N530US

Part: STRUCTURE — CRACKED (L2 DOOR) · airframe 80,876 hrs · 34,313 cycles

L2 DOOR CRACKED AT FWD DOOR HINGE CUTOUTS. REMOVED L2 DOOR IAW AMDS CARD 5211-9001-2L. INSTALLED SERVICEABLE DOOR IAW AMDS CARD 5211-9001-2L. INSTALLED SLIDE IAW AMS CARD 2566-9001-2L. OK FOR SERVICE.

Part: CABLE — INADEQUATE (L2 DOOR) · airframe 80,876 hrs · 34,313 cycles

L2 DOOR EMERGENCY POWER ASSIST CABLE TRAVEL INSUFFICIENT. ADJUSTED L2 DOOR POWER ASSIST CABLE TRAVEL. OK FOR SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 79,653 hrs · 33,624 cycles

SEAT 4A/B EMERGENCY LIGHT INOPERATIVE AT CURVED EDGE OF STOWAGE BIN CK LIGHT ASSY CHECKED GOOD. RESEATED CONNECTOR ON M731 PWR SUPPLY-NOW OPS CK NML.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,559 hrs · 33,568 cycles

FWD EMERGENCY EXIT SIGN INOPERATIVE. REPLACED POWER SUPPY M730 IAW AMM 33-51.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,434 hrs · 33,510 cycles

EMERGENCY LIGHT IN OVERHEAD BIN ROW 4 A/B INOPERATIVE. R & R BATTERY CHARGER M731 IAW AMM 33-51 OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,823 hrs · 33,156 cycles

BULLNOSE EMERGENCY LIGHT INOPERATIVE AT ROW 4AB. R & R EMERGENCY LIGHT ASSY. OPS CHECKED GOOD.

Part: GROUND STUD — LOOSE (EMERGENCY LIGHTS) · airframe 78,798 hrs · 33,144 cycles

BULLNOSE EMERGENCY LIGHT AT SEAT 18ABC INOPERATIVE. NO POWER TO LIGHT, FUSES GOOD AT POWER SUPPLY. OTHER LIGHT IN CIRCUIT WORKING, SUSPECT POWER SUPPLY. FOUND RING TERMINAL LOOSE ON GROUND STUD GD475-DC. SECURED GROUND STUD. LIGHT NOW OPS NORMAL. REMOVED.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 77,732 hrs · 32,456 cycles

FLOOR EMERGENCY LIGHT (RED) INOPERATIVE AT DOORS. FOUND BROKEN WIRE AT SPLICE. LIGHTS PARTIALLY DISASSEMBLE. REF SWPM 20-30, REPAIRED WIRING AS REQUIRED. OP TEST EMERGENCY LIGHTS OK. REASSEMBLE TRACK.

Part: BEARING — SEIZED (L1 DOOR) · airframe 76,995 hrs · 31,988 cycles

SHIP 5530, MAINTENANCE DISCOVERED DURING THE DOOR 1L EMERGENCY POWER ASSIST MECH CHECK THAT THE TRIGGER BEARING WAS SEIZED. REPLACED BEARING REF AMM 52-11 RII PROCEDURES C/W.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,633 hrs · 31,821 cycles

DURING LAYOVER MAINTENANCE, FOUND EMERGENCY LIGHT ABOVE SEAT 4B IN NOSE INOPERATIVE. MAINTENANCE RELAMPED, REPLACED BATTERY PACK, AND CHARGER M731. OPERATION OF LIGHT NOW CHECKS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,266 hrs · 31,652 cycles

FLIGHT ATTENDANT WROTE UP EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. OPERATIONOF LIGHTS CHECK GOOD PER AMM.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 4,927 hrs · 2,707 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATH LIGHTS IN ROWS 16-22 INOPERATIVE. MAINTENANCE REPLACED BAD POWER SUPPLY IAW AMM 33-51. OPS TESTED OK.

Part: SKIN — DAMAGED (BS 348 S22R) · airframe 78,063 hrs · 32,659 cycles

LIGHTNING STRIKE FASTENER DAMAGE BS 348 S22R. REPLACED BLIND FASTENER WITH PERMANENT REPAIR FASTENER REF TO SRM 53-00-01-2R6, CATEGORY A REPAIR.

