N966AN

Part: GIRT BAR — OUT OF POSITION (ZONE 800) · airframe 70,106 hrs · 29,635 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS GIRT FLAP ON FORWARD ENTRY DOOR TOO LONG. MAINTENANCE TUCKED IN GIRT FLAP IN THE L1 DOOR SLIDE BUSTLE PER AMM 25-66-00.

Part: LIGHT — DETACHED (ZONE 200) · airframe 69,688 hrs · 29,443 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 15ABC SEAT, AISLE EMERGENCY LIGHT ASSEMBLY DETACHED FROM SEAT. RESECURED LIGHT ASSEMBLY TO SEAT. PER CMM 25-23-67.

Part: SIGN — DISLODGED (ZONE 200) · airframe 69,421 hrs · 29,311 cycles

AIRCRAFT WAS NOT GROUNDED: 14C EMERGENCY EXIT SIGN POPPED OUT ON ONE SIDE. REINSTALLED 14C SEAT EMERGENCY EXIT LIGHT ASSEMBLY.

Part: SLIDE — DISLODGED (ZONE 800) · airframe 69,383 hrs · 29,289 cycles

AIRCRAFT WAS NOT GROUNDED: MAIN ENTRY SLIDE PARTIALLY FALLEN OUT OF HOUSING. ADJUSTED THE L1 DOOR SLIDE FOLD ADJACENT TO THE GIRT BAR. PER AMM25-66-01.

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 69,037 hrs · 29,114 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDENT REPORTS DOOR 1L GIRT BAR BRACKET IS TOO TIGHT. ADJUSTED CLIPS TO CONFORM TO SPECIFICATION IN FIGURE 602 VIEW A-A. PER AMM 25-66-01-200-802. OPERATIONAL CHECK GOOD.

Part: GIRT BAR — UNSECURE (ZONE 800) · airframe 68,997 hrs · 29,094 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY SLIDE ON BOARDING DOOR L1 HAS A FLAP EXPOSED AFTER DISARMING. RESECURED LOOSE FABRIC STRAP ON L1 DOOR EMERGENCY SLIDE PACK AND PERFORMED OPERATIONAL CHEC KOF THE GIRT BAR SYSTEM. PER AMM 25-66-01. NO FURTHER DEFECTS NOTED.

Part: GIRT BAR — LACK OF LUBE (ZONE 800) · airframe 68,799 hrs · 28,998 cycles

AIRCRAFT WAS NOT GROUNDED: R1 SERVICE DOOR GIRT BAR STOWED BRACKETS ARE REPORTED TO TIGHT TO DETACH GIRT BAR. LUBED GIRT BAR. PER AMM 25-66-01. OPERATIONAL CHECK GOOD.

Part: SIGN — DETACHED (ZONE 200) · airframe 68,646 hrs · 28,923 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT SIGN ROW 15 FELL OFF WALL. RESECURED OVERWING EMERGENCY EXIT SIGN LENS, PER AMM 33-51-01.

Part: WARNING LIGHT — FALSE ACTIVATION (FLOW SENSOR) · airframe 68,367 hrs · 28,801 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: EQUIPMENT COOLING EXHAUST OFF LIGHT ILLUMINATED DURING FLIGHT. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. REMOVED AND REPLACED EXHAUST LOW FLOW DETECTOR SENSOR. PER AMM 21-21-03. OPERTIONAL CHECK NORMAL.

Part: FITTING — DELAMINATED (GIRT BAR) · airframe 68,316 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATION OF RUBBER FROM THE GIRT BAR R-1 DOOR EMERGENCY ESCAPE SLIDE. REMOVED AND INSTALLED NEW R1 DOOR EMERGENCY ESCAPE SLIDE. PER CARD 08L22125001.

Part: SKIN — CRACKED (ZONE 200) · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN R1 DOOR SURROUND FUSELAGE SKIN AT BS 295 FROM S6R TO S10R. REPAIRED SKIN PER SRM 53-10-01-2R-6 AND EA 364150.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM BS 312 TO BS 328 AT LBL 28. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM BS 947 TO BS 967, AT LBL 24. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL BETWEEN BS 277 AND BS 294.5 AT BL 0. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT INTERCOSTAL FROM BS 847 TO BS 856, AT S25R. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT BS 946, RBL 51. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (ZONE 100) · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL UPPER ANGLE FROM BS 380 TO BS 400, AT RBL 10. REPLACED ANGLE PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL UPPER ANGLE FROM BS 380 TO BS 400, AT BL 0. REPLACED ANGLE PER AARD 51-00-05-1.

Part: BRACKET — CORRODED (ZONE 300) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON APU COMPARTMENT BRACKET AT BS 1088, LBL 2. REPLACED BRACKET PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (ZONE 100) · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL UPPER ANGLE FROM BS 500I TO BS 520 AT BL 0. REPLACED ANGLE PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT BS 950, FRM RBL 24 TO RBL 51. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR SUPPORT AT BS 950 FROM LBL 18 TO LBL 24. REPLACED FLOOR SUPPORT PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL UPPER ANGLE FROM BS 380 TO BS 400, AT LBL 12. REPLACED ANGLE PER AARD 51-00-05-1.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR SUPPORT AT BS 950 FROM RBL 16 TO RBL 24. REPLACED FLOOR SUPPORT PER AARD 51-00-05-1.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER CHORD (T-CAP) OF PASSENGER CABIN FLOOR BEAM AT BS 328, RBL 52. REPAIRED FLOOR BEAM UPPER CHORD PER SRM 53-10-51-2R-7 ALTERNATIVE 2.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM BS 500F TO BS 500G, AT S25L. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R-5.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL FROM BS 867 TO BS 947.5 AT S25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM BS 500G TO BS 500H, AT S25L. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R-5.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM BS 500H TO BS 500I, AT S25R. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R-5.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM BS 500D TO BS 500E, AT S25R. REPLACED TRANSITION PANEL SECTION PER SRM 53-00-53-2R-5.

Part: SHIELD — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHIELD FROM BS 847 TO BS 867, AT RBL 21. REPLACED SHIELD PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM BS 927 TO BS 947, AT RBL 24. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM BS 950 TO BS 967 AT RBL 51. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT STA 947, RBL 14. REPAIRED CHORD PER SRM 53-70-51-2R-5 AND EA 364121.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT DOOR CUT OUT WEB AT STA 449, RBL 24. REPLACED WEB PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM BS 500C PLUS 12 INCHES TO BS 500I, AT S25R. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R-5.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM BS 500E TO BS 500F, AT S25R. REPLACED TRANSITION PANEL SECTION PER SRM 53-00-53-2R-5.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR SUPPORT AT BS 950 FROM LBL 24 TO LBL 48. REPLACED FLOOR SUPPORT PER AARD 51-00-05-1.

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT AFT BULKHEAD BRACKET AT BS 947.5, FROM S25L TO S25R. REPLACED BRACKET PER AARD 51-00-05-1.

Part: SHIELD — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHIELD FROM BS 767 TO BS 797, S24R, RBL 21. REPLACED SHIELD PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100 -) · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM BS 500E TO BS 500F, AT LBL 25. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R-5.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT DOOR THRESHOLD WEB FROM BS 797 TO BS 847 AT S25R. REPLACED WEB PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM BS 500F TO BS 500G, AT S25R. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R-5.

