N969AN

Part: BONDING JUMPER — DISLODGED (ZONE 800) · airframe 67,836 hrs · 28,641 cycles

AIRCRAFT WAS NOT GROUNDED: AFT SERVICE DOOR EVACUATION SLIDE HAS A PIECE OF STRAP HANGING OUTSIDE THE COVER. RESECURED BONDING JUMPER ON AFT RIGHT SERVICE DOOR SLIDE PACK COVER. PER MM 25-66-01.

Part: FAN — CONTAMINATED (ZONE 100) · airframe 67,737 hrs · 28,592 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED STRONG ODOR ON TAKEOFF AND ON CLIMB OUT THAT SMELLED LIKE DIRTY SOCK. GOT BETTER IN CRUISE AND WORSE ON DESCENT. FOUND LEAKING GREY WATER HOSE ABOVE LEFT HAND RECIRCULATING FAN FILTER. REMOVE AND REPLACED HOSE (AALA202509256714), LEFT HAND RECIRCULATING FAN FILTER (AALA202509259393), AND INSULATION (AALA202509257830) UNDERNEATH. CLEANED AREA (AALA202509257742) AND RECIRCULATING FAN, PER AMM 21-25-01, AFMM 20-12-12. ACCOMPLISHED SOF TROUBLESHOOTING CARD 08L00021001. CONFIRMED NO SOF AFTER WORK ACCOMPLISHMENT.

Part: WIRE — LOOSE (ZONE 200) · airframe 67,737 hrs · 28,592 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHTING WIRING ON SEAT 20C LOOSE. RESTOWED EMERGENCY EXIT LIGHTING WIRING IN CLIPS ON SEAT 20C. PER AMM 33-51-11.

Part: INSULATION — CONTAMINATED (ZONE 100) · airframe 67,737 hrs · 28,592 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED STRONG ODOR ON TAKEOFF AND ON CLIMB OUT THAT SMELLED LIKE DIRTY SOCK. GOT BETTER IN CRUISE AND WORSE ON DESCENT. FOUND LEAKING GREY WATER HOSE ABOVE LEFT HAND RECIRCULATING FAN FILTER. REMOVE AND REPLACED HOSE (AALA202509256714), LEFT HAND RECIRCULATING FAN FILTER (AALA202509259393), AND INSULATION (AALA202509257830) UNDERNEATH. CLEANED AREA (AALA202509257742) AND RECIRCULATING FAN, PER AMM 21-25-01, AFMM 20-12-12. ACCOMPLISHED SOF TROUBLESHOOTING CARD 08L00021001. CONFIRMED NO SOF AFTER WORK ACCOMPLISHMENT.

Part: HOSE — LEAKING (ZONE 100) · airframe 67,737 hrs · 28,592 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED STRONG ODOR ON TAKEOFF AND ON CLIMB OUT, THAT SMELLED LIKE DIRTY SOCKS. GOT BETTER IN CRUISE AND WORSE ON DESCENT. FOUND LEAKING GREY WATER HOSE ABOVE LT RECIRCULATING FAN FILTER. REMOVE AND REPLACED HOSE (AALA202509256714), LT RECIRCULATING FAN FILTER (AALA202509259393), AND INSULATION (AALA202509257830 ) UNDERNEATH. CLEANED AREA (AALA202509257742) AND RECIRCULATING FAN, IAW AMM 21-25-01, & AFMM 20-12-12. ACCOMPLISHED SOF TROUBLESHOOTING CARD 08L00021001. CONFIRMED NO SOF AFTER WORK ACCOMPLISHMENT.

Part: AIR FILTER — CONTAMINATED (ZONE 100) · airframe 67,737 hrs · 28,592 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED STRONG ODOR ON TAKEOFF AND ON CLIMB OUT THAT SMELLED LIKE DIRTY SOCK. GOT BETTER IN CRUISE AND WORSE ON DESCENT. FOUND LEAKING GREY WATER HOSE ABOVE LEFT HAND RECIRCULATING FAN FILTER. REMOVE AND REPLACED HOSE (AALA202509256714), LEFT HAND RECIRCULATING FAN FILTER (AALA202509259393), AND INSULATION (AALA202509257830) UNDERNEATH. CLEANED AREA (AALA202509257742) AND RECIRCULATING FAN, PER AMM 21-25-01, AFMM 20-12-12. ACCOMPLISHED SOF TROUBLESHOOTING CARD 08L00021001. CONFIRMED NO SOF AFTER WORK ACCOMPLISHMENT.

Part: FLASHLIGHT — NOT SEATED (ZONE 200) · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: OUTBOARD FLASHLIGHT AT FLIGHT ATTENDANT 2L DOES NOT TEST. RESEATED FLASHLIGHT AT FLIGHT ATTENDANT SEAT 2L. OPERATIONAL CHECK GOOD.

Part: GIRT BAR — FRAYED (ZONE 800) · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 DOOR SLIDE GIRT IS FRAYED AND WORN. REPLACED R1 DOOR SLIDE. PER 08L22125001.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER UPPER ATTACH ANGLE AT STA 663, LBL 8. REPAIRED PER SRM 57-10-10-2R-5.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER UPPER ATTACH ANGLE AT STA 663, RBL 8. REPAIRED PER SRM 57-10-10-2R-5.

Part: ANGLE — CORRODED (ZONE 200) · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR LOWER SILL INNER CHORD (CREASE ANGLE) AT BS 303.9, LBL 48. REPLACED CHORD PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT BS 291, BL 0. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER S23L CHORD AT BS 338. REPAIRED CHORD PER EA 365282.

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT BRACKET AT BS 847, S24R. REPLACED BRACKET PER AARD 51-00--05-1.

Part: RAIL — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT AFT BULKHEAD LOWER LOBE RAIL ASSEMBLY AT BS 500I, LBL 20. REPLACED RAIL ASSEMBLY PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,008 hrs · 28,249 cycles

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

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM BS 500D TO BS 500E PLUS 10 INCHES, AT RBL 24. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD (T-CAP) AT STA 947, FROM LBL 15 TO RBL 15. REPAIRED UPPER CHORD PER SRM 53-70-51-2R-5.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM BS 956 TO BS 959 AT LBL 50. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD AT STA 986.5, RBL 53. REPAIRED CHORD PER SRM 53-70-51-2R-6.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR LOWER SILL INNER CHORD (CREASE ANGLE) FROM BS 308 TO BS 320 AT LBL 52. REPLACED CHORD PER AARD 51-00-05-1.

Part: TIE DOWN — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR FLOOR MOUNTED AFT GIRT BAR TIEDOWN AT BS 344, LBL 59. REPLACED TIEDOWN PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM BS 490 TO BS 500B PLUS 12 INCHES, AT LBL 24. REPLACED TRANSITION PANEL PER AARD 51-00-05-1

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN FLOOR STRUCTURE INTERCOSTAL FROM BS 956 TO BS 959 AT RBL 50 REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: TIE DOWN — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,008 hrs · 28,249 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR FLOOR MOUNTED FORWARD GIRT BAR TIEDOWN AT BS 312, LBL 55. REPLACED TIEDOWN PER AARD 51-00-05-1.

