N960DL

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,121 hrs · 57,081 cycles

FWD GALLEY EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN FWD BATTERY CHARGER. CKS GOOD REF MD88 AMM 33-53. (LP5487110)

Part: BATTERY — MISSING (SMOKE DETECTOR) · airframe 76,085 hrs · 57,047 cycles

LAVATORY SMOKE DETECTOR BATTERY MISSING. R/R LACATORY SMOKE DETECTOR BATTERY IN LAV 203 OK FOR SVC. (LP1348156)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,917 hrs · 56,899 cycles

CEILING EMERGENCY LIGHTS FROM ROW 4-1 ARE INOP. REPLACED BATTERY PACK LIGHT BATTERIES IN OVERHEAD BIN AT ROW 4D, C PER MD88 AMM 33-53-00. EMERGENCY LIGHTS WORK GOOD. (LP5588281)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,874 hrs · 56,857 cycles

EMERGENCY LIGHTS AT L1, R1 AND CO INOP. R/R BATTERIES AT BATERY PACK B5211 IAW MM 33-53.

Part: CABLE — FRAYED (TAILCONE) · airframe 75,712 hrs · 56,692 cycles

FOUND KEVLAR CABLE IN TAIL CONE FRAYED WHILE WORKING 88-0553-8-0066. REPLACED TAILCONE KEVLAR CABLE REF MD88 AMM 53-53 AND DRAWING LONG BEACH 5913350.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,455 hrs · 56,471 cycles

THE PASSENGER CABIN EMERGENCY LIGHTS IN THE LAST 8 ROWS ON THE RIGHT SIDE ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK ON THE POWER SUPPLY AND CHECKED THE LIGHTS PER AMM 33- 53. ALL TESTS ARE GOOD. (LP #5773638)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,025 hrs · 56,089 cycles

15 D SEAT EMERGENCY LIGHT INOP. R&R LIGHT ASSY AT SEAT 15D OPS NML REF AMM 33-52. (LP5654544)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 74,828 hrs · 55,915 cycles

FLOOR DELAMINATED 18" AFT OF COCKPIT THRESHOULD,4" LEFT OF CENTER, 18" FORWARD OF START OF CARPET. SPOT IS 4" WIDE BY 8" LONG BY 3/8" DEEP. TIME LIMITED REPAIR PER ERA 576928-14 REV ORGINAL HAS BEEN ACCOMPLISHED.REMOVED FLOOR PANELS LETTERS J & K PER MD88 IPC 53-21-00-02J READY FOR MFG. REMOVED F/A SEAT & STAIR CRANK, ELECTRICAL PANEL COVER & GIRTBARS. INSTALLED FLOOR PANELS J&K PER MD88 AMM 25-00. INSTALLED STAIR CRANK PER MD88 AMM 52-60. C/W SECTION 2 PERMANENT REPAIR OF ERA 576928-14 PER MD88 AMM 25-00. REINSTALLED ELECTRICAL PANEL COVER , GIRT BAR FITTINGS AND F/A SEAT. (LP5666402)

Part: PIN — PULLED (L1 DOOR SLIDE) · airframe 74,528 hrs · 55,653 cycles

FOUND PINS OUT ON L1 DOOR SLIDE. R/R L1 SLIDE PER W/C 2561-4964. OK FOR SVC. (LP5545438)

Part: ACCESS PANEL — MISSING (RT WING FLAP) · airframe 74,436 hrs · 55,575 cycles

RT 111B FLAB O/B FAIRING MISSING ACCESS PANEL. REPLACED MISSING ACCESS COVER ON RT WING 11B FLAP O/B FAIRING.(LP5545402)

Part: LENS — MISSING (POSITION LIGHT) · airframe 74,345 hrs · 55,499 cycles

LEFT FIXED AFT POSITION LIGHT LENS COVER MISSING. REPL LIGHT ASSY PER AMM 33-43. SDR REPORTED DUE TO POSSIBILITY THAT PART MAY HAVE DEPARTED FROM AIRCRAFT DURING FLIGHT. (LP5538812)

Part: FRAME — CRACKED (TAILCONE) · airframe 73,927 hrs · 55,151 cycles

TAILCONE-AFT CANT. FRAME OF FUSELAGE IS CRACKING AT ALIGNMENT PINS-7 O'CLOCK POS. & 12 O'CLOCK POS. REPAIRED STA 1510 FRAME @ 7 O'CLOCK POSIION PER ERA 497316-14MA. (LP0829967)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,557 hrs · 54,826 cycles

EXTERNAL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTING BATTERY PACK IAW AMM 33-55.

Part: WIRE — BROKEN (CABIN) · airframe 73,445 hrs · 54,726 cycles

EMER PATH LIGHT AT 11E INOP. FOUND BROKE WIRE IN HARNESS. R&R HARNESS P/N 0201875-001.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,419 hrs · 54,706 cycles

FOUND CELING EMERGENCY LIGHTS OUT A ROWS 22 - 25. REPLACED THE BATTERY PACK IAW AMM 33-53.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,203 hrs · 54,518 cycles

EMER LIGHTS IN FWD CEILING OF THE CABIN INOP. REPLACED B523/P5 BATTERY PACK REF AMM 33-53.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 72,952 hrs · 54,303 cycles

UPPER FRAME DAMAGED AT LATCH STRIKE AREA FOR CONDITIONED AIR SERVICE DOOR. LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0349:5300-2960/006 00017. REPAIRED PER PRI 569302-14 REV O MATCHES ERA 569302-14 REV O.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 72,952 hrs · 54,303 cycles

CRACK INDICATION RT SIDE OF VERTICAL L/E RT HAND FRONT SPAR ZFS 52.267 11TH HOLE ABOVE SPICE MKTG. LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 172-0001:5530-01045-0602/001 00206 PRI 569170-14AD REV O-1 MATCHES ERA 569170-14AD REVO.

