N771AS

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 62,777 hrs · 35,969 cycles

SEAT 17F, EMERGENCY EXIT COVER IS MISSING. REPLACED & INSTALLED SEAT 17F EMERGENCY EXIT SIGN COVER AS REQUIRED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,345 hrs · 34,266 cycles

REF T/C AD20090206 400 53 1 WIRE PENETRATION HOLE INSPECTION STATION 500C RT SIDE 1.04 IN HOLE IS CRACKED. REPAIRED IAW SRM 53 00 07 REPAIR 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,345 hrs · 34,266 cycles

REF T/C AD20090206 400 53 1 WIRE PENETRATION HOLE INSPECTION STATION 500C RT SIDE 1.04 INCH HOLE IS CRACKED. REPAIRED IAW SRM 53 00 07 REPAIR 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,345 hrs · 34,266 cycles

REF T/C AD 20090206 400 53 1 WIRE PENETRATON HOLE INSPECTION STATION 500B RT SIDE .500 HOLE HAS A CRACK. REPAIRED FRAME REF SRM 53 00 07 REPAIR 13. EA 400 53EA 07274 AND IS COMPLETED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,345 hrs · 34,266 cycles

REF T/C AD 20090206 400 53 1 WIRE PENETRATON HOLE INSPECTION STATION 500B RT SIDE .500 HOLE HAS A CRACK. REPAIRED FRAME REF SRM 53 00 07 REPAIR 13 EA 400 53EA 07274 AND IS COMPLETED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

DURING CLEANING OF FLOORBEAM FOUND INTERCOSTAL CRACKED ON UPPER FLANGE AT FLOORBOARD HOLE LOCATIONS STA 380 400 BL 0. REMOVED OLD AND INSTALLED NEW INTERCOSTAL UPPER FLANGE BETWEEN STA 380 400 BL 0 IAW B737 400 SRM 51 40 02.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

DURING OK TO INSTALL APU DIFFUSER DUCT FOUND I/B VERTICAL STIFFENER CORRODED FWD SIDE OF STA 1088 RBL 22. REPLACED STIFFENER IAW B737 400 SRM 51 40 02 PAGES 2 AND 3.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

STRINGER CLIP CRACKED STA 500F STR 5R. REMOVED AND REPLACED CLIP IAW ASA DWG A53100265816.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

E AND E BAY FRAME STA 360 SHEAR TIE CORRODED FROM STR 28R TO 29R. REMOVED, FABRICATED, TREATED, PRIMED, TOPCOATED AND INSTALLED SHEAR TIE IAW B737 400 SRM 51 40 02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,038 hrs · 33,486 cycles

E&E BAY FRAME STA 380 SHEAR TIE CORRODED FROM STRINGER 28L TO 28R. REMOVED AND REPLACED FRAME AT STA 380 FROM STR 25L TO 25R LOWER SECTION IAW B737 400 SRM 51 40 02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,038 hrs · 33,486 cycles

E&E BAY STA 360 SHEAR TIE CORRODED FROM STR 28L TO 29L FWD SIDE. REMOVED FABRICATED NEW AND INSTALLED SHEAR TIE IAW B737 400 SRM 51 40 02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

STRINGER CLIP CRACKED AT STA 827 STR 4L. REMOVED AND REPLACED CLIP IAW ASA DWG A53100265816.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

STRINGER CLIP CRACKED AT STA 807 STR 4L. REMOVED AND REPLACED CLIP IAW ASA DWG A53100265816.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

STRING CLIP CRACKED AT STA 887 STRINGER 4L. REMOVED AND REPLACED CLIP IAW ASA DWG A53100265816.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,038 hrs · 33,486 cycles

FRAME FS 767 CORRODED ON AFT SIDE BETWEEN STRINGER 25R 26L. REMOVED FABRICATED AND INSTALLED FAIL SAFE ANGLE ON FRAME 767 IAW B737 400 SRM 53 60 07 FIG 1 AND 51 40 02 PAGES 2 AND 3.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

SHEAR TIE CORRODED AT FS 927 STR 27R TO 27L. FABRICATED, DRILLED, TREATED AND INSTALLED SHEAR TIE REPAIR IAW B737 400 SRM 53 00 07 FIG 201.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

STRINGER TIE CRACKED STA 727D STRINGER 5R. REMOVED AND REPLACED CLIP IAW ASA DWG A53100265816.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,038 hrs · 33,486 cycles

FRAME STA 867 CORRODED AT STRINGER 22L TO 23L. REMOVED DAMAGED SECTION FABRICATED REPAIR PARTS AND INSTALLED IAW ASA EA 40053EA05865.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

STRINGER CLIP CRACKED AT STA 727E STRINGER 7R. REMOVED AND REPLACED CLIP IAW ASA DWG A53100265816.

