N705AS

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 52,006 hrs · 29,320 cycles

F/A REPORTS EXIT SIGN NEXT TO 4-25 GALLEY AREA IS MISSING. ACFT GROUNDED. LOCATED AND REINSTALLED L2 GALLEY MOUNTED EXIT SIGN COVER REF AMM 33-51-11. NO FURTHER DEFECTS NOTED.

Part: LENS — MISSING (L2 DOOR) · airframe 51,986 hrs · 29,300 cycles

L2 EXIT DOOR LIGHT COVER MISSING. ACFT GROUNDED. INSTALLED NEW LIGHT COVER ON L-2 DOOR EMERGENCY EXIT LIGHT.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 51,980 hrs · 29,297 cycles

AFT GALLEY SIGN, ACFT LEFT, MISSING COVER. ACFT GROUNDED. REPLACED EXIT LIGHT LENS AT L2 DOOR.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 51,275 hrs · 28,889 cycles

LEFT WING INBD MID FLAP INBD UPPER SKIN INBD EDGE IS CHAFED. ACFT GROUNDED. REPAIRED LT WING INBD MIDFLAP INBD UPPER SKIN IAW SRM 57-53-01-2R3.

Part: FRAME — CRACKED (BS 360) · airframe 51,275 hrs · 28,889 cycles

BS 360, FRAME WEB CRACKED BETWEEN S12-13L. ACFT GROUNDED. REPAIRED THE FRAME IAW EA 400-53EA-13352.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 50,143 hrs · 28,229 cycles

AFT GALLEY EXIT SIGN LENS COVER BROKEN. ACFT GROUNDED. REMOVED & INSTALLED NEW EXIT SIGN COVER PLATE LT AFT GALLEY NEXT TO L2 DOOR.

Part: CARGO TRACK — CRACKED (BS 767) · airframe 48,757 hrs · 27,381 cycles

AFT CARGO BAY RBL 13.8 CARGO TRACK CRACKED AT STA 767. R & R CARGO TRACK SECTION IAW SRM 53-00-53-2R-2.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 48,116 hrs · 26,986 cycles

LT INBD MIDFLAP UPPER SURFACE AT INBD EDGE IS CHAFED ON A PREVIOUS BLEND OUT. ACFT GROUNDED. REPAIRED DAMAGE TO UPPER SURFACE OF LT MIDFLAP IAW SRM 57-53-01-2R-3, REP 3.

Part: ANGLE — CORRODED (RT MLG WW) · corrosion level 2 · airframe 48,116 hrs · 26,986 cycles

RT MLG WW LOWER AFT ANGLE HAS EXFOLIATING CORROSION ON LWR OTBD SURFACE. R & R ANGLE.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 48,116 hrs · 26,986 cycles

LEFT VERTICAL STAB TO FUSELAGE SKATE ANGLE CHAFED BETWEEN FWD AND AFT ATTACH LUG GROUNDED. REPAIRED DAMAGE TO SKATE ANGLE IAW EA 400 53EA 10673.

Part: STRUCTURE — CORRODED (MLG WW) · airframe 48,116 hrs · 26,986 cycles

MLG WW LOWER AFT STRUCTURE HAS SEVERAL AREAS OF CORROSION AND BARE METAL. ACFT GROUNDED. REMOVED DAMAGED. FOUND TO BE OUT OF LIMITS. FABRICATED NEW STRUCTURE AND REPLACED IAW SRMS 53-60-71-1A-1, 51-40-02-0G-0 AND 51-40-05.

Part: PANEL — CHAFED (RT NACELLE) · airframe 48,116 hrs · 26,986 cycles

RT PYLON PANEL 5829R CUT OUT HAS A CHAFED SPOT (INTERIOR SIDE). ACFT GROUNDED. REPAIR NR 2 ENGINE PYLON ACCESS DOOR LAND (PANEL 5829R LOCATION) DOUBLER IAW ASA EA 400-54EA-10681.

Part: BULKHEAD — CORRODED (RT MLG WW) · airframe 48,116 hrs · 26,986 cycles

RIGHT MLG WW BULKHEAD HAS SEVERAL AREAS OF CORROSION AFT SIDE. ACFT GROUNDED. REPLACED BULKHEAD WEB IAW ASA EA 400-53EA-10613.

Part: BULKHEAD WEB — CORRODED (LT MLG WW) · airframe 48,116 hrs · 26,986 cycles

LEFT MLG WW BULKHEAD WEB HAS SEVERAL AREAS OF CORROSION ON AFT SIDE. ACFT GROUNDED. REPAIRED BULKHEAD WEB IAW EA 400-53EA-10615, REV NEW.

Part: DOUBLER — CRACKED (BS 1196) · airframe 48,116 hrs · 26,986 cycles

APU EXHAUST TAIL CONE INTERNAL, LT SIDE AT AFT FAIRING ATTACH SKIN DOUBLER TORN. ACFT GROUNDED. REMOVED SKIN DOUBLER (SEAL PLATE) FABRICATED NEW AND INSTALLED IAW 51-40-02-0G-0 AND 51-40-05-0G-0.

Part: STRUCTURE — DENTED (LT WING TIP) · airframe 48,116 hrs · 26,986 cycles

LEFT AFT WING TIP DAMAGED AT STATIC WICK. ACFT GROUNDED. R & R MID AND AFT WING TIPS IAW AMM 57-21-11-404-013, SEAM C.

Part: ANGLE — CHAFED (FLAP TRACK) · airframe 48,116 hrs · 26,986 cycles

LEFT WING UPPER T/E PANEL INBD OF THE NR 3 FLAP TRACK FAIRING, ANGLE IS CHAFED. ACFT GROUNDED. REMOVED CHAFED ANGLE AND REPLACED WITH NEW ANGLE IAW SRM 51-740-02-0G-0.

Part: STRUCTURE — DENTED (LT WING) · airframe 48,116 hrs · 26,986 cycles

LEFT AFT WING TIP DAMAGED AT STATIC WICK. ACFT GROUNDED. R & R MID AND AFT WING TIPS IAW AMM 57-21-11-404-013.

