N927DA

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 75,240 hrs · 56,654 cycles

EMERGENCY LIGHTS INOPERATIVE SEATS 10D, 27D, AND 33D. CHECK LIGHTS AND WIRING. CONNECTED THE CONNECTORS. CHECKED GOOD.

Part: SHUTOFF VALVE — LEAKING (RUDDER) · airframe 74,284 hrs · 55,910 cycles

DURING FLIGHT, CREW REPORTED RIGHT HYDRAULIC FLUID QUANTITY LOSS AND ACCOMPLISHED QRH PROCEDURE SECURING RIGHT HYDRAULIC SYSTEM PUMPS. ON APPROACH, ATTEMPTED TO RE-PRESSURIZE RIGHT HYDRAULIC SYSTEM PER QRH AND THE SYSTEM FAILED TO PRESSURIZE. ACCOMPLISHED ALTERNATE GEAR EXTENSION, LANDED SAFELY, AND TOWED TO THE GATE. APU WAS NOT OPERATED. MAINTENANCE CONFIRMED LEAK AT THE RUDDER SHUT-OFF VALVE. THE RUDDER SHUT-OFF VALVE WAS REMOVED AND REPLACED, AIRCRAFT TAIL COMPARTMENT CLEANED AND MINI DUCT BURN OUT ACCOMPLISHED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,860 hrs · 55,599 cycles

AIR STAIR EMER LIGHTS INOP. REPLACED BATTERIES AFT EMER LIGHT BATTERY PACK REF AMM 33-53.

Part: PIN — OUT OF ADJUST (TAILCONE RELEASE) · airframe 73,692 hrs · 55,467 cycles

TAILCONE RELEASE MECHANISM CAM ASSY. PIN IS IMPROPERLY INDEXED ON SPLINE. REINDEXED CAM RELEASE PIN PER MD88 AMM 53-53-02-201, O.K. FOR SERVICE.

Part: VALVE — FAILED (CABIN PRESSURE) · airframe 73,578 hrs · 55,381 cycles

AFTER TAKEOFF AT 3000FT CABIN AND FLIGHT CREW NOTICED THAT AIRCRAFT WAS LOSING CABIN PRESSURE. AT 12,000FT MSL MAX CABIN ALTITUDE REACHED 10,500FT. CABIN ALTITUDE AND MASTER WARNING LIGHTS WERE ILLUMINATED ALONG WITH CABIN ALTITUDE WARNING HORN SOUNDING. ATB TO SAV. INSPECTED PACKS FOR DUCT LEAKS IN TAIL COMPARTMENT. NO LEAKS NOTED. CABIN WOULD NOT PRESSURIZE ABOVE 3.5 PSI. FOUND OUTFLOW NOZZLE VALVE LEAKING EXCESSIVE AIR. REMOVED AND REPLACED NOZZLE VALVE AND ADAPTER RING SHIM IAW AMM 21-32.

Part: SLIDE — MALFUNCTIONED (L1 DOOR) · airframe 73,244 hrs · 55,128 cycles

DOOR 1L OPENED BY FA WHILE ARMED. SLIDE DID NOT DEPLOY. INSPECTED SLIDE VERIFIED PARACHUTE PINS ARE INSTALLED. REINSTALLED SLIDE ON L1 DOOR PER AMDS CARD 2561-4964. OK FOR SERVICE.

Part: SKIN — DAMAGED (BS 1174) · airframe 71,566 hrs · 53,837 cycles

LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN BS 1174 AND LONGERON 1. EXTERNAL FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04-1, PAR 6 D, 3, COND 3, AMM 25-28-00-201, AMM 21-00-00-401, ETI 88-16 -175, REV 5, ER/A 545136-14 MA, REV ORIGINAL, AND PS 900-5-1, NR 04. REPETITIVE INSPECTIONS MUST BE ACCOMPLISHED WITH LOG 2455633.

Part: SKIN — CORRODED (BS 200-218) · corrosion level 2 · airframe 71,560 hrs · 53,833 cycles

CORRODED PREVIOUS REPAIR DOUBLER BETWEEN BS 200 TO 218, LONGERON 29LT TO 30 AT ELECTRONIC EQUIPMENT COMPARTMENT. REPAIR WAS ACCOMPLISHED IAW ER/A 545129-14, REV ORIGINAL AND ERI -88-16-171, REV 1, SECTION 1.

Part: SKIN — CORRODED (BS 1309) · corrosion level 2 · airframe 71,560 hrs · 53,833 cycles

CORROSION ON INNER PRODUCTION DOUBLER BS 1309, OUTFLOW VALVE AREA. DUE TO EXCESIVE CORROSION DOUBLER WAS REPLACED IAW SRM 51-10-4M, 51-10-3, PAR 21 AND 14, 51-30-2 AND 51-30-5, AND DWG 5936021.

Part: SKIN — DAMAGED (RUDDER) · airframe 71,560 hrs · 53,833 cycles

EXPOSED MATERIAL ON LT, RT SIDE AT RUDDER. DAMAGE AREA BOTH SIDE WERE REPAIRED IAW ERA NR 092613-14MA, REV "A", SRM 51-70-01A, PAR 23 AND ERA NR 545122-14, REV ORIGINAL.

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 71,560 hrs · 53,833 cycles

HINGE EDGE ON RUDDER LT/RT SIDE. EDGE ON RUDDER LT & RT SIDE WERE REPAIRED IAW SRM 51-70-4AD AND OPEN 2304653.

Part: SKIN — CORRODED (BS 200-218) · corrosion level 2 · airframe 71,560 hrs · 53,833 cycles

FUSELAGE, SKIN, FS 200-218, L29-30L AT MODE S ANTENNA CORROSION REPAIR. ACCOMPLISH ER/A 545129-14, SECTION II.

Part: PAN — CRACKED (R1 DOOR) · airframe 71,560 hrs · 53,833 cycles

CRACKED PAN ON AFT UPPER AT R1 DOOR. PAN WAS REPAIRED IAW SRM 52-03D, FIG 3.

Part: LONGERON — CRACKED (BS 200) · airframe 71,560 hrs · 53,833 cycles

CRACKED LONGERON 29L, BS 200. THE LONGERON WAS REPLACED IAW SRM 53-14-1, FIG 3, 51-30-2 AND 51-30.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 71,560 hrs · 53,833 cycles

CRACKED BEAM NR 1 AFT EDGE AT FWD SERVICE DOOR. BEAM WAS REPLACED IAW SRM 51-30-2.

Part: BEAM — DAMAGED (R1 DOOR) · airframe 71,560 hrs · 53,833 cycles

CRACKED PAN ON FWD EDGE AT NR 4BEAM FWD R1 SERVICE DOOR. BEAM WAS REPAIRED IAW SRM 52-03, FIG 3.

Part: SKIN — DAMAGED (RUDDER) · airframe 71,560 hrs · 53,833 cycles

EXPOSED MATERIAL ON LT & RT SIDE AT RUDDER. LT & RT SIDE AT RUDDER WERE REPAIRED IAW ER/A 092613-14MA, REV A, ER/A 545141-14, REV ORIGINAL.

Part: SKIN — DAMAGED (BS 484) · airframe 71,560 hrs · 53,833 cycles

ASSESS DAMAGE ON FUSELAGE SKIN BS 484, BETWEEN LONGERON 23-24 RT, SPEED TAPE ID DATA. REPAIR WAS EVALUATED AND FOUND ACCOMPLISHED IAW INSTRUCTIONS OF SRM 53-04-2, FIG 2, SHEET 5, AS PERMANENT REPAIR.

Part: BEAM — CRACKED (R1 DOOR) · airframe 71,560 hrs · 53,833 cycles

CRACKED BEAM NR 4 FWD EDGE AT FWD R1 DOOR. NR 4 BEAM WAS REPLACED IAW DWG 9911582, REV T, 51-30-1, 51-30-2, 51-30-4 AND 51-30-5.

