N930DL

Part: SKIN — DAMAGED · airframe 72,935 hrs · 55,466 cycles

STRUCTURAL DAMAGE ON RIGHT SIDE, FWD OF FWD CARGO DOOR. REPAIR ACCOMPLISHED PER ERA 553592-14 REV ORIG AND ERA 553600-14.

Part: SKIN — DAMAGED (BS 218) · airframe 72,935 hrs · 55,466 cycles

SKIN DAMAGED AT LONGERON 25R BS 218. REPAIR ACCOMPLISHED IAW ER/A#553592-14, REV. 1 AND ER/A 553592-14.

Part: BULKHEAD — DAMAGED (BS 218) · airframe 72,935 hrs · 55,466 cycles

FORWARD CARGO BULKHEAD DAMAGED BETWEEN LONGERON 24 AND 25R AT BS 218. FABRICATED AND INSTALLED STRUT AND BULKHEAD IAW DWG 9951888 AND SRM 51-01, PG. 1.

Part: BEAM — GOUGED (NLG WW) · airframe 72,935 hrs · 55,466 cycles

NLG LEFT NOSE WHEEL WELL BEAM WEB GOUGED AND INDENTED BELOW BEAM. REPAIRED IAW ER/A #553598-14, REV. ORIGINAL AND ER/A 553598-14.

Part: SKIN — DAMAGED (BS 229) · airframe 72,935 hrs · 55,466 cycles

PRODUCTION SPLICE DAMAGED AT BS 229 BETWEEN LONGERONS 23 AND 25 RIGHT. REPAIRED IAW ER/A 553600-14, REV. O AND ER/A 553600-14.

Part: LONGERON — DAMAGED (BS 218) · airframe 72,917 hrs · 55,455 cycles

LONGERON 25R DAMAGED AT BS 218. REPAIRED IAW PRI 553592-14REV 1 AND SRM 53-02 FIG 18.

Part: LONGERON — DAMAGED (BS 218) · airframe 72,917 hrs · 55,455 cycles

LONGERON 24R DAMAGED AT BS 218. REPAIRED IAW PRI 553592-14 REV 0 AND SRM 53-02 FIG 18.

Part: LONGERON — DAMAGED (BS 218) · airframe 72,917 hrs · 55,455 cycles

LONGERON 24R DAMAGED AT BS 218. REPAIRED IAW SRM 53-02 FIG 18 AND PRI 553592-14 REV.0.

Part: FRAME — DAMAGED (BS 218) · airframe 72,917 hrs · 55,455 cycles

FRAME DAMAGED AT BS 218 BETWEEN LONGERONS 23 - 25R. INSTALLED A FRAME REPAIR SPLICE IAW SRM 53-03D FIG 2A.

Part: LONGERON — CRACKED (BS 218) · airframe 72,917 hrs · 55,455 cycles

CRACKED LONGERON 23, BS 218. REPAIRED IAW PRI 553592-14 REV 0 AND SRM 53-02 FIG. 18.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,853 hrs · 55,403 cycles

EEPL SEAT LIGHT INOP AT SEAT 21 D/E. RMVD & RPLCD EEPL LIGHT ASSY AT SEAT 21D/E. OPS CK GOOD.

Part: SCOOP — CRACKED (E&E EXHAUST) · airframe 70,158 hrs · 53,388 cycles

AVOINIC EXHAUST VENT SCOOP HAD THREE CRACKS. REMOVED SCOOP FOR WELD REPAIR IAW ER/A 464964-14MA. INSTALLED REPAIRED SCOOP.

Part: FRAME — CRACKED (BS 1485) · airframe 70,158 hrs · 53,388 cycles

TAIL INTERIOR - CANTED FRAME RT WEB IB EDGE HAS 1.2500" LONG CRACK AT HORIZONTAL "T" ANGLE, BS 1485, NEAR RUDDER TRIM CABLE DRUM. REPAIRED CANTED FRAME REF SRM 53-03D, FIG 49.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 70,115 hrs · 53,355 cycles

MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS FOR THE CENTER CATWALK HAD A BROKEN WIRE AND WAS INOPERATIVE. MAINTENANCE REPAIRED THE WIRE CONNECTOR FOR THE NOTED LIGHTED AREA AND AN OPS CHECK WAS GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,082 hrs · 52,638 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTS IN ROWS 1-12 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED A FAILED FUSE AT THE POWER SUPPLY AND REPOSITIONED SOME WIRES. THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. LP 6444926.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,900 hrs · 51,840 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS AT ROWS 12 & 29 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND THE OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,688 hrs · 51,683 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 19D & 35D OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,897 hrs · 51,103 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: STRUCTURE — DAMAGED (RT WING) · airframe 65,818 hrs · 50,346 cycles

DURING LIGHTNING STRIKE INSPECTION, NOTED DAMAGE AT RT WING STA 555 T/E. BLENDED REPAIR BEYOND SRM LIMITS. REPAIRED IAW ER/A 521853-14.

Part: SKIN — DAMAGED (RT WING) · airframe 65,818 hrs · 50,346 cycles

DURING LIGHTNING STRIKE INSPECTION, NOTED DAMAGE RT WING STA 62 AT THE T/E. BLENDED DAMAGE WAS BEYOND LIMITS. REPAIRED IAW SRM 51-70-6, PAR D2.

Part: RELEASE CABLE — DAMAGED (TAILCONE) · airframe 65,374 hrs · 50,031 cycles

DURING SCHEDULED CHECK, THE TAIL CONE RELEASE CABLE HAS SPIRAL COATING THAT IS PEELING AND WAS PREVENTING SMOOTH CABLE OPERATION. REPLACED RELEASE CABLE IAW AMM 53-53 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: COVER — DAMAGED (ESCAPE SLIDE) · airframe 65,374 hrs · 50,031 cycles

DURING SCHEDULED CHECK, THE TAIL CONE SLIDE COVER WAS FOUND TO BE SATURATED WITH HYD FLUID AND THE VELCRO WAS MISSING. THE TAIL CONE SLIDE COVER WAS REPLACED IAW AMDS WC 2500-4484 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: RETAINER — CORRODED (TAILCONE RELEASE) · airframe 65,374 hrs · 50,031 cycles

DURING SCHEDULED CHECK IN MSP, THE TAIL CONE TEE PIN RETAINING CLIPS WERE FOUND TO BE RUSTY AT THE TEE PIN MOUNT CLIPS. REPLACED TEE PIN RETAINING CLIPS IAW AMM 53-53. THE REQUIRED INSPECTION WAS COMPLETED.

