N974DL

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,576 hrs · 52,957 cycles

AFT CAT WALK TAIL CEILING LIGHTS INOP. REMOVED AND REPLACED BATTERIES IN AFT RIGHT LAV OPS CHECK IAW AMM 33-50 P/N OFF/ON AD4002P. (LP5352836)

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 70,997 hrs · 52,467 cycles

AFT LT LAV SMOKE DET INOP. REPLACED AFT LEFT SMOKE DETECTOR, OPS CHECK GOOD PER AMM 26-10 MEL REMOVED.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 70,902 hrs · 52,391 cycles

EMERGENCY LIGHT BATTERY PACK B5-27 IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK B5-27 IAW AMM 33-53-00. OPS CHECK GOOD.

Part: ENGINE — FAILED (RIGHT) · airframe 70,456 hrs · 52,003 cycles

DURING TAKEOFF ROLL, AT APPROXIMATELY 120 KTS, THE RT ENGINE EPR AND N1 BEGAN TO ROLL BACK. SYSTEM ACTIVATED. REJECTED THE TAKEOFF. TOWER REPORTED FIRE FROM THE RT ENGINE. F/A'S REPORTED A LOUD BANG. OPS FOUND DEBRIS ON RUNWAY. INSPECTED THE RT ENGINE AND COWLING. FOUND A HOLE AT THE 12 OCLOCK POSITION OF ENGINE ACOUSTACAL SECTION. NO COWL DAMAGE. THE RIGHT ENGINE WAS REPLACED.

Part: CONTROL QUADRANT — CRACKED (RUDDER PEDAL) · airframe 69,831 hrs · 51,498 cycles

DURING REMOVAL OF CAPT'S RUDDER PEDAL BRACKET, FOUND RUDDER PEDAL ADJUSTMENT QUADRANT CRACKED. RMVD AND REPL CAPT'S RUDDER PEDAL ADJUSTMENT QUADRANT PER AMM 27-20(134146). C/W RII INSTALL OF RUDDER PEDAL ADJ QUADRANT PER AMM 27-20.

Part: BRACKET — CRACKED (RUDDER PEDAL) · airframe 69,831 hrs · 51,498 cycles

WHILE PERFORMING HFEC INSPECTION OF CAPTAINS RUDDER PEDAL BRACKET PER EM2720-01088-0901, FOUND CRACK IN AFT OUTBOARD WEB RADIUS. MARKED. CAPTAINS RUDDER PEDAL BRACKET REPLACED IAW AMDS W/C 2720-01088-0701.

Part: ACM — FAILED (RIGHT) · airframe 69,804 hrs · 51,477 cycles

FLOW LIGHT ILLUMINATED, BOTH PACKS TRIPPED. EMERGENCY DECLARED WITH ACCOMPANYING DESCENT TO 10K FEET WHERE PACKS WERE RESET AND PRESSURIZATION REGAINED. OXYGEN MASKS DID NOT DROP. REPLACED MULTIPLE TEMP AND FLOW CONTROL REGULATING COMPONENTS INCLUDING RT ACM AND NUMEROUS DUCT LEAKS WERE ALSO ADDRESSED. ALL CHECKS SATISFACTORY INCLUDING SINGLE PACK CONFIDENCE CHECKS.

Part: ACTUATOR — FAULTY (OUTFLOW VALVE) · airframe 68,958 hrs · 50,808 cycles

WHILE DESCENDING INTO ATL PASSING THROUGH 18,000 FT, A DUAL AUTO PRESSURIZATION INOP INDICATION OCCURRED. THE QRH WAS FOLLOWED AND MANUAL CABIN PRESSURIZATION WAS SELECTED BUT CABIN ALTITUDE CONTINUED TO CLIMB. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS DESCENDED BELOW 10,000 FT. THE MASKS DID NOT DEPLOY. THE FLOW LIGHT ILLUMINATED ABOUT SAME TIME AS THE INOP LIGHTS DID. MAINTENANCE TESTED BOTH CABIN PRESSURE CONTROLLERS AND FOUND AN "AC MOTOR" FAULT. THE CABIN AIR OUTFLOW VALVE DRIVE ACTUATOR ASSEMBLY WAS REPLACED PER AMM 21-32-05 AND THE CONTROLLERS TESTED OK. A PACK CONFIDENCE CHECK WAS PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SCHRADER VALVE — LEAKING (NLG) · airframe 68,620 hrs · 50,539 cycles

ATB - AFTER TAKEOFF WITH THE GEAR HANDLE RAISED, THE NOSE GEAR DID NOT RETRACT. THE NOSE GEAR UNSAFE RED LIGHT ILLUMINATED ACCOMPANIED BY AN ASSOCIATED AIR NOISE. THE GEAR WAS CYCLED PER THE QRH WITH THE SAME RESULTS. THE CREW EXTENDED THE GEAR AND RETURNED TO ATL. THE NOSE STRUT WAS FOUND FLAT ON ARRIVAL WITH NO CHROME SHOWING WITH THE SCHRADER VALVE LEAKING AT THE PACKING. THE NOSE STRUT SCHRADER VALVE WAS REPLACED AND THE NOSE STRUT WAS REPACKED PER WC 3221-6192. A SUCCESSFUL GEAR SWING WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 68,074 hrs · 50,114 cycles

EMERGENCY LIGHT AT SEAT 31DE IS INOPERATIVE. REPLACED SEAT WIRE HARNESS IAW 33-53. OPS NORMAL.

Part: HANDSET — ODOR (CABIN) · airframe 67,846 hrs · 49,937 cycles

FWD FA HANDSET INOP AND HAS SLIGHT ELECTRICAL ODOR. REPLACED HANDSET. CKS GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 67,543 hrs · 49,704 cycles

ON SVC CK FOUND EMERGENCY LIGHT INOP AT SEAT ROW 24 AND LENS MISSING 23. INSTALLED LENS AT SEAT ROW 23 AND FOUND CONNECTOR DISCONNECTED UNDER SEAT RESECURED OPS CK GOOD.

Part: SLIDE — DAMAGED (TAILCONE) · airframe 67,325 hrs · 49,542 cycles

TAIL CONE SLIDE NOT CLOSING, COMING APART. REMOVED AND REPLACED IAW AMM 25-62-01.

Part: BARREL NUT — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 67,325 hrs · 49,542 cycles

LEFT HORIZONTAL STAB UPPER AFT BARREL NUT SHOWS SIGNS OF RUST. COMPLIED WITH PRI 553953-14AD REV ORIG AND REV1. AND ER/A 553953-14AD REV. ORIGINAL.

Part: SPLICE — NOT REPORTED (FUSELAGE) · airframe 72,206 hrs · 53,502 cycles

FUSELAGE APB TEE SPLICE FS 1338 L26 AND L27 LT AND RT. PERMANENT REPAIR WAS PERFORMED PER ER/A 554000-14 REV.A SEC III AND ETI-88-19-001 REV.4. PLEASE CLOSE THIS LOG DUE TO PERMANENT REPAIR WAS ALREADY ACCOMPLISHED. (LP2837424)

Part: FITTING — CRACKED (RT WING) · airframe 67,325 hrs · 49,542 cycles

RT WING GROUND SPOILER ACTUATOR ATTACH FRAME CRACKED AT FWD. INSTALLED THE FITTING IAW SRM 51-01 PG 1 AND SRM 51-30-02/05.

Part: COVER — LOOSE (EVAC SLIDE) · airframe 67,059 hrs · 49,360 cycles

EVACUATION SLIDE BUSTLE COVER LOOSE LOCATIONS 601. SLIDE COVER WILL NOT STAY CLOSED WHEN SLIDE IS ARMED INTERIOR. CLOSED COVER REINSTALLED SLIDE COVER TOGGLE CLIP. CKS GOOD PER AMM 25-62.

