N606DL

Part: ENGINE — MAKING METAL (NR 2) · airframe 72,753 hrs · 36,972 cycles

RT ENG IFSD DUE TO OIL PRESS GOING INTO THE RED POSITIVE OIL PRESS NOTED PER FLT CREW. NO INDICATION OF OIL LOSS AS OIL QTY INDICATED 18 PTS AT GATE. T/S OIL PRESS SYSTEM FOUND METAL ON MAIN CHIP DETECTOR. NO METAL ON ALL OTHER CHIP DETECTORS. AIR SPUN ENG RT OIL PRESS 40 A 26 PERCENT N1 HIGH. RAN ENG OIL PRESS CLIMBED TO 80 PLUS BEF IDLE AT STARTER CUTOUT. OIL PRESS DROPPED. S/D ENGINE AT 4 PSI. FOUND MORE METAL ON MAIN CHIP DETECT. SPUN 2 MORE TIME OIL PRESS AT IDLE LIMITS. AT 26-28 PERCENT N2. FOUND METAL CHIP DETECTOR EACH TIME, 4 TIMES. REPLACED ENG PER TANS 6T1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,571 hrs · 35,662 cycles

THE FUSELAGE SKIN AT THE UPPER FORWARD L1 DOOR OPENING CORNER HAS A CRACK IN IT. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED. REF. AD 2004-09-32

Part: TRANSMITTER — INTERMITTENT (LT WING T/E FLAP) · airframe 62,754 hrs · 33,148 cycles

DECLARED EMERGENCY LANDING WITH FLAPS FULL UP, T/E FLAPS ASYMMETRY STATUS MSG AND ASSOCIATED LIGHT. FOUND ASYMMETRY TROUBLES INTERMITTANT. REPLACED FSEU WHICH FAULTED LT FLAP POS XMTR / WIRING. RAN WIRING FROM FSEU-1 TO LT FLAP POSITION XMTR, CHECKED GOOD. REPLACED LT FLAP POSITION XMTR PER AMM. ALL FLAP ANGLE VALUES WITHIN TOLERANCE. CYCLED FLAPS THROUGH FULL TRAVEL SEVERAL TIMES. ALL OPS NORMAL. AFCT RETURNED TO SERVICE.

Part: SPLICE — SEPARATED (EMERGENCY LIGHT) · airframe 61,766 hrs · 32,741 cycles

EMERGENCY TRACK LIGHTS INOP ROWS 19-27. REPLACED SPLICE AT SEAT ROW 27.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 61,316 hrs · 32,567 cycles

THE 1R DOOR OPENED WHILE STILL ARMED, R1 DOOR ASSIST BOTTLE DISCHARGED. R1 DOOR FULLY OPENED, BUT SLIDE PACK FELL ON TO CATERING TRUCK PLATFORM AND DID NOT DEPLOY. REPLACED SLIDE PACK.

Part: FIRE BOTTLE — DEFECTIVE (CARGO BAY) · airframe 58,244 hrs · 31,266 cycles

CARGO BTL 1 EICAS MSG ILLUMINATED ALONG WITH DISCHARGE LIGHT ON CENTER CONSOLE FIRE PANEL. REPLACED CARGO FIRE BOTTLE NR 1. OPS CHECK OK. NO MESSAGES OR LIGHTS ON FLIGHT DECK.

Part: WIRE — BURNED (ELECTRICAL SYS) · airframe 57,896 hrs · 31,105 cycles

IN FLT, R FWD AND L AFT FUEL PUMP C/B'S POPPED AND LOST NR 1 ATC XPONDER, GPS, L EICAS COMP, ASA, CAPT INST XFER, WX RADAR. T/S FOUND BURNT WIRE ON TB5012 BEHIND P6-3 PANEL. REPLACED TB5012 AND RETERMINATED WIRES. CHECKED BOOST PUMPS, ATC, TCAS, L EICAS COMP AND WX RADAR ON GROUND POWER AND ON L ENG GEN ALL IND NORMAL.

Part: ODOR — DETECTED (CABIN) · airframe 57,805 hrs · 31,054 cycles

5 MIN FROM LANDING F/A CALLED COCKPIT AND SAID THEY SMELLED SMOKE NEAR ROW 36. VECTORED FOR IMMEDIATE LANDING. LANDED W/O INCIDENT. STOPPED ON TAXIWAY, F/A REPORTED SMELL HAD CLEARED. AIRCRAFT INSPECTED BY FIRE OFFICIALS W/O RESULT. RAN ENGS AND PACKS W/ NO RESULT. DUE TO EVOLVING HISTORY OF AFT CARGO HEAT FAN, REPLACED SAME. CKS OK.

