N608DA

Part: SKIN — DAMAGED (FUSELAGE) · airframe 89,683 hrs · 42,393 cycles

LIGHTNING STRIKE, BS 335, STR 19 RT BS 347, STR 20 RT, BS 364, STR 18 RT-STA 440 STR 16-17 RT. REPAIRED DAMAGE IAW SRM 53-00-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 89,683 hrs · 42,393 cycles

LIGHTNING STRIKE BS 260, STR 20 RT - STA 263 STR 18-20 RT -STA 278, STR 20, RT 2EA- STA 292, STR 19RT. REPAIRED DAMAGE IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 200-2360) · airframe 89,683 hrs · 42,393 cycles

LIGHTNING STRIKE BS 200 - 2360, STR 18-20 RT. REPAIRED DAMAGE IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 500) · airframe 89,683 hrs · 42,393 cycles

STRINGER 10 LEFT AT BS 500 LIGHTNING STRIKE ON SKIN. REPAIRED IAW SRM 53-00-01.

Part: STRUCTURE — DAMAGED (THRUST REVERSER) · airframe 89,683 hrs · 42,393 cycles

LIGHTNING STRIKE DAMAGE ON T/E OF NR 1 ENG OTBD THRUST REVERSER HALF AT 7 AND 8 O`CLOCK POS, 2 PLACES. PERFORMED PERMANENT REPAIR IAW SRM 54-31-01.

Part: SKIN — DAMAGED (BS 470) · airframe 89,683 hrs · 42,393 cycles

BS 470 LIGHTNING STRIKE ON SKIN. REPAIRED IAW SRM 53-00-01.

Part: FAIRING — DAMAGED (LT FLAP INBD) · airframe 89,522 hrs · 42,340 cycles

LEFT FLAP INBD POSITION OTBD AFT FLAP TRACK FAIRING. CONFIGURED INCORRECT FOR NEW FLAP INSTALLED. REPLACED ATTACH FITTINGS IAW DWG 113N2383. INSTALLED FAIRING IAW AMM 27-51-30.

Part: SKIN — DAMAGED (BS 254 S23L) · airframe 89,390 hrs · 42,292 cycles

DURING LIGHTNING STRIKE INSPECTION, DAMAGE WAS FOUND AT BS 254 AND JUST BELOW STRINGER 23L IAW ER/A 509083-14, REV ORIG; A DOUBLER AND TRIPLER HAS BEEN INSTALLED.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 86,154 hrs · 41,037 cycles

FUSELAGE SKIN EXISTING REPAIR DOUBLER DENTED. TIME LIMITED REPAIR COMPLETED IAW ERA 497497-14 REV ORIG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 86,154 hrs · 41,037 cycles

FUSELAGE RIGHT SIDE AT STA 900 SPLICE ABOVE WING BELOW WINDOW LINE CORRODED. FOUND AT PSV 1. RECORDED ON NR 72. REPLACED STRAP PER ERA 497410-14.

Part: SKIN — DAMAGED (BS 620 S16L) · airframe 75,266 hrs · 37,297 cycles

SKIN DAMAGE STATION 620 STRINGER 16 LEFT. REPAIR INSTALLED PER SRM 53-00-01.

Part: SKIN — DAMAGED (BS 324 S23-24L) · airframe 75,261 hrs · 37,296 cycles

FUSELAGE DAMAGE STA 324 STRINGER 23 -24 LEFT.

Part: SKIN — DAMAGED (BS 410-430) · airframe 75,261 hrs · 37,296 cycles

SKIN DAMAGE AT STA 410-430 STRINGER 21 LEFT TO 22 LEFT.

Part: SKIN — DAMAGED (BS 1390) · airframe 75,261 hrs · 37,296 cycles

FOUND SKIN DAMAGE AT STA 1390 STRINGER 24L - 25L. REPAIR INSTALLED PER SRM 53-00-01.

Part: SKIN — DAMAGED (BS 1550 S25-26L) · airframe 75,249 hrs · 37,293 cycles

FOUND SKIN DAMAGE AT STA 1550 STRINGER 25L TO 26L. REPAIRED PER SRM 53-00-01.

Part: SKIN — DAMAGED (BS 1700 S15L) · airframe 75,242 hrs · 37,291 cycles

FOUND SKIN DAMAGED AT STATION 1700 STRINGER 15L. REPAIR INSTALLED PER SRM 53-00-01.