Part: STIFFENER — CORRODED (APU BAY) · corrosion level 2 · airframe 59,038 hrs · 33,486 cycles

APU COMPT AIR INLET TORQUE BOX INLET LOWER AFT FLANGE (OUTBOARD SIDE) VIEWED FROM INSIDE TORQUE BOX ABOVE BLEED AIR DUCT CORRODED AFT OF STA 1121. REMOVED CORRODED STIFFENER AND REPLACED WITH FABRICATED STIFFENER IAW B737 400 SRM 53 80 15.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

STRINGER TIE CRACKED AT 727B STRINGER 4R. REMOVED AND REPLACED CLIP IAW ASA DWG A53100265816.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 58,038 hrs · 33,486 cycles

AFT PIT AFT BULKEAD LOWER SUPPORT ANGLE CORRODED. REMOVED CORRODED ANGLE, FABRICATED AND INSTALLED NEW ANGLE IAW B737 400 SRM 51 40 02 FIGURE 2.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

STRINGER TIE CRACKED AT STA 272A STRINGER 6L. REMOVED AND REPLACED CLIP IAW ASA DWG A53100265816.

Part: FRAME — CORRODED (FUSELAGE)

FRAME 747 CORRODED AT STR 25R 27R. REPAIRED FRAME IAW B737 400 SRM 53 00 07 FIG 201. THIS IS A CATEGORY B REPAIR REQUIRING REPEAT INSP AT 66 000 TOTAL FLIGHT CYCLES.

Part: FAILSAFE — CORRODED (BS 827 S22L) · airframe 59,038 hrs · 33,486 cycles

FRAME 827 CORRODED AT STR 22L AFT SIDE. REMOVED CORROSION AND REPAIRED FAIL SAFE CHORD IAW ASA EA 40053EA 05872.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,846 cycles

SHEAR TIE CORRODED AT STR 27L TO 27R FS 887. FABRICATED, DRILLED, TREATED AND INSTALLED SHEAR TIE REPAIR IAW B737 400 SRM 53 00 07 FIG 201.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

AFT PIT AFT BULKHEAD LOWER SUPPORT ANGLE CORRODED. REMOVED CORROEDED ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW B737 400 SRM 51 40 02 FIG.2.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,038 hrs · 33,486 cycles

APU COMPTAIR INLET TORQUE BOX INLET LOWER AFT FLANGE FOUND CORRODED AFT OF STA 1121. REPLACED STRINGER IAW B737 400 SRM 53 80 15 FIG 101 51 40 02 FIG 8 AND 51 40 12 PAGES 2 AND 3.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

STRINGER CLIP CRACKED AT STA 727B STRINGER 7R. REMOVED AND REPLACED CLIP IAW ASA DWG A53100265816.

Part: FRAME — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

AFT CARGO COMPARTMENT FRAME STA 747 CORRODED AT 25L. REPAIRED SHEAR TIE AT STA 747 STR 25L IAW B737 400 SRM 53 00 07 FIG 201.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,038 hrs · 33,486 cycles

IN AFT PIT STA 1013 STR 22L FOUND CORRODED. REPAIRED STRINGER IAW B737 400 SRM 53 00 01 FIG 201.

Part: FRAME — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

FRAME 827 CORRODED AT STR 26L 27R. REPAIRED FRAME 827 IAW B737 400 SRM 53 00 07 FIG 201. THIS IS A CATEGORY B REPAIR AND REQUIRES REPEAT INSP AT 66 000 TOTAL FLIGHT CYCLES.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

STRINGER CLIP CRACKED AT STA 727C STRINGER 7R. REMOVED AND REPLACED CLIP IAW ASA DWG A53100265816.