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 75,997 hrs · 56,971 cycles

CRACK INDICATION ON RHS VERTICAL STABILIZER NEAR ZFS=52. FOLLOW ON ACTION IS REQUIRED. ERA 569170-14AD ISSUED FOR REPAIR TO CRACK INDICATION ON RHS VERTICAL STABILIZER NEAR ZFS=52. FOLLOW ON ACTION IS REQUIRED. TEMPORARY REPAIR APPROVAL GRANTED FOR 24 MONTHS FROM TIME OF REPAIR INSTALLATION/ACCOMPLISHMENT (08JUN2018) UNTIL DAMAGE TOLERANCE ASSESSMENT IS ACCOMPLISHED. AD 2011-15-01. AD 2011-15-01. REF NEW LP 1318019 FOR TRACKING, AND ERA 569170-14AD REV A, THIS LP MAY BE CLOSED. (LP0593184)

Part: BATTERY — DISCHARGED (CABIN) · airframe 72,909 hrs · 54,274 cycles

CEILING EMER LIGHTS AT ROWS 26-31 INOP. REPLACED BATTERIES AT PACK B5-106. OPS CK OK.

Part: FLOOR PANEL — WORN (CABIN) · corrosion level 2 · airframe 72,724 hrs · 54,128 cycles

GIRT BAR BRACKETS HARD TO OPERATE AT THE L1 DOOR. REMOVED BRACKETS AND FOUND FLOOR PANEL 160 WORN. FABRICATED A NEW FLOOR PANEL, .FOUND CORROSION ON THE AFT GIRT BAR ATTACH BRACKET. REPLACED FLOOR SUPPORT IAW DWG 9936534.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 72,247 hrs · 53,765 cycles

FWD GALLEY FLOOR SAGGING. REMOVED TWO FLOOR PANELS ADJACENT TO SERVICE DOOR. REMOVED GALLEY DOOR AND GALLEY MOUNT. MANUFACTURED AND INSTALLED FLOOR PANELS PER MD88AMM 53-20. INST GALLEY MOUNT AND DOOR.

Part: FITTING — CORRODED (LAVATORY) · airframe 71,865 hrs · 53,463 cycles

CORROSION FOUND IN THE FWD LAV WASTE BIN AT FLOOR. REPLACED THE LAVATORY FITTING IAW CMM 25-41-19.

Part: JACKSCREW — WORN (HORIZONTAL STAB) · airframe 71,705 hrs · 53,337 cycles

HORIZONTAL STAB JACKSCREW FAILED A WEAR CHECK IAW WORK CARD 2740-01113-08. REMOVED AND REPLACED THE HORIZONTAL STAB JACKSCREW ASSY IAW WORK CARD 2742-4540. ACFT OK FOR SERVICE.

Part: SKIN — CRACKED · airframe 70,761 hrs · 52,568 cycles

LOWER AFT SKIN AT STRINGER 17 CRACKED. REPAIRED IAW ER/A 560178-14AD.

Part: STRUCTURE — CRACKED (CENTER WING) · airframe 70,741 hrs · 52,552 cycles

HFEC INSPECTION OF RIGHT SIDE CENTER WING SHOWS A CRACK INDICATIONON AFT ROW OF S-17 AT 7TH FASTENER OUTBOARD IN SCAN AREA. CRACK EXTENDS APPROX. 1/4" INBOARD OF FASTENER HEAD. REMOVED FASTENER AT CRACK INDICATION. REPAIRED PER PRI560178-14 REV 0-6 252477 PRI 560178-14 REV 0 - 6 MATCHES ER/A 560178-14 ORIGINAL.

Part: FRAME — CRACKED (BS 1510) · airframe 70,339 hrs · 52,241 cycles

CANTED FRAME BS 1510 CRACKED AT TAILCONE PIN GUIDE AT 5:30 POSITION. REPLACED THE FRAME IAW DRAWINGS 5966769, AND 9911843-6.

Part: PIN — WORN (TAILCONE) · airframe 70,339 hrs · 52,241 cycles

TAILCONE LOCK PIN SPADE WORN AR 10:00 POSITION. REPLACED WORN SPADE PIN.

Part: STRAP — FRAYED (TAILCONE SLIDE) · airframe 70,339 hrs · 52,241 cycles

TAILCONE SLIDE CONTAINER AFT DOUBLE D RING HOLD DOWN STRAPS FRAYED. REPLACED BOTH TAILCONE SLIDE CONTAINER AFT DOUBLE D RING HOLD DOWN STRAPS.

Part: LANYARD — FRAYED (TAILCONE RELEASE) · airframe 70,339 hrs · 52,241 cycles

TAILCONE RELEASE CAM LANYARD FRAYED. REPLACED TAILCONE CAM LANYARD.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 70,339 hrs · 52,241 cycles

ATB DUE TO BOTH AFT LAVATORY SMOKE DETECTOR SOUNDING DURING CLIMB-OUT BUT WITH NO VISIBLE SMOKE. FLIGHT ATTENDANT ASSOCIATED A BURNED ODOR WITH THE EVENT. CONTAMINATION INSPECTION COMPLETED WITH NO CONFIRMED FINDINGS. DUE TO A REPEAT EVENT ON THIS AIRCRAFT, APU WAS REPLACED, BOTH RIGHT AND LEFT PRIMARY AND SECONDARY HEAT EXCHANGERS WERE REPLACED, CROSS OVER DUCT WAS REMOVED, STEAM CLEANED AND REPLACED. VERIFICATION FLIGHT WAS PERFORMED WITH NO SMOKE ODOR OR FUMES

Part: CAP — DAMAGED (APU OIL TANK) · airframe 70,339 hrs · 52,241 cycles

DURING BOARDING, A BURNING OIL ODOR AND HAZE WAS NOTICED WHEN TURNING ON BOTH PACKS OFF APU AIR. FOUND APU INLET CONTAMINATED WITH TURBINE OIL. REPLACED APU OIL TANK SERVICE CAP. CLEANED APU INLET AND PERFORMED PNEUMATIC DUCT BURNOUT PROCEDURE. NO FURTHER SMOKE/FUMES FOUND. (LP# 9612796)

Part: SKIN — CRACKED (BS 1401) · airframe 70,272 hrs · 52,190 cycles

SKIN CRACKED APPROXIMATELY 6 INCHES ABOVE THE NR 2 PYLON IN DIRECT LINE OF AFT ENG MOUNT. BS 1401 BETWEEN LONG 13R-14R. REMOVED FASTENERS AND CUT OUT DAMAGE SKIN IAW SRM 53-04 FIG 18 SH.1. FABRICATED REPAIR PARTS IAW SRM 53-04 FIG 18 SH 1. INSTALLED REPAIR IAW SRM 53-04 FIG 18 SH 1. C/W PERMANENT REPAIR INSTRUCTIONS. NO FURTHER INSPECTION REQUIRED IAW SRM 53-04 FIG 18 SH 1.

