N991AN

Part: SPRING — BROKEN (ZONE 800) · airframe 49,129 hrs · 20,935 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED THAT THE FORWARD LEFT DOOR OUTSIDE HANDLE NOT SECURE WHEN CLOSED. HANDLE WAS NOT FLUSH WITH AIRCRAFT FUSELAGE UPON INSPECTION AFTER LANDING. MAINTENANCE FOUND THE L1 DOOR OUTER HANDLE WOULD NOT STOW DUE TO THE INNER RETRACT SPRING BEING BROKEN AND REPLACED THE SPRING PER AMM 52-11-11. A SATISFACTORY OPERATIONAL WAS ACCOMPLISHED WITH NO ISSUES NOTED.

Part: PUMP — LOW PRESSURE (NR 2 ENGINE FUEL) · airframe 46,221 hrs · 19,510 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: DURING CRUISE BOTH OF NUMBER 2 ENGINE AFT FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED AND STAYED ON; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: PUMP — LOW PRESSURE (ZONE 500) · airframe 46,221 hrs · 19,510 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: DURING CRUISE BOTH OF NUMBER 2 ENGINE AFT FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED AND STAYED ON; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. **SUPPLEMENTAL REPORT FOR (AALA202501034549): ACCOMPLISHED FUEL QUANTITY CHECKS WITH FUELSTICKS, PER AIRCRAFT 737-800 FUELING MANUAL 12-11-02. CONFIRMED CORRECT QUANTITY. SUMPED NUMBER 2 FUEL TANK, PER AMM 12-11-00. NO WATER CONTANIMINANTS FOUND. TRANSFERED FUEL, PER AMM 28-26-00-201-650-802. FOUND NUMBER 2 FUEL TANK AFT FUEL BOOST PUMP LOSING PRESSURE. REMOVED AND REPLACED NUMBER 2 AFT BOOST PUMP, PER AMM 28-22-41 REF TSI 0106154**(CLOSED).

Part: ROD — OUT OF ADJUST (ZONE 800) · airframe 45,219 hrs · 19,010 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY-D DOOR HARD TO OPEN FROM INSIDE. ADJUSTED LOWER LOCKING ROD. OPERTIONAL CHECK GOOD. PER CMM 25-40-64.

Part: LOCK — OUT OF ADJUST (ZONE 800) · airframe 45,188 hrs · 18,994 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT LAVATORY DOOR LOCK STICKING IN LOCKED POSITION. ADJUSTED DOOR LATCH ON AFT RT LAVATORY DOOR LOCK. OPERTIONAL CHECK GOOD. PER CMM 25-40-65.

Part: INDICATOR — FAILED (ZONE 200) · airframe 43,849 hrs · 18,340 cycles

AIRCRAFT WAS GROUNDED: ON APPROACH TO CLT, FLAPS FAILED AT APPROX 4 DEGREES. THERE WAS A 1 DEGREE OR LESS SPLIT BETWEEN FLAPS. LANDING WAS UNEVENTFUL. RETRACTED FLAPS AFTER ARRIVING AT GATE. STILL ABOUT A 0.25 DEGREE SPLIT BETWEEN INDICATORS. LEFT FLAP INDICATOR NOT INTO THE UP BAND. REPLACED FLAP POSITION INDICATOR PER AMM 27-58-02.

Part: SENSOR — BINDING (ZONE 600) · airframe 43,849 hrs · 18,340 cycles

AIRCRAFT WAS GROUNDED: TRAILING EDGE FLAPS JAMMED AT FLAPS 10 UNITS DURING APPROACH. USED ALTERNATE FLAP EXTENSION PROCEDURE TO EXTEND TO FLAPS 15. REPLACED RIGHT-HAND LEADING EDGE RETRACT F4 SENSOR S174 PER AMM 27-88-11.

