N914DL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,370 hrs · 57,483 cycles

EMERGENCY OVERHEAD LIGHTS INOPERATIVE FROM ROWS 27 - 36. REPLACED THE BATTERY PACK AT ROW 29 IAW AMM 33-50. ALL EMERGENCY LIGHTS OPS CHECKED GOOD.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 74,783 hrs · 57,011 cycles

DURING SERVICE CHK FOUND FWD OVERWING EMER EXIT SIGNS NOT LIGHTING UP. T/S AND FOUND BAD BATTERY CELL FOR FWD OVERWING EMERGENCY EXIT SIGNS IAW AMM 33-50 SYSTEM CHECKS GOOD.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 73,314 hrs · 55,875 cycles

VERTICAL STAB LEADING EDGE, 5TH FASTENER HOLE FROM LOWER EDGE IS OUT OF ROUND. REPAIRED IAW ER/A 556179-14.

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 73,314 hrs · 55,875 cycles

VERTICAL STAB LT SIDE FRONT SPAR CAP FWD FLANGE 5TH FASTENER ABOVE VSS ZFS 52.267 HOLE IS OUT OF ROUND. REPAIRED IAW ER/A 556179-14AD.

Part: BRACKET — CRACKED (TAILCONE) · airframe 73,314 hrs · 55,875 cycles

TAIL CONE RIGHT UPPER BAYONET FITTING BRACKETS CRACKED. DRILLED REPLACEMENT BRACKETS. TREATED, PRIMED & PAINTED PART. INSTALLED THE BRACKETS IAW SRM 51-30-02.

Part: FORMER — BROKEN (RT WING) · airframe 73,314 hrs · 55,875 cycles

FOUND RT WING UPPER FILLET PANEL MOUNT FORMER BROKEN AT WS 886. REMOVED AND REPLACED THE FORMER IAW DWG 9951259.

Part: FRAME — CRACKED (RT MLG WW) · airframe 73,304 hrs · 55,869 cycles

F/AS REPORTED VIBRATION AT 25DE. HYDRAULIC PUMPS OFF OR ON DOES NOT CHANGE VIBRATIONS. LOAD AND VIBRATING ALL PHASES NO VISIBLE FAILURES. FOUND A CRACK ON THE RT MLG WHEEL WELL AREA. REMOVED DAMAGED FRAME. FOUND SEALS JUST FWD OF MLG DOORS VERY LOOSE AND IN POOR CONDITION. REPLACED THE SEALS. DRILLED AND INSTALLED IAW DWG 5930584U124.

Part: CAP — UNSECURE (APU OIL) · airframe 72,529 hrs · 55,330 cycles

PERFORMED ATB DUE TO REPORTED SMOKE IN CABIN AFTER TAKEOFF. FOUND APU OIL CAP NOT SECURE. APU COMPARTMENT AND INLET CLEANED. LEAK CHECKED GOOD. PERFORMED DUCT BURNOUT PROCEDURE WC 7100-2619. NO ODOR PRESENT.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 70,206 hrs · 53,614 cycles

AWR DAMAGE T, WEAR ON INBD GUIDE VANE LWR SKIN AT LT WING. INBD GUIDE VANE AT LT WING WAS R & R AND INSTALLED IAW AMM 27-51-03-201, PAR 3A, B, AND SRM 57-03D, PAR II AND ACFT 0914, CARD 2000-8149-8149-03.

Part: FRAME — CRACKED (BS 1380) · airframe 70,204 hrs · 53,613 cycles

ELONGATED HOLE ON FRAME BS 1380 BETWEEN LONGERON 12 LT TO 13 LT AT AFT ACCESSORY COMPARTMENT. PARTS REPAIR WERE FABRICATED, TREATED, PAINTED, SHEAR CLIP AND SHIM WERE INSTALLED IAW SR 51-10-3, PAR 14, 21, 51-30-5, ETI-88-15-425, REV 2 AND ER/A 541544-14 REV ORIG.

Part: FRAME — CRACKED (BS 1388) · airframe 70,204 hrs · 53,613 cycles

CRACKED FRAME, BS 1388 LONG 2RT AT AFT ACC COMPARTMENT. REPAIR SPAR FRAME BS 1388 WAS ATTENDED WITH ER/A N; 541564-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 1485) · airframe 70,204 hrs · 53,613 cycles

CRACKED FRAME BS 1485 AT AFT ACCCOMPARTMENT. FRAME WAS REPAIRED IAW SRM 53-03, FIG 49, SHEET 2, 3 AND SRM 51-10-3, PARA 21, 14 AND SRM 51-30-5 AND SRM 51-30-2.

Part: SKIN — DAMAGED (BS 693-712) · airframe 70,204 hrs · 53,613 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN AT AFT UPPER CORNER LT WINDOW BELT BETWEEN BS 693 AND 712. LIGHTNING STRIKE WAS REPAIRED AND DIMENTIONS AS FOLLOW: (UT) WAS ACCOMPLISHED IAW NDT-SPM 04-00-07, PARA 5, FIG. 5, ON AFT UPPER CORNER ORIGINAL THICKNESS 0.090 AND REMAINING THICKNESS 0.083, THEREFORE IT IS WITHIN LIMITS IAW ER/A 541576-14, REV ORIGINAL.

Part: SKIN — DAMAGED (BS 655-674) · airframe 70,204 hrs · 53,613 cycles

LIGHTNING STRIKES ON FUSELAGE SKIN AT FWD UPPER CORNER LT WINDOW BELT BETWEEN BS 655 AND 674. LIGHTNING STRIKES WERE REPAIRED AND DIMENTIONS AS FOLLOW: UT, WAS ACCOMPLISHED IAW NDT-SPM, 04-00-07, PARA 5, FIG 3, ON FWD UPPER CORNER ORIGINAL THICKNESS 0.135" AND REMAINING THICKNESS 0.128", NO CRITICAL ZONE, ON AFT UPPER CORNER ORIGINAL THICKNESS 0.120" AND REMAINING THICKNESS 0.118" ON AFT LWR CORNER, ORIGINAL THICKNESS 0.096" AND REMAINING THICKNESS 0.089" CRITICAL ZONE. THEREFORE THESE ARE WITHIN LIMITS IAW ER/A 541575-14, REV ORIGINAL.

