N778AS

Part: FRAME — CRACKED (BS 827) · airframe 66,425 hrs · 37,874 cycles

FRAME 827R, CRACKED AT INBD BRACKET FASTENER. ACFT GROUNDED. REPAIRED FRAME IAW WO 292077 TASK CARD AD20062609-400-53-1, REV 01, REV DATE 3-30-15, FIG 3. REF TASK CARD: AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 727F) · airframe 66,425 hrs · 37,874 cycles

FRAME BS 727F, CRACKED AT INBD BRACKET FASTENER. ACFT GROUNDED. REPAIRED FRAME IAW W/O 292077 TASK CARD AD20062609-400-53-1, REV 01, REV DATE 03/30/2015, FIG 3. REF TASK CARD: AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 500A) · airframe 66,425 hrs · 37,874 cycles

FRAME AT BS 500A CRACKED AT INBD FASTENER BETWEEN S8 & 9L BRACKET ATTACH FASTENER. ACFT GROUNDED. REPAIRED FRAME 500A LT IAW ASA WO 292077 TASK CARD, AD 20062609-400-53-1, REV 01, REV DATE 3-30-15, FIG 3. REF TASK CARD: AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 907) · airframe 66,425 hrs · 37,874 cycles

FRAME BS 907R, CRACKED AT INBD BRACKET FASTENER. ACFT GROUNDED. REPAIRED FRAME 907R IAW W/O 292077 T/C AD20062609-400-53-1, REV 1, REV DATE 3-30-15, FIG 3 REF TASK CARD: AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 480) · airframe 66,425 hrs · 37,874 cycles

FRAME AT BS 480 HAS CRACK AT INBD FASTENER BETWEEN S8 & 9L, AC BRACKET ATTACH FASTENER. ACFT GROUNDED. REPAIRED FRAME 480L IAW W/O 292077 TASKCARD AD 20062 609-400-53-01, REV 01, REV DATE 03/30/2015, FIG 3. REF TASK CARD: AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 867) · airframe 66,425 hrs · 37,874 cycles

FRAME AT STA 867 HAS CRACK AT INBD FASTENER BETWEEN S8L & S9L ACFT BRACKET ATTACH FASTENER. ACFT GROUNDED. REPAIRED FRAME 867 LT IAW W/O 292077 T/C AD20062609-400-53-1, REV 1, REV DATE 3-30-15, FIG 3, REF TASK CARD: AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 500A) · airframe 66,425 hrs · 37,874 cycles

FRAME AT BS 727B HAS CRACK AT INBD FASTENER BETWEEN S8 & 9L BRACKET ATTACH FASTENER. ACFT GROUNDED. REPAIRED FRAME 727B LT IAW ASA WO 292077, TASK CARD AD 20062609-400-53-1, REV 01, REV DATE 3-30-15, FIG 3. REF TASK CARD: AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 440) · airframe 66,425 hrs · 37,874 cycles

FRAME AT BS 440L HAS CRACK AT INBD FASTENER BETWEEN S8 & 9L A/C BRACKET ATTACH FASTENER. ACFT GROUNDED. REPAIRED FRAME IAW AD 20062609-400-53-1, REV 01, REV.

Part: FRAME — CRACKED (BS 440) · airframe 66,425 hrs · 37,874 cycles

FRAME 440 CRACK AT INBD BRACKET FASTENER TO RADIUS. ACFT GROUNDED. REPAIRED FRAME IAW 10 292077 TASKCARD AD 200 62-6009-400-53-1, REV 01, REV DATE 03, 30, 2015, FIG 3. REF TASK CARD: AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 400) · airframe 66,425 hrs · 37,874 cycles

FRAME AT BS 400L HAS CRACK AT INBD FASTENER BETWEEN S8 & 9L BRACKET ATTACH FASTENER. ACFT GROUNDED. REPAIRED FRAME IAW WO 292077 TASK CARD AD 20062609-400-53-1, REV 01, REV DATE 3-30-15, FIG 3. REF TASK CARD: AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 867) · corrosion level 2 · airframe 66,425 hrs · 37,874 cycles

FRAME BS 867, CRACKED AT INBD BRACKET FASTENER. ACFT GROUNDED. REPAIRED FRAME IAW W/O 292077 T/C AD20062609-400-53-1, REV 1, REV DATE 3-30-15, FIG 3 REF TASK CARD: AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 500C) · airframe 66,425 hrs · 37,874 cycles

FRAME AT BS 500C CRACKED AT INBD FASTENER BETWEEN S8 & 9L BRACKET ATTACH FASTENER. ACFT GROUNDED. REPAIRED FRAME 500C LT IAW W/O 292077, TASK CARD AD20062609-400-53-1, REV 01, REV DATE 03/30/2015, FIG 3.

Part: FRAME — CRACKED (BS 907) · airframe 66,425 hrs · 37,874 cycles

FRAME BS 907, CRACKED AT INBD BRACKET FASTENER. ACFT GROUNDED. REPAIRED FRAME 907R IAW W/O 292077 T/C AD20062609-400-53-1, REV 1, REV DATE 3-30-15, FIG 3, REF TASK CARD: AD20062609-400-53-1.

Part: FRAME — CRACKED (BS 500A) · airframe 66,425 hrs · 37,874 cycles

FRAME BS 500A RT CRACK AT INBD BRACKET FASTENER FRAME. ACFT GROUNDED. REPAIRED FRAME 500A IAW W/O 292077, T/C AD 2002609-400-53-1, REV 1, REV DATE 3-30-15, FIG 3, REF TASK CARD: AD20062609-400-53-1.

Part: SPAR — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 66,425 hrs · 37,874 cycles

LT HORIZONTAL STABILIZER ATTACH FITTING UPPER LUG CORRODED AROUND BUSHING. ACFT GROUNDED. REPAIRED LT HORIZONTAL STABILIZER FRONT SPAR UPPER TERMINAL FITTING LUG AND JOINT IAW EAC MPT-55EA-14908 IAW ASSOCIATED FORM 8100-9. THIS IS A CATEGORY B REPAIR FIRST STAGE DTE HAS BEEN PROVIDED STAGE 2 APPROVAL IS REQUIRED ON OR BEFORE APRIL 16 2017, W 2, O 1.200, R 1.062, L 2, D .138.

Part: ATTACH ANGLE — CRACKED (BS 348) · airframe 66,425 hrs · 37,874 cycles

INTERCOSTAL ATTACH ANGLE CRACKED AT BS 348 AND STR 16 LT. ACFT GROUNDED. R & R INTERCOSTAL WEB, ATTACH ANGLE IAW TC AD20121205-400-53-2, STEP 15, 16, 17. REF TASK CARD: AD20121205-400-53-4A.

Part: ATTACH ANGLE — CRACKED (BS 348) · airframe 66,425 hrs · 37,874 cycles

INTERCOSTAL ATTACH ANGLE CRACKED AT BS 348 AND STR 15L. ACFT GROUNDED. R & R CLIP ANGLE IAW TASK CARD AD20121205-400-53-2, STEP 9, 10, 11. REF TASK CARD: AD20121205-400-53-4A.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 65,869 hrs · 37,543 cycles

WHILE PERFORMING INTERIOR EMERGENCY LIGHT CHECK. FOUND INTERIOR EMERGENCY LIGHT ROW 25 LEFT INOPERATIVE. ALSO, FOUND LT AFT OFF WING EXTERIOR LIGHTS INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMP IAW AMM 33-55-00. OPS CHECK NO GOOD. R & R M1576 BATTERY CHARGER AND M1134 BATTERY REF WDM 33-51-14 AND WDM 33-51-13.

Part: REFLECTOR — FAILED (EMERGENCY LIGHT) · airframe 65,869 hrs · 37,543 cycles

DURING EMERGENCY LIGHT CK FOUND RT FWD EXTERIOR LIGHT INOPERATIVE AFT OF THE R1 DOOR. ACFT GROUNDED. REPLACED LIGHT REFLECTOR IAW CMM 33-50-27, OPS CHECK GOOD.

Part: SKIN — CRACKED (NR 3 SLAT ACT) · airframe 63,208 hrs · 35,930 cycles

NR 3 L/E SLAT ACTUATOR CUTOUT CRACKED. ACFT GROUNDED. REPAIRED NR 3 L/E SLAT ACTUATOR CUTOUT IAW SRM 57-41-01-2R-7, REPAIR 4, PROCEDURE 1.

Part: WEB — DAMAGED (BS 348.2-351.2) · airframe 63,208 hrs · 35,930 cycles

SHEAR WEB AFT OF L1 DOOR IS DAMAGED. ACFT GROUNDED. DISSASSEMBLED SHEAR WEB AFT OF L2 DOOR, FABBED NEW WEB, RE-ASSEMBLED SHEAR WEB IAW SRM 51-40-02-0G-0, 4-51-30-01-0G-0, NR 8.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 63,208 hrs · 35,930 cycles

RIGHT OTBD MID FLAP OTBD L/E CORNER IS CHAFED. REPAIRED RT OTBD MID FLAP OTBD L/E CORNER IAW SRM 57-53-01-2R-8.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 63,208 hrs · 35,930 cycles

LEFT WING OTBD MIDFLAP INBD L/E IS CHAFED. REPAIRED LT OTBD MIDFLAP INBD L/E IAW SRM 57-53-01-2R-8.

Part: ATTACH ANGLE — CORRODED (BS 1129) · corrosion level 2 · airframe 63,208 hrs · 35,930 cycles

APU COMPARTMENT RT TORQUE BOX SUPPORT ANGLE LOCATED AFT OF AFT AIR INLET CUTOUT HAS MID ATTACH CLIP CORROSION AND TWO ATTACH FASTENERS MISSING. ACFT GROUNDED. R & R SUPPORT ANGLE IAW SRM 51-40-02.

Part: STRINGER — CORRODED (BS 1139) · corrosion level 2 · airframe 63,208 hrs · 35,930 cycles

APU RT TORQUE BOX AREA, APU INLET CUTOUT LWR STRINGER IS CORRODED, ACFT GROUNDED. BLENDED DAMAGED AREA REMAINING MATERIAL FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED STRINGER AND INSTALLED NEW STRINGER IAW SRM 51-40-02-0G-0.

Part: BEAM — CRACKED (BS 1118-1120) · airframe 63,208 hrs · 35,930 cycles

HORIZONTAL STABILIZER CENTER SECTION LT THRUST BEAM LOWER OTBD CORNER FITTING IS CRACKED ON HORIZONTAL FLANGE. COMPLIED WITH T/C SB737-55-1091-400-1 FOR LEFT SIDE THRUST BEAM CORNER FITTING REPLACEMENT ONLY IAW EA 400-55EA-11823.

Part: SUPPORT ANGLE — CORRODED (BS 737-817) · corrosion level 2 · airframe 63,208 hrs · 35,930 cycles

AFT CARGO BAY LT TRANSITION ANGLE HAS CORROSION FROM BS 767 TO 817. REMOVED CORROSION IAW SRM 53-60-53-1A-1. REPAIRED ANGLE IAW SRM 53-60-53-2R-4, REP 4.

Part: TEE FITTING — CORRODED (APU BAY) · corrosion level 2 · airframe 63,208 hrs · 35,930 cycles

ON BACK SIDE OF APU COMPARTMENT, RT WEB, THE SUPPORT FRAME FWD OF THE AFT CUTOUT HAS MID ATTACHMENT ANGLE CORRODED. ACFT GROUNDED. R & R TEE ANGLE IAW SRM 51-40-02, W .5", O .094, R .049", L .5", D .045".

