N926DL

Part: SKIN — CORRODED (BS 1155-1212) · corrosion level 2 · airframe 74,988 hrs · 56,497 cycles

AFT CARGO HAD MULTIPLE AREAS OF CORROSION ON INNER SKIN UNDER CARGO DOOR BEAM BETWEEN BS 1155 AND 1212. COMPLIED WITH PRI ER/A 560725-14, REV 0, AND ER/A 560725-14, REV ORIGINAL. RECEIVED FINAL ER/A 560725-14, REV ORIGINAL.

Part: THRESHOLD — DAMAGED (AFT CARGO DOOR) · corrosion level 2 · airframe 74,988 hrs · 56,497 cycles

AFT CARGO DOOR THRESHOLD FWD AND AFT OF DOOR STOP FITTINGS. NUMEROUS FASTENER AND RIVNUT HOLES ARE OUT OF ROUND AND CORRODED BS 1155 - 1212. BEAM INSTALLATION COMPLETED IAW DWG 5930483.

Part: TEE FITTING — CORRODED (BS 1212) · corrosion level 2 · airframe 74,988 hrs · 56,497 cycles

AFT CARGO BAY LONGERON 28 AND 29R, BS 1212 LIGHT CORROSION ON TEE BRACKET. REPLACED THE TEE BRACKET IAW DWG 5930483.

Part: TEE FITTING — CORRODED (BS 1231) · corrosion level 2 · airframe 74,988 hrs · 56,497 cycles

AFT CARGO BAY LONGERONS 28 AND 29R, BS 1231 FOUND CORROSION ON TEE BRACKET. REPLACED THE TEE BRACKET IAW DWG 5930483.

Part: STRAP — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 74,988 hrs · 56,497 cycles

AFT CARGO DOOR FRAME STRAP CORRODED. THE STRAP WAS REPLACED.

Part: SHEAR TIE — CORRODED (BS 1212) · corrosion level 2 · airframe 74,988 hrs · 56,497 cycles

AFT CARGO, CORROSION ON SHEAR TIE BS 1212 BETWEEN LONGERONS 29-30R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-10-03, AND 51-30-05.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 74,261 hrs · 55,924 cycles

L1 DOOR SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED THE SLIDE IAW AMDS 2561-4964.

Part: FITTING — CRACKED (SPOILER ACTUATOR) · airframe 73,563 hrs · 55,408 cycles

RIGHT WING GROUND SPOILER ATTACH FITTING CRACKED AT ACTUATOR FWD POINT. REPLACED THE FITTING ASSY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,563 hrs · 55,408 cycles

CEILING EMERGENCY LIGHTING INOP-ROWS 16 THROUGH 20. REMOVED AND REPLACED B5-102 BATTERY PACK PER AMM 33-53.

Part: WIRE — BROKEN (CABIN) · airframe 73,563 hrs · 55,408 cycles

SEAT EMERGENCY LIGHT INOP ROW 31-36. FOUND BROKEN WIRE AT SEAT 31. REPAIRED WIRE PER SWPM 20-10-03.

Part: SKIN — DAMAGED (BS 1128) · airframe 73,560 hrs · 55,406 cycles

SKIN BS 1128, STRINGER 29L DAMAGED. REPAIRED IAW PRI 554017 REV. 0 AND REV. 1 AND ER/A 554017-14 REV. ORIGINAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,486 hrs · 55,357 cycles

FWD RED EMER LIGHT INOP. RELAMPED PER AMM 33-53.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 71,950 hrs · 54,226 cycles

SEAT ROW 34ED EMERGENCY LIGHT INOPERATIVE. REPLACED PIGTAIL LIGHT ASSEMBLY, OPS NOW OK IAW AMM 33-51.

Part: CAM — LOOSE (TAILCONE JET) · airframe 71,692 hrs · 54,023 cycles

TAILCONE JETTISON CAM ASSY LOOSE. RIGGED JETTISON CAM IAW AMM 53-50.

Part: SKIN — NOT REPORTED (RUDDER) · airframe 71,692 hrs · 54,023 cycles

RUDDER FLAME SPRAY BAD. REPLACED RUDDER IAW WC 2720-4187.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,662 hrs · 54,003 cycles

EMERGENCY LIGHT ON SEAT 26RT IS INOPERATIVE. REPLACED WIRING HARNESS ON SEAT 26 RT.

Part: SKIN — CRACKED (BS 535) · airframe 71,472 hrs · 53,875 cycles

CRACKED FUSELAGE SKIN IN BS 535 BETWEEN LONG 18R AND 19R. REPAIRED IAW ETI-88-16-080 REV 3 AND ER/A 543170-14, REV ORIGINAL.

Part: SHEAR ANGLE — DAMAGED (BS 1338) · airframe 71,472 hrs · 53,875 cycles

MINIMUM FASTENER REQUIRMENT ON SHEAR ANGLE FWD TAB, EITHER SIDE OF THE LOWER TEE CHORD CUT LINE DOES NOT COMPLY BS 1338 BETWEEN LONGERONS 26-27L, & 26-27R. REPAIR WAS PERFORMED IAW ER/A 543163-14, REV ORIGINAL

Part: PAN — CRACKED (L1 DOOR) · airframe 71,472 hrs · 53,875 cycles

CRACKED PAN INNER STRUCTURE AFT EDGE OF FWD MAIN ENTRANCE DOOR, L1 ON AFT UPPER CORNER POSITION. DUE TO EXCESSIVE DAMAGE THE L1 DOOR WAS REPLACED AND WILL BE INSTALLED UNDER CARD 48, ZONE 201.

Part: SKIN — CORRODED (BS 1250-1271) · corrosion level 2 · airframe 71,472 hrs · 53,875 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER AT FUSELAGE SKIN INNER STRUCTURE BETWEEN BS 1250- 1271 AND LONGERON 29RT AND LONGERON 28RT AT AFT CARGO COMPARTMENT INNER STRUCTURE. DOUBLER WAS REPLACED IAW ETI-88-16-078, REV 1 AND ER/A 543166-14, REV ORIGINAL.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 71,472 hrs · 53,875 cycles

CRACKED INTERCOSTAL BETWEEN BEAM NR 4 AND 5 AT L1 PASSENGER DOOR. INTERCOSTAL WAS REPLACED IAW SRM 51-30-2, 51-10-4, 51-10-3 PAR 14/21 AND DWG: 9955763, REV: M.

Part: INTERCOSTAL — CORRODED (BS 1212-1231) · corrosion level 2 · airframe 71,472 hrs · 53,875 cycles

CORROSION ON INTERCOSTAL BETWEEN BS 1212 TO 1231 LONGERON 29LT AT AT AFT CARGO COMPARTMENT STRUCTURE. INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · airframe 71,472 hrs · 53,875 cycles

ELONGATED HOLE ON FUEL ACCESS PLATE NR 1454C. FUEL ACCESS PLATE NR 1454C WAS REPLACED IAW IPC 57-30-00 AND WIL BE INSTALLED UNDER CARD 5710-01110-05, JOB 022-0001.

Part: DOOR FRAME — CORRODED (BS 1155-1190) · corrosion level 2 · airframe 71,472 hrs · 53,875 cycles

CORROSION ON AFT CARGO COMPARTMENT DOOR JAMB UPPER BEAM FROM BS 1155 TO 1190. BEAM WAS REPLACED IAW SRM 51-30-5, 51-10-4, 51-10-3, PAR 14 AND 21.

Part: BEAM — CRACKED (L1 DOOR) · airframe 71,472 hrs · 53,875 cycles

CRACKED BEAM NR 1 AFT EDGE AT FWD MAIN ENTRANCE DOOR. L1, BEAM NR 1 AFT EDGE AT FWD MAIN ENTRANCE DOOR WAS REPAIR IAW SRM 52-05D, FIG 81, SHEET 3, 51-30-1, 51-30-5 AND 51-10-3, PAR 14.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 71,472 hrs · 53,875 cycles

CRACKED INTERCOSTAL BETWEEN BEAM NR 4 AND NR 5 AND MECHANISM AT FWD MAIN ENTRANCE DOOR, L1. INTERCOSTAL MAIN ENTRANCE DOOR WAS REPLACE IAW SRM 51-30-2.

Part: DOOR FRAME — CRACKED (NLG DOOR) · airframe 71,472 hrs · 53,875 cycles

CRACKED PREVIOUS REPAIR ON NLG DOOR JAMB BS Y=46, X=+18LHZ=-29 AT NLG WHEEL WELL. DOUBLER PREVIOUS REPAIR WAS REPLACED IAW 53-05, FIG 110, 51-10-2, 51-10-4, 51-10-3 AND 51-30-2.

Part: BEAM — CRACKED (PAX DOOR) · airframe 71,472 hrs · 53,875 cycles

CRACKED BEAM NR 4 FWD EDGE AT FWD MAIN ENTRANCE DOOR. L1 BEAM NR 4 WAS REPAIRED IAW SRM 52-05 D FIG 88, SHEET 3, 51-30-1, 51-10-3, PAR 14, 51-10-2 AND 51-30-5.

Part: SKIN — NOT REPORTED (BS 1271) · airframe 71,472 hrs · 53,875 cycles

DURING NDT INSPECTION 2 DISCREPANT AREAS, DOUBLER REPAIRS WERE FOUND ON FUSELAGE SKIN AT BS 1271, BETWEEN LONGERON 1 AND 2 RT, ID TAG: "P" 6-25-12 ER/A 504801-14AD AND BS 1193, BETWEEN LONGERON 1 AND 3 LT.

Part: DOOR — CORRODED (STRUT) · airframe 71,472 hrs · 53,875 cycles

CORROSION ON SEATING AREA OF RUB STRIP AT RT MLG STRUT DOOR. RT MLG STRUT DOOR WAS REPLACED DUE EXCESIVE DAMAGE.

