY LIGHT IS INOPERATIVE AT ROW 5. REMOVED AND REPLACED THE BULBS AT ROW 5 CABIN FLOOR EMERGENCY LIGHTS, OPS CHECKED GOOD.

Part: BUTTON — DAMAGED (MASTER CAUTION) · airframe 52,656 hrs · 63,322 cycles

MASTER CAUTION LIGHT MODULE POPPED OUT AND HARD TO GET RESET. REMOVED AND REPLACED MASTER CAUTION PUSH TO RESET.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,054 hrs · 62,539 cycles

EXIT LIGHT IS DIM AT ROW 11AC..... REMOVED AND REPLACED BULB. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,710 hrs · 62,111 cycles

4TH EMERGENCY ESCAPE PATH FLOOR LIGHT FROM FRONT IS INOPERATIVE. LIFTED EMERGENCY ESCAPE PATH FLOOR LIGHTS COVER, R & R BULB ON 4TH LIGHT FROM FRONT REINSTALLED COVER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,710 hrs · 62,111 cycles

MISSING 1 EMERGENCY ESCAPE PATH FLOOR LIGHT 28 INSTEAD OF 29. LIFTED EMERGENCY ESCAPE PATH LIGHT COVERS AND FOUND 1 LIGHT INOPERATIVE AT ROW 11DF. R & R LIGHT BULB, NO LIGHTS WERE MISSING, REINSTALLED COVERS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,569 hrs · 61,914 cycles

EMERGENCY FLOOR LT AT ROW 11 INOPERATIVE. R & R BULB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,530 hrs · 61,865 cycles

MOST FWD EMERGENCY ESCAPE PATCH FLOOR LIGHT, R & R BULB FOR FWD FLOOR PATCH EMERGENCY LIGHT, RESECURED FLOOR TRIM.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 51,019 hrs · 61,201 cycles

FUME ISSUE IN CABIN DURING FLIGHT. FORWARD CABIN AREA BALLAST AT ROW 3 SHOWS BURN MARKS AND SCORCH MARKS IN AREA. LEFT SIDE FORWARD END.

Part: BUSS — MALFUNCTIONED · airframe 50,851 hrs · 60,980 cycles

CLOSE WITH BOTH ENGINES RUNNING, COULD NOT GET SECONDARY BUS TO POWER UP. INSPECTED PDPU, OPS CHECKED GOOD WITH NO DEFECTS AT THIS TIME. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,826 hrs · 60,947 cycles

12TH EMERGENCY LIGHT IS INOPERATIVE. R & R BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,826 hrs · 60,947 cycles

CEILING EMERGENCY LIGHTS ARE INOPERATIVE AT ROW 7. R & R BULBS. OPS CHECKED GOOD.

Part: IGNITER — INOPERATIVE (NR 1 ENGINE) · airframe 50,825 hrs · 60,947 cycles

NR 1 ENGINE HAS NO ITT RISE ON STARTUP. R & R IGNITERS IAW 72-01-20. OPS CHECKED GOOD.

Part: HOSE — DETACHED (DEICE BOOT) · airframe 50,645 hrs · 60,730 cycles

RT WING DEICE BOOT INBD OF NACELLE, INTAKE BOOT AND DEICE BOOT JUST OTBD OF NACELLE DO NOT APPEAR TO BE INFLATING. NO LIGHT INDICATION. RE-ATTACHED DEICE HOSE TO LEADING EDGE 6112DR AND 613AR. GROUND RAN ACFT, DEICE BOOT SYSTEM OPS CHECKED GOOD, OK FOR SERVICE.

Part: PSEU — WARNING LIGHT · airframe 49,900 hrs · 59,741 cycles

ON APPROACH AND LANDING GEAR EXTENDED, NO INDICATIONS ON LANDING GEAR PANEL. CREW FOLLOWED CHECKLIST. VERIFIED MLG DOWN AND AND ALL GEARS DOWN. R & R LANDING GEAR PANEL IAW MM 32-30-05. R & R PSEU IAW MM 32-61-50 AND OPS CHECKED GEAR IAW 32-30-01. OPS CHECKED NOSE STEERING IAW 32-50-00. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,845 hrs · 59,675 cycles

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

Part: PSEU — INOPERATIVE (NLG) · airframe 49,374 hrs · 59,057 cycles

DURING GEAR EXTENSION LANDING GEAR SELECTOR PANEL SHOWED NO INDICATION OF GEAR MOVEMENT OR GEAR DOWN. NOSE HAS NO NOSE WHEEL STEERING DURING TAXI. INSPECTED AND FOUND PSEU INOPERATIVE. R & R PSEU IAW MM 32-61-50. OPS CHECKED GOOD. NO STEERING OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 48,652 hrs · 58,136 cycles

EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE AT 9DF. R & R THE BULB.

Part: CONNECTOR — DIRTY (WOW SENSOR) · airframe 48,350 hrs · 57,757 cycles

WOW CAUTION LIGHT INTERMITTENT DURING TAXI. COMPLIED WITH PSEU SYS TEST WITH NO FAULTS NOTED. RESEATED CONNECTOR FOR NOSE WOW SENSORS, TAXIED ACFT, OPS CHECKED GOOD AT THIS TIME.

Part: RELAY — MALFUNCTIONED (AUTOFEATHER) · airframe 48,266 hrs · 7,646 cycles

REJECTED TAKEOFF. AUTOFEATHER NOT ARMING. RIG CHECKED BOTH ENGINES, MADE ADJUSTMENT TO POWER ROD ON NR 2. ALL DONE IAW WC 76-00-02Q. R & R AUTOFEATHER ARM CONTROL RELAY 6121-K5 IAW STANDARD MAINTENANCE PRACTICES. TRIMMED BOTH ENGINES AND OPS CHECKED AUTO FEATHER. ALL IAW RUN MANUAL. OPS CHECKED GOOD.

