N953DL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,403 hrs · 55,912 cycles

OVERHEAD EMERG LIGHTS INOP 10-26, 27-33. R/R BATTERIES IN EMERG BATT PACKS OVERHEAD BIN 10,27,33. LIGHTS NOW OP NML. ALL WORK PER MD88 AMM 33-53. (LP4695976)

Part: CABLE — CORRODED (TAILCONE) · airframe 75,160 hrs · 55,688 cycles

CORROSION ON TAILCONE INTERNAL PULL CABLE NR 28 AT FITTING. REPLACED AND ADJUSTED CABLE PER AMM 53-53-00. (LP0766216)

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,476 hrs · 55,114 cycles

EMERGENCY LIGHTS AT ROWS 11, 13, AND 15 INOP. REMOVED AND REPLACED BATTERIES OF BATTERY PACK B5-101 IN REF TO AMM 33-53. CHECKS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,476 hrs · 55,114 cycles

EMERGENCY LIGHTS AT L1 DOOR, COCKPIT, AND R1 DOOR INOP. REMOVED AND REPLACED BATTERIES OF BATTERY PACK B5-23 IN REF TO AMM 33-53. CHECKS GOOD.

Part: LINE — LEAKING (THRUST REVERSER) · airframe 74,034 hrs · 54,754 cycles

WAX LIKE BURNING ODOR IN THE AFT CABIN DURING DESCENT AND APPROACH, DISSIPATED ON LANDING. PERFORMED ODI PREVENTION AND FOUND A SMALL LEAK OUT OF THE RT THRUST REVERSR VALVE LINE. TIGHTENED THE LINE AND OPS OK. C/W AMDS CARDS 2120-2367, 4950-2815, 4900-2215, AND 2170-4139.

Part: ENGINE — MAKING METAL · airframe 72,788 hrs · 53,760 cycles

LEFT ENGINE SHUT DOWN, AN EMERGENCY WAS DECLARED. CREW FELT COMPRESSOR STALL AT 7000 FT. DURING CLIMB OUT, WITH NO ABNORMAL ENG PARAMETERS. APPROXIMATELY ONE MINUTE LATER, ANOTHER COMPRESSOR STALL, ENGINE ROLL BACK. IAW QRH SHUT DOWN ENGINE. MAINTENANCE FOUND METAL IN TAIL PIPE. ENGINE CHANGED.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 72,648 hrs · 53,644 cycles

AIR TURNBACK DUE TO THE LEFT AFT LAVATORY SMOKE DETECTOR SOUNDED SHORTLY AFTER PASSING THROUGH 18,000 FT DURING CLIMB. NO SMOKE OR FUMES WERE OBSERVED. SMOKE DETECTOR SILENCED AROUND 10,000 FT DURING DESCENT. REPLACED AFT LEFT LAVATORY SMOKE DETECTOR. REMOVED DETECTOR DID SOUND OFF SEVERAL TIMES OUTSIDE OF LAV. INSPECTED LAVATORY AND SURROUNDING AREAS. NO DEFECTS NOTED. NO SMOKE OR FUME REPORT BY FLIGHT CREW. PRESSURIZED AIRCRAFT AND PERFORMED NOGO ODI TASK LIST. NO DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,644 hrs · 53,640 cycles

EMERGENCY LIGHTS BATTERY PACK B5-23 INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-53-00.

Part: SKIN — CORRODED (BS 465) · corrosion level 2 · airframe 72,630 hrs · 53,630 cycles

FUSELAGE SKIN HAD POPPED FASTENERS AND PILLOWING AT BS 465, LONGERON 30L. REPAIRED IAW ER/A 560971-14.

Part: DOOR SILL — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 72,630 hrs · 53,630 cycles

AFT CARGO DOOR SILL CORRODED AT THE LOWER ZEE ANGLE NEAR FWD AND AFT DOOR STOPS. REPAIRED IAW ER/A 561446-14.

Part: CAM — WORN (TAILCONE RELEASE) · airframe 72,630 hrs · 53,630 cycles

TAIL CONE RELEASE CAM IS WORN. HAS A GROOVE IN THE RAMP AREA. REPLACED CAM ASSY.

Part: CAM — WORN (TAILCONE RELEASE) · airframe 72,630 hrs · 53,630 cycles

TAIL CONE RELEASE CAM IS WORN. HAS A GROOVE IN THE RAMP AREA. REPLACED THE CAM ASSY.

Part: DOOR SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 72,630 hrs · 53,630 cycles

FWD CARGO DOOR SILL HAS PILLOWING AT LOWER ZEE ANGLE BETWEEN STOPS. REPAIRED IAW SRM 53-05, FIG 44A.

Part: DOOR SILL — CORRODED (MID CARGO) · corrosion level 2 · airframe 72,630 hrs · 53,630 cycles

MID CARGO DOOR SILL HAS CORROSION AT LOWER ZEE ANGLE BETWEEN STOPS AND FWD OF FWD STOP. REPAIRED THE DOOR SILL IAW SRM 53-05, FIG 123, OPTION 2.

Part: DOOR FRAME — CORRODED (MID CARGO) · corrosion level 2 · airframe 72,630 hrs · 53,630 cycles

MID CARGO DOOR FRAME CORRODED JUST IN FRONT OF THE LOWER AFT DOOR FRAME STOP. REMOVED DAMAGE AND REPAIRED IAW SRM 53-05, FIG 123, OPTION 2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,661 hrs · 52,148 cycles

BOTH VENTRAL STAIR LIGHTS INOP. RELAMPED, OPS NORMAL.