Part: SKIN — CRACKED (ZONE 300) · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 157.10, 9 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.

Part: SKIN — CRACKED (ZONE 300) · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 129.50, 9 INCHES FROM FRONT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.

Part: SKIN — CRACKED (ZONE 300) · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 138.70, 9 INCHES FROM FRONT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.

Part: SKIN — CRACKED (ZONE 300) · airframe 68,315 hrs · 28,773 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 129.50, 26 INCHES FROM FRONT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.

Part: HYDRAULIC SYSTEM — LEAKING · airframe 67,454 hrs · 28,379 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: HYDRAULIC SYSTEM-A QUANTITY DECREASED FROM 93% TO 77% WITHIN 5 MINUTES AFTER TAKEOFF. CONTINUED LOSS AT 1% EVERY TEN MINUTES THERE AFTER; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DFW. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: ACTUATOR — LEAKING (ZONE 300) · airframe 67,454 hrs · 28,379 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: HYDRAULIC SYSTEM-A QUANTITY DECREASED FROM 93% TO 77% WITHIN 5 MINUTES AFTER TAKEOFF. CONTINUED LOSS AT 1% EVERY TEN MINUTES THERE AFTER; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DFW. **SUPPLEMENTAL REPORT FOR (AALA202412021566): REMOVE AND REPLACED ELEVATOR FEEL ACTUATOR. PER AMM 27-31-67. ALL OPERTIONAL AND LEAK CHECK GOOD**(CLOSED).

Part: LIGHT — MISSING (SEAT 2B) · airframe 66,254 hrs · 27,787 cycles

AIRCRAFT WAS GROUNDED: WHILE WORKING INSIDE AIRCRAFT NOTICED SEAT 2B HAS BOTH FORWARD AND AFT SEAT MOUNTED EMERGENCY LIGHT ASSEMBLIES MISSING. INSTALLED FLOOR PROXIMITY LIGHTS ON FORWARD (AALA202407011909) AND AFT (AALA202407019096) SIDE OF SEAT 2B. PER AMM 33-51-11, OPERTIONAL CHECK GOOD PER AMM 33-51-00. NO FURTHER DEFECTS NOTED.

Part: LIGHT — MISSING (SEAT 2 B) · airframe 66,254 hrs · 27,787 cycles

AIRCRAFT WAS GROUNDED: WHILE WORKING INSIDE AIRCRAFT NOTICED SEAT 2B HAS BOTH FORWARD AND AFT SEAT MOUNTED EMERGENCY LIGHT ASSEMBLIES MISSING. INSTALLED FLOOR PROXIMITY LIGHTS ON FORWARD (AALA202407011909) AND AFT (AALA202407019096) SIDE OF SEAT 2B. PER AMM 33-51-11, OPERTIONAL CHECK GOOD PER AMM 33-51-00. NO FURTHER DEFECTS NOTED.

Part: DOOR — OUT OF ADJUST (FWD LAVATORY) · airframe 66,057 hrs · 27,690 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN (STICKING AT BOTTOM OF DOOR). **SUPPLEMENTAL REPORT FOR (AALA202406037651): ADJUSTED FORWARD LAVATORY DOOR. PER AMM FIN TASK 52-99-00. **(CLOSED).

Part: DOOR — BINDING (FWD LAVATORY) · airframe 66,057 hrs · 27,690 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN (STICKING AT BOTTOM OF DOOR). **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 65,839 hrs · 27,578 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT FORWARD ENTRY DOOR FLASH LIGHT INOPERATIVE. REPLACED FLASHLIGHT AS REQUIRED. PER AMM 25-20-00.

Part: FITTING — CRACKED (ZONE 100 - FUSE) · airframe 63,879 hrs · 26,630 cycles

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

Part: FITTING — CRACKED (ZONE 100 - FUSE) · airframe 63,879 hrs · 26,630 cycles

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

Part: FITTING — CRACKED (ZONE 100 - FUSE) · airframe 63,879 hrs · 26,630 cycles

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

Part: FITTING — CRACKED (ZONE 100 - FUSE) · airframe 63,879 hrs · 26,630 cycles

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

Part: FITTING — CRACKED (ZONE 100 - FUSE) · airframe 63,879 hrs · 26,630 cycles

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

Part: FITTING — CRACKED (ZONE 100 - FUSE) · airframe 63,877 hrs · 26,629 cycles

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

Part: FITTING — CRACKED (ZONE 100 - FUSE) · airframe 63,879 hrs · 26,630 cycles

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

Part: FITTING — CRACKED (ZONE 100 - FUSE) · airframe 63,879 hrs · 26,630 cycles

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

Part: FITTING — CRACKED (ZONE 100 - FUSE) · airframe 63,879 hrs · 26,630 cycles

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

Part: FITTING — CRACKED (ZONE 100 - FUSE) · airframe 63,879 hrs · 26,630 cycles

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

Part: PLATE — BROKEN (ZONE 100 - FUSE) · airframe 63,877 hrs · 26,629 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR CROSS STRUCTURE BETWEEN CENTER FLOOR BEAM AND RIGHTHAND INBOARD FLOOR BEAM BROKEN. LOCATED AT BS 540 BETWEEN BL 0 TO RBL 33. REPLACED FLOOR PLATE (AALA202309075735) AND PANEL (AALA202309077642) PER SRM 51-40-02.

Part: FLOORBEAM — BROKEN (ZONE 100 - FUSE) · airframe 63,877 hrs · 26,629 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR CROSS STRUCTURE BETWEEN CENTER FLOOR BEAM AND RIGHTHAND INBOARD FLOOR BEAM BROKEN. LOCATED AT BS 540 BETWEEN BL 0 TO RBL 33. REPLACED FLOOR PLATE (AALA202309075735) AND PANEL (AALA202309077642) PER SRM 51-40-02.

Part: BULB — NOT SEATED (ZONE 200 - FUSE) · airframe 63,655 hrs · 26,519 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 16 DEF EMERGENCY LIGHT IS INOPERATIVE. ADJUSTED/RESET BULB.

Part: DOOR — STUCK (ZONE 900 - LAV/G) · airframe 63,640 hrs · 26,512 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR STICKS AT BOTTOM MAKING IT DIFFICULT TO OPEN AND CLOSE. ADJUSTED FORWARD LAVATORY DOOR PER CMM 25-45-46.

Part: GIRT BAR — WILL NOT ARM (ZONE 800 - DOORS) · airframe 63,240 hrs · 26,308 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD ENTRY CABIN DOOR SLIDE HAS TOO MUCH SLACK AND DIFFICULT TO ARM. ADJUSTED GIRT BAR SKIRT.