Part: BUSHING — WORN (TAILCONE PIN) · airframe 65,374 hrs · 50,031 cycles

DURING SCHEDULED CHECK IN MSP, THE TAIL CONE TEE PIN BUSHINGS AND HARDWARE WERE FOUND TO BE WORN. REPLACED TEE PIN BUSHINGS AND HARDWARE IAW AMM 53-53 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: CAM — WORN (TAILCONE) · airframe 65,374 hrs · 50,031 cycles

DURING SCHEDULED CHECK, THE TAIL CONE RELEASE CAM BASE WAS FOUND TO BE WORN. REPLACED TAILCONE CAM BASE IAW AMM 53-53 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: RELEASE CABLE — DAMAGED (TAILCONE RELEASE) · airframe 65,374 hrs · 50,031 cycles

DURING SCHEDULED CHECK IN MSP, THE TAIL CONE RELEASE CABLE LOWER CONDUIT WAS FOUND TO BE IN POOR CONDITION. REPLACED LOWER CONDUIT IAW AMM 53-53 AND COMPLETED THE REQUIRED INSPECTION.

Part: ATTACH ANGLE — CRACKED (TAILCONE) · airframe 65,374 hrs · 50,031 cycles

TAIL CONE LT UPPER LATCH RECEPTICAL UPPER ATTACH ANGLE IS CRACKED. INSTALLED NEW BRACKET IAW SRM 51-30. THE REQUIRED INSPECTION WAS COMPLETED.

Part: TAIL CONE — OUT OF RIG · airframe 65,374 hrs · 50,031 cycles

DURING TAILCONE CHECK, FOUND TOP OF DOOR STOP DOES NOT CLEAR ARM ASSY BY .2500 IN, REQUIRES SHIMS IAW AMDS 5350-01077-0101, STEP 1. INSTALLED SHIMS AND RIGGED ARM ASSY IAW AMDS 5350-01077-0101 STEP 1 (E). THE REQUIRED INSPECTION WAS COMPLETED.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 65,374 hrs · 50,031 cycles

MX DISCOVERED THAT THE TAILCONE EMERGENCY RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS ON THE END AND AT THE CAM. THE CABLE WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: BRACKET — DAMAGED (TAILCONE RELEASE) · airframe 65,374 hrs · 50,031 cycles

MX DISCOVERED THAT THE EMERGENCY ESCAPE PATH TAILCONE RELEASE CABLE SPRING MOUNT BRACKETS HAD MISSING HARDWARE. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYSTEM AND COULD HAVE AN ADVERSE AFFECT ON THE EVACUATION ROUTE IF IT PREVENTED PROPER DEPLOYMENT OF THE TAILCONE. THIS NOT IN COMPLIANCE WITH 14 CFR, PART 121.703. THE SPACER AND BOLT WERE REPLACED, ADJUSTED, AND THE RII WAS SATISFACTORY.

Part: RECEPTACLE — WORN (TAILCONE) · airframe 65,374 hrs · 50,031 cycles

MX DISCOVERED THAT BOTH THE LT AND RT UPPER RELEASE LATCH RECEPTACLES FOR THE TAILCONE WERE WORN OUT OF ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: RELEASE CABLE — MISROUTED (TAILCONE) · airframe 65,374 hrs · 50,031 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE CABLE WAS MISROUTED. THIS IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE CABLE ROUTING WAS CORRECTED PER THE MM.

Part: SKIN — CRACKED (BS 1380) · airframe 65,374 hrs · 50,031 cycles

DURING SCHEDULED INSPECTION, FUSELAGE SKIN CRACKS WERE FOUND AT TWO FASTENER HOLES AT BS 1380 ABOVE L14R. REPAIRED IAW ER/A 519602-14.

Part: DOOR FRAME — CRACKED (MLG WW) · airframe 65,181 hrs · 49,883 cycles

FOUND LT WHEEL WELL DOOR JAMB FWD CRACKED. REPAIR IAW ER/A 497265-14MA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,164 hrs · 49,868 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 11-13 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AT ROW 12 AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: CATWALK — STUCK · airframe 65,008 hrs · 49,758 cycles

F/A REPORTED A LOUD BANGING NOISE BELOW THE ACFT WHILE SEATED ON THE AFT JUMPSEAT. IT WAS DISCOVERED THAT THE CATWALK HAD REMAINED STUCK IN THE UP POSITION -BLOCKING THE EMERGENCY ESCAPE PATH. MX FOUND THE REMOVABLE CEILING PANEL OUT OF ADJUSTMENT AND RESTRICTING THE CATWALK FROM RETURNING TO THE "EXIT PATH" POSITION. THE CEILING PANEL WAS ADJUSTED AND A FUNCTIONAL CHECK PROVED THE CATWALK MOVED FREELY.

Part: PULLEY — BROKEN (CABLE) · airframe 64,293 hrs · 49,222 cycles

MX DISCOVERED THAT THE RETRACT CABLE FOR THE CATWALK IN TAIL SECTION, WAS BROKEN. CATWALK WILL NOT COME UP WHEN THE AIRSTAIRS GO DOWN. THE SYS WAS FORWARDED AND PLACARD PROCEDURES WERE COMPLIED WITH. THE STAIRS WERE IDENTIFIED AS INOPERATIVE. ON 07MAY, THE LOWER CABLE PULLEY WAS FOUND TO BE BROKEN. ON 09MAY, THE PULLEY ASSY AND THE CABLE WERE BOTH REPLACED AND THE AFT WAS RETURNED TO SERVICE.