Part: LONGERON — CRACKED (BS 180) · airframe 71,560 hrs · 53,833 cycles

CRACKED LONGERON 29R BS 180. LONGERON WAS REPLACED IAW SRM 53-02, FIG 18, SHEET 2, 51-30-2, 51-10-4, 51-30-5, PAR 7, FIG 10, PAR 14, 21.

Part: LONGERON — CRACKED (BS 200) · airframe 71,560 hrs · 53,833 cycles

CRACK ON LONGERON 4L BS 200. LONGERON WAS REPLACED IAW SRM 53-02, FIG 18, PAR 12, 51-30-5, AND CARD 5330-01204-02-03.

Part: LONGERON — CRACKED (BS 180) · airframe 71,560 hrs · 53,833 cycles

CRACKED LONGERON 29R BS 180 AT ELECTRONIC EQUIPMENT COMPARTMENT. LONGERON WAS REPLACED IAW SRM 53-02, FIG 18, SHEET 2, 51-30-2, 51-10-4, 51-30-5 PAR 7, FIG 10, PAR 14, 21.

Part: CARGO TRACK — CRACKED (BS 1212-1231) · airframe 71,560 hrs · 53,833 cycles

CRACK ON LOWER SUPPORT OF TIE TRACK BETWEEN BS 1212 TO 1231 AND PROJECTION LONGERONS 28LT TO 27LT AT AFT CARGO COMPARTMENT. SUPPORT WAS REPLACED IAW SRM 53-05, FIG 4G, 51-10-3, PAR 21,14, 51-30-2, 51-30-5.

Part: RIB — CRACKED (RT WING) · airframe 71,560 hrs · 53,833 cycles

CRACKED RIB ON RT WING FIXED L/E BS XRS 324. THE RIB WAS REPAIRED IAW SRM 57-06 B, D, FIG 18.

Part: SKIN — DAMAGED (BS 1287-1309) · airframe 71,560 hrs · 53,833 cycles

FUSELAGE SKIN DAMAGED BETWEEN BS 1287- 1309, LONGERON 26L.

Part: SUPPORT FITTING — CORRODED (MLG) · corrosion level 2 · airframe 71,560 hrs · 53,833 cycles

CORROSION ON MLG SUPPORT FITTING LOWER AREA BS XCW=98.500. AREA WAS REPAIRED IAW SRM 57-03, FIG 34, 51-10-3, P 14-21 AND 51-30-5.

Part: LONGERON — CRACKED (BS 160) · airframe 71,560 hrs · 53,833 cycles

AD 98-13-35, REV 1: CRACK ON LONGERON 2 LT BS 160, AT CPAX COMPLETE WC 5330-01204-0205. 1ST EVAL, LONGERON NR 2 WAS REPAIRED IAW SRM 51-30-2, 53-02, FIG 18, 51-10-4, 51-10-3 PAR 14 AND 21, 51-30-5.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 71,560 hrs · 53,833 cycles

CORROSION ON DOOR FRAME AT CARGO DOOR BS 650 - 690 LONGERON 28R. CORROSION WAS REMOVED AND REWORKED AREA WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 26, 21, 14. WITHIN LIMITS IAW SRM 53-05, FIG 123.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,215 hrs · 53,604 cycles

MAINTENANCE FOUND THE AFT CEILING EMERGENCY LIGHTS INOPERATIVE. BATTERIES WERE REPLACED AND THE LIGHTS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 66,283 hrs · 50,146 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 27D/E IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYS.

Part: TOGGLE — FAILED (TAILCONE SLIDE) · airframe 65,165 hrs · 49,383 cycles

ACFT FAILED THE FUNCTIONAL CHECK OF TAILCONE RELEASE SYS WHEN A WORN TOGGLE ON THE SLIDE LANYARD PREVENTED THE SLIDE FROM DEPLOYING. THE TOGGLE WAS REPLACED, THE SYS WAS RETURNED OPERATIONAL STATUS, AND THE RII WAS COMPLETED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,052 hrs · 49,309 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE LT AND RT OVERWING DOORS WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 65,032 hrs · 49,297 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 19R IN THE CABIN WAS INOPERATIVE. MX FOUND A LOOSE PIN IN THE CONNECTOR AND RE-PINNED IT. THE SYS RETURNED TO NORMAL OPERATION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,986 hrs · 49,259 cycles

DURING LINE CHECK, MX FOUND THAT MULTIPLE OVERHEAD EMERGENCY PATHWAY LIGHTS IN THE MID-CABIN WERE INOPERATIVE. MX REPLACED THE POWER SUPPLY AND RELAMPED AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 63,325 hrs · 48,072 cycles

ON BOLT HOLE INSPECTION OF VERTICAL STAB, FOUND OVERSIZED HOLE WITH CRACK INDICATION. FOUND HOLE TO BE LARGER THAN .202" ALLOWABLE HOLE SIZE. OVERSIZED HOLE WAS REPAIRED IAW FINAL ER/A 510507-14AD REV ORIG ASSOCIATED ER/A 14-510507 ADDED FOR AC 0927.

Part: RELEASE MECH — STUCK (TAIL CONE) · airframe 63,325 hrs · 48,072 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE SYS CAM WAS STUCK, CAM AND BLOCKS FOR THE RELEASE CABLE WERE WORN AND OUT OF RIG BEYOND ALLOWABLE LIMITS. THE MATING FLANGE WAS CRACKED AT MULTIPLE ALIGNMENT PIN POSITIONS. THE CABLE CAMS AND BLOCKS WERE REPLACED AND RIGGED TO SPECIFICATIONS. CRACKS WERE REPAIRED IAW AMM 53-53.

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 63,325 hrs · 48,072 cycles

ON BOLT HOLE EC INSPECTION OF RT SIDE VERTICAL, 3 HOLE DOWN FROM COLLAR, FAULT FOUND OVERSIZED HOLE WITH CRACK INDICATION, CLEAN UP OF HOLE, NO HELP. FURTHER CLEANUP OF SUSPECTED HOLE WITH CRACK AND FOUND HOLE TO BE LARGER THAN .202" ALLOWABLE HOLE SIZE. OVERSIZE HOLE WAS REPAIRED IAW PRI 510499-14AD. FINAL ER/A 510499-14AD, REV ORIG APPLIED. ASSOCIATED ER/A 14-510499 ADDED FOR AC 0927.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 63,325 hrs · 48,072 cycles

ON BOLT HOLE INSPECTION OF VERTICAL STAB, FOUND THREE HOLES DAMAGED. DAMAGE CLEAN-UP RESULTED IN OVERSIZING HOLES LARGER THAN ALLOWED SIZE. OVERSIZED HOLES WERE REPAIRED IAW ER/A 510499-14AD, REV ORIG ASSOCIATED ER/A 14-510499 ADDED FOR AC 0927.

Part: ATTACH FITTING — DAMAGED (VERTICAL STAB) · airframe 63,325 hrs · 48,072 cycles

COMPLETING BOLT HOLE EC OF VERTICAL STAB, FOUND 3 RT SIDE HOLES, THREAD CUT-DAMAGED INSIDE OF HOLES. REMOVED NUT PLATE CHANNEL & POLISHED HOLES. ACCOMPLISHED DVI OF REWORKED AREA, DAMAGE CONTAINED. ALL 3 HOLES ARE LARGER THAN THE .202" ALLOWABLE HOLE SIZE. ER/A 14-510499 ADDED FOR AC 0927.

Part: SEAT TRACK — CORRODED (BS 1287-1309) · airframe 1 hrs · 1 cycles

SEAT TRACK AT STA 1287-1309 LBL 22 HAS CORROSION ON TOP OF TRACK INSIDE CHANNEL IN 3 AREAS. SEAT TRACK REPLACED ON NRC7000098670001.

