N924DL

Part: FITTING — BENT (FUSELAGE) · airframe 75,005 hrs · 56,735 cycles

CUSP FITTING AT FRAME 275 BENT. REMOVED AND REPLACED CUSP FITTING WITH SERVICEABLE NEW P/N 3912075U506. STANDARD HARDWARE INSTALLATION PER SRM 51-40.

Part: FRAME — DAMAGED (BS 313) · airframe 74,998 hrs · 56,732 cycles

FUSELAGE FRAME AT BS 313 BETWEEN LONGERONS 18R AND 24R DAMAGED. REMOVED DAMAGE. FABRICATED A FRAME SPLICE IAW SRM 53-03 1C AND INSTALLED THE REPAIR IAW SRM 53-03 1C.

Part: FRAME — DAMAGED (BS 332) · airframe 74,998 hrs · 56,732 cycles

FRAME BS 332 BETWEEN LONGERONS 20R AND 25R DAMAGED. REMOVED DAMAGE AND FABRICATED A REPAIR IAW SRM 53-03, FIG 45. INSTALLED IAW SRM 53-03D, FIG 45.

Part: LONGERON — DAMAGED (BS 256-332) · airframe 74,998 hrs · 56,732 cycles

LONGERON 20R BETWEEN BS 256 TO 332 DAMAGED. REPLACED WITH A NEW LONGERON IAW SRM 51-30-0 AND DRAWING 5920323.

Part: LONGERON — NOT REPORTED (BS 256-332) · airframe 74,998 hrs · 56,732 cycles

LONGERON 23R BETWEEN BS 256 TO 332. REPLACED THE LONGERON IAW SRM 51-30-0, AND DRAWING 5920323.

Part: LONGERON — DAMAGED (BS 256-332) · airframe 74,998 hrs · 56,732 cycles

LONGERON 19R BETWEEN BS 256 TO 332 DAMAGED. REPLACED THE LONGERON IAW SRM 51-30-0 AND DRAWING 5920323.

Part: LONGERON — DAMAGED (BS 256-332) · airframe 74,998 hrs · 56,732 cycles

LONGERON 21R BETWEEN BS 256 TO 332 DAMAGED. INSTALLED IAW SRM 51-30-0 , AND DRAWING 5920323.

Part: LONGERON — DAMAGED (BS 256-332) · airframe 74,998 hrs · 56,732 cycles

LONGERON 22R BETWEEN BS 256 TO 332 DAMAGED. REPLACED THE LONGERON IAW SRM 51-30-0 AND DRAWING 5920323.

Part: FRAME — DAMAGED (BS 256) · airframe 74,998 hrs · 56,732 cycles

FUSELAGE FRAME AT BS 256 BETWEEN LONGERONS 18R AND 24R DAMAGED. CUT THE DAMAGE SECTION OF FRAME BETWEEN LONGERON 18R AMD 21R IAW SRM 53-03 FIG 2A MIP302615. PERFORMED DAMAGE CONTAINMENT REF NDTSPM06-10-01-001. NO DAMAGE NOTED. FABRICATED A FRAME SPLICE REPAIR IAW SRM 53-03-1CMIP296748. INSTALLED THE FRAME SPLICE REPAIR IAW SRM 53-03.

Part: FRAME — DAMAGED (BS 275) · airframe 74,998 hrs · 56,732 cycles

FUSELAGE FRAME AT BS 275 BETWEEN LONGERONS 18R AND 24R DAMAGED. FABRICATED A FRAME SPLICE REPAIR IAW SRM 53-03-1C.. INSTALLED FRAME SPLICE IAW SRM 53-03 1C.

Part: FRAME — DAMAGED (BS 294) · airframe 74,998 hrs · 56,732 cycles

FUSELAGE FRAME AT BS 294 BETWEEN LONGERONS 18R AND 24R DAMAGED. REMOVED DAMAGE FRAME 294 BETWEEN STR 18R AND 24R CUT LINE BETWEEN STR 25R AND24R. FABRICATED REPAIR PARTS FOR SPLICE REPAIR. COMPLETED SPLICE REPAIR IAW SRM 53-03.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,755 hrs · 56,536 cycles

CEILING EMERGENCY LIGHTS INOPERATIVE AT ROW 12 - 14 AND ROW 25 - 30. REPLACED THE BATTERY PACKS. CHECKED NORMAL.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 74,374 hrs · 56,206 cycles

BURNING RUBBER SMELL IN CABIN/COCKPIT MOST NOTICEABLE IN AFT CABIN AREA. SEEMED TO IMPROVE DURING CRUSE. ATS ALSO DISCONNECTED W/THROTTLE SPLIT APPROACHING LEVEL OFF. ATS DISCONNECT W/THROTTLE SPLIT SIGNED ON LOG PAGE. PERFORMED AMDS CARDS 2120-2367 SMOKE/ODOR TROUBLESHOOTING AND 7100-2619 PNEU DUCT BURN OUT. NO ORDERS NOTED.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 73,559 hrs · 55,557 cycles

DURING TAXI-OUT CREW REPORTED ODOR AND HAZE IN THE CABIN AND RETURNED TO THE DEPARTURE GATE. MAINTENANCE FOUND A HYDRAULIC LEAK AT THE LEFT ENGINE FILTER MODULE PRESSURE LINE FITTING. THE FITTING O-RING WAS REMOVED AND REPLACED AND A GOOD LEAK CHECK ACCOMPLISHED. COMPLETED MINI DUCT BURNOUT AND DEFERRED THE APU FOR CLEANING.

Part: PIN — WORN (TAILCONE) · airframe 73,270 hrs · 55,329 cycles

TAIL CONE LOCK PINS WORN, RIGHT SIDE UPPER & LOWER. R & R BOTH RT UPPER & LOWER LOCK PIN ASSEMBLIES IAW AMM 53-53-00-501.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 73,175 hrs · 55,261 cycles

THE RED AFT CARGO BIN FIRE LIGHT ILLUMINATED BRIEFLY, EXTINGUISHED FOR ABOUT 30 SECONDS, AND THEN CAME BACK ON AND STAYED ON. MAINTENANCE INSPECTED THE AFT CARGO BIN AND FOUND NO EVIDENCE OF SMOKE OR FIRE. MAINTENANCE DID FIND LUGGAGE WEDGED AGAINST SMOKE DETECTOR NR 2. AS A PRECAUTION SMOKE DETECTOR NUMBER 2 AND THE OVERHEAD CARGO SMOKE CONTROL PANEL WERE BOTH REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (SEAT 22) · airframe 72,756 hrs · 54,955 cycles

SEAT 22 EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY IAW MM 33-52.

