N907DL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,552 hrs · 62,593 cycles

FOUND ROW 10-12 CEILING OVERHEAD EMER LIGHTS OUT ON SVC. R+R ROW 10-12 CEILING LIGHT BATTERY PER MD AMM 33-50. OPS CHECK GOOD. (LP4755447)

Part: DUCT — BLOWN (RT ACM) · airframe 80,885 hrs · 62,019 cycles

DIVERTED DUE TO A LOSS OF PRESSURIZATION DURING CLIMB, AFTER A TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. THE CREW FOLLOWED THE QRH PROCEDURES AND WITH LEFT ENGINE AT IDLE THE LIGHT WENT OUT. AFTER THE QRH STEPS WERE COMPLETED, THE FLOW LIGHT CYCLED ON AND OFF DURING CLIMB TO FL240 WITH A CABIN ALTITUDE WARNING. AN EMERGENCY DESCENT TO FL8K WAS ACCOMPLISHED. THE CABIN ALTITUDE NEVER WENT ABOVE 11K. MAINTENANCE PERFORMED NOGO ODI WORK CARD PROCEDURES AND PERFORMED A LEAK CHECK OF THE TAIL COMPARTMENT. THE RIGHT AIR CYCLE MACHINE BOOT WAS FOUND BLOWN OFF. MAINTENANCE CONNECTED THE BOOT AND A PACK LEAK CHECK WAS PERFORMED. A RIGHT PRSOV ELECTRICAL CONNECTOR WAS FOUND DAMAGED. THE CONNECTOR AND PRSOV WERE REPLACED IAW THE AMM. THE RIGHT PACK CHECKED OK. THE LEFT PACK FAILED THE CONFIDENCE CHECK. MAINTENANCE FOUND A DUCT ON LEFT PACK TO WATER SEPARATOR TEMP CONTROL VALVE LEAKING. THE DUCT WAS REPLACED IAW THE AMM.

Part: SKIN — CRACKED (FUEL TANK) · airframe 79,332 hrs · 60,769 cycles

DURING BHEC/HFEC INSPECTIONS OF CENTER TANK LOWER SKIN REPAIR AREA PER PRI 563649-14AD REV 1 STEPS 7 AND 8 CRACK FOUND IN CENTER TANK LOWER FWD SKIN IN AND AROUND FASTENER HOLE JUST FORWARD OF CUTOUT IN AFT SKIN (SHOWN IN FIG 1 SHEET 1 OF PRI). CRACKS EXTEND FWD OF AND AFT OF FASTENER HOLE. (MARKED ENDS OF CRACKS FROM INSIDE TANK). COMPLIED WITH PRI / ERA 563649-14AD REV 7 AND ERA 563883-14 REV ORIG. PRI 563649-14AD REV 7 MATCHES FINAL ERA 563649-14AD REV ORIG.

Part: BARREL NUT — CORRODED (HORIZONTAL STAB) · airframe 79,332 hrs · 60,769 cycles

BARREL NUT - RUSTY. AFT BARREL NUT ON UPPER AFT SPAR OF LH HORIZONTAL STABILIZER ON INBOARD END REF. REPLACED HARDWARE REF; MD88 SRM 51-30-01, AND MD88 AMM 20-10-14 REF N/R CARD 00024. (LP0337760)

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 79,332 hrs · 60,769 cycles

BARREL NUT HOLE HAS CORROSION - HORIZONTAL STABILIZER-LEFT SIDE REAR SPAR AFT ATTACH BOLT HOLE. REPAIRED PER ER/A 563685-14AD. (LP# 0329725)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,825 hrs · 60,349 cycles

OVERWING EMERGENCY LIGHT (AFT) INOPERATIVE. R & R POWER SUPPLY BATTERIES IAW AMM 33-53. OPS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,529 hrs · 59,340 cycles

SEAT MOUNTED EMERGENCY LIGHTS WERE INOPERATIVE AT 13ED, 17ED AND 19ED. REPLACED THE LAMPS. CHECKED GOOD IAW AMM 33-53. OK FOR SERVICE.

Part: BATTERY PACK — ABNORMAL (EMERGENCY LIGHTS) · airframe 77,087 hrs · 59,000 cycles

LT & RT AUX EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES ON EMERGENCY POWER PACK B5-103.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 76,293 hrs · 58,430 cycles

NR 2 HYDRAULIC PRESSURE WENT TO ZERO IN FLIGHT WITH HIGH HYDRAULIC QTY. HYDRAULIC PRESSURE REGAINED WITH THE AUXILIARY PUMP ON IAW CHECKLIST, QTY RETURNED TO NORMAL. MAINTENANCE FOUND EXCESSIVE AIR IN RT HYDRAULIC SYSTEM AND ALSO NOTED GROUND CONTROL ACTUATOR VALVE LEAKING FROM FITTING. REPLACED HYD LINE WITH ALL SUBSEQUENT CHECKS GOOD.

Part: SENSOR — MALFUNCTIONED (OIL TEMP) · airframe 75,725 hrs · 57,998 cycles

WHILE ENROUTE FLIGHT DIVERTED DUE TO RT ENGINE HIGH OIL TEMP, THE ENGINE WAS NOT SHUTDOWN BUT AN EMERGENCY WAS DECLARED. MAINTENANCE RAN ENGINE AND DUPLICATED THE OIL TEMP ISSUE, REPLACED OIL TEMP BULB AND PERFORMED IMMERSION THERMOCOUPLE TEST. OIL TEMP GOOD.

Part: WIRE — UNSECURE (TEMP PROBE) · airframe 74,958 hrs · 57,421 cycles

THE NR 2 ENGINE OIL TEMPERATURE WENT TO 170 DEGREES C WITH AN ASSOCIATED RED WARNING LIGHT. THE OIL PRESSURE REMAINED WITHIN LIMITS. CREW SHUTDOWN THE NR 2 ENGINE IAW THE QRH. TEMPERATURE DECALS HAD NO COLOR CHANGE. OIL FILTER AND CHIP DETECTORS WERE CLEAN. FOUND WIRE CRIMP LOOSE AT WIRE E355A18N. RETERMINATED WIRE AND REPLACED, B3-2 OIL TEMP PROBE. IMMERSION THERMOCOUPLE CHECK GOOD IAW AMDS 7900-01123-0201. SATISFACTORY TEST FLIGHT COMPLETED ON LP 8007091. THE ACFT HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,765 hrs · 57,275 cycles

MAINTENANCE FOUND 1R, 1L AND THE COCKPIT EMERGENCY LIGHTS INOPERATIVE. BATTERY PACKS REPLACED. EMERGENCY LIGHTS CHECKED OK.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 74,734 hrs · 57,247 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE IN THE AFT CABIN ZONE. A BLOWN F1 FUSE WAS FOUND AND REPLACED IN THE AFT CABIN BATTERY PACK. ALSO, WIRE L962U14 ADJACENT TO LIGHT ASSY L2-848 WAS FOUND CHAFING AGAINST A STRUCTURE AND THE WIRE WAS REPAIRED. ALL EMERGENCY LIGHTS CHECKED GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY SEAT ROW LIGHTING INOPERATIVE ROW 31 AND AFT RT SIDE. REPLACED FUSE ON BATTERY PACK.

Part: STRUCTURE — DAMAGED · airframe 74,413 hrs · 57,022 cycles

TWO FASTENERS ON ONE SIDE OF THE CUT LINE OF THE APB LOWER CHORD BETWEEN LONGERONS 26RT AND 27RT. CUT LINE OF THE APB LOWER CHORD BETWEEN LONGERONS 26RT AND 27RT WAS REPAIRED IAW ER/A 541554-14, REV ORIGINAL. RII COMPLETED.

Part: FASTENER — NOT REPORTED (NOT REPORTED) · airframe 74,413 hrs · 57,022 cycles

TWO FASTENERS ON ONE SIDE OF THE CUT LINE OF THE APB LOWER CHORD BETWEEN LONGERONS 26 LT AND 27 LT. FASTENERS WAS ATTENDED WITH ER/A 541554-14, REV ORIGINAL. RII COMPLETED.

Part: DOUBLER — CORRODED (BS 584) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON PRODUCTION DOUBLER BS 584 BETWEEN LONGERONS 28 - 29L. PRODUCTION DOUBLER WAS REPAIRED IAW ER/A 539957-14, REV ORIGINAL EQUIPMENT, PANAMETRICS NDT35DL. TRANSDUCER SON OPEN V260SM.

Part: WEB — CRACKED (BS 1437) · airframe 74,413 hrs · 57,021 cycles

CRACK ON WEB BS 1437 PROJECTION LONGERON 10L AFT ACCESORY COMPARTMENT. WEB WAS REPAIRED BS 1437 IAW ER/A 519146-14, MA REV B. HFEC INSPECTION WAS PERFORMED CRACKED OF 1.450" NDT SPM 06-10-01.001. PHASECAD 16D-1041.

Part: DOOR FRAME — CORRODED (BS 370-427) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON LOWER DOOR JAMB BETWEEN BS 370 - 427 FWD CARGO COMP. LOWER DOOR JAMB BETWEEN BS Y=370-427 WAS REPLACED IAW SRM 53-05, FIG 44A AND ER/A 539923-14, REV ORIG RII.

Part: FRAME — WORN (BS 218) · airframe 74,413 hrs · 57,021 cycles

WORN FRAME AT BS 218 BETWEEN LONGERONS 9RT AND 10RT. FRAME WAS REPAIRED IAW ER/A 539935-14 REV ORIGINAL.

Part: PAN — CRACKED (BS 160) · airframe 74,413 hrs · 57,021 cycles

CRACKED PAN ON MAIN ENTRANCE DOOR BETWEEN BEAMS 7 AND 8, BS 160. CRACK PAN ON MAIN ENTRANCE DOOR BETWEEN BEAM 7 AND 80 BS Y=160 WAS REPAIR IAW SRM 52-05D FIG 41 AND ER/A 539945-14, REV ORIG RII COMPLETED.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 74,413 hrs · 57,021 cycles

WEAR ON PREVIOUS REPAIR DOUBLER, UPPER SKIN, APPROXIMATELY XV2=299 ON OTBD VANE OF OTBD FLAP AT LT WING. REPAIR DOUBLER, UPPER SKIN APPROXIMATELY BS XV2=299 ON OTBD VANE OTBD FLAP AT LT WING WAS REPLACED IAW SRM 57-30D, PAR II AND CARD 2000-8149-06 CREW 02, 1329807, JOB 000-0036.