Part: CONTROL UNIT — FAILED (AUTOFEATHER) · airframe 48,061 hrs · 57,370 cycles

AUTOFEATHER FAILED TO ARM ON TAKEOFF ROLL, 70 KNOTS AT 90 PERCENT TORQUE. R & R NR 2 TSCU IAW P/W MANUAL 72-01-10. GROUND RAN ACFT, OPS CHECKED GOOD IAW P/W RUN UP MANUAL.

Part: WIRE — CHAFED (FMS) · airframe 47,827 hrs · 57,067 cycles

FLIGHT MANAGEMENT SYSTEM, FOUND WIRES CHAFED WITH BARE WIRES SHOWING. REPAIRED WIRES IAW MM 20-45-07FMS. CHECKED GOOD IAW CMM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,074 hrs · 56,045 cycles

TWO FWD RED PATH EMERGENCY LIGHTS ARE INOPERATIVE AT RT SIDE ROW 11. R & R EMERGENCY LIGHT BATTERY IAW MM 33-51-05. OPS CHECKED GOOD.

Part: ADC — FAILED · airframe 46,769 hrs · 55,655 cycles

REJECTED TAKEOFF DUE TO AIR DATA COMPUTER FAILURE ALONG WITH YAW DAMPER FAILED, TAKEOFF WARNING HORN SOUNDING. F/O HSI SELECTED AND NR 2 Y/D. COULD NOT DUPLICATE. CREW REPORTED HSI SELECTED TO RT SIDE. R & R NR 2 DADC IAW MM 34-12-01. OPS CHECKED GOOD.

Part: BLEED VALVE — INOPERATIVE · airframe 46,766 hrs · 55,647 cycles

DURING START, NR 1 ENGINE CAUTION LIGHT ILLUMINATED AFTER PROPELLER SELECTED TO MINIMUM. AFTER NR 1 ECU RESET, IT IS ABOUT 120 DEGREES WARMER THAN NR 2 ENGINE WITH EITHER NR 1 A/C GEN OR NR 1 BLEED SELECTED OFF, TEMP RETURNS TO NORMAL INTERMITTENLY. CYCLED BETA LOCK OUT CIRCUIT BREAKERS. GROUND RAN ACFT AND FOUND NR 2 HP BLEED VALVE INOPERATIVE. R & R HP BLEED VALVE IAW MM 21-11-16. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 46,480 hrs · 55,305 cycles

FLOOR EMERGENCY LIGHTS REMAINED ON, CYCLED SWITCHES, F/A AND FLIGHT DECK AND CYCLED CIRCUIT BREAKER C-3 AND L-2. SYSTEM OPS CHECKED NORMALLY. PERFORMED OPS CHECK OF EMERGENCY LIGHT SYS IAW WC 33-50-03Q. OPS CHECKED GOOD.

Part: STROBE — INOPERATIVE (TAIL) · airframe 46,372 hrs · 55,167 cycles

TAIL STROBE LIGHT INOP DUE TO LIGHTNING STRIKE. R & R TAIL STROBE, RT LIGHT IAW WC 33-00-01. OPS CHECKED GOOD.

Part: GENERATOR — FAILED (NR 2) · airframe 46,372 hrs · 55,167 cycles

AFTER LIGHTNING STRIKE, NR 2 DC GENERATOR STOPPED WORKING AND WOULD NOT RESET. PERFORMED WC 23-60-01F AS REQUIRED IAW WC 23-60-01F. COMPLETED ALL STEPS ON WC 05-50-31I. INSPECTION FOR REPORTED LIGHTNING STRIKE.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 46,359 hrs · 55,150 cycles

NR 1 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED DURING FLIGHT. QTY DROPPED TO BETWEEN .5 AND 1 QUART. R & R NR 1 ENGINE DRIVEN HYD PUMP IAW WC 29-00-00R AND CASE DRAIN FILTER WAS ALSO R & R IAW MM 29-10-20. GROUND RAN ACFT. OPS AND LEAKED CHECKED GOOD.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 46,169 hrs · 54,907 cycles

NR 2 HYDRAULIC QTY WENT FROM 3 TO 2 QUARTS DURING TAXI. FOUND STEADY DRIP FROM B-NUT ON SPOILER LIFT DUMP VALVE. TIGHTENED B-NUT AND SERVICED HYDRAULIC SYS. GROUND RAN ACFT. NO LEAKS NOTED. OK FOR SERVICE.

Part: SWITCH — OUT OF ADJUST (POWER LEVER) · airframe 45,743 hrs · 54,362 cycles

BETA WARNING HORN SOUNDED AFTER TAKEOFF AT APPROX 50 FT, EXTINGUISHED AT 50 FT DURING LANDING. INSPECTED POWER LEVER TRIGGER SWITCH. FOUND TOO TIGHT. ADJUSTED. COMPLETED OPS TEST IAW AMM 31-51-02. OPS CHECKED GOOD.

Part: STIFFENER — CORRODED (BS 624-642) · corrosion level 2 · airframe 45,043 hrs · 53,450 cycles

LOWER BAG BAY DOOR CUTOUT IS CORRODED. R & R WEB STIFFENER IN BAG BAY CUTOUT AREA IAW AMM 20-14-01 AND SRM 51-40-10.

Part: SEAT TRACK — CORRODED (BS 588-660) · corrosion level 2 · airframe 45,043 hrs · 53,450 cycles

LEFT INBD SEAT TRACK IS CORRODED IN CARGO UNDERFLOOR. R & R SEAT TRACK IN FORWARD CARGO UNDERFLOOR IAW SRM 51-42-05 AND RD 8-51-102.