Part: FLOORBEAM — DAMAGED (BS 1640) · airframe 75,229 hrs · 37,287 cycles

CABIN FLOOR BEAM UPPER CAP REQUIRES REPLACEMENT AT STA 1640 REPLACED CABIN FLOOR BEAM

Part: STRAP — DAMAGED (BS 1390 RBL 48) · airframe 75,220 hrs · 37,282 cycles

CABIN FLOORBEAM LOWER TORSION STRAP REQUIRES REPLACENT AT STA 1390 RBL 48

Part: UNKNOWN — ODOR (ENTERTAIN SYS) · airframe 70,729 hrs · 35,875 cycles

A SLIGHT ELECTRICAL ODOR WAS DETECTED AROUND ROW 39DEF. PAX WERE REMOVED WHILE ODOR WAS THROUGHLY INVESTIGATED, ODOR DISSIPATED WHEN ENTERTAINMENT SYS SHUTDOWN, THIS OCCURRED DURING FLIGHT 1418 FROM SLC TO EWR.. OPERATED SYSTEM, NO ELECTRICAL ODOR NOTED. ALL IFE CHKS GOOD 39 DEF. REMOVED MCO AND PLACARDS.

Part: INTERCOSTAL — CRACKED (R-2 DOOR) · airframe 69,645 hrs · 35,550 cycles

INTERCOSTAL FOUND CRACKED DURING AD INSPECTION, LOCATED ON R2 PASSENGER DOOR. REPAIRED PER DELTA ERA 459424-14 REV A.

Part: CONTROL PANEL — SMOKE (COCKPIT) · airframe 68,828 hrs · 35,240 cycles

JUST PRIOR TO PUSHBACK, SMOKE BEGAN COMING FROM CAPTS SIDE VOR/DMA CONTROL PANEL. AFTER POWER REMOVED SMOKE STOPPED. REMOVED AND REPLACED VOR/DME CONTROL PNL IAW MM 34-51-02.

Part: DOOR SEAL — DEFECTIVE (AFT CARGO DOOR) · airframe 66,626 hrs · 34,440 cycles

LOSS OF PRESSURIZATION AT FL380. CABIN ALT INDICATED 10K FT DIFF PRESS APPROX 6.5 PSID. MODE SELECTED IN AUTO 1 WITH NO AUTO INOP LIGHT. MANUAL AND AUTO 2 WORKED AT 10K FT. ON AFT CARGO DOOR, REPLACED MISSING UPPER AFT STOP AND DOOR SEAL.

Part: WINDSCREEN — FAILED (COCKPIT) · airframe 66,357 hrs · 34,348 cycles

AIRCRAFT DIVERTED OFF FLT 2009/15 TPA-BDL DUE TO REPORT OF SMOKE/FIRE IN COCKPIT LOWER LEFT CORNER OF CAPTS WINDSHIELD. REPLACED WINDSHIELD.

Part: SKIN — DAMAGED (BS 445 S22L) · airframe 66,136 hrs · 34,273 cycles

FOUND LIGHTNING STRIKE DAMAGE FOUND ON FUSELAGE SKIN AT THE FIFTH FASTENER AFT OF BS 440 BUTT JOINT COMMON TO STR 22L. BURNED AREA OF SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 66,114 hrs · 34,265 cycles

FOUND 1R DOOR EXT EMERGENCY LIGHT INOP. RELAMPED.

Part: WIRE — DAMAGED (CABIN) · airframe 63,585 hrs · 33,399 cycles

EMERGENCY EXIT LIGHT AT SEAT 2CD INOP. REPAIRED WIRE.

Part: OIL SYSTEM — LOW (APU) · airframe 60,867 hrs · 32,343 cycles

APU FAULT LIGHT AND APU SHUTDOWN FOLLOWED WITH APU OIL QTY MESSAGE. SERVICED OIL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,192 hrs · 32,077 cycles

THE UPPER FWD CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A 1.6 INCH CRACK IN THE SKIN WITH A SMALLER CRACK IN THE UNDERLYING BEARSTRAP. THE SKIN AND BEARSTRAP WERE LOCALLY CUTOUT TO REMOVE THE CRACK. THE AREA WAS REPAIRED WITH THREE EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 089063-14AD.

Part: B-NUT — LOOSE (NR 2 ENG HYD SYS) · airframe 57,144 hrs · 30,872 cycles

RIGHT ENG HYD PUMP EICAS MSG AND RT ENG HYD PRESS LIGHT ILLUM ON TAKEOFF. RIGHT ENG HYD PUMP SWITCH TURNED OFF. FOUND PYLON SUPPLY LINE B-NUT LOOSE, SECURED SAME. MOTORED ENG. GOOD PRESSURE, NO LEAKS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,927 hrs · 30,774 cycles

EMERGENCY LIGHTS AFT OF SEAT 38 INOP. REMOVED AND REPLACED LIGHT PACK AND BATTERY ASSEMBLY.