Part: SEAT TRACK — CORRODED (BS 1271-1287) · airframe 1 hrs · 1 cycles

SEAT TRACK AT BS 1271-1287 HAS CORROSION ON TOP OF TRACK AND INSIDE CHANNEL. SEAT TRACK REPLACED ON NRC 7000098670001.

Part: SEAT TRACK — CORRODED (BS 1155 LBL 22) · airframe 1 hrs · 1 cycles

SEAT TRACK STA 1155 LBL 22 HAS AREA OF CORROSION ON LT FLANGE AND BARE META. SEAT TRACK REPLACED ON NRC 7000098670001.

Part: SEAT TRACK — CORRODED (BS 1174-1193) · airframe 1 hrs · 1 cycles

SEAT TRACK AT STA 1174-1193 LBL 22 HAS 2 AREAS OF CORROSION ON LT FLANGE AND BARE METAL. SEAT TRACK REPLACED ON NRC 7000098670001.

Part: SEAT TRACK — CORRODED (BS 1250 RBL 54) · airframe 62,535 hrs · 47,495 cycles

SEAT TRACK AT BS 1250-1271 HAS CORROSION ON TOP OF TRACK AND DOWN IN CHANNEL. REPAIRED PER MD-88 SRM 51-30-1.

Part: CUSP WEB — CORRODED (FS 218-237) · airframe 62,535 hrs · 47,495 cycles

AIRCRAFT CABIN FLOOR RT CUSP WEB BS 218-237 HAS CORROSION ON FWD EDGE AND 11 ELONGATED AND CORRODED HOLES RBL 5H. CUSP WEB REPAIRED ON NRC 70000998860001/210013.

Part: SKIN — DENTED (BS 1375 L7R) · airframe 62,535 hrs · 47,495 cycles

RT FUSELAGE STA 1375 L-7R HAS A DENT JUST BELOW SKIN OVERLAP. ACCOMPLISHED ER/A 505309-14 REV ORIG.

Part: CUSP WEB — CORRODED (BS 933) · airframe 62,535 hrs · 47,495 cycles

MAIN CABIN RT CUSP WEB LOWER SURFACE HAS CORROSION AT BS 933. WEB REPLACED ON NRC 210001.

Part: DOUBLER — CORRODED (BS 593 L29-30R) · airframe 62,535 hrs · 47,495 cycles

MID CARGO LOWER BILGE POTABLE WATER DRAIN RING DOUBLER HAS CORROSION BS 593 BETWEEN L-29R AND L-30R. REPAIRED IAW SRM 53-04-2.

Part: CUSP WEB — CORRODED (BS 1060-1079) · airframe 62,535 hrs · 47,495 cycles

RT CUSP WEB CORRODED ON TOP THROUGHOUT BS 1060-1079. CUSP WEB REPLACED ON NRC 210624.

Part: SEAT TRACK — CORRODED (BS 266-797) · airframe 62,535 hrs · 47,495 cycles

CABIN SEAT TRACK SECTION LBL 54 FS 266-797 HAS PITTING CORROSION AT CTR CHANNEL AND LUGS FS 790-797. REPLACED SEAT TRACK IAW SRM 53-05.

Part: BEAM — CORRODED (BS 636 L29R) · airframe 62,535 hrs · 47,495 cycles

MID CARGO LOWER BILGE BEAM HAS CORROSION AT BS 636 AND L29R. COMPLIED WITH ER/A 505651-14 REV ORIG.

Part: PAN — CORRODED (AFT LAVATORY) · airframe 62,535 hrs · 47,495 cycles

LEFT AFT LAVATORY SERVICE PAN AND SERVICE LIGHT PLATE HAS CORROSION. REPAIRED PLATE PER SRM 51-30--0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,535 hrs · 47,495 cycles

WHILE PREFORMING NDT INSPECTION OPN NR 87052 AD, DETECTED SEVERAL CRACKS IN SKIN EMANATING FROM 4 FASTENERS AT UPPER FORWARD DOOR JAMB CORNER OF FORWARD CARGO COMPARTMENT. ACCOMPLISHED ER/A 505312-14AD REV ORIG.

Part: INTERCOSTAL — CORRODED (BS 629-636) · airframe 62,535 hrs · 47,495 cycles

MID CARGO LOWER BILGE INTERCOSTAL HAS CORROSION BETWEEN STA 629 TO 636 AND BETWEEN L-30/L-29R. REPLACED INTERCOSTAL IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 769-814) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN RT CUSP WEB HAS CORROSION BETWEEN BS 769 TO 814. REPLACED CUSP WEB IAW SRM 51-30-1.

Part: CUSP WEB — CORRODED (BS 465-522) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN LT CUSP WEB CORRODED UPPER AND LOWER SURFACE BS 465 TO 522. REPLACED CUSP WEB IAW SRM 51-30-0.

Part: SEAT TRACK — CORRODED (BS 252) · airframe 62,534 hrs · 47,494 cycles

CABIN SEAT TRACK SECTION RBL 54 FS 218-266 HAS CTR CHANNEL PITTING CORROSION AT FS 252. REPLACED SEAT TRACK IAW SRM 51-30-1.

Part: CUSP WEB — CORRODED (BS 712-807) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN LT CUSP WEB BS 712 TO 807 HAS CORROSION ON MULTIPLE PLACES. REPLACED CUSP WEB IAW SRM 51-30-0.

Part: FLOORBEAM — CORRODED (BS 1307 LBL 20) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN FLOORBEAM HAS CORROSION AT BS 1307 LBL 20. REPAIRED PER ERA 505314-14 ORIG.

Part: DOUBLER — RUSTED (BS 88.55) · airframe 62,534 hrs · 47,494 cycles

NLG LT TUNNEL BS 83.55 FLIGHT INTERPHONE INTERNAL REPAIR DOUBLER IS RUSTED/BARE METAL. COMPLIED WITH ERA 505304-14 REV ORIG.

Part: SKIN — CORRODED (BS 759-772.75) · airframe 62,534 hrs · 47,494 cycles

LOWER FUSELAGE PREVIOUS REPAIR DOUBLER AND RUBSTRIP HAVE CORROSION AT STA 759 TO 772.75 AND BETWEEN L-28-29R. REPAIRED PER ERA 505667-14 REV ORIG.

Part: SKIN — PUNCTURED (BS 1338 L9L) · airframe 62,534 hrs · 47,494 cycles

LEFT FUSELAGE EXTERNAL SKIN HAS DRILL START OR SEMI-PUNCTURE AT EDGE OF SKIN SPLICE BS 1338 AND L9L. REPAIRED PER ER/A505307-14 REV ORIG.

Part: SKIN — DAMAGED (BS 759 L28-29R) · airframe 62,534 hrs · 47,494 cycles

ONE ELONGATED HOLE ON FUSELAGE SKIN AT BS 759 BETWEEN L28-29R. REPAIRED PER ERA 505667-14 REV ORIG.

Part: CUSP WEB — CORRODED (BS 805) · airframe 62,534 hrs · 47,494 cycles

MID CARGO CEILING RT CUSP WEB LOWER SURFACE HAS CORROSION AT BS 805. CUSP WEB REPLACED ON NRC 210023.

Part: SEAT TRACK — CORRODED (BS 266-740) · airframe 62,534 hrs · 47,494 cycles

CABIN SEAT TRACK SECTION RBL 54 BS 266-740 HAS CENTER CHANNEL CORRODED. REPLACED SEAT TRACK IAW SRM 51-30-5.

Part: FITTING — CORRODED (R1 DOOR GIRT BAR) · airframe 62,534 hrs · 47,494 cycles

R1 DOOR GIRT BAR LATCH SUPPORT FITTINGS CORRODED FWD AND AFT. REPLACED FITTINGS IAW SRM 51-10-4.

