N615DL

Part: LENS — MISINSTALLED (EMERGENCY LIGHT) · airframe 90,506 hrs · 41,739 cycles

R1 DOOR LOWER EMERGENCY EXIT IDENTIFIER ARROW IS POINTING IN THE WRONG DIRECTION. REPLACED R1 DOOR LOWER EMERGENCY EXIT IDENTIFIER WITH IDENTIFIER LENS WITH THE ARROW POINTING IN THE DIRECTION OF THE DOORWAY.

Part: SKIN — DAMAGED (BS 281) · airframe 88,692 hrs · 41,106 cycles

MX DISCOVERED A LIGHTNING STRIKE DAMAGE AT BS 281 AND EIGHTEEN INCHES ABOVE NOSE GEAR DOOR CUTOUT. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 327) · airframe 88,692 hrs · 41,106 cycles

MX DISCOVERED LIGHTNING STRIKE DAMAGE AT BS 327 AND TWO INCHES ABOVE S26L. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 327.5) · airframe 88,692 hrs · 41,106 cycles

MX DISCOVERED LIGHTNING STRIKE DAMAGE AT BS 327.5 AND S28L. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 348) · airframe 88,692 hrs · 41,106 cycles

MX DISCOVERED LIGHTNING STRIKE DAMAGE AT BS 348 AND FOUR INCHES ABOVE S26L. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 264) · airframe 88,692 hrs · 41,106 cycles

MX DISCOVERED A LIGHTNING STRIKE AT BS 264 AND 9" BELOW WINDOW FRAME. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 290) · airframe 88,692 hrs · 41,106 cycles

MX DISCOVERED LIGHTNING STRIKE DAMAGE AT BS 290 ABOVE NOSE GEAR DOOR CUTOUT. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 290) · airframe 88,692 hrs · 41,106 cycles

MX DISCOVERED A LIGHTNING STRIKE DAMAGE AT BS 290 AND NINETEEN INCHES ABOVE NOSE GEAR DOOR CUTOUT. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 313.5) · airframe 88,692 hrs · 41,106 cycles

MX DISCOVERED LIGHTNING STRIKE DAMAGE AT BS 313.5 AND S26L. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 282) · airframe 88,692 hrs · 41,106 cycles

MX DISCOVERED LIGHTNING STRIKE DAMAGE AT BS 282 AND FOUR INCHES ABOVE NOSE GEAR DOOR CUTOUT. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 348) · airframe 88,692 hrs · 41,106 cycles

MX DISCOVERED A LIGHTNING STRIKE AT BS 348 AND THREE INCHES BELOW S27L. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 300) · airframe 88,692 hrs · 41,106 cycles

MX DISCOVERED A LIGHTNING STRIKE DAMAGE AT BS 300 AND TWENTY ONE INCHES ABOVE NOSE GEAR DOOR CUTOUT. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 327.5) · airframe 88,692 hrs · 41,106 cycles

MX DISCOVERED LIGHTNING STRIKE DAMAGE AT BS 327.5 AND 17 INCHES ABOVE DOOR CUTOUT. REPAIRED IAW SRM 53-00-01.

Part: POWER SUPPLY — ODOR (E/E BAY) · airframe 87,544 hrs · 40,693 cycles

AIRCRAFT DIVERTED, DUE TO ACRID FUMES IN COCKPIT. FOUND THE 2R FLIGHT CONTROL ELECTRICAL POWER SUPPLY CIRCUIT BREAKER TRIPPED AND UNIT HAD ELECTRICAL ODOR. REPLACED THE 2R POWER SUPPLY AND THE 3R SCM PER AMM 27-09. CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 84,197 hrs · 39,454 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK WAS GOOD.

Part: SKIN — DENTED (BS 620 S16-17L) · airframe 80,284 hrs · 38,126 cycles

SKIN DAMAGED AT STA 600-620 BETWEEN STRINGER 16L AND 17L REPAIRED IAW ERA385158-14.

Part: SKIN — DENTED (FUSELAGE) · airframe 77,347 hrs · 37,151 cycles

RT LOWER FUSELAGE STA 1620 S26R 1EA DENT AND 1EA PROTRUDING DENT. C/W AT SAA - SAT OM N/R 106382 JOB 83163750001.