Part: PRESSURE SWITCH — FAULTY (ZONE 500 FUEL) · airframe 66,206 hrs · 27,875 cycles

AIRCRAFT WAS NOT GROUNDED: NUMBER 1 AFT FUEL PUMP LOW PRESSURE LIGHT DOES NOT TURN ON WITH THE PUMP OFF. VERIFIED FAULTY SWITCH; REMOVE AND REPLACED NUMBER 1 AFT LEFT FUEL BOOST PUMP PRESSURE SWITCH. PER AMM 28-42-11. OPERTIONAL TEST GOOD. LOW PRESS LIGHT ILLUMINATES ON OFF. NO LEAKS DETECTED.

Part: LIGHT — MISSING (ZONE 200) · airframe 66,135 hrs · 27,848 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT AT 19ABC BROKEN AND MISSING. INSTALLED FLOOR PROXIMITY LIGHT ASSEMBLY AT ROW 19ABC, OPERTIONAL CHECK GOOD. PER AMM 33-51-11.

Part: BATTERY — FAULTED (ZONE 200 FLSHLIT) · airframe 65,843 hrs · 27,711 cycles

AIRCRAFT WAS NOT GROUNDED: NEED NEW FWD FA FLASHLIGHT. STATUS LIGHT FLASHING RED. REPLACED 1L DOOR JUMPSEAT FLASHLIGHT BATTERY.

Part: FITTING — CRACKED (ZONE 200) · airframe 64,679 hrs · 27,142 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 64,679 hrs · 27,142 cycles

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

Part: FITTING — CRACKED (ZONE 100) · airframe 64,679 hrs · 27,142 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 64,679 hrs · 27,142 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 64,679 hrs · 27,142 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 64,679 hrs · 27,142 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 64,679 hrs · 27,142 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 64,679 hrs · 27,142 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 64,679 hrs · 27,142 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 64,679 hrs · 27,142 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: LIGHT — UNSECURE (SEAT 13ABC) · airframe 64,632 hrs · 27,118 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 13ABC SEAT EMERGENCY LIGHTING MODULE LOOSE. RESECURED EMERGENCY LIGHT MODULE ASSEMBLY AT ROW 13ABC. PER AMM 33-51-11.

Part: HINGE — BROKEN (LAVATORY DOOR) · airframe 64,473 hrs · 27,033 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR GETS STUCK. PASSENGERS ARE HAVING A DIFFICULT TIME OPENING AND CLOSING THE DOOR.**SUPPLEMENTAL REPORT FOR (AALA202405291255): REPLACED FORWARD LAVATORY DOOR HINGE. PER CMM 25-45-46**(CLOSED).

Part: DOOR — BINDING (LAVATORY) · airframe 64,473 hrs · 27,033 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR GETS STUCK. PASSENGERS ARE HAVING A DIFFICULT TIME OPENING AND CLOSING THE DOOR. (OPEN).

Part: OVEN — SHORTED (FWD GALLEY NR 2) · airframe 64,299 hrs · 26,944 cycles

AIRCRAFT WAS NOT GROUNDED: CIRCUIT BREAKER FOR THE OVEN NUMBER 2 IN THE FORWARD GALLEY POPPED AND FLIGHT ATTENDANTS REPORTED SMELLING FUMES. REMOVED AND REPLACED NUMBER 2 OVEN. PER AMM 25-32-03.

Part: MOUNT — DISLODGED (WIRE HARNESS) · airframe 64,184 hrs · 26,866 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT WIRING HANGING FROM 12C. REPLACED MOUNT ASSEMBLY. OPERTIONAL CHECK NORMAL. PER GPM 02.01.2.

Part: LIGHT — DETACHED (SEAT ROW 21C) · airframe 64,118 hrs · 26,832 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT IN AISLE 21C FELL OFF. **SUPPLEMENTAL REPORT FOR (AALA202404011828): REMOVE AND REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSYMBLY. FUNCATIONAL CHECK GOOD. PER AMM REF 33-51-11**(CLOSED).

Part: LIGHT — DETACHED (SEAT ROW 21C) · airframe 64,118 hrs · 26,832 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT IN AISLE 21C FELL OFF. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: TUBE — MISSING (GIRT BAR) · airframe 63,131 hrs · 26,390 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT DOOR GIRT BAR IS MISSING RED SAFETY TAB.**SUPPLEMENTAL REPORT FOR (AALA202311295230): INSTALLED NEW RED GIRT BAR TUBING AS PER REF AARD 25-66-00-4. OK FOR SERVICE.**(CLOSED).

Part: UNKNOWN — MISSING (ZONE 800 - DOORS) · airframe 63,131 hrs · 26,390 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT DOOR GIRT BAR IS MISSING RED SAFETY TAB. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: WIRE — LOOSE (ZONE 200 - FUSE) · airframe 63,006 hrs · 26,336 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTS HAS LOOSE WIRES HANGING UNDERNEATH SEAT 13C. SECURED LOOSE WIRES HANGING UNDERNEATH SEAT 13C FOR EMERGENCY LIGHTS, OPERATIONAL CHECK GOOD. PER AMM 33-51-00.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 61,855 hrs · 25,754 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD MEGAPHONE IN COMPARTMENT 302 IS INOPERABLE. REPLACED MEGAPHONE BATTERIES.

Part: BRACKET — LOOSE (ZONE 800 - DOORS) · airframe 61,254 hrs · 25,457 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT ENTRY DOOR BOLT LOOSE ON SLIDE PACK. REMOVED AND REPLACED AFT LEFT ENTRY DOOR SLIDE MOUNTING BRACKET.

Part: FILTER — INOPERATIVE (ZONE 100 - FUSE) · airframe 61,206 hrs · 25,439 cycles

AIRCRAFT WAS GROUNDED: SYSTEM A AND B QUANTITY 80 PERCENT IN CRUISE. 1 HOUR LATER SPLIT 64/104. 1 HOUR LATER SYSTEM B STARTED DROPPING 1/10 MIN 70 PERCENT WENT TO 0 PERCENT IN 1 MINUTE SYSTEM B PRESSURE NORMAL UNTIL FLAPS EXTENDED. REMOVED AND REPLACED ELEVATOR FEEL COMPUTER FILTER.

Part: GIRT BAR — WORN (R1 DOOR SLIDE) · airframe 60,937 hrs · 25,312 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 SERVICE DOOR SLIDE PACK GIRT ASSEMBLY WORN. REPLACED SLIDE PER JOB CARD 08L22125001.

Part: GIRT BAR — WORN (L2 DOOR SLIDE) · airframe 60,937 hrs · 25,312 cycles

AIRCRAFT IN BASE MAINTENANCE: L2 ENTRY DOOR SLIDE PACK GIRT ASSEMBLY WORN. REPLACED SLIDE PER JOB CARD 08L22125001.