Part: BATTERY PACK — MALFUNCTIONED (CABIN) · airframe 70,373 hrs · 51,936 cycles

EXTERIOR EMERGENCY LOWERING LIGHTS INOPERATIVE. RESET BATTERY PACK EMERGENCY LIGHT IAW AMM 33-53. OPERATED EMERGENCY LIGHTS, WORKS NORMAL , OK FOR SERVICES.

Part: SKIN — DAMAGED (BS 1193) · airframe 67,380 hrs · 49,795 cycles

FUSELAGE EXTERIOR, EIGHT DAMAGED FASTENERS AFT AT BS 1193 LONGERON NR 1. REPAIRED IAW ERA 538516-14AD, REV A.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 66,324 hrs · 49,054 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 22DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND WIRES BROKEN IN THE HARNESS. THE WIRE HARNESS WAS REPLACED AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 65,906 hrs · 48,805 cycles

MAINTENANCE FOUND SEAT 19ED EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND WIRING HARNESS DAMAGED AND REPLACED SAME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,372 hrs · 48,457 cycles

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

Part: OIL SYSTEM — OVERTEMP (NR 1 ENGINE) · airframe 64,369 hrs · 47,697 cycles

EXECUTED A DIVERSION, DUE TO HIGH OIL TEMP ON NR 1 ENGINE. AS HIGH AS 198 DEGREES. CREW SHUTDOWN ENGINE. MCD CHECKED GOOD, OIL FILTER CLEAN , TEMP DECALS INDICATE NORMAL. ENGINE CHANGED DUE TO OIL TEMP.

Part: RELEASE CABLE — KINKED (TAILCONE) · airframe 62,559 hrs · 46,461 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE CABLES WERE KINKED AND FRAYED BEYOND ALLOWABLE LIMITS. THE CABLES WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: SEAT TRACK — CORRODED (BS 1024-1030) · corrosion level 2 · airframe 62,559 hrs · 46,461 cycles

CORROSION ON SET A TRACKS, X=54 BETWEEN BS 1024 TO 1030 AT PAX CABIN. SEAT TRACK REPAIRED IAW SRM 53-05 FIG 4F.

Part: LONGERON — CRACKED (BS 1446 L6R) · airframe 62,559 hrs · 46,461 cycles

CRACKED LONGERON 6R AT INTERSECTION WITH AFT CANTED FRAME BS 1446. LONGERON REMOVED. NEW SECTIONS INSTALLED IAW SRM 53-02, FIG 18, 51-10-3, PAR 21 AND 14, 51-30-2, 51-30-5, 51-10-4.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,557 hrs · 46,460 cycles

CRACKED LONGERON 3R AT INTERSECTION WITH AFT ACCESSORY COMPARTMENT FRAME BS 1437. LONGERON REMOVED & NEW LONGERON AND SPLICE INSTALLED PER IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,557 hrs · 46,460 cycles

CRACK ON LONGERON 12 LT AT STA Y=1437 IN AFT ACCESSORY COMPARTMENT. LONGERON CRACKED WAS REMOVED NEW LONGERON AND SPLICE WERE DRILLED AND ADJUSTED AREA AND REPAIR PARTS WERE TREATED AND PAINTED AND REPAIR PARTS (LONGERON AND SPLICE) WERE INSTALLED IAW IAW SRM 53-02, FIG 18.

Part: RIB — DAMAGED (HORIZONTAL STAB) · airframe 62,557 hrs · 46,460 cycles

ELONGATED HOLES ON CENTER TORSION BOX RIB AT HORIZONTAL STABILIZER. REPAIRED IAW ERA 517500-14, REV ORIG RII.

Part: FLOOR SUPPORT — CORRODED (BS 1212) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION ON FLOOR SUPPORT FROM BS 1212 BETWEEN LONG 28L-29R AT AFT CARGO COMPARTMENT. FLOOR SUPPORT REPLACED IAW DWG 5436660, REV B2 AND SRM 51-30-2.

Part: TORSION BAR — CORRODED (SPOILER) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION FOUND ON THE LT WING OTBD FLIGHT SPOILER TORSION BAR. TORSION BAR REPLACED IAW AMM 27-61-06 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: TORSION BAR — CORRODED (SPOILER) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION FOUND ON THE LT WING INBD FLIGHT SPOILER TORSION BAR. TORSION BAR REPLACED IAW AMM 27-61-06 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: SKIN — CRACKED (BS 423) · airframe 62,557 hrs · 46,460 cycles

AN EXTERNAL SKIN CRACK WAS FOUND AT THE FWD CARGO DOOR FRAME AFT CORNER AT BS 423 BETWEEN L27 - 28R. REPAIRED IAW SRM 53-05, FIG 105, 51-10-3 PAR 14 & 21 AND ER/A 514801-14AD.

Part: TORSION BAR — CORRODED (SPOILER) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION FOUND ON OTBD FLIGHT SPOILER TORSION BAR AT RT WING REAR SPAR. THE TORSION BAR REPLACED IAW AMM 27-61-06 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION FOUND IN THE COUNTERSINK HOLES ON FUEL TANK ACCESS PANEL 1367C ON THE LT WING. ACCESS PNAEL REPLACED IAW SRM 51-22-2A.