Part: SKIN — DAMAGED (BS 310.5 S22R) · airframe 78,063 hrs · 32,659 cycles

LIGHTNING STRIKE FASTENER DAMAGE, BS 310.5 1.5" BELOW S22R REPLACED BLIND FASTENER WITH PERMANENT REPAIR FASTENER REF TO SRM 53-00-01-2R6, CATEGORY A REPAIR.

Part: SKIN — DAMAGED (BS 326 S22R) · airframe 78,063 hrs · 32,659 cycles

LIGHTNING STRIKE FASTENER DAMAGE BS 326, S22R. REPLACED BLIND FASTENER WITH PERMENT REPAIR FASTENER REF TO SRM 53-00-01-2R6, CATEGORY A REPAIR.

Part: SKIN — DAMAGED (BS 310.5 S24L) · airframe 78,063 hrs · 32,659 cycles

LIGHTNING STRIKE FASTENER DAMAGE BS 310.5 1.5" BELOW S24L. REPLACED BLIND FASTENER WITH PERMANENT REPAIR FASTENER REF TO SRM 53-00-01-2R6, CATEGORY A REPAIR.

Part: SKIN — DAMAGED (BS 297 S23L) · airframe 78,063 hrs · 32,659 cycles

LIGHTNING STRIKE FASTENER DAMAGED BS 297 8.75" BELOW S-23L REPLACED BLIND FASTENER WITH PERMENT REPAIR FASTENER REF TO SRM 53-00-01-2R6, CATEGORY A REPAIR.

Part: SKIN — DAMAGED (BS 278 S23R) · airframe 78,063 hrs · 32,659 cycles

LIGHTNING FASTENER DAMAGE BS 278 8.5" ABOVE S23R. REPLACED BLIND FASTENER WITH PERMANENT REPAIR FASTENER REF SRM 53-00-01-2R6.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 73,781 hrs · 30,222 cycles

EMERGENCY EXIT LIGHT ABOVE DOOR 2R INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY PER AMM 33-51-07.

Part: SKIN — DAMAGED (BS 500) · airframe 82,925 hrs · 35,591 cycles

DURING MAINTENANCE CHECK, INSPECTION FOUND A LIGHTNING STRIKE ON THE FUSELAGE SKIN AT BS 500 BETWEEN S16-17R. THE DAMAGE WAS BLENDED AND FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101. COMPLIED WITH ERA 488999-14, REV ORIGINAL.

Part: INTERCOSTAL — CRACKED (BS 1420-1440) · airframe 73,043 hrs · 29,787 cycles

INTERCOSTAL CRACKED BETWEEN STA 1420 TO 1440, RBL 10. REMOVED INTERCOSTAL. REMOVED DAMAGED FLANGE AND PERFORMED HFEC ON CUTOUT FLANGE NO NOTED CRACKS, FABRICATED 1EA REPAIR DOUBLER AND 2EA FILLERS FOR INTERCOSTAL TREATED AND PRIMED AND TOP COATED DOUBLER REPAIR 1EA AND FILLERS 2 EA INSTALLED DOUBLER REPAIR AT INTERCOSTAL AND INTERCOSTAL. INSTALLED 2EA FILLERS.

Part: SKIN — DENTED (BS 1394-1400) · airframe 73,043 hrs · 29,787 cycles

LOWER EXTERIOR FUSELAGE IS DENTED FROM STA 1394 TO STA 1400 BETWEEN STR 29L TO 27R. ACCOMPLISHED ER/A 489003-14 REV ORIGINAL THIS REPAIR IS MAJOR AND PERMANENT. REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE ONLY. ADDITIONAL EA IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR LONGER THAN 12 MONTHS FROM REPAIR APPROVAL. REQUIRED INSP ITEM COMPLETED.

Part: SKIN — DENTED (BS 1425-1430) · airframe 73,039 hrs · 29,784 cycles

DURING M-CHECK AT SAT, WHILE ACCOMPLISHING THE PERMANENT REPAIR AT STA 1420, 2 EACH DENTS WERE FOUND ON THE 146N3511-12 SKIN PANEL BETWEEN STA1425 AND STA1430, S-28R AND S-29L. ER/A 488486-14 SECT.I ACCOMPLISHED DURING M-CHECK AT SAT, FEB2011. SECTION II- APPROVAL IS LIMITED TO 12 MONTHS (365 DAYS) SERVICE ONLY.