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,763 hrs · 30,211 cycles

FUSELAGE SKIN & KEEL CHORD AT LOWER FWD VHF ANTENNA. FS 730 STR 28L&R. CORROSION REPAIR, THE THE SKIN AROUND THE LOWER VHF ANTENNA CUTOUT WAS FOUND CORRODED. THE HORIZONTAL FLANGES OF THE STRINGER 28L & 28R KEEL CHORDS WERE ALSO FOUND WITH CORROSION. THE SKIN CUTOUT WAS ENLARGED TO REMOVE THE CORROSION AND THE KEEL CHORDS, BLENDED. THE SKIN WAS REPAIRED WITH 2 EXTERNAL DOUBLERS AND THE CHORDS WITH REPAIR ANGLES PER ER/A 383812-14, REV B.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,762 hrs · 30,210 cycles

FUSELAGE SKIN, FS 590-660, STR 14L-19L. THE FUSELAGE SKIN WAS FOUND WITH SEVERAL DENTS NEAR FS 640 ALONG STRINGER 17L. THE DAMAGES WERE IN CLOSE PROXIMITY TO AN EXISTING REPAIR. THE SKIN WAS CUT AT FS 590 FROM STRINGER 14L TO 19L AND THE AFT SECTION OF PANEL REMOVED. A NEW SECTION WAS INSTALLED AND SPLICED IN PLACE WITH INTERNAL AND EXTERNAL DOUBLERS PER ER/A 383714-14, REV A.

Part: SILL — CORRODED (FUSELAGE) · airframe 55,762 hrs · 30,210 cycles

SILL CORROSION AND FRAME SPLICE REPAIR THE OUTER CHORD OF THE LOWER SILL OF THE C2 DOOR OPENING WAS FOUND CORRODED AND REQUIRED REPLACEMENT. A NEW SILL CHORD WAS INSTALLED, AND THE FRAME CHORD AND WEB WERE SPLICE BACK IN WITH REPAIR DOUBLERS AND ANGLES PER ER/A 383694-14, REV A.

Part: FRAME — CORRODED (FS 620, S-25R) · airframe 55,762 hrs · 30,210 cycles

FUSELAGE / C1 DOOR OPENING / LOWER SILL AND FS 620 FRAME : CORROSION REPAIR THE OUTER CHORD OF THE C1 DOOR OPENING LOWER SILL WAS FOUND DAMAGED DUE TO CORROSION. TO FACILITATE REPLACEMENT OF THE CHORD, THE FS 620 FRAME OUTER CHORD AND WEB WERE CUT BETWEEN STRINGERS 25R & 26R AND LOWER ENDS REMOVED. A NEW SILL CHORD WAS INSTALLED AND THE FRAME CHORD AND WEB SPLICED BACK IN PLACE WITH ALUMINUM REPAIR DOUBLERS AND ANGLES PER ER/A 383668-14, REV A.

Part: ENGINE — LACK OF LUBE (NR 1) · airframe 52,886 hrs · 28,799 cycles

EN ROUTE DFW-ATL, GOT A LOW OIL QTY EICAS MSG, LEFT ENGINE OIL QTY READ 0. OIL PRESSURE MIN IN RED, CAPT PER POM SHUT ENGINE DOWN. REPLACED ENGINE.

Part: MOUNT — DAMAGED (NR1 ENGINE) · airframe 51,538 hrs · 28,151 cycles

THE FWD INBD GUIDE PIN HOLE ON THE NR 1 ENGINE AFT MOUNT WAS OVERSIZED TO 1.126 INCH DIA TO CLEAN UP DAMAGE FROM A MIGRATED BUSHING. A NEW OVERSIZE BUSHING WAS INSTALLED TO RESTORE THE AREA. THE REPAIR WAS ACCOMPLISHED PER B757 SRM 54-51-02-2, FIG 202 AND ER/A 378101-14, REV A.

Part: ENGINE — FLAMED OUT (LEFT) · airframe 50,263 hrs · 27,553 cycles

LEFT ENGINE FLAMED OUT AT FL 350, RELIGHT ATTEMPTED SUCCESSFUL AFTER THREE MINUTES OF WINDMILLING. ENGINE LEFT AT IDLE AND LANDED. REPLACED ENGINE.

Part: VALVE — BLOWN (LT MLG WW) · airframe 49,923 hrs · 27,385 cycles

ON TAXI OUT, RT HYD QTY WENT TP .26 FOUND LT BRAKE METERING VALVE END CAP LEAKING. BLOWN PARTIALLY OFF. REPLACED LT BRAKE METERING VALVE IAW MM 32-41-03 LEAK CKS OK. PERFORMED ADJ/TEST OF METERING VAVLE PER MM 32-41-00 OPS CK OK.