Part: BULKHEAD WEB — CRACKED (RT MLG WW) · airframe 48,116 hrs · 26,986 cycles

RT WW UPPER WEB IS TORN. ACFT GROUNDED. REMOVED, FABRICATED NEW RT WHEEL WELL UPPER WEB AND INSTALLED IAW SRM 51-40-02 AND EA 400-53EA-10617.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 48,116 hrs · 26,986 cycles

VERTICAL STAB TO FUSELAGE SKATE ANGLE CHAFED BETWEEN DORSAL T/E STAB FORWARD ATTACH LUG. ACFT GROUNDED. REMOVED DAMAGED SKATE ANGLE, FABBED NEW ANGLE AND INSTALLED IAW SRM 51-40-02-0G-0 AND 51-40-05-0G-0.

Part: ACCESS PANEL — CHAFED (VERTICAL STAB) · airframe 48,116 hrs · 26,986 cycles

LEFT VERTICAL STAB ACCESS PANEL 4503 CHAFED ON FORWARD LOWER CORNER. ACFT GROUNDED. FABRICATED NEW ACCESS PANEL FACTORY DOUBLER AND INSTALLED IAW SRM 51-40-05-0G-0 AND 51-40-02-0G-0.

Part: SUPPORT ANGLE — CRACKED (BS 278) · airframe 48,116 hrs · 26,986 cycles

RT PYLON OTBD SUPPORT ANGLE, STA 278 CRACKED, FABRICATED NEW SUPPORT ANGLE AT STA 278.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 48,116 hrs · 26,986 cycles

RT INBD FORE FLAP UPPER SURFACE CHAFED. ACFT GROUNDED. REPAIRED RT INBD FOREFLAP UPPER SURFACE CHAFED IAW SRM 51-70-10-2R-4, REPAIR 4, PAGE 1.

Part: FLOOR SUPPORT — CORRODED (BS 727F) · corrosion level 2 · airframe 48,116 hrs · 26,986 cycles

AFT CARGO FLOORBOARD SPLICE TEE AT BS 727F IS CORRODED. FABRICATED NEW FLOORBOARD SPLICE TEE IAW SRM 51-40-02-0G-0.

Part: STRUCTURE — CHAFED (NR 4 SLAT) · airframe 48,116 hrs · 26,986 cycles

CHAFE ON LOWER FLANGE FOUND TO BE OUT OF LIMITS ON NR 2 SLAT. ACFT GROUNDED. REPAIRED IAW SRM 57-43-01-2R-6, REPAIR FIG 201.

Part: SKIN — DENTED (SPOILER) · airframe 48,116 hrs · 26,986 cycles

SPOILER HAS TWO PROTRUDING DENTS ON UPPER SURFACE. ACFT GROUNDED. REPLACED SPOILER IAW SRM 51-20-10-2R-4.

Part: ANGLE — CORRODED (RT MLG WW) · corrosion level 2 · airframe 48,116 hrs · 26,986 cycles

RT MLG WW LOWER FWD ANGLE HAS CORROSION. R & R ANGLE.

Part: ANGLE — CORRODED (RT MLG WW) · corrosion level 2 · airframe 48,116 hrs · 26,986 cycles

RT MLG WW NR 2 LWR CHORD SEGMENT HAS SEVERAL AREAS OF CORROSION. R & R NR 2 LWR CHORD SEGMENT IAW SRM 51-40-02, W 2.55, O .062, R .045, L 3.30, D .017.

Part: STOP FITTING — CRACKED (GALLEY DOOR) · airframe 48,116 hrs · 26,986 cycles

RT FWD GALLEY SERVICE DOOR R1 AFT SIDE STOP PIN FITTING NR 3 UPPER SIDE OF FITTING EVIDENCE OF A CRACK ON DOOR PAN FRAME. ACFT GROUNDED. REPAIRED CRACK AT R1 GALLEY SERVICE DOOR FWD FRAME PAN IAW EA 400, 52EA 10694.

Part: RETAINER — CHAFED (BS 1022-1048) · airframe 48,116 hrs · 26,986 cycles

LEFT VERTICAL ACCESS PANEL 9501, LOWER RETAINING FLANGE CHAFED REMOVED, FABRICATED AND INSTALLED NEW RETAINER IAW SRM 53-30-01.

Part: PANEL — CHAFED (BS 1156) · airframe 48,116 hrs · 26,986 cycles

RT HORIZONTAL BOW TIE PANEL CHAFED. ACFT GROUNDED. R & R BOW TIE PANEL IAW AMM 20-50-11-912-002, FIG 203.

Part: PANEL — CHAFED (BS 1156) · airframe 48,116 hrs · 26,986 cycles

LT HORIZONTAL BOW TIE CHAFED. ACFT GROUNDED. R & R BOW TIE LEFT.

Part: BEAM — CORRODED (BS 312-344) · corrosion level 2 · airframe 48,116 hrs · 26,986 cycles

FWD ENTRY DOOR THRESHOLD CENTER SUPPORT CORRODED NEAR AFT END IN PREVIOUSLY BLENDED AREA. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-10-15-1A1. R & R SUPPORT IAW SRM 51-40-02-0G0 AND DWG 69-02471.

Part: WINDOW — BINDING (COCKPIT) · airframe 47,509 hrs · 26,644 cycles

F/OS SLIDING WINDOW DIFFICULT TO OPEN AND CLOSE. BINDING IN TRACK AND REQUIRES EXCESSIVE FORCE TO OPERATE. SLIDING WINDOW REPAIRED IAW AMM 56-12-11-308-008. WINDOW INSTALLED & FUNCTIONED IAW AMM 56-12-11-404-007, CHECKED SERVICEABLE.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 47,348 hrs · 26,520 cycles

FWD GALLEY EXIT LIGHT COVER FELL OFF. INSTALLED FWD GALLEY EXIT LIGHT COVER, OK FOR SERVICE.

