N610DL

Part: LATCH — FAILED (OXYGEN MASK DOOR) · airframe 92,914 hrs · 43,465 cycles

SHIP 610, DURING PASS OXYGEN DOOR DEPLOYMENT TEST THE FOLLOWING DOORS FAILED TO OPEN. 20ABC, 21ABC, 27DEF, 29ABC, 33ABC, 38ABC, 41DEF. REPLACED AFFECTED DOORLATCH ACTUATORS IAW AMM 35-21-06.

Part: LATCH — FAILED (OXYGEN MASK DOOR) · airframe 92,914 hrs · 43,465 cycles

MASKS FAILED TO DEPLOY WHEN LOSS OF CABIN PRESSURE -3A/B, 26ABC, 36DEF. REPLACED DOOR LATCH ACTUATORS 3A/B AND 26ABC. OPS CHECKED OK INCLUDING 36DEF. REF AMM 35-21-06 AND 35-21-00.

Part: CONTROLLER — FAILED (NR 1) · airframe 92,914 hrs · 43,465 cycles

AUTO INOP LIGHT ILLUMINATED WITH CABIN ALTITUDE, DEPLOYED PASSENGER OXYGEN MASKS. BITE CHECKED BOTH CABIN PRESSURE CONTROLLERS NR 1 FAULTS AC PWER LOSS REPLACED SAME. REPLACED UPPER POS PRESSURE RELIEF VALVE. PERFORMED O2 MASK DROP TEST INCLUDING ALT SWITCH IAW AMM 35-21. TESTED GOOD.

Part: LIGHT — INOPERATIVE (SEAT 1B) · airframe 92,723 hrs · 43,390 cycles

EMERGENCY LIGHT ABOVE SEAT 1B AND 4B INOPERATIVE, REPLACED LIGHT ASSY AT 1B AND FUSE ON POWER SUPPLY, OPS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,584 hrs · 43,347 cycles

EMERGENCY LIGHTS OUT AT ROW 40C. R & R AFT EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-51. OPS CHECKED GOOD.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 91,396 hrs · 42,936 cycles

SURFACE CORROSION FOUND ON LWR TCAS ANTENNA AND DOUBLER. REMOVED OLD DOUBLER AND CLEANED IAW SRM 43-00-01. PERFORMED DETAILED INSPECTION. TREATED AND PRIMED IAW PS 900-4-1-N2 AND 900-3-6N3 R/R TCAS ANTENNA DOUBLER IAW DELTA EO NR 6-59954-3, REV D. R & R TCAS ANTENNA IAW AMM.

Part: STANCHION — DAMAGED (RT SIDE) · airframe 90,552 hrs · 42,654 cycles

DURING OPS 25505, FOUND ONE STANCHION MISSING OFF RT SIDE OF RESTRAINT AFT OF DOOR. REPAIRED AND INSTALLED STANCHION IAW SRM 51-70-11, FIG 1.

Part: FILTER — LEAKING (NR 1 ENGINE) · airframe 90,497 hrs · 42,631 cycles

SUSPECTED LT ENG FUEL LEAK DUE TO FUEL CONFIG LIGHT ILLUM WITH 3.7 IN LT TANK AND 6.3 IN RT TANK. LT FUEL QTY DROPPING. MX REPLACED THE FUEL PUMP FILTER AND RAN ENGINE AT IDLE AND TAKEOFF POWER, NO LEAKS, CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 88,256 hrs · 41,811 cycles

DURING INSPECTION, MAINTENANCE DISCOVERED SEAT ROW 42D EMERGENCY LIGHTS INOPERATIVE. FOUND BROKEN LIGHT ASSY WIRING AND REPLACED LIGHT ASSY. OPERATES NORMAL.

Part: FLOOR SUPPORT — PUNCTURED (FUSELAGE) · airframe 86,411 hrs · 41,072 cycles

DUE ERA 49384-14MA TIME LIMITED REPAIR AT PUNCTURE AFT CARGO FLOOR STATION 1380. DRILLED UP REPAIR DOUBLER AND CLEANED UP HOLE PER ERA 489384-14MA REV C. HFEC INSP PER ERA 489384-14MA REV C. NO CRACKS FOUND. INSTALLED DOUBLER TO COMPLETE TEMP TIME LIMITED SEC II DOUBLER PER ERA 489384-14MA REV C.