Part: AXLE — GOUGED (MLG) · airframe 43,657 hrs · 18,247 cycles

AIRCRAFT IN BASE MAINTENANCE: MLG NUMBER 3 AXLES REQUIRE INSPECTION FOR DAMAGES. FOUND GOUGES ON NUMBER 3 AXLE OUTER SLEEVE INNERMOST EDGE (AALA202402199003) AND MATERIAL LOSS ON FACE. HAND POLISHED ALL PER MPSM 27-09-9. FOUND MARRING ON #3 INNER SLEEVE TOP SIDE (AALA202402197870), SCRATCHES ON TOP SIDE MIDDLE SECTION, AND NICKS ON OUTER FACE. REPAIRED MARRING AND SCRATCHES WITH HAND POLISHING AND HAND BLENDED NICKS, PER MPSM 27-09-9.

Part: AXLE — NICKED (MLG) · airframe 43,657 hrs · 18,247 cycles

AIRCRAFT IN BASE MAINTENANCE: MLG NUMBER 3 AXLES REQUIRE INSPECTION FOR DAMAGES. FOUND GOUGES ON NUMBER 3 AXLE OUTER SLEEVE INNERMOST EDGE (AALA202402199003) AND MATERIAL LOSS ON FACE. HAND POLISHED ALL PER MPSM 27-09-9. FOUND MARRING ON #3 INNER SLEEVE TOP SIDE (AALA202402197870), SCRATCHES ON TOP SIDE MIDDLE SECTION, AND NICKS ON OUTER FACE. REPAIRED MARRING AND SCRATCHES WITH HAND POLISHING AND HAND BLENDED NICKS, PER MPSM 27-09-9.

Part: SLEEVE — CRACKED (MLG) · airframe 43,657 hrs · 18,246 cycles

AIRCRAFT WAS GROUNDED: NUMBER 1 MAIN WHEEL AXLE BETWEEN THE AXLE AND THE INNER CYLINDER HAS SEVERAL CRACKS. **SUPPLEMENTAL REPORT FOR (AALA202402151112): REMOVED AND REPLACED NUMBER 1 AXLE INBOARD SLEEVE DUE TO FINDINGS. PER AMM 32-11-12 REPAIR 4-1.**(CLOSED).

Part: AXLE — CRACKED (NR 1 WHEEL) · airframe 43,657 hrs · 18,246 cycles

AIRCRAFT WAS GROUNDED: NUMBER 1 MAIN WHEEL AXLE BETWEEN THE AXLE AND THE INNER CYLINDER HAS SEVERAL CRACKS.**SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: CONNECTOR — MISINSTALLED (MLG) · airframe 43,657 hrs · 18,246 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AIRCRAFT COULD NOT STOP WITHIN RUNWAY LENGTH; OVER RAN THE RUNWAY. **SUPPLEMENTAL REPORT FOR (AALA202402128047): REMOVE AND REPLACED AUTOBRAKE CONTROL MODULE (AALA202402128047), PER AMM 32-42-81. CORRECTED SWAPPED ANTI-SKID CONNECTORS (D1120) WIRING AND CONNECTIONS BACK TO PROPER LOCATIONS (AALA202402201276), PER EDM 32-41-11. CORRECTED ROUTING AND INSTALLED HYDRAULIC LINES IN CORRECT POSITIONS (AALA202402209476), PER WC 3222J004-001.**(CLOSED).

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,657 hrs · 18,246 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AIRCRAFT COULD NOT STOP WITHIN RUNWAY LENGTH, OVER RAN THE RUNWAY. (OPEN).

Part: MODULE — INOPERATIVE (ZONE 100 - FUSE) · airframe 43,657 hrs · 18,246 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AIRCRAFT COULD NOT STOP WITHIN RUNWAY LENGTH; OVER RAN THE RUNWAY. **SUPPLEMENTAL REPORT FOR (AALA202402128047): REMOVE AND REPLACED AUTOBRAKE CONTROL MODULE (AALA202402128047), PER AMM 32-42-81. CORRECTED SWAPPED ANTI-SKID CONNECTORS (D1120) WIRING AND CONNECTIONS BACK TO PROPER LOCATIONS (AALA202402201276), PER EDM 32-41-11. CORRECTED ROUTING AND INSTALLED HYDRAULIC LINES IN CORRECT POSITIONS (AALA202402209476), PER WC 3222J004-001.**(CLOSED).

