N954DL

Part: WIRE — SHORTED (CABIN) · airframe 74,243 hrs · 55,535 cycles

SEAT EMERGENCY LIGHTS INOP FROM 31ED AFT TO TAILCONE AREA. FOUND WIRE L982U14 GROUNDING OUT/CHAFFED AT LIGHT ASSY L2-848. REPAIRED WIRE AND REPLACED FUSE AT BATTERY PACK B5-212 PER SWPM CH.20. CKS GOOD. OK FOR SVC.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 74,249 hrs · 55,540 cycles

CABIN CARPET (AISLE AND CROSS-AISLE) WORN/TORN/FRAYED/MISSING. AC FLOORING SOFT BETWEEN 10ABC AND 10DE AND 4AB AND 4CB / INTERIOR. FOUND DAMAGE TO EXTEND WITHIN 3" OF PANEL EDGE. REMOVED SEAT ROW 10ABC FOR ACCESS. REMOVED FLOOR PANEL 9936585-2. FABRICATED NEW PANEL PER BAC DWG 9936585. INSTALLED NEW FABRICATED PANEL AND CARPET REF AMM 25-31.

Part: WIRE — BROKEN (CABIN) · airframe 74,160 hrs · 55,466 cycles

EMERGENCY LIGHT ON SEAT 34D INOP. REPAIRED BROKEN WIRING IAW AMM 20-50. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 74,124 hrs · 55,430 cycles

ON SVC CK, FOUND SEATS 31-36 EMERGENCY LIGHT AND AFT STAIRS EMERGENCY LIGHTS INOP. T/S PER AMM 33-50-00-001. FOUND EMERGENCY LIGHT BATTERY PACK B5-212 POWER SUPPLY INOP. REPLACED POWER SUPPLY ASSY IAW AMM 33-53. OPS CK NML. OK FOR SVC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,109 hrs · 55,418 cycles

FOUND SKIN CRACK AT LWR FWD CORNER OF AFT LAV PAN. REPAIRED PER ERA 569781-14 REV ORIGINAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,328 hrs · 55,601 cycles

REPAIR OF CORROSION AT AFT LAV SERVICE PANEL CUTOUT, STA 1322 BETWEEN L-21L AND L-22L. REPAIRED AFT LAV SERVICE PANEL CUTOUT PER ER/A 569781-14.

Part: SUPPORT ANGLE — CRACKED (TAILCONE) · airframe 73,650 hrs · 55,037 cycles

TAIL CONE LT UPPER LOCK BAYONET RECEPTACLE, UPPER SUPPORT ANGLE CRACKED. REPLACED THE SUPPORT ANGLE IAW DWG 9911957.

Part: FRAME — CRACKED (TAILCONE) · airframe 73,650 hrs · 55,037 cycles

TAIL CONE ATTACH CANTED FRAME BS 1310 WAS FOUND CRACKED, TWO AREAS 2:00 & 7:00 O`CLOCK. REPLACED THE FRAME IAW DRAWING 5966769.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,270 hrs · 54,732 cycles

TAIL COMPARTMENT CENTER STAIR LIGHT INOPERATIVE. FOUND BATTERY PACK INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-50.

Part: BATTERY PACK — INOPERATIVE (SMOKE DETECTOR) · airframe 72,946 hrs · 54,488 cycles

RIGHT AFT LAVATORY, CREW REPORTED A CHIRPING NOISE. REPLACED THE LAVATORY SMOKE DETECTOR BATTERY. OPS CHECKED GOOD IAW AMM 26-13.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 72,309 hrs · 53,992 cycles

SEAT 22DE EMERGENCY LIGHT INOPERATIVE. FOUND A WIRE BROKEN AT THE SEAT FRAME, TERMINATED THE WIRE AS REQUIRED.

Part: FRAME — CRACKED (BS 1437) · airframe 70,440 hrs · 52,491 cycles

DURING BHEC INSPECTION, A CRACK WAS FOUND ON CAP AT BS 1437 BETWEEN LONGERONS 1-2L. THE CAP WAS REPAIRED IAW ETI-88-17-003 REV. 3 AND ER/A 552910-14 REV. ORIGINAL.

