N906DE

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,226 hrs · 51,771 cycles

FOUND ROWS 1-4 CIELING EMERGENCY LIGHTS INOP. R&R BATTERIES AT BATTERY PACK B5-100. CHECKS OK. A/C OK FOR SVC. REF MD-88 AMM 33-53. (LP5587492)

Part: FAIRING — MISSING (FLAP HINGE) · airframe 70,242 hrs · 51,785 cycles

RH WING INBOARD FLAP HINGE SECONDARY FAIRING MISSING. INSTALLED RT WING FLAP TRACK FAIRING PER ERA 580914-14 REV ORIGINAL. (LP5587434)

Part: B-NUT — LOOSE (THRUST REVERSER) · airframe 69,942 hrs · 51,486 cycles

ON POST FLIGHT FOUND MORE RESIDUAL FLUID ENTERING APU FWD NON RAM DOOR INLET. AFTER ENGS SHUT DOWN AND APU SUPPLY TO PACKS NOTICED BURNING OIL ODOR IN COCKPIT COMPLETED A/C SMOKE FUME QUESTIONNAIRE. INSPECTED FOR LEAKS AROUND TAIL COMP, SPUN ENGINES, RAN THRUST REVERSES, NO LEAKS ON LEFT SIDE, FOUND T UNION AT RT T/R ACCUMULATOR UPPER BNUT LEAKING AND LOOSE SECURED BNUT LEAK CK OK. WITH NO OTHER LEAKS ON RT SIDE --856586--LEAK AT T FITTING AT ACCUMULATOR LOW PRESSURE SWITCH--856586--C/W MD NO GO ODI PREVENTION 21-72 WITH CARDS 2120-2367, APU INLET AND TAIL CLEANED ON LOGS 5774185-5774186 ALSO C/W W/C 2700-4139 A/C OK FOR SERVICE (LP5774182)

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,645 hrs · 51,224 cycles

THE AFT OVERWING UPPER EXIT LIGHTS WENT INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES B5-105 PER AMM 33-53. OPERATION IS NOW NORMAL. (LP #5773704)

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,832 hrs · 50,475 cycles

EMERGENCY LIGHTS INOP IN OVERHEAD FROM SEAT 11-14. R/R BATTERIES FOR OVERHEAD LIGHTS 11-14. PER AMM 33-53. CHECKS NRML. OK FOR SVC. R/R BATTERIES FOR OVERHEAD LIGHTS 11-14. PER MD88 AMM 33-53. CHECKS NRML. OK FOR SVC. (LP5765823)

Part: LIGHT — DISCONNECTED (CABIN) · airframe 68,832 hrs · 50,475 cycles

EMERGENCY LIGHT OUT AT SEAT 33 E&D. FOUND LIGHT UNPLUGGED. CONNECTED SAME. CHECKS GOOD OK FOR SVC. (LP5765822)

Part: DOUBLER — WORN (CARGO DOOR) · airframe 68,101 hrs · 49,862 cycles

WEAR ON EXTERNAL REPAIR DOUBLERS AT FWD/ AFT LOWER CORNER OF FWD CARGO DOOR. EXTERNAL REPAIR DOUBLERS AT FWD/ AFT LOWER EDGE CORNERS WERE REPLACED PER ER/A 486624-14MA REV ORIGINAL.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 67,843 hrs · 49,624 cycles

AISLE SEAT EMERGENCY LIGHTS INOP 23D AND 33D. REPLACED WIRING HARNESS UNDER SAET 23D AND REPLACED LIGHT ASSEMBLY ON 33D REF AMM 33-53.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,823 hrs · 49,609 cycles

LEFT EXTERIOR EMERGENCY LIGHT IS OUT. R&R LT EMERGENCY EXTERIOR LIGHT IAW AMM 33-41, OP CKS GOOD.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 67,188 hrs · 49,067 cycles

AFT LEFT LAVATORY SMOKE DETECTOR SOUNDING UPON ARRIVAL IN ATL. NO SMOKE FOUND. REPLACED AFT LEFT SMOKE DETECTOR PER AMM 26-21.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 66,586 hrs · 48,583 cycles

ON SVC CK FOUND EMERGENCY LIGHT OUT, ROW 26. FOUND PLUG DISCONNECTED UNDER SEAT RECONNECTED. CKS OK.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 66,426 hrs · 48,459 cycles

EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:13D INTERIOR. FOUND CONNECTOR UNPLUGGED, RE-CONNECTED OPS NML.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,343 hrs · 48,393 cycles

EMERGENCY LIGHTS IN FIRST CLASS CEILING INOPERATIVE. REPLACED THE BATTERY PACK B5-100 IAW AMM 33-53. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,626 hrs · 47,829 cycles

RT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-50.

Part: SKIN — CRACKED (TE FLAP VANE) · airframe 63,058 hrs · 45,884 cycles

DAMAGE TO CRACKED UPPER SKIN, FORWARD OTBD STUD AREA, AT LT OTBD FLAP MID GUIDE VANE. LEFT OTBD FLAP MID GUIDE VANE WAS REPAIRED BY ER/A 550294-14, REV ORIGINAL.