Part: HYDRAULIC LINE — MISINSTALLED (MLG) · airframe 43,657 hrs · 18,246 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AIRCRAFT COULD NOT STOP WITHIN RUNWAY LENGTH; OVER RAN THE RUNWAY. **SUPPLEMENTAL REPORT FOR (AALA202402128047): REMOVE AND REPLACED AUTOBRAKE CONTROL MODULE (AALA202402128047), PER AMM 32-42-81. CORRECTED SWAPPED ANTI-SKID CONNECTORS (D1120) WIRING AND CONNECTIONS BACK TO PROPER LOCATIONS (AALA202402201276), PER EDM 32-41-11. CORRECTED ROUTING AND INSTALLED HYDRAULIC LINES IN CORRECT POSITIONS (AALA202402209476), PER WC 3222J004-001.**(CLOSED).

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 43,627 hrs · 18,229 cycles

AIRCRAFT IN BASE MAINTAINCE: L2 DOOR ESCAPE SLIDE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK FUSE. PER AMM 33-51-06.

Part: LIGHT — INTERMITTENT (ZONE 200 - FUSE) · airframe 42,700 hrs · 17,780 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT OVERWING EXIT LIGHT FLICKERING. REMOVE AND REPLACE RIGHT HAND OVERWING SIDEWALL EMERGENCY LIGHT. PER AMM 33-51-01.

Part: GIRT BAR — MISALIGNED (ZONE 800 - DOORS) · airframe 42,132 hrs · 17,490 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR GIRT BAR MISALIGNED. REPOSITIONED L1 GIRT BAR INTO CORRECT STOW POSITION.

Part: BULB — INOPERATIVE (ZONE 200 - FUSE) · airframe 42,005 hrs · 17,428 cycles

AIRCRAFT IN BASE MAINTENANCE: WHILE PERFORMING THE EXTERIOR LIGHTS TEST, FOUND THE RIGHT WING FORWARD EXTERIOR EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED RIGHT WING FORWARD EXTERIOR EMERGENCY LIGHT BULB PER AMM 33-51-04. TESTS GOOD.

Part: BULKHEAD WEB — CRACKED (ZONE 100 - FUSE) · airframe 42,004 hrs · 17,428 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT WHEEL WELL VAPOR BARRIER WEB LOCATED AT BS 663.75 AT RBL 45.64. REPAIRED VAPOR BARRIER PER AARD 57-10-10-9 REPAIR 9 PAR 3B.

Part: CONTROL UNIT — FAILED (ZONE 200 - FUSE) · airframe 39,354 hrs · 16,155 cycles

AIRCRAFT WAS GROUNDED: ON TAKEOFF GOT "CONFIG" - ABORT TAKEOFF ON RECALL "OVERHEAD" PROXIMITY SENSOR ELECTRONIC UNIT LIGHT IN NOW ON. ABORT WAS BELOW 80 KNOTS. REMOVED AND REPLACED TAKE OFF WARNING SWITCH (S651) REFERENCE ITEM NUMBER 2, REMOVED AND REPLACED PROXIMITY SENSOR ELECTRONIC UNIT.

Part: SWITCH — FAILED (ZONE 200 - FUSE) · airframe 39,354 hrs · 16,155 cycles

AIRCRAFT WAS GROUNDED: ON TAKEOFF GOT "CONFIG" - ABORT TAKEOFF ON RECALL "OVERHEAD" PROXIMITY SENSOR ELECTRONIC UNIT LIGHT IN NOW ON. ABORT WAS BELOW 80 KNOTS. REMOVED AND REPLACED TAKE OFF WARNING SWITCH (S651) REFERENCE ITEM NUMBER 2, REMOVED AND REPLACED PROXIMITY SENSOR ELECTRONIC UNIT.

Part: DOOR LATCH — OUT OF ADJUST (ZONE 200 - FUSE) · airframe 38,778 hrs · 15,889 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR DIFFICULT TO CLOSE. ADJUSTED COCKPIT DOOR LOCK PER AMM 52-51-02. OPERATIONAL CHECK GOOD.