Part: DUCT — CRACKED (EXHAUST) · airframe 71,472 hrs · 53,875 cycles

CRACKED RATIO RACK EXHAUST DUCT BETWEEN BS Y=256 TO 275 LONG 20LT TO 21LT AT FUSELAGE SKIN. RADIO RACK EXHAUST DUCT WAS REPAIRED IAW ER/A 464964-14 MA, REV C.

Part: FRAME — CRACKED (BS 1510) · airframe 71,472 hrs · 53,875 cycles

CRACKED FRAME BS 1510 . THE FRAME WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3, PAR 21 AND 14.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 70,618 hrs · 53,259 cycles

A PASSENGER REPORTED A BROKEN WIRE ALONG THE GROUND NEAR THE SIDEWALL, AT ROW 20 IN THE CABIN. MAINTENANCE FOUND A WIRE FOR THE EMERGENCY LIGHTS AT ROW 20DE TO BE LOOSE AND IT WAS REPAIRED. THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 68,288 hrs · 51,673 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE EMERGENCY RELEASE CABLE WAS BULGED AND FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: LATCH — WORN (TAILCONE RELEASE) · airframe 68,288 hrs · 51,673 cycles

MAINTENANCE DISCOVERED THAT THE LT LOWER RELEASE LATCH ASSEMBLY FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE ASSEMBLY WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: BRACKET — WORN (TAILCONE RELEASE) · airframe 68,288 hrs · 51,673 cycles

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

Part: PAN — CRACKED (OVERWING) · airframe 68,288 hrs · 51,673 cycles

LEFT FWD OVERWING EMERGENCY DOOR PAN CRACKED AT UPPER AFT SUPPORT BRACKET. REMOVED LINER AND SUPPORT BRACKET. HFEC IAW NDT SPM 06-10-01.001 TO VERIFY CRACK AND MARK ENDS. REMOVED FASTENERS TO PEEL UP INNER SKIN FOR ACCESS. STOP DRILLED ENDS OF CRACK TO 1/4 DIA. AT MARKED LOCATIONS. HFEC IAW NDT SPM 06-10-01 CRACK CONTAINED WITHIN STOP DRILLS. INSTALLING DOUBLER. INSTALLED ALL FASTENERS. INSTALLED NEW CLIP. COMPLETED REPAIR IAW SRM 52-05D, FIG 51 AND ER/A 530841-14, REV 0, REF NR 14. ASSOCIATED ER/A 14-530841 ADDED FOR AC 0926.

Part: RECEPTACLE — WORN (TAILCONE RELEASE) · airframe 68,288 hrs · 51,673 cycles

MAINTENANCE DISCOVERED THAT ALL OF THE TAILCONE RELEASE SYSTEM GUIDE PIN RECEPTACLES WERE WORN BEYOND ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,038 hrs · 50,744 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE COCKPIT, L1, AND R1 OVERHEAD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE LIGHTS CHECKED NORMAL.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,619 hrs · 50,480 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE AFT RT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: UNKNOWN — ODOR (CABIN) · airframe 66,619 hrs · 50,480 cycles

CREW ELECTED TO TURN BACK AFTER TAKEOFF DUE TO BOTH AFT LAVATORY SMOKE DETECTORS SOUNDING AND PASSENGERS REPORT AN ODOR. MAINTENANCE INSPECTED BOTH ENGINES INLETS AND EXHAUST BUT FOUND NO DISCREPANCIES. NO TROUBLE WAS FOUND AND A DUCT BURNOUT WAS PERFORMED. ACFT HAS RETURNED TO SERVICE.

Part: WIRE — PULLED (EMERGENCY LIGHTS) · airframe 65,723 hrs · 49,913 cycles

DURING FUNCTIONAL CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT ROW 27DE INOPERATIVE. FOUND A WIRE PULLED LOOSE FROM THE SPLICE CONNECTOR, REPAIRED CONNECTOR & WIRE, AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: RUB STRIP — MISSING (CATWALK) · airframe 64,861 hrs · 49,276 cycles

PILOT DISCOVERED THAT THE CATWALK IN TAIL SECTION, WOULD NOT RETRACT BECAUSE A RETRACT PANEL WAS BINDING ON THE CEILING PANEL. THE SYS WAS FORWARDED AND PLACARD PROCEDURES WERE COMPLIED WITH. ON 17JUL, IT WAS FOUND THAT THE LT SIDE RUB STRIP WAS MISSING, BUT WAS REPLACED ON 18JUL. THE SYS WAS OPERATIONALLY CHECKED AND THE ACFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (BS 1510) · airframe 64,568 hrs · 49,065 cycles

BS 1510, FRAME CRACKED. RT UPPER, AT RUDDER PCU ATTACH. REMOVED UPPER RT TAILCONE LATCH, CUTOUT CRACKS, CUTOUT SIZE 1" X 1.375". HFEC INSP AND NO OTHER CRACKS FOUND. FABRICATED AND INSTALLED REPAIR WORK IAW ERA 515449-14, REV ORG ASSOCIATED ER/A 14-515449, ADDED FOR AC 0926.

Part: STRAP — DISCONNECTED (ESCAPE SLIDE) · airframe 64,568 hrs · 49,065 cycles

INSPECTION DISCOVERED EMERGENCY ESCAPE SLIDE COVER SECURING STRAPS DISCONNECTED. THE TAILCONE SLIDE COVER STRAPS WERE REINSTALLED AND AN RII WAS COMPLETED SATISFACTORILY.

Part: SKIN — CRACKED (BS 1437) · airframe 64,552 hrs · 49,059 cycles

FUSELAGE SKIN CRACKED AT BS 1437, BETWEEN LONGERON 2 - 3L. REPAIRED IAW ERA 515409-14, REV ORIGINAL.

Part: SKIN — CRACKED (BS 1437) · airframe 64,552 hrs · 49,059 cycles

FUSELAGE SKIN CRACKED AT BS 1437, BETWEEN LONGERON 2-3R, REPAIRED IAW ERA 515410-14, REV ORIGINAL.

Part: BUSHING — WORN (TAILCONE RELEASE) · airframe 64,552 hrs · 49,059 cycles

DURING AN INSPECTION, MX DISCOVERED THAT THE TAILCONE JETTISON RELEASE PULL-CABLE BUSHINGS, PIN 11, LATCH RECEPTACLE, AND ALIGNMENT PIN RECEPTACLES WERE ALL WORN BEYOND ALLOWABLE LIMITS. THE SYS WAS REPAIRED BY BUSHING REPLACEMENTS IAW AMM 53-53-00/02, SRM 51-30, AND AMDS 5350-01077-0101.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,494 hrs · 49,020 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT SEAT ROWS 1-4 INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,494 hrs · 49,020 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT SEAT ROWS 32-34 INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: WIRE — MISINSTALLED (EMERGENCY LIGHT) · airframe 64,494 hrs · 49,020 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MX FOUND A WIRE INSTALLED ON AN INCORRECT TERMINAL AT THE BATTERY PACK. THE BATTERIES AND THE BATTERY PACK WERE REPLACED AND THE WIRES INSTALLED IAW THE WDM. THE LIGHTS HAVE RETURNED TO AN OPS CONDITION.

Part: LANYARD — FRAYED (L2 DOOR SLIDE) · airframe 63,293 hrs · 48,162 cycles

L2 DOOR SLIDE LANYARD FRAYED. R & R SLIDE LANYARD IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,190 hrs · 47,362 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 31 OF THE CABIN ALL THE WAY THROUGH THE TAIL COMPARTMENT WERE INOPERATIVE. MAINTENANCE FOUND A SHORT AT A LIGHT ASSEMBLY IN THE TAIL COMAPRTMENT, REPAIRED IT, AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: SKIN — CORRODED (BS 1155-1174) · airframe 62,139 hrs · 47,324 cycles

AFT CARGO COMPARTMENT BILGE AREA BETWEEN STA 1155 AND 1174 LONGERON 29 L HAS POCKETS OF MATERIAL MISSING AT FASTENER LOCATIONS ON LOWER INTERIOR OF CHANNEL FOUND AFTER REMOVAL OF VHF ANTENNA MOUNT FITTINGS. BLENDED AREAS OF CORROSION, FOUND TO BE OUT OF LIMITS, ACCOMPLISHED ERA 503728-14 REV ORG.

Part: SKIN — GOUGED (BS 330-370) · airframe 62,139 hrs · 47,324 cycles

LEFT EXTERIOR FUSELAGE SKIN IS DENTED AND GOUGED FROM BS 330 TO 370 AND BETWEEN LONGERON 17L -15L. CUT AND REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND DOUBLERS. INSTALLED PER DC9/MD80 SRM 53-04.

Part: SKIN — CRACKED (BS 1271 1L) · airframe 62,139 hrs · 47,324 cycles

CRACK IN FUSELAGE SKIN COMING OUT OF FASTENER HOLE AT STA 1271 BETWEEN LONGERON 1L AND 1R. CUT OUT DAMAGE, FABRICATED INTERNAL REPAIR DOUBLER, FILLER AND INTERNAL FINGER DOUBLER AND INSTALLED IAW SRM 53-04-02.

Part: CUSP WEB — DAMAGED (BS 1230-1307) · airframe 62,139 hrs · 47,324 cycles

MULTIPLE RIVETS DIMPLED INTO CUSP WEB STRUCTURE, TOOLING MARKS AROUND RIVET HEADS STA 1230-1307 LBL 44-55. REMOVED CUSP WEB FROM 1250-1307, FABRICATED AND INSTALLED CUSP WEB IAW SRM 53-05.

Part: DOUBLER — CRACKED (BS 984) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN BS 984, WINDOW DOUBLER CRACKED AT CORNER FASTENER. REMOVED AND REPLACED WINDOW DOUBLER BETWEEN STA 984-1003 LT SIDE IAW DC9/MD80 SRM 51-30-05 DURING HMV ST AEROSPACE SAN ANTONIO.

