N978AN

Part: ANGLE — CRACKED (BS 500H) · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED BAFFLE CLIP IN FORWARD CARGO COMPARTMENT ON AFT SIDE OF FRAME AT BS 500H AND S25R. REPLACED CLIP PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (BS 500H) · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED BAFFLE CLIP IN FORWARD CARGO COMPARTMENT ON FORWARD SIDE OF FRAME AT BS 500H AND S25R. REPLACED CLIP PER AARD 51-00-05-1.

Part: VAPOR BARRIER — CRACKED (BS 639) · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND MAIN LANDING GEAR WHEEL WELL VAPOR BARRIER AT BS 639 BETWEEN RBL 30 AND RBL 45. REPAIRED VAPOR BARRIER PER SRM 57-10-10-2R.

Part: BAFFLE — CRACKED (BS 500F-500G) · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED BAFFLE IN THE FORWARD CARGO COMPARTMENT BETWEEN BS 500F AND BS 500G AT S28R. REPLACED BAFFLE PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (BS 500G) · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FORWARD CARGO COMPARTMENT BAFFLE CLIP AFT SIDE OF FRAME AT BS 500G AND S23R. REPLACED CLIP PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (BS 500G) · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FORWARD CARGO COMPARTMENT BAFFLE CLIP FORWARD SIDE OF FRAME AT BS 500G AND S23R. REPLACED CLIP PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (BS 500D) · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FORWARD CARGO COMPARTMENT BAFFLE CLIP FORWARD SIDE OF FRAME AT BS 500D AND S23R. REPLACED CLIP PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (BS 500F) · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FORWARD CARGO COMPARTMENT BAFFLE CLIP FORWARD SIDE OF FRAME AT BS 500F AND S23R. REPLACED CLIP PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (BS 500E) · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FORWARD CARGO COMPARTMENT BAFFLE CLIP FORWARD SIDE OF FRAME AT BS 500E AND S23R. REPLACED CLIP PER AARD 51-00-05-1.

Part: EXPANSION JOINT — CRACKED (BS 540) · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED CABIN FLOOR EXPANSION JOINT AT BS 540 AND LBL 10. REPLACED EXPANSION JOINT PER AARD 51-00-05-1.

Part: EXPANSION JOINT — CRACKED (BS 540) · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED CABIN FLOOR EXPANSION JOINT AT BS 540 AND RBL 10. REPLACED EXPANSION JOINT PER AARD 51-00-05-1.

Part: MOUNT — CORRODED (BS 312) · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON TIE DOWN MOUNT CLIP AT BS 312 AND LBL 60. REPLACED TIE DOWN MOUNT CLIP PER SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 344-366) · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED CABIN FLOOR INTERCOSTAL BETWEEN BS 344 AND BS 366 AT RBL 6. REPLACED INTERCOSTAL PER AARD 51-00-05-1 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED CABIN FLOOR INTERCOSTAL BETWEEN BS 312 AND BS 328 AT RBL 33. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 727 AND BS 727H AT S25L. REPLACED TRANSITION PANEL PER 51-00-05-1. SUPPLEMENTAL REPORT: ENGINEERING REVIEWED THIS EVENT AND DETERMINED THE CORRECT LEVEL WAS LEVEL 1 NOT LEVEL 2. SECTION 7 CORROSION LEVEL FIELD WAS CORRECTED ACCORDINGLY.

Part: CHANNEL — CORRODED (BS 500I) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT "L" CHANNEL AT FR 500I BETWEEN S27L AND S27R. REPLACED "L" CHANNEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 727H AND BS 787 AT S25L. REPLACED TRANSITION PANEL PER 51-00-05-1. SUPPLEMENTAL REPORT: ENGINEERING REVIEWED THIS EVENT AND DETERMINED THE CORRECT LEVEL WAS LEVEL 1 NOT LEVEL 2. SECTION 7 CORROSION LEVEL FIELD WAS CORRECTED ACCORDINGLY.

