N691AA

Part: B-NUT — LOOSE (SENSE LINE) · airframe 90,172 hrs · 24,946 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS RT ENGINE BLEED LIGHT AND MASTER CAUTION LIGHT ILLUMINATED ON TAKEOFF ROLL AT 70KTS, MAX SPEED 82KTS. NO RTO ACTIVATION. MAINTENANCE ACCOMPLISHED FIM TASK 36-11-00 FIG 110. COMPLIED WITH FUNCTIONAL TEST OF HPSOV AND HS PILOT IAW FIG 502, FOUND B NUT ON DOWNSTREAM PRESS SENSE LINE DISCONNECTED AT TEE FITTING. REINSTALLED AND TIGHTENED LINE. FUNCTIONAL TEST OF FAMV OK IAW AMM 36-11-16-501. REPLACED RT BLEED OVERTEMP SW S359 IAW AMM 36-22-01-401 AS PRECAUTION. RT BLEED SYSTEM OPS CHECK OK IAW AMM 36-11-00-501.

Part: LIGHT — INOPERATIVE (L4 EXTERIOR) · airframe 90,085 hrs · 24,916 cycles

AIRCRAFT WAS NOT GROUNDED: 4L DOOR EXTERIOR SLIDE LIGHT WAS INOPERABLE. MAINTENANCE RELAMPED SLIDE LIGHT PER AMM 33-51-06.

Part: GCU — UNRELIABLE (RT GENERATOR) · airframe 90,051 hrs · 24,907 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS ON TAKEOFF ROLL PRIOR TO 80KNOTS RIGHT GEN TRIPPED OFFLINE #1 EICAS MESSAGE ILLUMINATED. DISCONTINUED T/O. FOLLOWED QRH. RESET GEN #1 RAN APU. NEXT TAKEOFF ABOVE 80 KNOTS RIGHT GEN TRIPPED OFFLINE. CONTINUED TAKEOFF. MAINTENANCE REPLACED RH GENERATOR CONTROL UNIT IAW AMM 24-22-02. OPS CHECKS GOOD. OK FOR SERVICE.

Part: LATCH — LACK OF LUBE (L1 DOOR) · airframe 89,559 hrs · 24,761 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS DOOR 1L DOOR HANDLE IS DIFFICULT TO OPERATE. MAINTENANCE LUBED L1 DOOR LINKAGE. OPERATED DOOR SEVERAL TIMES. OPS CHECKS NORMAL.

Part: INDICATOR — FAILED (COCKPIT) · airframe 88,104 hrs · 24,348 cycles

AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF LOSS OF STANDBY ATTITUDE INDICATION. AIRCRAFT OVERWEIGHT FOR LANDING. MAINTENANCE REPLACED THE STANDBY ATTITUDE INDICATOR AND ACCOMPLISHED ALL REQUIRED TESTS IAW AMM 34-24-01-404-088. ALL TESTS NORMAL.

Part: FLOOR SUPPORT — CORRODED (BS 1445-1495) · corrosion level 2 · airframe 87,611 hrs · 24,214 cycles

CORROSION FOUND ON THE AFT CARGO FLOOR SUPPORT BETWEEN BS 1445 AND 1495, RBL 7. REPLACED THE FLOOR SUPPORT IAW RD 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (BS 1445-1495) · corrosion level 2 · airframe 87,611 hrs · 24,214 cycles

CORROSION FOUND ON THE AFT CARGO FLOOR SUPPORT BETWEEN BS 1445 AND 1495, RBL 2. REPLACED THE FLOOR SUPPORT IAW RD 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (BS 1445-1495) · corrosion level 2 · airframe 87,611 hrs · 24,214 cycles

CORROSION FOUND ON THE AFT CARGO FLOOR SUPPORT BETWEEN BS 1445 AND 1495, LBL 7. REPLACED THE FLOOR SUPPORT IAW RD 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (BS 1445-1495) · corrosion level 2 · airframe 87,611 hrs · 24,214 cycles

CORROSION FOUND ON THE AFT CARGO FLOOR SUPPORT BETWEEN BS 1445 AND 1495, RBL 10. REPLACED THE FLOOR SUPPORT IAW RD 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (BS 1445-1495) · corrosion level 2 · airframe 87,611 hrs · 24,214 cycles

CORROSION FOUND ON THE AFT CARGO FLOOR SUPPORT BETWEEN BS 1445 AND 1495, LBL 2. REPLACED THE FLOOR SUPPORT IAW RD 51-00-05-1

Part: FLOOR SUPPORT — CORRODED (BS 1445-1495) · corrosion level 2 · airframe 87,611 hrs · 24,214 cycles

CORROSION FOUND ON THE AFT CARGO FLOOR SUPPORT BETWEEN BS 1445 AND 1495, LBL 10. REPLACED THE FLOOR SUPPORT IAW RD 51-00-05-1.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 87,611 hrs · 24,214 cycles

CORROSION FOUND ON THE LEFT WING UPPER SKIN, AT THE UPPER FUEL FILL PORT. REPAIRED THE SKIN IAW EA 289163.

Part: BATTERY — DISCHARGED (MEGAPHONE) · airframe 86,643 hrs · 23,964 cycles

REAR MEGAPHONE INOPERATIVE. REPLACED REAR MEGAPHONE BATTERIES IAW MM 25-64-00. CHECKS OK.