Part: CABLE — BROKEN (TAILCONE) · airframe 64,147 hrs · 49,120 cycles

MX DISCOVERED THAT THE TAILCONE CATWALK RT CABLE WAS BROKEN. THE CABLE WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS.

Part: SKIN — CRACKED (BS 1212) · airframe 71,269 hrs · 54,192 cycles

A 0.031 LONG CRACK WAS FOUND ON FUSELAGE SKIN APPROXIMATELY AT BS 1212, BETWEEN LONGERONS L1 AND L2 LT. THIS ER/A ADDED FOR REPAIR. AMOC RESTRICTION, REPAIR APPROVAL IS LIMITED TO 51466 TOTAL FLIGHT CYCLES ASSOCIATED ER/A 00-501103, ADDED FOR AC 0930. ER/A 501103-14AD, REV B. THIS LP FOR AMOC RESTRICTION IS TERMINATED. AMOC APPROVAL WAS OBTAINED AND INCORPORATED AT REV B, PLEASE TERMINATE THIS LP. CLOSED LOG AND REMOVED MONITOR INSPECTION IAW ALERT 03OCT13.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,969 hrs · 48,993 cycles

DURING OVERNIGHT MX, THE OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS WERE FOUND TO BE INOPERATIVE. BATTERIES WERE REPLACED IAW AMM 33-50 AND OPERATION CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,447 hrs · 48,604 cycles

DURING LINE CHECK, MX FOUND THAT THE UPPER EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: FUEL TANK — LEAKING (RT WING) · airframe 62,968 hrs · 48,233 cycles

CREW DIVERTED THE ACFT TO PIT DUE TO A REPORTED RT WING TANK FUEL LEAK. THE RIGHT TANK DECREASED TO 1200 LBS LESS THAN THE LEFT TANK. BOTH SIDES WERE BALANCED TO EQUAL LEVELS AND THEN THE RIGHT SIDE DECREASED AGAIN. AT THIS POINT THE QRH WAS COMPLIED WITH AND THE RIGHT ENGINE WAS SHUTDOWN. THE FLIGHT THEN DIVERTED TO THE NEAREST SUITABLE AIRPORT AND LANDED WITHOUT FURTHER INCIDENT. MX VERIFIED THAT ALL FUEL QUANTITY INDICATORS WERE FUNCTIONING PROPERLY, THAT THE ARRIVAL FUEL WAS 1200 LBS LESS THAN PLANNED, AND THAT ALL TRANSFER AND CROSSFEED SYSTEMS FUNCTIONED PROPERLY. A LEAK WAS FOUND ON THE UPPER WING AND WAS RE-SEALED.

Part: SKIN — GOUGED (BS 1212 S29-30R) · airframe 62,367 hrs · 47,788 cycles

FUSELAGE GOUGING AFT SECTION OF SCUFF PLATE AND CARGO DOOR DOUBLER APPROX AT STA 121 STR 29R AND 30R. REPAIRED ON ERA 505558-14 REV ORIG REF NRC 5.

Part: WEB — DAMAGED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV AN ELONGATED HOLE WAS FOUND OUT OF LIMITS. IAW SRM PROCEDURES EDGE DISTANCE BTW BLIND NUT AND FASTENER AT STA Y=428 AND BTW PROJECTION OF LONGERON 27R AND 28R AT FWD CARGO COMPARTMENT ELONGATED HOLE WAS REPAIRED IAW ERA 502175-14 REV ORIG.

Part: BELTFRAME — DAMAGED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

WINDOW BELT FRAME WAS REPAIRED IAW ER/A 501110-14 REV ORIG (REFER TO MRR #122287 ON 14APR12).

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV A CRACK WAS FOUND ON FUSELAGE SKIN OF 0.750" BTW LONGERON 1 AND 2 LT AT STATION Y=1418, A CRACK WAS FOUND ON INTERNAL ANGLE OF 0.718" BTW LONGERON 1 AND 2 LT AT STATION Y=1429, A CRACK WAS FOUND FUSELAGE SKIN OF 2.031" BTW LONGERON 1 AND 2 RT AT STA Y=1418, THREE CRACKS WERE FOUND ON INTERNAL ANGLE OF 1",1.046"AND 0.75" BTW LONG 1 AND 2 RT AT STA Y=1418, TWO CRACKS ON INTERNAL ANGLE OF 1"AND 1.406" BTW LONG 1 AND 2 RT AT STA Y=1422 AND A CRACK ON INTERNAL ANGLE OF 2.343" BTW LONG 1 AND 2 RT AT STA Y=1429. ALL ABOVE WAS REPAIRED IAW ERA 501111-14 REV ORIG.

Part: BELTFRAME — DAMAGED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV SCRIBE LINE WAS FOUND ON LT WINDOW BELT FRAME STA Y=750-769 ON AFT UPPER CORNER WINDOW BELT FRAME WAS BLENDED OUT AND LEFT AS IS TIL 61,666 TOTAL CYCLES IAW ERA 501110-14 REV ORIG.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV A CRACKED WAS FOUND ON WEB AT STA Y=432 BTW LONGS 27RT AND 28RT AT FWD CARGO COMPARTMENT. DAMAGE WAS TRIMMED OUT AND FILL/DOUBLER INSTALLED IAW ERA 502175-14 REV ORIG.

Part: BEAM — CORRODED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

BEAM WAS REPAIRED IAW MD88 SRM 53-05 FIG 123.

Part: SKIN — CORRODED (RT WING) · airframe 61,749 hrs · 47,366 cycles

DURING HMV CORROSION WAS FOUND ON RIGHT MAIN FUEL ACCESS DOOR CUTOUT. DOOR CUTOUT REPAIRED IAW ERA 502172-14 REV ORIG.