Part: TRANSITION PANEL — CORRODED (BS 727H-787) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 727H AND BS 787 AT S23R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 727 AND BS 727H AT RBL 27. REPLACED TRANSITION PANEL PER AARD 51-00-05-1. SUPPLEMENTAL REPORT: ENGINEERING REVIEWED THIS EVENT AND DETERMINED THE CORRECT LEVEL WAS LEVEL 1 NOT LEVEL 2. SECTION 7 CORROSION LEVEL FIELD WAS CORRECTED ACCORDINGLY.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 500A AND BS 500I AT S25R. REPLACED TRANSITION PANEL PER 51-00-05-1. SUPPLEMENTAL REPORT: ENGINEERING REVIEWED THIS EVENT AND DETERMINED THE CORRECT LEVEL WAS LEVEL 1 NOT LEVEL 2. SECTION 7 CORROSION LEVEL FIELD WAS CORRECTED ACCORDINGLY.

Part: PAD — CORRODED (GIRT BAR) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON GIRT BAR RETAINER PAD AT BS 344 AND LBL 60. REPLACED PAD PER SRM 51-40-02.

Part: ANGLE — CORRODED (BS 1014.5) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN WET AREA "Z" ANGLE AT BS 1014.5 AND LBL 29. REPLACED "Z" ANGLE PER AARD 51-00-05-1 AND SRM 51-40-02.

Part: SHIELD — CORRODED (BS 767) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANISITION PANEL SHIELD AT BS 767 AND RBL 21. REPLACED SHIELD PER AARD 51-00-05-1.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN WET AREA FLOOR BEAM AT BS 986 AND LBL 17. REPAIRED FLOOR BEAM PER EA 301074.

Part: ANGLE — CORRODED (BS 977-988) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN WET AREA INNER CREASE ANGLE BETWEEN BS 977 AND BS 988 BETWEEN RBL 49 AND RBL 53. REPLACED CREASE ANGLE PER AARD 51-00-05-1.

Part: ANGLE — CORRODED (BS 992) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN WET AREA "Z" ANGLE AT BS 992 AND LBL 29. REPLACED "Z" ANGLE PER AARD 51-00-05-1

Part: ANGLE — CORRODED (BS 951) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN WET AREA INNER CREASE ANGLE AT BS 951 BETWEEN RBL 52 AND RBL 55. REPLACED CREASE ANGLE PER AARD 51-00-05-1.

Part: ANGLE — CORRODED (BS 990-992) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN WET AREA INNER CREASE ANGLE BETWEEN BS 990 AND BS 992 BETWEEN RBL 45 AND RBL 47. REPLACED CREASE ANGLE PER AARD 51-00-05-1.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN WET AREA FLOOR BEAM AT BS 986 AND LBL 45. REPAIRED FLOOR BEAM PER EA 301074.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN WET AREA FLOOR BEAM AT BS 986 BETWEEN LBL 39 AND LBL 41. REPAIRED FLOOR BEAM PER EA 301074.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN WET AREA FLOOR BEAM AT BS 947 AND BL 0. REPAIRED FLOOR BEAM PER EA 300873 AND SRM 53-00-51-2R.

Part: FLOORBEAM — CORRODED (BS 792) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT BS 792 AND RBL 24. REPLACED FLOOR SUPPORT ANGLE PER AARD 51-00-05-1.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN WET AREA FLOOR BEAM AT BS 986 AND LBL 9. REPAIRED FLOOR BEAM PER EA 301074 AND SRM 53-70-51-2R.

Part: WEB — CORRODED (BS 842) · corrosion level 2 · airframe 55,003 hrs · 22,655 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO DOOR CUT OUT FLOOR SUPPORT WEB AT BS 842 AND RBL 27. REPLACED WEB PER AARD 51-00-05-1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,282 hrs · 21,442 cycles

LEFT AFT EMERGENCY LIGHT ASSEMBLY WAS INOPERATIVE. REPLACED THE LIGHT ASSY IAW AMM 33-51-01. FUNCTIONAL CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,272 hrs · 21,006 cycles

ROW 15D SIDEWALL LIGHT ON EMERGENCY EXIT DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE LAMPS IAW MM 33-21-00, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: FLASHLIGHT ASSY — INOPERATIVE (FWD CABIN) · airframe 50,686 hrs · 20,755 cycles

L1 JUMPSEAT AISLE POSITION EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT AND HOLDER ASSEMBLY IAW MM 25-64-00. OPS CHECKED GOOD.

Part: SLIDING WINDOW — DELAMINATED (COCKPIT) · airframe 49,278 hrs · 20,132 cycles

THE R2 SLIDING WINDOW WAS FOUND DELAMINATED. REMOVED AND REPLACED THE SLIDING WINDOW ASSY IAW MCM 56-94-02.