Part: SUPPORT ANGLE — CORRODED (BS 1088-1116) · corrosion level 2 · airframe 63,208 hrs · 35,930 cycles

APU COMPARTMENT ON RT WEB ANGLE BETWEEN TWO CUTOUTS HAS CORROSION ON AFT END. ACFT GROUNDED. R & R SUPPORT ANGLE IAW SRM 51-40-02.

Part: ATTACH ANGLE — CORRODED (BS 1129) · corrosion level 2 · airframe 63,208 hrs · 35,930 cycles

APU COMPARTMENT RT TORQUE BOX WEB SUPPORT FRAME BS 1129, MID ATTACH ANGLE HAS CORROSION. ACFT GROUNDED. REMOVED AND INSTALLED NEW ATTACH ANGLE IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (BS 1129) · corrosion level 2 · airframe 63,208 hrs · 35,930 cycles

APU COMPARTMENT, RT AFT AIR INLET CUTOUT, AFT SUPPORT ANGLE CORRODED. ACFT GROUNDED . R & R SUPPORT ANGLE IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (BS 1088-1156) · corrosion level 2 · airframe 63,208 hrs · 35,930 cycles

APU BAY RT SIDE AFT AIR INLET DUCT CUTOUT SURROUND LANDING HAS MULTIPLE CORROSION AREAS. ACFT GROUNDED. REMOVED AND INSTALLED NEW TEE IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 967) · corrosion level 2 · airframe 63,208 hrs · 35,930 cycles

FRAME BS 967 SHEAR TIE CORRODED BETWEEN S25-26L REMOVED CORROSION AND FOUND SHEAR TIE OUT OF LIMITS IAW SRM 53-00-07-1A-1 ALLOWABLE DAMAGE. R & R SHEAR TIE IAW SRM 51-40-02-0G-0.

Part: SHEAR TIE — CORRODED (BS 967) · corrosion level 2 · airframe 63,208 hrs · 35,930 cycles

FRAME BS 967 SHEAR TIE CORRODED BETWEEN S25-26L. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS FOUND SHEAR TIE OUT OF LIMITS IAW SRM 53-00-07-1A-1. ALLOWABLE DAMAGE R & R SHEAR TIE IAW SRM 51-40-02-0G-0.

Part: PAN — CORRODED (BS 947.5-967) · corrosion level 2 · airframe 63,208 hrs · 35,930 cycles

POTABLE WATER SERVICE CUT OUT BOX CORRODED AROUND THE WATER FILL LINE ATTACHMENT STA 947.5 TO 967, STGR26L TO STGR25L. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1, FIG 101. R & R POTABLE WATER CUTOUT BOX PAN IAW SRM 51-40-02-0G-0, W=7, O=.065, R=.049, L=.9, D=.014.

Part: STRUCTURE — CHAFED (RT WING TE FLAP) · airframe 63,208 hrs · 35,930 cycles

RIGHT OTBD MID FLAP L/E IS CHAFED BY NR 7 FLAP TRACK. REPAIRED RT OTBD MIDFLAP L/E BY NR 7 FLAP TRACK FAIRING IAW EA 15482, REV IR, DATE 20DEC13 AND EA 400-57EA-11877.

Part: SKIN — DAMAGED (NR 2 SLAT) · airframe 63,208 hrs · 35,930 cycles

LT NR 2 SLAT OTBD BOTTOM EDGE IS DAMAGED. ACFT GROUNDED. REPAIRED LT NR 2 SLAT OTBD BOTTOM EDGE IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 63,208 hrs · 35,930 cycles

RIGHT WING OTBD FOREFLAP INBD L/E IS CHAFED. R & R RT WING OTBD FOREFLAP INBD L/E SKIN IAW SRM 51-40-02-0G-0.

Part: COVER — DISLODGED (EXIT SIGN) · airframe 62,630 hrs · 35,600 cycles

EXIT SIGN COVER ON CEILING JUST AFT OF COCKPIT DOOR FELL OFF. ACFT GROUNDED. RESECURED SIGN COVER, OK FOR SERVICE.

Part: GUIDE ARM — FAILED (L1 DOOR) · airframe 62,470 hrs · 35,495 cycles

L1 LWR HINGE COVER BINDING DURING DOOR CLOSURE. ACFT GROUNDED. FOUND UPPER AFT DOOR DAMAGE. UPPER AFT DOOR DAMAGE REMOVED. REPLACED GUIDE ARM, ADJUSTED DOOR. OPS CHK GOOD IAW MM 52-11-21 INSTALLED GUIDE ARM IAW 52-11-21-404-007.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 62,444 hrs · 35,479 cycles

F/A REPORTED THAT THE L1 DOOR IS HARD TO CLOSE. ACFT GROUNDED. FOUND UPPER GUIDE ARM OUT OF ADJUSTMENT. ADJUSTED UPPER GUIDE ARM IAW MM 52-11-00-705-007, STEP 3.G. FORCE CHECKED OK IAW MM 52-11-00-755-051.

Part: WEB — CORRODED (BS 700-724) · airframe 61,421 hrs · 34,892 cycles

LT WHEEL WELL CUT OUT VERTICAL WEB CORRODED AFT SIDE 6 O`CLOCK TO 9 O`CLOCK POSITION. REPAIRED VERTICAL WEB IAW EA 400 53EA 10105 REV NEW ISSUED DATE 09APR13.

Part: WEB — CORRODED (LT MLG WW) · corrosion level 2 · airframe 61,418 hrs · 34,891 cycles

LT MAIN W/W AFT LOWER CHORD HAS FRETTING AND CORROSION. ACFT GROUNDED. REMOVED FASTENERS AND N/PS FROM LT W/W AFT LOWER CHORD, REINSTALLED FASTENERS AND N/PS ONTO LT W/W AFT LOWER CHORD. REPAIRED VERTICAL WEB IAW EA 53EA 10105 REV NEW.

Part: CHANNEL — CORRODED (BS 1088) · airframe 60,017 hrs · 34,010 cycles

AFT TAIL COMPARTMENT JACKSCREW SUPPORT FITTINGS LOWER BOX BRACE CHANNEL IS CORRODED. ACFT GROUNDED. REMOVED CORRODED CHANNEL IAW SRM 51-40-02. FABRICATED NEW SUPPORT CHANNEL IAW BAC DWG 69-56190, REV A. ALODINED AND PRIMED NEW SUPPORT CHANNEL IAW BAC DWG 69-56190 REV A. LOCATED DRILLED, DEBURRED SUPPORT CHANNEL IAW BAC DWG 69-56190. INSTALLED NEW SUPPORT CHANNEL IAW BAC DWG 09/22/2012 65-46847.

Part: LIGHT — BROKEN (CABIN) · airframe 59,039 hrs · 33,389 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT ASSY IS BROKEN. REMOVED & INSTALLED R1 DOOR LOWER EMERGENY EXIT LIGHT ASSY OPS NORMAL, REF 33-51-02.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 58,912 hrs · 33,306 cycles

F/A REPORTS R2 EXIT SIGN COVER IS MISSING. ACFT GROUNDED. INSTALLED LIGHT COVER R2 EXIT. LIGHTS OPS GOOD.

Part: CHARGER — FAILED (CABIN) · airframe 58,566 hrs · 33,125 cycles

EMERGENCY LT AT BULLNOSE ROW 25ABC INOP. REPLACED M1197 EMERGENCY BATTERY PACK CHARGER REF WDM 33 51 15, OPS NORMAL.

Part: SUPPORT BRACKET — GOUGED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT CARGO COMPARTMENT AT BS 827 AND RBL 13.80 FRAME TO CARGO TRACK SUPPORT BRACKET HAS DEEP GOUGES IN 2 PLACES. REMOVED AND REPLACED CARGO TRACK SUPPORT BRACKET IAW B737 400 SRM 51 40 02.

Part: STRUCTURE — CRACKED (BS 500D-500E) · airframe 56,444 hrs · 31,899 cycles

UPON REMOVAL OF THE FORWARD CARGO COMPARTMENT LT TRANSITION PANEL FOUND A CRACKED BAFFLE BETWEEN BS 500D AND 500E AT STR 26L. REMOVED AND REPLACED BAFFLE IAW SRM 51-40-02 AND 51-40-05.

Part: BAFFLE — CRACKED (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

UPON REMOVAL OF TRANSITION PANEL IN FWD CARGO COMPARTMENT FOUND BAFFLE CRACKED AT BS 500A TO 500B. REMOVED DAMAGED BAFFLE FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 30 01 FIG 7 AND 51 40 02.

Part: BAFFLE — BENT (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

UPON REMOVAL OF TRANSITION PANEL IN FWD CARGO COMPARTMENT FOUND BAFFLE BS 500E TO 500F HAS BENT UPPER FLANGE REMOVED AND REPLACED BAFFLE IAW B737 400 SRM 51 40 02.

Part: BAFFLE — CRACKED (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

UPON REMOVAL OF TRANSITION PANEL IN FWD CARGO COMPARTMENT FOUND BAFFLE HAS CRACKED FORWARD LIP BS 500F TO 500G STRINGER 26R. REMOVED AND REPLACED BAFFLE CLIP IAW BOEING DWG 69 51411.

Part: BAFFLE — CRACKED (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

UPON REMOVAL OF TRANSITION PANEL IN FWD CARGO COMPARTMENT FOUND BAFFLE CRACKED AT BS 500B TO 500C STRINGER 26R. REMOVED DAMAGED BAFFLE FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 30 01 AND 51 40 02.

Part: SHEAR TIE — CORRODED (BS 500G) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

UPON REMOVAL OF TRANSITION PANEL FOUND SHEAR TIE AT BS 500G BETWEEN 25R AND 26R CORRODED. REMOVED EXISTING SHEAR TIE FABRICATED REPLACEMENT PART AND INSTALLED IAW SRM 51-40-02.

Part: INTERCOSTAL — GOUGED (BS 947-967) · airframe 56,444 hrs · 31,899 cycles

UPON REMOVAL OF POTABLE WATER PAN STRUCTURE FOUND INTERCOSTAL GOUGED IN RADIALS. FABRICATED NEW INTERCOSTAL AND INSTALLED IAW SRM 51-40-05 AND DWG 65-51626.

Part: FITTING — GALLED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

UPON BOLT REPLACEMENT FOUND STRINGER 35 TO AFT PRESSURE BULKHEAD FITTING GALLED. REPLACED AFT PRESSURE BULKHEAD STRINGER FITTING IAW B737 400 SRM 51 40 05 AND B737 400 AMM 20 50 11 912 002.

Part: SKIN — CRACKED (TE FLAP) · airframe 56,444 hrs · 31,899 cycles

RT INBOARD MID FLAP LEADING EDGE SKIN CRACKED AT INBOARD TRACK. CUT OUT DAMAGE AND INSTALLED REPAIR IAW B737 400 SRM 57 53 01 FIG 201 REPAIR 2.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

STRINGER 20R TO AFT PRESSURE BULKHEAD END FITTING BOLT HOLES ELONGATED. REPLACED AFT PRESSURE BULKHEAD END FITTING IAW B737 400 SRM 51 40 05 51 40 02 B737 400 AMM 20 50 11 912 002 AND ASA TASK CARD 5310 02671 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

CRACK FOUND AT FASTENER HOLE BS 500G FRAME. REPAIRED FRAME IAW B737 400 SRM 53 00 07 REPAIR 6.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO COMPARTMENT BAFFLE AND CLIP CRACKED BETWEEN 500C AND 500D STR 26R. REMOVED AND REPLACED BAFFLE AND CLIP IAW B737 400 SRM 51 40 02.

