N831NN

Part: ELEC CONNECTOR — SHORTED (ZONE 100) · airframe 45,395 hrs · 19,491 cycles

AIRCRAFT WAS NOT GROUNDED: ANTI-SKID INOPERATIVE ON TOUCHDOWN AUTO-BRAKE DISARMED AND ANTI-SKIP INOPERATIVE LIGHT ILLUMINATED. ACCOMPLISHED BITE OF AACU FOUND FAULT FOR XDCR3. PERFORMED FIM 32-42-00-810-806. FOUND CONNECTOR D11124 IS INTERNALLY SHORTING. REPLACED CONNECTOR, PER SWPM 20-61-11. PERFORMED OPERATIONAL TEST OF TRANSDUCER, PER AMM 32-42-00 AND BITE TEST OF AACU, PER FIM 32-42-00. ALL CHECKED GOOD AND NO-FAULT CODE SHOWN AT THIS TIME.

Part: ANTI-SKID SYS — FAULTED (ZONE 700) · airframe 45,395 hrs · 19,491 cycles

AIRCRAFT WAS NOT GROUNDED: ANTI-SKID INOPERATIVE ON TOUCHDOWN AUTO-BRAKE DISARMED AND ANTI-SKIP INOPERATIVE LIGHT ILLUMINATED. ACCOMPLISHED BITE OF AACU FOUND FAULT FOR XDCR3. OPEN.

Part: FLASHLIGHT — NO TEST (ZONE 200) · airframe 45,135 hrs · 19,373 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS THAT THE FORWARD FLASHLIGHT CHARGER DOES NOT BLINK TO TEST. REPLACED CHARGING MOUNTING BRACKET. PER 25-64-00-200-802.

Part: HINGE — BINDING (ZONE 800) · airframe 44,277 hrs · 18,963 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTANDENTS REPORTS LAVATORY-E DOOR, RIGHT REAR, DIFFICULT TO OPEN AND CLOSE. REMOVED AND REPLACED LAVATORY-E HINGE. PER CMM 25-40-65. OPERTIONAL CHECK GOOD AT THIS TIME.

Part: DOOR — BINDING (ZONE 800) · airframe 44,277 hrs · 18,963 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTANDENTS REPORTS LAVATORY-E DOOR, RIGHT REAR, DIFFICULT TO OPEN AND CLOSE. (OPEN).

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 43,908 hrs · 18,796 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT UNDER NUMBER 3 JUMPSEAT IS INOPERATIVE. REMOVE AND REPLACE FLASHLIGHT BATTERY.

Part: DOOR — JAMMED (ZONE 800) · airframe 43,617 hrs · 18,665 cycles

AIRCRAFT WAS NOT GROUNDED: LAV D DOOR JAMMED. OUTSIDE HANDLE FELL OFF WHEN TRYING TO OPEN THE DOOR. SECURED HANDLE AND LUBRICATED LATCH.

Part: TRIM PANEL — NOT SEATED (SLIDING WINDOW) · airframe 42,367 hrs · 18,066 cycles

AIRCRAFT WAS NOT GROUNDED: CAPTAINS WINDOW WILL NOT OPEN PROPERLY. MAINTENANCE RESEATED CAPTAIN'S WINDOW TRIM. WINDOW OPERATED NORMAL IAW AMM 56-12-11.

Part: SLIDING WINDOW — NOT SEATED (ZONE 200) · airframe 42,367 hrs · 18,066 cycles

AIRCRAFT WAS NOT GROUNDED: CAPTAINS WINDOW WILL NOT OPEN PROPERLY. MAINTENANCE RESEATED CAPTAIN'S WINDOW TRIM. WINDOW OPERATED NORMAL IAW AMM 56-12-11.

Part: GUST LOCK — STUCK (ZONE 800) · airframe 42,274 hrs · 18,012 cycles

AIRCRAFT WAS NOT GROUNDED: GUST LUCK ON L1 MAIN ENTRY DOOR IS STUCK AND WILL NOT RELEASE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: GUIDE ARM — STUCK (ZONE 800) · airframe 42,274 hrs · 18,012 cycles

AIRCRAFT WAS NOT GROUNDED: GUST LUCK ON L1 MAIN ENTRY DOOR IS STUCK AND WILL NOT RELEASE. REPLACED L1 DOOR GUIDE ARM ASSEMBLY PER AMM 52-11-21.