Part: BRACKET — CRACKED (BS 63) · airframe 45,043 hrs · 53,450 cycles

BRACKET IS CRACKED IN COCKPIT AT BS 63.800 AND Z 144. R & R BRACKET WITH NEW IAW SRM 51-42-45 AND 51-40-10.

Part: PANEL — CORRODED (LT WING) · airframe 45,043 hrs · 53,450 cycles

CORROSION ON LT WING LADDER PLATE PANEL 523AT. INSPECTED LADDER PLATE WITH HFEC. NO DEFECTS NOTED. BLENDED AREA OF LT LADDER PLATE IAW EA 15-2013-260 AND EO8-57-13-0331.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 45,043 hrs · 53,450 cycles

CENTER CABIN UNDERFLOOR FLANGE SUPPORT CRACKED. FLANGE SUPPORT WAS R & R WITH NEW ON LT AND RT INBD SEAT TRACK IAW SRM 31-42-05 AND SRM 51-42-45.

Part: SEAT TRACK — CORRODED (BS 109-190) · corrosion level 2 · airframe 45,043 hrs · 53,450 cycles

LT INBD SEAT TRACK IS CORRODED AT FORWARD CABIN UNDERFLOOR. R & R LT FWD SEAT TRACK IAW SRM 51-42-05, RD8-53-3403 AND RD8-53-4473.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 45,043 hrs · 53,450 cycles

CRACK SUSPECTED ON RT FWD CLOSING ANGLE. SEALED RT FWD CLOSING ANGLE IAW RD8-53-2959 WHICH ALLOWS CONTINUOUS OPERATION UNTIL ANGLE REPLACEMENT.

Part: THRESHOLD — CORRODED (BS 149-180) · airframe 45,043 hrs · 53,450 cycles

PAX DOOR THRESHOLD IS CORRODED. R & R THRESHOLD MEMBER IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (BS 588-660) · corrosion level 2 · airframe 45,043 hrs · 53,450 cycles

LT FWD SEAT TRACK IS CORRODED IN CARGO UNDERFLOOR. R & R FWD INBD SEAT TRACK IN CARGO AREA IAW SRM 51-42-05 AND RD8-53-4472.

Part: MFC — FAILED (NR 2) · airframe 45,043 hrs · 53,450 cycles

NR 2 ENGINE FAILED TO MAKE TAKEOFF POWER. ONLY 70 PERCENT TORQUE WITH POWER LEVER COMPLETELY FORWARD. R & R NR 2 MFC IAW WC 76-00-02Q AND 73-00-01R. OPS AND LEAKED CHECKED GOOD.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 45,013 hrs · 53,411 cycles

LEFT ENGINE HAD CORROSION UNDER ENGINE MOUNT. BLENDED FORWARD MOUNT IAW MM 72-10-00. ALODINE AREA IAW 72-00-00, PAGE 809.

Part: SEAT TRACK — CORRODED (BS 109-190) · corrosion level 2 · airframe 45,013 hrs · 53,411 cycles

FORWARD LT SEAT TRACK IS CORRODED BETWEEN BS 109 TO 190. R & R LT FORWARD SEAT TRACK IAW RD8-53-3403.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 44,667 hrs · 52,904 cycles

EMERGENCY FLOOR PATH LIGHT AT ROW 2DF IS INOPERATIVE. REPAIRED BROKEN SPLICE IAW STANDARD WIRING PRACTICE. OPS CHECKED GOOD. RESECURED PATH LIGHT.

Part: BEARING — FAILED (NLG) · airframe 44,394 hrs · 52,611 cycles

LOUD NOISE COMING FROM NLG AREA DURING TAXI. REMOVED NOSE AXLE AND NOSE WHEEL ASSY DUE TO BEARING FAILURE. AXLE SN UNKNOWN.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,392 hrs · 52,610 cycles

SIDEWALL EMERGENCY EXIT SIGN DIM AT PAX DOOR AND ROW 11AC. R & R BULBS IN SIDEWALL EMERGENCY EXIT SIGN BY PAX DOOR AND ROW 11AC.

Part: BULB — FAILED (EMERGENCY LIGHTS) · airframe 43,805 hrs · 51,845 cycles

THIRD FLOOR EMERGENCY LIGHT (RED) IS INOPERATIVE. REMOVED CLEAR COVER, REMOVED RED LENS. R & R BULB, REINSTALLED RED LENS AND CLEAR COVER. OPS CHECKED GOOD.

Part: STRUT — OUT OF ADJUST (PAX DOOR) · airframe 43,609 hrs · 51,598 cycles

PAX DOOR WARNING LIGHT ILLUMINATED AT 10,000 FT. DEPRESSURIZED AND LIGHT WENT OUT. ADJUSTED DOOR LOCK STRUT IAW AMM 53-10-00. PERFORMED WC 55-00-03F AND PRESSURIZED. NO DEFECTS NOTED.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 43,251 hrs · 51,133 cycles

EMERGENCY FLOOR TRACK LIGHT IS OUT AT ROW 9DF. R & R BULB FOR EMERGENCY FLOOR LIGHT AT ROW 9DF. INSTALLED TRACK. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,238 hrs · 51,115 cycles

STRONG OIL ODOR DETECTED DURING TAXI. CHECKED ENGINE, APU AND ACM OIL LEVELS AND CHECKED FOR LEAKS. NONE DETECTED. GROUND RAN ACFT USING ENGINE AND APU BLEEDS. NO ODOR NOTED AT THIS TIME. OK FOR SERVICE.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 43,053 hrs · 50,863 cycles

NOSE GEAR FAILED TO RETRACT AFTER TAKEOFF. NOSE GEAR RED INTRANSIT LIGHT ILLUMINATED. CREW PERFORMED NOSE GEAR ALTERNATE EXTENSION. GEAR INDICATED DOWN AND LOCKED. MX JACKED AND CYCLED LANDING GEAR SEVERAL TIMES. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 42,896 hrs · 50,660 cycles

EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 13. R & R BULB. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 42,661 hrs · 50,361 cycles

TWO EMERGENCY EXIT SIDEWALL SIGN BULBS INOPERATIVE IN ROW 11AC. R & R EMERGENCY EXIT SIDEWALL SIGN BULBS AS REQUIRED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 42,587 hrs · 50,275 cycles

EMERGENCY FLOOR PATH LIGHT IS INOP AT ROW 3DF. R & R EMERGENCY FLOOR PATH LIGHT LAMP AT ROW 3DF. OPS CHECKED GOOD.

Part: LAMP — FAILED (LIGHT SWITCH) · airframe 42,337 hrs · 49,973 cycles

EMERGENCY LIGHT SWITCH DOES NOT TURN GREEN IN NORMAL POSITION. R & R F/A EMERGENCY LIGHT SWITCH LAMP AND CLOSED ACCESS PANEL.

Part: FIREWALL — CHAFED (NACELLE) · airframe 42,079 hrs · 49,653 cycles

REPAIR DOUBLER ON INBD SIDE OF FIREWALL IS CHAFED. REMOVED DOUBLER, FABRICATE NEW DOUBLER AND INSTALLED NEW IAW RD8-54-08 / EO8-54-12-0049.

Part: ACTUATOR — CRACKED (NR 2 PROPELLER) · airframe 42,079 hrs · 49,653 cycles

NR 2 PROP ACTUATOR CRACKED ON FACE NEAR THE TRANSFER TUBE PORT. R & R PROP ACTUATOR IAW WC 61-00-09R.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 49,079 hrs · 49,653 cycles

FLOOR EMERGENCY PATH LIGHT AT ROW 6 IS INOPERATIVE. REMOVED LENS, R & R BULB AT SAID LOCATION, REINSTALLED LENS. OPS CHECKED GOOD.

Part: FIREWALL — CHAFED (NR 1 NACELLE) · airframe 42,079 hrs · 49,653 cycles

NR 1 ENGINE FIRWALL CHAFED THRU AT THE 9 O`CLOCK POSITION AT THE EDGE WHERE IT MEETS AIRFRAME STRUCTURE. R & R FIREWALL.

Part: STRUT — DAMAGED (NR 2 NACELLE) · airframe 42,079 hrs · 49,653 cycles

NR 2 NACELLE LOWER OTBD ENGINE SUPPORT STRUT IS DAMAGED MIDWAY DOWN ON THE TUBE MEARSURING LENGTH 0.0467, WIDTH 0.553, DEPTH 0.029. REMOVED SUPPORT STRUT.

Part: SUPPORT — DAMAGED (NR 1 NACELLE) · airframe 42,079 hrs · 49,653 cycles

NR 1 INBD LOWER NACELLE SUPPORT TUBE HAS DAMAGE BEYOND LIMITS. 22" IN FROM KNUCKLE END. R & R STRUT.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 42,072 hrs · 50 cycles

EMERGENCY EXIT SIGN AT AIRSTAIR DOOR HAS BULB INOPERATIVE. RELAMPED EMERGENCY EXIT SIGN AT AIRSTAIR DOOR AS REQUIRED. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHTS) · airframe 42,056 hrs · 49,631 cycles

EMERGENCY FLOOR PATH LIGHTS ARE INOP AT ROW 1, ROW 5 AND ROW 7. R & R BULBS AT ROW 1, ROW 5 AND ROW 7.

Part: BRAKE ASSY — SMOKE (NR 1) · airframe 41,672 hrs · 49,155 cycles

NR 1 BRAKE HAS EXCESSIVE SMOKING ON LANDING AND AT THE GATE. INSPECTED NR1 BRAKE ASSY WITH NO LEAKS NOTED. BRAKE WEAR WAS IN LIMITS. TAXI ACFT WITH BRAKE ACTION GOOD. OK FOR SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 41,635 hrs · 49,111 cycles

EMERGENCY EXIT SIGN AT FLOOR BY AIRSTAIR DOOR HAS A BULB INOPERATIVE. R & R BULB IN EMERGENCY SIGN AT FLOOR BY AIRSTAIR DOOR. OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (WINDSHIELD HEAT) · airframe 41,403 hrs · 48,901 cycles

F/O WINDSHIELD DOES NOT HEAT IN NORM. DOES SHOW LOAD IN WARMUP. R & R COPILOTS'S WINDSHIELD HEAT CONTROLLER.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 41,452 hrs · 48,892 cycles

26TH EMERGENCY FLOOR LIGHT INOP. R & R LAMP MODULE IAW AMM 33-51-00.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 41,372 hrs · 48,796 cycles

ROW 12 EMERGENCY FLOOR PATH LIGHT INOP. FOUND DAMAGED WIRES. SPLICED IN NEW LIGHT ASSY AT ROW 12 EMERGENCY FLOOR PATH LIGHT. OPS CHECKED GOOD.

Part: GENERATOR — FAILED (NR 1) · airframe 41,132 hrs · 48,502 cycles

NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED IN FLIGHT, RESET AND RE-ILLUMINATED. R & R NR 1 AC GENERATOR AND NR1 AC GENERATOR CONTROL UNIT IAW WORK-CARD 24-20-11R. GROUND RAN NR1 ENGINE, OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 40,711 hrs · 47,953 cycles

ELECTRIC SMELL IN CABIN AT ROW 3 AND 4. CABIN INTERIOR NORMAL LIGHTING SYS PERFORMED HIDDEN DAMAGE INSP. NO DEFECTS NOTED. DEACTIVATED OVERHEAD LIGHTS IAW SP 33-1. PULLED AND COLLARD CBS S1/S2/R2 ON THE RT MAIN.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 40,474 hrs · 47,634 cycles

EMERGENCY FLOOR PATH LIGHT AT ROW 11DF IS RED, SHOULD HAVE AN ARROW. R & R FLOOR PATH LIGHT LENS. NEW LENS HAS AN ARROW POINTING TO EMERGENCY EXIT.

Part: LIGHT — MISSING (CABIN) · airframe 40,087 hrs · 47,158 cycles

AFT EMERGENCY PATH LIGHT MISSING. FOUND LIGHT UNDER FLOOR PANEL. INSTALLED EMERGENCY PATH LIGHT IAW AMM 33-51-03.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,080 hrs · 47,149 cycles

SMALL SPOT OF CORROSION UNDER LAV SERVICE DOOR ON AFT FRAME. REMOVED CORROSION AND RESTORED SURFACE PROTECTION IAW -8-300 SRM 51-20-11.

Part: NUT PLATE — CORRODED (DOOR) · airframe 40,080 hrs · 47,149 cycles

CORROSION ON NUTPLATE ON AIRSTAIR DOOR OUTER SKIN. REMOVED CORROSION AND TREATED AREA ON AIRSTAIR DOOR OUTER SKIN NUTPLATE IAW -8-300 SRM 51-20-11.

Part: PLATE — CRACKED (RT WING) · airframe 40,080 hrs · 47,149 cycles

LADDER PLATE CRACKED AT RT WING STATION YW139.00. CRACKED SECTION OF LADDER PLATE, CUT AND REMOVED AS REQUIRED. WORK DONE IAW RD8-57-2375. EDDY CURRENT AND ULTRASONIC INSP, REQUIRED ON CUTOUT LOCATION, NO CRACKS NOTED, NO DEBOND DETECTED IAW RD 8-57-2375.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 40,080 hrs · 47,149 cycles

PAX DOOR SUPPORT CABLE HARDWARE CORRODED. R & R PAX DOOR SUPPORT CABLE HARDWARE IAW -8-300 AMM 52-10-00.

Part: ATTACH ANGLE — CORRODED (DOOR) · airframe 40,080 hrs · 47,149 cycles

AIRSTAIR DOOR HAS CORRODED ATTACH ANGLES ON BOTTOM SIDE. R & R 3 CORRODED ATTACH ANGLES ON AIRSTAIR DOOR IAW -8-300 AMM52-10-00.

Part: PANEL — CORRODED (WING) · airframe 40,080 hrs · 47,149 cycles

CORROSION FOUND ON PANEL 623AT AND WING LADDER PLATE. REMOVED CORROSION FROM PANEL 623AT AND WING LADDER PLATE. BOTH ARE FOUND TO BE WITHIN LIMITS IAW -8-300 SRM CHAPTER 57-00-16. ALODINE IAW CHAPTER 51-20-16.

Part: PANEL — CORRODED (WING) · airframe 40,080 hrs · 47,149 cycles

CORROSION FOUND ON PANEL 523AT AND WING LADDER PLATE. REMOVED CORROSION FROM PANEL 523AT AND WING LADDER PLATE IAW RD8-57-455. NDT IAW RD8-57-455. NO CRACKS NOTED.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 40,080 hrs · 47,149 cycles

HORIZ STABILIZER LT AND RT INBD L/E HAS CORRODED HARDWARE. R & R HORIZONTAL STABILIZER RT AND LT INBD L/E HARDWARE IAW -8300 SERIES, AMM 55-10-05.

Part: HINGE BRACKET — CORRODED (RT AILERON) · airframe 40,080 hrs · 47,149 cycles

RT OTBD AILERON HINGE BRACKET HAS CORRODED HARDWARE. R & R CORRODED HARDWARE AT RT OTBD AILERON HINGE BRACKET IAW -8-300 AMM 27-12-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,080 hrs · 47,149 cycles

CORROSION FOUND ON BAGGAGE COMPARTMENT FLOOR FRAMES AT STATION X622.00, Z99.00. REMOVED CORROSION IN CARGO BAY ON FLOOR FRAMES AT STATION X622.00 AND Z99.00, FRAME. BOTH FRAMES ARE FOUND TO BE WITHIN LIMITS IAW DASH 8-300 SRM CHAPTER 51-20-36 AND CORROSION REMOVAL IAW CPCM CHAPTER 4, ALODINE IAW SRM CHAPTER 51-20-16, PRIMED IAW 51-20-36.

Part: WEB — CORRODED (FUSELAGE) · airframe 40,080 hrs · 47,149 cycles

SURFACE CORROSION ON CARGO DOOR ENTRANCE WEB AT FLOOR LEVEL. REMOVED CORROSION IN CARGO BAY AT DOOR ENTRANCE WEB FLOOR LEVEL IAW -8-300 CPCM CHAPTER 4, PRIMED AND ALODINED IAW SRM 51-20-16.

Part: SEAT TRACK — CORRODED (BS 129-149) · airframe 40,080 hrs · 47,149 cycles

RT INBD SEAT RAIL HAS CORROSION AT STA X129.75 TO X149.00. CORROSION BLENDED OUT AS REQUIRED, MATERIAL STILL WITHIN LIMITS. SURFACE ALIDINED AND PRIMED AS REQUIRED AND ALL WORK DONE IAW -8-300 RD8-53-4698,SRM 51-20-11, 51-20-16, 51-20-36.

Part: PANEL — CORRODED (RT AILERON) · airframe 40,080 hrs · 47,149 cycles

RT AILERON PANEL 643ER HAS DAMAGE OR CORRODED HARDWARE. R & R CORRODED HARDWARE FOR PANEL 643ER IAW 8-300 AMM06-40-10.

Part: SCREW — CORRODED · airframe 40,080 hrs · 47,149 cycles

LT NOSE COMPARTMENT HAS CORRODED SCREWS AT STATION X7 TO X34,Z112.0. R & R LT NOSE COMPARTMENT HARDWARE AT STA X7 TO X24 IAW -8-300 AMM 20-00-00.

Part: PANEL — CORRODED (AILERON) · airframe 40,080 hrs · 47,149 cycles

AILERON PANEL 643AR RT HAS CORRODED HARDWARE. R & R DAMAGED HARDWARE ON RT AILERON PANEL 643AR IAW -8300 AMM 20-00-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,079 hrs · 47,148 cycles

ROW 11 AC EMERGENCY LIGHT HAS 1 INOP BULB. REMOVED COVER, REMOVED INOP BULB, INSTALLED NEW BULB, INSTALLED COVER.

Part: BRAKE ASSY — WORN (MLG) · airframe 39,907 hrs · 46,916 cycles

F/A REPORTED RT GEAR SMOKING DURING TAXI. INSPECTED NR 3 AND NR 4 BRAKE ASSY. NO LEAKS NOTED. SUSPECT RESIDUAL HYD FLUID FROM PREVIOUS BRAKE CHANGE NR 3 POSITION. CLEANED AS REQUIRED. GROUND TAXI ACFT AND NO LEAKS NOTED OR SMOKE NOTED DURING TAXI AT THIS TIME.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 39,673 hrs · 46,604 cycles

EMERGENCY FLOOR PATH LIGHTS ARE INOP AT ROW 1 AND 7. R & R BURNED OUT BULBS AT 1 AND 7.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,270 hrs · 46,096 cycles

EMERGENCY EXIT SIGN LT OF PAX DOOR HAS INOP LAMP. R & R EMERGENCY EXIT SIGN ON LT SIDE OF PAX DOOR, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,169 hrs · 44,718 cycles

3 CEILING EMERGENCY LIGHT BULBS IN OP ON ROW 11. R & R BULBS IAW 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,169 hrs · 44,718 cycles

FLOOR EMERGENCY LIGHTS ARE IN OP AT ROWS 2 AND 4. R & R BULBS IAW 33-51-03.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 37,741 hrs · 44,188 cycles

EMERGENCY LIGHTS REMAIN ON WHEN SELECTED OFF. SLAVED IN EMERGENCY LIGHT CONTROL BOX, NO FIX. RECONNECTED ORIGINAL BOX. RESEATED CONNECTOR ON BOTH POWER SUPPLIES IN CLOSET AND CONNECTOR 9811-P45. OPS CHECK IN ACCORDANCE WITH 33-51-05.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 37,686 hrs · 44,124 cycles

FLOOR EMERGENCY LIGHT LENSE COVER CRACKED AT ROW 1. R & R FLOOR EMERGENCY LIGHT LENSE COVER WITH NEW. CLEARED MEL.

Part: LINK — DAMAGED (NLG STEERING) · airframe 371,667 hrs · 43,490 cycles

SUSPECT NOSE WHEEL STEERING WENT BEYOND 60 DEGREE LIMIT. REMOVED AND REPLACED STEERING LINKS AND TOWING FUSE IAW 35-50-31. NOSE STEERING FUNCTION CHECK AND NOSE GEAR RETRACTION/ EXTENSION CHECK REQUIRED DUE TO STEERING LINKS AND FUSE ASSY REMOVAL AND REPLACEMENT.

Part: SOCKET — DAMAGED (CABIN LIGHTS) · airframe 36,842 hrs · 43,088 cycles

F/A REPORTS BURNED ODOR AT APPROX SEAT 4A. REMOVED AND REPLACED CABIN LIGHT LAMP HOLDER ABOVE SEAT 4A AND SECURED WITH RETAINING HARDWARE, OPS CHECK GOOD.

Part: PUMP — WEAK (NR 1 ENGINE) · airframe 34,526 hrs · 40,817 cycles

NR 1 ENG WILL NOT GO ABOVE 86 PERCENT TRQ ON TAKEOFF. REMOVED AND REINSTALLED ORIGINAL MFC S/N C31224V, REMOVED AND REPLACED FUEL PUMP IAW 73-00-01R S/N 2170.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 36,242 hrs · 42,335 cycles

DURING TAKEOFF ROLL, NR 1 TORQUE SURGED ABOUT 110 PERCENT AND DROPPED TO 64 PERCENT, REJECTED TAKEOFF. RETRIMMED ENGINES IAW MFG MAINTENANCE RUN UP MANUAL. GROUND RAN AND PERFORMED HIGH SPEED TAXI GOOD. OK FOR SERVICE AT THIS TIME, CLEARED MEL.

Part: TERMINAL — ARCED (WINDSCREEN) · airframe 35,245 hrs · 41,034 cycles

DURING CRUISE, THE FLIGHT CREW SAW THE WINDSCREEN TERMINAL CONNECTIONS BEGIN TO ARC AND THROW SPARKS, THEN THE WINDSCREEN CRACKED. THE SYSTEM WAS TURNED OFF, AND THE FLIGHT CONTINUED ON TO DESTINATION. NO EMERGENCY WAS DECLARED. UPON LANDING, MX FOUND THE WINDSCREEN TO BE INTERNALLY SHORTED. THE WINDSCREEN WAS REPLACED AND OPS CHECKED GOOD. THE ACFT WAS THEN RELEASED FOR SERVICE.