Part: COMPRESSOR — OVERHEATED (POTABLE WATER) · airframe 66,411 hrs · 48,860 cycles

DURING CLIMB F/A NOTICED ODOR. ELECTRIC IN NATURE, IN CAB, STRONGER IN AFT. DISSIPATED AFTER A FEW MINUTES, NONE AT CRUISE. HAPPENED AGAIN DURING DESCENT, DISSIPATED BEFORE LANDING. NO SMOKE REPORTED. SIDEWALL LIGHTS WERE OFF. T/S IAW W/C 2120-2367. FOUND POTABLE WATER COMPRESSOR RUNNING CONTINUOUSLY AND OVERHEATING. REPLACED COMPRESSOR AND PRESSURE SWITCH IAW AMM 38-40. COMPRESSOR PLACED ON MEL REF LOG 8892214. PERFORMED ALTERNATE DUCT BURNOUT IAW W/C 4950-2215. REPLACED WATER SEPARATOR BAGS. LEAK CKS GOOD. OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 66,254 hrs · 48,737 cycles

FOUND AFT SECTION OF EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY CHARGER AND BATTERY IAW AMM 33-53, OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 66,230 hrs · 48,719 cycles

SEAT ROW 31-36 HAVE NO EMERGENCY LIGHTS WORKING. R & R EMERGENCY BATTERY POWER SUPPLY AT POSITION B5-212 REF WDM 33-51-14. OPS CHECK GOOD REF AMM 33-53.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,230 hrs · 48,719 cycles

EMERGENCY LIGHT AT SEAT 13 NOT OPERATIVE. REPAIRED BY REPLACING PIN ON WIRE. OPS CHECKS GOOD.

Part: WIRE — CUT (EMERGENCY LIGHT) · airframe 65,187 hrs · 48,009 cycles

MAINTENANCE FOUND ROW 17 EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND A CUT WIRE AND REPAIRED AND SEAT 17 EMERGENCY LIGHT CHECKED OK.

Part: SKIN — DAMAGED (BS 617-636) · airframe 64,567 hrs · 47,591 cycles

LIGHTNING STRIKE ON WINDOW BELT BETWEEN BS 617 AND 636. BLENDED LIGHTNING STRIKE ON WINDOW BELT BETWEEN BS 617 AND BS IAW SRM 53-05, FIG 111, FOUND TO BE WITHIN LIMITS.

Part: SKIN — DAMAGED (BS 598-617) · airframe 64,567 hrs · 47,591 cycles

LIGHTNING STRIKE ON WINDOW BELT BETWEEN BS 598A AND 617. BLENDED LIGHTNING STRIKE ON WINDOW BELT BETWEEN BS 598 AND 617 IAW SRM 53-05, FIG 111, FOUND TO BE WITHIN LIMITS.

Part: TAB — DAMAGED (LT ELEVATOR) · airframe 64,567 hrs · 47,591 cycles

LIGHTNING STIKE ON LT ELEVATOR GEARED TAB ON T/E. REMOVED LT ELEVATOR GEARED TAB IAW AMDS WC 2730-4590-LT. WEIGHT OF OLD TAB 5.25 LBS. INSTALLED AND ADJUSTED TAB ON AMDS WC 2730-4590-LH.

Part: SKIN — DAMAGED (BS 705) · airframe 64,567 hrs · 47,591 cycles

LIGHTNING STRIKE AT BS 705 ABOVE LONGERON 15 ON WINDOW BELT AREA. REMOVED DAMAGE FOUND WITHIN LIMITS OF SRM 53-05, FIG 111. RESTORED FINISH.

Part: WIRE — CORRODED (EMERGENCY LIGHTS) · airframe 64,383 hrs · 47,462 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE FOUND WIRES TO BE CORRODED AT TERMINAL NR 5. THE CORROSION WAS CLEANED AND THE SYSTEM RETURNED TO NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 63,345 hrs · 46,694 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 16 RT, 01 RT AND 31 RT. MAINTENANCE REPINNED THE CONNECTORS AND THE OPS CHECK WAS GOOD. LP 7002245.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 72,229 hrs · 53,520 cycles

THE AFT LAV WATE SERVICE DR JAMB INTERNAL DOUBLER REPAIR WAS PERFORMED AT HMV4 TO REPLACE THE EXTERNAL DOUBLER AND CLEAN UP ADDITIONAL CORROSION THAT IS THEN WITHIN LIMITS. REPAIR WAS ACCOMPLISHED IAW ER/A 472127-14 REV C. SUPPLEMENTAL INFORMATION: EXTERNAL GENERAL VISUAL INSPECTION WAS PERFORMED PER ER/A 472127-14 REV C SEC III AND CORROSION WAS FOUND ON DOUBLER THIS MON WAS ATTENDEN WITH LOG # 0919054 AND ER/A 472127-14 REV D SECTION VI TEMPORALY REPAIR PERFORM ER/A 472127-14 REV D SECTION V WITHIN 3000 CYCLES AFTER ACCOMPLISMENT OF SECTION I ALSO PERFORM ERA 472127-14 REV D SECTION VI BEFORE 3000 CYCLES AFTER INSTALLATION OF SECTION I BOTH FOLLOWED UNDER LOG 0918562 PLEASE CLOSE THIS LOG DUE TO THE FOLLOW UP IS PERFORMED UNDER LOG 0918562 INSPECTOR CFP 201326061. (LP1871988)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,381 hrs · 46,040 cycles

EXIT LIGHT INOPERATIVE AT AFT OVERWING DOOR, LT SIDE. REPLACED BATTERY PACK IAW AMM 33-53. OPS CKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,268 hrs · 45,962 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN THE COCKPIT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. OPS CHECKED GOOD.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 62,065 hrs · 45,842 cycles

ELONGATED HOLES ON REMOVABLE L/E STA ZFS=52.267 AT VERTICAL STABILIZER. REMOVABLE L/E WAS REPAIR IAW CARD 5530- 01045-08 AND SRM FIG 30.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,065 hrs · 45,842 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF RT WING ACCESS PANEL 1472C . CORROSION WAS REMOVED IAW SRM 51-22-2A AND FOUND TO BE OUT OF LIMITS IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,065 hrs · 45,842 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF RT WING ACCESS PANEL 1466C. CORROSION REMOVED IAW SRM 51-22-2A.

Part: WEB — CRACKED (BS 1485) · airframe 62,065 hrs · 45,842 cycles

CRACKED WEB BS 1485. WEB REPAIRED IAW SRM 53-03 D, FIG 48.

Part: LONGERON — DAMAGED (BS 1309-1322) · airframe 62,065 hrs · 45,842 cycles

LONGERON 19L BS 1309-1322 IN THE AFT CARGO BAY LT UTILITARY TUNNEL DAMAGED. LONGERON WAS REPLACED IAW SRM 51-30-5 AND 53-02, FIG 18 AND REPAIRED IAW SRM 51-30-5 AND 53-02, FIG 18.

Part: FRAME — DAMAGED (BS 1485) · airframe 62,065 hrs · 45,842 cycles

CRACKED REPAIR ON FRAME BS 1485 LONGERON 24R. REPAIR REMOVED IAW SRM 51-30-2, 51-30-3 AND A NEW REPAIR WAS FABRICATED IAW SRM 53-03, FIG 43, THE REPAIR WAS PAINTED IAW SRM 51-10-3 AND INTALLED IAW SRM 51- 30-2, 51-30-5.

Part: SHEAR TIE — CRACKED (BS 1380) · airframe 62,065 hrs · 45,842 cycles

CRACKED AFT ACCESSORY BAY SHEAR TIE AT BS 1380 AND LONGERON 15R. THE SHEAR TIE WAS REPLACED IAW SRM AND 51-30-5, 51-30-2 AND TREATED, PAINTED IAW SRM 51-10-3, PAR 21 & 14.

Part: FRAME — CORRODED (BS 1463) · corrosion level 2 · airframe 62,065 hrs · 45,842 cycles

CORROSION ON FRAME BS 1463 BETWEEN LONGERONS 24-25L. THE CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26, UT WAS ACCOMPLISHED IAW NDT SPM 06-04-PAR 5, FIG 7 AND FOUND OUT OF LIMITS IAW SRM 53-01 AND AREA WAS REPAIRED IAW SRM 53-01, FIG 2, SHEET 4.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON CARGO TRACK, BS 1212-1322. CARGO TRACK WAS REPLACED IAW SRM 51-10-3, PAR 14, 21 AND 51-30-1 AND 51-30-2.

Part: SPAR — DAMAGED (LT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION AND SCRATCHES ON HOLES OF LT WING SPAR XRS=267. DAMAGE REPAIRED IAW ETI-88-14-251, REV 2 AND ER/A 530137 -14, REV ORIGINAL.

Part: SPAR CAP — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON RT HORIZONTAL STABILIZER REAR SPAR CAP HOLES TO ATTACH ELEVATOR HINGE NR 6, VHS, REF ORNRC 4 ZONE 30. RT HORIZONTAL STABILIZER REAR SPAR CAP HOLES TO ATTACH ELEVATOR HINGE WAS REPAIRED IAW ETI-88 14-253, REV 1 AND ER/A 530134-14, REV ORIG.

