N929AN

Part: PANEL — DISCONNECTED (EMERGENCY LIGHT) · airframe 68,399 hrs · 29,007 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 19C LOWER AISLE EMERGENCY LIGHTING PANEL DISCONNECTED. (OPEN).

Part: LIGHT — DISCONNECTED (ZONE 200) · airframe 68,399 hrs · 29,007 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 19C LOWER AISLE EMERGENCY LIGHTING PANEL DISCONNECTED. REMOVED AND REPLACED EMERGENCY LIGHTING PANEL AT SEAT 19C. PER AMM 33-51-11.

Part: LIGHT — DISCONNECTED (ZONE 200) · airframe 67,873 hrs · 28,757 cycles

AIRCRAFT WAS NOT GROUNDED: 32C FLOOR EMERGENCY EXIT PATH LIGHTING HAS COME LOOSE AND IS DISCONNECTED. RESECURED 32C EMERGENCY LIGHT.

Part: WARNING LIGHT — ILLUMINATED (A/C PACK) · airframe 67,503 hrs · 28,561 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: CLIMBING THROUGH 10K RIGHT A/C PACK LIGHT CAME ON. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DFW. (OPEN).

Part: DUCT — DAMAGED (ZONE 100) · airframe 67,503 hrs · 28,561 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: CLIMBING THROUGH 10K RIGHT "PACK " LIGHT CAME ON. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DFW. PERFORMED MULTIPLE TROUBLESHOOTING OF LEFT HAND HEAT EXCHANGERS AND PLENUMS. PERFORMED CLEANING OF LEFT HAND HEAT EXCHANGERS. FOUND COMPRESSORE INLET DUCT ASSEMBLY AND PRIMARY HEAT EXCHANGER DUCT ASSEMBLY. DAMAGED. REMOVED AND REPLACED BOTH RIGHT (AALA202507141347) AND LEFT (AALA202507176778) DUCT ASSEMBLY. NO LEAKS DETECTED. RIGHT AND LEFT HAND PACK TEMPS PASSED.

Part: DUCT — DAMAGED (ZONE 100) · airframe 67,503 hrs · 28,561 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: CLIMBING THROUGH 10K RIGHT PACK LIGHT CAME ON. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DFW. PERFORMED MULTIPLE TROUBLESHOOTING OF LEFT HAND HEAT EXCHANGERS AND PLENUMS. PERFORMED CLEANING OF LEFT HAND HEAT EXCHANGERS. FOUND COMPRESSORE INLET DUCT ASSEMBLY AND PRIMARY HEAT EXCHANGER DUCT ASSEMBLY. DAMAGED. REMOVED AND REPLACED BOTH RIGHT (AALA202507141347) AND LEFT (AALA202507176778) DUCT ASSEMBLY. NO LEAKS DETECTED. RIGHT AND LEFT HAND PACK TEMPS PASSED.

Part: SIGN — INCORRECT (ZONE 200) · airframe 67,478 hrs · 28,549 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT SAYS DURING DEPLANING THEY NOTICED THE R1 DOOR EXIT SIGN ABOVE THE DOOR APPEARS TO BE INCORRECT SIGNAGE. INSTALLED NEW EXIT SIGN. PER AMM 33-51-01.

Part: DOOR — LACK OF LUBE (ZONE 800) · airframe 67,208 hrs · 28,424 cycles

AIRCRAFT WAS NOT GROUNDED: WHEN ATTEMPTING TO OPEN THE FLIGHT DECK DOOR WITH THE CORRECT CODE THE LIGHT ON THE DOOR TURNS YELLOW AND UPON TURNING GREEN TH EDOOR DOES NOT UNLOCK AND WILL NOT OPEN. LUBRICATED AND PERFORMED OPERATIONAL CHECK GOOD. PER AMM 52-51-00.

Part: FLASHLIGHT — MISSING (ZONE 200) · airframe 67,116 hrs · 28,383 cycles

AIRCRAFT WAS NOT GROUNDED: INOPERATIVE FLASHLIGHT REMOVED FROM NUMBER 1 JUMPSEAT AND INSTALLED IN 4R JUMPSEAT POSITION. **SUPPLEMENTAL REPORT FOR (AALA202505301666): REMOVE AND REPLACED JUMPSEAT 4R FLASHLIGHT. PER AMM 25-64-00. OPERTIONAL CHECK GOOD**(CLOSED).

Part: FLASHLIGHT — NO TEST (ZONE 200) · airframe 67,116 hrs · 28,383 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT UNDER NUMBER 1 FLIGHT ATTANDENT JUMPSEAT THE (FORWARD JUMPSEAT) GREEN BLINKING LIGHT IS NOT ILLUMINATING. REMOVED AND REPLACED FORWARD JUMP SEAT EMERGENCY FLASHLIGHT WITH 4R JUMP SEAT EMERGENCY FLASHLIGHT. PER MM 25-64-00.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 67,116 hrs · 28,383 cycles

AIRCRAFT WAS NOT GROUNDED: INOPERATIVE FLASHLIGHT REMOVED FROM NUMBER 1 JUMPSEAT AND INSTALLED IN 4R JUMPSEAT POSITION. (OPEN).

Part: SLIDE — UNSECURE (ZONE 800) · airframe 66,781 hrs · 28,217 cycles

AIRCRAFT WAS GROUNDED: AFT RIGHT SIDE DOOR SLIDE LOOKS TO BE PARTIALLY UNSEATED OR LOOSE. REMOVED AND REPLACED R2 EMERGENCY EXIT SLIDE. PER JOB CARD 08L22125001.

Part: CONNECTOR — DISCONNECTED (ZONE 200) · airframe 65,855 hrs · 27,801 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT ROWS 15 ABC, 16ABC, AND 17 ABC EMERGENCY ROW END RED LIGHTS INOP. T/S IN REF. TO FIM 33-50-00-810-801 AND FOUND CONNECTOR D95033 DISCONNECTED. RECONNECTED D95033.

Part: CONNECTOR — DAMAGED (ZONE 200) · airframe 65,209 hrs · 27,479 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY AISLE LIGHT ABOVE SEATS A/B/C IN ROW 17 WILL NOT ILLUMINATE. MAINTENANCE REPLACED PLUG AT RECEPTACLE D14816 ROW 17 OVERHEAD LEFT PER SWPM20-61-28. EMER LIGHT SYS OPERATIONAL CK OK PER AMM 33-51-00.

Part: WIRE HARNESS — DISCONNECTED (ZONE 200) · airframe 65,208 hrs · 27,479 cycles

AIRCRAT WAS NOT GROUNDED: EMERGENCY LAMPS FROM #27ABC THROUGH #33ABC INOP. MAINTENANCE FOUND SEAT HARNESS AT 27 ABC DISCONNECTED AT SEAT BOX. EMERGENCY LIGHTS OPS CK OK.

Part: FITTING — CRACKED (ZONE 100) · airframe 64,707 hrs · 27,217 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 100) · airframe 64,707 hrs · 27,217 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 64,707 hrs · 27,217 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 64,707 hrs · 27,217 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 100) · airframe 64,707 hrs · 27,217 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 64,707 hrs · 27,217 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 100) · airframe 64,707 hrs · 27,217 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 100) · airframe 64,707 hrs · 27,217 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: FITTING — CRACKED (ZONE 100) · airframe 64,707 hrs · 27,217 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 64,707 hrs · 27,217 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: DOOR — LACK OF LUBE (L1) · airframe 64,386 hrs · 27,056 cycles

AIRCRAFT WAS NOT GROUNDED: L1 ENTRY DOOR DIFFICULT TO CLOSE. LUBRICATED AND OPERATED L1 DOOR IN REFERENCE TO AMM 52-11-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: NONE — NONE (NONE) · airframe 64,104 hrs · 26,911 cycles

AIRCRAFT WAS NOT GROUNDED: PERFORM EMERGENCY LIGHT OPERATIONAL TEST. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: LIGHT — NO TEST (CABIN) · airframe 64,104 hrs · 26,911 cycles

AIRCRAFT WAS NOT GROUNDED: PERFORM EMERGENCY LIGHT OPERATIONAL TEST. **SUPPLEMENTAL REPORT FOR (AALA202402145963): PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS. PER B737NG AMM 33-51-00-710-801. CHECK GOOD AND TEST PASS.**(CLOSED).

Part: ANGLE — OUT OF TOLERANCE (ZONE 200 - FUSE) · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE IN PASSENGER CABIN SUPPORT ANGLE AT BS 500D, RBL 44.5. REPLACED VERTICAL SUPPORT ANGLE PER AARD 51-00-05-1

Part: WEB — ELONGATED (ZONE 100 - FUSE) · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLES IN WEB LOCATED AT BS 500C TO 500D AND RBL 44.5. REPLACED WEB PER AARD 51-00-05-1.