Part: CONNECTOR — INOPERATIVE (ZONE 200 - FUSE) · airframe 62,675 hrs · 26,008 cycles

AIRCRAFT WAS GROUNDED: WHILE PERFORMING JOB CARD FOR OPERATIONAL TEST EMERGENCY LIGHTS FOUND EMERGENCY AISLE LIGHT ABOVE BIN 19CBA INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY, LIGHT STILL INOPERATIVE. FOUND CONNECTOR D11321 LOOSE. INSPECTED CONNECTOR AND RESECURED. OPERATIONS CHECK GOOD

Part: GUST LOCK — INOPERATIVE (L1 DOOR) · airframe 62,118 hrs · 25,737 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 DOOR GUST LOCK WON'T STAY ENGAGED. ADJUSTED GUST LOCK PER AMM 52-11-21.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 62,116 hrs · 25,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CAPTAINÏ¿½S #1 WINDSHIELD DELAMINATED AT UPPER LEFT HAND CORNER. REPLACED WINDSHIELD PER JOB CARD 08L21056003.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 62,117 hrs · 25,736 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN PANEL LOCATED AT STABILIZER STA 129.50. REPAIRED SKIN PER SRM 55-10-01-2R REPAIR 11.

Part: LENS — MISSING (ZONE 200 - FUSE) · airframe 61,224 hrs · 25,305 cycles

AIRCRAFT WAS NOT GROUNDED: R4 DOOR EMERGENCY EXIT SIGN LENS MISSING. REPLACED SIGN ASSEMBLY PER AMM 33-51-01. OPERATIONAL CHECK NORMAL.

Part: CONTROL MODULE — WARNING LIGHT (ZONE 200 - FUSE) · airframe 60,821 hrs · 25,109 cycles

AIRCRAFT WAS NOT GROUNDED: DURING CLIMB OUT, ANTISKID LIGHT ILLUMINATED. LIGHT EXTINGUISHED IN DESCENT PASSING 25 THOUSAND FEET. AIRCRAFT DIVERTED TO IAD DUE TO SHORT RUNWAY AT DCA. **SUPPLEMENTAL REPORT FOR AALA202205205917: REMOVED AND REPLACED AUTO BRAKE CONTROL MODULE PER AMM 32-42-81-000-801** (CLOSED)

Part: NONE — NONE · airframe 60,821 hrs · 25,109 cycles

AIRCRAFT WAS NOT GROUNDED: DURING CLIMB OUT, ANTISKID LIGHT ILLUMINATED. LIGHT EXTINGUISHED IN DESCENT PASSING 25 THOUSAND FEET. AIRCRAFT DIVERTED TO IAD DUE TO SHORT RUNWAY AT DCA. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)

Part: ANTI-ICE SYSTEM — NONE (ZONE 700 - GEARS) · airframe 60,809 hrs · 25,103 cycles

AIRCRAFT WAS NOT GROUNDED: AFTER LEVEL OFF AT CRUISE ANTI SKID INOPERATIVE LIGHT ILLUMINATED LIGHT EXTINGUISHED APPROXIMATELY 1.5 HOURS LATER PRIOR TO DESCENT. TROUBLE SHOT ANTI SKID INOPERATIVE LIGHT PER FIM 32-42-00-810-829 NO FAULTS FOUND.

Part: DOOR — LACK OF LUBE (ZONE 800 - DOORS) · airframe 60,140 hrs · 24,813 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD ENTRY DOOR DIFFICULT TO CLOSE. LUBED DOOR AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK PER AMM 52-11-00-601.

Part: DOOR — DIRTY (ZONE 800 - DOORS) · airframe 59,770 hrs · 24,643 cycles

AIRCRAFT WAS NOT GROUNDED: THE 1L DOOR IS VERY DIFFICULT TO CLOSE. THE HANDLE CANNOT LOCK THE DOOR WITHOUT JOSTLING THE UPPER LEFT CORNER INTO POSITION. LUBRICATED L1 DOOR AND REMOVED DEBRIS. OPERATIONS CHECK NORMAL PER 52-11-00.

Part: BAR — UNSECURE (ZONE 800 - DOORS) · airframe 59,667 hrs · 24,597 cycles

AIRCRAFT WAS NOT GROUNDED: AFT GIRT BAR HOLDER ON THE FLOOR DOOR 1R DOES NOT HOLD THE BAR SECURELY. SECURED AS REQUIRED OK FOR CONTINUED SERVICE.

Part: PIN — INOPERATIVE (ZONE 800 - DOORS) · airframe 59,635 hrs · 24,576 cycles

AIRCRAFT WAS NOT GROUNDED: 1L DOOR WOULD NOT OPEN FULLY ON GATE ARRIVAL. STUCK HALF OPEN. REMOVED AND REPLACED RADIUS LINK PIN PER AMM 52-11-21.

Part: GUST LOCK — LOOSE (L1 DOOR) · airframe 58,948 hrs · 24,255 cycles

AIRCRAFT WAS GROUNDED: UPON ARRIVAL, WHEN 1L ENTRY DOOR WAS OPENED, CATCH ON HINGE APPEARED LOOSE AND DOOR SLAMMED ON TO FUSELAGE. DOOR WHEN FULLY OPENED IS NOW RESTING ON FUSELAGE. REMOVED AND REPLACED L1 DOOR SNUBBER (AALA202109072838) PER AMM 52-11-51. REMOVED AND REPLACED L1 DOOR GUST LOCK PER AMM 52-11-21. DOOR RIGGED PER AMM 52-11-00.

Part: SNUBBER — LOOSE (L1 DOOR) · airframe 58,948 hrs · 24,255 cycles

AIRCRAFT WAS GROUNDED: UPON ARRIVAL, WHEN 1L ENTRY DOOR WAS OPENED, CATCH ON HINGE APPEARED LOOSE AND DOOR SLAMMED ON TO FUSELAGE. DOOR WHEN FULLY OPENED IS NOW RESTING ON FUSELAGE. REMOVED AND REPLACED L1 DOOR SNUBBER PER AMM 52-11-51. REMOVED AND REPLACED L1 DOOR GUST LOCK (AALA202109079636) PER AMM 52-11-21. DOOR RIGGED PER AMM 52-11-00.

Part: PUMP — FAILED (FUEL BOOST) · airframe 57,913 hrs · 23,781 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT HAND CENTER BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED WITH 4000 LBS FUEL IN CENTER TANK CONFIRMED FUEL PUMP FAILURE WITH FUEL IMBALANCE IN MAIN TANKS. REPLACED RT CENTER FUEL PUMP AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 57,759 hrs · 23,701 cycles

AIRCRAFT NOT GROUNDED - L1 SLIDE DISLODGED DURING DOOR OPENING. REPACKED SLIDE PER AMM TASK 25-66-01-400-801, AND REINSTALLED WITH COVER PER AMM TASK 25-66-01-400-803.

Part: TRANSMITTER — DEFECTIVE (RT WING TE FLAPS) · airframe 57,626 hrs · 23,642 cycles

AIRCRAFT WAS GROUNDED: AFTER TAKEOFF , UNABLE TO RETRACT FLAPS FROM 1 TO UP. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW WHEERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT.FLIGHT CREW FOLLOWED QRH. ALT FLAPS USED FOR F15 LANDING WITH A NORMAL TOUCH DOWN AND LIGHT BRAKING. MAINTENANCE REPLACED THE RIGHT TRAILING EDGE FLAP POSITION TRANSMITTER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 27-58-01.

Part: BATTERY PACK — MISSING (EMERGENCY LIGHT) · airframe 57,607 hrs · 23,632 cycles

AIRCRAFT WAS NOT GROUNDED BUT WAS IN SHORT TERM STORAGE: FOUND LEFT HAND MAIN ENTRY EMERGENCY LIGHT BATTERY PACK MISSING. INSTALLED BATTERY PACK AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-06.

