N950AN

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 67,031 hrs · 28,601 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTS DO NOT COME ON DURING TEST FROM ROW 19ABC THRU 25ABC. REMOVED AND REPLACED BATTERY POWER PACK AT ROW 23ABC. PER AMM 33-51-06.

Part: LIGHT — DISLODGED (ZONE 200) · airframe 66,396 hrs · 28,284 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANTS REPORTS THAT SEAT 31C EXIT LIGHT IS HANGING ON FLOOR. REPOSITIONED AND SECURED 31C EMERGENCY LIGHT. PER AMM 33-51-11.

Part: MODULE — FAULTY (ZONE 700 LEVER) · airframe 66,341 hrs · 28,259 cycles

AIRCRAFT WAS GROUNDED: ANTI-SKID INOPERATIVE LIGHT ILLUMINATED ON TAXIWAY WITH PARKING BRAKE SET. RELEASED AND REAPPLIED THE PARKING BRAKE THE LIGHT TURNED OFF AND REILLUMINATED. T/S PER FIM 32-42-00-810-812. RESISTANCE CHECK FAILED ON THE S3 SWITCH OF THE LANDING GEAR CONTROL LEVER. REMOVE AND REPLACED LANDING GEAR LEVER MODULE, PER 32-31-11. LANDING GEAR CONTROL SYSTEM TEST GOOD, PER AMM 32-31-00. AACU GEARS FAULT WENT AWAY.

Part: SLIDE — DISLODGED (ZONE 800) · airframe 66,243 hrs · 28,214 cycles

AIRCRAFT WAS GROUNDED: R1 DOOR SLIDE BUSTLE LOOSE. RESECURED R1 DOOR BUSTLE. PERF AMM 25-66-01, OPERATIONAL CHECK GOOD.

Part: FLAP SYSTEM — FAULTED · airframe 66,211 hrs · 28,199 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: LEADING EDGE FLAPS WERE RAISED BUT THE FLAPS TRANSIT LIGHT REMAINED ILLUMINATED, RECYCLE FLAPS DID NOT HELP. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT LAX. (OPEN).

Part: TARGET — DAMAGED (ZONE 500 SLAT) · airframe 66,211 hrs · 28,199 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: LEADING EDGE FLAPS WERE RAISED BUT THE FLAPS TRANSIT LIGHT REMAINED ILLUMINATED, RECYCLE FLAPS DID NOT HELP. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT LAX. REMOVED AND REPLACED OUTBOARD SLAT UP SENSOR BRACKET (AALA202508196316) AND TARGET (AALA202508259181). ACCOMPLISHED SLAT ADJUSTMENT RIG (AALA202508254942). ACCOMPLISHED SLAT SENSOR ADJUSTMENTS. OPERATIONAL CHECK SLAT SENSORS AND SLAT ALL CHECKS GOOD. PRT AMM 27-81-21, 27-81-00, 27-88-11.

Part: SLAT — OUT OF RIG (ZONE 500) · airframe 66,211 hrs · 28,199 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: LEADING EDGE FLAPS WERE RAISED BUT THE FLAPS TRANSIT LIGHT REMAINED ILLUMINATED, RECYCLE FLAPS DID NOT HELP. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT LAX. REMOVED AND REPLACED OUTBOARD SLAT UP SENSOR BRACKET (AALA202508196316) AND TARGET (AALA202508259181). ACCOMPLISHED SLAT ADJUSTMENT RIG (AALA202508254942). ACCOMPLISHED SLAT SENSOR ADJUSTMENTS. OPERATIONAL CHECK SLAT SENSORS AND SLAT ALL CHECKS GOOD. PRT AMM 27-81-21, 27-81-00, 27-88-11.

Part: SENSOR — FAULTED (ZONE 500) · airframe 66,211 hrs · 28,199 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: LEADING EDGE FLAPS WERE RAISED BUT THE FLAPS TRANSIT LIGHT REMAINED ILLUMINATED, RECYCLE FLAPS DID NOT HELP. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT LAX. REMOVED AND REPLACED OUTBOARD SLAT UP SENSOR BRACKET (AALA202508196316) AND TARGET (AALA202508259181). ACCOMPLISHED SLAT ADJUSTMENT RIG (AALA202508254942). ACCOMPLISHED SLAT SENSOR ADJUSTMENTS. OPERATIONAL CHECK SLAT SENSORS AND SLAT ALL CHECKS GOOD. PRT AMM 27-81-21, 27-81-00, 27-88-11.

Part: SLIDE — DISLODGED (ZONE 800) · airframe 65,506 hrs · 27,852 cycles

AIRCRAFT WAS NOT GROUNDED: AFT ENTRY SLIDE FALLING OUT OF BUSTLE. RESECURED SLIDE AT AFT CABIN DOOR. PER AMM 52-00-00.

Part: OVEN — ODOR (ZONE 900) · airframe 64,694 hrs · 27,484 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: BURNING OIL SMOKE ODOR IN THE CABIN AND FLIGHT DECK DURING FINAL STAGES OF CLIMB, O2 MASK HAD TO BE DEPLOYED AND USED BY EVERYONE ON THE FLIGHT; AIRCRAFT DIVERTED TO AND LANDED SAFELY AT RDU. DURING SOF CARD TROUBLESHOOTING FORWARD GALLEY NUMBER 1 OVEN FOUND TO BE THE SOURCE OF ODOR IN THE CABIN. REMOVED AND REPLACED FORWARD GALLEY NUMBER 1 OVEN. OPERTIONAL CHECK GOOD. PER AMM 25-32-03-400-801.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 64,271 hrs · 27,303 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED BREAK ASSEMBLY PANEL LOCATED AT STA 537.45 BETWEEN LBL 24.75 AND LBL 45.50. REPLACED BREAK ASSEMBLY PANEL PER SRM 51-40-02.

Part: FITTING — CRACKED (ZONE 100) · airframe 64,271 hrs · 27,303 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (ZONE 200) · airframe 64,271 hrs · 27,303 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 6.14. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (ZONE 200) · airframe 64,271 hrs · 27,303 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (ZONE 200) · airframe 64,271 hrs · 27,303 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (ZONE 200) · airframe 64,271 hrs · 27,303 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 15.04. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (ZONE 100) · airframe 64,271 hrs · 27,303 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (ZONE 200) · airframe 64,271 hrs · 27,303 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (ZONE 100) · airframe 64,271 hrs · 27,303 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 6.14. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (ZONE 100) · airframe 64,271 hrs · 27,303 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: FITTING — CRACKED (ZONE 100) · airframe 64,271 hrs · 27,303 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 15.04. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.

Part: ANTI-SKID SYS — FAULTY (ZONE 100) · airframe 63,621 hrs · 26,967 cycles

AIRCRAFT IN BASE MAINTENANCE: UPON TOUCHDOWN, WITH AUTO BRAKES SET TO 3, AUTO BRAKE DISARM LIGHT ILLUMINATED AND ANTI-SKID INOPERATIVE LIGHT BEGAN FLASHING. REPLACED ANTI-SKID AUTOBRAKE CONTROL UNIT AND PERFORMED OPERTIONAL CHECK GOOD. PER AMM 32-42-00-720-801.

Part: BAFFLE — CRACKED (ZONE 100) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT WAS GROUNDED: CRACK IN AFT CARGO COMPARTMENT FLOOR STRUCTURE AT STA 946, RBL 14. REPLACED BAFFLE PER AARD 51-00-05-01.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN SHEAR TIE ABOVE R1 DOOR AT STA 310, S6R. REPLACED SHEAR TIE PER SRM 51-10-02.

Part: SKIN — CRACKED (ZONE 300) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 157.10, 15 INCHES FORWARD OF AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.

Part: CHANNEL — NONE (ZONE 300) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER FORWARD SPAR J-CHANNEL HAS HAD THE INTERIM REPAIR PERFORMED PREVIOUSLY ON THE RIGHT HAND RELIEF CUTOUT PER AARD 55-30-09-3 REPAIR 3. COMPLETED PERMANENT REPAIR. PER AARD 55-30-09-3 REPAIR 3.

Part: BEAR STRAP — CRACKED (ZONE 200) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN R1 DOOR FRAME BEAR STRAP AT STA 312, RBL 8. ACCOMPLISHED DOUBLER REPAIR TO FUSELAGE SKIN PER SRM 53-10-01-2R-6 AND EA 356702.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOORBOARD INTERCOSTAL SUPPORT (CHORD) AT STA 390, LBL 11. REPLACED CHORD PER AAED 51-00-05-1.

Part: ANGLE — CRACKED (ZONE 100) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT INTERCOSTAL SUPPORT ANGLE AT STA 390, RBL 11. REPLACED SUPPORT ANGLE PER AARD 51-00-05-1.