Part: SERVO — FAULTY (ZONE 200 - FUSE) · airframe 38,573 hrs · 15,799 cycles

AIRCRAFT WAS GROUNDED: ON TAKE OFF LEFT ENGINE NUMBER 1 WAS 5 TO 7 PERCENT LOWER AT TAKEOFF POWER .BELOW 80 PERCENT NUMBER 1 THROTTLES MATCHED. AT TAKEOFF POWER LEFT ENGINE WOULD NOT ACHIEVE TAKEOFF OR CLIMB NUMBER 1 POWER. AUTO THROTTLE ON, LEFT THE NUMBER 1 ENGINE PHYSICALLY ABOUT AN INCH BELOW NUMBER 2 ENGINE. ALL OF THIS OCCURRED ABOVE 80 PERCENT OF NUMBER 1. FUEL FLOW WAS ALSO ABOUT 1500 POUNDS LESS ON LEFT ENGINE AS THIS OCCURRED. REPLACED AUTO THROTTLE SERVO PER AMM 22-31-91.

Part: LENS — MISSING (ZONE 200 - FUSE) · airframe 37,183 hrs · 15,173 cycles

AIRCRAFT WAS NOT GROUNDED: LENS COVER FOR EXIT SIGN IN REAR GALLEY MISSING. REPLACED LENS COVER.

Part: DOOR — STICKING (ZONE 800 - DOORS) · airframe 37,178 hrs · 15,168 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN OR CLOSE. CLEANED AND LUBED FLIGHT DECK DOOR CHECKS OK.

Part: GIRT BAR — STICKING (ZONE 800 - DOORS) · airframe 37,083 hrs · 15,116 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD SERVICE DOOR GIRT BAR STUCK IN DISARMED POSITION. UNSTUCK GIRT BAR ON R1 DOOR AND SECURED IN SAFE POSITION.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 36,833 hrs · 15,003 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY SMOKE LIGHT ILLUMINATED DURING CRUISE QRH PROCEDURE PERFORMED NO SMOKE PRESENT VERIFIED ATTENDANT. LIGHT ILLUMINATED 3 SEPARATE TIMES. CHECKED AND ACCOMPLISHED FIRST CLASS LAVATORY SMOKE DETECTOR AND NOTED TEST OK PER AMM 26-14-00.

Part: SEAL — LEAKING (OIL SCAV FILTER) · airframe 36,008 hrs · 14,625 cycles

AIRCRAFT WAS GROUNDED: ENGINE OIL DECREASED DURING FLIGHT. #2 ENGINE FROM 9 QTS AT CRUISE DOWN TO 4 QTS. DECISION MADE TO DIVERT TO MSY. EMERGENCY DECLARED. TEMPERATURE AND PRESSURE NORMAL THROUGHOUT. OIL QUANTITY AS LOW AS 2 QTS ON APPROACH. FOUND OIL LEAK AT THE SCAVENGE OIL FILTER RETURN LINE AND CLOGGING TRANSMITTER BASE. REMOVED AND REPLACE TRANSMITTER (AALA202105019001) IAW AMM 79-21-07. REMOVED AND REPLACED BOTH SEALS (AALA202105039010) AT OIL RETURN LINE IAW AMM 79-21-04.

Part: OIL FILTER — LEAKING (NR 2 ENGINE) · airframe 36,008 hrs · 14,625 cycles

AIRCRAFT WAS GROUNDED: ENGINE OIL DECREASED DURING FLIGHT. #2 ENGINE FROM 9 QTS AT CRUISE DOWN TO 4 QTS. DECISION MADE TO DIVERT TO MSY. EMERGENCY DECLARED. TEMPERATURE AND PRESSURE NORMAL THROUGHOUT. OIL QUANTITY AS LOW AS 2 QTS ON APPROACH. FOUND OIL LEAK AT THE SCAVENGE OIL FILTER RETURN LINE AND CLOGGING TRANSMITTER BASE. REMOVED AND REPLACE TRANSMITTER (AALA202105019001) IAW AMM 79-21-07. REMOVED AND REPLACED BOTH SEALS (AALA202105039010) AT OIL RETURN LINE IAW AMM 79-21-04.