Part: FRAME — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

FRAME 787 CORRODED AT FRONT SIDE AT STR 25L TO 27L. PERFORMED SHEAR TIE REPAIR AT FS 787 BETWEEN STRINGER 25L AND 27L IAW B737 400 SRM 53 00 07 FIG 201.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

STRINGER CLIP STA 727C STRINGER 6L CRACKED. REMOVED AND REPLACED CLIP IAW ASA DWG A53100265816.

Part: FRAME — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

AFT PIT STA 1006 FRAME CORRODED BETWEEN STR 23L AND 21L. REPAIRED FRAME IAW ASA EA 400 53EA 05908.

Part: FRAME — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

FRAME STA 807 CORRODED AT STR 24L TO 26L (AFT CARGO COMPARTMENT). REPAIRED SHEAR TIE AT STA 807 BETWEEN STR 24L TO 26L IAW B737 400 SRM 53 00 07 FIG 201.

Part: FRAME — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

AFT CARGO COMPARTMENT FRAME STA 767 CORRODED AT STR 25L TO 26L. REPAIRED SHEAR TIE AT STA 767 BETWEEN STR 25L TO 26L IAW B737 400 SRM 53 00 07 FIG 201 REPAIR 1.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

CORROSION IN AFT PIT STA 967 ON INTERNAL DOUBLER. REPAIRED INTERNAL DOUBLER IAW ASA EA 400 53EA 05911.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,038 hrs · 33,486 cycles

IN AFT PIT STA 1016 STRINGER ATTACH FITTING FOUND CORRODED. REMOVED AND REPLACED FITTING IAW B737 400 SRM 51 40 02 FIG 2.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

SHEAR TIE CORRODED AT FS 807 STR 27R 27L. FABRICATED, DRILLED, TREATED AND INSTALLED SHEAR TIE IAW B737 400 SRM 53 00 07 FIG 201.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

STRINGER CLIP CRACKED AT STA 727F STRINGER 4R. REMOVED AND REPLACED CLIP IAW ASA DWG A53100265816.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

AFT CARGO STRINGER AT 25L FOUND CORRODED AT STA 747. REMOVED AND REPLACED STRINGER CLIP IAW B737 400 SRM 51 40 02 STEP 4.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

STRINGER TIE CRACKED AT STA 727A AND STRINGER 5L. REMOVED AND REPLACED CLIP IAW ASA DWG A53100265816.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

CORRODED STRINGER TIE BS 767 STR 26R. REMOVED AND REPLACED WITH NEW STRINGER TIE PER B737 400 SRM 53 00 03.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

STRINGER CLIP CRACKED AT STA 727A STRINGER 7R. REMOVED AND REPLACED CLIP IAW ASA DWG A53100265816.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

STRINGER TIE BS 787 STR 26R CORRODED. REMOVED AND REPLACED WITH NEW STRINGER TIE PER B737 400 SRM 53 00 03.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 59,038 hrs · 33,486 cycles

CARGO COMPARTMENT TRACK CORRODED AT FS 946 RBL 18. INSTALLED CARGO TRACK REPAIR IAW SRM B737 400 SRM 53 60 53.

Part: TRANS PANEL — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

TRANSITION PANEL FOUND CORRODED AFT OF FRAME STA 787 AND LBL 21.8. REPLACED TRANSITION PANEL IAW B737 400 SRM 53 60 53 FIG 201.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

LEFT I/B SEAT TRACK GOUGED SEVERAL AREA STA 520 540. REMOVED FABRICATED NEW SEAT TRACK, INSTALLED IAW B737 400 MM 20 50 11 912 002 AND B737 400 SRM 51 40 05 AND ASA EA 400 53EA 0493.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

SIDEWALL LINER SUPPORT CRACKED AT FRAME 727D AND STR 18R 19R. REPLACED WITH FABRICATED NEW SUPPORT PER DWG 69 73199 AND B737 400 SRM 51 40 02 AND SRM 51 40 05.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

SHEAR TIE CORRODED AT FS 500D STR 27 28L. FABRICATED, DRILLED, TREATED AND INSTALLED SHEAR TIE REPAIR IAW B737 400 SRM 53 00 07 FIG 201.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

PAX CABIN LT CUSP WEB CORRODED ON OUTBOARD EDGE AROUND FASTENERS BETWEEN STA 867 AND 887 STR 17L. REPLACED WITH NEW FABRICATED WEB IAW B737 400 SRM 53 60 13.