Part: KNOB — OUT OF POSITION (OUTFLOW VALVE) · airframe 35,167 hrs · 40,938 cycles

CLIMBING OUT TO 14,000 FT ALTITUDE, ACFT CREW COULD NOT CONTROL CABIN PRESSURE IN MANUAL MODE ON THE PRESSURE CONTROL PANEL AND THE MASTER CAUTION WARNING LIGHT ILLUMINATED. A LOUD AIRFLOW NOISE WAS HEARD FROM BEHIND THE INSTRUMENT PANEL. THE CREW ELECTED TO RETURN TO THE AIRFIELD. UPON INVESTIGATION IT WAS DISCOVERED THAT THE MANUAL CONTROL KNOB FOR THE FWD OUTFLOW VALVE WAS NOT IN THE CLOSED POSITION. AN EVALUATION FLIGHT WAS REQUESTED AND WAS SUCCESSFUL. THE ACFT WAS THEN RELEASED FOR SERVICE.

Part: SENSOR — FAILED (COCKPIT)

WHEN FLIGHT CREW POWERED ACFT UP FOR PRE-FLIGHT CHECKS, A NOISE WAS HEARD BEHIND THE CAPTAINS SEAT AND AN ODOR OF RUBBER WAS DETECTED. MX FOUND THE ZONE TEMP SENSOR FAN BEHIND CAPTAINS SEAT TO BE THE SOURCE OF THE ODOR. SYSTEM WAS DEACTIVATED AT THAT TIME. WHEN ACFT REACHED A MX BASE, THE TEMP SENSOR UNIT WAS CHANGED. OPS CHECKS WERE GOOD AND SYSTEM WAS REACTIVATED. ACFT WAS THEN RELEASED FOR SERVICE.

Part: PSEU — MALFUNCTIONED (WARNING HORN)

ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN. MAINTENANCE COMPLIED WITH TAKEOFF WARNING WORK CARD. CHECK GOOD WITH NO FAULTS. MAINTENANCE REPLACED THE PSEU AS A POSITIVE MAINTENANCE ACTION. (S)

Part: WARNING HORN — FALSE ACTIVATION

ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN SOUNDED. RECONFIGURED TRIM AND FLAPS, RESET CB 4A FOR TAKEOFF WARNING HORN. NO HORN SOUNDED. (S)

Part: ACM — MALFUNCTIONED

CABIN HOT PACK CAUTION LIGHT ILLUMINATED ON TAXI OUT. MAINT REPLACED REAR AIR CYCLE MACHINE. OPS CHECK GOOD. (K)

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 33,726 hrs · 39,129 cycles

LOSS OF NR 2 HYD FLUID AFTER GEAR EXTENSION FOLLOWED BY ISO VALVE & OUTBOARD SPOILER HYD CAUTION LIGHTS. NR 2 HYD SYSTEM QTY AT .5 QTS. INSTALLED TFL FROM DOOR CONTROL SOLENOID TO UNION IN FRONT OF NOSE GRAVEL GUARD IAW SPECIAL PROCEDURES 20.1 SERVICED NR 2 HYD SYSTEM IAW MAINT MANUAL 12-10-29. OPS & LEAK CHECK GOOD. PLACED ON 70 HR DMT WC 20-50-52T. REF SAME LOG PAGE SEQ NR 1.

Part: GCU — INTERMITTENT (NR 2) · airframe 33,337 hrs · 38,665 cycles

AFTER TAKEOFF EMERGENCY LIGHTS IN CABIN, ENGINE INTAKE HEAT (BOTH LEFT AND RIGHT OPEN AND HEATER) AND PROP SYNC ADVISORY LIGHTS FLICKERED INTERMITTENTLY UNTIL EMERGENCY LIGHTS WERE SELECTED OFF. REPLACED NR 2 GCU, ADVISORY LIGHTS DIM AND TEST BOX AND F/A'S EMERGENCY LIGHT SWITCH.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 33,211 hrs · 38,507 cycles

BAG BAY SMOKE WARNING LIGHT ILLUMINATED INTERMITTENTLY AFTER TAKEOFF. REPLACED NR 1 AND NR 2 SMOKE DETECTORS, OPS CK'D GOOD AT THIS TIME.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 33,064 hrs · 38,328 cycles

A HEAVY CHEMICAL SMELL IN CABIN DURING FINAL PHASE OF FLIGHT WAS NOTICED. REMOVED AND REPLACED THE LEAKING SECTION OF HYDRAULIC LINE FOR LANDING GEAR DOWN SELECT UNDER THE CABIN FLOOR AT FORWARD EMERGENCY EXIT. LEAK CHECK GOOD.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 32,726 hrs · 37,931 cycles

CABIN EMERGENCY LIGHTS CYCLING ON AND OFF IN FLIGHT. PROP HEAT WAS SELECTED ON AT THE TIME. GROUND RAN AIRCRAFT WITH PROP HEAT ON AND OFF, NO DEFECTS NOTED. COULD NOT DUPLICATE CONDITION. NO FURTHER REPORTS OF EMERGENCY LIGHTS CYCLING ON AND OFF REPORTED SINCE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,595 hrs · 37,771 cycles

TWO ADJACENT FLOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. THE BATTERY PACKS WERE SLAVED IN FOR PS1 AND PS2 IN THE COAT CLOSET. THIS DID NOT FIX THE PROBLEM. SO THE ORIGINALS BATTERY PACKS WERE REINSTALLED. NEXT THE PS2 BASE WAS SLAVED IN AND THAT DID NOT FIX THE PROBLEM EITHER. THE ORIGINAL BASE WAS REINSTALLED. THE EMERGENCY BATTERY POWER SUPPLY 3352-PS2 AT ROW 3D WAS REMOVED AND REPLACED. OPS CHECK GOOD.

