N572SC

Part: DUCT — BROKEN (NR 1 ENGINE)

SF/OGG - FLT 0007 - ON DESCENT, FIRE WARNING ON NR 1 ENGINE. THROTTLE TO IDLE WARNING WENT OUT. HIGH PRESSURE BLEED CONTROL T-DUCT FLANGE AND THRUST REVERSER CROSS-OVER DUCT BROKEN AND LEAKING. REPAIRED BOTH DUCTS. OPERATIONAL CHECK WERE NORMAL. (X)

Part: SLIDE — FAILED (PAX DOOR)

DURING FAA MINI EVACUATION DEMONSTRATION, THE R3 DOOR SLIDE/RAFT FAILED TO DEPLOY FULLY. THE RAFT PORTION OF THIS TWO PART ASSEMBLY IS THE ONLY PART TO FAIL. THE SLIDE PORTION PERFORMED ITS INTENDED FUNCTION. (M)

Part: SLIDE — FAILED (R4 DOOR)

DURING DEPLOYMENT OF THE R4 DOOR SLIDE FOR TRAINING PURPOSES THE SLIDE FAILED TO INFLATE FULLY.

Part: LIGHT — SHORTED (CABIN)

DURING A-LINE CHECK, THE EMERGENCY FLOOR TRACK LIGHTING IN THE AFT MID CABIN AND FORWARD PART OF AFT CABIN WAS FOUND INOPERATIVE. REPAIRED SHORTED WIRING IN TRACK BASE, ALL FLOOR TRACK LIGHTING CHECKS GOOD.

Part: BULKHEAD WEB — CRACKED (BS 595)

DURING SCHEDULED MAINTENANCE, FOUR CRACKS WERE FOUND AT STA 595 LEFT HAND SIDE LONGERON 43 INBOARD OF AREA A REFERENCE NDI MANUAL 531003 FIGURE 1. AREA REPAIRED IN ACCORDNACE WITH DOUGLAS REWORK DRAWING SR105300647001.

Part: COALESCER BAG — CONTAMINATED (NR 1 PACK)

WHILE WARMING THE COCKPIT TEMPERATURE ZONE TWO HAZY FOG POURED IN VENTS THROUGHOUT THE AIRCRAFT. FOUND NUMBER ONE PACK WATER SEPARATOR DIFFERENTIAL PRESSURE INDICATOR POPPED. RESET INDICATOR AND REPLACED WATER SEPARATOR BAG PER MAINTENANCE MANUAL CHAPTER 215100.

Part: BOLT — CRACKED (LT WING)

DURING INSPECTION IN ACCORDANCE WITH AD 96-06-08 AND DC-10 SERVICE BULLETIN 57-126, REV 1, THE BOLT LOCATED IN THE NUMBER 2 POSITION OF THE LEFT WING MILKSTOOL FITTING, (P/N 71658-18-58), WAS FOUND TO HAVE CRACK INDICATIONS. THE BOLT WAS REPLACED WITH (P/N 84779-18-58) IN ACCORDANCE WITH AD 96-06-08 AND DC-10 S/B 57-126, REV 1.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

THE FORWARD CABIN EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED FORWARD CABIN POWER SUPPLY, LIGHTS TESTED GOOD.

Part: OVRHD DECODER — FAILED (CABIN)

PASSENGERS SEATED NEAR SEATS 35 HJK NOTED SMOKE COMING FROM OVERHEAD BINS. REMOVED AND REPLACED OVERHEAD DECODER AT THAT LOCATION, FUNCTIONALLY CHECKED READING AND CALL LIGHTS PER DC-10 MM 23-30-00, OPS CHECKED NORMAL.

Part: SEAT ENCODER — FAILED (CABIN)

THE NUMBER 3 GENERATOR TRIPPED OFF-LINE AND WAS UNABLE REINSTATE USING COM PROCEDURES. SMOKE WAS THEN NOTED IN FORWARD CABIN, AIRCRAFT DIVERTED FOR LANDING. GENERATOR WAS REINSTATED ON APPROACH FOR LANDING. DURING POST FLIGHT INSPECTION, COULD NOT DUPLICATE NUMBER 3 GENERATOR DROPPING OFF-LINE. FOUND FORWARD CABIN SECTION TIMER OVERLOAD LIGHT ON, AND SEAT ENCODER AT SEAT 2E THE CAUSE OF THE SMOKE IN FORWARD CABIN. REMOVED AND REPLACED FORWARD CABIN SECTION TIMER AND SEAT 2E ENCODER. GENERATOR AND MUX SYSTEMS TESTED GOOD PER THE DC-10 MAINTENANCE MANUAL.