Part: BATTERY PACK — MISSING (EMERGENCY LIGHT) · airframe 57,607 hrs · 23,632 cycles

AIRCRAFT WAS NOT GROUNDED BUT WAS IN SHORT TERM STORAGE: FOUND EMERGENCY BATTERY PACK AT RIGHT HAND OVER WING EMERGENCY EXIT LIGHT MISSING. INSTALLED BATTERY PACK AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-06.

Part: BATTERY PACK — MISSING (EMERGENCY LIGHTS) · airframe 57,607 hrs · 23,632 cycles

AIRCRAFT WAS NOT GROUNDED BUT WAS IN SHORT TERM STORAGE: LEFT HAND AFT ENTRY DOOR EMERGENCY EXIT LIGHT BATTERY PACK MISSING. INSTALLED BATTERY PACK PER AMM 33-51-06.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND WEB AT BS 1016 AND RBL 32. REPLACED WEB PER 51-00-05-1.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND AFT WEB AT BS 1016 AND LBL 32. REPLACED WEB PER 51-00-05-1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON Z ANGLE AT BS 993 AND RBL 33. REPLACED Z ANGLE PER SRM 51-40-02.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED SILL WEB AT BS 937 AND RBL 58. REPLACED SILL WEB PER 51-00-05.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE CORROSION ON "Z" ANGLE BETWEEN BS 991 AND BS 1016 AT LBL 32. REPLACED ANGLE PER 51-00-05-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOORBEAM AT BS 986 BETWEEN LBL 42 AND RBL 42. REPAIRED FLOORBEAM PER SRM 53-70-51-2R-4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOORBEAM AT BS 1016 BETWEEN RBL 30 AND RBL 32. REPAIRED FLOORBEAM PER EA 295799 AND SRM 53-70-51-2R-4.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON INTERCOSTAL AT BS 990 AND LBL 32. REPLACED INTERCOSTAL PER SRM 53-70-51-2R.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON Z ANGLE AT BS 993 BWTEEN LBL 33 AND LBL 45. REPLACED ANGLE PER 51-00-05-1.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND SHEAR WEB BETWEEN BS 986 AND BS 992 AT S17L. REPLACED SHEAR WEB PER 51-00-05-1.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON INTERCOSTAL AT BS 951 AND RBL 50. REPLACED INTERCOSTAL PER SRM 51-70-51.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON K WEB AT BS 986 AND S17R. REPLACED WEB PER 51-00-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOORBEAM AT BS 947 BETWEEN LBL 11 AND RBL 16. REPAIRED FLOORBEAM PER SRM 51-70-51-2R-5.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON Z ANGLE BETWEEN BS 991 AND BS 1016 AT RBL 32. REPLACED ANGLE PER SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION IN INTERCOSTAL AT BS 990 AND RBL 32. REPLACED INTERCOSTAL PER 51-00-05-1 AND SRM 53-70-51-2R.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND HORIZONTAL STABILIZER RIB, SECOND RIB FROM THE INBOARD BOX AT 97.2 CRACKED. REPAIRED RIB PER SRM 55-10-09-2R, REPAIR 4.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R1 DOOR CUT OUT LOWER CREASE ANGLE BETWEEN BS 291 AND BS 360. REPLACED CREASE ANGLE PER 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT BS 887 AND S27L. REPLACED FLOOR SUPPORT PER SRM 53-00-53.

Part: TRANSITION PANEL — CORRODED (BS 727-847) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL BETWEEN BS 727 AND BS 847. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL BETWEEN BS 328 AND BS 344 AT LBL 45.6. REPLACED INTERCOSTAL PER AARD 51-10-05-1

Part: TRANSITION PANEL — CORRODED (BS 727-767) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL BETWEEN BS 727 AND BS 767. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT STRAP BETWEEN BS 772.6 AND BS 774.6 AT S24L, REPLACED FLOOR SUPPORT STRAP PER 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR SUPPORT (TEE) AT BS 887 AND S27L. REPLACED FLOOR SUPPORT PER SRM 53-00-53.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 55,464 hrs · 22,620 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL BETWEEN BS 328 AND BS 344 AT LBL 35. REPLACED INTERCOSTAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 52,189 hrs · 21,220 cycles

EMERGENCY LIGHT LENS MISSING AT THE R1 DOOR. REPLACED EMERGENCY LIGHT LENS IAW AMM 33-51-01.

Part: LINE — BROKEN (HYD SYSTEM) · airframe 50,761 hrs · 20,583 cycles

HYDRAULIC A SYSTEM FAILURE. EMERGENCY DECLARED, AND FLIGHT DIVERTED. LANDING UNEVENTFUL. REMOVED AND REPLACED A BROKEN HYDRAULIC LINE ON THE NR 1 ENGINE PYLON IAW AMM 20-50-11. LEAK AND OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: UNKNOWN — UNKNOWN · airframe 49,497 hrs · 20,067 cycles

TAKEOFF REJECTED AT 144 KNOTS, DUE TO AN UNCOMMANDED YAW. ACCOMPLISHED INSPECTION OF RUDDER, PEDALS, STEERING, BRAKES, LANDING GEAR, WHEELS AND THRUST REVERSER. OPS CHECKED GOOD. THE AIRCRAFT WAS GROUNDED.

Part: PANEL — CORRODED (LAVATORY) · corrosion level 2 · airframe 49,437 hrs · 20,039 cycles

CORROSION WAS FOUND ON THE AFT LAVATORY SERVICE PANEL. REMOVED AND REPLACED THE SERVICE PANEL IAW SRM 51-10-02, 51-00-05, SRM 51-40-02, DRAWING 146A7400, AND EA 269977.

Part: FLOOR SUPPORT — CRACKED (ZONE 100 - FUSE) · airframe 49,437 hrs · 20,039 cycles

FLOOR SUPPORT CRACKED BETWEEN FUSELAGE BS 312 AND 328, LBL 46. REMOVED AND REPLACED THE FLOOR SUPPORT IAW 51-00-05-1, DRAWINGS 141A5410 AND 141A5400.

Part: INTERCOSTAL — CRACKED (BS 328-344) · airframe 49,437 hrs · 20,039 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 328 AND 344, LBL 46. REMOVED AND REPLACED THE FLOOR SUPPORT IAW 51-00-05-1, DRAWINGS 141A5410 AND 141A5400.

Part: FUEL SYS — LOW PRESSURE · airframe 48,722 hrs · 19,742 cycles

DURING TAKE OFF ROLL WITH THE RIGHT FOWARD BOOST PUMP ON MEL THE RIGHT AFT MAIN TANK LOW PRESSURE LIGHT ILLUMINATED. TAKE OFF ABORTED AT APPROXIMATELY 70 KNOTS. MAINTENANCE SUMPED FUEL TANKS IAW AMM 12-11-00 WITH NO WATER FOUND. ACCOMPLISHED OPERATIONAL TEST IAW AMM 28-42-11-700-801 WITH NO DISCREPANCIES NOTED. AIRCRAFT WAS GROUNDED.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 48,425 hrs · 19,627 cycles

FORWARD GALLEY EMERGENCY FLOOD LIGHT HAS A BROKEN LENS. REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51-01. OPERATIONAL CHECKED GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 48,425 hrs · 19,627 cycles

BLUE EMERGENCY LIGHTS ON IN ALL FIRST CLASS AISLE SEATS. CYCLES ON AND OFF DURING FLIGHT. REMOVED AND REPLACED POWER BUSS CONTROL UNIT IAW AMM 24-41-21. OPERATIONAL CHECKED GOOD.

Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 48,077 hrs · 19,485 cycles

AIRCRAFT NOT GROUNDED. RIGHT FORWARD FUEL BOOST PUMP FLICKERD LOW PRESSURE DURING CLIMB AND CRUISE. FUEL IMBALANCE DEVELOPED OVER TIME. LEFT TANK INDICATED GREATER BURN RATE. REMOVED AND REPLACED TANK 2 FORWARD FUEL BOOST PUMP PRESSURE SWITCH IAW AMM 28-42-11. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — FAULTY (HORIZ STAB) · airframe 47,911 hrs · 19,409 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. LANDING UNEVENTFUL. DURING FLIGHT BOTH YOKE AUTOMATIC TRIM SWITCHES FAILED FOLLOWED BY ILLUMINATION OF THE STABILIZER OUT TRIM LIGHT. MAINTENANCE REMOVED AND REPLACED THE STABILIZER TRIM ACTUATOR AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK IAW AMM 27-41-71.

Part: FILTER — LEAKING (HYD SYSTEM) · airframe 47,181 hrs · 19,104 cycles

DURING DESCENT "B" HYDRAULIC SYSTEM QUANTITY DECREASED TO UNUSEABLE LEVEL. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE FOUND "B" SYSTEM HYDRAULIC ACOUSTIC FILTER LEAKING. REMOVED AND REPLACED THE FILTER IAW AMM 29-11-27. OPS AND LEAK CHECKED NORMAL.

Part: INTERCOSTAL — CRACKED (BS 344-360) · airframe 43,281 hrs · 17,556 cycles

E & E COMPARTMENT INTERCOSTAL AT BL 0 CRACKED BETWEEN BS 344 & 360, FLOORBEAMS AT FWD CLIP NUT HOLE. R & R INTERCOSTAL IAW SRM 51-10-02-0G.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 43,281 hrs · 17,556 cycles

E & E COMPARTMENT FLOOR SUPPORT INTERCOSTAL AT LBL 46 CRACKED BETWEEN BS 328 & 344. R & R THE FLOOR SUPPORT IAW AARD 51-00-05-1 & PRINT 141A5410.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 43,281 hrs · 17,556 cycles

E & E COMPARTMENT FLOOR SUPPORT AT LBL 46 CRACKED BETWEEN STATIONS 312 & 328. R & R FLOOR SUPPORT IAW AARD 51-00-05-1 & PRINT 141A5410.

Part: LIGHT — DAMAGED (CABIN) · airframe 41,210 hrs · 16,767 cycles

SEAT 14D FWD EMER LIGHT LAMP DAMAGED. REPLACED LAMP FOR SEAT 14D FWD EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LENS — DAMAGED (CABIN) · airframe 41,210 hrs · 16,767 cycles

SEAT 14D FWD EMER LIGHT LENS DAMAGED. REPLACED LENS FOR SEAT 14D EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,932 hrs · 16,291 cycles

LEFT OVERWING EXIT SIGN FAILED TEST. REPLACED BATTERY PACK FOR LT OVERWING EXIT SIGN, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,932 hrs · 16,291 cycles

EMERGENCY LIGHTS AT POSITIONS ROW 13 & 14 ON RT SIDE INOPERATIVE. REPLACED BATTERY PACK AT OVERWING EXIT AISLE, OPERATIONS CHECKED NORMAL.

Part: VALVE — LEAKING (AC BAY) · airframe 38,584 hrs · 15,780 cycles

SFO LT PACK TRIM AIR CHECK VLV LEAKING. VLV INSTALLED WITH AXIS VERTICAL ALLOWING VLV SEGMENTS TO WEAR THROUGH VLV BODY. REPLACED LT HAND TRIM AIR CHECK VLV. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: BUSHING — CORRODED (RT HORIZ STAB) · airframe 36,471 hrs · 14,947 cycles

RIGHT HORIZONTAL STAB LUG BUSHINGS CORRODED AT CENTER SECTION FORWARD SPAR UPPER TERMINAL FITTING FORWARD CLEVIS LUG BUSHING. REPAIRED BUSHING PER EA B737-55-029632.

Part: BUSHING — CORRODED (RT HORIZ STAB) · airframe 36,471 hrs · 14,947 cycles

RIGHT HORIZONTAL STAB LUG BUSHINGS CORRODED AT CENTER SECTION LOWER FORWARD TERMINAL FITTING AFT LUG BUSHING. REPAIRED BUSHING PER EA B737-55-029632.

Part: STIFFENER — CORRODED (APU BAY) · airframe 36,471 hrs · 14,947 cycles

CORROSION ON AUXILIARY POWER UNIT INLET PLENUM DOUBLER (AFT STIFFENER). INSTALLED NEW STIFFENER PER AARD 51-10-05-1.

Part: WEDGE — CHAFED (LE SLAT) · airframe 36,471 hrs · 14,947 cycles

NUMBER 2 SLAT TRAILING EDGE WEDGE OUTBOARD LOWER SURFACE CHAFED. REPAIRED TRAILING EDGE WEDGE PER SRM 57-42-01-2R-6.

Part: WEDGE — CHAFED (LE SLAT) · airframe 36,471 hrs · 14,947 cycles

NUMBER 7 SLAT TRAILING EDGE WEDGE LOWER SURFACE CHAFED AT SEVERAL AREAS. REPAIRED WEDGE PER SRM 57-42-01-2R-6.

Part: BUSHING — CORRODED (RT HORIZ STAB) · airframe 36,471 hrs · 14,947 cycles

RIGHT HORIZONTAL STAB LUG BUSHINGS CORRODED AT STAB FRONT SPAR FORWARD UPPER TERMINAL FITTING BUSHING. REPAIRED BUSHING PER EA B737-55-029632.

Part: BUSHING — CORRODED (RT HORIZ STAB) · airframe 36,471 hrs · 14,947 cycles

RIGHT HORIZONTAL STAB LUG BUSHINGS CORRODED AT CENTER SECTION LOWER FORWARD TERMINAL FITTING FORWARD LUG BUSHING. REPAIRED BUSHING PER EA B737-55-029632.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

CORROSION ON BS 847 PRIMARY STRUCTURE FRAME BETWEEN STRINGERS 24 AND 25 LEFT. INSTALLED DOUBLER PER EA B737-53-029674.

Part: SUPPORT — CHAFED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CHAFE DAMAGE ON WING TO BODY SUPPORT, BODY STATION 545.6 AT OUTBOARD EDGE OF CUTOUT FOR PANEL 192DR AT LATCH BLOCK. REPAIRED DAMAGE PER EA B737-57-029653.

Part: PANEL — CRACKED (LT WING) · airframe 36,471 hrs · 14,947 cycles

LEFT WING PANEL 521NB HAS DISBOND/CRACK ON CORNER OF PANEL. REPAIRED PANEL 521NB PER EA B737-57-029668.