Part: INTERCOSTAL — OUT OF TOLERANCE (ZONE 100 - FUSE) · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE IN FORWARD CARGO COMPARTMENT INTERCOSTAL FROM BS 500G TO BS 5OOH, AT LBL 24. REPLACED INTERCOSTAL PER AARD 51-00-01-1.

Part: BAFFLE — OUT OF TOLERANCE (ZONE 100 - FUSE) · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: OVERSIZED / OBLONG HOLE IN FORWARD CARGO COMPARTMENT BAFFLE FROM BS 500 TO BS 500A AT LBL 24. REPLACED BAFFLE PER AARD 51-00-05 REPAIR 1.

Part: INTERCOSTAL — OUT OF TOLERANCE (ZONE 100 - FUSE) · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE IN FORWARD CARGO COMPARTMENT INTERCOSTAL FROM BS 500A TO BS 5OOB, AT LBL 24. REPLACED INTERCOSTAL PER AARD 51-00-01-1.

Part: BAFFLE — CRACKED (ZONE 100 - FUSE) · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE FROM BS 440 TO BS 460, AT LBL 25. REPLACED BAFFLE PER AARD 51-00-05.

Part: RIB — CRACKED (ZONE 300 - STABS) · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER RIB NUMBER 5 THIRD STIFFENER, LOCATED AT STABILIZER STA 92.70, REPAIRED RIB PER SRM 55-10-09-2R REPAIR 4.

Part: DOUBLER — DAMAGED (ZONE 300 - STABS) · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: ACCESS HOLE FOR STAB RIB AT STAB BS 97.02 RIGHT HAND SIDE NEEDS TO BE REPAIRED. REPAIRED WITH EXTERNAL DOUBLE REPAIR. PER SRM 55-10-01-2R-11.

Part: INTERCOSTAL — NONE (ZONE 100 - FUSE) · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT INTERCOSTAL BETWEEN BS 440 AND BS 460 AT LBL 24 REQUIRES REPLACEMENT DUE EXISTING REPAIR. REPLACED INTERCOSTAL PER AARD AARD 51-00-05-1.

Part: INTERCOSTAL — NONE (ZONE 100 - FUSE) · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT INTERCOSTAL BETWEEN BS 460 AND BS 480 AT LBL 24 REQUIRES REPLACEMENT DUE EXISTING REPAIR. REPLACED INTERCOSTAL PER AARD AARD 51-00-05-1.

Part: INTERCOSTAL — NONE (ZONE 100 - FUSE) · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT INTERCOSTAL BETWEEN BS 500D AND BS 500E AT LBL 24 REQUIRES REPLACEMENT DUE EXISTING REPAIR. REPLACED INTERCOSTAL PER AARD AARD 51-00-05-1.

Part: PANEL — CRACKED (ZONE 100 - FUSE) · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOORBOARD SUPPORT BREAK ASSEMBLY PANEL AT STA 540, RBL 0 TO RBL 24.7. REPLACED FLOORBOARD SUPPORT BREAK ASSEMBLY PANEL PER AARD 51-00-05-01 REPAIR 1.

Part: INTERCOSTAL — NONE (ZONE 100 - FUSE) · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT INTERCOSTAL BETWEEN BS 500G AND BS 500H AT LBL 24 REQUIRES REPLACEMENT DUE EXISTING REPAIR. REPLACED INTERCOSTAL PER AARD AARD 51-00-05-1.

Part: PANEL — CRACKED (ZONE 100 - FUSE) · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOORBOARD SUPPORT BREAK ASSEMBLY PANEL AT STA 540, LBL 0 TO LBL 24.7. REPLACED FLOORBOARD SUPPORT BREAK ASSEMBLY PANEL PER AARD 51-00-05-01 REPAIR 1.

Part: ANGLE — CORRODED (BS 955 LBL 54) · corrosion level 2 · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CREASE ANGLE LOCATED FROM BS 947 TO BS 955, LBL 54. REPAIRED CREASE ANGLE PER SRM 51-10-02 AND EA 349654.

Part: INTERCOSTAL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR INTERCOSTAL BETWEEN BS 947 AND BS 967, LBL 50. REPLACED INTERCOSTAL PER AARD 51-11-05.

Part: ANGLE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR BOARD SUPPORT ANGLE AT BS 772, LBL 13. REPAIRED ANGLE PER SRM 53-00-53 R2.

Part: TRANSITION PANEL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 500CAND BS 500I AT LBL 24. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN UPPER CHORD OF FLOOR BEAM AT BS 986, LBL 41. REPAIRED CHORD PER SRM 53-70-51-2R-4 AND EA 349708 AND EA 349842

Part: TRANSITION PANEL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 500A AND BS 500I AT RBL 24. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 500B AND BS 500E AT RBL 24. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: ANGLE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,789 hrs · 26,768 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR BOARD SUPPORT ANGLE AT BS 772, LBL 9. REPAIRED ANGLE PER SRM 53-00-53 R2.

Part: AOA — FAULT MESSAGE (ZONE 100 - FUSE) · airframe 63,340 hrs · 26,540 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO TUL. AFTER TAKEOFF AMBER SPEED LIMIT FLAG ON UPPER LEFT CAPARTAINS PFD INTERMITTENT WITH ASSOCIATED LOSS OF FLIGHT DIRECTOR IN PFD AND HUD INTERMITTENT. RED LOWER AIRSPEED BAR INTERMITTENTLY. THE AIRCRAFT LANDED SAFELY AT TUL WITHOUT FURTHER INCIDENT. THE CREW ALSO REPORTED THAT AFTER LANDING, THE #1 STICK SHAKER TEST FAILED. MAINTENANCE REPLACED THE LEFT-HAND ANGLE OF ATTACK SENSOR (AOA) PER AMM 34-21-05-400-801 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: PUMP — LEAKING (ZONE 400) · airframe 63,138 hrs · 26,424 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MIA DUE TO HYDRAULIC QUANTITY LOSS. THE AIRCRAFT LANDED SAFELY AT MIA WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGINE #1 HYDRAULIC PUMP PER AMM 29-11-11 (AALA202308049161). REPLACED SYSTEM B ELECTRIC MOTOR DRIVEN PUMP AMM 29-11-21 (AALA202308044396).

Part: PUMP — LEAKING (ZONE 100 - FUSE) · airframe 63,138 hrs · 26,424 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MIA DUE TO HYDRAULIC QUANTITY LOSS. THE AIRCRAFT LANDED SAFELY AT MIA WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGINE #1 HYDRAULIC PUMP PER AMM 29-11-11 (AALA202308049161). REPLACED SYSTEM B ELECTRIC MOTOR DRIVEN PUMP AMM 29-11-21 (AALA202308044396).

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 61,105 hrs · 25,420 cycles

AIRCRAFT WAS GROUNDED: DURING EMERGENCY LIGHT TEST FOUND EXIT LIGHT ASSEMBLY NOT WORKING BESIDE LAVATORY D. FOUND WIRE W4142-0415-20 STOWED BY CONNECTOR D10744. TERMINATED WIRE PER WDM 33-51-22. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: DOOR — BINDING (LAVATORY) · airframe 61,105 hrs · 25,420 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE. REMOVED AND REINSTALLED DOOR PER AMM 25-40-00. OPERATES NORMAL.

Part: DOOR — STICKING (ZONE 800 - DOORS) · airframe 60,555 hrs · 25,160 cycles

AIRCRAFT WAS GROUNDED: GATE AGENT REPORTS L1 FORWARD ENTRY DOOR HANDLE DIFFICULT TO OPEN BECAUSE HANDLE DID NOT TURN EASILY FROM OUTSIDE OF THE AIRCRAFT. ADJUSTED AND RIGGED L1 DOOR PER AMM 52-11-00.

Part: NONE — FAULTY (ZONE 200 - FUSE) · airframe 60,302 hrs · 25,031 cycles

AIRCRAFT WAS GROUNDED: AFTER LEVEL OFF FUEL INDICATIONS SHOWED 7.43, 5.91, 5.41 WITH TANK TO ENGINE WE CONFIGURED BOTH MOTORS OFF LEFT TANK AND RIGHT WING TANK CONTINUED TO GO LOWER. AT 1407Z L 7.37 C 6.3 R 5.3. EMERGENCY WAS DECLARED AND AIR RETURNED TO MIA. ACCOMPLISHED UNWANTED FUEL TRANSFER FROM NUMBER 1 TANK PER FIM TASK 28-21-00-810-803. NO FAULTS ALSO INSPECTED ENGINE NUMBER 1 FOR FUEL LEAKS NO LEAKS AND FUEL QUANTITY INDICATION SYSTEM BUILT IN TEST EQUIPMENT NO FAULTS. DUE TO HISTORY ACCOMPLISHED MORE TROUBLE SHOOTING. RIGHT CENTER TANK PUMP " LOW PRESSURE" LIGHT ILLUMINATED WITH PUMP ON. CENTER RIGHT TANK PUMP UNIVERSAL FAULT INTERRUPTER REPLACED AND TESTED PER AMM 28-22-99.

Part: DOOR — STICKING (ZONE 800 - DOORS) · airframe 60,152 hrs · 24,945 cycles

AIRCRAFT WAS NOT GROUNDED: 1L FORWARD ENTRY DOOR OBSERVED TO BE DIFFICULT TO OPEN FROM JET BRIDGE. ADJUSTED 1L DOOR PER AMM 52-11-00.

Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 60,116 hrs · 24,928 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 1L EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED DOOR 1L EXIT LIGHT LAMP ASSEMBLY PER AMM 33-51-01.

Part: GIRT BAR — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 60,051 hrs · 24,894 cycles

AIRCRAFT WAS NOT GROUNDED: 1L DOOR GIRT BAR DIFFICULT TO ARM AND DISARM. ADJUSTED GIRT BAR. OPERATIONAL CHECK GOOD.

Part: LOCK — STICKING (ZONE 800 - DOORS) · airframe 60,051 hrs · 24,894 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO LOCK AND UNLOCK. LUBRICATED LATCH ASSEMBLY. OPERATIONS OKAY.

Part: THRESHOLD — STICKING (ZONE 200 - FUSE) · airframe 59,958 hrs · 24,854 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING MAIN BASE VISIT FUNCTIONAL CHECK FLIGHT, LAVATORY A DOOR HARD TO OPEN AND CLOSE IN FLIGHT. REPLACED DOOR THRESHOLD PER AMM 25-40-01.

Part: SKIN — DAMAGED (ZONE 500 - LH WI) · airframe 59,956 hrs · 24,852 cycles

AIRCRAFT IN BASE MAINTENANCE: DAMAGE ON WING FIXED LEADING EDGE SKIN BEHIND THE NUMBER 4 SLAT TEMPORARY REPAIR INSTALLED FOR MAINTENANCE FERRY FROM GSO TO TUL PER EA 336732. **SUPPLEMENTAL REPORT FOR AALA202206103613: LEFT WING LEADING EDGE REPAIRED PER SRM 51-70-04.** (CLOSED)

Part: SKIN — DAMAGED · airframe 59,956 hrs · 24,852 cycles

AIRCRAFT IN BASE MAINTENANCE: DAMAGE ON WING FIXED LEADING EDGE SKIN BEHIND THE NUMBER 4 SLAT TEMPERARY REPAIR INSTALLED FOR MAINTENANCE FERRY FROM GSO TO TUL PER EA 336732. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)

Part: DOOR — STICKING (ZONE 800 - DOORS) · airframe 59,953 hrs · 24,851 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD ENTRY DOOR IS HARD TO CLOSE. PERFORMED L1 DOOR ADJUST PER B737NG AMM 52-11-00-820-801.

Part: RETAINER — CRACKED (ZONE 300 - STABS) · airframe 59,953 hrs · 24,851 cycles

AIRCRAFT WAS NOT GROUNDED: PARTS RACK - PANEL 323CL HAS A CRACKED RETAINER ON THE INSIDE OF THE PANEL. REMOVED AND REPLACED PANEL 323CL RETAINER PER B737 SRM 51-40-02.

Part: RIB — DAMAGED (ZONE 300 - STABS) · airframe 59,954 hrs · 24,851 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT HORIZONTAL STABILIZER INTERNAL RIB HAS TOOLING MARKS AT APPROXIMATELY STAB STA 129. 6 INCHES AFT OF FRONT SPAR. REMOVED DAMAGE AND ADDED DOUBLER REPAIR PER EA 336294.

Part: NONE — NONE · airframe 59,953 hrs · 24,851 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HORIZONTAL LOWER SKIN ACCESS PANEL 342BB CRACKED ON EDGE OF FASTENER HOLE. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)

Part: WINDOW FRAME — ELONGATED (ZONE 200 - FUSE) · airframe 59,954 hrs · 24,851 cycles

AIRCRAFT IN BASE MAINTENANCE: CAPTAIN'S SIDE EYEBROW WINDOW FRAME LOCATED AT BS 220.8 HAS ELONGATED HOLES. REPAIRED FRAME PER EA 336065.

Part: ACCESS PANEL — CRACKED (ZONE 100 - FUSE) · airframe 59,953 hrs · 24,851 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HORIZONTAL LOWER SKIN ACCESS PANEL 342BB CRACKED ON EDGE OF FASTENER HOLE. **SUPPLEMENTAL REPORT FOR AALA202206039977: FABRICATED NEW ACCESS PANEL 342BB PER DRAWING #182A4002 AND PER GPM SECTION 27.22.** (CLOSED)

Part: NONE — NONE · airframe 59,953 hrs · 24,851 cycles

AIRCRAFT IN BASE MAINTENANCE: L2 DOOR GIRT BAR FITTINGS MISSING SEALED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: LENS — DAMAGED (ZONE 200 - FUSE) · airframe 59,953 hrs · 24,851 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND OVER WING EMERGENCY EXIT LIGHT LENS DAMAGED. REPLACED LENS PER AMM 33-51-04.

Part: FITTING — NONE (ZONE 800 - DOORS) · airframe 59,953 hrs · 24,851 cycles

AIRCRAFT IN BASE MAINTENANCE: L2 DOOR GIRT BAR FITTINGS MISSING SEALED. **SUPPLEMENTAL REPORT FOR AALA202205275291: SEALED GIRT BAR FITTINGS.** (CLOSED)

Part: SKIN — PUNCTURED (ZONE 300 - STABS) · airframe 59,954 hrs · 24,851 cycles

AIRCRAFT IN BASE MAINTENANCE: HORIZONTAL STABILIZER LEFT HAND ELEVATOR SKIN HAS A PUNCTURE LOCATED AT STABILIZER STA 83.50 AND ELEVATOR STA 41. REPAIRED PUNCTURE PER SRM 55-20-01-2R-1 AREA 1.

Part: SKIN — PUNCTURED (ZONE 300 - STABS) · airframe 59,954 hrs · 24,851 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR HAS PUNCTURE 1 INCH DIAMETER 118 INCHES FROM INBOARD EDGE AND 13.5" FROM TRAILING EDGE. LOCATED AT STA 184.70, AND BUTT LINE 142.9. PERFORMED BONDED REPAIR ON LEFT ELEVATOR UPPER SKIN PER SRM 55-20-01-2R-1.

Part: SKIN — PUNCTURED (ZONE 300 - STABS) · airframe 59,954 hrs · 24,851 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR HAS PUNCTURE 1 INCH DIAMETER 88 INCHES FROM OUTBOARD EDGE AND 4 INCHES FROM TRAILING EDGE. LOCATION: STA 129.5 AND BUTT LINE 88. PERFORMED A BONDED REPAIR TO SKIN PER SRM 55-20-01-2R-1.

Part: SKIN — PUNCTURED (ZONE 300 - STABS) · airframe 59,954 hrs · 24,851 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR HAS PUNCTURE 1 INCH DIAMETER 69 INCHES FROM OUTBOARD EDGE AND 5 INCHES FROM TRAILING EDGE. LOCATION: STA 120.3 AND BUTT LINE 69. PERFORMED BONDED REPAIR ON ELEVATOR PER SRM 55-20-01-2R-1.

Part: SKIN — PUNCTURED (ZONE 300 - STABS) · airframe 59,954 hrs · 24,851 cycles

AIRCRAFT IN BASE MAINTENANCE: HORIZONTAL STABILIZER LEFT HAND ELEVATOR SKIN HAS A PUNCTURE LOCATED AT STABILIZER STA 83.50 AND ELEVATOR STA 38. REPAIRED PUNCTURE PER SRM 55-20-01-2R-1 AREA 2.

Part: SKIN — PUNCTURED (ZONE 300 - STABS) · airframe 59,954 hrs · 24,851 cycles

AIRCRAFT IN BASE MAINTENANCE: HORIZONTAL STABILIZER LEFT HAND ELEVATOR SKIN HAS A PUNCTURE LOCATED AT STABILIZER STA 66.50 AND ELEVATOR STA 29. REPAIRED PUNCTURE PER SRM 55-20-01-2R-1 AREA 3.

Part: STRAP — DAMAGED (ZONE 200 - FUSE) · airframe 59,954 hrs · 24,851 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND OUTBOARD UPPER SEAT TRACK STRAP SPLICE LOCATED AT STA 887 AND RBL 45.50 HAS A DAMAGED HOLE. REPLACED SEAT TRACK STRAP SPLICE PER SRM 51-40-02 AND 51-40-05.

Part: INTERCOSTAL — OUT OF POSITION (ZONE 100 - FUSE) · airframe 59,954 hrs · 24,851 cycles

AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN INTERCOSTAL AT STA 334 RIGHT BUTT LINE 10.40 HAS NUTPLATE HOLE THAT INTERFERES WITH NEW LOCATION FOR G2 MOUNTS. REMOVED AND REPLACED INTERCOSTAL WITH NEW ONE THAT FITS PER SRM 51-40-02.

Part: INDICATOR — FALSE INDICATION (FUEL SYSTEM) · airframe 59,664 hrs · 24,724 cycles

AIRCRAFT WAS GROUNDED: DIVERTED IAH ACCOUNT REPORTED FUEL IMBALANCE. FUEL QUANITY IMBALANCE. LEFT MAIN DECREASING RIGHT,MAIN DOES NOT. EMERGENCY DECLARED. PERFORMED FUEL TRANSFER AND FUEL QUANITY STICK CHECK.FOUND NORMAL.READINGS MATCH. ACCOMPLISHED OPS TEST FQIS IAW AMM 28-41-00-710 NO FAULT FOUND, NO POPPED C/B FOUND. PERFORMED ENGINE RUN USING R/H FUEL PUMPS. OPS CHECK NORMAL IAW 71-00-00 COULD NOT DUPLICATE FAULT.

Part: RECEPTACLE — FAULTY (EXTERNAL POWER) · airframe 59,544 hrs · 24,676 cycles

AIRCRAFT WAS GROUNDED: FA REPORTS OUTSIDE MAIN DOOR AIRCRAFT SKIN GIVING ELECTRIC SHOCKS. REPLACED EXTERNAL PWR RECEPTACLE PER AMM 24-42-11.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 59,146 hrs · 24,485 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS R/H AFT LAV SMOKE DETECTOR CONSTANTLY CHIMES. REMOVED AND REPLACED RT AFT LAV SMOKE DET IAW MM 26-14-01. OPS CHECKS NORMAL.

Part: ACTUATOR — FAULTY (ELEVATOR) · airframe 58,341 hrs · 24,100 cycles

AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO ORD ON ACCOUNT OF AUTO PILOT TRIM FAULTED. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED OVERWEIGHT WITHOUT INCIDENT. MAINTENANCE REPORTS DFCS BITE SHOWS FAULT - A/P DISC CHAN-A VNAV SPD LNAV ENG - RAN LRU TEST. HAD FAULT SPEED/STAB CHAN-A ELEV POS SEN-1. MAINTENANCE REPLACED ELEV POS SEN M929 IAW AMM 22-11-30-400-801, NO HELP. MAINTENANCE REMOVED A/P ELEVATOR ACTUATOR SYS A IAW AMM 22-11-26. ACCOMPLISHED AUTOPILOT ELEVATOR ACTUATOR ADJUSTMENT AND TEST IAW AMM 22-11-26-820-801. ALL INDICATION NORMAL, OK FOR SERVICE.

Part: SPRING — STICKING (DOOR GUST LOCK) · airframe 57,572 hrs · 23,764 cycles

AIRCRAFT WAS GROUNDED. PILOT REPORTS GUST LOCK ON MAIN ENTRANCE DOOR STICKS AND IS DIFFICULT TO OPERATE. MAINTENANCE REPLACED ASSITS LEVER SPRING ON L1 DOOR IAW AMM 52-11-21. OPS CHECKED GOOD.

Part: CONNECTOR — FAULTY (ZONE 300) · airframe 57,310 hrs · 23,648 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTS THAT DURING CLIMBOUT FROM SJU WITH AUTOPILOT ENGAGED, A/C HAD 2 UNCOMMANDED ELEVATOR INPUTS WHICH SHOOK THE CONTROL COLUMNS. 1ST TIME WAS AT FL180 AND THE 2ND WAS AT FL260. MAINTENANCE CURRENTLY WORKING THIS EVENT.***SUPPLEMENTAL INFORMATION: MAINTENANCE REMOVED AND REPLACED CONNECTORS D1679 AND D1711 FOR ELEVATOR POSN SENS (M929) IAW SWPM 20-61-11 AND WDM 22-12-41 & WDM 22-12-31. ACCOMPLISHED ELEVATOR POSITION SENSOR TEST IAW AMM 22-11-30-710-801.OPS CHECK GOOD.***(CLOSED)

Part: COMPUTER — FAULTY (NAV) · airframe 57,210 hrs · 23,605 cycles

AIRCRAFT WAS GROUNDED: DURING DECENT IN VNAV MODE AIRCRAFT SUFFERED UNCOMMANDED ELEVATOR INPUTS FROM THE AUTO PILOT. THESE UNCOMMANDED INPUTS WERE MODERATE, AUTO PILOT CMD - A THE FIRST ONE WAS PASSING 25,000 FEET THE SECOND ONE WAS PASSING 18,000 FEET. ACCOMPLISHED DFCS BITE FAULT HISTORY AND CURRENT FAULTS IAW FIM 22-11-00 ,NO FAULTS FOUND. REMOVED AND REPLACED FCC-A IAW MM 22-11-33.ALL CKS NORMAL ACCOMPLISHED AND VERIFY IAW MM 22-11-00 AND BITE TEST IAW MM 34-36-00. ALL CKS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,892 hrs · 23,471 cycles

MAINTENANCE FOUND THE RT EXTERIOR OVERWING SLIDE EMERGENCY LIGHT AND THE LAMP WAS INOPERATIVE. TROUBLESHOT IAW WDM 33-51-11. FOUND THE BATTERY PACK FAILED. REMOVED AND REPLACED THE BATTERY PACK M1672 IAW AMM 33-51-06. OPS CHECKED NORMAL.

Part: SLIDE — DETACHED (L1 DOOR) · airframe 56,892 hrs · 23,471 cycles

L1 DOOR SLIDE FOUND DETACHED AND ON THE FLOOR, STILL IN COVER. MAINTENANCE INSTALLED THE L1 DOOR SLIDE IAW 25-94-10.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LEFT) · airframe 56,888 hrs · 23,469 cycles

THE PILOT REPORTED THAT THE AFT LEFT SMOKE ALARM SOUNDED. NO SMOKE PRESENT. MAINTENANCE VISUALLY INSPECTED THE SMOKE DETECTOR, SEALS WERE PRESENT AND POWER LIGHT WAS ON. NO VISUAL DEFECTS WERE NOTED AND THE SELF TEST WAS OK IAW AMM 26-14-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,888 hrs · 23,469 cycles

MAINTENANCE REPORTED THAT THE EXTERIOR LIGHT FOR THE RT OVERWING SLIDE AT THE AFT FILLET PANEL WAS FOUND INOPERATIVE. THE BATTERY PACK WAS FOUND TO BE THE ISSUE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-06, OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 55,455 hrs · 22,850 cycles

L1 DOOR EMERGENCY LIGHTS WERE INOPERATIVE. FOUND THE CONNECTOR WAS DISCONNECTED, REPLACED THE POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED NORMAL.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 54,240 hrs · 22,308 cycles

THE AIRCRAFT WAS NOT GROUNDED. FABRIC THAT CONNECTS GIRT BAR TO SLIDE APPEARS TO BE LONG AND DRAGS ALONG FLOOR WHEN DOOR 1R IS OPEN. REMOVED AND REPLACED R1 DOOR SLIDE PER MAINTENANCE WORK CARD 25-94-11.

Part: ANGLE — CORRODED (BS 960) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON THE LEFT CREASE ANGLE AT BS 960, LBL 50. REMOVED AND REPLACED THE CREASE ANGLE IAW SRM 51-00-05-1, DRAWING 147A8501 AND EA 274115.

Part: STRAP — CORRODED (BS 1006-1023) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON THE G4 GALLEY REINFORCEMENT STRAP BETWEEN BS 1006 AND 1023, LBL 18. REMOVED AND REPLACED THE STRAP SRM 51-00-05-1, SRM 51-40-02, AND DRAWING 147A5700.

Part: STRAP — CORRODED (BS 1006-1023) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON G4 GALLEY REINFORCEMENT STRAP BETWEEN BS 1006 AND 1023 AT LBL27. REMOVED AND REPLACED STRAP PER SRM 51-00-05-1 AND DRAWING 147A5700.

Part: STRAP — CORRODED (BS 1006-1023) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON G4 GALLEY REINFORCEMENT STRAP BETWEEN BS 1006 AND 1023, LBL 3. REMOVED AND REPLACED STRAP IAW SRM 51-00-05-1, SRM 51-40-02, AND DRAWING 147A5700.

Part: INTERCOSTAL — CORRODED (BS 1019) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT PRESSURE BULKHEAD WATER SEAL INTERCOSTAL AT BS 1019, LBL 20. REMOVED AND REPLACED THE INTERCOSTAL SRM 51-00-05-1.

Part: INTERCOSTAL — CORRODED (BS 1020) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT PRESSURE BULKHEAD WATER SEAL INTERCOSTAL AT BS 1020, RBL 5. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-00-05-1.

Part: INTERCOSTAL — CORRODED (BS 1020) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT PRESSURE BULKHEAD WATER SEAL INTERCOSTAL AT BS 1020, LBL 5. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-00-05-1.