Part: CAMSHAFT — OUT OF ADJUST (R2 WINDOW) · airframe 47,251 hrs · 26,465 cycles

F/O WINDOW WILL NOT CLOSE IN THE LOCKED POSITION. ADJUSTED LOWER CAM ASSY AND CAMSHAFT ASSY FOR CORRECT ENGAGEMENT IN REF TO MM 56-12-11, PAR G, SECTION 4. VERIFIED CORRECT HANDLE FORCE AND LOCK POSITION, OPS CHECK GOOD, M/M 56-12-11.

Part: COVER — DISLODGED (EMERGENCY LIGHT) · airframe 47,231 hrs · 26,452 cycles

EMERGENCY EXIT LIGHT COVER NEXT TO R1 DOOR CAME OFF. INSTALLED COVER.

Part: SLIDING WINDOW — INOPERATIVE (R2) · airframe 47,156 hrs · 26,408 cycles

F/O SLIDING R2 WINDOW VERY DIFFICULT TO OPEN. REMOVED WINDOW. VERIFIED MEASUREMENT OF FWD AND AFT BELLCRANK, REF MM 56-12-11-404-007, STEP 3.D.(7). REPLACED F/O SLIDING WINDOW HAS WINDOW CODE H14. MOVED TAP TO TERMINAL 3 OF T 269 REF WDM 30-41-11. ACCOMPLISHED WINDOW HEAT OPS TEST FOR F/O SLIDING WINDOW TEST PASSED REF AMM 30-41-00. FINISHED WINDOW INSTALLATION AND ADJUSTMENT REF MM 56-12-11-404-007, OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,589 hrs · 24,881 cycles

EMERGENCY EXIT LIGHTS AT LOCATION FWD RIGHT OVERWING AND LEFT DIM (EXTERIOR LIGHTS). REMOVED AND REPLACED BATTERY ASSEMBLY IAW MM 33-51-51-962-015 STEPS D1A E3A. LIGHTS OPS CHECK GOOD IAW STEPS E4A E4B2A.

Part: SNUBBER — DEFECTIVE (L2 DOOR) · airframe 43,695 hrs · 24,339 cycles

F/A REPORTS AFT LEFT DOOR L2 WILL NOT FULLY OPEN. REPLACED L2 DOOR SNUBBER PER AMM 52 41 71. OPS CHECK OF L2 DOOR NORMAL PER AMM 52 41 00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,301 hrs · 24,066 cycles

L1 EMERG EXIT LIGHT ON EXTERIOR INOP. L1 EMERG EXTERIOR PWR SUPPLY AND BATTERY PACK REPLACED PER 33 51 51 962 016 AND 33 51 51 962 015 M1133. OPS CHECK NORMAL.

Part: UNKNOWN — MALFUNCTIONED (L1 DOOR) · airframe 43,203 hrs · 24,006 cycles

L1 DOOR HARD TO OPEN FLIGHT ATTENDANT STATED DOOR WAS HARD TO SWING OPEN & CLOSED. PERFORMED GVI OF HINGES & SNUBBER PERFORMED FWD ENTRY DOOR TEST PER MM 51 11 00, NO DEFECTS NOTED DOOR MOVED SMOOTHLY & SNUBBER OPS NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

AFT PIT STRINGER 25R IS CRACKED BETWEEN BS 927 AND BS 947. CUT OUT DAMAGE FABRICATED REPAIR ANGLE AND INSTALLED IAW B737 400 SRM 53 00 03 FIG 201.

Part: FITTING — CRACKED (CARGO BAY) · airframe 41,570 hrs · 23,034 cycles

AFT PIT LT BAFFLE CLIP CRACKED BS 947. REMOVED CRACKED CLIP FABRICATED TREATED PRIMED TOP COATED AND INSTALLED NEW CLIP IAW B737 400 SRM 51 40 02.

Part: FITTING — CRACKED (CARGO BAY) · airframe 41,570 hrs · 23,034 cycles

AFT PIT LT BAFFLE CLIP BS 927 CRACKED. REMOVED CRACKED CLIP FABRICATED TREATED PRIMED TOP COATED AND INSTALLED NEW CLIP IAW B737 400 SRM 51 40 02.

Part: BAFFLE — CORRODED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

AFT PIT BAFFLE CORRODED BS 927. REMOVED CORRODED BAFFLE FABRICATED TREATED PRIMED TOP COATED AND INSTALLED NEW BAFFLE IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 867 BETWEEN STR 8L AND 9L. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 45,170 hrs · 23,034 cycles

AFT ACCESSORY SECTION INTERCOSTAL CORRODED AT STR 26R BS 965. FABRICATED AND REPLACED INTERCOSTAL IAW B737 400 SRM 51 30 01 AND 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 827 BETWEEN STR 8R AND 9R. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CORROSION AT BS 500B BL 0 LBL 4. REPAIRED FRAME IAW B737 400 SRM 53 00 07 FIG 201.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FORWARD PIT BS 500G AFT CENTER SUPPORT STIFFENER CORRODED. REMOVED STIFFENER AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.

Part: CARGO TRACK — DEFECTIVE (CARGO BAY) · airframe 41,570 hrs · 23,034 cycles

CARGO TRACK AT RBL 13.8 BS 860 HAS NO JOGGLE FOR FLOOR PANEL STRAP. CUT OUT SECTION OF CARGO TRACK FABRICATED AND INSTALLED REPAIR PARTS IAW ASA EA 400 53EA 04666.

Part: TRANS PANEL — CORRODED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

AFT PIT RT TRANSITION PANEL CORRODED BS 867 - 887. REMOVED DAMAGED SECTION AND INSTALLED NEW TRANSITION PANEL IAW B737 400 SRM 51 40 02.

Part: TRANS PANEL — CORRODED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

AFT PIT RT TRANSITION PANEL CORRODED BS 767 - 787. REMOVED DAMAGED SECTION AND INSTALLED NEW TRANSITION PANEL IAW B737 400 SRM 51 40 02.

Part: SUPPORT ANGLE — BENT (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

AFT PIT LT FORWARD BULKHEAD SUPPORT ANGLE IS BENT. REMOVED SUPPORT ANGLE FABRICATED AND INSTALLED NEW ANGLE IAW B737 400 SRM 51 40 02.

Part: STRIP — CORRODED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FORWARD PIT LT NR 2 CAPSTRIP HAS CORROSION. FABRICATED NEW CAP STRIP AND INSTALLED IAW B737 400 SRM 53 30 53 AND 51 40 05.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

RT OUTBOARD SEAT TRACK GOUGED BS 520. REMOVED DAMAGED SECTION AND INSTALLED NEW SEAT TRACK IAW B737 400 SRM 53 00 52 FIG 201.

Part: STRIP — CORRODED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FORWARD CARGO PIT LT NR 3 CAP STRIP HAS CORROSION BLENDED CORROSION OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 51 40 05 FIG 2.

Part: STRIP — CORRODED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FORWARD CARGO PIT RT NR 2 CAP STRIP HAS CORROSION AROUND FASTENER HOLES. BLENDED CORROSION OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 51 40 05 FIG 2.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

LT OUTBOARD SEAT TRACK GOUGED BS 520. REMOVED DAMAGED SECTION AND INSTALLED NEW SEAT TRACK IAW B737 400 SRM 53 00 52 FIG 201.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

RT OUTBOARD SEAT TRACK WORN BS 887. REMOVED DAMAGED SECTION AND INSTALLED NEW SEAT TRACK IAW B737 400 SRM 53 00 52 FIG 201.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,570 hrs · 23,034 cycles

AFT PRESSURE BULKHEAD CENTER RADIAL STIFFENER CORRODED BL 0 AFT OF BS 1016. CUT OUT DAMAGED STIFFENER FABRICATED REPAIR PARTS AND INSTALLED IAW BOEING DRAWING 65C28106.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 41,570 hrs · 23,034 cycles

LEFT NR 3 FLAP TRACK HORIZONTAL ROLLER SURFACES HAVE PITTING. REMOVED DAMAGE ROTO PEENED AREA CAD PLATED AND RESTORED FINISH IAW BOEING CMM 57 53 16.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,570 hrs · 23,034 cycles

AFT PRESSURE BULKHEAD WEB CORRODED AFT OF BS 1016. CUT OUT DAMAGED AREA FABRICATED REPAIR PARTS AND INSTALLED IAW ASA EA 400 53EA 04709.

Part: TRANS PANEL — CORRODED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

AFT PIT LT TRANSITION PANEL CORRODED BS 727B - 777. REMOVED DAMAGED SECTION AND INSTALLED NEW TRANSITION PANEL IAW B737 400 SRM 51 40 02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,570 hrs · 23,034 cycles

AFT PRESSURE BULKHEAD CENTER RADIAL STIFFENER CORRODED BL 0 AFT OF BS 1016. CUT OUT DAMAGED STIFFENER FABRICATED REPAIR PARTS AND INSTALLED IAW BOEING DRAWING 65C28106.

Part: FLAP TRACK — WORN (TE FLAP) · airframe 45,170 hrs · 23,034 cycles

RIGHT NR 8 FLAP TRACK VERTICAL ROLLER SURFACES HAVE BEARING CONTACT WEAR GROOVES. REMOVED DAMAGE ROTO PEENED AND RE-APPLIED PROTECTIVE FINISH IAW BOEING CMM 57 53 15.

Part: TRANS PANEL — CORRODED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

AFT PIT LT TRANSITION PANEL CORRODED BS 847 - 927. REMOVED DAMAGED SECTION AND INSTALLED NEW TRANSITION PANEL IAW B737 400 SRM 51 40 02.

Part: FLAP TRACK — WORN (TE FLAP) · airframe 41,570 hrs · 23,034 cycles

RIGHT NR 8 FLAP TRACK HORIZONTAL ROLLER SURFACES HAVE BEARING CONTACT WEAR GROOVES. REMOVED DAMAGE ROTO PEENED AND RESTORED PROTECTIVE FINISH IAW BOEING CMM 57 53 15.

Part: TRANS PANEL — CORRODED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

AFT PIT RT TRANSITION PANEL CORRODED BS 727B - 767. REMOVED DAMAGED SECTION AND INSTALLED NEW TRANSITION PANEL IAW B737 400 SRM 51 40 02.

Part: STRAP — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

PASSENGER CABIN FLOORBEAM SUPPORT STRAP CORRODED AT BS 312. REMOVED AND REPLACED STRAP IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 907 BETWEEN STR 8R AND 9R. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 727F BETWEEN STR 8L AND 9L. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FORWARD CARGO PIT TRANSITION STRIP (SIDE PLATE) CORRODED BS 500- 500G. REMOVED DAMAGED SECTION AND INSTALLED NEW SIDE PLATE IAW B737 400 SRM 51 40 02.

Part: TRANS PANEL — CORRODED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FWD CARGO PIT STA 500 TO 500G LEFT TRANSITION PANEL HAS AREAS OF CORROSION. BLENDED CORROSION OUT OF LIMITS. FABRICATED TREATED PRIMED TOP COATED AND INSTALLED REPLACEMENT TRANSITION PANEL IAW BOEING 737 400 SRM 51 30 01 FIG 8.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,570 hrs · 23,034 cycles

FORWARD CARGO SHEAR TIE AT BS 500C BETWEEN STR 28R AND 28L HAS CORROSION. BLENDED CORROSION OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 53 00 07 FIG 201 REPAIR 3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 787 BETWEEN STR 8R AND 9R. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 907 BETWEEN STR 8R AND 9R. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 787 BETWEEN STR 8L AND 9L. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 727D BETWEEN STR 8R AND 9R. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 747 BETWEEN STR 8L AND 9L. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 867 BETWEEN STR 8R AND 9R. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 747 BETWEEN STR 8R AND 9R. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 41,570 hrs · 23,034 cycles

FORWARD CARGO PIT LEFT CARGO TRACK HAS CORROSION AT BS 500G. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 53 00 53 FIG 201.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 41,570 hrs · 23,034 cycles

FORWARD CARGO PIT RAIL AT BS 500G IS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 53 00 53 FIG 201.

Part: FLOOR SUPPORT — GOUGED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FORWARD CARGO PIT 6 INCHES AFT OF BS 500A AT RBL 3 FLOOR SUPPORT HAS SURFACE DAMAGE. REPAIRED IAW B737 400 SRM 53 00 53 FIG 201.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FORWARD CARGO PIT SHEAR TIE (FRAME) AT BS 500E AND BETWEEN STR 28R AND 28L HAS CORROSION. REPAIRED SHEAR TIE IAW B737 400 SRM 53 00 07 FIG 201.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,570 hrs · 23,034 cycles

R1 (FORWARD GALLEY SERVICE) DOOR MOP SILL CORRODED. REMOVED CHORD AND INSTALLED NEW PART IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 480 BETWEEN STR 8L AND 9L. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 400 BETWEEN STR 8L AND 9L. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 360 BETWEEN STR 8L AND 9L. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 400 BETWEEN STR 8L AND 9L. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 500F BETWEEN STR 8L AND 9L. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 440 BETWEEN STR 8L AND 9L. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 480 BETWEEN STR 8R AND 9R. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

FRAME CRACKED AT BS 440 BETWEEN STR 8R AND 9R. REPAIRED CRACKED FRAME IAW EA AD20062609 400 53 109 REV NEW DATED 28JAN11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,570 hrs · 23,034 cycles

L1 (FORWARD ENTRY DOOR) MOP SILL CORRODED. REMOVED CORRODED MOP SILL AND INSTALLED NEW MOP SILL IAW B737 400 SRM 51 40 02.

Part: SKIN — DENTED (SPOILER) · airframe 41,570 hrs · 23,034 cycles

RIGHT WING INBOARD SPOLIER HAS A DENT IN THE UPPER SURFACE 4 INCHES FROM OUTBOARD EDGE 11 INCHES FROM LEADING EDGE. REPAIRED SPOILER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SLAT — DELAMINATED (NR 2) · airframe 41,570 hrs · 23,034 cycles

NR 2 SLAT UPPER OUTBOARD TRAILING EDGE DELAMINATED. REPAIRED SLAT IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (SPOILER) · airframe 41,570 hrs · 23,034 cycles

RIGHT WING INBOARD SPOILER HAS A DENT IN THE LOWER SURFACE 6 INCHES FROM LEADING EDGE 20 INCHES FROM OUTBOARD EDGE. REPAIRED SPOILER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SLAT — DELAMINATED (NR 2) · airframe 41,570 hrs · 23,034 cycles

NR 2 SLAT UPPER INBOARD TRAILING EDGE DELAMINATED ON PREVIOUS REPAIR. REPAIRED SLAT IAW B737 400 SRM 51 70 10 REPAIR 4

Part: STRAP — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

PASSENGER CABIN FLOORBEAM SUPPORT STRAP CRACKED IN HALF. REPAIRED IAW B737 400 SRM 53 10 51.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,570 hrs · 23,034 cycles

SHEAR TIE AT BS 500D BETWEEN STR 28L AND 28R CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 53 00 07.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,397 hrs · 21,162 cycles

FLOORBEAM AT STA 986.5 IS SHOWING SIGNS OF CORROSION UNDER FLOOR PANEL ON FORWARD SIDE OF BEAM. REPAIRED FLOORBEAM AT STA 986.2 IAW AAR EA 13619 REV 1/2 DATED 23OCT2009 AND ASA EA 400 53EA 02304 REV NEW DATED 26OCT09.

Part: WEDGE — CHAFED (LE SLAT) · airframe 38,396 hrs · 21,162 cycles

LEFT WING L/E SLAT NR 3 T/E WEDGE I/B AFT CORNER CHAFED. REPAIRED CHAFE DAMAGE AT I/B AFT CORNER OF SLAT NR 3 T/E WEDGE.

Part: SKIN — GOUGED (MIDFLAP) · airframe 38,396 hrs · 21,162 cycles

LEFT O/B MIDFLAP SECOND FROM O/B AFT FLAP TRACK CUTOUT SKIN IS GOUGED. REPAIRED GOUGE DAMAGE TO LOWER SKIN.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,396 hrs · 21,162 cycles

FLOORBEAM AT STA 986.5 IS CORRODED UNDER FLOOR PANEL ON FORWARD SIDE OF BEAM. REPAIRED FLOORBEAM AT STA 986.5.

Part: SKIN — GOUGED (MIDFLAP) · airframe 38,397 hrs · 21,162 cycles

LT O/B MIDFLAP SECOND FROM O/B AFT FLAP TRACK CUTOUT SKIN IS GOUGED. REPAIRED GOUGE DAMAGE TO LWR SKIN ON LT O/B MIDFLAP AT O/B FLAPTRACK IAW IAW B737 400 SRM 57 53 01 REPAIR 9 PG 201 206.

Part: SKIN — DENTED (SPOILER) · airframe 38,397 hrs · 21,162 cycles

NR 5 SPOILER DENTED OUT OF LIMITS I/B LOWER SURFACE 9 INCHES FROM FORWARD END. REPAIRED 9 OUT OF LIMIT DENTED AREAS INCORPORATED INTO 8 BONDED DOUBLER REPAIRS ON LWR SKIN OF NR 5 SPOILER AT VARIOUS LOCATIONS IAW B737 400 SRM 51 70 10 REPAIR 2 PG 201.

Part: SKIN — DENTED (SPOILER) · airframe 38,396 hrs · 21,162 cycles

NR 5 SPOILER DENTED BEYOND LIMITS I/B LOWER SURFACE 9 INCHES FROM FORWARD END. REPAIRED 9 OUT OF LIMITS DENTS INCORPORATED INTO 8 BONDED DOUBLER REPAIRS ON LOWER SKIN OF NR 5 SPOILER.

