N992DL

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,451 hrs · 49,253 cycles

TAIL COMPARTMENT WALKWAY CENTER EMERGENCY LIGHT OUT. REFERENCED WDM 33-51-13. FOUND NO POWER AT LAMP. REPLACED BATTERIES IN POWER SUPPLY B5-28 (LOCATED IN AFT RIGHT LAVATORY CEILING). OPS CHECK OK. PN'S OFF AND ON TWO 41B004AD07G3 BATTERIES.

Part: SLAT — DAMAGED (L1) · airframe 68,370 hrs · 49,184 cycles

NR 1 LEFT SLAT WAS DAMAGED. REPLACED THE SLAT IAW W/C 2700-4224-LH-01.

Part: STRUCTURE — DAMAGED (LT WING) · airframe 68,375 hrs · 49,189 cycles

DURING A WALK AROUND, FOUND THE GAUGE ON THE LT WING L/E UNDER SLAT NR 1, XFS 136. COMPLIED WITH A DETAILED VISUAL INSPECTION OF THE DAMAGED AREA. FABRICATED A REPAIR DOUBLER IAW SRM 57-06B, FIG 13. COMPLETED INSTALLATION OF REPAIR IAW SRM 57-06B, FIG 31.

Part: CONTROL CABLE — SEVERED (NLG STEERING) · airframe 67,948 hrs · 48,821 cycles

TAKING THE RUNWAY LOST ALL STEERING TO THE RIGHT VIA THE TILLER. FOUND NOSE WHEEL STEERING CONTROL CABLE 123A SEVERED. REMOVED AND REPLACED 123A REF AMM 32-51. PERFORMED STEERING TEST REF AMM 32-52. CKS NML.

Part: DOOR FRAME — CRACKED (LT MLG WW) · airframe 66,884 hrs · 48,042 cycles

CRACK ON CORNER UP SIDE OF DOOR JAMB FWD WHEEL WELL LT. DOOR JAMB FWD WHEEL WELL LT ( PAN ) WAS REPLACED PER DC9/MD80 SRM 51-30-2 AND 51-30-5.

Part: DOOR FRAME — CRACKED (RT MLG WW) · airframe 66,884 hrs · 48,042 cycles

CRACK ON CORNER UP SIDE OF DOOR JAMB FWD WHEEL WELL RT. DOOR JAMB FWD WHEEL WELL RT ( PAN ) WAS REPLACED PER SRM 51-30-02 AND 51-30-05.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,580 hrs · 47,834 cycles

EMERGENCY LIGHTS FOR SEATS ROWS 31 AFT INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERIES IAW AMM 33-53. OPS CHECKED GOOD.

Part: WIRE — SHORTED (EMERGENCY LIGHT) · airframe 66,566 hrs · 47,823 cycles

EMERGENCY LIGHTS FOR SEATS 31-36 WILL NOT WORK IN TEST MODE. REPLACED AFT EMERGENCY LIGHTS BATTERY AND CHARGER, B5-212, IAW AMM 33-53. REPAIRED A SHORTED WIRE L902T14 IAW WDM 33-51-14. THE SYSTEM CHECKED GOOD IAW AMM 33-53.

Part: SUPPORT FITTING — WORN (TAILCONE) · airframe 64,797 hrs · 46,483 cycles

TAIL CONE CAM MECHANISM SUPPORT FITTING WORN, AND FAILED TORQUE CHECK. REMOVED THE TAIL CONE SUPPORT FITTING AND REPLACED THE SHAFT AND SUPPORT FITTING IAW AMM 53-53-02 AND AMDS 5350-010770101.

Part: SKIN — DETERIORATED (RUDDER) · airframe 63,631 hrs · 45,659 cycles

FLAME SPRAY DETERIORATED ON RUDDER WITHIN 7" OF FORWARD SPAR ON BOTH SIDES. R & R RUDDER.

Part: LIGHT — DAMAGED (GALLEY) · airframe 62,411 hrs · 44,807 cycles

THE FLIGHT CREW FOUND EMERGENCY LIGHTS DAMAGED. MAINTENANCE RESECURED THE EMERGENCY EXIT LIGHT AT DOOR R1 AND THE FORWARD EMERGENCY EXIT FLOOR LIGHT IN THE G2 GALLEY.

Part: FAN — FAILED (RECIRCULATION) · airframe 62,059 hrs · 44,573 cycles

F/A NOTICED AN ACRID ODOR AT 1300 FT ON ARRIVAL. TURNED OFF ALL CABIN LIGHTS, ODOR DISSAPATED YET NEVER WENT AWAY. W/C 2120-2367, FOUND RECIRCULATION FAN WITH SMOKE ODOR AND EXCESSIVE VIBRATION. R & R RECIRCULATION FAN IAW AMM 21-20, CONTACTED OK FOR SERVICE.

Part: SPAR CAP — DAMAGED (HORIZONTAL STAB) · airframe 61,722 hrs · 44,342 cycles

PREVIOUS TOOL DAMAGE ON NEW RT HORIZONTAL STABILIZER REAR SPAR UPPER CAP XHS=115. REAR SPAR UPPER CAP WAS REPAIRED IAW ER/A 541579-14AD, REV ORIGINAL ETI-88-15-435, REV 2.

Part: PAN — CRACKED (CARGO DOOR) · airframe 61,722 hrs · 44,342 cycles

CRACKED OUTER PAN BETWEEN BEAM 1 AND 2 FWD EDGE AT AFT CARGO COMPARTMENT DOOR. OUTER PAN BETWEEN BEAM 1 AND 2 FWD EDGE AT AFT CARGO COMPARTMENT DOOR, C3 WAS REPAIRED IAW ERA 541561-14, REV ORIG PERMANENT REPAIR.

Part: SUPPORT FITTING — CORRODED (LT MLG WW) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION ON LT RETRACT ACTUATOR SUPPORT FITTING BORE. REPAIRED IAW DWG SR09570087, REV B.

Part: HINGE — DAMAGED (CARGO DOOR) · airframe 61,722 hrs · 44,342 cycles

ELONGATED HOLES ON FWD/AFT HINGE AT MID CARGO COMPARTMENT DOOR. FWD/AFT HINGES AT MID CARGO COMPARTMENT DOOR WERE REPLACED THEREFORE HINGES ARE OUT OF LIMITS IAW MD-88 52-31- 02 AND ER/A 497387-14MA, REV B. ADJUST AND TEST WILL BE ACCOMPLISHED WITH CARD 5200-4291, JOB 001-0319.

Part: PAN — CRACKED (BS 370) · airframe 61,722 hrs · 44,342 cycles

CRACKED INNER PAN BS 370 . INNER PAN WAS REPAIRED IAW ER/A 541559-14, REV ORIG.

Part: SUPPORT FITTING — CORRODED · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION ON RT MLG RETRACT ACTUATOR SUPPORT FITTING BUSHING VERTICAL FACE AND BORE. REPAIRED IAW DWG SR09570087, REV B.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 61,722 hrs · 44,342 cycles

DELAMINATED AND DAMAGED FLOOR PANEL BS 1231 - 1338 . THE FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.

Part: SPAR CAP — DAMAGED (HORIZONTAL STAB) · airframe 66,708 hrs · 47,940 cycles

MD88 - STABILIZERS / H.S. / RH REAR SPAR UPPER CAP, XHS 115 / TOOLING DAMAGE. DTA MONITOR INSPECTION LOG REFERENCE ER/A 541579-14AD SECTION II REQUIRES DTA APPROVAL WITHIN 24 MONTHS AFTER SECTION I. ER/A 541579-14AD REV A IS CURRENT. DTA RESTRICTION REMOVED, LOGPAGE TO BE TERMINATED. (LP2268848)

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND COUNTER SKIN AREAS OF FUEL ACCESS PANEL 1466C. FUEL ACCESS 1466C WAS REPLACED IAW SRM 51-22-2A AND IPC 57-30-00-05B AND WILL BE INSTALLED UNDER CARD 2800-0390, JOB 001-0454.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION ON BARREL NUT HOLE NR 13, BS XM=27.234 AT LT HORIZONTAL STABILIZER. BARREL NUT NR 13 AT LT HORIZONTAL STABILIZER WAS REMOVED IAW AMM 20-10-14 CORROSION WAS REMOVED IAW ER/A 541539-14, REV ORIGINAL. BUSHING WAS FABRICATED AND INSTALLED IAW ER/A REV ORIGINAL 541539-14 AND A NEW BARREL NUT WAS INSTALLED IAW AMM 20-10-14.

Part: CUSP WEB — CORRODED (BS 627-653) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION ON LT CUSP WEB LOWER SURFACE BETWEEN X= 54-X=60 AND BETWEEN BS 627-632, 636-641 AND 648-653. CUSP WEB X 54, 522 TO 788 WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 9930538, REV CF.

Part: RIB — DAMAGED (HORIZONTAL STAB) · airframe 61,722 hrs · 44,342 cycles

ELONGATED HOLE ON RIB AT RT HORIZONTAL STABILIZER OUTER CONSTANT SECTION REAR SPAR BS XH=27.234 ELONGATED HOLE WAS REPAIR IAW ETI-88-15-418 AND ER/A 541547-14, REV ORIGINAL.

Part: HINGE — CRACKED (SPOILER) · airframe 61,722 hrs · 44,342 cycles

CRACK INBD HINGE FITTING AT LT GROUND SPOILER BS XW=47.450, REAR SPAR WING RIB. REAR SPAR WING RIB WAS REPLACED IAW SRM 51-30-2, 51-30-1 AND DWG 5936830-501.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1335C. FUEL ACCESS 1335C WAS REPLACED IAW SRM 51-22-2A AND WILL BE INSTALLED WITH CARD 2800-0120, JOB 001-0445.

Part: TRIPLER — PUNCTURED · airframe 61,722 hrs · 44,342 cycles

PUNCTURED PREVIOUS REPAIR TRIPLER ON AFT LAVATORY SERVICE PANEL CUTOUT. REPLACE REPAIR TRIPLER IAW ER/A 529789-14, REV A AND SRM 51-30-2 AND 51-30-5.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 61,722 hrs · 44,342 cycles

CRACK ON HORIZONTAL STABILIZER RT REAR SPAR CAP AT CRITICAL HOLE CARD. REAR CAP WAS REPLACED IAW DWG 09550030, REV C AND SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 61,722 hrs · 44,342 cycles

TOOL DAMAGE ON BARREL NUT HOLE NR 8 AT RT HORIZONTAL STABILIZER BS XH=27.234. BARREL NUT WAS REMOVED IAW AMM 20-10-14. NEW BUSHING WAS FABRICATED IAW ER/A 541558-14, REV ORIGINAL AND NEW BUSHING WAS INSTALLED IAW 541558-14, REV ORIGINAL AND NEW BARREL NUT WAS INSTALLED IAW AMM 20-10-14.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1472C. FUEL PANEL WAS REPLACED.

Part: DOUBLER — CORRODED (BS 714-724) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION ON PRODUCTION DOUBLER RADIO ALTIMETER ANTENNA SETTLEMENT CUTOUT BS 724 TO 714. PRODUCTION DOUBLER DUE TO EXCECESIVE CORROSION WAS REPLACED IAW DWG 5911412-309, REV DV AND 51-30-5, 51-30-2.

Part: SPLICE — LOOSE (VERTICAL STAB) · airframe 61,722 hrs · 44,342 cycles

LOOSE FASTENERS ON SPLICE OF L/E AT VERTICAL STABILIZER BS ZFS=52.26. ALL HOLES COUNTERSINK WERE MEASURED IAW CARD 5530-01045-05, STEP 2, JOB 055-0001 AND WAS FOUND OUT OF LIMITS, 49 EA. REPAIRED IAW CARD 5530-01045-08, STEP 1, JOB 167-0001 AND SRM 55-03D, PARA 27 AND 28.

Part: SLAT TRACK — WORN (LT WING) · airframe 61,722 hrs · 44,342 cycles

WEAR ON FLANGES OF LT WING SLAT TRACKS 7, 9 AND 13. LT WING SLAT TRACKS 7, 9 AND 13 WERE REPLACED IAW AMM 27-80-00.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION ON FRAME 1380 BETWEEN BS 24L-24R. FRAME WAS REPLACED IAW SRM 51-30-5, 51-30-2, 51-10-4, 53-01 FIG 1.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION OUT OF LIMITS ON 2 COUNTERSINK HOLES ON FUEL ACCESS PLATE NR. 1371C. SRM 51-22-2A. FUEL ACCESS PLATE AND BUSHINGS WERE TREATED IAW SRM 51-10-3, NEW BUSHINGS WERE INSTALLED.

Part: SLAT TRACK — WORN (RT WING) · airframe 61,722 hrs · 44,342 cycles

WEAR RT WING SLAT TRACK 13. SLAT TRACK 13 AT RT WING WAS REPLACED IAW AMM 27-80-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,722 hrs · 44,342 cycles

LIGHTNING STRIKE ON AFT EDGE AT WINDOW BELT NR 57 EXTERNAL FUSELAGE SKIN. DAMAGE WAS REMOVED, MEASURED AND TREATED IAW 53-05, FIG 111, SHEET 10 AND 51-10-3 PAR-21. PERFORM DECAL CONDITION INSPECTION EVERY C-CHECK IAW TOPP 30-10-70 PAR I PAGE 13.

Part: SKIN — DAMAGED (BS 200-207) · airframe 61,722 hrs · 44,342 cycles

PROTRUSION ON EXTERNAL FUSELAGE, SKIN BS 200-207 BETWEEN LONGERON 30-29 LT ALSO 214 LONGERON 28-29 LT. DENTS ON FUSELAGE SKIN WERE MEASURED PRESENTING THE FOLLOWING CONDITIONS: BS 200-207, LONGERON 29-30 LT X= DEPTH= 0.042 ", D= DIMENTION= 1.500". D/X = 1.560/0.038=41.05. IT IS WITHIN LIMITS IAW SRM 53-04-01, PARR 7E, CONDITION 1B.

Part: PAN — CRACKED (PAX DOOR) · airframe 61,722 hrs · 44,342 cycles

CRACKED REPAIR DOUBLER ON FORWARD UPPER PAN AT FORWARD PASSENGER DOOR LT. FORWARD UPPER PAN AT FWD PASSENGER DOOR L1 WAS REPLACE IAW SRM 51-30-4, 51-30-1, 51-30-2 AND DWG 591421, REV AV.

Part: SKIN — DENTED (BS 148) · airframe 61,722 hrs · 44,342 cycles

DENT ON EXTERNAL FUSELAGE SKIN BS 148 BETWEEN LONGERON 24 LT ON LONG 25 LT. FOUND WITHIN LIMITS IAW SRM 53-04-1, PARR 7E CONDITION 1B.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND COUNTERSKIN AREAS OF FUEL ACCESS PANEL 1409C. FUEL ACCESS 1409C WAS REPLACED IAW SRM 51-22-2A CONDITION II PARAGRAPH, B.

Part: CARGO TRACK — CORRODED (BS 1003-1155) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION ON CARGO TRACK, AROUND FASTENERS FROM BS 1003 TO 1155. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1 AND 51-30-2, 51-10-4, 51-10-3 PARS 14 AND 21 AND 38.

Part: SKIN — WORN (BS 1287-1309) · airframe 61,722 hrs · 44,342 cycles

WORN PREVIOUS REPAIR FILLER ON FUSELAGE SKIN BETWEEN BS 1287-1309 AND LONGERONS 18R-19R. FILLER WAS REPLACED IAW SRM 51-30-5, 51-10-3, PAR 14 AND 21 AND 53-04-2, FIG 2.

Part: HINGE — DAMAGED (CARGO DOOR) · airframe 61,722 hrs · 44,342 cycles

ELONGATED HOLE ON FWD/AFT HINGE AT AFT CARGO COMPARTMENT DOOR. DAMAGED HOLE ON FWD HINGE WAS REPAIRED IAW ER/A 497387-14MA, REV B AND AFT HINGE WAS REPLACED FOR A NEW HINGE.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 61,722 hrs · 44,342 cycles

CRACK ON RT WING SLAT PANEL NR 2 INNER SKIN BS XOS 240, CARD 04, ZONE 12. CRACK ON INNER SKIN WAS ATTENDED IAW SRM 57-01, FIG 3, SHT 2.

Part: VANE — WORN (RT WING TE FLAP) · airframe 61,722 hrs · 44,342 cycles

WORN PREVIOUS REPAIR DOUBLER ON INBD VANE, OTBD FLAP AT RT WING. REPAIR DOUBLER INBD VANE, OTBD FLAP AT RT WING WAS REPLACED IAW A/C 0992, CARD 2000-8149-05.

Part: CUSP WEB — CRACKED (BS 1136) · airframe 61,722 hrs · 44,342 cycles

CUSP WEB CRACKED AT PREVIOUS REPAIR IN AFT CARGO RT SIDE BETWEEN BS 1136-1155. CUSP WEB REPAIR IAW SRM 51-30-2, 53-05, FIG 131A-1, 51-30-5.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 61,722 hrs · 44,342 cycles

CRACK ON FLOOR PANEL 1079A. FLOOR PANEL REPAIRED IAW SRM 51-70-1, PAR 10.

Part: FLOOR SUPPORT — CRACKED (BS 1271-1287) · airframe 61,722 hrs · 44,342 cycles

FLOOR SUPPORT CRACKED AT UPPER SUPPORT ANGLE BETWEEN CABIN FLOORBEAMS 1271-1287 LBL 5. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-01 51-30-2 AND 51-30-5.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 61,722 hrs · 44,342 cycles

CRACK ON FLOOR PANEL. FLOOR PANEL WAS REPAIRED IAW SRM 51-70-1-D, PAR 10, AND SRM 53-05, FIG 131-B.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND CONTERSINK AREAS OF FUEL ACCESS PANEL 1470C, AYP. CORROSION ON FUEL ACCESS PLATE 1470C WAS REMOVED IAW SRM 51-22-2A AND COUNTERSINK HOLES WERE MEASURED AND MAX DIAMETER ALLOWABLE IS 0.532" AND MAX DIAMETER MEASURED IS 0.535" THEREFORE WAS FOUND WITHIN LIMITS, SETTLEMENT AREA WAS MEASURED ORIGINAL THICKNESS IS .150" AND MAX DIAMETER REMOVED IS .026" THEREFORE IT IS OUT OF LIMITS IAW SRM 51-22-2A AND FUEL ACCESS PLATE 1470C WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390, JOB 001-0454.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 61,722 hrs · 44,342 cycles

CRACKED STOP FITTING NR 2, 3, 4 AT AFT CARGO COMPARTMENT DOOR AFT EDGE, C3, SM. STOP FITTINGS NR 2, 3, 4 AT AFT CARGO DOOR, C3, WERE REPLACED IAW SRM 51-30-01.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 61,722 hrs · 44,342 cycles

DELAMINATED ON LOWER SKIN AT LT ELEVATOR CONTROL TAB BTW STA XET=65 TO XET=46 AND XET=46 TO XET=26 (VHS) (SM) (CARD 3 ZONE 65). LH ELEVATOR CONTROL TAB WAS REPLACED IAW SRM 55-04 AND WILL BE INSTALLED UNDER CARD 2730-4334, JOB 001-0229.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1454C, AYP. CORROSION ON FUEL ACCESS 1454C WAS REMOVED IAW SRM 51-22-2A, COUNTERSINK HOLES WERE MEASURED AND MAX DIAMETER ALLOWABLE IS 0.532" AND MAX DIAMETER IS .528". FOUND WITHIN LIMITS, SETTLEMENT AREA WAS MEASURED, ORIGINAL THICKNESS IS .150" AND MAX MATERIAL REMOVED IS .028". ITS OUT OF LIMITS IAW SRM 51-22-2A AND FUEL ACCESS 1454C WAS REPLACED.