Part: SKIN — DENTED (BS 1695-1705) · airframe 73,039 hrs · 29,784 cycles

DURING M-CHECK AT WHILE ACCOMPLISHING A PERMANENT BETWEEN STA1695 AND STA1705, S-17L AND S-19L, IT WAS NOTED THAT STR 18L WAS DENTED AT STA 1695. DENT IS LOCATED ON THE SKIN ATTACHMENT FLANGE OF STRINGER. ACCOMPLISHED DURING M-CHECK AT SAT, FEB2011. SECTION II- APPROVAL IS LIMITED TO 12 MONTHS SERVICE. ONLY FROM SECT I. ADDITIONAL ER/A REVISION IS REQUIRED FOR CONTINUED SERVICE LONGER THAN APPROVED.

Part: SKIN — GOUGED (EMPENNAGE) · airframe 73,039 hrs · 29,784 cycles

EMPENNAGE EXTERNAL R 2"L AREA OF GOUGE DAMAGE JUST AFT OF HORIZ STAB CUTOUT AND FS 1862.7. ACCOMPLISHED ERA 489457-14 REV ORIG THIS REPAIR WAS CLASSIFIED AS PERMANENT AND MAJOR WITH NO INSP REQUIRED COMPLETED.

Part: DOUBLER — DAMAGED (BS 560-580) · airframe 73,039 hrs · 29,784 cycles

DURING M-CHECK OF THE ACFT A DEFERRED ITEM WAS WORKED TO INCORPORATE DL/NWA EA 55-214988 TO INSTALL A PERMANENT REPAIR DOUBLER. DURING INITIAL WORK TO INSTALL EA 55-214988. REPAIR AN UNREPORTED EXISTING SKIN REPAIR WAS FOUND AT BS560-580 S26L-S28L. ER/A 488997-14, SEC I-ACCOMPLISHED DURING M-CHECK AT SAT, FEB 11. ER/A SECTION II, APPROVAL IS LIMITED TO 12 MONTHS SERVICE ONLY. ADDITIONAL ER/A REVISION IS REQUIRED FOR CONTINUED SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,039 hrs · 29,784 cycles

FLOORBEAM STA 345, LBL-63 TO RBL-63 HAS CORROSION. COMPLIED WITH ERA 489011-14 REV ORIGINAL. THIS REPAIR IS MAJOR & PERMANENT WITH NO FURTHER INSPECTIONS REQUIRED. INSPECTION COMPLETED.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 73,039 hrs · 29,784 cycles

FLOORBEAM, STA 324, BL 0, RBL 63 HAS CORROSION. REMOVED CORROSION FROM FLOOR BEAM STA 324, BL-0. FOUND OUT OF LIMITS. REMOVED WEB FROM RBL 24, STA 324 TO STA 345. FLOORBEAM REPAIRED IAW ERA 488481-14, REV D AND REINSTALLED WEB AT RBL24 STA 324 TO STA 345 IAW SRM 51-40-02. COMPLETED.

Part: CREASE BEAM — CORRODED (BS 1400-1420) · airframe 73,039 hrs · 29,784 cycles

CREASE BEAM ASSY HAS CORROSION STA 1400-1420, RBL 63. COMPLIED WITH ERA 489013-14 REV ORIGINAL. COMPLETED INSPECTION.

Part: SKIN — DAMAGED (BS 1661-1681) · airframe 73,039 hrs · 29,784 cycles

DURING M-CHECK AT SAT A FLUSH SKIN REPAIR WAS FOUND AT STA 1661 TO STA 1681, S-20R TO S-22R. ADDITIONAL DENTS AND TOOLING MARKS WERE ALSO FOUND AT THE REPAIR LOCATION. ER/A 488989-14 SECTION I ACCOMPLISHED AT SAT M-CK FEB 2011. SECTION II REPAIR APPROVAL LIMITED TO 42900 TOTAL CYCLES. ADDITIONAL ER/A REVISION IS REQUIRED FOR CONTINUED SERVICE BEYOND 42900 TOTAL CYCLES. PENDING FOR DTA. INSP TO BE ACCOMPLISHED AT EVERY L-CK AFTER SECTION I.

Part: SKIN — DENTED (FUSELAGE) · airframe 73,039 hrs · 29,784 cycles

DURING M-CK AN EXISTING FLUSH SKIN REPAIR WAS FOUND AT STA 1661 TO STA 1681, S-20R TO S-22R. ADDITIONAL DENTS AND TOOLING MARKS WERE ALSO FOUND. ER/A 488989-14AD SECTION I ACCOMPLISHED DURING M-CK AT SAT FEB 2011. SECTION II REPAIR APPROVAL LIMITED TO 42900 TOTAL CYCLES. ADDITIONAL ER/A REVISION IS REQUIRED FOR CONTINUED SERVICE BEYOND 42900 TOTAL CYCLES.