Part: SKIN — CRACKED (TE FLAP) · airframe 38,396 hrs · 21,162 cycles

LEFT WING O/B AFT FLAP UPPER SKIN HAS A SHARP DENT WITH CRACK AT I/B END. REPAIRED DAMAGE ON UPPER LEFT O/B AFT FLAP.

Part: SKIN — DAMAGED (SPOILER) · airframe 38,396 hrs · 21,162 cycles

NR 1 SPOILER LOWER SURFACE CREASED 5 INCHES FROM O/B EDGE. BONDED REPAIR.

Part: SKIN — DENTED (SPOILER) · airframe 38,396 hrs · 21,162 cycles

LEFT WING NR 2 SPOILER DENTED LWR SURFACE 8 INCHES FROM THE O/B EDGE. REPAIRED LEFT WING NR 2 SPOILER DENTED LWR SURFACE.

Part: SKIN — DAMAGED (SPOILER) · airframe 38,397 hrs · 21,162 cycles

NR 1 SPOILER LOWER SURFACE CREASED 5 INCHES FROM O/B EDGE 5 INCHES FROM L/E BONDED REPAIR IAW B737 400 SRM 51 70 10 PG 201 REPAIR 4.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 38,397 hrs · 21,162 cycles

RT I/B FOREFLAP LWR SKIN DELAMINATED 40 INCHES FROM I/B EDGE AND 4.5 INCHES FROM T/E. REPAIRED R/H I/B FOREFLAP LWR SKIN DAMAGE IAW B737 400 SRM 51 70 10 REPAIR 4 PG 201.

Part: FLAP — DENTED (LT WING) · airframe 38,397 hrs · 21,162 cycles

LT WING I/B FOREFLAP HAS NUMEROUS DENTS AT LOWER CHAMBER REPAIRED DAMAGED AREA IAW B737 400 SRM 51 70 10 PG 241 254

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 38,396 hrs · 21,162 cycles

RT WING I/B FORE FLAP LOWER SKIN DELAMINATED 40 INCHES FROM I/B EDGE AND 4.5 INCHES FROM T/E. REPAIRED RT WING I/B FORE FLAP LOWER SKIN DAMAGE.

Part: SKIN — DENTED (FOREFLAP) · airframe 38,396 hrs · 21,162 cycles

LT WING I/B FORE FLAP HAS NUMEROUS DENTS AT LOWER CAMBER. REPAIRED DAMAGED AREA.

Part: SKIN — DENTED (FOREFLAP) · airframe 38,397 hrs · 21,162 cycles

LEFT INBOARD FORE FLAP HAS NUMEROUS DENTS ON UPPER CHAMBER. REMOVED DAMAGED SKIN, FABBED FILLER & DOUBLER & BONDED REPAIR IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (SPOILER) · airframe 38,396 hrs · 21,162 cycles

NR 6 SPOILER DENTED 17 INCHES FROM I/B EDGE ON UPPER SURFACE. PREPPED DAMAGED AREA, FABBED DOUBLER AND BONDED REPAIR.

Part: SKIN — DELAMINATED (SPOILER) · airframe 38,396 hrs · 21,162 cycles

NR 3 SPOILER UPPER SURFACE DELAMINATED 3 INCHES FROM I/B EDGE 7 INCHES FROM TRAILING EDGE. CUT OUT DAMAGED AREA, FABRICATED AND BONDED DOUBLER AND FILLER.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,396 hrs · 21,162 cycles

L2 DOOR MOP SILL IS CORRODED. REMOVED CORRODED MOPSILL DRILLED AND INSTALLED NEW MOPSILL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,397 hrs · 21,162 cycles

CABIN FLOOR SUPPORT AT STA 951 RBL 24 IS CORRODED. REMOVED DAMAGED SUPPORT FABBED REPLACEMENT PARTS AND INSTALLED REPAIR PARTS IAW B737 400 SRM 51 40 02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,396 hrs · 21,162 cycles

R2 DOOR MOPSILL IS CORRODED. REMOVED CORRODED MOPSILL DRILLED AND INSTALLED NEW MOPSILL.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,396 hrs · 21,162 cycles

DENT BELOW THE R1 DOOR STA 328 STR 20. REPAIRED DENT.

Part: SKIN — CRACKED (LE SLAT) · airframe 38,397 hrs · 21,162 cycles

NR 3 SLAT SKIN CRACKED AT INBOARD AFT RIVET ON THE INBOARD END OF THE SLAT. REMOVED DAMAGED AREA, FABBED FILLER & DOUBLER & INSTALLED REPAIR PARTS IAW B737 400 SRM 57 43 01 FIG 207 REP 6.

Part: SKIN — DENTED (HORIZ STAB) · airframe 38,397 hrs · 21,162 cycles

RT HORIZ STAB LEADING EDGE DAMAGED / DENTED 96 INCHES FROM INBOARD EDGE. REMOVED DAMAGE FABBED FILLER & DOUBLER & INSTALLED REPAIR PARTS IAW B737 400 SRM 55 10 01 FIG 201.

Part: SKIN — DENTED (SPOILER) · airframe 38,396 hrs · 21,162 cycles

NR 3 SPOILER LOWER SURFACE HAS A SHARP DENT. FABBED DOUBLER AND BONDED REPAIR.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,397 hrs · 21,162 cycles

RT SHEER WEB UPPER SURFACE CORRODED JUST FWD OF RT FWD MOUNT FOR THE AFT GALLEY. REMOVED WEB FABBED REPLACEMENT WEB & INSTALLED WEB IAW B737 400 SRM 51 40 02.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,397 hrs · 21,162 cycles

SHEAR WEB UPPER SURFACE CORRODED JUST FWD OF AFT GALLEY LT FWD MOUNT FITTING. REMOVED CORRODED SHEAR WEB FABBED REPLACEMENT WEB AND INSTALLED REPAIR PARTS IAW B737 400 SRM 51 40 02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,397 hrs · 21,162 cycles

FUSELAGE LF SIDE APPROX STA 1020 HAS A CREASE ABOVE AND FORWARD OF PREVIOUS REPAIR AT STR 12L. REMOVED DAMAGED AREA & PREVIOUS REPAIR FABBED REPAIR FOR ENTIRE AREA & INSTALLED REPAIR IAW B737 400 SRM 53 80 01 FIG 201 DETAIL II.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,396 hrs · 21,162 cycles

L1 DOOR LOWER HINGE CUTOUT SHOWS CRACK INDICATION AT FASTENER HOLE C 10 CUT 1 INCH HOLE, NO CRACK FOUND. FABBED FILLER AND DOUBLER FOR REPAIR AREA AND INSTALLED.