Part: SMOKE DETECTOR — FAILED (NR 6 LAV)

THE NUMBER 6 LAVATORY SMOKE DETECTOR WAS FOUND TO GIVE A VERY SLOW ALERT AND NO LAV SMOKE INDICATION WAS RECEIVED IN COCKPIT. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR, DETECTOR OPS CHECKED GOOD.

Part: MODULE PIGTAIL — BROKEN (CABIN)

FOUND EMERGENCY FLOOR TRACK LIGHTING MODULE AND LIGHT RIPPED AT SEAT ROW 15. DISCOVERED PIGTAIL ON LIGHT MODULE BROKEN AND SECTION OF FLOOR TRACK COVER DAMAGED. REPLACED LIGHT MODULE PIGTAIL AND SECTION OF FLOOR TRACK COVER.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS IN AFT CABIN CAME ON WITH SWITCH IN THE OFF POSITION. ALSO, FAILED SELF TEST. REMOVED AND REPLACED OVERWING EMERGENCY POWER SUPPLY IN ACCORDANCE WITH MM 33-51-01 AND FUNCTIONALLY TESTED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS IN MID CABIN CAME ON WITH SWITCH IN OFF POSITION. ALSO, FAILED SELF TEST. REMOVED AND REPLACED MID CABIN EMERGENCY POWER SUPPLY IN ACCORDANCE WITH MM 33-51-01 AND OPS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FOUND OVERWING EMERGENCY EXIT SIGNS INOP DURING LINE CHECK. REMOVED AND REPLACED OVERWING EMERGENCY POWER SUPPLY AND BATTERY PACK IN ACCORDANCE WITH MM 33-50-00 AND FUNCTIONALLY TESTED NORMAL.

Part: OVHD PANEL — ARCING (CABIN)

OVERHEAD PANEL ROWS 25-26 BEGAN ARCING AND FLIGHT ATTENDANT SMELLED SMOKE. INSPECTED OVERHEAD PANELS AT ROWS 25-26 AND ALL COMPONENTS ASSOCIATED WITH PANELS OPERATED FOR SEVERAL HOURS WITH NO DISCREPANCIES NOTED.

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE)

L1 DOOR SLIDE LIGHT WAS FOUND INOP. REMOVED AND REPLACED DOOR SLIDE LIGHT ASSEMBLY AND OPS CHECKED GOOD IN ACCORDANCE WITH MM 25-61-03.

Part: BATTERY PACK — DISCHARGED (CABIN)

AFT CABIN EMERGENCY LIGHT BATTERY POWER SUPPLY FAILED EMERGENCY LIGHT TEST. REMOVED AND REPLACED BATTERY PACK AND OPS CHECKED GOOD IN ACCORDANCE WITH 33-51-01.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND OVERHEAD EMERGENCY LIGHT IN MID CABIN INOP. REMOVED AND REPLACED BATTERY PACK AND OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND MID CABIN OVERHEAD EMERGENCY LIGHTS INOP OVER BOTH AISLES. REMOVED AND REPLACED MID CABIN EMERGENCY LIGHT BATTERY PACK AND OPS CHECKED IN ACCORDANCE WITH MM 33-51-01 PAGE 201.

Part: SCUFF PLATE — DAMAGED (L2 DOOR)

JET BRIDGE CONTACTED AIRCRAFT ON PUSHBACK. INSTALLED TEMPORARY REPAIR ON L2 DOOR SCUFF PLATE. FERRIED TO PHX. REMOVED AND REPLACED L2 FORWARD SCUFF PLATE IN ACCORDANCE WITH MM 53-30-1.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS CHARGE AND STANDBY CIRCUIT BREAKER POPPED IN FLIGHT. REMOVED AND REPLACED LEFT OVERWING BATTERY CHARGER POWER SUPPLY AND OPS CHECKED GOOD IN ACCORDANCE WITH MM 33-50-11.

Part: BATTERY PACK — DISCHARGED (CABIN)

FWD EMERGENCY BATTERY POWER SUPPLY FAILED EMERGENCY LIGHTING SELF TEST. REMOVED AND REPLACED FORWARD POWER SUPPLY BATTERY PACK AND OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FOUND EMERGENCY LIGHT CHARGE AND STANDBY BREAKERS OPEN. REMOVED AND REPLACED LEFT HAND OVERWING BATTERY POWER SUPPLY AND OPS CHECKED GOOD IN ACCORDANCE WITH MM 33-51-01.

Part: LIGHTING — INOPERATIVE (CABIN)

FOUND AFT CABIN TRACK LIGHTING LOOSE AND BROKEN WIRES ON THE RIGHT HAND SIDE. SECURED TRACK, REPAIRED WIRES AND OPS CHECKED IN ACCORDANCE WITH MM 33-50-00.

Part: SPLICE — CORRODED (BS 890)

DURING HEAVY MAINTENANCE, FOUND LONGERON 52 SPLICE CRACKED AND CORRODED AT BS 890. FABRICATED AND INSTALLED NEW SPLICE IN ACCORDANCE WITH SRM 53-10-00.

Part: STIFFENER — CORRODED (BS 475)

DURING HEAVY MAINTENANCE, FOUND CORROSION AT FRAME AND SKIN INTERSECTION AT BS 475 FROM LONGERON 44L TO 44R. REMOVED CORROSION, REMOVED AND REPLACED STIFFENER IN ACCORDANCE WITH SRM 51-21-01, 51-31-01 AND 51-35-01.

Part: SEAT TRACK — CORRODED (CARGO COMPT)

DURING HEAVY MAINTENANCE FOUND AFT CARGO PIT LEFT HAND FORWARD OUTBOARD CARGO TRACK HAS EXFOLIATION CORROSION. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-33-01 AND 53-70-00 FIGURE 2.

Part: SHEAR TIE — CORRODED (BS 1039)

DURING HEAVY MAINTENANCE, FOUND SHEAR TIES LEGS CORRODED AT LONGERON 52, BS 1039. REMOVED CORRODED SHEAR TIES, CLEANED SKIN, FABRICATED AND INSTALLED NEW SHEAR TIES IN ACCORDANCE WITH SRM 53-15-01.

Part: SPLICE — CORRODED (BS 1801-1821)

DURING HEAVY MAINTENANCE, FOUND LONGERON 46R SPLICE CORRODED BETWEEN FRAMES AT BS 1801 THROUGH BS 1821. REMOVED LONGERON SPLICE, FABRICATED AND INSTALLED A NEW SPLICE IN ACCORDANCE WITH SRM 51-33-01.

Part: WEB — CRACKED (BS 1780)

DURING HEAVY MAINTENANCE, FOUND THE LOAD BAR TRACK WEB CRACKED AT BS 1780. STOP DRILLED CRACK, FABRICATED AND INSTALLED A DOUBLER IN ACCORDANCE WITH SRM 53-00-01 FIGURE 4 SHEET 2.

Part: SKIN — CUT (BS 816)

DURING HEAVY MAINTENANCE, FOUND CUT IN FUSELAGE SKIN AT BS 816, BETWEEN LONGERON 50R AND 51R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER AND SKIN FILLER IN ACCORDANCE WITH SRM 53-20-00 FIGURE 13 SHEET 8.

Part: SPOOL BOLT — CORRODED (CARGO DOOR)

DURING HEAVY MAINTENANCE, FOUND CENTER PIT AFT LATCH SPOOL MOUNT HAS CORROSION AT SPOOL MOUNT BOLT INNER SURFACE. REMOVED CORROSION BY OVERSIZING HOLES TO 1.089 DIAMETER. FABRICATED SLEEVE FROM 17-4 AND CADMIUM PLATED IN ACCORDANCE WITH SRM 52-10-00, FIGURE 9.

Part: LONGERON — CORRODED (BS 775-889)

DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND FASTENER HOLES ON LONGERON 51R FROM BS 775 TO BS 889. FABRICATED AND SPLICED IN NEW LONGERON SECTION IN ACCORDANCE WITH SRM 51-30-01.

Part: FRAME — CORRODED (BS 1902)

DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND NUTPLATE HOLES ON FRAME 1902. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLERS IN ACCORDANCE WITH SRM 53-00-01 FIGURE 2.

Part: LONGERON — CORRODED (BS 775-850)

DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND RIVET HOLES ON LONGERON 50L BETWEEN BS 775 AND BS 850. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED A REPAIR SECTION IN ACCORDANCE WITH SRM 53-10-00.