Part: INTERCOSTAL — CORRODED (BS 1017) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT PRESSURE BULKHEAD INTERCOSTAL AT BS 1017, LBL 32. REMOVED AND REPLACED THE INTERCOSTAL SRM 51-00-05-1.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 52,669 hrs · 21,639 cycles

CRACK INDICATION ON RIGHT MAIN LANDING GEAR WHEEL WELL VERTICAL PRESSURE BULKHEAD WEB AT BS 663, RBL 32. REPAIRED THE BULKHEAD WEB IAW SRM 57-10-10-2R-3, AND EA 273405.

Part: INTERCOSTAL — CORRODED (BS 1021) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT PRESSURE BULKHEAD WATER SEAL INTERCOSTAL AT BS 1021, LBL 12. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-00-05-1.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 52,669 hrs · 21,639 cycles

CRACK INDICATIONS ON CENTER WING REAR SPAR LEFT MAIN LANDING GEAR WHEEL WELL VERTICAL PRESSURE WEB AT BS 663, BETWEEN LBL 24.92 AND LBL 40. REPAIRED THE BULKHEAD WEB IAW SRM 57-10-10-2R-3, EA 273401, AND EA 273603.

Part: TRANSITION PANEL — CORRODED (BS 727-807) · airframe 52,669 hrs · 21,639 cycles

CORROSION ON AFT CARGO TRANSITION PANEL BS 727 TO 807. REMOVED AND REPLACED THE TRANSITION PANEL IAW SRM 53-00-53-2R, EA 273810, AND EA 273598.

Part: CHANNEL — CORRODED (BS 947-967) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON CABIN AFT ENTRY DOOR FORWARD DOOR DRAIN CHANNEL BETWEEN BS 947 AND 967, LBL 50. REMOVED AND REPLACED THE CHANNEL IAW D 51-00-05-1, SRM 51-40-02, AND DRAWING 147A5650.

Part: INTERCOSTAL — CORRODED (BS 1024 BULKHEAD) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON AFT PRESSURE BULKHEAD WATER SEAL INTERCOSTAL AT BS 1024, RBL 20. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (BS 1018) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON AFT PRESSURE BULKHEAD WATER SEAL INTERCOSTAL AT BS 1018, RBL 32. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02.

Part: CHANNEL — CORRODED (BS 947-967) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON CABIN AFT SERVICE DOOR DRAIN CHANNEL BETWEEN BS 947 & 967, RBL 50. REMOVED AND REPLACED THE CHANNEL IAW SRM 51-40-02, D 51-00-05-1, AND DRAWING 147A5650.

Part: INTERCOSTAL — CORRODED (BS 1022 BULKHEAD) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON AFT PRESSURE BULKHEAD WATER SEAL INTERCOSTAL AT BS 1022, RBL 12. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02.

Part: PLENUM — CRACKED (APU) · airframe 52,669 hrs · 21,639 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACKED AUXILIARY POWER UNIT INLET DUCT PLENUM ASSEMBLY. REMOVED AND REPLACED PLENUM PANEL PER SRM 53-80-30-01, AARD 51-20-01-1, AND AMM 49-15-15.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON THE FLOORBEAM AT BS 947, LBL 50 AND RBL 50. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-2.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON G4 GALLEY FLOOR ZEE ANGLE AT FUSELAGE STATION 993 BETWEEN RBL33 AND RBL45. REMOVED AND REPLACED ANGLE PER AARD 51-00-05-1 AND PRINT 147A5700.

Part: FLOOR SUPPORT — CORRODED (BS 990-992) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON THE FLOOR SUPPORT AT RBL 32 BETWEEN BS 990 AND 992. REMOVED AND REPLACED THE FLOOR SUPPORT IAW D 51-00-05-1 AND DRAWING 147A5700.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT GALLEY FLOOR ZEE ANGLE BETWEEN FUSELAGE STATIONS 991 AND 1016 AT LBL32. REMOVED AND REPLACED ANGLE PER AARD 51-00-05-1 AND PRINT 147A5700.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON G4 GALLEY FLOOR ZEE ANGLE BETWEEN FUSELAGE STATIONS 997 AND 1016 AT RBL32. REMOVED AND REPLACED ANGLE PER AARD 51-00-05-1 AND PRINT 147A5700.

Part: WEB — CORRODED (BS 986-1016) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION FOUND ON THE AFT CABIN WEB BETWEEN BS 986 -1016, RBL 30 - 45. REMOVED AND REPLACED THE WEB IAW D 51-00-5-1 AND DRAWING 147A5700.

Part: FRAME — CRACKED (APU) · airframe 52,669 hrs · 21,639 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACKED AUXILIARY POWER UNIT INLET DUCT PLENUM ASSEMBLY FRAME. REPLACED PLENUM FRAME PER SRM 53-80-30-01 AND AMM 49-15-15.

Part: INTERCOSTAL — CORRODED (BS 947-967) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON INTERCOSTAL AT THE R2 DOOR BETWEEN BS 947 & 967, RBL 50. REMOVED AND REPLACED THE INTERCOSTAL IAW D 51-00-05-1, AND SRM 53-70-51.

Part: WEB — CORRODED (BS 986-1016) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON AFT CABIN LEFT WEB BETWEEN BS 986 AND 1016, LBL 30 - LBL 45. REMOVED AND REPLACED THE WEB IAW D 51-00-05-1 AND DRAWING 147A5700.

Part: WEB — CORRODED (BS 1020) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON AFT CABIN LEFT FLOOR WEB FORWARD OF AFT PRESSURE BULKHEAD AT BS 1020, LBL31. REMOVED AND REPLACED THE WEB IAW D 51-00-05-1 AND DRAWING 147A5700.

Part: ANGLE — CORRODED (BS 992) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON THE ZEE ANGLE AT BS 992, BETWEEN LBL 32 AND LBL 42. REMOVED AND REPLACED THE ANGLE IAW SRM 51-00-05-1 AND DRAWING 147A5700.

Part: FLOOR SUPPORT — CORRODED (BS 986-1006) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT BS 986 TO 1006, LBL 32. REMOVED AND REPLACED THE FLOOR SUPPORT IAW D 51-00-05-1 AND DRAWING 147A5700.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 52,669 hrs · 21,639 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT CARGO FLOOR STRINGER AT FUSELAGE STATION 767 +5 AND LBL3. REPAIRED STRINGER PER SRM 53-00-53-2R-2 AND EA 273506.

Part: FLOORBEAM — CORRODED (BS 1016) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON AFT CABIN FLOORBEAM AT BS 1016, LBL 30. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-R4, AND EA 273426.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,669 hrs · 21,639 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT CARGO FLOOR STRINGER AT FUSELAGE STATION 767 +5 AND RBL11. REPAIRED STRINGER PER SRM 53-00-53-2R-2 AND EA 273506.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,669 hrs · 21,639 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT CARGO FLOOR STRINGER AT FUSELAGE STATION 767 +5 AND RBL3. REPAIRED STRINGER PER SRM 53-00-53-2R-2 AND EA 273506.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON AFT CABIN FLOORBEAM AT BS 986 BETWEEN LBL 46 AND RBL 46. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-4.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 52,669 hrs · 21,639 cycles

CRACK INDICATIONS ON THE RIGHT HORIZONTAL STABILIZER RIB LOWER RADIUS AT HSS 92.7. REMOVED AND REPLACED THE RIB IAW SRM 55-10-09, SRM 51-40-02, AND DRAWING 182A5301.

Part: WEB — CORRODED (BS 793-847) · airframe 52,669 hrs · 21,639 cycles

CORROSION ON AFT CARGO DOOR FRAME LOWER SILL PLATE WEB BETWEEN BS 793 AND 847. REMOVED AND REPLACED THE WEB IAW D 51-00-05-1, DRAWING DBF192, AND DRAWING 146A8123.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 52,669 hrs · 21,639 cycles

CRACK INDICATIONS ON LEFT HORIZONTAL STABILIZER RIB INBOARD RADIUS AT HSS 92.7. REMOVED AND REPLACED INSPAR RIB IAW SRM 55-10-09 AND SRM 51-40-02.

Part: WEB — CORRODED (BS 986) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON THE R2 DOOR THRESHOLD WEB AT BS 986, RBL 50. REMOVED AND REPLACED THE WEB IAW D 51-00-05-1, DRAWING 147A8510, AND EA 273488.

Part: WEB — CORRODED (BS 967-986) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON THE L2 DOOR THRESHOLD WEB BETWEEN BS 967 AND 986. REMOVED AND REPLACED THE WEB IAW D 51-00-05-1, DRAWING 147A8510 AND EA 273488.

Part: TRANSITION PANEL — CORRODED (BS 727-767) · airframe 52,669 hrs · 21,639 cycles

AFT CARGO RIGHT TRANSITION PANEL AT BS 727C HAS FASTENER PULLED THROUGH WHERE IT IS ATTACHED TO FRAME. INSTALLED A NEW TRANSITION PANEL IAW SRM 53-00-53-2R-5.

Part: TRANSITION PANEL — CORRODED (BS 767) · airframe 52,669 hrs · 21,639 cycles

CORROSION ON AFT CARGO RIGHT TRANSITION PANEL AT BS 767. INSTALLED NEW TRANSITION PANEL IAW D 51-00-05-1, AND SRM 53-00-53.

Part: BAFFLE — CRACKED (BS 460-480) · airframe 52,669 hrs · 21,639 cycles

CRACKED BAFFLE IN THE FORWARD CARGO UNDER THE LEFT TRANSITION PANEL BETWEEN SS 460 AND 480. REMOVED AND REPLACED BAFFLE IAW D 51-00-05 AND DRAWING 143A7510.

Part: FLOORBEAM — CORRODED (BS 500I) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON FORWARD CARGO AFT FLOORBEAM ANGLE AT BS 500I, LONGERONS 25L AND 25R. REMOVED AND REPLACED THE FLOORBEAM ANGLE SRM 51-10-02 AND D 51-00-05.

Part: WEB — CORRODED (BS 440-492) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON FORWARD CARGO LOWER DOOR FRAME SILL PLATE WEB BETWEEN BS 440 AND 492, STRINGER 26R. REMOVED AND REPLACED THE WEB IAWSRM 51-40-02.

Part: WEB — CORRODED (BS 1016-1026) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION FOUND ON THE RIGHT HALF MOON WEB BETWEEN BS 1016 AND 1026, RBL 28 TO RBL 38. REMOVED AND REPLACED THE WEB IAW D 51-00-05-1 AND DRAWING 147A5700.

Part: TRANSITION PANEL — CORRODED (BS 420-500I) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON FORWARD CARGO RIGHT TRANSITION PANELS BETWEEN FUSELAGE STATIONS 420 AND 440 AND BETWEEN FUSELAGE STATIONS 500 AND 500I. REMOVED AND REPLACED TRANSITION PANELS IAW DWG 51-00-05-1, SRM 51-10-02, SRM 53-00-53-2R, AND DRAWING 143A8126.

Part: TRANSITION PANEL — CORRODED (BS 500-500I) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON FORWARD CARGO LEFT TRANSITION PANEL FROM BS 500 TO 500I. REMOVED AND REPLACED THE TRANSITION PANEL IAW SRM 53-00-53-2R.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 52,669 hrs · 21,639 cycles

CRACKED FLOOR SUPPORT BETWEEN BS 328 AND 344, LBL45. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 51-00-05-1 AND DRAWING 141A5400.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 52,669 hrs · 21,639 cycles

CRACKED CABIN FLOOR SUPPORT BETWEEN BS 312 AND 328, LBL 45. REMOVED AND REPLACED THE FLOOR SUPPORT IAW D 51-00-05-1 AND DRAWING 141A5400.

Part: TRANSITION PANEL — CORRODED (BS 847-867) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON AFT CARGO RIGHT TRANSITION PANEL BETWEEN BS 847 AND 867, STRINGER 25R. INSTALLED A NEW TRANSITION PANEL IAW SRM 53-00-53.

Part: ANGLE — CORRODED (BS 300-306) · corrosion level 2 · airframe 52,669 hrs · 21,639 cycles

CORROSION ON THE L1 DOOR LOWER SILL CREASE ANGLE BETWEEN BS 300 AND 306. REMOVED AND REPLACED THE CREASE ANGLE IAW SRM 53-10-15, DWG 51-00-05-1, AND DRAWING 141A8110.

Part: SHUTOFF VALVE — UNCONTROLLABLE (CABIN TEMP) · airframe 51,822 hrs · 21,255 cycles

EMERGENCY DECLARED. FLIGHT DIVERTED DUE TO CABIN TEMPERATURE WAS EXTREMELY HOT. REMOVED AND REPLACED THE ZONE TEMPERATURE CONTROL TRIM AIR PRESSURE REGULATOR AND SHUTOFF VALVE ASSEMBLY IAW AMM 21-62-01. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: SIGN — DETACHED (CABIN) · airframe 50,672 hrs · 20,780 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY EXIT SIGN AT R2 DOOR NEAR TRASH BIN IS DETACHED. SECURED EXIT SIGN IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: VALVE — OUT OF ADJUST (MLG) · airframe 49,590 hrs · 20,320 cycles

DURING CLIMB LANDING GEAR RETRACTED NORMALLY BUT EXTENDED UNCOMMANDED WHEN GEAR HANDLE WAS PLACED IN THE OFF POSITION. EMERGENCY DECLARED. LANDING UNEVENTFUL. THE AIRCRAFT WAS GROUNDED. MAINTENANCE ADJUSTED GEAR SELECTOR VALVE IAW 32-31-00. ACCOMPLISHED SUCCESSFUL GEAR SWING IAW 32-32-00.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 48,437 hrs · 19,897 cycles

AIRCRAFT WAS IN BASE MX. FLIGHT DECK R1 WINDOW FRAME IS CRACKED AT UPPER OTBD CORNER. REPAIRED WINDOW FRAME IAW EA 259557 & SB 737-53-136.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 48,437 hrs · 19,897 cycles

AIRCRAFT WAS IN BASE MX. VERTICAL PRESS WEB AT FS 663.75 IS CRACKED, BETWEEN RBL 31.83 & RBL 40. REPAIRED WEB IAW EA 259600.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,437 hrs · 19,897 cycles

AIRCRAFT WAS IN BASE MX. CABIN FLOOR INTERCOSTAL AT FWD ENTRY DOOR, BETWEEN FUSELAGE STATIONS 312 & 328 IS CRACKED. R & R INTERCOSTAL IAW AARD 51-10-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,437 hrs · 19,897 cycles

AIRCRAFT WAS IN BASE MX. CABIN FLOOR INTERCOSTAL AT FWD ENTRY DOOR, BETWEEN FUSELAGE STATIONS 328 & 344 IS CRACKED. R & R INTERCOSTAL IAW SRM 53-10-51 & DWG 141A5400.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,922 hrs · 19,692 cycles

AIRCRAFT WAS IN BASE MX. FWD CARGO COMPARTMENT LT TRANSITION PANEL IS CORRODED, AT APPROX FS 480. REPAIRED TRANSITION PANEL IAW SRM 53-00-53-2R.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,318 hrs · 18,648 cycles

EMERGENCY AREA FLOODLIGHT ASSEMBLY ON OVERHEAD ABOVE SEAT 25D FOUND INOPERATIVE DURING OPERATIONAL TEST OF EMERGENCY LIGHTS IAW MCM CARD 2904. RELAMPED EMER LIGHT IAW AMM 33-51-03. SYS CHECKED NORMAL.

Part: COVER — MISSING (CABIN) · airframe 44,099 hrs · 18,157 cycles

R2 DOOR AREA INTERIOR EMER EXIT IDENTIFIER LIGHT COVER MISSING. REPLACED EMER EXIT IDENTIFIER LIGHT AT R2 DOOR AFT IAW AMM 33-51-01. SYS CHECKED NORMAL.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 41,790 hrs · 17,264 cycles

SMALL HOLE IN AFT CARGO FLOOR PANEL AT STATION 792 RT. REPLACED PANEL IAW AMM 25-52-10.

Part: SCUFF PLATE — GOUGED (FUSELAGE) · airframe 41,790 hrs · 17,264 cycles

DENT WITH GOUGE IN AFT CARGO DOOR SCUFF PLATE. R & R SCUFF PLATE IAW AMM 53-11-02.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 40,920 hrs · 16,903 cycles

SPLICE PLATE & SEAT TRACK CRACKED AT STATION 727B & LBL 24.75. REPAIRED CRACKED SPLICE PLATE & SEAT TRACK IAW ECO J1707AA/AB & EA B737-53-032183.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 40,920 hrs · 16,903 cycles

SPLICE PLATE & SEAT TRACK CRACKED AT STATION 727B & RBL 45.50. REPAIRED CRACKED SPLICE PLATE & SEAT TRACK IAW ECO J1707AA/AB & EA B737-53-032183.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 40,920 hrs · 16,903 cycles

SPLICE PLATE & SEAT TRACK CRACKED AT STATION 727B & LBL 45.50. REPAIRED CRACKED SPLICE PLATE & SEAT TRACK IAW ECO J1707AA/AB & EA B737-53-032183.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 40,920 hrs · 16,903 cycles

SPLICE PLATE & SEAT TRACK CRACKED AT STATION 727B & RBL 24.75. REPAIRED CRACKED SPLICE PLATE & SEAT TRACK IAW ECO J1707AA/AB & EA B737-53-032183.

Part: FASTENER — SHEARED (FUSELAGE) · airframe 40,920 hrs · 16,903 cycles

FASTENER SHEARED IN SEAT TRACK AT STATION 727B & RBL 45.50. ACCOMPLISHED FASTENER REPAIR IAW ECO J1707AB CARD 003 & EA B737-53-032813.