Part: BATTERY — DISCHARGED (CABIN) · airframe 72,531 hrs · 54,811 cycles

SEVERAL CELLING STANDBY LIGHTS INOP. FOUND BATTERY PACKS B5-100 AND B5-102 BAD. SWAPPED IN KNOWN GOOD BATTERIES. OPS NORMAL. REMOVED AND REPLACED BATTERIES IN PACK B5-100. STILL NEEDS BATTERIES FOR POWER PACK B5-105. REPLACED BATTERIES IN POWER PACK B5-102. OPS NORMAL. OK FOR SERVICE REF 33-53-00.

Part: SLIDE — DISCONNECTED (L1 DOOR) · airframe 72,457 hrs · 54,757 cycles

L1 DOOR SLIDE NOT CONNECTED TO GIRT BAR. SLIDE TO GIRT BAR. CHECKS OK. AIRCRAFT OK FOR SERVICE.

Part: TIRE — SEPARATED (MLG) · airframe 71,758 hrs · 54,202 cycles

CREW REPORTED STRONG BURNING RUBBER ODOR IN CABIN AFTER TAKEOFF. SUSPECTED TIRE ISSUE AND DECLARED EMERGENCY FOR LANDING. MAINTENANCE FOUND NR 2 MAIN TIRE TREAD SEPARATED. REPLACED NUMBER 1 AND 2 MLG WHEEL/TIRE ASSEMBLIES. ACFT WAS FERRIED TO MSP FOR REPAIRS TO FLAP, BUTE DOOR, WING T/E PANEL, AND MLG SPRAY DEFLECTOR. ACFT HAS RETURNED TO SERVICE.

Part: CONNECTOR — CORRODED (BRAKE TRANSDUCER) · airframe 71,256 hrs · 53,827 cycles

CREW REPORTED MINIMAL BRAKING AVAILABLE DURING LANDING WITH MANUAL APPLICATION. A POST FLIGHT INVESTIGATION REVEALED A BRAKE TEMP DIFFERENCE BETWEEN THE OTBD, HOT AND INBD, COOL. MAINTENANCE FOUND CONNECTORS ON NR 3 WHEEL TRANSDUCER AND NR 2 BRAKE SERVO BADLY CORRODED, BOTH CONNECTORS WERE REPLACED WITH SATISFACTORY CHECK OUTS.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 71,240 hrs · 53,809 cycles

ON TOUCHDOWN, CREW NOTED DEGRADED BRAKING ACTION WITH NORMAL BRAKE APPLICATION. FULL BRAKE PEDAL APPLICATION RESULTED IN PARTIAL BRAKING FORCE ACCORDING TO THE FLIGHT CREW. OBSERVED BRAKE TEMPS WERE NOT BALANCED BUT NO ASSOCIATED WARNINGS ON THE EOAP . MAINTENANCE CHECKED ANTI-SKID FUNCTION WITH NO FINDINGS BUT REPLACED THE ANTI-SKID CONTROL UNIT. FUNCTIONAL CHECKS WERE GOOD.

Part: BEAM — CRACKED (GALLEY DOOR) · airframe 70,952 hrs · 53,613 cycles

FWD GALLEY SERVICE DOOR, BEAM NR 4 CRACKED AT AFT END. INSTALLED REPAIR IAW SRM 52-05, FIG 25, SHEET 11.

Part: BRACE — CRACKED (GALLEY DOOR) · airframe 70,952 hrs · 53,613 cycles

DURING SCHEDULED MAINTENANCE WITH GALLEY SERVICE DOOR IN THE OPEN POSITION, LOWER FWD INSPECTION HOLE, BRACE IS CRACKED. REPLACED SUPPORT IAW DWG 911582.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 70,952 hrs · 53,613 cycles

FWD GALLEY SERVICE DOOR- BEAM NR 4 CRACKED AT FWD END. INSTALLED REPAIR PART REF MD 88, SRM 52-05, FIG 25, SHEET 17.

Part: BRACE — CRACKED (GALLEY DOOR) · airframe 70,952 hrs · 53,613 cycles

GALLEY SERVICE DOOR, LOOKING FROM THE OPEN POSITION, SECOND INSPECTION HOLE DOWN FROM TOP ON AFT SIDE, BRACE IS CRACKED. REPLACED ANGLE IAW DWG 9911579.

Part: SKIN SPLICE — CRACKED (FUSELAGE) · airframe 73,758 hrs · 55,714 cycles

ER/A 545885-14 SECTION I ADDRESSES CRACK DAMAGE FOUND ON SKIN SPLICE AT FS1429 BETWEEN L2L/L3L AND L2R/L3R. THIS REPAIR COMPLETED 16APR16.

Part: GUSSET — CORRODED (BS 636) · corrosion level 2 · airframe 70,952 hrs · 53,613 cycles

MID CARGO BILGE-FLOOR SUPPORT GUSSET HAS CORROSION, BS 636 ABOVE & OTBD OF L29R. REPLACED FLOOR SUPPORT GUSSET IAW SRM 51-30-05.

Part: SKIN — CRACKED (BS 1474) · airframe 70,952 hrs · 53,613 cycles

EXTERIOR SKIN IS CRACKED AT BS 1474 LT SIDE JUST OTBD OF AIRSTAIR CUTOUT. REPAIRED IAW PRI 544929-14, REV 0, 07APR16 AND C/W ER/A 544929-14, REV ORIGINAL.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 69,842 hrs · 52,869 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING AT THE FORWARD EXIT AND FOR ROWS 1-14 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED A FAILED FUSE AT THE POWER SUPPLY AND REPAIRED A DAMAGED WIRE, DUE TO BEING PINCHED IN THE WALL, AT DOOR 2R BY SPLICING.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 67,363 hrs · 51,158 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 18E WAS INOPERATIVE. MAINTENANCE FOUND WIRES PULLED OUT OF THE LIGHT SOCKET. REPAIRED AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 66,957 hrs · 50,850 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FRONT SECTION OF THE CABIN, FORWARD DOORS TO ROW 11, HAD FAILED. MAINTENANCE REPAIRED A WIRE CONNECTOR FOR THE NOTED LIGHTED AREAS AND THE FOLLOW-UP, OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,919 hrs · 50,823 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN THE FRONT SECTION OF THE CABIN, ROWS 1 - 12, HAD FAILED. MAINTENANCE REPLACED THE BATTERY PACKS AND OPS CHECKED GOOD.

Part: FUSE — LOOSE (EMERGENCY LIGHTS) · airframe 66,879 hrs · 50,794 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY SEAT LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. MAINTENANCE FOUND THAT A FUSE WAS LOOSE. THE FUSE WAS RE-SECURED AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: DOOR — CRACKED (PAX) · airframe 66,807 hrs · 50,737 cycles

DURING MAINTENANCE WALKAROUND, SUSPECTED CRACK ON AFT RIVET HOLE LOWER AFT CORNER OF FWD AIR STAIR DOOR. VERIFIED CRACK APPROXIMATELY .5" THROUGH RIVET FASTENER HOLE IAW NDT SPM 06-10-01.001. REMOVED DAMAGE AND DRILLED UP REPAIR DOUBLER IAW SRM 53-05, REPAIR 57A. INSPECTED AREA AND REPAIR DOUBLER IAW SRM 53-01-1A4, NO CRACKS FOUND. INSTALLED REPAIR IAW SRM 53-05, FIG 57A. REPAIR INSTALLATION OK IAW SRM 53-05, FIG 57A. RESTORED FINISH IAW SRM 53-05, FIG 57A.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 66,020 hrs · 50,182 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 12D WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS DISCONNECTED, CONNECTED AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: SPAR — CRACKED (WING) · airframe 65,719 hrs · 49,966 cycles

WING REAR SPAR LOWER ANGLE CRACKED AT STATION 164 FLAP HINGE FITTING LOWER INBD MOUNT STUD. REPAIRED IAW ERA 523539-14AD, REV ORIGINAL. TASK STEPS COMPLETED ON NR 110.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 65,719 hrs · 49,966 cycles

LIGHTING STRIKE AROUND FASTENER HEAD ON VERTICAL STABILIZER L/E SKIN ON DOUBLER REPAIR LT SIDE, 9" UP FROM FRONT SPAR, STA ZFS 52.267-M. REMOVED VERTICAL SATBILIZER L/E REF MM 55-30-01. L/E INSTALLED, REPAIRED IAW ER/A 523587-14AD.

Part: SKIN — DAMAGED (BS 1167-1174) · airframe 70,952 hrs · 53,613 cycles

ERA 523551-14AD SECTION I ISSUED FOR FUSELAGE SKIN DAMAGE REPAIR AT BS 1167-1174, L1-2R. REF NRC 134, ACCOMPLISHED DURING C-CHECK IN MSP.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 65,719 hrs · 49,966 cycles

LEFT FWD OVERWING EMERGENCY EXIT DOOR PAN CRACKED AT AFT UPPER PAN SUPPORT BRACKET. REPAIRED OVERWING EXIT DOOR IAW ER/A 523654-14, REV 0 ASSOCIATED ER/A 14-523654 ADDED FOR AC 0924.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 65,706 hrs · 49,957 cycles

DURING LINE CHECK, NOTED BOTH FWD OVERWING EXIT SIGNS WERE INOPERATIVE. REPLACED DEAD BATTERY PACK B5-104 IAW AMM 33-51. OPS CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 65,186 hrs · 49,603 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROW 21DE WAS INOPERATIVE. MAINTENANCE REPLACED THE PIGTAIL WIRES AT THE LIGHT AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,037 hrs · 49,493 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE VENTRAL STAIRWAY INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: LATCH — UNSECURE (TAILCONE RELEASE) · airframe 64,448 hrs · 49,042 cycles

PILOT DISCOVERED ONE TAILCONE RELEASE LATCH RECEPTACLE WAS POPPED AND ANOTHER WAS NOT FULLY LATCHED. THE RECEPTACLES WERE REATTACHED AND THE SYS CHECKED GOOD.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 63,243 hrs · 48,233 cycles

FLIGHT CREW DIVERTED THE ACFT AFTER THE COCKPIT AND CABIN EXPERIENCED SMOKE WHEN THE ENGINE ANTI-ICE VALVES WERE TURNED ON. CREW TURNED OFF ANTI-ICE SYS AND THE SMOKE DISSIPATED. MX CLEANED FLUID FROM THE WHEEL WELLS, LOWER FUSELAGE, AND APU INLET. PERFORMED OPN 2903 AND OPN 5088 AND NO FURTHER FAULTS WERE IDENTIFIED. ALSO COMPLIED WITH OPN 5090 AS AN ALT DUCT BURNOUT AND NO SMOKE OR ODOR WAS DETECTED. ENGINE ANTI-ICE OPS TEST OF BOTH ENGINES RESULTED IN NO FINDINGS.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 63,195 hrs · 48,203 cycles

DURING LINE INSPECTION, THE FWD OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. TROUBLESHOOTING INDICATED THE BATTERIES WERE DISCHARGED AND NEEDED REPLACEMENT. BATTERIES WERE REPLACED AND TESTED IAW AMM 33-53. OPS NORMAL AFTER BATTERY REPLACEMENT NR 30 DAY HISTORY FOR THIS DISCREPANCY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,572 hrs · 47,781 cycles

DURING LINE CHECK, MX FOUND THAT FWD OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: LONGERON — CRACKED (BS 465 L4R) · airframe 62,391 hrs · 47,645 cycles

MAIN CABIN BS 465, LONGERON 4R IS CRACKED. REPAIRED IAW SRM 51-30-2, PAGE 24.

Part: LONGERON — CORRODED (BS 1287-1309) · airframe 62,391 hrs · 47,645 cycles

AFT CARGO LONGERON 27R CORRODED BS 1287-1309. REPAIRED IAW SRM 53-02.

Part: LONGERON — CRACKED (BS 541 L4L) · airframe 62,391 hrs · 47,645 cycles

LONGERON 4L, CRACKED AT FS 541, REPAIRED IAW SRM 53-02, PARA 12.

Part: SKIN — CRACKED (L1 DOOR) · airframe 62,386 hrs · 47,642 cycles

L1 DOOR LOWER EDGE SKIN IS BENT AND PREVIOUS REPAIR IS CRACKED. REPAIRED IAW SRM 51-30-2.

Part: FRAME — CRACKED (BS 1437 L8R) · airframe 62,386 hrs · 47,642 cycles

AFT ACCESSORY BAY FRAME WEB CRACKED AT L8R. REPAIRED IAW ER/A 507856-14, REV ORIG.

Part: SKIN — CORRODED (BS 760-772) · airframe 62,386 hrs · 47,642 cycles

FUSELAGE EXTERNAL SKIN CORROSION AT RT FILLET ATTACH POINT FS 760-772, L27R, 28R. REPAIR IAW SRM 53-04, PAR 57 AND ER/A 507877-14, REV ORIG.