Part: SKIN — DAMAGED (BS 636-655) · airframe 70,204 hrs · 53,613 cycles

LIGHTNING STRIKES, 3 EAS, ON FUSELAGE SKIN AT FWD LOWER CORNER LT WINDOW BELT BETWEEN BS 636 AND 655. LIGHTNING STRIKES WERE REPAIRED AND DIMENTIONS AS FOLLOW : UT WAS ACCOMPLISHED IAW NDT-SPM 04-00-07, PARA 5, FIG 3, ON FWD LWR CORNER, ORIGINAL THICKNESS 0.093 AND REMAINING THICKNESS 0.084, CRITICAL ZONE, ON AFT UPPER CORNER . ORIGINAL. THICKNESS 0.086 AND REMAINING THICKNESS 0.081 ON AFT CENTER SECTION ORIGINAL THICKNESS 0.120 AND REMAINING THICKNESS 0.100. THEREFORE THESE ARE WITHIN LIMITS IAW ER/A 541574-14 REV ORIGINAL.

Part: SKIN — DAMAGED (BS 617-536) · airframe 70,204 hrs · 53,613 cycles

TWO LIGHTNING STRIKES ON FUSELAGE SKIN AT AFT LOWER CORNER LT WINDOW BELT BETWEEN BS 617 AND 636. REPAIRED IAW ER/A 541573-14 REV ORIGINAL., UT WAS ACCOMPLISHED IAW NDT-SPM, 04-00-07, PAR. 5, FIG 3

Part: STRUCTURE — DAMAGED · airframe 70,204 hrs · 53,613 cycles

TWO FASTENERS IN THE FWD TAB ON EITHER SIDE OF THE CUT LINE OF LT APB LOWER CHORD. REPAIRED IAW ER/A 541560-14, REV ORIG.

Part: SUPPORT — CRACKED (BS 1437) · airframe 70,204 hrs · 53,613 cycles

CRACKED SUPPORT ON AFT FACE FRAME, BS 1437, LONG 1 AT AFT ACCESSORY COMPARTMENT. SUPPORT WAS REPLACED IAW SRM 53-30-5, 51-10-3 AND DWG 9911840-115, REV DC.

Part: DUCT — WORN (RT WING) · airframe 70,204 hrs · 53,613 cycles

WEAR AT FUEL VENT DUCT, RT WING. EDGE OF CUTOUT ON Y=1211 AND LONGERON 23 TO 24 RT WAS REPAIRED IAW SRM 53-05, FIG 155, OPTION 1.

Part: SKIN — DAMAGED (BS 1211) · airframe 70,249 hrs · 53,652 cycles

CREASE ON EDGE OF CUT OUT BS 1211 AND LONGERON PROJECTION 23 TO 24 RT. EDGE OF CUT OUT ON BS 1211 AND LONGERON PROJECTION 23 TO 24 RT WAS REPAIRED IAW SRM 53-05, FIG 155, OPTION 1.

Part: DOOR FRAME — CRACKED (RT MLG) · airframe 70,204 hrs · 53,613 cycles

CRACK ON FWD INBD DOOR JAMB OF RT MLG. CHANNEL WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4 AND DWG 5930584.

Part: DOOR FRAME — CRACKED (RT MLG) · airframe 70,204 hrs · 53,613 cycles

CRACK ON FWD OTBD DOOR JAMB OF RT MLG, W/W, SM. FWD OTBD DOOR JAMB WAS REPLACED IAW SRM 51-30-2. DIMENTION CRACK IS 2.875".

Part: WIRE HARNESS — BROKEN · airframe 70,204 hrs · 53,613 cycles

BROKEN WIRING BUNDLES ON RT AILERON BUS CONTROL CABLE 35C, REF CARD 85, ZONE 10. CONTROL CABLE SEGMENT 35C WAS REMOVED IAW AMM 20-10-17 AND WILL BE INSTALLED AND ADJUSTED UNDER CARD 2000-9000-02.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 70,204 hrs · 53,613 cycles

CRACKED BEAM NR 1 AFT SIDE AT FWD SERVICE DOOR. INNER SKIN CAP PLATE, HANDLE, FWD, AFT SUPPORT, INTERCOSTALS, AND BEAM WERE REMOVED. NEW BEAM WAS DRILLED, TREATED, AND PAINTED. BEAM, INNER SKIN CAP PLATE, HANDLE, FWD, AFT SUPPORT, INTERCOSTALS WERE INSTALLED IAW SRM 51-30-2, 51-30-4, 51-30-5, 51-10-4, 51-10-3 PAR 21 AND 14. CRACK LONG 0.725".

Part: PAN — CRACKED (SERVICE DOOR) · airframe 70,204 hrs · 53,613 cycles

CRACKED PAN ON FWD SERVICE DOOR AFT UPPER CORNER, TREATED AND PAINTED IAW SRM 51-10-4, 51-10-3 PAR 21 AND 14 DWG REV.

Part: PAN — CRACKED (SERVICE DOOR) · airframe 70,204 hrs · 53,613 cycles

CRACKED PAN AT FWD SERVICE DOOR. SECTION WEB, STRAP WERE REMOVED, REPAIR PARTS WERE FABRICATED, TREATED, PAINTED, SECTION WEB, STRAP AND REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2, 51-30-4, 51-30-5, 52-03D, FIG 3, 51-10-3, PAR 21 AND 14. CRACK. 0.180".

Part: SKIN — CRACKED (BS 1474) · airframe 70,204 hrs · 53,613 cycles

CRACK ON FUSELAGE SKIN BS 1474 LONGERON 15L,. SKIN WAS REPARED IAW SRM 53-01, FIG 4, 51-30-2, AND 51-10-3, PAR 14 AND 21.

Part: FRAME — CRACKED (BS 1485) · airframe 65,470 hrs · 50,210 cycles

FRAME WEB CRACKED AT BS 1485, LBL 20. REPAIRED IAW PRI 522045-14, REV 0. COMPLIED WITH ER/A 522045-14, REV O.

Part: SKIN — CRACKED (BS 1418) · airframe 65,470 hrs · 50,210 cycles

FUSELAGE SKIN CRACKED AT BS 1418 . REPAIRED IAW ER/A 522025-14, REV. ORIG.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 72,479 hrs · 55,287 cycles

MID CARGO DOOR OPENING LOWER FRAME CORRODED. REPAIR IAW SRM 53-05 FIG 123.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 62,237 hrs · 47,913 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT SEAT 32 WAS INOPERATIVE. MAINTENANCE FOUND A LOOSE NUT AND WIRE ON THE TERMINAL STRIP. THE NUT WAS REPLACED AND THE WIRE WAS SECURED. THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: SKIN — CRACKED (BS 1416 L2R) · airframe 1 hrs · 1 cycles

INDICATION OF CRACK AT FASTENER HOLE THRU SKIN BS 1416 INBOARD OF L2R. REPAIRED PER ERA 505959-14 ORIG.