Part: SKIN — GOUGED (BS 1700-1720) · airframe 73,039 hrs · 29,784 cycles

DURING M-CHECK AN EXISTING FLUSH REPAIR AT STA 1700-1720, S-17R TO S-20R WAS FOUND WITH GOUGES AND TOOLING MARKS AT THE REPAIR LOCATION. ER/A 488988-14 SECTION I ACCOMPLISHED DURING M-CK FEB 11 AT SAT SECTION II REPAIR APPROVAL IS LIMITED TO 50000 TOTAL CYCLES ADDITIONAL ER/A REVISION IS REQUIRED TO CONTINUE SERVICE BEYOND 50000 TOTAL CYCLES.

Part: SKIN — DAMAGED (STA 1460 S26L) · airframe 73,039 hrs · 29,784 cycles

FUSELAGE SKIN PANEL, STA 1460, STRINGER 26L DAMAGED. DISCONTINUE REVENUE SERVICE ON OR BEFORE 42,200 TOTAL FLIGHT CYCLES PENDING STAGE III DTA APPROVAL. COMPLIED WITH ERA 488480-14AD REV ORIGINAL. TIME LIMITED REPAIR, REPAIR APPROVAL IS LIMITED TO 42,200 TOTAL FLIGHT CYCLES COMPLETED.

Part: SKIN — DENTED (STA 640 S15-19L) · airframe 73,039 hrs · 29,784 cycles

DTA MONITOR INSP, FUSELAGE SKIN PANEL DENTS STA 640 AND STG 15L - 19L. ER/A 488485-14AD WAS APPROVED FOR STAGE I DTA, STATIC STRENGTH, AND IS PENDING STAGE II APPROVAL. THIS APPROVAL IS TEMPORARY FOR ASSOCIATED ER/A 13-488485. THE ER/A 488485-14AD SECTION I REPAIR IS TIME LIMITED FOR 12 MONTHS. IF THE LOGPAGE AND ER/A HAVE NOT BEEN REVISED 3JAN12 TO INCLUDE STAGE II DTA RESULTS, CONTACT ENGINEERING.

Part: DOUBLER — DENTED (BS 348 S14L) · airframe 73,039 hrs · 29,784 cycles

DURING M-CHECK, DENT WAS FOUND AT STA 378, S-14L WITHIN SRM LIMITS EXCEPT ONLY 5.4 INCHES FROM THE L-1 DOOR CUTOUT. DENT WAS CUT OUT AND REPAIRED WITH AN EXTERNAL DOUBLER COMPLIED WITH ERA 488990-14 REV ORIGINAL. THIS IS A TIME LIMITED REPAIR. REPAIR APPROVAL IS LIMITED TO 75,000 TOTAL AIRFRAME FLIGHT CYCLES. COMPLETED, RII INSP COMPLETED.

Part: SKIN — DENTED (STA 1520 S19-20L) · airframe 73,039 hrs · 29,784 cycles

DURING M-CHECK, A DENT WAS FOUND ON THE FUSELAGE SKIN BETWEEN STA 1500 AND STA 1520 AND S-19L AND S-20L. THE DENT MEASURES 8.0" L X 3.50" W X 0.041" DEEP DENT IS LOCATED NEAR TO THE LAP SPLICE AT S-20L. ER/A SECTION, REPAIR APPROVAL IS LIMITED TO 50,000 TOTAL AIRFRAME FLIGHT CYCLES. ADDITIONAL ER/A REVISION IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR BEYOND 50,000 TOTAL AIRFRAME FLIGHT CYCLES.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,039 hrs · 29,784 cycles

DURING MAINTENANCE CHECK INSPECTION FOUND A LIGHTNING STRIKE ON THE FUSELAGE SKIN AT STA 500 BETWEEN S-16R AND S-17R. THE DAMAGE BLENDED AND FOUND OUT OF LIMITS PER B757-200 SRM 53-00-01, FIG 101 ER/A SECTION I REPAIR APPROVAL IS LIMITED TO 38,633 TOTAL AIRFRAME FLT CYCLES. ADDITIONAL ER/A REVISION IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR BEYOND 38,633 TOTAL AIRFRAME FLIGHT CYCLES.