Part: LONGERON — CORRODED (BS 1220-1231) · airframe 62,534 hrs · 47,494 cycles

LONGERON 29L CORROED FS 1220 - 1231. REPLACED LONGERON SECTION 1185-1240 IAW SRM 51-30-5.

Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 62,534 hrs · 47,494 cycles

FLOOR PANEL BETWEEN PILOTS AFT SEAT TRACKS CORRODED AT UPPER SURFACE. REPLACED FLOOR PANEL IAW SRM 53-20-01.

Part: CUSP WEB — CORRODED (BS 522-598) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN LEFT CUSP WEB CORRODED AND CRACKED UPPER AND LOWER SURFACE BS 522 TO 598. REPLACED CUSP WEB IAW SRM 51-10-4.

Part: FLOOR SUPPORT — CORRODED (BS 147-200) · airframe 62,534 hrs · 47,494 cycles

FLOOR SUPPORT FS 147-200 LBL 7 CORRODED UPPER SURFACE. REPLACED FLOOR SUPPORT PER SRM 51-30-1.

Part: CARGO TRACK — CORRODED (BS 788) · airframe 62,534 hrs · 47,494 cycles

MID CARGO TRACK CORRODED BS 788. REPLACED SEAT TRACK IAW SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 266-797) · airframe 62,534 hrs · 47,494 cycles

CABIN SEAT TRACK SECTION LBL 54 FS 266-797 CORRODED. SEAT TRACK REPLACED.

Part: CUSP WEB — CORRODED (BS 522-598) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN LT CUSP WEB CORRODED AND CRACKED UPPER AND LOWER SURFACE BS 522 TO 598. REPLACED WEB IAW SRM 51-30-1.

Part: SEAT TRACK — CORRODED (FS 266-797) · airframe 62,534 hrs · 47,494 cycles

SEAT TRACK SECTION LBL 54 FS 266-797 CORROED AT CTR CHANNEL AND LUGS. REPLACED SEAT TRACK IAW SRM 51-30-1.

Part: FRAME — CORRODED (BS 1307) · airframe 62,534 hrs · 47,494 cycles

CORROSION ON FRAME UPPER AND LWR SURFACE OF BILGE AREA FS 1307 BTW L 27R AND L23L IN AFT CARGO COMPT. REPLACED FRAME IAW SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 1117-1136) · airframe 62,534 hrs · 47,494 cycles

CUSP WEB AT BS 1117-1136 CORRODED ON TOP THROUGHOUT. REPLACED CUSP WEB IAW SRM 51-30-1.

Part: SKIN — CORRODED (VERTICAL STAB) · airframe 62,534 hrs · 47,494 cycles

ON DRILLING AND LOCATING NEW PANEL TO VERTICAL STABILIZER, SKIN FOUND WITH CORROSION ON MATING SURFACE. FABRICATED AND INSTALLED NEW MATING SURFACE IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 1322 LBL 21) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN FLOORBEAM HAS CORROSION AT BS 1322 LBL 21 UPPER SURFACE. REPAIRED PER SRM 51-30-1.

Part: CUSP WEB — CORRODED (BS 552-560) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN RT CUSP HAS CORROSION AT BS 552 TO 560. REPLACED CUSP WEB PER SRM 53-14-2, 51-30-0.

Part: CUSP WEB — CORRODED (BS 1079-1098) · airframe 62,534 hrs · 47,494 cycles

RT CUSP WEB BS 1079-1098 CORRODED. REPLACED WEB PER SRM 51-30-1, 51-30-2, 1ND 51-30-5.

Part: CUSP WEB — CORRODED (BS 1117-1136) · airframe 62,534 hrs · 47,494 cycles

RT CUSP WEB AT BS 1117-1136 CORRODED. REPLACED CUSP WEB PER SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 579-598) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN RT CUSP WEB HAS CORROSION FROM BS 579 TO 598. REPLACED CUSP WEB PER SRM 53-14-2 & 51-30-0.

Part: LONGERON — CRACKED (BS 522 L4L) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN LONGERON CRACKED BS 522 L4L. REPAIRED PER SRM 53-02 FIG 18.

Part: CUSP WEB — CORRODED (BS 915) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN RT CUSP WEB HAS CORROSION AT BS 915. REPLACED WEB PER SRM 51-30-2, 51-30-5, AND 51-30-1.

Part: SEAT TRACK — CORRODED (BS 1022-1041) · airframe 62,534 hrs · 47,494 cycles

SEAT TRACK AT BS 1022-1041 LBL 22 HAS CORROSION. REPAIRED PER SRM 53-05 FIG 4F.

Part: INTERCOSTAL — CORRODED (BS 788) · airframe 62,534 hrs · 47,494 cycles

FOUND INTERCOSTAL CORRODED BS 788. REPLACED INTERCOSTAL IAW SRM 51-30-2.

Part: LONGERON — CORRODED (BS 1280-1316) · airframe 62,534 hrs · 47,494 cycles

LONGERON 24L BS 1307-1309 FOUND TO HAVE CORROSION ON THE UPPER FLANGE. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW LONGERON SECTION 24L BS 1280-1316 IAW SRM 51-30-2 51-30-5.

Part: BULKHEAD — CRACKED (AFT) · airframe 62,534 hrs · 47,494 cycles

DURING EDDY CURRENT INSPECTION OF LT LOWER FWD SIDE OF AFT PRESSURE BULKHEAD, ONE CRACK WAS DETECTED EMANATING FROM FASTENER DOUBLER. COMPLIED WITH ER/A 505310-14AD REV ORIG.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 62,534 hrs · 47,494 cycles

L1 DOOR LOWER FORWARD CORNER SKIN HAS EDGE DAMAGE. CUT OUT DAMAGE. INSTALLED REPAIR DOUBLER AND FILLER ON L1 DOOR PER SRM 52-05D PG 210 FIG 37.

Part: YOKE — CRACKED (NR 2 PYLON) · airframe 62,534 hrs · 47,494 cycles

NR 2 PYLON YOKE FOUND CRACKS DURING NDT CHECK ON OPN NR 82002 AD, NEW PYLON YOKE INSTALLED ON OPN 7250 DURING HMV.

Part: YOKE — CRACKED (NR 1 PYLON) · airframe 62,534 hrs · 47,494 cycles

NR 1 PYLON YOKE FOUND CRACKED 2 PLACES DURING NDT CHECK ON OPN 81002, NEW PYLON YOKE INSTALLED ON OPN 7150 DURING HMV.

Part: CUSP WEB — CORRODED (BS 237-313) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN CUSP WEB BS 237-313 RBL 54 HAS CORROSION ON UPPER AND LOWER SURFACES ON SEVERAL AREAS. REPLACED CUSP WEB IAW SRM 51-10-4.

Part: CARGO TRACK — CORRODED (BS 522-598) · airframe 62,534 hrs · 47,494 cycles

MID CARGO TRACK IS GOUGED AT NUT PLATE HOLES BS 522-598 AND HAS CORROSION AT BS 538. FOUND TO BE OUT OF LIMITS. INSTALLED NEW CARGO TRACK BS 428-636 IAW SRM 51-30-1 AND 51-30-2.

Part: CUSP WEB — CORRODED (BS 946-984) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN LT CUSP WEB HAS CORROSION ON MULTIPLE PLACES BS 946-984. INSTALLED REPAIR SHIMS DOUBLERS AND RING DOUBLERS IAW SRM 53-05 FIG 131A AND 51-30-0.

Part: CUSP WEB — CORRODED (BS 237-313) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN LEFT CUSP WEB CORRODED BS 237-313 MULTIPLE AREAS. CORROSION OUT OF LIMITS. CUT OUT DAMAGE. FABRICATED AND INSTALLED DOUBLERS, FILLERS AND RING DOUBLERS IAW SRM 53-05 FIG 131A-6.