Part: INTERCOSTAL — CRACKED (ZONE 100 - FUSE) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 284, RBL 2. REPLACED INTERCOSTAL PER AARD 51-00-05-1

Part: INTERCOSTAL — CRACKED (ZONE 100 - FUSE) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 308, RBL 31. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION CHANNEL OF FORWARD CARGO COMPARTMENT LOWER LOBE FRAME AT STA 500D, S25R. REPLACED CHANNEL PER SRM 53-00-07.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT AFT BULKHEAD REMOVABLE PANEL SUPPORT RAIL AT STA 500I, FROM S23L TO S25L. REPLACED RAIL PER AARD 51-00-05-1.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT AFT BULKHEAD SUPPORT ANGLE AT STA 947.5, FROM LBL 20 TO RBL 20. REPLACED SUPPORT ANGLE PER AARD 51-00-05-01.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT CLIP UNDER TRANSITION PANEL AT STA 727 FORWARD BULKHEAD, LBL 24.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR STRUCTURE TRANSITION PANEL FROM STA 727 TO STA 847, S25L REPLACED TRANSITION PANEL PER SRM 51-40-02..

Part: SHIELD — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHIELD BETWEEN STA 767 AND STA 787, RBL 21. REPLACED SHIELD PER AARD 51-00-05.

Part: SHIELD — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHIELD AT STA 439, RBL 23. REPLACED SHIED PER AARD 51-00-05-1. **SUPPLEMENTAL REPORT FOR AALA202408088853: QC REVIEWED THIS EVENT AND DETERMINED THAT IT WAS A LEVEL 2 FINDING. SECTION 7 CORROSION LEVEL FIELD UPDATED ACCORDINGLY.**

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 500E TO STA 500F, LBL 23, S24L. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R REPAIR 6.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 500G TO STA 500F, S24L. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R REPAIR 6.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 500C TO STA 500D, LBL 23, S24L. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R REPAIR 6.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 500D TO STA 500E, LBL 23, S24L. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R REPAIR 6.

Part: SHIELD — CORRODED (ZONE 100) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHIELD AT STA 439, RBL 23. REPLACED SHIED PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 500 TO STA 500I, S24L. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R-6.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 63,619 hrs · 26,965 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 500H TO STA 500G, S24L. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R REPAIR 6.

Part: LIGHT — DETACHED (ZONE 200) · airframe 63,522 hrs · 26,914 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT AT SEAT 32C IS DETACHED. SECURED EMERGENCY LIGHT AT ROW 32C. OPERTIONAL CHECKS GOOD.

Part: GUST LOCK — INOPERATIVE (L1 DOOR) · airframe 63,451 hrs · 26,865 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR GUST LOCK INOPERATIVE, WILL NOT STAY LOCKED OPEN. L1 DOOR GUST LOCK GUIDE ARM REPLACED. PER AMM 52-11-00.

Part: DOOR — OUT OF ADJUST (LAVATORY) · airframe 62,606 hrs · 26,441 cycles

AIRCRAFT WAS NOT GROUNDED: FWD LAV DOOR DIFFICULT TO OPEN - MORE PRONOUNCED AT ALTITUDE. MAINTENANCE ADJUSTED FWD LAV DOOR PER IAW AMM 25-40-00.

Part: SLIDE — MISALIGNED (ZONE 800 - DOORS) · airframe 62,242 hrs · 26,271 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS GIRT BAR ON R1 DOOR DIFFICULT TO STOW WHEN DISARMED. REMOVED R1 DOOR SLIDE AND COVER ASSEMBLY, RESET SLIDE INSIDE COVER ASSEMBLY, REINSTALLED ASSEMBLY.

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 62,018 hrs · 26,156 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY.

Part: FLASHLIGHT — NO TEST (ZONE 200 - FUSE) · airframe 61,631 hrs · 25,955 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT FLASHLIGHT FAILS BITE TEST AND TAMPER SEALS BROKEN. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY. PER AMM 25-64-00.

Part: RELAY — FAULTY (FUEL PUMP) · airframe 61,434 hrs · 25,856 cycles

AIRCRAFT WAS NOT GROUNDED: AFTER TAKEOFF RIGHT CENTER TANK FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED. REMOVE AND REPLACE THE PUMP CENTRAL RELAY AND POWER SWITCH RELAY ASSEMBLY. PER AMM 28-22-00. FUNCTIONAL CHECK GOOD AT THIS TIME.

Part: DOOR LATCH — DAMAGED (ZONE 800 - DOORS) · airframe 60,035 hrs · 25,175 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DOOR DIFFICULT TO CLOSE. REPLACED COCKPIT DOOR LATCH.

Part: UNKNOWN — UNSECURE (ZONE 800 - DOORS) · airframe 59,898 hrs · 25,110 cycles

AIRCRAFT WAS NOT GROUNDED: 1R DOOR GIRT BAR BRACKET LOOSE. SECURED GIRT BAR RETAINING CLIPS PER AMM 25-66-01.

Part: PUMP — LEAKING (ELECTRIAL HYD) · airframe 59,140 hrs · 24,748 cycles

AIRCRAFT WAS GROUNDED: PRIOR TO DESCENT MASTER CAUTION HYDRAULIC A ENGINE 1 LOW PRESSURE LIGHT ILLUMINATED. HYDRAULIC A PRESSURE AT 20% PERFORMED QUICK REFERENCE HANDBOOK LOSS OF SYSTEM A CHECKLIST. EMERGENCY WAS DECLARED INTO DFW. TROUBLESHOOTING FOUND HYDRAULIC LEAK IN A ELECTRIC HYDRAULIC PUMP. REMOVED AND REPLACED A ELECTRIC HYDRAULIC PUMP ACOUSTIC FILTER PER AMM 29-11-21.

Part: TANK UNIT — UNSERVICEABLE (FUEL SYSTEM) · airframe 58,845 hrs · 24,601 cycles

AIRCRAFT WAS GROUNDED: ON CLIMB A FUEL IMBALANCE WAS NOTED. LEFT HAND QUANTITY DECREASING AT AN EXCESSIVE RATE. FLIGHT DECLARED EMERGENCY AND RETURN TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202210179427: REPLACED ALL 12 LEFT WING TANK UNITS AND THE COMPENSATOR (AALA202210179427) PER AMM 28-41-21. REPLACED LEFT WING FUEL QUANTITY INDICATING SYSTEM (FQIS) WIRE HARNESS (AALA202210251119) PER AMM 28-41-44. ACCOMPLISHED SATISFACTORY BITE CHECK AND OPERATIONAL CHECK. (SEE AALA202210259769, AALA202210250626, AALA202210252619, AALA202210252070, AALA202210252089, AALA202210256264, AALA202210257099, AALA202210258998, AALA202210251438, AALA202210251858, AALA202210258884, AND AALA202210255105 FOR TANK UNIT PART INFORMATION).** (CLOSED)

Part: TANK UNIT — UNSERVICEABLE (FUEL SYSTEM) · airframe 58,845 hrs · 24,601 cycles

AIRCRAFT WAS GROUNDED: ON CLIMB A FUEL IMBALANCE WAS NOTED. LEFT HAND QUANTITY DECREASING AT AN EXCESSIVE RATE. FLIGHT DECLARED EMERGENCY AND RETURN TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202210179427: REPLACED ALL 12 LEFT WING TANK UNITS AND THE COMPENSATOR (AALA202210179427) PER AMM 28-41-21. REPLACED LEFT WING FUEL QUANTITY INDICATING SYSTEM (FQIS) WIRE HARNESS (AALA202210251119) PER AMM 28-41-44. ACCOMPLISHED SATISFACTORY BITE CHECK AND OPERATIONAL CHECK. (SEE AALA202210259769, AALA202210250626, AALA202210252619, AALA202210252070, AALA202210252089, AALA202210256264, AALA202210257099, AALA202210258998, AALA202210251438, AALA202210251858, AALA202210258884, AND AALA202210255105 FOR TANK UNIT PART INFORMATION).** (CLOSED)

Part: TANK UNIT — UNSERVICEABLE (FUEL SYSTEM) · airframe 58,845 hrs · 24,601 cycles

AIRCRAFT WAS GROUNDED: ON CLIMB A FUEL IMBALANCE WAS NOTED. LEFT HAND QUANTITY DECREASING AT AN EXCESSIVE RATE. FLIGHT DECLARED EMERGENCY AND RETURN TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202210179427: REPLACED ALL 12 LEFT WING TANK UNITS AND THE COMPENSATOR (AALA202210179427) PER AMM 28-41-21. REPLACED LEFT WING FUEL QUANTITY INDICATING SYSTEM (FQIS) WIRE HARNESS (AALA202210251119) PER AMM 28-41-44. ACCOMPLISHED SATISFACTORY BITE CHECK AND OPERATIONAL CHECK. (SEE AALA202210259769, AALA202210250626, AALA202210252619, AALA202210252070, AALA202210252089, AALA202210256264, AALA202210257099, AALA202210258998, AALA202210251438, AALA202210251858, AALA202210258884, AND AALA202210255105 FOR TANK UNIT PART INFORMATION).** (CLOSED)

Part: TANK UNIT — UNSERVICEABLE (FUEL SYSTEM) · airframe 58,845 hrs · 24,601 cycles

AIRCRAFT WAS GROUNDED: ON CLIMB A FUEL IMBALANCE WAS NOTED. LEFT HAND QUANTITY DECREASING AT AN EXCESSIVE RATE. FLIGHT DECLARED EMERGENCY AND RETURN TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202210179427: REPLACED ALL 12 LEFT WING TANK UNITS AND THE COMPENSATOR (AALA202210179427) PER AMM 28-41-21. REPLACED LEFT WING FUEL QUANTITY INDICATING SYSTEM (FQIS) WIRE HARNESS (AALA202210251119) PER AMM 28-41-44. ACCOMPLISHED SATISFACTORY BITE CHECK AND OPERATIONAL CHECK. (SEE AALA202210259769, AALA202210250626, AALA202210252619, AALA202210252070, AALA202210252089, AALA202210256264, AALA202210257099, AALA202210258998, AALA202210251438, AALA202210251858, AALA202210258884, AND AALA202210255105 FOR TANK UNIT PART INFORMATION).** (CLOSED)

Part: TANK UNIT — UNSERVICEABLE (FUEL SYSTEM) · airframe 58,845 hrs · 24,601 cycles

AIRCRAFT WAS GROUNDED: ON CLIMB A FUEL IMBALANCE WAS NOTED. LEFT HAND QUANTITY DECREASING AT AN EXCESSIVE RATE. FLIGHT DECLARED EMERGENCY AND RETURN TO PLS LANDING SAFELY. SUPPLEMENTAL REPORT FOR AALA202210179427: REPLACED ALL 12 LEFT WING TANK UNITS AND THE COMPENSATOR (AALA202210179427) PER AMM 28-41-21. REPLACED LEFT WING FUEL QUANTITY INDICATING SYSTEM (FQIS) WIRE HARNESS (AALA202210251119) PER AMM 28-41-44. ACCOMPLISHED SATISFACTORY BITE CHECK AND OPERATIONAL CHECK. (SEE AALA202210259769, AALA202210250626, AALA202210252619, AALA202210252070, AALA202210252089, AALA202210256264, AALA202210257099, AALA202210258998, AALA202210251438, AALA202210251858, AALA202210258884, AND AALA202210255105 FOR TANK UNIT PART INFORMATION).** (CLOSED)

Part: TANK UNIT — UNSERVICEABLE (FUEL SYSTEM) · airframe 58,845 hrs · 24,601 cycles

AIRCRAFT WAS GROUNDED: ON CLIMB A FUEL IMBALANCE WAS NOTED. LEFT HAND QUANTITY DECREASING AT AN EXCESSIVE RATE. FLIGHT DECLARED EMERGENCY AND RETURN TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202210179427: REPLACED ALL 12 LEFT WING TANK UNITS AND THE COMPENSATOR (AALA202210179427) PER AMM 28-41-21. REPLACED LEFT WING FUEL QUANTITY INDICATING SYSTEM (FQIS) WIRE HARNESS (AALA202210251119) PER AMM 28-41-44. ACCOMPLISHED SATISFACTORY BITE CHECK AND OPERATIONAL CHECK. (SEE AALA202210259769, AALA202210250626, AALA202210252619, AALA202210252070, AALA202210252089, AALA202210256264, AALA202210257099, AALA202210258998, AALA202210251438, AALA202210251858, AALA202210258884, AND AALA202210255105 FOR TANK UNIT PART INFORMATION).** (CLOSED)

Part: TANK UNIT — UNSERVICEABLE (FUEL SYSTEM) · airframe 58,845 hrs · 24,601 cycles

AIRCRAFT WAS GROUNDED: ON CLIMB A FUEL IMBALANCE WAS NOTED. LEFT HAND QUANTITY DECREASING AT AN EXCESSIVE RATE. FLIGHT DECLARED EMERGENCY AND RETURN TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202210179427: REPLACED ALL 12 LEFT WING TANK UNITS AND THE COMPENSATOR (AALA202210179427) PER AMM 28-41-21. REPLACED LEFT WING FUEL QUANTITY INDICATING SYSTEM (FQIS) WIRE HARNESS (AALA202210251119) PER AMM 28-41-44. ACCOMPLISHED SATISFACTORY BITE CHECK AND OPERATIONAL CHECK. (SEE AALA202210259769, AALA202210250626, AALA202210252619, AALA202210252070, AALA202210252089, AALA202210256264, AALA202210257099, AALA202210258998, AALA202210251438, AALA202210251858, AALA202210258884, AND AALA202210255105 FOR TANK UNIT PART INFORMATION).** (CLOSED)

Part: COMPENSATOR — UNSERVICEABLE (FUEL SYSTEM) · airframe 58,845 hrs · 24,601 cycles

AIRCRAFT WAS GROUNDED: ON CLIMB A FUEL IMBALANCE WAS NOTED. LEFT HAND QUANTITY DECREASING AT AN EXCESSIVE RATE. FLIGHT DECLARED EMERGENCY AND RETURN TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202210179427: REPLACED ALL 12 LEFT WING TANK UNITS AND THE COMPENSATOR (AALA202210179427) PER AMM 28-41-21. REPLACED LEFT WING FUEL QUANTITY INDICATING SYSTEM (FQIS) WIRE HARNESS (AALA202210251119) PER AMM 28-41-44. ACCOMPLISHED SATISFACTORY BITE CHECK AND OPERATIONAL CHECK. (SEE AALA202210259769, AALA202210250626, AALA202210252619, AALA202210252070, AALA202210252089, AALA202210256264, AALA202210257099, AALA202210258998, AALA202210251438, AALA202210251858, AALA202210258884, AND AALA202210255105 FOR TANK UNIT PART INFORMATION).** (CLOSED)

Part: SENSOR — UNSERVICEABLE (FUEL SYSTEM) · airframe 58,845 hrs · 24,601 cycles

AIRCRAFT WAS GROUNDED: ON CLIMB A FUEL IMBALANCE WAS NOTED. LEFT HAND QUANTITY DECREASING AT AN EXCESSIVE RATE. FLIGHT DECLARED EMERGENCY AND RETURN TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202210179427: REPLACED ALL 12 LEFT WING TANK UNITS AND THE COMPENSATOR (AALA202210179427) PER AMM 28-41-21. REPLACED LEFT WING FUEL QUANTITY INDICATING SYSTEM (FQIS) WIRE HARNESS (AALA202210251119) PER AMM 28-41-44. ACCOMPLISHED SATISFACTORY BITE CHECK AND OPERATIONAL CHECK. (SEE AALA202210259769, AALA202210250626, AALA202210252619, AALA202210252070, AALA202210252089, AALA202210256264, AALA202210257099, AALA202210258998, AALA202210251438, AALA202210251858, AALA202210258884, AND AALA202210255105 FOR TANK UNIT PART INFORMATION).** (CLOSED)

Part: TANK UNIT — UNSERVICEABLE (FUEL SYSTEM) · airframe 58,845 hrs · 24,601 cycles

AIRCRAFT WAS GROUNDED: ON CLIMB A FUEL IMBALANCE WAS NOTED. LEFT HAND QUANTITY DECREASING AT AN EXCESSIVE RATE. FLIGHT DECLARED EMERGENCY AND RETURN TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202210179427: REPLACED ALL 12 LEFT WING TANK UNITS AND THE COMPENSATOR (AALA202210179427) PER AMM 28-41-21. REPLACED LEFT WING FUEL QUANTITY INDICATING SYSTEM (FQIS) WIRE HARNESS (AALA202210251119) PER AMM 28-41-44. ACCOMPLISHED SATISFACTORY BITE CHECK AND OPERATIONAL CHECK. (SEE AALA202210259769, AALA202210250626, AALA202210252619, AALA202210252070, AALA202210252089, AALA202210256264, AALA202210257099, AALA202210258998, AALA202210251438, AALA202210251858, AALA202210258884, AND AALA202210255105 FOR TANK UNIT PART INFORMATION).** (CLOSED)

Part: TANK UNIT — UNSERVICEABLE (FUEL SYSTEM) · airframe 58,845 hrs · 24,601 cycles

AIRCRAFT WAS GROUNDED: ON CLIMB A FUEL IMBALANCE WAS NOTED. LEFT HAND QUANTITY DECREASING AT AN EXCESSIVE RATE. FLIGHT DECLARED EMERGENCY AND RETURN TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202210179427: REPLACED ALL 12 LEFT WING TANK UNITS AND THE COMPENSATOR (AALA202210179427) PER AMM 28-41-21. REPLACED LEFT WING FUEL QUANTITY INDICATING SYSTEM (FQIS) WIRE HARNESS (AALA202210251119) PER AMM 28-41-44. ACCOMPLISHED SATISFACTORY BITE CHECK AND OPERATIONAL CHECK. (SEE AALA202210259769, AALA202210250626, AALA202210252619, AALA202210252070, AALA202210252089, AALA202210256264, AALA202210257099, AALA202210258998, AALA202210251438, AALA202210251858, AALA202210258884, AND AALA202210255105 FOR TANK UNIT PART INFORMATION).** (CLOSED)

Part: WIRE HARNESS — DAMAGED (FUEL SYSTEM) · airframe 58,845 hrs · 24,601 cycles

AIRCRAFT WAS GROUNDED: ON CLIMB A FUEL IMBALANCE WAS NOTED. LEFT HAND QUANTITY DECREASING AT AN EXCESSIVE RATE. FLIGHT DECLARED EMERGENCY AND RETURN TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202210179427: REPLACED ALL 12 LEFT WING TANK UNITS AND THE COMPENSATOR (AALA202210179427) PER AMM 28-41-21. REPLACED LEFT WING FUEL QUANTITY INDICATING SYSTEM (FQIS) WIRE HARNESS (AALA202210251119) PER AMM 28-41-44. ACCOMPLISHED SATISFACTORY BITE CHECK AND OPERATIONAL CHECK.