Part: LIGHT — MALFUNCTIONED (ZONE 200) · airframe 41,940 hrs · 17,836 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT IN ROW 16DEF IS FLASHING.**SUPPLEMENTAL REPORT FOR (AALA202407307521): TROUBLESHOT PER JC 08L20033001 ACCOMPLISHED FULL SYSTEM RESET, OPERTIONAL CHECK PASSED, NO FAULT FOUND**(CLOSED).

Part: LIGHT — MALFUNCTIONED (ZONE 200) · airframe 41,940 hrs · 17,836 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT IN ROW 16DEF IS FLASHING. (OPEN).

Part: SKIN — CORRODED (ZONE 100) · airframe 41,694 hrs · 17,700 cycles

AIRCRAFT WAS GROUNDED: LAVATORY VENT HAS MINOR CORROSION. REMOVED MINOR CORROSION. PER SRM 51-10-02-0G.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 40,972 hrs · 17,367 cycles

AIRCRAFT IN BASE MAINTENANCE: ROW 3AB EMERGENCY SEAT LIGHT INOPERATIVE. RECONNECTED EMERGENCY PATH LIGHT CONNECTOR. PER B737NG CMM 25-23-67.

Part: LIGHT — DAMAGED (CABIN) · airframe 40,992 hrs · 17,376 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD LEFT HAND OVERWING LOWER EXIT LIGHT DAMAGE. REMOVED AND REPLACED FORWARD LEFT HAND OVERWING LOWER EXIT LIGHT. PER B-737NG AMM 33-51-01 AND AMM 33-51-00.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 20,362 hrs · 8,672 cycles

AIRCRAFT IN BASE MAINTENANCE: FIRST CLASS ROW 3AB EMERGENCY SEAT LIGHTS INOPERATIVE. FOUND EPL CONNECTORS LOOSE AND NOT PROPERLY CONNECTED TO SEAT. RECONNECTED, PER B737 NG CMM 25-23-67. PERFORMED SATISFACTORY EMERGENCY LIGHTS OPERATIONAL CHECK ON SEAT ROW 3ABC, PER B737NG AMM 33-51-00.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 40,972 hrs · 17,367 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY BIN MOUNTED AISLE LIGHT BETWEEN ROWS 17 AND 18 ABC DOES NOT ILLUMINATE. FOUND CONNECTOR D12038 NOT CONNECTED PROPERLY, RECONNECTED CONNECTOR, FUNCATIONAL CHECK GOOD.

Part: SKIN — DENTED (BS 967 S23L) · airframe 40,972 hrs · 17,367 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT LOWER FUSELAGE HAS DENTS (FOUND TO BE PREVIOUS BLENDS), AT BS 967, S23L. REPAIRED SKIN PER EA 352758.

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 40,972 hrs · 17,367 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND WHEEL WELL VAPOR BARRIER AT BS 663.75, FROM LBL 31.83 TO LBL 54.21. REPARED VAPOR BARRIER PER AARD 57-10-10-9 AND SRM 51-70-04-2R-10.

Part: PITOT TUBE — FAULTY (RT ELEVATOR) · airframe 40,615 hrs · 17,196 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: RIGHT ELEVATOR PITOT LIGHT CAME ON DURING FLIGHT AIRCRAFT RETURN TO AND LANDED SAFELY AT MIA WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED RIGHT ELEVATOR PITOT PROBE. PER AMM 27-31-94 ACCOMPLISHED ALL REQUIRED TEST.

Part: DOOR — LACK OF LUBE (ZONE 900 - LAV/G) · airframe 40,504 hrs · 17,143 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT LAVATORY ENTRY DOOR DIFFICULT TO OPEN AND CLOSE. LUBED HINGE AND DOOR SILL AS REQUIRED. PER AMM 25-40-00.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 39,677 hrs · 16,740 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE. ADJUSTED AFT RIGHT LAVATORY DOOR PER AMM 25-40-15.