Part: SKIN — CORRODED (LT WING) · airframe 61,749 hrs · 47,366 cycles

DURING HMV CORROSION WAS FOUND ON LEFT MAIN FUEL TANK ACCESS DOOR CUTOUT DOOR CUTOUT WERE CLEANED AND NO CORROSION FOUND. REPAIRED IAW ERA 502171-14 REV ORIG AND ERA 502172-14 REV ORIG.

Part: SKIN — DAMAGED (LT WING) · airframe 61,749 hrs · 47,366 cycles

DURING HMV TOOLING MARKS WERE FOUND ON LEFT MAIN FUEL TANK ACCESS DOOR CUT OUT NBR 1365C. DOOR CUT OUT REPAIR WILL BE ATTENDED WITH AN ERA. DAMAGE RIVET HOLES WERE STEP UP AND BUSHING INSTALLED IAW ERA 502171-14 REV ORIG.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 61,749 hrs · 47,366 cycles

DURING HMV, SUNKEN FASTENERS WAS FOUND ON VERTICAL STABILIZER LEADING EDGE SKIN TOW ROW OF FASTENERS BELOW THE SPLICE AT STA ZFS=52.2. VERTICAL STABILIZER SKIN WAS REPAIRED IAW EO 09-470871-12AD ME08 REV G AND DWG SG09550004 REV ORIG.

Part: SKIN — DENTED (BS 225 L17L) · airframe 61,749 hrs · 47,366 cycles

DENT ON SKIN BS 225 LONGERON 17LT. REPAIRED IAW ERA 501088-14 REV ORIG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

FUSELAGE SKIN DAMAGE WAS CUT OUT, FILLER, DOUBLERS INSTALLED IAW ERA 501108-14 REV ORIG.

Part: ANGLE — GOUGED (BS 1338 L24-26R) · airframe 61,749 hrs · 47,366 cycles

REPLACE SECTION OF TEE FROM LONGERON 22RT TO 26RT IAW SRM 53-03D FIG 37.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 61,749 hrs · 47,366 cycles

ELONGATED RIVET HOLES AND DRILL MARKS ON RT WING FUEL TANK ACCESS PLATE RUB STRIP SETTLEMENT AREA CUTOUT. REPAIRED PER AMR 09570436.

Part: SKIN — DAMAGED (LEFT WING) · airframe 61,749 hrs · 47,366 cycles

DAMAGE ON LEFT MAIN FUEL TANK ACCESS DOOR CUTOUT. REPAIRED PER AMR 09570436.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 61,749 hrs · 47,366 cycles

CORROSION AND DRILL MARKS ON RT WING FUEL TANK ACCESS PLATE RUB STRIP SETTLEMENT AREA CUTOUT NUMBER 1414C. REPAIRED PER AMR 09570436.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 61,749 hrs · 47,366 cycles

DAMAGE ON RT WING FUEL TANK ACCESS PLATES RUB STRIP SETTLEMENT AREA CUTOUT NUMBER 1436C. REPAIRED PER AMR 09570436.

Part: SKIN — DAMAGED (RUDDER) · airframe 61,749 hrs · 47,366 cycles

DURING HMV DAMAGE FLAME SPRAY WAS FOUND ON LT AND RT RUDDER SURFACE. LT AND RT RUDDER SURFACE WAS REPAIRED IAW MD-99 SRM51-70-1A, PARA 23.

Part: TEE FITTING — GOUGED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV A GOUGE WAS FOUND ON THE LOWER T P-DOME AT STA Y1338 BETWEEN LONGERON PROJECTION 24RT TO 26RT. REF MD-88 SRM 53-03 FIG 37 FOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=723-807 BETWEEN LONGERON 16LT TO30. REF MD-88 SRM 53-04D PARA 57 FOR REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV AN CRACK WAS FOUND OF 0.031" ON FUSELAGE SKIN AT STA Y=1212 AND BETWEEN LONGERON 1 AND 2LT. SKIN WILL BE REPAIRED ON A ERA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FAIRING STA Y=826-886,1000-1060 BETWEEN LONG 17L TO 19LT. REF MD-88 SRM 53-04D PARA 57 FOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=1060-1073 BETWEEN LONG 18LT-19LT,Y=1117 LONG 27LT AND Y=1098 BETWEEN 28LT TO 29LT. REF MD-88 SRM 53-04D PARA 57 FOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV CORROSION WAS FOUND ON FILLET PANEL RUBSTRIP FUSELAGE SKIN AT STA Y=738 AND Y=735 LONG 25RT REF MD-88 SRM 53-04D PARA 57 FOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV CORROSION WAS FOUND ON FILLET PANEL RUBSTRIP FUSELAGE SKIN FRON STA Y=864 TO 927 ALSO Y=927 TO 1003 LONG 18RT REF MD88 SRM 53-04D PARA 57 FOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV CORROSION WAS FOUND ON FILLET PANEL RUBSTRIP FUSELAGE SKIN FROM STA Y=1117 TO 1136 LONG 21RT TO 29RT REF MD88 SRM 53-04D PARA 57 FOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=812 TO 820 BTWEEN LONGS 30 AND 29RT. REF MD88 SRM 53-04D PARA 57 FOR REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV A CRACK WAS FOUND ON FUSELAGE SKIN OF 0.062" AT STA Y=374 UPPER FWD CORNER BTWEEN LONGERON 20 AND 21RT. REF MD- 88 SRM 53-05 FIG 105 FOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN OF FILLET PANEL AREA FROM STA Y=760 TO 769 BTWEEN LONGS 27R AND 28R ALSO STA Y=758 BTWEEN LONGS 27L AND 28L. REF MD88 SRM 53-04D PARA 57, FOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=823-826 BTWEEN LONGS 29LT AND 29RT REF MD88 SRM 53-04D PARA 57 FOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=812 TO 820 BTWEEN LONGS 30 TO 29LT. REF MD88 SRM 53-04D PARA 57 FOR REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