Part: SLIDING WINDOW — FAILED (COCKPIT) · airframe 49,278 hrs · 20,132 cycles

R2 WINDOW SHATTERED. REMOVED AND REPLACED THE R2 COCKPIT SLIDING WINDOW ASSEMBLY IAW MCM 56-94-02. AIRCRAFT WAS GROUNDED.

Part: SWITCH — STUCK (EMERGENCY LIGHTS) · airframe 49,175 hrs · 20,080 cycles

AFT GALLEY EMERGENCY EXIT LIGHT REMAINS ON AND WILL NOT TURN OFF. FOUND AFT FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH STUCK. FREED THE SWITCH AND CYCLED SEVERAL TIMES. THE EMERGENCY LIGHTS TESTED NORMAL IAW AMM 33-51-00.

Part: BAR — OUT OF POSITION (R1 DOOR) · airframe 49,117 hrs · 20,055 cycles

AIRCRAFT NOT GROUNDED. R1 DOOR SLIDE ACTIVATION BAR OUT OF HOLDERS. RESECURED AND STOWED R1 DOOR SLIDE ACTIVATION BAR IN HOLDERS PER MM 25-66-01.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 49,102 hrs · 20,047 cycles

CRACK IN LOWER SKIN OF LEFT HORIZONTAL STABILIZER AT HSS 147.90, SEVERAL INCHES AFT OF FRONT SPAR. REPAIRED THE DOUBLER IAW SRM 55-10-01-2R-11.

Part: LENS — MISSING (EXIT SIGN) · airframe 48,267 hrs · 19,673 cycles

THE AIRCRAFT WAS NOT GROUNDED. DOOR EMERGENCY EXIT SIGN COVER IS MISSING. THE SIGN COVER WAS PLACED ON NEF. REMOVED AND REPLACED EMERGENCY EXIT SIGN AT THE L4 DOOR PER AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: COFFEEMAKER — NOT SEATED (GALLEY) · airframe 47,823 hrs · 19,511 cycles

COFFEEMAKER NR 4 IN THE AFT GALLEY PRODUCED SMOKE & STEAM AFTER TAKEOFF. SEATED THE COFFEEMAKER IAW AMM 25-32-00. LEAK AND OPERATIONAL CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 47,240 hrs · 19,242 cycles

AIRCRAFT WAS NOT GROUNDED. LEFT MAIN TANK AFT FUEL PUMP LOW PRESSURE LIGHT DISAGREE WITH PUMP STATUS. TRANSFERRED FUEL INTO LEFT WING FUEL TANK, PRIMED LEFT MAIN TANK AFT FUEL PUMP IAW AMM 28-22-41. LOW PRESSURE LIGHT WENT OUT AND PUMP OPERATES PROPERLY. OPERATIONAL CHECK GOOD. (CLOSED)

Part: LENS — CRACKED (CABIN) · airframe 47,078 hrs · 19,175 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT R2 DOOR HAS A CRACKED LENS COVER. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 47,060 hrs · 19,168 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT L1 DOOR OUTBOARD SEAT FAILED TEST. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 47,060 hrs · 19,168 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT L1 DOOR INBOARD SEAT FAILED TEST. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: CONTROL MODULE — INOPERATIVE (BOOST PUMP SWITC) · airframe 46,460 hrs · 18,929 cycles

DURING CRUISE, THE RIGHT CENTER FUEL PUMP DID NOT FULLY SUPPLY THE NR 2 ENGINE FUEL FLOW. RIGHT MAIN TANK QUANTITY DECREASES WITH CENTER FUEL AND BOTH CENTER PUMPS ON. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE ACCOMPLISHED FIM 28-21-00, CHECKED PUMP OPERATIONS ON GROUND. CHECKED HISTORY. SYSTEM CHECKED NORMAL. MAINTENANCE FOUND THE LEFT CENTER BOOST PUMP SWITCH INOPERATIVE. REMOVED AND REPLACED THE FUEL CONTROL MODULE ASSEMBLY.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,044 hrs · 17,518 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN HAS TWO CRACKS ALONG RIB AREA. RIB APPROX 70" FROM INBD END , SEAL & BETWEEN 22" & 33" FROM FWD SPAR. INSTALLED DOUBLER & FILLERS IAW 55-10-01-2R-11.