Part: GIRT BAR — WORN (L1 DOOR SLIDE) · airframe 60,937 hrs · 25,312 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 ENTRY DOOR SLIDE PACK GIRT ASSEMBLY WORN. REPLACED SLIDE PER JOB CARD 08L22125001.

Part: NONE — NONE (NONE) · airframe 60,938 hrs · 25,312 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING INSPECTION MAINTENANCE FOUND AN EXISTING UNDOCUMENTED FUSELAGE SKIN PANEL REPAIR LOCATED BETWEEN BS 500B AND BS 500C, AND BETWEEN S1R AND S3R. DOUBLER REPAIR INSPECTED PER SRM 53-00-01-2R PROCEDURE 3 REPAIR 3.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 60,938 hrs · 25,312 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON INSPAR TRANSVERSAL RIB 2 LOCATED AT LEVEL STA 92.70 LEFT STABILIZER HORIZONTAL. LENGTH IS 0.380 INCHES. PERFORMED PERMANENT SPLICE REPAIR PER SRM.

Part: CABIN AIR SYS — ODOR · airframe 60,862 hrs · 25,276 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT SMELLED SMOKE IN BACK OF AIRCRAFT ON TAKEOFF. DID NOT SEE SMOKE OR FIRE. EMERGENCY DECLARED. FLIGHT DIVERTED TO IAD LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202212099254: MAINTENANCE ACCOMPLISHED SMOKE ODOR FUME TROUBLESHOOTING JOB CARD 08L00021001. NO FINDINGS. AIRCRAFT RETURNED TO SERVICE.** (CLOSED)

Part: UNKNOWN — ODOR (CABIN) · airframe 60,862 hrs · 25,276 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT SMELLED SMOKE IN BACK OF AIRCRAFT ON TAKEOFF. DID NOT SEE SMOKE OR FIRE. EMERGENCY DECLARED. FLIGHT DIVERTED TO IAD LANDING SAFELY. (OPEN)

Part: SKIN — CORRODED (BS 968-1016) · airframe 60,846 hrs · 25,266 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SKIN PANEL AROUND AFT DRAIN MAST LOCATED BETWEEN BS 968.5 AND BS 1016, AND BETWEEN S24L AND S25L. REPAIRED SKIN PANEL PER EA 328200 AND SRM 51-40-02-0G.

Part: DOOR — OUT OF ADJUST (FWD LAVATORY) · airframe 60,620 hrs · 25,156 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN / LOCK. ADJUSTED FORWARD LAVATORY DOOR.

Part: GIRT BAR — LOOSE (ZONE 800 - DOORS) · airframe 59,998 hrs · 24,851 cycles

AIRCRAFT WAS NOT GROUNDED: L1 GIRT-BAR LOOSE. ADJUSTED L1 DOOR GIRT-BAR TO CORRECT TENSION IN ACCORDANCE WITH AMM 25-66-01.

Part: LIGHT — UNSECURE (ZONE 200 - FUSE) · airframe 59,885 hrs · 24,799 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 31C ESCAPE PATH LIGHT HANGING DOWN. REPLACED SEAT PLASTIC HOLDING ESCAPE LIGHT AT SEAT 31C.

Part: LIGHT — UNSECURE (ZONE 200 - FUSE) · airframe 59,693 hrs · 24,715 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY ESCAPE PATH LIGHT AT SEAT 31C INOPERATIVE. SECURED LIGHT BASE. OPERATIONAL CHECK GOOD PER AMM 33-51-11.

Part: LIGHT — UNSECURE (ZONE 200 - FUSE) · airframe 59,622 hrs · 24,678 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED ESCAPE PATH LIGHTING HOUSING NOT SECURE AT SEAT 28C. REMOVED AND REPLACED SEAT MOUNTED ESCAPE PATH LIGHTING HOUSING PER AMM 33-51-11.

Part: COVER — LOOSE (ZONE 200 - FUSE) · airframe 58,880 hrs · 24,331 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 26C EMERGENCY LIGHT COVER LOOSE. LIGHT COVER SCREW TIGHTEN PER AMM 33-51-00 OPERATIONAL CHECK NORMAL.

Part: NONE — UNSECURE (ZONE 900 - LAV/G) · airframe 58,838 hrs · 24,310 cycles

AIRCRAFT WAS NOT GROUNDED: FIRST CLASS LAVATORY DOOR STICKS. SECURED BOTTOM DOOR TRIM. OPERATIONAL CHECK GOOD.

Part: GUST LOCK — DAMAGED (ZONE 800 - DOORS) · airframe 58,526 hrs · 24,167 cycles

AIRCRAFT WAS GROUNDED: L1 DOOR LIFTED UP BY JET-BRIDGE WHILE IN OPEN POSITION. REMOVED AND REPLACED L1 DOOR GUST LOCK ASSEMBLY PER AMM 52-11-21.

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 58,115 hrs · 23,977 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT ASSEMBLY FELL DOWN HANGING BY WIRING AT SEAT 19C. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT ASSEMBLY AT ROW 19C PER AMM 33-51-11.

Part: PRESSURE SWITCH — FAULTY (ZONE 300 - STABS) · airframe 57,848 hrs · 23,854 cycles

AIRCRAFT WAS GROUNDED: AT FL360 APU SHUT DOWN A COUPLE OF TIMES AND RESTARTED NORMALLY. APU SHUTDOWN AGAIN. FLIGHT DIVERTED TO DEN, LANDING SAFELY. REPLACED APU OIL PRESSURE SWITCH PER AMM 49-94-22.

Part: DOOR — NONE (ZONE 800 - DOORS) · airframe 57,709 hrs · 23,791 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN/CLOSE. CLEANED AND LUBRICATED FIRST CLASS LAVATORY DOOR OPERATIONS CHECKS GOOD. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 57,514 hrs · 23,698 cycles

AIRCRAFT WAS GROUNDED: ROW 29 EMERGENCY EXIT LIGHT COVER IS DETACHED AND HANGING DOWN. INSTALLED SERVICEABLE EMERGENCY LIGHT ASSEMBLY AT PASSENGER SEAT ROW 29.

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 900 - LAV/G) · airframe 57,495 hrs · 23,690 cycles

AIRCRAFT WAS NOT GROUNDED: FWD LAVATORY SMOKE LIGHT ILLUMINATED AT CRUISE FOR APPROXIMATELY 60 SECONDS, THEN EXTINGUISHED; NO SMOKE OR DETECTOR TAMPERING PRESENT. ACCOMPLISHED A FUNCTIONAL TEST OF THE SMOKE DETECTOR IAW AMM 26-14-00, OPS CHECK GOOD.

Part: PIN — OUT OF POSITION (ZONE 200 - FUSE) · airframe 57,482 hrs · 23,684 cycles

AIRCRAFT WAS NOT GROUNDED: CEILING EMERGENCY LIGHT BY ROW 32 DEF INOPERATIVE. FOUND CONNECTOR D11321 INCORRECTLY PINNED. REPINNED CONNECTOR D11321.