Part: STOP FITTING — CHAFED (DOOR) · airframe 36,471 hrs · 14,947 cycles

FORWARD AFT FRAME LOWER STOP PIN FITTING HAS CHAFE DAMAGE. REPAIRED CHAFE DAMAGE PER EA COMP-52-029590.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 36,471 hrs · 14,947 cycles

ACB FLOORBOARD INTERM REPAIR 28 INCHES AFT OF DOOR CUTOUT. FABRICATED AND INSTALLED NEW FLOORBOARD PER AARD 51-10-05-1.

Part: PIVOT ASSY — MISALIGNED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

MISALIGNMENT BETWEEN THE PIVOT LINK ASSAMBLY AND THE SEAT TRACK ALONG LEFT BUTTLINE 45.5. REPAIRED MISALIGNMENT PER EA B737-53-029605.

Part: RIB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

CORROSION ON INTERNAL SUPPORT RIB ON LAVATORY SERVICE PAN, BODY STATION 764. REPLACED RIB PER AARD 51-10-05-1.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

FUSELAGE EXTERNAL CROWN SKIN SCRATCH AT BODY STATION 727+16 BETWEEN STRINGERS 2 AND 3 LEFT. REPAIRED SCRATCH PER EA B737-53-029620.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CORROSION ON STRINGER CLIP BODY STATION 847 AND STRINGER 25 LEFT. REPLACED CLIP PER SRM 53-00-53-2R-5.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT FROM BODY STATION 727H+10 TO 727J, LEFT BUTTLINE 20 AND WATERLINE 156. REPAIRED FLOOR TO SIDEWALL SUPPORT PER SRM 53-00-53-2R-5.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

CORROSION ON KEELBEAM ATTACH CLIP AT BODY STATION 727I AND STRINGER 27 LEFT. REPLACED CLIP PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

FCB INTERCOSTAL ANGLE CRACKED AT BODY STATION 500G, LEFT BUTTLINE 24 AFT SIDE. REPLACED ANGLE PER AARD 51-00-05-1.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 36,471 hrs · 14,947 cycles

RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STATION 138.7, 26 INCHES AFT OF FRONT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11 AND CARD 51-92-02 NUMBER 4.

Part: STRAP — CORRODED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CORROSION ON ACB FLOOR SPLICE STRAP AT BODY STATION 887 AND LEFT BUTTLINES 1.5, 12 AND 14.5. REPLACED FLOOR STRAP PER SRM 51-40-02-0G.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT BODY STATIONS 767 TO 794, RIGHT BUTTLINE 21 AND WATERLINE 156. REPLACED SUPPORT PER AARD 51-00-05-1.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

FCB INTERCOSTAL SUPPORT ANGLE CRACKED ON AFT SIDE AT BODY STATION 500H, LEFT BUTTLINE 24 AND WATERLINE 152. REPLACED ANGLE PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

FCB INTERCOSTAL ANGLE CRACKED AT BODY STATION 500H, LEFT BUTTLINE 24 AND WATERLINE 156. REPLACED ANGLE PER AARD 51-00-05-1.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

CORROSION ON KEEL BEAM ATTACH INBOARD AND OUTBOARD CLIPS AT BODY STATION 717J AND STRINGER 27. REPLACED CLIPS PER AARD 51-00-05-1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT BODY STATION 251.6 AND STRINGER 24 LEFT LAP. REPAIRED DAMAGE PER EA 737-53-029560.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

LIGHTNING STRIKE DAMAGE ON LEFT FUSELAGE SKIN FASTENER AT BODY STATION 251.6, STRINGER 24 LEFT ON LOWER LAP SKIN MIDDLE ROW FASTENER. ACCOMPLISHED REPAIR PER EA B737-53-029560.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

SEAT TRACK HAS SEVERAL AREAS OF DAMAGE ON SEAT ATTACH TABS FROM BODY STATIONS 727C TO 727J, RIGHT BUTTLINE 25 AND WATERLINE 208. REPLACED TRACK PER AARD 51-00-05-1.

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

BODY STATION 727 FLOORBEAM UPPER SURFACE HAS 2 AREAS OF CHAFE DAMAGE AT NUT CLIP HOLES, WATERLINE 208 AT RIGHT BUTTLINES 4 AND 12.5. ACCOMPLISHED REPAIR PER EA 737-53-029553.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

CORROSION ON ACB FLOOR TIEDOWN TRACK BODY STATIONS 794 TO 853, RIGHT BUTTLINE 14 AND WATERLINE 156. REPAIRED TRACK PER SRM 53-00-53-2R-3 REPAIR 3.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT FROM BODY STATIONS 727F+10 AND 767, RIGHT BUTTLINE 20 AND WATERLINE 156. REPLACED SUPPORT PER AARD 51-10-05-1.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

MECHANICAL DAMAGE ON FLOOR INTERCOSTAL AT FLOOR PANEL HOLE BODY STATION 300, RIGHT BUTTLINE 45 AND WATERLINE 208. ACCOMPLISHED REPAIR PER EA B737-53-029547.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 36,471 hrs · 14,947 cycles

RIGHT HORIZONTAL STABILIZER INNER 4TH RIB CRACKED AT STATION 92.7. REPAIRED RIB PER SRM 55-10-09-2R-4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

LIGHTNING STRIKE DAMAGE ON LEFT FUSELAGE SKIN AT BODY STATION 250 AND STRINGER 24 LEFT LAP. REPAIRED DAMAGE PER EA 737-53-029560.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

SEAT TRACK HAS SEVERAL AREAS OF DAMAGE ON SEAT ATTACH TABS FROM BODY STATIONS 727C TO 867, RIGHT BUTTLINE 45 AND WATERLINE 208. REPLACED TRACK PER AARD 51-00-05-1.

Part: FLOORBOARD — OUT OF ALIGNMENT (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

FOUND FLOORBOARD HOLES DO NOT MATCH STRUCTURE FOR HOLE DRILLING ON FLOORBOARDS 815A8005-13, -8 AND -11. REPAIRED FLOORBOARDS PER EA B737-53-029509 REVISION A.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

CORROSION ON KEELBEAM ATTACH CLIP AT BODY STATION 727G AND STRINGER 27 LEFT. REPLACED CLIP PER AARD 51-00-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

FCB INTERCOSTAL ANGLE CRACKED AT BODY STATION 500G AND RIGHT BUTTLINE 24 FORWARD SIDE OF FRAME. REPLACED ANGLE PER AARD 51-00-05-1.

Part: WEDGE — CHAFED (LE SLAT) · airframe 36,471 hrs · 14,947 cycles

NUMBER 8 SLAT TRAILING EDGE WEDGE LOWER SURFACE CHAFFED IN SEVERAL AREAS. REPAIRED TRAILING EDGE WEDGE PER SRM 57-42-01-2R-6.

Part: STRAP — CORRODED (FLOOR PANEL) · airframe 36,471 hrs · 14,947 cycles

CORROSION ON CARGO FLOOR PANEL SPLICE STRAP. REPLACED SPLICE STRAP PER AARD 51-00-05-1.