Part: INTERCOSTAL — CORRODED (STA 640-660) · airframe 77,347 hrs · 37,151 cycles

INTERCOASTAL HAS LOWER CORRODED IN FWD CARGO BILGE AREA BETWEEN STA 640-660,RBL 16 CP53-124-01L/C/W AT SAA - SAT ON N/R 133618 JOB 83170400001.

Part: SKIN — DENTED (NR 4 SLAT) · airframe 77,347 hrs · 37,151 cycles

LT WING NR 4 SLAT UPER SKIN SURFACE AT TRAILING EDGE HAS MULTIPLE DENTS HAIL DAMAGE. C/W AT SAA - SAT ON N/R 117666. JOB 83164050001.

Part: WEDGE — WORN (NR 7 SLAT T/E) · airframe 77,347 hrs · 37,151 cycles

NR 7 SLAT T/E WEDGE LOWER SURFACE FOUND WEAR MARK ON I/B SIDE.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 77,347 hrs · 37,151 cycles

AFTER REMOVAL OF STA 1380 LBL 8 FLOOR STRINGER CLIP FOUND CORRODED AT LOWER FASTENER HOLES. REPAIRED AT SAA SAT DURING HMV ON N/R CARD 121930.

Part: FLOORBEAM — CORRODED (BS 1681) · airframe 77,347 hrs · 37,151 cycles

WHILE REPLACING 1 EA NUTPLATE FOR FLOOR PANEL INSTALLATION FOUND CORROSION AT FASTENER HOLE BETWEEN DECK PLATE AND FLOORBEAM FLANGE STA 1681 RBL40. COMPLIED WITH ER/A 475621-14 REV ORIG DATED 07/08/09 AT SAA SAT ON N/R CARD 108718.

Part: SKIN — CORRODED (BS 740-770) · airframe 77,347 hrs · 37,151 cycles

RT FUSELAGE EXTERNAL SKIN HAS CORROSION AT LAP JOINT FROM STA 740-770 S19R FOUND DURING FUSELAGE SKIN SCRIBE LINE DETAILED INSPECTION / COMPLIED WITH ER/A 475624-14 REV ORIG DATED 07/08/09 AT SAA SAT ON N/R CARD 117498

Part: INTERCOSTAL — CORRODED (BS 640-660) · airframe 77,347 hrs · 37,151 cycles

INTERCOASTAL HAS LOWER ANGLE CORRODED IN FWD CARGO COMPATMENT BILGE AREA BETWEEN STA 640-660 RBL 16 / REPAIRED AT SAA SAT DURING HMV ON N/R CARD 133618

Part: FRAME — CORRODED (BS 1400 S26L-26R) · airframe 77,347 hrs · 37,151 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE FRAME AT STA 1400 HAS CORROSION S26L TO S26R / REPLACED FRAME AT SAA SAT DURING HMV ON N/R CARD 118452

Part: FLOORBEAM — CORRODED (BS 760 LBL48-63) · airframe 77,347 hrs · 37,151 cycles

CABIN FLOORBEAM UPPER CAP SURFACE CORRODED STA 760 LBL 48-63 / REPAIRED AT SAA SAT DURING HMV ON N/R CARD 117934

Part: FLOORBEAM — CORRODED (BS 365) · airframe 77,347 hrs · 37,151 cycles

CABIN FLOORBEAM FS 365.25 BL0 TO RBL45 UPPER CAP SURFACE CORRODED / ACCOMPLISHED ER/A 475623-14 REV ORIG DATED 07/07/09 AT SAA SAT ON N/R CARD 127408

Part: FLANGE — GOUGED (BODY TO VERT) · airframe 77,347 hrs · 37,151 cycles

BOTTOM OF LT VERTICAL BODY TO FIN FLANGE IS GOUGED WHERE ACCESS PANEL 322AL SEATS / COMPLIED WITH ER/A 475625-14 REV ORIG DATED 07/08/09 AT SAA SAT ON N/R CARD 127112

Part: SKIN — DENTED (LT WING I/B FLAP) · airframe 77,347 hrs · 37,151 cycles

LT WING I/B FLAP FORE FLAP LOWER SKIN SURFACE APROX WS 165 HAS 3 EA SMALL DINGS / COMPLIED WITH ER/A 474949-14 AT SAA SAT ON N/R CARD 132698 DURING HMV