Part: STOP PIN — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 57,450 hrs · 23,669 cycles

AIRCRAFT WAS GROUNDED: L1 DOOR DIFFICULT TO CLOSE. ADJUSTED STOP PIN IAW AMM 52-11-00, OPS CHECK GOOD.

Part: GIRT BAR — LOOSE (RT FWD) · airframe 57,154 hrs · 23,530 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT FORWARD ENTRY DOOR GIRT BAR LOOSE. ADJUSTED GIRT BAR RETAINER PER AMM 25-61-01.

Part: RELAY — INOPERATIVE (CABIN PRESSURE) · airframe 56,786 hrs · 23,362 cycles

AIRCRAFT WAS NOT GROUNDED: PRESSURIZATION PANEL AUTO FAIL AND ALTERNATE LIGHT ILLUMINATED WITH CONTROL SWITCH IN AUTO. FLIGHT DECLARED EMERGENCY. WAS NOT OVERWEIGHT FOR LANDING. REMOVED AND REPLACED RELAYS 556, 557 (AALA202106149024), 558 (AALA202106149025) PER SSM 21-31-23 ESPM CH 20 CABIN PRESSURE SYSTEM CHECK NORMAL PER AMM 21-31-00.

Part: RELAY — INOPERATIVE (CABIN PRESSURE) · airframe 56,786 hrs · 23,362 cycles

AIRCRAFT WAS NOT GROUNDED: PRESSURIZATION PANEL AUTO FAIL AND ALTERNATE LIGHT ILLUMINATED WITH CONTROL SWITCH IN AUTO. FLIGHT DECLARED EMERGENCY. WAS NOT OVERWEIGHT FOR LANDING. REMOVED AND REPLACED RELAYS 556 (AALA202106149013), 557 (AALA202106149024), 558 PER SSM 21-31-23 ESPM CH 20 CABIN PRESSURE SYSTEM CHECK NORMAL PER AMM 21-31-00.

Part: RELAY — INOPERATIVE (CABIN PRESSURE) · airframe 56,786 hrs · 23,362 cycles

AIRCRAFT WAS NOT GROUNDED: PRESSURIZATION PANEL AUTO FAIL AND ALTERNATE LIGHT ILLUMINATED WITH CONTROL SWITCH IN AUTO. FLIGHT DECLARED EMERGENCY. WAS NOT OVERWEIGHT FOR LANDING. REMOVED AND REPLACED RELAYS 556 (AALA202106149013), 557, 558(AALA202106149025) PER SSM 21-31-23 ESPM CH 20 CABIN PRESSURE SYSTEM CHECK NORMAL PER AMM 21-31-00.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 56,727 hrs · 23,341 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 DOOR EXIT SIGN INOPERATIVE. RESEATED CONNECTOR D40042P IAW B737NG AMM 33-51-00, OPS CHECK GOOD.

Part: CONNECTOR — OUT OF POSITION (EMERGENCY LIGHTS) · airframe 56,727 hrs · 23,341 cycles

AIRCRAFT IN BASE MAINTENANCE: OVER WING RIGHT AFT EXIT DOOR EXIT SIGN INOPERATIVE. TROUBLESHOT SYSTEM FOUND OVER WING EXIT CONNECTORS SWAPPED. RECONNECTED CONNECTORS PER B737NG WDM33-51-14.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 56,727 hrs · 23,341 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHTING CONNECTOR D11100 DAMAGED ON TOP OF BIN 19/20 ABC. REPLACED CONNECTOR PER SWPM 20-61-00.

Part: CHARGER — DAMAGED (EMERGENCY LIGHTS) · airframe 56,727 hrs · 23,341 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY M1695 MISSING TEST BUTTON. REPLACED EMERGENCY BATTERY CHARGER IAW B737-NG AMM 33-51-06, OPS CHECK GOOD.

Part: MEGAPHONE — DAMAGED (CABIN) · airframe 56,727 hrs · 23,341 cycles

AIRCRAFT IN BASE MAINTENANCE: MEGAPHONES FOUND TO BE MISSING HARDWARE. REPLACED MEGAPHONES IN G7 AND L17 BIN IAW AMM 25-64-00.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 56,727 hrs · 23,341 cycles

AIRCRAFT IN BASE MAINTENANCE: SIDEWALL PANEL L11 EMERGENCY EXIT LIGHT LENS HAS BROKEN TAB. REPLACED SIDEWALL L11 EMERGENCY EXIT LIGHT LENS ASSEMBLY IAW B737 AMM 33-51-01, OPS CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (LAVATORY) · airframe 55,919 hrs · 22,941 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY SMOKE LIGHT CAME ON IN COCKPIT AND BEEPER CAME ON IN FORWARD LAVATORY, DURING CRUISE. ALL INDICATIONS WENT OUT, CEASED, WITHIN ABOUT 10 SECONDS. NO SMELL, HEAT, OR SMOKE PRESENT IN FORWARD LAVATORY. MAINTENANCE PERFORMED SATISFACTORY OPERATIONAL CHECK OF SMOKE DETECTOR PER AMM 26-14-00.

Part: FRAME — CRACKED (BS 727D-727E) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FITTING BETWEEN BS 727D AND BS 727E, BETWEEN S8R AND S9R. REPAIRED FRAME PER EA 296947.

Part: BAFFLE — CRACKED (BS 500F-500G) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FORWARD CARGO COMPARTMENT BAFFLE BETWEEN BS 500F AND BS 500G AND LBL 25. REPLACED BAFFLE PER AARD 51-00-05.

Part: ATTACH BRACKET — CRACKED (BS 887) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED LOWER HORIZONTAL LEFT ANGLE, AFT PANEL ATTACH BRACKET CRACKED AT FR 887, LBL 15. REPLACED ATTACH BRACKET PER BOEING DRAWING 143A5240 AND AARD 51-00-05 AND SRM 51-40-02.

Part: TRANSITION PANEL — CRACKED (BS 747) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND TRANSITION PANEL AROUND FASTENER HOLE AT FR 747, LBL 20. REPLACED ATTACH BRACKET PER BOEING DRAWING 146A7502-31, PER IPC 53-42-11-26A.

Part: WEB — CORRODED (BS 1006) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA FLOOR "K" WEB AT BS 1006 AND RBL 45. REPLACED WEB IAW 51-00-05-1.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND HORIZONTAL STABILIZER RIB AT STATION 92.70. REPAIRED RIB PER SRM 55-10-09-2R-5.

Part: TRANSITION PANEL — CORRODED (BS 727I) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL, BS 727I, RBL -20, AT S-25R. REPLACED TRANSITION PANEL PER AARD AARD 51-00-05-1.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND HORIZONTAL STABILIZER SECOND RIB VERTICAL STIFFENER AT STATION 92.70. REPAIRED RIB PER SRM 55-10-09-2R-4.

Part: SEAT TRACK — WORN (BS 517-518) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: WORN SEAT TRACK BETWEEN BS 514 AND BS 518 AT RBL 45. REPLACED SEAT TRACK PER EA 297065 AND SRM 53-00-52-1A.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLOOR BOARD SUPPORT AT FR 540, RBL -2. REPLACED FLOOR BOARD SUPPORT PER BOEING DRAWING 143A5240 AND AARD 51-00-05 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLOOR BOARD SUPPORT AT FR 540, LBL 2. REPLACED FLOOR BOARD SUPPORT PER BOEING DRAWING 143A5240 AND AARD 51-00-05 AND SRM 51-40-02.

Part: SEAT TRACK — WORN (BS 515-516) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: WORN SEAT TRACK BETWEEN BS 515 AND BS 516 AT LBL 45. REPLACED SEAT TRACK PER AARD 51-00-05-1.

Part: SUPPORT FRAME — CORRODED (BS 695) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SUPPORT FRAME AT BS 695 AND RBL 70. REPLACED SUPPORT FRAME PER 51-00-05-1.

Part: SUPPORT FRAME — CORRODED (BS 695) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SUPPORT FRAME AT BS 695 AND RBL 70. REPLACED SUPPORT FRAME PER AARD 51-00-01.

Part: TRANSITION PANEL — CORRODED (BS 727J) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL, BS 727J+2, RBL -20, AT S-25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727J) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL, BS 727J+18, RBL -20, AT S-25R. REPLACED TRANSITION PANEL PER AARD AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727I) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL, BS 727I+16, RBL -20, AT S-25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: SHIELD — CORRODED (BS 782) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION SHIELD AT BS 782 AND RBL 21. REPLACED TRANSITION SHIELD PER AARD 51-00-05.

Part: TRANSITION PANEL — CORRODED (BS 727J) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL, BS 727J+5, RBL -20, AT S-25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 775) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 775, LBL 20, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 770) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 780, LBL 20, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727I) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL, BS 727I+8, RBL -20, AT S-25R. REPLACED TRANSITION PANEL PER 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727I) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 727I+14.5, LBL 21, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 802) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 802, LBL 20, AT S26L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727D) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 727D+8, LBL 21, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: SHIELD — CORRODED (BS 792) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION SHIELD, BS 792, RBL -20, AT S-25R. REPLACED TRANSITION SHIELD PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 770) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 770, LBL 21, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 775) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 775, LBL 21, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727J) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL BS 727J+8, RBL-20, S-25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 767) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL, BS 767, RBL -20, AT S-25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727I) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 727I+8, LBL 20, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 755) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL, BS 755.5, RBL -20, AT S-25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 765) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL, BS 765, RBL -20, AT S-25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 770) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 770, LBL 20, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 752) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL, BS 752, RBL -20, AT S-25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 759) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 759, LBL 20, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727C) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 727C+16, LBL 21, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727I) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 727I+8, LBL 21, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 759) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL, BS 759, RBL -20, AT S-25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727J) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL BS 727J+15, RBL-20, S-25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727I) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 727I+6.5, LBL 21, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 761) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 761, LBL 20, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 783) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 783, LBL 20, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 763) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL, BS 763, RBL -20, AT S-25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 766) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 766, LBL 20, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727J) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 727J+10, LBL 21, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 787) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 787, LBL 20, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727J) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 727J+12, LBL 21, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727J) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 727J+11.5, LBL 20, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 747) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 747, LBL 20, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 748) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL, BS 748.5, RBL -20, AT S-25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 778) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 778, LBL 21, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727D) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 727D+4, LBL 21, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727J) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL, BS 727J+12, RBL -20, AT S-25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 777) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 777, LBL 20, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL, BS 727+4, LBL 21, AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: SHIELD — CORRODED (BS 775) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION SHIELD, BS 775, RBL -20, AT S-25R. REPLACED TRANSITION SHIELD PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 500G-500H) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT LEFT HAND TRANSITION PANEL FROM BS 500G TO BS 500H, S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 500B-500C) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT LEFT HAND TRANSITION PANEL FROM BS 500B TO BS 500C, S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 500C-500D) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT LEFT HAND TRANSITION PANEL FROM BS 500C TO BS 500D, LBL25. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: WEB — CORRODED (BS 831) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO DOOR CUT OUT LOWER THRESHOLD WEB AT BS 831 AND RBL 25. REPLACED THRESHOLD WEB PER SRM 51-10-02-0G.

Part: TRANSITION PANEL — CORRODED (BS 500F-500G) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL FROM BS 500F TO BS 500G, S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 500E-500R) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT LEFT HAND TRANSITION PANEL FROM BS 500E TO BS 500F, S25L. REPLACED TRANSITION PANEL PER 51-00-05-1.

Part: WEB — CORRODED (BS 807-827) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO DOOR THRESHOLD WEB BETWEEN BS 807 AND BS 827 AT RBL25. REPLACED THRESHOLD WEB PER SRM 51-40-02-0G.

Part: TRANSITION PANEL — CORRODED (BS 492-500) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL FROM BS 492 TO BS 500, -S25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: WEB — CORRODED (BS 800) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO DOOR CUT OUT LOWER THRESHOLD WEB AT BS 800 AND RBL 25. REPLACED THRESHOLD WEB PER SRM 51-10-02-0G.

Part: TRANSITION PANEL — CORRODED (BS 500D-500E) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT LEFT HAND TRANSITION PANEL FROM BS 500D TO BS 500E, S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 500H-500I) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT LEFT HAND TRANSITION PANEL FROM BS 500H TO BS 500I, S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (BS 927-947) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA FLOOR INTERCOSTAL BETWEEN BS 927 AND BS 947 AT LBL 52. REPLACED INTERCOSTAL PER AARD 51-00-05-1

Part: FLOOR SUPPORT — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA INTERCOSTAL AT BS 951 AND RBL 50. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: SUPPORT ANGLE — CORRODED (BS 329) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R1 DOOR SCUFF PLATE SUPPORT ANGLE AT BS 329 AND RBL 55. REPLACED SUPPORT ANGLE PER 51-00-05-1.

Part: ANGLE — CORRODED (BS 321) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R1 DOOR CUT OUT CREASE ANGLE AT BS 321 AND RBL 55. REPLACED CREASE ANGLE PER 51-00-05-1

Part: ANGLE — CORRODED (BS 312) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R1 DOOR CUT OUT CREASE ANGLE AT BS 312 AND RBL 55. REPLACED CREASE ANGLE PER 51-00-05-1.

Part: WEB — CORRODED (BS 987-991) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA FLOOR "K" WEB BETWEEN BS 987 AND BS 991 AT LBL 37. REPLACED WEB PER AARD 51-00-05-1.

Part: ANGLE — CORRODED (BS 939-998) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CREASE ANGLE BETWEEN BS 939 AND BS 998, BETWEEN LBL 46 AND LBL 57. REPLACED CREASE ANGLE PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL AT FR 312 TO FR 328, LBL 45. REPLACED INTERCOSTAL PER BOEING DRAWING #141A5410-141 AND AARD 51-00-05 AND SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 987) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA FLOOR BEAM UPPER FLANGE AT BS 987 BETWEEN RBL 22 AND RBL 44. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-4.

Part: SUPPORT FRAME — CORRODED (BS 951) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA SUPPORT FRAME AT BS 951 AND LBL 25. REPLACED SUPPORT FRAME PER 51-00-05-1.

Part: SUPPORT ANGLE — CORRODED (BS 992-1016) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA FLOOR SUPPORT ANGLE BETWEEN BS 992 AND 1016 AT RBL 37. REPLACED SUPPORT ANGLE PER AARD 51-00-05-1.

Part: WEB — CORRODED (BS 1007) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON WEB AT BS 1007 AND LBL 32. REPLACED WEB PER 51-00-05-1.

Part: SUPPORT FRAME — CORRODED (BS 949-971) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA SUPPORT FRAME BETWEEN BS 949 AND BS 971 AT LBL 50. REPLACED SUPPORT FRAME PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (BS 951) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA INTERCOSTAL AT BS 951 AND RBL 25. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL AT FR 328 TO FR 344, LBL 45. REPLACED INTERCOSTAL PER BOEING DRAWING #141A5410-141 AND 51-00-05 AND SRM 51-40-02.

Part: ANGLE — CORRODED (BS 325) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENNACE: CORROSION ON R1 DOOR CUT OUT CREASE ANGLE AT BS 325 AND RBL 55. REPLACED CREASE ANGLE PER 51-00-05-1.

Part: FLOORBEAM — CORRODED (987) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA FLOOR BEAM AT BS 987 BETWEEN LBL 43 AND RBL 43. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-4.

Part: ANGLE — CORRODED (BS 947.5-997.5) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CREASE ANGLE BETWEEN BS 947.5 AND BS 997, BETWEEN RBL 46 AND RBL 56. REPLACED CREASE ANGLE PER AARD 51-00-05-1.

Part: FLOORBEAM — CORRODED (BS 994) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA FLOOR SUPPORT ANGLE AT BS 994 BETWEEN LBL 39 AND LBL 51. REPLACED SUPPORT ANGLE PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL AT FR 328 TO FR 344, RBL -45. REPLACED INTERCOSTAL PER BOEING DRAWING #141A5410-141 AND AARD 51-00-05 AND SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (BS 992) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA FLOOR SUPPORT ANGLE AT BS 992 AND LBL 37. REPLACED SUPPORT ANGLE PER AARD 51-00-05-1.

Part: ANGLE — CORRODED (BS 344) · corrosion level 2 · airframe 54,526 hrs · 22,305 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R1 DOOR CUT OUT CREASE ANGLE AT BS 344 AND RBL 55. REPLACED CREASE ANGLE PER 51-00-05-1.

Part: CONNECTOR — ARCED (HYD PUMP) · airframe 53,389 hrs · 21,793 cycles

MAINTENANCE DISCOVERED EVIDENCE OF ARCING IN ONE PIN RECEPTICAL ON THE -B- SYSTEM ELECTRIC PUMP ELECTRICAL CONNECTOR ON THE RT FWD WHEEL WELL BULKHEAD. REPLACED THE CONNECTOR IAW WDM 29-11-12 AND SWPM 20-61-11.

Part: ROD END — BROKEN (L1 DOOR) · airframe 52,211 hrs · 21,261 cycles

ON OPENING THE L1 DOOR, TOP GUST LOCK BRACKET BOLT SEVERED AT THE EYE BOLT. THE DOOR WAS HALFWAY THROUGH ROTATION WHEN A POP WAS HEARD. VERIFIED THE L1 DOOR CLOSED AND LOCKED. THE AIRCRAFT WAS GROUNDED. REPLACED THE ROD END AND ADJUSTED THE NUT ON THE L1 DOOR GUIDE ARM IAW MM 52-11-21. ADJUSTED GUIDE ARM IAW MM 52-11-00. OPS CHECKED GOOD.

Part: DOOR — OUT OF ADJUST (R1) · airframe 52,211 hrs · 21,261 cycles

AIRCRAFT WAS NOT GROUNDED: R1 SERVICE DOOR HARD TO CLOSE, HAD TO PUSH ON UPPER AFT CORNER TO CLOSE DOOR AND HAD SOFT LATCH ISSUE ON DOOR HANDLE (SEE AALA201810129029). MAINTENANCE ADJUSTED R1 SERVICE DOOR GUIDE ARM PER MM 52-41-00 AND ADJUSTED R1 GALLEY SERVICE DOOR FOR SOFT UNLATCHING AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: GUIDE ARM — OUT OF ADJUST (R1 DOOR) · airframe 52,211 hrs · 21,261 cycles

AIRCRAFT WAS NOT GROUNDED: R1 SERVICE DOOR HARD TO CLOSE, HAD TO PUSH ON UPPER AFT CORNER TO CLOSE DOOR (SEE AALA201810129024) AND HAD SOFT LATCH ISSUE ON DOOR HANDLE. MAINTENANCE ADJUSTED R1 SERVICE DOOR GUIDE ARM PER MM 52-41-00 AND ADJUSTED R1 GALLEY SERVICE DOOR FOR SOFT UNLATCHING AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — DAMAGED (CABIN) · airframe 50,878 hrs · 20,686 cycles

THE AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT LENS OFF IN FORWARD GALLEY. FOUND LENS AND LIGHT ASSEMBLY DAMAGED. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONS CHECK GOOD PER MM 33-00-00.

Part: SHADE — BROKEN (CABIN) · airframe 50,675 hrs · 20,594 cycles

AIRCRAFT WAS NOT GROUNDED. WINDOW SHADE AT EMERGENCY EXIT SEAT 14F IS BROKEN. WINDOW SHADE EMERGENCY EXIT SEAT 14F WAS REPLACED PER IAW AMM 25-21-12-400-802. OK FOR SERVICE.

Part: BRACKET — OUT OF ADJUST (ZONE 800) · airframe 50,367 hrs · 20,460 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD ENTRY GIRT BAR IS LOOSE. ADJUSTED GIRT BAR BRACKET PER MM 52-11-00.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR SLIDE) · airframe 50,290 hrs · 20,430 cycles

L1 DOOR GIRT BAR OUT OF ADJUSTMENT, HAS TO MUCH SLACK. MAINTENANCE ADJUSTED THE L1 GIRT BAR AND PERFORMED SATISFACTORY OPS CHECK IAW MM 25-66-01.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 48,842 hrs · 19,812 cycles

CRACKS THE BULKHEAD WEB AT BS 663, RBL 25 TO RBL 46. REPAIRED IAW SRM 57-10-10-2R-3 ALTERNATIVE 2.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 48,842 hrs · 19,812 cycles

CRACKS ON BULKHEAD WEB AT BS 663, LBL 25 TO LBL 46. REPAIRED IAW SRM 57-10-10-2R-3 ALTERNATIVE 2.

