N802DE

Part: GENERATOR — ACTIVATED (CREW REST AREA) · airframe 49,061 hrs · 6,684 cycles

OXYGEN GENERATOR FIRED IN CREW REST COMPARTMENT. REPLACED GENERATOR AND BROKEN OXYGEN COMPARTMENT DOOR.

Part: ODOR — DETECTED (CABIN) · airframe 48,922 hrs · 6,649 cycles

ACRID ODOR RESEMBLING BURNING WIRE REPORTED NEAR VIDEO EQUIPMENT, PAX AND CREW NEAR SEATS 12 A/B 13 A/B REPORTED THE ODOR DURATION OF ABOUT 5 MINUTES THEN DISSAPATED. ALL VIDEO EQUIPMENT WAS TURNED OFF. NO OTHER ABNORMAL INDICATIONS OBSERVED. CHECKED SEAT 12 A/B 13 A/B FOR ELECTRICAL OPS FOUND OK ALL VIDEO PLAYERS FOUND OPS OK NO ODOR, NO ABNORMAL INDICATIONS FOUND OK FOR SERVICE.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 46,428 hrs · 6,288 cycles

MID GALLEY OVENS OVERHEAT AND CAUSE SURROUNDING PANELS TO WARM BEYOND TOUCH SLIGHT BURNING SMELL REPORTED BY F/A. REMOVED AND REPLACED OVEN NR 2 MID GALLEY, OPS GOOD.

Part: COMPRESSOR — STALLED (NR 3 ENGINE) · airframe 46,161 hrs · 6,258 cycles

ON T/O, NR 3 ENGINE HAD COMP STALL, ENGINE PARAMETERS CHANGED SLIGHTLY AND RETURNED TO NORMAL, N1 N2 EGT ALL NORMAL AFTER T/O EAD MSG ENGINE 3 FADEC. MAINT FOLLOWED POM PROC P23-107 23-108. REPLACED NR 3 ENGINE PER ROUTINE CARD DECK TRANSMITTAL 8T301.

Part: PIPE — UNSERVICEABLE (RIGHT GEAR) · airframe 46,070 hrs · 6,249 cycles

AFTER TAKEOFF GEAR HANDLE WOULD NOT COME UP PUSHED HANDLE RELEASE BUTTON STILL WOULD NOT COME UP. FOUND RT MLG TRIM CYL HYD PIPE CRACKED AND HYD FUSE SET. REMOVED PIPE INSTALLED NEW LINE AND SAFTYWIRED HYD FUSE LEAK CHK GOOD CYCLED GEAR OPS NORMAL GOOD INDICATIONS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,045 hrs · 6,247 cycles

EMERGENCY LIGHTS REMAIN ON AT ALL TIMES. REPLACED BATTERY PACK.

Part: ACM — CONTAMINATED (A/C BAY) · airframe 45,958 hrs · 6,236 cycles

AIRCRAFT DIVERTED TO PDX DUE TO SMOKE/FUMES IN COCKPIT. ISOLATED NR 3 PACK AS SOURCE OF ODOR. PERFORMED DUCT BURN OUT 21-53-00-7 AND DEFERRED NR 3 PACK.

Part: SPAR CAP — CORRODED (HORIZ STAB) · airframe 45,927 hrs · 6,225 cycles

AT HMV 2, CORROSION WAS FOUND WHILE INSPECTING HORIZONTAL STABILIZER UPPER SURFACE BARREL NUT BORES PER SI8-85288-12. CORROSION WAS ON LT AND RT UPPER SKINS AS WELL AS FRONT AND REAR SPAR CAPS. REPAIRED PER ER/A 412285-14.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,927 hrs · 6,225 cycles

CORROSION WAS FOUND DURING MTC ON PREVIOUSLY INSTALLED REPAIR DOUBLERS AT STA 1937 AND 1959 NEAR THE AFT LAV AIR EXHAUST PORTS. THE DOUBLERS HAD BEEN INSTALLED IN NOV 1996. REPAIRED PER ER/A 360666-14, REV B.

Part: ODOR — DETECTED (CABIN) · airframe 45,239 hrs · 6,129 cycles

ACRID ODOR COMING FROM AIR COND SYS, RAN PACKS AND INSPECTED AIRCRAFT.

Part: RCCB — FAILED (ELECTRICAL SYS) · airframe 44,871 hrs · 6,082 cycles

WHILE VERIFYING BOTH RCCBS B1-1649 AND B1-391 TO BE IN OPEN STATE REFERENCE MEL 28-22-06E L2 FWD AUX PUMP LOW PRESSURE CONDITION RCCB BI-1649 L2 PUMP WOULD NOT GO TO THE OPEN CONDITION, STUCK IN THE CLOSE CONDITION. REMOVED AND REPLACED RCCB B1-1649 PER M/M PERFORMED SATISFACTORY OPERATIONAL CHECK PER M/M .