Part: FRAME — CRACKED (BS 1510) · airframe 69,895 hrs · 51,920 cycles

CRACK IN FRAME AT BS 1510 AT 5:00 POSITION. CUTOUT DAMAGE IAW ERA 497316-14MA, REV O. ACCOMPLISHED HFEC INSPECTION OF CUT OUT AREA IAW NDT SPM 06-00-06. LOCATED A REPAIR DOUBLER IAW ERA497316-14MA. DOUBLER INSTALLED IAW ERA 497316-14MA, OK FOR SERVICE.

Part: FRAME — CRACKED (BS 1510) · airframe 69,895 hrs · 51,920 cycles

CRACK IN FRAME AT BS 1510 AT 4:00 POSITION. CUTOUT DAMAGE IAW ERA 497316-MA, REV O. ACCOMPLISHED HFEC INSPECTION OF CUTOUT AREA IAW NDT SPM 06-00-06. LOCATED A REPAIR DOUBLER IAW ERA 497316-14MA. DOUBLER INSTALLED IAW ERA 497316-14MA. OK FOR SERVICE

Part: SWITCH — FAILED (LANDING LIGHT) · airframe 69,879 hrs · 51,911 cycles

WING LANDING LIGHTS SPARKED WHEN TURNED ON. REMOVED AND REPLACED LEFT WING LANDING LIGHT SWITCH IAW SWPM 20-20. OPS CHECKED GOOD . OK FOR SERVICE.

Part: WIRE — LOOSE · airframe 69,781 hrs · 51,845 cycles

AFTER TOUCHDOWN IN GCM, THE FLIGHT CREW REPORTED A MOMENTARY SHOWER OF SPARKS FROM UNDERNEATH THE STICK PUSHER INDICATOR AREA. NO ASSOCIATED ISSUES WERE REPORTED. FOUND LOOSE WIRES BEHIND THE STALL LIGHT PUSH SWITCH. THE WIRING WAS SECURED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FIRE BOTTLE — LEAKING (CABIN) · airframe 68,834 hrs · 51,124 cycles

WATER EXTINGUISHER LEAKING INTO 1ST CLASS CLOSET. R & R WATER EXTINGUISHER IAW AMM 26-20, SN ON: 12967, SN OFF: CRS140.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,171 hrs · 50,656 cycles

AFT CARGO FRAME 1271, LONGERON 30 LIGHT CORROSION. CUTOUT CORRODED FRAME SECTION AT STA 1271, LONGERON 30. SPLICED IN NEW SECTION IAW SRM 53-03, FIG 2A.

Part: WIRE — OPEN (CABIN) · airframe 68,171 hrs · 50,656 cycles

F/A PANEL EMERGENCY EXIT LIGHTS SWITCH DOES NOT ACTIVATE EMERGENCY EXIT LIGHTS. FOUND OPEN BATTERY JUMPER WIRE AT OVERWING EMERGENCY EVAC LIGHTS BATTERY, PACK, B5-49. RETERMINATED WIRE REF AMM 25-50-04. OPS CHECK GOOD.

Part: RIVET — LOOSE (BS 1437) · airframe 68,079 hrs · 50,588 cycles

WORKING RIVETS ON FUSELAGE AT BS 1437, RT SIDE L6. REPAIRED IAW PRI 547965-14, REV 0 AND COMPLIED WITH ERA 547965-14, REVISION ORIGINAL.

Part: FRAME — CRACKED (RT MLG WW) · airframe 68,079 hrs · 50,588 cycles

RIGHT WHEEL WELL AFT FRAME CRACKED AT OTBD END. REPAIRED IAW SRM 53-05, FIG 141 AND ERA 520687-14 MA, REV A.

Part: THRESHOLD — CORRODED (CARGO BAY) · corrosion level 2 · airframe 68,079 hrs · 50,588 cycles

CORROSION ON AFT CARGO DOOR THRESHOLD LOWER AFT CORNER. REPLACED SUPPORT IAW SRM 51-30-05 AND DWG 5936469.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,079 hrs · 50,588 cycles

FWD GALLEY EMERGENCY AISLE LIGHTS INOPERATIVE. REPLACED LAMPS IAW AMM 33-53-01-401.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 67,881 hrs · 50,442 cycles

MAINTENANCE FOUND THE EMERGENCY SIGNS FROM SEAT ROW 31 TO THE AFT CABIN INOPERATIVE. WIRES FOR LIGHT FIXTURE L2-845 WERE FOUND SHORTING TO A CLAMP. THE WIRES WERE REPAIRED AND THE CLAMP WAS REPLACED. THE LIGHTS CHECKED OK.

Part: TRANSDUCER — FAULTED (ANTI SKID SYS) · airframe 67,361 hrs · 50,082 cycles

THE LEFT OTBD NR 1 ANTI-SKID FAULT ILLUMINATED ON THE EOAP ON APPROACH, WHEN GEAR WAS EXTENDED. CREW INITIATED A GO AROUND AND COMPLIED WITH QRH. DUE TO LANDING FIELD CONDITION DIVERTED. MAINTENANCE FOUND INTERMITTENT TRANSDUCER FAULT AND REPLACED THE LT OTBD ANTI-SKID TRANSDUCER AND ANTI-SKID CONTROL BOX IAW AMM 32-43. ADJUSTMENT/TEST AMM 32-43-02 GOOD.

Part: SKIN — CORRODED (BS 725) · corrosion level 2 · airframe 65,827 hrs · 48,986 cycles

CORROSION FOUND ON THE SKIN BS 725, NEAR L29L ALONG AFT EDGE OF NR 2 RADIO ALTIMETER RECEIVER ANTENNA CUTOUT. REPAIRED THE DAMAGE IAW ERA 537426-14, REV ORIGIONAL.