SCRATCHES AND LIGHTNING STRIKES AT LWR CORNER OF WINDOW BELT FRAME. REWORK ACCOMPLISHED STATED AS IAW ERA 51110-14 REV ORIG.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

SCRATCHES TO UPPER AFT CORNER OF LT WINDOW BELT. REPAIR BQ AND BR ACCOMLISHED IAW ERA 501110-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

SCRIBE LINES ON LT WINDOW BELT FRAME. REPAIR AA, AB, & AC ACCOMPLISHED IAW ER/A 501110-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

SCRIBE LINES ON LT WINDOW BELT FRAMES BTW STA Y=636-655, 655-674, 674-693, AND 693-712. REWORKED STATED AS AD, AH, AI, &AJ ACCOMPLISHED IAW ERA 501101-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

SCRIBE LINES LT WINDOW BELT. REPAIR ACCOMPLISHED IAW ER/A 501110-14 REV ORIG.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

SCRATCH TO LWR CORNER WINDOW BELT FRAME AT STA 1212 - 1231. REWORKED BELT FRAME IAW ERA 501110-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

SCRATCH AND LIGHTNING STRIKES TO CORNER OF RT WINDOW BELT FRAMES. REWORK STATED AS F WAS ACCOMPLISHED IAW ER/A 501101-14 REV ORIG AND ER/A 501110-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

SCRATCHES AND LIGHTNING STRIKES TO WINDOW BELT FRAME. REWORKS STATED AS B ACCOMLISHED IAW ER/A 501101-14 REV ORIG REWORKS STATED AS E AND V ACCOMPLISHED IAW ER/A 501110-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

SCRIBE LINES LT WINDOW BELT FRAME. REWORK BE & BD ACCOMPLISH IAW ER/A 501101-14 REV ORIG & 502220-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

SCRATCHES AND LIGHTNING STRIKES ON RT WINDOW BELT FRAMES. REWORKED AREAS IAW ERA 501110-14 REV ORIG.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

SCRATCH TO LT WINDOW BELT FRAME. REWORK BL ACCOMPLISHED IAW ER/A 501110-14 REV ORIG.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

SCRATCH LT WINDOW BELT FRAME. REWORK BM ACCOMPLISHED IAW ER/A 501110-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

SCRIBE LINE ON LOWER CORNER LT WINDOW BELT FRAME. REPAIR ACCOMPLISHED IAW BJ AND BK OF ERA 501110-14 REV ORIG.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

SCRATCHES TO RT WINDOW BELT FRAME. REPAIR ACCOMPLISHED IAW ER/A 502168-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

SCRIBE LINE LT WINDOW BELT FRAME. REWORK AV, AW, AS, AU, AX,AND AY WERE ALL ACCOMPLISHED IAW ERA 501110-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,749 hrs · 47,366 cycles

LIGHTNING STRIKES TO WINDOW BELT FRAME. REPAIR ACCOMPLISHED IAW ERA 502167-14 REV ORIG.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,202 hrs · 46,991 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 20 - 26 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (2011-D1388)

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,007 hrs · 46,873 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE AFT OVERWING EMERGENCY SIGN INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY BATTERIES. OPERATIONAL CHECK WAS GOOD.

Part: WIRE — DISCONNECTED (CABIN) · airframe 60,898 hrs · 46,796 cycles

FORWARD GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. FOUND FWD GALLEY RED EMERGENCY EXIT LIGHT WIRING NOT CONNECTED. REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD PER REF MD88 WDM 33-51 AND BOEING DC MODEL SWPM 20-31.

Part: WIRE — BROKEN (CABIN) · airframe 60,212 hrs · 46,304 cycles

DURING LINE CHECK MAINTENANCE FOUND BROKEN WIRE AT SEAT 2C EMERGENCY LIGHT CONNECTOR. MAINTENANCE RE-TERMINATED WIRE AT CONNECTOR. OPERATION OF LIGHT NOW CHECKS GOOD.

Part: SOCKET — BURNED (CABIN) · airframe 59,876 hrs · 46,066 cycles

CREW WROTE UP THAT SMOKE WAS DETECTED IN SEAT ROW 15 AT GATE. MAINTENANCE REPLACED BURNT OVERHEAD LIGHT SOCKET AT ROW 15D PER MD88 WSP 20-10-02. LIGHT NOW OPERATES NORMALLY. AIRCRAFT OK FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,793 hrs · 46,008 cycles

FUSELAGE SKIN STA 1437 BELOW LONGERON 3L. REPAIRED IAW ERA 492715-14.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 59,642 hrs · 45,894 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY PATHWAY LIGHT INOPERATIVE AT ROW 31DE. MX FOUND WIRE DAMAGED TO LIGHT ASSY. R & R SAME. OPERATION CHECKS GOOD.

Part: PIN — LOOSE (EMERGENCY LIGHT) · airframe 58,897 hrs · 45,434 cycles

DURING LINE CHECK, MX FOUND EMERGENCY PATH LIGHTS INOPERATIVE FROM ROWS 1 THRU 12 AND L1 AND R1 DOORS. MX TROUBLESHOT AND FOUND A LOOSE PIN IN THE SIDEWALL AT ROW 10. REPLACED PIN AT CONNECTOR. ALL CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,838 hrs · 44,710 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHT AT ROW 1CD TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY AT ROW 1CD. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (2010-D0928) ATL 423424 (DLM88101996).

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,900 hrs · 44,034 cycles

DURING EMERGENCY PATH LIGHTING OPS CHECK FOUND AFT OVERWING EXIT LIGHT INOP. REPLACED BATTERIES, OPS NORMAL.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 56,211 hrs · 43,603 cycles

VERT STAB L/E SKIN UPPER XFS-52 HOLE. REPAIRED IAW ERA 478349- 14.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 56,211 hrs · 43,603 cycles

VERTICAL STABILIZER FRONT SPAR CHORD BHEC CRACK INDICATION AT RT SIDE SECOND FASTENER ABOVE ZFS 52 REF EA 09-470871-12. REPAIRED PER ER/A 478340-14 ORIG.