Part: HEATER BLANKET — CRACKED (RT WING) · airframe 63,056 hrs · 45,883 cycles

INITIAL, CRACK ON RT WING HEATER BLANKET AFT EDGE. CRACK WAS REPAIRED IAW ER/A 494597-14AD MA, REV A. CRACK WAS REPAIRED IAW ER/A 494597-14AD MA REV A.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,056 hrs · 45,883 cycles

AWR: HIDDEN DAMAGE, CRACK ON INNER PAN BELOW PRESSURE SEAL AT STOP FITTING 1 AFT EDGE. THIS CARD WAS ATTENDED IAW ER/A 550269-14, REV ORIGINAL AND ETI-88-16-325.

Part: HEATER BLANKET — CRACKED (RT WING) · airframe 63,056 hrs · 45,883 cycles

INITIAL, CRACK ON RT WING HEATER BLANKET AFT EDGE. CRACK WAS REPAIRED IAW ER/A 494597-14AD MA, REV A.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,056 hrs · 45,883 cycles

INITIAL, CRACKED PAN BELOW STOP FITTING 1 AND 2 AT FWD CARGO COMPARTMENT DOOR AFT EDGE. THIS CARD WAS ATTENDED IAW ER/A 550269-14, REV ORIGINAL.

Part: STRUCTURE — CRACKED (LT WING) · airframe 63,056 hrs · 45,883 cycles

INITIAL, AD, CRACKED AND SHEARED RIVET ON UPPER BEAVER TAIL STA XW=47 AT LT WING. SHEARED FASTENER WAS REPLACED IAW SRM 51-30-2 AND CRACK .656" WAS REPAIRED IAW ER/A 550300-14, REV: ORIGINAL AND ETI-88-16-341, REV: ORIGINAL.

Part: SKIN — WORN (LT WING) · airframe 63,056 hrs · 45,883 cycles

WORN PRODUCTION DOUBLER AND INTERNAL WING SKIN BETWEEN STA XW=540 TO STA XW=550, AT LT WING VENT BOX. DAMAGE WAS REMOVED IAW ER/A 094477-14, REV A.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

CRACKED AND ELONGATED HOLES AT AFT CARGO DOOR SCUFF PLATE. ELONGATE HOLES AND CRACKS WERE WELDED, HOLES WERE RE-DRILLED AND AREAS WERE GROUND, FPI WAS ACCOMPLISHED ON WELDED AREAS, NO CRACKS WERE FOUND IAW ER/A 491023-14MA, REV A.

Part: STRINGER — CRACKED (RT WING) · airframe 63,056 hrs · 45,883 cycles

CRACK ON STRINGER 17 RT ON STA XCW=12 INSIDE CENTER TANK. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM THE FORM 8100-9 APPROVAL DATE: 7-SEP-16. AN ADDITIONAL ERA REVISION IS REQUIRED FOR CONTINUED REVENUE SERVICE BEYOND THIS LIMIT, IAW ERA 549279-14, REV ORIG MONITORING UNDER LOG 2673825.

Part: HINGE — DAMAGED (CARGO DOOR) · airframe 63,056 hrs · 45,883 cycles

INITIAL: ELONGATED HOLES ON HINGE 2 EA AT MID CARGO COMPARTMENT DOOR. FWD AND AFT MID CARGO DOOR HINGES WERE REMOVED IAW AMM 52-31-02-201. REPAIRED IAW ER/A 497387-14MA AND ER/A 10521061-14, REV ORIGINAL. REPAIRED HINGES WERE INSTALLED IAW AMM 52-31-02-201.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,056 hrs · 45,883 cycles

CORROSION ON INTERCOSTAL JUST AROUND NUT PLATES STA Y=1307 TO Y=1322 BETWEEN LONG 27LT -28 LT AT AFT CARGO COMPARTMENT. INTERCOSTAL STA Y=1307 TO Y=1322 BETWEEN LONGERON 27LT -28 LT AT AFT CARGO COMPARTMENT WAS REPLACED IAW SRM 51-30-2 AND 51-10-3 PAR 21 AND PAR 14 AND DWG 9936718.

Part: HINGE — DAMAGED (CARGO DOOR) · airframe 63,056 hrs · 45,883 cycles

AWR, HIDDEN DISCREPANCY. ELONGATED HOLES ON FWD & AFT HINGE, BOLT AND SPRING AREA, AT AFT CARGO COMPARTMENT DOOR. AFT CARGO COMPARTMENT DOOR HINGES WERE REMOVED IAW AMM 52-30-02, REPAIRED IAW ER/A 497387-14MA, REV B AND REPAIRED HINGES WERE INSTALLED IAW AMM 52-30-02.

Part: SPLICE — CRACKED (RT WING) · airframe 63,056 hrs · 45,883 cycles

INITIAL: CRACKED SPLICE STA XFS=194 AT RT WING L/E STRUCTURE. CRACK .265" WAS REPAIRED IAW ER/A 379404-14MA, REV A.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,056 hrs · 45,883 cycles

AWR: CORROSION ON INTERCOSTAL STA Y=769-Y=788 BETWEEN LONGERON 27 LT AND 28 LT LONG AT MID CARGO COMPARTMENT. INTERCOSTAL WAS REPAIRED IAW SRM 51-70-5, FIG 1.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,056 hrs · 45,883 cycles

INITIAL: CORROSION ON LONGERON NR 20 RT STA Y=1250-1271 AT AFT CARGO COMPARTMENT. SECTION DAMAGE OF LONGERON WAS REMOVED IAW SRM 53-02, FIG 18. SPLICE WAS FABRICATED IAW SRM 53-02, FIG 18. NEW SECTION LONGERON WAS DRILLED AND ADJUSTED IAW SRM 51-10-4. FPI WAS ACCOMPLISHED ON TRIMMED EDGES OF LONGERON NR 20 RT AT AFT CARGO COMPARTMENT NO CRACKS WERE FOUND IAW NDTSPM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

INITIAL, CRACKED FRAME STA Y=1510 UPPER SECTION, LOWER RT/LT SECTION AT AFT ACCESSORY COMPARTMENT. FRAMES SECTIONS Y=1510 UPPER CENTRAL AND LOWER RT/LT WERE REPLACED IAW DWG 9911843, REV C.

Part: BEAM — CRACKED (L1 DOOR) · airframe 63,056 hrs · 45,883 cycles

INITIAL: DOOR CRACKED L1 DOOR BEAM 1 FWD/AFT FITTINGS. DAMAGE BEAM WERE REPAIRED IAW SRM 52-05, FIG 81.

Part: REPAIR — WORN (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

INITIAL, WORN PREVIOUS REPAIR ON WEB BETWEEN STA Y=629 TO 636 BETWEEN LONG PROJECTION 27 RT TO 28 RT AT MID CARGO COMPARTMENT. PREVIOUS REPAIR WAS REPLACED IAW SRM 53-01, FIG 2.

Part: TAB — DENTED (RT ELEVATOR) · airframe 63,056 hrs · 45,883 cycles

DAMAGE T-DENT ON RT ELEVATOR GEARED TAB. RT ELEVATOR GEARED TAB WAS REPAIRED IAW SRM 55-04, P 4.

Part: WEB — WORN (L1 DOOR) · airframe 63,056 hrs · 45,883 cycles

DOOR WEAR L1 DOOR WEB AT BEAM 5 AFT SECTION, SN 00698. WEB ON BEAM 5 AFT SECTION WAS REPAIRED IAW SRM 52-01, FIG 4.

Part: FRAME — CRACKED (LT WING) · airframe 63,056 hrs · 45,883 cycles

A CRACK WAS FOUND ON LT WING FRAME STR 11 OF 1.250" AT STA XRS=160. LT WING FRAME STR 11 WITH CRACK 1.250" WAS REPAIRED WITH CARD 5712-01030-03.

Part: SKIN — CRACKED (L1 DOOR) · airframe 63,056 hrs · 45,883 cycles

DOOR CRACKED L1 DOOR EXTERNAL SKIN LOWER/AFT SECTION. SN 00696 CRACK ON EXTERNAL SKIN LOWER AFT SECTION WAS REPAIRED IAW SRM 52 05D, FIG 37.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

INITIAL CRACKED WEB ON FRAME STA Y= 1485, CANT POSITION 10 HRS AT AFT ACCESSORY COMPARTMENT. WEB ON FRAME STA Y=1485, CANT POSITION 10 HRS AT AFT COMPARTMENT WAS REPAIRED IAW SRM 53-03D, FIG 48, PAR 43.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,056 hrs · 45,883 cycles

INITIAL, CRACK ON INNER PAN, BEAM NR 1 FWD EDGE AT MID CARGO COMPARTMENT DOOR C2. INNER PAN WAS REPAIRED IAW SRM 52-03D, FIG 8.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

RE-WRITE: INITIAL, CRACKED END LONGERON 2 RT STA Y=1418 AT AFT ACCESSORY COMPARTMENT. REASON FOR RE-WRITE: LONGERON AND END LONGERON NOT INSTALLED. LONGERON AND LONGERON END WERE INSTALLED IAW SRM 51-30-5 AND 53-02, FIG 18.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

INITIAL, CRACKED LONG 4 LT AND 5 LT STA Y=1437 AT AFT ACCESSORY COMPARTMENT. LONGERONS 4 LT AND 5 LT STA Y=1437 WERE REPAIRED IAW SRM 53-02, FIGURE 18.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 63,056 hrs · 45,883 cycles

DENT AND SRATCHES ON UPPER SKIN XET=82 AT RT ELEVATOR. AREA WAS FOUND OUT OF LIMITS AND WAS REPAIRED IAW ETI-88-16-327 REVISION 1 AND ER/A 550271-14 REV. ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

INITIAL, CRACKED FRAME STA Y=1452, LONGERON 8RT AT AFT ACCESSORY COMPARTMENT. FRAME WAS REPLACED IAW DWG 9911860-3, REV L.

Part: FRAME — CRACKED (BS 1474) · airframe 63,056 hrs · 45,883 cycles

CRACKED FRAME BS 1474, LONGERON 18R AT AFT ACCESSORY COMPARTMENT. THE FRAME WAS REPAIRED IAW SRM 51-70-5 FIG. 1.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 63,056 hrs · 45,883 cycles

CRACK ON CHANNEL OF FLOOR PANEL. THE FLOOR PANEL REPAIRED IAW SRM 53-05 FIG 131B AND 131C, AND SRM 51-70-1 PAG. 10.