Part: SKIN — CORRODED (BS 750) · corrosion level 2 · airframe 65,827 hrs · 48,986 cycles

SKIN HAS CORROSION DAMAGE AT BS 750. REPAIRED IAW PRI 537431-14, REV 2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,827 hrs · 48,986 cycles

DURING SERVICE CHECK, FOUND A CRACK AND BULGING SKIN JUST AFT OF MID CARGO DOOR NEAR CENTER LINE ON BELLY.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,884 hrs · 47,658 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING IN THE VENTRAL STAIRWAY WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER AND THE BATTERIES. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (BS 813-816) · airframe 62,941 hrs · 46,952 cycles

LIGHTNING STRIKE AT WINDOW BELT AT CUTOUT NR 32 LT SIDE, STA 813 TO 816. BLENDED AREA, HFEC & UT INSPECTED AREA WITH NO CRACKS NOTED, FABRICATED, TREATED, PRIMED & TOP COATED, & INSTALLED REPAIR PART AT WINDOW BELT CUT-OUT F/S 788-826, LONG 13L, LONG 15L ALL IAW ER/A 523926-14, REV "O", REQ HFEC INSP AT 24 MONTH INTERVALS ASSOCIATED ER/A 14-523926, ADDED FOR AC 0960.

Part: SKIN — DAMAGED (BS 774) · airframe 62,941 hrs · 46,952 cycles

LIGHTNING STRIKE AT WINDOW BELT BS 774. BLENDED AREA, AND FOUND TO BE WITHIN LIMITS.

Part: SKIN — DAMAGED (BS 754) · airframe 62,941 hrs · 46,952 cycles

LIGHTNING STRIKE AT WINDOW BELT BS 754.5. BLENDED AREA, HFEC & UT INSPECTED AREA WITH NO CRACKS NOTED, FABRICATED REPAIR, TREATED, PRIMED, INSTALLED, IAW ER/A NR 523926-14, REV. "O".

Part: BRACKET — CRACKED (BS 1425) · airframe 62,941 hrs · 46,952 cycles

CRACK ON INSIDE BRACKET OF DORSAL FIN AREA, BS 1425, BETWEEN STR 1 AND 2R. REMOVED ANGLE, FABRICATED, HEAT TREATED TO T6 CONDITION TREATED, PRIMED & INSTALLED ANGLE AT F/S 1425, BETWEEN STR 1-2R ALL IAW SRM 51-30-2, 51-30-05, 51-10-3, DWG 5912188, REV BD.

Part: BRACKET — CRACKED (BS 1425) · airframe 62,941 hrs · 46,952 cycles

CRACK ON INSIDE BRACKET OF DORSAL FIN AREA, BS 1425, BETWEEN STR 1 AND 2L. REMOVED ANGLE, FABRICATED, HEAT TREATED TO T6 CONDITION TREATED, PRIMED, & INSTALLED ANGLE AT F/S 1425 BETWEEN LONG 1 & 2L ALL IAW SRM 51-30-2, 51-30-5, 51-10-3 DWG 5912188, REV BD & FASE REPORT 2-37153-801, REV A.

Part: ANGLE — CRACKED (BS 1401) · airframe 62,941 hrs · 46,952 cycles

AFT ACCESSORY BAY AT BS 1401 ABOVE L17L INTERCOASTAL ANGLE CRACKED. REMOVED AFT ACCESSORY COMP AT STA 1401 ABOVE LONG 17L INTERCOSTAL IAW SRM 51-30-2 & 51-30-05, FABRICATED NEW INTERCOSTAL IAW DW3G 9936696 & SRM 51-10-4, HEAT TREATED NEW PART FROM 7075 "0" TO T6 CONDITION IAW FASER. NR 2-37153-801A, REV A, ALODINED & PRIMED NEW INTERCOSTAL IAW SRM 51-10-3 AND INSTALLED NEW INTERCOSTAL IAW DWG 9936696, REV O.

Part: SKIN — CORRODED (BS 810-829) · airframe 69,121 hrs · 51,361 cycles

REMOVED CORROSION ON LOWER SKIN AT BS 810 - 829 LONGERONS 29R - 29L AND FOUND TO BE OUT OF LIMITS. REPAIRED THE AREA IAW ER/A 523966-14 REV.O.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,941 hrs · 46,952 cycles

CRACK ON SHEAR TIE BETWEEN STRINGERS 1 AND 2R, ORIGINATING FROM FIRST FASTENER, FROM INBD CLOSE TO VERTICAL STABILIZER DORSAL FIN ATTACH FITTING. REMOVED SHEAR TIE, FABRICATED NEW SHEAR TIE, TREATED AND PRIMED SHEAR TIE AND INSTALLED IAW SRM 51-30-5, 51-10-3, DWG 9911860, REV L, FAS ENGINE REPORT NR 2-37153-801A, REV A.

Part: BUSHING — MIGRATED (LT ELEVATOR) · airframe 62,941 hrs · 46,952 cycles

LT ELEVATOR INBD TORQUE SPRING BUSHING HAS MIGRATED. FABRICATED BUSHING IAW ER/A 523974-14 REV O, INSTALLED BUSHING IAW CMM 22-30-1 & DWG 5930557-505.

Part: SHEAR TIE — CRACKED (BS 1429) · airframe 62,941 hrs · 46,952 cycles

CRACK ON SHEAR TIE BETWEEN STRINGERS 2 AND 3 LEFT. BS 1429,. REMOVED SHEAR TIE , FABRICATED NEW SHEAR TIE AND INSTALLED IAW SRM 51-30-05, 51-10-03, FAS ENG REPORT 2-37153-801A, REV A DWG 9911860, REV L.

Part: ATTACH ANGLE — LOOSE (BS 1225) · airframe 62,941 hrs · 46,952 cycles

RIGHT FUSELAGE SKIN HAS TWO LOOSE FASTENERS ON LOWER FLANGE OF VERTICAL TO FUSELAGE ATTACH ANGLE WITH POSSIBLE CRACKS FROM FASTENER HOLES "MARKED" APPROXIMATELY CANT STA 1225, I-34 NR 55. IDENTIFIED CRACK, CUT-OUT DAMAGED AREA DIM: 1.8" X 1.7", FABRICATED, LOCATED, DRILLED, DEBURRED NEW ANGEL REPAIR PART, VERIFIED HEAT TREATMENT OF FABRICATED REPAIR PART, ANGLE, TREATED FILLER & PRIMED FILLER & ANGLE, TOP COATED & INSTALLED REPAIR PARTS AT RT FUSELAGE SKIN LOWER FLANGE OF VERT T/O FOS. APPROXIMATELY CANT STA 1225 ALL IAW SR930296, REV A, SRM 51-30-05, 51-10-3, 51-10-4, DPS 1.05-4 AND NDTSPM P6, 06-10-01.