Part: SKIN — DENTED (FUSELAGE) · airframe 1,902 hrs · 948 cycles

FUSELAGE DENT WAS FOUND AT STA 500, S-27R. THE DENT WAS REMOVED BY TRIMMING THE SKIN. REPAIR WAS COMPLETED PER SRM 53-00-01 REPAIR 2 EXCEPT THE REPAIR DOUBLER WAS 0.063" THICK. ER/A SECTION I REPAIR IS APPROVED FOR 12 MONTHS (365 DAYS) ONLY. ADDITIONAL ER/A REVISION IS REQUIRED FOR CONTINUED SERVICE BEYOND 365 DAYS FROM 1 FEB 2011. PENDING FOR DTA. MONITOR TO CONTACT LIAISON ENGINEERING 30 DAYS. BEFORE DUE DATE OF APPROVED REPAIR. ASSOCIATED ER/A 13-488482 ADDED FOR AC 5530.

Part: BOX BEAM — CORRODED (BS 1640-1660) · airframe 73,039 hrs · 29,784 cycles

BOX BEAM HAS CORROSION STA 1640-1660, RBL-60. R & R BOX BEAM AT STA FS, STA 1640-1660 RBL-60 IAW SRM 51-40-02, PAGE 1-10.

Part: BOX BEAM — CORRODED (STA 1660-1680) · airframe 73,039 hrs · 29,784 cycles

BOX BEAM HAS CORROSION STA1660-1680, RBL-60. R & R BOXBEAM AT FS STA 1660-1680, RBL-60 IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (BS 660-760) · airframe 73,039 hrs · 29,784 cycles

CREASE BEAM TO FLOOR TRANSITION ANGLE HAS CORROSION STA 660-760 RBL-60. R & R CHORD ZEE ANGLE FROM MAIN CABIN STA 660-760, RBL 60 IAW SRM 51-40-02.

Part: BOX BEAM — CORRODED (STA 1660-1680) · airframe 73,039 hrs · 29,784 cycles

BOX BEAM HAS CORROSION STA 1660-1680 AT BL-0. R & R BOX BEAM AT FS STA 1660-1680, BL-0 IAW SRM 51-40-02, PAGE 1-10.

Part: BOX BEAM — CORRODED (BS 1660-1680) · airframe 73,039 hrs · 29,784 cycles

BOX BEAM HAS CORROSION STA 1660-1680, LBL-60. REMOVED CORROSION BOX BEAM STA 1660-1680, LBL-60 OUT OF LIMITS IAW SRM 53-00-51, PG:103. R & R BOX BEAM IAW SRM 51-40-02, COMPLETED.

Part: BOX BEAM — CORRODED (BS 1640-1660) · airframe 73,039 hrs · 29,784 cycles

BOX BEAM HAS CORROSION STA 1640-1660, LBL-60 BLENDED. CORROSION FROM BOX BEAM STA 1640-1660, LBL-60 OUT OF LIMITS IAW SRM 53-00-51. R & R BOX BEAM STA 1640-1660, LBL-60 IAW SRM 51-40-02, COMPLETED.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 73,039 hrs · 29,784 cycles

FLOORBEAM HAS CORROSION STA 1640, BL-0, RBL-55. REMOVED CORROSION ON FLOORBEAM AT FS STA 1640, BL-0 TO RBL-55, NO CORROSION FOUND. REMOVED CORROSION AT BS 1640 RBL-63. FOUND CORROSION AND DOUBLE HOLES OUT OF LIMITS IAW SRM. REMOVED FLOOR BEAM BS 1640 FROM LBL 10 TO RBL 66 SPLICE ANGLES SPLICE STRAPS IAW SRM 53-00-51. FABRICATED FLOORBEAM T-CHORD SPLICE, ANGLES, SPLICE STRAPS LOCATED AND DRILLED HOLES IAW SRM 53-00-51, FIG 201, REPAIR 3, PG: 202 AND SRM 51-40-02, PG1-10. COMPLETED.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 73,039 hrs · 29,784 cycles

RT WING OTBD AFT FLAP LOWER SURFACE PREVIOUS REPAIR AREA DELAMINATED AT STA 450. REMOVED SKIN AND CORE DAMAGE IAW SRM 51-70-04 PARA 4E PG:4-5 FG:7. REMOVED WATER IAW SRM 51-70-04, PARA 4B, PG:4 -5 HOT BONDED CORE PLUG AND APPLIED REPAIR PLIES IAW SRM 51-70-04, PARA 4D DETAIL 2 PG:14 AND PAGE 48 APPLIED PRIMER TO AREA IAW SRM 51-70-04 PARA 4F, PG:18 TOP COAT TO BE APPLIED ON CARD 8, ZONE 100 IDENTIFIED REPAIRED IAW PS 900-5-11.04. SKIN DAMAGED 5.5" DIAMETER AND CORE DAMAGED 5.5" DIAMETERS DEPTH 0.5" COMPLETED.