Part: FRAME — CORRODED (BS 1117 L29L/R) · airframe 1 hrs · 1 cycles

AFT CARGO FRAME BS 1117 ANGLE CORRODED L29L TO L29R. REPAIRED PER ERA 505970-14 REV ORIG.

Part: FRAME — CORRODED (BS 1406 L25L) · airframe 62,169 hrs · 47,858 cycles

AFT ACCESORY COMPARTMENT BS 1406 BETWEEN LONG 25 LT AND AFT ENTRANCE STAIRWAY DOOR CUTOUT SUPPORT CHANNEL WITH CORROSION. REPLACED FRAME IAW MD-88 SRM 51-30-2.

Part: SKIN — CORRODED (BS 1184) · airframe 1 hrs · 1 cycles

LOWER BILGE SKIN BUTT SPLICE STRAP HAS CORROSION AT BS 1184 FROM L-26L TO L-29R. REPAIRED PER ER/A 505963-14REV ORIG.

Part: TORQUE BOX — CORRODED (FUSELAGE) · airframe 1 hrs · 1 cycles

AFT CARGO TORQUE BOX UPPER WEB FS 1146 L30-L26R UPPER SURFACE CORRODED, ER/A 493766-14MA REV ORIG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 1 hrs · 1 cycles

AFT CARGO TORQUE BOX LWR INTERNAL BEAM AT L 29R LWR H2 FLANGE HAS A CORRODED STRAP FS 1167-1177. REPAIRED PER ER/A505658-14 REV A.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 1 hrs · 1 cycles

FWD CARGO DOOR INNER SKIN GOUGED AT AFT LOWER END ABOVE LATCH. REPAIRED PER ER/A 505965-14 REV ORIG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 1 hrs · 1 cycles

MAIN CABIN FLOORBEAM STA 1338 HAS CORROSION AND ELONGATED FASTENER HOLES LBL 58 TO RBL 58. REPAIRED PER ER/A 397783-14 MA ORIG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 1 hrs · 1 cycles

AFT CARGO LEFT TIE DOWN TRACK STA 1007 TO 1221 CORRODED. REPAIRED IAW MD-88 SRM 51-30-2.

Part: SKIN — CORRODED (FUSELAGE) · airframe 1 hrs · 1 cycles

AFT CARGO HAS CORROSION IN 4 AREAS ON INSIDE. 3 AREAS WHERE INTERNAL SKIN PIECES TOGETHER AND 1 AREA APPROX 6 INCHES BELOW SEAM. REPAIRED PER MD-88 SRM 51-30-01.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 1 hrs · 1 cycles

CORROSION ON 2 GIRT BAR FITTING SUPPORT CHANNELS FOR SERVICE DOOR ON CUSP WEB STA 1142 AND 1165. REPAIRED IAW MD-88 SRM 51-30-5.

Part: PANEL — CORRODED (RT WING) · airframe 1 hrs · 1 cycles

RT WING FUEL PNL 1462C LANDING HAS PITTING ALL. BLENDED AREA AND FOUND WITHIN LIMITS IAW MD-88 SRM 57-32-4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 1 hrs · 1 cycles

MAIN CABIN FLOORBEAM STA 1309 HAS CORROSION AND ELONGATED FASTENER HOLES AT LBL 18 AND RBL 18. REPAIRED IAW MD-88 SRM 51-70-5.

Part: PANEL — CORRODED (RT WING) · airframe 1 hrs · 1 cycles

RT WING PNL 1456C LANDING AREA HAS PITTING. BLENDED AREA AND FOUND WITHIN LIMITS IAW MD-88 SRM 57-32-4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 1 hrs · 1 cycles

MAIN CABIN SEAT TRACK STA 798 TO 1032 LBL HAS CORROSION AND GOUGES THROUGHOUT. REPAIRED IAW MD-88 SRM 51-30-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 1 hrs · 1 cycles

CORROSION ON MAIN CABIN LT CUSP WEB BETWEEN STA 389-408. REPAIRED IAW MD-88 SRM 51-30-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 1 hrs · 1 cycles

MAIN CABIN RT CUSP WEB STA 1174 HAS CORROSION. REPAIRED IAW MD-88 SRM 51-30-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 1 hrs · 1 cycles

LOWER FUSELAGE STA Y157.5 BELOW LONG 21 RT EXTERNAL SKIN WITH DENT. REPAIRED IAW MD-88 SRM 53-04-3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 1 hrs · 1 cycles

MAIN CABIN SEAT TRACK LBL44 STA 1203 TO 1309 HAS CORROSION AND GOUGES THROUGHOUT. REPLACED SEAT TRACK IAW MD-88 SRM 51-30-01.

Part: STRIP — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

FWD CARGO AT FLOOR TRANSITION STRIP CORRODED STA 427 TO 465 ABOVE L28R. INSTALLED 1 ATTACH STRAP FOR TRANSITION STRIP AT STA 427 ABOVE L28R IAW DC9/MD80 SRM 51-30-5 P1,10,12.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

CORROSION ON LT CUSP WEB BOTTOM SIDE BETWEEN STA636-655 LBL-61. REMOVED DAMAGE. REPAIRED FABRICATED DOUBLER FILLER AND INSTALLED IAW DC-9/MD-80 SRM 53-05 FIG 131A-6 SHEET 1-11.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

AFTER GIRT BAR FITTING REMOVAL CORROSION WAS FOUND IN THE SERVICE DOOR LT CUSP WEB STA 1142 AND LT CUSP WEB EXISTING. REPAIR DOUBLER AT STA 1165 REF CARD NRC NR 212240. INSTALLED 1 REPAIR DOUBLER ON LT CUSP WEB STA 1142 PER ER/A NR 3988191-14MA STEP.

Part: COVER — CORRODED (LT WING) · airframe 62,169 hrs · 47,858 cycles

LT WING HEATER BLANKET COVER NR 1307C CORRODED AND HARDWARE HAS HEAVY RUST OFF A/C. LT WING BLANKET REPLACED.

Part: COVER — CORRODED (RT WING) · airframe 62,169 hrs · 47,858 cycles

RT WING HEATER BLANKET COVER NR 1410 HAS CORROSION ON LANDING AREA AND UPPER SURFACE AROUND SCREW HOLES (HARDWARE RUSTED). RT WING HEATER BLANKET COVER NR 1410 REPLACED.