Part: DOUBLER — CRACKED (BS 1463-1474) · airframe 61,722 hrs · 44,342 cycles

CRACK DOUBLER BETWEEN BS 1463 - 1474 BETWEEN LONGERONS 1-2R. DOUBLER WAS REPLACED IAW DWG 5710228-298, REV KT AND WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 21, 14.

Part: SKIN — DAMAGED (RUDDER) · airframe 61,722 hrs · 44,342 cycles

DAMAGE METALIZER ON BOTH SIDE RUDDER,VHS, SM, CARD 10, ZONE 65. METALIZER ON BOTH SIDE RUDDER WAS REPAIRED IAW SRM 51-70-1AD.

Part: TAB — DAMAGED (RT ELEVATOR) · airframe 61,722 hrs · 44,342 cycles

LIGHTNING STRIKE ON T/E AT RT ELEVATOR CONTROL TAB BETWEEN BS XET=26.178 TO XET=46.293, VHS, SM, CARD 24, ZONE 060. RT ELEVATOR CONTROL TAB WAS REPLACED IAW SRM 55-04 AND WILL BE INSTALLED UNDER CARD 2730-4832, JOB 001-0233.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 61,722 hrs · 44,342 cycles

CRACKED INNER PANE BETWEEN BEAM 5 AND AFT EDGE AT AFT CARGO COMPARTMENT DOOR, INNER PANE BETWEEN BEAM 5 AND AFT EDGE AT AFT CARGO COMPARTMENT DOOR, C3 WAS REPAIRED IAW SRM 52-03D, FIG 8 CRACK LENGTH, 1".

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 2301C. FUEL ACCESS 2301C WAS REPLACED IAW SRM 51-22-2A.

Part: CABLE — CORRODED (TAILCONE) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

RUSTED TAIL CONE CONTROL CABLE NR 547, AT BS 1510. RUSTED TAIL CONE MECHANIC CONTROL CABLE NR 547, AT BS 1510 WAS REMOVED IAW AMM 20-10-17 AND NEW CONTROL CABLE PN 3913359-547 WAS INSTALLED IAW AMM 20-30-01 AND WILL BE ADJUSTED UNDER CARD 5350-01077-0101.

Part: CUSP WEB — CORRODED (BS 1235-1238) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 1235 - 1238, X 54-60 AT PAX CABIN. CUSP WEB WAS REPAIRED IAW SRM 51-30-1, SRM 51-30-5, SRM 53-05 FIG 131A-6, SRM 51-10-3 PAR 14 & 21, SRM 51-30-2.

Part: SKIN — DENTED (CARGO DOOR) · airframe 61,722 hrs · 44,342 cycles

DENTS ON OUTER SKIN AT AFT CARGO COMPARTMENT DOOR. DENT WERE MEASURED IAW ERA 541545-14, REV ORIGINAL HFEC INSPECTION WAS ACCPOMPLISHED, NO CRACKS WERE FOUND IAW ERA 541545-14, REV ORIGINAL.

Part: PAN — CRACKED (CARGO DOOR) · airframe 61,722 hrs · 44,342 cycles

CRACKED INNER PAN BELOW STOP FITTING NR 2 AT MID CARGO COMPARTMENT DOOR. DAMAGE INNER PAN BELOW STOP FITTING WAS REWORKED AND MEASURED TRIM TO REMOVE DAMAGE: 0.236" LONG, IT IS WITHIN LIMITS IAW SRM 52-03D, FIG 10.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 61,722 hrs · 44,342 cycles

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

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 61,722 hrs · 44,342 cycles

CRACKED STOP FITTING NR 2 AND 5 AT MID CARGO COMPARTMENT DOOR FWD EDGE. CRACK STOP FITTING NR 2 AND 5 WERE REMOVED IAW SRM 51-30-2 AND 51-30-5, NEW FITTINGS WERE DRILLED, TREATED AND PAINTED IAW 51-10-4, 51-10-3, PAR 14 AND 21. NEW STOP FITTINGS WERE INSTALLED IAW SRM 51-30-1 AND 51-30-5.

Part: GUSSET — CORRODED (BS 1211-1219) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION ON GUSSET BETWEEN BS 1211-1219, LONGERONS 30-26R AT AFT CARGO COMPARTMENT. GUSSET WAS REPLACED IAW SRM 51-10-3, PAR 14, 21, 38, SRM 51-30-2, SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 524-552) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION OUT OF LIMITS ON LT CUSP WEB BS 524-536 AND 552 AT PAX CABIN. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14, SRM 51-10-3, PAR 21 AND 14, SRM 51-30-2 AND 51-30-5 AND CIC WILL BE APPLIED WITH NRC 20000088777 CARD 17, ZONE 201.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PANEL 1462C. FUEL ACCESS PANEL WAS REPLACED IAW SRM 51-22-2 AND IPC 57-30-00.

Part: CUSP WEB — CRACKED (BS 1122-1138) · airframe 61,722 hrs · 44,342 cycles

CRACKED WEB ON RT CUSP WEB BETWEEN BS Y=1122-1138 AND X=-54 TO X=-60. CRACK ON WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-6, SRM 51-10-3, PAR 21 AND 14 AND SRM 51-30-2 AND 51-30-5.

Part: BOLT — DAMAGED (ENGINE MOUNT) · airframe 61,722 hrs · 44,342 cycles

SCRATCHES OF LT UPPER ENGINE MOUNT BOLT. LT UPPER ENGINE MOUT BOLT WAS REPLACED IAW AMM 71-20-03.

Part: BOLT — DAMAGED (ENGINE MOUNT) · airframe 61,722 hrs · 44,342 cycles

SCRATCHES AT RT UPPER ENGINE MOUNT BOLT. RT UPPER ENGINE MOUNT BOLT WAS REPLACED IAW AMM 71-20-03.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 61,722 hrs · 44,342 cycles

CRACKED INTERCOSTAL ON FWD ENTRANCE DOOR BETWEEN BEAM 4 AND 5. INTERCOSTAL WAS REPLACED IAW SRM 51-30-2.

Part: FAIRING — DAMAGED (RUDDER) · airframe 61,722 hrs · 44,342 cycles

DAMAGED METALIZER ON RUDDER FAIRINGS NR 6502G AND 6508G. METALLIZED ON RUDDER FAIRINGS NR 6502G AND 6508G WERE REPAIRED IAW SRM 51-70-1A, PAR 23.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1464C. ACCESS PANEL WAS FOUND OUT OF LIMITS IAW SRM 51-22-2A ACCESS WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390, JOB 001-0454.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

ACCESS PANEL 1456C WAS FOUND CORRODED OUT OD LIMITS IAW SRM 51-22-2A. ACCESS PANEL WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390, JOB 001-0454.

Part: SKIN — DENTED (LT ELEVATOR TAB) · airframe 61,722 hrs · 44,342 cycles

SEVERAL DENTS ON UPPER SKIN AT LT ELEVATOR ANTI-FLOAT TAB BETWEEN XEFT=167 TO XEFT =173. UPPER SKIN AT LT ELEVATOR ANTI-FLOAT TAB BETWEEN XEFT=167 TO XEFT=173 WAS REPAIRED IAW SRM 55-04, PAR 2.

Part: LONGERON — CRACKED (BS 1380) · airframe 61,722 hrs · 44,342 cycles

CRACK LONGERON 8R AT FRAME 1380, A/A, SM. CARD 07, ZONE 61. LONGERON WAS REPAIRED IAW SRM 51-30-5, 51-30-2, 53-02 FIG 18, 51-10-4, 51-10-3, PAR 14 AND 21. UT WAS ACCOMPLISHED WITH NDT, SPM 06-10-01-001. EQUIPMENT PANAMETRICS MENTOR, GD-974, EXP 25-MAR-16. RII COMPLETED.

Part: CUSP WEB — CORRODED (BS 1035-1039) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION ON LT CUSP WEB BELOW PREVIOUS REPAIR BETWEEN BS 1035-1039 AT PAX CABIN. CFS, SM, CARD 82, ZONE 201. PREVIOUS REPAIR WAS REPLACED IAW SRM 51-30-2, 51-30-5, 53-03, FIG 131, A-13, 51-10-3, PAR 14 AND 21.

Part: CUSP WEB — CRACKED (BS 218) · airframe 61,722 hrs · 44,342 cycles

CRACK ON RT CUSP WEB BS 218 X=-54 RT. CUSP WEB WAS REPLACED IAW SRM 51-30-2, 51-10-4, 51-10-3 PAR 14 AND 21, 51-30-2, AND 51-30-1.