Part: BEAM — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 62,065 hrs · 45,842 cycles

CORROSION ON REPAIR DOUBLERS OF DOOR FRAME LOWER BEAM IN THE MID CARGO BAY. BEAM REPAIRED IAW SRM 53-05, FIG 123 AND ER/A 530126-14, REV ORIG.

Part: BEAM — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 62,065 hrs · 45,842 cycles

CORROSION ON SEVERAL POINTS OF DOOR FRAME LOWER BEAM BS 660-678 IN THE MID CARGO BAY. THE DOOR FRAME BEAM WAS REPAIRED IAW SRM 53-05, FIG 123 AND ER/A 530126-14, REV ORIGINAL,

Part: INTERCOSTAL — CORRODED (BS 1145-1155) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON INTERCOSTAL BS 1145-1155 BETWEEN LONGERONS 29 - 30R. INTERCOSTAL REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: FRAME — CRACKED (BS 1451) · airframe 62,064 hrs · 45,841 cycles

FRAME CRACKED BS 1451 LONGERON 1. FRAME, REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 9911860-3, REV=L.

Part: LONGERON — CRACKED (BS 1418) · airframe 62,064 hrs · 45,841 cycles

CRACKED AFT ACC COMP LONGERON 2R BS 1418. LONGERON WAS REPLACED IAW SRM 53-02, FIG 18, SRM 51-10-3, PAR 14, 21. SRM 51-30-5, SRM 51-30-2.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION WAS FOUND ON RT LOWER ACCESS PANEL CUTOUT XRS =189.0-214.0 . REPAIRED IAW SRM 51-22-2A, PAGE 29. REPAIRED IAW ETI-88-14-250, REV 1 AND ER/A 530131-14 REV ORIGINAL.

Part: CARGO TRACK — CORRODED (BS 1003-1212) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON LT CARGO TRACK BS 1003-1212. UT IAW NDT SPM 04-00-07 PAR 5 FIG 3 SHEET 1 -2 AND FOUND OUT OF LIMITS. CARGO TRACK REPLACED IAW SRM 51-30-1 AND 51-30-2.

Part: SKIN — DAMAGED (BS 786) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING BS 786 BETWEEN LONGERONS 28 - 29R. FOUND TO BE OUT LIMITS. REPAIRED IAW SRM 53-04 FIG 57 AND 51-30-5.

Part: CARGO TRACK — CRACKED (BS 1271) · airframe 62,064 hrs · 45,841 cycles

CRACKED RT CARGO TRACK BS 1271 BETWEEN LONGERONS 27R AND 28R. RT CARGO TRACK WAS REPLACED IAW SRM 51-10-3, PAR 14, 21, SRM 51-30-2 AND SRM 51-30-2.

Part: CARGO TRACK — CORRODED (BS 1212-1231) · corrosion level 2 · airframe 62,065 hrs · 45,842 cycles

CORROSION ON SPLICE OF CARGO TRACK, BS 1212- 1231 BETWEEN LONGERONS 27 - 28L. SPLICES WERE REPLACED IAW SRM 53-24-0 51-40-2, 51-10-3, PAR 11 AND 14 51-30-5.

Part: CUSP WEB — CORRODED (BS 1022-1041) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON LEFT CUSP WEB X 54 - 60 BETWEEN BS 1022 - 1041. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,064 hrs · 45,841 cycles

CRACKED AFT ACCESSORY BAY LONGERON 3R BS 1437. SECTION OF LONGERON WAS REMOVED IAW SRM 53-02, FIG 18. FABRICANT REPAIR IAW SRM 53-02, FIG 18, SECTION OF LONGERON WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21, REPAIR INSTALLED IAW SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 794-796) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON LT SEAT TRACK, BS 794-796. SEAT TRACK WAS REPAIRED IAW SRM 51-30-1, 53-05 FIG 4F, 51-10-4, & 51-10-3 PAR 14 AND 21.

Part: DOUBLER — CRACKED (BS 1380) · airframe 62,064 hrs · 45,841 cycles

DOUBLER ON FUSELAGE SKIN, BS 1380 ABOVE NR 2 ENGINE PYLON HAS CRACKS. DOUBLER WAS REPLACED IAW SRM 5304, FIG 18.

Part: SUPPORT — BROKEN (BS 1193) · airframe 62,064 hrs · 45,841 cycles

BROKEN SLANT PANEL SUPPORT ON STA Y=1193, BETWEEN LONGERONS 27LT TO 24LT SLANT SUPPORT WAS REPLACED IAW ER/A 413029-14MA, REV D AND SRM 51-30-5 AND 51-30-3, PAR 14,21.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF RT WING FUEL ACCESS PANEL NR 1456C CORROSION WAS REMOVED IAW SRM 51-22-2A AND FOUND OUT OF LIMITS IAW SRM 51-22-2A.

Part: ANGLE — CORRODED (BS 1338-1344) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON APU FWD DOOR FRAME ANGLE LONGERON 30, BETWEEN BS 1338 - 1344. ANGLE WAS REPLACED IAW SRM 53-14-4, ITEM 22 AND SRM 51-30-2.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF RT WING FUEL ACCESS DOOR NR 1360C. CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF RT WING FUEL ACCESS DOOR NR 1460C WAS REMOVED IAW SRM 51-22-2A AND COUNTERSINK HOLES WERE MEASURED MAX DIAMETER ALLOWABLE IS .532" AND MAX DIAMETER MEASURED IN (3) HOLES .562 IT IS OUT OF LIMITS IAW SRM 51-22-2A AND WAS REPLACED.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON HINGE FITTING AT LT WING XRS 267. HINGE FITTING REPLACED IAW AMM 57-40-01.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS PANEL NR 1311C. ACCESS PANEL REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING ACCESS PANEL 1335C. FOUND OUT OF LIMITS IAW SRM 51-22-2A. THE ACCESS PANEL WAS REPLACED.

Part: INTERCOSTAL — CORRODED (BS 1212-1231) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON INTERCOSTAL ON LONGERON 29LT, BS 1212-1231. REPAIRED IAW SRM 51-30-5,51-30-2, 51-10-4, 51-10-2,53-14-3, ITEM 18 AND 51-10-3 P 21 AND 14.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF RT WING FUEL ACCESS DOOR 1409C. ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1363C. CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA WAS REMOVED IAW SRM 51-22-2A. COUNTERSINK HOLES WERE MEASURED MAX DIAMETER ALLOWABLE IS 0.532" AND MAX DIAMETER MEASURED IS .540" IN 3 ADJACENT HOLES THEREFORE WAS FOUND OUT OF LIMITS SRM 51-22-2A. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER JIC 2800-0120.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF RT WING FUEL ACCESS DOOR NR 1363, 1462C, MRB 57-31-082. CORROSION ON COUNTERSINK HOLE AND SETTLEMENT AREA WAS REMOVED IAW SRM 51-22-2A. COUNTERSINK HOLES WERE MEASURED MAX DIAMETER ALLOWED IS 0.0532" AND MAX DIAMETER MEASURE IS 0.0550" IN 3 ADJACENT HOLES THEREFORE WAS FOUND OUT OF LIMIT IAW SRM 51-22-2A, ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER JIC 2800-0390, JOB 001-0391.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1355C. CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA WAS REMOVED IAW SRM 51-22-2A. COUNTERSINK HOLES WERE MEASURED MAX DIAMETER ALLOWABLE IS 0.532" AND MAX DIAMETER MEASURED IS 0.575" IN 4 ADJACENT HOLES THEREFORE WAS FUOND OUT LIMITS IAW SRM 51-22-2A. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER JIC 2800-0120 JOB 001-0385.

Part: SKIN — CORRODED (BS 1066-1079) · airframe 67,037 hrs · 49,341 cycles

CORROSION ON RT REPAIR DOUBLER FROM X 54 TO X -60, BS 1066 TO 1079. REPAIR DOUBLER WAS REPLACED.