Part: SENSOR — UNSERVICEABLE (FUEL SYSTEM) · airframe 58,845 hrs · 24,601 cycles

AIRCRAFT WAS GROUNDED: ON CLIMB A FUEL IMBALANCE WAS NOTED. LEFT HAND QUANTITY DECREASING AT AN EXCESSIVE RATE. FLIGHT DECLARED EMERGENCY AND RETURN TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202210179427: REPLACED ALL 12 LEFT WING TANK UNITS AND THE COMPENSATOR (AALA202210179427) PER AMM 28-41-21. REPLACED LEFT WING FUEL QUANTITY INDICATING SYSTEM (FQIS) WIRE HARNESS (AALA202210251119) PER AMM 28-41-44. ACCOMPLISHED SATISFACTORY BITE CHECK AND OPERATIONAL CHECK. (SEE AALA202210259769, AALA202210250626, AALA202210252619, AALA202210252070, AALA202210252089, AALA202210256264, AALA202210257099, AALA202210258998, AALA202210251438, AALA202210251858, AALA202210258884, AND AALA202210255105 FOR TANK UNIT PART INFORMATION).** (CLOSED)

Part: TANK UNIT — UNSERVICEABLE (FUEL SYSTEM) · airframe 58,845 hrs · 24,601 cycles

AIRCRAFT WAS GROUNDED: ON CLIMB A FUEL IMBALANCE WAS NOTED. LEFT HAND QUANTITY DECREASING AT AN EXCESSIVE RATE. FLIGHT DECLARED EMERGENCY AND RETURN TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202210179427: REPLACED ALL 12 LEFT WING TANK UNITS AND THE COMPENSATOR (AALA202210179427) PER AMM 28-41-21. REPLACED LEFT WING FUEL QUANTITY INDICATING SYSTEM (FQIS) WIRE HARNESS (AALA202210251119) PER AMM 28-41-44. ACCOMPLISHED SATISFACTORY BITE CHECK AND OPERATIONAL CHECK. (SEE AALA202210259769, AALA202210250626, AALA202210252619, AALA202210252070, AALA202210252089, AALA202210256264, AALA202210257099, AALA202210258998, AALA202210251438, AALA202210251858, AALA202210258884, AND AALA202210255105 FOR TANK UNIT PART INFORMATION).** (CLOSED)

Part: NONE — NONE · airframe 58,845 hrs · 24,601 cycles

AIRCRAFT WAS GROUNDED: ON CLIMB A FUEL IMBALANCE WAS NOTED. LEFT HAND QUANTITY DECREASING AT AN EXCESSIVE RATE. FLIGHT DECLARED EMERGENCY AND RETURN TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: PRESSURE SWITCH — FAULTY (ZONE 100 - FUSE) · airframe 58,616 hrs · 24,486 cycles

AIRCRAFT WAS NOT GROUNDED: AFTER TAKE OFF LOW HYDRAULIC B PRESSURE LIGHT CAME ON. PERFORMED TROUBLESHOOTING IN ACCORDANCE WITH FIM 27-21-00-810-814. CONFIRMED INTERMITTENT FAULT. CLEANED FLIGHT CONTROL B PRESSURE SWITCH AND PLUG IN ACCORDANCE WITH AMM 20-60-02.

Part: AIR DATA MODULE — INOPERATIVE (ZONE 100 - FUSE) · airframe 58,569 hrs · 24,463 cycles

AIRCRAFT WAS GROUNDED: AT APPROXIMATELY 16000 FEET IN THE CLIMB "AIRSPEED" DISAGREE ILLUMINATED ON BOTH PRIMARY FLIGHT DISPLAY'S. DETERMINED CAPTAIN'S AIR SPEED WAS UNRELIABLE AND FIRST OFFICER'S AND STANDBY AIRSPEED AGREED WITH EACH OTHER AND GROUND SPEED AS WE RUN QUICK REFERENCE CARD PLUS QUICK REFERENCE HANDBOOK CHECK LISTS, CONTINUED CLIMB AND CAPTAIN'S AIRSPEED INDICATOR CONTINUED DEVIATING TO APPROXIMATELY 18 KNOTS COMPARED TO FIRST OFFICER'S AND INTEGRATED STANDBY FLIGHT DISPLAY'S ENGINE INSTRUMENTS WENT TO DASHES AND RETURNED AS WE DESCENDED AND NORMALIZED TO EACH OTHER THE LOWER WE DESCENDED. REMOVED AND REPLACED LEFT AIR DATA MODULE PER AMM 34-21-04 (PITOT MODULE).

Part: NONE — OUT OF POSITION (ZONE 800 - DOORS) · airframe 58,404 hrs · 24,373 cycles

AIRCRAFT WAS NOT GROUNDED: A PORTION OF THE GIRT BAR RETAINING STRAP IS OUT OF THE RETAINING COVER. RE SECURED RETAINING STRAP IN POSITION FOR L1 DOOR, OK FOR CONTINUED SERVICE, REFERENCE AMM 25-66-01.

Part: NONE — NONE (ZONE 100 - FUSE) · airframe 58,134 hrs · 24,239 cycles

AIRCRAFT WAS GROUNDED: TANK FUEL IMBALANCE STARTED HAPPENING AT A HIGHER RATE THAN FUEL BURN FROM CENTER TANK AFTER TAKE OFF. UNABLE TO BURN CENTER TANK FUEL TO ARRIVE AT DESTINATION WITH SUFFICIENT FUEL AND BALANCED MAIN TANKS. AIRCRAFT DIVERTED TO IAH EMERGENCY DECLARED. LEFT CENTER BOOST PUMP REINSTATED. PERFORMED FUEL TRANSFER TEST, FUEL PUMP OPERATION, FUEL QUANTITY BITE, PUMP UFI TEST. ALL PASS, NO FAULTS NOTED.

Part: LENS — MISSING (ZONE 200 - FUSE) · airframe 57,805 hrs · 24,074 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT AT OVER WING EMERGENCY EXIT NEAR SEAT 16A MISSING LENS COVER. REPLACED LIGHT PER AMM 33-51-01-960-802.

Part: COVER — OUT OF POSITION (ZONE 200 - FUSE) · airframe 57,775 hrs · 24,053 cycles

AIRCRAFT WAS NOT GROUNDED: 16A EMERGENCY EXIT LIGHT COVER FOUND OFF DURING FLIGHT. RESECURED EMERGENCY LIGHT EXIT COVER. SYSTEM OPERATIONS CHECKS NORMAL PER AMM 33-51-01.

Part: BATTERY — MISSING (ZONE 200 - FUSE) · airframe 57,758 hrs · 24,044 cycles

AIRCRAFT IN BASE MAINTENANCE: QTY 6 EMERGENCY BATTERIES MISSING. INSTALLED QTY 6 BATTERIES (AALA202202185768, AALA202202182658, AALA202202180937, AALA202202185936, AALA202202187128) IAW AMM 33-51-06-960-806, OPS CHECK GOOD.

Part: BATTERY — MISSING (ZONE 200 - FUSE) · airframe 57,758 hrs · 24,044 cycles

AIRCRAFT IN BASE MAINTENANCE: QTY 6 EMERGENCY BATTERIES MISSING. INSTALLED QTY 6 BATTERIES (AALA202202185768, AALA202202181050, AALA202202182658, AALA202202185936, AALA202202187128) IAW AMM 33-51-06-960-806, OPS CHECK GOOD.

Part: BATTERY — MISSING (ZONE 200 - FUSE) · airframe 57,758 hrs · 24,044 cycles

AIRCRAFT IN BASE MAINTENANCE: QTY 6 EMERGENCY BATTERIES MISSING. INSTALLED QTY 6 BATTERIES (AALA202202185768, AALA202202181050, AALA202202182658, AALA202202180937, AALA202202187128) IAW AMM 33-51-06-960-806, OPS CHECK GOOD.

Part: BATTERY — MISSING (ZONE 200 - FUSE) · airframe 57,758 hrs · 24,044 cycles

AIRCRAFT IN BASE MAINTENANCE: QTY 6 EMERGENCY BATTERIES MISSING. INSTALLED QTY 6 BATTERIES (AALA202202185768, AALA202202181050, AALA202202182658, AALA202202180937, AALA202202185936) IAW AMM 33-51-06-960-806, OPS CHECK GOOD.