Part: STRINGER CLIP — BENT (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

STRINGER ATTACH CLIP BENT. REMOVED AND REPLACED STRINGER CLIP IAW B737 400 SRM 51 40 02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

CORROSION FOUND ON FRAME BS 500G STR 27R TO STR 28R, FOUND OUT OF LIMITS. REPAIRED FRAME IAW B737 400 SRM 53 00 07 REPAIR 6.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,879 cycles

FRAME TO STRINGER ATTACH CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW B737 400 SRM 51 40 02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT CARGO COMPARTMENT BS 727G RT WALL SUPPORT CORRODED AROUND FASTENERS BETWEEN STR 19R AND 25R. REMOVED AND REPLACED SIDEWALL SUPPORT ANGLE IAW B737 400 SRM 51 40 02

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

CABIN FLOOR SUPPORT CHANNEL FOUND CRACKED AT BS 500G+3. REPLACED WITH NEW SUPPORT CHANNEL IAW B737 400 SRM 51 40 02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

INTERCOSTAL CRACKED BS 360 BL 0. REMOVED CRACKED INTERCOSTAL FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

SEAT TRACK FROM BS 520 TO BS 540 LEFT OUTBOARD GOUGED. REMOVED SEAT TRACK FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 AMM 20 50 11 912 002 AND B737 400 SRM 51 40 05.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT PRESSURE BULKHEAD RISER CORRODED AT BS 1016 BL 0. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PARTS IAW ASA EA 400 53EA 05516.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

AFT CARGO EQUIPMENT BAY RT FRAME BS 1006 SHEAR TIE CORRODED BETWEEN STR 27L AND 27R. REMOVED AND REPLACED SHEAR TIE IAW B737 400 SRM 51 40 05 AND 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT CARGO EQUIPMENT BAY LT FRAME BS 986.5 CORRODED AT SHEAR TIE BETWEEN STR 27R AND 27L. REMOVED CORRODED SHEAR TIE AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

FRAME AT BS 1006 CORRODED ON UPPER FLANGE AND UNDER FRAME SPLICE BETWEEN REPAIRED FRAME IAW ASA EA 400 53EA 05595.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT PRESSURE BULKHEAD WEB CORRODED AT BS 1016 BETWEEN STR 26L AND 26R. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PARTS IAW ASA EA 400 53EA 05516.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT CARGO EQUIPMENT BAY FRAME BS 947 AFT SIDE CORRODED ON LT SKIN BETWEEN STR 25L AND 26R. REPAIRED FUSELAGE SKIN IAW ASA EA 400 53EA 05574.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO PIT FRAME BS 380 SHEAR TIE CORRODED ON AFT SIDE BETWEEN STR 29L AND 29R FOUND CORRODED AREA TO BE OUT OF LIMITS. FABRICATED NEW SHEAR TIE AND DOUBLER AND INSTALLED IAW B737 400 SRM 53 00 07 REPAIR 5.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

FRAME AT BS 1006 CORRODED ON LOWER FLANGE BETWEEN STR 22R AND 24R. REPAIRED FRAME IAW ASA EA 400 53EA 05595.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT PRESSURE BULKHEAD STIFFENER CORRODED AT BS 1016 BL 0 LOWER END. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PARTS IAW ASA EA 400 53EA 05516.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT LAVATORY FLOOR SUPPORT CORRODED BS 947 LBL 53. REMOVED CORRODED SUPPORT INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO BAY SHEAR TIE FORWARD SIDE OF BS 500B BETWEEN STR 28R AND 28L HAS CORROSION AROUND FASTENERS. REMOVED CORRODED SHEAR TIE REPAIR FABRICATED NEW REPAIR AND INSTALLED IAW B737 400 SRM 51 40 02 AND 53 00 07 REPAIR 7.

Part: STRIP — CORRODED (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

AFT PIT LT NR 1 CAP STRIP CORRODED. REMOVED CORRODED STRIP FABRICATED TREATED PRIMED TOP COATED AND INSTALLED NEW CAP STRIP IAW B737 400 SRM 51 40 05.

Part: STRIP — CORRODED (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

AFT PIT LT NR 4 CAP STRIP CORRODED. REMOVED CORRODED STRIP FABRICATED TREATED PRIMED TOP COATED AND INSTALLED NEW CAP STRIP IAW B737 400 SRM 51 40 05.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO BAY SHEAR TIE ON FORWARD SIDE OF BS 480 BETWEEN STR 28L AND 28R HAS CORROSION AROUND FASTENER CORROSION OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR ANGLE IAW B737 400 SRM 53 00 07 REPAIR 10.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO BAY ANTENNA DOUBLER BETWEEN BS 500 AND 500A STR 28L AND 28R HAS CORROSION AROUND THE AFT TWO FASTENERS. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW B737 400 SRM 53 30 53 FIG 101. REMOVED AND REPLACED FITTING IAW B737 400 SRM 51 40 02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

LT OUTBOARD FLOOR SUPPORT ANGLE CORRODED BS 578. REPAIRED SUPPORT ANGLE IAW B737 400 SRM 51 70 12.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

KEEL BEAM LOWER CHORD OUTBOARD FLANGE CORRODED OUT OF LIMITS. REPAIRED CHORD IAW B737 400 SRM 53 30 12 REPAIR 2.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO PIT FRAME BS 500B SHEAR TIE CORRODED ON FORWARD SIDE BETWEEN STR 27L AND 28L. REMOVED CORRODED SHEAR TIE REPAIR FABRICATED NEW REPAIR AND INSTALLED IAW B737 400 SRM 53 00 07 REPAIR 7.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

KEEL BEAM LOWER CHORD OUTBOARD FLANGE CORRODED OUT OF LIMITS. REPAIRED CHORD IAW B737 400 SRM 53 30 12 REPAIR 2.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

LT OUTBOARD SLAT TRACK GOUGED SEVERAL AREAS BS 727B TO BS 927. REMOVED SEAT TRACK FABRICATED REPLACEMENT PART AND INSTALLED IAW B73 400 SRM 53 00 52 REPAIR 2.

Part: STRIP — CORRODED (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

AFT PIT LT NR 3 CAP STRIP CORRODED. REMOVED CORRODED STRIP FABRICATED TREATED PRIMED TOP COATED AND INSTALLED NEW CAP STRIP IAW B737 400 SRM 51 40 05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

RT OUTBOARD FLOOR SUPPORT ANGLE CORRODED BS 639. REPAIRED SUPPORT ANGLE IAW B737 400 SRM 51 70 12.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

FORWARD PIT LT TRANSITION ANGLE CORRODED BS 460 500D. REMOVED CORRODED ANGLE. FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO BAY SHEAR TIE FORWARD SIDE OF BS 500 BETWEEN STR 28L AND 28R HAS CORROSION AROUND FASTENERS. CORROSION FOUND OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR ANGLE IAW B737 400 SRM 53 00 07 REPAIR 10.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO PIT FRAME BS 500F SHEAR TIE CORRODED ON FORWARD SIDE BETWEEN STR 26R AND 27R. REMOVED CORROSION OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07 FIG 201.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

FORWARD PIT THRESHOLD WEB HAS CORROSION AT FASTENER HOLES. REMOVED AND REPLACED NEW THRESHOLD WEB IAW B737 400 SRM 53 30 15 FIG 1 AND 51 40 02 STEP 5.

Part: STRIP — CORRODED (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

AFT PIT RT CAP STRIP NR 3 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS. FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 30 01 AND BOEING DWG 65 49613.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO BAY LT SIDEWALL SUPPORT BRACKET FORWARD OF BS 500 ABOVE STR 22L HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED SUPPORT BRACKET IAW B737 400 SRM 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO PIT FRAME BS500B SHEAR TIE CORRODED ON FORWARD SIDE BETWEEN STR 27R AND 28R BLENDED CORROSION AND FOUND OUT OF LIMITS. REMOVED SHEAR TIE FABRICATED REPLACEMENT AND INSTALLED IAW B737 400 SRM 53 00 07 REPAIR 7.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO BAY SHEAR TIE FORWARD SIDE OF BS 500A BETWEEN STR 26L AND 26R HAS CORROSION. REMOVED CORROSION WAS OUT OF LIMITS. REMOVED CORRODED SHEAR TIE FABRICATED REPLACEMENT AND INSTALLED IAW B737 400 SRM 53 00 07 REPAIR 7.

Part: STRIP — CORRODED (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

AFT PIT RT CAP STRIP NR 2 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS. FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 30 01 AND BOEING DWG 65 49613.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FORWARD PIT SHEAR TIE CORRODED BS 500E STR 26R 27R. REMOVED CORRODED SECTION FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 53 0 07 FIG 201.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO PIT FRAME BS 500D SHEAR TIE CORRODED ON FORWARD SIDE BETWEEN STR 28L AND 28R. INSTALLED NEW SHEAR TIE IAW B737 400 SRM 51 40 02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO PIT RT STR 26R CORRODED FROM BS 500F TO 500G IN CENTER AREA. REMOVED CORROSION AND FOUND OUT OF LIMITS. STOPPED DRILL CRACK AND INSTALLED REPAIR CHANNEL IAW B737 400 SRM 53 00 53 FIG 201.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO BAY SHEAR TIE AFT SIDE OF BS 500 BETWEEN STR 28R AND 27R CORRODED BLENDED CORROSION AND FOUND OUT OF LIMITS. FABRICATED REPAIR ANGLE AND INSTALLED IAW B737 400 SRM 51 40 02 AND 51 40 05.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

LT INBOARD SEAT TRACK GOUGED AND CHAFED BETWEEN BS 460 AND BS 520. REPAIRED SEAT TRACK IAW B737 400 SRM 53 00 52.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO PIT SHEAR TIE AT BS 500F CORRODED ON FORWARD SIDE BETWEEN STR 28R AND 28L. REMOVED CORROSION OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07 FIG 201.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO PIT FRAME BS 500C SHEAR CLIP CORRODED ON FORWARD SIDE AT STR 28R. REMOVED EXISTING TIE CLIP LOCATED AND INSTALLED NEW STRINGER CLIP IAW B737 400 SRM 51 40 02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT FORWARD PIT BULKHEAD SUPPORT ANGLE CORRODED BS 500G STR 25L 22L. REMOVED CORRODED ANGLE INSTALLED NEW SUPPORT ANGLE IAW B737 400 SRM 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO PIT FRAME BS 500C SHEAR TIE CORRODED ON FORWARD SIDE BETWEEN STR 28L AND 28R. REMOVED CORRODED SHEAR TIE, FABRICATED AND INSTALLED REPLACEMENT IAW B737 400 SRM 53 00 07 REPAIR 7.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FORWARD CARGO PIT FRAME BS 500D SHEAR TIE CORRODED ON FORWARD SIDE BETWEEN STR 26R AND 27R. REPAIRED SHEAR TIE IAW B737 400 SRM 53 00 07 FIG 201 REPAIR 3.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

LT INBOARD SEAT TRACK GOUGED STA 540 727 LBL 24.25. REMOVED DAMAGED TRACK,TREATED PRIMED INSTALLED NEW SEAT TRACK IAW B737 400 SRM 51 40 04.

Part: STRIP — CORRODED (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

AFT PIT LT NR 2 CAP STRIP CORRODED. REMOVED CORRODED STRIP FABRICATED TREATED PRIMED TOP COATED AND INSTALLED NEW CAP STRIP IAW B737 400 SRM 51 40 05.

Part: SUPPORT — CRACKED (PYLON) · airframe 56,444 hrs · 31,899 cycles

LT WING NR 1 ENGINE AFT PYLON FLAP TRACK FAIRING INBOARD INTERIOR ANGLE SUPPORT CRACKED. REMOVED AND REPLACED ANGLE IAW B737 400 SRM 51 40 02.