Part: SKIN — CRACKED (BS 1437) · airframe 70,440 hrs · 52,491 cycles

A CRACK WAS FOUND ON THE SKIN AT BS 1437 BETWEEN LONGERONS 1 - 2L. THE SKIN WAS REPAIRED IAW ETI-88-17-005 REV 2 AND ER/A 552912-14 REV. ORIG.

Part: SKIN — CRACKED (BS 1437) · airframe 70,440 hrs · 52,491 cycles

TWO CRACKS WERE FOUND ON FUSELAGE SKIN AT THE BS 1437 AND BETWEEN LONGERON 3 AND 4L . THE SKIN WAS REPAIRED IAW ETI-88-17-005 REV 2 AND ER/A 552912-14 REV. ORIG.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 70,440 hrs · 52,491 cycles

PAX CABIN. CORROSION ON FLOOR SUPPORT BETWEEN BS 160 TO 200 AT LBL 54. THE FLOOR SUPORT WAS REPLACED IAW SRM 53-14-1 FIGURE 11 AND 51-30-5.

Part: STATIC PORT — DAMAGED (FUSELAGE) · airframe 70,438 hrs · 52,490 cycles

RT ALTERNATE STATIC PORT WAVINESS IS OUT OF LIMITS ON CRITICAL AREA. (MAX 0.006 IN - HAS 0.010 IN) WAVINESS CAUSED BY A PREVIOUS BLEND OUT. REPAIRED PER SRM 53-04 FIG 12C(SHEET 5).

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 70,438 hrs · 52,490 cycles

SKIN DENTED ON MID VANE OF LT WING TE FLAP. REPAIRED IAW SRM 57-03D P.11, AND 51-70-2D.

Part: PAN — CORRODED (CARGO DOORWAY) · airframe 70,438 hrs · 52,490 cycles

CORROSION ON PAN OF CARGO LOWER DOOR FRAME BS 370 - 427. THE PAN WAS REPAIRED IAW SRM 53-05 PAR 55A FIG.44A.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,438 hrs · 52,490 cycles

CORROSION ON INTERNAL DOUBLER AROUND AFT LAVATORY SERVICE PANEL CUT OUT. DAMAGE AREA WAS ACCOMPLISHED PER ERA 552906-14 REV. ORG. AND ETI-88-17-001 REV. 2.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,438 hrs · 52,490 cycles

CORROSION ON FUSELAGE SKIN AROUND AFTER LAVATORY SERVICE PANEL. REPAIRED IAW ERA 552906-14 REV. ORG. AND ETI-88-17-001 REV. 2.

Part: LONGERON — CORRODED (BS 1287) · corrosion level 2 · airframe 70,438 hrs · 52,490 cycles

AFT CARGO BAY HAS CORROSION ON LONGERON 28R AND BS 1287. THE LONGERON WAS REPAIRED IAW SRM 53-02 PAR 13 FIG 19.

Part: SKIN — CRACKED (LT PYLON) · airframe 70,438 hrs · 52,490 cycles

CRACKED LT PYLON UPPER SKIN. TRAILING EDGE PYLON LH WAS REMOVED AND INSTALLED IAW SRM 51-30-1. HFEC INSPECTION WAS ACCOMPLISHED.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,438 hrs · 52,490 cycles

MID CARGO COMPARTMENT, CORROSION ON DOOR JAMB BTW STA Y= 636 AND STA Y= 693 BTW LONGERON 28R AND 27R. DOUBLER WAS REPLACED PER SRM 53-05 PAR 140 FIG 123.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 70,438 hrs · 52,490 cycles

CRACKED AFT EDGE BEAM NR 2 ON MAIN ENTRANCE DOOR. BEAM NR 2 WAS REPAIRED PER SRM 52-05 REPAIR 69 FIGURE 83.

Part: FITTING — CRACKED (SERVICE DOOR) · airframe 70,438 hrs · 52,490 cycles

CRACKED AFT EDGE CLIP ON BEAM NR 1 AT FWD SERVICE DOOR. CRACK CLIP WAS REPLACED FOR ONE NEW PER SRM 51-30-05.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,438 hrs · 52,490 cycles

PAX CABIN, CRACKED LONGERON 3L ON STA Y=160 AT CABIN CROWN. LONGERON SECTION WAS REPAIRED PER 53-02 PAR 12 FIG 18 AND INSTALLED PER SRM 51-30-5, 51-30-2.