Part: CARGO TRACK — CORRODED (BS 1007-1155) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON RT CARGO TRACK FROM BS 1007 TO 1155. THE CARGO TRACK WAS REPLACED.

Part: HEATER BLANKET — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION POINTS ON RT HEATER BLANKET AT SETTLEMENT OF ACCESS COVER 1410C. CORROSION WAS ATTENDED IAW ER/A 539917-14AD, REV ORIGINAL. ACCESS PLATE 1410C ARE IS 0.004" THEREFORE IT'S OUT OF LIMITS AND WAS REPAIRED IAW ER/A 539917-14AD.

Part: RIB — CRACKED (BS 989) · airframe 74,413 hrs · 57,021 cycles

CRACK ON RIB BS Y=989, X=4 AT KEEL BEEM INTERNAL STRUCTURE. RIB WAS REPAIRED IAW SRM 53-01, FIG 2.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 74,413 hrs · 57,021 cycles

NICKS ON SKIN AT LT WING INBD FLAP BS XIFI=0.721 TO XW=4. 7. NICKS ON SKIN AT LT WING INBD FLAP WERE REPAIRED IAW SRM 57-01 AND 57-03, FIG 8.

Part: FRAME — CRACKED (BS 1418) · airframe 74,413 hrs · 57,021 cycles

CRACK ON FRAME BS 1418 BETWEEN LONGERON 2LT TO 2RT. FRAME WAS REPAIRED IAW SRM 53-01, FIG 2, 51-01, PAR 21, 51-30-5, 51-10-3, PAR 14/21, 51-30-2 AND DWG SR09530003-39.

Part: CARGO TRACK — CORRODED (BS 1007-1322) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON LT TIE TRACK BETWEEN BS 1007 TO 1322 AT AFT CARGO COMPARTMENT. DUE TO EXCESSIVE CORROSION TIE TRACKS WERE REPLACED IAW SRM 51-10-04 AND 51-30-2.

Part: FLOOR PANEL — DELAMINATED · airframe 74,413 hrs · 57,021 cycles

DELAMINATED FLOOR PANEL 886C. FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201. FLOOR PANEL WAS CLEANED. FLOOR PANEL REPLACED IAW DWG 9936639, REV P.

Part: VANE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON SETTLEMENT AREA OF CLEVIS BS XV1= 158 ON INBD VANE OF OTBD FLAP RT WING. INBD VANE OF OTBD FLAP RT WING WAS REPLACED IAW AMM 27-51-03.

Part: CARGO TRACK — CORRODED (BS 645-769) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON LT CARGO TRACK BETWEEN BS 645-769. THE CARGO TRACK WAS REPLACED IAW SRM 53-24-0D AND 53-05, FIG 4G.

Part: SKIN — WORN (RT WING TE FLAP) · airframe 74,413 hrs · 57,021 cycles

WEAR ON LOWER SKIN APPROXIMATELY XIVIF =47 ON INBD VANE OF INBD FLAP AT RT WING. THE FLAP WAS REPAIRED IAW SRM 57-03D, PAR II.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 74,413 hrs · 57,021 cycles

NICKS ON LOWER PREVIOUS REPAIR DOUBLER ON INBD VANE OF INBD FLAP AT RT WING. INBD VANE OF INBD FLAP WAS REPAIRED IAW SRM 57-03, D PAR II.

Part: CARGO TRACK — DAMAGED (BS 731-773) · airframe 74,413 hrs · 57,021 cycles

ELONGATED HOLES ON RT CARGO TRACK BETWEEN BS 731 - 773. THE CARGO TRACK WAS REPLACED IAW DWG 5936587, REV CC, AND SRM 51-30-1.

Part: LONGERON — CRACKED (BS 540) · airframe 74,413 hrs · 57,021 cycles

CRACK ON LONGERON 4R BS 540. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION OUT OF LIMITS ON FLOOR PANEL NR 120D. THE FLOOR PANEL WAS REPLACED.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 74,413 hrs · 57,021 cycles

NICKS ON PREVIOUS REPAIR, LE AND LOWER SKIN ON INBD VANE OF INBD FLAP AT LT WING. PREVIOUS DOUBLER REPAIR WAS REPLACED IAW SRM 57-03D P.11.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON RT CARGO TRACK BETWEEN BS 1212 - 1322. THE CARGO TRACK WAS REPLACED.

Part: SKIN — DAMAGED (RUDDER) · airframe 74,413 hrs · 57,021 cycles

DAMAGE METALLIZED OF RUDDER BOTH SIDE. RUDDER BOTH SIDE WAS REPAIRED AND PAINTED IAW SRM 51-70-1A, P23 AND 51-10-3B, PROCESS "B".

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR NR 1311C AT LT WING. ACCESS DOOR 1311C WAS REPLACED IAW SRM: 51-22-2A, COND 2, PAR 1.

Part: DOOR FRAME — CORRODED (BS 660-693) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

EXFOLIATION CORROSION ON LOWER DOOR JAMB BETWEEN BS Y=660 TO 693 MID CARGO COMP. PREVIOUS REPAIR AND CORROSION WERE REMOVED WITH ORIGINAL THICKNESS, BS Y=687 0.210" AND REMAINING IS 0.167", BS Y=645-686, ORIGINAL THICKNESS 0.280" AND REMAINING 0.219" THEREFORE WITHIN LIMITS BUT ON BS Y=643-644, ORIGINAL THICKNESS 0.280" AND REMAINING IS 0.195" THEREFORE OUT LIMITS IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-3, PAR 26 AND AREA WAS REPAIRED IAW SRM 53-05, FIG 123, OPTION 1.

Part: SKIN — DAMAGED (BS 148-160) · airframe 74,413 hrs · 57,021 cycles

WEAR ON RECEIVER OF L1 DOOR HOOK AT EXTERNAL FUSELAGE SKIN BETWEEN LONGERON 15LT AND 14LT, BS 160 TO 148. NEW DOUBLER WAS FABRICATED, DRILLED, PAINTED, AND INSTALLED IAW SRM 53-04, FIG 24, SHEET 2, 51-10-4, 51-10-3 PAR 14, 51-30-2, AND 51-30-5, 51-10-2. PIN WAS REPLACED.

Part: SUPPORT — BROKEN (BS 1271) · airframe 74,413 hrs · 57,021 cycles

BROKEN RT SLANT SUPPORT BS 1271 AT AFT CARGO COMPARTMENT. SLANT SUPPORT WAS REPLACED IAW ER/A NR 413029-14MA.

Part: DOOR FRAME — CRACKED (BS 937) · airframe 74,413 hrs · 57,021 cycles

CRACK ON FWD DOOR JAMB, BS 937, X-8 AT W/W . CRACK WAS STOP DRILLED AND FABRICATED DOUBLER TREATED AND PAINTED IAW SRM 53-01, FIG 2 AND 51-10-3, PAR 14.

Part: CUSP WEB — DAMAGED (BS 267-271) · airframe 74,413 hrs · 57,021 cycles

TOOL DAMAGE ON LT CUSP WEB, BS 267-271 BETWEEN X 44-X 54 AT PAX CABIN. THE CUSP WEB WAS REPAIRED WITH ER/A 539927-14, REV ORIGINAL.

Part: SUPPORT — BROKEN (BS 598) · airframe 74,413 hrs · 57,021 cycles

BROKEN SLANT SUPPORT, BS 598 BETWEEN LONGERONS 27-28L. SLANT SUPPORT WAS REPLACED IAW ER/A 413029-14MA, REV D.

Part: SKIN — DAMAGED (RUDDER) · airframe 74,413 hrs · 57,021 cycles

DAMAGE METALLIZED ON RUDDER FAIRING NR 6508A. RUDDER FAIRING NR 6508A WAS REPAIRED IAW SRM 51-70-1A, PAR 23 AND CARD 2000-8149-01.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 74,413 hrs · 57,021 cycles

DELAMINATED FLOOR PANEL. THE FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201. AND REPLACED THE FERRULE IAW AMM 53-20-01-201.

Part: LONGERON — CRACKED (BS 1437) · airframe 74,413 hrs · 57,021 cycles

CRACKED LONGERON 4L AT BS 1437 AFT ACCESSORY COMPARTMENT. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: FLOOR SUPPORT — CRACKED (BS 1287-1309) · airframe 74,413 hrs · 57,021 cycles

SEVERAL CRACKS IN FLOOR SUPPORT BS 1287-1309, BL 0 BETWEEN CABIN FLOORBEAMS AFT CARGO. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-5, 51-10-4, AND DWG 5930560, REV BC.

Part: LONGERON — CRACKED (BS 1437) · airframe 74,413 hrs · 57,021 cycles

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

Part: SEAT TRACK — CORRODED (BS 1214) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION OUT OF LIMITS ON LT SEAT TRACK, X=22 BS 1214. SEAT TRACK WAS REPLACED IAW SRM 53-05, PAR 4B AND FIGURE 4F.

Part: FRAME — CRACKED (BS 1380) · airframe 74,413 hrs · 57,021 cycles

CRACK ON FRAME ANGLE BS 1380 LONGERON 15R IN AFT ACCESSORY COMPARTMENT. THE FRAME ANGLE WAS REPLACED IAW SRM 53-14-4, FIG 1, SHEET 2, SRM 51-30-5, 51-30-2.

Part: SKIN — DENTED (ELEVATOR TAB) · airframe 74,413 hrs · 57,021 cycles

DENTS ON GEARED TAB UPPER SKIN AT LT ELEVATOR. GEARED TAP UPPER SKIN AT LT ELEVATOR WAS REPAIRED IAW SRM 55-04, PAR 2.