Part: SKIN — PUNCTURED (LT ELEVATOR TAB) · airframe 63,056 hrs · 45,883 cycles

INITIAL: PUNCTURE ON LT ELEVATOR ANTI-FLOAT TAB UPPER SKIN. LT ELEVATOR ANTI-FLOAT TAB WAS REPAIRED BY SRM 55-04, PAR 2.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,056 hrs · 45,883 cycles

INITIAL PART RACK. REPAIR AS REQUIRED, INSERT, DELAMINATION, PUNCTURE FLOOR PANEL OF CPAX NR 826B, C, D, E, F, NR 886 B, C, D AND NR 927 B, C, D, WING BOX AREA. FLOOR PANEL NR: 927C, 826F, 826C AND 886D WERE FABRICATED IAW AMM 53-20-01-201 AND FERRULES ON FLOOR PANEL NR: 826B, 927B, 927D, 826D, 826E, 886B AND 927C WERE REPLACED IAW AMM 53-20-01-201.

Part: DOUBLER — WORN (TE FLAP VANE) · airframe 63,056 hrs · 45,883 cycles

INITIAL WEAR REPAIR DOUBLER AT LT INBD VANE OF OTBD FLAP. LT INBD VANE OF OTBD FLAP WAS REPAIRED BY SRM 57-03D, PAR 11.

Part: DOUBLER — WORN (TE FLAP VANE) · airframe 63,056 hrs · 45,883 cycles

INITIAL WEAR DOUBLER ON T/E AT RT INBD VANE OF OTBD FLAP. RT INBD VANE OF OTBD FLAP WAS REPAIRED BY SRM 57-03D, PAR 11.

Part: PAN — CRACKED (L1 DOOR) · airframe 63,056 hrs · 45,883 cycles

DOOR CRACKED L1 DOOR FWD PAN ABOVE BEAM 1. CRACK ON FORWARD PAN ABOVE BEAM 1 WAS REPAIRED IAW 80 SRM 52-05-D, FIG 18A.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,056 hrs · 45,883 cycles

INITIAL PART RACK. REPAIR AS REQUIRED, INSERT, DELAMINATION, PUNCTURE FLOOR PANEL OF CPAX NRS 1003 B, C, D, E, 1079 B, C, D, 1117 C, D, E, 1155, B, 1174C, D, E, 1250B, C, D AND 1307B. FLOOR PANEL NR 1079D, 1079C WERE FABRICATED IAW 8 AMM 53-20-01-200 AND FLOOR PANEL NR 1079B, 1003 B, C, D, E, 1117C, D, E, 1155B, 1174C, D, E, 1250B, C, D, 1307B WERE REPLACED FERRULES IAW AMM 53-20-01-200.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

INITIAL, CRACKED FRAME CLIP STA Y=1437 PROYECTION LONGERON 2RT AT AFT ACCESSORY COMPARTMENT. CLIP WAS REPLACED IAW DWG 9953016-30, REV AT SRM 51-30-2 AND SRM 51-30-5.

Part: HINGE BRACKET — DAMAGED (TE FLAP) · airframe 63,056 hrs · 45,883 cycles

AWR: HIDDEN DISCREPANCY, ELONGATED HOLES ON NR 4 FORWARD FIXED FLAP HINGE BRACKET STA XW=333.147, RT WING. FORWARD FIXED FLAP HINGE BRACKET STA XW= 333.147, RT WING WAS REPLACED IAW AMM 57-40-01-201, STEP 3H 1 TO 9B.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,056 hrs · 45,883 cycles

INITIAL, CORROSION ON C-3 LOWER DOOR JAMB REPAIR DOUBLER. C3 REPAIR DOUBLER WAS REPLACED IAW 53-05, FIG 123. PERFORM DECAL VISUAL INSPECTION EVERY C-CHECK IAW TOPP 30-10-70, PAR I.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

AWR: CRACK LT CUSP WEB BETWEEN X=54 TO =60, STA Y=900 AT PASSENGER CABIN FLOOR STRUCTURE. THIS NRC WAS ATTENDED IAW SRM 53-05, FIGURE 131-4, SHEET 1 AND 131A--13, SRM 51-30-2 AND SRM 51-10-3, PAR 14, 21.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,056 hrs · 45,883 cycles

REPAIR AS REQUIRED: INSERT, DELAMINATION, PUNCTURE, FLOOR PANEL OF CPAX NR 256 B, C, D, 313B, 389C, E, 465C, 541C, D AND 769B, C, D, E, F. FLOOR PANEL NR 256D AND 313B WERE REPAIRED IAW AMM 25-00-00-801. FLOOR PANEL NR 389E, 769B, 769D AND 769E WERE FABRICATED AND IDENTIFIED IAW AMM 53-20-01-201. FERRULES ON FLOOR PANEL NR 256B, 769C, 541D, 541C, 256C AND 389C WERE REPLACED IAW AMM 53-20-01-201.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,056 hrs · 45,883 cycles