Part: SKIN — CORRODED (FUSELAGE) · airframe 77,347 hrs · 37,151 cycles

FUSELAGE EXTERIOR SKIN CORRODED AT LT AIRPHONE ANTENNA INSTALLATION / ACCOMPLISHED ER/A 474941-14 REV ORIG AT SAA SAT DURING HMV ON N/R CARD 127190

Part: SKIN — CORRODED (FUSELAGE) · airframe 77,347 hrs · 37,151 cycles

FUSELAGE EXTERIOR SKIN CORRODED AT RT AIRPHONE ANTENNA INSTALLATION / ACCOMPLISHED DELTA ER/A 474941-14 REV ORIG AT SAA SAT DURING HMV ON N/R CARD 127191

Part: SKIN — DAMAGED (BS 655 S17L) · airframe 77,347 hrs · 37,151 cycles

RE-EVALUATE ADF ITEM ENTRY 002 WRITTEN AS CREASE LT FUSELAGE BS 655 BELOW S17L, NO TAG / ACCOMPLISHED DELTA ER/A 474946-14 REV ORIG AT SAA SAT DURING HMV ON N/R CARD 127187.

Part: SKIN — DENTED (BS 1697-1701) · airframe 77,347 hrs · 37,151 cycles

DENT AT LT FUSELAGE STA 1697-1701 S17L TO 19L ACROSS STRINGER AND FRAME 1700 - NO TAG / REPAIRED DURING HMV AT SAA SAT ON N/R CARD 127182.

Part: SKIN — CORRODED (FWD OF E/E DOOR) · airframe 77,347 hrs · 37,151 cycles

E/E DOOR CUTOUT FWD SIDE HAS EXFOLIATING CORROSION / COMPLIED WITH DELTA ER/A 474943-14 REV ORIG AT SAA SAT DURING HMV ON N/R CARD 113384

Part: KEELBEAM — CORRODED (BS 1390) · airframe 77,310 hrs · 37,140 cycles

ACCOMPLISH INSPECTION PER ER/A 367870-14 REV B ACTL LINE 2301 FUSELAGE/KEELBEAM STR-29L, BS 1390 CORROSION AS DESCIBED IN REMARKS REF OMI LOG C/N C04159442. ACCOMPLISHED AND FOUND KEELBEAM AND REPAIR ANGLES CORRODED, REPAIRED PER ER/A 474950-14 REV ORIG DATED 07/09/09 AT SAA SAT ON N/R CARD 123777

Part: SKIN — DENTED (BS 215.25 S20R) · airframe 76,348 hrs · 36,824 cycles

FUSELAGE SKIN HAD A DENT AT STA 215.25, S-20R. CUTOUT THE DAMAGED SKIN AND INSTALLED AN EXTERNAL REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON SEAT TRACK AT BODY STATION 377 TO 440 WL 208. REPAIRED ON NR 00116 PER 51-40-02 BY REPLACEMENT.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION AND CRACKS WERE FOUND ON STRINGER S-29L AT STA 1452 TO THE AFT END OF THE STRINGER SEGMENT. A NEW STRINGER SEGMENT WAS SPLICED IN PER ER/A 06-470938-14 WITH BOEING APPROVAL.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION AT STATION 1470 BBL 0 TO RBL 6. REPAIRED ON NR 00049 PER 51-40-04 FIGURE 1.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION AT INTERCOSTAL STATION 1480 TO 1500 AT STRINGER 26L. REPAIRED ON NR 00124 PER 512-40-02.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

WEB ATTACH ANGLE CRACKED AT STATION 660 RBL 45. REPAIRED ON NR 00127 PER 51-20-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON FASTENERS AT STATION 1441 STRINGER 29L. REPAIRED ON NR 00078 PER 51-40-02 BY REPLACEMENT OF CLIP AND FASTENERS.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON CHANNEL AT STATION 1444 TO STATION 1460 AT RBL 17. REPAIRED ON NR 00045 PER SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON STANDOFF ANGLE AT STATION 1502 STRINGER 28R. REPAIRED ON NR 00069 PER 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