Part: LIGHT — INOPERATIVE (SEAT 4E) · airframe 86,560 hrs · 23,945 cycles

SEAT 4E AFT MOUNTED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51-11 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — INOPERATIVE (SLIDE EMER LIGHT) · airframe 86,557 hrs · 23,944 cycles

L1 DOOR SLIDE EXIT LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK AND POWER SUPPLY IAW MM 33-51-07, OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,560 hrs · 23,945 cycles

R1 DOOR SIDE EXIT SIGNS ARE INOPERATIVE. REPLACED THE BATTERY PACK AND POWER SUPPLY M730 IAW 33-51-07. OPS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,557 hrs · 23,944 cycles

L1 DOOR SLIDE EXIT LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK AND POWER SUPPLY IAW MM 33-51-07, OPS CHECKED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 86,560 hrs · 23,945 cycles

FIRST CLASS SEAT MOUNTED EMERGENCY LIGHTS WERE INOPERATIVE AT ROWS 1E TO 4E. MAINTENANCE REPLACED THE BATTERY PACK M730 IAW MM 33-51-07, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,560 hrs · 23,945 cycles

R1 DOOR SIDE EXIT SIGNS WERE INOPERATIVE. REPLACED THE BATTERY PACK IAW MM 33-51-07. OPS CHECKED NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,537 hrs · 23,938 cycles

EMERGENCY LIGHTS AT FIRST CLASS AND MAIN CABIN INOPERATIVE. THE AIRCRAFT WAS GROUNDED. REPLACED EMERGENCY LIGHT BATTERIES M10798, M10799, M10800, M10801 IAW AMM 33-51-07, TESTED NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,537 hrs · 23,938 cycles

EMERGENCY LIGHTS AT FIRST CLASS AND MAIN CABIN INOPERATIVE. THE AIRCRAFT WAS GROUNDED. REPLACED EMERGENCY LIGHT BATTERIES M10798, M10799, M10800, M10801 IAW AMM 33-51-07, ALL TESTED NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,537 hrs · 23,938 cycles

EMERGENCY LIGHTS AT FIRST CLASS AND MAIN CABIN INOPERATIVE. THE AIRCRAFT WAS GROUNDED. REPLACED EMERGENCY LIGHT BATTERIES M10798, M10799, M10800, M10801 IAW AMM 33-51-07, TESTED NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 85,327 hrs · 23,641 cycles

THE FLASHLIGHT AT FLIGHT ATTENDANT STATION AT THE R2 DOOR BATTERY INOPERATIVE. REPLACED THE BATTERY. THE FLASHLIGHT CHECKED OK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 84,894 hrs · 23,509 cycles

FLOOR EMERGENCY SIGN LENS MISSING IN THE AISLE, RIGHT SIDE. REPLACED THE LENS IAW AMM 33-51-00. OK FOR SERVICE.

Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 84,815 hrs · 23,488 cycles

R3 DOOR EXIT SIGN DETACHED. ATTACHED AND SECURED THE EXIT SIGN. OK FOR SERVICE.

Part: SENSOR — INOPERATIVE (L1 GIRT BAR) · airframe 84,728 hrs · 23,461 cycles

L1 DOOR SLIDE ANNUNCIATOR INOPERATIVE. REPLACED L1 GIRT BAR PROXIMITY SENSOR IAW MM 25-66-11.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 84,522 hrs · 23,402 cycles

RIGHT AFT OVERWING EMERGENCY DOOR MISSING THE EXIT SIGN LENS. REPLACED THE LENS.

Part: BULB — INOPERATIVE (ARMED LIGHT) · airframe 84,423 hrs · 23,377 cycles

AIRCRAFT WAS NOT GROUNDED. RIGHT FORWARD GALLEY ENTRY DOOR SLIDE (ARM LIGHT) IS INOPERATIVE. RE-LAMPED FORWARD GALLEY R 1IDE ARM LIGHT. OK FOR SERVICE.

Part: LAMP — FAULTY (EMERGENCY LIGHT) · airframe 84,234 hrs · 23,319 cycles

EXIT SIGN WAS VERY DIM ON THE LEFT OVERWING. REPLACED THE LAMPS IAW AMM 33-51-06. MAINTENANCE PERFORMED SUCCESSFUL OPERATIONAL CHECK.

Part: LENS — DAMAGED (CABIN) · airframe 84,235 hrs · 23,319 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN BY THE LEFT OVERWING DOOR HAS A DAMAGED LENS COVER. REMOVED AND REPLACED LENS COVER PER AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: GIRT BAR — DISCONNECTED (L3 DOOR) · airframe 84,202 hrs · 23,309 cycles

AIRCRAFT WAS NOT GROUNDED. CABIN CREW REPORTS THE L3 DOOR WILL NOT ARM. TROUBLESHOOTING FOUND GIRT BAR DISCONNECTED FROM SLIDE. REINSTALLED GIRT BAR PER AMM 25-66-01-404-044. OPERATIONAL CHECK GOOD.

Part: WIRE — DISCONNECTED (CABIN) · airframe 84,139 hrs · 23,291 cycles

THE AIRCRAFT WAS GROUNDED. FOUND W9000-9051 BN-22 BROWN WIRE IN TWO FORWARD SIDE OF OTTOMAN, DEPINNED FROM D06572P PIN 2, REQUIRES REPAIR /REPLACEMENT. REPAIRED WIRE W9000-9051-BN-22 PER SWPM 20-30-12 & TERMINATED AT CONNECTOR D06572P PER SWPM 20-61-11. PERFORMED EMERG. LIGHTS OPS CK PER AMM 33-51-00. OPS CHECKS GOOD. (SEE ALSO SDR AALA201711109025)

Part: WIRE — DISCONNECTED (CABIN) · airframe 84,139 hrs · 23,291 cycles

THE AIRCRAFT WAS GROUNDED. FOUND W9000-9051 BN-22 BROWN WIRE IN TWO FORWARD SIDE OF OTTOMAN, DEPINNED FROM D06572P PIN 5, REQUIRES REPAIR /REPLACEMENT. REPAIRED WIRE W90000-9051BK-22 PER SWPM 20-30-12 & TERMINATED AT CONNECTOR D06572P PER SWPM 20-61-11 PERFORMED EMERG. LIGHTS OPS CHECK PER AMM 33-51-00. OPS CKS GOOD. (SEE ALSO SDR AALA201711109024)

Part: SIGN — INOPERATIVE (CABIN) · airframe 83,787 hrs · 23,201 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD GALLEY BIDIRECTIONAL ARROW EMERGENCY EXIT IDENTIFIER SIGN / LIGHT INOPERATIONAL. REMOVED AND REPLACED THE FORWARD GALLEY BIDIRECTIONAL ARROW EMERGENCY EXIT IDENTIFIER SIGN /LIGHT IAW AMM REF 33-51-10.

Part: LENS — BROKEN (CABIN) · airframe 83,787 hrs · 23,201 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT ABOVE THE R2 DOOR HAS A BROKEN LENS COVER. REMOVED AND REPLACED LENS COVER PER AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 83,624 hrs · 23,166 cycles

AIRCRAFT WAS NOT GROUNDED. L2 DOOR AFT EMERGENCY EXIT LIGHT IS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM 33-51-10. OPERATIONAL CHECK GOOD.

Part: SIGN — DETACHED (CABIN) · airframe 83,438 hrs · 23,116 cycles

AIRCRAFT WAS NOT GROUNDED. RIGHT FORWARD OVERWING EMERGENCY EXIT SIGN IS DETACHED AND IN THE COCKPIT. REPOSITIONED EXIT SIGN.

Part: LENS — DAMAGED (CABIN) · airframe 83,429 hrs · 23,114 cycles

AIRCRAFT WAS GROUNDED. RIGHT FORWARD OVERWING EMERGENCY LIGHT LENS COVER, CLIP BROKEN. SECURED CLIP ASSEMBLY ON EMERGENCY SIGN LENS COVER. OPERATIONAL CHECK PER AMM 33-51-01 GOOD.

Part: STRAP — LOOSE (ZONE 800) · airframe 83,353 hrs · 23,093 cycles

AIRCRAFT WAS NOT GROUNDED. FOUND R2 DOOR SLIDE COVER LOOSE. TIGHTENED PULL STRAP PER AMM 25-00-00.

Part: FITTING — DAMAGED (RT WING) · airframe 83,255 hrs · 23,059 cycles

RIGHT WING OTBD SIDE LOAD FITTING AFT INBOARD VERTICAL FASTENER HAS HOLE DAMAGE. REPAIRED IAW EA 270320.

Part: GIRT BAR — DETACHED (L4 DOOR) · airframe 83,231 hrs · 23,048 cycles

L4 DOOR EMERGENCY EVACUATION SLIDE LIGHT EXTINGUISHED DURING DESCENT. INSTALLED THE GIRT BAR IN FORWARD FITTING IAW AMM 25-66-01. OPS CHECKED GOOD.

Part: CONTROL PANEL — FAULTY (ZONE 200) · airframe 83,189 hrs · 23,035 cycles

AIRCRAFT WAS NOT GROUNDED. SQUIB TEST 1 FOR SLIDE AND TEST 2 FOR BOTTLE PRESSURE WILL NOT TEST. RELAMP WAS NO HELP. REMOVED AND REPLACED SQUIB TEST CONTROL PANEL IAW AMM 26 21 04. OPERATIONAL CHECK GOOD.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 83,037 hrs · 22,984 cycles

AIRCRAFT WAS GROUNDED. L1 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR IS DIFFICULT TO OPEN. ADJUSTED GIRT BAR IAW AMM 52-11-25. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 83,037 hrs · 22,984 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT L2 DOOR HAS A MISSING LENS COVER. INSTALLED LENS COVER. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,604 hrs · 22,862 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT LIGHTS INOPERATIVE ON ALL DOORS AND ALL SEATS IN FIRST CLASS AND COACH. REMOVED AND REPLACED FOUR BATTERY PACKS AND THREE CONTROL MODULES AT M10798, M10799, M10800 AND M10801 IAW AMM 33-51-07. OPERATIONAL CHECK GOOD. REF: AALA20170220018, AALA20170220020, AALA20170220021, AALA20170220022, AALA20170220023, AALA20170220024.

Part: MODULE — INOPERATIVE (CABIN) · airframe 82,604 hrs · 22,862 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT LIGHTS INOPERATIVE ON ALL DOORS AND ALL SEATS IN FIRST CLASS AND COACH. REMOVED AND REPLACED FOUR BATTERY PACKS AND THREE CONTROL MODULES AT M10798, M10799, M10800 AND M10801 IAW AMM 33-51-07. OPERATIONAL CHECK GOOD. REF: AALA20170220018, AALA20170220019, AALA20170220020, AALA20170220021, AALA20170220022, AALA20170220024.

Part: LENS — MISSING (CABIN) · airframe 82,604 hrs · 22,862 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT FLOODLIGHT L9005 AT FORWARD GALLEY WALL HAS A MISSING LENS COVER. REPLACED LENS COVER IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: MODULE — INOPERATIVE (CABIN) · airframe 82,604 hrs · 22,862 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT LIGHTS INOPERATIVE ON ALL DOORS AND ALL SEATS IN FIRST CLASS AND COACH. REMOVED AND REPLACED FOUR BATTERY PACKS AND THREE CONTROL MODULES AT M10798, M10799, M10800 AND M10801 IAW AMM 33-51-07. OPERATIONAL CHECK GOOD. REF: AALA20170220018, AALA20170220019, AALA20170220020, AALA20170220021, AALA20170220023, AALA20170220024.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,604 hrs · 22,862 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT LIGHTS INOPERATIVE ON ALL DOORS AND ALL SEATS IN FIRST CLASS AND COACH. REMOVED AND REPLACED FOUR BATTERY PACKS AND THREE CONTROL MODULES AT M10798, M10799, M10800 AND M10801 IAW AMM 33-51-07. OPERATIONAL CHECK GOOD. REF: AALA20170220018, AALA20170220019, AALA20170220021, AALA20170220022, AALA20170220023, AALA20170220024.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,604 hrs · 22,862 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT LIGHTS INOPERATIVE ON ALL DOORS AND ALL SEATS IN FIRST CLASS AND COACH. REMOVED AND REPLACED FOUR BATTERY PACKS AND THREE CONTROL MODULES AT M10798, M10799, M10800 AND M10801 IAW AMM 33-51-07. OPERATIONAL CHECK GOOD. REF: AALA20170220018, AALA20170220019, AALA20170220020, AALA20170220022, AALA20170220023, AALA20170220024.

Part: MODULE — INOPERATIVE (CABIN) · airframe 82,604 hrs · 22,862 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT LIGHTS INOPERATIVE ON ALL DOORS AND ALL SEATS IN FIRST CLASS AND COACH. REMOVED AND REPLACED FOUR BATTERY PACKS AND THREE CONTROL MODULES AT M10798, M10799, M10800 AND M10801 IAW AMM 33-51-07. OPERATIONAL CHECK GOOD. REF: AALA20170220018, AALA20170220019, AALA20170220020, AALA20170220021, AALA20170220022, AALA20170220023.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,604 hrs · 22,862 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT LIGHTS INOPERATIVE ON ALL DOORS AND ALL SEATS IN FIRST CLASS AND COACH. REMOVED AND REPLACED FOUR BATTERY PACKS AND THREE CONTROL MODULES AT M10798, M10799, M10800 AND M10801 IAW AMM 33-51-07. OPERATIONAL CHECK GOOD. REF: AALA20170220019, AALA20170220020, AALA20170220021, AALA20170220022, AALA20170220023, AALA20170220024

Part: GCU — FAULTY (ZONE 100) · airframe 82,461 hrs · 22,831 cycles

AIRCRAFT WAS GROUNDED. JFK-CUN FLIGHT. DURING TAKEOFF, CREW REPORTED A LEFT GENERATOR DRIVE AND A LEFT IDG FAULT LIGHTS. ABORTED TAKEOFF AT 90 KNOTS. REMOVED AND REPLACED GENERATOR CONTROL UNIT IAW AMM 24-22-02 AND THE INTEGRATED DRIVE GENERATOR IAW AMM 24-11-01 (AALA20170201020). LEAK AND OPERATIONAL CHECK GOOD.

Part: IDG — FAULTY (LT ENGINE) · airframe 82,461 hrs · 22,831 cycles

AIRCRAFT WAS GROUNDED. JFK-CUN FLIGHT. DURING TAKEOFF, CREW REPORTED A LEFT GENERATOR DRIVE AND A LEFT IDG FAULT LIGHTS. ABORTED TAKEOFF AT 90 KNOTS. REMOVED AND REPLACED GENERATOR CONTROL UNIT IAW AMM 24-22-02 (AALA20170130003) AND THE INTEGRATED DRIVE GENERATOR IAW AMM 24-11-01. LEAK AND OPERATIONAL CHECK GOOD.

Part: ATTACH BRACKET — MISSING (ZONE 800) · airframe 82,287 hrs · 22,774 cycles

AIRCRAFT WAS GROUNDED. L4 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR MISSING PARTS. INSTALLED GIRT BAR ATTACHMENT BRACKET IAW AMM 52-11-25. OPERATIONAL CHECK GOOD.

Part: LENS — DAMAGED (CABIN) · airframe 82,231 hrs · 22,762 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY EXIT LIGHT AT R2 DOOR HAS A DAMAGED LENS COVER. REPLACED LENS COVER IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (EMEGENCY LIGHTS) · airframe 81,904 hrs · 22,669 cycles

R4 DOOR EMERGENCY EXIT SIGN LENS COVER DETACHED. SECURED THE LENS IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: CHAIN — DAMAGED (L2 DOOR SLIDE) · airframe 81,696 hrs · 22,622 cycles

L2 EMERGENCY DOOR EVACUATION SLIDE CHAIN ASSEMBLY DAMAGED. REMOVED AND REPLACED CHAIN ASSEMBLY IAW AMM 25-66-01. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,471 hrs · 22,552 cycles

INTERIOR EMERGENCY SIDE WALL LIGHT AT R3 AND L3 DOORS ARE INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-51-07. OPERATIONS CHECK GOOD IAW AMM 33-51-07. THE AIRCRAFT WAS GROUNDED.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,471 hrs · 22,552 cycles

SEAT MOUNTED EMERGENCY LIGHTS ON SEATS 9D - 15D ARE INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER MODULE AND BATTERY PACK IAW AMM 33-51-07. OPS CHECKED GOOD. THE AIRCRAFT WAS GROUNDED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,471 hrs · 22,552 cycles

INTERIOR EMERGENCY SIDE WALL LIGHT AT R2 AND L2 DOORS ARE INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER MODULE AND BATTERY PACK IAW AMM 33-51-07. OPS CHECKED GOOD. THE AIRCRAFT WAS GROUNDED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,471 hrs · 22,552 cycles

SEAT MOUNTED EMERGENCY LIGHTS ON SEATS 26D - 36D ARE INOPERATIVE. REPLACED BATTERY PACK IAW AMM 33-51-07. OPS CHECKED GOOD IAW AMM 33-51-07. THE AIRCRAFT WAS GROUNDED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,471 hrs · 22,552 cycles

SEAT MOUNTED EMERGENCY LIGHTS ON SEATS 26D - 36D ARE INOPERATIVE. REPLACED BATTERY PACK IAW AMM 33-51-07. OPS CHECKED GOOD, IAW AMM 33-51-07. THE AIRCRAFT WAS GROUNDED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,179 hrs · 22,070 cycles

FOUND CORROSION ON TOP OF FLOORBEAM AT STATION 1681, LBL 4. INSTALLED DOUBLER REPAIR IAW SRM 53-60-51-2R-3. ACFT IN BASE MX.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,179 hrs · 22,070 cycles

FOUND CORROSION ON STATION 1681, FLOORBEAM AT RBL 26, ON TOP OF BEAM. INSTALLED T CAP REPAIR ON FLOORBEAM IAW SRM 53-60-51-2R-3. ACFT IN BASE MX.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,179 hrs · 22,070 cycles

CORROSION FOUND ON 1661 FLOORBEAM AT L4 DOOR AREA. INSTALLED T CAP REPAIR IAW SRM 53-00-51-2R-8. ACFT IN BASE MX.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 80,179 hrs · 22,070 cycles

RIGHT WW CORROSION ON KEEL BEAM CTR WEB AROUND A HYD LINE FITTING AT STATION 1176, APPROX 28 INCHES ABOVE THE LOWER HORIZONTAL OF THE KEEL BEAM. DAMAGE WAS REMOVED BY BLENDING. THE BLENDED WEB WAS MAPPED ON A .5" GRID & HFEC SURFACE SCANNED & DIGITAL THICKNESS DONE. FASTENER HOLES COMMON TO THE REPAIR WERE HFEC INSPECTED. A DOUBLER WAS FABRICATED & INSTALLED. ALL WORK PERFORMED IAW EA 258086. ACFT IN BASE MX.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,179 hrs · 22,070 cycles

FOUND CORROSION ON FLOORBEAM UPPER FLANGE. REMOVED UPPER FLANGE & INSTALLED T CAP REPAIR IAW SRM 53-10-08-2R-1. ACFT IN BASE MX.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,179 hrs · 22,070 cycles

CORROSION STATION 377, LBL 39 - LBL 66, UPPER T CAP. ACCOMPLISHED T CAP REPAIR IAW SRM 53-00-51-2R-8. ACFT IN BASE MX.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,179 hrs · 22,070 cycles

CORROSION ON LOWER SURFACE OF PRESS DECK IN AREA OVER SLIDE BOX, APPROX 8 INCHES FWD OF STATION 1180, BULKHEAD & APPROX 60 INCHES LBL. REMOVED CORROSION & REPAIRED FOLLOWING INSTRUCTIONS OF EA 258179. ACFT IN BASE MX.

Part: SHIM — MIGRATED (FUSELAGE) · airframe 80,179 hrs · 22,070 cycles

SHIMS AT MAIN GEAR BODY DOOR CTR HINGE, ATTACH POINT ON KEEL BEAM WERE FOUND MIGRATED. REPAIRED FOLLOWING INSTRUCTIONS OUTLINED IN EA 258135. ACFT IN BASE MX.

Part: SHIM — MIGRATED (FUSELAGE) · airframe 80,179 hrs · 22,070 cycles

SHIMS AT THE RT MAIN GEAR DOOR CTR HINGE, ATTACH POINT ON KEEL BEAM WERE FOUND MIGRATED. REPAIRED FOLLOWING INSTRUCTIONS OUTLINED IN EA 258186. ACFT IN BASE MX.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,179 hrs · 22,070 cycles

RIGHT HAND WW CORROSION ON THE KEEL BEAM WEB UNDER THE ACFT LEVELING PLATE. REPAIRED FOLLOWING INSTRUCTIONS OUTLINED IN EA 258194. ACFT IN BASE MX.