Part: WEDGE — DELAMINATED (RT TE FLAP)

DURING HEAVY MAINTENANCE, FOUND RIGHT INBOARD FLAP TRAILING EDGE WEDGE DELAMINATED. REMOVED PREVIOUS REPAIR AND REPLACED WITH A NEW REPAIR IN ACCORDANCE WITH SRM 57-20-00 PARAGRAPH 2 A (1) (5) USING 151 CLOTH AND ADHESIVE 50A.

Part: INTERCOSTAL — CORRODED (BS 1721-1741)

DURING HEAVY MAINTENANCE, FOUND CORROSION ON WEBS AND AREA AROUND DOME NUTS THAT ATTACH THE ADF ANTENNA BETWEEN LONGERONS 51R AND 52, BS 1721 TO 1741. REMOVED AND REPLACED INTERCOSTAL IN ACCORDANCE WITH SRM 51-31-01.

Part: LONGERON — CORRODED (BS 775/899)

DURING HEAVY MAINTENANCE, FOUND CORROSION ON LONGERON 50 BETWEEN BS 775 AND BS 899. REMOVED CORRODED SECTION OF LONGERON, FABRICATED AND INSTALLED A SPLICED SECTION OF LONGERON IN ACCORDANCE WITH SRM 53-10-00.

Part: LONGERON — CORRODED (BS 775-889)

DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND FASTENER HOLES ON LONGERON 52 BETWEEN BS 775 AND 889. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICES IN ACCORDANCE WITH SRM 51-30-00.

Part: FRAME — CORRODED (BS 1942)

DURING HEAVY MAINTENANCE, FOUND CORROSION ON FRAME 1942 BETWEEN LONGERON 51L AND 49R. REMOVED DAMAGED MATERIAL, FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-00 FIGURE 5.

Part: SUPPORT — CORRODED (BS 735)

DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND FLOORBOARD SUPPORT NUT CLIP HOLES IN LOWER GALLEY, BS 735 LBL 8. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLERS IN ACCORDANCE WITH SRM 53-00-01.

Part: FRAME — CORRODED (BS 899)

DURING HEAVY MAINTENANCE, FOUND CORROSION ON FRAME AT BS 899 BETWEEN LONGERON 51L AND 51R. REMOVED DAMAGED MATERIAL, FABRICATED AND INSTALLED A FRAME CAP IN ACCORDANCE WITH SRM 53-30-00 PAGE 31.

Part: FRAME — CORRODED (BS 1787)

DURING HEAVY MAINTENANCE, FOUND CORROSION ON REINFORCING CHANEL FOR FRAME 1787, BETWEEN LONGERON 50L AND 50R. FABRICATED AND INSTALLED A NEW FRAME CAP IN ACCORDANCE WITH SRM 53-30-00, PAGES 15 AND 16.

Part: FRAME — CORRODED (BS 939)

DURING HEAVY MAINTENANCE, FOUND CORROSION ON FRAME AT BS 939 BETWEEN LONGERON 50L AND 50R. REMOVED DAMAGED MATERIAL, FABRICATED AND INSTALLED A FRAME CAP IN ACCORDANCE WITH SRM 53-30-00.

Part: DOUBLER — CORRODED (BS 1029)

DURING HEAVY MAINTENANCE, FOUND CORROSION ON ANTENNA DOUBLER AT BS 1029 BETWEEN LONGERON 51R AND 52. REMOVED LOWER ANTENNA DOUBLER, FABRICATED AND INSTALLED A NEW DOUBLER IN ACCORDANCE WITH SRM 53-20-00, PAGES 74 TO 84.

Part: SKIN — GOUGED (LT HORIZ STAB)

DURING HEAVY MAINTENANCE, FOUND GOUGE ON LEADING EDGE OF LEFT HAND HORIZONTAL STABILIZER, APPROXIMATELY 13 FEET OUTBOARD OF FUSELAGE. REMOVED DAMAGED MATERIAL, FABRICATED AND INSTALLED A FILLER AND DOUBLER IN ACCORDANCE WITH SRM 55-10-1 FIGURE 13.

Part: BULKHEAD TEE — DAMAGED (FWD PRESS BLKHD)

DURING HEAVY MAINTENANCE, FOUND FORWARD PRESSURE BULKHEAD TEE SUPPORT FOR HINGES WITH TWO LIGHTNING STRIKES. REMOVED TEE, FABRICATED AND INSTALLED A NEW TEE IN ACCORDANCE WITH SRM 51-30-2 AND DRAWING NBA6054. CLOSED AREA AND LEAK CHECKED GOOD.