Part: SIGN — DISLODGED (EMERGENCY LIGHTS) · airframe 48,789 hrs · 19,791 cycles

RIGHT REAR CABIN SERVICE DOOR EMERGENCY EXIT SIGN DISLODGED FROM DOOR. INSTALLED A NEW EXIT SIGN ASSY IAW AMM 33-51-01. OPS CHECKED OK.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 47,706 hrs · 19,310 cycles

AIRCRAFT WAS GROUNDED. DURING CRUISE WITH ALL FUEL PUMPS ON, THE RIGHT MAIN WENT TO 1000 LBS OUT OF BALANCE. REMOVED AND REPLACED RIGHT CENTER FUEL BOOST PUMP IAW AMM 28-22-41 AND ENGINE CROSSFEED VALVE IAW AMM 28-22-21(AALA20170124015). LEAK AND OPERATIONAL CHECK GOOD.

Part: VALVE — FAULTY (FUEL SYSTEM) · airframe 47,706 hrs · 19,310 cycles

AIRCRAFT WAS GROUNDED. DURING CRUISE WITH ALL FUEL PUMPS ON, THE RIGHT MAIN WENT TO 1000 LBS OUT OF BALANCE. REMOVED AND REPLACED RIGHT CENTER FUEL BOOST PUMP IAW AMM 28-22-41(AALA20170124014) AND ENGINE CROSSFEED VALVE IAW AMM 28-22-21. LEAK AND OPERATIONAL CHECK GOOD.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 47,691 hrs · 19,307 cycles

AIRCRAFT NOT GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE COMING OUT OF COVER. CHECKED AND FOUND SLIDE SECURED. REFOLDED GIRT BAR FLAP. OPERATIONAL CHECK GOOD.

Part: WARNING HORN — FALSE ACTIVATION · airframe 47,461 hrs · 19,232 cycles

DURING TAKEOFF, PUSHED POWER UP AND RECEIVED A WARNING HORN. PULLED BACK POWER, JIGGLED SPEED BRAKE AND FLAP HANDLES. THE WARNING DID NOT RECUR. OPERATIONAL CHECK GOOD. SUBSEQUENT FLIGHT UNEVENTFUL.

Part: SLIDE — MISALIGNED (L1 DOOR) · airframe 47,461 hrs · 19,232 cycles

L1 DOOR EMERGENCY EVACUATION SLIDE LOWER BALL IS NOT THROUGH THE BRACKET. RESEATED SLIDE IAW AMM 25-66-01. OPERATIONAL CHECKED GOOD.

Part: SLIDE — MISALIGNED (L2 DOOR) · airframe 47,461 hrs · 19,232 cycles

L2 DOOR EMERGENCY EVACUATION SLIDE LOWER BALL IS NOT THROUGH THE BRACKET. RE-SEATED SLIDE IAW AMM 25-66-01. OPERATIONAL CHECK GOOD.

Part: SIGN — DETACHED (CABIN) · airframe 47,371 hrs · 19,190 cycles

AIRCRAFT NOT GROUNDED. R4 DOOR EMERGENCY EXIT SIGN IS DETACHED. REPLACED EXIT SIGN ASSEMBLY IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — FAULTY (SPOILER) · airframe 45,491 hrs · 18,413 cycles

AIRCRAFT WAS GNDED. WHEN TOGA WAS PRESSED THE TAKEOFF CONFIGURATION WARNING LIGHT ILLUMINATED & HORN SOUNDED. TAKEOFF REJECTED AT APPROX 20 KNOTS. ACCOMPLISHED FIM TASK 27-62-00 & FOUND GND SPOILER CONTROL VLV BYPASSING. R & R VLV IAW AMM 27-62-41 & AUTO SPOILER ACTUATOR IAW AMM 27-62-31. SEE ALSO AALA 20160506001.

Part: CONTROL VALVE — BYPASSING (SPOILER) · airframe 45,491 hrs · 18,413 cycles

AIRCRAFT WAS GNDED. WHEN TOGA WAS PRESSED THE TAKEOFF CONFIGURATION WARNING LIGHT ILLUMINATED & HORN SOUNDED. TAKEOFF REJECTED AT APPROX 20 KNOTS. ACCOMPLISHED FIM TASK 27-62-00 & FOUND GND SPOILER CONTROL VLV BYPASSING. R & R VLV IAW AMM 27-62-41 & AUTO SPOILER ACTUATOR IAW AMM 27-62-31. SEE ALSO AALA 201605065003.

Part: SKIN — CRACKED (L1 DOOR) · airframe 44,559 hrs · 18,047 cycles

AIRCRAFT WAS GNDED. L1 DOOR EXTERIOR SKIN, DAMAGED & CRACKED AT LOWER HINGE CUT OUT AREA DUE TO DOOR SNUBBER FAILURE. ACCOMPLISHED SKIN REPAIR IAW SRM 52-10-01-2R-5. SEE AALA20160112003 FOR SNUBBER REPORT.

Part: SNUBBER — BROKEN (L1 DOOR) · airframe 44,559 hrs · 18,047 cycles

AIRCRAFT WAS GNDED. WHEN L1 DOOR WAS OPENED AT GATE A PIECE OF THE DOOR ASSIST & SNUBBER CYLINDER FELL FROM THE ACFT. R & R ASSIST & SNUBBER CYLINDER IAW AMM 52-11-51. OPERATIONAL CHECKED GOOD. MX NOTED ASSOCIATED DAMAGE TO THE DOOR EXTERIOR SKIN, SEE AALA20160112003.

Part: SLIDING WINDOW — DEFECTIVE (COCKPIT) · airframe 42,742 hrs · 17,358 cycles

RIGHT SLIDING WINDOW DOES NOT OPERATE, OPEN FROM EMER RELEASE HANDLE. R & R WINDOW.

Part: CONNECTOR — LOOSE (CABIN) · airframe 41,312 hrs · 16,787 cycles

SEAT MOUNTED EMER LIGHT SY SEAT ROW 9DEF IS INOPERATIVE. SECURED LOOSE CONNECTOR TO SEAT MOUNTED EMER LIGHT IAW 33-51-11. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,312 hrs · 16,787 cycles

SEAT MOUNTED EMER LIGHT AT SEAT ROW 9 DEF IS INOPERATIVE. RELAMPED SEAT MOUNTED EMERGENCY LIGHT IAW 33-51-11. SYS CHECKED NORMAL.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,486 hrs · 14,554 cycles

INTERCOSTAL FROM STATIONS 986 TO 1006 AND RIGHT BUTTLINE 33 HAS CORROSION ON TOP SURFACE. INSTALLED SERVICEABLE INTERCOSTAL PER AARD 51-10-05-1.

