N730DA

Part: OVEN — SMOKE (GALLEY) · airframe 60,966 hrs · 27,782 cycles

HALON EXTINGUISHER DISCHARGED INTO OVEN TO COMBAT SMOKE FROM GREASE. PER FLIGHT ATTEND, GREASE SMOKE FROM NR 2 OVEN. REPLACED NR 2 OVEN AND HALON EXTINGUISHER. CLEANED ALL OVENS IN GALLEY AND OPERATIONAL CHECKED NORMAL ALL OVENS.

Part: SKIN — CRACKED (RT WING) · airframe 60,832 hrs · 27,738 cycles

THE LOWER SKIN OF THE RT WING WAS FOUND WITH A .5 INCH CRACK AT THE RUNOUT OF STRINGER 19 AT IWS 600. THE CRACKED AREA OF SKIN WAS CUTOUT TO REMOVE THE CRACK. THE CUTOUT WAS REPAIRED WITH 3 ALUMINUM EXTERNAL DOUBLERS PER ER/A 378415-14, REV A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,832 hrs · 27,738 cycles

THE FUSELAGE SKIN WAS FOUND CORRODED BETWEEN FS 1523 & 1545 AND BETWEEN STRINGERS 33 & 35. THE CORROSION WAS REMOVED WITH A 9.1 X 5.6 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER AND TRIPLER INSTALLED PER ER/A378437-14.

Part: ENGINE — FIRE (NR 2) · airframe 59,886 hrs · 27,423 cycles

NR 2 ENG ROLLED BACK AFTER START. MAINT INSP TAILPIPE AND MADE NORMAL RESTART. REPORT BY TWR THAT A/C HAD FLAME FROM NR 2 ENG ON PUSHBACK. CREW REPORTED ENG DID NOT EXCEED 500 EGT. A/C WAS TAILED INTO WIND. ENGINE SPUN TO EXTINGUISH FIRE.

Part: ENGINE — MALFUNCTIONED (NR 2)

STEADY FILTER PRESSURE LIGHT NR 2 ENGINE, LEVEL AT 11,000 FT 250 KTS. POWER UP ON ENGINES, LIGHT WENT OUT WHEN ENGINE PULLED TO IDLE. ENGINE SHUTDOWN. CHECKD FILTER AND CHIP DETECTORS, NO PROBLEMS NOTED. REPLACED DIFF PRESSURE SWITCH.

Part: LE FLAP — MALFUNCTIONED (WINGS)

FLAP/SLAT LOCK LIGHT ILLUMINATED IMMEDIATELY AFTER TAKEOFF. PRIOR TO FLAP RETRACTION FLAPS RETRACTED OK BUT SLATS STAYED AT FULL DOWN AND LOCKED. REPLACED LT SLAT BRAKE, CHECKS GOOD PER MM. WHEN THE STROBE LIGHT SWITCH WAS TURNED ON, ALL 3 SLAT COMPARTOR LIGHTS FLASH AND FLAP/SLAT LOCK ANNUN. ALSO, FAINT CRACKING SOUND WAS HEARD ON SER INTERPHNE. REPLACED STROBE FLASHER AND ALL OK.

Part: COMPARATOR — MALFUNCTIONED (LE FLAP)

AFTER TAKEOFF, FLAP/SLAT LIGHT ILLUMINATED ON S/O PANEL. FLAPS CAME UP RETRACTED BUT SLATS LOCKED IN EXTENDED POSITION. FOUND BOTH ASYMMETRY BRAKES TRIPPED. RESET LT AND RT BRAKES. REPLACED L/E ASYMMETRY COMPARATOR. FLAP/SLAT OPN NORMAL.

Part: BALLAST — FAILED (ROW 5E)

F/A'S REPORTED SMOKE IN THE CABIN IN THE VICINITY OF SEAT 5E, BELIEVED TO BE COMING FROM LIGHTING BALLAST. DEACTIVATED SYSTEM, CONDITION IMPROVED. REPLACED OVERHEAD MODULE AT SEAT 5E/F, REACTIVATED LIGHTING SYS AND ALL CK NORMAL.