Part: BEAM — CORRODED (STA 1380-1440) · airframe 73,039 hrs · 29,784 cycles

AFTER REMOVAL OF SIDE PANEL AT AFT CARGO DOOR CUTOUT FOUND UPPER BEAM CHORD CORRODED AT STA 1380 TO 1440. R & R DAMAGED UPPER BEAM CHORD AT AFT CARGO FROM STA 1460 TO 1360, IAW SRM 51-40-02, PG 1-10. COMPLETED.

Part: INTERCOSTAL — CORRODED (BS 1220-1240) · airframe 73,039 hrs · 29,784 cycles

CORROSION ON AFT CARGO COMPARTMENT BILGE INTERCOSTAL BETWEEN STA 1220-1240, RBL 16.1. R & R INTERCOSTAL AT AFT CARGO COMPARTMENT BILGE, STA 1220-1240, RBL 16. IAW SRM 51-40-02, PG 7, PARA 7B. COMPLETED.

Part: WEB — CORRODED (BS 1675-1720) · airframe 73,039 hrs · 29,784 cycles

MAIN CABIN FLOOR WEB HAS CORROSION STA 1675-1720, LBL 55-RBL 55. REMOVED CORROSION ON MAIN CABIN FLOOR WEB IAW SRM 51-10-02, PG 15. HFEC SURFACE INSPECTED BLENDED AREA NO CRACKS NOTED. REPAIR DOUBLER AND FILLER ON MAIN CABIN FLOOR WEB, IAW SRM 53-60-51-R2. CUT OUT DAMAGE AT STA 1720, RBL 33 AND (HFEC NO CRACKS NOTED) IAW SRM 53-60-51-R2, COMPLETED.

Part: FLOORBEAM — CORRODED (BS 1660,LBL 60) · airframe 73,039 hrs · 29,784 cycles

FLOORBEAM HAS CORROSION STA 1660, LBL 60- RBL 60, RL056. REMOVED CORROSION AT FS 1660, LBL 60, FOUND OUT OF LIMITS IAW SRM 53-00-51, ALLOWABLE DAMAGE, PG 103, CUT OUT DAMAGED T-CAP FLOORBEAM FROM LBL 35 TO LBL 65, AT STA 1660, IAW SRM 53-00-51, REPAIR 3, PG 201, FIG 201, STEP 2. FABRICATED AND INSTALLED T-CAP FLOORBEAM REPAIR PARTS IAW SRM 53-00-51, REPAIR 3, PG 203, FIG 201, AND SRM 51-40-02, PG 1-10. INSP AND RII COMPLETED.

Part: FLOORBEAM — CORRODED (BS 377) · airframe 73,039 hrs · 29,784 cycles

FLOORBEAM HAS CORROSION STA 377, LBL 63 TO RBL 24, RL032. REMOVED FLOORBEAM STA 377, RBL 31 TO LBL 33" IAW SRM 51-40-02, PAGE 1 TO 10. FABRICATED FLOORBEAM AND 2 EA SPLICES ANGLES AND 2 EA STRAPS. INSTALLED FLOORBEAM, SPLICE ANGLES AND STRAPS IAW SRM 51-40-02, AND SRM 53-00-51, PAGE 204, REPAIR 3. REMOVED CORROSION STA 377 AT LBL 54", FOUND WITHIN LIMITS IAW SRM 53-00-51, FIG 1, DETAIL III, TREATED AND PRIMED IAW SRM 51-20-01.

Part: BOX BEAM — CORRODED (FUSELAGE) · airframe 73,039 hrs · 29,784 cycles

BOX BEAM STA 405, RBL 24-RBL 45 HAS CORROSION AFTER VALUATION FOUND BOX BEAM AT STA 405, RBL 24-RBL 45 OUT OF LIMITS IAW SRM 53-00-51, PG 103, DETAIL III. R & R BOX BEAM ON STA 405, RBL 24-RBL 45 IAW SRM 51-40-02, PG 7, PARA 7D.