INTERCOSTAL CRACKED AT BODY STATION 680 RBL 25 AT WL 204. REPAIRED PER 51-40-02D ON NR 00092.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON FLOORBEAM 1470 AT LBL 8. REPAIRED ON NR 00051PER 51-40-05 FIGURE 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON FLOORBEAM STATION 1510 AT LBL 3. REPAIRED ON NR 00061 PER SRM 53-60-53 FIGURE 206.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON FLOORBEAM STATION 1470 RBL 115. REPAIRED ON NR 00055 PER 51-40-02 STEP 7.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION FOUND FLOORBEAM SUPPORT ANGLE AT STATION 1497 AT RBL 14. REPAIRED ON NR 00065 PER 53-00-53 DETAIL V.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON FLOORBEAM AT STATION 1510 AT RBL 3. REPAIRED ON NR 00062 PER SRM 53-60-53.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON STRINGER 29L AT STATION 1510 AT STRINGER 29L. REPAIRED ON NR CARD 00074 PER SRM 53-00-03 DETAIL 2.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON SIDEWALL SUPPORT AT STATION 1463 RBL 20. REPAIRED PER 51-40-02 ON NR 00044.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON FLOORBEAM STATION 1510 AT LBL 7. REPAIRED ON NR 00060 PER 53-60-53 FIG 206.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON FLOORBEAM AT STATION 1470 LBL 3. REPAIRED ON NR 00052 PER 51-40-05 FIGURE 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON FLOORBEAM STATION 1470 RBL 3. REPAIRED ON NR 00053 PER 51-40-07 FIGURE 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

AFT CARGO FLOORBEAM STATION 1470 CORRODED AT LBL 17. REPAIRED ON NR 00050 PER 51-70-11 FIGURE 1 SHT 1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON FRAME 1480 AT STRINGER 26R -26L. REPLACED FRAME ON NR 00034 PER 51-40-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON FLOORBEAM BS 1470 AT RBL 8. REPAIRED ON NR 00054 PER 51-40-07 STEP 7.

Part: LENS — BROKEN (R1 DOOR) · airframe 75,279 hrs · 36,456 cycles

EMERGENCY EXIT LIGHT LENS MOUNT BROKEN AT R-1 DOOR. REPLACED PER AMM33-51-002-05 ON ATS NR CARD 00085.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON ACB CARGO TIE DOWN RAIL BS 1470-1481. RAIL REPLACED ON ATS NR 00056 PER 51-40-02 / 05.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 75,279 hrs · 36,456 cycles

CORROSION FOUND DURING AAI INSPECTION ON FLOOR PANEL STATION 1492-1538 RBL 17. FLOOR PANEL REPAIRED ON NR 00029 PER 51-70-1, 51-40-02 AND 51-30-01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION ON STR 29L BS 1510. REPAIRED STR PER SRM 53-00-03 STEP 1 FIG 201.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

DURING AAI INSPECTION AT ATS/PAE INSPECTION FOUND INTERCOSTAL WEB CORRODED BS 1470-1481 RBL 13 IN THE CARGO BILGE AREA. FOUND TO BE OUT OF LIMITS. REPLACED SAME.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

DURING AAI INSPECTION AT ATS/PAE INSPECTION FOUND THE INTERCOSTAL UPPER FLANGE CRACKED AT BS 662 RBL 45 WL 208. REMOVED UPPER ANGLE BS 662 RBL 45 WL 208 IAW SRM 51-40-04-0G. FABRICATED NEW ANGLE FROM 7075-T6 0.032 LOT 827686 IAW SRM 53-30-51, 51-40-02, 51-40-05, 51-30-01-0G, 51-20-01-0G. INSTALLED NEW ANGLE IAW SRM 51-40-04-0G.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

DURING AAI INSPECTION AT ATS/PAE INSPECTION FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT LBL 20 UPPER AND LOWER SURFACES BS 1450 AFT SEVERAL NUT PLATE LOCATIONS. INVESTIGATED CORROSION ON FLOOR TO SIDEWALL SUPPORT UPPER AND LOWER SURFACES AT BS 1450 LT AT SEVERAL NUT PLATE LOCATIONS, DETERMINED TO BE OUT OF LIMITS DUE TO 100 PERCENT MATERIAL LOSS IAW SRM 53-00-53. LOCATED AND DRILLED FASTENER HOLES AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT FROM BS 1410-1530 LT IAW 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSLAGE) · airframe 75,279 hrs · 36,456 cycles