Part: TORSION BAR — CORRODED (SPOILERS) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION FOUND ON THE RT INBD FLIGHT SPOILER TORSION BAR. TORSION BAR REPLACED IAW AMM 27-61-06 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: SUPPORT — CORRODED (SPOILERS) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION FOUND ON THE INNER/OUTER TORQUE TUBE SUPPORTS OF THE RT INBD FLT SPOILER. THE INNER/OUTER TORQUE TUBE SUPPORTS WERE REPLACED AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: SUPPORT — CORRODED (SPOILERS) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION WAS FOUND ON THE INNER/OUTER TORQUE TUBE SUPPORTS OF THE LT OTBD FLIGHT SPOILER. THE INNER/OUTER TORQUE TUBE SUPPORTS WERE REPLACED AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: SUPPORT — CORRODED (SPOILER) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION WAS FOUND ON THE INNER/OUTER TORQUE TUBE SUPPORTS OF THE RT OTBD FLIGHT SPOILER. THE INNER/OUTER TORQUE TUBE SUPPORTS WERE REPLACED AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: SUPPORT — CORRODED (SPOILER) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION FOUND ON THE INNER/OUTER TORQUE TUBE SUPPORTS ON THE LT INBD FLIGHT SPOILER. REPLACED AND INSPECTION COMPLETE.

Part: MOUNT — CORRODED (BS 1307) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION WAS FOUND IN THE UPPER HOLE OF THE LT FORWARD ENGINE MOUNT AT BS 1307. THE CORROSION WAS WAS REMOVED/REPAIRED IAW SRM 54-04, FIG 12A.

Part: CUSP WEB — CORRODED (BS 872-876) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION FOUND ON LT CUSP WEB BETWEEN BS 872 - 876. REPAIRED IAW 511165-14MA.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION WAS FOUND IN THE COUNTERSINK BORES OF THE RT WING FUEL TANK ACCESS PLATE 1466C. CORROSION WAS REMOVED & REPAIRED IAW SRM 51-22-2A.

Part: ACCESS PANEL — DAMAGED (LT WING) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION FOUND IN THE COUNTERSINK HOLES OF FUEL TANK ACCESS PANEL 1365C ON THE LT WING. CORROSION REMOVED AND HOLES WERE TREATED IAW SRM 51-10-3-3B.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION WAS FOUND ON FRAME BS 1309 BETWEEN LONG 28 TO 30 RT IN THE AFT CARGO COMPARTMENT. THE FRAME WAS REPLACED ON NON-ROUTINE CARD NR 471.

Part: ACCESS PANEL — DAMAGED (WING) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION WAS FOUND IN THE COUNTERSINK HOLES OF FUEL ACCESS PANEL 1466C. CORROSION WAS REMOVED THE HOLES TREATED IAW SRM 51-10-3/3B.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION WAS FOUND ON THE COUNTERSINK HOLES OF THE LT WING FUEL TANK ACCESS PLATE 1365C. REPAIRED IAW SRM 51-22-2A.

Part: BOLT — CORRODED (ENGINE MOUNT) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

DURING SCHEDULED MX INSPECTION, CORROSION WAS FOUND ON THE LOWER ENGINE MOUNT BOLT AT THE RT YOKE. (MRB 54-049-02). THE LOWER BOLT AT RT YOKE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION WAS FOUND ON THE COUNTERSINK HOLES ON THE RT WING FUEL ACCESS PANEL 1478C. REPAIRED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

DURING SCHEDULED HEAVY MX, CORROSION WAS FOUND ON TWO COUNTERSINK HOLES OF LT FUEL TANK ACCESS PLATE 1365C. COUNTERSINK HOLES OF LT FUEL TANK ACCESS PLATE 1365C WERE REWORKED AND REPAIRED IAW SRM 51-22-2A.

Part: SEAT TRACK — CORRODED (BS 1215-1234) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

DURING SCHEDULED HEAVY MAINTENANCE, CORROSION WAS FOUND ON SEAT TRACK X=22 BETWEEN BS 1215-1234. DAMAGED SEAT TRACK SECTION REMOVED IAW SRM 51-30-1 AND 51-30-5 NEW SEAT TRACK AND SPLICE REPAIR WERE DRILLED TRIMMED TREAT AND PAINT IAW SRM 51-10-4 AND 51-10-3, PAR 21 AND 14 AND 53-05, FIG 4E.

Part: CUSP WEB — CORRODED (BS 712-721) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION WAS FOUND ON THE LT CUSP WEB BETWEEN BS 712-721, BETWEEN X=54 & X=60. DAMAGED AREA WAS CUT OUT, REPAIR PARTS WERE FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 53-05, FIG 131A-14, 51-10-3 PAR. 21,14, AND 51-30-2.

Part: CUSP WEB — CORRODED (BS 625-634) · corrosion level 2 · airframe 62,557 hrs · 46,460 cycles

CORROSION WAS FOUND DURING SCHEDULED INSPECTION AT THE LT CUSP WEB BS 654 TO 634 BETWEEN X=54 & X=60. REPAIRED IAW SRM 53-05, FIG 131A-14, 53-30-5 & 53-10-3 & PS 900-5-1 NR 4.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,557 hrs · 46,460 cycles

DAMAGED PAINT AND METALIZED ON BOTH SURFACES OF RUDDER. BOTH SURFACES OF RUDDER WERE REPAIRED AND PAINTED IAW SRM 51-70-1, AD PAR 23

Part: COVER — DAMAGED (RUDDER) · airframe 62,557 hrs · 46,460 cycles

DURING SCHEDULE HEAVY MX, EXPOSED MATERIAL WAS FOUND ON COVER 6508A ON THE RUDDER. COVER 6508A OF RUDDER WAS REPAIRED IAW SRM 51-70-1, AD PAR 23 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 62,557 hrs · 46,460 cycles

DURING HEAVY MAINTENANCE, DENTS WERE FOUND ON THE LOWER AND UPPER MIDDLE SECTION OF THE RT INBD T/E FLAP. DENTS ON THE LOWER SURFACE EXCEEDED ALLOWABLE LIMITS AND THE FLAP ASSY WAS REPLACED.

