N920DL

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 74,774 hrs · 56,339 cycles

RIGHT WING HAD WEAR ON PREVIOUS REPAIR DOUBLER AT INBD FLAP VANE. REPAIRED IAW SRM 57-03D PAR 11.

Part: SKIN — DELAMINATED (RT AILERON) · airframe 74,774 hrs · 56,339 cycles

RIGHT WING. DELAMINATED RT AILERON TRAILING EDGE STA XA= 470. RH AILERON TRAILING EDGE XA=470 WAS REPAIRED IAW SRM 51-70-1D PAR- .10.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 74,774 hrs · 56,339 cycles

RIGHT WING HAD WEAR ON PREVIOUS REPAIR DOUBLER AT MID FLAP VANE. THE FLAP WAS REPAIRED IAW SRM 57-03D PAR 11.

Part: DOOR — DAMAGED (MLG) · airframe 74,774 hrs · 56,339 cycles

MAIN LANDING GEAR HAD WEAR ON REPAIR DOUBLER EDGE OF RT MLG INBD DOOR BS 995. REPLACED IAW ERA 490554-14MA REV.ORIG.

Part: DOUBLER — CRACKED (LT WING) · airframe 74,774 hrs · 56,339 cycles

LEFT WING CRACKED PRODUCTION DOUBLER AT LH WING UPPER SURFACE XW= 50. REPAIRED IAW SRM 57-03D FIG.34.

Part: BEARING — DAMAGED (ELEVATOR) · airframe 74,774 hrs · 56,339 cycles

HORIZONTAL STABILIZER FREE PLAY LT & RT ELEVATOR ANTI-FLOAT TABS. BEARING BUSHINGS AND HARDWARE WERE REPLACED FOR NEW ONES AT LH/RH ANTI-FLOAT TABS AND WERE INSTALLED AND ADJUSTED. (LP# 2827688)

Part: SKIN — CRACKED (L1 DOOR) · airframe 74,774 hrs · 56,339 cycles

L1 DOOR CRACKED ON EXTERNAL SKIN ABOVE HANDLE. THE DOOR SKIN WAS REPAIRED IAW ER/A 501106-14MA.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 74,774 hrs · 56,339 cycles

CRACK CUTOUT ACCESS PANEL 6301A OF VERTICAL STAB PREVIOUS DOUBLER REPAIR WAS REMOVED, NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 55-05 FIG 3.

Part: LONGERON — CRACKED (BS 160) · airframe 74,774 hrs · 56,339 cycles

CRACKED LONGERON 2L BS 160. REPAIRED IAW SRM 53-02 FIG. 18.

Part: PAN — CRACKED (R1 DOOR) · airframe 74,774 hrs · 56,339 cycles

R1 DOOR CRACKED ON PAN, FWD EDGE BETWEEN BEAMS 2 AND 3. THE PAN WAS REPAIRED IAW SRM 52-03 D FIGURE 3.

Part: BEAM — CRACKED (PAX DOOR) · airframe 74,774 hrs · 56,339 cycles

CRACKED BEYOND STOP DRILL ON AFT EDGE BEAM NR 1 AT MAIN ENTRANCE DOOR. REPAIRED IAW SRM 52-05 PAR 68 FIG 81.

Part: DOOR FRAME — DAMAGED · airframe 74,774 hrs · 56,339 cycles

MID CARGO BAY CORRODED ON PREVIOUS REPAIR SPACER AT LOWER DOOR JAMB. PREVIOUS REPAIR SPACER WAS REPLACED IAW SRM 53-05 FIG. 123.

Part: BEAM — CORRODED (DOOR FRAME) · airframe 74,774 hrs · 56,339 cycles

AFT CARGO COMPARTMENT: CORROSION ON LOWER DOOR JAMB BEAM. REPAIRED IAW SRM 51-02 PAR- .A (6), SRM 53-05 FIG. 123, SHEET 2, AND DWG 5936038 REV. A.

Part: SKIN — CRACKED (BS 1474) · airframe 74,774 hrs · 56,339 cycles

CRACK ON FUSELAGE SKIN BS 1474 LEFT SIDE (FUS). REPAIRED IAW SRM 53-01 FIG 4 SHEET 4,

Part: WIRE — PULLED (CABIN) · airframe 74,254 hrs · 55,939 cycles

DURING SERVICE CHECK FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOP. FOUND WIRES PULLED OUT AT CONNECTION, REPLACED CONNECTIONS AS REQUIRED PER WDM 33-51-14. OPS CHECKS GOOD, OK FOR SVC.