Part: GASKET — BLOWN (PNEUMATIC SYS) · airframe 51,365 hrs · 40,408 cycles

TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED IN FLIGHT. FOUND RT PNEU LOW TEMP SENSOR GASKET BLOWEN, REPLACED SAME. ALSO FOUND BLOWN SPIDER DUCT, REPLACED SAME.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 48,195 hrs · 38,286 cycles

ON TAKEOFF, OIL SMELL IN COCKPIT DISSIPATED QUICKLY ON APPROACH OIL SMELL IN CABIN AFT SMOKE DETECTORS SOUNDING. MAINTENANCE IN PROGRESS TROUBLSHOOTING FUMES IN CABIN. C/W OPN 5088 CABIN SMOKE T/S AND C/W OPN 5089 PNEU DUCT BURNOUT CKS GOOD. NO MORE SMELL NOTED.

Part: FRAME — WORN (BS 1418 S15R)

FOUND WORN AREA ON FRAME AT FS 1418 ABOVE LONGERON 15 RIGHT. REPAIRED BY FABRICATING AND INSTALLING REPAIR ANGLE 16" X 1.10" AND 3.10" X 1.6 FROM 7075-T6 .050 AND FRAME FLANGE REPAIR 11.5" X 1.80 FROM 7075-T6 .063 IAW DC-9/MD-80 53-03D PG 5 FIG 4, AND 51-30-5.

Part: LONGERON — CORRODED (BS 1307-1322) · corrosion level 2

CORROSION ON LONGERON 30 BETWEEN FS 1307 AND FS 1322. FABRICATED AND INSTALLED U-CHANNEL 13.5" X .750" X 6.25" FROM 7075-T6 063 IAW DC-9/MD-80 SRM 53-02D, FIG 19, 51-10-3D AND 51-30-5.

Part: STRINGER — CORRODED (BS 1307 S29L) · corrosion level 2

FOUND CORROSION ON FRAME TIE AT FS 1307 S-29L TO S-29R. REPAIRED BY FABRICATING AND INSTALLING FORMER REPAIR 13.75" X 1.875" FROM 7075-T6 .050 AND FORMER SPLICE 3.5" X 1" FROM 7075-T6 DC-9/MD-80 SRM 53-03D, 51-10-3D AND 51-30-2.

Part: STRINGER — CORRODED (BS 1287 S22L) · corrosion level 2

FOUND CORROSION ON STRINGER 22 LT IN AFT BAGGAGE PIT. REPAIRED BY FABRICATING AND INSTALLING NEW SECTION LONGERON 18.75" X 3" X .75" FROM 1242886 7075 T6, 626520 EXTRUSION AND 2 EACH SPLICES P/N 3914677-501N IAW DC-9/MD-80 53-02 PG 45 & 46 AND 53-02 FIG 15.

Part: CARGO TRACK — CORRODED (BS 1136-1261) · corrosion level 2

FOUND CORROSION ON LEFT CARGO TRACK FROM FS 1136 TO FS 1231 (AFT PIT). REPAIRED BY REMOVING CORRODED TRACK AND INSTALLING P/N 5936663U521, FABRICATING AND INSTALLING REPAIR SHIM 15" X 2" FROM 7075-T6 .040" IAW DC-9/MD-80 SRM 51-30-01, 51-10-4 AND 51-30-01.

Part: FRAME — WORN (BS 1401)

FOUND WORN AREA ON FRAME AT FS 1401 ABOVE LONGERON 21 RIGHT. REPAIRED BY FABRICATING AND INSTALLING FRAME FLANGE REPAIR 20" X 9.0" FROM 7075-T6 .063 AND 13" X 1.0" X .600" FROM 7075-T6 .050" IAW DC-9/MD-80 53-03D PG 5 FIG 4, 53-01 AND 51-30-2.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2

FOUND CORROSION ON CARGO TRACK RT SIDE FROM FS 1212 TO FS 1322. REPAIRED BY DRILLING UP AND INSTALLING TRACK P/N 5936663U505 IAW DC-9/MD-80 SRM 51-30-1 AND 51-10-4.

Part: FLOORBEAM — CORRODED (BS 1352) · corrosion level 2

FOUND CORROSION ON PAX CABIN FLOORBEAM STRUCTURE JUST FWD OF THE AFT CABIN PRESSURE BULKHEAD DOOR THRESHOLD FS 1352, BL 0 TO BL 11-L. REPAIRED BY FABRICATING AND INSTALLING DOUBLER REPAIR 33" X 5" AND ANGLE 23" X 46" FROM 7075-T6 .050" IAW DC-9/MD-80 SRM 53-05 FIG 34, AND 51-10-3.

Part: FLOOR SUPPORT — CORRODED (BS 522-693) · corrosion level 2

FOUND CORROSION ON LEFT OUTBOARD FLOOR SUPPORT FROM FS 522 TO 693. REPAIRED BY DRILLING UP AND INSTALLING TRACK P/N 5936594U529 IAW DC-9/MD-80 SRM 51-30-2, 51-10-4 AND 51-10-3D.

Part: LONGERON — CORRODED (BS 1231-1250) · corrosion level 2

CORROSION ON LONGERON 22L BETWEEN FS 1231 AND FS 1250. REMOVED CORRODED STRAP. FABRICATED AND INSTALLED STRAP 20" X .5" FROM 7075-T6 PER DWG 5911423 IAW DC-9/MD-80 SRM 51-10-3D AND 51-30-2.

Part: STRINGER — CORRODED (BS 1287-1307) · corrosion level 2

FOUND CORROSION ON STRINGER 30 BETWEEN FS 1287 AND 1307. REPAIRED BY REMOVING STRINGER SPLICE, FABRICATED AND INSTALLED REPAIR SPLICE 11.5" X 2.7" FROM 7075-T6 IAW DOUGLAS DWG 3914677 AND DC-9/MD-80 SRM 51-30-05 AND 51-10-3D.

