N626DL

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 76,510 hrs · 37,199 cycles

AT CRUISE, CREW NOTED AN ACRID SMELL IN THE FWD GALLEY AREA. FOLLOWED CHECKLIST AND SHUT OFF BOTH UTILITY BUSES AND RECIRCULATION FAN. MAINTENANCE DETERMINED THE FWD COFFEEMAKER TO BE THE SOURCE AND REPLACED SAME. NO FURTHER SMELLS. (2010-D1250) (DL757102854)

Part: WATER HEATER — MALFUNCTIONED (LAVATORY) · airframe 76,484 hrs · 37,191 cycles

AN ELECTRICAL SMELL OCCURRED IN THE FORWARD LAVATORY. THE HOT WATER HEATER WAS TURNED OFF IN FLIGHT. FLIGHT CONTINUED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE HOT WATER HEATER PER MM 38-13-51. (2010-D1238) (DL757102772)

Part: WATER HEATER — MALFUNCTIONED (LAVATORY) · airframe 76,484 hrs · 37,191 cycles

AN ELECTRICAL SMELL OCCURRED IN THE FORWARD LAVATORY. THE HOT WATER HEATER WAS TURNED OFF IN FLIGHT. FLIGHT CONTINUED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE HOT WATER HEATER PER MM 38-13-51. (2010-D1238)

Part: WINDOW — FAILED (COCKPIT) · airframe 74,623 hrs · 36,304 cycles

L1 WINDOW SHATTERED IN FLT. ARCING REPLACED WINDOW AND CONTROLLER.

Part: SKIN — DENTED (BS 620 S16L) · airframe 74,361 hrs · 36,155 cycles

FOUND ON ARRIVAL FUSELAGE DENT AT STA 630 STR 16L. REPAIRED DENT IAW ERA 479005-14 REV 2.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 74,000 hrs · 35,942 cycles

FUSELAGE SKIN FS 1621, L-26L TO L-27L PUNCTURE REPAIRED IAW ERA 477809-14.

Part: GEAR — DEFECTIVE (TE FLAP) · airframe 66,139 hrs · 32,315 cycles

TRAILING EDGE FLAP TRANSMISSION GEAR REPLACED IAW EA 06-097281-03, ME04.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 64,565 hrs · 31,632 cycles

FUSELAGE BEAR STRAP, FS 360, S-17R, R1 DOOR CUTOUT LOWER AFT CORNER CORROSION REPAIRED IAW ERA 450307-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 64,497 hrs · 31,609 cycles

FUSELAGE SKIN, FS 1435, S-3L LIGHTNING STRIKE DAMAGE REPAIRED IAW ERA 450494-14.

Part: SKIN — WORN (LT WING) · airframe 61,215 hrs · 30,430 cycles

WEAR DAMAGE WAS FOUND ON THE LEFT HAND SIDE LOWER WING SKIN CAUSED BY CONTACT WITH THE WING-TO-BODY FAIRING SKIN. THE DAMAGE WAS REPAIRED BY ACTS IN VANCOUVER PER ACTS PP B757-57-21136.

Part: PIN — MISSING (NR 4 BRAKE) · airframe 54,032 hrs · 27,598 cycles

NUMBER FOUR BRAKE WEAR PINS MISSING. REPLACED NUMBER FOUR BRAKE ASSY AND LEAK CHECKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,574 hrs · 26,906 cycles

AFT RT EMERGENCY LIGHTS WILL NOT TEST WITH FWD TEST SWITCHES. REPLACED BATTERY PACK CKS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 52,444 hrs · 26,846 cycles

ONE SECTION OF EMERGENCY LIGHTING IS INOP AFT CABIN RIGHT SIDE. REPLACED POWER SUPPLY M736. ALL EMERGENCY LIGHTS NOW OPERATE NORMALLY.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 51,908 hrs · 26,595 cycles

FOUND ON LAYOVER SEVERAL EMERGENCY LIGHTS INOP IN AFT CABIN OVERHEAD INBOARD OF PSU CLOSEOUT PANEL. REPLACED BASE M737 AND BATTERY PACK. NOW CHECKS GOOD.

Part: CHECK VALVE — OUT OF POSITION (A/C BAY) · airframe 51,778 hrs · 26,528 cycles

RIGHT PACK ON PREV MCO AS BEING INOP. DURING CLIMBOUT OF JAX CABIN TEMPS RAN HOT. UNABLE TO DECREASE CABIN TEMPS BELOW 90 DEGREES. FOUND RIGHT PACK TRIM AIR CHECK VALVE IMPROPERLY POSITIONED WHICH WAS ALLOWING LEFT PACK AIR TO PASS THROUGH THE RIGHT ACM. RIGHT PACK IS INOP AND CAUSED THE HI CABIN TEMPS. REPOSITIONED CHECK VALVE AND NO RIGHT PACK REMAINS ISOLATED FROM LEFT.