Part: BATTERY — MISSING (ZONE 200 - FUSE) · airframe 57,758 hrs · 24,044 cycles

AIRCRAFT IN BASE MAINTENANCE: QTY 6 EMERGENCY BATTERIES MISSING. INSTALLED QTY 6 BATTERIES (AALA202202181050, AALA202202182658, AALA202202180937, AALA202202185936, AALA202202187128) IAW AMM 33-51-06-960-806, OPS CHECK GOOD.

Part: BATTERY — MISSING (ZONE 200 - FUSE) · airframe 57,758 hrs · 24,044 cycles

AIRCRAFT IN BASE MAINTENANCE: QTY 6 EMERGENCY BATTERIES MISSING. INSTALLED QTY 6 BATTERIES (AALA202202185768, AALA202202181050, AALA202202180937, AALA202202185936, AALA202202187128) IAW AMM 33-51-06-960-806, OPS CHECK GOOD.

Part: BALLAST — FAULTY (CABIN) · airframe 57,411 hrs · 23,892 cycles

AIRCRAFT GROUNDED - SMOKE ODOR IN CABIN PASSING 12000 FEET; IT WAS A BURNING ELECTRICAL / BURNED POPCORN SMELL. ODOR PREVALENT IN ROWS 10-14 WITH A SLIGHT HAZE PRESENT. ACCOMPLISHED MCM 05-96-70 TO TROUBLESHOOT ODOR. FOUND FAULTY BALLAST FOR CEILING LIGHT AT ROW 18. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM 33-22-00, NO FURTHER ODORS NOTED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 56,240 hrs · 23,361 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERABLE AFT LEFT DOOR. MAINTENANCE REPLACED DOOR FLASHLIGHT PER AMM 25-64-00.

Part: CONTROL UNIT — FAILED (HF COMMS) · airframe 55,632 hrs · 23,020 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS BOTH HF #1 AND HF #2 RADIOS INOP. UNABLE TO TRANSMIT OR RECIEVE ON SEVERAL DIFFERENT FREQUENCIES. COULD NOT EVEN HEAR A TUNE SIGNAL WHEN INITAILLY KEYING MICROPHONE ON EACH FREQUENCY. MAINTENANCE REMOVED & REPLACED #1 & #2 HF ANTENNA COUPLERS IAW AMM 23-11-61. NO HELP. GOT TUNING TONE, BUT UNABLE TO TRANSMIT OR RECEIVE ON HF1 OR 2.***SUPPLEMENTAL INFORMATION: REMOVED AND REPLACED THE REMOTE ELECTRONICS UNIT IAW AMM 23-11-00-810-806. OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 54,271 hrs · 22,428 cycles

ONE FLASHLIGHT AT THE AFT RIGHT JUMPSEAT, NO FLASHING LED. REPLACED THE FLASHLIGHT, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: CIRCUIT BOARD — BURNED (PRINTER) · airframe 53,816 hrs · 22,235 cycles

ODOR OF OVERHEATED MOTOR EMITTED FROM PRINTER IN THE COCKPIT. THE AIRCRAFT WAS GROUNDED. NO ONE IN CABIN REPORTED THE ODOR. REPLACED PRINTER IAW AMM 31-33-01 AND ACCOMPLISHED SMOKE ODOR FUMES INITIAL TROUBLESHOOTING SIC 05-96-70.

Part: STARTER — LEAKING (LT ENGINE) · airframe 53,282 hrs · 21,986 cycles

LEFT OIL QUANTITY WENT TO ZERO ON DESCENT. EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DETERMINED THAT THERE WAS NO DISCREPANCY IN OIL PRESSURE. ENGINE STARTER WAS FOUND TO BE THE SOURCE OF THE OIL LEAK. THE AIRCRAFT WAS GROUNDED. MAINTENANCE ALSO REPLACED THE STARTER AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: RELAY — FAULTY (STAB TRIM) · airframe 53,158 hrs · 21,929 cycles

AFTER TAKEOFF, STAB TRIM INOPERATIVE. EMERGENCY WAS DELCARED AND ACFT RETURNED TO DEPARTURE. FLIGHT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED THE INTERLOCK RELAY R850 IAW AMM 27-41-98.

Part: RELAY — FAULTY (STAB TRIM) · airframe 53,158 hrs · 21,929 cycles

AFTER TAKE OFF, STAB TRIM WAS INOPERATIVE. EMERGENCY WAS DELCARED AND RETURNED TO DEPARTURE. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE STABILIZER TRIM CONT RELAY R64 IAW 20N-20-30-00. OPS NORMAL.

Part: TRIM MOTOR — FAULTY (STAB) · airframe 53,158 hrs · 21,929 cycles

AFTER TAKEOFF, STAB TRIM WAS INOPERATIVE. EMERGENCY WAS DELCARED AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED THE STABILIZER TRIM MOTOR IAW AMM 27-41-71. STAB TRIM SYS WAS NORMAL.

Part: STRAP — CORRODED (BS 1016-1028) · corrosion level 2 · airframe 52,950 hrs · 21,842 cycles

CORROSION UNDER THE G4 GALLEY WEB FLOOR STRAPS BETWEEN BS 1016 TO 1028, RBL 18. REPLACED THE WEB STRAPS IAW SRM 51-40-02, 51-00-05-1, AND PRINT 147S5700.

Part: ANGLE — CORRODED (BS 992) · corrosion level 2 · airframe 52,950 hrs · 21,842 cycles

ZEE ANGLE CORRODED AT BS 992.8, LBL 35 TO LBL 46. REPLACED THE ANGLE IAW PRINT 147A5700, AND 51-00-05-1.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 52,949 hrs · 21,842 cycles

LEFT MLG WHEEL WELL BULKHEAD WEB CRACKED ABOVE PREVIOUS REPAIR AND OUTBOARD OF THE KEEL BEAM. REPAIRED THE BULKHEAD WEB IAW 57-10-09, AND SRM 57-10-10-2R-2.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 52,950 hrs · 21,842 cycles

CORROSION ON THE TOP FLANGE OF THE FLOORBEAM, BS 947.5, BETWEEN RBL 4 TO RBL 6. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-5.

Part: FLOOR SUPPORT — CORRODED (BS 957) · airframe 52,950 hrs · 21,842 cycles

CORROSION ON THE TOP OF THE FLOOR SUPPORT, BS 957, LBL 50. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1, AND DRAWING 147A5660-21.

Part: SHEAR WEB — CORRODED (BS 986-996) · airframe 52,950 hrs · 21,842 cycles

CORROSION FOUND ON THE AFT LEFT GALLEY SHEAR WEB, BETWEEN BS 996 TO 986.5, BETWEEN LBL 30 TO LBL 55. REPLACED THE SHEAR WEB IAW 51-00-05-1 AND PRINT 147A5700.

Part: FLOOR SUPPORT — CORRODED (BS 790-847) · corrosion level 2 · airframe 52,950 hrs · 21,842 cycles

CORROSION ON AFT CARGO FLOOR SUPPORT BETWEEN BS 790 - 847, RBL 13.84, 5 INCHES INBOARD OF CARGO DOOR THRESHOLD WEB. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1 AND DRAWING 146A7500.

Part: TRANSITION PANEL — CORRODED (BS 420-440) · corrosion level 2 · airframe 52,950 hrs · 21,842 cycles

RIGHT, FORWARD TRANSITION PANEL HAS AREAS OF CORROSION BETWEEN BS 420 - 440. REPLACED THE TRANSITION PANEL IAW 51-00-05.

Part: TRANSITION PANEL — CORRODED (BS 727I-747) · airframe 52,950 hrs · 21,842 cycles

CORROSION TO THE RIGHT TRANSITION PANEL BETWEEN BS 727I TO 747. REPAIRED THE TRANSITION PANEL IAW SRM 53-00-53-2R, 51-00-05-1, AND DRAWING #146A7502.

Part: ANGLE — CORRODED (BS 940-992) · airframe 52,950 hrs · 21,842 cycles

R2 CREASE ANGLE CORRODED OUT OF LIMITS BETWEEN BS 940 - 992.8, RBL 56. REPLACED THE ANGLE IAW 52-00-05-1.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 52,950 hrs · 21,842 cycles

NUMEROUS AREAS OF HEAVY CORROSION FOUND ON THE FLOORBEAM AT BS 986.5, RBL 3 - 44. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-4.

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 52,950 hrs · 21,842 cycles

CABIN FLOORBEAM CORRODED AT BS 986.5, LBL 4 - 44. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-4.

Part: TRANSITION PANEL — CORRODED (BS 727D-767) · airframe 52,950 hrs · 21,842 cycles

CORROSION FOUND ON LEFT TRANSITION PANEL BETWEEN BS 727D AND 767. INSTALLED SPLICES AND ANGLE FROM BS 727E +12 - 747 +14 IAW SRM 53-00-53-2R, 51-00-05-1 AND DWG 146A7502.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 52,950 hrs · 21,842 cycles

CORROSION ON THE FLOORBEAM AT BS 947.5, LBL 4.5 TOP SIDE. REPLACED THE FLOORBEAM IAW SRM 53-70-51-2R-5.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · corrosion level 2 · airframe 52,950 hrs · 21,842 cycles

LAVATORY D INBOARD FLOOR SUPPORT BETWEEN STA 947 TO STA 967, LBL 25 CORRODED. REPLACED THE FLOOR SUPPORT IAW 51-00-05.