DURING AAI INSPECTION AT ATS/PAE INSPECTION FOUND CORROSION ON FLOOR SUPPORT LBL 12 BS 1510 UPPER SURFACE AT SEVERAL NUT PLATE LOCATIONS. REMOVED CORROSION ON FLOOR SUPPORT LBL 12 BS 1510 AT 3 NUT PLATE LOCATIONS. REMAINING MATERIAL THICKNESS 0.05, 0.05, 0.04 OUT OF LIMITS IAW SRM 53-00-53 DETAIL V. REMOVED DAMAGED NUT PLATE LOCATIONS AND FABRICATED REPAIR ANGLES IAW SRM 53-60-53D FROM BAC1505-100-246 7075-T6511 EXTRUSION LOT 840689. INSTALLED REPAIR ANGLE IAW SRM 53-60-53D AND SRM 51-20-01-0G.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

DURING AAI INSPECTION AT ATS/PAE INSPECTION FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 1531-1540 RBL 17 AT NUT PLATE LOCATIONS. REMOVED CORROSION FROM SIDEWALL SUPPORT BS 1531-1540 FOUND TO BE OUT OF LIMITS PER SRM 53-60-53. DRILLED AND LOCATED NEW PART PER SRM 51-40-02 FIG 1 AND INSTALLED PER SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

DURING AAI INSPECTION AT ATS/PAE INSPECTION FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 1531-1540 LBL 17 AT NUT PLATE LOCATIONS. REMOVED CORROSION FROM SIDEWALL SUPPORT BS 1531-1540. FOUND TO BE OUT OF LIMITS PER SRM 53-60-53. RECEIVED NEW PART. DRILLED AND LOCATED NEW PART PER SRM 51-40-02 FIG 1 AND INSTALLED PER 51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,279 hrs · 36,456 cycles

CORROSION AFT SIDE OF BS 1460 AT STR 29 LT. REPLACED SHEAR TIE IAW 51-40-05-00.

Part: ENGINE — OVERTEMP (NR 2) · airframe 70,228 hrs · 34,889 cycles

DURING TAXI, NR 2 ENG OCCURRED A TAILPIPE MAX EGT REACHED 796 FOR 7 SECONDS. FUEL CTRL JUST PREV REPLACED SUSP BAD, ENG CHG IN PROGRESS. REPLACED NR 2 ENG ON TRANS 6T103.

Part: LINE — RUPTURED (MLG HYD SYS) · airframe 69,885 hrs · 34,775 cycles

AFTER T/O THE GEAR HANDLE WOULD NOT RAISE. AS PER QRH NR 6 OVRD PROCEDURE ACCOMPLISHED AND RT MAIN STAYED DOWN AND GRN. LT MAIN AND NOSE CAME UP WITH GEAR DISAGREE LIGHT. LOWERED GEAR HANDLE AND HAD 3 GRN LANDED UNEVENTLY. FOUND RUPTURED HYD FLEX LINE NEAR RIGHT GEAR STRUT TRUNNION FOR RIGHT TRUCK POSITIONER SHUTTLE VALVE. REPLACED FLEXLINE. LEAK CHECK OK. NO FURTHER TROUBLE FOUND. ALSO, PERFORMED SHUTTLE TEST PER M/M 32-32-17-404-012. CHECKS OK.

Part: SKIN — CRACKED (L1 DOOR CUTOUT) · airframe 61,590 hrs · 31,729 cycles

FUSELAGE SKIN AND BEAR STRAP CRACKED AT THE UPPER FORWARD CORNER OF THE L1 DOOR CUTOUT. REPAIRED IAW ERA 094411-14AD.