Part: FLOOR SUPPORT — PUNCTURED (FUSELAGE) · airframe 86,411 hrs · 41,072 cycles

PUNCTURE IN AFT CARGO FLOOR CENTERLINE AT STA 1380. DRILLED UP REPAIR DOUBLER AND CLEANED UP HOLE PER ERA 489384-14MA. HFEC INSP PER ERA 489384-14MA REV C. NO CRACKS FOUND. INSTALLED DOUBLER TO COMPLETE TEMP TIME LIMITED SEC 11 DOUBLER PER ERA 489384-14MA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,790 hrs · 40,454 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE AFT TWO OVERHEAD COMPARTMENT EMERGENCY PATH LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD.

Part: UNKNOWN — ODOR (CABIN)

BURNED BALLAST SMELL NOTED IN OVERHEAD ABOVE SEAT 3DEF. TURNED LIGHTS OFF AND ODOR DISSIPATED. INSPECTED OVERHEAD LIGHTS, BALLASTS, PSUS AROUND ROW 31DEF. RAN BOTH ENGINES AND PACKS. ALL LIGHTS NORMAL. NO ODOR NOTED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,738 hrs · 39,113 cycles

DURING EMERGENCY EGRESS LIGHTING TEST, AISLE LIGHTING AT ROWS 39-44 FAILED AFTER ONE MINUTE. REPLACED AFT POWER SUPPLY AND BATTEY PACK, CHECKS OK.

Part: MOUNT — WORN (RT MLG DOOR) · airframe 77,063 hrs · 37,864 cycles

DURING HMV, THE RT MLG DOOR CENTER MOUNT FITTING, HINGE SUPPORT AND BRACKET ATTACHMENT HOLES WERE FOUND TO BE WORN AND ELONGATED. THE HOLES WERE CLEANED UP TO ROUND DIAMETERS AND OVERSIZE BOLTS WERE INSTALLED IN SOME OF THE HOLES.

Part: SKIN — CORRODED (BS 1510-1520) · airframe 77,063 hrs · 37,864 cycles

EXTERNAL SKIN AT BS 1510-1520 UNDER RT AIRPHONE ANTENNA HAS CORROSION. COMPLIED WITH AT SAA, SAT ON NON ROUTINE 81723520001.

Part: STRINGER — CORRODED (BS 1506 S28L) · airframe 77,063 hrs · 37,864 cycles

AFT CARGO FUSELAGE S28L BS 1506 HAS EXFOLIATION CORROSION C/W AT SAA - SAT ON NON ROUTINE 81720380001.

Part: SKIN — CORRODED (BS 1510, S28R) · airframe 77,063 hrs · 37,864 cycles

DURING HMV, CORROSION WAS FOUND UNDER THE AIRFONE ANTENNA BLANKING DOUBLER AT STA 1510, RT. THE CORRODED SKIN SECTION WAS CUT OUT AND AN SRM SKIN REPAIR WAS INSTALLED. A 12 MONTH DTA RESTRICTION WAS IMPOSED DUE TO CLOSE PROXIMITY OF ANOTHER EXISTING REPAIR DOUBLER.

Part: INTERCOSTAL — CORRODED (BS 1540-1560) · airframe 77,063 hrs · 37,864 cycles

AFT CARGO BETWEEN SAT, 1540 - SAT: 1560 BETWEEN STRINGERS S-26R AND S-27R FOUND SUPPORT WEB (INTERCOSTAL) WITH CORROSION AS MARKED C53-162-01L, COMPLIED WITH AT SAA-SAT ON NON ROUTINE 81721150001.

Part: SEAT TRACK — CORRODED (BS 1435 LBL48) · airframe 77,063 hrs · 37,864 cycles

CABIN COMPARTMENT FLOOR SEAT TRACK FOUND WITH CORRSION ON TOP SURFACE INBD FLANGE AT SAT, 1435 LBL48 AS MARKED W/L 208-10/COMPLIED WITH AT SAA -SAT ON NON- ROUTINE 81720150001.

Part: SILL — CORRODED (BS 1380-1440) · airframe 77,063 hrs · 37,864 cycles

AFT CARGO COMP BETWEEN BS 1380 TO 1440 RBL 21 HAS THE LOWER SILL OF NR 2 CARGO DOOR WITH SEVERAL CORRODED AREAS AT UPPER SURFACE, CP53-156-021/COMPLIED WITH AT SAA, SAT ON NON ROUTINE 81719980001.

Part: STRINGER — CORRODED (STA 1520 S29R) · airframe 77,063 hrs · 37,864 cycles

AFT CARGO BETWEEN STA, 1500 AND STA, 1520 STRINGER S-29R FOUND WITH CORROSION AS MARKED. COMPLIED WITH AT SAA, SAT ON NON-ROUTINE 8172105000.

Part: FITTING — CORRODED (AFT CARGO DOOR) · airframe 77,063 hrs · 37,864 cycles

FITTING AT BOTTOM OF AFT CARGO DOOR OPENING CORRODED ON BOTTOM STA 1400, NEW DOOR FITTING EXISTING PLATE AND NEW TIE DOWN FITTING INSTALLED IAW SRM 51-40-02 PG 39 FIG 12.

Part: SEAT TRACK — CORRODED (BS 1435) · airframe 77,063 hrs · 37,864 cycles

CABIN COMPT FLOOR SEAT TRACK FOUND WITH CORROSION ON TOP SURFACE INBOARD FLANGE AT BS 1435 LBL 48 AS MARKEDW/L08-10. COMPLIED WITH AT SAA- SAT ON NON ROUTINE 81720150001.

Part: O2 GENERATOR — DAMAGED (CABIN) · airframe 77,063 hrs · 37,864 cycles

FOUND ONE BLOWN OXYGEN CHEMICAL GENERATOR SN ARYD-F010-510 ON INSPECTION OF OXYGEN GENERATORS. COMPLIED WITH AT SAA- SAT ON N/R 81698450001 AND N/R 81707610001.

Part: FAILSAFE — CORRODED (BS 900) · airframe 77,063 hrs · 37,864 cycles

FAIL/SAFE STRAP CORRODED AT STA 900 SKIN BUTT JOINT BELOW WINDOW BELT RT SIDE OF FUSELAGE. COMPLIED WITH AT SAA SAT ON NON ROUTINE 81716550001.

Part: BELLMOUTH — CRACKED (APU INLET) · airframe 77,063 hrs · 37,864 cycles

DURING HMV, CRACKS WERE FOUND IN THE APU AIR INTAKE PLENUM BELLMOUTH. THE CRACKING WAS ADDRESSED IN BOEING SERVICE BULLETIN 757-49-0011 AND THE CRACKED BELLMOUTH WAS REPLACED WITH A MODIFIED BELLMOUTH ASSEMBLY AS DIRECTED BY THE SERVICE BULLETIN.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 76,746 hrs · 37,743 cycles

LIGHTNING STRIKE DAMAGE WAS FOUND IN THE FUSELAGE SKIN FORWARD OF STA 560 AT S-9R. THE DAMAGE WAS CUT OUT AND REPAIRED PER ER/A 06-450569-14 WITH BOEING APPROVAL.

Part: DUCT — CRACKED (WING) · airframe 75,310 hrs · 37,267 cycles

AT FLT LVL 240 WITH ENGINE AND WING ANTI-ICE ON LEFT ENG BLEED LIGHT ILLUMINATED. FOLLOWED QRH SHUT BLEED SW OFF. OPENED ISOLATION VLV AT FLT LVL 260 RIGHT ENGINE BLEED LIGHT ILLUM. CABIN PRESSURE CLIMBED THROUGH 10K DEPLOYED MASKS. DECLARED EMERGENCY INTO ORF. MTC FOUND SEAT ROWS 26 AND 27 DEF MASKS DID NOT DEPLOY. ALSO FOUND AFT RT LAV MASK DID NOT DEPLOY. MX HAS FOUND A DUCT IN THE UNDERWING SECTION CRACKED.