Part: REVEAL — GOUGED (FUSELAGE) · airframe 35,486 hrs · 14,554 cycles

AFT CARGO DOOR CUTOUT FORWARD REVEAL IS GOUGED FROM CONTACT WITH LOADING SYSTEM SIDE GUIDES. INSTALLED AFT CARGO DOOR CUTOUT FORWARD REVEAL PER AARD 51-10-05, BOEING DWG 146A9403 AND IPC 53-11-00-48A.

Part: BEAM — CORRODED (FUSELAGE) · airframe 35,486 hrs · 14,554 cycles

CORROSION ON BEAM 986.5 AT RIGHT BUTTLINE 23. INSTALLED T-CAP PER SRM 53-70-51-2R-4.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,486 hrs · 14,554 cycles

FORWARD CARGO DOOR CUTOUT LOWER THRESHOLD WEB CORRODED. REPLACED WEB PER SRM 51-10-2.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 35,486 hrs · 14,554 cycles

FORWARD SERVICE DOOR CUTOUT LOWER FORWARD CORNER CRACKED AT STATION 298. INSTALLED DOUBLER PER SRM 51-70-11.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · airframe 35,486 hrs · 14,554 cycles

CORROSION ON LEFT TRANSITION PANEL FROM STATIONS 787 TO 807. INSTALLED REPAIR TO LEFT TRANSITION PANEL FROM STATIONS 787 TO 807 PER SRM 53-00-53-2R 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,486 hrs · 14,554 cycles

CABIN STRUCTURE FLOORBEAM UPPER FLANGE CORRODED STATION 328, RIGHT BUTTLINE 13. INSTALLED STRAP PER SRM 53-10-51-2R-8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,486 hrs · 14,554 cycles

STATION 480L FRAME IS CRACKED AT THE SUPPORT BRACKET INBOARD FASTENER. ACCOMPLISHED NESTED ANGLE REPAIR PER ECO J1159AE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,486 hrs · 14,554 cycles

CABIN STATION 400, THE LEFT SIDE OVERHEAD BIN LOWER SIDE RAIL ATTACH SUPPORT AREA, OUTBOARD RIVET HOLE HAS A CRACK COMING OUT OF THE HOLE. ACCOMPLISHED NESTED ANGLE REPAIR PER ECO J1159AE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,486 hrs · 14,554 cycles

STATION 400R FRAME IS CRACKED AT THE SUPPORT BRACKET INBOARD FASTENER. ACCOMPLISHED NESTED ANGLE REPAIR PER ECO J1159AE.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,486 hrs · 14,554 cycles

DENT ON FUSELAGE SKIN, 18 INCHES BELOW AND IN LINE WITH THE LEADING EDGE OF THE CAPTAINS SLIDING WINDOW. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-01-2R-3.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 36,140 hrs · 14,797 cycles

RIGHT SEAT TRACK AT BS 727B, RT AND LT BUTTLINE 45.50, INBD AND OTBD FLANGE, AFT HOLE SHOWS CRACK INDICATION. ACCOMPLISHED REPAIR IAW EA B737-53-029840.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 36,140 hrs · 14,797 cycles

LEFT SEAT TRACK AT 727B, LEFT BUTTLINE 24.75, INBD FLANGE AFT HOLE SHOWS CRACK INDICATION. ACCOMPLISHED REPAIR IAW EA 737-53-029840.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 36,140 hrs · 14,797 cycles

RIGHT SEAT TRACK AT BS 727B, RBL 24.75, OTBD FLANGE AFT HOLE SHOWS CRACK INDICATION. ACCOMPLISHED REPAIR IAW EA B737-53-029840.

Part: WIRE HARNESS — FAULTY (LT ENGINE) · airframe 30,178 hrs · 12,790 cycles

LAX - INFLIGHT SAN-JFK. CREW REPORTED LEFT ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE FUEL FILTER BYPASS WIRE HARNESS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PSEU — MALFUNCTIONED (TE FLAP) · airframe 24,794 hrs · 10,449 cycles

CREW REPORTED SPLIT FLAP CONDITION ON TAKEOFF. RETURNED TO MSY AND LANDED WITHOUT INCIDENT. RESET PROXIMITY SWITCH ELECTRONICS UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA - BATTERY PACK FOR RIGHT EMERGENCY LIGHT AFT OVERWING WOULD NOT HOLD CHARGE. REPLACED BATTERY PACK FOR RIGHT EMERGENCY LIGHT AFT OVERWING.

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA - BATTERY PACK FOR EMERGENCY LIGHTS FROM ROW 15 TO 28 WOULD NOT HOLD CHARGE. REPLACED BATTERY PACK AT SEAT 19F FOR EMERGENCY LIGHTS FROM ROW 15 TO 28.

Part: SKIN — DENTED (FUSELAGE) · airframe 23,884 hrs · 10,040 cycles

FUSELAGE DAMAGE TO SKIN AT STATION 312, STRINGER 4 LEFT. THREE GOUGES MEASURING 3.75 INCHES BY .0937 DEEP, 2.5 INCHES BY .125 DEEP AND 2 INCHES BY .125 DEEP. REMOVED DAMAGED SKIN AND STRINGER AND INSTALLED REPAIR DOUBLER PER EA B737-53-006534.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 23,884 hrs · 10,040 cycles

FUSELAGE SKIN, 36 INCHES AFT OF FORWARD CARGO DOOR DAMAGED. CUT OUT DAMAGE, INSTALLED DOUBLER PER SRM 53-00-01-2R FIG 3.

Part: LENS — MISSING (EMERGENCY LIGHT) · 21,497 cycles

MIA EMERGENCY LIGHT AT SEAT 10D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: FSEU — INOPERATIVE (FLAP/SLAT SYS) · airframe 18,643 hrs

MEX INFLIGHT T2115/16NOV - ON APPROACH FLAPS REMAINED IN UP POSITION. LANDED MEX WITHOUT INCIDENT. TAXIED TO GATE WITH NO FURTHER PROBLEMS. REPLACED FLAP SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

MSP - EMERGENCY LIGHT AT SEAT 8ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 8ABC. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

TUL- EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK M1671 AT STATION 727 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

TUL - EMERGENCY LIGHTS IN COACH CABIN INOPERATIVE. REPLACED BATTERY PACK M1672 AT STATION 952 FOR EMERGENCY LIGHTS IN COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

MIA - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. RECHARGED EMERGENCY LIGHT SYSTEM FOR INOPERATIVE EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

MIA - EMERGENCY LIGHTS IN FIRST CLASS ROWS 1 TO 6 INOPERATIVE. CHARGED EMERGENCY LIGHT SYSTEM FOR INOPERATIVE EMERGENCY LIGHTS IN FIRST CLASS ROWS 1 TO 6. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

RNO - INSEAT EMERGENCY LIGHTS AT ROWS 12, 13 AND 14DEF INOPERATIVE. REPLACED BATTERY PACK AT RIGHT HAND OVERWING EMERGENCY EXIT FOR ROWS 12, 13, AND 14DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)