N134DL

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 53,334 hrs · 24,499 cycles

EMERGENCY LIGHTS FROM 13AB TO 20AB INOP. FOUND FUSE BLOWN ON PWR SUPPLY M9008. REPLACED SAME EMERGENCY LIGHTS FROM 13AB TO 20AB, OP CK NML.

Part: MODULE — FAULTED (TE FLAPS) · airframe 52,024 hrs · 24,074 cycles

UPON FLAP RETRACTION AFTER T/O FLAP HANDLE UP IND STUCK AT FLAPS 01. FLAP SLAT ELEC STATUS MSG AFTER APPROX 20 MIN . IND WENT TO FLAPS UP STATUS MSG GONE. PROBLEM REOCCURRED UPON FLAP RETRACT AFTER LANDING. REPLACED RT M840 MODULE, NO FAULTS PER FIM 27-51-00.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,355 hrs · 21,459 cycles

SEAT 30FG EMERGENCY LIGHT INOP AND LENS MISSING. REPLACED WIRE HARNESS AT SEAT 30FG AND INSTALLED NEW LENS COVER. CHECKS GOOD.

Part: ACTUATOR — CRACKED (NR 5 SPOILER) · airframe 43,114 hrs · 20,401 cycles

A/C LOST CENTER HYD SYSTEM PRESSURE AND QTY. REPLACED NUMBER 5 SPOILER ACTUATOR FOR CRACKED HOUSING.

Part: PSEU — FAILED (DOOR WARNING) · airframe 42,632 hrs · 20,138 cycles

ENTRY DOORS, EMERGENCY DOOR, CARGO DOORS, ACCESS DOOR ALL ILLUMINATED AT ONCE. PLUS THE SLIDE LIGHTS BLINKING IN CABIN WITH ASSOCIATED EICAS MSGS. SEAT BELT FAIL TO EXTINGUISH IN AUTO. REPLACED PSEU, CKS OK PER M/M. DOOR SLIDE SEAT BELT SIGNS WARNING INDICATIONS CHECK OK.

Part: FMC — ODOR (COCKPIT) · airframe 41,793 hrs · 19,691 cycles

FLT 1790 RTB WITH ODOR/SMOKE I9N COCKPIT. BY ARRIVAL AT GATE ALL EVIDENCE HAD DISSIPATED. FOUND F/O FMS CDU BLANK AND COMPLETELY INOP. REPLACED F/O CDU AND OK. NO REOCCURANCE OF SMOKE OR ODOR DURING GATE TIME, APPROX 45 MIN.

Part: SQUIB — FAILED (ESCAPE SLIDE) · airframe 40,974 hrs · 19,284 cycles

EMERGENCY ESCAPE SQUIBS DO NOT TEST - REPLACED SQUIB BATTERY PACKS

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,674 hrs · 19,142 cycles

CREW REPORTS L1 DOOR EMERGENCY LIGHT INOPERATIVE IN THRESHOLD UPPER FWD CORNER. RELAMPED, TESTED IAW M/M.

Part: FSEU — INTERMITTENT (E/E BAY) · airframe 40,175 hrs · 18,900 cycles

AFTER T/O AMBER PROBE HEAT STATUS. AFTER CLEANING UP A/C GOTRED FLAP AURAL WARNING W/FLAPS UP. ON LWR STATUS HAD AIR/GRD DISAGREE, LDG GEAR MON, AND NOSE A/G DISAGREE. CLEANED S244 - S245 - S246. CHECKED CONDUIT AND WIRING FOR S244 S245 AND S246. ALL CHECKS GOOD. REPLACED FSEU AND RAN SYS TEST OF FSEU PER MM ALL CHECKS NORMAL

Part: PANEL — FAILED (COCKPIT) · airframe 39,772 hrs · 18,683 cycles

WHILE AT THE GATE SMOKE AND ODOR STARTED COMING FROM NR 2 COMM PANEL. REPLACED SAME.

Part: BULB — BURNED OUT (LT OVERWING) · airframe 39,328 hrs · 18,459 cycles

LT AFT OVERWING EMERGENCY LIGHT INOPERATIVE RELAMPED CKS GOOD

Part: ACTUATOR — BINDING (APU DOOR) · airframe 38,841 hrs · 18,227 cycles

ELECTRICAL ODOR IN AFT CABIN REPORTED BY FLIGHT ATTENDANTS AFTER PUSHBACK AND ENGINE START. FOUND APU ACTUATOR STUCK OPEN WITH ELECTRICAL ODOR. R & R APU DOOR ACTUATOR. OPS CHECK NORMAL.

Part: SKIN — GOUGED (FUSELAGE) · airframe 31,432 hrs · 14,695 cycles

THE FUSELAGE SKIN WAS BADLY GOUGED AT FS 1365 AND STRINGER 27R. THE DAMAGE WAS REMOVED WITH A 5 X 3.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER AND TRIPLER INSTALLED PER ER/A 377917-14, REV B.

Part: SKIN — PUNCTURED (BS 1600)

EXISTING TIME-LIMITED SKIN REPAIR WAS REMOVED FROM STA 1600, STR 37R TO 38R, FOR INSTALLATION OF PERMANENT REPAIR. ORIGINAL REPAIR WAS INSTALLED DUE TO A PUNCTURE CAUSED BY GROUND DAMAGE. REPAIRED PER ERA 267563-14, REV B.