AWR: CORROSION ON COUNTERSINKS AND SETTLEMENT AREA AT FUEL TANK ACCESS NR 1414C AND NR 1462C. ACCESS PLATE 1414C AND 1462C WERE CLEANED, BOTH ACCESS PLATES HAD 3 COUNTERSINKS ADJACENT OUT OF LIMITS, THEREFORE WERE REPLACED IAW SRM 51-22-2A, PAR 6, CONDITION II ACCESS PLATE NR 1434C WAS REMOVED AND INSTALLED ON NEW ACCESS PLATE 1414C. IAW AMM 28-00-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

INITIAL, CRACKED END OF LONGERON 2RT STA Y=1418 AT AFT ACCESSORY COMPARTMENT. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 63,056 hrs · 45,883 cycles

INITIAL PART RACK, DELAMINATED COCKPIT FLOOR PANEL 120E AND CRACK ANGLES, 2 ALUMINUM AND 1 PLASTIC. FLOOR PANEL 120E WAS FABRICATED IAW AMM 53-20-01-201, PAR 7C AND ANGLE OF PLASTIC WAS REPAIRED IAW SRM 51-70-1D, PAR 10 AND ANGLES OF ALUMINUM WERE FABRICATED IAW DWG 9957820, REV.

Part: BEAM — CRACKED (L1 DOOR) · airframe 63,056 hrs · 45,883 cycles

INITIAL, DOOR CRACKED L1 DOOR BEAM 7 AFT SECTION. CRACK ON BEAM 7 AFT SECTION WAS REPAIRED IAW SRM 52-05-D, FIG 93.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,056 hrs · 45,883 cycles

CORROSION OUT OF LIMITS ON RT CUSP WEB UPPER AND LOWER SURFACE BETWEEN X--54 TO X -60, STA Y=1234 TO STA Y=1240 AT PASSENGER CABIN FLOOR. WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: LANYARD — BROKEN (EVAC SLIDE) · airframe 63,056 hrs · 45,883 cycles

BROKEN CABLES ON LANYARD OF FWD SERVICE DOOR EVACUATION SLIDE, R1. LANYARD OF FORWARD SERVICE DOOR EVACUATION SLIDE, R1 WAS REPLACED IAW AMM 25-62-00-201.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,056 hrs · 45,883 cycles

INSERT, DELAMINATION, PUNCTURE FLOOR PANEL OF CPAX NRS 148 A, B, C, D, 160 A, B, C, D, E, F AND 200 B, C, D, E. FLOOR PANEL NRS 148 B, C, D, 160 A, B, C, D, E, F AND 200 B, C, D, E WERE FABRICATED AND IDENTIFIED IAW AMM 53-20-01-201. FERRULES ON FLOOR PANEL 148A WERE REPLACED IAW AMM 53-20-01-20.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,056 hrs · 45,883 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA AT FUEL TANK ACCESS NR 1335C AND NR 1365C. FUEL TANK ACCESS PLATES NR 1335C AND NR 1365C WERE CLEANED, WERE FOUND OUT OF LIMITS AND WERE REPLACED.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,056 hrs · 45,883 cycles

INITIAL: CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE BETWEEN X= -54 TO-60 STA Y=1041 TO 1060 AT PASSENGER CABIN FLOOR STRUCTURE. WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,056 hrs · 45,883 cycles

CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE BETWEEN X-54 TO -60 STA Y=826 TO 845 AT PASSENGER CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIR IAW SRM 53-05, FIG 131A-7.

Part: WEB — CRACKED (L1 DOOR) · airframe 63,056 hrs · 45,883 cycles

DOOR CRACKED, L1 DOOR WEB AT BEAM 6 AFT SECTION. NEW WEB AT BEAM 6 AFT SECTION WAS INSTALLED IAW SRM 51-30-1, 51-30-2 AND 51-30-4.

Part: ACCESS DOOR — CORRODED (WING) · corrosion level 2 · airframe 63,056 hrs · 45,883 cycles

INITIAL PART RACK. CORROSION ON SETTLEMENT AREA OF FUEL ACCESS DOORS 1409C AND 1303C. ACCESS PLATE NR 1409C AND 1303C: BLEND OUT REPAIR IS NOT PERMITTED ON THE UPPER WING ACCESS DOOR, PN 3912757 DUE TO REDUCED AREA OF THE CONDUCTIVE INTERFACE. THEREFORE THEY WERE REPLACED IAW SRM 51-22-2A, PR 6, CONDITION III.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

HIDDEN DISCREPANCY: CRACKED FRAME ON STA Y=1418, LONGERON 2 RT AT AFT ACCESSORIES COMPARTMENT. STIFFENER, ON FRAME WAS REPLACED IAW SRM 51-30-5 AND 51-30-2.

Part: COTTER PIN — MISSING (TAILCONE RELEASE) · airframe 63,056 hrs · 45,883 cycles

MISSING COTTER PIN ON TAIL CONE RELEASE DOOR HANDLE MECHANISM AT AFT ENTRY DOOR. COTTER PIN ON TAIL CONE RELEASE DOOR HANDLE MECHANISM AT AFT ENTRY DOOR WAS INSTALLED IAW AMM 20-10-18.