Part: SENSOR — FAULTY (LT A/C PACK) · airframe 35,665 hrs · 14,468 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DIVERTED TO LAS FOR LH PACK FAILURE. REPLACED PRECOOLER SENSOR 390 AND PRECOOLER VALVE (AALA202103139004) IAW AMM 36-12-03, AMM 36-12-01, AND JOB CARD JC08L40036001, OPS CHECK GOOD.

Part: VALVE — FAULTED (PRECOOLER) · airframe 35,665 hrs · 14,468 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DIVERTED TO LAS FOR LH PACK FAILURE. REPLACED PRECOOLER VALVE AND PRECOOLER SENSOR 390 (AALA202103139005) PER AMM 36-12-03, AMM 36-12-01, AND JOB CARD JC08L40036001, OPS CHECK GOOD.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 34,149 hrs · 13,803 cycles

AIRCRAFT WAS GROUNDED: AT CRUISE ALTTITUDE FL 360, HYDRAULIC SYSTEM B FAILED, HYDRAULIC QUANTITY AND PRESSURE INDICATED 0. AN EMEREGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MIA WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE B SYSTEM HYDRAULIC PRESSURE MODULE LEAKING FLUID FROM THE INBOARD PLUG AND REPLACED THE O-RING WHICH WAS DAMAGED. THE HYDRAULIC SYSTEM WAS SERVICED AND A SATISFACTORY LEAK AN OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 29-11-71.

Part: ROLLER — OUT OF ADJUST (ENTRY DOOR) · airframe 34,021 hrs · 13,748 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT ENTRY DOOR LIGHT ILLUMINATED DURING POST CHECK TEST FLIGHT. DOOR VERIFIED CLOSED AND HANDLE STOWED. ADJUSTED LATCH ROLLERS PER AMM 52-13-00.

Part: STOP FITTING — OUT OF ADJUST (R1 DOOR) · airframe 34,021 hrs · 13,748 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING POST CHECK TEST FLIGHT DURING DESCENT WHISTLE/SQUEL AT R1 DOOR WHILE PASSING THRU 5 PSI DIFFERENTIAL, QUIT AT 2.8 DIFFERENTIAL. ADJUSTED LOWER DOOR STOPS PER AMM 52-41-00.

Part: HANDLE — LACK OF LUBE (ZONE 200) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING FIRE WARNING TEST NO. 1 FIRE HANDLE VERY DIFFULT TO PULL - IF ANY SIDE LOAD IS APPLIED OR IF HANDLE IS NOT PULLED EXACTLY STRAIGHT THE HANDLE WILL NOT EXTEND TO SHUTOFF. APPLIED LUBRICATION TO #1 ENGINE FIRE HANDLE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 26-21-00.

Part: LATCH — OUT OF ADJUST (WINDOW) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: FIRST OFFICERS WINDOW LATCH HAS PLAY WHEN IIN LOCKED POSITION. ADJUSTED WINDOW LATCH PER AMM 56-12-11.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK L1 WINDOW CUT OUT UPPER OUTBOARD CORNER C-D WINDOW POST FRAME CRACK SUSPECTED AT BS 219.8 AND LBL 30. UPON ADDITIONAL EVALAUATION NO CRACK WAS FOUND AND PREVENTATIVE MODIFICATION DOUBLER WAS INSTALLED PER EA 304961 AND SB 737-53-1335.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK R1 WINDOW CUT OUT UPPER OUTBOARD CORNER C-D WINDOW POST FRAME CRACK SUSPECTED AT BS 219.8 AND RBL 30. UPON ADDITIONAL EVALAUATION NO CRACK WAS FOUND AND PREVENTATIVE MODIFICATION DOUBLER WAS INSTALLED PER EA 304963 AND SB 737-53-1335.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK, RIGHT HAND #3 WINDOW CUT OUT E-F WINDOW POST FRAME #2 FASTENER HOLE CRACKED AT BS 196.5. REPAIRED WINDOW POST PER EA 304965.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK, LEFT HAND #3 WINDOW CUT OUT E-F WINDOW POST FRAME #2 FASTENER HOLE CRACKED AT BS 196.5. REPAIRED WINDOW POST PER EA 304965.