Part: SKIN — DENTED (BS 1197)

THE FUSELAGE SKIN WAS FOUND DENTED AT STA 1197+88 AT STRINGER 27R AND AT STA 1197+100 AT STRINGER 28R. THE DENT DAMAGE WAS CAUSED BY GROUND DAMAGE. REPAIRED PER ERA 331896-14.

Part: SKIN — DENTED (BS 1241)

THE FUSELAGE SKIN WAS FOUND DENTED AT STA 1241 BETWEEN STR 33L AND 34L. THE UNDERLYING FRAME SHEAR TIE WAS ALSO DENTED. THE DISCREPANT CONDITION WAS CAUSED BY GROUND DAMAGE. REPAIRED PER ERA 331906-14.

Part: COFFEEMAKER — FAILED (FWD GALLEY)

ELEC TYPE SMOKE WAS SEEN COMING FROM THE LIGHTING OVERHEAD IN THE FORWARD GALLEY, THE LIGHTS WERE TURNED OFF WITH SWITCHES AND CIRCUIT BREAKER THE SMOKE DISSIPATED QUICKLY 2-3 MINS THIS OCCURRED 10 MINS PRIOR TO LDG. ALL OTHER IND WERE NML. DURING POST FLT INSP, THE COMPARTMENT ABOVE THE TWO FIRST CLASS COFFEE MAKERS WAS FOUND TO BE VERY HOT TO THE TOUCH. FOUND NR 1 COFFEEMAKER FAILED. REPLACED NR 1 COFFEEMAKER AND NR 2 AS PRECAUTION ALL CKS NML

Part: ENGINE — MALFUNCTIONED (NR 2)

AFTER BEGINING TAXI OUT BOSTON, TOWER RADIOED TO COCKPIT THAT FLAMES WERE VISIBLE IN VICINITY OF RT ENG/WING. NO INDICATIONS FROM COCKPIT, ENGINE WAS SHUTDOWN AS A PRECAUTION FOR LOCAL AUTHORITIES AND MX PERFORMED CKS ON ENG. CHECKED INLET AND EXHAUST OF RT ENG, ALSO CHECKED DRAINS FOR FLUID LEAKS. NONE FOUND, CHECKED WING AREA FOR LEAKS OR DAMAGE, NONE FOUND. STARTED ENG ALL NORM.

Part: INVERTER — MALFUNCTIONED (NR 1 ENGINE)

REF LOG A175829 ITM 2, LOST STBY BUSSES 25 MIN AFTER T/O. MID LAV SMOKE DETECTOR WENT OFF W/LIGHT SMOKE IN AREA THEN DISAPPEARED. REPLACED STBY INVERTER CHKS OK PER MM. CAPT REPORTED, THE DAY BEFORE RANDOM SMOKE DETECTORS IN FRONT AND A FT LAVS WENT OFF THEN STOPPED WITH NO VISIBLE SMOKE IN A/C. THIS STATIC INVERTER (P/N 2410 02136) (S/N 339) IS SUSPECTED TO HAVE CAUSED PROBLEM.

Part: LIGHT SOCKET — DIRTY (MID GALLEY)

MID GALLEY WORK LIGHT SMOKING IN FLT, TURNED OFF LIGHT SMOKE STOPPED. MTC FOUNG COFFEE SPLASHED ON LIGHT SOCKETS. FWD TO MCO DUE TO TIME. SOCKETS NEED CLEANED AND RELAMPED.

Part: SMOKE DETECTOR — ACTIVATED (AFT LAVATORIES)

DURING CRUISE, SMOKE DETECTORS IN THE AFT LAVATORIES ACTIVATED. FLT ATTENDANT NOTED HIGH PITCH NOISE IN GALLEY AND LIGHT ODOR. CHECKED OVENS, COFFEE MAKERS AND LIGHT BALLASTS, NO PROBLEMS NOTED. REPLACED BATTERIES IN SMOKE DETECTORS, RETURNED TO SERVICE.

Part: SMOKE ALARM — ACTIVATED (LAVATORY)

DURING CRUISE, HAD FOUR LAVATORY SMOKE ALARMS SOUND. WITH NO VISIBLE SMOKE ONLY SLIGHT ELECTRICAL SMELL. SMELL DISSIPATED QUICKLY. AFTER LANDING, REACTIVATIED SMOKE, ALARMS, RAN PACKS, RECIC. FAN AND ALL GALLEY EQUIPMENT, NO TROUBLE FOUND RETURNED TO SERVICE.

Part: LONGERON — WORN (NR 1 NACELLE)

DURING SHOP INSPECTION, NR 1 ENGINE CORE COWL LOWER LONGERON WAS FOUND WORN AT THE AFT HINGE FITTING. REPAIRED PER SRM 54-41-02 FIG 207.

Part: COWLING — WORN (LT ENGINE)

DURING SHOP INSP THE AFT LOWER LONGERON OF THE LEFT ENGINE SIDE COWL WAS FOUND TO BE WORN AT THE HINGE FITTING AND THE HINGE FITTING WAS WORN AND BENT. A NEW SECTION WAS SPLICED IN PER SRM 54-41-02, AND THE HINGE FITTING WAS BLENDED TO ALLOWABLE LIMITS OF SRM 54-41-90.