Part: BULKHEAD WEB — CRACKED (BS 328)

THE BULKHEAD STIFFENER PANEL AT FS 328, RBL 22 WAS FOUND CRACKED AT THE END OF THE FOURTH MILLED STIFFENER FROM THE BOTTOM. CRACK TRIMMED OUT WITH A 1 BY 0.5 TRIM OUT. REPAIRED PER ERA 330780-14.

Part: BULKHEAD WEB — CORRODED (BS 328)

FS 328 BULKHEAD WEB AT LBL 90 WAS FOUND TO HAVE CORROSION. CORROSION WAS CUTOUT. WEB WAS REPAIRED PER ERA 330749-14.

Part: WEB — CORROSION (NLG WW)

THE LBL 22 WEB JUST AFT OF THE FWD NLG DOOR HINGE CUTOUT WAS FOUND CORRODED. A SECTION OF THE WEB MEASURING 8 BY 12 WAS CUT OUT. THE WEB IS MADE FROM TWO BONDED SHEETS OF 7075-T6 CLAD MATERIAL, ONE MEASURING .071 THK AND THE OTHER .025 THK. INSTALLED DOUBLER.

Part: SPAR CAP — CRACKED (BS 1103)

THE CENTER WING INTERMEDIATE SPAR UPPER CAP LOCATED AT STA 1103 WAS FOUND TO HAVE A CRACK 2.3437 ON THE RT OUTBOARD SIDE. THE CRACK IS TYPICAL OF THOSE DESCRIBED IN S/B 093-57-087, BUT IS BEYOND THE ALLOWABLE LIMITS. DURING THE INSTALLATION OF THE REPAIR, TWO FASTENERS HAD SHORT EDGE DISTANCE. THIS IS A PRE-EXISTING CONDITION FROM THE MANUFACTURER. THIS REPAIR INSTALLED AT THIS LOACTION WAS APPROVED PER FAA/ DER FORM 8110-3, DER DESIGNATION SO-775, DTD 6-30-97.

Part: SIDEWALL — CRACKED (BS 349)

THE NLG WHEEL WELL SIDEWALL BULKHEAD UPPER CAP AT LBL 22.5 WAS FOUND CRACKED ON THE I/B SIDE OF THE HORIZONTAL FLANGE AT STA 349. THE CRACK RUNS FORWARD APPROX 2 INCHES. THE CRACK WAS TRIMMED OUT AND A REPAIR ANGLE WAS INSTALLED AND APPROVED PER FAA/DER FORM 8110-3, DER DESIGNATION SO-775, DTD 6-27-97.

Part: POWER PACK — INOPERATIVE (CABIN)

A AND B ZONE EMER TRACK LIGHTING INOP. REPLACED FWD RT BATT POWR PAK, CK OK.

Part: ACM — SEIZED (FUSELAGE)

DURING TAXI OUT, THERE WAS A LOUD BANG FROM UNDER AREA NEAR 2R DOOR. SHORTLY AFTER AFT PART OF CABIN BEGAN TO FILL WITH SMOKE. ALL PACKS AND ENG BLEEDS SHUT OFF AND SMOKE STOPPED. FOUND ACM SEIZED, REPLACED ACM.

Part: BLKHD WEB — CRACKED (FS 1212)

WHILE PERFORMING INSPECTIONS PER SI 7-70645-12, THE FS 1212 CANTED BULKHEAD WAS FOUND WITH CRACKS IN THE TYPICAL LOCATION AT LBL 30, LBL 10, RBL 22.5 AND RBL 42.5. THE SUBJECT WEB IS M/F FROM .050 7075-T6 SHEET AND WILL BE REPAIRED PER DL ERA 273246 REV A.

Part: FITTING — CRACKED (AFT P-DOME)

COMPLYING WITH INSPECTION SI 7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTINGS CRACKED AT STRINGERS NR 5 AND NR 58. FITTINGS SCHEDULED FOR REPLACEMENT PER DL ERA 272720-14.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

ON LAYOVER, D-SECTION EMERGENCY TRACK LIGHTING INOP. REPLACED BATTERY PACK, OPERATION NORMAL.

Part: ANGLE — CRACKED (LT WING)

LEFT T/E BAT STRUCTURE LWR CAP AT ITES 275.00 APPROX 13 INCHES OUTBD OF OUTBD HINGE FITTING NBR 2 SPOILER LWR CAP HAS A 2 INCH CRACK GOING THROUGH FASTENER HOLE.