Part: GUIDE ARM — LOOSE (ZONE 800 - DOORS) · airframe 39,110 hrs · 16,469 cycles

AIRCRAFT WAS GROUNDED: R1 ENTRY DOOR HANDLE IS LOOSE. REMOVED AND REPLACED R1 DOOR GUIDE ARM PER AMM 52-41-21.

Part: LATCH — LACK OF LUBE (LAVATORY DOOR) · airframe 36,949 hrs · 15,394 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT LAVATORY DOOR LATCH DIFFICULT TO OPERATE AND DOES NOT ILLUMINATE INTERIOR LIGHT WHEN ENGAGED. LUBED RIGHT AFT LAVATORY DOOR LATCH IN ACCORDANCE WITH CMM 25-40-65.

Part: LIGHT — DAMAGED (ZONE 200 - FUSE) · airframe 36,805 hrs · 15,318 cycles

AIRCRAFT WAS NOT GROUNDED: CEILING EMERGENCY EXIT LIGHT LOCATED IN AISLE AT ROW 18 HAS A WIRE STICKING OUT OF IT. REPLACED CEILING LIGHT ASSEMBLY PER AMM 33-51-03.

Part: PROXIMITY SENSOR — INOPERATIVE (ZONE 500 - LH WI) · airframe 35,978 hrs · 14,918 cycles

AIRCRAFT WAS GROUNDED: LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED/SLAT DISAGREE WITH SELECTED POSITION.(FOUND NUMBER 7 SLAT TRANSIT LIGHT STAYS ON. MESSAGE 27-81212 FAULTED). INSTALLED PROXIMITY SENSOR S1006 ON NUMBER 7 SLAT PER AMM 27-88-11.

Part: KNOB — BROKEN (ZONE 900 - LAV/G) · airframe 35,331 hrs · 14,605 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY L1 LATCH BROKEN. REINSTALLED L1 LAVATORY DOOR SLIDE LATCH KNOB, OPS CHECK GOOD.

Part: FASTENER — LOOSE (ZONE 900 - LAV/G) · airframe 34,984 hrs · 14,436 cycles

AIRCRAFT WAS NOT GROUNDED: FIRST CLASS LAVATORY DOOR HANDLE LOOSE. TIGHTENED LOOSE FASTENER ON DOOR HANDLE PER CM 25-46-96.

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 34,510 hrs · 14,225 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT INOPERATIVE ON BULLNOSE TRIM AT SEAT 17ABC. REPLACED LIGHT WITH SERVICEABLE UNIT IAW AMM 33-51-03, OPS CHECK GOOD.

Part: HANDLE — LOOSE (ZONE 900 - LAV/G) · airframe 34,381 hrs · 14,158 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR HANDLE IS LOOSE. SECURED HANDLE.

Part: OUTFLOW VALVE — INOPERATIVE (ZONE 100 - FUSE) · airframe 34,308 hrs · 14,124 cycles

AIRCRAFT WAS GROUNDED: DURING CRUISE CABIN ALTITUDE BEGAN TO CLIMB AND COULD NOT BE CONTROLLED IN AUTO. INITIATED EMERGENCY DESCENT AND FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES FOR RAPID DEPRESSURIZATION. CABIN OXYGEN MASKS MANUALLY DEPLOYED. REMOVED AND REPLACED OUTFLOW VALVE PER AMM 21-31-03. OPERATIONS CHECK GOOD PER AMM 21-31-00. REMOVED AND REPLACED BOTH CABIN PRESSURE CONTROL MODULES (AALA202110063947) (AALA202110063377) PER AMM 21-31-02.

Part: CONTROL UNIT — INOPERATIVE (ZONE 200 - FUSE) · airframe 34,308 hrs · 14,124 cycles

AIRCRAFT WAS GROUNDED: DURING CRUISE CABIN ALTITUDE BEGAN TO CLIMB AND COULD NOT BE CONTROLLED IN AUTO. INITIATED EMERGENCY DESCENT AND FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES FOR RAPID DEPRESSURIZATION. CABIN OXYGEN MASKS MANUALLY DEPLOYED. REMOVED AND REPLACED OUTFLOW VALVE (AALA202110069636) PER AMM 21-31-03. OPERATIONS CHECK GOOD PER AMM 21-31-00. REMOVED AND REPLACED BOTH CABIN PRESSURE CONTROL MODULES (AALA202110063377) PER AMM 21-31-02.