Part: SKIN — DAMAGED (BS 683 S4L) · airframe 71,862 hrs · 36,184 cycles

LIGHTNING DAMAGE IN FUSELAGE SKIN S-4L LAP SPLICE. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS.

Part: SKIN — LIGHTNING STRIKE (BS 878, S4R) · airframe 68,969 hrs · 35,157 cycles

REPAIR TO LIGHTNING STRIKE REQUIRED REMOVAL AND INSTALLATION WITH SOLID FASTENERS. CORRECTIVE ACTION PER ERA 450656-14 REV B.

Part: VALVE — MALFUNCTIONED (MLG) · airframe 68,470 hrs · 34,963 cycles

ON T/O FROM LGA, HAD DOOR LIGHT ILLUMINATE AND GEAR DOOR EICAS MSG WITH GEAR HANDLE UP, SAME LIGHT WHEN PUT GEAR DOWN T/S PER M/M CYCLED NOSE GEAR DOOR OPS NML. REPLACED DOOR, SAFETY VALVE PER M/M 32-35-23-004-001 AS PRECAUTIONARY MEASURE NEEDS OPS CHK. REMOVED AND REPLACED NOSE GEAR DOOR ACTUATOR PER AMM 32-34-03-004-037. ALL OPS NML. ALL LEAK CKS GOOD DOOR SAFETY VLV OPS NML. A/C OK FOR SERVICE.

Part: SKIN — CRACKED (L1 DOOR) · airframe 65,078 hrs · 33,815 cycles

SUPPLEMENTAL SDR FUSELAGE/SKIN L-1 DOOR CUTOUT/UPPER FWD CORNER-CRACK IAW ERA 090914-14. C/W ERA 090914-14.

Part: SKIN — LIGHTNING STRIKE (BS 878) · airframe 65,899 hrs · 34,159 cycles

LIGHTNING STRIKE DAMAGE TO THE FUSELAGE SKIN AT FS 878, ABOVE STRINGER 4R. DAMAGE TO OUTER SKIN ONLY AT A PRODUCTION FASTENER LOCATION. REPAIR DOUBLER INSTALLED TO REPAIR THE DAMAGE CUTOUT.

Part: SKIN PANEL — DAMAGED (BS 520) · airframe 65,899 hrs · 34,159 cycles

LIGHTNING STRIKE DAMAGE TO THE FUSELAGE SKIN AT FS 520 ABOVE STR 10R. INSTALLED REPAIR DOUBLER PER ER/A 450613-14.

Part: PSEU — FAULTY (E/E BAY) · airframe 60,221 hrs · 31,931 cycles

DIVERSION TO PHX - APPARENT GROUND PROX SYS ERROR-AT CRUISE ALT GOT F/O PITOT- RT AUX PITOT- TAT - A/T DISC - PROBE HEAT CAUTIONS. LEFT GREEN SIDE OF NOSE AND RIGHT MAIN GEAR LIGHTS ILLUMINATED. STATUS MSGS GROUND PROX SYS - LANDING GEAR MONITOR - NOSE A/G DISAGREE - AIR GROUND DISAGREE - CABIN TEMP HARD TO CONTROL TOO. FLT CREW GAVE AMT VERBAL REPORT OF FULL SPOILER DEPLOYMENT ON APPROACH RESULTING IN CONTROL DIFFICULTIES. CREW SUBSEQUENTLY STOWED SPOILERS. FOUND CARD 5 BAD IN PSEU. REPLACED PSEU. PERFORMED SUCCESSFUL TEST OF PSEU.

Part: FITTING — CRACKED (NR 2 PYLON) · airframe 57,754 hrs · 30,852 cycles

DURING ACCOMPLISHMENT OF EO 6-75079-3 OPN 0206, A CRACK WAS FOUND IN THE RIGHT WING UPPER LINK WING FITTING OUTBOARD LUG. REPAIRED PER ER/A 389433-14. BORE OVERSIZED AND OVERSIZED BUSHING INSTALLED.