Part: SKIN — CORRODED (LE SLAT) · airframe 75,613 hrs · 20,834 cycles

NUMBER 2 SLAT LE CORRODED FWD OF OTBD DRIVE TRACK. ACCOMPLISHED PERMANENT FLUSH REPAIR FWD OF OTBD DRIVE TRACK NR 2 SLAT IAW AARD 57-43-00-1 FIGURE 2, SRM 57-43-01-2R DETAIL 1 & EA B757-57-036052.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 75,293 hrs · 20,750 cycles

RIGHT PACK FAILED WITH LT PACK ON MEL. ACFT WAS UNABLE TO PRESSURIZE. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT AIR CYCLE MACHINE & FLOW CONTROL VLV MPN S210T130608.

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 72,750 hrs · 20,140 cycles

HNL LT FUEL QUANTITY INDICATION BLANKED THEN RETURNED & RIGHT FUEL QUANTITY THEN WENT ERRATIC & LOST THE TOTAL FUEL INDICATION. EMERGENCY DECLARED FLIGHT RETURNED HNL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED QUANTITY INDICATOR, SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: BLEED VALVE — MALFUNCTIONED (LT ENGINE) · airframe 71,722 hrs · 19,894 cycles

LAX CREW REPORTED ON TAKEOFF LT ENGINE HI STAGE LIGHT ILLUMINATED. FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HIGH STAGE VALVE. SYSTEM GROUND CHECKED NORMAL. OPERATION (CLOSED)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,174 hrs · 19,499 cycles

WING TO BODY ATTACH FRAME STATION 1200, RIGHT BUTTLINE 40 IS CORRODED. INSTALLED NEW FRAME PER B757 SRM 51-40-02 AND AARD 51-00-05-1.

Part: SKIN — CHAFED (TE FLAP) · airframe 70,174 hrs · 19,499 cycles

LEFT MAIN FLAP LEADING EDGE SKIN CHAFFED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER AND FILLER PER EA B757-57-028330.

Part: STIFFENER — CORRODED (LT WING) · corrosion level 2 · airframe 70,174 hrs · 19,499 cycles

LEFT WING, REAR SPAR STIFFENER AT RSS 202.92 IS CORRODED AT DEFUEL VALVE BONDING FASTENER LOCATION. REMOVED CORROSION FROM STIFFENER PER EA B757-57-028324.

Part: PRESSURE DECK — DAMAGED (RT MLG WW) · airframe 70,174 hrs · 19,499 cycles

INTERIM REPAIR ACCOMPLISHED ON WHEEL WELL PRESSURE DECK STATION 1100 RIGHT BUTTLINE 49. REPAIRED WHEEL WELL PRESSURE DECK PER EA B757-53-028413 AND REO G15873 REVISION F.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,174 hrs · 19,499 cycles

FUSELAGE INTERNAL RIGHT SIDE CUSP WEB CORRODED FROM BODY STATIONS 940 TO 960, STRINGER 17 RIGHT. REMOVED AND REPLACED WEB PER AARD 51-00-05-1.

Part: SHIM — MIGRATED (LT PYLON) · airframe 70,174 hrs · 19,499 cycles

LEFT ENGINE PYLON MID BULKHEAD INBOARD LOWER FORWARD ATTACH SHIMS MIGRATING. HIGH FREQUENCY EDDY CURRENT INSPECTION REVEALED CRACK INDICATIONS ON BOTH HOLES. REPAIRED AFT FASTENER LOCATION AND INSTALLED NEW SHIMS AT BULKHEAD TO CHORD ATTACH POINT PER AARD 54-50-02-1, REPAIRED FORWARD FASTENER LOCATION PER EA B757-54-028295.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 70,174 hrs · 19,499 cycles

LEFT AFT FUSELAGE, DENT AND GOUGE IN SKIN, FORWARD OF AFT BODY ACCESS DOOR AT STATION 1738. INSTALLED DOUBLER REPAIR PER EA B757-53-028384 AND REO G15978 REVISION B.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,174 hrs · 19,499 cycles

REPAIR DOUBLER FRAME STATIONS 1710 TO 1720, RIGHT BUTTLINE 50 TO LEFT BUTTLINE 50, HAS CORROSION ON TOP SIDE. REMOVED AND REPLACED DOUBLER PER SRM 53-60-51-2R2 TABLE II.

Part: SUPPORT — GOUGED (R1 DOOR) · airframe 70,174 hrs · 19,499 cycles

RIGHT NUMBER 1 DOOR FORWARD SEAL RETAINER SUPPORT GOUGED. REPLACED SEAL RETAINER SUPPORT PER BOEING DRAWING 141N6237 AND SRM 51-40-02.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 70,174 hrs · 19,499 cycles

MAIN CABIN, NUMBER 3 SEAT TRACK GOUGED, BODY STATION 810, RIGHT BUTTLINE 25. INSTALLED NEW SEAT TRACK PER BAC DRWG 143N5080 AND SRM 51-40-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,174 hrs · 19,499 cycles

RIGHT SIDE CUSP WEB CORRODED FROM BODY STATIONS 996 TO 1020, STRINGER 17 RIGHT. REMOVED AND REPLACED WEB PER AARD 51-00-51-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,174 hrs · 19,499 cycles

FUSELAGE INTERNAL RIGHT SIDE CUSP WEB CORRODED FROM BODY STATIONS 996 TO 1020, STRINGER 17 RIGHT. REMOVED AND REPLACED WEB PER AARD 51-00-51-1.