Part: TRANSITION PANEL — CORRODED (BS 492-500A) · corrosion level 2 · airframe 52,950 hrs · 21,842 cycles

CORROSION ON THE RIGHT TRANSITION PANEL BETWEEN BS 492 TO 500A. REPLACED THE TRANSITION PANEL IAW 51-00-05.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · corrosion level 2 · airframe 52,950 hrs · 21,842 cycles

CORROSION ON TOP OF THE FLOOR SUPPORT BETWEEN BS 947 TO 967. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND 51-00-05.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · corrosion level 2 · airframe 52,950 hrs · 21,842 cycles

CORROSION FOUND ON THE FLOOR SUPPORT BETWEEN BS 947.5 AND 967, RBL 50. REPLACED THE FLOOR SUPPORT IAW 51-00-05 & SRM 51-40-02.

Part: TRANSITION PANEL — CORRODED (BS 480-500I) · corrosion level 2 · airframe 52,950 hrs · 21,842 cycles

LEFT TRANSITION PANEL HAD AREAS OF CORROSION BETWEEN BS 480 - 500. REPLACED THE TRANSITION PANEL IAW SRM 53-00-53-2R-5.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 52,950 hrs · 21,842 cycles

CABIN FLOORBEAM CRACKED AT BS 540 RBL 2. REPLACED FLOORBEAM IAW 52-00-05-1.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 52,950 hrs · 21,842 cycles

CABIN FLOORBEAM CRACKED AT BS 540, LBL 2. REPLACED THE FLOORBEAM IAW 51-00-05-1.

Part: FITTING — CORRODED (GIRT BAR) · airframe 52,950 hrs · 21,842 cycles

L1 DOOR FORWARD GIRT BAR FITTING CORRODED AT BS 312, LBL 45. REPLACED GIRT BAR FITTING PER SRM 51-40-02.

Part: FITTING — CORRODED (GIRT BAR) · airframe 52,950 hrs · 21,842 cycles

L1 DOOR AFT GIRT BAR FITTING IS CORRODED AT BS 344. REPLACED GIRT BAR FITTING IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 334) · airframe 52,950 hrs · 21,842 cycles

CABIN FLOOR SUPPORT CRACKED AT BS 334, LBL 45. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 321) · airframe 52,950 hrs · 21,842 cycles

CABIN FLOOR SUPPORT CRACKED AT BS 321 LBL 45. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1.

Part: AIR FILTER — CONTAMINATED (ZONE 100) · airframe 51,890 hrs · 21,380 cycles

THE AIRCRAFT WAS GROUNDED. ON CLIMB OUT EXPERIENCED FUMES IN THE COCKPIT. PERSIST UP TO 12,000 FEET, WENT 100% OXYGEN. APU WAS OFF. THE FLIGHT DECLARED AN EMERGENCY AND DIVERTED TO JFK. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. FUMES NOT NOTICED ON GROUND. ACCOMPLISHED AMM 21-00-01-100-801 AND WORK CARD 05-96-70. RAN ENGINES AND NOTED NO ODOR. NO CONTAMINATION. FOUND TWO DIRTY AIR RECIRCULATION FILTERS REPLACED. ACCOMPLISHED ENGINE RUN WITH BOTH PACKS ON AT 70% POWER. NO SMOKE/ODOR NOTICED.

Part: COVER — MISSING (CABIN) · airframe 50,401 hrs · 20,768 cycles

AIRCRAFT WAS NOT GROUNDED. OVERWING EMERGENCY EXIT LIGHT LENS COVER BY FLOOR MISSING AT SEAT15A. INSTALLED NEW LENS COVER BY SEAT 15A PER AMM 33-51-01.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 49,554 hrs · 20,420 cycles

EMERGENCY EXIT LIGHT, AFT LEFT, HAS A DETACHED LENS. SECURED THE LENS IAW AMM 33-51-02. OPERATIONAL CHECKED GOOD.

Part: CONNECTOR — DIRTY (BRAKE SYSTEM) · airframe 48,655 hrs · 20,065 cycles

AIRCRAFT WAS GROUNDED. STL-DFW FLIGHT ABORTED TAKEOFF AT LESS THAN 40 KNOTS DUE TO TAKEOFF CONFIGURATION WARNING INDICATION. BRAKES MADE A LOUD SQUEALING SOUND. PERFORMED TAKEOFF WARNING SYSTEM TEST IAW AMM 31-51-00-730-803 AND BITE FSEU IAW TSM 27-51-00-810-801. CLEANED PARKING BRAKE SHUTOFF VALVE CONNECTOR. OPERATIONAL CHECK GOOD.

Part: LENS — LOOSE (CABIN) · airframe 48,602 hrs · 20,043 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT BETWEEN GALLEY AND FIRST CLASS CABIN HAS A LOOSE LENS COVER. SECURED THE LENS COVER IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: DOOR — STICKING (E&E BAY) · airframe 48,208 hrs · 19,880 cycles

AIRCRAFT WAS NOT GROUNDED. DURING TAKEOFF ROLL CREW REPORTED RECEIVING AN "E&E ACCESS DOOR OPEN INDICATION". TAKE OFF ABORTED AT APPROXIMATELY 70KTS. CLEANED AND LUBED FORWARD E&E DOOR. ACCOMPLISHED OPERATIONAL CHECKS IAW 52-48-31. SYSTEM CHECK NORMAL.

Part: FITTING — DAMAGED (FLAP SYSTEM) · airframe 48,054 hrs · 19,814 cycles

NR 3 FLAP JACK SCREW AFT CARRIAGE LOWER MOUNT FITTING IS DAMAGED. REMOVED AND REPLACED THE FITTING IAW SRM 51-40-02-0G AND 51-00-05-1.

Part: WEB — CORRODED (BS 440-492) · corrosion level 2 · airframe 48,054 hrs · 19,814 cycles

FORWARD CARGO THRESHOLD WEB UNDER SCUFF PLATE IS CORRODED. REMOVED AND REPLACED THRESHOLD WEB IAW 51-00-05-1 REPAIR 1.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 48,054 hrs · 19,814 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN IS CRACED AT HSS 101.9. REPAIRED THE SKIN IAW SRM 55-10-01-2R-11.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 48,054 hrs · 19,814 cycles

FLOOR SUPPORT BETWEEN BS 328 - 344 IS CRACKED. REMOVED AND REPLACED FLOOR SUPPORT IAW 51-00-05-1 AND DRAWING 141A5400.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 46,796 hrs · 19,306 cycles

AIRCRAFT WAS GNDED. LT MAIN WW VERTICAL WEB AT FS 663.75 IS CRACKED AT APPROX LBL 39. ACCOMPLISH TIME LIMITED REPAIR IAW EA 260675.

Part: LIGHT — MISSING (CABIN) · airframe 46,087 hrs · 19,025 cycles

1R FRONT EMER EXIT LIGHT LOWER LT SIDE LENS MISSING. R & R DOOR 1R EMER LIGHT EXIT IDENTIFIER ASSEMBLY IAW AMM 33-51-01. OPERATIONS CHECKED NORMAL. THE ACFT WAS NOT GNDED.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 44,228 hrs · 18,276 cycles

LEFT AFT DOOR EMERGENCY LIGHT LENS IS MISSING. REPLACED EMER LIGHT ASSEMBLY & PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 40,702 hrs · 16,852 cycles

SEAT TRACK CROWN FROM STATIONS 847 TO 887 BROKEN. ACCOMPLISHED SPLICE REPAIR IAW EA737-53-035230.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,702 hrs · 16,852 cycles

CORROSION WAS FOUND AT STATION 540 LT SIDE. REMOVED CORROSION IAW SRM & ACCOMPLISHED REPAIR IAW EA B737-53-025793.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 40,702 hrs · 16,852 cycles

THE INBD & OTBD FASTENER HOLES IN THE SEAT TRACKS & SPLICE STRAPS LOCATED AT STATION 727B LBL 45.50 HAD CRACKS. ACCOMPLISHED ECO J1707 FOR THE REPAIR OF THE STRAPS IN CONJUNCTION WITH RECEIVING EA B737-53-035100 FOR THE REPAIR OF THE SEAT TRACKS.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 40,702 hrs · 16,852 cycles

THE INBD & OTBD FASTENER HOLES IN THE SEAT TRACKS & SPLICE STRAPS LOCATED AT STATION 727B LBL 24.75 HAD CRACKS. ACCOMPLISHED ECO J1707 FOR THE REPAIR OF THE STRAPS IN CONJUNCTION WITH RECEIVING EA B737-53-035100 FOR THE REPAIR OF THE SEAT TRACKS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,655 hrs · 16,041 cycles

BATTERY PACK AT M1695 INOPERATIVE. REPLACED BATTERY PACK AT M1695. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,655 hrs · 16,041 cycles

BATTERY PACK AT M1672 INOPERATIVE. REPLACED BATTERY PACK AT M1672. OPERATIONS CHECKED NORMAL.