Part: DOUBLER — CRACKED (BS 1231-1250) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN LT SIDE BETWEEN BS 1231-1250 UPPER AFT CORNER OF WINDOW DOUBLER CRACKED. REMOVED AND REPLACED WINDOW RING PLATE LT SIDE AT STA 1231-1250 IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 1032-1307) · airframe 62,139 hrs · 47,324 cycles

CORROSION AND CHAFE WEAR ON MAIN CABIN SEAT TRACK STA 1032-1307, X22. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-01 P1-24.

Part: CUSP WEB — CORRODED (BS 769-788) · airframe 62,139 hrs · 47,324 cycles

CORROSION ON CUSP WEB BETWEEN BS 769 TO 788 NEAR TO RBL 56 AT THE FLOOR CABIN RIGHT SIDE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREAS, FABRICATED, FILLERS, AND DOUBLERS AND INSTALLED IAW SRM 53-05.

Part: CUSP WEB — CORRODED (BS 826-845) · airframe 62,139 hrs · 47,324 cycles

CORROSION ON CUSP WEB BETWEEN STA 826-845 NEAR RBL 56 AT THE FLOOR CABIN RT SIDE. CUTOUT DAMAGE AREA PER MD80 SRM 53-05 FIG 131A-6 PG 908. FABRICATED AND INSTALLED FILLER DOUBLER RING DOUBLER IAW MD80 SRM 5305 CONFIG 7005 AND 7011 AND 51-30-2 PG24 FIG 20 AND 51-30-5 PAGR 7 AT STA 826-845.

Part: CUSP WEB — CORRODED (BS 750-769) · airframe 62,139 hrs · 47,324 cycles

CORROSION ON CUSP WEB BETWEEN STA 750 TO 769 NEAR TO RBL 56, AT THE FLOOR CABIN RIGHT SIDE. REMOVED CORROSION ON CUSP WEB, FOUND TO BE OUT OF LIMITS, REMOVED DAMAGE, FABRICATED FILLERS AND DOUBLERS AND INSTALLED IAW SRM 53-05.

Part: CUSP WEB — CRACKED (BS 1174-1212) · airframe 62,139 hrs · 47,324 cycles

IN CABIN, LT SIDE CUSP WEBBING JUST OTBD OF SEAT TRACK AT X=55, BS 1212 TO 1174 HAS CORROSION AT 1 FASTENERS, AT 1 CLIP AROUND LIGHTENING HOLES, 1 CRACK AT BS 1203, 4 CORRODED CLIPS. REMOVED CORROSION AT ALL AREAS, FOUND TO BE WITHIN LIMITS, CUT OUR CRACK DAMAGE AT BS 1203. FABRICATED FILLER, REPAIR DOUBLER AND RING DOUBLER AND INSTALLED IAW SRM 53-05.

Part: CUSP WEB — CORRODED (BS 655-674) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN LEFT CUSP WEB HAS CORROSION BETWEEN BS 655 TO 674 LBL 59. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED CUSP WEB, FABRICATED, FILLERS AND DOUBLERS AND INSTALLED IAW SRM 53-05.

Part: CUSP WEB — CORRODED (BS 1041-1003) · airframe 62,139 hrs · 47,324 cycles

CUSP WEB OTBD OF X55 SEAT TRACK STA 1041-1003 HAS CORROSION AT INBD EDGE TOP SIDE AT SEAT TRACK, OUT OF LIMITS. FABRICATED DOUBLER AND FILLER AND FRAME FITTING AND INSTALLED REF MD80 SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 395-799) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN SEAT TRACK AT RBL 55 HAS CORROSION FROM BS 399 TO 799. REMOVED CORROSION FROM SEAT TRACK IAW SRM 51-10-3 PG 46-48. FOUND TO BE OUT OF LIMITS IAW SRM 53-05 PG28. REMOVED SEAT TRACK FROM BS 395-800 IAW SRM 51-30-6. INSTALLED SEAT TRACK IAW SRM 50-05 FIG 4F.

Part: SEAT TRACK — DAMAGED (BS 1164-1222) · airframe 62,139 hrs · 47,324 cycles

IN CABIN, LT SIDE, SEAT TRACK AT X44 , STA 1164 TO 1222 HAS CHAFE DAMAGE AND SCRIBE MARKS AS INDICATED AND 1 ELONGATED HOLE. REMOVED DAMAGED, FOUND TO BE OUT OF LIMITS, REMOVED SEAT TRACK FROM STA 1164 TO 1222, FABRICATED SEAT TRACK AND INSTALLED IAW SRM 51-10-4.

Part: CUSP WEB — CRACKED (BS 1174-1250) · airframe 62,139 hrs · 47,324 cycles

IN CABIN, LT SIDE WEB BETWEEN SEAT TRACKS AT X=55 AND X=44, AT STA 1227 HAS A CRACK, BS 1250 TO 1174 HAS SCRIBE MARKS CHAFING AND CORROSION AROUND LIGHTENING HOLES. REMOVED CORROSION AND MARKS, AREAS FOUND TO BE WITHIN LIMITS. CUT OUT DAMAGED & CRACKED AREA, FABRICATED REPAIR DOUBLERS AND INSTALLED IAW SRM 53-05.

Part: CUSP WEB — DAMAGED (BS 1230 - 1271) · airframe 62,139 hrs · 47,324 cycles

CABIN, LT SIDE CUSP WEB JUST OTBD OF SEAT TRACK AT X=55, STA 1271 TO 1250 HAS CORROSION AT 3 FASTENERS AND AROUND 2 LIGHTENING HOLES UPPER SURFACE. FOUND TOOLING MARKS IN AREA OUT OF LIMITS, REPAIR TO CUSP WEB ACCOMPLISHED ON NRC 225785. MULTIPLE RIVETS DIMPLED INTO CUSP WEB SUB-STRUCTURE. REMOVED CUSP WEB, FABRICATED AND INSTALLED NEW WEB FROM STA 1250-1307 LBL 55 IAW SRM 53-05.

Part: CUSP WEB — CORRODED (BS 560-579) · airframe 62,139 hrs · 47,324 cycles

CORROSION RUNNING UNDER CUSP WEB AND RIVETS, BETWEEN STA 560 TO 579, AT THE PAX CABIN FLOOR AREA RT NEAR TO RBL 56. REMOVED CORROSION ON CUSP WEB, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA, FABRICATED DOUBLER, FILLER AND INSTALLED IAW DC9/MD80 SRM 53-05 DURING HMV AT ST AEROSPACE SAN ANTONIO.

Part: CUSP WEB — CORRODED (BS 655-674) · airframe 62,139 hrs · 47,324 cycles

CORROSION ON CUSP WEB AND RIVETS BTW STA 655-674 NEAR TO RBL 56 AT THE FLOOR CABIN RT SIDE. FOUND CORROSION OUT OF LIMITS. CUSP WEB SECTION REPLACED FROM BS 598-712 RBL 56.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN SEAT TRACK HAS CORROSION AT LBL 55 STA 215-245, STA 278-437. REMOVED CORROSION AT LBL 55 STA 215-245 AND 278-437 FOUND OUT OF LIMITS IAW MD80 SRM 53-05 PG 28 AND MD80 SRM 51-10-1 PG 121. REMOVED AND REPLACED SEAT TRACK AT STA 215-437 LBL 55 IAW DC9/MD80 SRM 53-05-4F. AT SAA/SAT DURING HMV.

Part: SEAT TRACK — CORRODED (BS 1031-1139) · airframe 62,139 hrs · 47,324 cycles

IN CABIN, LT SEAT TRACK AT X=44, BS 1031 TO 1139 HAS NUMEROUS LOCATIONS WITH CORROSION GOUGES AND SCRAPE, ON FLANGES, CROWN AND CHANNEL. REMOVED DAMAGE FROM SEAT TRACK, FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK FROM STA 1031 TO 1139 LBL 55 AND REPLACED IAW SRM 53-05.

Part: ANGLE — CORRODED (BS 160 LBL 55) · airframe 62,139 hrs · 47,324 cycles

L1 DOOR LOWER SILL ANGLE HAS CORROSION FROM STA 160 TO 200 LBL 55. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-10-4.

Part: SEAT TRACK — CORRODED (BS 797-937) · airframe 62,139 hrs · 47,324 cycles

CORROSION ON SEAT TRACK RBL 56 BTW STA 797-937 FLOOR CABIN AREA, FOUND OUT OF LIMITS. SEE CARD NR222863 FOR CABIN SEAT TRACK REPLACEMENT FROM RBL 55 STA 797-1033.

Part: SEAT TRACK — CORRODED (BS 807-1032) · airframe 62,139 hrs · 47,324 cycles

CORROSION ON MAIN CABIN SEAT TRACK BTW BS 807-1032 X55, OUT OF LIMITS. CABIN SEAT TRACK FROM STA798-1033 X55 TO BE REPLACED.

Part: SEAT TRACK — CORRODED (BS 1032-1307) · airframe 62,139 hrs · 47,324 cycles

CORROSION AND CHAFE WEAR ON MAIN CABIN SEAT TRACK STA 1032 TO1307. REMOVED DAMAGE FROM SEAT TRACK, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED 3 SEAT TRACK SECTIONS FROM 1032 TO 1307 RBL 22 AND SPLICES IAW SRM 53-05 AND 51-30-0.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN CUSP WEB REPAIR DOUBLER AND WEB HAVE CORROSION AT LBL 59 BETWEEN STA 617 TO 63. REMOVED REPAIR DOUBLER, REMOVED CORROSION ON CUSP WEB, CUSP WEB WITHIN LIMITS, FABRICATED NEW REPAIR DOUBLER AND TRIPLER AND INSTALLED IAW DC9/MD80 SRM 53-05 DURING MAINTENANCE VISIT.

Part: CUSP WEB — CORRODED (BS 864-927) · airframe 62,139 hrs · 47,324 cycles

CUSP WEB STA 864-927 HAS CORROSION, OUT OF LIMITS. CUT OUT DAMAGE AT STA 877-881. FABRICATED AND INSTALLED DOUBLER, FILLER AND RING DOUBLER IAW MD80 SRM 53-05 PG 908AC(7005) FIG 131A 3 SHT 1-10 STA 875-884. STA 905-927 FOUND OUT OF LIMITS.

Part: CUSP WEB — CRACKED (BS 693-712) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN LT CUSP WEB HAS CORROSION AT STA 693 TO 712 LBL 59 (WEB IS CRACKED THRU). REMOVED DAMAGED AREA, FABRICATE FILLER AND DOUBLERS AND INSTALLED IAW SRM 53-05.

Part: CUSP WEB — CORRODED (BS 1174-1250) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN CUSP WEB RBL 58 HAS CORROSION FROM BS 1174-1193, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW WEB AT STA 1174-1250 RBL 58 PER SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 1250-1271) · airframe 62,139 hrs · 47,324 cycles

MAIN CUSP WEB RT SIDE RBL 58 HAS CORROSION ON MULTIPLE PLACES STA 1250-1271. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9/MD80 SRM 53-05 DURING HMV AT ST AEROSPACE SAN ANTONIO.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN CEILING AREA L4R CRACKED STA 522 AND 541 2 PLACES. REMOVED L4R FROM STA 519 TO 546 IAW MD80/DC9 SRM 53-02 PG 49-56. INSTALLED REPLACEMENT LONGERON SECTION FROM STA 519 TO 546 IAW DC9/MD80 SRM 53-02 PG 49-56 AND DC9/MD88 SRM 51-30-2. IDENTIFIED ALL REPAIRS IAW PS 900-5-1 NO 4. DURING HMV AT SAA/SAT.

Part: FLOOR SUPPORT — CRACKED (BS 503 RBL 10) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN FLOOR SUPPORT IS CRACKED AT STA 503 RBL 10. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 1193-1212) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN CUSP WEB, RBL 58 HAS CORROSION BS 1193-1212. REMOVED CORROSION FOUND OUT OF LIMITS. CUSP WEB REPLACED FROM BS 1174-1250 RBL 58.

Part: SEAT TRACK — CORRODED (BS 298-799) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN SEAT TRACK HAS CORROSION AT LBL 22 STA 298-799. OUT OF LIMITS, CUT OUT AND REMOVED IAW SRM 53-05 FIG 4F PG32. REPLACED SEAT TRACK IAW SRM 53-05 FIG 4F.

Part: LONGERON — CRACKED (BS 1212 L5L) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN LONGERON 5L IS CRACKED BS 1212. REMOVED DAMAGED SECTION OF LONGERON FROM 1206 TO 1221. FABRICATED, LONGERN FROM EXTRUSION, SPLICE AND INSTALLED IAW SRM 53-02.

Part: SEAT TRACK — CORRODED (BS 589-799) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN SEAT TRACK HAS CORROSION AT LBL 55 FROM STA 589 TO STA 799. REMOVED CORROSION AT LBL 55 FROM BS 589-799, FOUND TO BE OUT OF LIMITS IAW SRM 53-05 PG 28 AND MD80 SRM 51-10-1 PG 121. REMOVED SEAT TRACK IAW SRM 51-30-1 PG 1. INSTALLED NEW SEAT TRACK IAW SRM 53-05 FIG 4F.

Part: CUSP WEB — CORRODED (BS 1117-1174) · airframe 62,139 hrs · 47,324 cycles

IN CABIN, LT SIDE CUSP WEB STA 1117 TO 1174 OTBD OF SEAT TRACK X=44 HAS ONE BROKEN WIRE BUNDLE RETAINING CLIP AND HAS CORROSION AT SEVERAL LOCATIONS ALONG INBD EDGE UPPER SURFACE. REMOVED CORROSION STA 1155, FOUND TO BE OUT OF LIMITS AT THIS AREA, CUT OUT DAMAGE, FABRICATED FILLERS AND DOUBLERS AND INSTALLED IAW SRM 53-05.

Part: SEAT TRACK — CORRODED (BS 1222-1307) · airframe 62,139 hrs · 47,324 cycles

IN CABIN, LT SIDE SEAT TRACK AT X=44, STA 1222-1307 HAS GOUGES AND SCRIBE MARKS THROUGH OUT PANEL LAND AREAS AND INBD FLANGE HAS AREAS WITH DEEP BLEND AND CHAFE MARKS. REMOVED CORROSION FROM SEAT TRACK, OUT OF LIMITS, REMOVED LT SEAT TRACK AT X-44 STA 1160-1307, LOCATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-30-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN CUSP WEB HAS CORROSION AT LBL 59 BETWEEN STA 598 AND STA 617 (WEB IS CRACKED THRU) / CUSP WEB OUT OF LIMITS DUE TO 100 PERCENT MATERIAL LOSS. REMOVED DAMAGED CUSP WEB, FABRICTED DOUBLER AND FILLER AND INSTALLED IAW DC9/MD80 SRM 53-05. DURING MAINTENANCE VISIT.

Part: CUSP WEB — CORRODED (BS 1022-1041) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN, CUSP WEB RBL 58 HAS CORROSION ON MULTIPLE PLACES BS 1022 TO 1041. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGED WEB, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW SRM 53-05.

Part: CUSP WEB — CORRODED (BS 905-946) · airframe 62,139 hrs · 47,324 cycles

IN CABIN, WEBBING MEMBRANE BETWEEN SEAT TRACKS AT X=44 AND X=55, STA 905 TO 946 HAS CHAFE DAMAGE WITH PITTING SPOTS WITH CORROSION AND MISSING FASTENER AS MARKED. REMOVED CORROSION, AND CHAFE DAMAGE, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-05.

Part: CUSP WEB — CRACKED (BS 275-294) · airframe 62,139 hrs · 47,324 cycles

CUSP WEB WITH CORROSION ON IT, BETWEEN STA 275 TO STA 294 RIGHT SIDE AT THE PAX CABIN FLOOR AREA. REMOVED CORROSION, HFEC DETECTED CRACKED AREA, BLENDED CRACK, REMOVED DAMAGED CUSP WEB. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-05.

Part: CUSP WEB — CORRODED (BS 788-807) · airframe 62,139 hrs · 47,324 cycles

CORROSION ON CUSP WEB, BETWEEN STA 788 TO STA 807 NEAR TO RBL 56 AT THE FLOOR CABIN RIGHT SIDE. REMOVED CORROSION, OUT OF LIMITS, REMOVED DAMAGE CUSP WEB, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 53-05.

Part: LONGERON — CRACKED (BS 522-541 L4R) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN CEILING AREA, L4R CRACKED STA 522 AND 541. REMOVED LONGERON FROM STA 519 TO 546, FABRICATED LONGERON AND REPAIR SPLICES AND INSTALLED IAW SRM 53-02.

Part: SEAT TRACK — CORRODED (BS 799-826) · airframe 62,139 hrs · 47,324 cycles

SEAT TRACK AT X22 BS 799-826 HAS CORROSION AND CHAFE DAMAGE ON FLANGES, CROWN, AND CHANNEL.

Part: CUSP WEB — CORRODED (BS 984-1003) · airframe 62,139 hrs · 47,324 cycles

CORROSION ON CUSP WEB LOWER SURFACE BETWEEN BS 984-1003, RBL 56 AT FLOOR CABIN RT SIDE. CUTOUT AND REMOVED DAMAGE REF SRM 53-05 FIG 131-A-18. FABRICATED DOUBLER, FILLER AND INSTALLED REF SRM 51-30-2 PG2-4.

Part: BULKHEAD — CORRODED (BS 1309) · airframe 62,139 hrs · 47,324 cycles

CORROSION ON CUSP WEB RUNNING UNDER FRAME AND PYLON BULKHEAD ATTACH FITTING AT STA 1309 LONGERON 18R NEAR TO RBL 56 AT THE FLOOR AFT CABIN AREA RIGHT SIDE. FOUND TO BE OUT OF LIMITS FABRICATED AND INSTALLED SPLICE RING REPAIR AND CUSP WEB REPAIR PER MR80 SRM 53-05 FIG131A SH1. A

Part: FLOOR SUPPORT — CORRODED (BS 826) · airframe 62,139 hrs · 47,324 cycles

IN CABIN, CENTER FLOOR SUPPORT AT STA 826, X=0 HAS CHAFE DAMAGE WITH CORROSION ON UPPER FLANGE, TOP AND BOTTOM SURFACES. REMOVED CORROSION AND DAMAGE, FOUND TO BE OUT OF LIMITS. REMOVED CENTER FLOOR SUPPORT, FABRICATED AND INSTALLED IAW SRM 51-30-05.

Part: SEAT TRACK — CORRODED (BS 221) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN SEAT TRACK HAS CORROSION AT LBL 44 STA 221, OUT OF LIMITS. REMOVED AND REPLACED AND INSTALLED SEAT TRACK PER SRM 51-10-04 AT STA 221-208.

Part: SEAT TRACK — CORRODED (BS 798-1032) · airframe 62,139 hrs · 47,324 cycles

CORROSION AND CHAFE WEAR ON MAIN CABIN SEAT TRACK BTW BS 798 AND 1032, OUT OF LIMITS. SEAT TRACK REPLACED AT LBL 24 BS 798-1033.

Part: CUSP WEB — CORRODED (BS 427-446) · airframe 62,139 hrs · 47,324 cycles

CORROSION ON FLOOR CUSP WEB BETWEEN STA 427-446 AT THE PAX CABIN RT SIDE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AT BS 437 RBL 55 IAW MD80 SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 674-693) · airframe 62,139 hrs · 47,324 cycles

CORROSION ON CUSP WEB AND RIVETS BTW BS 674-693 NEAR TO RBL 56 AT THE FLOOR CABIN RT SIDE. REPLACED CUSP WEB PER SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 798-1033) · airframe 62,139 hrs · 47,324 cycles

CORROSION AND CHAFE WEAR ON MAIN CABIN SEAT TRACK BETWEEN STA 798 AND STA 1032. FOUND TO BE OUT OF LIMITS. CABIN SEAT TRACK FROM STA 798-1033 TO BE REPLACED ON NR 222861. NO FURTHER ACTION REQUIRED ON THIS NR.