Part: FAN — FAILED (CARGO BAY) · airframe 60,119 hrs · 31,134 cycles

RT RECIRC FAN SHUTDOWN INFLIGHT AND PRODUCED AN ACRID SMELL. SMELL DISSIPATED AFTER FAN SWITCH SHUT OFF. REPLACED FAN.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,408 hrs · 30,051 cycles

THE FUSELAGE SKIN WAS FOUND DENTED BETWEEN FS 422 & 434 AND BETWEEN STRINGERS 15L & 16L. THE DENT WAS REMOVED WITH A 12.6 X 11.9 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385124-14, REV A.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,408 hrs · 30,051 cycles

THE FUSELAGE SKIN WAS FOUND WITH A DENT AND GOUGE NEAR AN EXISTING SKIN DOUBLER REPAIR BETWEEN FS 600 & 620 AND BETWEEN STRINGERS 16L & 17L. THE DAMAGE AND THE EXSITING DOUBLER REPAIR WERE REMOVED WITH A SINGLE 22 X 8.8 INCH CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385158-14, REV A.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 57,408 hrs · 30,051 cycles

THE FUSELAGE SKIN SUFFERED A LIGHTNING BURN AT FS 724 AND STRINGER 1. THE DAMAGE WAS REMOVED WITH A CUTOUT THROUGH THE SKIN AND UNDERLYING DOUBLER. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 385154-14, REV A.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,408 hrs · 30,051 cycles

THE FUSELAGE SKIN WAS FOUND WITH SEVERAL SMALL DENTS NEAR STRINGER 28L BETWEEN FS 1454 & 1466. THE DAMAGES WERE REMOVED WITH A SINGLE 6.8 X 3.4 INCH SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385095-14, REV A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,408 hrs · 30,051 cycles

FUSELAGE, SKIN AT STA 1685-1695 AND STRINGER 17R TO 19R. SEVERAL SKIN LOCATIONS WERE FOUND DAMAGED. SKIN CUTOUTS WERE MADE AND A REPAIR DOUBLER AND TRIPLER INSTALLED TO REPAIR THE DAMAGE. ACCOMPLISHED PER ER/A 385112-14.

Part: FITTING — CORRODED (NR 1 PYLON) · airframe 57,408 hrs · 30,051 cycles

DURING THE ACCOMPLISHMENT OF SIP MODIFICATION, CORROSION WAS FOUND ON THE UPPER SURFACE OF THE LT DOUBLER OF THE MID SPAR INSTALLATION. REPAIRED PER: ER/A 385115-14AD.

Part: FITTING — MISMANUFACTURED (NR 1 NACELLE) · airframe 57,408 hrs · 30,051 cycles

LEFT WING, PYLON BACKUP FITTING, NR 2 HOLE THE FACTORY HOLE ON THE FITTING DID NOT LINE UP WITH THE EXISTING HOLE IN THE WING. OPENED UP HOLE TO INSTALL BUSHING TO ALLOW INSTALLATION OF THE NEW FITTING. REINSTALLED THE ORIGINAL FASTENER TYPE. ER/A 385153-14AD

Part: PITOT LINE — OBSTRUCTED (COCKPIT) · airframe 52,029 hrs · 27,500 cycles

ON TAKEOFF ROLL F/O AIRSPEED LAGGED CAPTS AIRSPEED BY 30KTS. FOUND F/O PITOT TUBE OBSTRUCTED. CLEARED OBSTRUCTION AND BLEW PITOT LINE CLEAR FROM ADC. LEAK CKS GOOD PER FIM.

Part: LENS — MISSING (CABIN) · airframe 48,775 hrs · 25,942 cycles

EMERGENCY EXIT SIGN TRIM ON LENS MISSING. REPLACED EXIT SIGN.

Part: ROD END — DISCONNECTED (PAX DOOR) · airframe 47,647 hrs · 25,387 cycles

L2 DOOR WOULD NOT OPEN UPON ARRIVAL. FOUND LWR GATE WOULD MOVE INTO OPEN DOOR, FOUND ROD END GOING TO LWR GATE DISCONNECTED. RECONNECTED ROD AND SECURED AND CKD OPN OF L2 DOOR PER M/M, CKS GOOD.

Part: KEEL — CORRODED (BS 1390)

FUSELAGE KEEL CHORD STRINGER 29L, FS 1405, CORROSION REPAIR. THE FUSELAGE STRINGER 29L KEEL CHORD WAS FOUND CORRODED AT FS 1405. THE CHORD WAS CUT AT FS 1390 AND THE AFT END OF THE CHORD REMOVED. A NEW SECTION OF CHORD WAS SPLICED IN PER ER/A 367870-14, REV A.