Part: PUMP — MALFUNCTIONED (HYDRSAULIC SYS) · airframe 38,655 hrs · 16,041 cycles

MIA CREW REPORTED HYDRAULIC SYSTEM A LOSS, ALONG WITH LT ENGINE DRIVEN PUMP. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT ENGINE DRIVEN PUMP. SYSTEM GROUND CHECK NORMAL OPERATION CLOSED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,655 hrs · 16,041 cycles

BATTERY PACK AT M1671 INOPERATIVE. REPLACED BATTERY PACK AT M1671. OPERATIONS CHECKED NORMAL.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 36,026 hrs · 14,996 cycles

SHEAR TIE AT STATION 867 AND STRINGER 20 LEFT DAMAGED. REPLACED SHEAR TIE PER EA B737-53-026791.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,026 hrs · 14,996 cycles

FUSELAGE DENTED, PUNCTURED, AND SCRATCHED AT STATION 867, STRINGER 20 LEFT. INSTALLED DOUBLER PER SRM 53-00-02 REPAIR 1 AND EA B737-53-026790.

Part: SEAL — STUCK (L1 DOOR) · airframe 35,875 hrs · 14,928 cycles

JFK - CREW REPORTED AFTER TAKEOFF UNABLE TO PRESSURIZE CABIN. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. FOUND LOWER HINGE ARM FLAPPER SEAL STUCK PREVENTING LEFT NUMBER 1 DOOR FROM SEALING. REPOSITIONED FLAPPER SEAL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

LEFT FRAME 480 IS CRACKED AT AIR CONDITION RAIL SUPPORT BRACKET. ACCOMPLISHED NESTED ANGLE REPAIR PER PER EA B737-53-025864.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

FRAME CRACKED AT AIR CONDITION RAIL SUPPORT BRACKET, STATION 559 RIGHT. ACCOMPLISHED NESTED ANGLE REPAIR PER EA B737-53-025864.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

FRAME CRACKED AT AIR CONDITION RAIL SUPPORT BRACKET, STATION 559 LEFT. ACCOMPLISHED NESTED ANGLE REPAIR PER EA B737-53-025864.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

THE NUMBER 4 SEAT TRACK HAS CRACK EXTENDING FROM RIVET ON INBOARD FLANGE, 4 INCHES FORWARD OF STATION 720B. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER EA 737-53-025793.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

THE NUMBER 3 SEAT TRACK IS CRACKED EXTENDING FROM RIVET ON INBOARD FLANGE, 4 INCHES FORWARD OF STATION 720B. REMOVED THE DAMAGE AND INSTALLED DOUBLER REPAIR PER EA B737-53-025793.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

FOUND RIVET SET DAMAGE TO OUTER FUSELAGE SKIN AT STA 727G PLUS 4 BETWEEN STRINGERS 27R AND 27L. INSTALLED EXTERNAL DOUBLER REPAIR PER SRM 53-00-01-2R 3.

Part: SPLICE — CORRODED (FLOORBOARD) · corrosion level 2 · airframe 35,732 hrs · 14,863 cycles

AFT CARGO FLOORBOARD SPLICE IS CORRODED. REMOVED AND REPLACED THE FLOORBOARD SPLICE AT STATION 767+4 PER AARD 51010-05.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,732 hrs · 14,863 cycles

CORROSION ON STRINGER 23 LEFT AT STATION 312. REMOVED CORROSION AND INSTALLED DOUBLER PER EA B737-53-025688.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

INTERIM REPAIR WAS MADE USING BLIND FASTENERS IN LIEU OF SOLID RIVETS. INSTALLED EXTERNAL DOUBLER AND FILLER PER EA B737-53-025746.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

FRAME CRACKED AT AIR CONDITIONING RAIL SUPPORT BRACKET, STATION 907 RIGHT. INSTALLED REPAIR ANGLE PER ECO J1159AD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

CORROSION FROM STATIONS 792 TO 847 ON THE FLOOR SUPPORT AT RIGHT BUTTLINE 14. INSTALLED REPAIR STRAP PER EA B737-53-025704.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,732 hrs · 14,863 cycles

AFT CARGO, LEFT TRANSITION PANEL FROM STATIONS 727+4 TO 847 HAS NUMEROUS AREAS OF CORROSION AND UPPER ATTACH FASTENERS EITHER WORKING OR PULLED THRU AT EVERY FRAME STATION. INSTALLED NEW LEFT TRANSITION PANEL FROM STATIONS 727+4 TO 847 PER SRM 53-00-53-2R 5.

Part: FLAP — PUNCTURED (LT WING) · airframe 35,732 hrs · 14,863 cycles

LEFT INBOARD TRAILING EDGE AFT FLAP HAS 2 PUNCTURES LESS THAN 1/4 INCH IN DIAMETER 4 INCHES APART. FILLED HOLES WITH POTTING COMPOUND AND INSTALLED TWO EACH HOT BONDED PERMANENT REPAIRS PER SRM 51-70-10-2R 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

FRAME CRACKED AT AIR CONDITIONING RAIL SUPPORT BRACKET, STATION 400 RIGHT. INSTALLED NESTED ANGLE REPAIR PER ECO J1159AD.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,732 hrs · 14,863 cycles

FORWARD SERVICE DOOR THRESHOLD SILL PLATE ATTACH ANGLE CORRODED AT STATION 322 AND RIGHT BUTTLINE 59. INSTALLED NEW SILL PLATE ANGLE PER AARD 51-00-05-1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

FRAME CRACKED AT AIR CONDITIONING RAIL SUPPORT BRACKET, STATION 727D LEFT. ACCOMPLISHED NESTED ANGLE REPAIR PER J1159AD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,732 hrs · 14,863 cycles

CORROSION ON FLOOR SUPPORT FROM STATIONS 312 TO 328. REPLACED FLOOR SUPPORT PER AARD 51-00-05-1.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,732 hrs · 14,863 cycles

AFT CARGO DOORWAY WEB CORRODED BETWEEN STATIONS 793 TO 847. INSTALLED WEB IN AFT CARGO PER THE AARD 51-10-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

FRAME CRACKED AT AIR CONDITIONING RAIL SUPPORT BRACKET, STATION 500A RIGHT. INSTALLED NESTED ANGLE REPAIR PER ECO J1159AD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

FRAME CRACKED AT STATION 400 LEFT. INSTALLED REPAIR ANGLE PER ECO J1159AD.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,732 hrs · 14,863 cycles

CORROSION ON FORWARD RIGHT SERVICE DOOR CREASE ANGLE BETWEEN STATIONS 308 AND 328. INSTALLED NEW CREASE ANGLE PER AARD 51-00-05-1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

FRAME CRACKED AT AIR CONDITIONING RAIL SUPPORT BRACKET, STATION 480 RIGHT. INSTALLED NESTED ANGLE REPAIR PER ECO J1159AD.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,732 hrs · 14,863 cycles

AFT CARGO FLOOR: RIGHT Z-CHANNEL SIDE PLATE FROM STATIONS 727+4 TO 767 HAS NUMEROUS AREAS OF CORROSION. REPLACED RIGHT Z-CHANNEL SIDE PLATE FROM STATIONS 727+4 TO 767 PER SRM 53-00-53-2R 5.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,732 hrs · 14,863 cycles

CORROSION ABOVE DOOR LATCH ON WEB, AUXILIARY POWER UNIT COMPARTMENT LEFT WALL. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-70-13 R1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,732 hrs · 14,863 cycles

AUXILIARY POWER UNIT COMPARTMENT LEFT SIDE WALL ANGLE HAS CORROSION, ABOVE FORWARD DOOR LATCH. INSTALLED NEW ANGLE PER AARD 51-10-05 AND BOEING DWG 148A8620.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

INTERCOSTAL BETWEEN STATIONS 328 AND 344 AT LEFT BUTTLINE 45 CRACKED. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

INTERCOSTAL BETWEEN STATIONS 312 AND 328 AT RIGHT BUTTLINE 32 CRACKED. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

INTERCOSTAL BETWEEN STATIONS 312 AND 328 AT LEFT BUTTLINE 45 CRACKED. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

INTERCOSTAL BETWEEN STATIONS 277 AND 294 AT BUTTLINE 0 CRACKED. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: SHIELD — CRACKED (FUSELAGE) · airframe 35,732 hrs · 14,863 cycles

RIGHT TRANSITION SHIELD FROM STATIONS 767 TO 792 CRACKED. REPLACED TRANSITION SHIELD PER AARD 51-10-05.

Part: VAPOR BARRIER — CRACKED (LT WING) · airframe 35,732 hrs · 14,863 cycles

LEFT VAPOR BARRIER IS CRACKED BETWEEN BAYS 2 AND 4 LEFT. INSTALLED CROSSBRACE REPAIRS TO BAYS 2 AND 4 LEFT PER SRMSUP 57-10-10-2R 2.