Part: SUPPORT ANGLE — CORRODED (BS 1003 KEEL) · airframe 69,121 hrs · 51,361 cycles

BS 1003 KEEL BEAM LOWER SUPPORT ANGLE CORRODED, REPLACED THE SUPPORT ANGLE.

Part: SKIN — DAMAGED (BS 190) · airframe 62,941 hrs · 46,952 cycles

LIGHTNING STRIKE BS 190, BETWEEN LONGERONS 29-30L. REMOVED PAINT, BLENDED AREA, AND FOUND TO BE OUT OF LIMITS. CUT-OUT DAMAGE AREA. FABRICATED REPAIR DOUBLER, FINGER DOUBLER, TREATED, PRIMED, TOP, COATED & INSTALLED REPAIR IAW SRM 53-04-1, PARA 6, FIG 2, 51-10-3 DELTA PSM 900-5-1, NR 4 & NDTSPM P4, 04-00-07.

Part: FRAME — CRACKED (BS 1343) · airframe 62,941 hrs · 46,952 cycles

CRACK ON LOWER FIREWALL FRAME BS 1343, BETWEEN LBL-12 & RBL-12. REMOVED FRAME ASSY FROM BS 1343, LBL 12 TO RBL 12. REPAIRED IAW ERA 094719-14 MA. PRIMED AND INSTALLED FRAME IAW SRM 51-30-2, SRM 51-30-5, ERA 094719-14MA, SRM 51-10-3, & SRM 51-30-2.

Part: BEAM — CRACKED (PAX DOORWAY) · airframe 62,941 hrs · 46,952 cycles

FWD ENTRY DOOR UPPER BEAM FWD & AFT ENDS ARE CRACKED. REMOVED BEAM & INSTALLED NEW IAW SRM 51-30-2, & 52-13-0.

Part: BEAM — CORRODED (THRESHOLD) · airframe 69,121 hrs · 51,361 cycles

AFT CARGO BAY C-3 THRESHOLD BEAM CORRODED, FABRICATED AND REPLACED EXISTING REPAIR.

Part: MOUNT — CORRODED (ANTENNA) · corrosion level 2 · airframe 62,941 hrs · 46,952 cycles

RADIO ALTIMETER TRANSMIT ANTENNA 1 MOUNT EXHIBITS CORROSION. REMOVED CORROSION FROM RADIO ALTIMETER TRANSMIT ANTENNA 1 MOUND IAW SRM 51-10-3, PARA 26. EVALUATED DAMAGE, REMOVED ORIG T .090 MAT REMOVED .035 MAT REMAINING .055 FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1, SHT 3. REMOVED ANTENNA MOUNT IAW SRM 51-30-2 & 51-30-5. LOCATED & DRILLED NEW MOUNT. ALODINED & PRIMED & TOP COATED ANTENNA MOUNT IAW SRM 51-10-3, PARA 14 & 21, ALSO 51-30-3B. INSTALLED NEW ANTENNA MOUNT IAW SRM 51-30-2 & 51-30-5. ALSO DWG 5936004, REV C FOR PART IDENTIFICATION.

Part: LONGERON — CORRODED (BS 1285-1295) · airframe 69,121 hrs · 51,361 cycles

LONGERON 29R BS 1285 - 1295 CORRODED OUT OF LIMITS, FABRICATED AND INSTALLED U-CHANNEL REPAIR.

Part: CUSP WEB — CORRODED (BS 714-788) · corrosion level 2 · airframe 62,941 hrs · 46,952 cycles

MAIN CABIN BS 712-788, CUSP WEB CORRODED. BLENDED CORROSION IAW ER/A 508307-14MA, REV A. FOUND TO BE OUT OF LIMITS IAW ER/A 508307-14MA REV A. CUT OUT DAMAGED AREA IAW SRM 53-05, FIG 131A-9. FABRICATED LOCATED AND DRILLED FILLER, REPAIR DOUBLER IAW SRM 53-05, FIG 131A9. INSTALLED REPAIR IAW SRM 53-05, FIG 131A9.

Part: SEAT TRACK — CORRODED (BS 1022-1041) · corrosion level 2 · airframe 62,941 hrs · 46,952 cycles

SEAT TRACK RBL 56 BETWEEN FS 1022 - 1041 CORRODED. REMOVED SEAT TRACK FROM BS 1050-1332. LOCATED, DRILLED, & DEBURRED SEAT TRACK & INSTALLED ALL IAW SRM 53-05, FIG 4B, 51-30-1, 51-10-4 & 51-10-3.

Part: CUSP WEB — CORRODED (BS 541-560) · corrosion level 2 · airframe 62,941 hrs · 46,952 cycles

MAIN CABIN CUSP WEB BS 541-560 CORRODED. BLENDED CORROSION AND FOUND OUT OF LIMITS. FABRICATED DOUBLER REPAIR AND FILLER. INSTALLED DOUBLER REPAIR IAW SRM 51-30-2, 51-10-3, 53-05, FIG 131A-5.

Part: CUSP WEB — CORRODED (BS 541-560) · airframe 69,121 hrs · 51,361 cycles

LEFT CUSP WEB CORRODED BEYOND LIMITS, BS 541-560, CORROSION REMOVED, DOUBLER FABRICATED AND INSTALLED.

Part: CUSP WEB — CORRODED (BS 636-655) · corrosion level 2 · airframe 62,941 hrs · 46,952 cycles

MAIN CABIN LT CUSP WEB IS CORRODED BETWEEN BS 636 & BS 655. BLENDED OUT CORROSION AND ALODINED AREAS AND FOUND OUT OF LIMITS. FABRICATED, & INSTALLED DOUBLER REPAIR.

Part: CUSP WEB — CORRODED (BS 579-598) · airframe 69,121 hrs · 51,361 cycles

LEFT CUSP WEB CORRODED BS 579-598, FABRICATED AND INSTALLED A REPAIR DOUBLER.

Part: CUSP WEB — CORRODED (BS 598-617) · airframe 69,121 hrs · 51,361 cycles

MAIN CABIN LT CUSP WEB IS CORRODED BETWEEN BS 598 & 617. FOUND TO BE OUT OF LIMITS IAW ERA 508307-14. CUT OUT DAMAGE, FABRICATED A REPAIR, TREATED, PRIMED, PAINTED AND INSTALLED THE REPAIR.