Part: WEDGE — CHAFED (LE SLAT) · airframe 36,471 hrs · 14,947 cycles

NUMBER 6 SLAT TRAILING EDGE WEDGE LOWER SURFACE CHAFED IN SEVERAL AREAS. REPAIRED TRAILING EDGE WEDGE LOWER SURFACE PER SRM 57-42-01-2R-6.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 36,471 hrs · 14,947 cycles

LEFT VERTICAL STAB TO FUSELAGE PANEL SKATE ANGLE SUPPORT CHAFED IN SEVERAL AREAS. REPLACED SKATE ANGLE PER AARD 51-10-05-1.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 36,471 hrs · 14,947 cycles

RIGHT VERTICAL STAB TO FUSELAGE PANEL SKATE ANGLE CHAFING IN SEVERAL AREAS. REPLACED SKATE ANGLE PER AARD 51-10-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

FCB INTERCOSTAL ANGLE CRACKED AT BODY STATION 500G AND RIGHT BUTTLINE 24, AFT SIDE OF FRAME. REPLACED ANGLE PER AARD 51-00-05-01.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

FCB INTERCOSTAL ANGLE CRACKED AT BODY STATION 500G AND LEFT BUTTLINE 24, FORWARD SIDE OF FRAME. REPLACED ANGLE PER AARD 51-00-05-1.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CRACKED FASTENER HOLES ON INBOARD FORWARD AND OUTBOARD AFT SEAT TRACK FLANGE AT BODY STATION 727B AND RIGHT BUTTLINE 25. REPAIRED FLANGES PER EA B737-53-029511.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

4 HOLES CRACKED ON SEAT TRACK FLANGES AT BODY STATION 727B AND RIGHT BUTTLINE 45. REPAIRED FLANGES PER EA B737-53-029511.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

CORROSION FCB THRESHOLD WEB FROM BODY STATIONS 441 TO 492, RIGHT BUTTLINES 24 TO 30. REPLACED WEB PER AARD 51-00-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

FORWARD CARGO BAY, INTERCOSTAL ANGLE CRACKED AT BODY STATION 500H AND RIGHT BUTTLINE 24. REPLACED ANGLE PER AARD 51-10-05-1.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

CORROSION ON KEEL BEAM ATTACH CLIP AT BODY STATION 727H AND STRINGER 27 LEFT. REPLACED CLIP PER AARD 51-00-05-1.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

SEAT TRACK FLANGE OUTBOARD AFT FASTENER HOLE CRACKED AT BODY STATION 727B AND LEFT BUTTLINE 25. REPAIRD FLANGES PER EA B737-53-029511.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CORROSION ON STRINGER CLIP AT BODY STATION 867 AND STRINGER 25 LEFT. REPLACED CLIP PER SRM 51-40-02-0G.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

SEAT TRACK FLANGES CRACKED ON AFT OUTBOARD AND INBOARD FASTENER HOLES AT BODY STATION 727B AND LEFT BUTTLINE 45. REPAIRD FLANGES PER EA B737-53-029511.

Part: HINGE — CRACKED (LT MLG DOOR) · airframe 36,471 hrs · 14,947 cycles

LEFT MAIN LANDING GEAR INBOARD DOOR, DOOR SIDE AFT HINGE UPPER BOLT HOLE CRACKED. HINGE REPLACED PER ECO J1655AT-1.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CORROSION ON STRINGER CLIP AT BODY STATION 727I AND STRINGER 26 LEFT. REPLACED CLIP PER SRM 51-40-02-0G.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CORROSION ON STRINGER CLIP AT BODY STATION 727J AND STRINGER 26 LEFT. REPLACED CLIP PER SRM 51-40-02-0G.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT FROM BODY STATIONS 847 TO 867, RIGHT BUTTLINE 21 AND WATERLINE 156. FABRICATED AND REPLACED FLOOR TO SIDE WALL SUPPORT PER AARD 51-10-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

FORWARD CARGO BAY, INTERCOSTAL ANGLE IS CRACKED AT BODY STATION 500H AND RIGHT BUTTLINE 24 AFT SIDE. REPLACED ANGLE PER AARD 51-10-05-1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

EXTERNAL POWER SERVICE PANEL CUTOUT AFT EDGE CRACKED. INSTALLED DOUBLER PER SRM 53-10-15-2R-4.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

FORWARD CARGO BAY INTERCOSTAL ANGLE CRACKED AT BODY STATION 500E AND RIGHT BUTTLINE 24. REPLACED ANGLE (CLIP) PER SRM 51-40-02-0G.

Part: BRACKET — DAMAGED (RT PYLON) · airframe 36,471 hrs · 14,947 cycles

RIGHT ENGINE FIRE BARRIER BRACKET INBOARD SIDE IS DAMAGED JUST BELOW PYLON TORQUE BOX, 8 INCHES AFT OF EXHAUST NOZZLE SEPARATION FLANGE. REPLACED FIRE BARRIER BRACKET PER SRM 51-40-02-0G.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CORROSION ON STRINGER CLIP AT BODY STATION 907 AND STRINGER 27 LEFT. REPLACED CLIP PER AARD 51-10-05-1.

Part: STABILIZER — CORRODED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CORROSION ON G4 GALLY FLOOR STABLIZER FROM STATIONS 987 TO 1007 RIGHT BUTTINE 12 AND WATERLINE 208.5. REPLACED FLOOR STABLIZER PER SOPM 20-50-01.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

CORROSION ON FORWARD CARGO BAY RIGHT FLOOR TO BULKHEAD SUPPORT SURFACE, BODY STATION 500I, LEFT TO RIGHT BUTTLINE 24. REPLACED FORWARD CARGO BAY FLOOR TO BULKHEAD SUPPORT PER AARD 51-00-05-1.

Part: STABILIZER — CORRODED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CORROSION ON G4 GALLY FLOOR STABILIZER FROM STATIONS 987 TO 1007 LEFT BUTTLINE 12 AND WATERLINE 208.5. REPLACED STABILIZER FITTING ASSEMBLY PER SOPM 20-50-01.

Part: SUPPORT — CRACKED (LT WING) · airframe 36,471 hrs · 14,947 cycles

SEAL SUPPORT AT RSS 272 AT UPPER TRAILING EDGE PANEL IS CRACKED. REPLACED LEFT WING SEAL SUPPORT AT RSS 272 PER SRM 51-40-02-0G.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CORROSION ON STRINGER CLIP AT BODY STATION 807 AND STRINGER 26 LEFT. REPLACED CLIP PER SRM 51-40-05-0G, BOEING DWG 146A1263, SM 51-40-02-0G AND AARD 51-10-05-1.

Part: PLATE — DAMAGED (RT WING) · airframe 36,471 hrs · 14,947 cycles

RIGHT WING PANEL 651GB WIGGLE PLATE ATTACH FASTENERS ARE PULLED THROUGH. REPLACED PLATE PER SRM 51-40-02.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CORROSION ON STRINGER CLIP AT BODY STATION 787 AND STRINGER 26 LEFT. REPLACED CLIP PER SRM 51-40-05-0G, BOEING DWG 146A1262, SRM 51-40-02-0G AND AARD 51-10-05-1.

Part: SUPPORT — CRACKED (RT WING) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

SEAL SUPPORT AT RSS 272 INBOARD FIXED BULKHEAD ON RIGHT WING CRACKED. REPLACED SEAL SUPPORT PER SRM 51-40-02-0G.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

FORWARD CARGO BAY INTERCOSTAL ANGLE IS CRACKED AT BODY STATION 500E, LEFT BUTTLINE 24, FORWARD SIDE OF FRAME. REPLACED CLIP PER AARD 51-00-05-01.