Part: BATTERY PACK — DISCHARGED (CABIN)

FIRST CLASS EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK.

Part: OVEN — SMOKING (GALLEY)

FLT ATTENDANT REPORTED SMOKE IN MID GALLEY AREA, MADE EMERGENCY LANDING BOS. INSPECTED AIRCRAFT, PERFORMED PWR RUN. PRESSURIZED AIRCRAFT, FOUND MID GALLEY FWD OVEN SMOKING. REPLACED SAME.

Part: SKIN — TORN (BS 1720)

THE FUSELAGE SKIN WAS BADLY GOUGED/TORN AT THE SKIN BUTT SPLICE AT FS 1720. THE DAMAGED AREA OF SKIN WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 365333-14, REV A. THE DAMAGED WAS CAUSED BY OVER ROTATION ON TAKEOFF.

Part: POWER SUPPLY — INOPERATIVE (R2 DOOR)

R2 DOOR EXIT SIGN INOP. REPLACED POWER SUPPLY.

Part: WEDGE — DELAMINATED (NR 3 LE SLAT TE)

THE NR 3 SLAT WAS FOUND WITH A 4 BY 2 AREA OF DELAMINATION ON THE TRAILING EDGE WEDGE. A COMPOSITE REPAIR WAS INSTALLED PER THE B757 SRM AND DOCUMENTED PER ER/A 363470-14AD.

Part: WEDGE — DELAMINATED (NR 9 LE SLAT)

THE NR 9 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 2 BY 2 AREA OF DELAMINATION. THE DAMAGE WAS REPAIRED PER B757 SRM 51-70-10 AND DOCUMENTED PER ER/A 363471-14AD.

Part: FLIGHT DIRECTOR — FAILED (E/E COMPT)

LT AND RT FLT DIRECTORS FAILED SIMULTANEOUSLY IN FLT, CTR FLT DIRECTOR WORKED OK. ODOR OF HEATED PLASTIC IN COCKPIT AT TIME OF LOSS. MCDP CK FAILED LT FCC, LT FCC VERY HOT WITH SLIGHT BURN ODOR COMING FROM BOX FWD LT F/D TO MCO/PLACARD PER MEL 34-22-04A. ALSO, FWD LT AUTOPILOT TO MCO/PLACARD PER MEL 22-10-01A. BOTH C/BS FOR LT FCC COLLARED. RT F/D CKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

FLOOR TRACK LIGHTS INOP FROM SEAT ROW 39 AFT INOP. REPLACED AFT BATTERY PACK M9002 SYTEM, CHECKS GOOD PER MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY TRACK LIGHTING IN CABIN AFT OF ROW 39 INOP. REPLACED POWER SUPPLY, OPS NML.

Part: BULB — FAILED (L-4 DOOR)

L-4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE DURING TEST. RELAMPED LIGHT ASSEMBLY AND OPERATION NOW NORMAL DURING TEST.

Part: TE WEDGE — DELAMINATED (NR 5 LE SLAT)

DURING SHOP INSPECTION, NR 5 L/E SLAT T/E WEDGE WAS FOUND DELAMINATED. REPLACED T/E WEDGE PER SRM.

Part: RADOME — DELAMINATED (NOSE)

RADOME TEST FOUND DELAMINATION AND MOISTURE ABOVE LIMITS. ALSO, FOUND OLD WET LAY-UPS. RADOME WAS REBUILT, COMPLETE FROM BASE RING UP PER SRM 53-10-72.

Part: SKIN — DAMAGED (TE FLAP)

NR-664 HOLE ON UPPER AND LOWER SURFACE APPROX 47 INCHES FROM INBD END AND 6 INCHES FROM T/E OF LT AFT FLAP ASSEMBLY. ACCOMPLISHED REPAIRS PER DL ERA 301659-14 AND SRN 57-53-01.

Part: FLOORBEAM — CORRODED (FS 345)

AT HMV, FLOORBEAM CORRODED AT FS 345 FROM 0BL TO LBL 18. CLEANED CORROSION, FOUND OUT OF LIMITS PER SRM 53-00-51 PG 103. MADE BEAM REPAIR PER SRM 53-30-51 PG 208.