Part: TRANS PANEL — CORRODED (CARGO BAY) · airframe 59,038 hrs · 33,486 cycles

FWD CARGO LT TRANSITION PANEL FROM STA 500F 500G CORRODED. REPAIRED LT CARGO TRANSITION PANEL FROM STA 500B TO 500G IAW B737 400 SRM 53 30 53 FIG 201.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

AFT PIT FWD LT SIDEWALL LINER SUPPORT BROKEN. REPLACED WITH FABRICATED NEW SUPPORT PER DWG 65 55726 AND B737 400 SRM 51 40 05.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

TRANSITION PANEL LBL 21.8 NUT PLATE ZEE SUPPORT FROM FRAME 727C 727G WAS FOUND CORRODED. REPLACED TRANSITION PANEL ZEE PER B737 400 SRM 53 60 53 FIG 201.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

PAX CABIN RT SHEAR WEB CORRODED ON OUTBD EDGE AROUND FASTENERS BETWEEN STA 807 AND 827 STR 17R. FABRICATED NEW WEB IAW B737 400 SRM 51 30 01 AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 59,038 hrs · 33,486 cycles

L1 DOOR FWD GIRT BAR MOUNT AT FS 344 LBL 55 WAS FOUND CORRODED. REMOVED AND REPLACED FWD GIRT BAR MOUNT PER B737 400 AMM 20 50 11 912 002 FIG 203.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

RBL 13.8 CARGO TIEDOWN TRACK CORRODED. FABRICATED REPAIR PARTS AND REPLACED CARGO TRACK IAW B737 400 SRM 53 00 53 REPAIR 2 (CARGO TRACK REPAIR LOWER LOBE).

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

RT INBOARD TRACK GOUGED AT SEVERAL AREA STA 480 520. REPAIRED SEAT TRACK IAW B737 400 SRM 53 00 52 FIG 201 AND AS EA 400 53EA 04953.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

OVERHEAD BIN ATTACH POINT CRACKED AT STA 727D BETWEEN STRINGER 8L AND 9L. REPAIRED FRAME AT STA 827 STR 8L & 9L IAW ASA EA AD20062609 400 53 121.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

FWD CARGO SUPPORT ANGLE CORRODED AT FS 500F TO FS 500G AND STR 28R. FABRICATED, DRILLED, TREATED AND INSTALLED NEW SECTION OF FLOOR SUPPORT ANGLE IAW B737 400 SRM 51 40 05 AND SRM 53 00 03.

Part: FRAME — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

FRAME 727B CORRODED INBOARD OF STR 27R. REPAIRED THE 727B FRAME IAW B737 400 SRM 53 00 07 FIG 201.

Part: FRAME — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

FRAME STA 727G CORRODED AT STR 26L AFT CARGO COMPARTMENT. REPAIRED SHEAR TIE AT STA 727G IAW B737 400 SRM 53 00 07 FIG 201.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

AFT CARGO COMPARTMENT RBL 71.8 NUT PLATE SUPPORT CORRODED AT 727B TO 727E. REMOVED PANEL, FABRICATED A NEW ONE AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

ANTENNA DOUBLER CORRODED AT FRAME 727D 2727E BOTTOM CENTER (AFT CARGO). REPLACED WITH FABRICATED NEW DOUBLER IAW B737 400 SRM 51 40 02 AND 51 40 05 AND BAC DWG 65 65710.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

FWD CARGO SHEAR TIE CORRODED AT STA 460 BETWEEN STR 28R AND 27R. REPAIRED SHEAR TIE IAW B737 400 SRM 53 00 07 FIG 201.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,038 hrs · 33,486 cycles

PAX CABIN RT CUSP WEB CORRODED BETWEEN STA 877 TO 847 STR 174. REPLACED WITH NEW FABRICATED WEB PER B737 400 SRM 51 30 01 AND 51 40 02.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,038 hrs · 33,486 cycles

PAX CABIN RT CUSP WEB CORRODED AT STA 787 STR 17R. REPLACED WITH NEW FABRICATED WEB AND INSTALLED IAW B737 400 SRM 51 40 01 AND SRM 51 40 02.