Part: WEB — WORN (FUSELAGE) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: E&E ACCESS DOOR CUT OUT WEB ABOVE STOP FITTING WORN AT BS 338 AND LBL 10. REPLACED WEB PER AARD 51-00-05-1 AND SRM 53-10-15-01-3.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN FLOOR ZEE ANGLE AT BS 990 AND LBL 32. REPLACED ZEE ANGLE PER AARD 51-00-05-1.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND MAIN LANDING GEAR WHEEL WELL VAPOR BARRIER ORIGINATING AT A FASTENER LOCATION APPROXIMATELY 5.0 INCHES ABOVE THE BOTTOM OF THE VAPOR BARRIER AT RBL 50. REPAIRED VAPOR BARRIER PER AARD 57-10-10-9 AND SRM 57-10-10-2R-2.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER WING SECTION REAR SPAR VERTICAL PRESSURE DECK WEB AT BS 663 AND RBL 45.64. REPAIRED VERTICAL PRESSURE DECK WEB PER SRM 57-10-10-2R-3.

Part: SHIELD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARMTENT SHIELD BETWEEN BS 500 AND BS 500A AT S25R. REPLACED SHIELD PER AARD 51-00-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED CABIN FLOOR INTERCOSTAL CRACKED BETWEEN BS 277 AND BS 294.5 AT RBL 2. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FORWARD CARGO COMPARTMENT BAFFLE CLIP AT BS 500G AND S26R. REPLACED BAFFLE CLIP PER SRM 51-40-02.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 500 AND BS BS 500I AT S25R. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R-5 AND AARD 51-00-05.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FORWARD CARGO COMPARTMENT BAFFLE CLIP AT BS 400 AND S17R. REPLACED BAFFLE CLIP PER SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FORWARD CARGO COMPARTMENT BAFFLE CLIP AT BS 500G AND S25L. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FORWARD CARGO COMPARTMENT BAFFLE CLIP AT BS 500H AND S25L.REPLACED CLIP PER AARD 51-00-05-1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN FLOOR ZEE ANGLE BETWEEN BS 991 AND BS 104 AT RBL 32. REPLACED ZEE ANGLE PER AARD 51-00-05-1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FORWARD CARGO COMPARTMENT BAFFLE CLIP AT BS 400 AND S25L. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL AT BS 500I AND S25R. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 727A AND BS 840 AT S25L. REPAIRED TRANSITION PANEL PER SRM 53-00-53-2R.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN FLOOR ZEE ANGLE AT BS 990 BETWEEN RBL 34 AND RBL 47. REPLACED ZEE ANGLE PER AARD 51-00-05-1.

Part: SHIELD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHIELD BETWEEN BS 767 AND BS 790 AT S25R. REPLACED SHIELD PER AARD 51-00-05-1.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT THRESHOLD PAN BETWEEN BS 790 AND BS 847 AT RBL 25. REPLACED THRESHOLD PAN PER AARD 51-00-05.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FORWARD CARGO COMPARTMENT BAFFLE CLIP AT BS 500H AND S25L.REPLACED BAFFLE CLIP PER AARD 51-00-05-1.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR INTERCOSTAL AT BS 957 AND LBL 50. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN FLOOR SUPPORT ANGLE AT BS 1015 AND LBL 34. REPLACED SUPPORT ANGLE PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 727A AND BS 767 AT S25R. REPAIRED TRANSITION PANEL PER AARD 51-00-05-1 AND SRM SRM 53-00-53-2R.

Part: RETAINER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT FALSE WALL RETAINER AT BS 500I AND S25L. REPLACED WALL RETAINER PER SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,019 hrs · 13,747 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R2 DOOR CUT OUT LOWER CREASE ANGLE BETWEEN BS 862 AND BS 1006 AT RBL 52. REPLACED CREASE ANGLE PER AARD 51-00-05-1.

Part: FUEL SYS — MALFUNCTIONED · airframe 31,542 hrs · 12,624 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS BOTH WING TANKS FEED 400 LBS THEN STOP WITH CENTER FUEL PUMPS ON. AFTER FEEDING 400LBS OUT OF WINGS, ALL FUEL FEED IS OK. MAINTENANCE ACCOMPLISHED WORK CARD 28-26-00, OPS CHECK GOOD. ALSO ACCOMPLISHED FQIS BITE TEST NO FAULTS OK FOR SERVICE.