Part: CUSP WEB — CORRODED (BS 1203-1212) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 1203-1212 AND X=54 TO 60 AT PAX CABIN. CFS, SM. CARD 73, ZONE 201. CUSP WEB WAS REPAIRED IAW SRM 51-30-2, 53-05, FIG 131A-6, 51-10-3 PAR 14 AND 21.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1363C. FUEL ACCESS 1363C WAS REPLACED IAW SRM 51-22-22.

Part: CUSP WEB — CRACKED (BS 803) · airframe 61,722 hrs · 44,342 cycles

CRACK ON LT CUSP WEB BS 803 AND X 55 AT PAX CABIN. CRACK WAS REPAIRED IAW SRM 53-05, FIG 131A-1, SRM 51-10-3, PAR 21 AND 14, AND SRM 51-30-2, AND 51-30-5.

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION ON FLOOR PANEL 160G. THE FLOOR PANEL WAS FABRICATED, TREATED, AND PAINTED IAW DWG 9957828-11 AND 21 AND SRM 51-10-3, PAR 14, 21.

Part: PAN — CRACKED (CARGO DOOR) · airframe 61,722 hrs · 44,342 cycles

CRACKED INNER PAN BELOW STOP FITTINGS NR 3 AND 4 AT AFT CARGO COMPARTMENT DOOR AFT EDGE, AREA WAS REWORKED AND FOUND WITHIN LIMITS IAW SRM 52-03D, FIG 10.

Part: CUSP WEB — CORRODED (BS 585-750) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION ON LT CUSP WEB PREVIOUS REPAIR, BETWEEN L=54-X=60 AND BETWEEN BS 585-591, 674-693, AND 731-750. SM MRB 53-037-02, CARD 64, ZONE 201. BS 674-693 WAS ATTENDED WITH CARD NR 65 AND BS 585-591 AND 731-750 WERE REPAIRED IAW SRM 53-05, FIG 131A-6.

Part: ANGLE — CRACKED (BS 1451 FRAME) · airframe 61,722 hrs · 44,342 cycles

CRACK CLIP AND FRAME CLIP ON FRAME BS 1451 BETWEEN LONGERON 2-3L. CLIP AND FRAME CLIP WERE REPLACED IAW DWG 9911860-17 AND 21.

Part: CUSP WEB — PUNCTURED (BS 452) · airframe 61,722 hrs · 44,342 cycles

PUNCTURE ON LT CUSP WEB BS 452 AND X 53 AT PAX CABIN. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-1.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1436C. CORROSION ON SETTLEMENT AND COUNTERSINK HOLES WERE REMOVED IAW SRM 51-22-2A, COUNTERSINK HOLES WERE MEASURED AND MAX DIAMETER ALLOWABLE IS .660" AND MAX DIAMETER MEASSURED IS .680" IN, 3 ADJACENT HOLES THEREFORE OUT OF LIMITS IAW SRM 51-22-2A AND FUEL ACCESS WAS REPLACED IAW SRM 51-22-2A AND WILL BE INSTALLED UNDER CARD 2800-0390, ACFT 0992, JOB 001-0454.

Part: PAN — CRACKED (CARGO DOOR) · airframe 61,722 hrs · 44,342 cycles

CRACKED INNER PAN BETWEEN BEAM NR 5 AND FWD CARGO EDGE AT MID CARGO COMPARTMENT DOOR, C2, SM. CRACKED INNER PAN WAS STOPPED IAW SRM 51-01, PAR 21. CRACKED LONGERON .755", NEW DOUBLER WAS FABRICATED IAW SRM 52-03D NEW DOUBLER WAS PAINTED AND INSTALLED IAW SRM 51-10-3, PAR 14 AND 21, 51-30-2 AND 51-30-4.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL PANEL 1357C. CORROSION AT SETTLEMENT AREA AND COUNTERSINK HOLES WERE REMOVED IAW SRM 51-22-2. COUNTERSINK HOLES WERE MEASURED MAX DIAMETER ALLOWABLE IS 0.532" AND MAX DIAMETER MEASURED IS .610" IN 3 ADJACENT HOLES THEREFORE ACCESS PANEL WAS FOUND OUT OF LIMITS IAW SRM 51-22-2. ACCESS PANEL WAS REPLACED PN WAS VERIFIED IAW IPC 57-30-00-05B, AND WILL BE INSTALLED UNDER JIC 2800-0120.

Part: BRACKET — WORN (HORIZONTAL STAB) · airframe 61,722 hrs · 44,342 cycles

WORN RT/ LT ROLLER BRACKET AT HORIZONTAL STABILIZER, VHS. RIGHT, LEFT ROLLER BRACKETS AT HORIZONTAL STABILIZER WERE REPLACED IAW AMM 55-10-00-501 AND WILL BE INSTALLED AND ADJUSTED UNDER CARD 5510-4135, ACFT 992, JOB 000-0002, TORQUE USED QD2R1000, DUE DATE 20-AUG-16.

Part: LONGERON — CRACKED (BS 1437) · airframe 61,722 hrs · 44,342 cycles

CRACK LONGERON 16L AT BS 1437. SECTION OF THE LONGERON WAS REPLACED IAW SRM 51-30-2, 51-30-5, 53-14-4, 51-10-4, AND 51-10-3.

Part: CUSP WEB — CRACKED (BS 1024) · airframe 61,722 hrs · 44,342 cycles

CRACK ON RT CUSP WEB BS 1024 BETWEEN X -55 TO X -60 AT PAX CABIN. REPAIRED IAW SRM 53-05, FIG 131A-17, 51-30-2 AND 51-10-3 PAR 14 AND 21.

Part: LONGERON — CRACKED (BS 1380) · airframe 61,722 hrs · 44,342 cycles

CRACKED LONGERON 11R AT BS 1380. THE LONGERON WAS REPLACED IAW SRM 51-30-2, 51-30-05, 51-10-3, PAR 14 AND 21.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1476C. CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1476C WERE REMOVED IAW SRM 51-22-2A, COUNTERSINK WERE MEASSURED MAXIMUM DIAMETER ALLOWABLE IS 0.532" AND WERE FOUND 3 ADJACENT COUNTERSINK OUT OF LIMITS. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A. MAXIMUM DIAMETER OF OUT LIMITS 0.538".

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 61,722 hrs · 44,342 cycles

CRACKED FWD LINER SUPPORT ON FWD ENTRANCE DOOR UPPER EDGE, SM. SUPPORT ON FWD ENTRANCE DOOR UPPER EDGE WAS REPLACED IAW DWG 5901804, REV CF AND 51-30-2, SRM 51-10-3, PAR PAR 14, 21, LENGTH CRACK 0.150".

Part: ACCESS PANEL — CORRODED (WING) · airframe 64,032 hrs · 45,965 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF WING ACCESS PANEL 1365C. FOUND 6 ADJACENT COUNTERSINKS OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED.

Part: FRAME — CRACKED (BS 1380) · airframe 61,722 hrs · 44,342 cycles

CRACK FRAME CLIP BS 1380 BETWEEN LONGERON 13L -14L. FRAME CLIP WAS REPLACED IAW SRM 51-30-2, 51-30-5, 53-14-4, FIG 1, .500" LONGITUDE CRACK.

Part: PAN — CRACKED (SERVICE DOOR) · airframe 61,722 hrs · 44,342 cycles

CRACK ON FWD SERVICE DOOR PAN NEXT TO BEAM NR 4 FWD EDGE, SM. FWD SERVICE DOOR PAN NEXT TO BEAM NR 4 WAS REPAIRED IAW SRM 52-03, FIG 3.

Part: LONGERON — CRACKED (BS 1437) · airframe 61,722 hrs · 44,342 cycles

CRACKED LONGERON 16R AT BS 1437. SECTION OF THE LONGERON WAS REPLACED IAW SRM 51-30-5, 53-14-4, 51-10-4, AND 51-10-3.

Part: EYEBOLT — DAMAGED (RT AILERON) · airframe 61,722 hrs · 44,342 cycles

DAMAGE NR 2 HINGE EYEBOLT AT RT AILERON. EYEBOLT ON HINGE NR 2 AT RT AILERON WAS REPLACED IAW AMM 20-30-01. RII COMPLETED BY INSPECTION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,722 hrs · 44,342 cycles

CRACKED FWD/AFT CLIPS OF UPPER CHANNEL AT RT FWD OVERWING EMERGENCY EXIT DOOR, ST-SM. FWD/AFT CLIPS AT RT FWD EMERGENCY EXIT DOOR WERE REPLACED IAW SRM 51-30-2.

Part: BUSHING — DAMAGED (LT ELEVATOR) · airframe 61,722 hrs · 44,342 cycles

SCRATCHES ON BUSHING OF HINGE ATTACH POINTS NR 2, 3, AND 4 AT LT ELEVATOR. VHS, AYP. BUSHING OF HINGE ATTACH POINTS NR 2, 3, AND 4 AT LT ELEVATOR WERE REMOVED IAW CMM 27-30-1, NEW BUSHING OF HINGE ATTACH POINTS 2 AND 4 WERE INSTALLED IAW CMM 27-30-1. BORE HINGE 3 WAS FOUND OUT OF LIMITS AND A NEW BUSHINGS IN BORE HINGE 3 WILL BE ATTENDED UNDERCARD 38 AC ZONE 30, RII COMPLETED BY INSPECTION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,722 hrs · 44,342 cycles

CRACKED AFT CLIP OF UPPER CHANNEL AT LT FWD OVERWING EMERGENCY EXIT DOOR. CFS, SM. CLIP WAS REPLACED IAW SRM 51-30-2, 51-30-5, AND DWG: 9957735, REV G.

Part: BUSHING — DAMAGED (RT ELEVATOR) · airframe 61,722 hrs · 44,342 cycles

SCRATCHES ON BUSHINGS OF HINGE ATTACH POINT NR 2, 3, 4, AND 6 AT RT ELEVATOR. VHS, AYP. BUSHINGS OF HINGE ATTACH POINST NR 2, 3, 4, AND 6 AT RT ELEVATOR WERE REPLACE IAW CAM 27-30-1, RII COMPLETED BY INSPECTION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,722 hrs · 44,342 cycles

CRACKED FORWARD AFT CLIP OF UPPER CHANNEL AT RT AFT OVERWING EMERGENCY EXIT DOOR, ST-SM. FDW/AFT CLIPS AT RT AFT EMERGENCY EXIT DOOR WERE REPLACED IAW SRM 51-30-2.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION ON AFT CARGO COMPARTMENT LOWER DOOR JAMB BEAM REPAIR, SM. SPACER WAS REPLACED IAW SRM 53-05, FIG 123, 51-30-5, AND 51-10-3, RII COMPLETED BY INSPECTION.

Part: PAN — CRACKED (CARGO DOOR) · airframe 61,722 hrs · 44,342 cycles

CRACKED INNER PAN, BELOW STOP FITTING, NR 1 AFT EDGE AT FWD CARGO COMPARTMENT DOOR. IN REF ORNRC CARD 120 ZONE 100, 20000089334, C1, SM. CRACK ON INNER PAN BELOW STOP FIRING NR 1 WAS REMOVED IAW SRM 53-03 D, FIG 10, CRACK LONGERON .400", HFEC WAS PERFORMED AND CRACKS WERE NOT FOUND ON TRIMMED AREA IAW NDT SPM 06-10-01.001.

Part: HOUSING — WORN (DOOR HANDLE) · airframe 61,722 hrs · 44,342 cycles

WORN INNER HANDLE HOUSING AT FWD CARGO COMPARTMENT DOOR, C1, SM. HANDLE HOUSING DAMAGE WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: CUSP WEB — CRACKED (BS 868-906) · airframe 61,722 hrs · 44,342 cycles

CRACK ON LT CUSP WEB BETWEEN X=54 TO X=60, BS Y=868, Y=885, AND Y=906 ON REF CARD 76 AC ZONE 201. REPAIRED CUSP WEB LT BETWEEN X=54 TO X=60 ON BS Y=686; Y=885 AND Y=906 IAW SRM 53-05, FIG 131A-4 AND FIG 131A-10, SRM 51-30-2.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1307 C. CORROSION ON FUEL ACCESS PLATE 1307C WAS REMOVED IAW SRM 51-22-2, COUNTERSINK HOLES WERE MEASSURED AND MAXIMUN DIAMETER ALLOWABLE IS .660" IN AND MAXIMUN DIAMETER MEASURED IS .677" , 3 HOLES ADJACENT AT WERE FOUND OUT OF LIMITS IAW SRM 51-22-2 AND ACCESS PLATE WAS REPLACED IAW IPC 57-30-00-31A AND WILL BE INSTALLED UNDER CARD 2800-0120, JOB 001-0448.

Part: SEAT TRACK — CORRODED (BS 516-517) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION OUT OF LIMITS ON LT SEAT TRACK X 54 BETWEEN BS 516 AND 517. AREA WAS REPAIRED IAW SRM 53-05, FIG 4A.

Part: VANE — WORN (RT WING TE FLAP) · airframe 61,722 hrs · 44,342 cycles

WORN INBD AFT CORNER AT RT WING OTBD FLAP, OTBD GUIDE VANE. INBD AFT CORNER AT RT WING OTBD FLAP, OTBD GUIDE VANE WAS REPAIRED IAW ER/A 492663-14MA, REV ORG.

Part: ACCESS PANEL — CORRODED (WING) · airframe 64,032 hrs · 45,965 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF WING ACCESS PANEL 1373C. FOUND OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1460C. CORROSION ON SETTLEMENT AND COUNTERSINK AREAS WERE REMOVED IAW SRM 51-22-2 AND COUNTERSINK HOLES WERE MEASURED AND MAX DIAMETER ALLOWABLE .537" AND MAX DIAMETER MEASURED IS .580" IN 3 ADJACENT HOLES. THEREFORE, OUT OF LIMITS IAW SRM 51-22-2 AND FUEL ACCESS WERE REPLACED IAW IPC 57-30-00 AND MAGNETIC PROBE WAS INSTALLED IN NEW FUEL ACCESS IAW AMM 28-40-02.

Part: CUSP WEB — CRACKED (BS 1031) · airframe 61,722 hrs · 44,342 cycles

CRACK ON RT CUSP WEB BS 1031 X -45 RT CUSP WEB REPAIR IAW SRM 53-05, FIG 131A-19.

Part: LONGERON — CRACKED (BS 1437) · airframe 61,722 hrs · 44,342 cycles

CRACK LONGERON 12L AT BS 1437. SECTION LONGERON 12L WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. SECTION LONGERON 12L WAS REPLACED AND INSTALLED IAW DWG 5911433-13, REV BS AND SRM 51-30-2, 51-30-5.

Part: LONGERON — CRACKED (BS 1307) · airframe 61,722 hrs · 44,342 cycles

CRACKED LONGERON 8 LT, BS 1307 AT PAX CABIN. SECTION LONGERON DAMAGE WAS REMOVED AND NEW SECTION LONGERON WAS DRILLED, ADJUSTED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-3, PAR 14/21 AND 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 522) · airframe 61,722 hrs · 44,342 cycles

CRACKED LONGERON 4L BS 522. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANELS 1355C. ACCESS PLATE WAS REPLACED.

Part: BEAM — CRACKED (PAX DOOR) · airframe 61,722 hrs · 44,342 cycles

CRACKED BEAM NR 1 AFT EDGE ON FWD ENTRANCE DOOR. CRACK WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 51-30-1, 51-10-3 PAR 14/21, 51-10-2 AND 52-05D, FIG 81, SHEET 3.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION ON LT FUEL TANK ACCESS PLATE 1303C. FUEL ACCESS 1303C WAS REPLACED IAW SRM 51-22-2 AND WILL BE INSTALLED UNDER CARD 2800-0120, JOB 001-0448.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 61,722 hrs · 44,342 cycles

CORROSION AT COUNTERSINK AREAS OF FUEL ACCESS PANEL 2302C. ACCESS PLATE 2302C WAS REPLACED

Part: LONGERON — CRACKED (BS 984) · airframe 61,722 hrs · 44,342 cycles

CRACKED LONGERON 4 LT, BS 984. CRACKED LONGERON WAS REMOVED, NEW SECTION LONG AND SPLICES WERE ADJUSTED, DRILLED, TREATED, PAINTED AND INSTALLED SRM 53-02, FIG 18; 51-10-3, 51-10-4.

Part: PAN — CRACKED (BS 712-731) · airframe 61,722 hrs · 44,342 cycles

CRACK AFT UPPER CORNER RING PAN BETWEEN BS 712 TO 731 RT SIDE, FCS, SM. AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-30-5, 51-30-2, 51-10-3 PAR 14 AND 21, ER/A'S 487747-14MA, REV A, 493648-14, MA REV A.

Part: LONGERON — CRACKED (BS 522) · airframe 61,722 hrs · 44,342 cycles

CRACKED LONGERON 4R BS 522 AT CPAX. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-30-2, 51-30-5, AND51-10-3 PAR 14 & 21.

Part: PAN — CRACKED (BS 769-788) · airframe 61,722 hrs · 44,342 cycles

CRACKED LT RING PAN AFT LOWER CORNERS BETWEEN BS Y=769-788 AT PAX CABIN. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122, 51-10-3, PAR 14, 21, 51-30-2, 51-30-5 ER/AS 487747-14MA, REV A, 493648-14MA, REV A .

Part: PAN — CRACKED (BS 503-522) · airframe 61,722 hrs · 44,342 cycles

CRACK FWD UPPER CORNER RING PAN BETWEEN BS 503 TO 522 RT SIDE. AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5, 51-10-3, PAR 14 & 21 AND ER/AS 487747-14MA REV A,AND 493648-14MA, REV A.

Part: PAN — CRACKED (BS 1231-1250) · airframe 61,722 hrs · 44,342 cycles

CRACK AFT UPPER CORNER RING PAN BETWEEN BS Y=1231 TO Y=1250 LT SIDE. RING PAN AND SHIM WERE REPLACED IAW SRM 51-30-2, 51-30-5, SRM 51-30-3, PAR 14 AND 21, ER/A'S 493648-14MA, REV A AND 487747-14 MA, REV. A.

Part: PAN — CRACKED (BS 845-1041) · airframe 61,722 hrs · 44,342 cycles

CRACKED LT RING PAN FWD LOWER CORNER BETWEEN BS Y=845-864, 946-965, 1022-1041 AT PAX CABIN. RING PAN WERE REPAIRED IAW SRM 51-30-2, 51-30-3, 53-05, FIG 122, SRM 51-10-4, 51-10 -3 PAR 14 AND 21 AND ER/A'S 493648-14MA REV A AND 487747-14MA REV A.

Part: PAN — CRACKED (BS 1022-1041) · airframe 61,722 hrs · 44,342 cycles

CRACK AFT UPPER CORNER RING PAN BETWEEN BS 1022 TO 1041 RT SIDE. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122 AND 51-10-3 PAR 14 AND 21 AND ER/A'S 487747-14MA, 493648-14MA.

Part: PAN — CRACKED (BS 886-905) · airframe 61,722 hrs · 44,342 cycles

CRACK AFT LOWER CORNER RING PAN BETWEEN BS 886 TO 905 RT SIDE. AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5, 51-10-3, PAR 14 & 21 AND ER/AS 487747-14 MA, REV A, AND 493648-14 MA, REV A.

Part: PAN — CRACKED (BS 1136-1155) · airframe 61,722 hrs · 44,342 cycles

CRACK FWD LOWER CORNER RING PAN BETWEEN BS 1136 TO 1155 RT SIDE. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122 AND 51-10-3, PAR. 14 AND 21 AND ER/A 487747-14MA REV A, AND 493648-14MA, REV A.

Part: PAN — CRACKED (BS 237-256) · airframe 61,722 hrs · 44,342 cycles

CRACK FWD LOWER CORNER RING PAN BETWEEN BS 237 TO 256 RT SIDE. AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-10-3, PAR 14 AND 21, 51-30-5, 51-30-2 ER/AS 487747-14MA REV A AND 493648-14MA, REV. A.

Part: PAN — CRACKED (BS 807-826) · airframe 61,722 hrs · 44,342 cycles

CRACK FWD LOWER CORNER RING PAN BETWEEN BS 807 TO 826 RT SIDE. AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5, 51-10-3 PAR 14 AND 21 AND ER/AS 487747-14 MA, REV A AND 493648-14MA, REV A.

Part: PAN — CRACKED (BS 845-864) · airframe 61,722 hrs · 44,342 cycles

CRACK FWD LOWER CORNER RING PAN BETWEEN BS 845 TO 864 RT SIDE. AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-30-5, 51-30-2, 51-10-3, PAR 14 AND 21, ER/A 487747-14MA, REV A AND 493648-14 MA, REV A.

Part: PAN — CRACKED (BS 769-788) · airframe 61,722 hrs · 44,342 cycles

CRACK FWD UPPER CORNER RING PAN BETWEEN BS 769 TO 788 RT SIDE. AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5, 51-10-3 PAR 14 & 21 ER/AS 487747-14 MA REV A, 493648-14 MA REV A.

Part: TAB — CONTAMINATED (RT ELEVATOR) · airframe 61,722 hrs · 44,342 cycles

PRESENCE OF WATER WAS FOUND ON RT ELEVATOR ANTI-FLOAT TAB HONEYCOMB STRUCTURE. RT ANTI-FLOAT TAB WAS REMOVED WITH CARD AC 0992, CARD 2730-4830 AND REPLACE DUE TO PRESENCE OF WATER WITH REPAIRED RT ANTI-FLOAT TAB AND WILL BE INSTALLED WITH CARD 2730-4832.

Part: SKIN — DAMAGED (RT ELEVATOR TAB) · airframe 61,722 hrs · 44,342 cycles

DENTS ON UPPER SKIN AND NICK ON LOWER SKIN AT RT ELEVATOR GEARED TAB. RT GEARED TAB WAS REMOVED WITH CARD 2730-4830 AND WAS REPLACED DUE TO EXCEED THE ALLOWABLE REPAIRS IAW SRM 55-04, PAR 2 (4) AND REPAIRED RT GEARED TAB WILL BE INSTALLED WITH CARD 2730-4832.

Part: PAN — CRACKED (BS 446-1079) · airframe 61,722 hrs · 44,342 cycles

CRACKED LT RING PAN FWD UPPER CORNERS BETWEEN BS Y= 446-465, 655-674, 731-750, 1022-1041, 1060-1079 AT PAX CABIN. RING PAND WERE REPAIRED IAW SRM 51-30-2, 51-30-5 53-05, FIG 127 AND 51-10-3, PAR 14, 21 ERAS 487747-14MA REV A, 493648-14 MA, REV A.

Part: PAN — CRACKED (BS 788-807) · airframe 61,722 hrs · 44,342 cycles

CRACK FWD UPPER CORNER RING PAN BETWEEN BS 788 TO 807 RT SIDE. AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5, 51-10-3 PAR 14 & 21, ERAS 487747-14MA, REV A, 493648-14 MA, REV A.

Part: CUSP WEB — DAMAGED (BS 1218-1307) · airframe 61,722 hrs · 44,342 cycles

CUSP WEB BETWEEN BS 1218 - 1307 FOUND DAMAGED. CRACKS AND CORROSION REPAIRED IAW SRM 53-05 AND SRM 51-10-3, PAR 14, 21.

Part: SKIN — CRACKED (BS 1380) · airframe 62,529 hrs · 44,892 cycles

ER/A 529770-14 FUSELAGE, SKIN, BS 1380 AND L13R-L14R, CRACKED.

Part: DOOR FRAME — CRACKED (RT MLG) · airframe 61,392 hrs · 44,094 cycles

ACFT RT MLG DOOR JAM, HOCKEY STICK, CRACKED WITH REPAIR DOUBLER ALSO CRACKED. BEGIN REMOVING RT MLG DOOR JAM FRAME, 653188, COMPLETED REMOVAL OF RT MLG JAM IAW DWG 5930584, 413699, INSTALLED RT MLG DOOR JAM IAW DWG 590584.

Part: TAB — DAMAGED (LT ELEVATOR) · airframe 61,181 hrs · 43,932 cycles

FOUND LT ELEVATOR INBD TAB WITH LIGHTNING STRIKE AND DAMAGE TO T/E OF TRIM TAB OF MORE THAN 6". R & R LT ELEVATOR CONTROL TAB IAW AMDS CARD 2730-4634.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,653 hrs · 43,558 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY CEILING LIGHTS INOPERATIVE AT ROW 34. MAINTENANCE INSTALLED NEW BATTERIES AND THE OPS CHECKED GOOD.

Part: FITTING — NOT REPORTED (SLAT) · airframe 59,020 hrs · 42,451 cycles

SLAT DRIVE FITTING REPAIRED IAW AA 2700-01074.

Part: RELEASE CABLE — CORRODED (TAILCONE) · airframe 59,054 hrs · 42,473 cycles

DURING CHECK, MAINTENANCE FOUND THE TAIL CONE RELEASE CABLE CORRODED AND DAMAGED. MAINTENANCE REPLACED THE CABLE AND A FUNCTIONAL CHECK WAS PERFORMED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,054 hrs · 42,473 cycles

CORROSION AROUND AND IN AFT LAVATORY SERVICE PANEL. REPAIRED IAW PRI 529789-14, REV 0 AND ERA 529789-14, REV ORIGINAL AND PRI 529923-14, REV "0" AND ER/A 529923-14, REV ORIGINAL.

Part: STRINGER — DAMAGED · corrosion level 2 · airframe 59,054 hrs · 42,473 cycles

STRINGER DAMAGED. FABRICATED A REPAIR HAT CHANNEL AND REPAIR STRAP IAW PRI 529775-14.

Part: SLIDE BLOCK — WORN (TAILCONE RELEASE) · airframe 59,054 hrs · 42,473 cycles

DURING CHECK, MAINTENANCE FOUND THE UPPER LT SLIDING BLOCK FOR THE TAIL CONE RELEASE CABLE WAS WORN. MAINTENANCE REPLACED BOTH THE UPPER LT AND RT CABLE BLOCKS AND A FUNCTIONAL TEST WAS PERFORMED.

Part: DOUBLER — CORRODED (LAV SERVICE) · airframe 59,018 hrs · 42,450 cycles

FUSELAGE AFT LAV SERVICE DOOR SURROUND DOUBLER CORRODED, BS 1307 REPAIRED IAW ERA 529789-14.

Part: PAN — CORRODED (LAV SERVICE) · airframe 63,991 hrs · 45,935 cycles

AFT LAV SERVICE PAN CORRODED. REPLACED THE PAN.

Part: SKIN — CORRODED (BS 1285) · corrosion level 2 · airframe 59,045 hrs · 42,467 cycles

CORROSION AROUND OUTFLOW VALVE SCOOP. BS 1285. REMOVED SKIN CORROSION AND CHECKED LIMITS TO BE WITHIN IAW SRM 53-01, PG 5. R & R VENT SUPPORT PLATE IAW DWG 5936021.

Part: DOOR SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 59,037 hrs · 42,461 cycles

MID CARGO DOOR OPENING LOWER SILL HAS CORROSION. REPAIRED IAW SRM 53-05, FIG 123 AND DWG SR09520008.

Part: SKIN — CRACKED (BS 1379-1383) · airframe 59,037 hrs · 42,461 cycles

ACFT SKIN HAS FOUR CRACKS, ONE IS FOUR INCHES LONG THRU ADJACENT FASTENER HOLES IN LONGERON 14R BS 1379-1383, ANOTHER IS .2500 INCHES LONG AT BS 1380 AT A FASTENER HOLE .7500" ABOVE L14RT, ANOTHER IS .6250 INCHES LONG AT BS 1380 AT A FASTENER HOLE 1.5 ABOVE L14R & THE LAST IS .1250 INCH LONG AT BS 1380 AT A FASTENER HOLE 1.5 ABOVE L13R. COMPLIED WITH PRI 529770-14, REV 1 AND REPAIRED IAW ERA 529770-14.

Part: SUPPORT — CORRODED (BS 1287-1307) · corrosion level 2 · airframe 59,037 hrs · 42,461 cycles

VENT SUPPORT PLATE HAS CORROSION AT BS 1287-1307. REPAIRED IAW PRI 529794-14, REV 0 AND ERA 529794-14, REV ORIG.

Part: PIN — DAMAGED (L1 DOOR SLIDE) · airframe 58,416 hrs · 42,003 cycles

MAINTENANCE DISCOVERED THE L1 DOOR SLIDE CABLE PINS WERE MISSING THE SECURITY STRING. MAINTENANCE R & R THE L1 SLIDE.

Part: DUCT — BLOWN (NR 2 ANTI ICE) · airframe 58,343 hrs · 41,951 cycles

AIR RETURNED FOLLOWING A NR 2 ENGINE FIRE INDICATION. MAINTENANCE FOUND THAT THE NR 2 ENGINE ANTI-ICE DUCT WAS BLOWN OUT AND REPLACED THE DUCT. ALL CHECKED NORMAL AND THE ACFT HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,837 hrs · 41,623 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT ROWS 10-15 AND ROW 22 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECKED GOOD.

Part: FITTING — SHEARED (CONTROL VALVE) · airframe 57,750 hrs · 41,571 cycles

FLIGHT DIVERTED DUE TO RT HYDRAULIC SYS QUANTITY LOSS. CREW MANUALLY EXTENDED LANDING GEAR DUE TO ZERO HYD PRESSURE INDICATING DURING APPROACH. MAINTENANCE FOUND EVIDENCE OF HYD LEAKAGE IN RT WHEELWELL AND NOTED A FITTING SHEARED FROM THE DUAL BRAKE CONTROL VALVE HOUSING BODY. THE VALVE WAS REPLACED AND BOTH HYD SYSTEMS WERE SERVICED INCLUDING A FULL FUNCTIONAL CHECK OF BOTH HYD SYSTEMS FOR PROPER OPERATION. A DUAL ENGINE RUN, PNEUMATIC DUCT BURNOUT & HYD FILTER REPLACEMENTS WERE ALSO ACCOMPLISHED WITH NO ADDITIONAL FINDINGS. A CORRESPONDING LOG SHEET INDICATES THE ACFT EXPERIENCED A LOSS OF BRAKE ACTUATING FORCE WHILE THE ACFT WAS IN MOTION ON THE GROUND.

Part: JACKSCREW — NOT REPORTED (HORIZONTAL STAB) · airframe 59,197 hrs · 42,587 cycles

HORIZONTAL STABILIZER JACKSCREW REPAIRED IAW AA 2740-01113.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 57,069 hrs · 41,152 cycles

DURING LINE CHECK, NOTED THE SEAT EMERGENCY PATH LIGHTS INOPERATIVE AT ROW 27. FOUND WIRE PULLED FROM CONNECTOR. REPINNED IAW SWPM 20-31 AND OPS CHECKED NORMALLY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,578 hrs · 40,821 cycles

DURING LINE CHECK, COCKPIT, L1 & R1 OVERHEAD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. POWER PACK REPLACED AND OPS CHECKED NORMALLY IAW AMM 33-51.

Part: DOOR — NOT REPORTED (CARGO) · airframe 56,538 hrs · 40,792 cycles

CARGO DOOR REPAIRED IAW AA 5230-01159.

Part: CARGO TRACK — CORRODED (BS 1212-1217) · airframe 55,373 hrs · 39,990 cycles

DURING SCHEDULED MX, CORROSION WAS FOUND ON THE AFT CARGO BAY BS 1212-1217 RT TIE DOWN TRACK MRB 53-100-17. THE CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW SRM 53-01. INSTALLED NEW TRACK IAW SRM 51-30-1.

Part: SKIN — DENTED (BS 1303) · airframe 55,373 hrs · 39,990 cycles

DURING SCHEDULED MX, AN EXTERNAL SKIN DENT WITH GOUGE WAS DOCUMENTED AT BS 1303 1" ABOVE LONGERON 19R. EVAULATED SKIN DENT WITH GOUGE AT BS 1303 1" ABOVE LONGERON 19R. DENT MEASURED 1.7" X 2.2" X .053". AND IS OUT OF LIMITS IAW SRM 53-04-1. TRIMMED OUT DAMAGE AND ACCOMPLISHED REPAIR IAW SRM 53-04-2.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,157 hrs · 39,861 cycles

DURING CHECK, FOUND MULTIPLE EMERGENCY CEILING LIGHTS INOPERATIVE. REPLACED SEVERAL BATTERIES IN BATTERY PACKS. OPERATION CHECKED GOOD.

Part: FRAME — DAMAGED (FUSLEAGE) · airframe 54,293 hrs · 39,313 cycles

ON REMOVING NLG GUIDE AND STOP, FOUND CRACK ON LT FRAME FORWARD OF FORWARD DOOR HINGE AND AFT OF THE REMOVED GUIDE. REMOVED FASTENERS AND CUT OUT DAMAGED AREA. DURING DAMAGE CONTAINMENT FOUND MISDRILLED FASTENER HOLES ON WHEELWELL CUTOUT FRAME. REMOVED MISDRILLED AREA. FABRICATED PART, HEAT TREATED, TESTED CONDUCTIVITY, DRILLED UP FABRICATED FRAME, DOUBLER AND DOUBLER SPLICE. TREATED AND PRIMED. HFEC OF CUT LINE, NO CRACKS.

Part: SKIN — PUNCTURED (RT WING SLAT) · airframe 54,215 hrs · 39,262 cycles

L/E SKIN PUNCTURED AT CANT STATION 624. WING TIP ASSEMBLY NOT DAMAGED. MX R & R SUPPORT ASSEMBLY AND RIB AT RT WING IAW SRM 51-30-02 AND 51-20-00. SECURITY CHECKED GOOD. ACFT OK FOR SERVICE.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 53,532 hrs · 38,832 cycles

FUSELAGE SKIN L1 DOOR GUST LATCH CUTOUT. REPAIR OF SKIN EDGE DAMAGE REPAIRED IAW ERA 482628-14, LOG 0566314, T354299, T352719, T352467, T353270, T353597.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 52,967 hrs · 38,480 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND BROKEN WIRE AT SEAT 10D EMERGENCY PATHWAY LIGHT. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM. OPERATION CHECKED NORMAL.

Part: SPRING — MISSING (TAILCONE) · airframe 52,226 hrs · 38,006 cycles

THE TAIL CONE FAILED TO UNLOCK AND DROP DURING THE FUNCTIONAL CHECK OPN 6908. MAINTENANCE FOUND THE SPRING IN THE T-PIN PLUNGER WAS MISSING SO THEY INSTALLED A NEW SPRING, CLEANED, AND LUBRICATED THE CLIPS AT THE T-PIN PLUNGER. SYSTEM REQUIRES AN OPERATIONAL CHECK.

Part: SKIN — NOT REPORTED (HORIZONTAL STAB) · airframe 52,214 hrs · 38,000 cycles

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

Part: RIB — NOT REPORTED (HORIZONTAL STAB) · airframe 52,214 hrs · 38,000 cycles

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

Part: SPAR — CRACKED (WING) · airframe 51,993 hrs · 37,867 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,543 hrs · 37,583 cycles

DURING LINE CHECK, MAINTENANCE FOUND SEVERAL CEILING PANEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK AT ROW 17DE. OPERATION CHECKS GOOD. AIRCRAFT IS OKAY FOR SERVICE.

Part: HOUSING — NOT REPORTED (NLG) · airframe 50,864 hrs · 37,094 cycles

NLG HOUSING ASSY REPAIRED IAW ERA 493413-14.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 50,568 hrs · 36,911 cycles

DURING LINE CHECK, MX FOUND EMERGENCY PATHWAY LIGHTS ROWS 16-23 INOPERATIVE. MX FOUND LOOSE CONNECTOR. SECURED THE SAME. OPERATION CHECKS GOOD. ACFT IS OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,534 hrs · 36,891 cycles

DURING LINE CHECK, MX FOUND EMERGENCY PATHWAY LIGHTS INOPERATIVE FROM ROWS 16-23. MX RESET BATTERY PACKS. OPS CHECKS GOOD. ACFT IS OK FOR SERVICE.

Part: THERMAL SWITCH — ARCED (CTR WINDSHIELD) · airframe 48,134 hrs · 35,318 cycles

WINDSHIELD ANTI-FOG SWITCH TURNED ON DURING DESCENT AND ABOUT 5 MIN AFTER A WHITE SMOKE CAME FROM THE CTR WINDSHIELD SENSOR. THE ANTIFOG WAS TURNED OFF AND PROBLEM STOPPED. FOUND ARCING ON CTR WINDSHIELD THERMAL SWITCH. REPLACED SWITCH, S1-221 AND TERMINALS IAW AMM. HEATING ELEMENT ON CTR WINDSHIELD WITHIN AMM TOLERANCES. APPLICABLE PART OF OPN 5088 C/W. OK FOR SERVICE. CTR WINDSHIELD ANTI-FOG CHECKS IAW AMM.

Part: PAN — CRACKED (L1 DOOR) · airframe 47,446 hrs · 34,892 cycles

CRACKED FWD UPPER INNER PAN ON L1 DOOR. REPAIRED IAW DWG NR AMR 0952147 REV 2.

Part: SKIN — DENTED (WINDOW BELT) · airframe 47,444 hrs · 34,891 cycles

DENT ON FUS LT SIDE APPROX 8 INCHES BELOW WINDOW BELT, 3 INCHES IN LENGTH APPROX 39 INCHES AFT OF L1 CUTOUT. REPAIRED IAW SRM 53-04D.

Part: BEAM — CORRODED (CARGO DOOR FRAME) · airframe 47,444 hrs · 34,891 cycles

EXFOLIATION CORROSION ON AFT CARGO COMPARTMENT DOOR JAMB LOWER BEAM. REPAIR IAW SRM 53-05 FIG123.

Part: LIGHT — SMOKE (ROW 20 ABC) · airframe 45,300 hrs · 33,528 cycles

PASSENGER REPORTED SMOKE FROM READING LIGHTS IN ROW 20ABC SEATS. CREW ADVISED TO TURN LIGHTS OFF AND NO SMOKE WAS NOTED. PERFORMED OP 5088. OPENED PSU ON ROW 19 20 21 ABC INCLUDING OVERHEAD AND SIDEWALL LIGHT POWER SUPPLY. VISUALLY INSPECTED FOR SMOKE BURN OR ODOR. NO EVIDENCE NOTED. CK OK, CLOSED ALL PANELS.

Part: ENGINE — LEAKING (NR 2) · airframe 40,379 hrs · 30,468 cycles

NR 2 ENGINE IFSD DUE TO LOSS OF OIL QTY AND PRESSURE. REPLACED NR 2 ENGINE PER TRANS 9T102.

Part: GENERATOR — MALFUNCTIONED (NR 1 ENGINE) · airframe 40,223 hrs · 30,375 cycles

AT 1000 FT AGL BOTH ENG GENERATORS WERE PROVIDING INTERMIT POWER. BOTH SIDES PFD AND ND WERE FLASHING ON AND OFF WITH THE PWR CYLING. THIS WAS HAPPENING EVERY 1-2 SECS. CAPTS SIDE SWITCHED TO STBY PWR TO REGAIN INST. THE F/O SIDE CONTINUED TO FLICKER AFTER 30 SECS WHEN THE APU WAS UP AND RUNNING PLACED THE F/O SIDE ON APU GEN AFTER TRIPPING THE RT GEN MANUALLY. AFTER THAT WE DID THE CAPTS SIDE AND IT ALL WORKED FINE. WE HAD NO AC CROSS-TIE LOCK OUT DID NOT NOTICE FREQS OR VOLTS AT THE TIME.REPLACED RT GENERATOR AND CSD PER AMM OPS CKS OK.

Part: SWITCH — SPARKS (COCKPIT PEDESTAL) · airframe 39,106 hrs · 29,671 cycles

DURING FLIGHT CREW PREFLIGHT WHILE OPERATING THE ALTERNATE STABILIZER TRIM SWITCHES, A POP AND A FLASH OCCURRED WITH A SMALL FIRE BELOW TRIM SWITCHES UNDER PEDESTAL, FIRST OFFICER BLEW FIRE OUT. C/B D-10 POPPED. REPLACED ALTERNATE TRIM BRAKE RELEASE SWITCH S10-8. FOUND THAT SWITCH SPARKED IGNITING DUST IN PEDESTAL. NO DAMAGE RESULTED DUE TO SMALL FIRE.

Part: ACTUATOR — INTERMITTENT (VERT STAB) · airframe 38,661 hrs · 29,393 cycles

LOST PRIMARY TRIM CONTROL USING THUMB SWITCHES ON PILOTS CONTROL WHEEL DURING APPROACH. EXECUTED MISSED APPROACH AND FLEW APROX 5 MIN WHEN PRIM TRIM CONTROL RETURNED TO PILOTS CONTROL WHEELS. CHECKED BOTH CONTROL WHEEL SWITCHES AT ALL TIMES. REPLACED PRIMARY AND ALTERNATE LONGITUDINAL TRIM ACTUATORS PER M/M. OPS CK PRIMARY AND ALT OK PER M/M. NOT AN RII ITEM.

Part: TRANSMITTER — FAILED (NR 1 ENGINE) · airframe 32,771 hrs · 25,357 cycles

UPON T/O LEFT EPR HUNG AT 1.6 WITH RAPIDLY RISING EGT, ABORTED AT 30 KNOTS. REPLACED EPR TRANSMITTER.

Part: WIRE — BURNED (E/E COMPARTMENT) · airframe 29,205 hrs · 22,848 cycles

WIRE BUNDLE AT STATION 110 PANEL, FORWARD AND BELOW THE COCKPIT TEMP CONTROLLER, SHORTED AND CAUGHT FIRE, WHILE REMOVING CONTROLLER. CA REPAIRED DAMAGED WIRE.

Part: ODOR — DETECTED (CABIN) · airframe 26,373 hrs · 20,730 cycles

DURING DESCENT AT 2500 FT SMELLED STRONG ELECTRICAL BURNING ODOR. CONFIRMED BY F/A IN AFT OF A/C. TURNED OFF GALLEY PWR AS PRECAUTION AND SMELL DISSIPATED. MTC INSPD TAIL COMPRT-BAG BINS-CBN-POWERED ALL GALLEY EQUIP AND INSPD CB PNL BEHIND CAPT SEAT AND E/E COMPT AND ALL WAS NORMAL, NO ELECTRICAL ODOR DETECTED. RAN ENGS AND APU PNEUS FOR AIR COND OPRN NO ODOR DETECTED.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 25,516 hrs · 20,088 cycles

ON CLIMBOUT AT APPROX 23K FEET, LEFT OIL STRAINER CLOG MESSAGE ILLUMINATED. REDUCED THROTTLE AND MESSAGE REMAINED ILLUMINATED. IAW POM SHUT DOWN ENGINE. REPLACED ENGINE FOR INTERNAL FAILURE.

Part: UNKNOWN — ODOR (LAVATORY & CABIN) · airframe 25,349 hrs · 19,953 cycles

CAPT SIDE AFT LAV SMOKE ALARM WENT OFF IN FLIGHT. LAV INSPECTED, TRASH BIN REMOVED AND REPLACED, NO EVIDENCE OF SMOKE AFTER LANDING. A PAX ROW 29 REPORTED A BURNING ODOR COMING FROM LAV AREA. INSPECTED LAV AND GALLEY AREAS, NO TROUBLE FOUND.

Part: APU — CONTAMINATED · airframe 24,646 hrs · 19,431 cycles

AFTER TAKE OFF, SMELLED AN ODOR SIMILAR TO AN ELECTRICAL FIRE IN THE COCKPIT AND CABIN. THE LT AFT LAV FIRE DETECTOR WENT OFF. NO FIRE EVIDENCE WAS FOUND. USED FLASHLIGHT TO MAKE THOROUGH SEARCH OF LAV. SUSPECT AIR CONDITIONING. FOUND 2 B-NUTS ON IB OF LT IB FLAP LOOSE AND 2 B-NUTS ON UPLOCK LOOSE, TIGHTENED SAME. PERFORMED DUCT BURN-OUT REPLACED APU AND CLEANED INLET ON ITEM NO.3 REPLACED WATER BAGS ON OPN 5088.

Part: GENERATOR — FAILED (APU)

APU GENERATOR FAILED IN FLIGHT AND WOULD NOT RESET. LT GENERATOR ON PREVIOUS DEFERRAL. REPLACED APU GCU.

Part: SCHRADER VLV — FAILED (NLG STRUT)

AFTER GEAR RETRACTION THE RED LIGHT IN NOSE GEAR REMAINED ILLUMINATED WITH VIBRATIONS FROM GEAR DOOR. RECYCLED GEAR IAW CHECKLIST WITH NO EFFECT. GEAR LOWERED NORMALLY FOR LANDING. FOUND NOSE GEAR STRUT FLAT AND SCHRADER VALVE LEAKING. REPLACED SCHRADER VALVE AND SERVICED NOSE STRUT PER MM 32-21-02 CONFIG 2. LEAK CHECK OK.

Part: AIR DISTRIBUTION — HAZE (CABIN)

CLIMBING THRU 18,000, RT AFT LAV SMOKE DET WENT OFF. HAZE NOTED IN AFT CABIN AREA, SMOKE DISSAPATED AFTER 10 MINS, DURING RETURN TO TPA. CHECKED ENGINES APU AND PACKS, NO TROUBLE FOUND.

Part: ANTI-ICE SENSOR — FAILED (LT WINDSHIELD)

PILOTS W/S A/I SNSR BEGAN SMOKING. TURNED OFF W/S A/I AND SMOKE ABATED. T/S IN PROGRESS, REPOSITIONED WIRE BUNDLE, CKD ALL LUGS, WIRES, TERMINALS. PHENOLIC ON WINDOW SMELLS OF SMOKE. NO APPARENT BLUEING, SCORCH, CHAR OR BURN MARKS. REPLACED WINDOW AS PRECAUTION.

Part: FUEL NOZZLE — LOOSE (NR 2 ENGINE)

ENGINE WAS REMOVED FOR 7TH STAGE COMPRESSOR BLADES DAMAGED BEYOND LIMITS. ENGINE WAS DISASSEMBLED IN ENGINE SHOP AND NR 3 FUEL NOZZLE WAS FOUND TO HAVE DAMAGE. FUEL NOZZLE SCOOP BECAME LOOSE, ROTATED AND CUT INTO FUEL NOZZLE SUPPORT CAUSING FUEL NOZZLE TO LEAK. FUEL NOZZLE SCOOP CAME OFF AND BECAME LODGED IN NR 2 BURNER CAN. FINDINGS HAVE BEEN REPORTED TO THE LOCAL PRATT AND WHITNEY OFFICE.

Part: ANGLE — CRACKED (RT ENG PYLON)

FOUND DURING D-1 LETTER CHECK - .25 INCH CRACK IN RT UPPER ENG PYLON TO FUSELAGE ANGLE 12 INCHES FROM AFTM EDGE. REPAIRED PER SRM 54-04A PG17 FIG 4.