Part: TERMINAL BLOCK — BROKEN (ZONE 200) · airframe 42,710 hrs · 17,382 cycles

EMERGENCY EXIT LIGHT, NOT ARMED, LIGHT NOT ILLUMINATED WITH SWITCH IN OFF POSITION, OVERHEAD PANEL. R & R TERMINAL BLOCK TB505 IAW AMM STANDARD & PRACTICE 20-90-15. EMER LIGHT INDICATION OPERATIONS CHECKED OK.

Part: SIGN — DAMAGED (CABIN) · airframe 41,478 hrs · 16,887 cycles

EMERGENCY EXIT SIGN IN G4 GALLEY BY R2 DOOR WAS HANGING DOWN & DAMAGED. R & R EXIT SIGN IAW AMM 33-51-01.

Part: CONNECTOR — BROKEN (CABIN) · airframe 39,206 hrs · 15,991 cycles

SEAT 9 EMER LIGHT INOPERATIVE. REPLACED EMER LIGHT CONNECTOR AT SIDEWALL. OPERATIONS CHECKED NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 39,206 hrs · 15,991 cycles

EMERGENCY LIGHT AT SEAT ROW 24DEF HAS A BROKEN WIRE AT THE SEAT ROW TO FLOOR TRACK CONNECTOR. REPLACED EMER LIGHT CONNECTOR AT SEAT LEG. OPERATIONS CHECKED NORMAL.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · corrosion level 2 · airframe 37,152 hrs · 15,185 cycles

CORROSION ON RT MLG FWD TRUNNION SUPPORT FITTING AT OTBD LUG OTBD FACES & INBD LUG INBD FACES. ACCOMPLISHED REPAIR IAW SRM 57-20-90-2R-2.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · corrosion level 2 · airframe 37,152 hrs · 15,185 cycles

CORROSION ON LT MLG FWD TRUNNION SUPPORT FITTING AT INBD LUG INBD FACES & OTBD LUG OTBD FACES. ACCOMPLISHED REPAIR IAW SRM 57-20-90-2R-2.

Part: REVEAL — GOUGED (CARGO BAY) · airframe 36,640 hrs · 14,991 cycles

GOUGE IN FWD REVEAL PANEL OF AFT CARGO DOOR STRUCTURE. INSTALLED AFT CARGO DOOR CUTOUT FWD REVEAL IAW AARD 51-10-5 & IPC 53-11-10-48A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,640 hrs · 14,991 cycles

CORROSION ON FLOORBOARD SUPPORT AT BS 887. R & R FLOORBOARD SUPPORT.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 36,640 hrs · 14,991 cycles

RT FRAME FASTENER HOLE THAT ATTACHES TO THE TRANSITIONAL PANEL AT BS 727J IS ELONGATED. OVERSIZED HOLE IAW EA B737-53-031774.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,640 hrs · 14,991 cycles

CORROSION ON TRANSITION PANEL IN AFT CARGO INBD & AFT OF DOOR. REPLACED TRANSITION PANEL.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,640 hrs · 14,991 cycles

TRANSITION PANEL CORRODED IN AFT CARGO, LT HAND STATION 847. REPLACED TRANSITION PANEL.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,640 hrs · 14,991 cycles

TRANSITION PANEL HAS CORROSION AT FROM STATIONS 727+10 TO 847 LT. REPLACED TRANSITION PANEL.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,640 hrs · 14,991 cycles

CORROSION AROUND NUT PLATES ON LT TRACK FROM BS 771 TO 774 & LBL 16. INSTALLED REPAIR STRAP IAW EA B737-53-031785.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 36,640 hrs · 14,991 cycles

STATION 727B LONGITUDINAL FLOOR BEAM FLANGE CRACKED. ACCOMPLISHED REPAIR IAW EA B737-53-031789.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,640 hrs · 14,991 cycles

AFT CARGO TRANSITION PANEL HAS CORROSION IN NUMEROUS AREAS ON RT HAND SIDE FROM STATIONS 767 TO 727I-H. REPLACED TRANSITION PANEL.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,640 hrs · 14,991 cycles

TRANSITION PANEL CORRODED FROM STATIONS 727F TO 760 LT. REPLACED TRANSITION PANEL.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,640 hrs · 14,991 cycles

FORWARD CARGO THRESHOLD WEB CORRODED. REPLACED WEB IAW AARD 51-10-05-1 & DRAWING 143A8122.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,640 hrs · 14,991 cycles

INTERCOSTAL BETWEEN BS 747 TO 767 AT STRINGER 25 RT CORRODED AROUND NUTPLATE HOLES ON UPPER FLANGE. INSTALLED NEW INTERCOSTAL IAW AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · airframe 36,640 hrs · 14,991 cycles

CARGO TRANSITION PANEL CORRODED. REPLACED CARGO TRANSITION PANEL.

Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 36,640 hrs · 14,991 cycles

CRACKED OTBD LOWER END OF VAPOR BARRIER WEB BAY 7L. INSTALLED VAPOR BARRIER WEB FULL CROSS BRACE REPAIRS TO BAYS 5L, 7L, & 8L IAW SRMSUP 57-10-10-2R-2 REPAIR 2.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,640 hrs · 14,991 cycles

BS 1088 BULKHEAD AUXILIARY POWER UNIT PLENUM CUTOUT, OTBD VERTICAL STIFFENER CORRODED. REPLACED OTBD VERTICAL STIFFENER IAW AARD 51-00-05-1 & DRAWING 148A0924.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 36,640 hrs · 14,991 cycles

RT NR 1 DOOR CUTOUT CRACKED AT FRAME ATTACH FASTENER TO CREASE ANGLE, STATION 312. INSTALLED DOUBLER REPAIR IAW SRM 51-70-11-2R.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,640 hrs · 14,991 cycles

CRACKED FLOOR SUPPORT BETWEEN STATIONS 277 & 291.5 AT BL 0. INSTALLED NEW INTERCOSTAL IAW AARD 51-10-05.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,640 hrs · 14,991 cycles

RT HAND CREASE ANGLE CORRODED AT STATION 310. REPLACED CREASE ANGLE IAW AARD 51-10-05.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,640 hrs · 14,991 cycles

CABIN FLOOR SUPPORT CRACKED FROM STATIONS 328 TO 344 & LBL 40. REPLACED FLOOR SUPPORT IAW AARD 51-10-05.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,640 hrs · 14,991 cycles

CRACK IN BS 727B & RBL 45.5 LONGITUDINAL FLOOR BEAM FLANGE. ACCOMPLISHED REPAIR IAW EA B737-53-031789.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 36,640 hrs · 14,991 cycles

CORROSION ON CARGO TIEDOWN TRACK RT HAND FROM STATIONS 807 TO 847. REPLACED TIEDOWN TRACK IAW AARD 51-10-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,640 hrs · 14,991 cycles

CRACKED FLOOR SUPPORT BETWEEN STATIONS 312 & 328 AT LBL 40. INSTALLED NEW INTERCOSTAL IAW AARD 51-10-05.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,640 hrs · 14,991 cycles

CRACK IN LONGITUDINAL FLOOR BEAM AT BS 727B & RBL 24.75. INSTALLED REPAIR IAW EA B737-53-031789.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,640 hrs · 14,991 cycles

STATION 727B & LBL 24.75 LONGITUDINAL FLOOR BEAM FLANGE CRACKED. ACCOMPLISHED REPAIR IAW EA B737-53-031789.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,640 hrs · 14,991 cycles

CRACKED FLOOR SUPPORT BETWEEN STATIONS 312 & 328 AT RBL 26. INSTALLED NEW INTERCOSTAL IAW AARD 51-10-05.

Part: SKIN — GOUGED (FUSELAGE) · airframe 36,640 hrs · 14,991 cycles

SCRATCH WITH GOUGE IN LOWER FS AT STATION 450 BETWEEN STRINGERS 25 & 26 RT. CUTOUT DAMAGE & INSTALLED EXTERNAL DOUBLER IAW SRM 53-00-01-2R.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,640 hrs · 14,991 cycles

CORROSION ON RT WEB IN APU AT AFT END OF INLET PLENNUM CUTOUT APPROXIMATELY STATION 1129. INSTALLED NEW STIFFENER IAW AARD 51-00-05-1 & DRAWING 148A8650.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,640 hrs · 14,991 cycles

CORROSION ON UPPER FLANGE OF 986.5 FLOOR BEAM & RBL 43. R & R CORROSION & REPLACED 986.5 FLOOR BEAM T CAP IAW EA B737-53-031764.

Part: STRUCTURE — CORRODED (CENTER WING) · corrosion level 2 · airframe 36,640 hrs · 14,991 cycles

CORROSION ON CENTER WING BOX LOWER SKIN FWD SECTION LT SIDE, STRINGERS 21 TO 22 LT & STATION 540.5. ACCOMPLISHED CORROSION REMOVAL IAW SRM 51-10-02 & REPAIR IAW EA B737-57-031846.

Part: STRUCTURE — CORRODED (CENTER WING) · corrosion level 2 · airframe 36,640 hrs · 14,991 cycles

CORROSION DISCOVERED ON CENTER WING BOX LOWER SKIN AT STATION 540.5 & STRINGER 21 & 22 RT. ACCOMPLISHED CORROSION REMOVAL IAW SRM 51-10-02 & REPAIRED IAW EA B737-57-031846.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 32,363 hrs · 13,478 cycles

DEN - INFLIGHT ORD-SFPO. CREW REPORTED AUXILIARY POWER UNIT SHUTDOWN WITH RIGHT INTEGRATED DRIVE GENERATOR ON MEL. EMERGENCY DECLARED FLIGHT DIVERTED DEN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NO EXTERNAL LEAKS HOWEVER OIL CONSUMPTION WAS HIGH. PLACARD APU INOPERATIVE PER MEL. REPLACED RIGHT ENGINE INTEGRATED DRIVE GENERATOR. REPLACED APU (MPN 351A10001) AT ORD ON 05/30/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,700 hrs · 12,896 cycles

SKIN CORRODED AT STATION 888 TO 947 STRINGERS 21 TO 27 LEFT. ACCOMPLISHED REPAIR PER EA 020420.

Part: FIRE DETECTOR — FAULTY (RT ENGINE) · airframe 29,896 hrs · 12,618 cycles

LAS - CREW REPORTED RIGHT ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED LAS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LOWER FAN FIRE WARNING AND CORE LEFT AND RIGHT FIRE WARNING / DETECTORS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,245 hrs · 11,490 cycles

ROW 10 ABC OVERHEAD BIN MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR ROW 10 ABC OVERHEAD BIN MOUNTED EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: STRUCTURE — DENTED (VERTICAL STAB) · airframe 24,915 hrs · 10,428 cycles

DENT ON VERTICAL STABILIZER LEADING EDGE 2 INCHES BY .5 INCH BY ONE 16TH INCH DEEP AT LEADING EDGE STATION 252. REWORKED DENTED AREA ON STABILIZER LEADING EDGE STATION 252 TO WITHIN LIMITS GIVEN IN SRM 55-30-01-1A.

Part: PUSHROD — BROKEN (NLG DOOR) · airframe 24,895 hrs · 10,421 cycles

AFTER GEAR RETRACTION A STRONG VIBRATION AND LOUD NOISE COMING FROM THE NOSE GEAR AREA. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. FOUND RIGHT NOSE GEAR DOOR PUSHROD BROKEN. REPLACED THE ROD.

Part: LIGHT — DAMAGED (CABIN) · airframe 24,781 hrs · 10,375 cycles

EMERGENCY LIGHT AT SEAT 24D DAMAGED. REPLACED LIGHT ASSEMBLY AT SEAT 24D.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 22,537 hrs · 9,415 cycles

BWI - DURING CLIMBOUT FIRST OFFICER RIGHT NUMBER 2 WINDSHIELD CRACKED. RETURNED BWI WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FIRST OFFICER RIGHT NUMBER 2 WINDOW. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 20D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 18,774 hrs

MIA - EMERGENCY LIGHT AT SEAT 5E MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,774 hrs

MIA EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,593 hrs · 7,699 cycles

TUL - EMERGENCY SEAT MOUNTED LIGHTS AT SEAT ROWS 7 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY SEAT MOUNTED LIGHTS AT SEAT ROWS 7 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,593 hrs · 7,699 cycles

TUL - EMERGENCY SEAT MOUNTED LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY SEAT MOUNTED LIGHTS AT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,593 hrs · 7,699 cycles

TUL - EMERGENCY SEAT MOUNTED LIGHTS AT SEAT 19A INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY SEAT MOUNTED LIGHTS AT SEAT 19A. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT OVERWING RIGHT EXIT DOOR INOPERATIVE. REPLACED SWITCH FOR EMERGENCY LIGHT AT OVERWING RIGHT EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.