Part: SUPPORT BEAM — CORRODED (FUSELAGE) · airframe 73,039 hrs · 29,784 cycles

SEAT TRACK SUPPORT BEAM AND SEAT TRACK HAS CORROSION STA 395-418, RBL 24 RL042. REMOVED CORROSION SEAT TRACK SUPPORT BEAM IAW SRM 51-10-02, OUT OF LIMITS IAW SRM 53-00-52. CLEANED SEAT TRACK, STA 395, RBL 24, IAW AMM 51-21-00-377-001, NO CORROSION NOTED. INSTALLED NEW SEAT TRACK SUPPORT BEAM IAW SRM 51-40-02, PG 7, PARA 7D. INSTALLED IAW SRM 51-40-02, PG 7, PARA 7D.

Part: FLOOR SUPPORT — CORRODED (BS 377-440) · airframe 73,039 hrs · 29,784 cycles

CREASE BEAM TO FLOOR TRANSITION ANGLE HAS AREAS OF CORROSION-STA 377-440, LBL 63. REMOVED CORROSION FROM FLOOR TRANSITION ANGLE STA 377 TO STA 440, LBL 63, FOUND OUT OF LIMITS, REMOVED FLOOR TRANSITION ANGLE SECTION FROM STA 310.5 TO STA 430 AND ANOTHER SECTION FROM STA 430 TO STA 450, LBL 63. REPLACED BOTH SECTIONS WITH EXTRUSION IAW DWG NR140N0504, REV J, SRM 53-00-01, FIG 101, AND SRM 51-40-02, PG 7, PARA 7D.

Part: CONTROL PANEL — GOUGED (CARGO BAY) · airframe 73,039 hrs · 29,784 cycles

FWD CARGO CONTROL PANEL LOWER EDGE IS GOUGED. ACCOMPLISHED ER/A 488998-14, REV ORIG. THIS IS A PERMANENT REPAIR, NO FURTHER INSP REQUIRED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 72,506 hrs · 29,466 cycles

DURING LAYOVER CHECK MAINTENANCE FOUND FIRST CLASS EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REPLACED POWER SUPPLY M9001. (2010-00810)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,433 hrs · 28,266 cycles

DURING AN OVERNIGHT LINE CHECK THE OVERHEAD EMERGENCY EXIT SIGN ABOVE DOOR 2R WOULD NOT ILLUMINATE. MAINTENANCE FOUND THE ASSOCIATED BATTERY PACK TO DEFECTIVE AND REPLACED IT. SYSTEM OPERATION WAS NORMAL AFTER THE BATTERY PACK WAS REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,062 hrs · 28,124 cycles

DURING AN OVERNIGHT LINE CHECK THE EMERGNECY EXIT SIGN AT DOOR 3R WAS FOUND TO BE INOPERATIVE. MAINTEANCE FOUND THE ASSOCIATED BATTERY PACK TO BE DEFECTIVE AND REPLACED IT. SYSTEM OPERATION WAS NORMAL AFTER THE BATTERY PACK WAS REPLACED.

Part: BEAR STRAP — CRACKED (FUSELAGE)

DURING L-CHECK A CRACK WAS FOUND IN FASTENER HOLE OF BEAR STRAP SKIN COMMON TO THE UPPER FWD CORNER OF MAIN ENTRY DOOR 1L. REPAIRED IAW EA55-214984 SECTION 1. SECTION II REQUIRES MFG TOLERANCE ANALYSIS NO LATER THAN 10 JAN 2010. (K).

Part: STATOR — FAILED (ENGINE) · airframe 56,749 hrs · 23,432 cycles

DURING CRUISE FLIGHT ENGINE NR 1 OIL PRESSURE DROPPED TO 12 PSI. ENGINE NR 1 FLAMED OUT. FLIGHT CREW DIVERTED AC TO CLT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED THE PMA STATOR AND ROTOR. NOTE: THIS EVENT WAS ORIGINALLY BELIEVED TO BE A COMMANDED ENGINE SHUTDOWN AND REPORTED INTERNALLY ONLY. POST EVENT INVESTIGATION HAS REVEALED THAT THIS EVENT WAS A FLAMEOUT AND IS SDR REPORTABLE.