Part: BEAM — CRACKED (PAX DOOR) · airframe 70,438 hrs · 52,490 cycles

CRACKED FWD EDGE BEAM NR 1 AT MAIN ENTRANCE DOOR. THE BEAM WAS REPAIRED IAW SRM 52-05 FIG.98 SHEET 3.

Part: LINER — DEBONDED (RT NACELLE) · airframe 69,025 hrs · 51,405 cycles

PERFORMED DUE TO REPORT OF RT ENGINE COMPRESSOR STALL. FOUND ACOUSTIC LINER DIS-BONDED FRONT OF ENGINE NEAR THE BLEED VALVES. THE ENGINE WAS REPLACED.

Part: CABLE — DAMAGED (TAILCONE) · airframe 69,012 hrs · 51,393 cycles

TAILCONE KEVLAR CABLE DAMAGED. REPLACED KEVLAR CABLE REF. AMDS CARD 5350-01077-0101.

Part: FLOORBOARD — DAMAGED · airframe 69,012 hrs · 51,393 cycles

ALLEY FLOOR IS DEPRESSED SLIGHTLY APPROXIMATELY 12" X 18" LOCATED JUST INBD OF THE 2L DOOR THERE IS A SLIGHT RISE IN THE FLOOR ALONG THE INBOARD EDGE. R & R FLOORBOARD INBD OF 2R DOOR AND REPLACED GALLEY MATERIAL.

Part: TURBINE — FAILED (RIGHT ENGINE) · airframe 68,970 hrs · 51,362 cycles

RETURNED TO DEPARTURE DUE TO A RT ENGINE TURBINE FAILURE DURING CLIMB AT AT 800-1000 FT. RT ENGINE WAS SHUTDOWN IFSD. CREW NOTED MAXIMUM EGT 800DEG. MAINTENANCE FOUND TURBINE DAMAGE AND AN ENGINE CHANGE WAS REQUIRED. ENGINE WAS REPLACED AND SUBSEQUENT CHECKS WERE GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 68,908 hrs · 51,335 cycles

AFT CEILING LIGHTS, EMERGENCY, INOPERATIVE. CHANGED BATTERY'S AD2013-1A, 2 EACH. OPS CHECK GOOD.

Part: TARGET — DAMAGED (MLG DOOR SENSOR) · airframe 68,698 hrs · 51,184 cycles

AFTER EXTENDING THE LANDING GEAR IN PREPARATION FOR LANDING, CREW REPORTED MLG DOOR OPEN LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURE AND PERFORMED AN ALTERNATE GEAR EXTENSION RESULTING IN BOTH MAIN GEAR DOORS CONTACTING THE RUNWAY DURING LANDING. MAINTENANCE FOUND THE RT MLG DOOR PROXIMITY SENSOR TARGET DAMAGED. REPLACED TARGET SUPPORT AND INSTALLED & ADJUSTED TARGET ON RT GEAR DOOR. REPLACED RT & LT GEAR SKIDS AND SPACERS.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 68,658 hrs · 51,156 cycles

RIGHT HYDRAULIC QTY DROPPED TO 2 QTS AND AFTER GEAR AND FLAPS WERE LOWERED QTY WENT TO 0 QTS. FOLLOWED BY PRESSURE DROPPING TO 0 PSI. REPLACED RT ENGINE DRIVEN HYD PUMP.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 68,435 hrs · 51,009 cycles

THE FLIGHT CREW FOUND 1 RED EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 24DE. MCO MAINTENANCE REPLACED THE HARNESS ASSY AND THE LIGHT CHECKED OK.

Part: CONTROL BOX — FAILED (ANTI SKID SYSTEM) · airframe 68,263 hrs · 50,912 cycles

RIGHT OTBD ANTI-SKID LIGHT ILLUNINATED ON OAP AFTER GEAR WAS LOWERED. CREW DECLARED EMERGENCY. REPLACED ANTI-SKID CONTROL BOX AND RIGHT OTBD A/S TRANSDUCER.