Part: PIN — DISENGAGED (L1 DOOR SLIDE) · airframe 73,172 hrs · 55,107 cycles

MAINTENANCE FOUND A L-1 DOOR EMERGENCY ESCAPE SLIDE PARACHUTE PIN DISENGAGED. THE SLIDE RAFT WAS REPLACED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,005 hrs · 54,274 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: LIGHT — INOPERATIVE (SEAT 12DE) · airframe 71,304 hrs · 53,766 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 12DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE ILLUMINATOR FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,170 hrs · 53,662 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS IN THE 1ST CLASS SECTION WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 1155-1211) · corrosion level 2 · airframe 69,363 hrs · 52,526 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED. BS 1155-1211. BLENDED THE FLOOR SUPPORT AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-01. REMOVED THE FLOOR SUPPORTIAW SRM 51-30-01. NEW FLOOR SUPPORT LOCATED, DRILLED, ALODINED, PRIMED, TOP COATED, AND INSTALLED, IAW SRM 51-30-01 AND SRM 51-10-3B.

Part: WEB — CORRODED (BS 427-435) · corrosion level 2 · airframe 69,392 hrs · 52,546 cycles

CARGO DOOR CUTOUT AFT WEB CORRODED APPROXIMATELY BS 427-435, BETWEEN LONGERONS 25-28R. REMOVED CORROSION IAW SRM 53-01, FIG 1 AND 51-10-3, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. CUTOUT DAMAGED AREA IAW SRM 53-01. FABRICATED NEW DOUBLER REPAIR, ALODINED, PRIMED, AND INSTALLED NEW DOUBLER IAW SRM 53-01, FIG 2, 53-14-2, FIG 2, 51-10-3, AND 51-30-8.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,514 hrs · 51,225 cycles

EMERGENCY CEILING LIGHTS INOPERATIVE AT ROW 26-33. REPOSITIONED BATTERY PACK. EMERGENCY LIGHTS OPS CHECKED GOOD.

Part: BUSHING — CORRODED (RT MLG) · airframe 66,901 hrs · 50,822 cycles

RT MLG BOTTLE BOLT BUSHING DAMAGED. REMOVED BUSHING IAW CMM 57-40-02. REMOVED CORRISION IAW ER/A 520710-14AD

Part: BUSHING — MIGRATED (LT MLG) · airframe 66,901 hrs · 50,822 cycles

BOTTLE BOLT BORE, OUTBD BUSHING MIGRATED IN LEFT MLG. REMOVED BUSHING PER CMM 57-40-02. MANUFACTURED, HEAT TREATED, CLEANED, INSPECTED, AND CAD PLATED IAW PRI 520700-14AD DWG 2937332.

Part: BUSHING — MIGRATED (MLG) · airframe 66,901 hrs · 50,822 cycles

BOTTLE BOLT BUSHING AT GEAR FITTING MIGRATED. REMOVED BUSHINGS IAW CMM 57-40-02. MANUFACTURED, HEAT TREATED, CLEANED, INSPECTED, AND CAD PLATED PER PRI 520700-14AD, DWG 2937332. ALL STEPS COMPLETED FOR PRI 520700-14AD REV. 2.

Part: BEARING — DAMAGED (RT MLG) · airframe 66,901 hrs · 50,822 cycles

RT MLG BOTTLE BOLT OTBD BEARING DAMAGED. REMOVED BEARING IAW CMM 57-40-02. ACCOMPLISHED MPI OF FABRICATED BEARING IAW P/S 900-6-2 PER ER/A 520710-14AD REV 1, NO CRACK INDICATIONS NOTED. COMPLETED STEPS 1 THRU 12 PER PRI 520710-14AD. ALL STEPS 1-18 ON PRI 520710-14AD REV I COMPLETED AWAITING ERA. FINAL ER/A RECIEVED. (LP #1188046)

Part: FEEDER CABLE — OVERHEATED (GALLEY) · airframe 66,790 hrs · 50,741 cycles

RETURNED TO DEPARTURE AFTER TAKEOFF, DUE TO A SMOKING COFFEEMAKER IN L1 GALLEY. F/A SAW SMOKE, & NOTED AN ELECTRICAL ODOR, DISCHARGED TWO FIRE EXTINGUISHERS. SMOKE DISSIPATED. ALL GALLEY CIRCUIT BREAKERS TRIPPED. MAINTENANCE FOUND AN OVERHEATED SWITCH, S3-23, AT LUG AND ALSO AN OVERHEATED APU FEEDER WIRE AT THE CONNECTION BLOCK. TERMINAL STRIP, GROUND SERVICE RELAY, AND APU BREAKER WERE REPLACED ALONG WITH A SEVEN FOOT SECTION OF WIRE. NR 2 COFFEEMAKER REPLACED.

Part: RECEPTACLE — WORN (TAILCONE RELEASE) · airframe 65,590 hrs · 49,895 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE SYS LATCH RECEPTACLES WERE WORN BEYOND OF ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: SKIN — CRACKED (BS 1437) · airframe 65,590 hrs · 49,895 cycles

ACFT SKIN CRACKED APPROX .5" LONG THROUGH RIVET HOLE BS 1437, 1" INBD OF LONGERON 3 LT. ALL WORK COMPLETED ON PRI 514384-14, REV-O AND REV-1.