Part: SKIN PANEL — CRACKED (NR 2 PYLON) · airframe 54,984 hrs · 22,735 cycles

DURING H-CHECK FOUND CRACK IN NR 2 PYLON RT SIDE SKIN PANEL NACELLE STA 136. REPAIRED PER EA 55-202910.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,906 hrs · 19,418 cycles

DURING "L" CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 25. REPAIRED PER EA 55-189610.

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 46,446 hrs · 19,240 cycles

UPON GEAR EXTENSION, THE LEFT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. THE LANDING GEAR WAS CYCLED; NO CHANGE IN INDICATION. THE FLIGHT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN GEAR INDICATOR ASSEMBLY. SYSTEM TESTS WERE SATISFACTORY.

Part: HOUSING — LEAKING (NR 2 OIL FILTER) · airframe 42,791 hrs · 17,839 cycles

NR 2 ENGINE WAS SHUTDOWN DURING CRUISE AT 35,000 FEET DUE TO OIL QUANTITY AND PRESSURE LOSS. FLIGHT CREW DIVERTED TO SYR AND MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND OIL LEAK AT OIL FILTER HOUSING. REPLACED THE O-RINGS AND FILTER. GROUND RUN AND REQUIRED INSPECTIONS WERE COMPLETED. AIRCRAFT RETURNED TO SERVICE.

Part: SLIDE — DISLODGED (PAX DOOR)

WHEN DOOR 1R WAS OPENED BY CATERING FOR GALLEY SERVICE, THE ESCAPE SLIDE FELL OUT. SLIDE DID NOT INFLATE. MAINTENANCE REPLACED THE DOOR EMERGENCY POWER RESERVOIR AND THE ESCAPE SLIDE.. OPERATIONAL CHECK OK.

Part: VIDIO MONITOR — ODOR (CABIN)

DURING CRUISE, FLIGHT CREW NOTICED ELECTRICAL ODOR NEAR DOOR 2L. AIRCRAFT DIVERTED TO SEA AND LANDED WITHOUT INCIDENT. MAINTENANCE DEACTIVATED VIDEO MONITOR SYSTEM AND DEFERRED FOR FURTHER HUGHES AVICOM REVIEW. SPECIFIC PART CAUSING PROBLEM PENDING FURTHER INVESTIGATION.

Part: OIL FILTER LIGHT — ILLUMINATED (NR 1 ENGINE)

AFTER PUSHBACK, THE NR 1 ENIGNE OIL FILTER MESSAGE WAS DISPLAYED. AIRCRAFT RETURNED TO THE GATE AFTER ENGINE SHUTDOWN AND RESTART. MESSAGE DID NOT REPEAT. GROUND MAINTENANCE INSPECTED AND REPLACED THE ENGINE OIL FILTER. NO CONTAMINATION WAS FOUND.

Part: BATTERY PACK — DISCHARGED (CABIN)

FLOOR EMERGENCY LIGHTS BETWEEN ROWS 15 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY AT DOOR 2R, CHECKED OK.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

DURING CLIMB, NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. THE ENGINE OIL PRESSURE DROPPED AND ENGINE WAS SHUT DOWN. AIRCRAFT RETURNED TO MSP. GROUND MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE.

Part: FITTING — CORRODED (FS 1380)

DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT CARGO DOOR FORWARD THRESHOLD FITTING FS 1380. REPLACED FITTING.

Part: RETRACT MECH — MALFUNCTIONED (LE FLAPS)

LEADING EDGE SLAT DISAGREE LIGHT CAME ON DURING APPROACH. AIRCRAFT MADE A GO-AROUND AND EMERGENCY EQUIPMENT WAS REQUESTED BY THE CREW. USED ALTERNATE FLAP PROCEDURE AND LANDED WITHOUT INCIDENT. MAINTENANCE IS IN PROGRESS.

Part: CIRCUIT BREAKER — TRIPPED (LE FLAPS)

ON TAKEOFF, THE LEADING EDGE SLAT DISAGREE MESSAGE AND LEADING EDGE LIGHTS ILLUMINATED. DURING FLAP RETRACTION, THE FLAP NEEDLES STOPPED AT FLAPS 1/2 POSITION AND DID NOT COME UP USING THE ALTERNATE PROCEDURES. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. RESET THE POWER CONTROL AND SENSOR CIRCUIT BREAKERS ON NR 1, NR 2, AND NR 3 FLAP/SLAT ELECTRONIC UNITS. NO FAULTS WERE INDICATED, SYSTEM CHECKED NORMAL.