Part: PRESSURE SWITCH — FAILED (FUEL SYSTEM) · airframe 39,592 hrs · 16,391 cycles

CREW REPORTED RT ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. EMERGENCY DECLARED, FLIGHT RETURNED T/O DEPARTURE, LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE FOR REPAIR. REPLACED S241 DIFFERENTIAL PRESSURE SWITCH. SYS GROUND CHECK NORMAL OPS. (CLOSED)

Part: FSEU — INOPERATIVE (TE FLAPS) · airframe 39,573 hrs · 16,384 cycles

INFLIGHT, CREW REPORTED FLAPS WOULD NOT DEPLOY FURTHER THAN 1 DEGREE. EMERGENCY DECLARED, FLIGHT DIVERTED, AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED FLAP SLAT ELECTRONICS UNIT. SYS GROUND CHECK NORMAL OPERATION.

Part: SENSOR — INOPERATIVE (TE FLAP SYS) · airframe 38,723 hrs · 16,047 cycles

CREW REPORTED T/E FLAP ASYMMETRY MESSAGE. EMERGENCY DECLARED, FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NR 7 SKEW SENSOR. SYS GROUND CHECK NORMAL OPERATION.

Part: TRANSMITTER — INOPERATIVE (ZONE 600) · airframe 38,723 hrs · 16,047 cycles

BOS - CREW REPORTED FLAP LEVER SELECTED TO 1 DEGREE AND NOTHING HAPPENED. FOLLOWED QRH AND EXTENDED SLATS WITH ALTERNATE FLAP SWITCH. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP LEVER POSITION TRANSMITTER AND FLAP SKEW SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 38,007 hrs · 15,756 cycles

SFO - FLIGHT ATTENDANTS REPORTED A STRONG SMELL OF SMOKE IN THE AFT CABIN JUST BEFORE LANDING. FLIGHT ATTENDANTS TURNED OFF THE POWER PORTS AND SMELL OF SMOKE SLOWLY DISSIPATED. AIRCRAFT REMOVED FROM SERVICE. REPLACED R917. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — MISSING (CABIN) · airframe 36,669 hrs · 15,210 cycles

BULLNOSE EMERGENCY LIGHT LENS AT ROW 18ABC IS MISSING. REPLACED LENS FOR BULLNOSE EMERGENCY LIGHT AT ROW 18ABC. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,445 hrs · 15,114 cycles

FOUND BATTERY PACK M1674 INOPERATIVE. REPLACED BATTERY PACK M1674. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,445 hrs · 15,114 cycles

SEAT 7D FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT 7D FORWARD EMERGENCY EXIT LIGHT. OPS CHECK NORMAL.

Part: LENS — DAMAGED (CABIN) · airframe 36,445 hrs · 15,114 cycles

RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT LENS ASSEMBLY DAMAGED. REPLACED LENS FOR RIGHT FORWARD OVERWING EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 36,445 hrs · 15,114 cycles

EMERGENCY LIGHT AT 18A UPPER BULLNOSE MISSING LENS. REPLACED LENS FOR 18A UPPER BULLNOSE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,445 hrs · 15,114 cycles

EMERGENCY LIGHTS BATTERY PACK M1670 INOPERATIVE. REPLACED BATTERY PACK M1670 FOR CABIN EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 36,445 hrs · 15,114 cycles

BULLNOSE EMERGENCY EXIT LIGHTS THROUGHOUT CABIN INOPERATIVE. RESEATED CONNECTORS THROUGHOUT CABIN, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,445 hrs · 15,114 cycles

RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP RIGHT FORWARD OVERWING EMERGENCY EXIT. OPS CHECK NORMAL.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 36,445 hrs · 15,114 cycles

BULLNOSE EMERGENCY LIGHTS THRU-OUT CABIN INOPERATIVE. RESEATED CONNECTORS FOR EMERGENCY LIGHTS THRU-OUT CABIN. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,445 hrs · 15,114 cycles

RIGHT FORWARD CABIN OVERWING EMERGENCY EXIT HANDLE LAMP INOPERATIVE. REPLACED LAMP IN RIGHT FORWARD CABIN OVERWING EMERGENCY EXIT HANDLE LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 35,653 hrs · 14,780 cycles

CORROSION ON AFT CARGO SUPPORT TRACK BETWEEN STATIONS 787 TO 847. INSTALLED STRAP PER EA B737-53-021410.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,653 hrs · 14,780 cycles

CORROSION ON UPPER SURFACE OF FLOORBEAM STATION 312 RIGHT BUTTLINE 13. ACCOMPLISHED NESTED ANGLE REPAIR PER AARD 53-00-00-7.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,653 hrs · 14,780 cycles

CORROSION ON UPPER SURFACE OF INTERCOSTAL BETWEEN STATIONS 312 AND 328, APPROXIMATELY RIGHT BUTTLINE 26. REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,653 hrs · 14,780 cycles

CORROSION ON UPPER CAP OF TRANSVERSE FLOORBEAM STATION 294. INSTALLED UPPER CAP SPLICE REPAIR PER EA B737-53-021106.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,653 hrs · 14,780 cycles

INTERCOSTAL BETWEEN STATIONS 312 AND 328 FLOORBEAMS, RIGHT BUTTLINE 31 CRACKED. REMOVED AND REPLACED INTERCOSTAL PER AARD 51-10-05-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,653 hrs · 14,780 cycles

STATION 328 TEE CAP CORRODED AT RIGHT BUTTLINE 1. REMOVED CORRODED FLANGE AND INSTALLED REPAIR PER SRM 53-10-51-2R 7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,653 hrs · 14,780 cycles

ENTIRE FLOORBEAM UPPER CAP AT STATION 986 CORRODED. INSTALLED T-CAP REPAIR PER SRM 53-70-51.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,653 hrs · 14,780 cycles

CORROSION ON LEFT Z-CHANNEL FASTENER HOLES. INSTALLED NEW SECTION OF Z-CHANNEL FROM STATIONS 767 TO 847 PER SRM 53-00-53-2R.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,653 hrs · 14,780 cycles

CORROSION ON STATION 947 BEAM. INSTALLED NEW T-CAP, DOUBLERS AND STIFFENERS ON FLOORBEAM 947.5 PER SRM 53-70-51-2R REPAIR 5 AND EA B737-53-021293.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,653 hrs · 14,780 cycles

FORWARD AUXILIARY POWER UNIT INLET PLENUM VERTICAL ANGLE CORRODED. REMOVED AND REPLACED ANGLE PER AARD 51-00-05-1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,653 hrs · 14,780 cycles

T-ANGLE RIGHT SIDE AUXILIARY POWER UNIT COMPARMENT STATION 1116 CORRODED. REMOVED AND REPLACED ANGLE PER AARD 51-00-05-1.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 35,653 hrs · 14,780 cycles

STATION 986.5 FRAME DAMAGED AT TIE IN TO 986.5 FLOORBEAM. ACCOMPLISHED NESTED ANGEL REPAIR PER EA B737-53-021120.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,653 hrs · 14,780 cycles

AUXILIARY POWER UNIT INLET PLENUM AFT VERTICAL STIFFENER CORRODED. REMOVED AND REPLACED STIFFENER PER AARD 51-00-05-1.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,653 hrs · 14,780 cycles

CORROSION AT SEVERAL PLACES ON LEFT Z-CHANNEL AFT ENTRY DOOR. INSTALLED NEW LEFT Z-CHANNEL (CREASE ANGLE) PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,653 hrs · 14,780 cycles

C-CLIP ANGLE CRACKED BELOW FLOORBOARD TRANSITION ANGLE, LEFT STATION 500I. REMOVED AND REPLACED ANGLE PER SRM 53-00-53.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 35,653 hrs · 14,780 cycles

WEB ATTACH ANGLE CRACKED BELOW FLOORBOARD TRANSITION ANGLE LEFT STATION 500F. REMOVED AND REPLACED ANGLE PER SRM 53-00-53.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 35,653 hrs · 14,780 cycles

WEB ATTACH ANGLE CRACKED BELOW FLOORBOARD TRANSITION ANGLE, RIGHT STATION 500G. REMOVED AND REPLACED TRANSITION ANGLE AT RIGHT STATION 500G PER SRM 53-00-53.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 35,653 hrs · 14,780 cycles

WEB ATTACH ANGLE CRACKED BELOW FLOORBOARD TRANSITION ANGLE, RIGHT STATION 500F. REMOVED AND REPLACED WEB ATTACH ANGLE PER SRM 53-00-53.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 35,653 hrs · 14,780 cycles

WEB ATTACH ANGLE CRACKED BELOW FLOORBOARD TRANSITION ANGLE, LEFT STATION 500E. REMOVED AND REPLACED WEB ATTACH ANGLE PER SRM 53-00-53.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 35,653 hrs · 14,780 cycles

WEB ATTACH ANGLE CRACKED BELOW FLOORBOARD TRANSITION ANGLE, LEFT STATION 500G. REMOVED AND REPLACED ANGLE PER SRM 53-00-53.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,653 hrs · 14,780 cycles

C-CLIP CRACKED BELOW TRANSITION PANEL LEFT STATION 500H. REMOVED AND REPLACED ANGLE PER SRM 53-00-53.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,653 hrs · 14,780 cycles

STATION 400 BELOW STRINGER 8 RIGHT, FRAME CRACKED AT BIN RAIL ATTACH BRACKET RIVET HOLES. INSTALLED DOUBLER PER ECO J1159AD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,653 hrs · 14,780 cycles

STATION 500D RIGHT FRAME CRACKED AT BIN RAIL ATTACH BRACKET RIVET HOLES. INSTALLED DOUBLER PER ECO J1159AD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,653 hrs · 14,780 cycles

STATION 400 BELOW STRINGER 8 LEFT, FRAME CRACKED AT BIN RAIL ATTACH BRACKET RIVET HOLES. INSTALLED DOUBLER PER ECO J1159AD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,653 hrs · 14,780 cycles

STATION 480 LEFT AT FRAME RAIL ATTACH POINT SHOWS CRACK INDICATION. INSTALLED DOUBLER PER ECO J1159AD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,653 hrs · 14,780 cycles

STATION 440 BELOW STRINGER 8 LEFT, FRAME CRACKED AT BIN RAIL ATTACH BRACKET RIVET HOLES. INSTALLED DOUBLER PER ECO J1159AD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,653 hrs · 14,780 cycles

STATION 480 BELOW STRINGER 8 RIGHT, FRAME CRACKED AT BIN RAIL ATTACH BRACKET RIVET HOLES. INSTALLED DOUBLER PER ECO J1159AD.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,653 hrs · 14,780 cycles

CORROSION ON Z-CHANNEL AT RIGHT SERVICE DOOR FLOOR AREA. REPLACED Z-CHANNEL.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 35,653 hrs · 14,780 cycles

INTERCOSTAL BETWEEN BS 312 AND 328, LBL 34 CRACKED. REPLACED INTERCOSTAL PER 51-00-05-1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,653 hrs · 14,780 cycles

CORROSION ON CREASE ANGLE AT RIGHT NUMBER DOOR. REPLACED WITH A NEW CREASE ANGLE PER AARD 51-10-05-1.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 35,653 hrs · 14,780 cycles

VERTICLE STIFFENER ON WHEEL WELL SIDE JUST OUTBOARD OF LEFT AIR CONDITIONING EXHAUST DUCT CUTOUT (APPROXIMATELY LEFT BUTTLINE 25) IS CRACKED AT LOWER END. REPLACED STIFFENER PER AARD 51-10-05 REPAIR 1.

Part: FLAP — DAMAGED (LT WING) · airframe 33,733 hrs · 14,161 cycles

LEFT WING INBOARD TRAILING EDGE FLAP HAS DENT WITH CRACK AND TEMPORARY REPAIR IN THE SAME AREA ON THE BOTTOM SIDE. INSTALLED ONE PERMANENT BONDED DOUBLER AS PER SRM 51-70-10-2R.

Part: FILLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,733 hrs · 14,161 cycles

CORROSION AT AUXILIARY POWER UNIT INLET DUCT LOWER SIDE OF BULKHEAD STATION 1088 (FILLER STRAP). INSTALLED LOWER FILLER AT APU INLET STATION 1088, PER AARD 51-10-05.

Part: SKIN — DENTED (CARGO DOOR) · airframe 33,733 hrs · 14,161 cycles

FORWARD CARGO DOOR FIELD REPORTED 3 DENTS IN FORWARD CARGO DOOR ABOVE THE HANDLE. INSTALLED NEW SKIN PER ESO 60654.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,733 hrs · 14,161 cycles

INTERCOSTAL IS CRACKED UNDER CABIN FLOOR AT STATION 312 TO 328 LEFT. REMOVED AND REPLACED THE INTERCOSTAL PER AARD 51-00-05.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,733 hrs · 14,161 cycles

CORROSION AT AUXILIARY POWER UNIT INLET DUCT UPPER SIDE OF BULKHEAD STATION 1088. INSTALLED NEW UPPER STIFFENER AT APU INLET STATION 1088 PER AARD 51-10-05 AND EA B737-53-017012.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,733 hrs · 14,161 cycles

CRACK IN INTERCOSTAL UNDER CABIN FLOOR AT NUTCLIP HOLES STATIONS 344 TO 360 AT LEFT BODY LINE 11. REPLACED CRACKED INTERCOSTAL PER AARD 51-00-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,733 hrs · 14,161 cycles

CRACKED INTERCOSTAL UNDER CABIN FLOOR AT NUTCLIP HOLES STATIONS 344 TO 360 BUTTLINE 0. INSTALLED NEW INTERCOSTAL PER AARD 51-00-05-1.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,527 hrs · 11,857 cycles

LEFT AFT EXTERIOR EMERGENCY OVERWING LIGHT INOP. RELAMPED LEFT AFT OVERWING EMERGENCY LIGHT. OPS CHECK GOOD.

Part: PUMP — INOPERATIVE (NR 1 ENGINE) · airframe 27,916 hrs · 11,606 cycles

MIA - INFLIGHT PAP-FLL. SYSTEM A HYDRAULIC ENGINE LOW PRESS LIGHT ILLUMINATED. EMERGENCY DECLARED, LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER ONE ENGINE HYDRAULIC PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SUPPORT BRACKET — DAMAGED (CARGO DOOR) · airframe 27,769 hrs · 11,543 cycles

FORWARD CARGO CABLE PULLEY SUPPORT BRACKETS ON DOOR HOLES ELONGATED. INSTALLED 2 EACH NEW PULLEY SUPPORT CASTINGS PER SRM 51-10-02G.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,769 hrs · 11,543 cycles

INTERCOSTAL CRACKED STATION 328 TO 344 LEFT BODY LINE 48 INCHES. INSTALLED NEW INTERCOSTAL PER SRM 52-10-02G.

Part: PUMP — INOPERATIVE (ENGINE) · airframe 26,766 hrs · 11,118 cycles

LAS - INFLIGHT IAD-LAX - CREW REPORTED LOW PRESSURE LIGHTS FOR BOTH HYDRAULIC SYSTEMS CAME ON. EMERGENCY DECLARED, LANDED LAS WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. BOTH HYDRAULIC SYSTEM LOW PRESSURE LIGHTS ON. REPLACED RIGHT AND LEFT ENGINE DRIVEN HYDRAULIC PUMPS AND HYDRAULIC RESERVOIR PRESSURE MODULE MOD 7321124005. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,762 hrs

MIA - EMERGENCY LIGHT AT OVERHEAD SEAT 25C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT 25C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,762 hrs

MIA - EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHTS AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,762 hrs

MIA - EMERGENCY LIGHT AT OVERHEAD SEAT 5E INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,762 hrs

MIA - EMERGENCY LIGHT AT OVERHEAD SEAT 22C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,762 hrs

MIA - EMERGENCY LIGHT AT OVERHEAD SEAT 26D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COMPUTER — FAILED (FLT MANAGE) · airframe 23,173 hrs

MEX INFLIGHT T2114/02JAN - DURING CLIMB BOTH FLIGHT MANAGEMENT COMPUTERS FAILED. LANDED MEX WITHOUT INCIDENT. BOTH FLIGHT MANAGEMENT COMPUTERS WERE WORKING PRIOR TO ARRIVAL. REPLACED RIGHT AND LEFT FLIGHT MANAGEMENT COMPUTERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SENSOR — INOPERATIVE (RT OVERHEAT)

CUN INFLIGHT T2199/16OCT - DURING CLIMB-OUT RIGHT WING TO BODY OVERHEAT INDICATION ILLUMINATED. LANDED CUN WITHOUT INCIDENT. REPLACED SENSOR M1763. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR SLIDE INOPERATIVE. FOUND MISCONNECTION FOR DOOR EXIT IDENTIFIER. RECONNECTED WIRING FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

TUL - EMERGENCY LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

TUL - EMERGENCY LIGHT AT AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 21D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 21D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 14C INOPERATIVE. SECURED CONNECTOR AT SEAT 14C FOR INOPERATIVE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHTS AT SEAT ROW 14DEF INOPERATIVE. RELAMPED INOPERATIVE EMERGENCY LIGHTS AT SEAT ROW 14DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — FAILED (CABIN)

TUL- EMERGENCY LIGHT BATTERY PACKS IN CABIN FAILED TEST. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS ABOVE SEATS 8A AND 7D ON OVERHEAD BIN INOPERATIVE. REPLACED BATTERY PACK M01676 FOR EMERGENCY LIGHTS ABOVE SEATS 8A AND 7D ON OVERHEAD BIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — DEFECTIVE (NLG)

BOS - FLT 527 - EN ROUTE YUL-MIA, NOSE LANDING GEAR WOULD NOT RETRACT. DIVERTED BOS AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NOSE LANDING GEAR SHRADER VALVE. SYSTEM GROUND CHECKED NORMAL OPS. (M)