Part: SKIN — GOUGED (FS 710, S-19R) · airframe 55,536 hrs · 29,953 cycles

FUSELAGE / SKIN / FS 706 & 725 / STRG. 19R : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH A GOUGE IN THE UPPER SKIN AT STRINGER 19R AT FS 706 AND ANOTHER AT FS 725. THE GOUGES WERE REMOVED WITH 2 LOCAL CUTOUS TO THE UPPER SKIN AT THE LAP JOINT. THE CUTOUTS WERE REPAIRED WITH SEPERATE EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 382422-14, REV A.

Part: SKIN — GOUGED (FS 460, S-27R) · airframe 55,536 hrs · 29,953 cycles

FUSELAGE / SKIN / FS 460 / STRG. 27R : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND GOUGED AT FS 460 BETWEEN STRINGERS 26R & 27R. THE GOUGE WAS REMOVED WITH A 3.4" X 2.9" CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 382428-14, REV A.

Part: SKIN — GOUGED (FS 310, S-5R) · airframe 55,536 hrs · 29,953 cycles

FUSELAGE / SKIN / FS 310 / STRG. 4R-5R : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND GOUGED AT FS 310 BETWEEN STRINGERS 4R & 5R. THE GOUGE WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 382362-14, REV A.

Part: SKIN — GOUGED (FS 505, S-27L) · airframe 55,536 hrs · 29,953 cycles

FUSELAGE / SKIN / FS 499-515 / STRG. 26L-28L : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH SEVERAL GOUGES BETWEEN FS 499 & 515 AND BETWEEN STRINGERS 26L & 28L. THE GOUGES WERE REMOVED WITH A SINGLE 16.1" X 4.4" CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 382448-14, REV A.

Part: SUPPORT FITTING — CORRODED (RH WING) · airframe 55,536 hrs · 29,953 cycles

WING / RH MLG FWD TRUNNION SUPPORT FITTING : LUG CORROSION REPAIR WHILE ACCOMPLISHING INSPECTIONS OF THE RH WING MLG FWD TRUNNION FITTING FUSE PINS AND LUGS PER AD 2000-07-13, CORROSION WAS FOUND ON THE SURFACE OF THE LUGS AND THE LUG BORES. THE LUG BORES WERE OVERSIZED AND THE FACES MACHINED TO REMOVE THE DAMAGE. OVERSIZE BUSHINGS WERE INSTALLED TO RESTORE THE AREA PER ER/A 382408-14AD.

Part: SKIN — CORRODED (FS 770, S-19R) · airframe 55,536 hrs · 29,953 cycles

FUSELAGE / SKIN / FS 770-780 / STRG. 18R-19R : CORROSION CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND CORRODED AT SEVERAL NUTPLATE ATTACH HOLES FOR THE WING-TO-BODY FAIRING BETWEEN FS 770 & 780, ABOVE THE STRINGER 19R SKIN LAP JOINT. TWO AREAS OF CORROSION WERE REMOVED WITH 1" HOLES. THE AREA WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 382459- 14, REV A.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 55,536 hrs · 29,953 cycles

WHILE REPLACING LOOSE SEALER AT THE FUSELAGE STATION 900 SPLICE CORROSION WAS FOUND. THE CORROSION EXTENDED FROM STR 16R TO STR 13R ON THE STA 900 SPLICE STRAP. THE SPLICE STRAP WAS REMOVED AND REPLACED DUE TO THE CORROSION BEING OUT OF LIMITS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,552 hrs · 29,496 cycles

ALL FIRST CLASS EMERGENCY TRACK LIGHTING INOP. REPLACED F/C BATTERY PACK. CKS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 54,552 hrs · 29,496 cycles

RT OVERWING LIGHT EMER EXIT SIGN INOP. REPLACED PWR SUPPLY AND BATT PACK.

Part: SKIN — DENTED (FUSELAGE) · airframe 52,877 hrs · 28,731 cycles

THE FUSELAGE SKIN WAS DENTED AND GOUGED AT FS 670 JUST BELOW THE STRINGER 19R SKIN LAP JOINT. THE DAMAGED SKIN WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND STRUCTURAL FILLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 379856-14, REV A.

Part: APU — ODOR (AFT) · airframe 52,223 hrs · 28,420 cycles

BOTH ENGINES WERE SLOW TO START AND DURING THE START AFT CABIN GOT HEAVY EXHAUST ODORS. FUMES WERE IN THE CABIN UNTIL THE PACKS WERE TURNED ON. FOUND SLIGHT ODOR WHILE OPERATING APU. NO FUMES NOTED WITH APU SHUT DOWN AND AIR STARTERS USED. FWD APU TO MCO AND PLACARD.

Part: ACTUATOR — FAILED (OUTFLOW VALVE) · airframe 51,174 hrs · 27,905 cycles

ON TAKEOFF PASSING 5,000, RECEIVED CABIN AUTO INOP EICAS CAUTION MSG AND CABIN ALT AUTO 1 AND 2 STATUS MSG. SELECTED MANUAL BUT UNABLE TO MOVE OUTFLOW VLV, UNABLE TO PRESS AIRCRAFT. FOUND OUTFLOW VLV ACTUATOR CAP BROKEN OFF. REPLACED ACTUATOR ASSY, CKS OK. PRESSURIZED A/C, NO PROBLEMS NOTED.

Part: DUCT — FAILED (LT ENGINE) · airframe 50,268 hrs · 27,476 cycles

DUE TO LEFT BLEED DUCT LEAK, OPERATED LEFT ENG FOR 3 MIN IN ICING CONDITIONS WITH NO ANTI-ICE. REPLACED ANTI-ICE DUCT IN LEFT WING-CHECKED INLET AND LEADING EDGE FOUND OK.

Part: COFFEEMAKER — UNSERVICEABLE (GALLEY)

UNIDENTIFIED SMOKE IN AFT GALLEY. DIVERTED TO JFK FOR LANDING. FOUND AFT LT COFFEE MAKER OVERFLOWING. REPLACED COFFEE MAKER AND OPS CHECK OK. ALSO, REMOVED OVENS AND INSPECTED WIRING. ALL CHECKS OK.

Part: SHEAR PANEL — CUT (BS 1680-1720)

FUSELAGE FLOOR STRUCTURE SHEAR PANEL, FS 1681-1720, SPLICE REPAIR. TO GAIN ACCESS TO THE FS 1681.8 FLOORBEAM UPPER CAP, THE HORIZONTAL SUBFLOOR SHEAR PANEL HAD TO BE TRIMMED OFF FROM FS 1720 TO FS 1680. A NEW SECTION OF SHEAR PANEL WAS SPLICED IN PER ER/A 363925-14, REV A.

Part: FLOORBEAM — CORRODED (BS 1681.8)

FUSELAGE PASSENGER FLOORBEAM, FS 1681.8, UPPER CAP, SPLICE REPAIR. THE UPPER CAP OF THE FS 1681.8 PASSENGER FLOORBEAM WAS FOUND CORRODED IN NUMEROUS AREAS. TO REPAIR THE DAMAGE, THE UPPER CAP WAS TRIMMED OFF AND A NEW CAP WAS FABRICATED FROM ALUMINUM EXTRUSION AND INSTALLED IN ITS PLACE. THE REPAIR WAS ACCOMPLISHED PER ER/A 363852-14, REV A.

Part: SKIN — CRACKED (NR 2 PYLON)

NR 2 ENG NACELLE PYLON STRUT SKIN AT NAC STA 107.7 CRACKED SKIN AT INBD AND OUTBD SIDE. PERMANENT REPAIRS ACCOMPLISHED PER SRM 54-51-01-2-203 ON N/R CARD 19 AND 515 MIDVISIT.

Part: SLIDE — LOW PRESSURE (2R DOOR)

FOUND 2R DOOR EMERGENCY SLIDE BOTTLE PRESS LOW. REPLACED SLIDE ASSY.

Part: LENS AND LIGHT — MISSING (CABIN)

LIGHT AND LENS MISSING ON EMERGENCY LIGHT TRACK AT ROWS 25 AND 39.

Part: BOLT — CORRODED (LT MLG TRUNNION)

DURING LETTER CHECK INSPECTION, FOUND RUST AROUND NUTS FOR LT MAIN LANDING GEAR FORWARD TRUNNION BEARING SUPPORT LOWER BOLTS. REMOVED BOLTS AND FOUND RUSTY/PITTED. REPLACED BOLTS AND NUTS.

Part: EEL TRACK — CRACKED (CABIN)

DURING INSPECTION, FOUND EMERGENCY PATH LIGHT TRACK CRACKED JUST INBOARD OF AFT LAVATORY. REPLACED SECTION OF TRACK LIGHT, OPERATION NORMAL.

Part: RADOME — DELAMINATED (NOSE)

INITIAL SHOP INSPECTION, MAINTENANCE FOUND 2 LARGE AREAS OF DELAMINATION AT THE 7 O'CLOCK POSITION. ALL REPAIRS WERE ACCOMPLISHED AS PER SRM 53-10-72. INTERIOR SKIN AND ALL HONEYCOMB CORE WERE REPLACED DURING REPAIR PROCEDURES. UPON REPAIR BEING COMPLETED RADOME EROISION AND PAINT WERE REAPPLIED PER PS 900-9-1-11 NR 05.

Part: NOSE COWL — DAMAGED (NR 1 ENGINE)

DURING LETTER CHECK L-1, FOUND NR 1 ENG O/B NOSE COWL DAMAGED. REPAIRED NR 1 ENG O/B NOSE COWL PER SRM 51-70-12 AND PAINTED AREA.