Part: ENGINE — FIRE (INTERNAL) · airframe 30,770 hrs · 12,273 cycles

ANOTHER AIRCRAFT REPORTED THERE WAS FIRE COMING OUT OF THE LEFT ENGINE TAILPIPE. AIRCRAFT ABORTED TAKEOFF AT 60KTS. NO ABNORMAL ENGINE INDICATIONS WERE OBSERVED AND THE FIRE BOTTLES WERE NOT DISCHARGED. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND OIL PUDDLING IN THE TAILPIPE AND EXHAUST CONE. CARD 21090307042, STATED THE NR ONE ENGINE HAS EXPERIENCED A POSSIBLE NR 3 BEARING AIR-OIL PTFE SEAL DEGRADATION. MAINTENANCE COMPLETED INSPECTION OF THE SUMP SCAVENGE SCREENS IAW AMM 79-00-00 AND FOUNDTEFLON MATERIAL IN THE SCREEN. OPEN.

Part: ENGINE — FIRE (LEFT) · airframe 30,599 hrs · 12,198 cycles

GROUND CREW WAS ADVISED OF A TAILPIPE FIRE ON THE LEFT ENGINE ABOUT 6 TO 7 MINUTES AFTER ENGINE START. CREW PULLED FIRE HANDLE AND NO BOTTLES WERE NEEDED TO EXTINGUISH. ENGINES WERE RUNNING NORMALLY PRIOR TO TAXI OUT, BOTH ENGINES HAD NORMAL STARTS. THE AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED FIM 71-05-00, NO ABNORMALITIES FOUND. ACCOMPLISHED LEFT HAND ENGINE RUN AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: WINDOW — GOUGED (R3) · airframe 29,776 hrs · 11,822 cycles

R3 WINDOW HAD A COUPLE OF GOUGES THAT WERE OUT OF LIMITS. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE R3 WINDOW IAW MM 56-11-21, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FLASHLIGHT — NO TEST (FWD CABIN) · airframe 28,729 hrs · 11,381 cycles

EMERGENCY FLASHLIGHT AT THE L1 DOOR JUMPSEAT WOULD NOT TEST. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25-64-00-200-802.

Part: PRESSURE SWITCH — FAILED (RT ENGINE FUEL) · airframe 28,672 hrs · 11,352 cycles

FUEL FILTER BYPASS LIGHT, RIGHT ENGINE, DURING CLIMBOUT, CAME ON TWICE AND STAYED ON THRU LANDING. EMERGENCY WAS DECLARED, FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RIGHT ENGINE FUEL DIFFERENTIAL PRESSURE SWITCH IAW AMM 73-34-01 AND PERFORMED SATISFACTORY OPERATIONAL CHECK, NO LEAKS NOTED. AIRCRAFT WAS GROUNDED

Part: LENS — MISSING (CABIN) · airframe 26,405 hrs · 10,363 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT IN LAVATORY E HAS A MISSING LENS COVER. INSTALLED LENS COVER PER AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: COVER — MISSING (CABIN) · airframe 25,899 hrs · 10,160 cycles

THE AIRCRAFT WAS NOT GROUNDED. PLASTIC COVER ON EMERGENCY EXIT LIGHT IS MISSING AFT LAV E. INSTALLED NEW E EXIT COVER AT AFT LAV E WALL PER AMM 33-50-00. OPS CHECKS NORMAL.

Part: BEAM — WORN (BS 540-542) · airframe 25,534 hrs · 10,002 cycles

WEAR DAMAGE ON THE SUPPORT BEAM AT THE PNEUMATIC ACCESS DOOR LANDING. REPAIRED IAW EA 269925.