Part: CUSP WEB — CORRODED (BS 617-636) · airframe 62,139 hrs · 47,324 cycles

CORROSION ON CUSP WEB BTW BS 617-636 NEAR RBL 56 AT THE FLOOR CABIN RT SIDE, OUT OF LIMITS. CUSP WEB WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 1060-1079) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN CUSP WEB RBL 58 HAS CORROSION MULTIPLE PLACES BS 1060 TO 1079. REMOVED CORROSION, OUT OF LIMITS, REMOVED DAMAGED AREA, FABRICATED FILLERS, DOUBLERS AND INSTALLED IAW SRM 53-05.

Part: CUSP WEB — CORRODED (BS 731-750) · airframe 62,139 hrs · 47,324 cycles

CORROSION ON CUSP WEB BETWEEN STA 731 TO STA 750 NEAR TO RBL 56 AT THE FLOOR CABIN RIGHT SIDE. REMOVED CORROSION ON CUSP WEB, FOUND AREAS OUT OF LIMITS. FABICATED REPAIR DOUBLERS AND FILLERS AND 2 RING DOUBLERS AND INSTALLED IAW 53-05.

Part: MOUNT — CORRODED (GIRT BAR) · airframe 62,139 hrs · 47,324 cycles

AT L2 DOOR STA 1166, AFT GIRT BAR LATCH MOUNT HAS CORROSION AT FASTENER HOLES, LOWER DOUBLER HAS CORROSION AT FASTENER HOLES. NO ALLOWABLE DAMAGE LIMITS FOR LATCH MOUNT OR LOWER DOUBLER, BOTH REQUIRE REPLACMENT. REMOVED AND REPLACE LATCH MOUNT IAW SRM 51-30-5 PG1 THRU PG10. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 1032-1309) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN SEAT TRACK BS 1032-1309 HAS CORROSION AND GOUGES ON SEVERAL AREAS. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-05 FIG 4F.

Part: CUSP WEB — CORRODED (BS 522-560) · airframe 62,139 hrs · 47,324 cycles

CORROSION ON CUSP WEB BTW BS 522 AND 560 LBL 56 FLOOR CABIN AREA. REMOVED CORROSION ON CUSP WEB, FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW SRM 53-05.

Part: LONGERON — CRACKED (BS 541 L4L) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN LONGERON 4L IS CRACKED AT STA 541. CUT OUT DAMAGE ON LONGERON 4L STA 515 TO 549, FABRICATED LONGERON SEGMENT, SPLICES AND REPAIR SPLICE DOUBLERS AND INSTALLED IAW SRM 53-02.

Part: SEAT TRACK — CORRODED (BS 1307-1174) · airframe 62,139 hrs · 47,324 cycles

IN CABIN SEAT TRACK AT X=55, BS 1307 TO 1174 HAS CORROSION, CHAFE DAMAGE, SCRAPE, AND SCRIBE MARKS THROUGH OUT. REMOVED DAMAGE FROM CABIN LT SIDE SEAT TRACK IAW SRM 51-10-3 PARA 26. FOUND TO BE OUT OF LIMITS IAW SRM 51-10-1 AND SRM 53-05 PG 24. REMOVED SEAT TRACK IAW SRM 51-30-01. INSTALLED NEW SEAT TRACK IAW SRM 51-30-1 FIG1 PG4.

Part: CUSP WEB — DAMAGED (BS 594-598) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN CUSP WEB IS BULGING AN CREASED BETWEEN STA 598 TO 594.5 LBL 59. CUSP WEB FOUND TO BE OUT OF LIMITS, REMOVED CUSP WEB FROM STA 591 TO 598. FABRICATED CUSP WEB REPAIR AND DOUBLERS AND INSTALLED IAW SRM 53-05.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN CEILING AREA L-4R CRACKED STA 464. REMOVED CRACKED LONGERON 4R FROM STA 439 TO 470RT IAW DC9/MD80 SRM 53-02 PG 49-56. INSTALLED REPLACEMENT LONGERON SECTION FROM STA 439 TO 470 (4R) IAW DC9/MD80 SRM 53-02 PG 99 THRU 56 AND DC9/MD80 SRM 51-30-2. DURING HMV AT SAA/SAT.

Part: LONGERON — CRACKED (BS 464 L4R) · airframe 62,139 hrs · 47,324 cycles

MAIN CABIN CEILING ARA L-4R CRACKED STA 464. REMOVED LONGERON 4R FROM STA 439 TO 470, FABRICATED LONGERON, REPAIR SPLICE DOUBLERS AND INSTALLED IAW DC9/MD80 SRM 53-02 DURING HMV AT ST AEROSPACE SAN ANTONIO.

Part: SEAT TRACK — CRACKED (BS 968-1032) · airframe 62,139 hrs · 47,324 cycles

CORROSION ON MAIN CABIN SEAT TRACK BOTTOM AND CROWN BS 968-1032, OUT OF LIMITS. CABIN SEAT TRACK BEING REPLACED ON CARD 222863 FROM RBL 55 BS 798-1033.

Part: SKIN — CRACKED (SERVICE DOOR) · airframe 62,139 hrs · 47,324 cycles

FWD SERVICE DOOR UPPER FWD DOOR CUT OUT CORNER HAS 4 CRACKS THAT EXTEND FROM CUT OUT EDGE TO NEAR FASTENERS ON OUTER SKIN. HFEC SURFACE INSPECTION PER NDTSPM 06-10-01.001 DETECTED 3 CRACKS. REPAIRED IAW PRI ER/A 502454-14 REV. O.

Part: SEAT TRACK — CORRODED (BS 798-1033) · airframe 62,139 hrs · 47,324 cycles

SEAT TRACK LBL 24 HAS AREAS OF WEAR AND CORROSION FROM BS 798 TO 1033. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED SEAT TRACK STA 798 TO 1033 LBL 24, FABRICATED SEAT TRACK, AND SPLICE AND INSTALLED IAW DC9/MD80 SRM 51-30-1.

Part: SEAT TRACK — CORRODED (BS 798-1033) · airframe 62,139 hrs · 47,324 cycles

FOUND SEAT TRACK RBL -24 HAS AREAS OF WEAR AND CORROSION FROM STA 798 TO 1033. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK RBL 24 FROM STA 797 TO 1041, REPLACED SEAT TRACK AND SPLICES IAW SRM 51-30-5.

Part: LONGERON — CRACKED (BS 160 L3L) · airframe 62,139 hrs · 47,324 cycles

BS 160 LONGERON 3L CRACKED IN RADIUS JUST FWD OF FRAME ATTACH BOLT HOLE. REMOVED DAMAGED LONGERON SECTION, LOCATED, DRILLED AND INSTALLED NEW SECTION AT 3L STA 148 TO 160 IAW DC9/MD80 SRM 51-10-4 DURING HMV AT ST AEROSPACE SAN ANTONIO.

Part: FRAME — CORRODED (BS 1309 L22-23R) · airframe 62,139 hrs · 47,324 cycles

AFT CARGO COMPT FRAME CORRODED ON FRONT AT FS 1309 LONGERON 23R-22R. REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS. REMOVED GUSSET AND REPLACED IAW SRM 51-30-2.

Part: ANGLE — CORRODED (BS 1060-1032) · airframe 62,139 hrs · 47,324 cycles

LOWER WING TO BODY FAIRING TEE ANGLE HAVE CORROSION AT BS 1060 TO 1032 BL0. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, ACCOMPLISHED ER/A 503011-14.

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 62,139 hrs · 47,324 cycles

AFT CARGO DOOR EXTERIOR SKIN HAS 8 AREAS DENTED. FOUND DENTS 1, 2, 3 ON AFT CARGO DOOR EXT SKIN TO BE OUT OF LIMITS DUE TO MORE THAN 3 ADJACENT DENTS IAW SRM 53-04-01 PG 28. COMPLIED WITH ERA 502453-14 REV ORIG.

Part: SHEAR TIE — CORRODED (BS 1174 L27-30L) · airframe 62,139 hrs · 47,324 cycles

AFT CARGO FRAME FS 1174 SHEAR TIE CORRODED L27L - L30. SHEAR TIE OUT OF LIMITS DUE TO 100 PERCENT EXFOLIATION, FABRICATED NEW SHEAR TIE AND INSTALLED IAW SRM 51-30-2.

Part: CHANNEL — CORRODED (FS 1155 L28R) · airframe 62,139 hrs · 47,324 cycles

AFT CARGO FS 1155 L28R CHANNEL AT TOP OF TORQUE BOX CORRODED. REMOVED CORROSION FROM CHANNEL, FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED NEW CHANNEL IAW SRM 51-30-05.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 62,139 hrs · 47,324 cycles

AFT CARGO DOOR AFT SIDE SKIN IS CRACKED AT LATCH FITTING CLIP ATTACH. REMOVED FASTENERS FOR ACCESS, STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAR DOUBLER IAW SRM 52- 05.

Part: LONGERON — CORRODED (BS 1380) · airframe 62,139 hrs · 47,324 cycles

IN AFT ACC COMPARTMENT LT LOWER SIDE FRAME MOUNT STIFFENER JUST BELOW LAST LONGERON HAS CORROSION FROM STA 1380-1437 OTBD SIDE. REMOVED ALL CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW SRM 53-01.

Part: DOOR FRAME — CORRODED (AFT CARGO DOOR) · airframe 62,139 hrs · 47,324 cycles

AFT CARGO BAY LOWER DOOR FRAME AT APPROXIMATELY FS 1183 HAS 2 RIVNUTS WITH ELONGATED HOLES. REMOVED RIVNUTS AND REPAIR DOUBLER, FOUND THE CORROSION AT RIVNUT HOLES OUT OF LIMITS. FABRICATE NEW DOUBLER AND INSTALLED IAW SRM 53-05.