Part: SKIN — CORRODED (BS 610) · corrosion level 2 · airframe 67,236 hrs · 50,170 cycles

DURING WALK AROUND FOUND FUSELAGE SKIN PILLOWED AND CRACKED AT BS 610 AND STR 28R. REMOVED MID CARGO SLANT AND FLOOR PANEL FWD OF DOORWAY TO GET ACCESS TO CORROSION. REINSTALLED CARGO SLANT PANEL AND FLOOR PANEL FWD OF DOOR WAY IAW AMM 25-52. REPAIRED IAW ER/A 539610-14, REV A ASSOCIATED ER/A 14-539610 ADDED FOR AC 0954.

Part: OVEN — ODOR (GALLEY) · airframe 65,771 hrs · 49,165 cycles

ON CLIMBOUT A STRONG ELECTRICAL ODOR WAS NOTICED THROUGHOUT CABIN AND COCKPIT IAW SMOKE AND FUMES CHECKLIST. TURNED GALLEY POWER OFF AND ELECTRICAL ODOR DISSIPATED. CONTINUED FLIGHT WITH GALLEY POWER OFF. PERFORMED PNEUMATIC DISTRIBUTION CABIN SMOKE/ODOR TROUBLESHOOTING IAW WC 2120-2367. REPLACED FWD GALLEY OVEN IAW AMM 25- 30. RAN ENGINES AND APU AND PACKS AND ALL GALLEY EQUIPMENT. NO ELECTRICAL ODOR NOTICED. OVEN OPS NORMAL. OK FOR SERVICE.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 65,435 hrs · 48,921 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS AT 24DE TO BE INOPERATIVE. MAINTENANCE REPLACED THE PIGTAIL LIGHT ASSEMBLY AT SEAT 20DE AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,543 hrs · 47,560 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS AT ROWS 11-20 AND 27 & AFT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,543 hrs · 47,560 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS IN COCKPIT AND AT DOORS L1 & R1 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 62,760 hrs · 47,045 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. MAINTENANCE REPLACED THE CONNECTOR WIRES AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: LANYARD — MISSING (TAILCONE SLIDE) · airframe 61,707 hrs · 46,302 cycles

INSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE HAD THE LANYARD PULLED FROM ITS OUTER PROTECTIVE SLEEVE. THE TAILCONE SLIDE LANYARD WAS REPLACED.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 61,706 hrs · 46,301 cycles

L1 DOOR EXTERNAL LOWER SKIN PREVIOUS REPAIR DAMAGE ALONG LENGTH OF DOOR. REMOVED DOUBLER AND INSTALLED NEW ONE. REPAIR ALL IAW SRM 52-05D, FIG 37, 51-10-3, AMM 52-11-02 & PSM 900-5-1, NR 4.

Part: FRAME — CRACKED (BS 1437) · airframe 61,706 hrs · 46,301 cycles

BS 1437. STR 1, FRAME CRACKED. REMOVED FASTENERS, STRIPPED DAMAGE AREA, COMPLETED NDT INSPECTION AT AREA IAW NDT SPM 06-10-01. CUT OUT DAMAGE AREA, FABRICATED, AND INSTALLED REPAIR PARTS IAW SRM 53-03 FIG 4.

Part: CUSP WEB — CORRODED (BS 1174-1193) · airframe 61,706 hrs · 46,301 cycles

RT SIDE CUSP WEB BETWEEN BS 1174 AND 1193, RBL-58 CORRODED. BLENDED TWO AREAS OF CORROSION, BS 1174-1193 RT IAW ER/A 508307-14MA, REV A. MATERIAL REMAINING IS .010 IAW SRM 53-14-3 FIG 12, SHEET 1 AND 2. FOUND TO BE OUT OF LIMITS IAW ER/A 508307MA, REV A. PERFORMERD CUTOUT OF CORROSION DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-05, FIG 131A-14, SHEET 1.9.