Part: FAIRING — DAMAGED (RUDDER) · airframe 62,064 hrs · 45,841 cycles

MISSING MATERIAL ON AFT FAIRING NR 6508A OF RUDDER. CARD 144, ZONE 00, LOG-PAGE UPDATED AT 12NOV14 1355 UTC LOG-PAGE UPDATED. AFT FAIRING NR 6508A WAS REPAIRED IAW SRM 51-70-1A, PARR 23.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1357C. CORROSION ON COUTERSINK HOLE AND SETTLEMENT AREA WAS REMOVED IAW SRM 51-22-2A. COUNTERSINK HOLES WERE MEASURE MAX DIAMETER ALLOWABLE IS 0.532" AND MAX DIAMETER ALLOWABLE IS 0.532" AND MAX DIAMETER MEASURE IS 0.560 IN 3 ADJACENT HOLE THEREFORE WAS FOUND OUT OF LIMIT IAWW SRM 51-22-2A. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER JIC 2800-0120.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1371C. CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA WAS REMOVED IAW SRM 51-22-2A. COUNTERSINK HOLES WERE MESURED MAX DIAMETER ALLOWABLE IS .532" AND MAX DIAMETER MEASURED IS .569" IN 3 ADJACENT HOLES THEREFORE WAS FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER JIC 2800-0120,

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1365C. CORROSION ON SETTLMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1365C WAS REMOVED IAW SRM 51-22-2A, COUNTERSINK HOLES WERE MEASURED. MAX DIAMETER ALLOWED IS .532" AND MAX. DIAMETER MEASURED IS .548" IN 3 ADJACENT OLES THEREFORE WAS FOUND OUT OF LIMITS IAW SRM 51-22-2A. FUEL ACCESS DOOR WAS REPLACED AND WILL BE INSTALLED UNDER JIC 2800-0120.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF RT WING FUEL ACCESS DOOR NR 1464C. CORROSION ON COUNTERSINK HOLES SETTLEMENT AREA WAS REMOVED IAW SRM 51-22-2A. COUNTERSINK HOLES WERE MEASURED MAX DIAMETER, ALLOWABLE IS 0.532" AND MAX DIAMETER MEASURED IS .569" IN 3 ADJACENT HOLES THEREFORE WAS FOUND OUT LIMITS IAW SRM 51-22-2A. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER JIC 2800-0390,

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF RT WING FUEL ACCESS DOOR NR 1470C. CORROSION ON COUNTERSINK HOLE AND SETTLEMENT AREA WAS REMOVED IAW SRM 51-22-2A. COUNTERSINK HOLES WERE MEASURE MAX DIAMETER ALLOWABLE IS 0.532" IN AND MAX DIAMETER MEASURE IS 0.569" 3 ADJACENT HOLE THEREFORE WAS FOUND OUT OF LIMIT IAW SRM 51-22-2A. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER JIC 2800-0120.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1367C. CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS DOOR WAS REMOVED IAW SRM 51-22-2A. COUNTERSINK HOLE WERE MEASURED MAX DIAMETER ALLOWABLE IS 0.532" AND MAXIMUM DIAMETER MEASURE IS 0.555" IN 6 ADJACENT HOLES THEREFORE WAS FOUND OUT LIMITS IAW SRM 51-22- 2A. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER JIC 2800-0120.

Part: TEE FITTING — DAMAGED (BS 1338 BULKHEAD) · airframe 62,064 hrs · 45,841 cycles

DAMAGE ON INNER SPLICE OF PRESSURE BULKHEAD TEE BS 1338 BETWEEN LONGERONS 26-27L. INNER SPLICE WAS REPLACED IAW SRM 53-03, FIG 37.

Part: SEAT TRACK — CORRODED (BS 935-937) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON LT SEAT TRACK X=54 FROM STA Y=935 TO Y=937 AT CABIN FLOOR STRUCTURE IN REF CARD 52 ZONE 201 AND 20000026751. SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIG 4.

Part: CUSP WEB — CORRODED (BS 636-655) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON RT CUSP WEB STA Y=636-655 BETWEEN X=-54 TO X=-60, REF ORNRC 96, ZONE 201, MRB 53-037-02, CARD 325, ZONE 201. NEW REPIAR WAS INSTALLED IAW SRM 53-05, FOG 131 A-5 AND 51-30-1, 51-10-3 PAR 14-21, 51-30-5 AND PS 900-5-1, NR 04.

Part: CUSP WEB — CORRODED (BS 579-598) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON RT CUSP WEB BS 579-598 BETWEEN, X -54 AND X -60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-13 AND 51-30-2, 51-30-5, SL 10-3, PAR 14, 21.

Part: LONGERON — DAMAGED (BS 273) · airframe 62,064 hrs · 45,841 cycles

ELONGATED HOLERS ON LONGERON 21L BS 273.5. LONGERON WAS REPLACED IAW SRM 53-02, FIG 18, SRM 53-14-2, FIG 3 SRM 51-30-2, SRM 51-30-5, SRM 51-10 -3, PAR 14, 21.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,064 hrs · 45,841 cycles

DAMAGED FLAME SPRAY ON RUDDER SKIN BOTH SIDES, SM, CARD 4, ZONE 65. FLAME SPRAY WAS REPAIRED IAW SRM 51-70-1A, PAR 23.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1303C, MRB 57-31-082, LW, AYP, CARD 170, ZONE 10. LT WING FUEL ACCESS DOOR NR 1303C WAS REPLACED IAW SRM 51-22-2A, DUE TO BLEND OUT IS NOT PERMITTED UPPER ACCESS DOOR, PN 3912757 IAW SRM 51-22-2A.

Part: FLOOR PANEL — CORRODED (BS 148-200) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON FITTINGS AND FLOOR PANEL NR 160G FROM BS 148 - 200 X -55 . FITTING AND FLOOR PANEL 160G WERE REPLACED IAW DWG 9957828, REV AB AND SRM 51-10-3, PAR 14, 21 SRM 51-10- 4.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CPCP EXFOLIATION CORROSION ON RT HORIZONTAL STABILIZER UPPER SKIN PANEL, STA XH=27.2. CORROSION REMOVED AND FOUND TO BE WITHIN LIMITS. REPAIRED IAW ETI-88-14-246, REV. ORIG AND ER/A 530127-14, REV ORIG.

Part: CUSP WEB — CORRODED (BS 788-807) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON RT CUSP WEB BS 788-807 BETWEEN X -54 AND X -60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13 AND 51-10-3 PAR 14, 21 AND 38.

Part: CUSP WEB — CORRODED (BS 636-655) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER OF LT CUSP WEB BS 636 - 655 BETWEEN X 54 AND X 60. CORROSION ON CUSP WEB WAS REPAIRED IAW SRM 51-30-5, 53-05, FIG 131A-14, 51-10-3 PAR 14, 21, 26 AND 38.

Part: CUSP WEB — CORRODED (BS 446-465) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER OF LT CUSP WEB BS 446-465 X 54 AND X 60. PREVIOUS REPAIR DOUBLER OF LT CUSP WEB WAS REPLACED WITH NEW REPAIR PARTS IAW SRM 53-05, FIG 131A-7.

Part: CUSP WEB — CORRODED (BS 868-881) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON RT CUSP WEB BS 868 - 881. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A.

Part: CUSP WEB — CORRODED (BS 731-740) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER OF RT CUSP WEB BS 731 -740 BETWEEN X -54 AND X -60. DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131A -6 , 51-30-5, 51-30-2, 51-10-3 PAR 14 AND 21 AND PS 900-5-1, NR 04.

Part: CUSP WEB — CORRODED (BS 598-617) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON RT CUSP WEB BS 598 - 617 BETWEEN X -54 TO X -60. DAMAGE AREA WAS REPAIRED IAW SRM 53-05, FIG 131A-6, 51-10-3, PAR 21 AND 14, 51-30-2 AND 51-30-5.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 62,064 hrs · 45,841 cycles

CRACKED CHANNELS ON PAX CABIN FLOOR PANELS NR 886C AND 826D. THE CHANNELS "W" WERE REPLACED ON FLOOR PANELS 826D AND 886C. REMOVED SRM 51-30-1 AND 51-30-8 DRILLED SRM 51-10-4. INSTALLED DWG 9936639, REV. P.

Part: SUPPORT — CORRODED (BS 1155-1212) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON FWD/AFT SCUFF PLATE SUPPORT BS 1155 - 1212 ABOVE DOOR JAMB LOWER BEAM AT AFT CARGO COMPARTMENT CORROSION WAS REMOVED , AREA WAS MEASURED THICKNESS ORIGINAL 0.093" REMAINING .048" IS OUT LLIMITS, FLOOR SUPPORT WAS R & R NEW SUPPORT WAS DRILLED AND ADJUSTED/ HOLES TREATED AND PAINTED, NEW SUPPORT WAS INSTALLED IAW SRM 51-10-3, 51-30-11 50-30-2, D/DWG 5936660 REV B2, 51-10 -41, 51-10-3, PAR 21 AND 14.

