N327EN

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 49,845 hrs · 72,348 cycles

ON GEAR EXTENSION, THE NLG RED UNSAFE LIGHT & AMBER GEAR DOOR LIGHT. CREW TRIED TWICE. LOWERED GEAR WITH THE ALTERNATE EXTENSION, RECEIVED 3 GREEN LIGHTS. OPEN

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 49,699 hrs · 72,179 cycles

FWD MOST FLOOR EMERGENCY LIGHT HAS A BROKEN WIRE. REPAIRED THE WIRE IAW AMM 20-45-07.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 49,436 hrs · 71,841 cycles

EMERGENCY LIGHTS ILLUMINATE IN ARM POSITION. PERFORMED AN EMERGENCY LIGHTS OPS CHECK IAW 33-51-05. R & R THE EMERGENCY LIGHTS CONTROL BOX AS PRECAUTION IAW 33-51-05 OPS CHECKED GOOD. OK FOR SERVICE AND CLEANED AND RESEATED EMERGENCY LIGHTS CONTROL BOX. NO FIX.

Part: HOSE — LEAKING (PARKING BRAKE) · airframe 49,178 hrs · 71,496 cycles

PARK BRAKE HYD LEAK. R & R NR 1 MWA BRAKE FLEX HOSE. LEAK AND OPS CHECKED GOOD. OK FOR SERVICE.

Part: RELAY — MALFUNCTIONED · airframe 48,440 hrs · 70,536 cycles

UTO FX DID NOT ARM ON TAKEOFF ROLL WITH TQ UP TO 90 PERCENT. R & R THE NR 2 ENGINE TSEU AND ARM CONTROL RELAY. GROUND RAN ACFT IAW RUNUP MANUAL, OPS CHECKED GOOD. OKAY FOR SERVICE.

Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 48,411 hrs · 70,501 cycles

AUTOFEATHER DID NOT ARM DURING TAKE OFF ROLL. TORQUE WAS UP TO 90 PERCENT. INSPECTED FOR DEFECTS, NONE NOTED. PERFORMED ENGINE RUNS, SYSTEM OPS CHECKED GOOD IAW MX RUNUP MANUAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,011 hrs · 69,973 cycles

FORWARD MOST FLOOR EMERGENCY LIGHT INOPERATIVE. R & R THE BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,884 hrs · 69,816 cycles

12TH EMERGENCY FLOOR LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD.

Part: CIRCUIT CARD — FAILED (AUTOPILOT) · airframe 47,684 hrs · 69,548 cycles

AUTOPILOT DISENGAGE CAUTION LIGHT WILL NOT RESET AFTER DC BUSS FAULT DURING ENGINE START. R & R THE AUTOPILOT DISENGAGE PANEL CIRCUIT CARD ASSEMBLY ON PILOT SIDE. OPS CHECKED GOOD IAW MM 22-10-01 AND WDM 22-10-10.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,414 hrs · 69,186 cycles

FORWARD MOST RED EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,142 hrs · 68,835 cycles

LEFT AFT EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.

Part: CONTROL BOX — MALFUNCTIONED (SMOKE WARNING) · airframe 45,497 hrs · 68,001 cycles

WHEN PERFORMING BAG BAY SMOKE DETECTOR TEST WARNING LIGHTS DID NOT EXTINGUISH AFTER TEST. R & R WARNING LIGHT CONTROL BOX IAW -8 MM 26-12-00, OPS CHECK OK, OK FOR SERVICE.

Part: TIRE — FAILED (MLG) · airframe 46,490 hrs · 67,993 cycles

CAPT SIDE INBD TIRE POPPED ON TAXI OUT. R & R NR 1 AND NR 2 MWA'S IAW AMM 32-41-11 AS REQUIRED. OK FOR SERVCICE.

Part: LINE — BENT (APU) · airframe 46,287 hrs · 67,725 cycles

JET FUEL ODOR IN CABIN. AFTER MAINTENANCE INSPECTION, FOUND OIL RESIDUE ON RECIRC FAN AND ADJACENT DUCT WORK. AUXILIARY POWER UNIT. FOUND TEFLON CONNECTOR HOSE ON APU OIL DRAIN LINE ABOVE RECIRC FAN TO BE BENT IN A BLOCKED POSITION. REMOVED HOSE AND REPOSITIONED ADEL CLAMP ON RIGID LINE. INSTALLED NEW TEFLON HOSE. RAN APU, OPS AND LK CHECKS GOOD. CLEAR MEL.

Part: LIGHT — BROKEN (CABIN) · airframe 45,580 hrs · 66,803 cycles

LOWER ENTRY WAY EMERGENCY EXIT LIGHT IS MISSING SHIELD AND LIGHT ASSEMBLY IS BROKEN AT THE SCREWS. R & R LOWER ENTRY WAY EMERGENCY LIGHT AND INSTALLED NEW BACK SHIELD ONTO ASSEMBLY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,313 hrs · 66,446 cycles

EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 3 AND 9. R & R BULB, OPS CHECKED GOOD.

Part: TRANSCEIVER — MALFUNCTIONED (RADAR) · airframe 44,634 hrs · 65,554 cycles

EGPWS PERFORMED AN UNCOMMANDED TEST CYCLE AT BEGINNING OF TAKEOFF ROLL. R & R RADAR RT. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,443 hrs · 65,299 cycles

AFT CENTER AISLE AND RT AFT EGRESS LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PS6 IAW MM 33-51-00. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,443 hrs · 65,299 cycles

LEFT AFT EGRESS LIGHT IS INOPERATIVE. R & R EMERGENCY BATTERY PS7 IAW MM 33-51-00. OPS CHECKED GOOD.

Part: FUEL SYS — LEAKING (RT WING) · airframe 43,659 hrs · 64,278 cycles

NR 2 BLEEDS FUEL ODOR WHEN PROPELLERS ARE IN FEATHER. GROUND RAN ACFT. COULD NOT DUPLICATE. SUSPECT FUEL ODOR IS FROM SEEP FROM RT WING.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,307 hrs · 63,813 cycles

FLOOR EMERGENCY LIGHT IS INOPERATIVE AT ROW 12DF. R & R THE BULB. OPS CHECKED GOOD.

Part: PROPELLER — FAILED (NR 1) · airframe 43,217 hrs · 63,691 cycles

ENROUTE, CREW NOTICED BURNING ODOR. ISOLATED TO NR 1 BLEED. SELECTED BLEEDS OFF, ODOR DISSIPATED. ON GROUND WITH POWER LEVERS ADVANCED AND LP BLEEDS ACTIVATED, ODOR RETURNED. R & R NR 1 PROP ASSEMBLY. OPS CHECKED GOOD.

Part: PROPELLER — FAILED (NR 1) · airframe 43,206 hrs · 63,678 cycles

NR 1 PROPELLER VIBRATION, RETURN TO FIELD. OIL LEAKING ON GROUND. CREW REPORTED BLADE NOT STRAIGHT. R & R THE NR 1 PROPELLER

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,605 hrs · 62,885 cycles

EMERGENCY EXIT SIGN LIGHTS ARE INOPERATIVE ON UPPER HALF. R & R BULBS IN EMERGENCY EXIT SIGNS UPPER HALF. OPS CHECKED GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 42,390 hrs · 62,615 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT IS DIM. R & R BULB, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,390 hrs

EMERGENCY CEILING LIGHT IS INOPERATIVE AT ROW 13, ROW 9 AND ROW 1. R & R BULBS. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,330 hrs · 62,537 cycles

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

Part: LINE — LEAKING (HYD SYSTEM) · airframe 42,237 hrs · 62,420 cycles

WITH NR 2 ENGINE RUNNING AT FLT IDLE AND START FEATHER BLEEDS ON IN AUTO SET AT MAX AFTER 3-4 MINS STRONG ODOR IN MID TO AFT CABIN. PAX COMPLAINED AND DEPLANED ACFT. INSPECTED AND FOUND HYD LEAK AT NOSE GEAR DOWN LINE IN CABIN. CAPPED AND PLUGGED LINE OUTSIDE OF PRESSURE VESSEL BEHIND LARGE ARM PIT PANEL. R & R NLG DOWN LINE AND ASSOCIATED FITTINGS IAW STD MNT PRACTICES AND RING LOCK KIT PROCEDURES, OPS & LK CHECK GOOD.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 42,066 hrs · 62,204 cycles

LOWER SIDEWALL EMERGENCY LIGHT IS DIM AT ROW 11DF. R & R BULBS IN LOWER SIDEWALL EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,648 hrs · 61,677 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,304 hrs · 61,264 cycles

RIGHT SIDE, REAR FUSELAGE EMERGENCY LIGHT IS DIM. R & R BULB. OP CHECKED GOOD.

Part: LONGERON — CRACKED (NACELLE) · airframe 41,135 hrs · 61,040 cycles

UPPER INBD LEFT LONGERON IS CRACKED ON OUTER RADIUS. REPAIRED DAMAGE IAW EO8-54-13-0664.

Part: ACTUATOR — FAILED · airframe 40,827 hrs · 60,653 cycles

BETA WARNING HORN SOUNDED AFTER TAKEOFF AT APPROX 50 FT AND SOUNDED CONTINUOUSLY UNTIL 50 FT ON APPROACH. R & R BAD ROLLER ACTUATOR AT SWITCH IAW MM 31-51-02 AND MM 76-10-13. RESET CIRCUIT BREAKER C8. OPS CHECKED GOOD.

Part: WARNING HORN — ACTIVATED · airframe 40,549 hrs · 60,289 cycles

TAKEOFF WARNING SOUNDED DURING TAKEOFF ROLL. CONFIGURED ACFT SETTING, NO FIX. GROUND RAN ACFT AND CYCLED ALL RELATED ITEMS. COULD NOT DUPLICATE AT THIS TIME.

Part: RADAR — MALFUNCTIONED (WX SYS) · airframe 40,271 hrs · 59,945 cycles

ACT WEATHER RADAR DISPLAYS RED DURING TURNS AND SPIKES IN LEVEL FLIGHT. R & R RADAR RT. OPS CHECKED GOOD. OK FOR SERVICE.

Part: WINDSHIELD — DAMAGED (COCKPIT) · airframe 40,005 hrs · 59,608 cycles

F/O WINDSHIELD TERMINAL HAD SMOKE WITH WINDSHIELD HEAT APPLIED. R & R F/O WINDSHIELD IAW 56-00-00R. OPS AND LEAKED CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,910 hrs · 59,483 cycles

RED EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE AT ROW 11D. REPLACED BULB AT ROW 11D IAW AMM. OPS CHECKED GOOD.

Part: BRACKET — BROKEN (RT WING) · airframe 39,910 hrs · 59,496 cycles

RT WING, FRONT SPAR, LOWER SPAR CAP BRACKET FOUND BROKEN. R & R BRACKET IAW SRM 51-42-10.

Part: PLATE — CRACKED (WING) · airframe 39,910 hrs · 59,496 cycles

LADDER PLATE FOUND CRACKED UNDER STRESS PANEL 622AT. CUTOUT DAMAGE IAW RD8-57-2387 AND FABRICATED NEW PART IAW RD8-57-2387. HFEC INSPECTION DONE ON REPAIRED AREA. NO DEFECTS NOTED.

Part: STRINGER — CORRODED (BS 107) · corrosion level 2 · airframe 39,910 hrs · 59,496 cycles

CORROSION FOUND UNDER STRINGER 31P AT BS 107. R & R STRINGER IAW RD8-53-1243 AND EO8-53-13-0264.

Part: FRAME — CRACKED (BS 251 S32-33R) · airframe 39,910 hrs · 59,496 cycles

CRACK FOUND ON FRAME IN CABIN UNDERFLOOR AT BS 251, BETWEEN S33-32S. REPAIRED IAW RD8-53-4811. COMPLIED WITH HFEC INSPECTION. NO OTHER DEFECTS FOUND.

Part: FLAP TRACK — RUSTED (NR 2 FLAP) · airframe 39,910 hrs · 59,496 cycles

RT WING FLAP TRACK NR 2 MATING SURFACE IS RUSTED. R & R NR 2 FLAP TRACK IAW MM 57-50-26.

Part: SEAT TRACK — CORRODED (BS 196-607) · airframe 39,910 hrs · 59,496 cycles

CORROSION FOUND ON LT AND RT OTBD SEAT TRACK AT BS 196 - 607. BLENDED LT AND RT OTBD SEAT TRACK IAW RD8-53-8319 & RD8-53-3644.

Part: CARGO TRACK — CORRODED (BS 588-660) · airframe 39,910 hrs · 59,496 cycles

CORROSION FOUND ON CARGO TRACK INBD SIDE FROM BS 588 - 660. BLENDED CORROSION, HFEC INSPECTION COMPLIED WITH. NO DEFECTS FOUND.

Part: FLOOR SUPPORT — CORRODED (BS 543-572) · airframe 39,910 hrs · 59,496 cycles

SURFACE CORROSION FOUND UNDERFLOOR BETWEEN BS 543 - 572, S31-33S. BLENDED SURFACE IAW SRM 51-00-16.

Part: HINGE — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 39,911 hrs · 59,496 cycles

RT INBD ELEVATOR ARM ASSY BEARING BORE IS CORRODED. R & R RT INBD ELEVATOR HINGE ARM ASSEMBLY IAW SRM 51-40-10, SRM 51-42-05 AND SRM 51-42-45.

Part: HINGE — CORRODED (RUDDER) · airframe 39,910 hrs · 59,496 cycles

FORE RUDDER MIDDLE HINGE, LOWER FITTING BEARING RACE IS CORRODED. BLENDED LOWER FITTING BEARING BORE MAIN HINGE FITTING IAW EO8-55-13-0228.

Part: FLAP TRACK — RUSTED (NR 3 FLAP) · airframe 39,910 hrs · 59,496 cycles

LT NR 3 FLAP TRACK MATING SURFACE IS RUSTED. R & R FLAP TRACK IAW AMM 57-50-26.

Part: ANGLE — CORRODED (SERVICE DOORWAY) · corrosion level 2 · airframe 39,910 hrs · 59,496 cycles

AFT SERVICE DOOR LOWER SILL ANGLE FOUND CORRODED. R & R SERVICE DOOR THRESHOLD PLATE IAW SRM 51-42-05 AND SRM 51-42-45. DIAPHRAGM AND LOWER SILL ANGLE INSTALLED IAW SRM 51-42-05.

Part: FRAME — CORRODED (BS 503) · airframe 39,910 hrs · 59,496 cycles

SURFACE CORROSION AND CRACK FOUND ON FRAME AT BS 503.80, STR 31S. CLEANED CORROSION, REPAIRED FRAME MEMBER. HFEC INSPECTION WAS COMPLIED WITH. NO CRACK FOUND. FRAME REPAIR WAS IAW RD8-53-4811 AND EO8-53-13-0267.

Part: FLAP TRACK — CORRODED (NR 3 FLAP) · airframe 39,910 hrs · 59,496 cycles

RIGHT NR 3 FLAP TRACK MATING SURFACE IS RUSTED. R & R NR 3 RT FLAP TRACK IAW RD8-57-5933 AND MM 57-50-26.

Part: FLAP TRACK — CORRODED (NR 1 FLAP) · airframe 39,910 hrs · 59,496 cycles

LT NR1 FLAP TRACK MATING SURFACE IS RUSTED. R & R NR 1 FLAP TRACK IAW MM 57-50-11.

Part: BRACKET — CRACKED (LT NACELLE) · airframe 39,910 hrs · 59,483 cycles

LEFT ENGINE INBD COWLING GENERATOR INTAKE DUCK BRACKET CRACKED. LEFT ENGINE INBD COWLING GENERATOR INTAKE DUCT BRACKET WELDED IAW RD8-71-969 AND EAO5-2013-019.

Part: SKIN — DAMAGED (RT NACELLE) · airframe 39,910 hrs · 59,483 cycles

RT NACELLE SKIN AT INBD AFT CORNER OF MLG DOOR AFT HINGE ARM. CUTOUT DONE ON RT NACELLE SKIN AT INBD AFT CORNER OF FWD MLG DOOR AFT HINGE ARM IAW RD8-54-892. HFEC INSPECTION DONE ON RT NACELLE SKIN CUTOUT IAW RD8-54-892.

Part: CONTROL CABLE — FRAYED (AILERONS) · airframe 39,910 hrs · 59,483 cycles

AILERON CABLE FOUND UNSERVICEABLE ON LT WING T/E, ONLY ONE STRAND WAS REMAINING. OPEN

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 39,894 hrs · 59,466 cycles

INOP EMERGENCY PATH FLOOR LIGHT AT ROW 12. FOUND LAMP ASSY WIRES BROKEN. R & R LAMP ASSY AND SPLICED WIRES ONE AT A TIME IAW STANDARD PRACTICES. OPS CK GOOD, SECURED LENS COVER.

Part: WIRE — SHORTED (PSU) · airframe 39,433 hrs · 58,882 cycles

WITH OVERHEAD AND SIDEWALL LIGHTS OFF. PSU AT ROW 3DF FLICKERING WITH ELECTRICAL ODOR. INSPECTED AREA, FOUND TWO GROUND WIRES DISCONNECTED. CONNECTED WIRES AND R & R PSU AT ROW 3D IAW AMM 25-22-15. OPS CHECKED GOOD. FOUND NO OTHER DEFECTS.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 39,170 hrs · 58,541 cycles

ROW 11, FLOOR EMERGENCY LIGHT IS INOP. REMOVED LENS, REMOVED RED FILTER, R & R BULB. INSTALLED FILTER AND LENS. OPS CHEKCED GOOD.

Part: ELEMENT — ARCED (WINDSHEILD HEAT) · airframe 38,687 hrs · 57,934 cycles

PILOTS SIDE WINDOW HEATING ELEMENT BURNED AND ARCING. R & R CAPTS SIDE WINDOW AND INSPECTED WIRES FOR DAMAGE. NO DAMAGE TO THE WIRING WAS FOUND. OPS AND LEAK CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 38,630 hrs · 57,864 cycles

TWO RED EMERGENCY PATH LIGHTS AT FORWARD EMERGENCY EXIT ARE INOPERATIVE. R & R 2 RED EMERGENCY PATH LIGHT AT FORWARD EMERGENCY EXIT. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 38,592 hrs · 57,812 cycles

EMERGENCY OVERHEAD LIGHT AT ROW 7 IS INOPERATIVE. R & R BULB FOR EMERGENCY OVERHEAD LIGHT AT ROW 7 AND SECURED LENS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,306 hrs · 51,208 cycles

EMERGENCY FLOOR PATH LIGHT INOPERATIVE ROW 1. R AND R EMERGENCY FLOOR PATH LIGHT IN ROW 1, VERY FIRST ONE FORWARD, REPLACED TRACK, OPS CHECKED GOOD.

Part: EEC — FAILED (NR 1 ENGINE) · airframe 38,312 hrs · 57,432 cycles

NR 1 ECU FAILED DURING CLIMBOUT. R & R NR 1 EEC IAW MM 72-01-10. GROUND RAN AIRCRAFT. OPS CHECKED GOOD IAW -8 RUN UP MANUAL.

Part: APU — INOPERATIVE · airframe 38,301 hrs · 57,421 cycles

APU WILL NOT START. APU CAUTION LIGHT ILLUMINATED AND CHECK FIRE DETECT WARNING LIGHTS ILLUMINATED. BOTH LIGHTS EXTINGUISHED WHEN APU PANEL WAS SELECTED OFF. CREW NOTED BOTH DISC ARE STILL ON OUTSIDE OF AIRCRAFT TAIL. INSPECTED APU, NO DAMAGE NOTED, FUEL VALVE VERIFIED CLOSED- PULLED AND COLLARED CIRCUIT BREAKER N8. TROUBLESHOT AND FOUND INTERNAL FAULT IN APU FIRE BOTTLE. R & R FIRE BOTTLE IAW WC 26-21-01I.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,663 hrs · 56,591 cycles

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

Part: STRUCTURE — BROKEN (STATIC WICK) · airframe 37,588 hrs · 56,495 cycles

INBD STATIC WICK BASE HAS WICK BROKEN INSIDE. REMOVED STATIC WICK, INSTALLED NEW STATIC. WICK BASE READS .11 MIL OHMS AND STATIC WICK READS 40 MEGA OHMS.

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 37,588 hrs · 56,495 cycles

STATIC WICK BASE IS OUT OF LIMITS ON RUDDER, SECOND FROM BOTTOM. REMOVED PAINT AND PRIMER FROM BASE, REINSTALLED STATIC WICK AS REQUIRED.

Part: GENERATOR — MALFUNCTIONED (NR 1 DC) · airframe 37,580 hrs · 56,485 cycles

NR 1 DC GENERATOR KICKED OFF LINE. CYCLED AND RESET NR 1 DC GENERATOR, POSSIBLE LIGHTNING STRIKE IN FLIGHT. INSPECTED ACFT IAW AMM 05-50-31. NO LIGHTNING DAMAGE FOUND. GROUND RAN ACFT. ALL SYS CHECKED NORMAL. OK FOR SERVICE.

Part: DADC — FAILED · airframe 37,330 hrs · 56,191 cycles

ON TAKE, MESSAGE ON 802 DADC DATA INVALID MESSAGE ON APPROACH F/O ALT FLAGGED. PERFORMED ALTITUDE CORRELLATION CHECK DUE TO NR 2 DADC REMOVAL AND REPLACEDMENT IAW MM 34-53-01F. ALL ALTITUDE ON WORKCARD CHECKED GOOD FOR NR 2 DADC.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 36,947 hrs · 55,709 cycles

ROW 11DF EMERGENCY LIGHT INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 36,784 hrs · 55,504 cycles

FLOOR EMERGENCY LIGHT INOPERATIVE BETWEEN ROW 9 AND 10. R & R EMERGENCY LIGHT BULB ON FLOOR BETWEEN ROWS 9 AND 10. OPS CHECKED GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 36,804 hrs · 55,528 cycles

FLOOR LEVEL EMERGENCY EXIT SIGN AT PAX DOOR HAS ONE BULB INOPERATIVE. R & R BULB FOR FLOOR LEVEL EMERGENCY EXIT SIGN AT PAX DOOR.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 35,682 hrs · 54,057 cycles

AFTER GEAR RETRACTION, NOSE GEAR DOORS OPENED AND NOSE GEAR PARTICAIALLY EXTENDED AND RETRACTED TWICE WITH ALL ASSOCIATED LIGHTS. JACKED ACFT AND PERFORMED LANDING GEAR, OPS CHECK 3 TIMES. CLEARED PSEU MEMORY. PERFORMED OPS CHECK 3 TIMES. PSEU CODED 55 AND 53 OBSERVED. R & R GEAR SELECTOR HANDLE. R & R PSEU. PERFORMED OPS CHECK 15 TIMES. MEASURED INDUCTANCE AND SERIES RESISTANCE USING BOB OF ALL PROX SENSORS ASSOCIATED WITH DISCREPANCY.

Part: CONNECTOR — BROKEN (CABIN LIGHT) · airframe 35,352 hrs · 53,641 cycles

ELECTRIC ODOR IN CABIN, STRONGEST AT ROW 4-5. FOUND OVERHEAD LIGHT CONNECTORS BROKEN AND MELTED ON RT SIDE OF CABIN AT ROW 3DF. PERFORMED HIDDEN DAMAGE INSP IAW SPECIAL 33.1. NO ADDITIONAL DAMAGE FOUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,208 hrs · 53,470 cycles

ROW 4, EMERGENCY FLOOR PATH LIGHT INOP. R & R ROW 4 EMERGENCY FLOOR PATH LIGHT, OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 35,049 hrs · 53,255 cycles

2ND LAST EMERGENCY FLOOR LIGHT HAS A BROKEN WIRE. R & R EMERGENCY FLOOR LIGHT.

Part: LIGHT — MISSING (CABIN) · airframe 35,049 hrs · 53,255 cycles

EMERGENCY FLOOR LIGHT COUNT 28 MISSING 1 LIGHT SOMEWHERE. 1 AFT FOUND UNDER FLOOR AT ROW 13. SECURED PANEL AND INSTALLED CARPET AND LIGHT COVER.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 39,409 hrs · 46,267 cycles

EMERGENCY FLOOR LIGHT AT ROW 4 INOP. R & R BULB AN ROW 4 EMERGENCY PATH FLOOR LIGHT. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,228 hrs · 52,195 cycles

FLOOR LEVEL EMERGENCY LIGHT AT ROW 2 AND 8 ARE INOP. RELAMPED FLOOR LEVEL EMERGENCY LIGHTS AT ROW 2 AND 8. OPS CHECKED GOOD.

Part: PIPE — LOOSE (BLEED AIR SYS) · airframe 33,427 hrs · 51,200 cycles

BURNING/HOT SMELL IN MID CABIN. REMOVED LT BLEED PIPE FROM WING ROOT TO Y IN CTR OF WING. INSTALLED LT BLEED PIPE FROM WING ROOT TO Y IN CTR OF WING. OPS CKD GOOD. NO SMELL NOTED.

Part: CHECK VALVE — LEAKING (BLEED AIR SYS) · airframe 33,390 hrs · 51,156 cycles

VERY STRONG ODOR IN PASSENGER COMPARTMENT FROM MIDSECTION GOING AFT. FOUND BLEED AIR LEAK AT RT ENGINE CHECK VALVE IN BLEED AIR DUCT. REPLACED GASKETS AT REAR LT CHECK VALVES. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,385 hrs · 51,151 cycles

STRONG ELECTRICAL ODOR TOWARD REAR OF ACFT. REPLACED BULB IN SIDEWALL AT ROW 13AC. INSPECTED SOCKETS WITH NO DEFECTS NOTED. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,901 hrs · 50,561 cycles

EMERGENCY FLOOR PATH LIGHT IS NOT WORKING AT SEAT 2DF. REMOVED AND REPLACED LAMP IAW 33-20-00. CHECKED GOOD.

Part: GARLOCK SEAL — LEAKING (HYD PUMP) · airframe 32,140 hrs · 49,612 cycles

NR 2 ENGINE PRESSURE FLUX BETWEEN 50-55 PSI, THEN WENT TO 35-40 PSI WITH LOW WARNING LIGHT. ENGINE MANUAL SHUTDOWN. OIL PRESSURE NEVER REACHED O PSI RAN ENGINES AT OR BELOW 40 PSI FOR 2 MINUTES. INSPECTED AND FOUND ENG LOW ON OIL. HYD PUMP GARLOC SEAL LEAKING. REMOVED AND REPLACED GARLOC SEAL IAW 72-10-00 AND SERVICED ENGINE OIL. OPS AND LEAK CHECKED GOOD.

Part: WIRE — BROKEN (HYD TRANSMITTER) · airframe 31,298 hrs · 48,582 cycles

NR 2 ENGINE HYD CAUTION LIGHT ILLUMINATED FOR APROX 30 SECONDS THEN EXTINGUISHED FOLLOWED BY NR 2 MAIN HYD PRESSURE GOING TO 0 PSI. FOUND BROKEN WIRE AT TRANSMITTER CONNECTOR PLUG REPAIRED IAW SMP GROUND RAN. OPS CHECK GOOD.

Part: INDICATOR — BROKEN (HYD SYSTEM) · airframe 31,298 hrs · 48,582 cycles

ACFT 327 EN PUSHED OFF FROM THE GATE AND TAXIED TO THE RUNWAY FOR TAKE OFF. AT THAT TIME THE NR 1 HYD PRESSURE INDICATOR WAS READING ZERO PSI. FLIGHT 4645 RETURNED TO THE GATE AND LINE MX WAS CALLED. THE MAIN HYD INDICATOR WAS CHANGED AND THE PROBLEM WAS CORRECTED WITHOUT FURTHER INCIDENT.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 31,131 hrs · 48,375 cycles

NR 1 HYD QUANTY DROPPED TO 1 QUANTY AND ISOLATION VALVE CAUTION LIGHT ILLUMINATED. INSPECT ACFT FOR HYD LEAKS, BELLY, TAIL, UNDER WING, OVER CTR FUSELAGE BOTH NACELLE HYD LINES SERVICED. NR 1 HYD SYS EMPTIED BOTH OVERSPILL CONTAINERS. NO FILTER BYPASS NOTED PRESSURIZED HYDR SYS WITH HYD MULE AND RAN ACFT. NO OBVIOUS HYD LEAKS NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,470 hrs

FWD 2 MID CABIN CEILING LIGHTS ARE INOP. R&R EMERGENCY LIGHT BATTERY AT ROW 3 LT LOCATION IAW 33-51-00. OPS CHECK GOOD.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 30,034 hrs · 46,998 cycles

FLOOR BEAM DAMAGE AT STA X129 BENEATH RT INBD SEAT RAIL ATTACHMENT. PERFORM LIQUID PENETRANT INSPECTION PER EO8-53-08-337 NO DEFECT FOUND. REPAIR DAMAGE PART PER EO8-53-08-337

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,034 hrs · 46,998 cycles

DURING 'C' CHECK INSPECTIONS, A REPAIR WITH NO DOCUMENTATION WAS FOUND ON THE FUSELAGE BELLY SKIN AT X198 BETWEEN STRINGERS 30P AND 32P. THIS PATCH WAS R&R AND NEW DOCUMENTATION ISSUED FOR THIS REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,034 hrs · 46,998 cycles

DURING 'C' CHECK INSPECTIONS, A REPAIR WITH NO DOCUMENTATION WAS FOUND ON THE FORWARD FUSELAGE BELLY SKIN AT X225 TO X230 BETWEEN STRINGERS 28P AND 29P. THE PATCH WAS R&R AND NEW DOCUMENTATION WAS ISSUED FOR THE ACFT.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,034 hrs · 46,998 cycles

DURING 'C' CHECK INSPECTIONS, A REPAIR WITH NO DOCUMENTATION WAS FOUND ON THE FUSELAGE BELLY SKIN AT X210 TO X221 BETWEEN STRINGERS 29P TO 32P. DOCUMENTATION WAS FOUND FOR THIS REPAIR UNDER DHC RD8-53-10353.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 30,034 hrs · 46,998 cycles

2 PROTRUDING DENTS BETWEEN STATION X179-X199 STRINGER 29P-30P. REPAIRED DAMAGE IAW RD8-53-2181.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,034 hrs · 46,998 cycles

DURING 'C' CHECK INSPECTIONS, A REPAIR WITH NO DOCUMENTATION WAS FOUND ON THE FUSELAGE SKIN ON THE FORWARD BELLY AREA, LOCATED AT X231 TO X238 BETWEEN STRINGERS 30P TO 32P. THIS PATCH WAS REPLACED AND NEW DOCUMENTATION ISSUED FOR THE ACFT.

Part: SKIN — CORRODED (RT WING) · airframe 30,034 hrs · 46,998 cycles

CORROSION FOUND ON LOWER SKIN OF THE RT WING BETWEEN STA 130.0 TO 145 AT REAR ON RT WING AT REAR SPAR, LOWER FLAP SHROUD. P/N 85730018-011 R&R IAW STRUCTURAL REPAIR MANUAL 51-40-00.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 30,485 hrs · 47,549 cycles

RT INBD SEAT RAIL CORRODED FROM STATION X 423 TO X 588. FABRICATED LT HAND AND RT IAW DRAWING 85331406. USED ON ALODINE SURFACE IAW ESR 07-07-3003.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 30,034 hrs · 46,998 cycles

PROTRUDING DENT ON LT FUSE STA X444.8, STR 30P - STR 31P. REPAIR DAMAGE IAW EO8-53-08-3363 EDDY CURRENT AND BONT TEST.

Part: ATTACH FITTING — CORRODED (NACELLE) · airframe 30,034 hrs · 46,998 cycles

CORROSION AROUND 1 FASTENER ON THE REAR SPAR ATTACHMENT TO OTBD NACELLE. REPAIR ATTACHMENT TO OTBD NACELLE WITH HI LOCKS IAW STRUCTURAL REPAIR MANUAL 51-40-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 30,034 hrs · 46,998 cycles

PROTRUDING DENT ON BELLY SECTION OF FORWARD FUSELAGE AT STATION X223 BETWEEN STRINGER 32S-33S. REPAIR SKIN IAW RD8-53-2181.

Part: SPAR — CRACKED (LT WING) · airframe 30,034 hrs · 46,998 cycles

SUPECTED CRACK ON LT WING FRONT SPAR AT INBD NACELLE ATTACHMENT TOP CORNER. R&R ANGLE IAW STRUCTURAL REPAIR MANUAL 51-40-00.

Part: CONTROL VALVE — BROKEN (HYD SYSTEM)

NR 1 HYDRAULIC QTY DROPPED TO 1 QUART FOLLOWED BY ISO VALVE CAUTION LIGHT ILLUMINATED. LOST NORMAL BRAKES. R&R NR 2 ANTI-SKID CONTROL VALVE. IAW 32-46-11. LEAK CHECK AND OPS CHECKS GOOD. SERVICED HYDRAULIC SYSTEMS AND RETURNED ACFT TO SERVICE.

Part: SEQUENCE VALVE — INOPERATIVE (NLG)

ON CLIMBOUT NOSE GEAR DOOR ADVISORY LIGHT ILLUMINATED ALONG WITH LOUD NOISE FROM NOSE GEAR AREA. LIGHT WENT OUT AND THEN SAME PROBLEM REOCCURRED. GEAR SELECTED DOWN. PERFORMED LANDING GEAR DOOR SEQ CONTROL CIRCUIT OPS CHECK IAW WC 32-32-15Q. REPLACED NW DOOR SEQ VALVE IAW MM 32-20-36. (S)

Part: RELAY — DEFECTIVE (NLG)

UPON LANDING GEAR RETRACTION NOSE RED UNSAFE LIGHT ILLUMINATED ALONG WITH TRANSIT LIGHT IN HANDLE AND AMBER NOSE GEAR DOOR LIGHTS. NOSE GEAR RETRACTED AND AFTER ABOUT 10 SECONDS THERE WAS A THUMPING NOISE ALONG WITH DOOR AND UNSAFE LIGHTS STILL ILLUMINATING INTERMITTENTLY. REPLACED TIME DELAY RELAY 3261-K11, MM 32-20 RESET PSEU, CYCLED GEAR, OPS CHECK GOOD. (S)

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR SYS)

LOG PAGE 271884, SEQ NR 1- RADAR ONLY PAINTS 2 RED SPOKES. REMOVED AND REPLACED RT IAW 34-41-01. OPS CHECK GOOD. (K)

Part: BALLAST — BURNED (CABIN LIGHTS)

STRONG ELECTRICAL ODOR WHEN OVERHEAD LIGHT SELECTED ON, AT ROWS 9 THRU 11. INSPECTED AND FOUND ODOR COMES FROM ROW 9/10 AC OVERHEAD BULBS. REMOVED BOTH BULBS FROM OVERHEAD LIGHT SOCKETS 9/10 AC. PULLED C/B S2 ON RT C/B PANEL IAW SP 33.1 MEL 31MAY 08 15:47 PHL C15211 33-2 CABIN INTERIOR NORMAL LIGHTING SYSTEM JUN 08 03:42 ROA FOUND SOCKET AFT AT ROW9 AC BURNT AND SMOKED. REPLACED SOCKET AND BALLAST IAW 33-00. OPS CHECK GOOD. CLEARED MEL. (S)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,779 hrs · 45,451 cycles

WHITE LOW LEVEL EMERGENCY LIGHT AT ROW 7 INOP. RELAMPED WHITE LOW LEVEL EMERGENCY LIGHT AT ROW 7, OPS CHECKED GOOD.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 28,667 hrs · 45,315 cycles

ENCOUNTERED LIGHTNING STRIKE, INFLIGHT SYSTEM CHECK GOOD. INSPECTED AIRCRAFT, EVIDENCE OF BURN MARKS ON RIGHT HAND SIDE OF RADOME, WILL FERRY AIRCRAFT TO ROA. REMOVED AND REPLACED RADOME.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 28,122 hrs · 44,651 cycles

ELECTRICAL SMELL IN CABIN, MORE NOTICEABLE AT ROW 7. PERFORMED HIDDEN DAMAGE INSPECTION, FOUND OVERHEAD LIGHT ASSEMBLY AT 7C BURNT. REPLACED LAMP HOLDER BV03300-12-150 AND BALLAST, OPERATIONAL CHECK GOOD.

Part: PSU — HOT (CABIN)

BURNING ODOR AT AFT CABIN, NOTICED BY CREW MEMBERS & AFT F/A CONTROL PANEL APPEARS TO BE HOT TO TOUCH. INSPECTED F/A PANEL NO DEFECT NOTED CREW GROUND RAN AIRCRAFT WITH BLEEDS ON, NO ABNORMAL ODOR NOTED. DEACTIVATED PSU AT 8DF DUE TO INTERMIT CHIM ACTIVATION IAW SPECIAL PROCEDURES 23.3. REMOVED AND REPLACED PSU, OPS CHECK GOOD.

Part: FLEX LINE — LEAKING (HYD SYSTEM)

NR 1 HYD QTY DROPPED TO 1.3, SYSTEM WENT INTO ISO, PRESSURE REMAINED GOOD AND FLUID DRIPPING FROM NR 2 NACELLE. INSTALLED TFL AT RT WING I/B SPOILER ACTUATOR ON REAR SPAR. REF MP&P VOL 2 20.1. LEAK CHECK GOOD. SERVICE HYD SYSTEM.

Part: ENGINE — DAMAGED (NR 1) · airframe 26,311 hrs · 42,436 cycles

AFTER TAKEOFF ON CLIMB OUT AT ABOUT 4 THOUSAND FEET THE NR 2 ENGINE SHUT DOWN. INSPECTED ENGINE AND FOUND TO BE SERVICEABLE. FOUND FOD DAMAGE ON NR 1 ENGINE AND IT WAS REPLACED.

Part: INVERTER — FAILED (ELECTRICAL SYS) · airframe 26,123 hrs · 42,199 cycles

CREW NOTICED SMOKE COMING OUT OF LEFT DC C/B PANEL. TURNED OFF INVERTER AND SMOKE DISSIPATED. REPLACED PRIMARY INVERTER.

Part: ODOR — DETECTED (COCKPIT) · airframe 24,672 hrs · 40,430 cycles

STRONG ELECTRICAL SMELL IN COCKPIT. FOUND ODOR DISSIPATED UPON ARRIVAL TO AIRCRAFT, INSPECTED AVIONICS RACK, AREA BEHIND WARDROBE WALL, UNDER COCKPIT FLOOR AND ABOVE COCKPIT CEILING PANELS FOR SIGNS OF ELECTRICAL PROBLEMS, NO DEFECTS FOUND NO CIRCUIT BREAKERS POPPED. ALL SYSTEMS OPERATED NORMALLY WITH NO ELECTRICAL SMELL. OPERATED APU AND ENGINE BLEEDS, NO ODORS.

Part: TERMINAL BLOCK — OVERHEATED (APU) · airframe 24,672 hrs · 40,430 cycles

SMOKE IN COCKPIT. FOUND APU STARTER GENERATOR CABLES AT AFT SIDE OF FORWARD PRESSURE BULKHEAD OVERHEATED AT TERMINAL BLOCK 24459-TB1. REMOVED AND REPLACED CABLES 2449-7B1 AND 2449-1AL. PART INFORMATION TO FOLLOW

Part: ODOR — DETECTED (CABIN) · airframe 24,672 hrs · 40,430 cycles

STRONG ELECTRICAL ODOR IN COCKPIT. FOUND ODOR DISSIPATED UPON ARRIVAL TO AIRCRAFT, INSPECTED AVIONICS RACK, AREA BEHIND WARDROBE WALL, UNDER COCKPIT FLOOR AND ABOVE COCKPIT CEILING PANELS FOR SIGNS OF ELECTRICAL PROBLEMS. NO DEFECTS FOUND, NO CIRCUIT BREAKERS POPPED. ALL SYSTEMS OPERATED NORMALLY WITH NO ELECTRICAL ODOR. OPERATED APU AND ENGINE BLEEDS, NO ODORS.

Part: SOCKET — BURNED (LIGHT) · airframe 24,531 hrs · 40,256 cycles

ELECTRICAL SMELL IN CABIN. FOUND LIGHT SOCKET AT 2D BURNED. C/W MP&P VOL 2 33.1

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 24,531 hrs · 40,256 cycles

ELECTRICAL SMELL IN CABIN. FOUND SIDEWALL LIGHT 8AC INOP. PERFORMED HIDDEN DAMAGE INSPECTION, NO DISCREPANCIES NOTED.

Part: GENERATOR — FAILED (NR 2) · airframe 23,253 hrs · 38,602 cycles

AT APPROXIMATELY 400 FEET ON DEPARTURE, NR 2 AC GEN CAUTION LIGHT ILLUMINATED. APPROXIMATELY ONE MINUTE LATER THE MASTER WARNING AND NR 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. CONFIRMED OIL PRESSURE WAS AT 0 AND SHUTDOWN ENGINE. REMOVED AND REPLACED AC GENERATOR.

Part: ENGINE — OVERTEMP (NR 2) · airframe 23,107 hrs · 38,414 cycles

NR 2 ENGINE OIL TEMP WENT INTO RED ON TAKEOFF, REDUCED POWER AND STABILIZED IN YELLOW. REMOVED AND REPLACED THE OIL FUEL HEATER.

Part: PSEU — DAMAGED (MLG INDICATOR) · airframe 20,357 hrs · 35,033 cycles

NOSE GEAR AND NOSE GEAR DOOR ADVISORY LIGHT & GEAR UNSAFE LIGHT CYCLED 4 TIMES WHILE AIRBORNE WITH GEAR HANDLE CYCLED UP. INSPECTED NOSE GEAR SENSORS AND PERFORMED NEAR, FAR TEST, NO DEFECTS NOTED. REMOVED AND REPLACED PSEU, SYSTEM TEST. EVALUATION FLIGHT CHECK GOOD.

Part: ACTUATOR — LACK OF LUBE (ELEVATOR TRIM)

UNABLE TO MOVE ELEVATOR TRIM TO NOSE DOWN POSITION IN FLIGHT , OPS NORMAL ON THE GROUND. LUBED ELEVATOR TRIM ACTUATOR AS REQ, OPS CHECK GOOD.

Part: SEAT BELT — LOOSE (CABIN) · airframe 18,560 hrs · 32,880 cycles

SEAT BELT AT 10D CAME LOOSE, INSTALLED SEAT BELT HARDWARE, OPS CHECK GOOD.

Part: CONTROL BOX

Overhead and sidewall emergency lights flickered in flight. R&R of emergency light control box followed by a ground operational check.

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 14,691 hrs · 27,995 cycles

NUMBER 1 HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED, QUANTITY GOOD SYSTEM PRESSURE 3000 PSI WITH STANDBY PUMP OFF. NUMBER 1 SYSTEM FAILED IN FLIGHT, SYSTEM QUANTITY GOOD.

Part: SKIN — DEPARTED (NR 2 PROP) · airframe 13,535 hrs · 26,099 cycles

ON APPROACH AT 200 FEET, CREW AND FLIGHT ATTENDANT HEARD A LOUD BANG FOLLOWED BY AIRFRAME VIBRATION FELT THROUGHOUT THE CABIN AND FLIGHT DECK. FOUND NUMBER TWO PROP, NUMBER ONE BLADE MISSING THE NICKLE SHEATH. REMOVED AND REPLACED PROP BLADE.

Part: HYDRAULIC SYSTEM — OVERSERVICED (NR 2 SYS) · airframe 13,514 hrs · 26,063 cycles

LOSS OF NR 1 HYDRAULIC SYSTEM FLUID IN FLIGHT. NR 1 HYDRAULIC ISO VALVE LIGHT AND ROLL SPOILER INBOARD LIGHT ILLUMINATED. NR 1 HYDRAULIC SYSTEM DID NOT GO TO ZERO. FOUND NR 2 HYDRAULIC SYSTEM OVERSERVICED AND OVERSPILL CONTAINER FULL. INSPECTED FILTERS AND BYPASS INDICATORS, NO DEFECTS NOTED. OPERATED HYDRAULIC SYSTEMS, NO LEAKS OR FLUID LOSS NOTED.