Part: SILL — CORRODED (FUSELAGE) · airframe 57,754 hrs · 30,852 cycles

THE OUTER CHORD OF THE C2 DOOR OPENING WAS FOUND CORRODED. TO REMOVE THE CHORD, THE FS 1440 FRAME OUTER CHORD AND WEB WERE CUT AND THE LOWER ENDS REMOVED. A NEW SECTION OF SILL CHORD WAS INSTALLED, AND THE FRAME WEB AND CHORD SPLICED BACK IN PLACE WITH ALUMINUM REPAIR DOUBLERS. THE REPAIR WAS ACCOMPLISHED PER ER/A 384242-14, REV A.

Part: SKIN — DENTED (FS 1694, S-14L) · airframe 57,754 hrs · 30,852 cycles

FUSELAGE / SKIN / FS 1694 / STRG. 13L-15L : DENT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED ABOVE AN EXISTIN REPAIR FOR A SMALL CUTOUT. THE DENT WAS CUTOUT AND THE EXISTING REPAIR REMOVED. THE NEW AND EXISTING CUTOUTS WERE THEN REPAIRED WITH A SINGLE REPAIR DOUBLER/TRIPLER COMBINATION PER ER/A 384264-14, REV A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,754 hrs · 30,852 cycles

THE UPPER CAP OF THE FS 1681 FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION. TO REMOVE ALL OF THE DAMAGE, THE UPPER CAP WAS TRIMMED OFF FROM LBL 60 TO RBL 60. A NEW CAP WAS FABRICATED AND INSTALLED PER ER/A 384247-14, REV A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,754 hrs · 30,852 cycles

THE UPPER CAP OF THE FS 377 FLOORBEAM WAS FOUND CORRODED. THE UPPER CAP WAS TRIMMED OFF AND A NEW SECTION FABRICATED. DURING INSTALLATION OF THE NEW SECTION, SEVERAL ATTACH HOLES COMMON TO THE FS 377 FRAME AT LBL 65 WERE DAMAGED. THE AFFECTED HOLES WERE OVERSIZED, BUSHED, AND REPAIRED WITH AN ALUMINUM DOUBLER. THE REPAIRS WERE ACCOMPLISHED PER ER/A 384265-14, REV A.

Part: SILL — CORRODED (FUSELAGE) · airframe 57,754 hrs · 30,852 cycles

THE INNER CHORD OF THE LOWER SILL OF THE C1 DOOR OPENING WAS FOUND WITH CORROSION AND TOOLING DAMAGE. THE INNER CHORD WAS REMOVED AND DISCARDED. A NEW CHORD WAS INSTALLED PER ER/A 384233-14.

Part: SKIN — GOUGED (FS 600, S-26L) · airframe 57,754 hrs · 30,852 cycles

FUSELAGE / SKIN / FS 600 / STRG. 26L-27L : GOUGE REPAIR THE FUSELAGE SKIN WAS FOUND WITH 3 GOUGES AT FS 600 BETWEEN STRINGERS 26L & 27L. THE GOUGES WERE REMOVED WITH A SINGLE CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 384277-14.

Part: SUPPORT FITTING — DAMAGED (NR 1 PYLON) · airframe 57,754 hrs · 30,852 cycles

DURING COMPLETION OF PYLON MOD EO 6-70332-3AD, HOLE NR 2 IN LEFT WING SUPPORT FITTING HAD DAMAGE THAT REQUIRED REMOVAL PRIOR TO FASTENER INSTALLATION. REPAIRED PER ER/A 389426-14AD. REPAIR OVERSIZED HOLE, INSTALLED FREEZE PLUG, AND INSTALLED EO FASTENER.

Part: SUPPORT FITTING — TOOL DAMAGE (#1 PYLON) · airframe 57,754 hrs · 30,852 cycles

DURING ACCOMPLISHMENT OF PYLON MOD EO 6-70332-3AD, HOLE 5 IN THE LEFT WING SUPPORT FITTING HAD DAMAGE THAT REQUIRED REMOVAL PRIOR TO FASTENER INSTALLATION. REPAIRED PER ER/A 389427-14AD. REPAIR OVERSIZED HOLE, INSTALLED FREEZE PLUG, THEN INSTALLED FASTENER PER EO.

Part: FITTING — GOUGED (NR 2 PYLON) · airframe 57,754 hrs · 30,852 cycles

WHILE WORKING PYLON MOD EO 6-70332-3AD, HOLE NR 65 IN RIGHT WING SIDE LOAD FITTING WAS GOUGED. REPAIRED PER ER/A 389430-14AD. REPAIR OVERSIZED HOLE TO REMOVE DAMAGE AND INSTALLED OVERSIZED FASTENER.

Part: B-NUT — LOOSE (NR 2 ENGINE) · airframe 57,657 hrs · 30,798 cycles

FLIGHT DIVERTED TO DEN EN ROUTE TO SAN BECAUSE OF OIL LOSS IN THE RIGHT ENGINE. FOUND OIL LINE LEAKING AT FUEL/OIL HEAT EXCHANGER. TIGHTENED B-NUT ON LINE ALONG WITH ALL OTHER LINES GOING TO AND COMING FROM EXCHANGER. RAN ENGINE LEAK CKS OK. ENGINE WAS NOT SHUTDOWN INFLIGHT.

Part: ENGINE — DAMAGED (NR 1) · airframe 55,990 hrs · 29,948 cycles

ON TAKEOFF AT 140 KNTS AND 800 FT LEFT ENGINE LOST POWER DURING GEAR RETRACTION. ENGINE CONTINUED TO ROLLBACK AND SHUTDOWN. SURGE AND FLAME FROM INLET REPORTED BY PASSENGERS. CONTRACT MTC REPORTS METAL PARTICLES IN TAILPIPE. ENGINE WILL REQUIRE REPLACEMENT IN BNA. REPLACED ENGINE.

Part: ENGINE — SURGES (NR 2) · airframe 53,802 hrs · 28,901 cycles

RIGHT ENG SURGED ON TAKEOFF BETWEEN 80 AND 95 KTS. TWO LARGE SURGES AND DISCONTINUED AT 95 KTS. EPCS PAGE SHOWED P SVA F/B INT. T/S PER FIM. NO FAULTS IN CIRCUIT BETWEEN EEC AND SVA. CLEANED C/PS. RAN ENG TO T/O PWR REF PFHB. NO SURGES - SVA MSG DID NOT RE-APPEAR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,451 hrs · 28,272 cycles

ON INSPECTION FOUND ALL IN SEAT EMERGENCY PATH LIGHTS INOP IN FIRST CLASS. FOUND LIGHT SOCKET AT SEAT 2CD SHORTED. REPLACED LIGHT SOCKET AND POWER SUPPLY. OPN OF EMERGENCY LIGHT NORMAL PER MM.

Part: SMOKE ODOR — DETECTED (E/E BAY)

PASSING APPROX 10,000 FT FWD EQUIPMENT SMOKE EICAS, NOTICED CAUSTIC ELECTRICAL SMELL, BEGAN SMOKE AND FIRE PROCEDURE. EQUIPMENT OVERHEAT CAME ON IMMEDIATLY. DECLARED AN EMERGENCY AND REQUESTED APPROACH CLEARANCE. WENT TO EQUIP COOLING ALT, COMPLIED WITH PROCEDURE. NO VISABLE SMOKE, SMELL ONLY. SMOKE LIGHT ON OVERHEAD ALSO CAME ON. REPLACED SMOKE DETECTORS.

Part: SKIN — GOUGED (BS 1694)

THE FUSELAGE SKIN WAS FOUND WITH A BAD GOUGE AT FS 1694 BETWEEN THE STRINGER 14L SKIN LAP SPLICE AND STRINGER 15L. THE DAMAGE WAS CUTOUT WITH A 3.5 X 1 CUTOUT AND REPAIRED WITH AND EXTERNAL DOUBLER AND FILLER TO OVERLAP THE EXISTING LAP JOINT. THE REPAIR WAS ACCOMPLISHED PER ER/A 366716-14, REV A.