Part: LENS — MISSING (EXIT SIGN) · airframe 25,296 hrs · 9,902 cycles

EMERGENCY EXIT LENS CAP MISSING AT ROW 14. INSTALLED NEW LENS CAP ON EMERGENCY EXIT SIGN AT ROW 14 IAW IPC 33-51-01. THE AIRCRAFT WAS NOT GROUNDED.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 22,840 hrs · 8,897 cycles

FLIGHT ATTENDANT REPORTED SMOKE ODOR IN THE FORWARD ENTRY AREA. NOTICED SLIGHT WHITE SMOKE NEAR L1 DOOR. PERFORMED FIM TASK 21-00-00. FOUND BURNED PLASTIC ON OVEN VENT FAN. REMOVED PLASTIC. COULDN"T FIND ANY OTHER SOURCE. CHECKED ENGINE AND APU FOR EVIDENCE OF LEAK OR FLUIDS, NONE FOUND. ACCOMPLISHED OPERATIONS CHECK OF FIRST CLASS OVENS IAW AMM 25-32-02. OVENS RAN FOR 45 MINUTES AT MAX TEMPERATURE. NO ABNORMAL ODORS. OK FOR SERVICE.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 19,338 hrs · 7,531 cycles

CRACK INDICATION ON FWD SEAT TRACK AT FS 727B & LBL 24.75 OTBD SIDE AFT FASTENER HOLE. ACCOMPLISHED PERMANENT REPAIR IAW EA 252003 DATED 6 18 2015.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 19,338 hrs · 7,531 cycles

CRACK INDICATION ON FWD SEAT TRACK AT FS 727B & LBL 45.50 INBD SIDE FWD FASTENER HOLE. ACCOMPLISHED PERMANENT REPAIR IAW EA 252003 DATED 6 18 2015.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 19,338 hrs · 7,531 cycles

CRACK FOUND ON FWD SEAT TRACK AT RBL 45.50 & STATION 727B. ACCOMPLISHED PERMANENT REPAIR IAW EA 252003 DATED 6 18 2015.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 19,338 hrs · 7,531 cycles

CRACK INDICATION ON FWD SEAT TRACK AT FS 727B & LBL 24.75 INBD SIDE AFT FASTENER HOLE. ACCOMPLISHED PERMANENT REPAIR IAW EA 252003 DATED 6 18 2015.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 19,338 hrs · 7,531 cycles

CRACK FOUND ON FWD SEAT TRACK AT RBL 24.75 & FS 727B. ACCOMPLISHED PERMANENT REPAIR IAW EA 202003 DATED 6 18 2015.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 19,338 hrs · 7,531 cycles

CRACK INDICATION ON FWD SEAT TRACK AT FS 727B & LBL 45.50 OTBD SIDE FWD & AFT FASTENER HOLES. ACCOMPLISHED PERMANENT REPAIR IAW EA 252003 DATED 6 18 2015.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 19,338 hrs · 7,531 cycles

CRACKED FLOOR SUPPORT AT BS 540, BETWEEN BL 0 & RBL 24. REPLACED FLOOR SUPPORT AT BS 540, BETWEEN BL 0 & RBL 24.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 19,338 hrs · 7,531 cycles

CABIN FLOOR STRUCTURE INTERCOSTAL CRACKED AT FLOORBOARD ATTACH SCREW BETWEEN STATION 328 - 344, LBL 46. R & R INTERCOSTAL WITH NEW IAW AARD 51-00-05-01.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 19,338 hrs · 7,531 cycles

E & E COMPARTMENT INTERCOSTAL BETWEEN FS 312 & 328 FLOORBEAMS AT LBL 46 IS CRACKED AT CTR CLIP NUT HOLE. R & R INTERCOSTAL IAW AARD 51-00-05-1.

Part: TRIM MOTOR — INOPERATIVE (HORIZ STAB) · airframe 16,795 hrs · 6,539 cycles

STAB TRIM INDICATION FAULT. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED STAB TRIM MOTOR. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY PACK — FAILED (CABIN) · airframe 6,476 hrs · 2,383 cycles

BATTERY PACK FAILED TEST FOR EMERGENCY LIGHTS FROM RIGHT NUMBER 1 DOOR TO FIRST CLASS SEATS AND AISLE. REPLACED EMERGENCY LIGHT BATTERY PACK M1674. OPS CHECK NORMAL.