Part: CUSP WEB — CORRODED (BS 465-483) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON PREVIOUS DOUBLER REPAIR X0-52 TO X= -60 FROM BS 465 - 483 AT RT CUSP WEB OF PAX CABIN FROOM STRUCTURE MRB 53-037-1. PREVIOUS REPAIR WAS REPLACED IAW SRM 53-05, FIG. 131.

Part: INTERCOSTAL — WORN (BS 769-788) · airframe 62,064 hrs · 45,841 cycles

WEAR ON INTERCOSTAL BETWEEN BS 769 - 788, X 0. NEW INTERCOSTAL WAS INSTALLED IAW DWG 9936580 AND SRM 51-30-5, 51-30-2.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON LT HORIZONTAL STABILIZER UPPER SKIN PANEL STA XH27.2. CORROSION REMOVED AND REPAIR BUSHINGS WERE INSTALLED IAW SRM 55-03D, PAR 30.

Part: SEAT TRACK — CORRODED (BS 405-407) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON LT SEAT TRACK X=22 AT BS 405-407, MRB 53-037-01. LT SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIG 4A, SHEET 1, 51-10-3, PAR. 14 AND 21 AND 51-301.

Part: CUSP WEB — CORRODED (BS 579-598) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER OF LT CUSP WEB BS 579-598 BETWEEN X 54 AND X 60. PREVIOUS REPAIR DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131A-6 SRM 51-30-5, SRM 51-30-2, SRM 51-10-3, PAR 14, 21.

Part: CUSP WEB — CORRODED (BS 1239-1250) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON LT CUSP WEB X 54 TO X 60 BETWEEN BS 1239-1250. CUSP WEB REPAIRED IAW SRM 53-05, FIG. 131A-6, SHEET 1.

Part: SEAT TRACK — CORRODED (BS 562-654) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON RT SEAT TRACK X -54 AT BS 562-564. SEAT TRACK REPAIRED IAW SRM 53-05, FIG 4A, SHEET 1, 51-30-1 AND 51-10-3, PAR 14 AND 21.

Part: SEAT TRACK — CORRODED (BS 608-611) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON ON PREVIOUS REPAIR PLUG AT LT SEAT TRACK X=54 FROM BS 608 - 611, MRB 53-037-01,SM. PLUG AT LT SEAT TRACK WAS REPLACED IAW SRM 51-30-1, 53-05, FIG 4A, SHEET 1 AND 51-10-3 PAR 14 AND 21.

Part: SEAT TRACK — CORRODED (BS 935-937) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON LT SEAT TRACK X 22, FROM BS 935 - 937. SEAT TRACK REPAIRED IAW SRM 53-05, FIG 4F.

Part: FRAME — CORRODED (BS 1385) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON FRAME BS 1385, BETWEEN X -3 AND X -5. FRAME REPAIRED IAW SRM 53-10, FIG 2, SHEET 3.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,064 hrs · 45,841 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: SKIN — CRACKED (BS 1214) · airframe 62,064 hrs · 45,841 cycles

CRACKED INNER FUSELAGE SKIN ON STA Y=1214 BETWEEN LONGS 26LT AND 25LT. C3, SM, CARD 215, ZONE 201. DAMAGE FINGER DOUBLER WAS TRIMED NEW SECTION FROM FINGER DOUBLER WAS FABRICATED TRETAED AND PAINTED AND INSTALLED IAW SRM 51-10-3 AND 53-04, FIG 12D.

Part: CUSP WEB — CORRODED (BS 987-990) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON RT CUSP WEB BETWEEN STA Y=987-990 AND X=-54 TO X= 60, MRB 53-037-01, IN REF OR NRC 157 ACFT ZONE 201. SM, CARD 307, ZONE 201. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A.

Part: SKIN — CRACKED (BS 1214) · airframe 62,064 hrs · 45,841 cycles

CRACKED INNER FUSELAGE SKIN ON STA Y=1214 BETWEEN LONGERONS 26LT AND 25LT. DAMAGE FINGER DOUBLER WAS TRIMED NEW SECTION FROM FINGER DOUBLER WAS FABRICATED TREATED AND PAINTED AND INSTALLED IAW SRM 51-10-3 AND 53-04, FIG 12D.

Part: SHEAR TIE — DAMAGED (BS 256) · airframe 62,064 hrs · 45,841 cycles

ELONGATED HOLES ON FRAME SHEAR TIE BS 256 BETWEEN LONGERONS 20 AND 25 L. REMOVED AND REPLACED IAW SRM 51-30-2 SRM 53-14-2, FIG 2 AND SRM 51-10-3.

Part: LONGERON — DAMAGED (BS 235) · airframe 62,064 hrs · 45,841 cycles

ELONGATED DRILL HOLES ON LONGERON 24L BS 235. THE LONGERON WAS REMOVED IAW SRM 51-30-2/51-30-5. A NEW SECTION OF LONGERON WAS TRIMMED AND DRILLED IAW SRM 51-10-4, WAS TREATED AND PAINTED IAW SRM 51-10-3 AND WAS INSTALLED.

Part: CUSP WEB — CORRODED (BS 1165-1250) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON RT CUSP WEB FROM BS 1165 - 1250 X -54 AND X -60. REPAIRED IAW SRM 53-05, FIG 131A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1377C, MRB 57-31-082, LW, AYP, CARD 167, ZONE 10. CORROSION ON SETTLEMENT AREA AND CORROSION HOLES WERE REMOVED, COUNTERSINK HOLES WERE MEASURED MAX DIAMETER ALLOWABLE IS .532 AND MAX DIAMETER MEASURED IN 3 ADJACENT HOLES IS 0.541. THEREFORE IT IS OUT OF LIMITS IAW SRM 51-22-2A, FUEL ACCESS 1377C WAS REPLACED IAW IPC 57-30-00 AND WILL BE INSTALLED UNDER JIC 2800-1020, JOB 001-0385.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 62,064 hrs · 45,841 cycles

CRACKED RT AFT OVERWING EMERGENCY EXIT DOOR ANGLE AT STOP FITTING NR 1. RT AFT OVERWING EMERGENCY EXIT DOOR CLIP WAS FABRICATED IAW SRM 51-10-2 AND DWG 9957735, REV G AND INSTALLED IAW SRM 51-30-5.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF LT WING FUEL ACCESS DOOR NR 1307C, MRB 57-31-082, LW, AYP CARD 172, ZONE 10, CORROSION ON FUEL ACCESS PLATE 1307C ON SETTLEMENT AREA AND COUNTERSINK HOLES WAS REMOVED, COUNTERSINK HOLES WERE MEASURED MAX DIAMETER ALLOWABLE IS .660" AND MAX DIAMETER MEASURED IS .700" IN, 3 ADJACENT HOLES THEREFORE IT IS OUT OF LIMITS IAW SRM 51-22-24 AND FUEL ACCESS PLATE 1307C WAS REPLACED IAW IPC 57-30-00 AND WILL BE INSTALLED UNDER JIC 2800-0120, JOB 001-0385.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON FRAME WEB FWD FACE STA Y=1380 BETWEEN X=-8 TO X=-16 AT AFT ACCESS COMPARTMENT MRB 53-140-03, SM CARD 144, ZONE 100. REMOVE CORROSION AND MEASURE IAW SRM 51-10-3, PAR 26 NEW WEB WAS FABRICATED AND DRILL AND TRIMER NEW WEB IAW SRM 51-10-4 AND 53-14-3 AND DWG 9912246 NEW WEB WAS TREATED AND PAINTED IAW SRM 51-10-3, PARAGRAPH 14-21 NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5, UT, NDT SPM 04-00-07, FIG 3, SHEET 1 AND 2 WAS ACCOMPLISHED ORIGINAL THICKNESS IS 0.050 AND MINIMUM REMAINING THICKNESS IS 0.027", THEREFORE WEB IS "OUT OF LIMIT" IAW SRM 53-01, FIG 1.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON FRAME LOWER TEE STA Y=1380 BETWEEN X=-19 AND X=19, ALSO RUSTED FASTENERS AND WASHERS ON SAME TEE AT AFT ACCESS COMPARTMENT, MRB 53-140-03, SM CARD 137, ZONE 100. FRAME LWR TEE STA Y=1380 BETWEEN X=-19 AND X=19 WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: FLOORBEAM — CORRODED (BS 180) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION FOUND ON FLOORBEAM BS 180 BETWEEN X=7 TO X=44. REPLACED IAW SRM 51-30-2, 51-10-4, 51-10-3, PAR 14, 21 AND 38.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 62,064 hrs · 45,841 cycles

CRACKED LT AFT OVERWING EMERGENCY EXIT DOOR ANGLE AT STOP NR 12, SM, CARD 64, ZONE 201. LT AFT OVERWING EMERGENCY EXIT DOOR ANGLE CLIP WAS FABRICATED IAW SRM 51-10-2 AND DWG 9957735, REV G AND CLIP WAS INSTALLED IAW SRM 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF RT WING FUEL ACCESS DOOR NR 1454C, MRB 57-31-082, RW, AYP, CARD 174, ZONE 10. CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES WERE REMOVED, COUNTERSINK HOLES WERE MEASURED MAX DIAMETER ALLOWABLE IS .532" AND MAX DIAMETER MEASURED IS .586 IN 4 ADJACENT HOLES THEREFORE IT IS OUT OF LIMITS IAW SRM 51-22-2A.

Part: INTERCOSTAL — CORRODED (BS 437) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON INTERCOSTAL BETWEEN LONGERON 29R AND BS 437. INTERCOSTAL REPLACED IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-4, SRM 51-10-3 PAR 14 AND 21.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,064 hrs · 45,841 cycles

LONGERON 16L CRACKED BS 1437. LONGERON REMOVED IAW SRM 51-30-2, 51-30-3 AND 51-70-5. A NEW LONGERON WAS DRILLED AND ADJUSTED IAW SRM 51-10-3, PAR 14 AND 21 AND INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,064 hrs · 45,841 cycles

DELAMINATED FLOOR PANEL. FABRICATED IAW AMM 53-20-01-201.

Part: CUSP WEB — CORRODED (BS 525) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON REPAIR DOUBLER ON RT CUSP WEB BS 525 BETWEEN X -54 AND X -60. DOUBLER REPLACED IAW SRM 53-05, FIG 131A-6 AND 51-10-3, PAR 14-21, 51-30-5, AND 51-30-2.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 62,064 hrs · 45,841 cycles

CRACKED LT FWD OVERWING EMERGENCY EXIT DOOR PAN AT STOP NR 12. PAN WAS REPAIRED IAW SRM 52-05D, FIG-51

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 62,064 hrs · 45,841 cycles

CRACKED RT AFT OVERWING EMERGENCY EXIT DOOR PAN AT STOP NR 12, PAN WAS REPAIRED IAW SRM 52-05D.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 62,064 hrs · 45,841 cycles

CRACKED LT AFT OVERWING EMERGENCY EXIT DOOR PAN AT STOP NR 1. PAN WAS REPAIRED IAW SRM 52-05D, FIG 51.

Part: CUSP WEB — CORRODED (BS 535) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION FOUND ON REPAIR DOUBLER OF LT CUSP WEB BS 535 BETWEEN X=54 AND X=60. DOUBLER REPLACED IAW SRM 53-05, FIG 131A-13 AND 51-10-3 PAR 14, 21, 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 560-574) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON REPAIR DOUBLER FOR LT CUSP WEB BS 560-574 BETWEEN X=54 AND X=60. REPAIR REPLACED IAW SRM 53-05, FIG 13 1A-7 AND 51-30-5, 51-30-2, 51-10-3 PAR 14 AND 21.

Part: LONGERON — DAMAGED (BS 1401-1418) · airframe 62,064 hrs · 45,841 cycles

WEAR ON AFT ACCESSORY COMPARTMENT LONGERON 8R PREVIOUS REPAIR SECTION BETWEEN Y= 1401-1418. LONGERON WAS REMOVED FROM STA Y=1392 TO STA Y=1430 IAW SRM 51-30-1 AND 51-30-2, NEW SECTION LONG WAS ADJUSTED AND DRILLED IAW SRM 51-10-4, LONG WAS TREATED AND PAINT IAW SRM 51-10-3, PAR 14 AND 21. LONG WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5. RE-WRITE CARD 40, ZONE 61.

Part: LONGERON — CRACKED (BS 1380) · airframe 62,064 hrs · 45,841 cycles

CRACKED AFT ACC COMP LONGERON NR 13R AT INTERSECTION WITH FRAME 1380. SM, CARD 16, ZONE 61. LONGERON NR 13RT AT INTERSECTION WITH FRAME 1380 WAS REMOVED IAW SRM 51-30-2 AND 51-30-5; NEW LONGERON WAS DRILLED AND ADJUSTED IAW SRM 51-10-4, NEW LONGERON WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21, NEW LONGERON WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 1166) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION FOUND ON REPAIR DOUBLER FOR THE LT CUSP WEB BS 1166, X=54. DOUBLER AND FILLER REPLACED IAW SRM 51-30-5, 53-05, FIG 131A-3, 51-10-3 PAR 14,21.

Part: ANGLE — DAMAGED (BS 294 FRAME) · airframe 62,064 hrs · 45,841 cycles

ELONGATED DRILL HOLE ON FRAME ANGLE BS 294 BETWEEN LONGERONS 19 - 22L. A NEW FRAME ANGLE AND SPLICE WERE FABRICATED, TREATED AND PAINTED AND INSTALLED IAW SRM 53-14-2, FIG 2, 51-10-2, 51-10-3 PAR 14/21, & 51-30-2.

Part: CUSP WEB — CORRODED (BS 430) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION FOUND ON REPAIR DOUBLER OF LT CUSP WEB BS 430 BETWEEN X=54 AND X=60. DOUBLER REPLACED IAW 51-30-5, 51-30-1, 51-30-2, 53-05, FIG 131A-13 AND 51-10-3 PAR 14 AND 21.

Part: SEAT TRACK — CORRODED (BS 855-858) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION ON SEAT TRACK, RT X=-22, FROM BS 855 TO 858 AT PAX CABIN. REPAIRED IAW SRM 53-05, FIG 4A.

Part: CUSP WEB — CORRODED (BS 712) · corrosion level 2 · airframe 62,064 hrs · 45,841 cycles

CORROSION FOUND ON REPAIR DOUBLER OF LT CUSP WEB BS 712, BETWEEN X=54 AND X=60. DOUBLER REPLACED IAW SRM 53-05, FIS IBIA-13, SRM 51-10-3, PAR 14, 21 SRM 51-30-5.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 62,064 hrs · 45,841 cycles

CORROSION ON FLOOR PANEL 256E. FLOOR PANEL REPAIRED IAW SRM 51-10-3, PAR 14, 21, 26 AND SRM 53-01, FIG 2.

Part: LONGERON — CRACKED (BS 1413) · airframe 62,064 hrs · 45,841 cycles

CRACKED LONGERON 9R BS 1413. LONGERON TRIMMED IAW SRM 53-02, FIG 18, NEW LONGERON SECTION DRILLEAD IAW SRM 51-10-4, SPLICE DRILLED AND ADJUSTED IAW SRM 51-10-4, AND 53-02, FIG 18, SHEET 1, NEW LONGERON INSTALLED IAW SRM 51- 30-2 AND 51-30-5.

Part: LIGHT — INOPERATIVE (SEAT 18D) · airframe 61,844 hrs · 45,669 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 18D WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,156 hrs · 45,170 cycles

DURING LINE CHECK, MX FOUND THE EMERGENCY EXIT SIGNS WERE INOPERATIVE AT THE FORWARD AND AFT EXITS. MAINTENANCE REPLACED THE LAMPS AT THE FORWARD EXIT SIGN AND REPLACED THE BATTERIES IN THE AFT EXIT SIGN POWER SUPPLY AND THE SIGNS RETURNED TO NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,579 hrs · 44,767 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT SEVERAL LOCATIONS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 59,338 hrs · 43,890 cycles

DURING LINE CHECK, MX FOUND THAT THE SEAT MOUNTED EMERGENCY LIGHTING AT ROW 17D IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A "TORN PIN" AND A LOOSE IN-LINE CONNECTION. THE CONNECTION WAS RE-SEATED AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: WIRE — MISINSTALLED (LIGHTS) · airframe 58,748 hrs · 43,459 cycles

DURING ROUTINE LINE CHECK, IT WAS NOTED THAT THE AFT STAIR LIGHT ILLUMINATES WHEN THE F/A READING LIGHT WAS TURNED ON. MX FOUND THE WIRES TO THE LIGHTS SWITCHED AND REWIRED IAW THE WIRING DIAGRAM MANUAL REF: 33-23-01 AND OPS CHECKED GOOD.

Part: BUSHING — WORN · airframe 58,727 hrs · 43,440 cycles

MX DISCOVERED THAT THE TEE PIN AND THE TEE PIN BUSHING WERE WORN BEYOND ALLOWABLE LIMITS AND REQUIRED REPLACEMENT.

Part: RECEPTACLE — WORN (TAIL CONE) · airframe 58,727 hrs · 43,440 cycles

MX DISCOVERED THAT NUMEROUS TAILCONE GUIDE PIN RECEPTACLES WERE WORN OUT OF ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: LANYARD — MISROUTED (TAILCONE) · airframe 55,961 hrs · 41,428 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE TAIL CONE TO SLIDE LANYARD TO BE ROUTED IMPROPERLY. MAINTENANCE CORRECTLY ROUTED THE LANYARD AND THE PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF THE SYSTEM.

Part: RELEASE CABLE — MISROUTED (TAILCONE) · airframe 55,473 hrs · 41,110 cycles

TAIL CONE RELEASE MECHANISM INSTALLATION FAILED ROUTINE INSPECTION IN LGA. THE LANYARD WAS FOUND TO BE INCORRECTLY INSTALLED. MAINTENANCE DID CORRECT THE ROUTING PER AMM 53-53-00-401 FIG 402 VIEW A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,089 hrs · 40,888 cycles

FWD ENTRY AREA LT INBOARD SEAT TRACK WITH CORROSION BETWEEN STA 200 TO 237. REMOVED CORROSION ON LT INBD SEAT TRACK STA 200 TO 237, FOUND TO BE OUT OF LIMITS IAW DC9/MD80 SRM 53-05. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED SEAT TRACK SECTION FROM STA 200 TO 237 LEFT INBD, FABRICATED AND INSTALLED SEAT TRACK SECTION IAW DC9/MD80 SRM 53-05 DURING PAX MOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,089 hrs · 40,888 cycles

FWD ENTRY AREA SEAT TRACK WITH CORROSION STA 200-237LT . REMOVED CORROSION AT FWD ENTRY OUTBD SEAT TRACK, FOUND TO BE OUT OF LIMITS IAW DC9/MD80 SRM 53-05. REMOVED CORROSION ON OUTBD TRACK STA 200-237LT, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW DC9/MD80 SRM 53-05.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,089 hrs · 40,888 cycles

CRACK ON LOWER ANGLE OF MAIN ENTRANCE DOOR FWD SAA111 CRACKED MAIN ENTRANCE DOOR. FABRICATE FILLER AND DOUBLER TREATED AND PRIIMED ALL PARTS REF DC9/MD80 SRM 52-01 FIG 1 AND DC9/MD80 SRM 51-10-3. INSTALLED 2 DOUBLERS AND FILLER REF DC9/MD80 SRM 51-30-05 AND DC9/MD80 51-30-02. C/W AT SAA/SAT DURING PAX MOD ON N/R 268 W/O 89412420001. THIS TEXT SHOWS N/R 268 BUT REF SHOWS N/R 265.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,867 hrs · 40,751 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN AT ROW 31-38 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK & BASE AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 54,741 hrs · 40,663 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHTS FROM ROW 31 AND AFTWARD INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY CHARGER B5-212 AND BATTERY PACK PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD. AIRCRAFT IS OKAY FOR SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 54,643 hrs · 40,604 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND AFT SECTION OF SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY CHARGER PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (AC BAY) · airframe 53,626 hrs · 39,845 cycles

DURING LINE CHECK MAINTENANCE FOUND TAIL COMPARTMENT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK B5-28. OPERATION OF LIGHT NOW CHECKS OK.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,223 hrs · 39,575 cycles

C/W ACTL LINE 2104 ERA 487718-14 REV B REPAIR, REPAIRED DAMAGE PER ERA 490609-14 REV ORIGINAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,665 hrs · 38,566 cycles

MX FOUND THE EMERGENCY PATH LIGHT AT SEAT 30D TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 51,490 hrs · 38,441 cycles

AFTER TOW TO GATE AND AIRCRAFT STOPPED JETWAY IMPACT TO FUSELAGE 3.5 IN X 3.5 IN PUNCTURE TO SKIN APPROX STATION 220 JUST BELOW STRINGER 17L. REPAIRED FUSELAGE DAMAGE PER ERA 483689-14 REV A ALL RII REQUIREMENTS HAVE BEEN MET.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 50,628 hrs · 37,922 cycles

SEAT MOUNTED EMERG LIGHT AT ROW 21DE INOPERATIVE. REPAIRED CONNECTOR. OPS OK.

Part: DOUBLER — CORRODED (BS 1307 S19L) · airframe 47,879 hrs · 36,167 cycles

DURING HMV, CORROSION WAS FOUND AROUND THE AFT LAVATORY WASTE SERVICE DOOR JAMB PANEL BETWEEN STA 1307 AND 1322 AND LONGERONS 19L AND 22L. THE CORROSION WAS REMOVED AND REPAIRED PER BOEING REPAIR INSTRUCTIONS.

Part: BEAM — CRACKED (R1 DOOR) · airframe 47,879 hrs · 36,167 cycles

CRACKED R1 DOOR NR 4 BEAM FWD EDGE. CRACK WAS STOP DRILLED IAW SRM 52-05D FIG 25. DOUBLER FABRICATED IAW SRM 52-05D FIG 25. REPAIR PARTS INSTALLED IAW SRM 52-05D FIG 25 AND IDENTIFIED IAW PS 900-5-1 NR 4.

Part: FRAME — CRACKED (BS 1174) · airframe 47,879 hrs · 36,167 cycles

DURING HMV AT GDL, CRACKS WERE DISCOVERED IN THE FUSELAGE FRAME AT STA 1174 AND LONGERON 6L. THE CRACKED PORTION OF THE FRAME WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED PER BOEING INSTRUCTIONS.

Part: PAN — CRACKED (C1 DOOR) · airframe 47,879 hrs · 36,167 cycles

CRACK ON C1 DOOR FWD PAN BEHIND DOOR STOP NR 2. REF NRC T0118022. CRACK WAS STOP DRILLED IAW SRM 52-05D FIG 50. REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05D FIG 50 AND IDENTIFIED IAW PS 900-5-1 NR 4.

Part: PAN — CRACKED (C1 DOOR) · airframe 47,879 hrs · 36,167 cycles

CRACK ON C1 DOOR FWD PAN BEHIND DOOR STOP NR 4, REF NRC T0116928. CRACK WAS STOP DRILLED IAW SRM 52-05D FIG 50. INSTALLED REPAIR DOUBLER IAW SRM 52-05D FIG 50 AND IDENTIFIED IAW PS 900-5-1 NR4.

Part: TAB — CRACKED (LT ELEVATOR) · airframe 47,879 hrs · 36,167 cycles

CRACK ON TRAILING EDGE SKIN OF LT ELEVATOR ANTI-FLOAT TAB AT OTBD END. TRAILING EDGE SKIN OF LT ELEVATOR ANTI-FLOAT TAB WAS REPAIRED IAW SRM 55-09 FIG 3 AND OPN 1031 CARD 1361 AND 1369. PERFORMED WEIGHT AND BALANCE IAW SRM 55-20-2D.

Part: TAB — CRACKED (LT ELEVATOR) · airframe 47,879 hrs · 36,167 cycles

CRACK ON OTBD END T/E SKIN OF LT ELEVATOR GEARED TAB. THIS NRC WAS ACCOMPLISHED IAW OPN 1031 CARD 1254-1262 AND SRM 55-04D PAR 3A. THIS REPAIR WAS IDENTIFIED IAW PS 900-5-1 NR 4. WEIGHT AND BALANCE IN LIMITS IAW SRM 55-20-2D.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 47,879 hrs · 36,167 cycles

DELAMINATED LT ELEVATOR ANTI-FLOAT TAB SKIN. LEFT ELEVATOR ANTI-FLOAT TAB WAS REPAIRED IAW SRM 55-04 FIG 3 AND OPN 1031 CARD 1343 AND 1351.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 47,879 hrs · 36,167 cycles

DAMAGED METALIZED COAT ON RUDDER. SURFACE SANDED IAW SRM 51-70-1AD PARA 23 A. (1). PLY OF GLASS FABRIC AND LAMINATE ASTROSTRIKE WERE INSTALLED IAW SRM 51-70-1AD PARA 23 A. (2)(3). RUDDER PAINTED IAW SRM 51-10-3B.

Part: TAB — DENTED (LT ELEVATOR) · airframe 47,879 hrs · 36,167 cycles

DENTS ON LT ELEVATOR GEARED TAB SKIN. THIS NRC WAS ACCOMPLISHED IAW OPN 1031 CARD 1245-1253 AND SRM 55-04D PAR 3A FIG 2. THIS REPAIR WAS IDENTIFIED IAW PS 900-5-1 NO 4. WEIGHT AND BALANCE WITHIN LIMITS IAW SRM 55-20-2D.

Part: PANEL — CORRODED (AFT FUSELAGE) · airframe 47,879 hrs · 36,167 cycles

EXFOLIATION CORROSION ON AFT LAVATORY SERVICE PANEL. REMOVE CORROSION IAW SRM 51-10-3 PAR 35, FOUND OUT OF LIMITS. REPAIR PARTS FABRICATED IAW ERA 472127-14 REV ORIG. REPAIR PARTS INSTALLED IAW ERA 472127-14 REV ORIG AND IDENTIFIED IAW PS 900-5-1 NR 4.

Part: CONTROL VALVE — LOOSE (HYD SYSTEM) · airframe 42,961 hrs · 32,991 cycles

SMOKE AND FUMES IN CABIN AFTER EXTENDED RAMP DELAY. AFT SMOKE DETECTOR SOUNDED. FUMES SMELLED OF RUBBER WERE NOXIOUS AND BURNED EYES. AFTER BLOCK IN NR 1 HYD QTY DOWN TO 1 QT AND A LARGE POOL OF FLUID DISCOVERED ON RAMP. FOUND B-NUT LOOSE ON THRUST REVERSER CONTROL VALVE. TIGHTENED SAME. PERFORMED OPS 5088 2903 AND 5090. REPLACED BOTH WATER SEPARATOR BAGS. SERVICED HYD TO FULL. CLEANED 48 SEC OF EXCESS HYD FLUID. RAN PACKS WITH ENG AIR AT TAKEOFF POWER.

Part: HEATER — OVERHEATED (CARGO) · airframe 39,514 hrs · 30,571 cycles

ON DESCENT INTO ATL AT FL240, F/A REPORTED A STRONG SULFUR ODOR AND A LIGHT HAZE. TURNED OFF GALLEY POWER AND RADIO RACK SWITCH TO VENTURI. THE HAZE AND ODOR DISSIPATED WITHIN 2 MINUTES. REPLACED FWD CARGO HEATER.

Part: PACKING — LEAKING (LT ENG NOSE BUL) · airframe 39,312 hrs · 30,407 cycles

AFTER TAKEOFF, FLIGHT ATTENDANTS NOTIFIED FLIGHT CREW THAT BOTH AFT LAV SMOKE DETECTORS WERE GOING OFF. REPLACED PACKING IN LEFT ENGINE NOSE BULLET DUE TO OIL LEAK.

Part: JAM-NUT — LOOSE (COCKPIT) · airframe 34,638 hrs · 27,180 cycles

WHEN NOSE LIGHTS SWITCH TURNED OFF AFTER T/O, SPARKS FLEW FROM SWITCH UNIT. C/BS STAYED IN, BUT WERE PULLED BY CREW. FOUND JAM NUT LOOSE ON NOSE LIGHTS SWITCH CAUSING TERMINAL TO CONTACT METAL SUPPORT STRUCTURE. SECURED JAM NUT. CYCLED SWITCH SEVERAL TIMES, NO DEFECTS NOTED.

Part: DUCT — UNSERVICEABLE (NR 2 ENGINE) · airframe 33,369 hrs · 26,249 cycles

FOUND ON ARRIVAL DFW NR 2 ENGINE UPPER ENG COWL DAMAGED UPON FURTHER INVESTIGATION FOUND NBR 2 ENG ANTI-ICE DUCT BLOWN C/A RPLCD BOTH SECTIONS OF VSV ANTI-ICE DUCT AND VALVE. LEAKS CHECKS GOOD.

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 32,765 hrs · 25,818 cycles

DURING HMV-2, REPLACEMENT OF THE RT INNER & OUTER HINGE PLATES, TOOLING DAMAGE WAS INCURRED AT A SINGLE FASTENER LOCATION ON ANGLE PN 3912080504 AND REAR SPAR CAP PN 5911384506.THE HOLE WAS OVERSIZED AND BUSHED ON EACH PART.

Part: FAN — FAILED (RECIRCULATION) · airframe 32,418 hrs · 25,572 cycles

AFT FLIGHT ATTENDANT NOTED STRANGE NOISE AND HOT ODOR JUST AFTER ROTATION. A/C RETURNED PHL WITHOUT INCIDENT. RECIRCULATION FAN GROWLED UPON SPIN-UP WHILE TESTING. REPLACED FAN

Part: OVEN — DIRTY (GALLEY)

FWD GALLEY OVEN BEGAN TO SMOKE AND EMIT AUDIBLE CRACKLE AFTER T/O. CONTINUED WITH C/B PULLED AND GALLEY POWER OFF. REPLACED OVEN.

Part: CSD — FAILED (NR 2 ENGINE)

RT GEN DROPPED OFF LINE/AC X-TIE LOCKOUT/SPARKS REPORTED COMING FROM UNDERSIDE OF ENG. REPLACED CSD/GEN AND GCU.

Part: PULLEY — BROKEN (LT LE SLAT)

ON L/O, FOUND LT WING I/B SLAT POS NR 0 LOOSE. FOUND RETRACT CABLE PULLEY BROKEN FOR SLAT ZERO. PULLEY WAS SCARRED. FOUND SLAT 5 DRIVE CABLE PULLEY DENTED, FALSE RIB AT SLAT ZERO TORN, AND MAIN SLAT ZERO DRIVE CABLE IN BAG BIN KINKED. REPLACED ALL BROKEN OR DAMAGED PARTS.

Part: SKIN — DENTED (FS 218/207)

TWO DENTS HAVE BEEN FOUND IN THE FUSELAGE. ONE IS LOCATED AT THE FS 218, STR 17L. IT WAS MEASURED TO BE .105 DEEP. THE OTHER WAS FOUND AT FS 207, STR 17L AND IS 0.065 DEEP. THESE DENTS WERE REPAIRED WITH ONE DOUBLER PER THE MD-88 SRM 53-04, FIG 12B CLASS I. THIS REPAIR WAS APPROVED BY FAA/DER FORM 8110-3, DER DESIGNATION SO-889, DATED 7-24-97.

Part: SKIN — GOUGE (SERVICE DOORWAY)

THE FUSELAGE SKIN NEAR THE AFT SERVICE DOOR HOLD OPEN PIN CUTOUT WAS GOUGED ON THE INNER SURFACE. THE DAMAGE IS 0.050 DEEP AND MEASURES 2.5 FWD/AFT BY 1.5 UP/DOWN. THIS DAMAGE WAS REPAIRED WITH A DOUBLER AND APPROVED BY FAA/DER FORM 8110-3, DER DESIGNATION SO-889, DATED 7-24-97.

Part: FRAME — CRACKED (RT MLG CUTOUT)

A 3 INCH CRACK IN O/B FWD FRAME OF MLG DOOR CUTOUT. CRACK WASB FOUND AT E-1 LTR CKECK. REPAIRED PER SRM 53-05 FIG 78A.

Part: LINK — BROKEN (NLG DOOR)

ON DEPARTURE FROM SAN, NOTED VIBRATIONS DURING LDG GEAR RETRACTION. FOUND RT NOSE GEAR FWD DOOR LINK BROKEN. REPLACED LINK PER MM 32-22-01 PG 203 TO 204. GEAR RETRACTION NORMAL.

Part: NR 6 BRG SEAL — DAMAGED (NR 2 ENGINE)

RT ENGINE OIL QTY WENT TO ZERO ON DESCENT AT 16000 FEET, FOLLOWED BY LOW OIL PRESSURE LIGHT. SHUT DOWN ENGINE PER POM. REPLACED NR 6 BEARING CARBON SEAL AND SCAVENGE PUMP, OPERATION NORMAL.