Part: BRACKET — WORN (TAILCONE RELEASE) · airframe 65,590 hrs · 49,895 cycles

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

Part: BUSHING — WORN · airframe 65,590 hrs · 49,895 cycles

MX DISCOVERED THAT THE TEE PIN AND THE TEE PIN BUSHING WERE WORN BEYOND ALLOWABLE LIMITS AND REQUIRED REPLACEMENT. THE RII COMPLETED FOLLOWING MX.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 65,032 hrs · 49,529 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FORWARD SECTION OF THE CABIN HAD FAILED. MX REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,710 hrs · 49,291 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT ROWS 12-15 AND ROWS 29-31 WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 64,609 hrs · 49,211 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE COCKPIT WAS INOPERATIVE. MX RE-TORQUED A LOOSE WIRING CONNECTION AT THE LIGHT ASSY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,543 hrs · 49,164 cycles

DURING LINE CHECK, MX FOUND THAT THE SEAT MOUNTED EMERGENCY PATHWAY LIGHTING AT 20DE IN THE CABIN WAS INOPERATIVE. MX REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,494 hrs · 49,127 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE COCKPIT AND AT DOORS L1 & L2 WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 64,209 hrs · 48,915 cycles

DURING FLIGHT, CREW FOUND THEY HAD NO CONTROL OF THE EMERGENCY PATHWAY LIGHTING IN THE COCKPIT, THEY WOULD NOT TURN OFF. MX FOUND A LOOSE GROUND WIRE IN THE LIGHT SYS ABOVE THE R1 DOOR AND SECURED IT. THE FUNCTIONAL CHECK OF THE SYS WAS SATISFACTORY.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 64,209 hrs · 48,915 cycles

DURING FLIGHT, PILOTS FOUND THEY HAD NO CONTROL OF THE EMERGENCY PATHWAY LIGHTING IN THE COCKPIT, THEY WOULD NOT TURN OFF. MX REPLACED THE LIGHT ASSEMBLIES & POWER SUPPLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF THEM.

Part: LIGHT — LOOSE (COCKPIT) · airframe 64,182 hrs · 48,894 cycles

PILOT REPORTED THAT THE EMERGENCY PATHWAY LIGHTING IN THE COCKPIT REMAINS ILLUMINATED AT ALL TIMES. MX PROPERLY SECURED THE LIGHT ASSY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,175 hrs · 48,888 cycles

THE PILOT REPORTED THAT THE EMERGENCY PATHWAY LIGHTING IN THE COCKPIT HAD ILLUMINATED UNCOMMANDED, FOLLOWING ELECTRICAL POWER TRANSFER. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,182 hrs · 48,894 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY LIGHTING IN THE COCKPIT WOULD NOT SHUTOFF, NON-CONTROLABLE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHT RETURNED TO AN OPS CONDITION.

Part: CONTROL PANEL — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 64,102 hrs · 48,832 cycles

DURING LINE CHECK, MAINTENANCE FOUND THEY HAD NO CONTROL OF THE EMERGENCY LIGHTING IN THE COCKPIT, LIGHTS WOULD NOT TURN OFF. MAINTENANCE RESEATED THE CONTROL PANEL AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: HYDRAULIC LINE — LEAKING (RT MLG WW) · airframe 62,357 hrs · 47,596 cycles

CREW EXECUTED AN ATB DUE TO SMOKE IN THE CABIN AND COCKPIT DURING TAKEOFF. THE SMOKE DISSIPATED AFTER THE PACKS WERE TURNED OFF. MAINTENANCE FOUND THE APU INLET CONTAMINATED WITH HYDRAULIC FLUID FROM A LOOSE GROUND SPOILER LINE LOCATED IN RIGHT WHEEL WELL. THE LINE WAS SECURED, A DUCT BURNOUT ACCOMPLISHED, AND BOTH COALESCER BAGS WERE REPLACED.

Part: BELTFRAME — DAMAGED (FUSELAGE) · airframe 62,053 hrs · 47,415 cycles

LIGHTNING STRIKES ON RT WINDOW BELT FRAME UPPER SECTION AND AFT SECTION BTW STA 826 AND 845 AT FUSELAGE SKIN. LIGHTNING STRIKES WERE BLENDED OUT IAW DC9/MD88 SRM 53-05 FIG 111 SHEET 10 ZONE 1 AND REPAIRED IAW ERA 496433-14 REV ORIGINAL.

Part: BELTFRAME — DAMAGED (FUSELAGE) · airframe 62,053 hrs · 47,415 cycles

LIGHTNING STRIKES ON RT WINDOW BELT FRAME FWD SECTION AND AFT UPPER CORNER BTW STA 769-788 AT FUSELAGE SKIN. LIGHTNING STRIKES WERE BLENDED IAW DC9/53 SRM 53-05 FIG 111 SHEET 10 ZONE 1 AND FOUND WITHIN LIMITS. REPAIR WAS ACCOMPLISHED IAW ERA 496433-14 REV ORIG.

Part: BELTFRAME — DAMAGED (FUSELAGE) · airframe 62,053 hrs · 47,415 cycles

LIGHTNING STRIKE ON RT WINDOW BELT FRAME BTW STA 731-750 AND 750-769 LIGHTNING STRIKES WERE BLENDED IAW SRM 53-05 FIG 111 SHEET 10 ZONE 1. REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW AMR 0953943 REV ORIG.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 62,053 hrs · 47,415 cycles

SCRATCHES WERE FOUND ON FUSELAGE SKIN AT THE AFT LOWER CORNER BETWEEN STA Y=636 AND Y=655 AND BETWEEN STA Y=674 AND Y=693 AT THE UPPER SECTION OF THE CABIN WINDOW CUTOUTS. AREAS WERE BLENDED IAW DC9/MD88 SRM 53-05 FIG 111 ZONE 2. AREAS WERE REPAIRED IAW ERA 496433-14 REV ORIG.

Part: BELTFRAME — DAMAGED (FUSELAGE) · airframe 62,053 hrs · 47,415 cycles

LIGHTNING STRIKES ON LT WINDOW BELT FRAME FWD/AFT SECTIONS BTW STA 579 AND 598. LIGHTNING STRIKES WERE BLENDED OUT IAW DC9/MD88 SRM 53-05 FIG 111 SHEET 12 ZONE 2 AND REPAIRED IAW ERA 496433-14 REV ORIGINAL.

Part: BELTFRAME — DAMAGED (FUSELAGE) · airframe 62,053 hrs · 47,415 cycles

LIGHTNING STRIKE ON LT WINDOW BELT FRAME FWD/AFT LOWER SECTION BTW STA 845 AND 864. LIGHTNING STRIKE WAS BLENDED OUT IAW DC9/MD88 SRM 53-05 FIG 111 SHEET 10 ZONE 1 AND REPAIRED IAW ERA 496433-14 REV ORIGINAL.

Part: BELTFRAME — DAMAGED (FUSELAGE) · airframe 62,053 hrs · 47,415 cycles

LIGHTNING STRIKE ON RT WINDOW BELT FRAME FWD SECTION AND SCRATCH ON AFT LOWER CORNER BTW STA 886 AND 905. LIGHTNING STRIKES WERE BLENDED OUT IAW DC9/MD88 SRM 53-05 FIG 111 SHEET 14 ZONE 3 AND REPAIRED IAW ERA 496433-14 REV ORIGINAL.

Part: BELTFRAME — DAMAGED (FUSELAGE) · airframe 62,053 hrs · 47,415 cycles

LIGHTNING STRIKES ON LT WINDOW BELT FRAME FWD/AFT LOWER CORNER BTW STA 560 AND 579. LIGHTNING STRIKED WERE BLENDED OUT IAW DC9/MD88 SRM 53-05 FIG 111 SHEET 12 ZONE 2 AND REPAIRED IAW ERA 496433-14 REV ORIGINAL.

Part: BELTFRAME — DAMAGED (FUSELAGE) · airframe 62,053 hrs · 47,415 cycles

LIGHTNING STRIKES ON LT WINDOW BELT FRAME FWD LOWER CORNER, AFT CORNER AND AFT SECTION BTW STA 541 AND 560. LIGHTNING STRIKES WERE BLENDED OUT IAW DC9/MD88 SRM 53-05 FIG 111 SHEET 2 ZONE 2 AND REPAIRED IAW ERA 496433-14 REV ORIGINAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,053 hrs · 47,415 cycles

TEMP REPAIR ON FUSELAGE SKIN STA Y=157 BETWEEN STRINGERS 3 AND 4 LT. EXISTING REPAIR REMOVED IAW DC9/MD88 SRM 51-30-5 AND 51-30-8. REPAIR PARTS WERE INSTALLED IAW DC9/MD88 AMR 0953931 REV 2 AND REPAIR ACCOMPLISHED IAW ERA 497038-14AD.

Part: BELTFRAME — DAMAGED (FUSELAGE) · airframe 62,053 hrs · 47,415 cycles

LIGHTNING STRIKES ON LT WINDOW BELT FRAME FWD/AFT SECTIONS BTW STA 598 AND 617. AREAS WERE BLENDED OUT IAW DC9/MD88 SRM 53-05 FIG 111 SHEET 12 ZONE 2 AND REPAIRED IAW ERA'S 497046-14 REV ORIG AND 496433-14 REV ORIG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 62,051 hrs · 47,414 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER STA Y=1209-1215 BTW PROJECTION LONG 27RT AND 28RT IN REF N/R T0222097. TRIPLER WAS REMOVED IAW DC9 MD88 SRM 51-30-5. NEW TRIPLER WAS FABRICATED, DRILLED, AND ADJUSTED IAW DC9 MD88 ERA 463600-14 REV B.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 62,051 hrs · 47,414 cycles

DURING HMV DRILLED HOLES AND ELONGATED SCREW HOLES WERE FOUND ON FWD CARGO COMPARTMENT LOWER DOORJAMB BEAM BETWEEN STA Y=370 TO Y=426 DUE TO PREVIOUS REPAIR DOUBLER AND DOORJAMB PAN REMOVAL C1 LOWER DOORJAMB BEAM WAS REPAIRED IAW ERA 497043-14 REV ORIGINAL.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 62,051 hrs · 47,414 cycles

DURING HMV CORROSION WAS FOUND ON APU DOOR SETTLEMENT AREA STA Y=1380 BTW LONGERON 24LT TO 24RT. THE 1380 FRAME WAS REPLACED BTW 24LT-24RT IAW ERA 496446-14 REV ORIG.

