N911DL

Part: BATTERY — DISCHARGED (CABIN) · airframe 78,840 hrs · 61,037 cycles

ROW 10-15 CEILING EMER LIGHT OUT. R+R ROW 10-15 CEILING EMER LIGHT BATTERYS PER AMM 33-53. OPS CHECK GOOD. (LP4814589)

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 78,674 hrs · 60,885 cycles

AFT LEFT LAV SMOKE DETECTOR CHIRPING. REPLACED LEFT AFT SMOKE DETECTOR - CKS OK - REF MD88 AMM 26-17. (LP4698953)

Part: ACOUSTIC LINER — DAMAGED (NR 2 ENGINE) · airframe 78,489 hrs · 60,723 cycles

FLT 2179, RETURNED TO DEPARTURE, DUE TO THE NR 2 ENGINE COMPRESSOR STALL, SHORTLY AFTER TAKE-OFF. MAINTENANCE FOUND DAMAGE TO ACOUSTIC PANELS AND BLEED DUCTS IN COLD STREAM AROUND BLEED VALVES. THE ENGINE WAS REPLACED.

Part: LENS — MISSING (CABIN) · airframe 77,339 hrs · 59,767 cycles

EMERGENCY EXIT SIGNS INOPERATIVE, LOCATIONS 25E, ACARS TEXT FRC25600125E INTERIOR. FOUND OVERWING EXIT DOOR LIGHT UPPER LENS COVER MISSING. INSTALLED NEW COVER. OK FOR SVC.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 76,560 hrs · 59,165 cycles

EMERGENCY LIGHT RED LENS MISSING AT GALLEY AISLE INTERIOR. SECURED THE RED LENS.

Part: FAN — FAILED (RECIRCULATION) · airframe 76,275 hrs · 58,930 cycles

SMOKE AND FUMES DETECTED CLIMBING OUT OF 11,000 FT. DIVERTED. SMOKE ORIGINATED AT ROW 27ABC TO FWD CABIN . FOLLOWED NO GO ODI. TROUBLESHOT IAW AMDS 2120-2367. FOUND CABIN RECIRCULATION FAN NOT RUNNING. ALL THREE CIRCUIT BREAKERS PHASES TRIPPED. REPLACED THE CABIN AIR RECIRCULATION FAN.

Part: PANEL — CORRODED (LAV SERVICE) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON THE AFT LAVATORY SERVICE PANEL. THE LAVATORY SERVICE PANEL WAS REPLACED IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5, AND 51-30-1.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON FLAP HINGE SUPPORT STA XW 251 AT LEFT WING REAR SPAR. LT WING FLAP HINGE SUPPORT FITTING WAS REPAIRED, BUSHING WERE FABRICATED AND INSTALLED PER CMM 27-50-5 PAR 2 I AND HINGE WAS INSTALLED PER AMM 57-40-01-201.

Part: ATTACH BOLT — CORRODED (TE FLAP) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

RUSTED RT FLAP HINGE FITTING ATTACH BOLT STA XW= 251 AT RT WING. RUST WAS REMOVED PER SRM 51-10-03 PARA 26 VOL II AND SERVICEABLE FLAP HINGE AT RT WING STA 251 WAS INSTALLED PER AMM 57-40-01-201.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION AROUND STUD HOLES ON RT WING FLAP HINGE SUPPORT NR 3. DUE TO EXCESSIVE DAMAGE ON HINGE. THE HINGE WAS REPLACED.

Part: SKIN — CRACKED (BS 1418) · airframe 76,124 hrs · 58,812 cycles

TWO CRACKS WERE FOUND OF 0.064" AND 0.096" LENGTH ON THE FUSELAGE SKIN BS 1418, LONGERONS 1 AND 2R. REPAIRED IAW ER/A 559536-14 AD, REV ORG, AND ETI-88-17-200, REV 1.

Part: VANE — CRACKED (LT WING TE FLAP) · airframe 76,124 hrs · 58,812 cycles

CRACK ON UPPER INBD CIRCULAR PANEL AT LT OTBD FLAP OTBD FIXED VANE CIRCULAR PANEL ON TOP SURFACE IAW NRC 00935. THE FLAP OTBD FIXED VANE WAS REPLACED IAW AMM 27-51-03.

Part: SKIN — NICKED (TE FLAP VANE) · airframe 76,124 hrs · 58,812 cycles

NICK ON LOWER SKIN INBD EDGE ON RT OUTBD FIXED GUIDE VANE OUTBD FLAP. RT OUTBD FIXED GUIDE VANE OUTBD FLAP WAS REPAIRED PER SRM 57-03 D PAR 11.

Part: SKIN — CRACKED (LT WING) · airframe 76,124 hrs · 58,812 cycles

CRACKS ON 7 HOLES ON LT WING LWR ACCESS DOOR CUTOUT XRS = 189.0 TO 214.0. CRACKS ON 7 HOLES ON LT WING LWR ACCESS DOOR CUTOUT XRS = 189.0 TO 214.0 WERE REPAIRED PER ETI-88-17-199 REV 1 AND ER/A 559533-14AD REV ORIGINAL WITH LOG 0144928.

Part: PANEL — CRACKED (LE SLAT) · airframe 76,124 hrs · 58,812 cycles

CRACK ON SLAT PANEL NR 3 CENTER HINGE SUPPORT, RT WING. SLAT PANEL NR 3 RT WING WAS REMOVED PER AMM 27-80-01 S/N REMOVED 0022 AND SERVICEABLE SLAT PANEL 3 S/N DL51 RW MUST BE INSTALLED AND ADJUSTED UNDER JIC 2700-4224-RH-03 JOB 000-0003.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER STA Y=234 BTW LONGERON 26-25 RT SIDE AT FWD CARGO COMPARTMENT. PREVIOUS DOUBLER REPAIR STA Y=234 BTWN LONG 26 AND 25 RT SIDE WAS REPLACED AS PERMANENT REPAIR PER ETI- 88-17-203 REV 3 AND ER/A 559546-14 REV ORIG SECTION I.

Part: DOUBLER — WORN (TE FLAP VANE) · airframe 76,124 hrs · 58,812 cycles

WORN LEADING EDGE REPAIR DOUBLER ON RT OUTBOARD FLAP INBOARD GUIDE VANE. RT OUTBOARD FLAP INBOARD GUIDE VANE WAS REPAIRED PER SRM 57-03 D.

Part: SPAR CAP — CRACKED (LT ELEVATOR) · airframe 76,124 hrs · 58,812 cycles

A CRACK OF 4.400" WAS FOUND ON LT ELEVATOR SPAR CAP BETWEEN XE=133.411 AND XE=137.811. LT ELEVATOR SPAR CAP BTW XE=133.411 AND XE= 137.811 WAS REPAIRED PER ETI-88-17-197 REV 3 AND ER/A 559522-14 REV ORG SECTION I PERMANENT REPAIR.

Part: VANE — DELAMINATED (TE FLAP) · airframe 76,124 hrs · 58,812 cycles

HIDDEN DAMAGE DELAMINATION BELOW RUB STRIP ON LT OUTBD FIXED GUIDE VANE INBD FLAP. LT WING INBD FLAP OUTBD FIXED GUIDE VANE WAS REPAIRED PER SRM 57-03 D PARAGRAPH 11 FIG 11.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 76,124 hrs · 58,812 cycles

CRACKS ON THE RT WING LOWER ACCESS DOOR CUTOUT XRS 189 TO 214. REPAIRED IAW ETI-88-17-199, REV 1, AND ER/A 559533-14AD, REV ORIGINAL.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 76,124 hrs · 58,812 cycles

CRACKS ON THE LT WING LOWER ACCESS DOOR CUTOUT XRS 189 TO 214. REPAIRED IAW ETI-88-17-199, REV 1, AND ER/A 559533-14AD, REV ORIGINAL.