Part: RING — CORRODED (BS 886 CUSP WEB) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN CUSP WEB RING PLATE HAS CORROSION BS 886 LBL 58. FOUND TO BE OUT OF LIMITS. NEW RING PLATE INSTALLED IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 712-769) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN RT CUSP WEB HAS CORROSION BTW BS 727-769. REPLACED CUSP WEB FROM BS 712-788 IAW SRM 51-30-0.

Part: FLOORBEAM — CORRODED (BS 598) · airframe 62,534 hrs · 47,494 cycles

CARGO LOWER FLOORBEAM HAS CORROSION ON LOWER SURFACE AT BS 598 BETWEEN L28L AND L28R. FOUND OUT OF LIMITS. REPLACED MID CARGO FLOORBEAM IAW SRM 51-30-05.

Part: SHEAR TIE — CORRODED (BS 674) · airframe 62,534 hrs · 47,494 cycles

MID CARGO LOWER BILGE SHEAR TIE HAS CORROSION AT BS 674 BTW L28L, L29R. FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM 51-30-5.

Part: FLOOR SUPPORT — CORRODED (BS 147-200) · airframe 62,534 hrs · 47,494 cycles

CABIN FLOOR SUPPORT BS 147-200 LBL 7 CORROSION UPPER SURFACE. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-30-1.

Part: FLOOR SUPPORT — CORRODED (BS 168-198) · airframe 62,534 hrs · 47,494 cycles

CABIN FLOOR SUPPORT STA 168-198 LBL 44 CORRODED. REPLACED FLOOR SUPPORT IAW SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 853-845) · airframe 62,534 hrs · 47,494 cycles

CABIN SEAT TRACK LBL 54 BS 823-845 CORRODED AND GOUGED. INSTALLED NEW SEAT TRACK IAW SRM 51-30-1.

Part: CUSP WEB — CORRODED (BS 826-845) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN HAS CORROSION ON CUSP WEB BS 826-845. REPLACED CUSP WEB IAW SRM 51-30-0.

Part: CUSP WEB — CORRODED (BS 845-946) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN CUSP WEB HAS CORROSION ON MULTIPLE PLACES AND OPEN HOLES BS 845-946. REPLACED CUSP WEB IAW SRM 51-30-2 51-30-5 51-30-1.

Part: FLOOR SUPPORT — CORRODED (BS 788) · airframe 62,534 hrs · 47,494 cycles

MAIN CARGO FLOOR SUPPORT HAS CORROSION AT BS 788. REPLACED FLOOR SUPPORT IAW SRM 51-30-2.

Part: LONGERON — CRACKED (BS 522 L4L) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN LONGERON CRACKED BS 522 L4L. REPLACED LONGERON SECTION BS 521-550 PER SRM 53-02 FIG 18.

Part: SEAT TRACK — CORRODED (BS 1212-1231) · airframe 62,534 hrs · 47,494 cycles

SEAT TRACK BS 1212-1231 RBL 54 HAS CORROSION ON TOP OF TRACK AND DOWN INSIDE CHANNEL. REPLACED SEAT TRACK IAW SRM 51-30-1.

Part: SHEAR TIE — CORRODED (BS 655 L26L-29R) · airframe 62,534 hrs · 47,494 cycles

MID CARGO LWR BILGE SHEAR TIE HAS CORROSION AT BS 655 BETWEEN L26-29R. CORROSION OUT OF LIMITS AT THE END OF THE SHEAR TIE. CUT OUT DAMAGE, FABRICATED AND INSTALLED SHEAR TIE AND SPLICE IAW SRM 51-30-2, 51-30-5.

Part: FRAME — DAMAGED (BS 1271 L27R) · airframe 62,534 hrs · 47,494 cycles

CORROSION ON FRAME UPPER AND LOWER SURFACE BOTH SIDES INTERNAL BILGE AREA AT BS 1271, L27R AND FOUND OUT OF LIMITS. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM 53-05.

Part: SEAT TRACK — CORRODED (BS 266-740) · airframe 62,534 hrs · 47,494 cycles

CABIN SEAT TRACK SECTION BS 266-740 RBL 54 CORRODED. REPLACED SEAT TRACK IAW SRM 51-30-1.

Part: SEAT TRACK — CORRODED (BS 266-273) · airframe 62,534 hrs · 47,494 cycles

SEAT TRACK SECTION RBL 54 CORRODED BS 266-273. REPLACED SEAT TRACK BS 218-341 IAW SRM 51-10-4.

Part: LONGERON — CRACKED (BS 541 L4R) · airframe 62,534 hrs · 47,494 cycles

MAIN CABIN LONGERON CRACKED BS 541 L4R. FABRICATED AND INSTALLED NWW LONGERON SECTION BS 531-550 IAW 53-02.

Part: CARGO TRACK — CORRODED (BS 788) · airframe 62,534 hrs · 47,494 cycles

MID CARGO TRACK HAS CORROSION AT BS 788. FOUND TO BE OUT OF LIMITS. REPLACED LT MID CARGO TRACK BS 541-788 IAW SRM 51-30-5 PG12, 51-30-1 PG15.

Part: SHEAR TIE — CORRODED (BS 1136) · airframe 62,534 hrs · 47,494 cycles

SHEAR TIE WITH CORROSION BS 1136 BETWEEN L29R AND L29L IN BILGE AREA OF AFT CARGO COMPARTMENT. FOUND OUT OF LIMITS. FABRICATED AND INSTALLED NEW SHEAR TIE AND REPAIR SPLICE IAW SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 717) · airframe 62,534 hrs · 47,494 cycles

MID CARGO CEILING CUSP WEB LOWER SURFACES HAS CORROSION AT BS 717. REPLACED CUSP WEB STA 712-788 IAW SRM 51-30-1/51-30-2.

Part: CUSP WEB — CORRODED (BS 598-712) · airframe 62,534 hrs · 47,494 cycles

MID CARGO LT CUSP WEB LOWER SURFACE HAS CORROSION BTW BS 598-712. CORROSION OUT OF LIMITS. REPLACED CUSP WEB IAW SRM 51-30-1, 51-30-2, 51-30-5.

Part: CUSP WEB — CORRODED (BS 578-712) · airframe 62,534 hrs · 47,494 cycles

MID CARGO RT CUSP WEB LWR SURFACE HAS CORROSION FROM STA 598-712. REPLACED CUSP WEB IAW SRM 51-30-1 AND 51-30-2.

Part: TEE FITTING — CORRODED (BS 996-1041) · airframe 62,534 hrs · 47,494 cycles

LOWER WING TO BODY FAIRING SUPPORT TEE ANGLE HAS CORROSION FROM BS 1041 TO 996 RBL47. FABRICATED AND INSTALLED NEW SUPPORT TEE IAW SRM 51-30-2.

Part: SKIN — DENTED (BS 1265 L21-22R) · airframe 62,534 hrs · 47,494 cycles

FUSELAGE SKIN HAS A DENT AT BS 1265 BETWEEN L21-22R. FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-04-03 FIG 2.

Part: SKIN — DENTED (BS 348 L19-20R) · airframe 62,534 hrs · 47,494 cycles

RT FUSELAGE EXTERNAL SKIN HAS TWO DENTS WITH GOUGES. BLENDED, NO GOUGES. DENTS FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, INTERCOSTAL IAW SRM 51-04-3.

Part: SKIN — CRACKED (BS 1380) · airframe 62,534 hrs · 47,494 cycles

FUSELAGE EXTERNAL SKIN IS CRACKED AT BS 1380 L13-14RS. COMPLIED WITH ER/A 505007-14 REV ORIG.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,511 hrs · 47,480 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT TWO OF THE OVERHEAD EMERGENCY ESCAPE LIGHTING IN THE CABIN AT BS 812 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SPAR CAP — CRACKED (HORIZ STAB) · airframe 62,253 hrs · 47,285 cycles

HORIZONTAL STAB UPPER AFT SPAR CAP CRACKED AT UPPER INBOARD BOLT HOLE. INSTALLED SPLICE REPAIR IAW SR09550027.