Part: VIDEO UNIT — OVERHEATED (CABIN) · airframe 49,183 hrs · 27,032 cycles

VIDEO UNIT OPERATES HOT WITH A HOT SMELL. TURNED UNIT OFF NOW STILL WARM TO THE TOUCH. REPLACED VTR.

Part: WIRES BURNT (#1 ENGINE)

ON TO ROLL AT APPROXIMATELY 30 KIAS LEFT ENG GEN FAILED. ABORTED T/O AND RETURN TO GATE. FOUND PHASE B WIRE CHAFED IN PYLON. REPAIRED SAME.

Part: AIR DISTRIBUTION — ODOR (CABIN)

ON T/O, F/A REPORTED A STRONG BURNING SMELL FROM THE MID RT GALLEY AREA AND FWD. PERFORMED COMPRESSOR WASH ON LEFT ENGINE.

Part: FLOORBEAM — CORRODED (BS 1681.8)

FUSELAGE/FLOORBEAM, FS 1681.8 UPPER CAP, REPAIR FOR CORROSION. THE UPPER CAP OF THE FS 1681.8 FLOORBEAM WAS FOUND WITH EXTENSIVE AREAS OF CORROSION. THE UPPER CAP WAS TRIMMED OFF ALONG THE ENTIRE LENGTH OF THE BEAM. A NEW CAP WAS FABRICATED FROM THE SAME TYPE EXTRUSION AS THE ORIGINAL AND INSTALLED ON THE FLOORBEAM PER ER/A 366220-14, REV A.

Part: FLOORBEAM — CORRODED (BS 1681)

REPAIRED 1681 FLOORBEAM DUE TO CORROSION.

Part: DECK — CORRODED (BS 1681)

REPLACED AFT DECK AT FLOOR LEVEL STATION 1681 TO 1730 DUE TO CORROSION.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY FLASHLIGHT BATTERY LOW. REPLACED BATTERY.

Part: LIGHT — MISSING (CABIN)

FLOOR TRACK LIGHT INOP AT 1B. REPLACED TRACK AND LIGHT ASSY.

Part: LIGHT — MISSING (CABIN)

FLOOR TRACK LIGHT MISSING AT 1B. REPLACED TRACK PORTION AND TRACK LIGHT ASSY. CKS OK.

Part: LIGHT — DAMAGED (CABIN)

L2 EXIT DOOR SIGN DAMAGED. REPLACED LIGHT ASSEMBLY, OPS CKS NORMAL.

Part: ENGINE — FAILED (NR 1)

LEFT ENG FAILURE ON CLIMBOUT PASSING 5,000 FT, PERFORMED ENG FAILURE PROCEDURE. REPLACED SVC.

Part: TRACK LIGHT — MISSING (CABIN)

DURING INSPECTION, CABIN EMERGENCY EXIT TRACK LIGHTS INOP AT ROW 6B. REPLACED MISSING TRACK LIGHT ASSEMBLY, OPERATION NORMAL.

Part: ROD END — BROKEN (NLG)

JUST AFTER TAKEOFF, A THUD WAS HEARD IN THE FWD FUSELAGE AREA. EXTREME VIBRATION FOLLOWED GEAR RETRACTION IN NOSE WHEEL AREA. FOUND ROD END BROKEN ON FWD NOSE GEAR OPERATING ROD. REPLACED RT FWD OPERATION ROD ASSEMBLY, PERFORMED ADJ AND TEST.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND ON T/S CK - FIRST CLASS EMERGENCY TRACK LIGHTING INOP. CORRECTIVE ACTION - REPLACED M731 POWER SUPPLY AND BATTERY PACK.

Part: FAN — FAILED (RIGHT)

DURING CRUISE, HAD AN ELECTRICAL BURNING SMELL IN CABIN. UTILITY BUSES TURNED OFF AND SMELL WENT AWAY. FOUND RT RECIRC FAN MOTOR WINDINGS BURNT, FWD TO MCO. REPLACED FAN, OPERATION NORMAL.

Part: TE WEDGE — WORN (NR 4 LE FLAP)

T/E WEDGE WORN BOTTOM SIDE 36 INCHES FROM I/B END OF NR 4 SLAT. REPLACED WEDGE PER SRM 57-43-02, DURING SHOP VISIT.

Part: CHANNEL — DAMAGED (FUSELAGE)

FOUND DURING LETTER CHECK, DOOR CHANNEL HAS HOLE 12 INCHES AFT OF AFT DOOR CORNER, AFT B/B. REMOVED DAMAGE AND MFG DOUBLER PER SRM 51-70-11, INSTALLED DOUBLER PER SRM 51-70-11.