Part: WEB — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

IN AFT CARGO PIT CORROSION ON WEB STR 26R TO 25R BS 927. REMOVED AND REPLACED DAMAGED WEB IAW B737 400 SRM 51 40 02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

LT OUTBOARD FLOOR SUPPORT ANGLE CORRODED BS 639. REPAIRED SUPPORT ANGLE IAW B737 400 SRM 51 70 12.

Part: PANEL — CRACKED (COCKPIT) · airframe 56,444 hrs · 121,919 cycles

F/O'S WIRING RACEWAY PANEL IS CRACKED AT FORWARD CORNER. REMOVED DAMAGED AREA, FABRICATED REPAIR PART AND INSTALLED IAW B737 400 SRM 51 40 02 AND 51 70 13.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

FORWARD PIT LT TRANSITION ANGLE CORRODED BS 500D 500G. REMOVED TRANSITION ANGLE. FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

AFT CARGO COMPARTMENT CENTER FLOOR SUPPORT AT RBL 14 HAS LIGHT CORROSION AROUND FASTENER HOLES BS 807 TO BS 947. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW B737 400 SRM 53 60 53. REMOVED TRACK SECTION AND REPAIRED IAW ASA EA 400 53EA 05515.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT CARGO COMPARTMENT FLOORBOARD SUPPORT HAS CORROSION ON LOWER SIDE AT NUT PLATE BS 727F +7 RBL 2.5. TRIMMED OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW ASA EA 400 53EA 05500.

Part: ATTACH FITTING — BENT (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT CARGO COMPARTMENT BS 727A FRAME TO STRINGER 23R ATTACH CLIP IS BENT. REMOVED AND REPLACED CLIP IAW B737 400 SRM 51 40 02.

Part: SUPPORT — CORRODED (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

AFT CARGO COMPARTMENT BS 727G LT SIDEDWALL SUPPORT IS CORRODED AROUND FASTENER HOLES BETWEEN STR 19L AND 25L. REMOVED CORROSION OUT OF LIMITS, FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

SHEAR TIE CORRODED BS727A +15 RBL 2. REMOVED CORRODED SHEAR TIE, FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 20 01 AND 51 40 02.

Part: TRANS PANEL — CORRODED (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

AFT PIT TRANSITION PANEL CORRODED SEVERAL AREAS BS 727 TO BS 727F. REMOVED CORRODED PANEL AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 05.

Part: TRANS PANEL — CORRODED (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

AFT CARGO COMPARTMENT LEFT TRANSITION PANEL HAS CORROSION MULTIPE PLACES BS 807 TO BS 947. REMOVED TRANSITION PANEL, FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 05 AND 51 40 02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AT BS 360 STR 11L STRINGER TO FRAME CLIP IS CRACKED IN RADIUS. REPLACED CLIP IAW ASA EA 400 53EA 0543.

Part: ANGLE — CORRODED (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

AFT PIT TRANSITION "Z" ANGLE HAS CORROSION AT FASTENER HOLES BS 727 TO BS 767. BLENDED AREA FOUND OUT OF LIMITS, FABRICATED REPAIR PARTS IAW B737 400 SRM 51 40 05 AND 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

SHEAR TIE AT BS 520 BETWEEN STR 28L AND 28R IS CORRODED. REMOVED DAMAGED PART FABRICATED REPLACEMENT AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: PANEL — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT CARGO DOOR FORWARD CUTOUT LOWER CLOSE OUT PANEL IS CORRODED. REMOVED CORROSION OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR PARTS IAW B737 400 SRM 51 70 13 FIG 1.

Part: TRANS PANEL — CORRODED (CARGO BAY) · airframe 56,444 hrs · 31,899 cycles

AFT PIT LT TRANSITION PANEL CORRODED BS 727F TO BS 807. REMOVED CORRODED PANEL, FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 05.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT CARGO COMPARTMENT BS 727G REPAIR SPLICE IS CORRODED ABOVE STR 25L. REMOVED AND REPLACED REPAIR SPLICE IAW B737 400 SRM 53 60 07 FIG 1 AND 51 70 11 FIG 1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

IN AFT PIT BS 727B STR 27R TO 26R FRAME IS CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT CARGO COMPARTMENT BS 727C FRAME SHEAR TIE IS CORRODED BETWEEN STR 25L AND STR 26L. REMOVED CORROSION FOUND OUT OF LIMITS, FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 70 11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

FLOOR SUPPORT BETWEEN BEAMS AT BS 360 TO BS 380 CORRODED ON UPPER SURFACE AT RBL 12. REMOVED AND REPLACED FLOOR SUPPORT IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

PASSENGER CABIN FRAME CRACKED BS 400 STR 8R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 120.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

RIGHT FRAME BS 787 CRACKED AT PSU MOUNT BRACKET STR 8R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 120.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT CABIN LT FUSELAGE FRAME BS 787 CRACKED AT PSU MOUNT BRACKET STR 8L. REPAIRED FRAME IAW ASA EA AD20062609 400 53 120.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

TOP OF FLOORBEAM AT BS 360 CORRODED AT FASTENER HOLE LBL 10. REPAIRED FLOORBEAM IAW ASA EA 400 53EA 05459.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT PASSENGER CABIN BS 827 LT FRAME CRACKED AT PSU ATTACH BRACKET STR 8L. REPAIRED FRAME IAW ASA EA AD20062609 400 53 120.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

PASSENGER CABIN FRAME CRACKED BS480 STR 8R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 120.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

PASSENGER CABIN FRAME CRACKED AT BS 380 STR 8R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 120.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT CABIN LT FUSELAGE FRAME BS 907 CRACKED AT PSU MOUNT ATTACH BRACKET STR 8L. REPAIRED FRAME IAW ASA EA AD20062609 400 53 120.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FLOORBEAM STA 312 CORRODED BETWEEN LBL 12 TO RBL 12. REMOVED CORRODED UPPER CHORD, FABRICATED TREATED PRIMED TOP COATED AND INSTALLED NEW UPPER CHORD REPAIR IAW B737 400 SRM 53 10 51 FIG 201 REPAIR 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,444 hrs · 31,899 cycles

FLOOR BEAM CORRODED STA 294 BETWEEN BL 0 AND RBL 12. REMOVED UPPER CHORD. FABRICATED TREATED PRIMED TOP COATED AND INSTALLED NEW UPPER CHORD IAW B737 400 SRM 53 10 51 FIG 201 REPAIR 5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT PASSENGER CABIN BS 747 LT FRAME CRACKED AT PSU MOUNT ATTACH BRACKET STR 8L. REPAIRED FRAME IAW ASA EA AD20062609 400 53 120.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT PASSENGER CABIN BS 727F LT FRAME CRACKED AT PSU MOUNT ATTACH BRACKET STR 8L. REPAIRED FRAME IAW ASA EA AD20062609 400 53 120.

Part: SILL — CORRODED (FUSELAGE) · airframe 56,444 hrs · 31,899 cycles

AFT PIT LOWER SILL WEB CORRODED. REMOVED CORRODED WEB AND INSTALLED REPLACEMENT IAW B737 400 SRM 51 40 02.

Part: SKIN — DENTED (SPOILER) · airframe 56,449 hrs · 31,899 cycles

RIGHT WING SPOILER NR 6 UPPER SURFACE HAS TWO EACH PROTRUSIONS ON OUTBOARD HALF APPROX 8 IN FROM TRAILING EDGE. REPAIRED SPOILER IAW B737 400 SRM 51 70 10.

Part: SLAT — DELAMINATED (RT WING) · airframe 56,444 hrs · 31,899 cycles

RIGHT WING LEADING EDGE SLAT NR 6 INBOARD AFT CORNER DELAMINATED. REPAIRED DAMAGED SLAT IAW B737 400 SRM 51 70 02 REPAIR 4.

Part: SLAT — CHAFED (RT WING) · airframe 56,444 hrs · 31,899 cycles

RIGHT WING LEADING EDGE SLAT NR 5 INBOARD LOWER TRAILING EDGE CORNER CHAFED. REPAIRED DAMAGED SLAT IAW B737 400 SRM 51 70 02 REPAIR 4.

Part: WEDGE — CHAFED (LE SLAT) · airframe 56,444 hrs · 31,899 cycles

RT WING LEADING EDGE SLAT LOWER TRAILING EDGE CHAFED. REPAIRED DAMAGED AREA OF SLAT TRAILING EDGE WEDGE IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DELAMINATED (NR 3 SLAT) · airframe 56,444 hrs · 31,899 cycles

LEFT WING LEADING EDGE NR 3 SLAT INBOARD LOWER TRAILING EDGE CHAFED WITH DELAMINATION. BONDED REPAIR IAW SRM 51-70-10 REPAIR 4.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 56,444 hrs · 31,899 cycles

LEFT WING LEADING EDGE SLAT NR 2 OUTBOARD AFT CORNER DELAMINATED. BONDED REPAIR IAW SRM 51-70-10 REPAIR 4.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 56,444 hrs · 31,899 cycles

LEFT WING LEADING EDGE SLAT NR 2 INBOARD AFT CORNER DELAMINATED IN TWO PLACES. BONDED REPAIR IAW SRM 51-70-10 REPAIR 4.

Part: SKIN — DELAMINATED (NR 3 SLAT) · airframe 56,444 hrs · 31,899 cycles

LEFT WING LEADING EDGE NR 3 SLAT OUTBOARD AFT CORNER DELAMINATED. BONDED REPAIR IAW SRM 51-70-10 REPAIR 4.

Part: STRAP — CRACKED (BS 328) · airframe 56,444 hrs · 31,899 cycles

E&E BAY CABIN FLOOR SUPPORT STRAP CRACKED AT BS 328 LBL 46. STOP DRILLED CRACK AND INSTALLED REPAIR PLATE IAW SRM 53-10-51.

Part: BUSHING — GALLED (VERTICAL STAB) · airframe 56,444 hrs · 31,899 cycles

LEFT FORWARD VERTICAL STABILIZER BOLT FORWARD ATTACH LUG BUSHING IS GALLED. REPAIRED BUSHING PER ASA EA 400 55EA 05422.