Part: FRAME SPLICE — GOUGED (BS 1429) · airframe 62,139 hrs · 47,324 cycles

IN AFT ACCESSORY BAY AT VENTRAL STAIR CUT-OUT, LT FRAME HAS A GOUGE ON SPLICE DOUBLER AT BS 1429. BLENDED OUT GOUGE ON SPLICE DOUBLER IAW SRM 51-10-3 PG 46 PARAGRAPH 26. FOUND TO BE OUT OF LIMITS IAW SRM 53-01 PG8. REMOVED SPLICE IAW SRM 51-30-2. INSTALLED NEW SPLICE IAW SRM 51-30-2 AT STA 1429.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 62,139 hrs · 47,324 cycles

MID CARGO DOOR JAMB LWR SILL EXTERNAL DOUBLER HAS 3.5 GOUGE AT FWD END. BLENDED GOUGE, FOUND TO BE OUT OF LIMITS. REMOVED DOUBLER, FABRICATED AND INSTALLED EXTERNAL DOUBLER IAW SRM 51-10-3.

Part: DOOR FRAME — CORRODED (E & E DOOR) · airframe 62,139 hrs · 47,324 cycles

E/E DOOR FRAME HAS CORROSION UNDER LIP AT APPROX LT OTBD SIDE UNDER DOOR FWD ATTACH POINT. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND ANGLES AND INSTALLED PER ERA 503022-14 REV2, RECEIVED NEW PANEL, LOCATED AND INSTALLED PER SRM 51-10. FABRICATED NEW DOOR FITTING AND INTERCOSTAL. INSTALLED PER SRM 53-30.

Part: WIRE — BROKEN (CABIN) · airframe 60,253 hrs · 45,959 cycles

DURING LINE CHECK MAINTENANCE FOUND A BROKEN WIRE TO EMERGENCY LIGHT AT SEAT 38D. MAINTENANCE REPLACED LIGHT ASSEMBLY AT ROW 38D PER MD88 AMM 33-50. OPERATION OF LIGHT CHECKS OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,354 hrs · 45,365 cycles

DURING LINE CHECK MX FOUND FIRST CLASS EMERGENCY LIGHT INOPERATIVE. MX REPLACED EMERGENCY LIGHT BATTERY SUPPLY. OPS OF LIGHT NOW OK.

Part: HYDRAULIC LINE — LEAKING (THRUST REVERSER) · airframe 58,817 hrs · 44,993 cycles

DURING THE LAST THIRD PART OF FLIGHT, CREW NOTICED A FAINT SMELL IN COCKPIT THAT CAUSED MILD EYE AND NOSE IRRITATION. THE F/A REPORTED NO SMELL IN CABIN. MX FOUND LT THRUST REVERSER RETURN LINE LEAKING. INSTALLED TEMP LINE REPAIR IAW MM 20-12-04-201. LEAK CHECKS OK AND OPS OF THRUST REVERSER CHECKS GOOD.

Part: LIGHT — MISSING (AC BAY) · airframe 58,680 hrs · 44,880 cycles

DURING LINE CHECK MAINTENANCE FOUND CATWALK CENTER EMERGENCY LIGHT NOT INSTALLED AND WALL COVERING PLACED OVER MOUNTING HOLES. MAINTENANCE INSTALLED NEW LIGHT ASSEMBLY PER MM 33-53-01. OPERATION OF LIGHT NOW CHECK OK. (2010-D1258) (DLM88102867)

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 58,335 hrs · 44,634 cycles

DURING LINE CHECK MX FOUND FIRST SET OF EMERGENCY LIGHTS ON CATWALK INOPERATIVE. MX RE-LAMPED NO HELP. FOUND BROKEN WIRE BEHIND PANEL. REPAIRED WIRE IAW SWPM20. OPS CHECK OF LIGHTS NOW CHECKS OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 57,717 hrs · 44,190 cycles

INITIALLY AFTER TAKEOFF, CREW REPORTED SMOKE IN THE CABIN, THEN STATED IT HAD DISSIPATED AND WOULD CONTINUE. SMOKE LATER RETURNED AND DECISION WAS MADE TO DIVERT. MX ACCOMPLISHED DUCT BURN OUT IAW OPS 5089. (DLM88101485)

Part: INLET — CONTAMINATED (APU) · airframe 57,717 hrs · 44,190 cycles

AFTER TAKEOFF FLIGHT CREW NOTICED ODOR IN THE CABIN, F/A REPORTED GRAY HAZE IN THE PASSENGER CABIN WITH AFT LAVATORY SMOKE DETECTOR SOUNDING. FLIGHT CREW RETURNED ACFT TO MSP. FOUND APU INLET SOAKED WITH OIL PLACED APU ON MCO. ACCOMPLISHED FULL DUCT BURN OUT IAW OPSERATION 5089 AND REPLACED COALESCER BAGS.

Part: LIGHT — INOPERATIVE (SEAT 23D) · airframe 57,370 hrs · 43,934 cycles

MX FOUND THE EMERGENCY PATH LIGHT AT SEAT 23D TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY, AFTER WHICH THE OPS CHECK WAS NORMAL AND THE ACFT WAS RETURNED TO SERVICE.

Part: WINDOW FRAME — DAMAGED (FUSELAGE) · airframe 57,353 hrs · 43,921 cycles

DURING LIGHTNING STRIKE INSP, FOUND DAMAGE TO 2R, 3R, WINDOW FRAMES. REPAIRED DAMAGE IAW ERA 481177-14 BLENDED OUT DAMAGE AND HFEC INSPECTED BLENDS ALSO SUBMITTED DAMAGE TO MFG. ALL GOOD FOR CONTINUE IN SERVICE IAW ERA.

Part: SKIN — CRACKED (BS 1307 S7R) · airframe 57,353 hrs · 43,921 cycles

1.5 IN CRACK FOUND AT STA 1309, STR 7 DURING LIGHTNING STIKE INSP. REPAIRED IAW ERA 481141-14. EXTERNAL DOUBLER INSTALLED PERM REPAIR C/W IAW ERA.

Part: UNKNOWN — ODOR (CABIN) · airframe 57,185 hrs · 43,809 cycles

SHORTLY AFTER TAKE OFF FROM ATL AFT LAV SMOKE DETECTORS WENT OFF AND F/A'S REPORTED A HAZY SMOKE AND ODOR. FOLLOWED QRH PROCEDURE AND RETURNED TO ATL. DISCONNECTED APU SURGE VALVE NO DESCUEPENCES NOTED. APU BLEED AND EXHAUST DUCTS NTF. LEFT ACM TURBINE BYPASS DUCT NTF LT ENG BLEED DUCT 4A NTF PUT ABOVE ITEMS BACK TOGETHER VERIFIED NO LEAKS. NO APU FLUID LEAKS 886913 C/W 3RD BURN OUT RAN ENG TO T/O POWER AFTER BURN OUT CABIN SMOKED UP PERF BORO REF ITEM 6 CKS OK RAN ENGS TO T/O PWR 2ND

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,972 hrs · 43,675 cycles

FUSELAGE CRACKS REPAIRED IAW EA 09-460094-12, ME03.

Part: INDICATOR — BURNED (RADAR) · airframe 56,950 hrs · 43,663 cycles

STRONG BURNING ELECTRICAL ODOR IN COCKPIT. TCAS, DISTORTED. TURNED OFF TCAS ODOR DISP. NO BREAKERS POPPED. REPLACED RADAR INDICATOR CHECKS GOOD. VERIFIED REMOVED BOX HAD BURNED COMPONENTS.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 55,962 hrs · 43,008 cycles

INBOARD FLAP LOWER SKIN REPAIRED IAW SRM 57-03D FIGURE 8.

Part: SKIN — DENTED (BS 494-532) · airframe 50,232 hrs · 39,361 cycles

GROUND DAMAGE CAUSED BY RAMP DURING GROUND OPERATIONS. REPAIRED FUSELAGE SKIN AT FS 494-532 AT STR 24R-26R PER SRM 53-04 FIG 12B SHEET 4-6.

Part: AIRSTAIR — CORRODED (AFT) · corrosion level 2

FOUND CORROSION, EXFOLIATED IN SEVERAL PLACES THROUGHOUT AFT AIRSTAIRS INTERIOR CAVITIES. REPAIRED EXFOLIATED CORROSION IN SEVERAL PLACES THROUGHOUT AFT AIRSTAIRS INTERIOR CAVITIES BY FABRICATING AND INSTALLING FORMED ANGLE FROM 2024-T4 .040", AND 5 DOUBLERS FROM 2024-T3 .032 AND 1 ANGLE FROM 7075-T6, 1 ANGLE FROM S1419056, AND 7 ANGLES FROM S1249243 IAW MD-80 SRM 52-01, 51-30-2 AND DOUGLAS DWG 9915570 AS DIRECTED BY TIMCO RFTS NR 60005.

Part: FRAME — CRACKED (BS 1508)

FOUND CANTED FRAME HAD APPROX 2 INCH LONG CRACK AT FS 1508 LT SIDE AT 8 O'CLOCK POSITION. STOP DRILLED CRACK HFEC CRACK CONTAINED IAW MD-80 SPM 06-10-01-.001. FABRICATED AND INSTALLED REPAIR DOUBLERS 5.0" AND 6.7" X 5.7" FROM 7075-T6 .025 AND IAW MD-80 SRM 53-01 FIG 2, 51-10-3 AND 51-30-5.

Part: DOOR FRAME — CORRODED (BS 1165-1200) · corrosion level 2

FOUND CORROSION IN RT AFT PIT LOWER CUTOUT. FABRICATED AND INSTALLED REPAIR DOUBLER 34" X 1.25" X 2.25" X 1.5" FROM 6AL-4V .040" IAW MD-88 SRM 53-05D FIG 63 AND 51-10-3.

Part: SEAT TRACK — CORRODED (BS 359-378) · corrosion level 2

FOUND CORROSION ON RIGHT O/B SEAT TRACK FS 378 AND WEAR MARKS AT FS 359. REMOVED SEAT TRACK RIGHT O/B FS 342 - 380 AND INSTALLED SEAT TRACK P/N SRO9530115-7005 AND 4 EA REPAIRS FROM 60-11343, 2 EA REPAIRS 4" X 13" AND 2 EA 4" X 7" FROM 7075-T6 .063", 2 EA 1" X 7" AND 1" X 13" FROM 7075-T6 .090, AND 2 EA 1" X 13" AND 2" X 13" FROM 7075-T6 .100" IAW MD-80 SRM 53-05D FIG 4F.