Part: SKIN — DENTED (R1 DOOR) · airframe 38,396 hrs · 21,162 cycles

R1 DOOR OUTER SKIN DENTED ON FWD UPPER CORNER. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER AND INSTALLED REPAIR.

Part: SKIN — DAMAGED (AILERON TAB) · airframe 37,008 hrs · 20,302 cycles

LT AILERON TAB HAS EXPOSED FIBERS UPPER SURFACE I/B END. REPAIRED PER SRM 57 60 01.

Part: BEAM — GOUGED (HORIZONTAL STAB) · airframe 37,008 hrs · 20,302 cycles

LT HORIZONTAL STAB UPPER T/E BEAM AND COVER PLATE GOUGED ABOVE NR 2 ELEVATOR HINGE. REPAIRED LT HORIZONTAL STAB UPPER T/E BEAM AND PLATE.

Part: TAB — DAMAGED (ELEVATOR) · airframe 37,008 hrs · 20,302 cycles

RT ELEVATOR TAB HAS DAMAGE AT BOTH I/B AND O/B HINGE CUTOUTS. REMOVED AND REPLACED TAB.

Part: SKIN — PUNCTURED (ELEVATOR) · airframe 37,008 hrs · 20,302 cycles

RT ELEVATOR UPPER SKIN PUNCTURED. REPAIRED SKIN.

Part: HANDLE — STICKING (R1 DOOR) · airframe 36,576 hrs · 20,050 cycles

INTERIOR R1 DOOR HANDLE STIFF TO MOVE & OPERATE. R&R R1 DOOR REF.MM 52-41-00.

Part: FRAME — GOUGED (BS 440) · airframe 35,061 hrs · 19,170 cycles

FWD PIT FWD FRAME GOUGED BS 440 RBL 28 REPAIRED PER SRM 51 40 02

Part: STRINGER CLIP — CORRODED (BS 794) · airframe 35,061 hrs · 19,170 cycles

STRINGER TIE CLIP AT BS 794 RBL 13.8 HAS CORROSION REPAIRED IAW SRM.

Part: FRAME — CRACKED (BS 601) · airframe 35,061 hrs · 19,170 cycles

FOUND CRACK ON LT FUSELAGE FRAME AT STA 601 DIRECTLY ABOVE THE CENTER WING REPAIRED IAW EA 5310 02804. PERFORM 1 STAGE DTA INSPECTION REQUIREMENTS WITHIN 12 MONTH FROM JUL 11 2008.

Part: FRAME — CORRODED (BS 492) · corrosion level 2 · airframe 35,061 hrs · 19,170 cycles

FWD CARGO PIT FRAME UPPER STRAP CORRODED REPAIRED IAW SRM 51-40-02-51-50- 05.

Part: FRAME — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 35,061 hrs · 19,170 cycles

AFT CARGO DOOR AFT FRAME AT BS 847 FOUND CORRODED RBL 17 ON UPPER FLANGE REPAIRED IAW SRM.

Part: FRAME — GOUGED (BS 440) · airframe 35,061 hrs · 19,170 cycles

FWD CARGO PIT FWD FRAME HAS GOUGE AT BS 440 RBL 28 REPAIRED IAW SRM.

Part: SNAP RING — MISSING (L1 DOOR) · airframe 32,278 hrs · 17,649 cycles

L1 DOOR DIFFICULT TO OPEN. FOUND RETAINING RING FOR GUIDE ARM MISSING. REINSTALLED SNAP RING, OPS NORMAL.

Part: TERMINAL — CORRODED (OVERHEAT LOOP) · airframe 31,167 hrs · 17,011 cycles

FAULT LIGHT ILLUMINATED DURING OVERHEAT FIRE TEST. ENGINE NR 1 OVERHEAT LIGHT FAILED TO ILLUMINATE DURING TEST. A-LOOP FAILED. CHANGED ALL A I TERMINAL LUGS ON FAN AND FIREWALL OVERHEAT LOOPS.

Part: SKIN — DENTED (TE FLAP) · airframe 27,443 hrs · 14,929 cycles

LT IB MID FLAP AFT TE PANEL 7220 HAS CLUSTER OF DENTS ON LWR SURFACE. PREPPED AREA OF DAMAGE FABED AND INSTALLED REPAIR DOUBLERS IAW SRM 51 70 10 REPAIR 2.

Part: PANEL — DENTED (TE FLAPS) · airframe 27,443 hrs · 14,929 cycles

RT IB MID FLAP AFT T/E PANEL 7420 HAS CLUSTER OF DENTS ON LWR SURFACE. PREPPED AREA OF DAMAGE FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 51 70 10 REPAIR 3.

Part: STRUCTURE — DAMAGED (NR 6 SLAT) · airframe 27,443 hrs · 14,929 cycles

NR 6 SLAT CHAFED ON AFT SIDE AT SLAT STA 278. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51 70 10.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 27,443 hrs · 14,929 cycles

FOUND FLOORBEAM CORRODED ON UPPER SURFACE. REMOVED CORRODED AREA FLAT PEEN AND SPOT FACED AREA FABRICATED AND INSTALLED REPAIR STRAP IAW ASA EA 5310 02581.

Part: SKIN — DENTED (FORE FLAP) · airframe 27,443 hrs · 14,929 cycles

LT IB FORE FLAP LWR SURFACE HAS NUMEROUS DENTS. REMOVED DAMAGED AREA FAB`D AND INSTALLED FILLERS SKIN AND DOUBLERS IAW SRM 51 70 10.