Part: LONGERON — CRACKED (BS 1418 L2L) · airframe 62,557 hrs · 46,460 cycles

CRACKED LONGERON 2L AT INTERSECTION WITH AFT ACCESSORY COMP. FRAME BS 1418. LONGERON WAS REMOVED AND A NEW AND SPLICE WERE INSTALLED IAW SRM 53-02, FIG 18, SHEET 2. REPAIR WAS IDENTIFIED IAW PS 900-9-1, NR 04. RII COMPLETED.

Part: LONGERON — CRACKED (BS 522) · airframe 62,557 hrs · 46,460 cycles

CRACKED LONGERON 4L BS 522. LONGERON REPAIRED IAW SRM 53-02, FIG 18 AND 53-14-2, FIG 3.

Part: SKIN — CRACKED (BS 1437) · airframe 62,557 hrs · 46,460 cycles

CRACK ON FUSELAGE SKIN, BS 1437 BETWEEN L3-4L. CRACK WAS REMOVED, DOUBLER FABRICATED, AND WAS INSTALLED IAW SRM 53-04 51-10-3, PAR 21/14.

Part: LONGERON — CRACKED (BS 275) · airframe 62,557 hrs · 46,460 cycles

CRACKED LONGERON 16L AT INTERSECTION WITH FRAME BS 275. CRACK TRIMED OUT AND WAS REPAIRED IAW SRM 51-30-5, 53-14-2, 51-10-3, PAR 14,21 AND 51-10-4, 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 200) · airframe 62,557 hrs · 46,460 cycles

CRACKED LONGERON 4L BS 200 AT PAX CABIN. REPAIR SPLICE, PRODUCTION SPLICE AND DAMAGED LONGERON SECTION WERE REMOVED IAW SRM 51-30-2, 51-30-5 AND MFG NEW SECTION LONGERON, ADJUSTED AND DRILLED AND INSTALLED IAW SRM 53-02, FIG 18, 51-10-4, 51-30-2, 51-30-5. RII COMPLETED BY FOIM 200802821AM DELTA ID 761273.

Part: PAN — DAMAGED (LAV SERVICE) · airframe 61,812 hrs · 45,900 cycles

AFT LAV SERVICE DOOR PAN DAMAGED AT LOWER CORNER OF PAN AT EDGE OF DOOR OPENING. REPAIRED IAW ER/A 513241-14 REV ORIGINAL.

Part: PIN — UNSECURE (DOOR SLIDE) · airframe 61,812 hrs · 45,900 cycles

DURING SCHEDULED MX, THE L1 DOOR EVACUATION SLIDE WAS REPLACED BECAUSE THE PARACHUTE PINS WERE DETERMINED TO BE LOOSE & NOT SECURE. NO OTHER DEFECTS WERE NOTED IN THE DISCREPANCY. AS A PRECAUTION, THE SLIDE ASSY WAS REPLACED AND THE REQUIRED INSPECTION WAS COMPLETED. ANY SHOP FINDINGS SHALL BE REPORTED SEPARATELY AS REQUIRED.

Part: CAM — LACK OF LUBE (TAILCONE RELEASE) · airframe 61,812 hrs · 45,900 cycles

DURING SCHEDULED MX, THE TAILCONE CAM BASE MECHANISM WAS DETERMINED TO BE WORN. CHECKED BEARING, ROLLERS, CAM RAMPS. MINIMUM WEAR NOTED. LUBRICATED CAM MECHANISM. CHECKED TORQUE ON CAM ASSY AMM 53-53-02 AND AMDS 5330-01077-0101 STEP 7.

Part: RECEPTACLE — WORN (TAILCONE) · airframe 61,812 hrs · 45,900 cycles

DURING SCHEDULED MX, THE LT AND RT TAILCONE LATCH RECEPTICLES WERE FOUND TO BE WORN. REPLACED LATCH RECEPTICLES IAW AMM 53-53.

Part: CLAMP — OUT OF POSITION (TAILCONE) · airframe 61,812 hrs · 45,900 cycles

DURING SCHEDULED MX, THE TAILCONE LOCKING CABLE CLAMP DOES NOT CLEAR CONDUIT BY .5" AS REQUIRED IAW STEP 4.D.5. REPOSITIONED CABLE CLAMP CONDUIT TO OBTAIN .5" MINIMUM CLEARANCE IAW AMDS 5350-01077-0101, STEP 4.D.5.

Part: BLOCK — WORN (TAILCONE CABLE) · airframe 61,812 hrs · 45,900 cycles

DURING SCHEDULED MX, THE LT AND RT TAILCONE CABLE SLIDER BLOCKS WERE FOUND TO BE WORN. REPLACED SLIDER BLOCKS IAW AMM 53-53. REQUIRED INSPECTION COMPLETED.

Part: PIN — WORN (TAILCONE RELEASE) · airframe 61,812 hrs · 45,900 cycles

DURING SCHEDULED MX, THE TAILCONE RELEASE MECHANISM TEE PIN WAS FOUND TO BE WORN. REPLACED TEE PIN IAW AMM 53-53.

Part: SKIN — CRACKED (BS 1418) · airframe 61,812 hrs · 45,900 cycles

FUSELAGE SKIN CRACKED BS 1418 BETWEEN L2-3R COMING FROM FASTENER HOLE. REPAIRED IAW ER/A 513204-14AD.

Part: SKIN — CRACKED (BS 1437) · airframe 61,812 hrs · 45,900 cycles

FUSELAGE SKIN CRACKED BS 1437 BETWEEN L2R AND L3R COMING FROM FASTENER. REPAIRED IAW ER/A 513202-14.