Part: SKIN — CRACKED (BS 1418-1419) · airframe 62,386 hrs · 47,642 cycles

UPPER SKIN PANEL CRACKED BETWEEN FASTNERS BS 1418 TO 1419 L1L. REPAIRED REF ER/A 507050-14 RV ORIG.

Part: LONGERON — CORRODED (BS 1287-1309) · airframe 62,386 hrs · 47,642 cycles

AFT CARGO BAY, LONGERON CORRODED BS 1287-1309. REPAIR IAW SRM 53-02, FIG 18.

Part: SKIN — CORRODED (BS 1193 L28R) · airframe 62,386 hrs · 47,642 cycles

SKIN CORRODED. REPAIRED SKIN BS 1193 LONGERON 28R IAW ER/A 484416-14, REV D.

Part: SKIN — CRACKED (BS 826 L1) · airframe 62,386 hrs · 47,642 cycles

DENTED WITH CRACK INDICATION ON UPPER FUSELAGE LOCATED 4TH FASTENER AFT OF BS 826 AT L1. REPAIRED IAW ER/A 507668-14AD, REV ORIG.

Part: MOUNT — CORRODED (TCAS ANTENNA) · airframe 62,386 hrs · 47,642 cycles

TCAS ANTENNA BASE FOUND ON FUSELAGE WITH GOUGES & CORROSION. . REPAIRED IAW SRM 53-02, FIG 18.

Part: CUSP WEB — CORRODED (BS 606-614 L18L) · airframe 62,386 hrs · 47,642 cycles

LT CUSP WEB CORRODED AND CRACKED FS 606-614 L18L. REPAIRED SRM 51-10-4.

Part: SKIN — CORRODED (BS 729 L29-30R) · airframe 62,386 hrs · 47,642 cycles

MID CARGO LOWER BILDGE SKIN HAS CORROSION AT STA 729 BETWEEN L30, L29R. REPAIRED IAW ER/A 507665-14, REV ORIG.

Part: SUPPORT — CORRODED (BS 1212 L28-29) · airframe 62,386 hrs · 47,642 cycles

AFT CARGO BAY, CORROSION ON SUPPORT AFT OF BS 1212 BETWEEN LONGERNS 29 AND 28. REPAIRED IAW SRM 51-30-0.

Part: SHEAR WEB — CORRODED (BS 845 LBL 60) · airframe 62,386 hrs · 47,642 cycles

DURING DVI REF ER/A 507041 PART 1, STEP 4, CORROSION NOTED AT BS 845 LT AFT SIDE LBL 60 ON SHEAR WEB TOP OF TANK AND FUEL BARRIER. COATING IS CRACKED. REPAIRED IAW SRM 51-24-0.

Part: CUSP WEB — CORRODED (FS 583-595) · airframe 62,386 hrs · 47,642 cycles

LEFT CUSP WEB CORRODED, FS 583-595 L18L. REPAIRED IAW SRM 53-05, FIG 131A 24.

Part: CUSP WEB — CRACKED (BS 905) · airframe 62,386 hrs · 47,642 cycles

RIGHT CUSP WEB CRACKED AT IMPROPER DAMAGE REMOVAL SITE FS 905 ATCUTOUT FOR FUSELAGE FRAME. REPAIRED IAW SRM 51-30-2.

Part: SUPPORT — CRACKED (LT WING) · airframe 62,386 hrs · 47,642 cycles

LT WING L/E PANEL SUPPORT CRACKED AT APPROX XRS 220 FLANGE. REPAIRED ON ER/A 509999-14 REV ORIG.

Part: FRAME — CRACKED (L8R) · airframe 62,386 hrs · 47,642 cycles

AFT ACCY COMPT FRAME WEB CRACKED AT L8R.

Part: FRAME — CRACKED (BS 1174 L5-7L) · airframe 62,386 hrs · 47,642 cycles

MAIN CABIN FRAME IS CRACKED 2 PLACES, STA 1174 BETWEEN LONGERON 5L TO 7L. REPAIRED IAW ER/A 507858-14, REV ORIG.

Part: SKIN — CORRODED (BS 629 L 29-30R) · airframe 62,386 hrs · 47,642 cycles

MID CARGO LOWER BILDGE SKIN REPAIR FILLER HAS CORROSION AT BS 629 BETWEEN L-30-29R. REPAIRED IAW ER/A 094196-14, REV D.

Part: WEB — CORRODED (FS 200) · airframe 62,386 hrs · 47,642 cycles

FLOOR WEB CORRODED FS 200, RBL 19. REPAIRED IAW SRM 51-30-2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,386 hrs · 47,642 cycles

FUSELAGE CREASED BELOW FWD CARGO DOOR CUTOUT. REPAIRED IAW ER/A 507676-14, REV ORIG.

Part: DOOR FRAME — CORRODED (FWD CARGO) · airframe 62,386 hrs · 47,642 cycles

FWD CARGO COMPARTMENTS LWR DOOR FRAME HAS CORROSION . REPAIRED IAW SRM 51-30-5.

Part: ATTACH FITTING — CORRODED (E/E DOOR FRAME) · airframe 62,386 hrs · 47,642 cycles

E & E COMP DOOR FRAME, RT FWD ATTACH FITTING HAS CORROSION INSIDE LIGHTING HOLE. REPAIRED IAW SRM 51-30-5.

Part: STRUCTURE — CRACKED (BS 1510) · airframe 62,386 hrs · 47,642 cycles

EMPENNAGE STA 1510 CANT HAS CRACK JUST ABOVE SPRING RELEASE AT 11 O`CLOCK POS LT FACING FWD. REPAIRED IAW ER/A 507062-14, REV ORIG.

Part: ANGLE — CORRODED (BS 1338-1344) · airframe 62,386 hrs · 47,642 cycles

ANGLE CORRODED L30 BETWEEN P DOME AND APU SHROUD SUPPORT BS 1338-1344. REPLACED ANGLE IAW SRM 51-30-2.

Part: ATTACH ANGLE — CRACKED (LWS 993) · airframe 62,386 hrs · 47,642 cycles

LEFT WING ATTACH ANGLE CRACKED IN TWO PLACES LWS 993. REPAIRED IAW ER/A 507061-14 REV 0.

Part: CUSP WEB — CRACKED (BS 807-845) · airframe 62,386 hrs · 47,642 cycles

ON REMOVAL OF CUSP WEB BS 807-845, FOUND CRACKED ON AFT END OF FASTNER HOLE AND ON FWD END AT EXISTING REPAIR CORROSION ON UPPER AND LOWER SURFACE. INSTALLED DOUBLER IAW SRM 53-05-7047.