Part: SILL — CORRODED (BS 907-1007) · corrosion level 2 · airframe 27,443 hrs · 14,929 cycles

FOUND L2 DOOR MOPSILL IS CORRODED (INNER CHORD). REMOVED CORRODED INNER CHORD INSTALLED NEW INNER CHORD IAW SRM 51 40 02.

Part: SILL — CORRODED (BS 912-1006) · corrosion level 2 · airframe 27,443 hrs · 14,929 cycles

FOUND R2 DOOR LOWER SILL CORRODED (INNER CHORD). REMOVED CORRODED INNER CHORD. INSTALLED NEW INNER CHORD PER SRM 51 40 02.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,443 hrs · 14,929 cycles

3EACH DENTS ON LT SIDE OF FUSELAGE. REMOVED DAMAGED AREAS FABRICATED AND INSTALLED FILLERS AND DOUBLERS INSTALLED REPAIR PIECES IAW SRM 53 80 01 FIG 201 REPAIR 3.

Part: TAB — DELAMINATED (ELEVATOR) · airframe 27,443 hrs · 14,929 cycles

RT ELEV TAB AT NR 3 HINGE CUTOUT FM IB HAS SMALL AREA OF DELAMINATION.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 24,804 hrs · 13,530 cycles

PREVIOUS BLEND-OUT AT PAX CABIN SEAT TRACK, BS 500+12 INCHES, LBL 25, WL 208 OUT OF LIMITS. CUTOUT DAMAGE AND REPAIRED IAW SRM 53-00-52. (K)

Part: SEAT TRACK — GOUGED (FUSLEAGE) · airframe 24,804 hrs · 13,530 cycles

LT OB SEAT TRACK HAS MULTIPLE GOUGES AT BS 500C. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-00-52. (K)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY, FRAME TO FLOOR TO SIDEWALL SUPPORT PLATE CORRODED. REMOVED FABRICATED AND INSTALLED NEW SUPPORT PLATE PER SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PAE - AFT CARGO BAY, INTERCOSTAL UPPER FLANGE CORRODED. REMOVED AND REPLACED INTERCOSTAL PER SRM. (M)

Part: BRACKET — CORRODED (FUSELAGE)

PAE - FOUND AFT CARGO BAY, FRAME TO FLOOR TO SIDEWALL SUPPORT BRACKET CORRODED. FABRICATED AND INSTALLED NEW SIDEWALL SUPPORT BRACKET PER SRM. (M)

Part: BULKHEAD — DAMAGED (FUSELAGE)

GYR - FOUND STATION 178 WEB DAMAGED WL 219, LBL 18.1. REPAIRED DAMAGE IAW ASA EA NR 5310-02343 PG 3 STEP 3. (M)

Part: WEB — CHAFED (FUSELAGE)

PAE - DURING C-CHECK, FOUND LEFT MLG LOWER CUT OUT WEB CHAFED BEYOND LIMITS. REPAIRED IAW SRM. (M)

Part: CHANNEL — CRACKED (LT WING)

PAE - DURING C-CHECK, FOUND LEFT WING UPPER INBOARD TRAILING EDGE PANEL SUPPORT CHANNEL CRACKED WBL 87. REPAIRED IAW EA. (M)

Part: WEB — GOUGED (FUSELAGE)

DURING C-CHECK, FOUND GOUGE IN WEB AT RIGHT AIR CONDITIONING BAY 1 INCH BELOW THE AFT RT HEAT EXCHANGER OUTBOARD FLANGE INBOARD SIDE OF WEB. REPAIRED IAW SRM.

Part: SUPPORT ANGLE — CRACKED (T/E FLAP)

PAE - DURING C-CHECK, FOUND CRACKED SUPPORT ANGLE FOR LEFT INBOARD FLAP TRACK FAIRING. REPAIRED IAW SRM. (M)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR TO BULKHEAD SUPPORT AT BS 500G LBL 24-28 AND WL 156. REPAIRED IAW SRM. (M)

Part: FAIRING — CRACKED (ELEVATOR TAB)

PAE - DURING C-CHECK, FOUND RIGHT ELEVATOR TAB AFT MAST FAIRING CRACKED AT OUTBOARD CORNER. REMOVED AND REPLACED RIGHT ELEVATOR TAB AFT MAST FAIRING. (M)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON AFT BULKHEAD OF FLOOR SUPPORT. REPAIRED IAW SRM. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE MID SECTION AND AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED MID SECTION WIRING AND REPLACED AFT WIRING HARNESS, EMERGENCY EXIT TRACK LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 13-17. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROWS 13-17)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 13-17 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/LIGHTS AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROWS 14-17)

SEA - FLT 385 - CREW REPORTED EMERGENCY EXIT FLOOR TRACK LIGHT INOPERATIVE ROWS 14 THROUGH 17. RECONNECTED TWO WIRES AT FLOOR SOCKET AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO FLT 464 - THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 13-17 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 14-17 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROWS 14-17)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14-17. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROWS 14-17)

LAX - PRIOR TO FLIGHT 687, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14-17. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 14-17 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/LIGHT AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN) · airframe 6,017 hrs · 3,414 cycles

KTN - FLT 62 - PRIOR TO FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 15-17. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (ROW 28)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 23 THROUGH 28 WERE FOUND TO BE INOPERATIVE. RECONNECTED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROWS 15-18)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 15-18 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/LIGHT, AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — LOOSE (ROWS 14-17)

SEA - DURING MAINTENANCE CHECK THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 14-17. RE-CONNECTED WIRING/LIGHTS AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (ROWS 21-24)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 21-24. RECONNECTED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (ROWS 15-16)

SMF - FLT 409 - PRIOR TO FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 15 AND 16. CONTRACT MAINTENANCE RE-SECURED LOOSE WIRING TO THE LIGHT ASSEMBLIES AND THE LIGHTS OPERATED NORMALLY. (X)