Part: SILL — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

L1 DOOR MOP SILL IS CORRODED. REMOVED AND REPLACED OUT OF LIMITS L1 INNER CHORD IAW B737 400 SRM 53 10 15 FIG 101 51 40 05 AND 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

OVERHEAD BIN ATTACH POINT CRACKED AT STA 827 BETWEEN STRINGER 8L AND 9L. REPAIRED FRAME AT STA 827 STR 8L & 9L IAW ASA EA AD20062609 400 53 121.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

PAX CABIN RT CUSP WEB CORRODED ON O/B EDGE AROUND FASTENERS BETWEEN STA 867 AND 887 STR 17R. REMOVED FABRICATED AND INSTALLED NEW CUSP WEB IAW B737 400 SRM 53 60 13 51 40 02 AND DWG 65C26402.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

OVERHEAD BIN ATTACH POINT CRACKED AT STA 867 BETWEEN STRINGER 8L AND 9L. REPAIRED FRAME AT STA 867 STR 8L & 9L IAW ASA EA AD20062609 400 53 121.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

RT O/B SEAT TRACK GOUGED AT SEVERAL AREA STA 727B 927. REPAIRED SEAT TRACK IAW B737 400 SRM 53 00 52 FIG 201 AND AS EA 400 53EA 04953.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

PAX CABIN CUSP WEB CORRODED ON O/B EDGE AROUND FASTENERS BETWEEN STA 767 AND 787 STR 17R. REPLACED WITH NEW FABRICATED WEB IAW B737 400 SRM 53 60 13 51 40 02 AND BAC DWG 65C26402.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

PASSENGER CABIN RT CUSP WEB CORRODED ON OUTBD EDGE AROUND FASTENERS BETWEEN STA 757G AND 747 STR 17R. FABRICATED AND INSTALLED REPLACEMENT CUSP WEB IAW SRM 53 60 13 AND SRM 51 40 02 (BOEING 737 400).

Part: ANGLE — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

MAIN CABIN ZEE ANGLE WAS FOUND CORRODED AND OUT OF LIMITS. FABRICATED AND INSTALLED NEW ANGLE IAW B737 400 SRM 53 60 51.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

PASSENGER CABIN RT CUSP WEB CORRODED ON OUTBD EDGE AROUND FASTENERS BETWEEN STA 847 AND 867 STR 17R. FABRICATED NEW WEB IAW BOEING DRWG 65 47976. INSTALLED WEB IAW B737 400 SRM 51 40 02.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

PAX CABIN LT CUSP WEB CORRODED ON AFT END BETWEEN STA 727B AND 727C STR 17L. REPLACED WITH NEW FABRICATED WEB IAW B737 400 SRM 51 30 01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,038 hrs · 33,486 cycles

PAX CABIN LT CUSP WEB CORRODED ON FWD AND AFT ENDS AROUND FASTENERS BETWEEN STA 807 AND 827 STR 17L. REPLACED WITH NEW FABRICATED WEB IAW B737 400 SRM 51 30 01 NR 8.

Part: FRAME — CRACKED (FUSELAGE)

OVERHEAD BIN ATTACH POINT CRACKED AT STA 907 BETWEEN STRINGER 8R AND 9R. REPAIRED FRAME AT STA 907 STR 8R & 9R IAW ASA EA AD20062609 400 53 121.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 59,038 hrs · 33,486 cycles

L1 DOOR FWD GIRT BAR MOUNT AT FS 312 LBL 54 WAS FOUND CORRODED. REMOVED AND REPLACED FWD GIRT BAR MOUNT PER B737 400 AMM 20 50 11 912 002 FIG 203.