Part: PLATE — CORRODED (STABILIZER) · airframe 62,253 hrs · 47,285 cycles

IRR: RT OUTER INBOARD HINGE PLATE CORRODED BEYOND LIMITS. REPLACED RT OUTER INBOARD HINGE PLATE IAW ERA 502265-14.

Part: PLATE — CORRODED (STABILIZER) · airframe 62,253 hrs · 47,285 cycles

IRR: RT INNER INBOARD HINGE PLATE CORRODED BEYOND LIMITS. REPLACED RT INNER INBOARD HINGE PLATE IAW ERA 502265-14.

Part: PLATE — CORRODED (STABILIZER) · airframe 62,253 hrs · 47,285 cycles

IRR: RT INNER OUTBOARD HINGE PLATE CORRODED BEYOND LIMITS. REPLACED RT INNER OUTBOARD HINGE PLATE IAW ERA 502265-14.

Part: PLATE — CORRODED (STABILIZER) · airframe 62,253 hrs · 47,285 cycles

IRR: RT OUTER OUTBOARD HINGE PLATE CORRODED BEYOND LIMITS. REPLACED RT OUTER OUTBOARD HINGE PLATE IAW ERA 502265-14.

Part: PLATE — CORRODED (STABILIZER) · airframe 62,253 hrs · 47,285 cycles

IRR: LT OUTER INBOARD HINGE PLATE CORRODED BEYOND LIMITS. REPLACED LT OUTER INBOARD HINGE PLATE IAW ERA 502265-14.

Part: PLATE — CORRODED (STABILIZER) · airframe 62,253 hrs · 47,285 cycles

IRR: LT INNER INBOARD HINGE PLATE CORRODED BEYOND LIMITS. REPLACED INNER INBOARD HINGE PLATE IAW ERA 502265-14.

Part: PLATE — CORRODED (STABILIZER) · airframe 62,253 hrs · 47,285 cycles

IRR: LT INNER OUTBOARD HINGE PLATE CORRODED BEYOND LIMITS. REPLACED INNER OUTBOARD HINGE PLATE IAW ERA 502265-14.

Part: PLATE — CORRODED (STABILIZER) · airframe 62,253 hrs · 47,285 cycles

IRR: LT OUTER OUTBOARD HINGE PLATE CORRODED BEYOND LIMITS. CORR: REPLACED LT OUTER OUTBOARD HINGE PLATE IAW ERA 502264-14.

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 61,096 hrs · 46,536 cycles

LOWER CARGO COMPARTMENT HOLE IN FLOOR JUST INSIDE DOOR JAMB. INSTALLED TEMP PATCH PER SRM 53-05D FIG 802D.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 60,509 hrs · 46,120 cycles

RETURNED TO ATL DUE TO A REPORT OF A BURNING ODOR IN THE CABIN. NO VISIBLE SMOKE SEEN WITH LIGHTS OFF, STILL HAD ODOR IN CABIN. PERFORMED OPN 5088. FOUND HYDRAULIC LEAK FROM RT T/R CONTROL VALVE LINE. TORQUED SAME AND CLEANED APU INLET. PERFORMED OPN 5090 ALTERNATE DUCT BURNOUT. LEAK AND OPS CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,496 hrs · 46,110 cycles

REMOVED FASTENERS, HFEC INSP COMPLETED, INSTALLED FILLER AND DOUBLER, RESTORED FINISH, JOB COMPLETE PER ERA 494947-14, REV O NR 61 ZONE 9-0.

Part: LANYARD — DISCONNECTED (EVAC SLIDE) · airframe 60,397 hrs · 46,034 cycles

DURING LINE CHECK MAINTENANCE FOUND R1 DOOR LANYARD NOT ATTACHED TO GIRT BAR. MAINTENANCE INSTALLED R1 DOOR SLIDE LANYARD PER MM 25-62-00. OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 60,167 hrs · 45,861 cycles

DURING LINE CHECK MAINTENANCE FOUND AFT EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY CHARGER FOR LIGHTS. LIGHTS NOW CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,999 hrs · 45,765 cycles

DURING LINE CHECK, MAINTENANCE FOUND MID CABIN CEILING LIGHTS INOPERATIVE DURING EMERGENCY LIGHT TEST. MAINTENANCE FOUND BATTERY PACKS ABOVE SEAT 12DE BAD. REMOVED AND REPLACED SAME. OPERATION CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: LIGHT — WRONG PART (EXTERIOR) · airframe 59,999 hrs · 45,765 cycles

DURING LINE CHECK, MAINTENANCE FOUND BOTH EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE FOUND THE WRONG BULB INSTALLED IN RIGHT AFT EXTERIOR LIGHT SOCKET AND REPLACED IT WITH THE CORRECT BULB. OPERATION NOW CHECKS GOOD. AIRCRAFT IS OKAY FOR SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 58,863 hrs · 45,051 cycles

DURING LINE CHECK, MX FOUND EMERGENCY LIGHT AT 19DE INOPERATIVE. MX REPLACED CONNECTOR FOR LIGHT ASSY AND RE-SECURED THE WIRE HARNESS. OPS OF LIGHT NOW CHECKS OK.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 57,800 hrs · 44,323 cycles

DURING LAYOVER CHECK, MX FOUND THE EMERGENCY LIGHT AT SEAT 4N TO BE INOPERATIVE. MX REWIRED SEAT 4N. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 57,749 hrs · 44,292 cycles

MAINTENANCE FOUND BOTH OVERWING EMERGENCY EXIT SEAT LIGHTS HAVE DAMAGED WIRE. MAINTENANCE RE-WIRED BOTH OVERWING EMERGENCY EXIT SEAT LIGHTS. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (2010-D0857) (DLM88101927).

Part: LIGHT — DAMAGED (CABIN) · airframe 56,506 hrs · 43,470 cycles

JUMP SEAT AFT CTR LT EMERGENCY LIGHTING FLOOR LIGHTS INOP/DAMAGED. REINSTALLED LENS. CKS OK.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 56,506 hrs · 43,470 cycles

PASSENGER SEAT 04C EMERGENCY EXIT SIGNS INOPERATIVE. RELAMP NO HELP FOUND PIN PUSHED BACK IN CONNECTOR. REINSTALLED PIN LIGHT, CKS GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 56,506 hrs · 43,470 cycles

PASSENGER SEAT 37D, EMERGENCY EXIT SIGNS INOPERATIVE. FOUND SEAT HARNESS WITH BROKEN WIRE. REMOVED AND INSTALLED SEAT HARNESS IAW MM, CKS GOOD.

Part: SPRING — BROKEN (NOSE GEAR) · airframe 54,891 hrs · 42,432 cycles

ON GEAR RETRACTION HEARD BANG FROM NOSE GEAR AREA, DIVERTED. FOUND RT NOSE GEAR BUNGEE SPRING BROKEN. REPLACED SPRINGS.

Part: TIRE — FAILED (NR 2) · airframe 51,489 hrs · 40,242 cycles

NR 2 TIRE BLOWN IN LANDING LGA (MCC/1600Z), MED AUTOBRAKES IN USE AT TIME. REMOVED AND REPLACED NR 1 AND NR 2 MAIN TIRES INSPECTED A/C AND INLET OF NR 1 AND NR 2 ENG NO DAMAGE FOUND, PERFORMED ANTI-SKID TEST AND INSPECTED TRANSDUCERS ON NR 1 AND NR 2 AXLES ALL NORMAL. ITEM NR 2 REMOVED AND REPLACED ANTI-SKID CONTROL PER M/M 32-43-04-201 WORKING NML.

Part: OIL SYSTEM — LEAKING (APU) · airframe 51,372 hrs · 40,165 cycles

SMOKE IN CABIN, FOUND APU OIL LEAKING INTO APU INLET. FOUND OIL LEAK AT ATTA POINTS FOR OIL FILL/SIGHT GLASS, SECURED BOLTS THAT WERE FOUND LOOSE AND REPLACED OIL CAP. LEAK CKS OK REF ITEM 004 NEXT LOG PAGE FOR DUCT BURN OUT OPERATION.

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

S/O 291019 NR 25018 CORROSION IN SEVERAL AREAS AT AFT CARGO LOWER ANGLE FRAME STA. 1322, LONGERON 23L-23R. REMOVED AND REPLACED AFT CARGO LOWER ANGLE FRAME PN 9936664-23 FROM STA. 1322, LONGERON 23L-23R IAW SRM 51-30-2 AND 51-10-03.

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

CORROSION FWD FACE OF AFT PIT PRESSURE DOME UNDER SEALER LEFT BL 10 TO RIGHT BL 10. CUT OUT CORRODED AREA FROM AFT PIT PRESSURE BULKHEAD TEE CAP. DRILLED AND INSTALLED NEW SECTION OF TEE CAP P/N 9915561-73 AND P/N SRO9530001-33, FABRICATED AND INSTALLED TEE CAP REPAIRS 3 EA 7" X 2" FROM 2024-T3 .063" AND 5 EA 7" X 2" FROM 2024-T3 .071" IAW DC-9/MD-80 SRM 51-30-2D, 51-10-2 AND DPS 900-5-1.

Part: SKIN — CRACKED (BS 191 S22L)

HFEC CRACK INDICATION, FUSELAGE EXT SKIN FS 191 L-22L RADIAL ORIENTATION, 9 - 11 O'CLOCK POSITION, 0.125 INCH LONG, 0.20 INCHES FROM EDGE OF COUNTERSINK. REPAIRED CRACK BY FABRICATING AND INSTALLING REPAIR DOUBLER 50 INCHES X 22.375 INCHES FROM 7075-T6 .071 INCHES IAW ERA 09-069085-12AD REV D, ME-02, DATED 07-15-05, OPN 203.

Part: LONGERON — CORRODED (BS 1322) · corrosion level 2

CORROSION AT AFT CARGO LONGERON 24L FS 1322. CUT OUT CORRODED AREA. INSTALLED EXTRUSION P/N S2912727-12000 AND FITTING P/N 3913291U501 IAW DC-9/MD80 SRM 51-10-3D, 51-30-2 AND 51-30-5 AND 53-02D.

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

S/O 291019 NR 25070, CORROSION AT AFT CARGO LONGERON 28R BETWEEN FS 1287-1309. BLENDED OUT SURFACE CORROSION, MAX DEPTH .018 DEEP. FABRICATED AND INSTALLED U-CHANNEL LONGERON REPAIR 22 INCHES X .75 INCH X 1.5 INCH X 20 INCH FROM 7075-T6 .071 INCH IAW SRM 53-02D FIG. 19, PAGES 1, 52 AND 53.

Part: LONGERON — CORRODED (BS 489) · corrosion level 2

CORROSION AT LONGERON SPLICE FS 489 RIGHT LONGERON 30 FWD END. FABRICATED AND INSTALLED LONGERON SPLICE IAW DWG 3924814 FROM 7075-T6 IAW DC-9/MD-80 SRM 53-01 FIG 1, 51-10-3D, 51-10-2, 51-30-0 FIG 3 AND DC-9/MD-80 M/M 20-10-15-201.

Part: DOUBLER — CORRODED (BS 1438) · corrosion level 2

CORROSION AFT PRESSURE BULKHEAD LOWER DOUBLER BL 0. FABRICATED AND INSTALLED DOUBLER REPAIR 5" X 5.5" X 5.5" FROM 7075-T6 .080" IAW DC-9/MD-80 SRM 51-10-3D, AND 51-30-5.

Part: SKIN — GOUGED (BS 1418)

GOUGES IN SKIN NEXT TO LONGERON 1L AND STATION 1418. BLENDED GOUGED IAW 53-34-0, FABRICATED AND INSTALLED DOUBLER REPAIR AND FILLER IAW DC-9/MD-80 SRM 53-01, 51-10-3 AND 53-04D FIG 803D.

Part: SEAT TRACK — TOOL DAMAGE (BS 1322) · corrosion level 2

TOOL MARKS AT O/B FLANGE LOWER SURFACE IN CABIN RIGHT I/B SEAT TRACK FROM FS 370 TO 427. DRILLED AND INSTALLED SPLICE P/N ACA7413-505 AND PLATE P/N ACA7414-3 IAW DC-9/MD80 SRM 53-05 FIG 4F AND 51-10-3.

Part: SKIN — DENTED (BS 313 S17L)

SMALL DENT AT FS 313 LT LONGERON 17L. DENT OUT OF LIMITS IAW SRM 53-04D TABLE C. FABRICATED AND INSTALLED REPAIR DOUBLER 7.5 INCHES X 7.5 INCHES FROM 2024-T3 .032 INCHES IAW SRM 51-10-3D, 51-30-2 AND 53-04D.

Part: LONGERON — CRACKED (BS 408 L2L)

CABIN FS 408 LONGERON 2L HAS CHAFE. CHAFE FOUND TO BE A CRACK. FABRICATED AND INSTALLED LONGERON 18.6 X 2.1 INCHES FROM S2777922-1-26500 AND SPLICE 15.0 X 2.5 INCHES FROM 7637813-3 IAW DC-9/MD-80 SRM 53-02D FIG 18, 51-10-3D AND M/M 25-00-00-801.

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

S/O 291019 N/R 25244 CORROSION ON RT OB SEAT TRACK AT FS 1193. REMOVED CORRODED SECTION OF SEAT TRACK. INSTALLED REPAIR PLUG PN 7452952-3 AND CHANNEL PN 7452952-7 IAW SRM 53-05 FIG. 4A, AND 51-10-3.

Part: SKIN — CRACKED (BS 172 S11R)

CRACK AT COUNTER SINK FASTENER HOLE ON TOP FWD SERVICE DOOR, FWD UPPER FUSELAGE CUTOUT, FS 172.75, 2" BELOW LONGERON 11RH. CUT OUT CRACKED AREA 2" BY 1.4" IAW MD-88 SRM 53-05 FIG 112, HFEC, NO FURTHER CRACK INDICATIONS NOTED. FABRICATED 1 REPAIR DOUBLER 24.25" BY 17.5" BY 3" BY 5" FROM 2024-T3 .063", 1 REPAIR TRIPLER 21.5" BY 15.25" BY 3" BY 4" FROM 2024-T3 .090 AND FILLER 2.11" BY 1.5" FROM 2024-T3 .050 IAW MD-88 SRM 53-05 FIG 112, AND 51-10-3D.

Part: LINE — LEAKING (LT HYD SYSTEM) · airframe 47,581 hrs · 37,548 cycles

LEFT HYDRAULIC SYSTEM QTY AT 4 WITH LIGHT ON SECURED. LEFT HYDRAULIC SYSTEM QTY WENT TO 9 CONTINUED TO ATL. REPLACED LEFT HYDRAULIC AFT FILTER PRESSURE MODULE PIPE ASSEMBLY AND ADJACENT BRAIDED HOSE. SERVICE LEFT HYDRAULIC SYSTEM PER M/M. RAN LEFT ENGINE, NO LEAKS NOTED. APU WAS NOT RUNNING AT ANYTIME DURING THIS EVENT.

Part: PSEU — UNKNOWN (SLAT/FLAPS) · airframe 47,444 hrs · 37,460 cycles

ON INITIATION OF T/O ROLL TAKEOFF WARNING SOUNDED WITH INTERMITTENT SLAT DISAGREE LIGHT. MAX SPEED 90 KTS. RETURNED TO GATE. DISAGREE AT ALL SLAT/FLAP POSITIONS AT GATE. VISUALLY INSP SLATS / FLAPS NTF. NO FAULTS ON PSEU. REPLACED PSEU PER M/M, NO DISAGREE LIGHT, CKS GOOD.

Part: BATTERY — WEAK (FLASHLIGHT) · airframe 41,112 hrs · 32,960 cycles

EMERGENCY FLASHLIGHT AT AFT ATTENDANT SEAT HAS WEAK BATTERY. REPLACED BATTERY. CHECKS GOOD.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 39,442 hrs · 31,854 cycles

ON FINAL AT TIME OF AUTO THROTTLE DISCONNECT JUST PRIOR TO LANDING, A/C VEERED TO LEFT. EXECUTED GO-AROUND, NOTICED SMELL IN COCKPIT. INSPECTED ENGINES AND RAN, UNABLE TO DUPLICATE.

Part: MODULE — WILL NOT TEST (FIRE DETECTION) · airframe 39,206 hrs · 31,700 cycles

CARGO FIRE DETECTION SYSTEM ARMED LIGHTS AND SQUIB LIGHTS DO NOT ILLUMINATE DURING SQUIB TEST. REPLACED CONTROL MODULE.

Part: HARNESS — MELTED (APU SHROUD) · airframe 39,204 hrs · 31,699 cycles

A/C ARRIVED WITH APU GENERATOR INOP ON MCO. DURING TROUB LESHOOTING, WE FOUND TH APU GEN FIREWALL PLUG HAD A L OOSE CONTACT PIN . HARNESS WAS REMOVED AND PLUG WAS OPENED TO DISCOVER A MELTED CONNECTOR AND SHIELDING . HARNESS ASSEMBLY IS TO BE REPLACED ON AEROMEXICO NON ROUTINE CARD. PART # OF HARNESS IS7939409-501

Part: VALVE — STUCK (RT A/C BAY) · airframe 32,761 hrs · 26,979 cycles

AIRCRAFT ATB, WOULD NOT PRESSURIZE. LT PACK ON MCO AND RT PACK WOULD NOT HOLD PRESS. REPLACED PITOT PRESSURE REGULATOR AND FLOW CONTROL VALVE. PRESSURIZED AIRCRAFT TO 4 PSID WITH LEFT PACK, THEN RIGHT PACK AND BOTH PACKS CHECKED OK. ALSO, REPLACED LT FLOW CONTORL VALVE TO REMOVE MCO FOR LEFT PACK.

Part: COMPUTER — FAILED (E/E BAY)

IN FLT RECEIVED CADC 1 FAIL MSG ON MCDU. CADC SW PLACED ON, BOTH ON 2. ALSO RECEIVED MASTER WARN AND AN AC EMER BUS OFF LIGHT ON O/H PANEL. CAPT DISPLAY LOST, F/O DISPLAY NORMAL EXCEPT LOSS OF RDMI INFO. AC EMER BUS OFF LIGHT CYCLED ON AND OFF FOR REST OF FLT. REPLACED NR 1 CADC, OP CKS GOOD.

Part: BPU — FAILED (E & E BAY)

CLIMBING THROUGH 20K FT OVHD PANEL LIGHTS AND NUMEROUS OTHER COCKPIT LIGHTS BEGAN TO FLICKER. APPROX 5 SECS LATER ELECTICAL FAILURE OCCURED FOR APPROX 15 SEC, THEN PWR CAME BACK ON. THEN FOR APPROX 3-5 SECS PWR WOULD GO OFF THEN ON. WHEN PWR WENT OFF THE 1ST TIME THE EMER PWR SWITCH WAS TURNED ON AND THE APU WAS PLACED TO START. AFTER 5 SECS PWR CAME ON AND REMAINED ON AND THE FLICKERING STOPPED. A WINDSHIELD OVT LIGHT REMAINED ON THE OAP AND THE AUTO THROTTLES WOULD NOT ENGAGE. BOTH THE CAPTS AND F/OS PFDS AND NDS WENT BLANK. REPLACED BPU AND R2-50, RAN AND LOADED GENS SWAPPED PWR OK.

Part: ENGINE — FAILED (NR 2)

NR 2 ENGINE OIL TEMP WENT ABOVE 190 DEG'S FOR 15 TO 20 MINUTES AFTER TAKEOFF. WHEN CREW WENT TO SHUT DOWN ENGINE, ENGINE DID NOT APPEAR TO BE RUNNING. REPLACED ENGINE.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON INSPECTION, FOUND FWD I/B FLIGHT ATTENDANT EMERGENCY FLASHLIGHT NOT TESTING. REPLACED BATTERY PACK, CHECKS OK.

Part: FUEL/OIL COOLER — LEAKING (NR 2 ENGINE)

ENG FAILURE RT ON DEPARTURE AT 17K, RT ENG FLUX FOR APPROX 15 SEC BEFORE FAILURE. F/A REPORTED POPPING NOISES PRIOR TO FLUX OIL TEMP WENT TO 155 DEG. CHECKED INLET AND EXH, NO TROUBLE FOUND. CHECKED OIL FILTER AND REPLACED SAME. FILTER CLEAN, CHECKED CHIP DET, NO METAL. BORESCOPED 6TH, 7TH AND 13TH STAGE COMPRESSOR, NO DAMAGE FOUND. REPLACED FUEL CONTROL AND FUEL PUMP. PERFORMED OPN5034 HIGH OIL TEMP TEST, ENG PASSED. TRIMMED ENG PER PFHB, NR 2 ENG FUEL/OIL COOLER LEAKING AT WEEP HOLE. REPLACED NR 2 ENG FUEL/OIL COOLER AND OIL TEMP BULB. LK AND OPN CKS NORMAL.

Part: REGULATORS — LEAKING (FLT DECK OXYGEN)

CREW OXYGEN WENT TO ZERO IN FLIGHT. REPLACED CAPT AND OBSV O2 REG BOXES FOR LEAKING REGULATOR.

Part: OIL FILTER — DIRTY (NR 2 ENGINE)

R OIL STRAINER CLOG LOG WOULD NOT GO OUT WITH THROTTLE RETARDED TO IDLE. ENGINE SHUTDOWN. REPLACED FILTER, DRAINED AND REFILLED OIL, RAN ENGINE PER M/M. CHECKED FILTER AGAIN, EVIDENCE OF CARBON BUIL-UP ON ORIGINAL FILTER, SUBSEQUENT OK.

Part: GEARBOX — WORN (NR 2 ENGINE)

RT ENG OIL FILTER CLOG LIGHT ON OAP. REPLACED NR 2 ENGINE GEARBOX PER ROUTINE CARD DECK CKD PER PFHB 9-0-7-7.

Part: FAN HUB ASSY — CRACKED (NR 1 ENGINE)

DURING TAKEOFF ROLL, NR 1 ENGINE ENCOUNTERED AN UNCONTAINED FAILURE OF THE 1ST STAGE FAN HUB ASSEMBLY. ENGINE DEBRIS PENETRATED THE FUSELAGE. TWO FATALITIES OCCURRED. UNDER NTSB INVESTIGATION.

Part: WINDSHIELD — CRACKED (FLT DECK)

DURING CRUISE, CENTER WINDSHIELD DEVELOPED TWO CRACKS AND STARTED TO DELAMINATE. LANDED ATL. REPLACED WINDOW AND CONTROLLER, RETURNED TO SERVICE.

Part: HYD HOSE — LEAKING (NR 2 ENGINE)

DURING CLIMBOUT, RIGHT HYDRAULIC SYSTEM FAILED ON GEAR RETRACTION. RETURNED ATL. FOUND HOSE FROM RIGHT ENGINE PUMP RUBBED THROUGH AT CLAMP. REPLACED HOSE AND CLAMP OPERATION NORMAL.