Part: CUSP WEB — CORRODED (BS 931-941) · corrosion level 2 · airframe 62,941 hrs · 46,952 cycles

CORROSION ON CUSP WEB AT S 931-941, RBL 59, EVALUATED AREA WITH 100 PERCENT MATERIAL LOSS AT BS 934, RBL 59 CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS, TREATED AND PRIMED REPAIR AREA, AND REPAIR PARTS INSTALLED. REPAIR INSTALLED IAW SRM 51-10-3, SRM 53-05, FIG 131A-14, SRM 51-10-03.

Part: CUSP WEB — CORRODED (BS 674-693) · corrosion level 2 · airframe 62,941 hrs · 46,952 cycles

LEFT CUSP WEB IS CORRODED BETWEEN BS 674 & 693. TREATED & PRIMED INSTALLED REPAIR IAW SRM 51-30-02 53-05, FIG 131A 51-30-3.

Part: RELEASE CABLE — DAMAGED (TAILCONE) · airframe 62,941 hrs · 46,952 cycles

MAINTENANCE DISCOVERED THAT THE INSULATION ON THE LT RELEASE LATCH CABLE FOR THE TAILCONE WAS DAMAGED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPAIRED IAW ER/A 523964-14 AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: SKIN — DAMAGED (BS 754) · airframe 62,941 hrs · 46,952 cycles

LIGHTNING STRIKE AT WINDOW BELT BS 754.5. BLENDED AREA, HFEC & UT INSPECTED AREA WITH NO CRACKS NOTED, FABRICATED REPAIR, TREATED, PRIMED, INSTALLED, IAW ERA 523926-14, REV "O".

Part: BRACKET — WORN (TAILCONE) · airframe 61,140 hrs · 45,634 cycles

MX DISCOVERED THAT THE TAILCONE AFT RT SPRING BRACKETS ARE WORN FROM THE SPRING. THE BRACKETS WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: SLIDE BLOCK — WORN (TAILCONE) · airframe 61,148 hrs · 45,640 cycles

DURING A CHECK OF TAILCONE RELEASE SYS, MX FOUND THE UPPER RT SIDE SLIDING BLOCK FOR THE UPPER TAILCONE LATCH WAS WORN BEYOND ALLOWABLE LIMITS. MX REPLACED THE UPPER SLIDING BLOCKS FOR BOTH THE RT SIDE AND THE LT SIDE. THE TAILCONE WAS RIG CHECKED AFTER INSTALLATION AND FOUND OPERATIONAL. THE RII COMPLETED FOLLOWING MX.

Part: WEB — CORRODED (BS 897) · corrosion level 2 · airframe 61,140 hrs · 45,634 cycles

WEB CORRODED, RBL 65, BS 897. REMOVED CORRODED SECTION IAW SRM 53-05, FIG 131A-13. HFEC CUTOUT IAW NDT SPM 06-10-01.001, NO DEFECTS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-05, FIG 131A-13. IDENTIFIED REPAIR IAW PS 900-5-1, NR 04.

Part: PIN — WORN (TAILCONE RELEASE) · airframe 61,140 hrs · 45,634 cycles

DURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYS, MX FOUND THE LT SIDE INTERNAL RELEASE TEE PIN WORN BEYOND ALLOWABLE LIMITS. TEE PIN REPLACED.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 60,792 hrs · 45,390 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 28 IN THE CABIN WAS INOPERATIVE. MX REPAIRED EMERGENCY EXIT WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYS.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 60,136 hrs · 44,923 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 22DE OF THE CABIN WAS INOPERATIVE. MX FOUND A LOOSE WIRE IN THE CONNECTOR, REPAIRED THE CONNECTOR PIN AND THE SYS RETURNED TO NORMAL OPERATION.

Part: LEAD — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,737 hrs · 44,637 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 27 IN THE CABIN WAS INOPERATIVE. MX REPLACED A JUMPER LEAD BETWEEN THE LIGHT SOCKET AND THE WALL CONNECTION AND FUNCTIONALLY CHECKED THE SYS.

Part: WIRE — BROKEN (CABIN) · airframe 59,079 hrs · 44,133 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 30DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE IN THE SEAT WIRE HARNESS AND REPAIRED IT. THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,500 hrs · 43,034 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN AT THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,300 hrs · 42,909 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS AT DOOR L1 AND THE COCKPIT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK WAS GOOD.

Part: SKIN — GOUGED (FS 1300-1308) · airframe 56,658 hrs · 42,443 cycles

FUSELAGE SKIN BS 1300-1308, L20-21L, REPAIRED GOUGES IAW ERA 495783-14.

Part: BUSHING — CORRODED (VERTICAL STAB) · airframe 55,527 hrs · 41,656 cycles

BUSHINGS RUSTED ON LT STAB INBD ATTACH LUG AT TOP OF VERT STAB NR 77. REPLACED PER EA 09-073278-12 AD REV G.

Part: PLATE — CORRODED (VERTICAL STAB) · airframe 55,527 hrs · 41,656 cycles

PLATES RUSTED ON OUTBD SIDE OF LT STAB OUTBD ATTACH LUG AT TOP OF VERT STAB. REPLACED PLATES PER EA 09-073278-12 AD REV G.

Part: SPAR CAP — CORRODED (HORIZ STAB) · airframe 55,527 hrs · 41,656 cycles

BARREL NUT HOLES CORROSION LOC: LT HORIZONTAL STAB AT INBOARD END OF FRONT SPAR CAP SPLICED SPAR CAP PER ERA 490788-14 REV A.

Part: SPAR CAP — CORRODED (HORIZ STAB) · airframe 55,527 hrs · 41,656 cycles

STABILIZER/ HORIZONTAL/ LT FWD SPAR CAP/ LOWER BARREL NUT HOLES CORRODED. SPLICED IN NEW FWD SPAR CAP PER ERA 490788 -14.

Part: WIRE — BROKEN (CABIN) · airframe 54,040 hrs · 40,668 cycles

MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS AT SEATS 24DE - 27DE TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT A BATTERY PACK. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (2010-D0947 (DLM88102071).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,705 hrs · 39,766 cycles

PASSENGER SEAT 25E EMERGENCY EXIT SIGNS INOPERATIVE. REMOVED AND REPLACED LENSE ON PASS SEAT 25E EMERGENCY EXIT SIGN. OPS CK GOOD. MCO AND PLAC REMOVED.