Part: LIGHT — BROKEN (CABIN) · airframe 68,852 hrs · 19,190 cycles

SEAT 10D SEAT-MOUNTED EMERGENCY EVACUATION LIGHT ASSEMBLY BROKEN. REPLACED SEAT 10D SEAT-MOUNTED EMERGENCY EVACUATION LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,770 hrs · 19,172 cycles

EMERGENCY PATH LIGHTING, NO TEST. MODULE INOPERATIVE.

Part: SLIDE — LOW PRESSURE (R4 DOOR) · airframe 67,681 hrs · 18,899 cycles

FLIGHT ATTENDANT REPORTED RIGHT NUMBER 4 DOOR SLIDE PRESSURE SEEMED LOW. REMOVED AND REPLACED RIGHT NUMBER 4 DOOR SLIDE.

Part: STRAP — CRACKED (FUSELAGE) · airframe 65,602 hrs · 18,335 cycles

STRAP CRACKED IN LEFT HAND TUNNEL AREA CABIN FLOOR STATIONS 365 TO 377.7. REPAIRED STRAP PER SRM 51-10-51-2R AND EA B757-53-019794.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,602 hrs · 18,335 cycles

CORROSION ON CREASE BEAM WEB ASSEMBLY. REPLACED WEB PER SRM 51-10-02-0G.

Part: HYDRAULIC LINE — INOPERATIVE (HYDRAULIC SYS) · airframe 65,571 hrs · 18,324 cycles

DFW - INFLIGHT LAX-MIA. CREW REPORTED RIGHT HYDRAULIC QUANITITY AND RIGHT RESERVOIR LIGHTS ILLUMINATED. FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT HYDRAULIC HORIZONTAL STABILIZER TRIM CONTROL HYDRAULIC LINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BUTTON — MALFUNCTIONED (TORQUE LIMITER) · airframe 62,393 hrs · 17,559 cycles

LAX - CREW REPORTED LEADING EDGE SLAT STUCK AND ONLY ABLE TO LAND FLAPS 20. EMERGENCY DECLARED FLIGHT LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RESET TORQUE LIMITER OVERLOAD BUTTON THAT HAD BEEN EXTENDED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

FIRST CLASS SEATS MOUNTED EMERGENCY LIGHTS DIM ON TEST. LIGHT SYS TESTED GOOD AFTER REPLACED BATTERY PACK CPN NR BAT5016.

Part: PLACARD — PEELING (CABIN) · airframe 60,414 hrs · 17,122 cycles

AFT LEFT OVERWING HATCH EXIT MARKER PEELING. REMOVED AND REPLACED LEFT AFT OVERWING HATCH EXIT MARKER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,983 hrs · 16,789 cycles

AFT COACH EMERGENCY LIGHTS ARE DIM. REPLACED BATTERY PACK FOR AFT COACH EMERGENCY LIGHTS. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,983 hrs · 16,789 cycles

COACH EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK FOR COACH EMERGENCY LIGHTS. OPS CHECKED NORMAL.

Part: LIGHT — MISSING (CABIN) · airframe 58,983 hrs · 16,789 cycles

EMERGENCY LIGHT AT SEAT 27D MISSING LENS, GUARD, & BULBS. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 27D. OPS CHECKED NORMAL.

Part: MOUNT — BROKEN (CABIN) · airframe 57,907 hrs · 16,538 cycles

EMERGENCY LIGHT AT SEAT ROW 30D MOUNT BROKEN. INSTALLED NEW BASE AND LENS ON SEAT ROW 30D.

Part: LIGHT — INOPERATIVE (ZONE 200)

DFW - BULL NOSE EMERGENCY LIGHT AT 25DEF INOPERATIVE. REPLACED LIGHT ASSEMBLY AT BULL NOSE.

Part: PLACARD — DAMAGED (ZONE 200)

DFW - RIGHT AFT OVERWING SIDEWALL EXIT PLACARD DAMAGED. INSTALLED SERVICEABLE PLACARD.

Part: PLACARD — DAMAGED (ZONE 200)

DFW - LEFT AFT OVERWING SIDE WALL EXIT PLACARD DAMAGED. INSTALLED SERVICEABLE PLACARD.

Part: PLATE — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 16D MISSING BACKPLATE. REPLACED BACKPLATE FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

LAX - SEAT MOUNTED EMERGENCY LIGHTS AT AFT CABIN FAILED TEST. SECURED WALL SEAT CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 27DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — DENTED (FUSELAGE)

TUL - FUSELAGE SKIN HAS TWO DENTS/GOUGES FROM CARGO LOADER IMPACT AT STATION 1360 TO 1401 JUST BELOW AND FORWARD OF CARGO DOOR. THE AREAS AFFECTED ARE 15 INCHES BY 5 INCHES AND 10.5 INCHES BY 3.5 INCHES. DAMAGE WAS REMOVED AND REPAIRED PER AA ESO90309 REPAIR NUMBER 26536001 4688 DATED 25 MAY 2006.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS)