Part: ANGLE — CRACKED (BS 1380) · airframe 63,056 hrs · 45,883 cycles

CRACKED FRAME ANGLE BS 1380, LONGERONS 15 - 16L . ANEW FRAME ANGLE AND FITTINGS WERE INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: SKIN — DAMAGED (RT WING) · airframe 63,056 hrs · 45,883 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON LOWER SKIN REAR SPAR BETWEEN XRS 163 - 168 ON RT WING. REPAIRED IAW ER/A 549286-14AD REV.ORIGINAL.

Part: CUSP WEB — CORRODED (BS 475-484) · corrosion level 2 · airframe 63,056 hrs · 45,883 cycles

CORROSION ON RT CUSP WEB BS 475 - 484 AND X -54 TO X - 60. CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A-11.

Part: SKIN — DAMAGED (LT WING) · airframe 63,056 hrs · 45,883 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON LOWER SKIN REAR SPAR BETWEEN XRS 163 - 168 ON THE LT WING. REPAIRED IAW ER/A 549286-14AD REV. ORIGINAL.

Part: TAB — BROKEN (RUDDER) · airframe 63,056 hrs · 45,883 cycles

BROKEN RUDDER CONTROL TAB UPPER TRAILING EDGE. DUE TO SEVERAL DAMAGE AND THE ALLOWABLE LIMITS OF BALANCE IS NEAR TO THE MAXIMUM LIMIT THE RUDDER TAB WAS REPLACED IAW SRM 51-70-1A.

Part: CUSP WEB — CORRODED (BS 1241-1244) · corrosion level 2 · airframe 63,056 hrs · 45,883 cycles

CORROSOIN ON LEFT CUSP WEB UPPER SURFACE BETWEEN X=54 TO =60 BS 1241 - 1244. THE CUSP WEB WAS REPAIRED IAW SRM 53-05- FIG.131A-13.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

INITIAL, CRACKED FRAME CLIP STA Y=1380 BETWEEN LONGERON 13RT TO 14RT AT AFT ACCESSORY COMPARTMENT. FRAME CLIP WAS REPLACED IAW SRM 53-14-4 AND SRM 51-30-2, SRM 51-30-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,056 hrs · 45,883 cycles

CORROSION ON LT CUSP WEB UPPER AND LOWER SURFACE BETWEEN X=54 TO =60, STA Y=1060 TO 1079 AND 1093 TO 1096 AT PASSENGER CABIN FLOOR STRUCTURE. WEB STA=1093-1096 WAS REPAIRED IAW SRM 53-05, FIG 131A-13 AND STA Y=1060-1079 WAS ATTENDED WITH NRC 1155.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,112 hrs · 45,927 cycles

PREVIOUS BLEND OUT ON EXTERNAL FUSELAGE SKIN BTW STA 351-370 AND LONG 9R-10R. REPAIRED PER SRM 53-04-2 FIG 2 SHEET 5.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

CRACK UPPER AFT CORNER OF RING PAN, STA Y=1041 AT RT SIDE OF PASSENGER CABIN. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122 AND ERA 493648-14MA, REV A.

Part: HINGE — DAMAGED (CARGO DOOR) · airframe 63,056 hrs · 45,883 cycles

INITIAL: ELONGATED HOLES ON FWD AND AFT HINGE AT FWD CARGO COMPARTMENT DOOR. FWD AND AFT HINGES WERE REMOVED IAW AMM 52-31-02, REPAIRED IAW ER/A 497387-14MA, REV B AND INSTALLED IAW AMM 52-31-02.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

CRACKED WINDOW RING PAN BETWEEN STA Y=845-864 FWD UPPER CORNER LT SIDE. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122 AND ERA 493648-14MA.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

CRACKED WINDOW RING PAN BETWEEN STA Y=1079-Y-1098 ON FORWARD LOWER CORNER LT SIDE. RING PAN WAS REPAIRED IAW SRM 53-03, FIG 122 AND ERA 493648-14MA, REV A.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

CRACKED WINDOW RING PAN STA Y=1180-1193 AFT UPPER CORNER LT SIDE. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122 AND ERA 493648-14MA.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,056 hrs · 45,883 cycles

CRACKED WINDOW RING PAN STA Y=1180-1193 AFT UPPER CORNER LT SIDE. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122 AND ERA 493648-14MA.

Part: WINDOW FRAME — DAMAGED (RIGHT) · airframe 61,616 hrs · 44,877 cycles

LIGHTNING STRIKE, RT SIDE CABIN WINDOW FRAME NR 2 MARKED. BLENDED DAMAGE AND ROUTED MEASUREMENTS TO ENGINEERING IAW SRM 53-12, FIG 111, 112 AND 113. C/W ER/A 543428-14 REV-0, SECT 1.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 61,616 hrs · 44,877 cycles

LIGHTNING STRIKE, RT ELEVATOR OTBD AFT TIP. R & R RT ELEVATOR TIP END, PN 5910412-81 AND WEDGE COVER, PN 88277-5910412-35, REF DWG 5930557. SEALED TIP AND WEDGE COVER.

Part: FRAME — CRACKED (RT MLG WW) · airframe 60,701 hrs · 44,209 cycles

RT MLG WW FRAME IS CRACKED IN THE BEND RADIUS ALON THE OTBD END NEAR THE HYD SERVICE BAY. REMOVED FWD FRAME PN 5930584. REPLACED FWD W/W FRAME IAW DWG 5930584, SHEET 1.