Part: SKIN — DENTED (FUSELAGE) · airframe 62,051 hrs · 47,414 cycles

DURING HMV PER SMS PERFORM PERMANENT REPAIR TO DENT 10 INCH AFT R1 DOOR ABOVE FLOOR LINE. REPAIRED PER ERA 496448-14 REV ORG AND AMR 0953949 REV 1.

Part: SKIN — UNKNOWN (FUSELAGE) · airframe 62,051 hrs · 47,414 cycles

DURING HMV FOUND TEMP REPAIR ON FUSELAGE SKIN STA Y=157 BTW LONGERON 3LT-4LT. WILL BE REPAIRED WITH A ERA.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,051 hrs · 47,414 cycles

CORROSION ON RT CUSP WEB UPPER LOWER SURFACE BTW X=-54 TO X=-60 FROM STA 389-408, 408-427, 427-446 AND 446-449. CUSP WEB WAS REPLACED IAW MD88 SRM 53-20-02D.

Part: SKIN — DAMAGED (RUDDER TAB) · airframe 62,051 hrs · 47,414 cycles

DURING HMV DAMAGE WAS FOUND ON THE ALUMINUM FLAME SPRAY ON RUDDER TAB SURFACE. REF MD88 SRM 51-70-1AD PARA 23 FOR REPAIR.

Part: DOOR FRAME — CORRODED (VENTRAL DOOR) · airframe 62,051 hrs · 47,414 cycles

DURING HMV CORROSION WAS FOUND ON LOWER SECTION OF AFT VENTRAL DOORJAMB STA Y=1350 BTW X=18 TO X=-18 AT. CORRODED AREA WAS CUT OUT AND FILLER AND DOUBLER WERE INSTALLED IAW ERA 496443-14.

Part: SKIN — CRACKED (BS 197) · airframe 62,051 hrs · 47,414 cycles

DURING HMV, TWO CRACKS WERE FOUND ON FUSELAGE SKIN AT STA 197 BETWEEN LONGERON 16-17 OF .125 INCH LENGTH AND ANOTHER BETWEEN LONGERON 12 AND 13 OF .093 INCH AT DOOR STOP. ADJUST HOLES OF THE FWD PASSENGER DOOR JAMB LT SIDE REPAIRED IAW SRM 53-05D FIG 114.

Part: SKIN — CORRODED (BS 745-755) · airframe 62,051 hrs · 47,414 cycles

DURING HMV, SWOLLEN FUSELAGE SKIN WAS FOUND AT LONGERON 30 BETWEEN BS 745-755 REPAIRED IAW SRM 53-04D FIG 53.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,051 hrs · 47,414 cycles

DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN BETWEEN STA Y=750-769 LONGERON 28R-27 AND Y=769-788 LONGERON 30-29L AT MID CARGO COMPARTMENT SKIN WAS BLENDED AND WITHIN LIMITS REF MD88 SRM 53-04D FIG 53 AT STA Y=769-788 LONGERON 30-29L. CORROSION ON FUSELAGE SKIN STA Y=750-769 LONGERON 28R-27 WILL BE ATTENDED WITH ON NRCTO 222135. SDR REF REPORTING REQUIREMENTS TABLE.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,051 hrs · 47,414 cycles

DURING HMV DAMAGE PAINT COAT AND MISSING METALIZED PROTECTION WAS FOUND ON RUDDER SKIN LT/RT SIDE. RUDDER SKIN WAS REPAIRED IAW MD88 SRM 51-70-1AD PARA 23.

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,051 hrs · 47,414 cycles

DURING HMV A CRACK WAS FOUND ON THE PAN ON AFT EDGE BELOW STOP FITTING NR 4 AT AFT CARGO COMPARTMENT DOOR CRACK IN PAN WAS STOP DRILLED AND DOUBLER INSTALLED IAW MD88 SRM 52-05D FIG 50.

Part: SKIN — DENTED (ELEVATOR TAB) · airframe 62,051 hrs · 47,414 cycles

DURING HMV DENTS WERE FOUND ON RT ELEVATOR CONTROL TAB UPPER AND LOWER SKIN TAB WAS REPAIRED IAW MD88 SRM 55-04 PARA 2A AND 3A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,051 hrs · 47,414 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN AREA UNDER RUBSTRIPS FROM STA Y=1000-1134 BETWEEN LONGERON 18LT-18LT REF MD88 SRM 53-04 FIG 53 FOR REPAIR.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,051 hrs · 47,414 cycles

DURING HMV CORROSION WAS FOUND ON CUSP ANGLE BTW STA 176-206 BTW X-55 TO X-60 AT CABIN FLOOR STRUCTURE REF MD88 SRM 53-05 FIG 55 FOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,051 hrs · 47,414 cycles

DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN BETWEEN STA Y=788-792 BETWEEN LONGERON 29RT TO 29LT AT MID CARGO COMPARTMENT. SKIN WAS REPAIRED BY BLEND OUT AND WITHIN LIMITS PER MD88 SRM 53-04D FIG 53 PARA 27 SDR RECORDABLE REF REPORTING REQUIREMENTS TABLE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,051 hrs · 47,414 cycles

DURING HMV A CRACK WAS FOUND ON FUSELAGE SKIN AT STA Y=1436 BETWEEN LONGERON 3RT AND 4RT DAMAGE SKIN WAS CUT OUT AND DOUBLER INSTALL IAW MD88 SRM 53-04D FIG 27.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,051 hrs · 47,414 cycles

DURING HMV CORROSION WAS FOUND ON INNER SKIN X=60 Z=0 TO Z=-5 BETWEEN STA Y=878 TO 883 AT WING BOX AREA SKIN WAS BLENDED AND WITHIN LIMITS PER MD88 SRM 53-04D FIG 53 AND SDR RECORDABLE PER REPORTING REQUIREMENTS TABLE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,051 hrs · 47,414 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN AREA UNDER RUBSTRIPS AT STA Y=725-824 BETWEEN LONGERON 21RH-30 AND AT STA Y=769-824 BETWEEN LONGERON 30-27 LT. SKIN WAS REPAIRED BY BLENDING AND WAS WITHIN LIMITS PER MD88 SRM 53-04 FIG 53 SDR RECORDABLE REF REPORTING REQUIREMENTS TABLE.

Part: CUSP WEB — CORRODED (BS 1155-1250) · airframe 62,051 hrs · 47,414 cycles

DURING HMV, CORROSION WAS FOUND ON RT CUSP WEB X=-54 TO X=-60 BETWEEN BS 1155-1250. REPAIRED IAW SRM 53-20-02.

Part: PAN — CORRODED (CARGO DOOR FRAME) · airframe 62,051 hrs · 47,414 cycles

DURING HMV A BULGING PREVIOUS REPAIR WAS FOUND ON "Z" DOUBLER AT FWD CARGO COMPARTMENT LWR DOOR JAMB PAN BETWEEN STA 368-376 AND 405-412 C1 REPAIRED IAW SRM 53-05 FIG 44.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 62,051 hrs · 47,414 cycles

CRACK FOUND IN LOWER AFT CORNER FWD ENTRY DOOR. REPAIRED IAW ERA 494767-14

Part: TAB — DAMAGED (ELEVATOR) · airframe 62,051 hrs · 47,414 cycles

DURING HMV LIGHTNING STRIKE WAS FOUND ON LT ELEVATOR CONTROL TAB TRAILING EDGE TAB WAS REPAIRED IAW MD88 SRM 55-04 PARA 3A.

Part: BEAM — CORRODED (CARGO DOOR FRAME) · airframe 62,051 hrs · 47,414 cycles

DURING HMV, CORROSION WAS FOUND ON MID CARGO COMPARTMENT DOORJAMB LOWER BEAM BS 636-693 AND ON LOWER BEAM PREVIOUS REPAIR STRAP BETWEEN STA Y=640-650 REF MD88 SRM 53-05D FIG 123 FOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,051 hrs · 47,414 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN AREA UNDER RUBSTRIPS FRON STA Y=1003-1134 BETWEEN LONGERON 18RT-28RT REF MD88 SRM 53-04 FIG 53 FOR REPAIR.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,051 hrs · 47,414 cycles

CORROSION ON CUSP ANGLE BETWEEN STA Y=176 - 206 BTW X=-55 TO X=-60 AT CABIN FLOOR STRUCTURE. CUSP ANGLE WAS REPLACED IAW DC9/MD88 SRM 53-05,FIG 55.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,698 hrs · 47,191 cycles

ON WALK AROUND FOUND CRACK AT FWD AIR STAIR CUTOUT FWD OF STA 200 ABOVE STRINGER L22. CRACK REPAIRED ON N/R 1 REF ERA 494767-14 REV ORIG.

Part: LANYARD — DISCONNECTED (EVAC SLIDE) · airframe 61,598 hrs · 47,127 cycles

CREW FOUND L2 GIRT BAR LANYARD DISCONNECTED. CONTRACT MAINTENANCE RE-INSTALLED LANYARD PER AMM 25-62-00-201 ON L2 DOOR. DOOR OK FOR SERVICE.

Part: LANYARD — MISROUTED (TAILCONE) · airframe 61,375 hrs · 46,965 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,641 hrs · 46,486 cycles

FLIGHT CREW FOUND GALLEY 1A EMERGENCY PATHWAY LIGHTS INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT ASSEMBLY PER MAINTENANCE MANUAL. OPERATIONALLY CHECKS GOOD AND THE AIRCRAFT IS NOW OKAY FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 59,665 hrs · 45,807 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHTS AT ROW 2DE INOPERATIVE. MX REPAIRED BROKEN WIRE AT ROW 25DE IAW SWPM CHAP 20. OPS OF LIGHTS NOW CHECKS OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,136 hrs · 45,439 cycles

ON LAYOVER, MAINTENANCE FOUND THE LEFT AND RIGHT FORWARD OVERWING EXIT EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AT THE BATTERY PACK. AN OPS CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (DLM88101798).