Part: LONGERON — CRACKED (BS 1418 L2R) · airframe 61,812 hrs · 45,900 cycles

DURING SCHEDULED MX, A LONGERON WAS FOUND TO BE CRACKED AT BS 1418, L2R. DAMAGED PORTION OF LONGERON & SPLICE REPLACED IAW SRM 53-02.

Part: LONGERON — CORRODED (28R) · airframe 61,812 hrs · 45,900 cycles

DURING SCHEDULED MX, AFT CARGO DOOR FRAME LONGERON 28R WAS FOUND TO BE CORRODED AT THE UPPER SURFACE OF LOWER LEG OF THE BEAM BETWEEN THE DOOR STOP FITTINGS. CORROSION WAS REMOVED AND MATERIAL REMAINING WAS FOUND TO BE WITHIN LIMITS AND DOUBLER REPAIRS WERE COMPLETED SRM 53-05, FIG 123.

Part: PAN — CRACKED (FUSELAGE) · airframe 61,812 hrs · 45,900 cycles

DURING SCHEDULED MX, UPPER PAN WAS FOUND TO BE CRACKED AT THE FWD LT OVERWING EXIT. INSTALLED DOUBLER AND MODIFIED SEAL DEPRESSOR IAW SRM 53-05, FIG 32.

Part: BOTTLE — LOW PRESSURE (SLIDE) · airframe 61,812 hrs · 45,900 cycles

DURING SCHEDULED MX, THE NR 2 LT SERVICE ENTRY SLIDE WAS NOTED TO HAVE BOTTLE PRESSURE WAS LOW & OUT OF LIMITS. THE SLIDE ASSY WAS REPLACED IAW AMDS WORKCARD 2500-4484 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 61,812 hrs · 45,900 cycles

DURING SCHEDULED MX, WHILE REPLACING THE LANYARD, THE GIRT BAR LATCHES FAILED STEP 2 OF THE CHECK OUT PROCEDURE. THE GIRT BAR LATCH FITTING WAS ADJUSTED IAW AMM 25-62-00 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: SPRING — WEAK (TAILCONE RELEASE) · airframe 61,812 hrs · 45,900 cycles

LT AND RT TAILCONE LOWER LATCH SPRINGS WERE FOUND TO BE WEAK DURING SCHEDULED INSPECTION. REPLACED LATCH SPRINGS IAW AMM 53-53.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,482 hrs · 45,676 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 16D AND SEAT 34D IN THE CABIN, WERE INOPERATIVE. MX FOUND A LOOSE PIN IN THE CONNECTOR, A NEW CONNECTOR WAS SPLICED IN, AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,179 hrs · 43,426 cycles

DURING PSV IN MSP THE FUSELAGE SKIN WAS FOUND BULGED/CORRODED APPROX STA 720, BETWEEN LONGERONS 29L AND 30. REPAIRED PER ER/A 496608-14.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 58,179 hrs · 43,426 cycles

MX NOTED A 1.6 INCH LONG CRACK COMMON TO THE OVERWING EMERGENCY EXIT DOOR PAN. REPAIR IAW ERA 496667-14.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 58,016 hrs · 43,302 cycles

AIRCRAFT HAS A PUNGENT ODOR THROUGH BOTH PATHS AND WAS EVIDENT THROUGHOUT GROUND OPS, APU, AND FLIGHT. ALL PASSENGERS COMPLAINED. MAINTENANCE FOUND FLEX LINE BETWEEN PYLON AND EDP FILTER MODULE IN TAIL COMPARTMENT LEAKING. REPLACED LINE PER M/N 29-01 AND LEAK CHECK WAS PERFORMED AND CHECK OK. CLEANED APU INLET WITH ALCOHOL AND PERFORMED DUCT BURN OUT. COALESCER BAGS WERE REPLACED PER OPN 5090.

Part: CONTROL VALVE — DISCONNECTED (LT MLG WW) · airframe 57,814 hrs · 43,161 cycles

IN BOUND CREW WROTE UP RIGHT BRAKE PEDAL HAS LITTLE OR NO RESISTANCE ON TAXI IN. THE RIGHT BRAKE SHOOK ENTIRE AIRCRAFT WITHOUT BRAKES BEING APPLIED. ALL PRESSURE NORMAL. MAINTENANCE FOUND RIGHT CONTROL VALVE OUTBOARD INPUT DISCONNECTED. BRAKE CONTROL VALVE GOOD. RECONNECTED RIGHT BRAKE CONTROL VALVE OUTBOARD INPUT. FOUND IN LEFT WHEEL WELL CABLE 96B TO BRAKE CONTROL VALVE BROKEN. REPLACED CABLE 96B PER OPN 2000, RII INSPECTED.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHTS) · airframe 57,029 hrs · 42,625 cycles

DURING LINE CHECK, MX FOUND EMERGENCY PATHWAY LIGHTAT ROW 21CD INOPERATIVE. MX FOUND WIRING HARNESS BROKEN. R & R HARNESS IAW MM. OPERATION CHECKS GOOD.

Part: LIGHT — INOPERATIVE (ROW 1-4) · airframe 56,310 hrs · 42,174 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHTS INOPERATIVE. MX REPLACED CEILING LIGHTS AT ROW 1-4 AND ALSO REPLACED A DEFECTIVE BATTERY AT ROW 27. OPS OF LIGHTS NOW CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,769 hrs · 41,804 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY PATH LIGHT AT 21ED INOPERATIVE. MAINTENANCE RE-LAMPED AND REPLACED PULLED PINS AND SEAT HARNESS. OPERATION OF LIGHT NOW CHECKS GOOD. (2010-D1256) (DLM88102865)

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,697 hrs · 41,762 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY LIGHT AT ROW 2 INOPERATIVE. MX REPLACED WIRE HARNESS IN SEAT AND OPERATION OF LIGHTS NOW CHECKS OK.