Part: PLATE — CORRODED (RT WING) · corrosion level 2 · airframe 31,265 hrs · 36,208 cycles

CORROSION FOUND ON BOTH LADDER PLATES AND ACCESS PANEL 523AT AND 623AT. CORROSION, ON LADDER PLATES AND PANELS 523AT AND 623AT. REMOVED AND PROTECTED IAW RD 8-57-0469, RD 8-57-0455 AND RD8-57-3617. HFEC CHECK, NO CRACKS FOUND. MAINTENANCE PROGRAM TO BE AMENDED IAW RD8-57-3617.

Part: EEC — FAILED (NR 2 ENGINE) · airframe 30,874 hrs · 35,737 cycles

CLIMBING TO 500 FEET NR 2 ENGINE TORQUE FLUXED 70 TO 90 PERCENT SUSPECT BETA LOCKOUT, MEL'D USING 61-4. AT RON MAINTENANCE REMOVED AND REPLACED EEC, TSCU, REMOVED AND REPLACED THE BETA SWITCH 6141-S4. RIGGED SWITCH AND TRIMMED ENGINE.

Part: BETA LOCKOUT — MALFUNCTIONED (NR 2) · airframe 30,874 hrs · 35,737 cycles

CLIMBING AT 500 FT, NR 2 ENGINE TORQUE FLUXED 20 TO 90 PERCENT, SUSPECT BETA LOCKOUT. RESET BETA LOCKOUT CIRCUIT BREAKER GROUND RAN ENGINE, NO DEFECTS NOTED.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 1 AND 2) · airframe 30,163 hrs · 34,859 cycles

AFTER CLIMBOUT RUDDER PRESSURE RUDDER FULL PRESSURE AND NR 2 RUDDER HYDRAULIC CAUTION LIGHTS ILLUMINATED AND EXTINGUISHED AFTER 30 SECONDS. BLED NR 1 AND NR 2 HYDRAULIC SYSTEMS AS REQUIRED.

Part: REGULATOR — MALFUNCTIONED (RUDDER PRESSURE) · airframe 30,163 hrs · 34,859 cycles

ON CLIMB OUT RUDDER FULL PRESSURE AND RUDDER PRESSURE CAUTION LIGHTS ILLUMINATED AND EXTINGUISHED CAME ON FOR APROXIMATELY ONE MINUTE MORE AND EXTINGUISHED AGAIN. REPLACED RUDDER DUAL PRESSURE REGULATOR PART INFORMATION TO FOLLOW.

Part: BETA LOCKOUT — FAILED (NR 2 ENGINE) · airframe 28,214 hrs · 32,406 cycles

ON CLIMB OUT THE NR 2 ENGINE BETA LOCKOUT FAILED ASSOCIATED WITH NR 2 TORQUE FLUCTUATING BETWEEN 70 TO 105 PERCENT. POWER REDUCED TO 900 RPM AND ENGINE STABILIZED. DEACTIVATED BETA LOCKOUT SYSTEM IAW. MEL PROCEDURES. REPLACED MICRO SWITCH 6141-S4.

Part: BETA SWITCH — OUT OF RIG (NR 2) · airframe 25,628 hrs · 29,184 cycles

AFTER TAKEOFF, NR 2 ENGINE HAD BATE LOCKOUT FAILURE ASSOCIATED WITH THE NR 2 ENGINE TORQUE FLUX MAX TORQUE AT 100 PERCENT RETARDED NR 2 POWER LEVER TO 900 RPM SYSTEM RETURNED TO NORMAL. PHL MNT IS GOING OUT TO A/C TO DEACTIVATE BETA LOCKOUT SYSTEM. CAPT DID NOT DECLARE AN EMERGENCY. A/C NOT BACK TO GATE UNTIL 11:05 CHECKED RIGGING AND OPERATION OF NR 2 BETA BACK UP SWITCH 6141-S4 THROUGH PIN P AND Y AT 9811 P38, NO DEFECT NOTED FOUND SWITCH 6141 S4 DUSTY AND STICKY CLEANED SWITCH REACTIVATED BETA LOCKOUT PERFORMED BETA LOCKOUT GROUND LOGIC OPS CHECK W/C 61-20-10.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 25,474 hrs · 28,979 cycles

DURING C CHECK INSPECTION, NUMEROUS MINOR DENTS WERE FOUND IN THE SAME SKIN BAY. THIS WAS REPAIRED BY TRIMMING OUT THE DAMAGE AND INSTALLING AN EXTERNAL REPAIR DOUBLER. THIS IS A MAJOR REPAIR.

Part: ENGINE — OUT OF RIG (NR 2) · airframe 25,109 hrs · 28,525 cycles

AFTER TAKEOFF NR 2 ENGINE SURGED, POSSIBLE BETA LOCKOUT FAILURE. OPERATED PROP AT 900 RPM AND SURGE DISSIPATED. DEACTIVATED BETA LOCKOUT SYSTEM. RIGGED NR 2 ENGINE PER W/C 76-00-02Q REACTIVATED BETA LOCK OUT C/W W/C 61-20-10Q BETA LOGIC OPS CHECK BETA LOCKOUT AND PROP GOVERNOR OPS CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 24,129 hrs · 27,324 cycles

CAPT'S LEFT WINDOW (SIDE) CRACKED IN FLIGHT R & R CAPT'S SIDE WINDOW, OPS CHECK GOOD

Part: FUEL CONTROL — MALFUNCTIONED (ZONE 400) · airframe 22,511 hrs · 25,397 cycles

ON CLIMBOUT, NR 1 ENGINE TORQUE DROPPED TO 45 PERCENT. REPLACED MFC.

Part: ANTENNA — BROKEN (COMMS) · airframe 21,756 hrs · 24,417 cycles

CREW REPORTED VIBRATION DURING CLIMBOUT, WITH INCREASING INTENSITY. AIRCRAFT RETURNED TO FIELD. FOUND PORTION OF LOWER COMM ANTENNA MISSING. REPLACED ANTENNA.