Part: CONTROL UNIT — INOPERATIVE (ZONE 200 - FUSE) · airframe 34,308 hrs · 14,124 cycles

AIRCRAFT WAS GROUNDED: DURING CRUISE CABIN ALTITUDE BEGAN TO CLIMB AND COULD NOT BE CONTROLLED IN AUTO. INITIATED EMERGENCY DESCENT AND FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES FOR RAPID DEPRESSURIZATION. CABIN OXYGEN MASKS MANUALLY DEPLOYED. REMOVED AND REPLACED OUTFLOW VALVE (AALA202110069636) PER AMM 21-31-03. OPERATIONS CHECK GOOD PER AMM 21-31-00. REMOVED AND REPLACED BOTH CABIN PRESSURE CONTROL MODULES (AALA202110063947) PER AMM 21-31-02.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 33,940 hrs · 13,959 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN ENTRY DOOR 2L EMERGENCY EXIT LIGHT COVER DAMAGED. REPLACED 2L EMERGENCY LIGHT.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 32,884 hrs · 13,491 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HORIZONTAL STABILIZER BOTTOM SKIN HAS 1.00 INCH CRACK IN FRONT OF REAR SPAR AT STA 101.9. INSTALLED DOUBLER REPAIR IAW SRM 55-10-01-2R-11.

Part: DOUBLER — CRACKED (HORIZONTAL STAB) · airframe 32,884 hrs · 13,491 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HORIZONTAL STABILIZER HAS CRACK AT STATION 110. INSTALLED DOUBLER AND FILLERS PER SRM 55-10-01-2R-11.

Part: PRESSURE DECK — CRACKED (ZONE 100) · airframe 32,884 hrs · 13,491 cycles

AIRCRAFT IN BASE MAINTENANCE: WING CENTER SECTION KEEL BEAM VERTICAL PRESSURE DECK WEB LEFT BUTT LINE 40 TO LEFT BUTT LINE 45.64 HAS CRACK. LEFT PRESSURE DECK WEB REPAIR PER SRM 57-10-10-2R-3.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 32,884 hrs · 13,491 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HORIZONTAL STABILIZER LOWER SKIN HAS 1.5 INCH CRACK AT STA 157.10. ACCOMPLISHED DOUBLER AND FILLER REPAIR IAW SRM 55-10-01-2R-11 AND EA 326537.

Part: PRESSURE DECK — CRACKED (ZONE 100) · airframe 32,884 hrs · 13,491 cycles

AIRCRAFT IN BASE MAINTENANCE: WING CENTER SECTION KEEL BEAM VERTICAL PRESSURE DECK WEB RIGHT BUTT LINE 40 TO RIGHT BUTT LINE 45.64 HAS CRACK. RIGHT PRESSURE DECK WEB REPAIR PER SRM 57-10-10-2R-3.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 32,884 hrs · 13,491 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON LEFT HORIZONTAL STABILIZER RIB STATION 92.70. CRACK 3 INCHES LONG AND 0.001 INCHES WIDE. REPLACED RIB AT STATION 92.70 PER SRM 51-00-05-1.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 32,884 hrs · 13,491 cycles

AIRCRAFT IN BASE MAINTENANCE: FOUND CRACKED INTERCOSTAL BETWEEN STA 312 AND 328 AT LBL 46.25. REPLACED INTERCOSTAL PER SRM 51-00-05.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 32,884 hrs · 13,491 cycles

AIRCRAFT WAS GROUNDED: CRACKED INTERCOSTAL FLOOR SUPPORT 1.2 INCH LONG TERMINATING AT NUTPLATE HOLE. INSTALLED NEW INTERCOSTAL PER AARD 51-00-05 AND BOEING DRAWING 141A5400 AND SRM 51-40-02-0G.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 32,884 hrs · 13,491 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR SUPPORT FRAME LOCATED AT BS 947 LBL 24. REMOVED CORROSION AND BLENDED AREA PER SRM 51-10-02-0G.