Part: BOLT — MISSING (NLG STEERING) · airframe 48,530 hrs · 37,066 cycles

ON TAXI OUT NOSE WHEEL STEERING TO THE LEFT GAVE OUT. A/C BROUGHT BACK TO GATE BY SUPERTUG NO STEERING WORKING. FOUND BOLT MISSING FROM STEERING CONTROL VALVE ROD END. FOUND MISSING HARDWARE IN TUNNEL BELOW VALVE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 48,379 hrs · 36,978 cycles

GOUGE ON FUSELAGE SKIN AT STA 237 BTW LONG 17 LT AND 18 LT. REPAIRED PER SRM 53-04D.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 48,379 hrs · 36,978 cycles

EXFOLIATION CORROSION ON LT CUSP WEB STA Y=586-598 AND X=60 REPLACED WEB PER DWG 9930538.

Part: RIB — CRACKED (LT WING) · airframe 48,379 hrs · 36,978 cycles

CRACK ON LT WING LEADING EDGE RIB AT STA XRS=289. REPAIRED PER SRM 57-06BD.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 48,379 hrs · 36,978 cycles

CRACK ON RT CUSP WEB STA Y=218-228 AND X=-58 AT PAX CABIN. REPLACED WEB PER DWG 9930538.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,379 hrs · 36,978 cycles

DUE AT HMV, SRM 53-04 FIG 12B SHT 2, REPAIR T6 DOUBLER/2 FT BELOW FWD AIRSTAIR CONTROL BOX/LT SIDE STA 160. REPAIRED PER ERA 467994-14 REV ORG ON N/R T0092778 AT HMV-3 IN GDL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,379 hrs · 36,978 cycles

CRACK ON FRAME STA. Y=1451 LONG 1. REPAIRED PER DRAWING 9911860 AND SRM 51-10-3D ON N/R T0093001 AT HMV-3 IN GDL.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 48,379 hrs · 36,978 cycles

EXFOLIATION CORROSION ON LOWER DOOR JAMB OF C-3. REPAIRED PER SRM 53-05D FIG 63 ON N/R T0093048 AT HMV-3 IN GDL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 48,379 hrs · 36,978 cycles

FOUND CRACK ON LONGERON 2 LT AT STA 1418. REPAIRED PER SRM 53-02D FIG 18 ON N/R T0092996 AT HMV-3 IN GDL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,379 hrs · 36,978 cycles

THREE CRACKS ON FUSELAGE SKIN AT THE STATIONS; Y=172 OF .050 Y=174.5 OF .125 AND Y=175.25 OF .562 IN THE UPPER FORWARD CORNER OF THE FORWARD SERVICE DOOR JAMB. REPAIRED PER SRM 53-05D 112 ON N/R T0092302 AT HMV-3 IN GDL.

Part: CUSP WEB — CRACKED (PAX CABIN) · airframe 48,379 hrs · 36,978 cycles

DUE AT HMV ERA 087344-14 CODE 9-53-21-03 REV A REPAIR FOR MAIN CABIN SUBFLOOR CUSP WEB AT STA Y=224 LT. REPAIRED CUSP WEB IAW ERA 087344-14 REV A AS A PERMANENT REPAIR.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 48,379 hrs · 36,978 cycles

DUE AT HMV ERA 087344-14 CODE 9-53-21-03 REV ORG, REPAIR MAIN CABIN FLOOR/STA 224 ACTL 2301/2201. REPAIRED PER ERA 087344-14 REV A ON N/R T0092783 AT HMV-3 IN GDL.

Part: PUMP — UNKNOWN (HYD SYSTEM) · airframe 41,970 hrs · 32,634 cycles

AT FL350 LEFT HYD PSI=0. DUPLICATE REPORT TO DOCUMENT SECOND COMPONENT REPLACED. REPLACED PUMP.

Part: RESERVOIR — UNKNOWN (HY SYSTEM) · airframe 41,970 hrs · 32,634 cycles

AT FL350 LEFT HYD PSI=0 AND LEFT HYD PRESS LOW. DID CHECKLIST WITH NO RESOLVE. LEFT SYS STILL PSI=0, QTY 17-19. REPLACED LEFT HYD SYS RESERVOIR AND LEFT ENG PUMP AND FILTERS. PURGED LEFT SYS OF AIR AND BLED RESERVOIR.

Part: GEARBOX — CRACKED (NR 2 ENGINE) · airframe 41,166 hrs · 32,026 cycles

NR 2 ENGINE INFLT SHUTDOWN DUE TO LOSS OF ENGINE OIL AND PRESSURE. FOUND OIL LEAK AT OIL FILTER CAP. GEARBOX CRACK AT STUD HOLDING CAP - NDS ENG CHANGE.

Part: ADC — FAILED (NR 2) · airframe 40,323 hrs · 31,418 cycles

AIRBORNE A/T CLICKED OFF, DFGS ALT WINDOW BLANKED, AND FMS SCRATCH PAD SHOWED CADC NR 1 FAILED. USED CADC FAIL CHECKLIST. ON LEVEL OFF NR 1 ALT WAS 600 FT HIGHER THAN STBY. BECAUSE OF INDICATION IF INTERMITTENT FAILURE FROM BOTH CADC COMP, RETURNED TO CVG. REPLACED CADC NR 1 AND CADC NR 2. OPS AND LEAK CHECKED SYS PER AMM 34-11-00-201-1. RAN RT 1 AND 2, BOTH OK.

Part: TRIM MOTOR — FAILED (STAB TRIM) · airframe 37,340 hrs · 29,337 cycles

ALTERNATE TRIM INOP WITH AUTOPILOT ON OR WITH CHICLET SWITCHES. BOTH DFGC ATTEMPTED. REPLACED ALTERNATE STAB TRIM MOTOR.

Part: DUCT — RUPTURED (A/C BAY) · airframe 35,955 hrs · 28,420 cycles

AFTER TAKE OFF LEFT PNEUMATIC SUPPLY DUCT RUPTURED, CAUSING A TAIL COMPARTMENT TEMP HIGH CONDITION, THERMALLY DISCHARGING BOTH FIRE BOTTLES. COCKPIT INDICATING TAIL COMP TEMP HIGH AND BOTH AGENT LOW LIGHTS. AIRCRAFT PERFORMED AIR TURN BACK TO ATL. REPLACED DUCT AND BOTTLES

Part: PANEL — SEPARATED (NR 1 NACELLE) · airframe 34,739 hrs · 27,607 cycles

SECTION OF ACOUSTIC PANEL SEPARATED FROM INLET COWL OF NR 1 ENGINE. MINOR DAMAGE TO FAN BLADES. REPLACED INLET.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,418 hrs · 26,671 cycles

AIRCRAFT ARRIVED FOR HMV WITH A TIME-LIMITED SKIN REPAIR, SCHEDULED FOR PERMANENT TO OCCUR AT HMV, PER ERA 379153-14. ERA 379153-14 WAS REVISED TO REVISION -A- TO INCORPORATE PERMANENT REPAIR INSTRUCTIONS.