Part: SUPPORT FITTING — GOUGED (FUSELAGE) · airframe 56,313 hrs · 35,895 cycles

AFT PRESSURE BULKHEAD SUPPORT FITTING BOLT HOLE IS GOUGED AT BOLT 81L. REMOVED AND REPLACED AFT PRESSURE BULKHEAD FITTING IAW B737 400 SRM 51 40 02 AND 51 40 05.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 53,028 hrs · 29,849 cycles

NR 4 SLAT T/E OUTBOARD END UPPER SURFACE DELAMINATED. REPAIRED DELAMINATION ON OUTBOARD SURFACE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,028 hrs · 29,849 cycles

INTERCOSTAL CORRODED AT CARGO COMPARTMENT BS 727A - 727B BETWEEN STRINGER 26R - 27R. REMOVED DAMAGED INTERCOSTAL AND REPLACED WITH NEW.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 53,028 hrs · 29,849 cycles

LEFT CUSP WEB AT STA 867 - 887 HAS CORROSION. REMOVED CUP WEB, FABBED REPAIR PART AND INSTALLED.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 53,028 hrs · 29,849 cycles

RIGHT CUSP WEB AT STA 787 - 807 HAS CORROSION. REMOVED CORRODED WEB SECTION, FABBED DOUBLER AND FILLER AND INSTALLED REPAIR PARTS.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,028 hrs · 29,849 cycles

LEFT CUSP WEB AT STA 727G - 747 HAS CORROSION IN IT. REMOVED CORRODED CUSP WEB, FABBED REPLACEMENT WEB AND INSTALLED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 53,028 hrs · 29,849 cycles

INTERCOSTAL CORRODED AFT CARGO COMPARTMENT. REMOVED AND REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,028 hrs · 29,849 cycles

INTERCOSTAL CORRODED AT CARGO COMPARTMENT BS 727A - 727B BETWEEN STRINGER 26R - 27R. DURING DAMAGE REMOVAL FOUND CRACK IN RADIUS. REMOVED DAMAGED INTERCOSTAL AND REPLACED WITH NEW.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 53,028 hrs · 29,849 cycles

INTERCOSTAL CORRODED AFT CARGO COMPARTMENT BS 727A - 727B BETWEEN STRINGER 26R - 27R. REMOVED AND REPLACED WITH NEW.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,028 hrs · 29,849 cycles

FRAME AT STA 767 ABOVE STR 24L 24R HAVE CORROSION AT FASTENER HOLES. REMOVED CORRODED FRAME AND INSTALLED NEW FRAME.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,028 hrs · 29,849 cycles

FRAME AT STA 727C BETWEEN STR 26L 27L IS CORRODED AT PREVIOUS DOUBLER. REMOVED PREVIOUS REPAIR, FABBED NEW REPAIR AND INSTALLED REPAIR PARTS.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 53,028 hrs · 29,849 cycles

RIGHT WING I/B AFT FORE FLAP UPPER SURFACE DELAMINATED. REMOVED DAMAGED AREA, FABRICATED REPAIR AND BONDED.

Part: DOUBLER — CHAFED (VERTICAL STAB) · airframe 53,028 hrs · 29,849 cycles

DOUBLER CHAFED STN 887 TO 915 UNDER DORSAL FIN L/E AREA. REMOVED PREVIOUS DOUBLER, FABBED NEW DOUBLER AND REPAIR PARTS AND INSTALLED.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,028 hrs · 29,849 cycles

LEFT WING I/B FLAP T/E OUTBOARD END UPPER AND LOWER SURFACE DELAMINATED. REMOVED DAMAGED AREA, FABRICATED REPAIR AND BONDED.

Part: SKIN — DENTED (SPOILER) · airframe 53,028 hrs · 29,849 cycles

RT WING NR 5 SPOILER DENTED OUT OF LIMITS ON LOWER I/B SURFACE. REMOVED AREA OF DAMAGE, FABRICATED FILLER SKIN AND DOUBLER AND BONDED.

Part: SKIN — CHAFED (TE FLAP) · airframe 53,028 hrs · 29,849 cycles

RIGHT O/B AFT FLAP LOWER SURFACE CHAFED 1 FROM T/E BETWEEN NR 8 TRACK FAIRING CHAFE PAD. REMOVED CHAFED AREA, FABBED REPAIR PARTS AND BONDED.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,028 hrs · 29,849 cycles

RIGHT WING I/B AFT T/E FLAP UPPER O/B SURFACE AT PREVIOUS REPAIR DELAMINATED. REMOVED DAMAGED DOUBLER, PERFORMED MOISTURE EVACUATION, FABBED REPAIR PARTS AND INSTALLED.

Part: SKIN — CHAFED (TE FLAP) · airframe 53,028 hrs · 29,849 cycles

RIGHT WING O/B TRAILING EDGE FLAP IS CHAFED AT LOWER LEADING EDGE ON I/B END. REMOVED DAMAGED AREA, FABBED REPAIR PARTS AND INSTALLED.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 53,028 hrs · 29,849 cycles

RIGHT WING NR 5 L/E SLAT T/E WEDGE I/B SIDE DELAMINATED. REMOVED DAMAGED AREA, FABBED REPAIR PARTS AND BONDED.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,028 hrs · 29,849 cycles

LEFT T/E OUTBOARD AFT FLAP DELAMINATED 24 INCHES INBOARD OF NR 1 FLAP TRACK. REMOVED DAMAGED AREA, FABBED REPAIR SKIN AND DOUBLER, AND BONDED.

Part: SKIN — CHAFED (TE FLAP) · airframe 53,028 hrs · 29,849 cycles

LEFT WING O/B TRAILING EDGE FLAP LOWER SURFACE CHAFED JUST O/B OF NR 1 FLAP TRACK. REMOVED DAMAGED AREA, FABBED REPAIR AND BONDED.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 53,028 hrs · 29,849 cycles

RIGHT WING NR 5 L/E SLAT UPPER SURFACE OF T/E WEDGE DELAMINATED. REMOVED DAMAGED AREA, FABBED REPAIR PARTS AND BONDED.

Part: SKIN — DAMAGED (LE SLAT) · airframe 53,028 hrs · 29,849 cycles

LEFT WING NR 3 L/E SLAT OUTER L/E SKIN DENTED WITH CREASE. REMOVED DAMAGED AREA, FABBED REPAIR PARTS AND INSTALLED.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 53,028 hrs · 29,849 cycles

RIGHT WING NR 4 L/E SLAT I/B END OF T/E WEDGE PREVIOUS REPAIR DELAMINATED. REMOVED DAMAGED AREA, FABBED REPAIR PARTS AND BONDED.

Part: SKIN — CRACKED (LE SLAT) · airframe 53,028 hrs · 29,849 cycles

NR 6 SLAT LOWER L/E CRACKED AT 4 RIVETS UNDER THE I/B AND TRACK. REMOVED DAMAGED AREA FABBED AND INSTALLED REPAIR.

Part: SKIN — CHAFED (LE SLAT) · airframe 53,028 hrs · 29,849 cycles

LEFT WING L/E SLAT NR 3 T/E WEDGE I/B LOWER SURFACE CHAFED PREVIOUS REPAIR. REMOVED DAMAGED AREA, FABBED REPAIR AND BONDED.

Part: SKIN — CHAFED (TE FLAP) · airframe 53,028 hrs · 29,849 cycles

LEFT WING O/B AFT FLAP DEEP CHAFE BETWEEN RUB STRIPS 2 INCHES O/B OF NR 2 FLAP TRACK. REMOVED DAMAGED AREA, FABBED REPAIR PARTS AND BONDED.

Part: MECHANISM — LACK OF LUBE (L1 DOOR) · airframe 51,615 hrs · 29,030 cycles

F/A CANNOT CLOSE L1 DOOR. LUBRICATED GUIDE PLATES LATCH CRANK BEARINGS DOOR COUNTER BALANCE GUIDE ARM UPPER AND LOWER HINGE POINTS REF 737 MM 12 25 21 643 007. ACCOMPLISHED FWD ENTRY DOOR TEST PER 737 MM 52 11 00 755 051 TORQUE CHECK. DOOR OPENS AND CLOSES WITHIN TORQUE LIMITS, OK FOR SERVICE.

Part: MECHANISM — LACK OF LUBE (L1 DOOR) · airframe 51,615 hrs · 29,030 cycles

F/A CANNOT CLOSE L1 DOOR. LUBRICATED GUIDE PLATES LATCH CRANK BEARINGS DOOR COUNTER BALANCE GUIDE ARM UPPER AND LOWER HINGE POINTS REF 737 MM 12 25 21 643 007. ACCOMPLISHED FWD ENTRY DOOR TEST PER 737 MM 52 11 00 755 051 TORQUE CHECK. DOOR OPENS AND CLOSES WITHIN TORQUE LIMITS, OK FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,792 hrs · 28,547 cycles

DENT IN FUSELAGE JUST UNDER FWD CARGO DOOR NEXT TO EXISTING REPAIR DOUBLER. FABRICATED EXTERNAL DOUBLER/TRIPLER AND INSTALLED REPAIR PARTS.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 49,711 hrs · 27,910 cycles

LEFT INBOARD MIDFLAP T/E WEDGE HAS DENTS NEXT TO A PREVIOUS REPAIR. REMOVED DAMAGE, FABBED FILLER AND DOUBLER, BONDED THE REPAIR IAW B737 400 SRM 51-70-10 REPAIR 2.

Part: SKIN — DENTED (NR 7 SPOILER) · airframe 49,711 hrs

NR 7 SPOILER UPPER SURFACE HAS PROTRUDING DENT 5 INCHES AFT OF L/E. REMOVED DAMAGED AERA, FABBED DOUBLER AND INSTALLED REPAIR IAW B737 400 SRM 57 70 01.

Part: FRAME — CRACKED (BS 616) · airframe 49,711 hrs · 27,910 cycles

BODY STA 616 FRAME LT SIDE INNER CHORD IS CRACKED BELOW FLOOR WL 202. REMOVED DAMAGED AREA, FABBED FILLER AND STIFFENING ANGLES AND INSTALLED REPAIR PARTS IAW ASA EO 5310 02528.

Part: SKIN — DENTED (NR 7 SPOILER) · airframe 47,911 hrs · 27,910 cycles

NR 7 SPOILER UPPER SURFACE HAS PROTRUDING DENT 5 INCHES AFT OF L/E. PREPPED DAMAGED AREA, FABBED DOUBLER AND INSTALLED THE REPAIR IAW 57-70-01.

Part: SKIN — DELAMINATED (NR 1 SLAT) · airframe 49,711 hrs · 27,910 cycles

NR 1 SLAT LOWER T/E SURFACE IS DELAMINATED AT THE OUTBOARD CORNER. REMOVED DELAM SKIN AND CORE FABBED REPLACEMENT CORE, SKIN AND DOUBLER. BONDED REPAIR IAW B737 400 SRM 51 70 10 8.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 49,711 hrs · 27,910 cycles

NR 2 SLAT T/E LOWER SURFACE IS DELAMINATED AT OUTBOARD CORNER. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, INSTALLED REPAIR IAW B737 400 SRM 51-70-10 FIG 4.

Part: SKIN — CHAFED (NR 3 SLAT) · airframe 49,711 hrs · 27,910 cycles

NR 3 SLAT LOWER SURFACE T/E INBOARD END IS CHAFED. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER. BONDED REPAIR IAW B737 400 SRM 51-70-10.

Part: SKIN — DENTED (BS 390 S18L) · airframe 49,711 hrs · 27,910 cycles

FUSELAGE SKIN HAS A DENT LT SIDE STA 390 STR 18L. REMOVED DAMAGED AREA, FABBED DOUBLER AND INSTALLED REPAIR IAW AAREA 12887.

Part: SKIN — DELAMINATED (NR 4 SLAT) · airframe 49,711 hrs · 27,910 cycles

NR 4 SLAT INBOARD T/E IS DELAMINATED ON THE TOP INBOARD END. PREPPED DAMAGED AREA, FABBED CORE PLUG AND DOUBLER, INSTALLED REPAIR IAW B737 400 SRM 51-70-10 REPAIR 4.

Part: SKIN — CHAFED (NR 5 SPOILER) · airframe 49,711 hrs · 27,910 cycles

NR 5 SPOILER LOWER SURFACE CHAFED ON I/B 8D END. PREPPED DAMAGED AREA, FABBED FILLER AND DOUBLER, INSTALLED REPAIR IAW B737 400 SRM 51-70-10 REPAIR 4.