Part: ENGINE — POWER LOSS (NR 2) · airframe 51,165 hrs · 38,809 cycles

ON CLIMB-OUT FLT LEVEL 175, NR 2 ENGINE SHUTTERED, FLT CREW FOLLOWED ENGINE FAILURE PROCEDURES AND SHUT NR 2 ENGINE DOWN.

Part: ACM — INOPERATIVE · airframe 49,469 hrs · 37,616 cycles

AT FL 200 LOST PRESSURIZATION WITH FLOW LIGHT PRESSURIZATION SYSTEM MTC IN PROGRESS. REPLACED LT AND RT ACMS REF ITEM 8 AND 9 THIS LOG. PERFORMED VALVE CK OUT AN OPN 5089. CKS NML PER MCC REPLACED S1-115 AND C WIRING FROM S1-119, S1-121, S1-115, TO S1 113. NO FAULTS NOTED. REPLACED APU ECU FOR PRECAUTION HRS 6297 CYC 13 NO FAULTS NOTED. AT REMOVAL, ON LT PACK REPLACED COMPR DISCHARGE TEMP SENSOR TURBINE INLET SENSOR AND CABIN 190 DEG PER MM. ALL CKS OK. PRESSURIZED TO 3 PSI WITH BOTH PACKS OPN NML. ALL CKS OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 49,282 hrs · 37,482 cycles

BOTH LAV SMOKE DETECTORS BEEPED ON FINAL, F/A REPORT NO INDICATIONS OF SMOKE OR FIRE, HAD SMOKE ODOR IN COCKPIT FOR A FEW MOMENTS.

Part: CHANNEL — CRACKED (VENTRAL STAIR) · airframe 48,052 hrs · 36,721 cycles

DEFORMED AND CRACKED C CHANNELS ON LT VENTRAL STAIRWAY PANEL. REPLACED CHANNELS PER DWG 5910395.

Part: BRACKET — CRACKED (BS 1463) · airframe 48,052 hrs · 36,721 cycles

CRACKED BRACKET ON FRAME AT STA Y=1463 CANT AT 10:30 POS. REPLACED BRACKET PER DWG 5920838.

Part: FRAME — CRACKED (BS 1463) · airframe 48,052 hrs · 36,721 cycles

FOUND CRACKED ANGLES ON FRAME AT STA Y=1463 AFT SIDE. REPLACED ANGLES PER SRM 53-14-4.

Part: SUPPORT BRACKET — CRACKED (BS 1503) · airframe 48,052 hrs · 36,721 cycles

CRACKED SUPPORT BRACKET AT FUSELAGE STRUCTURE STA Y=1503 CANT PROJECTION OF LONG 17R. REPLACED BRACKET PER DWG 5930556.

Part: STRUCTURE — CRACKED (TAIL CONE) · airframe 48,052 hrs · 36,721 cycles

CRACKED LOWER TAIL CONE STRUCTURE. REPAIRED PER SRM 51-90-0D.

Part: RIB — CRACKED (RWS 448) · airframe 48,052 hrs · 36,721 cycles

CRACK ON RT WING FIXED LEADING EDGE RIB ANGLE AT STA XOS=448. REPLACED ANGLE PER DWG 9919329.

Part: RIB — CRACKED (RWS 455) · airframe 48,052 hrs · 36,721 cycles

CRACK ON RT WING FIXED LEADING EDGE RIB ANGLE AT STA XOS=455. REPLACED ANGLE PER DWG 9919329.

Part: SKIN — CRACKED (BS 1309 S6-7R) · airframe 48,052 hrs · 36,721 cycles

CRACK ON FUS SKIN STA 1309 BTW LONG 6R ANR 7R. REPAIRED PER SRM 53-04D.

Part: SEAT TRACK — CORRODED (BS 465) · airframe 48,052 hrs · 36,721 cycles

CORROSION ON SEAT TRACK AT STA Y=465 RBL54. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 498) · airframe 48,052 hrs · 36,721 cycles

CORROSION ON SEAT TRACK AT STA Y=498 RBL 54. REPLACED SEAT TRACK.

Part: CUSP WEB — CORRODED (BS 1155-1174) · airframe 48,052 hrs · 36,721 cycles

CORROSION IN RT CUSP WEB BTWN STA 1155/1174. REPAIRED PER SRM 51-70-4.

Part: SEAT TRACK — CORRODED (BS 469-533) · airframe 48,052 hrs · 36,721 cycles

CORROSION ON SEAT TRACK AT LBL 22 STA Y=469 TO 471, 485/487501/502, 515/518, 530/533. REPLACED SEAT TRACKS.

Part: CUSP WEB — CORRODED (1117-1148) · airframe 48,052 hrs · 36,721 cycles

FOUND AT HMV-3 CORROSION ON RT CUSP WEB BTWN STA 1117 AND 1148. REPAIRED PER 51-70-4.

Part: ANGLE — CRACKED (BS 984-1003) · airframe 48,052 hrs · 36,721 cycles

CRACK ON RT WINDOW RING PANE BTW STA 984 AND 1003 RT FWD LOWER CORNER. REPAIRED PER SRM 56-01D

Part: ANGLE — CRACKED (BS 1231-1250) · airframe 48,052 hrs · 36,721 cycles

CRACK ON AFT UPPER WINDOW RING PAN BTW STA Y=1231 AND 1250 LT. REPAIR ANGLE PER SRM DRD 56-01.