Part: SKIN — DENTED (ELEVATOR TAB) · airframe 74,413 hrs · 57,021 cycles

DENTS ON RT ELEVATOR ANTI-FLOAT TAB UPPER SKIN BS XEFT=163 AND XEFT=208. RT ELEVATOR ANTI-FLOAT TAB UPPER SKIN BS XEFT=163 AND XEFT=208 WAS REPAIRED IAW SRM 55-04, PAR 2.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 74,413 hrs · 57,021 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL REPAIRED IAW AMM 25-00-00-801.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 74,413 hrs · 57,021 cycles

CRACKED SUPPORT ON MAIN ENTRANCE DOOR BETWEEN BEAM 89 AND LOWER EDGE, BS Y=180. SUPPORT ON MAIN ENTRANCE DOOR WAS REPLACED IAW SRM 51-30-2.

Part: FORMER — CRACKED (LT WING) · airframe 74,413 hrs · 57,021 cycles

CRACKED FORMER ON LT WING FIXED L/E BS XFS=303.125, CARD 164, ZONE 10. FORMER WAS REPLACED IAW SRM 51-30-2 AND DWG 9937588, REV G. RE-WRITE TO CARD NR 20000088655, CARD 178, ZONE 10.

Part: SKIN — CRACKED (PAX DOOR) · airframe 74,413 hrs · 57,021 cycles

CRACKED SKIN ON MAIN ENTRANCE DOOR BETWEEN BEAM 4 AND 5, BS Y=180. SKIN WAS REPAIRED IAW ERA 501106-14MA, REV B.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 74,413 hrs · 57,021 cycles

DAMAGED FERRULE ON FLOOR PANEL. FERRULE REPLACED IAW AMM 53-20-01 201.

Part: HINGE — WORN (LT WING) · airframe 74,413 hrs · 57,021 cycles

LEFT WING OTBD FLAP HINGE AT BS XW= 333 HAS PLAY AT HINGE POINT, LW. AFT FLAP HINGE, BOLT OF HINGE POINT, AND BUSHINGS OF LT WING OTBD FLAP HINGE AT BS XW=333.147 WERE REPLACED IAW CMM 27-50-5 AND AMM 27-51-01.

Part: PANEL — CRACKED (NR 2 SLAT) · airframe 74,413 hrs · 57,021 cycles

CRACKS ON AFT FACE SLAT PANEL NR 2, BS XRS=240.000 APPROXIMATELY RT WING. CRACKS WERE REMOVED, FILLER AND DOUBLER WAS FABRICATED, TREATED, PAINTED AND INSTALLED, IAW SRM 57-09 FIG 10-13 AND 51-10-3, PAR 21 AND 14.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 74,413 hrs · 57,021 cycles

DELAMINATED FLOOR PANEL. THE FLOOR PANEL WAS REPAIRD AND REPLACED IAW AMM 53-20-01-201.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR NR 1414C AT RT WING. FUEL ACCESS DOOR 1414C WAS REPLACED IAW SRM 51-22-2A.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 74,413 hrs · 57,021 cycles

DELAMINATED FLOOR PANEL NR: 1079B. FLOOR PANEL NR 1079B WAS FABRICATED IAW AMM 53-20-01-201.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 74,413 hrs · 57,021 cycles

DELAMINATED FLOOR PANEL NR 200E. FLOOR PANEL NR 200E WAS FABRICATED IAW AMM 53-20-01-201.

Part: SKIN — DAMAGED (BS 965-684) · airframe 74,413 hrs · 57,021 cycles

LIGHTNING STRIKE ON LOWER AFT CORNER AT RT WINDOW BELT BETWEEN BS Y=965 TO Y=984. LIGHTNING STRIKE WAS BLENDED OUT AND EVALUATED IAW SRM 53-05, FIG 111 AND ERA 539930-14 REV ORIGINAL. NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1 AND 2 WAS ACCOMPLISHED.

Part: LONGERON — CRACKED (BS 160) · airframe 74,413 hrs · 57,021 cycles

CRACKED LONGERON NR 3L, BS Y=160. LONGERON WAS REPAIRED IAW SRM 51-30-5, 51-30-2 AND 51-10-3 PAR 14 AND 21, SRM 53-14-1, FIG 3, SRM 53-02, FIG 18 AND CARD 5330-01204-0205, JOB 040-0005.

Part: LONGERON — CRACKED (BS 200) · airframe 74,413 hrs · 57,021 cycles

CRACKED LONGERON NR 4L, BS 200. LONGERON WAS REPLACED IAW SRM 51-10-3, PAR 14 AND 21 51-30-2, 51-30-5.

Part: SKIN — CORRODED (BS 1322-1338) · airframe 76,771 hrs · 58,802 cycles

CORROSION ON FUSELAGE SKIN BETWEEN BS 1322 - 1338 AND LONGERONS 20 TO 23L. THE CORROSION WAS REMOVED IAW SRM.

Part: CUSP WEB — CORRODED (BS 532) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON PREVIOUSLY REPAIR DOUBLER RT CUSP WEB BS 532 BETWEEN X=54 -X=60 AT PAX CABIN. CUSP WEB WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5 AND 51-10-3 PAR 14, 21.

Part: SPAR — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON FRONT SPAR LOWER EDGE FROM BS=XTE=82 TO XET=98 AT RT ELEVATOR. CORROSION WAS REMOVED IAW SRM 51-10-3, PARR. 26, 21 AND 14 (UT) WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1 AND 2.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR NR 1303C AND 1409C. FUEL ACCESS DOOR NR 1303C AND 1409C WERE REPLACED IAW SRM: 51-22-2A.

Part: CUSP WEB — CORRODED (BS 1248) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON LT CUSP WEB BS 1248, BETWEEN X=50 TO X=60 AT CABIN FLOOR STRUCTURE. SEAT TRACK WAS REMOVED DAMAGE ON CUSP WEB WAS REMOVED, PARTS FOR REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIG 131A-14 AND SEAT TRACK WAS INSTALLED IAW SRM 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR NR 1464C AT RT WING. CORROSION ON COUNTERSINK WAS REMOVED AND MEASURED. 3 HOLES OUT OF LIMITS ADJACENT WERE FOUND WITH .544", .541", AND .559". THEREFORE IS OUT OF LIMITS AND THE ACCESS DOOR 1464C WAS REPLACED IAW SRM 51-22-2A.

Part: SEAT TRACK — CORRODED (BS 826) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON SEAT TRACK X=-54, BS 826 AT PAX CABIN IN REF ORNRC 49, ZONE 201. SEAT TRACK X=-54, BS Y=826 WAS REPAIRED IAW SRM 53-05, FIG 4A SH1.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR NR 1454C AT RT WING. CORROSION ON COUNTERSINK WAS REMOVED AND MEASURED 3 HOLES OUT OF LIMITS ADJACENT WERE FOUND WITH .539", .539", AND .541". THEREFORE IT IS OUT OF LIMITS AND FUEL ACCESS DOOR 1454C WAS REPLACED IAW SRM 51-22-2A.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 74,413 hrs · 57,021 cycles

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

Part: SEAT TRACK — CORRODED (BS 1055-1056) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION OUT OF LIMITS ON LT SEAT TRACK, X=54, BS 1055-1056. THE SEAT TRAC WAS REPAIRED IAW SRM 53-05, FIG 4A, 51-10-3 PAR 21, 14, 38.

Part: CUSP WEB — CORRODED (BS 892-901) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION OUT OF LIMITS ON RT CUSP WEB BETWEEN BS 892 TO 901 AT PASSENGER CABIN, IN REF TO CARD 92, AC ZONE 201, SM, CARD 289, ZONE 201. RT CUSP WEB BETWEEN BS Y=892 TO 901 WAS REPAIRED IAW SRM 53-05, FIG 131A -14, SH 1-9.

Part: DOUBLER — WORN (PAX DOOR) · airframe 74,413 hrs · 57,021 cycles

WORN DOUBLER ON MAIN ENTRANCE DOOR AT LOWER EDGE, SH-CP-SM, CARD 198, ZONE 201. WORN DOUBLER ON MAIN ENTRANCE DOOR AT LOWER EDGE WAS REPLACED IAW SRM 51-30-2 AND 52-05D FIG 37.

Part: CUSP WEB — CORRODED (BS 453-500) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON RT CUSP WEB BS 453-500 BETWEEN X -54 TO X -60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 PAR 144, FIG 131A-6, 51-30-5, 51-10-3, PAR 14 AND 21.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR NR 1462C AT RT WING. CORROSION ON COUNTERSINK WAS REMOVED AND MEASURED 3 HOLES OUT OF LIMITS ADJACENT WERE FOUND WITH .545" .555", AND .538". THEREFORE IS OUT OF LIMITS AND FUEL ACCESS DOOR 1426C WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR NR 1472C AT RT WING. CORROSION ON FUEL ACCESS DOOR 1472C WAS REMOVED AND IS OUT LIMITS AND WAS REPLACED IAW SRM 51-22-2A AND WILL BE INSTALLED WITH CARD 2800-0390, JOB 001-0401, STEP 8 AND 9.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR NR 1456C AT RT WING. CORROSION ON COUNTERSINK WAS REMOVED AND MEASURED. 3 HOLES OUT OF LIMITS ADJACENT WERE FOUND WITH .540" .546, AND .541". THEREFORE IS OUT OF LIMITS AND FUEL ACCESS DOOR 1456C WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR NR 1361C AT LT WING. CORROSION WAS REMOVED AND MEASURED ON SETTLEMENT AREA. ORIGINAL FIG 0.150" AND MINIMUM REMAINING THICKNESS IS 0.125". THEREFORE IT IS OUT OF LIMITS IAW SRM 51-22-2A AND FUEL ACCESS PLATE 1316C WAS REPLACED IAW IPC 57-30-00.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 74,413 hrs · 57,021 cycles

DELAMINATED FLOOR PANEL 160F. FLOOR PANEL 160F FABRICATED IAW AMM 53-20-01 201.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR 1379C AT LT WING. FUEL ACCESS PLATE 1379C IS OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A AND WILL BE INSTALLED WITH CARD 2800-0120, JOB 001-0395, STEP NR 10 AND 11.

Part: SEAT TRACK — CORRODED (BS 1018) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION OUT OF LIMITS ON RT SEAT TRACK, X -22, BS 1018 AT PAX CABIN. THE SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIG 4A, SHEET 1 AND 51-10-3, PAR 21-14 AND 38.

Part: LONGERON — CRACKED (BS 1437) · airframe 74,413 hrs · 57,021 cycles

CRACK ON LONGERON NR 16RT, BS 1437 AFT ACCESSORY COMPARTMENT. LONGERON WAS REPLACED IAW SRM 53-14-4, 51-30-2, 51-30-5, 51-10-3, PAR 21 AND 14.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR NBR 1436C AT RT WING. (AYP). (CARD 100, ZONE 00). ACCESS FUEL TANK 1436C WAS MEASURED MAX DIAMETER ALLOWED .660" AND FOUND 3 HOLES WITH .669" AND .670", .671" OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A.

Part: FRAME — CRACKED (BS 1450) · airframe 74,413 hrs · 57,021 cycles

CRACKED FRAME FWD EDGE BS 1450 APPROXIMATELY BETWEEN LONGERONS 2LT TO 3LT AFT ACCESORY COMPARTMENT. FRAME WAS REPLACED IAW DWG 9911860-3, REV L AND SRM 51-30-2, 51-30-5.

Part: SKIN — DAMAGED (BS 446) · airframe 74,413 hrs · 57,021 cycles

LIGHTNING STRIKE ON FASTENER BS 446, LONGERON 2LT FUSELAGE SKIN. LIGHTNING STRIKE ON FASTENER AND FUSELAGE SKIN STA Y=446 LONGERON 2LT WAS REPAIRED IAW SRM 53-04-2, SHEET 17. PERFORM VISUAL INSPECTION EVERY 8000 CYCLES IAW SRM 53-04-2.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR NR 1410C AT RT WING. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR NR 1410C AT RT WING WAS R & R IAW SRM 51-22-2A.

Part: SEAT TRACK — CORRODED (BS 952) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON SEAT TRACK BS 952, X -54 . DAMAGE WAS REMOVED, PLUG WAS ADJUSTED, AREA AND PLUG WERE TREATED AND PAINTED, PLUG WAS INSTALLED IAW SRM 53-05, FIG 4A, 51-10-3, PAR 14, 21 AND 38.

Part: WEB — CRACKED (BS 178-200) · airframe 74,413 hrs · 57,021 cycles

CRACKED DIAPHRAGM, BELLOW ON FLOOR SUPPORT, IN X=56 APPROXIMATELY BETWEEN BS Y=178-200 AT CABIN FLOOR STRUCTURE. W1, SM, CARD 212, ZONE 201. DIAPHRAGM WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-01, FIG 2, SH 3, 51-10-3 PAR 14, 21, & 38. CRACK IS .125".

Part: FLOOR SUPPORT — CRACKED (NOT REPORTED) · airframe 74,413 hrs · 57,021 cycles

CRACK ON FLOOR SUPPORT. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 51-70-1D PAR. 8.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 74,413 hrs · 57,021 cycles

DELAMINATED LT FLOOR PANEL . THE FLOOR PANEL WAS REPAIRED IAW SRM 51-70-1D, PAR 10.

Part: SKIN — WORN (WINDOW BELT) · airframe 74,413 hrs · 57,021 cycles

WEAR ON UPPER AFT CORNER AT LT WINDOW BELT BETWEEN BS 294 - 313. WEAR ON UPPER AFT CORNER AT LT WINDOW BELT BETWEEN BS 294 - 313 WAS REWORKED IAW ER/A 539921-14, REV. ORIGINAL SECTION 1. HFEC INSPECTION WAS PERFORMED ON BLENDED AREA NO CRACKS WERE FOUND IAW ER/A 539921-14, REV ORIGINAL SECTION 1 AND NDT SPM 06-10-01, 001.

Part: CUSP WEB — CORRODED (BS 237) · airframe 76,771 hrs · 58,802 cycles

CORROSION ON THE CUSP WEB AT BS 237 BETWEEN LBL 54 TO 60. THE CUSP WEB WAS REPAIRED.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 74,413 hrs · 57,021 cycles

DELAMINATED AND DAMAGE FERRULES ON FLOOR PANEL NR 160A. FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.

Part: SEAT TRACK — CORRODED (BS 670-704) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON PREVIOUS REPAIR PLUGS ON THE SEAT TRACK BS 670 - 704 X 22. THE REPAIR PLUGS WERE REPLACED IAW SRM 51-3-1, SRM 53-05, FIG 4A, SRM 51-10-3, PAR 14, 21, 38.

Part: SEAT TRACK — CORRODED (BS 450-455) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON SEAT TRACK LT X 22, BS 450 - 455. REPAIR PLUG PAX CABIN. PLUG REPAIR WAS REPLACED IAW SRM 53-05, FIG 4A, SH 18.

Part: CUSP WEB — CRACKED (BS 223) · airframe 74,413 hrs · 57,021 cycles

CRACK ON CUSP WEB BS 223 BETWEEN X 54 - 60. DAMAGE WAS REMOVED IAW SRM 53-05, FIG 131A-6. REPAIR FABRICATED IAW SRM 53-05, FIG 131A-6. AREA AND REPAIR TREATED, PAINTED IAW SRM 51-10-3, PAR 14 AND 21. REPAIR INSTALLED IAW SRM 53-05, FIG 131A-6.

Part: CUSP WEB — CORRODED (BS 807) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION OUT OF LIMIT ON LT CUSP WEB, BS 807. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, PAR 144, FIG 131A-1.

Part: DOUBLER — CORRODED (BS 736 CUSP WEB) · airframe 76,771 hrs · 58,802 cycles

CORROSION ON PREVIUSLY REPAIR DOUBLER ON CUSP WEB AT BS 736 BETWEEN RBL 54 - 60. THE REPAIR DOUBLER WAS REPLACED.

Part: PAN — CRACKED (BS 1098) · airframe 74,413 hrs · 57,021 cycles

CRACK ON AFT UPPER CORNER RING PAN BS 1098. UPPER CORNER RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122, AND ER/A 487747-14MA, REV A AND 493648-14MA, REV A.

Part: CUSP WEB — CRACKED (BS 218-237) · airframe 74,413 hrs · 57,021 cycles

THREE INCH CRACK ON CUSP WEB BS 218-237, RT SIDE UNDER SEAT TRACK CABIN. W1, CUSP WEB BS Y=218-237 WAS REPLACED IAW SRM 51-30-2 AND DWG 9930538, REV CF.

Part: CUSP WEB — CRACKED (BS 943) · airframe 74,413 hrs · 57,021 cycles

CRACK ON LT CUSP WEB BS 943. REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: FLOORBEAM — DAMAGED (BS 636) · airframe 74,413 hrs · 57,021 cycles

ELONGATED HOLES ON FLOORBEAM BS 636 BETWEEN LONGERONS 28R - 28L. REPLACED IAW SRM 53-24-0 AND 51-10-4.

Part: FLOOR PANEL — CORRODED (PAX CABIN) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON FLOOR PANEL 16DG. FLOOR PANEL WAS FABRICATED, TREATED, PAINTED, DRILLED AND ADJUSTED IAW SRM 51-10-3, PAR 14, 21, 26 DWG 9957828, REV AB.

Part: DOOR FRAME — CORRODED (BS 1155-1212) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON LOWER DOOR FRAME BETWEEN BS 1155 - 1212. REPAIR DOUBLER, SPACER WAS REPLACED IAW SRM 53-05, FIG 123, 51-30-2 AND 51-30-5.

Part: FLOOR PANEL — CRACKED (BS 168) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CRACK ON FLOOR PANEL IS BS 168, X -25. DAMAGE AREA WAS REMOVED, REPAIR PARTS WERE FABRICATED AND TREATED, PAINTED AND INSTALLED IAW SRM 51-70-4, FIG 2 AND 51-10-3, PAGE 14 / 21.

Part: CUSP WEB — CORRODED (BS 734) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON LT CUSP WEB BS 734 X 54 - 60. REPAIRED IAW SRM 53-05, FIG 131A-13, 51-10-3 PAR 14, 21, 26, 38, AND 51-30-2 E.

Part: CUSP WEB — CORRODED (BS 714) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON LT CUSP WEB BS 714, X 60. REPAIRED IAW SRM 51-10-3, PAR 14, 21, 26, 38, 51-30-2 AND 53-05 FIG 131A-13 E.

Part: CUSP WEB — CORRODED (RT WING) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON COUNTERSINK OF FUEL TANK ACCESS PANEL 1460C ON THE RT WING. ACCESS PANEL WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 667) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON LT CUSP WEB BS 667, X 60. REPAIRED IAW SRM 53-05, PAR 144, FIG 131A-13.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

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

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF ACCESS PANEL 1371C ON RT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00.

Part: LONGERON — CRACKED (BS 256) · airframe 74,413 hrs · 57,021 cycles

CRACKED LONGERON 17L BS 256. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: VANE — WORN (RT WING TE FLAP) · airframe 74,413 hrs · 57,021 cycles

WEAR ON T/E XV2=297, INBD EDGE, ON OTBD VANE OF OTBD FLAP AT RT WING. REPAIRED IAW ER/A 492663-14MA REV, ORIGINAL.

Part: VANE — WORN (RT WING TE FLAP) · airframe 74,413 hrs · 57,021 cycles

WEAR ON T/E IN XV1=211, OTBD EDGE, ON INBD VANE OF OTBD FLAP AT RT WING. RW, SH-CP-SM, CARD 120, ZONE 10. T/E IN BS XV1=211 WAS REPAIRED IAW ER/A 492663-14MA, REV ORIGINAL.

Part: PAN — CRACKED (BS 846) · airframe 74,413 hrs · 57,021 cycles

CRACK ON LT FWD LOWER CORNER RING PAN, BS 846. THE FWD LOWER CORNER RING PAN WAS REPAIRED IAW SRM 53-05, IG 122 AND ERA'S NR 487747-14MA, REV A AND NR 493648-14MA, REV A.

Part: CUSP WEB — CORRODED (BS 605-609) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON LT CUSP WEB BS 605 - 609. WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: CUSP WEB — CORRODED (BS 935-946) · corrosion level 2 · airframe 74,413 hrs · 57,021 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 935 TO 946 X -54 TO X -60 IN PAX CABIN. REPAIR INSTALLED IAW SRM 53-05, FIG 131A-10.

Part: FRAME — CRACKED (BS 1418) · airframe 74,413 hrs · 57,021 cycles

CRACKED FRAME ANGLE BS 1418 BETWEEN LONGERONS 1 TO 2R IN AFT ACCESSORY COMPARTMENT. THE FRAME ANGLE WAS REPAIRED IAW SRM 53-03, FIG 3 AND 35.

Part: PAN — CRACKED (BS 1231) · airframe 74,413 hrs · 57,021 cycles

CRACK ON UPPER AFT CORNER RING PAN BS 1231. THE RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122 AND ERA'S NR 487747-14MA, REV A AND NR 493648-14MA, REV A.

Part: SKIN — WORN (FUSELAGE) · airframe 74,413 hrs · 57,021 cycles

WEAR ON CUTOUT OF PNEUMATIC AIR GROUND CONNECTION FUSELAGE SKIN. DAMAGE DOUBLER WAS REMOVED, NEW DOUBLER WAS FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2.

Part: SKIN — WORN (CARGO DOOR) · airframe 74,413 hrs · 57,021 cycles

WEAR ON DOUBLER REPAIR OF EXTERNAL CARGO DOOR SKIN BS 376 FWD LOWER FRAME. DOUBLER WAS REPLACED IAW ERA 486624-14MA, REV ORIGINAL.

Part: LONGERON — CRACKED (BS 427) · airframe 74,413 hrs · 57,021 cycles

CRACK ON LONGERON 10R, BS 427. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: CUSP WEB — CRACKED (BS 907) · airframe 74,413 hrs · 57,021 cycles

CRACK ON RT CUSP WEB BS 907 BETWEEN X 53 - 56 IN PAX CABIN. DAMAGE WAS REMOVED IAW SRM 53-05, FIG 131A-10. A REPAIR WAS FABRICATED IAW SRM 53-05, FIG 131A-10. REPAIR AND AREA TREATED & PAINTED IAW SRM 51-10-3, PAR 14 AND 21. REPAIR WAS INSTALLED IAW SRM 53-05, FIG 131A-10.

Part: LANYARD — BROKEN (GIRT BAR) · airframe 74,150 hrs · 56,815 cycles

FLIGHT CREW FOUND GIRT BAR LANYARD AT L1 DOOR BROKEN. MAINTENACE INSTALLED A NEW LANYARD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,996 hrs · 56,701 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 31-36 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: LIGHT — INOPERATIVE (TAIL BAY) · airframe 72,430 hrs · 55,680 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT IN THE OVERHEAD PANEL IN THE TAIL COMPARTMENT WAS INOPERATIVE.

Part: SPAR — CRACKED (RT WING) · airframe 71,626 hrs · 55,122 cycles

RT WING REAR SPAR CRACKED, XRS 164, EMITTING APPROX 0.375 FROM INBD FLAP HINGE. CONFIRMED WITH EDDY CURRENT. INSTALLED REPAIR ON STA 164 RT LOWER SPAR CAP IAW AMDS 5710-01110-06, JO 060271-510, AND ER/A 529017-14AD.

Part: SHEAR TIE — CRACKED (BS 1380) · airframe 71,602 hrs · 55,111 cycles

SHEAR TIE CRACKED AT VERTICAL BULKHEAD, BS 1380 BETWEEN LONGERONS 13 -14R. SHEAR TIE REPAIRED IAW ERA 528972-14, REV ORIGINAL.

Part: TAIL CONE — LOOSE · airframe 71,602 hrs · 55,111 cycles

MAINTENANCE DISCOVERED THAT THE RT UPPER AND LOWER RELEASE SPADE RECEPTACLES FOR THE TAILCONE HAVE LOOSE AND MISSING HARDWARE. THE RECEPTACLE HARDWARE WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 71,505 hrs · 55,033 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT SEAT 23CD WAS INOPERATIVE. MAINTENANCE FOUND WIRES BROKEN AT THE LIGHT RECEPTACLE AND PLUG. REPLACED THE LIGHT ASSEMBLY AND THE SYSTEM RETURNED TO NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 70,998 hrs · 54,671 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 24DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,934 hrs · 54,624 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING FOR THE CATWALK AND IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: JACKSCREW — NOT REPORTED (HORIZONTAL STAB) · airframe 69,947 hrs · 53,906 cycles

HORIZONTAL STABILIZER JACKSCREW REPAIRED IAW AA 2740-01113.

Part: WARNING SYSTEM — MALFUNCTIONED (MLG DOOR) · airframe 69,938 hrs · 53,898 cycles

DID NOT GET A LEFT GEAR DOWN AND LOCKED INDICATION DURING APPROACH. CREW PERFORMED A GO AROUND AND DETERMINED INDICATOR BULBS BURNED OUT. AFTER REPLACING LAMPS IN THE INDICATOR, WHEN THE GEAR HANDLE WAS LOWERED ON NEXT APPROACH, THREE GREEN DOWN AND LOCKED INDICATIONS APPEARED BUT GEAR DOOR LIGHT WOULD NOT EXTINGUISH. PERFORMED ALTERNATE EMERGENCY GEAR EXTEND IAW QRH AND LANDED WITH MAIN GEAR DOORS OPEN. R & R LT GEAR DOOR OPEN PROXIMITY SENSOR IAW AMM 32-60. REPLACED PSEU IAW AMM 32-60-04. REPLACED LT MLG DOOR ACTUATOR IAW AMM 32-32. REPLACED RT GEAR DOOR IAW AMM 32-12-01. GEAR SWING CHECKS WERE GOOD AND THE ACFT WAS RETURNED TO SERVICE.

Part: DOOR — NOT REPORTED · airframe 69,566 hrs · 53,638 cycles

CARGO DOORS REPAIRED IAW AA 5230-01159.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,321 hrs · 53,451 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY ESCAPE LIGHTS ABOVE THE FWD OVERWING EXITS ON BOTH SIDE OF THE ACFT WERE INOPERATIVE. MX REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: SKIN — DAMAGED (BS 120) · airframe 68,090 hrs · 52,563 cycles

SKIN, BS 120 BELOW L-18L CREASED, AND DENTED. REPAIRED IAW ERA 508148-14.

Part: SKIN — CORRODED (VERTICAL STAB) · airframe 68,090 hrs · 52,563 cycles

VERTICAL STAB DORSAL FIN FASTENER HOLE HA CORROSION 25.5" FROM L/E 7.5" DOWN FROM STA ZFS 52.267. ON INVESTIGATION FOUND FASTENER HOLE 25.5" FROM L/E 7.5" DOWN FROM STA. ZFS 52.267 TO HAVE DRILL START IN COUNTERSINK AND NOT TO BE CORROSION. REPAIRED DAMAGED FASTENER HOLE IAW DELTA ER/A 512980-14AD REV ORIGINAL. ASSOCIATED ER/A 14-512980 ADDED FOR AC 0907. CORRECTION TO LOG PAGE 0819714 : AND ER/A 512980-14 PRI. REV. 1.

Part: FRAME — CORRODED (BS 1309) · airframe 68,090 hrs · 52,563 cycles

CORROSION AFT CARGO BAY BS 1309 BETWEEN LONGERON 28L TO 28R (53-139-05-1). NO ALLOWABLE LIMITS OF CORROSION -9 REPAIR ANGLE AT FS 1309 FRAME BETWEEN LONGERON 28L-28R. REPLACED PART-9 ANGLE IAW SRM 53-03, FIG 2A. FP 578644U 06APR13, ATS LEAD 33 06APR13.

Part: SKIN — DAMAGED (BS 503-598) · airframe 67,933 hrs · 52,449 cycles

WINDOW BELT DAMAGE RT SIDE FS 503-598 WINDOWS 17-20 LIGHTNING DAMAGE. REPAIRS ACCOMPLISHED IAW ER/A 512003-14, REV 0. REQUIRED INSPECTION COMPLETED.

Part: SKIN — DAMAGED (BS 1003-1098) · airframe 67,933 hrs · 52,449 cycles

WINDOW BELT DAMAGE RT SIDE FS 1003-1098 WINDOW 44-46. LIGHTNING STRIKE. INSPECTION AND REPAIRS ACCOMPLISHED IAW ER/A 512094-14. REQUIRED INSPECTION COMPLETED.

Part: SKIN — DAMAGED (BS 1098-1193) · airframe 67,933 hrs · 52,449 cycles

WINDOW BELT DAMAGE RT SIDE FS 1098-1193 WINDOWS 47-51 DUE TO LIGHTNING STRIKE. INSPECTION AND REPAIRS ACCOMPLISHED IAW ERA 512095-14. REQUIRED INSP COMPLETED.

Part: SKIN — DAMAGED (BS 598-674) · airframe 67,933 hrs · 52,449 cycles

WINDOW BELT DAMAGE RT SIDE FS 598-674 WINDOWS 21-24 DUE TO LIGHTNING STRIKE. INSPECTION AND REPAIRS COMPLETED IAW 512073-14 REV 0. REQUIRED INSPECTION COMLETED.

Part: SKIN — DAMAGED (BS 613) · airframe 67,925 hrs · 52,443 cycles

LIGHTNING STRIKE RT SIDE FS 613 WINDOW BELT AT WINDOW 21 AFT SIDE. REPAIRED IAW ERA 512073-14 REV ORIG SECTION II PERMANENT REPAIR. ASSOCIATED ER/A 88-512073 ADDED FOR AC 0907.

Part: SKIN — DAMAGED (BS 1212 S10R) · airframe 67,920 hrs · 52,440 cycles

BS 1212, STR 10R TWO RIVET HEADS HAS LIGHTNING STRIKE PITTED METAL. COMPLIED WITH CONDUCTIVITY CHECK OF SKIN IN AREA AROUND STRIKES IAW SRM 53-04-01 FOUND TO BE WITHIN LIMITS. REMOVED DAMAGED RIVETS. ACCOMPLISHED HFEC OF CUTOUT AND BHEC EXISTING FASTENER HOLES IAW SRM 51-30. NO DAMAMGE FOUND. TREAT AND PAINTED REPAIR PARTS IAW SRM 53-04-3 FIG 8, SHEET 1-10. VISUAL INSPECTION OF REPAIR IS GOOD IAW 53-04-3.

Part: WINDOW FRAME — DAMAGED (BS 1132) · airframe 67,925 hrs · 52,443 cycles

BS 1132, STR 13R ONE LIGHTING STRIKE ON WINDOW FRAME WINDOW 48. REPAIRED IAW ERA 512095-14 REV ORIG SECTION I TIME LIMITED REPAIR.

Part: SKIN — DAMAGED (BS 1075) · airframe 67,925 hrs · 52,443 cycles

LIGHTNING STRIKE RT FS 1075 AFT OF WINDOW NR 46 ONE FASTENER. REPAIRED IAW ERA 512094-14, REV ORIG SECTION I TIME LIMITED REPAIR.

Part: SKIN — DAMAGED (BS 1065) · airframe 67,925 hrs · 52,443 cycles

LIGHTNING STRIKE BS 1065 WINDOW BELT AT WINDOW NR 45. REPAIRED IAW ERA 512094-14, REV ORIG SECTION I TIME LIMITED REPAIR.

Part: WINDOW FRAME — DAMAGED (BS 1156) · airframe 67,925 hrs · 52,443 cycles

BS 1156, S13R LIGHTNING STRIKE ON WINDOW FRAME. WINDOW 49. REPAIRED IAW ERA 512095-14 REV ORIG SECTION I TIME LIMITED REPAIR.

Part: WINDOW FRAME — DAMAGED (BS 1102) · airframe 67,925 hrs · 52,443 cycles

STA 1102, STR 12R (1) LIGHTNING STRIKE ON WINDOW FRAME WINDOW NR 47. REPAIRED IAW ERA 512095-14, REV ORIG SECTION I TIME LIMITED REPAIR.

Part: SKIN — DAMAGED (BS 653) · airframe 67,925 hrs · 52,443 cycles

LIGHTNING STRIKE RT SIDE FS 653 WINDOW BELT AT WINDOW NR 23 UPPER FWD CORNER. REPAIRED IAW ERA 512073-14, REV ORIG SECTION I TIME LIMITED REPAIR.

Part: SKIN — DAMAGED (BS 604) · airframe 67,925 hrs · 52,443 cycles

LIGHTNING STRIKE RT SIDE FS 604 WINDOW BELT AT WINDOW 21 FWD SIDE. REPAIRED IAW ERA 512073-14, REV ORIG SECTION II- PERMANENT REPAIR.

Part: WINDOW FRAME — DAMAGED (BS 1155) · airframe 67,925 hrs · 52,443 cycles

BS 1155, S12R ONE LIGHTNING STRIKE ON WINDOW FRAME. WINDOW NR 50. REPAIRED IAW ERA 512095-14, REV ORIG SECTION I TIME LIMITED REPAIR.

Part: SKIN — DAMAGED (BS 667) · airframe 67,925 hrs · 52,443 cycles

LIGTHNING STRIKE RT FS 667 WINDOW BELT AT WINDOW 24 UPPER ARCH OF FRAME. REPAIRED IAW ERA 512073-14, REV ORIG SECTION I, TIME LIMITED REPAIR.

Part: WINDOW FRAME — DAMAGED (BS 1174) · airframe 67,925 hrs · 52,443 cycles

BS 1174, S12R ONE LIGHTNING STRIKE ON WINDOW FRAME. (WINDOW HAS HEAT DAMAGE) WINDOW 50. REPAIRED IAW ERA 512095-14, REV ORIG SECTION I TIME LIMITED REPAIR.

Part: SKIN — DAMAGED (BS 522-596) · airframe 67,925 hrs · 52,443 cycles

ON ARRIVAL, ACFT SUSTAINED MULTIPLE LIGHTNING STRIKES COMMON TO THE WINDOW BELT PANELS AND FRAMES ON THE RT SIDE OF FUSELAGE. LOCATED BETWEEN FS 522-596, WINDOWS 17-20. A TIME LIMITED REPAIR WAS ACCOMPLISHED IAW ERA 512003-14.

Part: WINDOW FRAME — DAMAGED (BS 1121) · airframe 67,925 hrs · 52,443 cycles

STA 1121, STR 13R ONE LIGHTNING STRIKE ON WINDOW FRAME WINDOW NR 48. REPAIRED IAW ERA 512095-14 REV ORIG SECTION I TIME LIMITED REPAIR.

Part: SKIN — DAMAGED (BS 1058) · airframe 67,925 hrs · 52,443 cycles

LIGHTNING STRIKE RT FS 1058 WINDOW BELT AT WINDOW 44 AFT UPPER CORNER. REPAIRED IAW ERA 512094-14 REV ORIG SECTION I TIME LIMITED REPAIR.

Part: SKIN — DAMAGED (BS 632) · airframe 67,925 hrs · 52,443 cycles

LIGHTNING STRIKE RT SIDE, FS 632 WINDOW BELT WINDOW 22. REPAIRED IAW ERA 512073-14, REV. ORIG SECTION I TIME LIMITED REPAIR.

Part: WINDOW FRAME — DAMAGED (BS 1113) · airframe 67,925 hrs · 52,443 cycles

BS 1113, STR 12R ONE LIGHTNING STRIKE ON WINDOW NR 47. REPAIRED IAW ERA 512095-14, REV ORIG SECTION I TIME LIMITED REPAIR.

Part: SKIN — DAMAGED (BS 661) · airframe 67,925 hrs · 52,443 cycles

LIGHTNING STRIKE RT FS 661 WINDOW BELT AT WINDOW NR 24 UPPER FWD CORNER. REPAIRED IAW ERA 512073-14, REV ORIG SECTION I TIME LIMITED REPAIR.

Part: WINDOW FRAME — DAMAGED (BS 1174) · airframe 67,925 hrs · 52,443 cycles

BS 1174, S12R ON WINDOW FRAME ONE LIGHTNING STRIKE (WINDOW HAS HEAT DAMAGE) WINDOW NR 51. REPAIRED IAW ERA 512095-14, REV ORIG SECTION I TIME LIMITED REPAIR.

Part: SKIN — DAMAGED (BS 649) · airframe 67,925 hrs · 52,443 cycles

LIGHTNING STRIKE, RT FS 649 WINDOW BELT AT WINDOW NR 23 AFT UPPER CORNER. REPAIRED IAW ERA 512073-14, REV ORIG SECTION I TIME LIMITED REPAIR.

Part: SKIN — DAMAGED (BS 1094) · airframe 67,925 hrs · 52,443 cycles

LIGHTNING STRIKE RT BS 1094, WINDOW BELT AT WINDOW NR 46. REPAIRED IAW ERA 512094-14 REV ORIG SECTION I TIME LIMITED REPAIR.

Part: WINDOW FRAME — DAMAGED (BS 1140) · airframe 67,925 hrs · 52,443 cycles

BS 1140, STR 13R, ONE LIGHTNING STRIKE ON WINDOW FRAME. WINDOW 49. REPAIRED IAW ERA 512095-14, REV ORIG SECTION I TIME LIMITED REPAIR.

Part: SKIN — DAMAGED (BS 1049) · airframe 67,925 hrs · 52,443 cycles

LIGHTNING STRIKE RT FS 1049 WINDOW BELT AT WINDOW 44. REPAIRED IAW ERA 512094-14 REV ORIG SECTION I TIME LIMITED REPAIR.

Part: VALVE — NOT REPORTED (STARTER) · airframe 66,609 hrs · 51,475 cycles

STARTER AIR SHUTOFF VALVE REPAIRED IAW AA 8012-01009.

Part: SEAT TRACK — CORRODED (BS 1171) · airframe 65,827 hrs · 50,941 cycles

CORROSION IN SEAT TRACK WELL BS 1171 LBL 44 AROUND LOCK FASTENERS. PRIOR TO CORROSION REMOVAL FOUND EVIDENCE OF PREVIOUS BLEND WITH NO BLUE MARKINGS. REMOVED 2 LOCK FASTENERS, REMOVED CORROSION L-2.5"X W-1"XD-.068. ORIGINAL THICKNESS OF TRACK WELL IS 1". FOUND TO BE OUT OF LIMITS PER SRM 53-05. REMOVED SEAT TRACK SECTION LBL 44 FROM BS 1164-1203. INSTALLED NEW SEAT TRACK & NEW SPLICE P/N ACA7413-505 PER SRM 53-05 FIG 4F. SRM 51-10-3 PGS 28-32.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,745 hrs · 50,893 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 31-38 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED A SHORTED LIGHT ASSEMBLY, ALL ASSOCIATED BULBS, AND INSTALLED THE FUSE IN THE POWER SUPPLY. A SATISFACTORY FUNCTIONAL CHECK WAS PERFORMED.

Part: WIRE — DAMAGED (CABIN) · airframe 65,700 hrs · 50,863 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 02C IN THE CABIN TO BE DAMAGED AND INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT A SPLICE UNDER THE SEAT AND RE-TERMINATED IT. THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,583 hrs · 50,787 cycles

DURING SERVICE CHECK MAINTENANCE FOUND EMERGENCY LIGHTS FROM ROW 31 AFT INOPERATIVE. REPLACED POWER SUPPLY PER AMM AND OPERATION CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 65,578 hrs · 50,785 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT THE AFT SEAT SECTION OF THE CABIN AND THE AFT ACCESSORY COMPARTMENT HAD ALL FAILED. MAINTENANCE REPLACED THE POWER SUPPLY AT SEAT ROW 35 AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: RIB — NOT REPORTED (HORIZONTAL STAB) · airframe 65,202 hrs · 50,529 cycles

HORIZONTAL STABILIZER HINGE RIB PIVOT BEARING LUG REPAIRED IAW AA 5500-01011.

Part: SKIN — NOT REPORTED (HORIZONTAL STAB) · airframe 65,202 hrs · 50,529 cycles

HORIZONTAL STABILIZER UPPER CENTER SKIN PANEL REPAIRED IAW AA 5510-01086.

Part: SPAR — CRACKED (WING) · airframe 64,822 hrs · 50,275 cycles

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

Part: WIRE — BROKEN (CABIN) · airframe 64,440 hrs · 49,997 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT INOPERATIVE AT SEAT 26D. MAINTENANCE REPLACED BROKEN WIRE. OPERATION OF LIGHT NOW CHECKS GOOD.

Part: PANEL — CORRODED (LAV SERVICE) · airframe 64,217 hrs · 49,861 cycles

AFT LAVATORY SERVICE PANEL BS 1307 - 1322 CORRODED, REPAIRED IAW ERA 477599-14.

Part: WIRE — BROKEN (CABIN) · airframe 63,990 hrs · 49,708 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 19DE INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY DUE TO BROKEN WIRES. OPERATION OF LIGHT NOW CHECKS OK.

Part: HEATER — NOT REPORTED (STATIC PORT) · airframe 63,707 hrs · 49,519 cycles

STATIC PORT HEATER REPAIRED IAW EA 09-465286-03.

Part: HEATER — NOT REPORTED (STATIC PORT) · airframe 63,707 hrs · 49,519 cycles

STATIC PORT HEATER REPAIRED IAW AA 3030-01027.

Part: SPAR — NOT REPORTED (VERTICAL STAB) · airframe 62,639 hrs · 48,824 cycles

VERTICAL STABILIZER FRONT SPAR RT CHORD ZFS=52 REPAIRED IAW ERA 484065-14.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,332 hrs · 48,617 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY PATH LIGHT AT SEAT 35D INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY PER AMM 33-53-01. OPERATION OF LIGHT NOW CHECKS GOOD. (2010-D1384) (DLM88103219)

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 62,179 hrs · 48,525 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY PATH LIGHTS ROW 31 AND AFT INOPERATIVE. MAINTENANCE REPLACED FUSE IN POWER SUPPLY B5-212. OPERATION OF LIGHTS NOW CHECKS OK. (2010-D1315) (DLM88103017)

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 59,781 hrs · 46,920 cycles

DURING HMV GENERAL SURFACE CORROSION WAS FOUND ON LT GEAR SUPPORT FITTING BUSHING BORE. SUPPORT FITTING BORE WAS REPAIR IAW EA 09-093855-03AD REV B.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,920 cycles

DURING HMV A CRACK WAS FOUND ON FUSELAGE SKIN STA Y=1437 LONGERON 3-4 LT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 27.

Part: SUPPORT FITTING — CORRUPTED (RT MLG) · airframe 59,781 hrs · 46,920 cycles

DURING HMV GENERAL SURFACE CORROSION WAS FOUND ON RT GEAR SUPPORT FITTING BEARING BORE. SUPPORT FITTING BEARING BORE WAS REPAIRED IAW EA 09-093855-03AD REV B.

Part: TAB — DELAMINATED (RUDDER) · airframe 59,781 hrs · 46,920 cycles

DURING HMV DAMAGE METALIZED COATING WAS FOUND ON RUDDER CONTROL TAB. RUDDER CONTROL TAB WAS REPAIRED IAW SRM 51-70-1AD PAR 23.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 59,781 hrs · 46,920 cycles

DURING HMV GENERAL SURFACE CORROSION WAS FOUND ON RT GEAR SUPPORT FITTING BUSHING BORE. SUPPORT FITTING BORE WAS REPAIRED IAW EA 09-093855-03AD REV B.

Part: STRUCTURE — DELAMINATED (RUDDER) · airframe 59,781 hrs · 46,920 cycles

DURING HMV DAMAGE METALIZED COATING WAS FOUND ON THE RUDDER. METALIZED COATING ON RUDDER WAS REPAIRED IAW SRM 51-70-1AD PAR 23A.

Part: BEAM — CRACKED (R1 DOOR) · airframe 59,781 hrs · 46,920 cycles

DURING HMV A CRACK WAS FOUND IN THE R1 DOOR BEAM 1 AFT EDGE. CRACK WAS REPAIRED IAW SRM 52-05D FIG 25.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,920 cycles

DURING HMV A CRACK WAS FOUND ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STATION Y=864 LT REF EA 09-460094-12AD. FRAME WAS REPLACE IAW EA 09-460094-12AD

Part: BEAM — CRACKED (R1 DOOR) · airframe 59,781 hrs · 46,920 cycles

DURING HMV A CRACK WAS FOUND ON THE R1 DOOR BEAM 4 FWD EDGE BEAM WAS REPAIRED IAW SRM 52-05D FIG 25

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 59,781 hrs · 46,920 cycles

DURING HMV INADEQUATE FASTENERS INSTALLED ON PREVIOUS FUSELAGE SKIN REPAIR AT STA Y=240 LONGERON 29L-29R AS REQUIRED PER ERA 455952-14 REV B DATED 08-JUN-2006. FASTENERS WAS REPLACED IAW ERA 455952-14 REV B.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,920 cycles

DURING HMV A CRACK WAS FOUND IN THE FUSELAGE SKIN STA Y=1437.5 BTW LONGERON 3 RT AND 4 RT. FUSELAGE SKIN WAS REPAIRED IAW ERA 477598-14 REV ORG.

Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 59,781 hrs · 46,920 cycles

DURING HMV EXFOLIATION CORROSION WAS FOUND ON LWR MID CARGO COMPARTMENT DOORJAMB STA Y=652. LOWER DOORJAMB WAS REPAIRED IAW SRM 53-05 FIG 123.

Part: BUSS CABLE — BROKEN (AILERONS) · airframe 54,084 hrs · 43,326 cycles

MOVING RT AILERON HAD NO EFFECT ON LT AILERON. FOUND AILERON BUSS CABLE BROKEN IN RT W/W. FOUND AILERON BOSS CABLE 36B BROKEN. REPLACED SAME ADJ/TEST AMM 460188. RII DEPT 625 B/O INSTALLATION AND ADJUSTMENT OF CABLE PER M/M 1506.

Part: SPAR CAP — DAMAGED (HORIZ STAB) · airframe 53,798 hrs · 43,150 cycles

HORIZONTAL STABILIZER REAR SPAR UPPER CAP (LT AND RT) REPAIR IAW 09-460214-12 ME02. C/W 09-460214-12 ME02.

Part: STOP FITTING — DAMAGED (CARGO DOOR) · airframe 53,721 hrs · 43,094 cycles

FWD /MID /AFT CARGO DOOR STOP REPLACEMENT IAW EO 09-451701-12 ME01, ME02, ME03. C/W 09-451701-12 ME01, ME02, ME03.

Part: SENSOR — FAILED (RT MLG DOOR) · airframe 52,890 hrs · 42,559 cycles

AFTER T/O, GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RAISED GEAR INDICATED UP AND LOCKED COMPLIED W/QRH LOWERED GEAR AND LIGHT REMAINED ILLUM GEAR INDICATED DOWN AND LOCKED C/W QRH PROCEDURES. FOUND SENSOR D1-29 BAD AND LATCH LINK LOOSE.

Part: SEAL — DAMAGED (APU OIL CAP) · airframe 51,368 hrs · 41,488 cycles

SMOKE IN AFT CABIN WITH SMOKE ALARMS AND SMELL IMMEDIATELY AFTER TAKEOFF. FOUND APU CONT WITH OIL FROM DAMAGED OIL CAP SEAL. REPLACED OIL CAP SEAL, C/W DUCT BURNOUT PER OPN 5089. C/W OVERWEIGHT LANDING INSP. NO DEFECTS NOTED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 51,221 hrs · 41,376 cycles

THE FUSELAGE SKIN WAS CORRODED UNDER THE LOWER TCAS ANTENNA DOUBLER. THE DAMAGE IS IN TWO PLACES, APPROXIMATELY 1.7 X 1.3 IN. AND 2.75 X 1.5 IN. AT FS 240, BETWEEN L-29R & L-30. THE CORRODED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 48,495 hrs · 39,429 cycles

CENTER WINDSHIELD BEGAN BUBBLING AT CRUISE 20 MINUTES INTO THE FLIGHT. AREA TURNED BLACK AND STARTED TO CRACK. AIR TURNBACK TO CVG. REPLACED WINDSHIELD.

Part: CSD — FAILED (NR 1 ENGINE) · airframe 48,114 hrs · 39,165 cycles

LT CSD TEMP STABILIZED IN EXCESS OF THE RED BAND. REPLACED CSD, GEN AND OIL COOLER.

Part: IRU — OUT OF ADJUST (E/E BAY) · airframe 44,973 hrs · 36,910 cycles

FLIGHT DIVERSION, MAP FAIL CAPT AND F/O`S FLIGHT DIRECTOR FAIL COURSE INFO NOT RELIABLE. FMA PANELS INTERMITTENT, STALL INDICATION FAIL AUTO SLAT FAIL. REALIGNED IRUS. PERFORMED RTS, CHECKS GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,970 hrs · 36,908 cycles

A CRACK WAS FOUND IN THE UPPER, FWD CORNER OF THE C-1 DOOR JAMB IN BOTH THE SKIN AND ALUM DOUBLER. A TYPICAL SRM REPAIR ALSO EXISTS IN THE NEARBY AREA. NEW DAMAGE AND OLD DAMAGE INCORPORATED INTO ONE REPAIR PER ERA 386012-14.

Part: HINGE FITTING — DAMAGED (T/E FLAP) · airframe 44,970 hrs · 36,908 cycles

OUTBOARD FLAP INBOARD HINGE FITTING DAMAGED AT PIVOT POINT AND PIVOT BOLT IS MISSING NUT AND COTTER PIN. REPLACED SAME.

Part: COFFEEMAKER — ODOR (FWD GALLEY) · airframe 43,889 hrs · 36,148 cycles

PRIOR TO LANDING ATTENDANTS REPORTED BURNING RUBBER ODOR IN FWD GALLEY/FC AREA. ATTENDANTS TURNED EVERYTHING OFF AND GALLEY POWER WAS REMOVED. JUST BEFORE LANDING SMOKE STARTED COMING FROM 1ST CLASS COFFEEMAKER, HALON FIRE EXTINGUISHER DISCHARGED. REPLACED COFFEEMAKER AND TRAY INSP AREA FOR ODOR OR BURNED/DAMAGED WIRING, NONE FOUND. CYL COFFEE POT, CHECK GOOD. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 43,485 hrs · 35,871 cycles

AFT EMERGENCY EXIT LIGHTS INOPERATIVE - FOUND RACK BAD - P/N 60-1177-9 S/N 223 - REPLACED SAME

Part: COALESCER BAG — DIRTY (AIR CONTDITIONER) · airframe 42,110 hrs · 34,881 cycles

AIR CONDITIONER PRODUCED A FUEL LIKE ODOR. COMPLIED WITH OP 5088, NO DEFECTS NOTED. CHANGED COALESCER BAGS AS PRECAUTION AWAITING DUCT BURN OUT, OP 5089. 449991. COMPLIED WITH OPN 5089- PNEUMATIC DUCT BURNOUT. ALL CHECKS OK.

Part: PUMP — DEFECTIVE (NR 2 ENGINE) · airframe 39,661 hrs · 33,002 cycles

ON T/O FROM PWM DURING CLIMBOUT NR 2 ENG ROLLED BACK TO IDLE MOMENTARILY THEN WENT BACK TO CLIMB POWER THEN SHUTDOWN AT APPROX 10,000 FT. DIVERTED TO BGR. REPLACED FUEL PUMP AND CONTROL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,596 hrs · 32,953 cycles

EMERGENCY LIGHTS AT 3C INOP. REPLACED LIGHT ASSY.

Part: PIN — BROKEN (R/H SLAT 0/1) · airframe 39,360 hrs · 32,770 cycles

IRR - ON L/O FOUND R/H SLAT "0" LOWER ALIGNMENT PIN BUSHING BROKEN. CORR- INSTALLED NEW ALIGNMENT PIN - CYCLED SLATS - ALL CKS NORMAL PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,042 hrs · 32,550 cycles

ON L/O FOUND EMERGENCY LIGHTS INOP SEAT 18ED-29ED-36ED. RELAMPED, OPS CKS GOOD.

Part: HARNESS — DISCONNECTED (CABIN) · airframe 38,476 hrs · 32,139 cycles

SEAT 34C/D WIRE HARNESS LOOSE ON FLOOR. FOUND BY FAA INSPECTOR. DETERMINED SEAT EMERGENCY LIGHTING WIRE HARNESS DISCONNECTED BETWEEN ROW 31C/D AND 34C/D. RECONNECTED AND SECURED WIRING. ALL EMERGENCY LIGHTS NOW CHECK NRML.

Part: COALESCER BAG — CONTAMINATED (AFT) · airframe 37,699 hrs · 31,552 cycles

VERY STONG OILY BURNING SMELL IN CABIN. - FOUND OIL LEAKING FROM APU - PERFORMED DUCT BURNOUT - REPLACED COALESCER SOCKS

Part: OUTFLOW VALVE — FAILED (AFT FUSELAGE) · airframe 37,582 hrs · 31,464 cycles

OUTFLOW VALVE STUCK FULL CLOSED AFTER T/O IN AUTO 1 AND AUTO 2. REPLACED OUTFLOW VALVE ACTUATOR AND PRESSURE CONTROLLER.

Part: BATTERY — OVERHEAT (E/E BAY)

ON TAXI INTO GATE AT CAE, RAMP REPORTED SMOKE FROM THE NOSE WHEEL WELL AREA. THE FIRE DEPT FOUND THE MAIN BATTERIES OVERHEATED AND REMOVED SAME. REPLACED BATTERIES, CHARGER AND RELAY.

Part: COALESCER BAG — CONTAMINATED (CABIN)

ON CLIMB-OUT ATL, WITH ENG ANTI-ICE ON, FLT ATT REPORTED ODOR AND SMOKE IN AFT CABIN. LAV SMOKE DET WENT OFF. ANTI-ICE TURNED OFF AND SMOKE DISSIPATED. DIVERTED TO CHA, CLEANED APU INLET. REPLACED COALESCER BAGS, PERFORMED DUCT BURNOUT.

Part: SKIN — DENTED (BS 237)

DENT FOUND IN FUSELAGE SKIN LHS AT STA 237 AT THE CUSP LINE. REPAIRED PER ERA 332853-14 REV A.

Part: SKIN — DENTED (BS 522)

DENT FOUND IN FUSELAGE SKIN AT STA 522 BETWEEN L20R AND L21R. REPAIRED PER ERA 332859-14.

Part: SKIN — DENTED (BS 218)

DENT FOUND IN SKIN AT STA 218, BETWEEN L18L AND L19L. REPAIRED PER ERA 332869-14 REV A.

Part: SKIN — DENTED (BS 229-244)

DENT IN FUSELAGE SKIN FROM STA 229-244 BETWEEN L-18L AND L-17L. DAMAGE TRIMMED OUT RESULTING IN A 15 FWD/AFT BY 9.5 UP/DOWN HOLE IN SKIN. ACTION TAKEN, ERA 332849-14.

Part: RIB — CRACKED (NR 3 SLAT)

LEFT AND RIGHT NR 3 SLATS CAME TO HMV WITH BROKEN RIBS WHICH ASSIST IN HOLDING AND ADJUSTING THE SLAT POSITION ON THE A/C. REPLACED SAME.

Part: SLIDE — FAILED TEST (TAILCONE)

DURING OPN 6910 OF TAIL SLIDE DEPLOYMENT, TAIL CONE HAD PROBLEMS RELEASING AND THE SLIDE LANYARD SNAP POPPED OFF. THE VELCRO GLUE DID NOT HOLD. HARNESS DID NOT ALLOW ENOUGH PULL ON LANYARD TO DEPLOY SLIDE. SLIDE MANUALLY DEPLOYED AFTER RELEASING FWD STRAP TOGGLE PINS. A/C WAS IN FOR NORMAL HMV.

Part: OVEN — DIRTY (GALLEY)

THERE WAS A BURNING SMELL /RUBBERY SCENT/ IN 4-5 ROW ZONE AREA NEAR FWD LEADING EDGE OF WING. INSP CABIN AREA 4-5 ROW AREA FWD OF LEADING EDGE OF WING. CLEANED DEBRIS FROM OVENS AND CLEANED SAME. PERFORMED HI PWR RUN OF ENGINES, NO DEFECTS NOTED. CHECKED CABIN LIGH BALLASTS IN SUSPECTED AREA.

Part: ANTI-ICE DUCT — BLOWN (NR 2 ENGINE)

ON TAKEOFF AT 8000FL, RT ENG FLAME OUT FOLLOWED POM. PLACED FUEL CONTROL TO OFF AND LANDED. REPLACED LEFT FRAME ANTI-ICE DUCT RAN ENGINE CKS OK.

Part: COWL — DAMAGED (NR 2 ENGINE)

ON POST FLIGHT INSPECTION, THE FLT CREW FOUND A HOLE IN THE LEADING EDGE OF THE NR 2 ENGINE NOSE COWL AT THE 12 O'CLOCK POSITION. CONTRACT MAINTENANCE WAS CALLED OUT, DAMAGE WAS COMPLETELY THROUGH THE EXTERIOR SKIN AND THE INNER LINER WAS EXPOSED. METAL WAS VERY THIN AND BRITTLE, MINOR DAMAGE TO FAN BLADES. REPLACED THE NR 2 ENGINE NOSE COWL ASSY, DRESSED OUT THE FAN BLADES PER M/M. ALSO, FOUND THE NOSE COWL ANTI-ICE THERMOSTATIC VALVE FAILED. REPLACED VALVE, COMPRESSOR WAS BORESCOPED.

Part: BRAKE — OVERHEATED (LT MLG)

TEN MINUTES AFTER TAKEOFF, BRAKE OVERHEAT LIGHT ILLUMINATED. TEMP ON NR 1 BRAKE, LEFT OUTBOARD, INDICATED 500 DEGREES. LOWERING GEAR PER POM REDUCED TEMPERATURE TO 300 DEGREES LESS THAN 300 DEGREES AND OVERHEAT LIGHT WENT OUT. AFTER RAISING GEAR, TEMPERATURE AGAIN ROSE TO ABOVE 300 DEGREES AND LIGHT RE-ILLUMINATED. TEMPERATURE, VERY GRADUALLY, APPROXIMATELY 1 HOUR, REDUCED TO 100 DEGREES . PRECAUTIONARY DIVERTED TO JFK FOR LONG RUNWAY.

Part: LIGHT — INOPERATIVE (OVERWING)

OVERWING EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY.

Part: JAMB — CORRODED (C1 CARGO DOOR)

FOUND ON C2 LTR CHECK, CORROSION C1 CARGO DOOR LWR JAMB LONGERON HAS CORROSION. REPAIRED PER SRM 53-05 FIG 44.

Part: DUCT CLAMP — WORN (RT PACK)

DURING CLIMB THROUGH FL 270, FLOW LIGHT ILLUMINATED AND CABIN BEGAN 1,000 FPM CLIMB, UNABLE TO CONTROL MIX VALVE POSITION AND CABIN PRESSURE. FOUND RT PACK DUCT BLOWN OFF. REINSTALLED DUCT, INSTALLED NEW NUT ON CLAMP AND LEAK CHECKED OK. ALSO, CHECKED ALL DOOR SEALS AND ALL CHECKS NORMAL.

Part: SENSE LINE — LOOSE (TAIL COMP)

CLIMB-OUT OF ATL 18,000 FEET MASTER WARNING AND TAIL COMP HIGH LIGHT CAME ON. TURNED OFF PNEU HANDLES AND CLOSED HP BLEEDS, LIGHT WENT OUT AFTER 1 MIN. FOUND ON LEFT AUG VALVE LOW PRESS SENSE LINE LOOSE, TIGHTENED AND CKD OK PER PFHB.