Part: DOUBLER — CRACKED (BS 200) · airframe 76,124 hrs · 58,812 cycles

CRACKS (2 EAS) 1)0..250" 2)0.125" WERE FOUND AT EXTERNAL DOUBLER THAT COVERS THE SKIN ADJACENT TO THE UPPER DOOR STOP ADJUST HOLES ON AFTER UPPER DOOR JAMB CORNER AT FWD PASSENGER DOOR BS 200. EXTERNAL DOUBLER THAT COVERS THE SKIN ADJACENT TO THE UPPER DOOR STOP ON AFTER UPPER DOOR JAMB CORNER AT FWD PASSENGER DOOR BS 200 WAS REPAIRED IAWETI-88-17-198 REV.1, AND ER/A 559525-14AD REV. ORIG.

Part: WEB — CORRODED (DOOR STEP) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON WEB ABOVE STEP NR 5 OF VENTRAL STAIRWAY DOOR STRUCTURE AT AFT ACCESSORY COMPARTMENT. THE WEB ON THE STEP WAS REPAIRED IAW SRM 53-01, FIG 4, SHT 4.

Part: CARGO TRACK — CRACKED (BS 1003-1265) · airframe 76,124 hrs · 58,812 cycles

CRACKED CARGO TRACK LT FWD BS 1003 AND 1265. THE CARGO TRACK WAS REPLACED IAW SRM 51-10-4, 51-30-05, 51-30-02, AND 51-10-3 PAR.14, 21, & 38.

Part: INTERCOSTAL — CRACKED (BS 937) · airframe 76,124 hrs · 58,812 cycles

CRACKED INTERCOSTAL BS 937, RBL 7 IN THE RT WHEEL WELL. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-02, 51-30-05, AND DWG:9936368, REV AW.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

PARTS RACK, CORROSION ON INNER INTERCOSTALS (3E/A) AT VENTRAL STAIRWAY MOVABLE CEILING. INTERCOSTAL WERE REPLACED PER SRM 51-30-2 AND DWG 9911993 REV CJ / BW.

Part: DOUBLER — WORN (FUSELAGE) · airframe 76,124 hrs · 58,812 cycles

WEAR ON DOUBLER PRODUCTION OUT OF LIMITS AT LT WW AFT DOOR JAMB STA Y= 941 X=55. REPLACED DOOR JAMB SRM 51-30-2, 51-30-05,51-30-1,51-10-3 PAR. 21 AND 14 DWG 5930584 REV BY.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,124 hrs · 58,812 cycles

CRACKS ON FRAME STA Y=1463 CANT FWD FACE BTW LONGS 17L AND 18L AT AFT ACCESSORY COMPARTMENT. FRAME STA Y 1463 CANT BTW LONGS 17L AND 18L WAS REPAIRED PER SRM 53-01 FIG 2.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORRODED COUNTERSINKS ON FUEL ACCESS PANEL. THE ACCESS PANEL ARE OUT OF LIMITS AND REPLACED IAW SRM 51-22-2A PAR. 6.

Part: FITTING — CORRODED (BS 1271) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON THE FRAME FITTING BS 1271, BETWEEN RBL 54 AND 60. A NEW FITTING INSTALLED IAW SRM 51-30-1 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON COUNTERSINK ON FUEL TANK ACCESS PANEL 1436C. THE ACCESS PANEL FOUND OUT OF LIMITS AND REPLACED IAW SRM 51-22-2A PAR 6.

Part: FRAME — CRACKED (BS 1474) · airframe 76,124 hrs · 58,812 cycles

CRACKED FRAME BS 1474 FWD FACE BETWEEN LONGERONS 17L AND 18L AT AFT ACCESSORY COMPARTMENT. THE FRAME WAS REPAIRED IAW SRM 53-01 FIG. 1.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON UPPER SURFACE ON FUEL TANK ACCES PANEL 1307C. THE ACCESS PANEL IS OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A PAR. 6.

Part: FLOOR SUPPORT — CRACKED (BS 1287-1309) · airframe 76,124 hrs · 58,812 cycles

CRACKS ON FLOOR SUPPORT BL 0, BETWEEN BS 1309 AND 1287. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-2, 51-30-5, AND DWG 9936580, REV BW.

Part: ANGLE — CORRODED (BS 1437-1443) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON INNER ANGLES LT BS 1437 TO 1443, SIDE OF VENTRAL STAIRWAY MOVABLE CEILING. AREA WAS REPAIRED IAW SRM 53-01, FIG 2.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK ON FUEL TANK ACCESS PANEL NR 1409C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, PAR 6, CONDITION III.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK ON THE FUEL TANK ACCESS PANEL NR 1303C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, PAR 6, CONDITION III.

Part: VANE — NICKED (RT WING TE FLAP) · airframe 76,124 hrs · 58,812 cycles

NICKS ON LOWER SKIN AT THE RT INBD FIXED GUIDE VANE INBD FLAP. THE GUIDE VANE WAS REPAIRED IAW SRM 57-03D, PAR 11.

Part: PANEL — CRACKED (LT WING LE SLAT) · airframe 76,124 hrs · 58,812 cycles

CRACKS FOUND ON THE LT WING SLAT PANELS 4 & 3 BOTH AT CENTER HINGES. THE SLAT PANELS WERE REPLACED.

Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · airframe 76,124 hrs · 58,812 cycles

ELONGATE HOLES AND TOOL DAMAGE ON THE FUEL TANK ACCESS PANEL. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, PAR 6.

Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · airframe 76,124 hrs · 58,812 cycles

ELONGATE HOLES AND TOOL DAMAGE ON THE FUEL TANK ACCESS PANEL. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, PAR 6.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 76,124 hrs · 58,812 cycles

CRACK ON UPPER HOLE IN THE HORIZONTAL STABILIZER RT REAR CAP. REPAIRED IAW DWG SR09550027, REV F, AND SRM 51-30-1 , 51-302 AND 51-30-5.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 76,124 hrs · 58,812 cycles

CRACKED FITTING BS 408 UPPER SECTION AT FWD CARGO DOOR. THE FITTING WAS REPLACED IAW SRM 51-30-02, AND 51-30-05.

Part: FERRULE — DAMAGED (FLOOR PANEL) · airframe 76,124 hrs · 58,812 cycles

DAMAGE FERRULES ON FLOOR PANELS NR 465C, 541C,160B, 160E, 256C, 200B, 693C,886C, 1003C, 1003D, 1003. COMPOSITES. FLOOR PANELS NR: 465C, 541C, 160E, 256C, 200B, 693C, 886C, 1003C, 1003D AND 1003E WERE REPLACED FERRULES PER AMM 53-20-01-201. FLOOR PANEL NR 160B WAS REPLACED AND IDENTIFIED PER AMM 53-20-01-201.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 76,124 hrs · 58,812 cycles

CRACKED ANGLE STA Y=408 UPPER SECTION AT FWD CARGO COMPARTMENT DOOR. NEW ANGLE WAS INSTALLED PER SRM 51-30-2 AND 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON RT SEAT TRACK X= 54 BTW STA 1032 TO STA 1036. SEAT TRACK WAS REPAIRED PER 53-05 FIG 4F.

Part: FITTING — CORRODED (CABIN FLOOR) · airframe 76,124 hrs · 58,812 cycles

CORROSION ON FITTINGS, AT FLOOR PANEL 160G. NEW FITTINGS WERE INSTALLED.