Part: LONGERON — CRACKED (BS 465 L4R) · airframe 62,386 hrs · 47,642 cycles

MAIN CABIN BS 465, LONGERON 4R IS CRACKED. REPAIRED IAW SRM 53-02, FIG 18, SHT 1. WHICH INCLUDES ER/A 507689-14 REV 0, RIG.

Part: CUSP WEB — CRACKED (BS 200 RBL 52) · airframe 62,386 hrs · 47,642 cycles

RT CUSP WEB CRACKED APPROX FS 200, RBL 52. REPAIRED IAW SRM 51-30-1.

Part: FRAME — CRACKED (BS 1510) · airframe 62,386 hrs · 47,642 cycles

EMPENNAGE BS 1510 CANT HAS CRACK JUST ABOVE SPRING RELEASE AT 11 O`CLOCK POS LT FACING FWD. REPAIRED IAW ER/A 507062-14, REV ORIG.

Part: CUSP WEB — CORRODED (BS 1250 LBL 54) · airframe 62,386 hrs · 47,642 cycles

ON REMOVAL OF SEAT TRACK LBL 54 FOUND CORROSION ON TOP OF CUSP WEB AT BS 1250 TO 1307 LBL 54. REPAIRED IAW SRM 53-05, FIG 131A-10.

Part: SKIN — DENTED (FUSELAGE) · airframe 62,386 hrs · 47,642 cycles

FUSELAGE CREASED BELOW FWD CARGO DOOR CUTOUT REJ REF N/R SUPPLEMENT 51464. NO REF GIVEN SUPPORTING ACTION TAKEN EXTERNAL DOUBLER, EXTERNAL SURFACE CLAD LAYER REMOVAL BY DIE GRINDER AND 2" S BRITE DISK PRIOR TO ALODINE APPLICATION. REPAIRED IAW ERA 507676-14, ORIG.

Part: TORQUE BOX — CORRODED (BS 636-693) · airframe 62,386 hrs · 47,642 cycles

MID CARGO DOOR CUTOUT LOWER TQ BOX UPPER SURFACE HAS CORROSION FROM BS 636 TO 693. REPAIRED IAW ER/A 507857-14, REV ORIG.

Part: CUSP WEB — CORRODED (BS 1193-1212) · airframe 62,386 hrs · 47,642 cycles

CORROSION AROUND FASTENERS AT LONGERON 18R CUSP WEB FS 1193 TO FS 1212. REPLACED CUSP WEB IAW MD-88 51-30-1.

Part: LONGERON — CORRODED (BS 1269 - 1338) · airframe 62,386 hrs · 47,642 cycles

ON REMOVAL OF LONGERON 23L BS 1269 TO 1338, FOUND LONGERON END FITTING WITH CORROSION (EXFOLIATION) AT STA 1335. REPLACED LONGERON END FITTING STA 1322 TO 1338 ON NRC 70001934190001.

Part: FRAME — CORRODED (BS 170 - 200) · airframe 62,386 hrs · 47,642 cycles

AFTER REMOVAL OF COMPOSITE FLOOR SUPPORT FOUND CORROSION ON FLOOR MAIN FRAME BS 170 - 200 RBL MULTIPLE PLACES. ACCOMPLISHED REPAIR IAW SRM 53-05D.

Part: FLOORBEAM — CORRODED (FS 200) · airframe 62,386 hrs · 47,642 cycles

UPON REMOVAL OF FLOOR SUPPORT, FS 200, LBL5 TO RBL5. FOUND CORROSION ON WEB WAS OUT OF LIMITS. ACCOMPLISHED REPAIR IAW ER/A 397952-14MA.

Part: CUSP WEB — CORRODED (BS 1250-1309) · airframe 62,386 hrs · 47,642 cycles

TWO SPOTS OF LIGHT CORROSION ON TOP OF RT CUSP WEB. BS 1250 RBL AND BS 1309, RBL 541. REPAIR IAW ER/A 398191-14MA.

Part: LONGERON — CORRODED (BS 1287-1309) · airframe 62,386 hrs · 47,642 cycles

AFT CARGO LONGERON 28L CORRODED STA 1287-1309. REPAIRED IAW SRM 53-02, FIG 19.

Part: FRAME — CORRODED (AFT CARGO BAY) · airframe 62,386 hrs · 47,642 cycles

AFT CARGO FRAME AT BS 1320 AFT BULKHEAD CORRODED FROM LONGERON 24 RT TO 22 LT. REPAIRED IAW SRM 53-03D, FIG2A.

Part: LONGERON — CORRODED (BS 1287-1309) · airframe 62,386 hrs · 47,642 cycles

AFT CARGO L29L CORRODED STA 1287-1309. REPAIRED SRM 53-02 FIG 14.

Part: PAN — CORRODED (AFT LAVATORY) · airframe 62,386 hrs · 47,642 cycles

AFT LAV SERVICE PAN HEAVILY CORRODED. REPLACED LAV PAN IAW SRM 51-30-1 & -2.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 62,386 hrs · 47,642 cycles

RT WING FUEL PANEL 1460C HAS CORROSION AND CHAFING ON THE FLANGE. REPLACED FUEL PANEL IAW SRM 51-30-5.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 62,386 hrs · 47,642 cycles

FWD CARGO COMPARTMENT LWR DOOR JAMBHAS CORROSION TO INCLUDE AROUND AND UNDER BOTH STOP MOUNT ASSY'S REPAIRED IAW SRM 53-05, FIG 44.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 62,386 hrs · 47,642 cycles

LT WING FUEL PANEL 1361L HAS CORROSION AND CHAFING ON FLANGE. REPLACED FUEL PANEL. INSTALLED IAW OPN 3551AD.

Part: SEAT TRACK — CORRODED (BS 1309-1174) · airframe 62,386 hrs · 47,642 cycles

SEAT TRACK GOUGED AND CORRODED FROM BS 1309-1174. REPLACED SEAT TRACK IAW SRM 51-30-1 & 5.

Part: LONGERON — CORRODED (BS 1269-1338) · airframe 62,386 hrs · 47,642 cycles

AFT CARGO LONGERON 23L CORRODED BS 1269-1338. ACCOMPLISHED REPAIR IAW SRM 53-02, FIG 18.

Part: CUSP WEB — CORRODED (BS 1098 - 1174) · airframe 62,386 hrs · 47,642 cycles

CORROSION ON FLOOR SKIN & AROUND FASTENERS AT LONGERON 18R BETWEEN FS 1155 & 1174. REPLACED FLOOR SKIN (CUSP WEB) FROM FS 1098 TO 1174 IAW SRM 51-30-1, 51-30-2, & 51-30-5.

Part: SEAT TRACK — WORN (FS 408-455) · airframe 62,386 hrs · 47,642 cycles

LEFT OTBD SEAT TRACK WORN, CORRODED AND BARE METAL SHOWING IN FOUR PLACES, FS 408-455. REPAIRED IAW SRM 53-05, FIG 4F.

Part: CUSP WEB — CORRODED (FS 546 L18L) · airframe 62,386 hrs · 47,642 cycles

LEFT CUSP WEB CORRODED, BS 546 L18L. REPAIRED IAW SRM 53-05, FIG 131A-24.

Part: CUSP WEB — CORRODED (BS 563-571 L18R) · airframe 62,386 hrs · 47,642 cycles

RT CUSP WEB CORRODED FS 563-571, L18R. REPLACED CUSP WEB SRM 51-30-2 AND 51-30-50.

Part: CUSP WEB — CORRODED (BS 636-655 L18R) · airframe 62,386 hrs · 47,642 cycles

RT CUSP WEB CORRODED ON WEB & AROUND SEVERAL FASTENERS FS 636-655 L18R. REPLACED WITH NEW CUSP WEB IAW SRM 51-30-1.

Part: CUSP WEB — CORRODED (FS 541 L18R) · airframe 62,386 hrs · 47,642 cycles

RT CUSP WEB CORRODED FS 541, L18R. REPLACED CUSP WEB IAW SRM 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 565 L18L) · airframe 62,386 hrs · 47,642 cycles

LEFT CUSP WEB CORRODED BS 565 L18L. REPAIRED IAW SRM 53-05, FIG 131A-24.

Part: MEMBRANE — CORRODED (BS 200 RBL 18-22) · airframe 62,257 hrs · 47,548 cycles

ON REMOVAL OF FLOOR SUPPORT CHORD FOR ACCESS ON N/R 256736. FOUND CORROSION ON FLOOR MEMBRANE UNDERCHORD STA 200 RBL 18-22 IN MAIN CABIN. REPAIRED IAW SRM 53-05D, FIG 825D.

Part: WIRE — DAMAGED (CABIN) · airframe 61,531 hrs · 47,033 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY ESCAPE LIGHTING IN THE AFT CABIN WAS INOPERATIVE. MAINTENANCE REPAIRED THE WIRING AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 61,329 hrs · 46,892 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 18E IN THE CABIN, WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: CIRCUIT BREAKER — FAILED (EMERGENCY LIGHTS) · airframe 61,100 hrs · 46,736 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY LIGHTS FROM ROX13R TO 34R INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHTS ARM AND CHARGE CIRCUIT BREAKER. OPS CHECKED GOOD.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 61,096 hrs · 46,734 cycles

WHILE IN WORK ON INTERIOR MODIFICATION, FOUND PREVIOUS REPAIR ON CUSP MEMBRANE TO BE CORRODED BS 1174 LBL 55. REMOVED PREVIOUS REPAIR, FABRICATED NEW REPAIR PARTS, AND INSTALLED PER SRM 53-02 PARA 144.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 61,096 hrs · 46,734 cycles

WHILE IN WORK ON INTERIOR MODIFICATION FOUND PREVIOUS REPAIR ON CUSP MEMBRANE TO BE CORRODED AT BS 1174 LBL 55. REMOVED PREVIOUS REPAIR. FABRICATED NEW REPAIR PARTS AND INSTALLED PER SRM 53-05 PARA 144. C/W AT ATS.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 61,096 hrs · 46,734 cycles

DURING CABIN INTERIOR MODIFICATION AT ATS FOUND CORROSION ON CUSP MEMBRANE AT BS 1140-1175 LBL 45 AT FWD GIRT BAR FITTING. CORROSION IS BEYOND SRM LIMITS. REMOVED CORRODED MEMBRANE AND SPLICED IN A NEW SECTION OF MEMBRANE PER SRM 53-05 PAGE 907 REPAIR 144 AND DRAWING SG09530019.

Part: LANYARD — MISROUTED (TAILCONE) · airframe 59,441 hrs · 45,592 cycles

PER ERA 10-493276-14 MAINTENANCE FOUND TAIL SLIDE LANYARD AT LEFT AND RIGHT NOT INSTALLED CORRECTLY. MAINTENANCE ROUTED LANYARD STRAP PER AMM 25-61.

Part: SOCKET — OVERHEATED (CABIN) · airframe 59,369 hrs · 45,541 cycles

JUST BEFORE PUSHBACK NUMEROUS PASSENGERS COMPLAINED OF A BURNING ODOR IN CABIN. MAINTENANCE FOUND OVERHEAD LIGHT SOCKET ABOVE PAX SEAT 20DE BURNT AND PLASTIC STARTED TO MELT. THIS WAS THE CAUSE OF BURNING SMELL. LIGHT SOCKET PN BV04055N-01-84 NIS IN ATL. OVERHEAD LIGHT WAS DISCONNECTED, CONNECTOR STOWED, BULB REMOVED, AND WAS FORWARDED TO MCO/PLAC AT SEAT 20DE. CURRENTLY ON MCO.

Part: SKIN — MISMANUFACTURED (HORIZONTAL STAB) · airframe 58,233 hrs · 44,763 cycles

WORKING THE STABILIZER LT HORIZ LOWER SKIN/SKIN SPLICE IAW EA 09-460214-12 AD, REV D ME-03 FOUND A TYPOGRAPHICAL ERROR IN THE FASTENER CALL-OUT OF A SYMBOL G FASTENER AND BARREL NUT COMBINATION AND SHOULD HAVE BEEN A SYMBOL E FASTENER (HTL435-6-Y) IAW SR 09550028, ENGINEERING PROVIDED ERA 487860-14, AD REV ORIG TO COVER THIS DEVIATION FROM THE DWG.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,226 hrs · 44,756 cycles

DURING LINE CHECK MAINTENANCE FOUND TAIL COMPARTMENT LIGHTS L2-637, L2-638, & L2-639 LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY POWER SUPPLY B5-28. OPERATION OF LIGHTS NOW CHECKS GOOD. (2010-D1407) (DLM88103256)

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 574,636 hrs · 44,253 cycles

CORROSION AT C-3 CARGO COMPARTMENT THRESHOLD AREA. REPAIRED PER ERA 484416-14.