Part: BRACE — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

ANTENNA DOUBLER CROSS BRACE CRACKED IN 3 PLACES AFT OF FRAME 727D. REMOVED CRACKED BRACE FABRICATED AND INSTALLED NEW CROSS BRACE PER B737 400 SRM 51 20 01, 51 40 05 AND SRM 51 40 02 PARA.7.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

PAX CABIN RT CUSP WEB CORRODED ON O/B EDGE AROUND FASTENERS BETWEEN STA 727D AND 727E STR 17R. REPLACED WITH NEW FABRICATED WEB IAW B737 400 SRM 53 60 13 AND 51 40 02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

ANTENNA SUPPORT ANGLES CRACKED AT FRAME 737D. REMOVED CRACKED ANGLES FABRICATED AND INSTALLED NEW ANGLES PER B737 400 SRM 51 20 01, 51 40 05 AND SRM 51 40 02 PARA 7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

MAIN CABIN FLOORBEAM CORRODED AT FASTENER HOLE AT FS 967 LBL 28. REMOVED CORROSION AND REPAIRED FLOORBEAM AT FS 967 LBL 28 IAW B737 400 SRM 53 00 51.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

PASSENGER CABIN RT CUSP WEB CORRODED ON OUTBD EDGE AROUND FASTENERS BETWEEN STATION 747 AND 767 STR 17R. FABRICATED NEW WEB IAW B737 400 DRAWING 65C26402 15 AND INSTALLED WEB IAW B737 400 SRM 51 40 02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,038 hrs · 33,486 cycles

CORROSION ON CABIN FLOORBEAM STA 947 LBL 24 RBL 24. C/W REPAIR OF 947 UPPER CAP IAW EA 400 53EA 05889 REV NEW DATE ISSUED 18 JUL 2011.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

FWD CARGO SHEAR TIE CORRODED AT FS 500D STR 28R 28L. FABRICATED DRILLED TREATED AND INSTALLED SHEAR TIE REPAIR IAW B737 400 SRM 53 00 07 FIG 201.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

LT INBOARD SEAT TRACK GOUGED IN SEVERAL AREAS FROM STA 344 TO 480. REPLACED SEAT TRACK PER B737 400 SRM 51 40 02.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

PAX CABIN RT CUSP WEB CORRODED ON O/B EDGE FWD CORNER AROUND FASTENERS BETWEEN STA 727E AND 727F STRINGER 17R. REMOVED FABRICATED AND INSTALLED NEW CUSP WEB IAW B737 400 SRM 53 60 13 51 40 02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

MAIN CABIN HAS CORROSION ON ANGLE AT STATION 991 LBL 32. REMOVED CORRODED ANGLE AND INSTALLED A FABRICATED NEW ANGLE PER B737 400 SRM 51 40 05.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

SHEAR TIE CORRODED AT FS 500B STR 27 28L. FABRICATED, DRILLED, TREATED AND INSTALLED SHEAR TIE REPAIR IAW B737 400 SRM 53 00 07 FIG 201.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

CORRODED STRINGER TIE BS 767 STR 26R. REMOVED AND REPLACED WITH NEW STRINGER TIE.

Part: TRANS PANEL — CORRODED (CARGO BAY) · airframe 59,038 hrs · 33,486 cycles

FWD CARGO COMPARTMENT LT TRANSITION PANEL CORRODED STA 500D. REPAIRED LT FWD CARGO TRANSITION PANEL FROM STA 500B TO 500G IAW B737 400 SRM 53 30 53 FIG 201.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

OVERHEAD BIN ATTACH POINT CRACKED AT STA 867 BETWEEN STRINGER 8R AND 9R. REPAIRED FRAME AT STA 867 STR 8R & 9R IAW ASA EA AD20062609 400 53 121.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

FWD CARGO SHEAR TIE CORRODED STA 500C BETWEEN STR 28L 28R. REPAIRED SHEAR TIE IAW B737 400 SRM 53 00 07 FIG 201.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,038 hrs · 33,486 cycles

PAX CABIN RT CUSP WEB HAS CORROSION ON UPPER SURFACE BETWEEN STA 440 AND 460. REPLACED WITH NEW FABRICATED WEB IAW B737 400 SRM 53 30 13.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

PAX CABIN RT CUSP WEB CORRODED AROUND O/B FASTENERS BETWEEN STA 360 AND 380. REPLACED WITH NEW FABRICATED WEB AND INSTALLED IAW B737 400 SRM 51 30 01 AND 51 40 02.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 59,038 hrs · 33,486 cycles

LT WING T/E FIXED PANEL ATTACH ANGLE IS CRACKED INBOARD OF NR 3 SPOILER. FABRICATED AND INSTALLED NEW ANGLE IAW B737 400 SRM 51 40 01, 51 40 02, 51 40 05 AND BOEING DRAWING BAC1470 2793.