Part: VANE — CRACKED (TE FLAP) · airframe 76,124 hrs · 58,812 cycles

CRACK ON TRAILING EDGE STA = XV2 296 FROM RT OUTBD FIXED GUIDE VANE OUTBD FLAP. RT OUTBD FIXED GUIDE VANE OUTBD FLAP WAS REPAIRED PER ER/A 521199-14MA REV ORIG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 76,124 hrs · 58,812 cycles

CRACKED WEB ON STA Y=219 AND X=-45. CUSP WEB WAS REPAIRED PER SRM 51-30-2, 51-30-5, 51-70-4, 51-10-3 PAR 14,21.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON COUNTERSINK ON FUEL TANK ACCESS PLATE NR 1311C. ACCESS PLATE 1311C WAS REPLACED PER SRM 51-22-2A PAR 6 CONDITION II AND SRM 51-10-3 PAR 26.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION BELOW R1 DOOR JAMB X= -55 TO X= -60 AT CABIN PAX. PERMANENT REPAIR ANGLE CUSP WAS ACCOMPLISHED PER SRM 53-05 FIG 55, 51-30-01, 51-30-02, 51-30-05 AND 51-10-03 PAR 14, 21.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON DIAPHRAGM BTW STA Y= 195 TO Y=-200 AND Y=200 TO Y=204 AND X=-56. DIAPHRAGM STA Y=200 TO Y=218, X= -22 TO X =-57 WAS REPLACED AND DIAPHRAGM WAS REPAIRED STA Y= 185 TO Y= 200 AND X=-50 TO X=-57 PER SRM 51-70-04, 53-14-1, 51-30-01, 51-30-02, 51-30-08.

Part: SKIN — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

PREVIOUS BLEND OUT ON EXTERNAL FUSELAGE SKIN STA Y=200 AND Y= 201 LONG 3 RT AT UPPER FUSELAGE. AREA OUT LIMITS ON FUSELAGE SKIN ON STA Y= 200 AND 201 LONG 3 RT WAS REPAIRED PER SRM 53-04-3 FIG 8.

Part: SEAT TRACK — CORRODED (BS 200) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON SEAT TRACK LBL 44, BS 200 IN THE MAIN CABIN. THE SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIG4F, 51-30-5, AND 51-10-3.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 76,124 hrs · 58,812 cycles

CRACKS ON FLOOR PANELS. CRACKS ON FLOOR PANELS 927E, DV1089, AND 313E WERE REPAIRED PER SRM 53-05 FIG131B.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 76,124 hrs · 58,812 cycles

PROTUBERANCE/BENT PRESSURE BULKHEAD SKIN ON STA Y=1338 BTW LONGERONS 28 RT AND 27 RT PROJECTION. PRESSURE BULKHEAD SKIN WAS FOUND ONE CRACK, DAMAGE WAS REMOVED, (HFEC) INSPECTION OK, NO CRACKS ON BULKHEAD SKIN ON STA. Y=1338 BTW LONGERONS 28 RT AND 27 RT PROJECTION ON TRIM OUT PER NDT SPM 06-10-01.001 AND BULKHEAD SKIN WAS REPAIRED PER SRM 53-05 FIG 116.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON FLOOR PANEL NR 160G AT PAX CABIN. FLOOR PANEL WAS REPLACED PER SRM 51-30-2 AND DGW 9957828 REV AB.

Part: CUSP WEB — CRACKED (FUSELAGE) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CRACK ON RT CUSP WEB STA Y= 852 BTW X= - 54 AND X= - 60. REPAIRED PER SRM 53-05 FIG 131 A--13.

Part: DOUBLER — CRACKED (ENTRY DOOR) · airframe 76,124 hrs · 58,812 cycles

HIDDEN DAMAGE, CRACKED PREVIOUS REPAIR DOUBLER ON FWD UPPER CORNER AT MAIN ENTRANCE DOOR ( L1 ). HIDDEN DAMAGE, CRACKED PREVIOUS REPAIR DOUBLER ON FWD UPPER CORNER AT MAIN ENTRANCE DOOR WAS REPLACED PER ER/A 493709 REV ORIGINAL.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON LOWER/UPPER PREVIOUS REPAIR DOUBLER STA Y = 489 BTW X= - 54 AND X= - 60 AT PAX CABIN. DOUBLER WAS REPLACED PER SRM 53-05 FIG.131A-13.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 76,124 hrs · 58,812 cycles

MISSING AND BROKEN FERRULES ON FLOOR PANEL AT PAX CABIN . FERRULES ON FLOOR PANEL WERE REPLACED PER AMM 53-20-01-201 AND FLOOR PANELS WERE FABRICATED PER AMM 53-20-01-201.

Part: FLOORBEAM — CORRODED (BS 197) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON FLOORBEAM BS 197 FROM LBL 43 TO 53.

Part: FLOOR SUPPORT — CRACKED (BS 769-1307) · airframe 76,124 hrs · 58,812 cycles

CRACKED FLOOR SUPPORT BL 0 BETWEEN BS 769 - 788 AND BS 1287 - 1307. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-01, FIG 2.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 76,124 hrs · 58,812 cycles

ELONGATED HOLES ON FLOOR PANEL. DRILLED NEXT OVERSIZE IAW SRM 51-10-4.

Part: ANGLE — CRACKED (BS 1380) · airframe 76,124 hrs · 58,812 cycles

CRACKED REPAIR ON FRAME ANGLE BS 1380 BETWEEN LONGERONS 14L AND 15L. REPLACED IAW SRM 53-14-04, AND 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION OUT OF LIMITS DUE FOUR CRACKS ON REWORKED AREAS LT CUSP WEB AT STA Y=846, Y=862, Y=899 AND Y=905. CUSP WEB AT STA?S Y=846, Y=862, Y=899 AND Y=905 WERE REPAIRED PER SRM 53-05 FIG 131A-1 AND FIG 131A-6, SRM 51-30-02.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 76,124 hrs · 58,812 cycles

CRACK ON RT CUSP WEB STA Y=905 TO 922 X= -54 TO X= -60 AT PASSENGER CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED PER SRM 53-05 FIG 131 A-4.

Part: SKIN — DAMAGED (RUDDER TAB) · airframe 76,124 hrs · 58,812 cycles

EXPOSED MATERIAL ON RUDDER TAB LT SIDE, BOTTOM AT VERTICAL STABILIZER RUDDER. RUDDER TAB LT SIDE, BOTTOM AT VERTICAL STABILIZER RUDDER WAS REPAIRED PER SRM 51-70-1A P 23.

Part: CUSP WEB — CRACKED (BS 348) · airframe 76,124 hrs · 58,812 cycles

CRACKED ON RT CUSP WEB BS 348, BETWEEN RBL 54 AND 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-1.

Part: STRUCTURE — CORRODED (AIR STAIR) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON VENTRAL STAIRWAY NR 11. THE SECTION OF STAIRWAY WAS REPLACED IAW SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 289) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON CUSP WEB BS 289 BETWEEN LBL 54 TO 60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: WEB — CORRODED (BS 469-471) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION OUT OF LIMITS ON LOWER AND UPPER WEB SURFACE FROM BS 469 - 471, RBL 54 TO 60. A NEW REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-05 FIG. 131A-13, 51-30-2, AND 51-10-3 PAR. 38.

Part: PAN — CRACKED (CARGO DOOR) · airframe 76,124 hrs · 58,812 cycles

CRACK ON OUTER PAN BELOW STOP FITTING NR 5 AT FWD CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-05, FIG 50.

Part: LONGERON — CRACKED (BS 1437) · airframe 76,124 hrs · 58,812 cycles

CRACKED LONGERON 12L, BS 1437 AT AFT ACCESSORY COMPARTMENT. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 1437) · airframe 76,124 hrs · 58,812 cycles

CRACKED LONGERON 3L, BS 1437 AT AFT ACCESSORY COMPARTMENT. THE LONGERON REPAIRED IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 1437) · airframe 76,124 hrs · 58,812 cycles

CRACKED LONGERON 16R, BS 1437 AT AFT ACCESSORY. THE SECTION OF THE LONGERON WAS REPLACED IAW SRM 53-14-04, 51-30-02, AND 51-30-05.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON FLOOR PANEL. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-01, FIG 4.

Part: CUSP WEB — CRACKED (BS 868) · airframe 76,124 hrs · 58,812 cycles

CRACKED LT CUSP WEB BS 868 BETWEEN LBL 54 AND 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A, 51-30-02, AND 51-10-03, PAR 14, 21.

Part: CUSP WEB — CORRODED (BS 459) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON CUPS WEB BS 459 BETWEEN LBL 54 TO 60. THE CUPS WEB WAS REPAIRED IAW SRM 53-05, FIG 131A - 13 (SHEET 1).