Part: SKIN — DENTED (NR 4 SPOILER) · airframe 49,711 hrs · 27,910 cycles

NR 4 SPOILER LOWER SURFACE HAS MULTIPLE DENTS IN 6 LOCATIONS. PREPPED 6 AREAS FOR REPAIRS FABBED 6 DOUBLERS AND BONDED REPAIRS IAW B737 400 SRM 51-70-10 REPAIR 2. NOTE THE 2 REPAIRS ON THE INBOAR END HAVE THE SAME DIMENSIONS WBL 87.75 92.25 ABOVE AND BELOW THE BULB SEAL.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 49,711 hrs · 27,910 cycles

RIGHT INBOARD FOREFLAP LOWER SURFACE HAS SEVERAL DENTS OUTBOARD OF INBOARD TRACK. REMOVED DAMAGED AREA, FABBED DOUBLER AND BONDED REPAIR IAW B737 400 SRM 51-70-10 REPAIR 2.

Part: SKIN — DENTED (BS 500B) · airframe 49,711 hrs · 27,910 cycles

FUSELAGE SKIN HAS A DENT AT STA 500B STR 29L A=.160 Y=.039 AY=4.10. AY MUST NOT BE LESS THAN 30. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, INSTALLED REPAIR PARTS IAW.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 49,711 hrs · 27,910 cycles

LEFT INBOARD FOREFLAP LOWER SURFACE HAS MULTIPLE SHARP DENTS. PREPPED DAMAGED AREA, FABBED DOUBLER AND BONDED REPAIR IAW B737 400 SRM 51-70-10 REPAIR 2.

Part: SKIN — DENTED (BS 727A-727C) · airframe 49,711 hrs · 27,910 cycles

DENT ON FUSELAGE SKIN AT BS 727C JUST BELOW STR 16R, GOES OVER STRINGER AND FRAME. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, INSTALLED REPAIR PARTS IAW AAREA 12889.

Part: LIGHT — MISSING (ROW 16 RH) · airframe 45,934 hrs · 25,887 cycles

SEVEN INCHES OF PHOTOLUMINSCENT EMERGENCY TRACK LIGHTING MISSING. MISSING STRIP LOCATED AT ROW 16 OVER THE MLG VIEWING WINDOW COVER. REPLACED THE MISSING SECTION OF THE PHOTOLUMINSCENT STRIP.

Part: BATTERY — OVERHEATED (MASTER) · airframe 44,455 hrs · 25,041 cycles

FLT CREW AND FLT ATTENDANTS REPORT BURNING PLASTIC SMELL IN CABIN AND COCPIT JUST BEFORE BEGINNING DESCENT. FOUND MAIN BATTERY VOLTAGE LESS THAN 20 VOLTS BATTERY VERY WARM AND SMELLING HOT REPLACED BATTERY.

Part: SHEAR TIE — CRACKED (BS 880-890) · airframe 43,464 hrs · 24,492 cycles

GROUND CREW REPORTS ACFT CONTACTED GROUND EQUIPMENT DURING THE PUSH FROM THE GATE. LARGE TEAR IN BELLY SKIN. SHEAR TIE DAMAGED. REMOVED DAMAGED SKIN AREA AND INSTALLED EXTERNAL DOUBLERS PER SRM. REPAIRED SHEAR TIE PER SRM 53 00 01 REPAIR 7. REPLACED SUPPORT CHANNEL.

Part: WEB — MISDRILLED (BS 353) · airframe 42,339 hrs · 23,865 cycles

FOUND MISDRILLED HOLE IN CASTING WEB. REMOVED DAMAGED CASTING WEB AND REPLACED PER EA 5310 02633.

Part: SKIN — LIGHTNING STRIKE (BS 3315) · airframe 42,339 hrs · 23,865 cycles

FOUND LIGHTNING STRIKE IN CROWN. CUTOUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND TRIPLER PER EA 5310 02636.

Part: SHEAR TIE — CORRODED (BS 727D) · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. REPAIRED DAMAGED SHEAR TIE PER SRM 53 00 07 REPAIR 3.

Part: DOUBLER — CRACKED (BS 361) · airframe 42,339 hrs · 23,865 cycles

FOUND CRACK ON CIRCUMFERENTIAL DOUBLERS. REPLACED DOUBLER PER EA 5310 02638.

Part: SILL — CORRODED (BS 947-986) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORRODED MOPSILL AT AFT ENTRY DOOR. BLENDED CORROSION ON MOPSILL OUT OF LIMITS. REMOVED AND REPLACED MOPSILL PER SRM 51 40 02.

Part: STRINGER — MISDRILLED (FUSELAGE) · airframe 42,339 hrs · 23,865 cycles

MISDRILLED STRINGER. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW SRM 53 00 03 AND EA 5310 02635.

Part: SHEAR TIE — CORRODED (BS 500G) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. CUT OUT DAMAGE AND FABRICATED AND INSTALLED REPAIR PER SRM 53 00 09.

Part: SHEAR TIE — CORRODED (BS 727F) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. REMOVED AND REPLACED SHEAR TIE FRAME PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 727F) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. REPLACED FRAME PER SRM 51 40 02.

Part: SHEAR TIE — CORRODED (BS 727D) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORRODED KEEL BEAM SUPPORT CLIP. REMOVED AND REPLACED PER SRM 51 40 02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND FLOORBEAM CORRODED. REMOVED DAMAGED UPPER CHORD AND INSTALLED DOUBLER PER EA 53 20 01755.

Part: FLOORBEAM — CORRODED (BS 1016) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORRODED FLOORBEAM UPPER FLANGE. REPAIRED FLOORBEAM IAW EA 53 10 02634 AND ER 06 1946 AND SRM 53 80 08.

Part: SILL — CORRODED (BS 300-350) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON MOPSILL. REPLACED PER SRM 51 40 02.

Part: FRAME — GOUGED (BS 1016) · airframe 42,339 hrs · 23,865 cycles

FOUND GOUGE IN FRAME. BLENDED OUT DAMAGE AND INSTALLED REPAIR STRAP IAW EA 5310 02630.

Part: FRAME — CRACKED (BS 303) · airframe 42,339 hrs · 23,865 cycles

FOUND FRAME CRACKED. REPAIRED BY CUTTING OUT DAMAGED AREA AND INSTALLING DOUBLER IAW EA 5310 02627.

Part: SKIN — DAMAGED (BS 727B) · airframe 42,339 hrs · 23,865 cycles

FOUND SCRIBE MARKS ON SKIN. BLENDED AND TREATED PER EA 5330 02097.

Part: SKIN — CORRODED (BS 727B-727D) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SKIN. BLENDED AND INSTALLED DOUBLER PER EA 5330 02097.

Part: FLOORBEAM — GOUGED (BS 927) · airframe 42,339 hrs · 23,865 cycles

FOUND FLOORBEAM GOUGED. REPAIRED FLOORBEAM PER EA 5310 02628.

Part: FRAME — CRACKED (BS 2915) · airframe 42,339 hrs · 23,865 cycles

FOUND CRACKED FRAME. REMOVED EXISTING REPAIR TRIMMED OUT CRACK AND INSTALLED NEW REPAIR IAW EA 5310 02626.

Part: SKIN — DAMAGED · airframe 42,339 hrs · 23,865 cycles

FOUND FUSELAGE SKIN HAS SCRIBE MARKS AT WING TO BODY FARINGS. BLENDED AND INSTALLED DOUBLER PER EA 5330 02097.

Part: FLOORBEAM — GOUGED (BS 927) · airframe 42,339 hrs · 23,865 cycles

FOUND FLOORBEAM GOUGED. REPAIRED FLOORBEAM PER EA 5310 02628.

Part: TEE FITTING — CORRODED (BS 355) · airframe 42,339 hrs · 23,865 cycles

FOUND T CHORD CORRODED. REMOVED AND REPLACED PER SRM 51 40 02 AND 51 70 12.

Part: FLOORBEAM — GOUGED (BS 927) · airframe 42,339 hrs · 23,865 cycles

FOUND FLOORBEAM GOUGED. REPAIRED FLOORBEAM IAW EA 531 02628.

Part: SHEAR TIE — CORRODED (BS 727E) · airframe 42,339 hrs · 23,865 cycles

FOUND CORRODED SHEAR TIE. FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER SRM 51 40 02.

Part: RIB — CRACKED (LWS 1355 S2-3L) · airframe 42,339 hrs · 23,865 cycles

FOUND LEFT WING RIB CRACKED. REPAIRED WING RIB PER EA 5310 02629 AND ER06 1899.

Part: SHEAR TIE — CORRODED (BS 727G) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORRODED SHEAR TIE. CUTOUT DAMAGE AND REPAIRED PER SRM 53 00 07.

Part: STOP FITTING — DAMAGED (BS 492 S24R) · airframe 42,339 hrs · 23,865 cycles

FOUND MECHANICAL DAMAGE ON DOOR STOP FITTING. REPLACED STOP FITTING PER SRM 51 40 02.

Part: SILL — CORRODED (BS 927-990) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON MOPSILL. INSTALLED NEW MOPSILL PER SRM 53 60 15.

Part: SILL — CORRODED (BS 277-280) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON MOPSILL CORROSION ON MOPSILL FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED MOPSILL PER SRM 53 10 15.

Part: FRAME — CORRODED (BS 787 S25-26L) · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON FRAME. CUT OUT DAMAGE AND INSTALLED REPAIR PER SRM 53 60 07.

Part: FRAME — DAMAGED (BS 727C) · airframe 42,339 hrs · 23,865 cycles

FOUND OVERSIZED FLOOR TO SIDEWALL SUPPORT PLATE ATTACH HOLE. REPAIRED DAMAGED FLOOR TO SIDEWALL SUPPORT ATTACH HOLE ON FRAME.

Part: SHEAR TIE — CORRODED (BS 727D) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORRODED SHEAR TIE. REMOVED CORRODED SHEAR TIE OUT OF LIMITS. REPLACED SHEAR TIE PER SRM 53 00 07.

Part: FRAME — CORRODED (BS 807 S25-26L) · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON FRAME. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 51 70 11.

Part: FRAME — CORRODED (BS 747 S25-26L) · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON FRAME. CORRODED OUT OF LIMITS REMOVED FABRICATED AND INSTALLED FRAME CAP PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 727D) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON ACB SHEAR TIE. REMOVED AND REPLACED SHEAR TIE PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 727D) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND SHEAR TIE CORRODED. FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 727D) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND SHEAR TIE CORRODED. FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 787) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORRODED SHEAR TIE. CUT OUT DAMAGE AND INSTALLED REPAIR PER SRM 53 00 07.

Part: FRAME — CORRODED (BS 727G) · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON FRAME. INSTALLED REPAIR DOUBLER PER SRM 51 70 11.

Part: FRAME — CORRODED (BS 947 S24-26R) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND AFT CARGO FRAME HAS CORROSION. FABRICATED AND INSTALLED REPLACEMENT FRAME PER SRM 51 40 02.

Part: STRINGER CLIP — CRACKED (BS 727E S24L) · airframe 42,339 hrs · 23,865 cycles

FOUND STRINGER CLIP CRACKED. REPLACED STRINGER CLIP PER SRM 51 40 02.

Part: SHEAR TIE — CORRODED (BS 727D) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND SHEAR TIE CORRODED. FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER SRM 53 00 07.

Part: STRINGER CLIP — CRACKED (BS 727E S25L) · airframe 42,339 hrs · 23,865 cycles

FOUND STRINGER CLIP CRACKED. REPLACED STRINGER CLIP PER SRM 51 40 02.

Part: SHEAR TIE — CORRODED (BS 727D) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND SHEAR TIE CORRODED. FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 767) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORRODED SHEAR TIE. CUT OUT AND REPAIRED PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 727F) · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON FRAME SHEAR TIE. REMOVED AND REPLACED FRAME SHEAR TIE PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 727F) · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. REMOVED AND REPLACED FRAME.