Part: FLOORBEAM — CORRODED (BS 1601)

DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND NUTPLATE HOLES ON CENTER CARGO BAY FLOORBEAM AT BS 1601, LBL 20. REMOVED DAMAGED SUPPORT, FABRICATED AND INSTALLED NEW SUPPORT IN ACCORDANCE WITH SRM 53-15-01 AND 51-33-01.

Part: FLOOR SUPPORT — CORRODED (BS 600)

DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND NUTPLATE HOLES FLOOR SUPPORT AT BS 60, BL 0 TO BL 29. REMOVED DAMAGED FLOOR SUPPORT, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00.

Part: PRESSURE WEB — CRACKED (BS 1156)

DURING HEAVY MAINTENANCE, FOUND A 19 INCH CRACK IN THE LOWER FORWARD PRESSURE BARREL OF THE CENTER ACCESSORY COMPARTMENT BAY AT BS 1156. THE CRACK PROTRUDES 5.25 INCHES UP FROM A LIGHTENING HOLE AND 13.7 INCHES DOWNWARD FROM LIGHTENING HOLE TO THE 11TH TOP FASTENER IN THE PRESSURE WEB. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IN ACCORDANCE WITH SRM 53-40-00.

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

FOUND FORWARD RIGHT HAND FLOOR TRACK LIGHTS INOP FROM ROW 1 TO ROW 9. REMOVED AND REPLACED BATTERY CHARGER AND OPS CHECKED GOOD.

Part: BEARING — SCORED (LT MLG)

DURING HEAVY MAINTENANCE, FOUND LEFT HAND MAIN LANDING GEAR UPPER BEARING ASSEMBLY SCORED AND GOUGED. REMOVED AND REPLACED LEFT HAND MAIN LANDING GEAR UPPER BEARING ASSEMBLY IN ACCORDANCE WITH CMM 32-11-04.

Part: BUSHING — CORRODED (RT MLG)

DURING HEAVY MAINTENANCE, FOUND RIGHT HAND MAIN LANDING GEAR FORWARD TRUNNION GEAR LUG INNER BUSHINGS PITTED. REMOVED RIGHT HAND MAIN LANDING GEAR FORWARD TRUNNION GEAR LUG INNER BUSHINGS. INSPECTED BORE AND FOUND TO BE WITHIN ORIGINAL HOLE SIZE LIMITS AND INSTALLED NEW BUSHINGS PER CMM 32-11-04.

Part: SWITCH — FAILED (NLG AVIONIC DOOR)

UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. ADJUSTED FUEL LEVEL TO MAXIMUM LANDING WEIGHT AND RETURNED TO LAS. FOUND NOSE WHEEL WELL AVIONICS DOOR OPEN AND DOOR WARNING SWITCH INOP. REMOVED AND REPLACED DOOR WARNING SWITCH.

Part: FIRE LOOP — MALFUNCTIONED (NR 2 ENGINE)

ENGINE NUMBER 2, LOOP-A LIGHT ILLUMINATED. PLACED ENGINE NUMBER 2 LOOP-A LIGHT ON MEL 26-1A.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FOUND MID-CABIN RIGHT EMERGENCY FLOOR LIGHT INOPERATIVE. REMOVED AND REPLACED MID-GALLEY EMERGENCY LIGHT BATTERY POWER SUPPLY (P/N 11-0049, S/N 1970) AND BATTERY ASSEMBLY (P/N 2D131A, S/N 43604). OPS CHECK GOOD IN ACCORDANCE WITH 33-51-01.

Part: FIRE BOTTLE — DISCHARGED (NR 2 RT)

NUMBER 2 ENGINE AGENT LOW LIGHT WAS FOUND ON. REMOVED AND REPLACED FIRE EXTINGUISHING BOTTLE IAW MAINTENANCE MANUAL 26-20-01, OPS AND LEAK CHECKED OK.

Part: FIRE BOTTLE — DISCHARGED (NR 2)

NUMBER 2 ENGINE AGENT LOW LIGHT WAS FOUND ON. REMOVED AND REPLACED FIRE EXTINGUISHER BOTTLE IAW MAINTENANCE MANUAL CHAPTER 26-20-02 AND 26-21-06, OPS CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY IAW MM 33-50-00.