Part: WIRE — LOOSE (CABIN) · airframe 57,386 hrs · 44,201 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT 3C TO BE INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE AND REPAIRED IT. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (2010-D0845). (DLM88101915)

Part: WIRE HARNESS — SHORTED (EMERGENCY LIGHT) · airframe 56,355 hrs · 43,524 cycles

CABIN EMERGENCY PATH LIGHTING INOP AT 18ED AND 31ED. RELAMPED ROW 18. CHECKS GOOD. REPLACED SHORTED WIRE HARNESS ON 31ED. CKS GOOD.

Part: LIGHT — INOPERATIVE (OVERWING) · airframe 56,167 hrs · 43,413 cycles

BOTH EXTERIOR OVERWING EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY NO HELP. REPLACED RT LIGHT ASSY FOR HIGH RESISTANCE AND SECOND POWER SUPPLY SYS OPN NML. MCO/PLAC REMOVED.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 55,691 hrs · 43,108 cycles

CRACK INDICATION FOUND AT TWO HOLES COMMON TO THE VERTICAL STABILIZER FRONT SPAR LIGHT AND RT CHORDS, AT LOWER SKIN PANEL. THE TWO DAMAGED HOLES ARE EXACTLY SITUATED AT THE UPPER MOST LOCATION OF THE SKIN PANEL (6TH HOLE FROM BOTTOM OF THE INSPECTION AREAS ON BOTH SIDES). REPAIRED ON ER/A 478044-14 ORIG: VERTICAL STABILIZER / FRONTSPAR / RT AND LT CHORD / ZFS=52 / FATIGUE CRACKS.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 55,691 hrs · 43,108 cycles

ON UPPER LEADING EDGE PANEL NUMEROUS HOLES WERE FOUND ELONGATED, WITH VISIBLE CRACKS IN THE COUNTERSINKS OF THE FASTENERS. REPAIRED ON ER/A 478045-14 ORIG: VERTICAL STABLIZER / UPPER FIXED LEADING EDGE / ZFS=52 / HOLE DAMAGE.

Part: WARNING LIGHT — FALSE ACTIVATION (NLG) · airframe 53,750 hrs · 41,857 cycles

AFTER TO NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION COMPLIED WITH QRH CYCLED GEAR DOWN BACK UP AND NOSE GEAR STILL NOT RETRACTED. ACFT BUFFET CONFIRMED NOSE GEAR NOT RETRACTED. GEAR EXTENDED NORMALLY. RETURNED TO IAD, NO DAMAGE NOTED.

Part: FRAME — CHAFED (BS 1497)

FUSELAGE FRAME STA 1497 CANT HAS CHAF AT 8 O'CLOCK. CUT OUT CHAFED AREA FS 1497 IAW MD-80 SRM 53-03D FIG 4. HFEC NO CRACKS NOTED. FABRICATED AND INSTALLED REPAIR 2.4" BY 18.0" FROM 7075-T6 .050" MD-80 SRM 51-10-3, 51-70-5.

Part: BULKHEAD — CORRODED (BS 1338) · corrosion level 2

CORROSION ON AFT PRESSURE BULKHEAD LWR T-CHORD AND SURROUNDING AREAS IN AFT CARGO AT FS 1338 AND BETWEEN LONGERONS 24L AND 24R. REMOVED AND REPLACED WEB DOUBLER FABRICATED 6.0" BY 4.90" FROM 7075-T6 CLAD .080" IAW DELTA DC-9/MD-80 SRM 51-30-2, 51-10-2.

Part: SKIN — GOUGED (FUSELAGE)

LT I/B FLAP LOWER SKIN GROUP OF NICKS AT 16 INCHES FROM I/B EDGE. BLENDED GOUGES OUT OF LT I/B FLAP LOWER SKIN. REMOVED AND REPLACED SKIN 22-3/4" BY 1-3/8", 24-7/8" BY 4" FROM 7075-T6 .063 AND 42-1/4" BY 25" FROM 7075-T6 .040" AND LOWER TEE REPAIR 41" BY 12.6" FROM S2914520S IAW DELTA DC-9/MD-80 SRM 51-30-3, 51-60-0 AND DELTA DWG NR 57-0506.

Part: SKIN — LIGHTNING STRIKE (BS 655)

LIGHTNING STRIKE AT FS 655 LONGERON 1 AND 2R. CUT OUT LIGHTNING STRIKE AREA. FABRICATED AND INSTALLED DOUBLER 6.25" X 6.40" FROM 6AL-4V TITANIUM .040" IAW DC-9/MD-80 SRM 53-04D FIG 38, 51-10-3D.

Part: SKIN — DENTED (FUSELAGE)

S/O 291020, NR 32111 DENT EXT FUSELAGE SKIN AT C-1 DOOR AFT UPPER CORNER. FABRICATED REPAIR DOUBLER 15.5 INCH X 13 INCH X 2.5 INCH X 2.5 INCH FROM 2024-T3 .160 INCH IAW SRM 51-10-3, 51-30-5 AND 51-30-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2

S/O 291020 N/R 32059 RT OB SEAT TRACK AT FS 418-800 RBL 54 CORRODED. REMOVED CORRODED SEAT TRACK, CUT AND INSTALLED 48 FOOT SECTION OF TRACK P/N 5930547U70 IAW SRM 51-10-4 AND 53-05D.

Part: SKIN — LIGHTNING STRIKE (BS 1170)

LIGHTNING STRIKE AT FS 1170 LONGERON 1. FABRICATED AND INSTALLED DOUBLER 5.3" X 5.7" FROM 2024-T3 .032" IAW DC-9/MD-80 SRM 53-04D FIG 38, 51-10-3D.

Part: CUSP WEB — CORRODED (BS 1174-1193) · corrosion level 2

CORROSION ON CUSP WEB AT FS 1174 RT TO 1193 RT. BLENDED, FABRICATED AND INSTALLED DOUBLER AND FILLER 12 INCHES X 7.5 INCHES, 5.5 INCHES X 3.5 INCHES FROM 7075-T6 .020 INCHES IAW REPAIR DOCUMENT 53-20-02D, FIG 802 DATED 03-05-2003, AND SRM 51-10-3D.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2

CORROSION AROUND FASTENER HOLES ON UPPER SURFACE OF CABIN FLOORBEAMS UNDER LT AFT LAV AT FS 1322 B/L 22L TO B/L 44L. FABRICATED AND INSTALLED REPAIR STRIP 4.02 INCHES X .090 INCHES FROM STAINLESS STEEL .025 INCHES IAW SRM 53-01, 53-05D FIG 20, AND 51-10-3.