Part: SKIN — GOUGED (BS 620)

FUSELAGE SKIN FS 619-623 STRINGER 15-16, REPAIR FOR GOUGES. THE FUSELAGE SKIN WAS FOUND WITH TWO GOUGES BETWEEN FS 619 AND 623 AND BETWEEN STRINGERS 15 AND 16. BOTH GOUGES WERE CUT OUT OF THE SKIN WITH APPROX 2 BY 2 CUTOUTS. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER. INSTALLED PER ER/A 366676-14.

Part: FLOOR BEAM — CORRODED (STA 377 LBL54)

DURING HMV, INSPECTION FOUND FLOOR BEAM CORRODED AT STA 377 LBL 54 AT FASTENER HOLES. REPAIRED PER SRM 53-10-51.

Part: WEDGE — DAMAGED (NR 1 SLAT)

AT HMV, LEFT WING NR 1 SLAT WAS FOUND WITH DELAMINATION ON THE TRAILING EDGE WEDGE. REPLACED WEDGE PER SRM 57-43-02.

Part: PLATE OPENINGS — CORROSION (RT WING LWR SKIN)

AT HMV, FOUND ALL TANK PLATE OPENINGS IN RT WING LOWER SKIN TO HAVE FRETTING WEAR AND CORROSION. REMOVED CORROSION AND FRETTING DAMAGE PER SRM 57-20-01. ROTO PEENED TANK PLATE OPENINGS PER SRM 57-20-01. DYE CHECKED PER SRM 57-20-01. NO CRACKS FOUND.

Part: SKIN — LIGHTNING DAMAGE (STA 520 S-10L)

DURING HMV, INSPECTION FOUND UPPER FUSELAGE SKIN AREA AT STATION 520 STRINGER 10L TO BE BURNISHED BEYOND LIMITS, .25 INCH LIGHTNING STRIKE. REPAIRED PER SRM 53-00-01.

Part: WEDGE — DAMAGED (RT LE SLAT)

DURING HMV, NR CARD 125 WAS WRITTEN FOR HAIL DAMAGE ON THE T/E WEDGE OF THE NR 10 L/E SLAT. THE WEDGE WAS REPLACED PER SRM 57-43-02.

Part: WEDGE — DENTED (RT LE SLAT)

THE NUMBER NINE LEADING EDGE SLAT WAS FOUND TO HAVE HAIL DAMAGE DURING INSECTION AT HMV. NRC 124. REPAIRED BY REPLACING TRAILING EDGE WEDGE PER SRM 57-43-02.

Part: SKIN — CRACKED (LT SPOILER)

DURING SHOP INSPECTION, LEFT WING SPOILER PANEL WAS FOUND WITH 6 INCH CRACK ON LOWER SKIN AND A 2 INCH CRACK ON UPPER SKIN AT INBOARD END OF SPOILER. REPAIRED PER SRM 51-70-04.

Part: RADOME — DELAMINATED (NOSE)

INTERIOR AFT EDGE OF RADOME DELAMINATED AT 12 O'CLOCK POSTION. DAMAGE OCCURED WHILE INSTALLING RADOME IN HANGAR. REPAIRED AS PER SRM 53-10-72. REMOVED HINGES AND HINGE BRACKET, REPAIRED FIBERGLASS, INSTALLED BRACKET AND HINGES, AND PAINTED AS PER PS 900-9-1-11 NR 05. RETURNED RADOME TO A SERVICEABLE UNIT.

Part: WEDGE — DENTED (LT LE SLAT)

DURING INSPECTION, HAIL DAMAGE WAS FOUND ON NR 2 L/E SLAT WEDGE. REPLACED WEDGE PER SRM 57-43-02.

Part: RADOME — DELAMINATED (NOSE)

RADOME WAS ROUTED TO SHOP FOR REWORK, DUE TO DAMAGE FROM DELAMINATION AND MOISTURE ENTRAPMENT. REWORKED RADOME PER SRM 53-10-72.