Part: PAN — GOUGED (CARGO DOOR) · airframe 35,732 hrs · 14,863 cycles

AFT CARGO DOOR HANDLE PAN GOUGED AND TEFLON BUTTON MISSING. REPLACED HANDLE MECHANISM WITH NEW TEFLON BUTTON AND HANDLE PAN PER ESO 60651 AND EA COMP-52-025539.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 35,732 hrs · 14,863 cycles

CRACK ON RIGHT VAPOR BARRIER IN THE RIGHT MAIN LANDING GEAR WHEEL WELL, RIGHT BUTTLINES 10 TO 15. INSTALLED CROSS BRACE REPAIR AT BAYS 2R AND 4R PER SRMSUP 57-10-10-2R.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,732 hrs · 14,863 cycles

VERTICAL STIFFENER CORRODED AT STATION 1125 RIGHT SIDE. REPLACED VERTICAL STIFFENER AT STATION 1125 RIGHT SIDE PER AARD 51-10-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,732 hrs · 14,863 cycles

CORROSION ON FLOORBEAM STATION 328 RIGHT BUTTLINE 19. INSTALLED DOUBLER PER SRM 53-10-51-2R.

Part: FLAP — PUNCTURED (LT WING) · airframe 35,732 hrs · 14,863 cycles

LEFT INBOARD TRAILING EDGE AFT FLAP HAS 2 PUNCTURES LESS THAN 1/4 IN DIAMETER 4 INCHES APART. FILLED HOLES WITH POTTING COMPOUND AND INSTALLED TWO EACH HOT BONDED PERMANENT REPAIRS PER SRM 51-70-10-2R 2.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 35,732 hrs · 14,863 cycles

LEFT INBOARD TRAILING EDGE AFT FLAP BOTTOM SIDE HAS 2 SMALL PUNCTURES APPROXIMATELY 4 INCHES APART. FILLED HOLES WITH POTTING COMPOUND AND INSTALLED TWO EACH HOT BONDED PERMANENT REPAIRS PER SRM 51-70-10-2R 2.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,732 hrs · 14,863 cycles

AFT CARGO, LEFT TRANSITION PANEL FROM STATIONS 727 TO 847 HAS NUMEROUS AREAS OF CORROSION. INSTALLED NEW LEFT TRANSITION PANEL FROM STATIONS 727 TO 847 PER SRM 53-00-53-2R 5.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,960 hrs · 13,739 cycles

RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT OVERWING EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,960 hrs · 13,739 cycles

ROW 21 AFT SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR ROW 21 AFT SEAT MOUNTED EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,960 hrs · 13,739 cycles

ROW 21 AFT BULLNOSE EMERGENCY PATH LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR ROW 21 AFT BULLNOSE EMERGENCY PATH LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,960 hrs · 13,739 cycles

RIGHT NUMBER 1 DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT NUMBER 1 DOOR EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,960 hrs · 13,739 cycles

LEFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT OVERWING EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,302 hrs · 13,092 cycles

EMERGENCY LIGHTS AT ROWS 16 TO 20 ARE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AT STATION 727C. OPC CHECK NORMAL.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,309 hrs · 12,723 cycles

LEFT CREASE ANGLE CORRODED STATIONS 986 TO 990. REMOVED AND INSTALLED NEW CREASE ANGLE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,309 hrs · 12,723 cycles

RIGHT NUMBER 2 EXTERNAL EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 EXTERNAL EMERGENCY LIGHT. OPS CHECKS NORMAL.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,309 hrs · 12,723 cycles

AT STATION 983 AND RIGHT BUTTLINES 33 TO 43 WALL SUPPORT Z-ANGLE IS CORRODED. REMOVED AND REPLACED Z-ANGLE PER SRM 53-00-07-2R1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,309 hrs · 12,723 cycles

STATION 986.5 FLOORBEAM HAS CORROSION ON UPPER SURFACE OF BEAM AT LEFT BUTTLINES 22, 29, 32 AND 42. INSTALLED T-CORD REPAIR AT STA 986.5 FLOORBEAM RIGHT BUTTLINES 5 TO LEFT BUTTLINES 52 AS PER SRM 53-70-51-2R-4.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,309 hrs · 12,723 cycles

BEAM CORRODED AT STATION 947 RIGHT BUTTLINE 3 TO LEFT BUTTLINE 3. ACCOMPLISHED SPLICE REPAIR PER SRM 53-70-51-2R 5.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,309 hrs · 12,723 cycles

BEAM CORRODED AT STATION 947 RIGHT BUTTLINES 23 TO 27. ACCOMPLISHED SPLICE REPAIR PER SRM 53-70-51-2R 5.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,017 hrs · 12,595 cycles

POSITION M1672 EMERGENCY LIGHT FAILED. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,017 hrs · 12,595 cycles

POSITION M1695 EMERGENCY LIGHT FAILED. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,017 hrs · 12,595 cycles

POSITION M1671 EMERGENCY LIGHT FAILED. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,017 hrs · 12,595 cycles

POSITION M1674 EMERGENCY LIGHT FAILED. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,017 hrs · 12,595 cycles

POSITION M1670 EMERGENCY LIGHT FAILED. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,017 hrs · 12,595 cycles

POSITION M1673 EMERGENCY LIGHT FAILED. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,017 hrs · 12,595 cycles

POSITION 1676 EMERGENCY LIGHT FAILED. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,017 hrs · 12,595 cycles

POSITION M1675 EMERGENCY LIGHT FAILED. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,017 hrs · 12,595 cycles

POSITION M1694 EMERGENCY LIGHT FAILED. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL.

Part: SKIN PANEL — GOUGED (CARGO DOOR) · airframe 28,605 hrs · 11,952 cycles

AFT CARGO DOOR HAS 8 INCH GOUGE WITH 8.25 INCH DENT LOCATED 5 INCHES OF AFT HANDLE. INSTALLED NEW SKIN PANEL PER ESO 60651 AND SRM 51-10-02-0G.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,605 hrs · 11,952 cycles

INTERCOSTAL CRACKED AT SCREW HOLE BELOW ENTRY FLOORBOARD FORWARD OF STATION 328. INSTALLED NEW INTERCOSTAL PER SRM 51-00-00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,605 hrs · 11,952 cycles

INTERCOSTAL CRACKED AT SCREW HOLE BELOW FORWARD ENTRY FLOORBOARD AFT OF STATION 328. REPAIRED INTERCOSTAL PER SRM 51-00-00.

Part: SKIN — GOUGED (FUSELAGE) · airframe 28,605 hrs · 11,952 cycles

FUSE SKIN GOUGE AT STATION 500. INSTALLED INTERIM REPAIR PER EA B737-53-009257.

Part: WINDOW — CRACKED (COCKPIT) · airframe 28,493 hrs · 11,907 cycles

DFW - CAPTAIN REPORTED CRACK IN FIRST OFFICER’S WINDOW ON CLIMB OUT. EMERGENCY DECLARED RETURNED DEW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FIRST OFFICER’S WINDSHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROLLER — MALFUNCTIONED (WINDSHIELD HEAT) · airframe 26,147 hrs · 10,932 cycles

MIA - LEFT NUMBER 1 WINDOW ARCING. EMERGENCY DECLARED RETURNED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED WINDOW AND CONTROLLER CON3030.

Part: MANIFOLD — DAMAGED (ANTI-SKID SYS) · 23,454 cycles

IAD INFLIGHT T1060 13 AUG DFW TO DCA. CREW REPORTED ANTI SKID INDICATION INTERMITTENT. LANDED IAD WITHOUT INCIDENT. REPLACED NR 4 MANIFOLD. SYSTEM GROUND CHECKED NORMAL OPS.

Part: CONTROL UNIT — FAILED (ANTI-SKID SYS) · 23,444 cycles

IAD INFLIGHT T2192/11AUG MIA TO DCA. CREW REPORTED ANTI SKID LIGHT ILLUMINATED. LANDED IAD WITHOUT INCIDENT. REPLACED ANTI SKID AUTOBRAKE CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 22,509 hrs

MIA - EMERGENCY LIGHT CIRCUIT BREAKER POPPED LEFT AFT EMERGENCY CHARGER. REPLACED BATTERY PACK M1673 AND RESET CIRCUIT BREAKER FOR EMERGENCY LIGHT LEFT AFT CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 21,668 hrs

LGA - EMERGENCY LIGHTS AT SEAT ROW 9 INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 9. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 15D HAS MISSING LENS COVER. REPLACED LENS COVER FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

TUL - EMERGENCY LIGHTS IN COACH INOPERATIVE. REPLACED BATTERY PACK AT STATION 967 FOR EMERGENCY LIGHTS IN COACH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHT AT SEAT 7D INOPERATIVE. REPLACED END CONNECTOR AT SIDE WALL FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ORD - ALL AIRCRAFT EMERGENCY LIGHTS FAILED WHILE PERFORMING CARD 0299. REPLACED ALL BATTERY PACKS FOR ALL AIRCRAFT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, L2 DOOR EMERGENCY EXIT LIGHT UNDER EXIT SIGN INOPERATIVE. RECONNECTED L2 DOOR EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)