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. SECURED CONNECTOR AT SEAT 24F FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED MODULE P4010051112 BY DME CORPORATION AND BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS. FOUND LOOSE WIRE UNDER SEAT 5F. SECURED AND ROUTED WIRES FOR EMERGENCY LIGHTS AT SEAT 5F. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (ROW 16)

DFW - AFT EMERGENCY PATH LIGHT AT ROW 16 INOPERATIVE. REPLACED AFT EMERGENCY PATH LIGHT ASSEMBLY AT SEAT ROW 16. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - EMERGENCY LIGHTS FROM 27D TO BACK OF AIRCRAFT INOPERATIVE. REPAIRED SHORT NEAR L4 DOOR LIGHT AT L759 AND REPLACED BATTERY PACK ASSEMBLY FOR EMERGENCY LIGHTS FROM 27D TO BACK OF AIRCRAFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW EMERGENCY LIGHTS AT ROWS 27 THROUGH 36D INOPERATIVE. REPLACED BATTERY PACK M10801 FOR EMERGENCY LIGHTS AT ROWS 27 THROUGH 36D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

DFW SEAT MOUNTED EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. REPLACED SEAT 10D MOUNTED EMERGENCY LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TPU — FAILED (ENGINE)

APPROX 1 HOUR AFTER DEPARTURE AT COMPLETION OF CLIMB TO FL 380, THE THROTTLES RETARD TO 1.35 EPR A POSSIBLE COMPRESSOR STALL HAPPENED AT THAT POINT AS WE HEARD A POP AND THE AIRCRAFT BOUNCED. NEITHER PILOT WAS LOOKING AT ENGINE INSTRUMENTS TO SEE ANY INDICATIONS. ENGINES RAN SMOOTHLY AND NO OTHER INDICATIONS ON INSTRUMENTS. T/S IAW FIM AND FOUND RT TPU AT FAULT, REPLACED TPU AND ACCOM ALL REG CKS IAW MM. ALL CKS NORMAL. OK FOR SERVICE. REPLACED RT TPU. (SW21200401256)

Part: SENSOR — MALFUNCTIONED (HYD QTY)

CLIMBING OUT OF FL350 EICAS DISPLAYED LOSS OF LT HYD SYS QTY, RSVS LINE ON OVHD PANEL ILLUMINATED. AILERON INPUT, ON AUTOPILOT) INCREASED BY 3 UNITS. A LOUD BANG HEARD IN AIRFRAME. ABOUT ONE MINUTE AFTER INDICATIONS, BOTH PUMP PRESS LIGHTS WERE EXTINGUISHED ON LT SIDE. AN LEFT SYSTEM PRESSURE WAS NORMAL ON EICAS DURING DESCENT THROUGH 10,000 HYD QTY RETURNED FROM 0.0 TO 1.09 NORMAL. PLACARDED L HYD QTY IN COCKPIT (EICAS) INOPERATIVE PER MEL. ALL HYD QUANTITIES CHECKED AND FULL. NO LEAKS FOUND. PERFORMED WALKAROUND INSPECTION WITH ALL PUMPS ON. ALL FLIGHTS CONTROLS OPERATED NORMAL. REPLACED HYDRAULIC QUANTITY MONITOR UNIT PER M/M ALL REQUIRED TESTS CHECKED OK. REMOVED PLACARD CLEARED MIC SHEET. (M)

Part: LINE — LEAKING (RT MLG)

HYDRAULIC QTY LEAK RT MAIN GEAR FLEX LINE FOR TRUCK POSITION ACT. REMOVED AND REPLACED FLEX LINE, OPS AND LEAK CHECKED OK ACT CHECKED NORMAL. (M)

Part: HYDRAULIC LINE — RUPTURED (HYD SYSTEM)

DFW - FLT 1108 - EN ROUTE CUN-DFW, CAPTAIN REPORT LEFT HYDRAULIC QUANTITY LOSS. CAPTAIN DECLARED EMERGENCY AND LANDED AT DFW WITHOUT INCIDENT. FOUND RUPTURED LINE IN LEFT WHEEL WELL. REPLACED LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON FLOORBEAM MID SPAN. REPAIRED FLOORBEAM PER BOEING 757 SRM 53-00-51-2 AND 51-70-00. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 1E THROUGH SEAT 16D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (COCKPIT)

SNA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT DID NOT ILUMINATE IN ARMED POSITION. RE-CONNECTED EMERGENCY EXIT LIGHT AT CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DISCONNECTED (ROW 1)

SFO -DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS IN ROW ONE DISCONNECTED. RECONNECTED FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS IN ROW ONE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — DEFECTIVE (CABIN)

DFW - DURING MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT NOPERATIVE IN FORWARD CABIN. REPLACED EMERGENCY EXIT FLOOR PATH CONNECTOR IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (ROW 9D)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT ROW 9D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT ROW 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — SHORTED (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 17D FOUND INOPERATIVE. REPAIRED SHORTED FLAT CONDUCTOR AT SEAT 17D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTING IN THE AFT CABIN DIM. REPAIRED BROKEN WIRE ON THE EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL STRIP — BROKEN (CABIN)

JFK - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHT STRIP BROKEN AT SEAT 1. REPAIRED LIGHT STRIP, SYSTEM GROUND CHECKED NORMAL OPERATION. (X)