Part: SEAT TRACK — DAMAGED (BS 350-369)

FOUND WEAR MARKS RT I/B SEAT TRACK FS 350 TO FS 369 APPROX. CUT OUT SECTION OF SEAT TRACK FROM FS 322 TO 437. FABRICATED AND INSTALLED SEAT TRACK REPAIR IAW DC-9/MD-80 SRM 53-05D FIG 4F SHEET 1 & 2.

Part: FRAME — CRACKED (BS 1485)

CANTED FRAME AT FS 1485 ON LT SIDE HAS A CRACKED WEB. CUT OUT CRACKED WEB ON FRAME 1485 ON LT SIDE. FABRICATED AND INSTALLED DOUBLERS 9.5 X 2.2 X 9.25 INCHES, 5.4 X 7.25 X 6 X 4.5 INCHES AND 1.1 X 2.7 INCHES FROM 7075-T6 .032 AND FILLER FROM 7075-T6 .025 IAW MD-80 SRM 53-01.

Part: DOOR FRAME — CORRODED (BS 408-1320) · corrosion level 2

FOUND CORROSION AT FWD CARGO DOOR OPENING LOWER JAMB, AT AFT DOOR STOP, FS 408. CUT OUT CORRODED DOOR JAMB. FABRICATED AND INSTALLED DOOR JAMB PAN, SPLICE REPAIR AND ANGLE FROM 2024-T3 .030 AND .040 IAW MD-80 SRM 53-05 FIG 44.

Part: SEAT TRACK — CORRODED (BS 427-579) · corrosion level 2

FOUND CORROSION ON LT O/B SEAT TRACK FS 484, 503, 541, 579. SPLICED IN NEW SEAT TRACK FS 437 TO 589 6 EA. REPAIRS FROM 60-11343, 2 EA. REPAIRS 4 X 13 AND 2 EA. 4 X 7 FROM 7075-T6 .063, 2 EA. 1 X 7 AND 1 X 13 FROM 7075-T6 .090, AND 2 EA. .75 X 13 AND 1.42 X 13 FROM 7075-T6 .100, 14 X 5 FROM 7075-T6 .063 AND WEB REPAIR 2 X 2 AND FILLER 1 X 1 FROM 7075-T6 .020 CLAD IAW MD-80 SRM 53-05D FIG. 4F.

Part: CUSP WEB — CORRODED (BS 211-218) · corrosion level 2 · airframe 47,338 hrs

FOUND CORROSION OUT OF LIMITS ON RT CUSP FLOOR PANEL AT AIRCRAFT CONDITION DISTRIBUTION DUCT THRU HOLE FROM FS 211 - 218. REMOVED CORRODED CUSP WEB SECTION FS 211 - 218 IAW DC-9/MD-88 53-05 AND 51-30-2. FABRICATED/TRIMMED NEW SPLICE SECTION IAW MD88/DC9 SRM 53-05D AND 51-30-2.

Part: SKIN — DENTED (BS 205-220) · airframe 47,338 hrs

FOUND DENT UNDER R-1 DOOR 15 INCHES BELOW DOOR AND 16 INCHES AFT OF DOOR. CUT OUT DENTED AREA. FABRICATED AND INSTALLED DOUBLER 14.6" X 10.7" FROM 2024-T3 .071" IAW MD-88 SRM 53-04D, AND 51-10-30.

Part: LONGERON — CORRODED (BS 1200-1338) · corrosion level 2

FOUND CORROSION LONGERON 28L BETWEEN FS 1287 TO FS 1320. CUT OUT SECTION OF LONGERON FS 1200 TO 1338. DRILLED UP AND INSTALLED NEW LONGERON IAW MD-80 SRM 51-30-1 AND 51-10-3.

Part: LONGERON — CORRODED (BS1154-1338 S19L) · corrosion level 2

FOUND EXFOLIATED CORROSION ON UPPER CORNER CAVITY OF AFT CARGO DOOR ABOVE LONGERON 19R STA Y = 1154. REMOVED AND REPLACED UPPER DOOR BEAM AT FWD CORNER OF AFT CARGO DOOR ABOVE L-19R STA Y = 1154 IAW DOUGLAS DWG 5936072 AND MD-88 SRM 51-30-5.

Part: SKIN — GOUGED (BS 1260-1270)

FUSELAGE SKIN GOUGED AT FS 1260 L-23R APPROX. CUT OUT GOUGED SECTION OF SKIN. FABRICATED AND INSTALLED REPAIR SKIN DOUBLER 12.25 X 10 INCHES FROM 2024-T3 .071 AND REPAIR STRAPS 13 X 3 INCHES FROM 2024-T3 .025 AND 12 X 3 INCHES FROM 2024-T3 .025" IAW DC-9/MD-80 SRM 53-04D, 51-10-3 AND 51-20-0.

Part: INTERCOSTAL — CORRODED (BS 1210-1320) · corrosion level 2

CORROSION ON TRANSITION TRACK LT SIDE AFT PIT FROM STA 1210 - 1320. REMOVED AND REPLACED TRANSITION TRACK 5936663-503N LT SIDE AFT PIT FROM FS 1210-1320 IAW MD-80 SRM 51-30-5. REMOVED AND REPLACED INTERCOSTAL P/N 9936718U3 LT SIDE FROM FS 1300 - 1320 IAW MD-80 SRM 51-30-5.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON AFT VENTRAL AIR STAIR SUPPORT ANGLE ON RT SIDE. FABRICATED AND INSTALLED REPAIR SUPPORT ANGLE 11.0" FROM 7075-T6511 IAW 51-10-1 AND 51-30-0.

Part: SEAT TRACK — CORRODED (BS 1117-1174) · corrosion level 2

CORROSION ON LT SEAT TRACK AT LBL 50 AND BETWEEN FS 1117 AND 1174. FABRICATED AND INSTALLED REPAIR SEAT TRACK 6' 3" FROM S00201/SRO9530115-7003 IAW MD-88 SRM 51-30-01, 51-30-06 AND 53-05D FIG 4F.

Part: FLOOR SUPPORT — CORRODED (BS 1165-1174) · corrosion level 2

CORROSION ON PANEL SUPPORT AT L-2 DOORWAY THRESHOLD FS 1165. FABRICATED AND INSTALLED REPAIR BRACKET 6" X 4" FROM 7075-T6 .071" IAW MD-88 SRM 51-30-2 AND DOUGLAS DWG 9930612.

Part: SUPPORT ANGLE — CORRODED (AIR STAIR) · corrosion level 2

CORROSION ON AFT VENTRAL AIR STAIR SUPPORT ANGLE ON LT SIDE. FABRICATED AND INSTALLED REPAIR SUPPORT ANGLE 11.0" FROM 7075-T6511 IAW 51-10-1 AND 51-30-0.

Part: SKIN — DENTED (BS 355-415)

FUSELAGE SKIN 375, 389 - 408, 425 L-29R & L-30 HAS DENTS. CUT OUT DENTED SECTION OF SKIN FS 355 TO 415. FABRICATED AND INSTALLED REPAIR SKIN SECTIONS 6.0" X 43.0", 6.0" X 35.0" AND 6.0" X 32.0" FROM 2024-T3 .025 AND SKIN REPAIR 56.0" X 51.0" FROM 2024-T3 .050" AND REPAIRS 17.0" X 4.0", 6.0" X 4" AND 8.0" X .75" FROM 2024-T3 .063" IAW DC-9/MD-80 SRM 53-04 FIG 12C, AND DELTA ERA 385140-14 REV ORIG DATED 05-24-03.

Part: LONGERON — CORRODED (BS 1287-1309) · corrosion level 2

FOUND CORROSION ON STR 29L BETWEEN FS 1287 AND 1309. REMOVED CORRODED SECTION OF RT SEAT TRACK FS 1287 - 1309. FABRICATED AND INSTALLED SEAT TRACK REPAIR 36 INCHES LONG FROM S1242886-7800 AND SPLICE P/N 3914677-501N IAW MD-80 SRM 53-05D FIG 18, 51-10-3.

Part: LONGERON — CORRODED (BS1287-1320 S27L) · corrosion level 2

FOUND CORROSION ON LT L-27L FS 1287 - 1307 AND FS 1320. REMOVED CORRODED SECTION OF LONGERON 27L FS 1290 TO 1338. FABRICATED AND INSTALLED REPAIR LONGERON 60 INCHES FROM S1242886-7844 IAW MD-80 SRM 53-05D FIG 18 AND 51-10-3.

Part: INTERCOSTAL — CORRODED (BS 1210-1320) · corrosion level 2

CORROSION ON TRANSITION TRACK LT SIDE AFT PIT FROM STA 1210 - 1320. REMOVED AND REPLACED TRANSITION TRACK 5936663-503N LT SIDE AFT PIT FROM FS 1210 - 1320 IAW MD-80 SRM 51-30-5. REMOVED AND REPLACED INTERCOSTAL P/N 9936718U3 LT SIDE FROM FS 1300 - 1320 IAW MD-80 SRM 51-30-5.

Part: FLOOR PANEL — CRACKED (BS 101)

CO-PILOT'S FLOORING, BACKSIDE UNDER SEAT TRACKS CRACKING/TORN. CUT OUT CRACKED AND TORN SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER 3" X 3.375" FROM 7075-T6 .032" IAW MD-88 SRM 53-05, AND 51-10-3.

Part: SUPPORT BRACKET — CORRODED (BS 1145) · corrosion level 2

CORROSION ON PANEL SUPPORT AT L-2 DOORWAY THRESHOLD BS 1145. FABRICATED AND INSTALLED REPAIR BRACKET 6" X 4" FROM 7075-T6 .071" IAW DOUGLAS DWG 9930612 AND MD-88 SRM 51-30-2.