Part: CUSP WEB — CORRODED (BS 1193-1212) · airframe 61,706 hrs · 46,301 cycles

RT SIDE CUSP WEB BETWEEN BS 1193 AND 1212, RBL-58 CORRODED. BLENDED CORROSION FROM FS 1202-1206 RT IAW ERA 508307-14MA, REV A. CORROSION AF FS 1202 TO 1206 RT GOES THROUGH MATERIAL WITH ZERO MATERIAL REMAINING. FOUND TO BE OUT OF LIMITS IAW ER/A 508307-14MA, REV A. PERFORMED CUTOUT OF CORROSION DAMAGE, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW SRM 53-05, FIG 131A-13,

Part: CUSP WEB — CORRODED (BS 1110) · airframe 61,706 hrs · 46,301 cycles

RIGHT SIDE CUSP WEB BS 1110, RBL 58 CORRODED. REPAIRED IAW SRM 53-05, FIG 131A-2, 51-30-5, 51-30-2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,500 hrs · 46,162 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 61,500 hrs · 46,162 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 18DE IN THE CABIN WAS INOPERATIVE. MX FOUND WIRES BROKEN IN THE HARNESS. THE WIRE HARNESS WAS REPLACED AND THE SYS RETURNED TO NORMAL OPERATION.

Part: SKIN — CRACKED (BS 1380) · airframe 61,069 hrs · 45,838 cycles

DURING MX CHECK AT MSP, FUSELAGE SKIN WAS FOUND CRACKED AT BS 1380, BETWEEN L13-14L. REPAIRED IAW ERA 512170-14, SECTION 1 PERMANENT REPAIR. CLASSIFIED AS MAJOR REPAIR IAW ENGINEERING.

Part: LONGERON — CORRODED (BS 1155-1180) · airframe 61,069 hrs · 45,838 cycles

LONGERON 28 RT- CORRODED AT AFT BAG BIN DOOR LOWER FRAME, APPROX. BS 1155 TO 1180. REPAIRED IAW SRM 53-05, FIG 123. REQUIRED INSPECTION COMPLETED.

Part: COVER — DAMAGED (ESCAPE SLIDE) · airframe 61,069 hrs · 45,838 cycles

DURING SCHEDULED MX, THE SLIDE COVER ON THE AFT TAILCONE SLIDE WAS FOUND TO BE IN POOR CONDITION WITH SOME MISSING VELCRO AND A LOOSE STENCIL. THE SLIDE COVER WAS R & R IAW AMM 25-62-01 AND THE RII INSPECTION WAS ACCOMPLISHED.

Part: SPRING — BROKEN (TAILCONE LATCH) · airframe 61,069 hrs · 45,838 cycles

DURING SCHEDULED MX, THE LOWER LT TAILCONE LATCH SPRING WAS FOUND TO BE WORN, THE WORN SPRING WAS REPLACED IAW AMM 53-53 AND THE RII INSPECTION WAS COMPLETED.

Part: RELEASE CABLE — WORN (TAILCONE) · airframe 61,069 hrs · 45,838 cycles

DURING INSPECTION, FOUND TAILCONE RELEASE CABLE TO BE WORN. REPLACED KEVLAR CABLE IAW AMM 53-53.

Part: BRACKET — WORN (RELEASE CABLE) · airframe 61,069 hrs · 45,838 cycles

DURING SCHEDULED CHECK, FOUND AFT TAILCONE RELEASE CABLE SPRING BRACKETS WORN. REPLACED WORN BRACKETS IAW SRM 51-30.

Part: RECEPTACLE — WORN (TAILCONE RELEASE) · airframe 61,069 hrs · 45,838 cycles

DURING SCHEDULED MX, THE UPPER TOP RT TAILCONE LATCH RECEPTACLE WAS FOUND TO BE WORN. THE TOP RT LATCH RECEPTACLE WAS R & R IAW AMM 53-53. THE REQUIRED RII INSPECTION WAS PERFORMED.

Part: LATCH — WORN (TAILCONE RELEASE) · airframe 61,069 hrs · 45,838 cycles

DURING SCHEDULED MX, THE LOWER RT TAILCONE RELEASE LATCH WAS FOUND TO BE WORN. THE LOWER RT LATCH WAS REPLACED IAW AMM 53-53 AND THE RII INSPECTION WAS PERFORMED.

Part: COVER — DAMAGED (ESCAPE SLIDE) · airframe 61,069 hrs · 45,838 cycles

DURING SCHEDULED MX, THE SLIDE COVER ON THE AFT TAILCONE SLIDE WAS FOUND TO BE IN POOR CONDITION WITH SOME MISSING HOOK AND LOOP STRAP, AND LOOSE STENCIL. THE SLIDE COVER WAS R & R IAW AMM 25-62-01 AND THE RII INSPECTION WAS ACCOMPLISHED.