Part: DOOR FRAME — CRACKED (RT MLG DOOR) · airframe 60,701 hrs · 44,209 cycles

DURING SERVICE CHECK, RT MLG FWD DOOR FRAME CRACKED. STOP DRILLED ALL CRACK TIPS ON THE FRAME WITH A .2500 DIA HOLE IAW TOPP 40-60-05, SECTION X B2 CRACKS ARE ACCEPTABLE TO ENGINEERING FOR A 1-TIME NON REV. PRESSURIZED FERRY FLIGHT CONTINGENT UPON COMPLETION OF THE FOLLOWING REMEDIAL MEASURES.

Part: DOOR FRAME — CORRODED (BS 636-693) · corrosion level 2 · airframe 57,854 hrs · 42,204 cycles

CENTER CARGO DOOR CUTOUT LOWER DOOR FRAME SURFACE HAS CORROSION , BS 636 - 693. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FABRICATED AND INSTALLED PERMANENT REPAIR IAW SRM 53-05, FIG 123, OPTION 1.

Part: RELEASE CABLE — OUT OF RIG (TAILCONE) · airframe 57,854 hrs · 42,204 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE CABLE WAS OUT OF ALLOWABLE RIG LIMITS. THE CABLE WAS ADJUSTED AND THE SYSTEM WAS RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: SKIN — DAMAGED (BS 1304) · airframe 57,854 hrs · 42,204 cycles

FUSELAGE SKIN DENTED AND SCRATCHED BS 1304 ABOVE L19R. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-04-2 PARA 3C, FIG 2, PAGE 27.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 57,848 hrs · 42,198 cycles

FOUND TWO GOUGES ON RT WING INBD FLAP LOWER SKIN. REPAIRED GOUGES IAW SRM 57-01, FIG 1 AND 57-03D, FIG 8.

Part: PRESSURE SWITCH — MALFUNCTIONED (ENGINE OIL) · airframe 57,352 hrs · 41,843 cycles

ENROUTE, FLIGHT CREW DIVERTED BECAUSE THE RT ENGINE OIL STRAINER CLOGGED LIGHT ILLUMINATED. THE ENGINE WAS NOT SHUTDOWN. MAINTENANCE CHECKED THE OIL FILTER AND MAIN CHIP DETECTOR. ALL CHECKS WERE GOOD AND NO MAJOR DEBRIS WAS FOUND IN THE FILTER. MAINTENANCE REPLACED THE DIFFERENTIAL PRESSURE SWITCH.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,182 hrs · 41,083 cycles

DURING LINE CHECK, SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 14DE. LIGHT ASSY REPLACED AND OPS CHECKED NORMAL IAW AMM 33-53.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,909 hrs · 39,498 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 18D IN THE CABIN WAS INOPERATIVE. MX REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: LEVER — DISCONNECTED (THROTTLE) · airframe 53,646 hrs · 39,318 cycles

DIVERTED DUE TO LT ENGINE OVERSPEED CONDITION. CREW COULD NOT CONTROL ENGINE. THROTTLE LOCKED IN FORWARD POSITION. CREW SHUTDOWN ENGINE. MX FOUND NR 1 ENGINE THRUST LEVER DISCONNECTED AND FUEL SHUTOFF BOLT BACKED OUT. INSTALLED NEW HARDWARE. R & R OIL FILTER, CHECKED CHIP DETECTOR AND RIGGED AND OPERATION CHECK FUEL CONTROL IAW AMM. ALL CHECKS GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 52,665 hrs · 38,609 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT ROWS 11, 21, 25 AND 35. CONNECTED CONNECTORS AT ROWS 11, 21 AND 25. FOUND PIN PUSHED BACK AT CONNECTOR ROW 35. REINSTALLED PIN. OPERATION OF EMERGENCY EXIT LIGHTS CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: FAN — MALFUNCTIONED (AC BAY) · airframe 52,125 hrs · 38,253 cycles

FLIGHT CREW REPORTED THAT PASSENGER HEARD ELECTRICAL ARCING NOISE FROM FLOOR AT ROW 27 WHEN GEAR RETRACTED, FOLLOWED BY ELECTRICAL BURNING SMELL. UPON LANDING FOUND RECIRCULATION FAN BREAKERS POPPED. MAINTENANCE REMOVED AND REPLACED RECIRCULATION FAN PER AMM. OPERATION AND LEAK CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,639 hrs · 37,937 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND ESCAPE PATH LIGHTING INOPERATIVE AT ROWS 11DE, 13DE AND 21DE. MAINTENANCE RELAMPED. OPERATION CHECKS GOOD.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 51,253 hrs · 37,696 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 10D IN THE CABIN, WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 50,581 hrs · 37,207 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHT AT ROW 31 INOPERATIVE. MAINTENANCE SECURED CONNECTOR. OPERATION CHECKS GOOD AND THE AIRCRAFT IS OKAY FOR SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 49,449 hrs · 36,409 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHTS INOPERATIVE AT COCKPIT AND SEAT 15. MAINTENANCE RE-LAMPED BOTH LIGHTS AND OPERATIONALLY CHECKED. CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,449 hrs · 36,409 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHTS INOPERATIVE AFT OF SEAT 31, AFT EXIT DOOR AND L2 DOOR. MAINTENANCE REMOVED AND REPLACED BATTERY AND POWER SUPPLY PER MAINTENANCE MANUAL. OPERATION CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE.