Part: COVER — CORRODED (LT WING) · airframe 62,169 hrs · 47,858 cycles

RT WING HEATER BLANKET COVER 1409 HAS CORROSION ON LANDING AREA OF A/C. RT WING HEATER BLANKET COVER 1409 REPLACED.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 62,169 hrs · 47,858 cycles

AFT CARGO COMPARTMENT DOOR HAS CORROSION IN 4 ON INSIDE. THREE AREAS WHERE INTERNAL SKIN PIECES TOGETHER AND ONE AREA APPROXIMATELY 6 INCHES BELOW SEAM. CLEANED UP CORROSION ON AFT CARGO DOOR AREA 8 INCHES ABOVE SEAM AND FWD OF AFT HINGE 9.5 INCHES REMOVAL FOUND AREA OUT OF LIMITS. REPAIRED WITH DOUBLERS INSTALLATION STA 1171 L25 IAW MD-88 SRM 52-01 52-05 51-10-03.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 62,169 hrs · 47,858 cycles

RUST ON TOP SURFACE OF RIGHT WING FUEL TANK ACCESS DOOR 1410. REPLACED RT WING FUEL TANK ACCESS DOOR PANEL ARBO872-513.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

RT SIDE EXTERIOR FUSELAGE SKIN HAS A CRACK AT APPROX STA 1380 AND L-14R. ACCOMPLISHED PRI 505302-14 REV 0. ACCOMPLISHED PRI 505302-14 REV 1. COMPLIED WITH ER/A 505302-14 REV ORIGINAL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

SEAT TRACK CORRODED AT LUG AT LBL 22 STA 408-427. INSTALLED 4 PLATE AND SEAT TRACK SECTION AT MAIN CABIN LBL22 BETWEEN STA 427 TO 807 PER DC9/MD80 SRM 53-05 4F.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

LOW FREQUENCY EDDY CURRENT INSPECTION OF FWD SERVICE DOOR JAMB UPPER FWD CORNER DETECTED 2 CRACKS APPROX .125 IN LENGTH EMANATING FROM FASTENER AS MARKED. FABRICATED DOUBLER, TRIPLER, AND FILLERS AND INSTALLED IAW SRMDC-9/MD-8053-05 AND REINSTALLED RIVETS AT STEP 1 IAW SRM DC-9/MD-80.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

MAIN CABIN FLOORBEAM STA 1338 HAS CORROSION AND ELONGATED FASTENERS HOLES LBL58 TO RBL 58. REMOVED CORROSION MAIN CABIN FLOORBEAM STA 1338 BETWEEN RBL47 RBL 58 FOUND TO BE OUT OF LIMITS. REPLACED MAIN CABIN FLOORBEAM SECTION UPPER CAP IAW ER/A 397783-14MA STEPS 9 &10.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

CORROSION ON SHEAR TIE FORMER MID CARGO COMP STA 788 BETWEENL 29R AND L30. INSTALLED REPLACEMENT FORMER AND REPAIR SPLICES IAW MD-88 SRM 51-30-5.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

AFT CARGO COMPT L-29R STA 1290 HAS AREA OF CORROSION. INSTALLED SECTION LONGERON REPAIR AND 2 SPLICE AT AFT CARGO COMPT L29R STA 1283 TO 1301 PER SRM 51-30-5 PARA 7.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

LOW FREQUENCY EDDY CURRENT INSPECTION OF FWD SERVICE DOOR JAMB UPPER FWD CORNER DETECTED 2 CRACKS APPROX .125 IN LENGTH EMANATING FROM FASTENER. REMOVED FASTENERS, CUT OUT DAMAGED AREA. FABRICATED DOUBLER, TRIPLER AND FILLER AND INSTALLED IAW SRM 53-05 DURING HMV.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

MAIN CABIN SEAT TRACK LBL44 STA 1203 TO 1309 HAS CORROSION AND GOUGES THROUGHOUT. BLENDED OUT CORROSION AND GOUGES CHECKED LIMITS AND BLENDED AREA OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK SECTION STA 1203-STA 1309 LBL44 IAW DC9/MD80 SRM 51-30-1 P.1-23 AND AND DC9/MD80 SRM 51-30-5 P. 1-30.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

MAIN CABIN FLOOR STRUCTURE BEAM HAS CORRODED AND ELONGATED FASTENERS HOLES STA 1322 LBL 58 TO RBL 58. INSTALLED REPAIR ANGLES FOR FLOORBEAM REPAIRS AT STA 1322 BETWEEN LBL 41 TO LBL 44 AND BETWEEN RBL 17 TO RBL 21 IAW MD-88 SRM 5305 FIG 79 A AND SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 1273) · airframe 62,169 hrs · 47,858 cycles

MAIN CABIN SEAT TRACK BS 1032 TO 1309 RBL 54 HAS CORROSION GOUGES AND BARE METAL THROUGHOUT. REMOVED CORROSION AND BLENDED GOUGES, FOUND AREA OUT OF LIMITS. CUT OUT DAMAGE AT BS 1273 AND INSTALLED PLUG REPAIR IAW SRM 53-05 DURING HMV.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

AFT CARGO HAS CORROSION ON L-23L AT STA 1182 AND STA 1195. INSTALLED LONGERON SECTION AT AFT CARGO STA 1158 TO 1182 AND INSTALLED SPLICE AND STA 1158 TO 1182 PER DC9/MD80 SRM 53=02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

MAIN CABIN SEAT TRACK STA 1032 TO 1309 RBL 54 HAS CORROSION GOUGES AND BARE METAL THROUGHOUT. REMOVED CORROSION AT STA 1273 FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE AREA FOR PLUG REPAIR AT STA 1273 RT OTBD SEAT TRACK AND INSTALLED REPAIR PLUG IAW DC9/MD80 SRM 53-05 FIG 4ASH 1-2.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

MAIN CABIN RT SIDE CUSP WEB STA 864 TO 886 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW DC-9/MD-80 SRM 53-05 FIG 131A-2 CONFIG -7003. FABRICATED DOUBLERS AND FILLERS AND INSTALLED IAW DC-9/MD80 SRM 53-05 FIG 131A-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

MAIN CABIN SEAT TRACK STA 1032 TO 1309 RBL 22 CHAFED AND CORRODED AROUND SCREW HOLES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK SECTION FS 1032-1108 RBH 22 IAW DC-9/MD80 SRM 51-30-1.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

AFT CARGO LT CUSP WEB TEE ANGLE HAS CORROSION AT STA 1164 L5 AT PREVIOUS REPAIR. FABRICATED AND INSTALLED REPAIR DOUBLER IAW ER/A 398191-14MA AND ER/A 505953-14.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

AFT CARGO COMPT SHEAR TIE BETWEEN LONGERON 30 AND 29R STA 1136 CORRODED. INSTALLED NEW SHEAR CLIP AT STA 1136 LONGERON 26L TO 29R IAW DC-9/MD80 SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

MAIN CABIN RT CUSP WEB STA 503 HAS CORROSION. INSTALLED DOUBLER AND FILLER 1 SPLICE ON REPAIR AREA OF MAIN CABIN RT CUSP WEB STA 503 IAW DC9/MD80 SRM 53-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

MAIN CABIN SEAT TRACK STA 1174 TO 1309 LBL 54 HAS CORROSION AND GOUGES THROUGHOUT. INSTALLED MAIN CABIN SEAT TRACK AT STA 1174 TO 1309 LBL 54 IAW DC9/MD80 SRM 51-30-1 PG 1-23.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

LBL-54 SEAT TRACK HAS SURFACE CORROSION SMALL GOUGE AND BAREMETAL ON UPPER SURFACE BETWEEN STA 446-826. REMOVED AND REPLACED SEAT TRACK AND SPLICE REPAIR IAW DC9/MD80SRM 53-05 SHEET 1-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

LBL-22 SEAT TRACK HAS SURFACE CORROSION SMALL GOUGES AND BARE METAL ON UPPER SURFACE BETWEEN STA 446-826. INSTALLED NEW SEAT TRACK SECTION AT MAIN CABIN LBL 22 BETWEEN STA 427 TO 807 PER DC9/MD80 SRM 53-05 4F.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,169 hrs · 47,858 cycles

AFT CARGO RT CARGO TRACK FS1079-1155 ABOVE L28R HAS MUTIPLE CORRODED AND ELONGATED FASTENER HOLES. INSTALLED NEW SEAT TRACK ON AFT CARGO STA 1079-1155 ABOVE L-28R INCLUDING TORQUE REQUIREMENTS IAW MD-88 SRM 51-30-1 PG 1.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

AFT CARGO TORQUE BOX STA 1218 UPPER SPAN-WISE STRAP CORRODED AT UPPER SURFACE ABOVE L28R. INSTALLED NEW STRAP AT AFT CARGO STA 218 L26R TO L29R PER MD-88 SRM 51-30-5.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

AFT CARGO FS 1212 L30-L29R INTERCOSTAL UPPER FLANGE AFT ATTACH GUSSET CORRODED. INSTALLED -17 GUSSET IAW MD-88 SRM 51-10-9 PG 29-30 AND SRM 51-30-5.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

CABIN MEMBRANE UNDER FLOOR BOARDS IS CORRODED AT A PREVIOUS REPAIR AT FS STA 200 RBL 22 AREA. REMOVED AND REPLACED CORRODED SUBFLOOR PREVIOUS REPAIR STA 200 RBL 22 AREA IAW DC-9/MD80 SRM 51-30-2 PG14.

Part: WEB — CORRODED (BS 200 RBL 22) · airframe 62,169 hrs · 47,858 cycles

CABIN MEMBRANE UNDER FLOORBOARDS CORRODED AT FS 200 RBL 22. REMOVED EXISTING REPAIR, FOUND ADDITIONAL DAMAGE ON SUBFLOOR REQUIRED REPLACEMENT OF ENTIRE WEB. REMOVED WEB, FABRICATED REPLACEMENT AND INSTALLED IAW SRM 51-30-2 DURING HMV.

Part: BEAM — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

AFT CARGO TORQUE BOX LWR BEAM L28R FS1155-1212 HAS CORROSION AT OUTER SURFACE. INSTALLED NEW LOWER BEAM AT AFT CARGO S28R STA 1117-1250 PER MD-88 SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

AFT CARGO FS 1136-1211 RBL-8 T EXTRUSION FLOOR SUPPORT UPPER SURFACE CORRODED MARKED TR007 MRB 53-019-02. INSTALLED T SUPPORT FLOOR AT AFT CARGO FS1136-1211 RBL AND PER DC-9/MD80 SRM 51-30-5.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

AFT CARGO TORQUE BOX FWD UPPER SPAN WISE STRAP FS 1146 L30 -L27R CORRODED AT UPPER SURFACE. INSTALLED NEW STRAP AT AFT CARGO STA 1146 L30-L27R PER MD-88SRM 51-30-2.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

AFT CARGO FS 1155 L29R-28R CORRODED FORMED C ANGLE ATTACHED TO TOP OF TORQUE BOX. INSTALLED NEW C ANGLE STA 1155 L29R-L28R IAW DC9/MD80 SRM 51-30-5 PG 29 AND PG 12.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

CORROSION ON MAIN CABIN LT CUSP WEB AT STA 680 LBL-61. REMOVED CORROSION FROM CUSP WEB FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WEB SECTION IAW SRM 51-30-5 AND 53-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

CORROSION ON MAIN CABIN LT CUSP WEB BETWEEN STA 389-408 LBL-61 CORROSION 100 PERCENT OUT OF LIMITS. AT MAIN CABIN LT STA 389-408 INSTALLED REPAIR DOUBLER AND FILLER IAW DC9/MD80 SRM 53-05 51-30-01 PG 408.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

CORROSION ON MAIN CABIN LT CUSP WEB BETWEEN STA 598-617 LBL61. REMOVED AND REPLACED CORRODED CUSP WEB SECTION IAW DC9/MD80 SRM 53-05 FIG 131A-23.

Part: CUSP WEB — CORRODED (BS 680 LBL 61) · airframe 62,169 hrs · 47,858 cycles

CORROSION ON MAIN CABIN LT CUSP WEB AT S 680 LBL 61. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, TRIMMED OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-30-5 AND SRM 53-05 DURING HMV.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

CORROSION ON LT CUSP WEB UPPER SURFACE AT STA 307 LBL 61 MAIN CABIN. FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW DC-9/MD80 SRM 51-30-5 SRM 53-05 AND DRAWING NR 56-09530015.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

CORROSION ON MAIN CABIN LT CUSP WEB ON 3 AREAS OF SAME SECTION AT STA 550, 564, 588 LBL-61. INSTALLED CUSP WEB SPLICE AND 8 RING DOUBLERS ON MAIN CABIN STA 548 TO 598 LBL 44.5 TO LBL 61 IAW MD-88 SRM 53-05 FIG 131.