Part: SKIN — DENTED (BS 229)

DENT IN SKIN FS 229, L-17L TO L-18L REQUIRES PERMANENT REPAIR. REMOVED TEMP EXISTING DOUBLER PER DELTA ERA 365805-14. FABRICATED AND INSTALLED DOUBLER 17-1/2" BY 16-1/2" FROM 2024-T3 .063" AND FILLER 14" BY 13" FROM 2024-T3 .050" ALUM SHEET AND 2 FINGER DOUBLERS 8-3/8" BY 2-3/4", 6-1/4" BY 2-7/8" FROM 2024-T3 .025" IAW DELTA ERA 096199-14 REV IR DC-9/MD-80 SRM 51-30-1, 51-30-2, 51-30-5, 53-04D FIG 12B, AND 51-10-3D.

Part: SKIN — CRACKED (LT WING)

LEFT WING L/E SKIN PLATE HAS CRACK JUST AFT OF NR 2 SLAT LEFT WING REQUIRES PERMANENT REPAIR. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED SKIN REPAIRS 6.5 X 6.25 INCHES FROM 7075-T6 .063, 4.25 X 4.25 INCHES FROM TI-6AL-4V .063, 3.25 X 4.25 INCHES FROM 7075-T6 .050 AND 2.5 X 4.25 INCHES FROM 7075-T6 .100 IAW DELTA ERA 380953-14MA REV ORIG.

Part: SKIN — DENTED (BS 1322 S20R)

DENT IN FS 1322, L-20R REQUIRES PERMANENT REPAIR. REMOVED TEMP EXISTING DOUBLER. FABRICATED AND INSTALLED DOUBLER 7" BY 4-3/4" FROM 2024-T3 .063" AND FINGER DOUBLER 8-5/8" BY 6-3/4" FROM 2024-T3 .025" IAW DC-9/MD-80 SRM 51-30-2 PG 1, 53-04D FIG 38, AND 51-10-3D PG 1.

Part: MOTOR — FAILED (TRIM SYS) · airframe 47,477 hrs · 37,747 cycles

ACFT PRIMARY TRIM INOP NOSE DOWN AFTER TAKEOFF. REPLACED TRIM MOTOR.

Part: SKIN — CORRODED (FS L-30) · airframe 45,046 hrs · 36,008 cycles

FUSELAGE SKIN FS 630 LONGERON 29-30 RT : THE FUSELAGE SKIN AND UNDERLYING DOUBLER WERE FOUND CORRODED AT FS 630 BETWEEN LONGERON 29R AND 30. THE CORROSION WAS REMOVED WITH A 9 INCH X 5 INCH CUTOUT IN THE SKIN AND A 7 INCH X 5 INCH CUTOUT IN THE DOUBLER. THE CUTOUTS WERE REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS IAW ER/A 094196-14.

Part: LIGHT — MISSING (CABIN) · airframe 42,991 hrs · 34,570 cycles

DURING LAYOVER CHECK FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. FOUND ALL BULBS MISSING FROM ASSEMBLY. RELAMPED, OPS CHECKS NORMAL.

Part: CONTROL PANEL — DENTED (E/E BAY) · airframe 42,823 hrs · 34,451 cycles

FOUND E/E DOOR DENTED POWER CONTROL PANEL AT DOOR HOLD OPEN SUPPORT BRACKET. FOUND RELAY WIRES ARCHING BEHIND PANEL ASSY ON RACK SUPPORT BRACKET. REPAIRED WIRING.

Part: ENGINE — MAKING METAL (NR 2) · airframe 38,730 hrs · 31,642 cycles

RT ENG OIL STRAINER CLOG LIGHT ILLUMINATED SHORTLY AFTER T/O. IAW POM PROCEDURES RETARDED THE THROTTLE. THE STRAINER MESSAGE STAYED ON SO THE ENGINE WAS SHUTDOWN. RETURNED TO DFW. FOUND METAL IN OIL FILTER AND ON MCD. REPLACED FILTER AND CLEANED MCD. RAN ENG AND REINSPECTED MCD AND FILTER PER M/M 72-00-02-1 FIGURE 113A. FOUND METAL ON MCD. CHANGED ENGINE.

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 34,225 hrs · 28,347 cycles

OBSERVER OXYGEN MASK BROKEN. REPLACED OBSERVERS MASK, OPS CHECK AND LEAK CHECK OK.

Part: SKIN — DENTED (FS 218)

THE FUSELAGE SKIN AT FS 218 BETWEEN STRINGERS 18L AND 20L WAS FOUND DENTED/DEFORMED. THE DAMAGED AREA OF SKIN WAS CUTOUT OVER A 13.5 X 3.75 AREA. THE SKIN CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 365809-14, REV A.

Part: SKIN — GOUGED (BS 390)

THE FUSELAGE SKIN JUST ABOVE THE C1 DOOR CUTOUT WAS GOUGED BY GROUND EQUIPMENT. THE GOUGE WAS TO THE SKIN ONLY AND WAS CUT OUT. THE CUT OUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 365804-14, REV A.

Part: APU — CONTAMINATED (AFT)

FOUND APU INLET SOAKED WITH DE-ICING FLUID AND OIL MIX. DURING TAKEOFF DUCTS GOT HOT CAUSING BURNING SMELL IN CABIN. INOP APU.

Part: FAN — FAILED (CABIN)

SMOKE AND NOXIOUS FUMES IN MID CABIN AREA AFTER T/O. FOUND CABIN AIR RECIRCULATION FAN SIEZED. REPLACED FAN, RAN FAN AND AC PACKS TO PURGE DUCTS.

Part: AIR DISTRIBUTION — ODOR (CABIN)

ELECTRICAL SMELL AFTER TAKEOFF, CONTRACT MAINTENANCE INSPECTED APU INLET AND SURROUNDING AREAS. NO FLUIDS NOTED, RAN PACKS, NO SMELL NOTED.

Part: COALESCER BAG — CONTAMINATED (CABIN)

SET UP TO REPLACE BOTH WATER SEPARATOR BAGS DUE TO SMOKE IN CABIN IN RSW - REPLACED SAME - RAN PACKS WITH ENGINE AIR - NO SMOKE NOTED.

Part: DUCT — CRACKED (RT PACK)

DURING CLIMBOUT, HAD TAIL COMPARTMENT OVERHEAT. ISOLATED PROBLEM TO RIGHT PACK, SHUT PACK DOWN, LIGHT OUT, AND CONTINUED FLIGHT. FOUND CRACKED DUCT AT RIGHT PACK. REPLACED DUCT OPERATION NORMAL.