Part: BATTERY — MISSING (LAVATORY) · airframe 44,150 hrs · 5,992 cycles

FOUND DOOR 4L AFT LAV SMOKE ALARM INOP. FOUND 9V BATTERY HAD BEEN REMOVED AND MISSING. INSTALLED BATTERY AND SECURED COVER BY SAFETY WIRE. NO EVIDENCE OF FIRE IN LAV AND SMOKE ALARM OPS OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 44,123 hrs · 5,989 cycles

ON EMERGENCY LIGHT TEST NR 3 BATTERY FOUND BAD. REPLACED SAME.

Part: POWER SUPPLY — INOPERATIVE (CABIN ROW 38C) · airframe 43,063 hrs · 5,852 cycles

WITH A/C POWER ON,EMERGENCY LIGHTS AT ROWS 30-35 STAYED ILLUMINATED WITH EMERGENCY LIGHTS SELECTED OFF. REMOVED AND REPLACED POWER SUPPLY AND BATTERY. CHECKS OK

Part: CHILLER — MALFUNCTIONED (MID GALLEY) · airframe 42,284 hrs · 5,769 cycles

STRONG ELECTRICAL SMOKE SMELL REPORTED IN AREA OF BC GALLEY ODOR REPORTED BY PAX AND CREW. MID GALLEY A/C AND D/C CIRCUIT BREAKERS PULLED AND COLLARD FOUND CHILLER CYCLING ON AND OFF. CHILLER FWD TO MCO AND PLAC PER MEL 25-22-01. DUE TO CREW REPORTS OF CHILLER SMOKE SMELL INSP GALLEY COMPONENTS, NO OTHER DEFECTS NOTED.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 40,900 hrs · 5,586 cycles

THE FUSELAGE SKIN WAS PUNCTURED BY GROUND EQUIPMENT BETWEEN FS 640 & 650 AT STRINGER 38R. THE DAMAGED SECTION OF SKIN WAS REMOVED WITH A 6.5 X 7.5 INCH CUTOUT AND THE DAMAGED SECTION OF STRINGER REMOVED. THE STRINGER WAS REPAIRED PER THE MD-11 SRM AND THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 378097-14, REV A.

Part: LINE — CRACKED (NR 2 HYD SYSTEM) · airframe 39,942 hrs · 5,441 cycles

NR 2 HYD SYST EMPTY, LOSS OF FLUID DURING ENG REV ON GROUND. LEAK TRACED TO STOW LINE, CRACKED AT TOP OF HCU HYD LINE END. REPAIRED PIPE SECTION APPROX 20 INCHES LONG AND NEW COULPLING FITTED BY KLM IAW 20-10-01-02. REV CYCLED SEVERAL TIMES AND NO LEAKS FOUND. ALL IND NORMAL.

Part: UNKNOWN — ODOR (CABIN)

A/C RETURNED TO GATE DUE TO REPORTED ELECTRICAL ODOR IN CABIN. ODOR SMELL AT MID GALLEY AND 20 FEET AFT OF 3R DOOR. INSPECTED ALL MID GALLEY ELECT UNITS, NO DEFECTS. INSPECTED AREA BY 3R DOOR, ALL OK. ALL AFT GALLEY COMPONENTS RUN, PACK WITH ECON ON-OFF. CHECKED APU AIR SUPPLY, NO ODOR. AS PRECAUTION CHECKED ALL SEAT AND SIDE WALL BALLAST, NO PROBLEMS. AS PRECAUTION DEACTIVATED ENTERTAINMENT SYS.

Part: O2 MASK — WON'T TEST (CABIN)

F/O O2 MASK WILL NOT TEST. REPLACED O2 MASK.

Part: WIRE — FAILED (SEAT 13 A)

SLIGHT ARCING WITH FIRE SEAT 13A CAUSED BY PINCHED READING LIGHT CABLE UNDER SEAT CUSHION PAN. REMOVED PWR FROM CABLE TO LIGHT RENDERED LIGHT INOP. FOUND BY MTC.

Part: ENTERTAIN SYS — FAILED (ROW 3C)

STRONG SMELL COMING FROM ENTERTAINMENT SYSTEM AND FROM SEAT 03C. ENTERTAINMENT SYSTEM SHUTDOWN AND PAX MOVED FROM SEAT 3C. SMELL QUIT AFTER SHUTDOWN OF ENTERTAINMENT SYSTEM. REPLACED AUDIO VIDEO UNIT AT 3C.