Part: ANGLE — CRACKED (LT WING) · airframe 36,471 hrs · 14,947 cycles

LEFT WING TRAILING EDGE UPPER PANEL SUPPORT CRACKED AT INBOARD FLAP OUTBOARD DEFLECTION CONTROL ROLLER BEAM. REPLACED CRACKED ANGLE PER SRM 51-40-02-0G.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

RIGHT CREASE BEAM AT STATION 984, RIGHT BUTTLINE 48 AND WATERLINE 208 CORRODED. REPLACED SILL CHORD PER AARD 51-00-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CRACKED FLOOR INTERCOSTAL FROM BODY STATIONS 312 TO 328, RIGHT BUTTLINE 30 AND WATERLINE 208. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

BODY STATION 480 RIGHT FRAME IS CRACKED AT STRINGER 8 AIR CONDITIONING SUPPORT BRACKET. REPAIRED FRAME PER ECO J1159AE-0009.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

CORROSION ON ANGLE ATTACHED TO RIGHT NUMBER 1 DOOR MOP SEAL. REPLACED ANGLE PER AARD 51-00-05-1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

BODY STATION 480 LEFT FRAME IS CRACKED AT AIR CONDITIONING SUPPORT BRACKET. REPAIRED FRAME PER ECO J119AE-0008.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CRACKED INTERCOSTAL FROM BODY STATIONS 312 TO 328, LEFT BUTTLINE 6 AND WATERLINE 208. REPLACED INTERCOSTAL PER AARD 51-00-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CRACKED INTERCOSTAL FROM BODY STATIONS 328 TO 344, LEFT BUTTLINE 46 AND WATERLINE 208. REPLACED INTERCOSTAL PER AARD 51-00-05.

Part: VAPOR BARRIER — DAMAGED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

RIGHT AC BAY AFT BULKHEAD VAPOR BARRIER DAMAGED IN BAY 1. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04-2R-10 AND SRM 51-70-04-2R.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

CRACKED ANGLE AT FORWARD GALLEY DOORWAY, FORWARD FRAME (FORWARD SIDE) TO MOPSILL, BODY STATION 294.5, RIGHT BUTTLINE 54 AND WATERLINE 208. REPLACED CRACKED ANGLE PER AARD 51-00-05.

Part: VAPOR BARRIER — DAMAGED (FUSELAGE) · airframe 36,471 hrs · 14,947 cycles

RIGHT AC BAY AFT BULKHEAD VAPOR BARRIER DAMAGED IN BAY 2. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04-2R AND SRM 51-70-04-2R-10.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,471 hrs · 14,947 cycles

CORROSION ON SHEAR WEB AT MAIN CABIN FLOOR AT STATION 986 RIGHT BUTTLINE 32 AND WATERLINE 208. REMOVED WEB AND INSTALLED NEW WEB FROM BODY STATIONS 986 TO 1016 AND RIGHT BUTTLINES 32 TO 45 PER AARD 51-00-05.

Part: RIB — CRACKED (HORIZ STAB) · airframe 35,553 hrs · 14,636 cycles

LOWER FORWARD OUTBOARD CORNER OF RIB NUMBER 10 CRACKED (WHERE RIB OVERLAPS LOWER ANGLE OF FRONT SPAR). INSTALLED REPAIR STRAP PER EA B737-55-026751.

Part: CONNECTOR — LOOSE (CABIN) · airframe 34,940 hrs · 14,424 cycles

EMERGENCY LIGHT AT 24D INOPERATIVE. RE-SECURED CONNECTOR AT 24D SIDEWALL. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,536 hrs · 14,292 cycles

EMERGENCY LIGHTS FROM ROWS 15 TO 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM ROWS 15 TO 21. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,387 hrs · 11,920 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,387 hrs · 11,920 cycles

RIGHT AND WING OVERWING EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT WING OVERWING EXIT LIGHT. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,387 hrs · 11,920 cycles

ROW 13 THRU 21 EMERGENCY EXITS LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS FOR ROWS 13 THRU 21. OPS CHECKED NORMAL.

Part: TRANSMITTER — FAULTY (LT ENGINE) · airframe 27,252 hrs · 11,398 cycles

GUA - CREW REPORTED LEFT ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. ENGINE RETARDED THROTTLE AND LIGHT DID NOT EXTINGUISH. CREW SHUTDOWN ENGINE (SINGLE ENGINE TIME 5 MINUTES). EMERGENCY DECLARED FLIGHT RETURNED GUA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE OIL FILTER BYPASS TRANSMITTER AND OIL FILTER ELEMENT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TRANSMITTER — INOPERATIVE (OIL SYSTEM) · airframe 27,252 hrs · 11,398 cycles

GUA - CAPTAIN REPORTED LEFT ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED ON CLIMB. LEFT ENGINE SHUTDOWN PER QRH. SINGLE ENGINE TIME 5 MINUTES. EMERGENCY DECLARED RETURNED GUA LANDED WITHOUT INCIDENT. REPLACED CLOGGING TRANSMITTER AND LEFT ENGINE OIL FILTER ELEMENT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WINDOW — CRACKED (COCKPIT) · airframe 24,635 hrs · 10,277 cycles

MIA - INFLIGHT FLL-KIN. LEFT NUMBER 1 WINDOW CRACKED DURING FLIGHT. EMERGENCY DECLARED, LANDED MIA WITHOUT INCIDENT. REMOVED AND REPLACED LEFT NUMBER 1 WINDOW. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 24,103 hrs

ATL - EMERGENCY EXIT LIGHT AT ROW 13ABC MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT LIGHT AT ROW 13ABC.

Part: ACTUATOR — INOPERATIVE (HORIZ STAB) · airframe 20,840 hrs

MIA INFLIGHT T592/10MAR - BOTH CAPTAIN AND FIRST OFFICERS STABILIZER TRIM INOPERATIVE. RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED HORIZONTAL STABILIZER TRIM ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT ROW 27 HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT ROW 28 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT ROW 28 HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT ROW 27 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION

Part: LENS — BROKEN (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT ROW 27 LENS BROKEN. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT ROW 28 HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,837 hrs

MIA - EMERGENCY LIGHT AT SEAT ROW 14DEF DOOR SIDE WALL INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 14DEF DOOR SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT ROW 22DEF INOPERATIVE. SECURED PIN UNDER J BOX FOR EMERGENCY LIGHT AT LEFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT ROW 22D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 22D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LANYARD — OUT OF POSITION (SLIDE)

TUL - WHEN OPENED DOOR SLIDE DEPLOYED BUT RIGHT FORWARD DOOR WOULD NOT OPEN COMPLETELY DUE TO INFLATION BOTTLE LANYARD CAUGHT IN THE DOOR LATCH BRACKET. INSTALLED NEW EMERGENCY SLIDE PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

TUL - TWO EMERGENCY EXIT LIGHT BATTERY PACKS AT CABIN SIDEWALL DOES NOT HOLD CHARGE. REPLACED BATTERY PACKS AT CABIN SIDEWALL FOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: CONNECTOR — LOOSE (CABIN)

EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. RESEAT CONNECTOR AT 20D EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED--