N633DL

Part: GUARD — DAMAGED (LIGHT SWITCH) · airframe 93,214 hrs · 43,028 cycles

EMERGENCY LIGHTS SWITCH IS NOT ARMING WHEN COVER CLOSED. REPLACED EMERGENCY LIGHT SWITCH GUARD, CHECKED GOOD.

Part: STRINGER — CORRODED (BS 1681) · corrosion level 2 · airframe 91,849 hrs · 42,379 cycles

AFT CARGO BAY BS 1681, STR 29R IS CORRODED IN CENTER OF STRINGER. REMOVED CORROSION AND HAD 100 PERCENT MATERIAL LOSS. FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: PANEL — CRACKED (SLAT TRACK) · airframe 91,849 hrs · 42,379 cycles

RT WING NR 9 SLAT, AT OTBD MAIN TRACK. SLAT COVE PANEL HAS CRACK AT FASTENER HOLE. REMOVED CRACK AT SLAT COVE PANEL RT WING NR 9 SLAT HAD IT HFEC. NO DEFECTS NOTED. FABRICATED DOUBLER AND INSTALLED REPAIR IAW 366767-14MA AND AMM 27-81.

Part: SKIN — DAMAGED (BS 656) · airframe 91,849 hrs · 42,379 cycles

FWD CARGO BAY, LIGHTNING STRIKE OUTER SKIN, CAN NOT INSTALL SOLID FASTENER DUE TO THE VICINITY OF HOLE UNDER STR 27R. REPAIRED FUSELAGE SKIN AT BS 656, STR 27 RT IAW PRI 544317-14, REV 0.

Part: PANEL — CRACKED (SLAT TRACK) · airframe 91,849 hrs · 42,379 cycles

LEFT WING NR 1 SLAT, COVE PANEL INBD OF INBD MAIN TRACK IS CRACKED AT FASTENER. REPAIRED LT WING NR 1 SLAT COVE PANEL INBD OF INBD MAINTRACK IAW ER/A 366767-14MA.

Part: FRAME — CORRODED (BS 1681) · corrosion level 2 · airframe 91,849 hrs · 42,379 cycles

AFT CARGO PIT, UNDER POTABLE WATER TANK, FWD OF LAV PAN DUMP PAN AT BS 1681, BL 9 RT, FRAME CORRODED. REMOVED CORROSION, 100 PERCENT MATERIAL LOSS. INSTALLED NEW REF DWG AND SRM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 91,816 hrs · 42,366 cycles

LEFT WING FIXED L/E TOP SIDE, 40" FROM INBD END OF NR 4 SLAT, HAS APPROXIMATELY 6" AREA OF DELAMINATION. REPAIRED LT WING FIXED L/E TOP SIDE, 40" FROM INBD END OF NR 4 SLAT IAW SRM 51-70-17. INSTALLED REPAIR ID TAG IAW TOPP 30-10-70, PG 14.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 91,816 hrs · 42,366 cycles

AFT CARGO BAY, MOST FWD FLOOR PANEL CRACKED. REPAIRED AFT CARGO PIT MOST FWD FLOOR PANEL IAW ERA 489384-14MA REV F, SEC. V. PERMANENT REPAIR. REPAIR WEIGHS 388 GRAMS.

Part: PLATE — CORRODED (BS 764) · airframe 91,816 hrs · 42,366 cycles

FWD CARGO BIN FLOOR BS 764 RT SIDE PLATE HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. MATERIAL LOSS =100 PERCENT AND BEYOND ALLOWABLE LIMITS OF SRM 53-00-53 DETAIL V. REPAIRED RT SIDE PLATE AT BS 764 RT IAW AMM 53-88-01-801.

Part: SUPPORT ANGLE — CORRODED (BS 605) · corrosion level 2 · airframe 91,816 hrs · 42,366 cycles

FWD CARGO BAY BS 605, RBL 27.3 THRESHOLD SUPPORT ANGLES ARE CORRODED. REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS. FABRICATED REPAIR AND INSTALLED IAW DWG AND SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 91,788 hrs · 42,351 cycles

ROW 27 MISSING RED EMERGENCY LIGHT LENS. REPLACED LENS AS REQUIRED IAW AMM 33-51.

Part: POWER SUPPLY — SHORTED (EMERGENCY LIGHTS) · airframe 88,007 hrs · 40,738 cycles

DURING SERVICE CHECK FOUND F/C SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. T/S IAW WDM 33-51-16 , FOUND R2 DOOR EXIT ID LIGHT SHORTED SHORTED POWER SUPPLY. R & R SAME OPS CHECK GOOD. OK FOR SVC.

Part: TIRE — FAILED (MLG) · airframe 87,948 hrs · 40,714 cycles

TIRE, WHILE OPERATING ON FLIGHT 1916, DECLARED AN EMERGENCY DUE TO A BLOWN NR 4 TIRE DURING TAKEOFF. FOUND NR 4 MAIN TIRE FLAT AND RECAP MOSTLY GONE. REPLACED NUMBER 3 AND 4 MAIN WHEEL ASSEMBLIES PER AMM. OK FOR SERVICE .

Part: SKIN — DAMAGED (BS 494) · airframe 86,630 hrs · 40,129 cycles

SKIN BS 494, S26-27R, FWD ATG4 ANTENNA DAMAGED. REPAIRED IAW ER/A 519398-14, REV A.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 86,495 hrs · 40,074 cycles

EMERGENCY PROXIMITY LIGHTS INOPERATIVE. REPLACED BROKEN CONNECTOR AT SEAT 29E, CHECKS OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,359 hrs · 40,026 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS OUT AT L1 AND R1 DOOR. R & R BATTERY AND CHARGER IAW AMM 33-51.

Part: SKIN — DENTED (BS 680) · airframe 85,661 hrs · 39,759 cycles

LOWER FUSELAGE DENTED AT BS 680 BETWEEN S22-23R. REPAIR INSTALLED IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 610) · airframe 85,652 hrs · 39,756 cycles

FUSELAGE SKIN, BS 610 S26-27R, DAMAGED. REPAIRED IAW ER/A 503769-14AD, REV A.

Part: FRAME — DENTED (BS 1220) · airframe 85,652 hrs · 39,756 cycles

BS 1220 S26R FRAME DENTED. REPAIRED IAW ER/A 503771-14AD, REV A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 85,479 hrs · 39,684 cycles

POSSIBLE LIGHTENING STRIKE ON APPROACH. FOUND A MULTIPLE POINTS AHEAD OF NOSE GEAR DOOR AFTER LANDING. PERFORMED LIGHTENING STRIKE INSPECTION IAW AMM 05-51. REPAIRED DAMAGE IAW SRM 51-70-05.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 85,139 hrs · 39,531 cycles

EMERGENCY LIGHT AT SEAT 6C INOPERATIVE. FOUND BROKEN WIRE SPLICE. REPLACED JIFFY SPLICE IAW SWPM 20-90-14. ALSO RELAMPED . OPS CHECK NORMAL.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 83,682 hrs · 38,900 cycles

JUMPSEAT LT AFT ENTRY L4 DOOR FOR MX EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. REPLACED LENS.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 83,129 hrs · 38,696 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS ROW 12 DEF INOPERATIVE. FOUND BROKEN WIRE. SPLICED IAW WDM 33-51-16. OPS NORMAL.

Part: SKIN — DAMAGED (BS 800 S4-5R) · airframe 81,493 hrs · 38,006 cycles

BS 800 AND STR 4R, 5R. LIGHTNING STRIKE. REPAIRED IAW ERA 378696-AD, REV D.

Part: SKIN — DAMAGED (BS 610 S26-27R) · airframe 79,796 hrs · 37,256 cycles

FUSELAGE SKIN HAS A CREASE AREA BELOW AFT SIDE OF CARGO DOOR BS 600-620 BETWEEN S26 TO 27R. REPAIRED IAW ERA 503769-14 REV. ORIGINAL.

Part: FRAME — DENTED (BS 1380 S26L) · airframe 79,796 hrs · 37,256 cycles

SMALL DENT ON INNER FREE FLANGE OF FUSELAGE FRAME, BS 1380, APPROXIMATELY ABOVE STRINGER 26 LEFT. REPAIRED IAW SRM 53-00-07 FIG. 201 DETAIL 2.

Part: SKIN — CRACKED (R1 DOOR) · airframe 79,796 hrs · 37,256 cycles

CRACKED FASTENER HOLES R1 DOOR SKIN ASSY.

Part: FRAME — DENTED (BS 1220 S26R) · airframe 79,796 hrs · 37,256 cycles

SMALL DENT ON INNER FREE FLANGE OF FUSELAGE FRAME STA 1220 ABOVE STR 26R. REPAIRED IAW SRM 53-00-07 REPAIR 5, FIG. 201, DETAIL 2 ENCOMPASSED BY ERA 503771-14 REV ORIGINAL.

Part: SKIN — CORRODED (BS 600 S27R-27L) · airframe 79,796 hrs · 37,256 cycles

FUSELAGE SKIN BULGED AT BILGE AREA BS 600. REPAIRED AREA IAW SRM 53-00-01.

Part: SKIN — DENTED (BS 212 S20-21R) · airframe 79,796 hrs · 37,256 cycles

FUSELAGE SKIN DENTED BS 212, S20-21R. REPAIRED IAW ERA 503765-14 REV ORIG.

Part: SKIN — CORRODED (BS 580 S27R/L) · airframe 79,796 hrs · 37,256 cycles

FUSELAGE SKIN BULGED AT BILGE AREA BS 580. REPAIRED AREA IAW SRM 53-00-01.

Part: FLOOR SUPPORT — CORRODED (BS 1328-1333) · airframe 79,796 hrs · 37,256 cycles

AFT CARGO COMPARTMENT BILGE AREA, FLOOR SUPPORT STRUCTURE CORRODED, BS 1328-1333, STR 30R. CUT OUT DAMAGED AREA AND INSTALLED REPAIR ANGLES IAW SRM 51-70-12 FIG 1.

Part: FLOOR SUPPORT — CORRODED (BS 1328-1333) · airframe 79,796 hrs · 37,256 cycles

AFT CARGO COMPARTMENT BILGE AREA, FLOOR STRUCTURE CORRODED UNDERNEATH, BS 1328-1333, STR 28L. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 51-70-12 FIG 1.

Part: FLOOR SUPPORT — CORRODED (BS 1328-1333) · airframe 79,796 hrs · 37,256 cycles

AFT CARGO COMPARTMENT BILGE AREA, FLOOR SUPPORT STRUCTURE CORRODED, BS 1328-1333, STR 28R. CUT OUT DAMAGED AREA AND INSTALLED REPAIR ANGLES IAW SRM 51-70-12 FIG 1.

Part: SKIN — DAMAGED (BS 412 S15-17R) · airframe 79,796 hrs · 37,256 cycles

FUSELAGE SKIN HAS A CREASE BS 412, STR 17R- STR 15R. REPAIRED IAW ERA 503772-14 REV ORIGINAL.

Part: SKIN — DENTED (BS 1681-1701) · airframe 79,796 hrs · 37,256 cycles

FUSELAGE SKIN DENTED, BS 1681.8- 1701, STR 15- 16L. REPAIRED IAW ERA 503766-14 REV ORIGINAL.

Part: FLOORBEAM — CORRODED (BS1640 LBL21-60) · airframe 79,796 hrs · 37,256 cycles

MAIN CABIN FLOORBEAM TEE CORRODED AROUND NUT PLATE HOLES BS 1640 LBL 21- LBL60. REPAIRED IAW SRM 53-00-51 REPAIR3.

Part: FRAME — DENTED (BS 660 S26L) · airframe 79,796 hrs · 37,256 cycles

DENT ON FRAME BS 660 S26L. REPAIRED IAW SRM 53-00-07 FIG 201 REPAIR 5.

Part: SKIN — DAMAGED (BS 632) · airframe 79,796 hrs · 37,256 cycles

FUSELAGE SKIN DAMAGED AT BS 632 AND 2 INCHES BELOW S27L. REPAIRED IAW SRM 53-00-01 FIG 201.

Part: SKIN — DENTED (BS1681.8 S17-18R) · airframe 79,796 hrs · 37,256 cycles

FUSELAGE SKIN DENTED AT BS 1681.8 STR 17- 18R. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DENTED (BS 620 S16L) · airframe 79,796 hrs · 37,256 cycles

SKIN DAMAGED AT BS 620 S16L. REPAIRED IAW ERA 378785-14.

Part: SKIN — DAMAGED (BS 600-620) · airframe 79,796 hrs · 37,256 cycles

EXTERNAL FUSELAGE SKIN HAS A CREASE BELOW AFT SIDE OF CARGO DOOR BS 600-620 TO BE REPAIRED PER SRM 53-00-01.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 79,796 hrs · 37,256 cycles

AFT CARGO COMPARTMENT, FRAME SHEAR TIE CRACKED BS 1300, STR 21R-STR 20R. REMOVED AND REPLACED IAW B757 SRM 51-40-02.

Part: SKIN — DENTED (BS 212 S20-21R) · airframe 79,796 hrs · 37,256 cycles

FUESELAGE SKIN RT SIDE AREA DENTED AT BS 212, STR 20-21R. REPAIR IAW SRM 53-00-01.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 77,035 hrs · 36,130 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHT AT SEAT 3C INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS. OPERATIONAL CHECK WAS GOOD.

Part: FCU — MALFUNCTIONED (NR 2 ENGINE) · airframe 76,909 hrs · 36,087 cycles

THE NR 2 ENGINE FLAMED OUT WHILE ON FINAL APPROACH INTO DTW BUT THE LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE NR 2 ENGINE FCU AND RELAYS K10474 & K10475.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 74,082 hrs · 34,856 cycles

DURING OPN 2525 FOUND BROKEN HARNESS FOR EMERGENCY ESCAPE LIGHT AT 33DEF. REPLACED HARNESS. LIGHT OPS CHECKED NORMAL (2010-D0824)(DL757101804).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,053 hrs · 34,840 cycles

DURING LAYOVER CHECK, MAINTENANCE FOUND EMERGENCY PATH LIGHT AT ROW 26DEF INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD (2010-D0806)(DL757101772).

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 73,970 hrs · 34,812 cycles

DURING LAYOVER CHECK, MAINTENANCE FOUND RED EMERGENCY PATH LIGHT AT MID LAVATORY INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 72,764 hrs · 34,203 cycles

AFTER SWITCHING TO EXTERNAL POWER, CREW NOTED THE LT SIDE EMERGENCY LIGHTS ILLUMINATED. MX REPLACED THE BATTERY PACK AT LOCATION M731.

Part: DUCT — BLOWN (CABIN AIR) · airframe 72,698 hrs · 34,166 cycles

ON PUSHBACK DURING ENG START ON RAMP SMOKE/HEAT IN CABIN SLIDES DEPLOYED ACFT TOWED BACK INTO GATE, REMAINING PAX DEPLANED. FOUND DOOR BLOWN DUCT INSIDE FWD WALL OF AFT BAG BIN. REMOVED AND INSTALLED BLOWN DUCT. ALSO FOUND NEXT DUCT FWD IN RT W/W WORN. REMOVED AND REPLACED DUCT. COMPLETED OPS TEST OF WING AND BODY DUCT LEAK DETECT 28-18-00 AND SQUIB CIRCUIT 26-23-00 AND BOTTLE PRESS SW 26-23-00. OPS CKS GOOD. DUCTS LEAK CHECKED GOOD. RUN ENG IAW MM. PNEUMATIC CHECKS NORMAL. NO LEAKS.

Part: BEAR STRAP — CRACKED (L1 DOOR) · airframe 71,162 hrs · 33,369 cycles

DURRING PSV INSP FOUND BEAR STRAP AT THE FORWARD UPPER END OF THE L1 DOOR CUTOUT CRACKED. REPAIRED PER ERA 475387-14.

Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 70,154 hrs · 32,858 cycles

FLT DECK DOOR UNLOCK LIGHT OVERHEAD PANEL INOP, WHEN AMT ARRIVED SMOKE WAS COMING FROM LIGHT ASSY. RELAMPED, NO HELP. REMOVED AND REPLACED PANEL ASSY PER AMM NOW OK PANEL CKS.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 67,546 hrs · 31,639 cycles

SCRATCH IN FUSELAGE SKIN, FS440, STR6L TO 7L. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER AND TRIPLER.

Part: RECEIVER — FAILED (RT VOR) · airframe 66,660 hrs · 31,277 cycles

CREW REPORTED ELECTRICAL FUMES IN FLIGHT. RIGHT VOR C/B WAS FOUND POPPED AND WOULD NOT RESET. RT VOR RECEIVER WAS FOUND TO HAVE STRONG ELECTRICAL SMELL AND SIGNS OF FAILURE.

Part: LINE — RUPTURED (HYD SYS) · airframe 66,619 hrs · 31,257 cycles

LT SYS HYD QUANITY MSG FOUND LEAK IN LEFT WW. INSPECTED AND FOUND LT ELEC HYD PUMP HAS RUPTURED HOSE. REMOVED AND REPLACED RUPTURED HOSE. SERVICED AND LEAK CK IAW AMM12-12-01. NO LEAKS, NO DEFECTS NOTED.

Part: SKIN — DENTED (FUSELAGE) · airframe 63,242 hrs · 29,875 cycles

A DENT AND GOUGE WERE FOUND IN THE SKIN AFT OF FS 1260 BELOW S-14R. THE DAMAGED SKIN IS WITHIN 3 INCHES OF THE SKIN SPLICE. THE DAMAGED AREA WAS CUTOUT AND A BOEING APPROVED REPAIR WAS INSTALLED PER 456588-14

Part: SKIN — DENTED (FUSELAGE) · airframe 63,233 hrs · 29,871 cycles

A DENT WAS FOUND ON THE SKIN AT FS 223.50 BETWEEN WL200 AND WL 210, NEAR THE ANGLE OF ATTACH SENSOR. BOEING WAS CONTACTED AND AN APPROVED EXTERNAL REPAIR WAS INSTALLED PER 456555-14

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,233 hrs · 29,871 cycles

CORROSION WAS FOUND ON THE KEEL BEAM CHORD BETWEEN FS 660 AND FS 680, S-28R. THE CORROSION WAS REMOVED AND A BOEING APPROVED REPAIR INSTALLED PER 456557-14

Part: SILL — CORRODED (FUSELAGE) · airframe 63,233 hrs · 29,871 cycles

CORROSION WAS FOUND ON THE NR 2 CARGO DOOR LOWER MAIN SILL OUTBOARD CHORD ON THE UPPER FACE OF THE OUTBOARD SURFACE OF THE HORIZONTAL FLANGE FROM APPROXIMATELY FS 1400 TO 1440. THE CORROSION WAS BLENDED PER SRM REQUIREMENTS WITH A MAXIMUM DEPTH OF 0.065", AND WAS APPROVED BY BOEING, AS DETAILED IN 456371-14.

Part: SKIN — DAMAGED (FS 395 S2L) · airframe 63,233 hrs · 29,871 cycles

LIGHTNING STRIKE DAMAGE AT A FASTENER LOCATION AND ADJACENT SKIN WAS FOUND AT FS 395 BETWEEN S-2L AND S-3L. THE DAMAGE WAS CUT OUT IAW MFG APPROVED INSTRUCTIONS, AND IS DOCUMENTED IN ERA 456266-14.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,233 hrs · 29,871 cycles

CORROSION WAS FOUND ON THE FRAME ON THE INSIDE CHORD AT FS 729.6 ABOVE WL 210. THE DAMAGE WILL BE TRIMMED OUT AND BOEING APPROVED REPAIR ANGLE INSTALLED PER 456268-14.

Part: AIR DUCT — RUPTURED (CABIN) · airframe 62,393 hrs · 29,528 cycles

ON INITIAL CLIMBOUT EXCESSIVE AIR PRESSURE FROM PACKS CAUSED A CEILING PANEL IN CABIN TO BLOW OFF WITH HIGH AIRFLOW ON PASSENGERS IN THAT AREA. REMOVED CEILING PANELS IN AFFECTED AREA, BLOWN OUT SECTION OF DISTRIBUTION DUCT AND NUMBER 5 VIDEO SCREEN REPAIRED. REPLACED 7 SECTIONS OF DISTRIBUTION DUCT ON N/R CARDS 1-11. REMOVED AND REINSTALLED CEILING PANELS AND VIDEO MONITORS ON N/R CARDS 1-11, RAN PACKS AND PRESSURE CONTROL SYS IN HIGH AND LOW FLOW W/ENGS AND APU CHECKS GOOD PER AMM.

Part: POWER SUPPLY — INOPERATIVE (34ABC) · airframe 56,185 hrs · 27,404 cycles

AFT EMERGENCY EXIT LIGHTS WILL NOT GO OUT WHEN BATTERY IS RESET. LT SIDE ONLY REAR. REPLACED EMERGENCY EXIT PWR SUPPLY M735 AND BATTERY PACK.

Part: TERMINAL — BURNED (CABIN) · airframe 53,044 hrs · 26,217 cycles

RETURN TO GATE, F/A REPORT FAINT ELECTRICAL SMELL IN AFT LAV. LOCATED ELECTRICAL SMELL FROM ROW 44 RT SIDE CEILING LIGHTS FLUORESCENT LIGHT ASSY AFT END TERMINAL BURNT. PULLED C/B-7 IN P37 PANEL AND DEACTIVATED RT CEILING LIGHTS. FWD TO MCO AND PLAC PER 33-21-01. NO ELECTRICAL SMELL FROM AFT LAV.

Part: TAILPIPE — FIRE (NR 2 ENGINE) · airframe 52,381 hrs · 25,943 cycles

DURING NR 2 ENGINE START DURING/AFTER PUSHBACK FROM GATE, TAILPIPE FIRE OCCURRED. FIRE SELF-EXTINGUSHED ON ENGINE START. NO COCKPIT WARNINGS WERE NOTED BY THE FLIGHT CREW. HOWEVER PASSENGERS PANICKED AND DEPARTED THE AIRCRAFT THRU EMERGENCY EXITS. ALL SLIDES PERFORMED AS DESIGNED. REPLACED EEC PER AMM DUE TO FAULT CODE.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 52,236 hrs · 25,873 cycles

FUSELAGE SKIN WAS FOUND WITH 2 LIGHTNING STRIKES IN THE CROWN SKIN AREA. ONE STRIKE WAS AT FS 1540 AND STRINGER 6R AND THE OTHER STRIKE WAS AT FS 1560 AND STRINGER 5R. THE LIGHTNING STRIKES WERE REMOVED WITH SMALL CUTOUTS. EACH CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385182-14, REV A.

Part: SKIN — DAMAGED (FS S-6R) · airframe 52,236 hrs · 25,873 cycles

LIGHTNING DAMAGE, CUTOUT REPAIR. THE FUSELAGE SKIN WAS STRUCK BY LIGHTNING AT FS 1450 AND STRINGER 6R. THE DAMAGE WAS REMOVED WITH A 1.2 INCH CUTOUT IN THE CROWN SKIN. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS IAW ER/A 385187-14, REV A.

Part: ODOR — DETECTED (CABIN) · airframe 50,503 hrs · 25,103 cycles

ODORS DETECTED IN CABIN NEAR ROWS 26-29. NO SMOKE BUT STRONG RUBBER LIKE ODOR PRESENT. ODOR SUBSIDED AFTER LANDING. RAN ENGINES AND PRESSURIZED A/C TO 5 PSID. INSPECTED CABIN, GALLEYS AND LAVS. NO UNUSUAL ODORS PRESENT. VERIFIED CARGO COMPARTMENTS NORMAL. NO ODORS PRESENT.

Part: WIRE — PULLED (CABIN) · airframe 48,549 hrs · 24,212 cycles

EMERGENCY LIGHT AT SEAT 6CD INOP. FOUND SEAT WIRING HARNESS CONNECTOR WIRE PULLED OUT. REPLACED HARNESS.

Part: SENSOR — OUT OF ADJUST (L2 DOOR) · airframe 48,156 hrs · 24,032 cycles

ABORTED TAKEOFF AT 99 KTS DUE TO ENTRY DOOR WARNING. ADJUSTED DOOR INDICATOR, CHECKS OK.

Part: SLIDE — FAILED (R1 DOOR) · airframe 47,439 hrs · 23,667 cycles

SLIDE PACK FAILED TO DEPLOY WHEN DOOR OPENED WITH SLIDE ENGAGED. FOUND SLIDE DEPLOY MECHANISM LOCATED ON SLIDE PACK JAMMED NOT ALLOWING DEPLOYMENT. REPLACED SLIDE PACK WITH PART BORROWED FROM UAL.

Part: EEC — FAILED (NR 1 ENGINE) · airframe 44,306 hrs · 22,224 cycles

ON TAXI OUT -L ENG SEC CONT- MSG DISPLAYED ON EICAS. EPCS ASSOCIATED MSGS -S EEC- -EEC- -S275-16- AND -275-19-. REPLACED L EEC AS PER MM. TEST OK. L EEC PB SYS INSP AND CLEANING PERFORMED AS PER MM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,094 hrs · 22,134 cycles

AN EXISTING TEMPORARY SKIN REPAIR WAS REMOVED AT FS 600, BETWEEN STRINGERS 6R AND 7R FOR PERMANENT REPAIR. THE EXISTING DAMAGE CUTOUT AND THE FASTENER HOLES FROM THE TEMP REPAIR WERE REMOVED WITH A 8 X 8 INCH CUTOUT. THE NEW CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER INSTALLED PER ER/A 378711-14, REV B.

Part: SKIN — DENTED (FUSELAGE) · airframe 44,094 hrs · 22,134 cycles

THE FUSELAGE SKIN WAS DENTED AND GOUGED AT FS 620 AND STRINGERS 16L AND 17L. THE DAMAGE WAS REMOVED BY CUTTING OUT THE SKIN OVER A 14.5 X 14.5 INCH AREA. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER INSTALLED PER ER/A 378785-14, REV B.

Part: SKIN — TOOL DAMAGE (FUSELAGE) · airframe 44,094 hrs · 22,134 cycles

UPON REMOVAL OF A TEMPORARY SKIN REPAIR FOR ACCOMPLISHMENT OF A PERMANENT REPAIR, THE SKIN AND TEAR STRAP AT FS 640 WAS DAMAGED. THE DAMAGED SECTION OF SKIN AND TEAR STRAP WERE CUT OUT. THE TEAR STRAP WAS REPAIRED WITH AN INTERNAL ALUMINUM STRAP AND THE SKIN REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 378689-14, REV A.

Part: SKIN — TOOL DAMAGE (FUSELAGE) · airframe 44,094 hrs · 22,134 cycles

WHILE ACCOMPLISHING A DOUBLER MODIFICATION TO THE VHF ANTENNA CUTOUT AT FS 1460, THE SKIN WAS DAMAGED IN MULTIPLE AREAS BETWEEN STRINGERS 28L & 28R. THE DAMAGE WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED BY MODIFYING THE EXTERNAL ALUMINUM ANTENNA DOUBLER TO INCORPORATE THE NEW DAMAGE PER ER/A 378637-14, REV A.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 44,094 hrs · 22,134 cycles

THE FUSELAGE WAS FOUND WITH LIGHTNING STRIKE DAMAGE AT FS 800 BETWEEN STRINGERS 4R AND 5R. THE LIGHTNING DAMAGE WAS CUTOUT OF THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 378696-14, REV A.

Part: SKIN — DENTED (FUSELAGE) · airframe 44,094 hrs · 22,134 cycles

THE FUSELAGE SKIN WAS DENTED AT FS 478 ABOVE STRINGER 17L. THE DAMAGE WAS REMOVED WITH A 4.5 X 4 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 378729-14.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 44,094 hrs · 22,134 cycles

AN EXISTING TIME-LIMITED, BLIND FASTENER REPAIR DOUBLER WAS INSTALLED PREVIOUSLY TO REPAIR A SMALL CUTOUT DUE TO A LIGHTNING BURN AT FS 520 AND STRINGER 8R. THE TEMPORARY REPAIR WAS REMOVED AND ALL REPAIR FASTENERS AND DAMAGED CUTOUT REMOVED WITH A SINGLE 12.5 X 7 INCH CUTOUT. THE NEW CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND SOLID RIVETS PER ER/A 378648-14, REV A.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 44,094 hrs · 22,134 cycles

THE FUSELAGE SKIN NEAR FS 560 BETWEEN STRINGERS 7R AND 8R WAS PREVIOUSLY STRUCK BY LIGHTNING AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER ON A TIME LIMITED BASIS. THE TEMP REPAIR WAS REMOVED, 7.5 X 12 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH A NEW EXTERNAL ALUMINUM PERMANENT REPAIR DOUBLER PER ER/A 378647-14, REV A.

Part: LIGHT — FAILED (COCKPIT)

ELECTRICAL SMELL IN COCKPIT FOLLOWED BY SMOKE COMING FROM FWD GLARESHIELD. PWR REMOVED FROM AIRCRAFT WHICH CAUSED SMOKE TO DISSIPATE. FOUND BRAKE SOURCE LIGHT ASSY BURNED. REPLACED WIRE CONNECTORS AND LIGHT ASSY. NO DAMAGE TO SURROUNDING ASSYS. LIGHT OPS CKS NORMAL. MRR PARTS SENT AND PARTS ROUTED TO ATL DEPT 595 FAA LAISON.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

COMPRESSOR STALL RT ENG. REPLACED ENGINE.

Part: COFFEE JUG — ODOR (GALLEY)

BURNING SMELL AT GALLEY AT DOOR 2L-FORWARD FACING GALLEY. REPLACED FORWARD FACING COFFEE DISPENSER-NO SMELL NOTED-CHKS OK.

Part: BATTERY — DISCHARGED (CABIN)

MID CABIN EMERGENCY FLASHLIGHT WON'T TEST. REPLACED FLASHLIGHT AND BATTERY OP CK OK.

Part: LIGHT — MISSING (CABIN)

EMERGENCY TRACK LIGHT MISSING AT SEAT 3B. REPLACED LIGHT AND LENS.

Part: SLIDE BOTTLE — EMPTY (LT SIDE)

DURING S/C FOUND LEFT OVERWING SLIDE WOULD NOT TEST. FOUND LEFT BOTTLE EMPTY. REPLACED SAME PER MM 25-65-02, SYS TEST OK.

Part: HOUSING CAP — CRACKED (LT FUEL FILTER)

ON CLIMBOUT NOTICED EXCESSIVE FUEL CONSUMPTION ON LEFT ENGINE. FUEL IMBALANCE BECAME EXCESSIVE AND UNCONTROLLABLE, SHUTDOWN LEFT ENGINE AND FUEL CONSUMPTION BECAME NORMAL. FOUND LEFT ENGINE FUEL PUMP MAIN FILTER HOUSING CAP AND FILTER HAD BEEN BLOWN OFF. REPLACED FUEL PUMP AND FUEL CONTROL, OPERATION NORMAL.

Part: RADOME — DAMAGED (NOSE)

RADOME WAS REMOVED FOR MOISTURE. SHOP INSPECTION FOUND OLD REPAIRS TO BE OF WET-LAY REPAIRS. CUT OLD SHELL OFF FROM BASE RING AND REBUILD RADOME COMPLETE PER SRM 53-10-72 USING 757 RADOME MOLD AND BOEING SPEC MATERIAL.

Part: NOSE COWL — DAMAGED (NR 2 ENGINE)

GROUND DAMAGE TO NOSE COWL AT 10 O'CLOCK POSITION. REPAIRED PER SRM 54-11-01.

Part: COWL — DAMAGED (NR 1 ENGINE)

GROUND DAMAGE TO NOSE COWL PANEL WAS FOUND AT 10 O'CLOCK POSITION, DURING HMV. DAMAGE WAS REPAIRED PER SRM 54-11-01 REF 51-70-17.

Part: COWL — DAMAGED (NR 2 ENGINE)

GROUND DAMAGE TO NOSE LIP AT THE 11 O'CLOCK POSITION. REPAIRED PER SRM 54-11-01, FOR NR 2 INTAKE COWL AT SHOP INSPECTION.

Part: TE WEDGE — DELAMINATED (NR 9 LE SLAT)

DURING SHOP INSPECTION, DELAMINATION WAS FOUND ON THE T/E WEDGE OF A NR 9 SLAT. THE WEDGE WAS REPLACED PER SRM 54-43-02.

Part: SKIN — DAMAGED (NR 6 SPOILER)

ON INITIAL SHOP INSPECTION, MAINTENANCE FOUND 2 SMALL HOLES APPROX 1 INCH IN DIAMETER ON BOTTOM SKIN, LOCATED 4 INCHES FROM T/E. REPAIR WAS ACCOMPLISHED PER SRM 57-70-01 FOR NR 6 SPOILER PANEL.

Part: RADOME — PUNCTURED (FWD FUSELAGE)

FOUND DURING LETTER CHECK, RADOME HAS 2 PUNCTURES ON LT SIDE. REPAIRED PER SRM 53-10-72.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

FOUND DURING LETTER CHECK, 2 LIGHTNING STRIKES 1 PREVIOUSLY PAINTED OVER UPPER FUS CROWN AREA 6 FEET FWD VERT STAB. REPAIRED PER SRM 53-00-01. TIME LIMITED REP MUST BE REINSPECTED PRIOR TO 2,500 CYCLES AND REPLACED PRIOR TO 12,OOO CYCLES, E/C INSPD OK AT THIS TIME.