Part: DOOR — DAMAGED (CARGO COMPT)

AFT OF FWD CARGO DOOR LOWER AFT CORNER DAMAGED. REPAIRED PER SRM.

Part: OVEN — DIRTY (CABIN)

F/C OVENS 102 AND 103 HAD BURNING SMELL. THE OVENS WERE OFF AND HAD BEEN OFF FOR APPROX 30 MIN. RAN OVENS AT MEDIUM FOR 30 MIN. NO TROUBLE FOUND.

Part: CHILLER — FAILED (GALLEY)

AFT GALLEY CHILLER OVERHEATED CAUSING STRONG ELECTRICAL SMELL. CHILLERS SHUTOFF AND SMELL WENT AWAY. C/B FOR CHILLER PULLED AND COLLARD, REPLACED G8 GALLEY CHILLER.

Part: DETECTOR — INOPERATIVE (CABIN)

LAV 214 SMOKE DETECTOR INOP. REPLACED DETECTOR, CHECKS OK.

Part: BALLAST — INOPERATIVE (GALLEY)

F/A IN F/C GALLEY NOTICED ELEC SMOKE SMELL. WENT TO MANUAL ON ELEC AND NR 1 GALLEY OFF, SMELL DID NOT GO AWAY. TURNED WORK LIGHTS OFF AND PULLED C/B AND SMELL DISSIPATED. G4A LT WORK LIGHT INOP, NEEDS BALLAST. FWD TO MCO AND PLACARD. C/BS PULLED AND COLLARDED. NO DEFECTS NOTED ON ALL OTHER G4A GALLEY EQUIPMENT.

Part: FIRE DETECTOR — MALFUNCTIONED (NR 3 ENGINE)

AT 50 FT ON LANDING GOT NR 3 FIRE WARNING. AFTER LANDING THE THROTTLE WAS MOVED TO IDLE AND LIGHT REMAINED ON AND FIRE BELL SOUNDED. SHUT DOWN FUEL SW AND PULLED FIRE HANDLE ON NR 3. FIRED AGENT, NO SECONDARY INDICATIONS. FOUND PER CFDS NR 3 FDCU AT FAULT. REPLACED SAME AND REPLACED NR 1 BOTTLE AND CARTRIDGE. ALSO, CKD NR 3 ENGINE FOR EVIDENCE OF FIRE. FOUND ALL OK, FINAL FIRE WARN TEST OK.

Part: BOLTS — LOOSE (NR 3 ENGINE)

DURING CRUISE FL350 HAD SMOKE IN CABIN DIVERTED TO BOI. FOUND 3-2 NRMP 270001088 LEAKING AT MOUNTING BOLTS. RETORQUED BOLT AND LEAK STOPPED.

Part: ENGINE — FAILED (NR 1)

NR 1 ENG COMP STALL AT CRUISE STILL SURGED AT IDLE, ENG WAS SHUTDOWN. REPLACED ENGINE.

Part: RAM AIR INLET — WORN (FWD FUSELAGE)

THE RAM AIR INLET DOOR AT ALL THREE POSITIONS WAS FOUND TO BE SEVERELY WORN IN SEVERAL PLACES. THESE INCLUDE THE MOUNT POINTS (P/N ABM7060-503) (DP/N 210701279.

Part: OXY REGULATOR — LEAKING (E/E COMPARTMENT)

CREW O2 LOW, FOUND REGULATOR LEAKING AT BOTTLE CONNECTION. REPLACED REGULATOR, SERVICED O2 BOTTLE AND LEAK CK OK.

Part: BATTERIES — DISCHARGED (CABIN)

FLASHLIGHT AT L2 INB SEAL BROKEN RED DIODE NOT FLASHING. REPLACED BATTERY AND INSTALLED NEW SEAL.

Part: BATTERY — DISCHARGED (CABIN)

BATTERY PACK NR 3 FAILS LGT TEST, SHOWS LOW CHARGE. REPLACED BATTERY PACK, CKS GOOD.

Part: DOUBLER — DAMAGED (LT WING)

THE LT LOWER WING SPLICE DOUBLER WAS FOUND WITH A GROOVE IN THE TYPICAL LOCATION WITH THE MAX DEPTH BEYOND CONDITION 2 LIMITS STATED IN THE SERVICE BULLETIN MD11-53-048. ACCOMPLISHED REPAIRS PER DL ERA 271998-14.