Part: ANGLE — CRACKED (BS 1193-1212) · airframe 48,052 hrs · 36,721 cycles

CRACKED LT WINDOW RING PAN BTWN STA Y=1193 TO 1212. REPAIRED PER SRM DRD 56-01D.

Part: ANGLE — CRACKED (BS 1021) · airframe 48,052 hrs · 36,721 cycles

CRACKED LT WINDOW RING PAN AT STA Y=1021. REPAIRED PER SRM DRD 56-01.

Part: ANGLE — CRACKED (BS 1022-1041) · airframe 48,052 hrs · 36,721 cycles

CRACKED LT WINDOW RING PAN BTWN STA Y=1022/1041. REPAIRED PER SRM DRD 56-01D.

Part: ANGLE — CRACKED (R1 DOOR) · airframe 48,052 hrs · 36,721 cycles

CRACK ON RT FWD SERVICE DOOR R1 AT AFT UPPER CORNER OF BEAM NR 1 ANGLE. REPLACED ANGLE PER DWG 9919579.

Part: ANGLE — CRACKED (BS 1338) · airframe 48,052 hrs · 36,721 cycles

CRACKED STIFFENER ANDLE ON P-DOME AT STA Y=1338. REPLACED ANGLE PER DOUGLAS DWG 9915558.

Part: CUSP WEB — CORRODED (BS 1212-1250) · airframe 48,052 hrs · 36,721 cycles

EXFOLIATON CORROSION ON LT CUSP WEB AT STA Y=1212 TO 1230, 1233 TO 1250. REPAIRED PER SRM 51-70-4.

Part: INTERCOSTAL — CORRODED (BS 1321) · airframe 48,052 hrs · 36,721 cycles

GALVANIC CORROSION ON AFT FLOOR STRUCTURE INTERCOSTAL BETWEEN STA Y=1321 AND X=0. REPLACED INTERCOASTAL PER DOUGLAS DWG 9936705.

Part: ANGLE — CORRODED (BS 160) · airframe 48,052 hrs · 36,721 cycles

EXFOLIATION CORROSION ON WEB AT FWD CABIN STRUCTURE STA Y=160 LBL 14 TO 54. REPLACED ANGLE PER DWG 9955780.

Part: BRACKET — CORRODED (L2 DOOR GIRT BAR) · airframe 48,052 hrs · 36,721 cycles

EXFOLIATION CORROSION ON L2 DOOR GIRT BAR SUPPORT BRACKETS. REPLACED BRACKETS PER SRM 51-30-2 / 51-20-0.

Part: CUSP WEB — CORRODED (BS 1136-1174) · airframe 48,052 hrs · 36,721 cycles

EXFOLIATION CORROSION ON LT CUSP WEB AT STA Y=1136 TO 1174. REPLACED WEB PER BOEING DWG 9930612.

Part: CUSP WEB — CORRODED (BS 522-598) · airframe 48,052 hrs · 36,721 cycles

EXFOLIATION CORROSION ON LT CUSP WEB FROM STA Y=522 TO 598. REPLACED WEB PER SRM 51-10-3D.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 47,981 hrs · 36,677 cycles

EXFOLIATION CORROSION ON FWD FLOOR PANEL UNDER 61 POTABLE WATER PIPING CONNECTION PANEL. REPAIRED PER SRM 51-70-4.

Part: DUCT — CONTAMINATED (AIR DISTRIBUTION) · airframe 47,490 hrs · 36,336 cycles

DURING PUSHBACK AFT SMOKE DETECTORS WENT OFF WITH A SLIGHT ODOR OF SMOKE IN CABIN. FOUND SMALL AMT OF SYDROL STAINS IN APU INLET CLEANED SAME PERFORMED OPN 5090 ALT DUCT BURNOUT AND PERF OP 7804 WATER BAG REPLACED. RAN A/C SYSTEMS NO ODORS OR SMOKE PRESENT OK FOR SVC

Part: LINE — LEAKING (HYD SYSTEM) · airframe 46,158 hrs · 35,469 cycles

RT HYD QTY WENT TO 1 QT AT CRUISE FL240 QTY RETURNED TO 10 QT AFTER RT ENGINE DRIVEN HYD PUMP SHUTDOWN IAW QRH. LOST RT SYS PRESSURE DURING CONFIG FOR LANDING. USED ALTERNATE GEAR EXTENSION AND STOPPED ON RUNWAY FOUND PRESSURE FLEX LINE FROM NR 2 ENG TO PYLON LEAKING. REPLACED SAME. RAN ALL HYD SYSTEMS. NO LEAKS. RESERVICED RT HYD SYSTEM TO FULL. RT SYSTEM NEVER FULLY DEPLETED. CHECKED OPERATION OF ELECTRIC AND ENGINE DRIVEN PUMPS ALL CHECKS GO REPLACED MLG DOOR SKIDS ON BOTH DOORS.

Part: SKID — MISSING (LT ML DOOR) · airframe 44,277 hrs · 34,169 cycles

ON ARRIVAL FOUND THAT THE LEFT MLG DOOR SKID MISSING. REMOVED AND REPLACED GEAR DOOR AND SWING PER M/M 32-12-01-201.

Part: ADC — FAILED (E/E BAY) · airframe 40,729 hrs · 31,740 cycles

AFTER TAKEOFF, CAPT AIRSPEED WAS DECREASING, CAPT ALTIMETER STUCK AT FIELD ELEVATION. F/O AIRSPEED INDICATING ZERO, GPWS ALERT SOUNDING CONSTANTLY. REPLACED CADC.