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,136 hrs · 45,439 cycles

ON LAYOVER FOUND LEFT AND RIGHT FWD OVERWING EXIT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERIES AT BATTERY PACK. OPS CHECKS GOOD (DLM88101784).

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,739 hrs · 44,588 cycles

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

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 56,017 hrs · 43,406 cycles

LT HORIZONTAL STABILIZER REAR SPAR UPPER CAP CRACKED AT LOWER FASTENER HOLE SUBJECT TO INSPECTIONS PER S/B MD80-55A065 AND AD 2007-10-04. REAR SPAR CAP REPLACED IN ACCORDANCE WITH ERA 474061-14AD.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 53,019 hrs · 41,442 cycles

ELECTRICAL ODOR IN CABIN. REPLACED COFFEEMAKER, RAN A/C FOR SEVERAL HOURS. NO OTHER ODORS NOTED.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 52,708 hrs · 41,233 cycles

MISSING TAB ON REPLACEMENT LT LOWER AFT SKIN PANEL ON HORIZ STAB. INSTALLED REPAIR DOUBLER.

Part: SKIN — DENTED (FS 1211 L28R) · airframe 52,078 hrs · 40,782 cycles

AIRCRAFT STRUCK BY GROUND EQUIPMENT AT C-3 DOOR CUTOUT. LOWER SKIN AND DOUBLERS DENTED. DAMAGE CUTOUT AND DOUBLERS INSTALLED

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,072 hrs · 40,099 cycles

FWD O/WING EXITS INT EXIT SIGNS LIGHTS INOP. REPLACED BATTERIES IN CHARGER PACK.

Part: ODOR — DETECTED (CABIN) · airframe 48,717 hrs · 38,549 cycles

BURNT POPCORN SMELL MID CABIN SOMETIMES WORSE WHEN CABIN COLD, BETTER WHEN WARM. INSPECTED MID CABIN, NO UNUSUAL SMELL OR PROBLEMS FOUND.

Part: ENGINE — LEAKING (NR 2) · airframe 46,023 hrs · 36,590 cycles

ON CLIMB JUST AFTER TAKEOFF BOTH AFT LAV SMOKE DETECTORS SOUNDED FOLLOWED BY VISIBLE SMOKE IN THE CABIN. REPLACED RT ENGINE FOR INTERNAL OIL LEAKAGE.

Part: GEARBOX — MALFUNCTIONED (STAB TRIM) · airframe 45,867 hrs · 36,474 cycles

PRIMARY TRIM NOSE DOWN WOULD NOT WORK ON CLIMBOUT. ALT TRIM FUNCTIONED PROPERLY. REPLACED GEARBOX AND TRIM MOTORS.

Part: VALVE — FAILED (NR 1 ENGINE) · airframe 44,546 hrs · 35,517 cycles

LEFT ENGINE WOULD NOT ACCELERATE ABOVE 60 PERCENT N2 ON TAKEOFF ROLL. REPLACED PD VALVE.

Part: SENSOR — LOOSE (EMPENNAGE) · airframe 41,203 hrs · 33,248 cycles

TAIL TEMP HIGH MESSAGE DURING CLIMBOUT. FOUND CLAMP LEAKING FROM LT PRESSURE REGULATOR VALVE AND SECURED BOTH CLAMPS. REPLACED BOTH TEMP COMPT. OVERHEAT SENSORS FOR PRECAUTION PERFORMED GROUND CHECK AT NORMAL T/O PER PFHB 9-0-7-7 TEST B-TAIL HIGH TEMP LIGHT DID NOT ILLUMINATE. TESTS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,951 hrs · 33,070 cycles

EMERGENCY LIGHTS INOP LAST 8 ROWS. REPLACED POWER SUPPLY.

Part: POWER SUPPLY — INOPERATIVE (AFT CABIN) · airframe 40,872 hrs · 33,013 cycles

AFT SECTION EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY.

Part: ODOR — DETECTED (CABIN) · airframe 37,292 hrs · 30,512 cycles

ON APPROACH INTO DAB RT AFT LAVATORY SMOKE DETECTOR SOUNDED WITH A HOT BURNING SMELL IN CABIN. UNABLE TO DUPLICATE. PERFORMED DUCT BURNOUT AS PRECAUTION.

Part: SENSOR — MALFUNCTIONED (NLG) · airframe 37,228 hrs · 30,470 cycles

NOSE GEAR UNSAFE LIGHT CAME ON AFTER T/O. LIGHT WENT OUT AFTER AUX PUMPS TURNED ON. REPLACED D-132 LOCK SENSOR PER M/M. SWUNG GEAR SEVERAL TIMES, OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,699 hrs · 30,093 cycles

PAX SEAT 37DE EMERGENCY LIGHT INOP ON MTC TEST. REPLACED LIGHT ASSY, NOW TESTS NORMAL.