Part: SHEAR TIE — CORRODED (BS 500F) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. REMOVED CORROSION ON SHEAR TIE OUT OF LIMITS AND REPAIRED PER SRM 53 00 07 REPAIR 10.

Part: SHEAR TIE — CORRODED (BS 500F) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. REPAIRED PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 727E) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON AFT CARGO BAY SHEAR TIE. REPAIRED PER SRM 53 00 07.

Part: FRAME — GOUGED (BS 440 S25R) · airframe 42,339 hrs · 23,865 cycles

FOUND DEEP GOUGE ON RADIUS OF FRAME. REMOVED AND REPLACED FRAME PER SRM 51 40 02.

Part: SHEAR TIE — CORRODED (BS 727C) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORRODED SHEAR TIE. CUTOUT AND REPAIRED PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 787) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE OUT OF LIMITS. CUT OUT DAMAGED INSTALLED REPAIR PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 727F) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. CUT OUT CORROSION AND REPAIRED SHEAR TIE PER SRM 53 00 07.

Part: STRINGER CLIP — CRACKED (BS 947 S25R) · airframe 42,339 hrs · 23,865 cycles

FOUND STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM 51 40 02.

Part: STRAP — CORRODED (BS 787-852) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

AFT CARGO THRESHOLD IB UPPER STRAP CORRODED. REMOVED AND REPLACED STRAP PER SRM 51 40 02.

Part: SHEAR TIE — CORRODED (BS 727C) · airframe 42,339 hrs · 23,865 cycles

FOUND CORRODED SHEAR TIE. CUTOUT AND REPAIRED PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 727C) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION SHEAR TIE. CUTOUT AND REPAIRED PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 787) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. FABRICATED AND INSTALLED REPLACEMENT STRINGER TIE PER SRM 51 40 02.

Part: SHEAR TIE — CRACKED (BS 787) · airframe 42,339 hrs · 23,865 cycles

FOUND CRACKED SHEAR TIE. CUT OUT DAMAGED SHEAR TIE AND REPLACED WITH NEW SHEAR TIE PER SRM 53 00 07.

Part: SHEAR TIE — CRACKED (BS 787) · airframe 42,339 hrs · 23,865 cycles

FOUND CRACKED SHEAR TIE. CUTOUT SHEAR TIE AND REPLACED PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 500G S27-28R) · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. REMOVED AND REPLACED SHEAR TIE PER SRM 53 00 07 51 40 02 51 21 19.

Part: WEB — CORRODED (BS 790-847) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND AFT CARGO THRESHOLD WEB CORRODED. INSTALLED NEW THRESHOLD WEB PER SRM 53 60 15.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON FLOORBEAM. REPAIRED FLOORBEAM PER SRM 53 00 51.

Part: ANGLE — CRACKED (BS 277-294) · airframe 42,339 hrs · 23,865 cycles

L ANGLE CRACKED 9 INCHES FWD OF GALLEY DOOR 2 INCHES FROM TOP STOP. REMOVED AND REPLACED PER SRM 51 40 2.

Part: SHEAR TIE — CORRODED (BS 500G) · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. REMOVED CORROSION AND INSTALLED REPAIR PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 727F) · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON FRAME SHEAR TIE. REMOVED AND REPLACED FRAME PER SRM 53 00 07 AND 51 40 02.

Part: CLIP — CORRODED (BS 727F) · airframe 42,339 hrs · 23,865 cycles

FOUND CORRODED KEEL BEAM SUPPORT CLIPS. REMOVED AND REPLACED PER SRM 51 40 02.

Part: STRINGER CLIP — CRACKED (BS 440 S14R) · airframe 42,339 hrs · 23,865 cycles

FOUND CRACKED STRINGER CLIP. REMOVED AND REPLACED CRACKED STRINGER CLIPS PER SRM 51 40 02 AND 53 00 03.

Part: WEB — CORRODED (BS 312-344) · airframe 42,339 hrs · 23,865 cycles

FOUND SUB THRESHOLD WEB AT FED CORRODED. REPLACED PER SRM 53 10 15 AND 51 40 02.

Part: FRAME — CORRODED (BS 727F S25-26L) · airframe 42,339 hrs · 23,865 cycles

CORROSION FOUND ON FRAME. REPLACED FRAME PER SRM 51 40 2 AND 53 00 07.

Part: SHEAR TIE — CORRODED (BS 500F) · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. REPAIRED PER SRM 53 00 07 REPAIR 10.

Part: SHEAR TIE — CORRODED (BS 500D) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. REPAIRED PER SRM 53 00 07.

Part: STRINGER — CORRODED (BS 1117-1129) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON APU COMPARTMENT RT TORQUE BOX STRINGER BELOW APU AIR INLET CUTOUT. REMOVED AND REPLACED STRINGER PER SRM 53 80 13.

Part: SHEAR TIE — CORRODED (BS 727E) · airframe 42,339 hrs · 23,865 cycles

FOUND SHEAR TIE CORRODED. CUTOUT DAMAGE AND INSTALLED REPAIR PER SRM 53 00 07.

Part: STRINGER — CORRODED (BS 1129 S18R) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON APU COMPARTMENT RT TORQUE BOX STRINGER ABOVE APU AIR INLET CUTOUT. REMOVED AND REPLACED STRINGER PER SRM 53 80 13 AND 51 40 02.

Part: STIFFENER — CORRODED (BS 1119 S20R) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON APU COMPARTMENT RT TORQUE BOX VERTICAL STIFFENER AFT OF APU AIR INLET CUTOUT. REMOVED AND REPLACED STIFFENER PER SRM 53 80 13 AND 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. REMOVED DAMAGED SHEAR TIE FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53 00 07.

Part: FRAME — CORRODED (BS 500F S27-28R) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SHEAR TIE, FABRICATED REPAIR PARTS AND INSTALLED.

Part: SHEAR TIE — CORRODED (BS 500E S27-28L) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE. REMOVED DAMAGED SECTION OF SHEAR TIE FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53 00 07.

Part: FLOORBEAM — CORRODED (BS 312) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORRODED FLOORBEAM. CUTOUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 53 10 51.

Part: SHEAR TIE — CORRODED (BS 867) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION ON SHEAR TIE, CUT OFF SHEAR TIE AND INSTALLED REPAIR PER SRM 53 00 07.

Part: DOUBLER — CORRODED (BS 1117) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION IN APU COMPARTMENT RT TORQUE BOX EDGE DOUBLER FORWARD OF APU AIR INLET CUTOUT. FABRICATED AND INSTALLED DOUBLER PER SRM 51 40 02.

Part: DOUBLER — CORRODED (BS 1119) · airframe 42,339 hrs · 23,865 cycles

FOUND CORROSION IN APU COMPARTMENT RT TORQUE BOX EDGE DOUBLER AFT OF APU CUTOUT. FABRICATED AND INSTALLED DOUBLER PER SRM 51 40 02.

Part: FLOORBEAM — CORRODED (BS 967) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND FLOORBEAM CORRODED. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53 00 51

Part: FLOORBEAM — CORRODED (BS 294) · corrosion level 2 · airframe 42,339 hrs · 23,865 cycles

FOUND FLOORBEAM CORRODED. REPAIRED FLOORBEAM UPPER CHORD PER SRM 53 10 51 REPAIR 5.

Part: ANGLE — CRACKED (GALLEY DOOR) · airframe 42,339 hrs · 23,865 cycles

L ANGLE CRACKED FWD OF FWD GALLEY DOOR NR 3 (FROM TOP) STOP PAD FITTING. REMOVED FABRICATED AND REPLACED ANGLE.

Part: SKIN — DEBONDED (LT WING SLAT) · airframe 42,339 hrs · 23,865 cycles

FOUND LT WING SLAT O/B EDGE LWR SKIN DISBONDED. ACCOMPLISHED HOT BOND REPAIR PER SRM 51 70 10.

Part: SLIDE — NO TEST (R-1 DOOR) · airframe 42,285 hrs · 23,839 cycles

DURING R 1 ESCAPE SLIDE TEST PER ASA TASKCARD 48125002 SLIDE DEPLOYED AUTOMATICALLY INTEGRAL LIGHT ILLUMINATED SLIDE INFLATED AND REMAINED EXCEPT SLIDE DEPLOYED SIDEWAYS (LEFT SIDE UP) INSTALLED NEW SLIDE.

Part: FRAME — CORRODED (FUSELAGE)

YXX: DURING C-CHECK, FOUND FWD CARGO BILGE CORRODED ON FRAME AT BS 500D. REPAIRED IAW SRM. (K)

Part: SKIN — DENTED (HORIZ STAB)

YXX: DURING C-CHECK FOUND LT HORZ STAB AT STA 166 SKIN UPPER SURFACE HAS 2 PARALLEL DENT WITH CREASES. REPAIRED IAW SRM. (K)

Part: SKIN — DAMAGED (LT ELEVATOR)

YXX: DURING C-CHECK FOUND LT ELEVATOR UPPER IB SURFACE DAMAGED AT STA 24.00. REPAIRED IAW SRM. (K)

Part: SKIN — CHAFED (RT MIDFLAP)

YXX: DURING C-CHECK FOUND RT WING OB MIDFLAP T/E LOWER SIDE AT WBL 262, AHS CHAFFE DAMAGE. REPAIRED IAW SRM. (K)

Part: RIB — CRACKED (RT WING)

YXX: DURING C-CHECK FOUND RT WING FUEL TANK RIB LOWER CHORD CRACKED AT WING STA 135.5. REPAIRED IAW EA. (K)

Part: UNKNOWN — CORRODED (FUSELAGE) · corrosion level 2

YXX: DURING C-CHECK FOUND FWD CARGO BILGE CORRODED ON FLANGE AT BS 500D. REPAIRED IAW SRM. (K)

Part: DUCT — CRACKED (A/C SYSTEM)

YXX: DURING C-CHECK FOUND RT AC RAM AIR DUCT CRACKED AT ATTACH ANGLE AT FWD SECTION AT BS 540. REPAIRED IAW SRM. (K)

Part: SKIN — DENTED (LT FOREFLAP)

YXX: DURING C-CHECK FOUND LT OB FORE FLAP LOWER SKIN IN LINE WITH NR2 FLAP TRACK HAS 2 DENTS. REPAIRED IAW SRM. (K)

Part: FAIRING — CHAFED (FLAP TRACK)

YXX: DURING C-CHECK FOUND LT OB MID FLAP TRACK FAIRING LOWER SURFACE CHAFED. REPAIRED IAW SRM. (K)

Part: TORQUE TUBE — GOUGED (TAIL CONE)

YXX: DURING C-CHECK, FOUND TAIL CONE COMPARTMENT ELEVATOR OUTPUT TORQUE TUBE HAS A GOUDGE. REPAIRED IAW SRM. (K)

Part: SKIN — DENTED (RT FOREFLAP)

YXX - RT IB FORE FLAP DENT FOUND ON UPPER SURFACE AT WBL 107. REPAIRED DENT IAW SRM. (K)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2

YXX - FWD CARGO PIT BILGE, CORROSION ON FRAME LWR FLANGE @ B STA 500B, WBL 95. SHEAR TIE REPAIR ACCOMPLISHED IAW SRM. (K)

Part: SKIN — DELAMINATED (OB FORE FLAP)

YXX - LT WING OB FORE FLAP, OB END DAMAGED. REMOVED DAMAGE, INSTALLED LWR FILLER, INSIDE DOUBLER ( FOR LOWER SKIN), CORE AND UPPER DOUBLER. (K)