Part: CUSP WEB — CORRODED (BS 598-617) · airframe 62,169 hrs · 47,858 cycles

CORROSION ON MAIN CBIN LT CUSP WEB BETWEEN ST 598-617 LBL 61. REMOVED CORROSION FROM CUSP WEB, MATERIAL LOSS FOUND TO BE 100 PERCENT. REMOVED SECTION OF CUSP WEB FROM BS 598 TO 617. FABRICATED AND INSTALLED NEW SECTION OF WEB IAW SRM 51-10-02 DURING HMV.

Part: CUSP WEB — CORRODED (BS 307 LBL 61) · airframe 62,169 hrs · 47,858 cycles

CORROSION ON LT CUSP WEB UPPER SURFACE AT STA 307 LBL61 MAIN CABIN. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION OF CUSP WEB. FABRICATED REPAIR DOUBLERS, AND INSTALLED IAW SRM 51-30-5 DURING HMV.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 62,169 hrs · 47,858 cycles

ACCOMPLISH SRM 53-04D FIG 38 ACTL 3102 PERMANENT REPAIR TO DENT STA 214 BELOW L-17L. INSTALLED DOUBLER FILLER AND FINGER DOUBLER IAW MD-88 53-04-05 FIG 2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,969 hrs · 47,712 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS OVER BOTH THE LEFT MAIN CABIN DOOR AND THE RIGHT MAIN CABIN DOOR WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 61,619 hrs · 47,462 cycles

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

Part: SKIN PANEL — CRACKED (HORIZ STAB) · airframe 61,148 hrs · 47,158 cycles

EA 09-460214-12AD HORIZONTAL STAB UPPER LT AFT SKIN PANEL SPLICE PER DWG SR09550028 (EA09-460214-12).

Part: SPAR CAP — CRACKED (HORIZ STAB) · airframe 61,148 hrs · 47,158 cycles

EA-09-460214-12AD ME15 UPPER LT HORIZONTAL STAB CAP SPLICE C/W.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 59,873 hrs · 46,301 cycles

CREW WROTE UP COCKPIT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN POWER SUPPLY FOR LIGHTS PER AMM 33-50-00-001. OPERATION OF LIGHTS NOW CHECKS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,317 hrs · 45,935 cycles

FLIGHT CREW FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 13, 14, 15, THREE LIGHTS ON CAPTAINS SIDE AND ONE ABOVE 13 FIRST OFFICERS SIDE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES AND THE BATTERY PACK AT STATIONS 386 AND 500. OPERATION CHECKS GOOD.

Part: TERMINAL — DEFECTIVE (CABIN) · airframe 58,225 hrs · 45,203 cycles

CREW WROTE UP EMERGENCY PATH LIGHT AT ROW 3 AS INOPERATIVE. MAINTENANCE REPLACED THE TERMINAL END AT ROW 3. OPERATION OF LIGHT NOW CHECKS GOOD. (2010-D1406) (DLM88103255)

Part: WIRE — LOOSE (CABIN) · airframe 57,980 hrs · 45,041 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 3 INOPERATIVE. MAINTENANCE SECURED LOOSE WIRE AT THE QUICK DISCONNECT. OPERATION OF LIGHT NOW CHECKS OK. (2010-D1255) (DLM88102864)

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 56,981 hrs · 44,354 cycles

ON FLIGHT CHECK MX FOUND EMERGENCY LIGHTS AT SEAT 14 AND 24 WERE INOPERATIVE. MX REPLACED WIRE HARNESS AT SEAT 14 AND RE-LAMPED AT ROW 24. OPS CHECK OF LIGHTS NOW CHECKS GOOD.

Part: CHARGER — FAILED (E/E BAY) · airframe 49,325 hrs · 39,315 cycles

ON PREFLIGHT, FOUND BATTERY CHARGER C/B POPPED. RESET AND RAN EMERGENCY POWER CHECK. FOUND BATTERY CHARGER C/B RE-POPPED. T/S PER WDM FOUND A AND C PHASE WIRES FROM C/B TO CHARGER BOTH MOUNTED ON C PHASE LUG. REWIRED C/B PER WDM. REPLACED BATTERIES AND CHARGER AND C/B. ALL REST PER M/M NML. OK FOR SERVICE.

Part: CHARGER — BURNED (E/E BAY) · airframe 49,311 hrs · 39,306 cycles

BATTERY CHARGER CAUGHT ON FIRE AND POPPED C/B. INSTALLED NEW R2-56 RELAY NEW TEMP SENSORS, REINSTALLED BATTERY TRAY. INSTALLED NEW BATTERY CHARGER. REMOVED AND INSTALLED NEW BATTERY CHARGER C/B. BATTERIES LT S/N OFF 1030768 ON 10503139. RT S/N OFF 10503142 ON 10403938 DAL P/ 249701544.

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

AFT CARGO THRESHOLD BLENDED (SILL AREA) STILL SHOWS EVIDENCE OF CORROSION. FWD AND AFT HORIZ FLANGES BLENDED OUT OF LIMITS IAW DC-9/SRM MD-88 SRM 53-05 FIG 63. FABRICATED AND INSTALLED DOUBLER REPAIR FROM 6AL-4V.040 TITANIUM IAW DC-9/MD-88 SRM 53-05D FIG 63 AND 51-10-3D AND DELTA PS 900-5-1.

Part: SKIN — DAMAGED (BS 440 S30LR)

FS 440 L-30 AT ATC ANTENNA REQUIRES REPAIR. FABRICATED AND INSTALLED REPAIR 16" BY 18" FROM 2024-T3 .063", AND DOUBLER 19-1/2" BY 17" FROM 2024-T3 .025" IAW DC-9/MD-88 SRM 53-04D FIG 44 AND 51-10-3D AND DELTA PS 900-5-1.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2

CORROSION ON LT TRACK FROM FS 1231 TO 1322 IN SEVERAL PLACES AROUND SCREW HOLES IN AFT CARGO PIT. REMOVED SEAT TRACK SECTION. TRIMMED, DEBURRED, TREATED, PRIMED AND INSTALLED SEAT TRACK 100.5" FROM S2922357-14400 IAW DC-9/MD-88 SRM 51-10-3D, 51-10-4.

Part: SKIN — DENTED (ZONE 100)

DENTS IN FUSELAGE SKIN FS 246 L-18L AND FS 232 L-15L. FABRICATED AND INSTALLED REPAIR SKIN DOUBLER 22" BY 18" FROM 2024-T3 .063", AND DOUBLER 3.9" BY 3.5" FROM 2024-T3 .032" AND P/N S2912900-5U5000 IAW DC-9/MD-88 SRM 53-04D FIG 12B AND FIG 38 AND 51-10-3D.