Part: BUSHING — WORN (TAILCONE RELEASE) · airframe 61,069 hrs · 45,838 cycles

DURING SCHEDULED MX OF THE TAILCONE RELEASE MECHANISM, THE LT TAIL CONE TEE PIN & BUSHINGS WERE FOUND TO BE WORN BEYOND LIMITS. THE TEE PIN AND BUSHINGS WERE REPLACED IAW AMM 53-53 AND THE RII INSPECTION WAS COMPLETED.

Part: BLOCK — WORN (RELEASE CABLE) · airframe 61,069 hrs · 45,838 cycles

DURING SCHEDULED MX, AT THE UPPER LT TAILCONE LATCH, THE RELEASE CABLE BLOCK WAS FOUND TO BE WORN. THE CABLE BLOCK AT THE UPPER LT LATCH WAS REPLACED IAW AMM 53-53. THE REQUIRED RII INSPECTION WAS PERFORMED.

Part: RECEPTACLE — WORN (TAILCONE RELEASE) · airframe 61,069 hrs · 45,838 cycles

DURING SCHEDULED MX INSPECTION, THE TAILCONE ALIGNMENT PIN RECEPTACLES WERE FOUND TO BE WORN. THE WORN RECEPTACLES WERE REPLACED IAW AMM 53-53. THE REQUIRED RII INSPECTION WAS PERFORMED.

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 60,784 hrs · 45,626 cycles

FOUND L/E DAMAGE AT XFS 184.750 ON LT HORIZONTAL STAB. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-03, FIG 22.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 59,065 hrs · 44,423 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 6C IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS LOOSE, SECURED CONNECTOR, FUNCTIONALLY CHECKED SYSTEM.

Part: LANYARD — BROKEN (EVAC SLIDE) · airframe 58,644 hrs · 44,139 cycles

ON ARRIVAL PRIOR TO OVERNIGHT SERVICE CHECK, THE L1 DOOR SLIDE LANYARD CABLE WAS FOUND BROKEN AND NOT ATTACHED TO THE RELEASE FITTING. MAINTENANCE REPLACED THE LANYARD ASSEMBLY.

Part: BATTERY PACK — DISCHARGED (TAILCONE) · airframe 58,071 hrs · 43,743 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN AT THE TAIL CONE ACCESS DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHT RETURNEDTO AN OPERATIONAL CONDITION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,069 hrs · 43,741 cycles

FLOOR SUPPORT ANGLE AT RBL 7 FS 160 HAS CORROSION SAA102- CORROSION MAIN CABIN. FABRICATED FLOOR SUPPORT ANGLE IAW DC9/MD80 SRM 53-14-1 FIG 11. INSTALLED FLOOR SUPPORT ANGLE AT STA 148-200N RBL 7 IAW DC9/MD80 SRM 51-30-1 PG 11 AT SAA/SAT DURING PAX MOD ON W/O 89535230001.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,069 hrs · 43,741 cycles

FLOOR SUPPORT LBL 7 FS 160 HAS CORROSION FWC05 SAA102-CORROSION MAIN CABIN. FABRICATED FLOOR SUPPORT ANGLE IAW DC9/MD80 SRM 53-14-1 FIG 11. INSTALLED FLOOR SUPPORT ANGLE AT STA 148-200 LBL 7 IAW DC9/MD80 SRM 51-30-1 PG 11. AT SAA/SAT DURING PAX MOD ON W/O 89534210001.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,069 hrs · 43,741 cycles

LT SIDE EXTERIOR FUELAGE IS DENTED AT FSTA 213 AND BETWEEN LONGERONS 15L AND 16L SAA021-DENTED EXTERIOR FUSELAGE. FABRICATED INTERNAL DOUBLER REPAIR PER SRM MD80 53-04 FIG 38 PAGE 218H VIEW E. INSTALLED INTERNAL DOUBLER REPAIR AT FUSELAGE STA 213 BETWEEN 15 AND 16L PER SRM MD80 53-04 FIG 38 PAGE 218H AND INSTALLED TAG PER PS 900-5-1 NR 4 AT SAA/ SAT DURING PAX MOD ON N/R 28 W/O 89534000001. THIS TEXT SHOWS N/R 28 BUT REF # SHOWED N/R #29.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,069 hrs · 43,741 cycles

SEAT TRACK LBL 22 HAS CORROSION FS 218 FWC01 SAA102 CORROSION FWD ENTRY. FABRICATED LOCATED AND DRILLED REPLACEMENT SEAT TRACK SECTION REFERENCE DC9/MD80N SRM 53-05 FIG 4F AND FIG 4N. INSTALLED SEAT TRACK AT STA 200-247 LBL 22 IAW DC9/MD80 SRM 51-30-5 PG 12. C/W AT SAA/SAT DURING PAX MOD ON N/R 45 W/O 89534170001.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,579 hrs · 43,392 cycles

DURING PSV CHECK IN MSP THE FUSELAGE SKIN AT STA 588 BETWEEN L-27R AND L-30 WAS FOUND WITH SKIN PILLOWING. THE SUBJECT SKIN IS MANUFACTURED FROM 0.050" THICK 2024-T3 CLAD ALUMINUM.REF A/C NR 143.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,579 hrs · 43,392 cycles

16 SEP 11 FUSELAGE STR 28R STA 560-BULDGED--SKIN IS BULDGED WITHIN RVSM AREA. REPAIRED PER ERA 496280-14 REV ORIG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,468 hrs · 43,313 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT 31D INOPERATIVE. MAINTENANCE RE-LAMPED AND REPLACED A CONNECTOR IN THE SEAT. OPERATION OF LIGHT NOW CHECKS OK.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 55,652 hrs · 42,075 cycles

FASTENER HOLE - CRACKED - 1ST HOLE BELOW ZFS=52 VERT STAB FRONT SPAR RT CHORD REPAIRED IAW ERA 488178-14, REV ORIG.

Part: SEAT — MISLOCATED (CABIN) · airframe 54,619 hrs · 41,382 cycles

WHEN MX TRIED TO GAIN ACCESS TO THE WING SURFACE FROM THE CABIN, THEY FOUND THE EMERGENCY EXIT DOOR WOULD NOT OPEN BECAUSE IT WAS BLOCKED BY THE ARMREST OF THE SEAT. THIS WAS IN ROW 24DE. IT WAS DETERMINED THAT THE SEATS IN ROW 23DE AND IN ROW 24DE WERE IN THE WRONG LOCATIONS. THE SEATS WERE SWAPPED AND THE EXIT FUNCTIONED NORMALLY.

Part: LIGHT — INOPERATIVE (SEAT 31D) · airframe 54,102 hrs · 41,039 cycles

MX FOUND THE ESCAPE PATH LIGHT AT SEAT 31D TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 54,102 hrs · 41,039 cycles

ESCAPE PATH LIGHT INOP AT 31D. FOUND WIRE BROKEN AT PLUG ON LIGHT ASSY. REPLACED LIGHT ASSY.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHTS) · airframe 53,278 hrs · 40,474 cycles

EMERGENCY LIGHTS AT 34 ED INOP. R & R BROKEN WIRE HARNESS, OPS NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,025 hrs · 38,282 cycles

HMV AT ATL, DENTS AND CREASES WERE FOUND AT STA 120 BETWEEN S-18L AND S-19L. THE DAMAGE WAS REPAIRED PER ER/A 09-359999-14. NOTE: AT THE TIME OF ER/A ISSUE, AN MRR WAS NOT SUBMITTED. THIS CORRECTS THAT SITUATION.

Part: SLIDE — LOW PRESSURE · airframe 49,825 hrs · 38,144 cycles

FWD SVC DOOR SLIDE PRESSURE LOW. REPLACED SVC DOOR SLIDE PACK PER MM.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 47,895 hrs · 36,864 cycles

R1 DOOR SLIDE WAY DEPLOYED WHEN DOOR WAS OPENED BY GATE GROMMET. THE DOOR WAS UNLATCHED AND THE GIRT BAR WAS NOT LOCKED IN THE CLIPS. GIRT/SLIDE WAS HANGING ON THE LOWER DOOR FRAME CUT OUT. REMOVED AND REPLACED R1 DOOR SLIDE PER OP 7035.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 47,365 hrs · 36,553 cycles

A TIME-LIMITED REPAIR WAS REMOVED FROM THE RT WING INBD MAIN FLAP LOWER SKIN. PERMANENT REPAIR WAS MADE BY A SPLICE TO THE LOWER SKIN AT XIFO=90.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 44,463 hrs · 34,650 cycles

LT ENGINE ROLLED BACK ON T/O ROLL. ABORTED T/O. AFTER STOPPING EGT WAS RISING THRU 560 DEG AND N1/N2 WAS ROLLING BACK. SHUT DOWN ENGINE. REPLACED NR 1 ENG PER TRANS 9T102.