Part: ELECTRICAL SYS — MALFUNCTIONED (COCKPIT) · airframe 33,363 hrs · 26,629 cycles

JUST BEFORE TAXI OUT LOST BOTH BUSSES, ENGINE BUSSES DID NOT PICK UP FROM APU. COMPLETE ELECTRICAL FAILURE. RESET LT AND RT GEN SWITCHES TO ON. RAN ENGS BOTH GENS OPS CHECK OK.

Part: ACM — DAMAGED (A/C BAY) · airframe 33,141 hrs · 26,466 cycles

ATB - SMOKE IN AFT CABIN ON CLIMB, AFT LAV SMOKE DETECTORS SOUNDED, WHITE SMOKE, ELECTRICAL SMELL, STARTED 5 ROWS FWD OF MID JUMPSEAT. DISSIPATED AT 3000 FT. WING/ENG A/I OFF CROSSFEEDS CLOSED, APU OFF. FOUND CHUNKS MISSING FROM ACM TURBINE BLADES AND OIL IN DUCTS AFT OF ACM. REPLACED ACM PER M/M. LEAK CHECKS AND OPS CHECKS OKAY.

Part: FIRE BOTTLE — LOW (TAIL) · airframe 31,231 hrs · 25,068 cycles

AFTER TAKE OFF AGENT 2 LOW LIGHT ILLUMINATED. C/A RPLD AGENT 2 BOTTLE CKS GOOD.

Part: CLAMP — LOOSE (A/C BAY) · airframe 31,231 hrs · 25,068 cycles

TAIL COMP TEMP HIGH LIGHT ILLUMINATED AFTER T/O LIGHT, EXTINGUISHED AFTER RT PACK TURNED OFF. C/A FOUND HOT AIR COMING FROM RT ACM TURBINE CLAMP AT 1200 O'CLOCK TIGHTEN SAME CKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,154 hrs · 25,001 cycles

EMERGENCY LIGHT INOP AT SEAT 25. RELAMPED PER M/M, CHECKS NORMAL.

Part: STRAP — BROKEN (AFT DOOR) · airframe 31,154 hrs · 25,001 cycles

IRR- AFT DOOR FLASHLIGHT SEAL BROKEN CA- REPLACED SEAL

Part: TUBE — DAMAGED (COCKPIT) · airframe 29,654 hrs · 23,893 cycles

FIRST OFFICERS CREW O2 MASK HARNESS TUBE BLOWN OUT - REPLACED MASK ASSY

Part: DUCT — SEPARATED (LEFT A/C PACK) · airframe 28,851 hrs · 23,308 cycles

ON CLIMBOUT AT APPROX 12500, HEARD THUMP AND IMM CABIN PRESS BUMP. LEVEL OFF AT 14000. RETURNED TO MKE. ON DESCENT FLOW LIGHT WAS ILLUM WHEN THROTTLES WERE RETARDED. FOUND OUTLET DUCT OF LEFT COOLING TURBINE OFF. RESECURED AND TORQUED PER DMM 21-51-01-2. LEAK CHECKED DUCT AND RAN A/C PACK PER 21-00-00-0. RAN BOTH PACKS WITH ENG RUNNING. VERIFIED BOTH PACKS, PRESS AIRCRAFT NORMAL.

Part: DUCT — LOOSE (TAIL) · airframe 28,589 hrs · 23,109 cycles

RIGHT PACK FAILED IN CLIMBOUT. WORKED FINE FOR AWHILE, QUIT PASSING APPROXIMATELY 15,000 FT. FOUND DUCT FOR RIGHT ACM CAME OFF. REPLACED DUCT. RIGHT PACK LEAK AND OPERATIONAL CHECKS GOOD.

Part: O-RING — FAILED (RT HYD SYST)

RIGHT HYDRAULIC SYSTEM FAILURE. REPLACED O-RING ON RT PRESSURE LINE.

Part: ENGINE — FAILED (NR 2 ENGINE)

JUST AFTER LIFTOFF, RT OIL STRAINER CLOGGED ON AND RT OIL TEMP ROSE TO 120 AND CONTINUED TO CLIMB. SHUT DOWN RT ENGINE. FOUND METAL IN MAIN OIL FILTER AND CHIP DETECTOR FOR NR 3 BEARING. REPLACED ENGINE.

Part: ACTUATOR — FAILED (RUDDER)

ON T/O, RT RUDDER BECAME EXTREMELY DIFFICULT TO PUSH. PROBLEM CLEARED UP THEN HAPPENED AGAIN ON CLIMBOUT. RETURNED TO ATL. ON APPROACH RUDDER AGAIN BECAME DIFFICULT TO PUSH. INTERMITTANT, BUT REOCCURS OFTEN. REPLACED RUDDER POWER CONTROL ACTUATOR.

Part: SKIN — DENTED (BS 1287)

DURING REGULAR SERVICE IN ATL, A TAXIING L1011 SPOOLED THE ENGINES AS IT WAS MAKING A TURN AND CAUSED A BAG CART TO BLOW INTO THE SIDE OF THIS AIRCRAFT CAUSING A LARGE DENT. THE DENT IN THE SKIN IS LOCATED AT APPROXIMATELY FS 1287 AND STR 23R. THE DENT MEASURES 12 LONG BY 6 WIDE. THE DAMGE WILL BE REPAIRED PER ER/A 361318-14.

Part: BULB — MISSING (CABIN)

EMERGENCY TRACK LIGHT BULB AND COVER MISSING AT 4C. INST NEW BULB AND MODULE, CK'S OK (P/N 0L3071BPEGPL).

Part: ANGLE — CRACKED (NR 2 PYLON)

DURING LETTER CHECK, FOUND NR 2 PYLON WEDGE, UPPER SURFACE TO FUSELAGE ATTACH ANGLE CRACKED, REPAIRED PER SRM 54-04 FIG 4.