Part: FRAME — CRACKED (BS 1485)

RT EMPENNAGE AT CANT FRAME BS 1485 APPROX LONGERON 5R ANGLE SUPPORT WEB CRACKED. REMOVED CRACKED WEB. FABRICATED AND INSTALLED REPAIR DOUBLER 5.3" X 5.1" X 1.125" X 9.90" FROM 2024-T3 .032" IAW MD-88 SRM 51-10-3, 51-30-2 AND 51-30-1.

Part: SEAT TRACK — CORRODED (BS 200-256) · corrosion level 2

FOUND CORROSION ON RT SEAT TRACK AT RBL 24 AND BETWEEN FS 200 AND 256. REMOVED CORRODED SECTION OF RT SEAT TRACK AT RBL 24 BETWEEN FS 200 - 265. FABRICATED AND INSTALLED SEAT TRACK REPAIR 65 INCHES FROM SRO9530115-7001 IAW MD-80 SRM 53-05D FIG 4F SHEET 1, AND 2.

Part: SEAT TRACK — CORRODED (BS 579-617) · corrosion level 2

FOUND CORROSION ON LT, I/B SEAT TRACK AT FS 579 TO 617 IN 3 EA SPOTS. CUT OUT CORRODED SECTION OF SEAT TRACK. INSTALLED CHANNEL P/N 7452952-7 AND PLUG P/N 7452952-3 IAW DC-9/MD-80 SRM 53-05D FIG 4A, 51-10-03 AND 51-30-30 PG 19 & 24 AND DELTA PROCESS STD 900-2 NR 5 PG 2.

Part: ENGINE — MAKING METAL (NR 2) · airframe 45,643 hrs · 36,203 cycles

RIGHT ENGINE OIL STRAINER CLOG MSG. REPLACED ENGINE FOR METAL IN STRAINER.

Part: SHAFT — SHEARED (NR 2 FUEL PUMP) · airframe 44,573 hrs · 35,442 cycles

STARTING DOWN AT FL230, AROUND FL210 RT ENG FAILED GOOD HYD PRESS/OIL PRESS C/W ENG FAILURE W/QRH DURING FAILURE POWER WAS 55-60 N1 DUE TO 1 A/C PACK, APPROX TIME OF SHUTDOWN 2345Z LANDING AT 0009Z. REPLACED RIGHT ENGINE FUEL CONTROL AND PUMP. FUEL PUMP SHAFT SHEARED.

Part: SENSOR — MALFUNCTIONED (NLG) · airframe 43,195 hrs · 34,467 cycles

NOSE GEAR UNSAFE INDICATION AFTER T/O, CHECKLIST WAS C/W NON NORMAL CHECKLIST INITIATED FOR UNSAFE GEAR. INDICATION SHOWED SAFE AFTER ALL HYD PUMPS ON. REPLACED NOSE GEAR UP PROX SENSOR AND CENTER PROX SENSOR.

Part: STRUT — UNDERSERVICED (NLG) · airframe 42,131 hrs · 33,732 cycles

NOSE GEAR FAILED TO RETRACT ON T/O. RED NOSE GEAR LIGHT ILLUMINATED. SERVICED STRUT PER M/M 12-15-041 PG 201. SWUNG NOSE GEAR CHECKED OK.

Part: VALVE — FAILED (AFT) · airframe 39,476 hrs · 31,952 cycles

AT 350FL THE CABIN PRESS AND CABIN ALT WAS CLBING AT 2K FT/MIN. BOTH PACKS WERE IN AUTO AND WERE NOT RESPONDING. DESCENDING TO 280FL STILL NG. WENT TO MANUAL NO HELP. BOTH PACK PRESS READ ZERO. DESCENDED TO 100FL AND THE CABIN WAS 180FL AND THE O2 MASK DEPLOYED. REPLACED FLOW CONTROL VALVES

Part: PROXIMITY SWITCH — OUT OF ADJUST (NLG) · airframe 37,517 hrs · 30,566 cycles

AFTER T/O AND GEAR RETRACTION, NOSE GEAR UNSAFE INDICATION. EXTENDED GEAR ALL GREEN. RETRACTED GEAR, NOSE GEAR DIDN'T RETRACT FOR SEVERAL MINUTES. EXTENDED GEAR AGAIN AND ALL GREEN. ADJ D1-31 NOSE GEAR UP POSITION PROX SW PER M/M. SWUNG NOSE GEAR SEVERAL TIMES, OPERATION AND INDICATION NORMAL.

Part: RELAY — BURNED (COCKPIT) · airframe 37,106 hrs · 30,260 cycles

RELAY R2-50 GROUND SERVICE BUS TIE WAS FOUND BURNT AND TERMINALS A2 AND B2 SHORTED. REPLACED SAME.

Part: RELAY — BURNED (EPC PANEL) · airframe 37,106 hrs · 30,260 cycles

FOUND R2-50 AC GND SERVICE TIE RELAY BURNED AND DAMAGED, TERMINALS AT A2 AND B2 DAMAGED. REPLACED WIRE NB X226A10A. INSTALLED NEW TERMINAL ENDS AT A2 AND B2 AND REPLACED C/B B1-241.

Part: WIRE — SHORTED (CABIN) · airframe 36,604 hrs · 29,912 cycles

ON L/O, FOUND AFT EMERGENCY LIGHTS INOP. FOUND AFT POWER SUPPLY FUSE BLOWN. REMOVED AND REPLACED SUPPLY AND BATTERY. STILL NO HELP. FOUND WIRE SHORTED AT SEAT 30E. REPAIRED SAME. REMOVED AND REPLACED POWER SUPPLY. NOW TESTS OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,043 hrs · 29,480 cycles

F/C EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK.

Part: LINE — LEAKING (NR 2 ENGINE) · airframe 32,611 hrs · 26,942 cycles

AT CRUISE, RT HYD QTY DECREASED TO 1 QT. FOUND FLEX LINE TO RETURN MODULE LEAKING. REPLACED SAME.

Part: UPLOCK SWITCH — FAILED (NLG) · airframe 32,422 hrs · 26,809 cycles

UNSAFE NOSE GEAR INDICATION AFTER TAKEOFF AND GEAR RETRACTION. REPLACED NOSE GEAR UPLOCK SWITCHES AND SERVICED NOSE GEAR STRUT PER M/M, OP CHECKS NORMAL.

Part: CARPET — CONTAMINATED (CABIN)

AIRCRAFT DIVERTED TO PIT DUE TO ODOR REPORTED AROUNFD ROW 29 AND AFT. AIRCRAFT WAS THEN MAINTENANCE FERRIED TO CVG FOR INSPECTION/REPAIR. CVG REPLACED ALL UNDERSEAT CARPETS IN COACH CABIN.

Part: PAN — CORRODED (CARGO DOORWAY)

THE FWD CARGO DOOR OPENING WAS FOUND WITH EXTENSIVE CORROSION ON THE LWR JAMB PAN REQUIRING A SPLICE OF THE PAN. REPAIRED PER ERA 365892-14.

Part: STRUT — REQD SERVICE (NLG)

DURING GEAR RETRACTION, NOSE GEAR DID NOT STOW IN WELL PROPERLY. NOSE GEAR UNSAFE LIGHT ON. FOUND NOSE STRUT UNDERSERVICED. SERVICED STRUT PER MM.

Part: COALESCER — CONTAMINATED (CABIN)

ODOR IN AIRCRAFT SYSTEM ON GROUND AND IN FLIGHT. DID NOT DISSIPATE AFTER 45 MIN FLIGHT, SMELLS LIKE EXHAUST FUMES. REPLACED WATER SEPARATORS.

Part: WINDOW — CRACKED (COCKPIT)

FIRST OFFICER'S WINDSHIELD CRACKED AND SHATTERED AT FL 350. ACCOMPLISHED ABNORMAL PROCEDURES. DIVERTED TO CVG. C/A REMOVED AND REPLACED F/O'S WINDSHIELD AND CONTROLLER PER M/M CHAPTER 56 (CONTROLLER P/N 617-2).

Part: APU — OIL LEAK (AFT FUSELAGE)

AFTER TAKEOFF, 3 LAV SMOKE DETECTORS WENT OFF. FLIGHT ATTENDANT REPORTED FUMES IN CABIN. FOUND APU LEAKING OIL AT GEARBOX, BEING INGESTED, FWD TO MCO. PLACARD PER MEL 49-00-01A. RAN PACKS OFF ENG AIR. NO SMOKE NOTED.

Part: WIRE — CHAFED (RT AFT LAV)

F/A REPORTED, SPARKS WITH SMOKE MOMENTARILY IN RT AFT LAV FROM AREA OF FWD MIRROR LIGHT NEXT TO DOOR FRAME, WHEN DOOR CLOSED AND LOCKED. INSPECTION FOUND WIRE FROM DOOR SW CHAFED AND SHORTED TO FRAME FOR THE AFT LAV OCCUPIED SIGN. REMOVED AND TIED BACK WIRE PULLED AND COLLARD C/B FOR AFT LAV OCCUPIED SIGN. WIRE REPAIRED, FWD TO MCO AND PLAC 480194001.

Part: DEFECTOR — CRACKED (LT TE FLAP)

DEBRIS DEFLECTOR SHIELD CRACKED 1.25 INCH ON LEFT WING FLAP. FOUND DURING A-1 LTR CK. REPAIRED PER SRM 57-09 FIG 42.

Part: SKIN — CRACKED (NLG DR CUTOUT)

LEFT NLG DOOR HINGE CUTOUT CRACKED ( AFT HINGE ). FOUND AT A-1 LTR CK. REPAIRED PER SRM 53-05 FIG 62A.

Part: DOOR — DAMAGED (CARGO COMPT)

TRANSFERRED FROM A/C LOG BOOK Z272827. FOUND UPON ARRIVAL IN ATL, FWD B/B DOOR DAMAGED LWR EDGE. REPAIRED DAMAGED AREA PER SRM 52-05 FIG 4.