N919DE

Part: TAB — DAMAGED (RUDDER) · airframe 61,607 hrs · 44,436 cycles

COMPOSITE EXPOSED ON RUDDER TAB. REMOVED THE TAB IAW AMDS 2720-4438 AND INSTALLED A NEW TAB IAW AMDS 2720-4321.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,509 hrs · 43,586 cycles

FOUND OVERWING EXIT LIGHTS INOPERATIVE. REPLACED THE BATTERIES IAW AMM 33-53, LIGHTS CHECKED GOOD.

Part: FAN — FAILED (CABIN) · airframe 60,049 hrs · 43,243 cycles

FLT LEVEL 340, FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL WITH A HAZE IN THE CABIN. AFTER THE SMELL REACHED THE COCKPIT, ELECTRICAL, WE DIVERTED TO CAE. FOUND RECIRC FAN BAD. FWD TO MEL 21-00-43 AND PLA. C/W (M) PROCEDURES.

Part: WIRE — CHAFED (EMERGENCY LIGHT) · airframe 59,492 hrs · 42,839 cycles

AFT EMERGENCY LIGHT INOPERATIVE. FOUND CHAFED WIRE IN SERVICE LOOP. REMOVED THE PORTION OF WIRE AND SPLICED IAW AMM 20-50. LIGHTS OPERATE NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,400 hrs · 42,759 cycles

EMERGENCY LIGHT INOP FROM ROW 31 TO TAIL. REPLACED BATTERY PACK. OPS CKS GOOD.

Part: FUSE — BLOWN (BATTERY PACK) · airframe 59,267 hrs · 42,654 cycles

AFT SECTION EMERG LIGHTS INOP. REPLACED FUSE IN BATTERY PACK. OPS CK GOOD. REF WDM 33-51.

Part: FUSE — BLOWN (CABIN) · airframe 59,208 hrs · 42,611 cycles

FOUND DURING SERVICE CHECK, AFT CABIN AND TAIL COMPARTMENT EMERGENCY LIGHTS WILL NOT TEST. REPLACED BLOWN FUSE AT POWER SUPPLY B5-212, POSITION 9, IAW WDM 33-51-14. CHECKS OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,554 hrs · 40,740 cycles

MAINTENANCE FOUND THE COCKPIT EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACKS WERE REPLACED.

Part: DOOR — NO TEST (LT OVERWING) · airframe 56,371 hrs · 40,598 cycles

LEFT AFT OVERWING EMERGENCY EXIT DOOR FAILED EXTERIOR DOOR HANDLE RELEASE TEST IAW W/C 5200-2643. DOOR RELEASES AS SOON AS EXTERIOR HANDLE TAB PRESSED WHILE HANDLE WAS IN THE STOWED POSITION. REPLACED AND RIGGED THE DOOR IAW AMM 52-21-00.

Part: CONTAINER — CRACKED (TAILCONE SLIDE) · airframe 56,371 hrs · 40,598 cycles

DURING INSPECTION, MAINTENANCE FOUND TAILCONE EVACUATION SLIDE BASE PLATE CRACKED AT COVER ATTACH POINTS. THE CONTAINER ASSY WAS REPLACED IAW AMDS WORKCARD 2561-4001.

Part: FRAME — CRACKED (BS 1463) · airframe 56,371 hrs · 40,598 cycles

AFT FUESLAGE TAIL CONE AREA FRAME BS 1463, S25R FOUND A THREE INCH CRACK ON FRAME. REPAIRED IAW SRM 53-03D, FIG 38A.

Part: SKIN — DAMAGED (RT WING TIP) · airframe 58,001 hrs · 41,725 cycles

REMOVED RT WINGTIP ASSY IAW AMM 57-20. REPLACED RT WING TIP ASSY IAW AMM 57-20-02. OPS CHECKED GOOD. COMPLIED WITH ER/A 534223-14, REV ORIGINAL.

Part: PIN — SEIZED (TAILCONE RELEASE) · airframe 55,273 hrs · 39,862 cycles

DURING TAILCONE RELEASE SYS FUNCTIONAL CHECK, MAINTENANCE FOUND THE INTERIOR TAILCONE RELEASE CABLE RELEASE PIN SEIZED. MAINTENANCE R & R THE RELEASE CABLE RELEASE PIN. OPS CHECKED OK. LP1853095.

Part: CABLE — WORN (TAILCONE) · airframe 55,273 hrs · 39,862 cycles

MAINTENANCE FOUND KEVLAR CABLE ASSY WORN FOR TAILCONE ASSY. MAINTENANCE REPLACED THE KEVLAR CABLE ASSY, CHECKS OK. LP1853081.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,155 hrs · 39,080 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY OVERHEAD LIGHTING AT THE OVERWING EXIT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-104 AND THE LIGHTS RETURNED TO AN OPERATIONAL STATE.

Part: CABLE — DETACHED (GIRT BAR) · airframe 53,295 hrs · 38,432 cycles

THE CREW DISCOVERED THE 1L DOOR GIRT BAR WIRE CABLE WAS NOT ATTACHED TO THE GIRT BAR. MAINTENANCE REINSTALLED THE GIRT BAR CABLE AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (WINDOW BELT) · airframe 51,600 hrs · 37,211 cycles

WINDOW BELT FRAME FOUND CRACKED AT PREVIOUS LIGHTNING STRIKE BLEND. BS 541 TO 560 AREA C. NDT CONFIRMED 06-10-01-001. WORK ACCOMPLISHED ON PRI 518567-14. REPAIR COMPLETED.

Part: SKIN — CRACKED (BS 1310) · airframe 51,600 hrs · 37,211 cycles

DURING SCHEDULED MX, A .7500 INCH SKIN CRACK WAS FOUND AT BS 1310, APPROXIMATELY 2.5 INCHES ABOVE THE EDGE OF THE SKIN PANEL NEAR LONGERON 7R. REPAIRED IAW ER/A 518476-14, SECT 1.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,234 hrs · 36,955 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT DOOR L1 AND THE FIRST CLASS CABIN WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: PIN — LOOSE (L1 DOOR SLIDE) · airframe 50,862 hrs · 36,702 cycles

DURING ROUTINE INSPECTION, THE INSPECTOR NOTED THAT THE NR 1 LEFT DOOR SLIDE PACKING PIN WAS LOOSE. THE SLIDE WAS REPLACED IAW AMM 25-62 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: CABIN PRESSURE — MULTIPLE FAIL · airframe 49,469 hrs · 35,739 cycles

CREW REPORTED THAT THE ACFT COMPLETELY LOSS PRESSURIZATION NEAR THE TOP OF DESCENT. PASSENGER OXYGEN MASKS DID DEPLOYED AND AN EMERGENCY DESCENT TO 10K WAS DECLARED AND EXECUTED. MX FOUND CABIN PRESSURE CONTROLLER NR 2, LT PACK FLOW CONTROL VALVE, LT TRIM VALVE, AND LT PACK TEMPERATURE CONTROL ALL TO BE BAD AND THEY WERE ALL REPLACED. THE RT PILOT REGULATOR VALVE WAS ALSO REPLACED. OPS CHECKS WERE NORMAL AND THE ACFT HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,387 hrs · 35,685 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY PATHWAY LIGHTS INOPERATIVE FROM ROW 1 THROUGH 11 AND LT AND RT FORWARD ENTRY DOOR EXIT SIGNS OUT. REMOVED AND REINSTALLED BATTERY PACK. ALL LIGHTS OPERATIONS CHECKED GOOD.

Part: LANYARD — LOOSE (GIRT BAR) · airframe 49,286 hrs · 35,616 cycles

PILOT FOUND CABLE HANGING FROM FORWAD FO SIDE GALLEY DOOR. MX SECURED R1 DOOR GIRT BAR LANYARD. ACFT OK FOR SERVICE.

Part: SKIN — DAMAGED (BS 617-636) · airframe 48,762 hrs · 35,234 cycles

DURING HMV, LIGHTNING STRIKES WERE FOUND ON AFT UPPER CORNER OF LT WINDOW BELT FRAME BS 617-636. WINDOW BELT FRAME AFT UPPER CORNER LOWER OUT OF CRITICAL ZONE 1 IS WITHIN LIMIT PER SRM 53-05 FIG 111. THE AFT UPPER CORNER UPPER BLENDED OUT AND REPAIRED IAW ERA 504342-14 REV ORIG.

Part: SKIN — DAMAGED (BS 617-636) · airframe 48,762 hrs · 35,234 cycles

DURING HMV, LIGHTNING STRIKES WERE FOUND ON FWD AND AFT EDGES OF LT WINDOW BELT FRAME BS 617-636. WINDOW BELT FRAME WAS BLENDED OUT AFT EDGES AND WITHIN LIMITS PER SRM 53-05 FIG 111. THE FWD EDGE WAS REPAIRED IAW ERA 504342-14 REV ORIG.

Part: SKIN — DENTED (FUSELAGE) · airframe 48,762 hrs · 35,233 cycles

FOUND DENT TO FUSELAGE, APPROXIMATELY 2 FEET AFT OF L1 DOOR COMPLIED WITH PERMANENT REPAIR TO FUSELAGE DENT PER SRM 53-04-5.

Part: SKIN — DAMAGED (BS 788-807) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, LIGHTNING STRIKE WAS FOUND ON WINDOW BELT FWD EDGE BS 788-807. WINDOW BELT WAS BLENDED OUT AND REPAIR DOUBLER INSTALLED IAW ERA 504370-14 REV ORIG.

Part: SKIN — DAMAGED (BS 655-674) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, LIGHTNING STRIKES WERE FOUND ON LT WINDOW BELT FRAME FWD UPPER CORNER. ALSO, AFT UPPER CORNER BS 655-674. WINDOW BELT FRAME WAS BLENDED OUT AND REPAIR DOUBLER INSTALLED IAW ERA 504352-14 REV ORIG.

Part: SKIN — DAMAGED (BS 807-826) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, LIGHTNING STRIKE WAS FOUND ON LT WINDOW BELT FRAME AFT LOWER CORNER BS 807-826. WINDOW BELT FRAME WAS BLENDED OUT AND REPAIR DOUBLER WAS INSTALLED BS 788-845 IAW ERA 504370-14 REV ORIG.

Part: SKIN — CORRODED (BS 803) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN BS 803 AND LONGERON 29R. FUSELAGE SKIN WAS BLENDED OUT AND DOUBLER REPAIR INSTALLED IAW MD88 SRM 53-04 PARA 57.

Part: SKIN — CORRODED (BS 782) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN IN BS 782 BETWEEN LONGERON 28R-29R. FUSELAGE SKIN WAS BLENDED OUT AND REPAIR DOUBLER INSTALLED IAW 53-04 PARA 57.

Part: SKIN — DAMAGED (BS 693-674) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, LIGHTNING STRIKE WAS FOUND ON WINDOW BELT FRAME AFT LOWER CORNER BTW BS 693-674 RT SIDE. WINDOW BELT FRAME WAS BLENDED OUT AND REPAIR DOUBLER INSTALLED IAW ERA 504353-14 REV ORIG.

Part: SKIN — DAMAGED (BS 1193-1212) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, LIGHTNING STRIKES WERE FOUND ON WINDOW BELT FRAME ON FWD LOWER CORNER. ALSO ON AFT UPPER CORNER BTW BS 1193 AND 1212. WINDOW BELT FRAME WAS BLENDED OUT IAW ERA 504357-14 REV ORIG.

Part: SKIN — DAMAGED (BS 541-560) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, LIGHTNING STRIKES WERE FOUND ON LT WINDOW BELT FRAME LOWER AFT CORNER. ALSO LOWER FORWARD CORNER BS 541-560 WINDOW BELT FRAME WAS BLENDED OUT IAW ERA 504357-14 REV ORIG.

Part: SKIN — DAMAGED (BS 826-845) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, LIGHTNING STRIKE WAS FOUND ON LT WINDOW BELT FWD EDGE BS 826-845. WINDOW BELT WAS BLENDED OUT AND REPAIR DOUBLER INSTALLED IAW ERA 504370-14 REV ORIG.

Part: BEAM — CORRODED (C2 DOOR FRAME) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, CORROSION WAS FOUND ON MID CARGO COMPARTMENT LOWER BEAM BS 636-693 (C2). BEAM WAS BLENDED OUT AND BS 655 AND 674 WAS OUT OF LIMITS. THE AREA WAS CUT OUT FILLER AND Z REPAIR INSTALLED IAW SRM 53-05 FIG 123.

Part: SKIN — CRACKED (BS 1500 L17-18L) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, CRACKED FUSELAGE SKIN WAS FOUND BTW BS 1497 - 1501 LONGERONS 17-18L. DAMAGE AREA WAS CUT OUT AND SHIM DOUBLER REPAIR INSTALLED IAW SRM 53-04-3 FIG 2.

Part: ANGLE — DAMAGED (BS 1338) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, TOOLING MARKS WERE FOUND ON PRESSURE DOME LOWER TEE ANGLE AT BS 1338 BETWEEN LONGERON 26 LT AND 26 RT. REMOVED DAMAGE TEE ANGLE BETWEEN LONGERON 25 LT AND 25 RT AND INSTALLED REPAIR SPLICES TEE ANGLE IAW SRM 53-03 FIG 37.

Part: STRUCTURE — CORRODED (BS 1250-1271) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, CORROSION WAS FOUND ON REPAIR SPLICE OF LONGERON 28 LT AND 29 LT BTW STA Y=1250-1271 AT AFT CARGO COMPARTMENT LONGERON 28L WAS ATTENDED ON NRC 254176 AND REPAIR SPLICE OF LONGERON 29LH BTW Y=1250-1271 WAS REPLACED IAW SRM 53- 02 FIG 18.

Part: LONGERON — CORRODED (BS 1204-1330) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, CORROSION WAS FOUND ON LONGERON 27 LT FROM BS 1257-1330 AND LONGERON 28 LT. DAMAGE SECTION WAS REMOVED BS 1204-1330 AND REPAIRED IAW SRM 53-02 FIG 18.

Part: LONGERON — CORRODED (BS 1287 L23L) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, CORROSION WAS FOUND ON LONGERON 23L IN BS 1287 AT AFT CARGO COMPARTMENT. DAMAGE LONGERON WAS REMOVED7 AND REPAIR SPLICE INSTALLED IAW SRM 53-02 FIG 18.

Part: LONGERON — CORRODED (BS 1290 L24L) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, CORROSION WAS FOUND ON LONGERON 24 LT STA Y=1290, LONGERON WAS REMOVED FROM BS 1275-1328. REPAIR LONGERONS AND SPLICES INSTALLED IAW SRM 53-02 FIG 18.

Part: SKIN — CORRODED · airframe 48,762 hrs · 35,233 cycles

DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN BELOW WING TO FUSELAGE FILLET PANEL RUBSTRIPS ON BS 727-826 BETWEEN LONGERONS 16-30L AND BS 826-864 BETWEEN LONGERONS 17-19L. BLENDED FUSELAGE SKIN AND WITHIN LIMITS TO LEAVE AS IS IAW SRM 53-04 PARA 57.

Part: LONGERON — CORRODED (BS 1277-1335) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, CORROSION WAS FOUND ON LONGERON 22 LT BTW BS 1277 TO 1335. DAMAGE LONGERON WAS REMOVED AND REPAIR LONGERON AND SPLICE INSTALLED IAW SRM 53-02 FIG 18.

Part: LONGERON — DAMAGED (BS 1401-1418) · airframe 48,762 hrs · 35,233 cycles

DURING HMV, WEAR WAS FOUND ON STRAP AND LONGERON 8 RT AT BS 1401-1418. DAMAGED LONGERON 8 RT STA Y=1406-1429 AND SPLICE WAS REMOVED AND REPAIRED. PARTS INSTALLED IAW SRM 53-02 FIG 18.

Part: SKIN — DENTED (BS 239 L18L) · airframe 48,762 hrs · 35,233 cycles

DENT ON FUSELAGE AFT OF L1 DOOR APPROXIMATELY 2 FT AFT OF DOOR AT STA Y=239. REPAIRED FUSELAGE SKIN IAW WITH SRM 53-04-5 AND ERA 483596-14 REV ORIG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

FLOOR STRUCTURE SUPPORT ANGLE CORRODED LBL 06 TO RBL 08 AT STA 200. INSTALLED FLOOR STRUCTURE SUPPORT ANGLE LBL 06 TO RBL 08 AT STA 200 IAW DC9/MD80 SRM 51-10-4 PG 1 AND SRM 51-30-5 PG 3 MD80.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

FLOOR SUPPORT ANGLE CORRODED RBL 44 AT STA 148 AND 160. INSTALLED FLOOR SUPPORT ANGLE AT RBL 44 AT STA 148 - 160 IAW DC9/MD80 SRM 51-10-4 PG 1 MD80 SRM 51-30-5 PG 3 TORQUE WRENCH NR 11-750 DUE 11-19-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

FLOOR STRUCTURE SUPPORT CORRODED RBL 06 AT STA 200. INSTALLED FLOOR SUPPORT AT STA 200-148.5 RBL 6 IAW DC9/MD 80 SRM 51-30-1 PG 11-14 TORQUE WRENCH NR 11-750 DATE DUE NR 11-19-11 IAW DC9/MD80 SRM 51-30-1 PG 11-14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

FLOOR STRUCTURE SUPPORT ANGLE CORRODED LBL 10 TO LBL 14 AT STA 200. INSTALLED FLOOR STRUCTURE SUPPORT ANGLE LBL 10 TO LBL 14 AT STA 200 IAW DC9/MD80 SRM 51-10-4 PG 1 AND SRM 51-30-5 PG 3 DC9/MD80.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

FLOOR STRUCTURE SUPPORT CORRODED LBL 08 AT STA 148.5 AND 200. INSTALLED FLOOR SUPPORT AT STA 148.5 - 200 LBL 8 IAW DC9/MD80 SRA 51-30-1 PG 11-14 TORQUE WRENCH USED SAA ID 11-750 DUE 11-19-11 IAW DC9/MD8- SRM 51-30-1 PG 11-14.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

MEMBRANE SKIN SUB FLOOR CORRODED LBL 44.5 AT STA 198. INSTALLED FLOOR SUPPORT AT STA 198 LBL 44.5 TO LBL 15 PER DC9/MD80 SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

FLOOR STRUCTURE SUPPORT ANGLE CORRODED LBL 08 TO RBL 46 AT STA 200. INSTALLED FLOOR SUPPORT STRUCTURE ON LBL 8 TO RBL 46 STA 200 AT MAIN CABIN IAW DC9/MD80 SRM 51-30-5 PAR 7.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

SDR - CABIN SEAT TRACK AT STA 1250 LBL 22 IS CRACKED. INSTALLED NEW SEAT TRACK P/N SR09530115-7001 BACH # 00021084410IAW MD88 IPC 53-40-00-19B PG 1AND 2 AND DC9/MD80 SRM 53-05 PG 47. AT SAA/SAT DURING PAX MOD ON N/R 193089 W/O 89215000001.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

SDR - FLOOR STRUCTURE SUPPORT CORRODED LBL 08 ST STA 148.5 AND 200. REMOVED FLOOR STRUCTURE SUPPORT AT LBL 08 STA 148.5-200 PER DC9/MD88 SRM 51-30-1. FABRICATED FLOOR SUPPORT STRUCTURE PER DC9/MD88 SRM 53-14-1 USED EXTRUSION FROM 7075-T6 AT SAA/SAT DURING PAX MOD ON N/R 193029 W/O 89214600001.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

MEMBRANE SKIN SUB FLOOR CORRODED LBL 14 TO RBL 22 AT STA 200-207. INSTALLED MEMBRANE SKIN AT STA 200 TO 219 LBL 26 TO RBL 29 IAW MD8 SRM 5130-2 PG 28-29.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

SDR - FLOOR STRUCTURE SUPPORT ANGLE CORRODED LBL 06 TO RBL 08 STA 200 FABRICATED, LOCATED AND DRILLED FLOOR SUPPORT PER DC9/MD80 SRM 53-14-1 PG 29 AND 51-104 PAGE 1. AT SAA/SAT DURING PAX MOD ON W/O 892146660001.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

SDR - FLOOR STRUCTURE SUPPORT ANGLE CORRODED LBL 08 TO RBL 46 AT STA 200. FABRICATED FLOOR STRUCTURE SUPPORT ANGLE, LOCATED AND DRILLED PER SRM DC9/MD88 53-14-1 PG 29 AND 51-104 PAGE 1. AT SAA/SAT DURING PAX MOD ON W/O 89214630001.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

SDR - FLOOR STRUCTURE SUPPORT ANGLE CORRODED LBL 10 TO LBL 14 AT STA 200. FABRICATED, LOCATED, AND DRILLED FLOOR SUPPORT STRUCTURE PER DC9/MD80 SRM 53-14-1 PG 29 AND PAGE 1. AT SAA/SAT DURING PAX MOD ON W/O 89214670001.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

SDR - FLOOR STRUCTURE SUPPORT CORRODED RBL 06 AT STA 200. REMOVED FLOOR STRUCTURE AT RBL 06 STA 200 PER SRM DC9/MD88 SRM 51-30-1. AT SAA/SAT DURING PAX MOD ON W/O 89214620001.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

SDR - MEMBRANE SKIN SUBFLOOR CORRODED LBL 44.5 AT STA 198. FABRICATED REPAIR DOUBLER AND FILLER PER DC9/MD80- SRM 51-70-4 FIG 2. INSTALLED REPAIR DOUBLER PER DC9/MD80 SRM 51-70-4 FIG 2. SAA/SAT DURING PAX MOD ON NRC 193103 W/O 89215090001.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

MEMBRANE SKIN SUB FLOOR CORRODED LB 14 TO RBL AT STA 200-207. FABRICATED NEW MEMBRANE SKIN SECTION FROM SHT 7075-T6 .020 BATCH #0002111794 PER SRM 53-14-1 PG 29 FIG 11. AT SAA/SAT DURING PAX MOD DUCUMENTED ON W/O 89214700001.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

SDR - FLOOR SUPPORT ANGLE CORRODED RBL 44 AT STA 148 AND 160. FABRICATED FLOOR SUPPORT ANGLE, LOCATED AND DRILLED FLOOR SUPPORT STRUCTURE PER DC9/MD80 SRM 53-14-1 PG 29 AND 51-104 PG 1. INSTALLED FLOOR SUPPORT ANGLE AT RBL 44 AT STA 148-160 IAW DC9/MD80 SRM 51-10-4 PG 1 AND SRM 51-30-5 PG 3. AT SAA/SAT DURING PAX MOD ON W/O 89214580001.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,181 hrs · 34,164 cycles

SDR - FLOOR STRUCTURE SUPPORT CORRODED LBL 44 ST STA 190. FABRICATED FLOOR STRUCTURE SUPPORT AT LBL 44 AT STA 190 TO 160 PER DC9/MD88 SRM 53-14-1 FROM EXTRUSION FROM 7075-T6. AT SAA/SAT DURING PAX MOD ON (TO 193058) W/O 89214720001.

Part: CONDUIT — MISSING (WINDSHIELD) · airframe 47,175 hrs · 34,159 cycles

AT CRUISE, WITH WINDSHIELD ANTI-FOG AND ANTI-ICE SWITCH ON, FLIGHT CREW REPORTED SPARKS SHOOTING OUT OF PROBE ON CENTER WINDSHIELD. TURNED OFF BOTH SWITCHES, ARCHING STOPPED. FOLLOWED QRH AND PULLED BOTH CIRCUIT BREAKERS. CONTACTED ATL. MAINTENANCE FOUND HEAT SHRINK MISSING FROM SENSOR TERMINALS. INSTALLED HEAT SHRINK AND REINSTALLED SENSOR PER MAINTENANCE MANUAL. OPERATION OF ANTI-FOG AND ANTI-ICE CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: STRAP — CORRODED (FUSELAGE) · airframe 46,494 hrs · 33,655 cycles

DURING PSV IN MSP FOUND STRAP CORRODED AT STA 1183-1193, L28R. FABRICATED NEW STRAP PER DWG 5930481.

Part: STRAP — CORRODED (FUSELAGE) · airframe 46,494 hrs · 33,655 cycles

DURING PSV IN MSP FOUND STRAP AT STA 1155-1163, L28R CORRODED. FABRICATED NEW STRAP PER DWG 5930181.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 46,494 hrs · 33,655 cycles

DURING PSV IN MSP FOUND ATTACH ANGLE CORRODED AT STA 1212, L28R. INSTALLED NEW PART PER MD88 SRM 53-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,494 hrs · 33,655 cycles

DURING PSV IN MSP FLOOR SUPPORT ANGLE AT STA 1116 TO 1155, RBL 22 WAS FOUND CORRODED. FLOOR SUPPORT ANGLE REPLACED PER SRM 53-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,494 hrs · 33,655 cycles

DURING PSV IN MSP FOUND CLIP ANGLES CORRODED AT STA 1212, L28R. REPLACED PER MD88 SRM 51-30-00.

Part: STRAP — CORRODED (FUSELAGE) · airframe 46,494 hrs · 33,655 cycles

DURING PSV IN MSP FOUND CORROSION ON STRAP AT STA 1163-1174,L28R. FABRICATED NEW STRAP PER DWG 5930481.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 46,494 hrs · 33,655 cycles

DURING PSV IN MSP ATTACH ANGLE WAS FOUND CORRODED AT STA 1155. FABRICATED NEW ANGLE PER DWG 5936469.

Part: STRAP — CORRODED (FUSELAGE) · airframe 46,494 hrs · 33,655 cycles

DURING PSV IN MSP FOUND CORROSION ON STRAP AT STA 1203-1212 L28R. FABRICATED NEW STRAP PER DWG 5930481.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 46,494 hrs · 33,655 cycles

DURING PSV IN MSP FOUND INTERCOSTAL ATTACH FLANGE CORRODED. FABRICATED NEW ATTACH FLANGE PER SRM 53-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,494 hrs · 33,655 cycles

DURING PSV IN MSP FOUND FLOOR SUPPORT CORRODED AT STA 1212, L28R-L29R. REPLACED PER MD88 SRM 53-01.

Part: STRAP — CORRODED (FUSELAGE) · airframe 46,494 hrs · 33,655 cycles

DURING PSV IN MSP FOUND STRAP CORRODED AT STA 1174-1183, L28R. FABRICATED NEW STRAP PER DWG 5930481.

Part: STRAP — CORRODED (FUSELAGE) · airframe 46,494 hrs · 33,655 cycles

DURING PSV IN MSP FOUND CORROSION ON STRAP AT STA 1183 TO 1203 L28R. FABRICTED NEW STRAP PER DWG 5930481.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 46,494 hrs · 33,655 cycles

DURING PSV IN MSP A 2.5 INCH LONG CRACK COMMON TO THE CANTED PRESSURE PANEL JAMB PAN LOCATED AT STA 69. THE CRACK IS LOCATED IN THE LOWER RADIUS OF THE VERTICAL LEG OF THE PAN. REPAIRED PER ER/A 493840-14 REV 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,494 hrs · 33,655 cycles

DURING PSV VISIT IN MSP JUN2011, A CRACK WAS FOUND ON THE FUSELAGE SKIN AT APPROX STA 1437 JUST ABOVE L3R. THE CRACK EMANATES FROM AN EXISTING LOWER MOST FASTENER HOLE ALONG THE STA 1437 SHEAR TIE. SUBJECT FUSELAGE SKIN MADE FROM 0.063 INCH THICK 2024-T3 CLAD AL. REPAIRED PER ERA09-493755-14.

Part: SILL — CORRODED (FUSELAGE) · airframe 46,494 hrs · 33,655 cycles

DURING PSV IN MSP THE AFT CARGO DOOR SILL (L28R) WAS FOUND CORRODED. BEAM WAS REPLACED PER SRM 53-01 AND ER/A 493754-14.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,454 hrs · 33,629 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND BOTH EMERGENCY EXIT LIGHTS ABOVE FWD OVERWING DOORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACKS PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 44,517 hrs · 32,359 cycles

DURING LINE CHECK, MX FOUND EMERGENCY PATH LIGHTS INOP AT SEAT 25E. MX RELAMPED AND REPLACED A DISCONNECTED CONNECTOR IAW AMM 20-50-04. OPERATION OF LIGHT NOW CHECKS GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 43,089 hrs · 31,397 cycles

DURING L/O INSPN FOUND ROW 1-10 EMERGENCY LIGHTS NOT WORKING. REPLACED FWD EMERGENCY POWER SUPPLY AND REPAIRED WIRE AT SEAT 3C. OPS CHECKS GOOD IAW M/M.

Part: DAU — CONTAMINATED (E&E BAY) · airframe 41,665 hrs · 30,441 cycles

DURING DESCENT GOT BURNING ODOR IN CABIN AND GALLEY THAT SEEMED TO ORIGINATE FROM FWD GALLEY AREA. SIMULTANEOUSLY GOT "FLT RECORDER OFF" MSG ON OAP. SECURED GALLEY POWER AND CABIN LIGHTING AND SMELL DISSIPATED. NO SMOKE WAS NOTED. APPEARS COFFEE FROM GALLEY ABOVE DRIPPED ON DFDAU AND CAUSED FAULT. INSTALLED DFDAU. DFDR OPS CHECKS NORMAL AS PER M/M 31-31-02. CONFIRMED DFDAU BURNT.

Part: LATCH — WRONG PART (LT NACELLE) · airframe 39,702 hrs · 29,195 cycles

LEFT ENGINE COWL LATCH HOOK ASSEMBLIES (4) WERE ACTUALLY HAD THE WRONG PART NUMBER AND REPLACED IAW 09-056907-12.

Part: SLAT SYSTEM — INOPERATIVE (LE SLATS) · airframe 38,335 hrs · 28,273 cycles

SLATS WILL NOT RETRACT FROM ZERO DEGREE POSITION.

Part: FAN BLADE — BENT (NR 1 ENGINE) · airframe 37,773 hrs · 27,952 cycles

DURING CLIMB-OUT, NR 1 ENG HAD TWO COMPRESSOR STALLS AND FLAMES AS REPORTED BY F/A AND PASSANGERS. REPLACED 1ST STAGE FAN BLADES PER TRANS 9T133.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2

S/O 291016 N/R 20817 AND N/R 21350 CORROSION AROUND FASTENER HOLES IN L-22L END FITTING FWD OF FS 1338. REMOVED CORRODED END FITTING. REPAIRED CORROSION AROUND FASTENER HOLES IN L-22L END FITTING FWD OF FS 1338. REMOVED CORRODED END FITTING, FABRICATED AND INSTALLED END FITTING IAW DWG. NR 4914954 FROM S2647332-12000 EXTRUSION AND SRM 51-10-4, 51-10-3D, AND 51-30-5.

Part: CARGO TRACK — CORRODED (ZONE 600) · corrosion level 2

CORROSION IN FASTENER HOLES ON TRACK MID PIT FS 788 TO 769 RT. REMOVED CORRODED SECTION OF TRACK. FABRICATED AND INSTALLED REPAIR TRACK SECTION 75.5 X 3.75 INCHES FROM 7075-T6511 AND SPLICE 13 X 1.5 X .8 X 1.25 INCHES FROM 7075-T6 .071 AND 3 EACH SPLICE DOUBLERS 13 INCHES, 12 INCHES AND 12.25 INCHES FROM 7075-071 IAW MD80 SRM 51-10-3D, 51-30-1, AND 53-05D.

Part: SILL — CORRODED (AFT CARGO BAY) · corrosion level 2

FOUND CORROSION ON AFT PIT DOOR SILL 5TH HOLE INSIDE AFT O/B SIDE. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLERS 9" BY 2" FROM 7075-T6 .090" AND 9" BY 2-1/2" FROM .040" TITANIUM IAW MD-80 SRM 53-05D, 53-01, 51-30-5, 51-10-4 AND 53-34-0.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2

CORROSION ON FLOOR SUPPORT STRUCTURE AT LBL 46 AND BETWEEN FS 160 TO 200. REMOVED CORRODED SUPPORT. FABRICATED AND INSTALLED FLOOR SUPPORT 35" BY 1" FROM 7075-T6511 IAW MD-88 SRM 53-01 FIG 1, 51-30-2, 51-30-1, AND 51-10-4.

Part: CUSP WEB — CORRODED (BS 160-200) · corrosion level 2

CORROSION ON CUSP WEB AT L-1 DOOR CUTOUT FROM FS 160 TO 200 WL 208. REMOVED CORRODED CUSP WEB. FABRICATED AND INSTALLED CUSP WEB REPAIR 12.5" BY 1.3" FRP, 2024-T3 .071", 6-1/4" DIAMETER WEB REPAIR FROM 7075-T6 .025" AND 3 CUSP ANGLE SPLICE REPAIRS (1) 8.1" BY 4.8" BY 1.7" AND (2) FROM 7.6" BY 5.75" BY 2" FROM 7075-TPS-1003 .080" IAW MD-88 SRM 53-05D, 51-30-1, 53-01 FIG 1, 51-30-2, 51-30-1, 51-10-4.

Part: STRINGER — CRACKED (FUSELAGE) · corrosion level 2

PITTING CORROSION AND CRACK IN AFT ACCESSORY TAIL COMPT O/H AT FS 1418 S-2R. REMOVED CRACKED STRINGER, FABRICATED AND INSTALLED STRINGER REPAIR 15-1/8" BY 2-1/4" FROM 7075-T6511 60-4640 EXTRUSION IAW MD-80 SRM 53-02D, AND 51-30-5.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2

CORROSION AROUND FASTENER HOLES IN L-23L END FITTING AT FS 1338. REMOVED CORRODED END FITTING. FABRICATED AND INSTALLED END FITTING 14-3/8" BY 2-3/4" FROM 7075-T6 MATERIAL IAW DC-9/MD-80 SRM 51-10-3, 51-10-4, 51-30-5, AND 51-30-2.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2

CORROSION AROUND FASTENER HOLES IN L-28L END FITTING AT FS 1338. REMOVED CORRODED END FITTING. RECEIVED AND INSTALLED END FITTING P/N 5936439U1 IAW DC-9/MD-80 SRM 53-01, 51-30-5, AND 51-30-05.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2

S/O 291016 N/R #21053 CORROSION ON LOWER DOOR JAMB AREA FROM FS 370 TO 427 IN FWD CARGO COMPT. REPAIRED CORROSION ON LOWER DOOR JAMB AREA FROM FS 370 TO 427 IN FWD CARGO COMPT BY REMOVING CORRODED SPLICE, FABRICATED AND INSTALLED SPLICE 5.5” X .25” X .50” FROM 2024-T3 .063” IAW MD-80 SRM 51-10-4, 51-10-2, 53-21-0, 51-30-2 AND 51-30-5.

Part: SKIN — DENTED (MID CARGO DOOR)

TWO EACH DENTS ON FUSELAGE SKIN AT BS 218 AT L-19L. CUT OUT DENTED REPAIR AREA. FABRICATED AND INSTALLED REPAIR DOUBLER 13.5 X 2.5 FROM 2024-T3 .063, DOUBLER 14.5 X 14.5 FROM 2024-T3 .050 AND DOUBLER 7.25 X 3 FROM 7075-T6 .025 IAW MD80 SRM 53-04 FIG 12B AND 51-30-1.

Part: FRAME — CORRODED (BS 160)

FOUND CORROSION ON FRAME AT L-1 DOOR CUTOUT BS 160 WL-208. MECHANICALLY REMOVED CORROSION. ORIGINAL THICKNESS .125, MATERIAL LOSS .025. FOUND WITHIN LIMITS IAW MD-88 SRM 53-01 FIG 1. TREATED AND PRIMED IAW MD-88 SRM 51-10-3D.

Part: SKIN — LIGHTNING STRIKE (BS 360-438)

LIGHTNING STRIKE RT FUSELAGE SKIN FS 360 TO 438 L-18R TO L-22R. FABRICATED AND INSTALLED REPAIR DOUBLER 13.5 X 5.375 INCHES FROM 2024-T3 .160 IAW MD80 SRM 51-10-3, AND 53-05D.

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

FOUND CORROSION RT O/B SEAT TRACK FS 465 TO 217 ALSO NICKS AND GOUGES OUT OF LIMITS. REMOVED SECTION OF SEAT TRACK. FABRICATED AND INSTALLED SEAT TRACK REPAIRS 13" BY 3-5/16" AND 7.0" BY 3-5/16" FROM 7075-T6 .063" AND 2 REPAIR STRAPS FROM 7075-T6 .090" IAW DC-9 53-05D.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2

FOUND CORROSION ON NR 2 RAD/ALT ANTENNA LANDING BETWEEN FS 636 AND 655 B/L 0 (FWD PIT). REMOVED AND REPLACED ANTENNA DOUBLER P/N D539201648 IAW MD-80 53-01.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2

CORROSION ON CARGO TRACK LT AT FLOOR PANEL SCREW HOLES FROM FS 1220 TO 1322. REMOVED CORRODED CARGO TRACK END FITTING. RECEIVED AND INSTALLED P/N 5936663-503N IAW MD-80 SRM 53-05D, 51-30-0.

Part: SEAT TRACK — CORRODED (BS 1174-1309) · corrosion level 2

FOUND CORROSION MAIN CABIN LT O/B SEAT TRACK FS 1174 TO 1309 ALSO NICKS AND GOUGES OUT OF LIMITS. REMOVED SEAT TRACK. FABRICATED AND INSTALLED SEAT TRACK REPAIRS 13" BY 1" FROM 7075-T6 .125", 13.0" BY 1" FROM 7075-T6 .090", 13" BY 1" FROM 7075-T6 .100" AND 7.0" BY 4.0" FROM 7075-T6 .063" IAW DC-9 53-05D.

Part: SKIN — CHAFED (NR 2 SLAT)

RIGHT WING NR 2 SLAT AT MID TRACK, L/E CHAFED ON I/B SIDE. FABRICATED AND INSTALLED REPAIR DOUBLER 6 X 6.5 INCHES FROM 7075-T6 .063 IAW MD80 SRM 51-10-3, 51-30-5, AND 51-30-2.

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

FOUND CORROSION ON UPPER SURFACE OF CUSP WEB BETWEEN FRAMES AT BS 1174 TO BS 1193 RT SIDE OF PASSENGER CABIN. REMOVED CUSP WEB BS 1174 TO 1212 RT IAW DELTA MD-80 SRM 51-30-1. FABRICATED AND INSTALLED REPAIR CUSP 76.75" BY 14.75 FROM 2024-T3 .040" IAW MD-80 SRM 51-10-2, 51-10-3D, 51-10-4, 51-30-5, 53-24-00 FIG 802D.

Part: CUSP WEB — CORRODED (BS 1136-1155) · corrosion level 2

CORROSION ON CUSP WEB UPPER SURFACE FS 1136 TO 1155 RT SIDE. REMOVED CUSP WEB, FABRICATED AND INSTALLED WEB REPAIR 77.0" BY 15.0" FROM 7075-T6 .040 IAW MD-80 SRM 51-10-4, 51-10-2, 51-70-1, 51-30-5, 51-60-0 AND PROCESS STANDARD 900-2 NR 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON NUT PLATE ON FLOORBEAM LT AFT LAV COMPT FS 1338 (3 EA). DRILLED AND INSTALLED NEW FLOORBEAM REPAIR ANGLES 45.5 X 1 X .75 INCH FROM AND 10134-1601 7075-T6511 AND 10.5 X 1 X .75 INCHES FROM 7075-T6511.090" IAW MD-88 SRM 51-10-3, 51-40-4, AND 51-10-3D.

Part: SEAT TRACK — CORRODED (BS 217-266) · corrosion level 2

CORROSION BLENDED OUT OF LIMITS AT RIGHT INBOARD SEAT TRACK FS 217 - 266. REMOVED AND REPLACED CORRODED SEAT TRACK WITH P/N 539201580 65 X 4 INCHES IAW MD-80 SRM 53-05D, 51-10-3 AND 51-30-5.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,305 hrs · 29,686 cycles

S/O 291018 NR 24233 CORROSION WING TO BODY FAIRING SUPPORT BS 1020 TO BS 1040 LBL 6. FABRICATED AND INSTALLED REPLACEMENT SUPPORT 20" X 3" FROM BAC1505-100049 7075T73 IAW B757-200 SRM 53-40-71, 51-20-01 AND 51-40-02.

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

CORROSION ON LEFT I/B SEAT TRACK FS 217 TO FS 256. CUT OUT CORRODED SECTION OF SEAT TRACK FROM FS 200 TO FS 306 LEFT I/B. DRILLED UP AND INSTALLED NEW SECTION OF SEAT TRACK 104.75 X 3.75 INCHES FROM 7075-T6511 AND SPLICE 7.375 X 2.125 INCHES FROM 7075-T6 .050 INCH IAW DC-9/MD-80 SRM 53-05D FIG 4F.

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

S/O 291016 NR 20716 CORROSION ON CABIN FLOOR SUPPORT FS 1155 LBL 33 TO 42. REMOVED CORRODED SECTION OF SUPPORT. FABRICATED AND INSTALLED FLOOR SUPPORT 12.05" X 2.05" X .50" FROM 52929169 IAW MD-80 SRM 51-10-2, 51-30-5, 51-10-3 AND 53-01.

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

S/O 291016 NR 20715 CORROSION ON CABIN SEAT TRACK AT BS 1138 TO 1167 LBL 44. REMOVED CORRODED SECTION OF SEAT TRACK. INSTALLED SECTION OF SEAT TRACK P/N D539201581 IAW MD-80 SRM 51-30-1 PG 1 - 4, 4A, 53-05D FIG 4B, 4H, 4F, 53-24-0 FIG 6, 51-10-4, 51-10-1 FIG 26, 51-40-2 PG 6, 7.

Part: SKIN — DENTED (L/E SLAT)

S/O 291016 NR 20089 LT WING L/E SLAT NR 1 HAS SEVERAL DENTS ON TOP. CUT OUT DENTED AREA OF SKIN. FABRICATED AND INSTALLED SLAT NOSE REPAIR 14.25" X 2.55" AND 2.25" X 2.80" FROM 2014-T6 .050", AND 2.25" DIAMETER FROM 2024-T3 .100" AND SLAT LEADING EDGE REPAIR 16" X 9.35" FROM 2014-T6 .063" IAW MD80 SRM 51-10-3, 51-30-2, 57-09 FIG 10, 10A.

Part: SKIN — DAMAGED (FUSELAGE)

S/O 291016 NR 25470 RT FUSELAGE SKIN AT LONGERON 22 FS 270 DENT/CREASED. CUT OUT DENTED/CREASED SECTION OF SKIN. FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR 10-1/2" X 6-1/2 FROM 2024-T3 .050 AND INTERNAL FINGER DOUBLER 11.5" X 8-1/4" FROM 2024-T3 .025 IAW MD-80 SRM 53-04D FIG 38.

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

S/O 291016 NR 20611 CORROSION ON FLOOR SUPPORT STRUCTURE AT BS 160 TO 200 RBL 46. REMOVED CORRODED FLOOR SUPPORT. FABRICATED AND INSTALLED FLOOR SUPPORT 37" X 1.75" X .070" FROM 2929169 IAW MD-80 SRM 53-14-1, 51-30-2, 51-10-3 AND 51-30-5 PG 12.

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

S/O 291016 NR 20603 CORROSION ON FLOOR SUPPORT STRUCTURE AT BS 200 FROM RBL 12 TO RBL 56. REMOVED CORRODED FLOOR SUPPORT. FABRICATED AND INSTALLED FLOOR SUPPORT 46" X 2" FROM 2929169 IAW MD-80 SRM 53-14-1, 51-30-2, 51-10-3 AND 51-30-5 PG 12.

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

S/O 291016 NR 20985 CORROSION ON LT I/B SEAT TRACK FS 1155 TO 1309 ALSO NICKS AND GOUGES. REMOVED CORRODED SECTION OF SEAT TRACK. FABRICATED AND INSTALLED SEAT TRACK 123" X 4" FROM 539201580 EXTRUSION, SPLICE 5.19" X 3" FROM 60-7158 AND SPLICE 5.19" X 3" FROM 7075-T6 .050 IAW MD-80 SRM 53-05D.

Part: SKIN — DAMAGED (FUSELAGE)

S/O 291016 NR 20013 FUSELAGE SKIN AT BS 218 AT L19L HAS A TEMPORARY REPAIR. CUT OUT TEMPORARY REPAIR AREA. FABRICATED AND INSTALLED REPAIR DOUBLER 13-1/2 X 2-1/2 FROM 2024-T3 .063, DOUBLER 14-1/2 X 14-1/2 FROM 2024-T3 .050 AND DOUBLER 7-1/4 X 3 FROM 7075-T6 .025 IAW MD80 SRM 53-04 FIG 12B AND 51-30-1.

Part: SKIN — DAMAGED (FUSELAGE)

S/O 291016 NR 20108 AND 20109 CREASE AT LONGERON 18L & 19L FROM BS 230 TO 236AND 237. CUT OUT CREASED AREA OF SKIN. FABRICATED AND INSTALLED FUSELAGE SKIN REPAIRS 11-1/4" X 10-1/4" FROM 2024-T3 .050" AND 9-1/4" X 3" FROM 7075-T6 .025" AND 10-1/4" X 11-1/4" FROM 2024-T3 .050" IAW MD80 SRM 53-04D FIG 12B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,305 hrs · 29,686 cycles

S/O 291018 NR 24028 CORROSION ON CABIN RT I/B SEAT TRACK AT 3 EA PLACES FROM BS 365.25 TO 387. REMOVED CORRODED SEAT TRACK. FABRICATED AND INSTALLED SEAT TRACK SECTION FROM BAC1520-792 IAW B757 SRM 53-00-52 AND 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,305 hrs · 29,686 cycles

S/O 291018 NR 24041 CORROSION ON CABIN LT I/B SEAT TRACK AT 2 EA PLACES FROM BS 377 TO 395. REMOVED CORRODED SEAT TRACK BS 377 TO BS 440. INSTALLED SEAT TRACK SECTION FROM BAC1520-792 IAW B757 SRM 53-00-52 FIG 101.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · corrosion level 2 · airframe 61,305 hrs · 29,686 cycles

S/O 291018 NR 24066 CABIN FLOOR SUPPORT CORRODED AND CRACKED BS 1645 TO BS 1655 RBL 56. CUT OUT CORRODED AND CRACKED SECTION. NDT VERIFIED CRACK CONTAINMENT IAW B757 NDT MNC PART 6. FABRICATED AND INSTALLED DOUBLER FROM 7075-T6 .071 IAW B757-200 SRM 51-70-13 FIG 1 SHEET 2.

Part: LINE — CONTAMINATED (NR 2 ENGINE) · airframe 32,905 hrs · 24,772 cycles

RIGHT ENG EPR INDICATION STUCK AT 1.06, DRAINED WATER FROM PT7 LINES.

Part: PROXIMITY SWITCH — FAILED (MLG) · airframe 31,720 hrs · 23,898 cycles

AFTER RETRACTION OF LANDING GEAR RED UNSAFE LIGHT ON LEFT GEAR APPEARED. REPLACED UPLOCK PROX SWITCH.

Part: BALLAST — OVERHEATED (GALLEY) · airframe 30,178 hrs · 22,767 cycles

FIRST CLASS GALLEY COUNTER WORK LIGHT BALLAST OVERHEATED CAUSING HOT ODOR. REPLACED SAME.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 25,315 hrs · 19,357 cycles

FOUND ON L/O AFT EMERGENCY LIGHTS INOPERATIVE. FOUND FUSE F1 OPEN ON B5-212 REPLACED BASE AND FUSE OPEN CHECKS OK

Part: APU — CONTAMINATED (AFT) · airframe 19,269 hrs · 15,012 cycles

AFTER TO PASSING 3000 FT FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. RETURNED TO NEWARK. SMOKE SEEMED TO BE MOVING FROM FORWARD CABIN AFT SMOKE DISSIPATED AFTER APPROXIMATELY 5 MINS. PERFORMED DUCT BURNOUT. FOUND APU INLET CONTAMINATED. REPLACED COALESCER BAGS.

Part: STRUCTURE — VIBRATION (FUSELAGE) · airframe 18,846 hrs · 14,700 cycles

FLIGHT CONTROLS FEEL UNUSUAL DURING CLIMB. VIBRATION IN BOTH YOKES AND FLOOR, OCCURRED WITH A/P 1 AND 2 AND HAND FLOWN, ALL FLT LEVELS AND AIRSPEED. MORE PRONOUCED WITH PITCH CHANGES. REPLACED MACH TRIM ACTUATOR, NR 2 DFGC, AND AILERON DUAL SERVO.

Part: ACM — FAILED (LEFT)

ELECTRICAL FUMES DETECTED IN CABIN AND COCKPIT AT FL 350, HAZE DISSIPATED IN COCKPIT WITHIN ONE MINUTE AND WITHIN FOUR MINUTES IN CABIN. FOUND LT ACM SEIZED. REPLACED SAME, RAN PACKS AND ENGS. ALL CK GOOD.

Part: APU — LEAKING (CABIN)

AFTER T/O, MID CABIN TO AFT SMELL OF SMOKE. RETURNED ATL. F/A VERIFIED ODORS 3 TIMES DURING APPROACH. AN UNUSUAL VIBRATION AFT END WAS ACCOMPANYING THE SMELL. FOUND APU LEAKING INTERNALLY. REMOVED AND REPLACED APU, PERFORMED DUCT BURNOUT PER M/M. REMOVED AND REPLACED H2O SEPARATOR BAGS, A/C CKS OK.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

AT ROTATION, THE NR 2 ENGINE HAD A SEVERE COMPRESSOR STALL. FLIGHT RETURNED TO AUS. THE NR 1 ENGINE WAS FIREWALLED WITH FLASHING PARAMETERS. NR 2 ENGINE CHANGED.

Part: HOSE — LEAKING (RT HYD SYSTEM)

A/C LOST RT HYD PRESSURE AND FLUID, USED EMERGENCY PROCEDURES. REPLACED RT ENGINE HYD PUMP MAIN PRESSURE LINE.

Part: SLIDE — DEFECYIVE (L2 DOOR)

L2 DOOR SLIDE BOTTLE PRESS LOW. REPLACED DOOR SLIDE.

Part: LENS — MISSING (CABIN)

SEAT 23 EMERGENCY TRACK LIGHT HAS BULB COVER MISSING. REPLACED LENS AND BULB.

Part: FRAME — CRACKED (LT MLG DOORWAY)

FUSELAGE / OPENING FRAME / MLG DOOR / LH WHEEL WELL /FS937: CRACK REPAIR THE FWD SURROUND FRAME OF THE MLG DOOR CUTOUT AT FS 937 (LH)WAS FOUND WITH A 3 LONG CRACK IN THE INBD FLANGE. THE CRACK WAS TRIMMED OUT AND REPAIRED WITH 2 SHEET METAL ANGLESPER ER/A 363132-14.

Part: OXY REGULATOR — LEAKING (COCKPIT)

COCKPIT O2 PRESS LOW FOUND REGULATOR LEAKING AT B NUT INSP. HOLE. REPLACED REGULATOR AND BOTTLE. SYS LK CK GOOD.

Part: LIGHT — DAMAGED (CABIN)

PAX SEAT 37B EMERGENCY TRACK LIGHTING FLOOR LIGHT DAMAGED. REPAIRED LIGHT, OPS NML.

Part: OIL FILTER — LOOSE (NR 2 ENGINE)

AFTER T/O LGA, LOST OIL PRESSURE NR 2 ENGINE, ENGINE SHUTDOWN. DIVERTED PHL, FOUND 2 ENGINE OIL FILTER COVER STUDS LOOSE. REPLACED CKS OK.

Part: STRUT — REQD SERVICE (NLG)

NOSE GEAR UNSAFE LIGHT ON RETRACTION, CYCLED SAME LIGHT WITH CORRESPONDING NOISE. SERVICED NOSE STRUT PER JIC OP 4703, JACKED A/C, CYCLED NOSE GEAR AND ALL IND NORMAL. A/C OK FOR SERVICE.

Part: STRUT — REQD SERVICE (NLG)

NOSE GEAR UNSAFE LIGHT ON RETRACTION, CYCLED SAME LIGHT WITH CORRESPONDING NOISE. SERVICED NOSE STRUT PER JIC OPN 4703, JACKED AN CYCLED NOSE GEAR AND ALL INDICATIONS NORMAL. A/C OK FOR SERVICE.

Part: SYB GENERATOR — FAILED (LEFT)

DURING CRUISE, CAPTAINS PFD WENT BLANK, LANDED CVG. REPLACED SYB GENERATOR OPERATION NORMAL.