Part: THRUST REVERSER — CORRODED (NR 2 ENGINE) · airframe 59,038 hrs · 33,486 cycles

NR 2 ENGINE RT THRUST REVERSER IS CORRODED AT THE AFT UPPER END OF THE BYPASS AREA. REPAIRED THRUST REVERSER IAW ASA EA 400 78EA 04303 DATED 01/07/11.

Part: THRUST REVERSER — CORRODED (NR 1 ENGINE) · airframe 59,038 hrs · 33,486 cycles

NR 1 ENGINE RT THRUST REVERSER IS CORRODED AT THE AFT UPPER END OF THE FAN BYPASS AREA. REPAIRED THRUST REVERSER IAW ASA EA 400 78EA 04303 REV DATED 07JAN11.

Part: STRAP — BROKEN (FUSELAGE) · airframe 59,038 hrs · 33,486 cycles

FLOORBEAM STRAP BROKEN AT FS 312. FABRICATED, DRILLED, TREATED AND INSTALLED REPAIR IAW B737 400 SRM 53 10 51. FIG.201.

Part: BOLT — WORN (GALLEY DOOR) · airframe 58,831 hrs · 33,341 cycles

R2 (AFT GALLEY SERVICE) DOOR HARD TO CLOSE, ACFT GROUNDED. REPLACED R2 DOOR GUIDE ARM ASSY. IAW AMM 52-41-21-404-004 STEP C1 THRU C5 B. DOOR STILL DIFFICULT TO CLOSE. REMOVED DOOR FROM AIRCRAFT. FOUND THE DOOR MOUNTED TORQUE TUBE TO UPPER SPIGOT CROSSBOLTS WORN ALLOWING THE DOOR TO BECOME MISTIMED AND THE LOWER AND UPPER HINGE ARMS TO MOVE INDEPENDENTLY OF ONE ANOTHER. REPLACED THE BODY MOUNTED TORQUE TUBE RADIUS LINK UPPER/LOWER HINGE LINKS UPPER HINGE LOWER GUIDE PLATE/BEARING LOWER HINGE UPPER STOP PLATE/BEARING DOOR MOUNTED TORQUE TUBE UPPER SLEEVE CROSSBOLTS AND DOOR SNUBBER. REINSTALLED ADJ AND OPS CHECKED R 2 DOOR DOOR OPERATES NORMALLY OK FOR CONTINUED SERVICE.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,626 hrs · 32,649 cycles

CORROSION FOUND AT FWD LAVATORY SERVICE PANEL PAN UNDER WASTE TANK DRAIN NIPPLE. REMOVED PAN FABRICATED REPLACEMENT PAN AND INSTALLED IAW EA 400 53EA 04502.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 54,478 hrs · 30,842 cycles

FLT ATTENDANTTS REPORTED AFT GALLEY OVEN 4 13 (BIG OVEN) BEGAN SMOKING APPROX 2 MINS AFTER APPLYING POWER. TURNED OVEN OFF. OVEN DOOR CONTINUED TO GET HOTTER. SMELL OF ELECTRICAL WIRES. SMOKE COMING OUT OF VENTS ABOVE OVEN. COULD NOT PULL CB'S IN AFT GALLEY. SECURED POWER VIA FLT DECK GALLEY POWER SWITCH. OVEN DOOR CONTINUED TO GET HOTTER. ACCOMPLISHED QRH FOR SMOKE/FUMES IN CABIN. DIVERTED TO YVR. F/A'S WERE ABLE TO PULL AFT GALLEY C/B'S AFTER FLT. DECK GALLEY POWER SWITCH WAS TURNED OFF. ACCOMP GVI ON AFT GALLEY NR 1 OVEN C/B 1 PER MM 20 60 01. ALL CHECK NORMAL. REPLACED AFT GALLEY OVEN 4 13 PER MM 25 32 01 PB 401. OPS CHECK GOOD. C/B AFT GALLEY NR 1 OVEN RESET.