Part: TRANSITION PANEL — CORRODED (BS 500B-500I) · airframe 32,884 hrs · 13,491 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF TRANSITION PANEL BETWEEN STA 500B AND 500I AT LBL 24, MEASURING L=3.25 IN, W=0.5 IN, D=0.03 IN. ACCOMPLISHED PERMANENT, REINFORCING SPLICE REPAIR IAW SRM 53-00-53-2R-5 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 32,884 hrs · 13,491 cycles

AIRCRAFT IN BASE MAINTENANCE: FOUND CORRODED INTERCOSTAL AT STA 947 TO 967 AND LBL 24. REPLACED INTERCOSTAL REF SRM 51-00-05-1, SRM 51-40-02 AND BOEING DRAWING 147A5650.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 32,884 hrs · 13,491 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 500C AND 500I. REPLACED TRANSITION PANEL PER SRM 51-40-02.

Part: TRANSITION PANEL — CORRODED (BS 747-767 S25L) · airframe 32,884 hrs · 13,491 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION OF LH TRANSITION PANEL BETWEEN STA 747 AND STA 767 AT STR 25L, MEASURING L=1.0 IN, W=1.0 IN, D=0.017 IN. REPLACED TRANSITION PANEL WITH NEW IAW SRM 51-10-02-0G.

Part: TRANSITION PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 32,884 hrs · 13,491 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON TRANSITION PANEL SHIELD. REPLACED TRANSITION PANEL PER SRM 51-40-02.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 32,884 hrs · 13,491 cycles

AIRCRAFT IN BASE MAINTENANCE: FOUND CORROSION ON RIGHT TRANSITION PANEL BETWEEN STA 727I - 727J. REPLACED TRANSITION ZEE ASSEMBLY IAW SRM 51-40-02.

Part: FMC — FAILED (LEFT) · airframe 32,840 hrs · 13,473 cycles

AIRCRAFT WAS GROUNDED: DUAL FLIGHT MANAGEMENT COMPUTER FAILURE, FLIGHT DIVERTED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED LT FMC AND RT FMC (AALA202102239018) IAW AMM 34-61-02, OPS CHECK GOOD.

Part: FMC — FAILED (RIGHT) · airframe 32,840 hrs · 13,473 cycles

AIRCRAFT WAS GROUNDED: DUAL FLIGHT MANAGEMENT COMPUTER FAILURE, FLIGHT DIVERTED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED RT FMC AND LT FMC (AALA202102239011) IAW AMM 34-61-02, OPS CHECK GOOD.

Part: STOP — BROKEN (R1 GIRT BAR) · airframe 32,657 hrs · 13,394 cycles

AIRCRAFT WAS NOT GROUNDED. R1 GIRT BAR PLASTIC STOP CAME OFF OF THE BAR. REMOVED AND REPLACED R1 GIRT BAR, IAW AMM 25-66-01.

Part: PROXIMITY SWITCH — UNSERVICEABLE (ZONE 100) · airframe 31,655 hrs · 12,953 cycles

AIRCRAFT GROUNDED, PSEU LIGHT AND ASSOCIATED TAKE-OFF CONFIGURATION WARNING, LOW SPEED REJECTED TAKE OFF AT 34KTS. PROXIMITY SWITCH ELECTRONICS UNIT (PSEU) LIGHT SUBSEQUENTLY EXTINGUISHED AND DID NOT RETURN. ACCOMPLISHED FIM TASK 32-09-00, REMOVED AND REPLACED PSEU (PROXIMITY SWITCH ELECTRONICS UNIT) PER JOB CARD 08L00032003, OPERATIONAL CHECK GOOD, NO FURTHER FAULTS NOTED.

Part: BULB — FAULTY (EMERGENCY LIGHT) · airframe 30,791 hrs · 12,579 cycles

AIRCRAFT WAS NOT GROUNDED: L2 EMERGENCY EXTERIOR LIGHT INOPERATIVE. MAINTENANCE REPLACED BULB IAW AMM 33-51-04.

Part: PITOT TUBE — FAULTY (EXTERIOR) · airframe 28,898 hrs · 11,677 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AIRSPEED DISAGREE / ALT DISAGREE CAUTIONS, AIRSPEED LOW WARNING IN FLIGHT FL 280, EEC (S) WENT TO ALTERNATE MODE. EVENTUALLY FO SIDE RETURNED TO NORMAL, FOLLOWED BY CA SIDE RETURNING TO NORMAL APPROX. 5 MIN LATER. ALL ENGINE HEATS / PITOT HEATS TO PROPER POSITIONS. NO OTHER WARNINGS & CAUTIONS. MAINTENANCE FOUND THE L/H PITOT AT FAULT, REPLACED IAW AMM 34-11-01 LEAK AND OPS TEST OK.

Part: COMPUTER — FAULTY (FCC) · airframe 28,806 hrs · 11,634 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AFTER TOUCH DOWN, THE SPOILERS DEPLOYED THEN RETRACTED, THE THROTTLE ADVANCED, THEN THE SPOILERS DEPLOYED AGAIN. THEN THE PSEU LIGHT CAME ON FOR A FEW MINUTES THE EXTINGUISHED. MAINTENANCE REPLACED THE FCC IAW AMM 22-11-33. REQUIRED LMP TEST PASSED IAW AMM 34-36-00. SPEED BRAKE/ SPOILER TEST PASSED IAW AMM 27-62-00.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 28,656 hrs · 11,563 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD MEGAPHONE DID NOT WORK. MAINTENANCE REPLACED MEGAPHONE UNIT AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 25-64-00.

Part: LIFE RAFT — MISINSTALLED (NR 2) · airframe 28,322 hrs · 11,414 cycles

MAINTENANCE REPORTS THE #2 RAFT ASSY NOT INSTALLED PROPERLY IN COS BOX. REINSTALLED RAFT IAW ECO J2097.

Part: LIFE RAFT — MISINSTALLED (NR 4) · airframe 28,322 hrs · 11,414 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS THE RAFT IN COS #4 WAS INSTALLED IMPROPERLY. INSTALLED # 4 RAFT ASSY IAW ECO J2097AF.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,122 hrs · 11,324 cycles

AIRCRAFT WAS NOT GROUNDED: LIGHT FAILED TEST. MAINTENANCE REPLACED LIGHT ASSEMBLY AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: PROBE — DEFECTIVE (FUEL SYSTEM) · airframe 27,996 hrs · 11,269 cycles

THE AIRCRAFT WAS GROUNDED. FUEL FROM THE RIGHT TANK WAS EITHER BURNING OR TRANSFERRING TO CENTER TANK AT THE RATE OF 1000 LBS IN 3.0 HOURS. ALL FUEL SHOULD HAVE BURNED FROM CENTER ONLY. FUEL FLOW WERE MATCHED CENTER TANK HAD 8000 LBS WITH BOTH PUMPS ON AND X FEED VALVE CLOSED. VENDOR REPLACED NR 8 FUEL PROBE ON RIGHT HAND WING. OPERATIONS CHECK AND LEAK CHECK SATISFACTORY.

Part: PROBE — DEFECTIVE (FUEL SYSTEM) · airframe 27,996 hrs · 11,269 cycles

THE AIRCRAFT WAS GROUNDED. FUEL FROM THE RIGHT TANK WAS EITHER BURNING OR TRANSFERRING TO CENTER TANK AT THE RATE OF 1000 LBS IN 3.0 HOURS. ALL FUEL SHOULD HAVE BURNED FROM CENTER ONLY. FUEL FLOW WERE MATCHED CENTER TANK HAD 8000 LBS WITH BOTH PUMPS ON AND X FEED VALVE CLOSED. VENDOR REPLACED NR 7 FUEL PROBE ON RIGHT HAND WING. OPERATIONS CHECK AND LEAK CHECK SATISFACTORY.

Part: PROBE — DEFECTIVE (FUEL SYSTEM) · airframe 27,996 hrs · 11,269 cycles

THE AIRCRAFT WAS GROUNDED. FUEL FROM THE RIGHT TANK WAS EITHER BURNING OR TRANSFERRING TO CENTER TANK AT THE RATE OF 1000 LBS IN 3.0 HOURS. ALL FUEL SHOULD HAVE BURNED FROM CENTER ONLY. FUEL FLOW WERE MATCHED CENTER TANK HAD 8000 LBS WITH BOTH PUMPS ON AND X FEED VALVE CLOSED. VENDOR REPLACED NR 10 FUEL PROBE ON RIGHT HAND WING. OPERATIONS CHECK AND LEAK CHECK SATISFACTORY.

Part: PROBE — DEFECTIVE (FUEL SYSTEM) · airframe 27,996 hrs · 11,269 cycles

THE AIRCRAFT WAS GROUNDED. FUEL FROM THE RIGHT TANK WAS EITHER BURNING OR TRANSFERRING TO CENTER TANK AT THE RATE OF 1000 LBS IN 3.0 HOURS. ALL FUEL SHOULD HAVE BURNED FROM CENTER ONLY. FUEL FLOW WERE MATCHED CENTER TANK HAD 8000 LBS WITH BOTH PUMPS ON AND X FEED VALVE CLOSED. VENDOR REPLACED NR 9 FUEL PROBE ON RIGHT HAND WING. OPERATIONS CHECK AND LEAK CHECK SATISFACTORY.

Part: PROBE — FAILED (ZONE 100) · airframe 26,545 hrs · 10,606 cycles

DURING CRUISE, TOTAL AIR TEMPERATURE PROBE HAD MULTIPLE SYSTEM FAILURES. EMERGENCY DECLARED, FLIGHT DIVERTED TO CUN, AND LANDED OVERWEIGHT WITHOUT FURTHER INCIDENTS. MAINTENANCE REPLACED TOTAL AIR TEMPERATURE PROBE PER AMM 34-21-06-400-801 AND PERFORMED SATISFACTORY SYSTEM TEST. TH EAIRCRAFT WAS GROUNDED

Part: GIRT BAR — OBSTRUCTED (SERVICE DOOR) · airframe 24,730 hrs · 9,801 cycles

GIRT BAR AT FORWARD SERVICE DOOR BINDING. REMOVED DEBRIS FROM FORWARD SERVICE DOOR GIRT BAR AREA. OPS CHECKED OK.

Part: GIRT BAR — DIRTY (SERVICE DOOR) · airframe 24,730 hrs · 9,801 cycles

GIRT BAR AT FORWARD SERVICE DOOR JAMMED. REMOVED DEBRIS FROM FORWARD SERVICE DOOR GIRT BAR AREA. OPS CHECKED OK.

Part: LENS — LOOSE (CABIN) · airframe 23,951 hrs · 9,467 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN BY THE L2 DOOR HAS A LOOSE LENS COVER. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (OVERHEAT DETECT) · airframe 23,425 hrs · 9,238 cycles

RIGHT AFT WING BODY OVERHEAT INDICATION. EMERGENCY DECLARED, FLIGHT RETURNED TO DEPARTURE. LANDING UNEVENTFUL. ACCOMPLISHED WING TO BODY HEAT DETECTOR FAULT ISOLATION IAW 26-18-00-810-802, CONTROL MODULE BITE IAW AMM 26-18-00, AND HIGH POWER ENGINE RUN IAW AMM 71-00-00. NO FAULTS NOTED, OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 22,891 hrs · 9,049 cycles

EMERGENCY EXIT LIGHT COVER AT FWD SERVICE DOOR BROKEN. THE COVER WAS REPLACED IAW AMM 25-63-00, GOOD FOR SERVICE.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 22,891 hrs · 9,049 cycles

EMERGENCY EXIT LIGHT COVER AT CENTER FUSELAGE DAMAGED. THE COVER WAS REPLACED IAW AMM 25-63-00, GOOD FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 22,271 hrs · 8,803 cycles

AIRCRAFT WAS NOT GROUNDED. ON TAKEOFF RIGHT AFTER TOGA, RECEIVED TAKEOFF CONFIGURATION WARNING INDICATION. ABORTED TAKEOFF AND EXITED RUNWAY. ACCOMPLISHED FIM 27-62-00 FOR SPEED BRAKE AND ACCOMPLISHED FIM 32-09-00 FOR TAKE OFF WARNING. NO FAULTS NOTED. OPERATIONAL CHECK GOOD.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 22,041 hrs · 8,713 cycles