Part: LONGERON — CRACKED (BS 1437) · airframe 76,124 hrs · 58,812 cycles

CRACKED LONGERON 16L, BS 1437 IN THE AFT ACCESSORY BAY. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-14-4, 51-30-5, AND 51-30-2.

Part: DOUBLER — CORRODED (BS 720) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON CUSP WEB RING DOUBLER AT BS 728 AND RBL 54 - 60. RING DOUBLER WAS REPLACED SRM 53-05 FIG.131A-13.

Part: SKIN — DAMAGED (BS 726-727) · airframe 76,124 hrs · 58,812 cycles

INSPECTION SHOWS MATERIAL THINNING BS 726 - 727 BETWEEN LONGERON 29L & 30R, .041 REMAINING FROM .063.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON LT SEAT TRACK 22 FROM STA Y=1153 TO Y=1154. AREA OUT LIMIT WAS REPAIRED PER SRM 53-05, 51-30-1 AND 51-10-3 PAR 14, 21.

Part: BEAM — CRACKED (PAX DOOR) · airframe 76,124 hrs · 58,812 cycles

CRACKED BEAM NR 8 AFT EDGE AT FWD PASSENGER ENTRANCE DOOR (L1). CRACKED BEAM NR 8 AFT EDGE AT FWD PASSENGER ENTRANCE DOOR WAS REPAIRED PER SRM 52-05 FIG 111.

Part: DOUBLER — CORRODED (APU DOOR) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON PREVIOUS INNER DOUBLERS REPAIR ON APU RIGHT DOOR. INNER DOUBLERS ON APU RIGHT DOOR WERE REPLACED PER SRM 51-30-02, 52-05 FIG 9.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,124 hrs · 58,812 cycles

CRACKED LONG NR 13L ON STA Y=1437 AT AFT ACCESSORY COMPARTMENT. SPLICE AND LONGERON SECTION 13L WERE REMOVED AND NEW SECTION LONGERON AND NEW SPLICE REPAIR WERE DRILLED AND ADJUSTED PER SRM 51-30-2 AND 51-30-5 AND 51-10-4. NEW LONGERON AND NEW SPLICE WERE TREATED AND PAINT PER SRM 51-10-3 PAR 14, 21. SPLICE AND NEW LONGERON AND NEW SPLICE REPAIR WERE INSTALLED PER SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,124 hrs · 58,812 cycles

CRACKED LONG NR 12L ON STA Y=1437 AT AFT ACCESSORY COMPARTMENT. SPLICE AND LONGERON 12L WAS REMOVED AND NEW SECTION LONGERON AND NEW SPLICE REPAIR WAS DRILLED AND ADJUSTED PER SRM 51-30-2 AND 51-30-5, 53-02 FIG18, AND NEW LONGERON AND NEW SPLICE WERE TREATED AND PAINT PER SRM 51-10-3 PAR14,21, SPLICE AND NEW SECTION LONGERON AND NEW SPLICE REPAIR WERE INSTALLED PER SRM 51-30-2, 51-30-5.

Part: SEAT TRACK — CORRODED (BS 642-704) · corrosion level 2 · airframe 76,124 hrs · 58,812 cycles

CORROSION ON THE LEFT SEAT TRACK BS 642 AND 704. REPLACED.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 76,124 hrs · 58,812 cycles

CRACK ON RT CUPS WEB STA Y = 558 BTW X = - 54 AND X= - 60 AT PAX CABIN. RT CUPS WEB STA Y = 558 BTW X = - 54 AND X=- 60 AT PAX CABIN WAS REPLACED PER SRM 53-05 FIG 131A -24 AND DWG 9930538 REV BF.

Part: PAN — CRACKED (FUSELAGE) · airframe 76,124 hrs · 58,812 cycles

CRACKS ON WINDOW RING PAN AT STA Y=1155 FWD FACE (UPPER CORNER) STA Y=1060 FWD FACE (LWR CORNER) AND AT STA Y=845 AFT FACE (LWR CORNER).

Part: PAN — CRACKED (FUSELAGE) · airframe 76,124 hrs · 58,812 cycles

CRACKED WINDOW RING PAN ON UPPER CORNER STA Y=1041 AFT FACE. AREA WAS REPAIRED PER SRM 53-05 FIG 122, 51-30-2 AND 51-30-5 AND ER/A 493648-14MA REV A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,551 hrs · 58,402 cycles

OVERHEAD CABIN EMERGENCY LIGHTS INOPERATIVE FROM ROWS 1 TO 16. REMOVED AND REPLACED THE BATTERY PACKS IAW AMM 33-53. CHECKED GOOD.

Part: PUSHROD — OUT OF ADJUST (CABIN PRESSURE) · airframe 74,876 hrs · 57,901 cycles

BOTH AUTOMATIC CABIN PRESSURIZATION SYSTEMS FAILED AFTER TAKE-OFF. RETURNED TO DEPARTURE. PERFORMED BITE ON BOTH AUTO PRESSURE CONTROLLERS IAW AMM 21-32. BOTH HAVE AN AC MOTOR FAULT. FOUND INTERMITTENT AUTO PRESSURE INOPERATIVE, 1 AND 2 WHEN NOZZLE VALVE REACHES FULLY CLOSED POSITION. FOUND NOZZLE VALVE CAME TO STOP BEFORE ACTUATOR REACHED THE STOP POSITION. ADJUSTED NOZZLE VALVE PUSH ROD. OPS CHECKED GOOD.

Part: SPAR — CRACKED (WING) · airframe 74,374 hrs · 57,552 cycles

WING REAR SPAR CRACKING AT XRS 164, REPAIRED IAW 5710-01110, SECT 06.

Part: TAB — DAMAGED (RUDDER) · airframe 74,199 hrs · 57,406 cycles

RUDDER CONTROL TAB HAS FLAME SPRAY MISSING IN CRITICAL AREAS. REMOVED AND REPLACED RUDDER CONTROL TAB PER WORK CARD 2720-4321.

Part: STRUCTURE — MISSING (RUDDER) · airframe 74,199 hrs · 57,406 cycles

RUDDER HAS FLAME SPRAY MISSING IN CRITICAL AREAS. REMOVED AND REPLACED RUDDER PER WORK CARD 2720-4421 OK FOR SERVICE.

Part: LANYARD — BROKEN (L1 DOOR SLIDE) · airframe 73,829 hrs · 57,113 cycles

L1 DOOR SLIDE PARACHUTE PIN BREAK AWAY CORD BROKEN. REPLACED LACE CORD IAW CMM 25-66-16.

Part: LANYARD — MISROUTED (TAILCONE SLIDE) · airframe 73,820 hrs · 57,108 cycles

DURING TAIL CONE SLIDE INSTALLATION, FOUND LANYARD INCORRECTLY ROUTED AT CAM RELEASE MECHANISM. ROUTED OF LANYARD IAW AMM 53-53-00.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,471 hrs · 57,619 cycles

FWD L1 DOOR DRAIN PAN SUPPORT IS CORRODED. REPLACED FLOOR SUPPORT REF SRM 51-01 PG 1 PAR 2D.

Part: BULKHEAD WEB — CRACKED (BS 1485) · airframe 73,813 hrs · 57,105 cycles

TAIL INTERIOR BS 1485 BULKHEAD WEB CRACKED JUST BELOW LT VENT BOX. REPAIRED IAW PRI 548124-14 REV 0 AND COMPLIED WITH ERA 548124-14 REV ORIG.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 73,759 hrs · 57,065 cycles

EMERGENCY LIGHT AT SEAT 22 INOPERATIVE. FOUND HARNESS FROM LIGHT TO SIDEWALL BROKEN AT SIDEWALL SIDE. REPLACED HARNESS. CHECKS GOOD. REF AMM 33-53.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 73,160 hrs · 56,624 cycles

CREW REPORTED CAPTAIN'S L-1 WINDSHIELD CRACKED ON TAKEOFF SO THE FLIGHT RETURNED TO DEPARTURE. MAINTENANCE R & R THE CAPATIN'S L-1 WINDSHIELD AND WINDOW HEAT CONTROLLER IAW THE AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,453 hrs · 56,124 cycles

MAINTENANCE FOUND THE EMERGENCY SIGNS INOPERATIVE IN FIRST CLASS. THE BATTERIES WERE REPLACED. THE EMERGENCY LIGHTS CHECKED OK.

Part: SKIN — DAMAGED (BS 389) · airframe 73,160 hrs · 56,624 cycles

FUSELAGE SKIN LIGHTNING STRIKE DAMAGE AT BS 389 AND S-29R. DAMAGE WAS CUTOUT AND AN EXTERNAL DOUBLER INSTALLED IAW SECTION I OF ER/A 531742-14, REV ORIGINAL.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 69,846 hrs · 54,340 cycles

DURING WALK AROUND, FOUND EVIDENCE OF POSSIBLE LIGHTNING STRIKE ON THE RT ELEVATOR OTBD T/E. INSPECTED ELEVATOR FOUND LIGHTNING DAMAGE TO OTBD T/E. REPAIRED RT ELEVATOR OTBD T/E IAW ER/A 531740-14, REV ORIGINAL.

Part: SKIN — DAMAGED (BS 390) · airframe 69,852 hrs · 54,343 cycles

LIGHTNING STRIKE AT BS 390, 28R. DRILLED OUT DAMAGED AREA IAW PRI 531742-14, REV 0.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 69,421 hrs · 54,042 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT SEATS 15D & 20D WERE INOPERATIVE. MAINTENANCE REPLACED THE CONNECTOR IN THE WIRE HARNESS AT EACH SEAT AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 69,421 hrs · 54,042 cycles

DURING A LINE CHECK, MAINTENANCE FOUND THAT THE CENTER EMERGENCY LIGHT FOR THE CATWALK IN THE TAIL WAS INOPERATIVE. MAINTENANCE FOUND A WIRE BROKEN AT THE TERMINAL END. THE WIRE WAS REPAIRED AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 68,527 hrs · 53,402 cycles

DURING CHECK, MAINTENANCE FOUND THE TAILCONE RELEASE CABLE HAS A WORN SPOT WITH NUMEROUS BROKEN STRANDS. MAINTENANCE R & R THE TAILCONE RELEASE CABLE.

Part: DOOR FRAME — CORRODED (BS 370-427) · airframe 68,511 hrs · 53,391 cycles

FWD CARGO LOWER DOOR FRAME HAS COROSSION ON OUTER SURFACE IN SEVERAL AREAS BETWEEN BS 370-427. REPAIRED AREAS IAW ER/A 525958-14, REV ORIGINAL.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 67,122 hrs · 52,399 cycles

DURING EDDY CURRENT INSPECTION ON THE RT UPPER SKIN OF THE HORIZONTAL STABILIZER. A CRACKED FASTENER HOLE WAS IDENTIFIED ON THE UPPER RT AFT SKIN PANEL IAW ER/A 333575-14AD REV B.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,502 hrs · 51,242 cycles

DURING LINE CHECK, MX FOUND 3 ROWS OF THE OVERHEAD EMERGENCY PATHWAY LIGHTING TO BE INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 64,756 hrs · 50,719 cycles

CAPTAIN`S CLEARVIEW WINDOW CUTOUT UPPER AFT CORNER. WORK ACCOMPLISHED PER ER/A 509227-14 REV, ORIG REPAIR AT BS 133.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 76,124 hrs · 58,812 cycles

ERA 493715-14 REV B SECTION VII REPEAT INSPECTIONS ISSUED FOR BLENDOUTS AT STATION 1060-1079. FOLLOW ON ACTION IS REQUIRED. PERMANENT REPAIR ON WINDOW BELT PANEL STA Y=1060-1076 WAS ACCOMPLISHED PER ETI-88-17-195 AND ERA 559557-14 AD REV ORIG SECTION 1 AND ER/A 493715-14 REV C SEC XIII.

Part: COFFEEMAKER — INOPERATIVE (GALLEY) · airframe 64,413 hrs · 50,482 cycles

THE F/A REPORTED A BURNING WIRE ODOR IN THE GALLEY. THE QRH WAS COMPLIED WITH AND THE GALLEY POWER WAS SECURED. THE SMELL STOPPED ONCE THE POWER WAS TURNED OFF. NO VISIBLE SMOKE OR FLAME WAS EVER SEEN. MX FOUND THE LOWER COFFEEMAKER IN THE FWD GALLEY INOPERATIVE WITH ITS CIRCUIT BREAKER TRIPPED AND REPLACED IT.

Part: SKIN PANEL — WORN (VERTICAL STAB) · airframe 64,053 hrs · 50,223 cycles

VERTICAL STABILIZER LEADING EDGE SKIN UPPER REMOVABLE PANEL LOWER EDGE WEAR DAMAGE 484644-14.

Part: UNKNOWN — FUMES (COCKPIT & CABIN) · airframe 63,708 hrs · 49,977 cycles

CREW DIVERTED THE AIRCRAFT TO A SAFE LANDING AT IAD DUE TO FUMES IN CABIN AND COCKPIT DURING CLIMB-OUT. NO VISIBLE SMOKE AND ODOR SMELLED OF ENGINE EXHAUST AND WAS NOT ELECTRICAL. ODOR WAS WORSE AT HIGHER POWER SETTINGS. MAINTENANCE INSPECTED BUT NO LEAKS WERE LOCATED. PNEUMATIC SYSTEM TROUBLESHOOTING CHECKED GOOD. A DUCT SYSTEM BURNOUT WAS PERFORMED AND THE WATER SEPARATOR BAGS WERE REPLACED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,190 hrs · 49,602 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY ESCAPE LIGHTING IN THE GALLEY WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 62,753 hrs · 49,321 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 36E IN THE CABIN, WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY CONNECTORS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,661 hrs · 49,268 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE VENTRAL STAIRWAY WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS (B-25-28 & B5-27) AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 61,329 hrs · 48,275 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY EXIT SIGN LIGHTS VERY DIM ABOVE BOTH AFT OVERWING EXIT HATCHES. MAINTENANCE REPLACED CHARGER AND BATTERIES PER M/M 33-53-00. OPERATION OF LIGHTS NOW CHECKS OK.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 61,290 hrs · 48,252 cycles

ELONGATED HOLE ON FWD CARGO COMPT AFT DOOR JAMB BEAM UNDER MATERIAL COMPOUND STOP. REPAIR PER ERA 493724-14 REV ORG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,290 hrs · 48,252 cycles

CRACK ON AFT ACC COMPT FRAME CAPS STA Y-1437 AND LONG 2 RT. REPAIRED IAW ERA 493717-14 REV ORG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,290 hrs · 48,252 cycles

CRACK ON AFT ACC COMPT FRAME LOWER CAP STA Y-1437 AT LT/RT VERTICAL STABILIZER FRONT SPAR FITTINGS. REPAIRED PER ERA 493717-14 REV ORG.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,290 hrs · 48,252 cycles

CRACK ON WEB AT AFT ACCESSORY COMPARTMENT STA Y-1437 BTW LONG 1 AND 2. REPAIRED IAW ERA 493717-14 REV ORG.

Part: BELT — DAMAGED (FUSELAGE) · airframe 61,290 hrs · 48,252 cycles

LIGHTNING STRIKE ON FWD LOWER CORNER OF WINDOW BELT FRAME STA Y-1060-1079 AT FUSELAGE SKIN. REPAIRED AREA PER ERA 493715-14 REV ORG.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 61,289 hrs · 48,251 cycles

SCATCHES AT LOWER AFT CORNER OF CABIN WINDOW CUTOUT AT LT Y-275-294, Y-351-370, Y-579-598 AND Y-750-769. REPAIRED AREAS IAW ERA 493714-14 REV ORG AND ERA 493715-14 REV ORG.

Part: BELT — DAMAGED (FUSELAGE) · airframe 61,289 hrs · 48,251 cycles

LIGHTNING STRIKE ON UPPER AFT CORNER OF WINDOW BELT STA Y-674-693 AT FUSELAGE SKIN. REPAIRED WINDOW BELT IAW ERA 493713-14 REV ORG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,289 hrs · 48,251 cycles

CORROSION ON MID CARGO COMPT INTERNAL PRODUCTION DOUBLER STA 690 TO 726 BETWEEN LONGERONS 30 AND 29 RT. REPAIRED IAW ERA 493722-14 REV A.

Part: BEAM — CORRODED (FUSELAGE) · airframe 61,289 hrs · 48,251 cycles

CORROSION ON MID CARGO COMPT LWR DOOR JAMB BEAM REPAIR STRAP BTW STA 642-687. REPAIRED PER SRM 51-30-5.

Part: BEAM — CORRODED (FUSELAGE) · airframe 61,289 hrs · 48,251 cycles

RUSTED MID CARGO COMPT LWR DOOR JAMB BEAM REPAIR DOUBLER FROM STA 639-690. REPAIR PER SRM 53-05.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,289 hrs · 48,251 cycles

CORROSION ON INNER FUSELAGE SKIN FROM STA 724-737 BETWEEN LONG 29RT AND STA 737 BETWEEN LONG 27RT AND 28RT IN C2. REPAIRED IAW ERA 493722-14 REV A.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,289 hrs · 48,251 cycles

DENTS ON PREVIOUS PERMANENT REPAIR STA Y=295 AND BTW LONGS 19RT-20RT ALSO STA Y=313 AND BTW LONGS 18RT-19RT AT FUSELAGE OUTER SKIN. REPAIRED PER AMR 0953863 REV 6.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 61,289 hrs · 48,251 cycles

DAMAGE TO L1 DOOR IN AFT LOWER CORNER. REPAIRED PER AMR 0952167.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,289 hrs · 48,251 cycles

DAMAGED HOLE WAS FOUND BETWEEN STR 12 AND 15 AT STA 210.75 AT RT LOWER ACCESS DOOR CUTOUT. REPAIRED PER ERA 493100-14AD REV ORG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,289 hrs · 48,251 cycles

DAMAGED FUSELAGE SKIN PREVIOUS REPAIR BTW STA Y250- 260 AND BTW LONGERONS 20RT-22RT. REPAIRED SKIN IAW ERA 493705-14 REV ORG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 61,289 hrs · 48,251 cycles

CORROSION ON MID CARGO COMPT LOWER DOOR JAMB LOWER SURFACE AND OUTBOARD EDGE Y=631-645. REPAIRED PER ERA 493703-14 REV ORG.

Part: SKIN — DEFORMED (FUSELAGE) · airframe 61,289 hrs · 48,251 cycles

DEFORMED PREVIOUS REPAIR INTERNAL DOUBLER STA Y-260 BTW LONGERONS 28LT AND 29LT AT FWD CARGO COMPT. REPAIRED PER ERA 271965-14 REV A.

Part: BEAM — CORRODED (FUSELAGE) · airframe 61,289 hrs · 48,251 cycles

CORROSION ON MID CARGO COMPT DOOR JAMB BEAM SET SCREW HOLES STA Y-655 AND 674. REPAIRED PER SRM 53-05.

Part: BELT — DAMAGED (FUSELAGE) · airframe 61,289 hrs · 48,251 cycles

LIGHTNING STRIKE ON FWD LOWER CORNER OF WINDOW BELT FRAME STA Y=1060-1079. REPAIRED PER ERA 493715-14 REV ORG.

Part: LINE — LEAKING (HYDRAULIC SYSTEM) · airframe 60,463 hrs · 47,743 cycles

INBOUND CREW HAD RT FLUID DROP BELOW 9 QUARTS, THEY FOLLOWED QRH AND LANDED AT 5 QUARTS. MX DISCOVERED HYD LEAK FLUID INGESTED INTO APU. CABIN FILLED WITH SMOKE. MX REPAIRED LEAKING HYD LINE. CLEANED APU INLET AND PERFORMED PACK BURN OUT IAW AMM 21-20-02. COALESCER BAGS WERE REPLACED. ACFT OK FOR SERVICE.

Part: SHUTOFF VALVE — LEAKING (RUDDER) · airframe 60,007 hrs · 47,456 cycles

SOON AFTER GEAR EXTENSION ON APPROACH THE CAPTAINS' SIDE AFTLAVATORY SMOKE DETECTOR WENT OFF. A THIN WHITE HAZE WAS VISIBLE THOUGH OUT THE CABIN ALTHOUGH THE SMELL WAS WORSE INTHE AFT CABIN. THE FLIGHT ATTENDANTS DESCRIBED THE SMELL AS AN ELECTRICAL IN NATURE. MAINTENANCE ACCOMPLISHED OPN 5088 AND TROUBLESHOT FOR SMOKE/ODOR. APU WAS CONTAMINATED WITH HYDRAULIC FLUID. OPN 5090 ALT DUCT BURN OUT ACCOMPLISHED.MAINTENANCE FOUND RUDDER SHUT OFF VALVE LEAKING FLUID. VALVE WAS REPLACED WITH BORROWED PART FROM AMERICAN AIRLINES. (2010-D1373) (DLM88103220)

Part: LIGHT — MISSING (CABIN) · airframe 59,724 hrs · 47,241 cycles

DURING LINE CHECK, MX FOUND EMERGENCY LIGHT IN AIR STAIR MISSING. MX INSTALLED LIGHT ASSY AND OPERATION OF LIGHT NOW CHECKS GOOD.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,690 hrs · 47,222 cycles

DURING LINE MX, FOUND EMERGENCY PATH LIGHT AT 30D INOPERATIVE. MX REPLACED LIGHT HARNESS AT 30D. OPERATION OF LIGHT NOW CHECKS OK.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,408 hrs · 47,007 cycles

FUSELAGE C-3 DOOR SURROUND SKIN INTERNAL DOUBLER CORROSION. REPAIRED IAW ERA 484722-14.

Part: SKIN — WORN (VERTICAL STAB) · airframe 59,408 hrs · 47,007 cycles

VERTICAL STABILIZER/ L/E SKIN UPPER REMOVABLE PANEL LOWER EDGE WEAR DAMAGE.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 59,114 hrs · 46,811 cycles

THE PILOTS FOUND THE EMERGENCY EXIT PATH LIGHTS IN THE LAST SIX ROWS TO BE INOPERATIVE. MAINTENANCE REPLACED THE AFT EMERGENCY LIGHT POWER SUPPLY FUSE. AN OPS CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 58,376 hrs · 46,276 cycles

SEAT 20E PATHWAY LIGHT INOP. REMOVED AND REPLACED LIGHT HARNESS, CHECKS GOOD.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 57,910 hrs · 45,973 cycles

FUSELAGE MAIN FRAME OVERWING FRAMES REPAIRED IAW EA 09-460094-12, ME01.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 56,702 hrs · 45,191 cycles

AFTER T/O LEFT MAIN RED REMAINED ILLUMINATED W/GEAR LEVER UP, ALL OTHER INDICATION IND NORMAL. CYCLED GEAR PER QRH NO HELP PUT GEAR DOWN FOR RETURN IND NORMAL. FOUND LT MLG UP PROX SENSOR OUT OF ADJUSTMENT. REPLACED SENSOR IAW AMM 32-60-05-201. OPS CHECK GOOD

Part: SKIN — CRACKED (BS 645 L30) · airframe 54,886 hrs · 43,948 cycles

FUSELAGE SKIN FOUND CRACKED AND BULGED AT STA 645 AND L30. DAMAGE WAS TRIMMED OUT. WHILE TRIMMING ADDITIONAL DAMAGE WAS FOUND TO THE INTERNAL DOOR SURROUND DOUBLER AT STA 626. TOOLING DAMAGE AT HOLES LOCATED AT STA 629. THE SKIN WAS REPAIRED BY SPLICING A NEW SECTION PER SRM 53-04 FIG 12C, INTERNAL DOUBLER WAS REPAIRED BY INSTALLING AN INTERNAL REPAIR DOUBLER. OVERSIZED HOLES WERE REPAIRED BY INSTALLING OVERSIZED FASTENERS.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 53,028 hrs · 42,713 cycles

IRR/FLAPS WOULD NOT DEPLOY BEYOND 11 DEGREES DURING APPROACH. COMPLIED WITH QRH DIVERT TI JFK SOFT TOUCHDOWN. LEFT FLAPS AT 11 DEGREE POSITION FOR SHUTDOWN. CYCLED FLAPS TO UP THEN TO 28 FLAPS OPERATE NORMAL. RAN BOTH ENGINES FOR 15 MINS WITH FLAPS UP. ALL FLAP ACTUATORS COLD. PERFORMED BYPASS TEST ON ALL FLAP ACT. ALL OPS NML. OK FOR SVC. ALL RII CKS OK.

Part: STOP FITTING — UNKNOWN (CARGO DOOR) · airframe 51,857 hrs · 42,003 cycles

CARGO DOOR, FWD, MID, AFT STOP PAD SUPPORT FITTING REPLACED IAW EA 09-451701-12, ME09, ME10, ME11.

Part: MODULE — UNSERVICEABLE (HYD SYSTEM) · airframe 51,469 hrs · 41,750 cycles

AFTER TAKEOFF PASSING THRU 8000 FT TURNED OFF RT ELEC PUMP AND AUX PUMP, LT HYD PRESS DROPPED TO ZERO AND QTY TO 1. C/W QRH CKLIST AND TURNED OFF LT ENG PUMP APPROX 2 MINS LATER. FOUND POP OUT IND HOUSING IN LT SYS PRESS MODULE OFF OF MODU REPLACED FILTER HOUSING PER AMM. SEE ITEM 13 FOR PUMP AND FILTER CHECK. NDS LEAK CK 624270. LEAK CK GOOD. PERFORMED HY SYS CK AND RESERVICE FOLLOWING IN-FLIGHT FLUID LOSS PER AMM. REMOVED AND REPLACED NR 1 HYD EDP PER AMM 278549. REPLACED PRE RETURN AND CASE DRAIN FILTERS 278549. LEAK CK GOOD.

Part: FITTING — GOUGED (LT MLG) · airframe 49,631 hrs · 40,516 cycles

LEFT MLG SUPPORT FITTING COMMON TO THE LT MLG RETRACT ACTUATOR SUPPORT FITTING HAS TOOLING DAMAGE. THE BORE WAS OVERSIZED TO REMOVE THE DAMAGE AND AN OVERSIZED BUSHING WAS INSTALLED. REF AD 2004-25-14.

Part: WIRE HARNESS — DAMAGED (SEAT 2CD) · airframe 47,669 hrs · 39,020 cycles

ON INSPECTION, FOUND EMERGENCY TRACK LIGHT OUT SEAL 2CD. REPLACED LIGHT HARNESS.

Part: TRANSMITTER — LEAKING (RT RESERVOIR) · airframe 47,355 hrs · 38,774 cycles

RIGHT HYD QTY GAUGE DROPPED TO ZERO AFTER DEPARTURE FROM ATL. REPLACED HARDWARE ON RT RESERVOIR TRANSMITTER.

Part: PSEU — MALFUNCTIONED (MLG) · airframe 47,251 hrs · 38,705 cycles

AIR TURNBACK DUE TO LEFT GEAR UNSAFE LIGHT WHEN HANDLE RAISED. CYCLED GEAR WITH NO HELP. NO FAULTS FOUND ON PSEU. CYCLED GEAR SEVERAL TIMES, ALL IND CHECKS GOOD. REPLACED PSEU AND D1-26 UPLOCK PROX SENSOR LEFT GEAR, ALL CHECKS GOOD.

Part: HYDRAULIC LINE — CRACKED (LT ENGINE) · airframe 45,786 hrs · 37,691 cycles

DURING CLIMBOUT LT HYD QTY DECREASED TO 1 QUART. REPLACED NUMBER 1 ENGINE HYD PUMP SUPPLY LINE.

Part: GENERATOR — DISCHARGED (SEAT 11ABC OXY) · airframe 45,207 hrs · 37,302 cycles

WHILE CLOSING PSU AT SEAT 11ABC THE O2 GENERATOR FIRED INADVERTENTLY. REPLACED GENERATOR.

Part: FAN — MALFUNCTIONED (COCKPIT) · airframe 43,537 hrs · 36,163 cycles

AFTER TURNING OFF RUNWAY A HOT ODOR AND HAZE OF SMOKE WAS NOTICED WITH A GRINDING NOISE FROM FEET AREA ON F/O SIDE ODOR AND HAZE DISSIPATED DURING TAXI IN. FOUND INSTRUMENT COOLING FAN SOURCE OF NOISE AND ODOR DEACTIVATED COOLING FAN PER MEL. NO DAMAGE NOTICED IN AREA.

Part: CHARGER — MALFUNCTIONED (E/E COMP) · airframe 43,384 hrs · 36,058 cycles

AFTER PDC AND CREW WALKAROUND, RAMP NOTED SMOKE (ACTUALLY STEAM) FROM E&E DOOR AREA. DISCOVERED SHIPS BATTERIES IN OVERHEATED STATE AND BATTERY CHARGER FAIL IN HIGH CHARGER MODE. REPLACED BATTERY & CHARGER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 42,877 hrs · 35,697 cycles

CORROSION WAS FOUND ON THE FUSELAGE SKIN AT FS 712 BETWEEN LONGERONS 29L & 30. THE CORROSION WAS REMOVED WITH A SKIN CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 087519-14.

Part: FLOOR PANEL — PUNCTURED (C5 CARGO) · airframe 41,923 hrs · 35,071 cycles

ON ARRIVAL IAD FOUND HOLE IN FLOOR OF NR 5 BAG BIN. REPAIRED PER DRD 5305D.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 41,861 hrs · 35,033 cycles

ON POWER DOWN EMERGENCY EXIT LIGHTS STAY ON. REPLACED POWER SUPPLY.

Part: SKIN — CORRODED (FS 650, L-30) · airframe 39,939 hrs · 33,696 cycles

FUSELAGE / SKIN / FS 650 / L29-30 : CORROSION NEAR ANTENNA CUTOUT THE FUSELAGE SKIN WAS FOUND WITH A CORROSION BULGE AT AN EXISTING ANTENNA CUTOUT AT FS 655 AND LONG. 30. THE CORROSION WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383678 -14, REV A.

Part: SPAR — DAMAGED (LT WING) · airframe 39,897 hrs · 33,658 cycles

PERMANENT REPAIR FOR DAMAGE TO THE LT WING FRONT SPAR. DAMAGE RESULTED IN SPLICING IN NEW SECTION OF LOWER WING SKIN AT XRS540, SPLICING LOWER SPAR CHORD AT XFS 563 AND LEADING EDGE REPAIR AT XFS 596.

Part: SLIDE — DEPLOYED (R1 DOOR) · airframe 38,736 hrs · 32,838 cycles

DURING CATERING OF SHIP 911 FOR FLT 1444/14, THE R1 DOOR SLIDE WAS DEPLOYED. CATERING STATES THAT WHEN THE DOOR WAS OPENED THE GIRT BAR CAUGHT ON THE INSIDE OF THE DOOR FRAME, HINGE SIDE PULLED THE SLIDE FROM THE BUSSLE WHERE IT THEN FELL ON TO THE CATERING TRUCK AND THEN FELL TO THE GROUND WHERE THE BOTTLE ACTIVATED AND THE SLIDE INFLATED BETWEEN THE AIRCRAFT AND THE FRONT OF THE CATERING TRUCK. NO INJURIES WERE REPORTED NOR DAMAGE TO THE AIRCRAFT OR CATERING TRUCK. REPLACED SLIDE.

Part: THROTTLE CABLE — OBSTRUCTED (NR 2 ENGINE) · airframe 36,552 hrs · 31,167 cycles

RIGHT THROTTLE STUCK AT 79 PERCENT COULD NOT RETARD BELOW THAT SETTING. SHUT DOWN THE ENGINE. REMOVED OBSTRUCTION FROM TAIL COMPARTMENT QUADRANT, CHECKS OK.

Part: CSD — OVERTEMP (NR 1 ENGINE) · airframe 35,743 hrs · 30,589 cycles

LEFT CSD OUTLET TEMP HIGH, ABOVE RED LINE 180 DEGREES. PERFORMED DISCONNECT IN FLT. REPLACED NR 1 ENG CSD AND GEN PER M/M. OP AND LEAK CKS GOOD.

Part: INTAKE DUCT — CONTAMINATED (APU) · airframe 35,736 hrs · 30,585 cycles

WHILE AT CRUISE ALTITUDE FL 330 PILOTS DETECTED SMOKE AND FUMES IN THE COCKPIT. EMERGENCY DESCENT INITIATED INTO JAX. CLEANED APU INLET. PERFORMED DUCT BURNOUT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,534 hrs · 29,662 cycles

JUMP SEAT 1L FWD FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED BATTERY.

Part: UNKNOWN — ODOR (CABIN)

SHORTLY AFTER T/O THERE WAS A HOT SMELL IN THE COCKPIT FOLOWED BY A CALL FROM THE AFT F/A ATATING THAT THE CAPT. SIDE AFT LAV SMOKE ALARM WAS GOING EXPERIENCED ODOR, A SHORT TIME LATER THE RIGHT AFT LAV SMOKE ALARM WENT OFF. BEFORE THE APPROACH STARTED, BOTH ALARMS STOPPED AFTER BEING ON FOR A LONG TIME. THEN BOTH ALARMS CAME BACK ON. F/A REPORTED A BURNING SMELL, BUT NO VISIBAL SMOKE. AFTER LANDING, THE MID F/A SMELLED AN ELECTRICAL ODOR. REPLACED COALESCER BAGS. PERFORMED DUCT BURNOUT. CHECKED ACM FOR LEAKS, NONE FOUND. RAN ENGINES.

Part: UNKNOWN — SMOKE (CABIN)

SMOKEY SMELL OCCURRED AT 3500 FT WHILE ON APPROACH. SMOKE DETECTOR IN LT AFT LAV ACTIVATED, PWR SETTINGS WERE VARING GREATLY DUE TO STRONG GUSTY WINDS. SMELL DISSIPATED ON LAND. RAN ACFT TO T/O PWR AND VARIOUS PWR SETTINGS, NO PROBLEMS NOTED. ACFT OK FOR SVC.

Part: APU — LEAKING (APU)

DURING FLT, BURNING ODOR WAS NOTICED IN CABIN AND AFT LAV SMOKE DETECTOR WENT OFF. A/C RETURNED TO DEN. SUSPECT LEAK IN APU SYSTEM. DEACTIVATED APU. PERFORMED DUCT BURN-OUT PER MM. REPLACED COALESCER BAGS.

Part: SKIN — DENTED (BS 218)

THE FUSELAGE SKIN WAS FOUND DENTED AT FS 218 AND STRINGER 19L. THE DAMAGE WAS REPAIRED PER ERA 333534-14 AT HMV.

Part: SKIN — DENTED (BS 228)

GROUND DAMAGE WAS DISCOVERED TO THE FUSELAGE SKIN AT FS 228 BETWEEN STRINGERS 17L AND 18L. THE DAMAGE WAS REPAIRED AT HMV PER ERA 333535-14.

Part: SKIN — CRACKED (HORIZ STAB)

THE UPPER, AFT SKIN PANEL OF THE HORIZONTAL STABILIZER WAS FOUND CRACKED DURING AN INSPECTION BY EO 9-61905-3AD, (LT AND RT) THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333575-14AD.

Part: INLET — CONTAMINATED (APU)

ON FINAL APPROACH WITH AIRSPEED AT 150 KTS THE F/A AND PILOTS SMELLED A HOT ODOR WITH BOTH ENG AND WING A/I ON. SMELL DISSIPATED WHEN WING A/I TURNED OFF. FOUND OIL ON APU INLET. PERFORMED DUCT BURNOUT.

Part: ANGLE — CRACKED (BS 1463)

THE RT VERTICAL STABILIZER-TO-FUSELAGE ATTACH ANGLE WAS FOUND WITH A 1.5 INCH CRACK AT FS 1463. THE CRACK WAS ROUTED OUT AND A STEEL REPAIR ANGLE INSTALLED PER ER/A 366856-14, REV A.

Part: BATTERY — DISCHARGED (CABIN)

JUMPSEAT 1L FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED FLAHSLIGHT BATTERY AND BULB.

Part: COALESCER — DIRTY (CABIN)

AFT LAV SMOKE DETECTOR ACTIVATED ON SHORT FINAL. ENG AND AIRFOIL A/I HAD BEEN TURNED ON PASSING 15,000 FT AND TURNED OFF PASSING 2,000 FT. BURNING ODOR WAS NOTICED BUT NO SMOKE. REPLACED WATER BAGS, OPERATED PACKS NO ODORS NOTICED.

Part: SKIN — DENTED (BS 237)

THE FUSELAGE SKIN WAS BADLY DENTED AT FS 237 BETWEEN STR 17L AND 18L. STRINGER 17L WAS CRACKED AND THE FS 237 FORMER WAS CRACKED AND BUCKLED. THE STRINGER AND FRAME WERE REPAIRED PER THE SRM. THE SKIN DAMAGE WAS CUTOUT AND REPAIRED WITH AN EXTERNAL REPAIR DOUBLER AND INTERNAL FATIGUE DOUBLER PER ER/A 364128-14. DAMAGE WAS CAUSED BY GROUND EQUIPMENT IMPACT.

Part: LIGHT — FAILED (CABIN)

EMERGENCY FLOOR TRACK BULB FWD OF 31D INOP. REPLACED LIGHT FIXTURE, CKS OK.

Part: STRUT — REQD SERVICE (NLG)

AFTER TAKEOFF, NOSE GEAR UNSAFE LIGHT ILLUMINATED, AIR NOISE FROM NOSE GEAR AREA. DISASSEMBLED NOSE STRUT, FOUND THREE PINTS OF WATER AND ICE INSIDE STRUT. CLEANED STRUT, INSTALLED NEW SEALS, SERVICED PER MM AND OPERATION NORMAL.

Part: SKIN — PUNCTURED (FS 229-294)

THE LT LOWER FORWARD FUSELAGE WAS PUNCTURED BY GROUND EQUIPMENT RESULTING IN DAMAGE TO THE SKIN, FRAMES, AND STRINGERS AT FS 229-294. ACCOMPLISHED REPAIRS PER DL ERA 271965-14.

Part: EEL — INOPERATIVE (AFT STAIRS)

DURING INSPECTION, AFT AIRSTAIR EMERGENCY LIGHT FOUND INOP. REPLACED LIGHT ASSEMBLY, OPERATION NORMAL.

Part: PNEUMATIC SYSTEM — ODOR (CABIN)

DURING CRUISE, HAD SMOKE AND ODOR IN CABIN AFTER ANTI ICE WAS TURNED ON. DIVERTED TO TYS SMOKE DISSIPATED WHEN ANTI ICE WAS TURNED OFF. CHECKED APU AND ENGINE OIL QTY. FOUND NORMAL. PERFORMED DUCT BURN-OUT PROCEDURES, RETURNED TO SERVICE.

Part: FRAME — CRACK (LT WHEEL WELL)

FOUND ON B-1 LETTER CHECK, CRACK AT OUTBD FWD WHEEL WELL FRAME. REPAIRED PER SRM 53-05 FIG 78A.

Part: AIR DISTR — ODOR (CABIN)

ON TAKEOFF AND APP HAD SMOKE/FUMES IN CABIN. RAN PACKS, ENGINES AND APU COULD NOT DUPLICATE, PERFORMED DUCT BURNOUT, RETURNED TO SERVICE.