Part: SKIN — DAMAGED (BS 330)

THE FUSELAGE SKIN AND FRAME AT STATION 330 WERE DAMAGED DUE TO CONTACT WITH A GROUND VEHICLE. MAJOR REPAIR WAS ACCOMPLISHED PER SUN COUNTRY ENGINEERING ORDER 53-5225-1.

Part: OIL SYST — LOW (NR 2 ENGINE)

THE NUMBER 2 ENGINE OIL QUANTITY INDICATION DROPPED TO ZERO AND OIL PRESSURE FLUCTUATED DURING CLIMB. REDUCED NUMBER 2 ENGINE POWER TO IDLE AND AIRCRAFT RETURNED TO STATION. SERVICED OIL TO FULL AND ACCOMPLISHED LEAK CHECK PER DC10 MM 79-00-00, NO LEAKS WERE NOTED.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

THE FORWARD CABIN EMERGENCY LIGHTING FAILED SELF TEST. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHTING POWER SUPPLY FOR THE FORWARD CABIN IAW MM 33-50-01, OPS CHECKED NORMAL.

Part: SENSE ELEMENT — FAULTY (NR 2 PNUEMATICS)

THE NUMBER 2 MANIFOLD FAIL LIGHT ILLUMINATED DURING FLIGHT. SHUTDOWN THE NUMBER 2 ENGINE AND FAIL LIGHT REMAINED ON. FLIGHT DIVERTED TO DFW. FOUND BAD SENSE ELEMENT D1-28. REMOVED AND REPLACED SENSE ELEMENT IAW MM 36-23-02. TESTED MANIFOLD SYSTEM PER MM 36-23-00, OPS CHECKED NORMAL.

Part: FIRE LOOP — INTERMITTENT (NR 2 ENGINE)

THE NUMBER 2 ENGINE A-SYSTEM FIRE DETECTION LOOP FLICKERED DURING CLIMB AND DESCENT, BUT NOT IN CRUISE. ALL OTHER ENGINE PARAMETERS WERE NORMAL. FOUND IMPROPERLY ROUTED WIRING, REROUTED WIRING AND SYSTEM TESTED GOOD IAW MM 26-00-00.

Part: FIRE LOOP — INTERMITTENT (NR 2 ENGINE)

THE NR 2 ENGINE A-SYSTEM FIRE DETECTION LOOP FLICKERED DURING CLIMB. ALL OTHER ENGINE PARAMETERS WERE NORMAL. INSPECTED NR 2 A-SYSTEM LOOP AND NO DISCREPANCIES WERE NOTED.

Part: EEL POWER SUPPLY — FAILED (CABIN)

THE FORWARD CABIN CEILING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED FORWARD CABIN POWER SUPPLY AND BATTERY. CEILING EMERGENCY LIGHTS TEST GOOD.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHT FAILED TEST FROM COCKPIT. REMOVED AND REPLACED THE FORWARD CABIN OVERHEAD EMERGENCY BATTERY PACK AND THE SYSTEM TESTED GOOD PER MM 33-51-01.

Part: HYD PUMP — LEAKING (NR 2 ENGINE)

LOST ALL HYDRAULIC FLUID ON THE NUMBER TWO SYSTEM. FOUND RIGHT HAND ENGINE DRIVEN HYDRAULIC PUMP CASE LEAKING. REMOVED AND REPLACED PUMP IAW MM 29-11-01 SERVICED SYSTEM, OPS AND LEAK CHECKED GOOD.

Part: GENERATOR — FAILED (NR 3)

NUMBER 3 GENERATOR DROPPED OFFLINE IN CRUISE, COULD NOT BE RESET. GENERATOR FAIL NR 3 LIGHT CAME ON 25 MINUTES LATER. CSD WAS DISCONNECTED PER COM. CONTINUED TO DESTINATION WITH NR 3 DISCONNECTED. FOUND FAILED GENERATOR, REMOVED AND REPLACED GENERATOR IAW DC-10 MM 24-21-04, RAN ENGINE, OPS CHECK GOOD, LEAK CHECK GOOD.

Part: EEL TRACK — FAILED (CABIN)

MSP - THE FWD CABIN, LT AFT EMERGENCY TRACK LIGHTING IS INOPERATIVE. REPAIRED BROKEN WIRE AT 6 G, TRACK LIGHTING CHECKED GOOD PER 33-50-00. (W)