Part: SKIN — DAMAGED (ZONE 200)

FUSELAGE SKIN RT AFT CORNER OF NLG DOOR CUTOUT CRACKED. FABRICATED AND INSTALLED SKIN REPAIRS 25" BY 9" BY 3-1/2" BY 4" AND 6" BY 3" BY 6" BY 1-1/2" FROM 2024-T3 .040" IAW DC-9/MD-88 SRM 51-10-3D AND DELTA ERA NR 385558-14 IR, DATED 08-07-03.

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

CORROSION ON FLOOR SUPPORT AT RBL 45 AND BETWEEN FS 160 AND 200. BLENDED PER DC-9/MD-80 SRM 51-10-3 AND 53-01D, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED FLOOR SUPPORT 38" BY 2" BY 1" FROM 7075-T6511 IAW DC-9/MD-88 SRM 51-10-2, 51-10-4, 51-10-3D AND 51-30-05.

Part: SKIN — DAMAGED (BS 308 S29R)

LIGHTNING STRIKE RT FS 308 1-1/2" ABOVE L-29R. BLENDED LIGHTNING STRIKE, FABRICATED AND INSTALLED REPAIR DOUBLER 6-1/4" BY 6-1/4" FROM 2024-T3 .032" IAW DC-9/MD-80 SRM 53-04D FIG 38, SH 20, 51-10-3D AND 51-10-4D.

Part: SKIN — DAMAGED (BS 542) · corrosion level 2

LIGHTNING STRIKE RT FS 542.5, 1-1/4" ABOVE L-22R. BLENDED LIGHTNING STRIKE. FABRICATED AND INSTALLED REPAIR DOUBLER 6-1/2" BY 7" FROM 2024-T3 .032" IAW DC-9/MD-88 SRM 53-04 FIG 38, SH 20 AND 51-10-3D.

Part: SKIN — DAMAGED (ZONE 200)

LIGHTNING STRIKE LT FS 188.5 1" BELOW L-24L (3 EA.). BLENDED PER DC-9/MD-80 SRM 53-04D, FOUND TO BE CRACKED. ROUTED OUT CRACK. FABRICATED AND INSTALLED SKIN REPAIRS 9" BY 6" BY 5-1/2" FROM 2024-T3 .025" AND 3-3/4" BY 4-1/2" FROM 2024-T3 .050" IAW DC-9/MD-88 SRM 53-04 FIG 38.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2

CORROSION ON FLOORBEAM AT RBL 12 TO RBL 47 FS 200. BLENDED PER DC-9/MD-80 SRM 51-10-3 AND 53-01D, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED FLOORBEAM 37.5" BY 2-1/2" IAW DC-9/MD-88 SRM 51-10-2, 51-10-4, 51-10-3D AND 51-30-5.

Part: SKIN — DAMAGED (BS 440 S26L)

LIGHTNING STRIKE LT FS 440 1/2" ABOVE L-26L. BLENDED LIGHTNING STRIKE, CUT OUT WORN AREA, FABRICATED AND INSTALLED 3 REPAIR DOUBLERS 1" DIAMETER, 8" BY 1-5/8" BY 9" AND 5-5/8' BY 5-5/8' BY 5-1/4" FROM 2024-T3 .050" AND FINGER DOUBLER 7-1/4" BY 4-3/8" BY 8-3/8" FROM 2024-T3 .025" IAW DC-9/MD-80 SRM 53-04D FIG 38, VIEW V AND 51-10-3D.

Part: SKIN — DAMAGED (BS 1318 S20R)

LIGHTNING STRIKE RT FS 1318 2" ABOVE L-20R. BLENDED LIGHTNING STRIKE, FABRICATED AND INSTALLED REPAIR DOUBLER 5-3/4" BY 5-1/4" FROM 2024-T3 .032" IAW DC-9/MD-80 SRM 53-04D FIG 38, SH 20 AND 51-10-3D.

Part: SKIN — DENTED (BS 1448 S22R)

FOUND DENT AT FS 1448, L-22R. COLD WORKED SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER 5-1/4" BY 5" FROM 2024-T3 .032" IAW DC-9/MD-80 SRM 53-04D FIG 38, AND 51-10-3D.

Part: SKIN — DAMAGED (ZONE 100)

LIGHTNING STRIKE LT FS 265 4" BELOW L-29L (1 EA.). BLENDED PER DC-9/MD-80 SRM 53-04D, FOUND TO BE CRACKED. ROUTED OUT CRACK. FABRICATED AND INSTALLED SKIN REPAIR 3-3/4" BY 3-3/4" FROM 2024-T3 .032"IAW DC-9/MD-88 SRM 53-04 FIG 38, 51-10-3D AND 53-34-0 FIG 2.

Part: SKIN — DAMAGED (ZONE 100)

LIGHTNING STRIKE LT FS 353, 1" ABOVE L-25 (1 EA.). BLENDED PER DC-9/MD-80 SRM 53-04D FIG 38, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED INTERNAL DOUBLER 6" BY 8" IAW DC-9/MD-88 SRM 51-10-3D AND 53-04D FIG 38.

Part: WIRE — CHAFED (GALLEY) · airframe 44,470 hrs · 36,032 cycles

CREW REPORTED HEARING A BANG FROM BEHIND THE CB PANEL AT WHICH TIME THE COCKPIT FILLED WITH SMOKE. FLIGHT ATTENDANT REPORTED SEEING SPARKS FROM THE OVERHEAD PANEL JUST OUTSIDE ON THE FIRST CLASS GALLEY. NO SMOKE REPORTED IN CABIN AREA. SMOKE DISSIPATED AND NORMAL LANDING. FOUND GALLEY POWER CABLES CHAFED AGAINST A/C SUPPLY DUCT CLAMP. REPAIRED WIRING AND DUCT INSULATION. REPLACED DUCT CLAMPS.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 44,315 hrs · 35,923 cycles

CRACK IN NR 3 LT STRINGER AT JOINT WITH STA 160, CRACK IN NR 4 LT STRINGER AT JOINT WITH STA 160.

Part: LINE — LEAKING (LT ENGINE) · airframe 43,091 hrs · 35,059 cycles

EN ROUTE TO EWR FROM ATL A/C SUFFERED HYDRAULIC FAILURE. CREW ELECTED TO DIVERT TO GSO AS A PRECAUTION. REPLACED LT ENGINE HYDRAULIC RETURN LINE FOR LEAKAGE.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 39,424 hrs · 32,513 cycles

APPROCH FLT.615 AT 1329 - RT SYS HYD FLUID LOSS, HYD RETURN LINE WORN THRU RT SIDE AFT ACCESSORY BAY. FLEX LINE PN 299201301 REPLACED. REPLACED RT ENGINE DRIVEN HYD PUMP. REPLACED HYD FILTERS, WASHED APU INLET. REPLACED COALESCER BAGS & PERFORMED PNEUMATIC SYS DUCT BURNOUT-

Part: SKIN — CORRODED (FS 246, S-30) · airframe 38,685 hrs · 32,003 cycles

FUSELAGE / SKIN / TCAS ANTENNA CUTOUT / FS 246 / S-30 : CORROSION REPAIR THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION NEAR THE TCAS ANTENNA CUTOUT AT FS 246 BETWEEN STRINGERS 30 & 29L. THE CORROSION WAS REMOVED BY MACHINING AWAY. THE AREAWAS REINFORCED WITH AN EXTERNAL ALUMINUM DOUBLER TO ENCOMPASS THE ANTENNA INSTALLATION AREA. THE REPAIR WAS ACCOMPLISHED PER ER/A 383223-14, REV A.

Part: ODOR — DETECTED (CABIN) · airframe 38,013 hrs · 31,482 cycles

LEFT AFT LAV SMOKE DETECTOR SOUNDED ON APPROACH FOLLOWED BY HOT SMELL FUMES IN CABIN AND COCKPIT. NO VISIBLE SMOKE AND SMELL DISSIPATED ON TAXI. CROSSFEEDS CLOSED, AIRFOIL ANTI ICE OFF, ENGINE ANTI ICE ON, APU OFF, LEFT TEMP CONTROL COLD, RIGHT TEMP CONTROL WARM. SMELL DESCRIBED AS PACK OVERHEAT. NO PACK TRIP. PERFORMED DUCT BURNOUT.

Part: PUMP — FAILED (NR 2 ENGINE) · airframe 37,826 hrs · 31,336 cycles

RT ENGINE SHUT DOWN TWO MINUTES INTO CLIMB, EGT WENT TO ZERO, HAD F/F AND N1AND N2. SHUT ENGINE DOWN, WINDMILLED FOR 15 MIN WITH POSITIVE OIL PRESS. REPLACED FUEL PUMP.

Part: A/C PACK — CONTAMINATED (CABIN) · airframe 35,711 hrs · 29,778 cycles

IMMEDIATELY AFTER T/O , SMOKE DETECTOR IN AFT LAV WENT OFF. AFT F/A REPORTED SMOKE SMELL AS ELECTRICAL. FWD F/A COULD SMELL SMOKE AS WELL. BY THE TIME WE RETURNED FOR LANDING, SMOKE DISSAPATED. PERFORMED DUCT BURN OUT

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 34,281 hrs · 28,748 cycles

1R DOOR SLIDE PACK FELL OUT OF DOOR ONTO CABIN FLOOR, PINS IN PACK PULLED OUT. REPLACE PACK, NO DEPLOYMENT OF SLIDE AND SLIDE WAS NOT SECURED TO GIRT BAR. SLIDE FELL OUT OF PACK WHEN DOOR CLOSED.

Part: COVER — LOOSE (LT SLAT) · airframe 34,136 hrs · 28,639 cycles

AIR TURNBACK, ON SLAT RETRACT HEARD CONTINUOUS LOW FREQUENCY NOISE. SLATS EXTENDED WITH NO NOISE OR ABNORMAL FLIGHT CONTROL RESPONSES. RAN FLAPS AND FOUND LT INBOARD LEADING EDGE SLAT TRACK COVER LOOSE. TIGHTENED SAME.

Part: HYD LINE — LOOSE (T/R UNIT)

LOW HYD QTY ON LEFT SIDE (2 QUARTS) AND ASSOCIATED LEFT LOW HYD PRESSURE MESSAGE OCCURRED ON SHORT FINAL TO LANDING. AFTER LANDING GEAR AND FULL FLAPS EXTENDED. TIGHTENED B-NUT ON THRUST REVERSER MODULE.

Part: GPWS COMP — INOPERATIVE (E/E COMPT)

ON SHORT FINAL--500 AGL--GPWS WENT OFF WITH TOO LOW GEAR. EXECUTED A GO-AROUND AND TRIED ANOTHER APPROACH WITH SAME THING HAPPENING. GPWS WENT OUT AT 50 FT AGL. ALL GEAR WERE DOWN AND 3 GREEN ON BOTH APPROACHES. REPLACED GPWS COMPUTER, CHKS GOOD.

Part: WIRE — LOOSE (CABIN)

ON S/C, FOUND AIRSTAIR EMERG EXIT LIGHT INOP ON RT SIDE CTR POS. FOUND WIRES PULLED OUT OF CONTACTS. REPINNED, EMERG LIGHTS OP NML.

Part: BATTERY — DISCHARGED (CABIN)

AFT FLOOR TRACK LIGHTS WILL NOT ILLUMINATE. REPLACED BATTERY, OPS NORMAL.

Part: DUCT — WORN (RT AC TRIM VLV)

ON CLIMBOUT AT 310 TAIL COMP OVHT LIGHT CAME ON. PLACED A/C HP BLD SWITCHES TO OFF AND LIGHT EXTINGUISHED. ON DESCENT WITH THROTTLES BACK TO IDLE CABIN CLIMBED AT 1,000 FT A MIN AND FLOW LIGHT CAME ON. FOUND RUPTURED BOOT ON DUCT JUST ABOVE RT A/C TRIM VLV. REPLACED WORN DUCT BOOTS AND CLAMPS, LK CKD SYS AT T/O PWR.

Part: WIRE — CHAFED (YAW DAMPER)

AFTER T/O LOST DFGC CONTROL, DGF CIRCUIT BREAKER C-17 POPPED UNABLE TO RESET, LANDED CHA. FOUND WIRE 1C610R20RD CHAFING AND SHORTED AT APPROX 1 FOOT IN FRONT OF YAW DAMPENER ACTUATOR. REPAIRED WIRE OPERATION NORMAL.

Part: GENERATOR — FAILED (NR 1 ENGINE)

DURING CRUISE, LEFT GENERATOR WENT OFF LINE, STARTED APU HAD CROSS TIE LOCKOUT. DIVERTED CVG. RESET CROSSTIE OPERATION NORMAL, DEFERRED PER MEL NR 1 GEN. GENERATOR WAS REPLACED AND ROUTED TO SHOP, OPERATION NORMAL.