Part: RESERVOIR — CONTAMINATED (HYDRAULIC SYS) · airframe 41,470 hrs · 32,539 cycles

LEFT HYD PSI WENT TO ZERO AT SLAT EXTENSION. FOUND LARGE AMOUNT OF AIR IN LEFT HYD RESERVIOR. BLED LEFT HYD SYSTEM AND OPS CHECK OK.

Part: WEB — DAMAGED (FUSELAGE) · airframe 33,185 hrs · 26,660 cycles

CUSP WEB DAMAGED AT STA 579.

Part: APU — CONTAMINATED (APU BAY) · airframe 30,192 hrs · 24,445 cycles

DURING INITIAL CLIMBOUT HOT PACK ODOR IN C/PIT CABIN. TURNED RT PACK OFF AND ODOR WENT AWAY. PERF OPN 5088. FOUND APU CONTAMINATED WITH OIL. PERF DUCT- OUT PER M/M. FWD APU TO MCO/PLAC MEL 49-00-01A.

Part: ANNUNCIATOR — SHORTED (COCKPIT) · airframe 29,942 hrs · 24,260 cycles

ON GEAR EXTENSION INTO DCA, NO LANDING GEAR SAFE OR UNSAFE LIGHTS ILLUMINATED/ WITH LANDING GEAR WARNING C/B P-26 POPPED. VERIFIED GEAR DOWN WITH PERISCOPE. FOUND ANN PANEL BAD, REPLACED SAME, OP CKS GOOD.

Part: SMOKE DETECTOR — FAILED (LAVATORY)

AFT LT LAV SMOKE DETECTOR WOULD NOT TEST. REPLACED BATTERY, NO HELP. REPLACED DETECTOR ASSY, OPS CK NORMAL.

Part: HYD LINE — LEAKING (LT PYLON)

AFTER GEAR RETRACTION LEFT HYDRAULIC QUANTITY DROPPED TO 3 QUARTS AND PSI DROPPED TO 0. FOUND PRESSURE LINE LEAKING ABOVE UNION AT ENGINE BRACKET, SECURED SAME.

Part: WATER SEPARATOR — DIRTY (CABIN)

F/A REPORTED, LAV SMOKE ALARM ON F/O SIDE WENT OFF AND WOULD NOT STOP. SMELLED SMOKE LATER, REPORTED IT SMELLED ELECTRICAL. INSPECTED RIGHT AFT LAV, NOTHING FOUND. REPLACED SMOKE DETECTOR, WATER SEPARATOR BAGS AND PERFORMED CROSS OVER DUCT BURNOUT PROCEDURE PER M/M 36-10-00 PG 507 TO 508, RAN PACKS AND ALL CHECKS OK.

Part: HYD LINE — SPLIT (NR 2 ENGINE)

ON DEPARTURE (ABOUT 12,000 FEET), RT HYDRAULIC PRESSURE LOW MESSSAGE AND INDICATOR LIGHT ON FORWARD INSTRUMENT PANEL ILLUMINATED. BOTH RT HYDRAULIC PRESSURE AND QUANTITY READ ZERO. RETURNED TO ATLANTA. FOUND RT ENGINE HYDRAULIC RETURN FLEX LINE LEAKING AT FILTER MODULE. REPLACED LINE, BLED HYDRAULIC SYSTEM AND SERVICED. LEAK CHECK OK.

Part: HOSE — LEAKING (RT HYD SYS)

SHORTLY AFTER TAKEOFF USING NORMAL POWER, THE FLIGHT ATTENDANTS REPORTED THE SMELL OF SMOKE THROUGHOUT THE CABIN. FOUND HYD LEAK IN RT SIDE TAIL COMPARTMENT. HOSE MFG NR AS153-08-0254. REPLACED HOSE RETURNED TO SERVICE.