Part: WEDGE — DENTED (LT MIDFLAP) · airframe 39,950 hrs · 22,582 cycles

YXX - LT WING IB T/E MID FLAP WEDGE PANEL NR 7220L HAS 2 EACH DENTS ON THE OB EDGE. REMOVED DAMAGED FIBERS - POTTED PUNCTURE FLUSH AND REPAIRED PLIES INSTALLED AND CURED. (K)

Part: GUIDE ARM — WORN (L1 DOOR)

SEA - L-1 DOOR HARD TO OPEN AND CLOSE. REPLACED UPPER GUIDE ARM. (K)

Part: STRINGER CLIP — GOUGED (FUSELAGE)

FOUND FUSELAGE INTERNAL STATION 400 CLIP ATTACHED TO STRINGER NR 2 LEFT HAS A GOUGE. REMOVED AND REPLACED STRINGER TIE CLIP ON STRINGER NR 2 LEFT. (M)

Part: WIRE — BROKEN (CABIN)

PDX - FOUND AFT TWO RED EMERGENCY LIGHTS ARE NOT WORKING. REPLACED ONE SECTION BROKEN WIRE. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FORWARD CARGO BAY LEFT SIDEWALL SUPPORT AT BS 440 IS DAMAGED. REPAIRED IAW SRM. (M)

Part: WIRE — BROKEN (CABIN)

SFO - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT EMERGENCY EXIT ROW, BROKEN WIRE. REPAIRED WIRES, OPS CHECK NORMAL. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON SHEAR TIE AT STATION 767 TO WATERLINE 150 AND BUTT LINE 19. REMOVED AND REPLACED SHEAR TIE IAW SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM. REMOVED AND REPLACED IAW SRM. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL. REMOVED AND REPLACED IAW SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON FLOORBEAM. REPAIRED IAW SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL STRAP. REPLACED MOPSILL STRAP IAW SRM. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL. REPLACED MOPSILL IAW SRM. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - DURING MAINTENANCE INSPECTION, FOUND CRACK IN FRAME AT FASTENER AT STATION 360, WATERLINE 270, AND BUTTLINE 63 LEFT. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING MAINTENANCE INSPECTION FOUND CORROSION ON SHEAR TIE AT STATION 767 WATERLINE 149 AND BUTTLINE 10 RIGHT AND LEFT SIDES. REPAIRED IAW SRM. (M)

Part: SEAT TRACK — CORRODED (CABIN)

PAE - DURING SI CHECK, FOUND CORROSION OUT OF LIMITS ON SEAT TRACK FROM BS 360-480 AND RBL 24.75 AND WBL 208. REPAIRED IAW SRM. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CRACK 1 INCH LONG AT BS 178 SIDE CHORD AT WL 207, RBL 28 AND LBL 28. (M)

Part: LIGHT — DISCONNECTED (CABIN)

PDX - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE IN AFT CABIN AFT 3 LIGHTS. RECONNECTED EMERGENCY FLOOR LIGHTS IN AFT CABIN. OPERATIONAL CHECKS NORMAL. (M)

Part: LIGHT — DISCONNECTED (CABIN)

PDX - WHEN PERFORMING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 17-19. RECONNECTED LIGHTS OPS NORMAL. (M)

Part: LIGHT — DISCONNECTED (CABIN)

PDX - WHEN PERFORMING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN AFT CABIN. RECONNECTED LIGHTS, OPS NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING LINE CHECK INSPECTION, FOUND AFT 3 TRACK LIGHTS INOPERATIVE IN AFT CABIN, LOOSE WIRING. RECONNECT LIGHTS, OPERATIONAL CHECK NORMAL. (M)

Part: LIGHT — DAMAGED (ROW 17-20)

SEA-DURING LINE CHECK FOUND FLOOR EMERGENCY TRACK LIGHTS INOP AT ROWS 17-20. REMOVED AND REPLACED LIGHT ASSEMBLIES, OPERATIONAL CHECKS NORMAL.

Part: LIGHT — DISCONNECTED (ROW 1-2)

PDX - DURING SERVICE INSPECTION, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 1-2, WIRE DISCONNECTED. RECONNECTED TRACK LIGHTS, OPERATION CHECKED NORMAL. NO DEFECTS NOTED. (M)

Part: WIRE — DISCONNECTED (FWD CABIN)

PDX-DURING MAINTENANCE SERVICE CHECK FOUND FWD 5 EMERGENCY TRACK LIGHTS INOP. RECONNECTED LIGHTS, OPS CHECKED NORMAL.

Part: SKIN — TOOL DAMAGE (FUSELAGE CROWN)

SEA - DURING SCHEDULED C-CHECK, THE CROWN SKIN WAS FOUND TO HAVE TOOLING MARK AT BS 1007, 1 INCH FORWARD OF THE DORSAL FIN AFT RIGHT MOUNT BOLT HOLE. REPAIRED PER EA 5330-01446. (M)

Part: CREASE BEAM — GOUGED (FUSELAGE)

SEA - DURING SCHEDULED C-CHECK, THE L1 DOOR CREASE BEAM WAS FOUND TO BE GOUGED AND CORRODED. REPAIRED PER EA 5320-01414. (M)

Part: BEAM — DAMAGED (MLG)

SEA - DURING SCHEDULED C-CHECK, FOUND EVIDENCE OF PANEL CONTACT ON LEFT LOWER MLG BEAM 34 INCHES FROM INBOARD END. REPAIRED PER EA 5750-01431. (M)

Part: FAIRING — WORN (TE FLAP)

SEA - DURING SCHEDULED C-CHECK, THE NR 5 FLAP TRACK FAIRING INNER RUBSTRIP WAS FOUND TO BE WORN. REPAIRED PER EA 5720-01176. (M)

Part: HINGE — GOUGED (RT ELEVATOR)

SEA - DURING SCHEDULED C-CHECK, THE RIGHT ELEVATOR NR 1 HINGE INBOARD SIDE WAS FOUND TO BE GOUGED. REPAIRED PER EA 5520-01083. (M)

Part: FAIRING — CHAFED (NR 1 ENGINE)

SEA - DURING SCHEDULED C-CHECK, NR 1 ENGINE INBOARD BULLNOSE FAIRING WAS FOUND TO BE CHAFED AND GOUGED. REPAIRED PER EA 5430-01069. (M)

Part: DOOR — DAMAGED (THRUST REVERSER)

SEA - DURING SCHEDULED C-CHECK, NR 1 ENGINE OUTBOARD T/R HALF BLOCKER DOOR CONTACTED BULLNOSE. REPAIRED PER EA 5430-01068. (M)

Part: STRUCTURE — CHAFED (T/R BLOCKER DOOR)

SEA - DURING SCHEDULED C-CHECK, THE NR 2 ENGINE INBOARD T/R BLOCKER DOOR WAS FOUND TO BE CHAFING THE FORWARD BULLNOSE. REPAIRED PER EA 5430-01067. (M)

Part: SKIN — DENTED (FUSELAGE)

SEA - DURING SCHEDULED C-CHECK, A DENT WAS FOUND IN THE FUSELAGE BELOW THE R1 DOOR STATION 300-323. REPAIRED PER EA 5330-01443. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, FOUND THE AFT 4 EMERGENCY EXIT TRACK LIGHTS TO BE INOPERATIVE. RECONNECTED WIRING TO LIGHTS AND RELAMPED, LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED LIGHTS/WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

JNU - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT 6 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LIGHTS/WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: HINGE COVER — BENT (L2 DOOR)

PDX - FLT 604 - PRIOR TO 604, THE L2 DOOR UPPER FORWARD HINGE COVER WAS FOUND TO BE BENT, CAUSING INTERFERENCE WITH DOOR OPENING. REMOVED HINGE COVER AND RELEASED PER CDL 52-40-6. DOOR OPERATED NORMALLY. MAINTENANCE SUBSEQUENTLY INSTALLED A NEW UPPER FORWARD HINGE COVER AND THE DOOR OPERATED NORMALLY. (M)

Part: SKIN — DAMAGED (WS 340)

SEA - DURING SCHEDULED C-CHECK, FOUND DAMAGE TO THE NR 1 SLAT CENTER AUXILIARY TRACK CUTOUT SKIN AT SS 340.70. REPAIRED PER EA 5740-01159. (M)

Part: SKIN — SEPARATED (RUDDER)

SEA - DURING SCHEDULED C-CHECK, THE RIGHT SIDE OF THE RUDDER SKIN FIRST PLY WAS FOUND TO BE SEPARATED. REPAIRED PER EA 5540-01030 AND BOEING TELEX ASA-SEA-99-0114RR. (M)

Part: SNUBBER — INOPERATIVE (L1 DOOR)

PDX - PRIOR TO FLT 471, THE L1 DOOR WAS DIFFICULT TO CLOSE. REPLACED SNUBBER AND LUBRICATED PIVOT POINTS, DOOR OPERATED NORMALLY. ACFT TT: 17,769 HOURS. ACFT TC: 10,554. (X)

Part: BATTERY PACK — DISCHARGED (AFT CABIN)

PDX - FLT 504 - PRIOR TO FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 19 THRU 23. REPLACED BATTERY PACK AND BATTERY CHARGER AND LIGHTS OPERATED NORMALLY. REF: OPERATOR CONTROL NR 98ZZZX373. (X)

Part: CHARGER — DISCHARGED (AFT CABIN)

PDX - FLT 504 - PRIOR TO FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 19 THRU 23. REPLACED BATTERY PACK AND BATTERY CHARGER AND LIGHTS OPERATED NORMALLY. REF: OPERATOR CONTROL NR ASAA9740105.

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 18-21. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X)

Part: BRACKET — CORRODED (BS 729.35)

SEA - DURING C-CHECK, THE RT MLG FAIRING BRACKET AT STATION 729.35 WAS FOUND TO BE CORRODED AROUND ONE FASTENER HOLE. REPAIRED PER EA 5320-01330. (M)

Part: FITTING — CORROSION (BS 729.35)

SEA - DURING C-CHECK, THE RT MLG FAIRING ATTACH POINT AT STATION 729.35 WAS FOUND TO HAVE TWO ELONGATED HOLES AND CORROSION AROUND ONE FASTENER HOLE. REPAIRED PER EA 5320-01329. (M)

Part: SKIN — WORN (LT WING)

SEA - DURING C-CHECK, THE LOWER SURFACE OF THE LEFT WING SKIN WAS FOUND WORN AT TWO LOCATIONS NEAR THE ACCESS HOLES FOR THE BOOST PUMP. REPAIRED PER EA 5720-01133. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN THE FORWARD CABIN. REPLACED TWO EACH LIGHT ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT 402 - PRIOR TO FLIGHT, CREW REPORTED ONE SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS ON LEFT SIDE WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

ANC - PRIOR TO FLT, ONE SECTION OF THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPAIRED BY RECONNECTING WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS FROM ROWS 14 TO 18 WERE FOUND INOPERATIVE. RECONNECTED WIRING AT ROW 18 AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - CHECK, TRACK LIGHTS INOP ROWS 18 TO 22. MAINTENANCE RECONNECTED LIGHTS. (W)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - PILOT REPORT - FLOOR TRACK LIGHTS OUT BETWEEN ROWS 19 AND 21. MAINTENANCE CONNECTED WIRE HARNESS AT ROW 21. (X)

Part: EEL WIRING — DISCONNECTED (CABIN)

ANC - CHECK - FLOOR TRACK EMERGENCY LIGHTS BETWEEN ROWS 15 AND 18 INOP. MAINTENANCE RE-CONNECTED WIRING. (X)