Part: WATER HEATER — ODOR (LAVATORY) · airframe 49,295 hrs · 36,302 cycles

IN-FLIGHT PERSONNEL STATED THAT RIGHT AFT LAVATORY SMOKE DETECTOR WENT OFF. SMELL APPEARED TO BE COMING FROM HOT WATER HEATER. MAINTENANCE INSPECTED HEATER. NO EVIDENCE OF OVERHEAT. AIRCRAFT IS OKAY FOR SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 48,012 hrs · 35,435 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT ROW 3 INOPERATIVE. MAINTENANCE FOUND WIRE BROKEN AT PLUG AND RE-PINNED THE HARNESS CONNECTOR. OPERATIONAL CHECK OF LIGHT NOW CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,439 hrs · 34,979 cycles

MAINTENANCE FOUND THE FIRST SEVEN ROWS OF THE EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD BATTERY PACK. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — DAMAGED (FUSELAGE) · airframe 47,439 hrs · 34,979 cycles

"SUPPLEMENTAL INFORMATION" STRAP AND BUSHING REPAIR IAW 09-086680-12 ME015 C/W 09-086680-12 ME15.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 47,180 hrs · 34,820 cycles

SEAT 24DE FWD RED EMERGENCY PATH LIGHT INOP. T/S FOUND SEAT HARNESS CUT AT ZIP TIE NEEDS DAL PN 334202640, SHOULHAN 712232. REPLACE HARNESS AT SEAT 24DE. OPS CKS GOOD.

Part: CYLINDER — CORRODED (RT MLG) · airframe 43,761 hrs · 32,647 cycles

CORROSION PITTING WAS FOUND IN THE LOWER LEFT QUADRANT OF THE RT MLG OUTER CYLINDER. AN ER/A WAS ISSUED TO REWORK THE CYLINDER TO REMOVE THE DAMAGE. SAFE-LIFE LIMIT REDUCED TO 26000 CYCLES FROM FAA APPROVAL DATE OF 9-05-2006.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 39,499 hrs · 29,759 cycles

FOUND FATIGUE CRACK IN UPPER AFT SKIN ON LT HORIZONTAL STABILIZER. ACCOMPLISHED BAC APPROVED STOP DRILL REPAIR.

Part: ENGINE — OUT OF TRIM (NR 2) · airframe 29,799 hrs · 23,141 cycles

RTB NR 2 ENG FAILED TO ACCELERATE ABOVE IDLE DURING THROTTLE ADVANCE FOR T/O. PEAK OF EGT APPROX 490 RPM STAYED AROUND 47 PERCENT N2 ABORTED TAKEOFF BELOW 60 KTS. TRIMMED ENGINE, CHECKS GOOD.

Part: STRUT — UNDERSERVICED (NLG) · airframe 23,465 hrs · 18,551 cycles

NOSE GEAR UNSAFE LIGHT UPON RETRACTION AFTER T.O.(DIVERSION)PERFORMED VISUAL INSP OF ALL NLG LINKAGES, SUPPORTS, AND HARDWARE. SERVICED NLG STRUT PER M/M 32 21 01. JACKED A/C PER M/M 07 11 AND 07 12. CYCLED LDG SEVERAL TIMES. NLG OPERATION AND INDICATION. CHECKS NORMAL WITH EACH CYCLE. OCC CONCURRENCE RECEIVED

Part: COFFEEMAKER — CONTAMINATED (GALLEY) · airframe 22,890 hrs · 18,128 cycles

ELECTRICAL SMELL AFT OF OVERWING EXITS. FOUND AFT GALLEY COFFEEMAKER WITH PIECE OF PLASTIC MELTED ON IT. CLEANED SAME.

Part: BATTERIES — DISCHARGED (LAV SMOKE DET)

LEFT AFT LAV SMOKE DETECTOR WENT OFF ON TAKEOFF. PRECAUTIONARY LANDING AT KLGA. INSPECTED A/C OVENS AND VENTILATION SYSTEM. ALSO, INSPECTED TAIL CONE AREA, INCLUDING BOTH PACKS. RAN PACKS, NO SMOKE NOTED. REPLACED BATTERIES IN BOTH AFT LAVS SMOKE DETECTORS AS PRECAUTION.

Part: ANGLE — CRACKED (LT MLG WW)

FOUND DURING C-1 LETTER CHECK, LT WHEEL WELL AFT JAMB CRACKED 1 INCH LT O/B SIDE. INSTALLED DOUBLER PER MM 53-05 FIG 101.

Part: NOSE COWL — DELAMINATED (LT ENGINE)

DURING SHOP INSPECTION, NR 1 ENGINE NOSE COWL WAS FOUND WITH THE OUTER SKIN OF ACOUSTIC PANEL DELAMINATED OVER AN 8 INCH BY 20 INCH AREA AT THE 6 O'CLOCK POSITION. REPAIRED DAMAGE PER SRM 54-04.