AIRCRAFT WAS GROUNDED. ON TAKEOFF, CREW REPORTED SEEING AND SMELLING SMOKE IN THE COCKPIT. ABORTED TAKEOFF AT 110 KNOTS. PERFORMED CABIN ODOR TROUBLESHOOTING IAW SIC 05-96-20, AND PACK BURNOUT PROCEDURE. NO ODORS NOTED. OPERATIONAL CHECK GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,753 hrs · 7,367 cycles

AIRCRAFT WAS IN BASE MX. CABIN FLOOR INTERCOSTAL, BETWEEN FS 344 & 360 AT BL0 IS CRACKED. R & R INTERCOSTAL IAW AARD 51-00-05-1, SRM 53-10-51 & DWG 141A5400.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,753 hrs · 7,367 cycles

AIRCRAFT WAS IN BASE MX. CABIN FLOOR SUPPORT AT FS 540 & LBL 3 IS CRACKED. R & R SUPPORT IAW AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,753 hrs · 7,367 cycles

AIRCRAFT WAS IN BASE MX. CABIN FLOOR SUPPORT AT FS 540 & RBL 3 IS CRACKED. R & R SUPPORT IAW AARD 51-00-05-1.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 14,847 hrs · 5,805 cycles

EMERGENCY AISLE LIGHT AT ROW 16ABC WILL NOT ILLUMINATE. REPLACED BATTERY PACK M1670 IAW 33-51-06. SYS CHECKED NORMAL.

Part: FILTER — DIRTY (ZONE 100) · airframe 14,740 hrs · 5,768 cycles

AIR INTERRUPT DURING CRUISE AT FLIGHT LEVEL 370 FLIGHT ATTENDANTS ADVISED FLIGHT CREW THEY FELT LIGHT HEADED. NO SMOKE, NO FUMES IDENTIFIED. CABIN ALTITUDE WAS 6000 FEET. FLIGHT DIVERTED, LANDING UNEVENTFUL & NOT OVERWEIGHT. REPLACED LT & RT RECIRCULATION FILTERS. PERFORMED ENG RUNS & INSPECTED OVERHEAD BINS & CARGO COMPARTMENTS. ALL CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 12,883 hrs · 5,033 cycles

AISLE EMERGENCY LIGHTS AT 15DEF & 17DEF INOPERATIVE. REPLACED BATTERY PACK M1671, OPERATIONS CHECKED NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,291 hrs · 4,807 cycles

CORROSION ON AFT OF LAVATORY VENT AT STATION 927. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA B737-53-022395.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 11,283 hrs · 4,411 cycles

RT AFT LOWER BODY FAIRING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT AFT LOWER BODY FAILRING EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 11,283 hrs · 4,411 cycles

RT NR 2 DOOR SLIDE EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 2 DOOR SLIDE EXTERNAL EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: BELTFRAME — DAMAGED (FUSELAGE) · airframe 2,583 hrs · 930 cycles

BELLFRAME 1064 BULGED AND CRACKED AROUND FASTENER HOLE. REMOVED DAMAGED AREA TO .5 INCH DIAMETER AND INSTALLED SHANK-PLUG PER EA B737-53-015033.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 2,583 hrs · 930 cycles

FUSELAGE INTERCOSTAL, ABOVE LEFT FORWARD SKID MOUNT - VERTICAL ANGLE CRACKED. CUT OFF DAMAGED VERTICAL ANGLE AND INSTALLED FABRICATED REPAIR FITTING PER EA B737-53-015034.

Part: BULKHEAD — BUCKLED (FUSELAGE) · airframe 2,583 hrs · 930 cycles

AFT PRESSURE BULKHEAD 1016, AFT SIDE 12:30 O`CLOCK POSITION - WEB BUCKLED. REPAIRED BY PUSHING OUT OIL CANNING AND INSTALLING DOUBLER REPAIR PER EA B737-53-015036.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 987 hrs · 349 cycles

THE EXTERIOR RIGHT OVERWING EMERGENCY EXIT ESCAPE FLOOD LIGHT AFT OF THE RIGHT AFT OVERWING EXIT IS INOPERATIVE. REPLACED LAMP THE EXTERIOR RIGHT OVERWING EMERGENCY EXIT ESCAPE FLOODLIGHT AFT OF THE RIGHT AFT OVERWING EXIT. OPS CHECKED NORMAL.