Part: HYDRAULIC LINE — CHAFED (HYD SYSTEM) · airframe 39,254 hrs · 30,684 cycles

ON TAXI OUT SMOKE WAS SEEN COMING OUT OF RIGHT REAR OF A/C. RIGHT HYDRAULIC PRESSURE 0, RIGHT HYDRAULIC QUANTITY 2. PINNED GEAR, TAXIED BACK TO GATE. INSP RIGHT REAR OF A/C, NO EVIDENCE OF SMOKE OR FIRE. FOUND RT ENG HYDRAULIC FLEX LINE BETWEEN PYLON AND FILTER ASSY CHAFED THROUGH ON FASTENER. REPLACED LINE AND SERVICED HYDRAULIC RSVR TO FULL. RAN ENGS PER PFHB, LEAK CHECK NORMAL, QTY NORMAL, A/C OK FOR SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 38,007 hrs · 29,881 cycles

ROWS 10-13 EMERGENCY LIGHTS INOP. REPLACED PWR SUPPLY AND BATTERY PACK.

Part: TRANSMITTER — FAILED (LT HYD SYSTEM) · airframe 34,816 hrs · 27,703 cycles

ON APPROACH, LT HYD PRESS LOW MESSAGE APPEARED ON OAP AND LT HYD PRESSURE INDICATION DROPPED TO ZERO. PERFORMED ABNORMAL CHECK LIST PER POM. AFTER LANDING REVERSER UNLOCK AMBER LIGHT ILLUMINATED EVEN AFTER REVERSERS WERE STOWED. INSPECTED CASE DRAIN AND PRESSURE FILTERS FOR CONTAMINATION, NONE NOTED. REPLACED LT HYD SYS PRESSURE TRANSMITTER, ALL INDICATIONS NOW NORMAL.

Part: HYDRAULIC LINE — RUPTURED (HYD SYSTEM) · airframe 34,131 hrs · 27,211 cycles

RT ENG PRESSURE LINE IN AFT COMPARTMENT RUPTURED CAUSING RT SYS FAILURE AND LT GEAR DOOR DAMAGE ON LANDING. FOUND NR 2 ENG HIGH PRESSURE FLEX LINE BURST JUST BEFORE HIGH PRESSURE FILTER MODULE AND ADEL CLAMP BROKEN ON HYDRAULIC LINE WHERE IT MEETS THE FLEX LINE. REPLACED FLEX LINE AND BROKE CLAMP REF M/M. NEED LEAK CHECK. LEAK CHECK FLEX LINE. REPLACED RIGHT SYS ELECTRIC HYD PUMP AND RIGHT SYS FILTERS PER M/M. NO METAL NOTED AND FLUID IS CLEAN. LEAK CHECKS OK.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,734 hrs · 26,902 cycles

DURING HMV-2 DENTS WERE FOUND IN THE FUSELAGE SKIN FROM FS 275 TO 330 AT APPROX L20R. REPAIRED PER ERA 413006-14.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 33,732 hrs · 26,901 cycles

DURING HMV THE 9952521-12, -71, AND -84 FLOOR PANELS WERE FOUND DAMAGED. REPAIR PER ER/A 411064-14.

Part: SOCKET — DAMAGED (CABIN) · airframe 31,049 hrs · 24,956 cycles

ON INSPECTION FOUND EMERGENCY PATH LIGHT AT SEAT 2C INOP. FOUND LAMP SOCKET AND SEAT WIRING DAMAGED. REPLACED LAMP SOCKET AND SEAT ELECTRICAL HARNESS. OPN OF LIGHT NORMAL.

Part: BATTERY PACK — INOPERATIVE (AFT CABIN) · airframe 28,830 hrs · 23,345 cycles

ON INSPECTION, FOUND EMERGENCY EXIT TRACK LIGHTING OUT FROM OVERWING TO BACK OF CABIN. REPAIRED BROKEN WIRES AND REPLACED BATTERY PACK, CKS GOOD.

Part: POWER SUPPLY — INOP (ROW 24-33)

ON INSPECTION, FOUND EMERGENCY PATH LIGHTS FROM ROWS 24 TO 33 WOULD NOT TEST. REPLACED AFT POWER SUPPLY, OPS OF LIGHTS NORMAL.

Part: LUG — CRACKED (RT MLG STRUT)

DURING COMPLETION OF TRANS 9T149AD, RT MLG INSPECTION FOUND RT MLG PISTON I/B LUG RADIUS CRACKED. REPLACED STRUT ASSY.

Part: PRESSURE SYST — MALFUNCTIONED (CABIN)

LOST BOTH AUTO PRESS DESCENDING THROUGH FLT 230. UNABLE TO CONTROL CABIN ALT, CABIN O2 MASK DEPLOYED.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS FWD OF CABIN DIVIDER INOP. REPLACED FWD BATTERY PACK IN F/C OVERHEAD EMERGENCY EXIT LIGHTING SYSTEM, OPS CHECKS GOOD AND TESTS GOOD.

Part: ENGINE — FLAMED OUT (NR 2)

IN FLIGHT THE NR TWO ENGINE FLAMED OUT. THE ENGINE OVER TEMPED ON RESTART 720 C FOR 10 SEC. REPLACED ENGINE.

Part: COWL — DENTED (LT ENGINE)

L/E RING HAS DENT AT 9 O'CLOCK POS. REPAIRED PER SRM 54-04. FOUND DURING SHOP INSPECTION FOR NR 1 INTAKE COWL.

Part: RDMI UNIT — MALFUNCTIONED (FLIGHT DECK)

ON CLIMBOUT, HAD ATTITUDE FAIL ON COPILOTS, PRIMARY FLIGHT DISPLAY AND CAPTAINS RDMI. REPLACE TE NR 2 ATTITUDE HEADING REFERENCE SYSTEM. OPERATION NORMAL.