Part: SKIN — DAMAGED (NR 4 LE SLAT)

DURING SHOP INSPECTION, FOUND NR 4 SLAT WITH HOLE IN LOWER SURFACE OF T/E WEDGE. REPAIRED PER SRM 57-43-02 REF 51-70-10 PG 21 FIG 8.

Part: FLOORBEAM — CORROSION (FS 1640)

DURING HMV, FOUND FS 1640 FLOORBEAM CORRODED AT APPROX RBL 39. REPAIRED BY REMOVING CORROSION AND REPAIRED PER SRM 53-30-51 PG 208.

Part: FLOORBEAM — CORRODED (FS 720)

DURING HMV, FOUND FLOORBEAM CORRODED AT FS 720 BETWEEN LBL 14 AND BL 36. REPAIRED BY REMOVING CORROSION TREATED AND PAINTED LBL 14 AND RBL 36. INSTALLED REPAIR ANGLE AT RBL 3 AND 8. TREATED AND PAINTED PER PS 900-2-4-4 NR 02 AND PS 900-3-6 NR 03. INSTALLED REPAIR ANGLE AS PER SRM 53-30-51.

Part: FLOORBEAM — CORRODED (FS 1640)

DURING HMV, FOUND FS 1640 FLOORBEAM IS CORRODED ACROSS ENTIRE BEAM. REPAIRED BY CLEANING CORROSION, CHECKED DEPTH PER SRM 53-00-51, TREATED AND PAINTED AREA FROM RBL 5 TO O/B END, EXCEPT RBL 39 PER PS 900-2-4-1 NR 2 AND PS 900-3-6-03. FABRICATED T-CAP AND DOUBLERS PER SRM 530-30-51 PG 212, TREATED AND PAINTED T-CAP AND DOUBLERS PER PS 900-2-4-1 NR 2 AND PS 900-3-6-03. INSTALLED REPAIR T-CAP SPLICED AT LBL 51 TO RBL 5 PER SRM 53-50-51 PG 212.

Part: FLOORBEAM — CORRODED (FS 324)

AT HMV, FS 324 FLOORBEAM IS CORRODED AT BL 0. REPAIRED PER SRM 53-00-51 AND SRM 53-10-08.

Part: FIREWALL — DAMAGED (APU)

DURING HMV, FOUND LOWER VERTICAL FIREWALL HAS DEEP CHAFING MARKS FROM RIDING ON DOOR SAFETY LATCH ON RIGHT DOOR APU COMPARTMENT. REPAIRED PER SRM 53-80-08 FIG 202.

Part: DOUBLER — CRACKED (NR 2 PYLON)

NR 2 ENG PYLON CRACKED IN LWR AFT RADIUS OF FWD LIGHTNING HOLE INBD SIDE OF PYLON. REPAIRED PER SRM 54-51-01 PG 206 TO 211.

Part: LE SKIN — DAMAGED (VERT STAB)

DURING HMV, FOUND A TEMPORARY REPAIR INSTALLED ON THE LEADING EDGE OF THE VERTICAL STAB. THE REPAIR IS LOCATED MID SPAN. THE SHOP INSTALLED A PERMANENT REPAIR PER THE SRM 55-30-01.

Part: COWL — DENTED (NR 1 ENGINE)

AT HMV, NR 1 ENGINE NOSE COWL WAS FOUND WITH DENT IN L/E LIP ON LOWER EDGE. REPAIRED PER SRM 54-11-01.

Part: COWL — DAMAGED (NR 1 ENGINE)

AT HMV, FOUND NR 1 ENGINE NOSE COWL WITH HOLE IN COMPOSITE PANEL AT 1 O'CLOCK POSITION. REPAIRED PER SRM 54-11-01.

Part: NOSE COWL — DENTED (ENGINE)

DURING AN UNSCHEDULED SHOP O/H DUE TO GROUND DAMAGE, THE LEADING EDGE LIP WAS REPAIRED PER SRM 54-11-01 FIG 203 AT THE 12 O/C POS.

Part: SKIN — DENTED (BS 654)

AT LETTER CHECK, DUE PERMANENT REPAIR PER SRM 53-31-001 STA 654 WL 214.0 LT SIDE FUSELAGE SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-00-1.