Part: LONGERON — CRACKED (FUSELAGE)

FOUND LONGERON 29L CRACKED AT ATTACH POINT AT FS 218. REPAIRED LONGERON 29 LT CRACKED AT ATTACH POINT AT FS 218 BY REMOVING CRACKED LONGERON. FABRICATED AND INSTALLED REPAIR LONGERON 57-1/4" FROM P/N 2777922-4 IAW MD-80 SRM 51-30-2 AND DELTA DC-9/MD-80 SRM 51-10-3D.

Part: INTERCOSTAL — CORRODED (BS 1212-1231) · corrosion level 2

CORROSION ON INTERCOSTAL BETWEEN FS 1212 AND FS 1231 RT OF S-30. REMOVED INTERCOSTAL. FABRICATED AND INSTALLED INTERCOSTAL 4" X 1" X 6" FROM 7075-T6 .050 IAW DC-9/MD-80 SRM 51-30-2.

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

CORROSION ON VERT TEE BL 0 -L- ANGLE L-28L - L-28R. REPLACED TEE P/B 5910130-65 AND ANGLE P/N 9915561-73. FABRICATED AND INSTALLED FORMER DOUBLER 4.0" X 1.10" FROM 7075-T6 .063, WEB 28.0" X 9.5" FROM 7075-T6 .040, WEB REPAIR 3.6" X 9.50" FROM 7075-T6 .050", DOUBLER 7.0" X 6.0" FROM 7075-T6 .080" AND -L- ANGLE SPLICE DOUBLERS 10.0" X 2.0" AND 8.0" X 2.0" FROM BAC1490-2720/7075-T6 IAW DC-9/MD-80 SRM 51-30-5, 51-10-3.

Part: SEAT TRACK — CORRODED (BS 229-864) · corrosion level 2

CORROSION ON MAIN CABIN FS 229 TO FS 864 RIGHT O/B SEAT TRACK. INSTALLED SEAT TRACK P/N 5930547U709 IAW DC-9/MD-80 SRM 51-10-3, 53-05 FIG 4B1 AND 51-30-1.

Part: SEAT TRACK — CORRODED (BS 864-1322) · corrosion level 2

CORROSION ON MAIN CABIN FS 864 TO FS 1322 LEFT O/B SEAT TRACK. INSTALLED SEAT TRACK P/N 5930547U709 IAW DC-9/MD-80 SRM 51-10-3, 51-10-4 AND 51-30-1.

Part: SEAT TRACK — CORRODED (BS 436-457) · corrosion level 2

MAIN CABIN FS 229 TO FS 864 LEFT I/B SEAT TRACK HAS AREAS OF CORROSION. REMOVED CORRODED SEAT TRACK LEFT FS 436 - FS 457 AND INSTALLED REPAIR SPLICE P/N ACA7413-505 AND PLATE P/N ACA7414-3 IAW DC-9/MD-80 SRM 53-05D.

Part: LONGERON — CRACKED (BS 160 S30L)

LONGERON 3L CRACKED IN 2 EACH PLACES AT FS 160. REMOVED CRACKED SECTION OF LONGERON. DRILLED UP AND INSTALLED 17.5" X 2.25" SECTION FROM P/N S2777922-1-26500 AND 15.25" X 2.5" FROM P/N 7637813-3 IAW DC-9/MD-80 SRM 53-02 FIG 18.

Part: LONGERON — CRACKED (BS 1380 S14L)

LONGERON 14L FS 1380 ABOVE PYLON CRACKED IN RIVET HOLE. CUT OUT CRACKED SECTION. FABRICATED AND INSTALLED DOUBLER 4.2" DIAMETER AND FILLER .5" DIAMETER FROM 2024-T3 .040 IAW DC-9/MD-80 SRM 53-01 AND 51-10-3.

Part: FLOOR SUPPORT — CORRODED (BS 1136) · corrosion level 2

CORROSION ON FLOORBOARD SUPPORT IN THE AFT GALLEY AREA AT FS 1136 JUST I/B OF L-2 GALLEY DOORS L/E. REMOVED CORRODED FLOORBOARD SUPPORT. FABRICATED AND INSTALLED ANGLE SUPPORT 3.5" X 3.5" FROM 7075-T6 .063" IAW DC-9/MD-80 SRM 51-30-5, 51-10-2 PG 1 AND 51-10-3D.

Part: FLOOR SUPPORT — CORRODED (BS 1274) · corrosion level 2

CORROSION ON FLOORBOARD SUPPORT IN THE AFT GALLEY AREA AT FS 1274 JUST I/B OF L-2 GALLEY DOORS T/E. REMOVED CORRODED FLOORBOARD SUPPORT. FABRICATED AND INSTALLED ANGLE SUPPORT 3.5" X 2.75" FROM 7075-T6 .063" IAW DC-9/MD-80 SRM 51-30-5, 51-10-2 PG 1 AND 51-10-3D.

Part: STRINGER — CORRODED (BS 1307-1322) · corrosion level 2

FOUND CORROSION ON S-29L BETWEEN FS 1307 AND 1322. REPAIRED BY FABRICATING AND INSTALLING REPAIR U-CHANNEL 18.0" X .90 T= .050" FROM 60-25713/7075-T6511 IAW DC-9/MD-80 53-02D FIG 19, 51-10-3D AND 51-30-5.

Part: TARGET — UNKNOWN (MLG) · airframe 46,641 hrs · 37,178 cycles

ON APPROACH GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER ALL GEAR DOWN AND LOCKED. OPERATED ALT GEAR EXTEND HANDLE. STOPPED ON RWY. GEAR PINNED. TAXIED TO GATE. REPLACED LEFT MLG DOOR TARGET AND BRACKET.