Part: INDICATOR — DEFECTIVE (COCKPIT) · airframe 48,596 hrs · 24,993 cycles

NO SHUTDOWN OF RIGHT ENGINE AT GATE IN DFW WITH GROUND POWER CONNECTED, ELECTRICAL SMOKE POURED OUT OF F/O INSTURMENT PANEL ON RIGHT HAND SIDE. SECONDARY INDICATION WAS F/O VSI BLANKED OUT WITH NO DISPLAY. PULLED OUT ALL F/O'S INSTRUMENT PANELS AND INSPECTED INSTRUMENTS AND WIRING. FOUND F/O'S VSI INDICATOR WITH EVIDENCE OF SMOKE BURN. REPLACED INDICATOR. OPS GOOD. OK FOR SERVICE.

Part: CONNECTOR — DISCONNECTED (PITOT LINE) · airframe 45,678 hrs · 23,626 cycles

ABORTED TAKEOFF ROLL, NO AIRSPEED INDICAION ON CAPTAINS SIDE. RESEATED PITOT LINE QUICK DISCONNECT TO CAPTS ADC. BITE TEST ON CAPTS ADC TEST GOOD. CHECKED PITOT TUBES FOR OBSTRUCTION, CKS GOOD. PUMPED UP PITOT SYSTEM, AIRSPEED CKS GOOD.

Part: ENGINE — OVERSERVICED (NR 2) · airframe 45,306 hrs · 23,457 cycles

A/C RETURNED FROM FLIGHT WITH NR 2 ENGINE SHUT DOWN DUE TO HIGH OIL TEMP. ENGINE WAS FOUND WITH THE OIL OVER SERVICED BY APPROX 15 QUARTS. DRAINED EXCESSIVE OIL FROM GEARBOX AND ENGINE OPERATION NORMAL DURING ENGINE RUN.

Part: BALLAST — OVERHEATED (CABIN) · airframe 44,882 hrs · 23,249 cycles

BURNING RUBBER ODOR MID CABIN ON DESCENT. ODOR DISSIPATED WHEN OVERHEAD CABIN LIGHTS SECURED. SMELL ALSO DESCRIBED AS ELECTRICAL. STRONGEST BETWEEN ROWS 23 TO 25. REPLACED OVERHEATED LIGHT BALLAST.

Part: INSULATION — BURNED (BS 1440)

FOUND INSULATION BLANKET BEHIND E-6 RACK ADJACENT TO APU GROUND STUD ATTACHMENT TO BE BURNED. NO APPARENT DAMAGE TO SURROUNDING STRUCTURE WAS NOTED. IT APPEARS THAT LINT/DEBRIS COVERED THE BLANKET AND THE BLANKET WAS IGNITED.

Part: CONTROL CARD — INOPERATIVE (NR 2 ENGINE)

FIRE/OVERHEAT EICAS MSG AND SYS FAIL LIGHT. RESET WITH MAINT DIRECTION AND BOTH FAIL LIGHT AND EICAS MSG RETURNED. DIVERTED TO KMCO WITH DISPATCH DIRECTION. ONLY RT ENG FIRE LP2 STATUS MSG WHICH IS ALREADY ON MCO. T/S PER FIM AND WDM. REPLACED FIRE/OVERHEAT/LOGIC CARD M10274 SYSTEM TEST AND ENG RUN UP CKS NORMAL. ALSO, REPLACED LOOP, (P/N 266701017).

Part: SKIN — LIGHTNING STRIKE (BS 502.5)

THE WINDOW BELT SKIN AT FS 502.5 SUFFERED A LIGHTNING STRIKE REQUIRING A .75 DIAMETER HOLE TO CLEAN-UP THE DAMAGE. THE HOLE WAS REPAIRED WITH AN ALUMINUM DOUBLER INSTALLED PER ER/A 363663-14, REV A.

Part: BATTERY — DISCHARGED (CABIN)

AFT RT EMERG FLASHLIGHT INOP. REPLACED EMERG FLASHLIGHT PWR. UNIT OPN CKS NML.

Part: PBE — LOST VACUUM (COCKPIT)

F/C PBE RED BUTTON EXTENDED. INSTALLED NEW PBE.

Part: SKIN — CORRODED (RT WING)

DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND CORRODED AT THE RH FWD OVERWING EXIT DOOR, ON THE INNER SIDE, IN THE 'CUB STRAP' FROM APPROX. THE CENTER OF THE HATCH OPENING AND FWD. THE CORROSION WAS BLENDED IN ACCORDANCE WITH BACO TELEX DAL-ATL-96-1418RR DATED 11 SEP 96.

Part: BULB — FAILED (3L DOOR)

3L DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED SAME, OP CK GOOD.

Part: COWL — DAMAGED (NR 1 ENGINE)

FOUND DURING LETTER CHECK INSP, INBD SIDE OF INLET COWL HAS SMALL HOLE. REPAIRED INLET COWL PER SRM 54-11-01.