Part: SKIN — DENTED (BS 237)

A DENT WAS FOUND AT FS 237 AT LONGERON 17L. THE DAMAGE WAS REPAIRED PER ERA 333751-14 AT HMV.

Part: SKIN — DENTED (BS 237)

THE FUSELAGE SKIN WAS FOUND DENTED AT FS 237 AND STRINGER 17L. THE DAMAGE WAS REPAIRED PER ERA 333751-14 AT HMV.

Part: SKIN — DENTED (BS 213-229)

DENTS WERE FOUND IN THE FUSELAGE SKIN BETWEEN FS 213 AND 229 AND BETWEEN STRINGERS 16L AND 17L. THE DAMAGE WAS CUT OUT AND REPAIRED PER ERA 333730-14.

Part: TIRE — FAILED (NR 1 MLG)

ON ROTATION, NR 1 MAIN TIRE RECAP SEPARATED AND FODED OUT THE NR 1 ENGINE. REPLACED TIRE AND ENGINE.

Part: VALVE — STICKING (RT PACK)

DURING CLIMB AND INITIAL CRUISE, THE RIGHT PACK COULD NOT KEEP A/C COOL (LT PACK MEL INOP). CABIN SUPPLY TEMP WAS 108 DEG AND CABIN TEMP WAS 90 DEG. RAN PACK IN BOTH AUTO AND MANUAL. FOUND RIGHT FLOW CONTROL VALVE NOT OPENING ALL THE WAY. REPLACED VALVE.

Part: FILTER — LEAKING (RT HYD SYS)

ATB-RT HYD SYS LOW IN FLT. REPLACED RT HYD SYS ENGINE PRESSURE FILTER ASSY.

Part: WIRE — LOOSE (ROW 31)

EMERGENCY PATH LIGHTING INOP FROM ROW 31 AFT. REPAIRED WIRES.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHTS INOP ROW 29 AFT INOP. REPLACED POWER SUPPLY.

Part: COFFEEMAKER — FAILED (GALLEY)

DURING FLT, AFT GALLEY COFFEEMAKER STARTED TO SMOKE. REPLACED COFFEEMAKER.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON SVC CK, FOUND AFT SECTION OF EMERG TRACK LIGHTS INOP. REPLACED BATTERY PACK.

Part: WATER HEATER — OVER HEATED (AFT LAVATORY)

SMOKE DETECTOR IN RIGHT AFT LAV WENT OFF ON SHORT FINAL. PULLED ALL LAV C/B. CREW AND PASSENGERS REPORTED ELECTRICAL SMELL. C/B WAS PULLED FOR WATER HEATER AND ALARM STOPPED. INSPECTED AREA, FOUND OK. FORWARD WATER HEATER TO MCO/PLAC PER MEL 25-00-12 C/B CLAMPED.

Part: PACK — MALFUNCTIONED (CABIN)

ACRID BURNING SMELL IN A/C WITH AIRFOIL ANTI-ICE PROTECTION IN OPERATION. SET OFF ALL LAV SMOKE DETECTORS. OPERATED AIRFOIL ANTI-ICE SYSTEM, NO ODOR NOTED. RIGHT PACK EMITS ODOR. FWD TO MCO/PLAC. RIGHT PACK INOP.

Part: COALESCER — CONTAMINATED (CABIN)

OFFENSIVE FUMES COMING FROM AIR CONDITIONING PACKS FOLLOWING REPAIR OF HYDRAULIC LEAK. REPLACED COALESCER BAGS.

Part: STRUT — REQD SERVICE (NLG)

AFTER DEPARTURE AND GEAR RETRACTION NOSE GEAR INDICATION UNSAFE DID POM PROCEDURE STILL SHOWED UNSAFE HYD PRESS AND QTY NORMAL. INSP STRUT BUSHING AND PROX S/W SVC NOSE STRUT PER/M/ CHP 32 SWUNG NOSE GEAR SEVERALS TIMES, ALL INDICATION CHECKED GOOD.

Part: OVERFLOW CAN — OVERFLOWING (HYD SYST)

ON APPROACH WITH ENGINE ANTI-ICE ON, AFT SMOKE DETECTORS WENT OFF AND THERE WAS SMOKE IN THE CABIN. REPLACED WATER SEPARATOR BAGS AND LEAK CHECK OK. CHECKED ACM OIL, FOUND OK. FOUND HYD OVERFLOW CAN OVERFLOWING, EMPTIED SAME AND RAN ENGINES PACKS ANTI-ICE, APU COULD NOT DUPLICATE.

Part: SKIN — GOUGED (MAIN ENTRY DOOR)

FOUND DURING A-2 LETTER CHECK, MAIN ENTRY DOOR OUTER SKIN GOUGED AT HOOK BOX CUTOUT. REPAIRED PER SRM 52-05 FIG 20A.