Part: CONTROL VALVE — FAILED (RT A/C PACK) · airframe 44,180 hrs · 35,384 cycles

LOST ALL CABIN PRESSURIZATION DESCENDING THRU FL260, ON INITIAL DESCENT MASKS DROPPED CABIN ALTITUDE REACHED 14500 FT. CREW USED CREW OXYGEN. FLIGHT ATTENDANT REPORTED HUGE GAP IN 2L DOOR SEAL AND THE SOUND OF RUSHING AIR. REPLACED BROKEN SENSE LINE ON RT PACK FLOW CONTROL VALVE.

Part: ANNUNCIATOR — FAULTY (COCKPIT) · airframe 43,983 hrs · 35,246 cycles

F/O REPORTS SMOKE COMING FROM AROUND F/O FMA. REPLACED FMA.

Part: DEFLECTOR — WORN (NLG) · airframe 40,014 hrs · 32,494 cycles

NOSE GEAR WOULD NOT RETRACT AFTER T/O. REPLACED LT NOSE LANDING GEAR SPRAY DEFLECTOR.

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,376 hrs · 30,541 cycles

AFT OVERWING OVERHEAD EMERGENCY LIGHTS INOP. REPLACED BATTERIES.

Part: NUT — DAMAGED (R1 THRESHOLD) · airframe 37,224 hrs · 30,425 cycles

DOOR 1R GIRT BAR ATTACH FITTING COULD NOT BE SECURED. FOUND NUTS DAMAGED. REPLACED SAME.

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 35,253 hrs · 28,999 cycles

ON T/O NOSE GEAR FAILED TO RETRACT, HEAVY GRINDING AUDIBLE -RED LIGHT IN HANDLE. INSPECTED AND SERVICED NOSE STRUT PER M/M 32-21-02-3-1. CHECKED PROX SENSORS AND CLEANED SAME, ALL CHECKED NORMAL. PERFORMED NOSE GEAR SWING, ALL NORMAL. CHECKED WHEEL BEARINGS AND TIRE CONDITION, ALL CHECKED OK.

Part: CHARGER — BROKEN (FLASHLIGHT) · airframe 33,210 hrs · 27,520 cycles

WORKING MCO ON BROKEN EMERGENCY FLASHLIGHT AT MID F/A POSITION. REPLACED EMERGENCY FLASHLIGHT CRADLE AND REPLACED ANTI TAMPER BAND. MCO REMOVED.

Part: TIRE — FAILED (NR 3 MLG) · airframe 33,125 hrs · 27,470 cycles

NR THREE MAIN TIRE TREAD SEPARATED. REPLACED WHEEL ASSY.

Part: SENSOR — OUT OF ADJUST (NLG)

LANDING GEAR WOULD NOT RETRACT, HANDLE WOULD NOT GO PAST HALF WAY. PER CKLIST NOSE WHEEL STEERING AVAIL. A/T WOULD ENGAGE BUT NOT WORK. VARIOUS AURAL WARNINGS NONSTOP. JACKED NOSE LANDING GEAR AND ADJUSTED GROUND SENSING CONT MECHANISM PER M/M 32-23-01-02. RAN RETRACTION TEST. ALL CKS OK. A/C OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (ROW 1-12)

ON L/O, FOUND BOTH FWD DOOR EMERGENCY EXIT LIGHTS AND SEATS 1-12 INOP. REPLACED POWER SUPPLY, CHECKS GOOD.

Part: PSEU — MALFUNCTIONED (LANDING GEAR)

FLAPS AT 11 DEGREES GEAR HANDLE UP, NOSE RED LIGHT CAME ON. ALSO, FLAP/SLAT IND DISAG / AUTO/LAND WERE FLICKERING ON. WHEN GEAR HANDLE DOWN, RT MAIN GREEN IND HAD RED LIGHTS FLICKERING. INSPECTED GEAR AND FLAPS/SLATS, CLEANED NOSE AND MLG DOWNLOCKS, UPLOCKS AND AIR GROUND, SENSORS. REPLACED PSEU AND TESTED OK PER MAINT MANUAL.

Part: APU — OIL LEAK (FUSELAGE)

ON CLIMBOUT HAD ODOR IN COCKPIT/CABIN WITH LAVATORY SMOKE DETECTOR SOUNDING. FOUND APU CHIP DETECTOR LEAKING OIL AND APU INGESTED OIL AND CONTAMINATED THE AIR CONDITIONING SYS. FWD APU TO MCO AND PLACARD. CHANGED WATER SEPARATOR BAGS, RAN ENGS AND A/C OPS CKS NORMAL.

Part: LIGHT — DAMAGED (CABIN)

ON PREFLIGHT, EMERGENCY EXIT SIGN ON CEILING AT ROW 38 WILL NOT LIGHT AND DAMAGED ON BACK SIDE. REPLACED SIGN ASSEMBLY, OPERATION NORMAL.

Part: SPOILER — DELAMINATED (RT WING)

FOUND DURING A-2 LETTER CHECK, RIGHT I/B FLIGHT SPOILER DELAMINATED AT T/E. REPAIRED PER SRM 51-70-1B.

Part: BALLAST — FAILED (CABIN)

F/A AND GROUND CREW SMELLED ELECTRICAL BURNING IN AFT CABIN. FOUND OVHD LIGHTS INOP. BALLAST 26BD INOP. REPLACED BALLAST, OPERATION NORMAL.

Part: HYD LINE — LEAKING (AFT FUSELAGE)

ON CLIMB-OUT, HAD HOT OR BURNING ODOR IN CABIN AND FLIGHT DECK, RETURNED ATL. FOUND HYDRAULIC LINE LEAKING AND FLUID DRAINING INTO APU INLET. SECURED LINE, OPERATION NORMAL.

Part: COWL — DENTED (ENGINE)

DURING SHOP INSPECTION, FOUND DENTS AND GOUGE ON LEADING EDGE LIP AT 6,9,5,4 O'CLOCK POSITIONS OF ENGINE INTAKE COWL. REPAIRED DAMAGE PER SRM 54-04.