Part: STRINGER CLIP — CORRODED (BS 794) · corrosion level 2 · airframe 53,251 hrs · 30,154 cycles

STRINGER CLIP CORRODED AFT CARGO BAY. REMOVED CRACKED STRINGER CLIP INSTALLED NEW POS 794 RBL 9 WL 150.

Part: SKIN — DENTED (BS 810) · airframe 53,251 hrs · 30,154 cycles

DENT IN FUSELAGE SKIN BELOW AFT CARGO DOOR CUTOUT. REPAIRED USING DOUBLER AND TRIPLER PER ER 09-2311 AND SRM 53-00-01.

Part: GUIDE ARM — WORN (L1 DOOR) · airframe 53,191 hrs · 30,117 cycles

F/A REPORTS L1 DOOR EXTREMELY HARD TO CLOSE AND LATCH. REMOVED AND REPLACED UPPER GUIDE ARM AND ATTACH FITTING PER AMM 52 11 21. DOOR OPERATES AND CLOSES SMOOTHLY.

Part: REPAIR — DAMAGED (L1 DOOR) · airframe 52,326 hrs · 29,609 cycles

L1 DOOR AT PREVIOUS REPAIR TOP AFT CORNER OF REPAIR IS CURLED UP. REMOVED PREVIOUS REPAIR, FABRICATED AND INSTALLED NEW FILLER AND DOUBLER IAW B737 400 SRM 52 00 01.

Part: SKIN — PUNCTURED (NR 9 SPOILER) · airframe 52,326 hrs · 29,609 cycles

NR 9 SPOILER HAS A PUNCTURE ON LOWER SIDE 9 INCHES FROM INBD END. REPAIRED NR 9 SPOILER LOWER SKIN PUNCTURE IAW SRM 51-70-10 REPAIR 4.

Part: FRAME — CRACKED (BS 616) · airframe 52,326 hrs · 29,609 cycles

BS 616 LT SIDE FRAME CRACKED BELOW WL 208 ACCOMPLISHMENT OF EC 5310-0258-5 REQUIRED. REPAIRED LT SIDE FRAME AT STA 616 IAW EC 5310-0258-5.

Part: SKIN — DENTED (BS 832-844) · airframe 52,326 hrs · 29,609 cycles

FUSELAGE SKIN DENTED BELOW AFT CARGO DOOR. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND TRIPLER PER SRM 53-00-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 52,326 hrs · 29,609 cycles

EXTERNAL SKIN ON FUSELAGE DAMAGED BELOW FWD CARGO DOOR STA 480 BUTT LINE 0. CUT OUT DAMAGED AREA & REPAIRED AREA USING FABBED DOUBLER TRIPLER & FILLER IAW B737 400 SRM 53 00 01 FIG 201.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 52,326 hrs · 29,609 cycles

NR 5 SPOILER HAS A DENT WITH A CREASE ON THE UPPER SURFACE OTBD END. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER AND BONDED IAW SRM 51-70-10 REP 4.

Part: SKIN — DELAMINATED (NR 5 SPOILER) · airframe 52,326 hrs · 29,609 cycles

AFTER SEAL REMOVED FOUND DENT TO BE DELAMINATED IN THE CENTER OF NR 5 SPOILER. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REP 4.

Part: SKIN — DENTED (LT FOREFLAP) · airframe 52,326 hrs · 29,609 cycles

LT WING INBD FORE FLAP UPPER SURFACE DENTED 8 INCHES FROM T/E AND 47 INCHES FROM INBD SIDE. DENT MEASURES A=1.3 Y=.033 FOR A/Y 39.39, REPAIRED DENT DAMAGE ON LT WING INBD FOREFLAP UPPER SURFACE IAW SRM 51-70-10 REPAIR 2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 52,326 hrs · 29,609 cycles

FUSELAGE SKIN CREASED 24 INCHES AFT OF L2 DOOR CUTOUT. CUT OUT DAMAGED AREA, REPAIRED AREA USING FABBED DOUBLER TRIPLER AND FILLER IAW B737 400 SRM 53 00 01 FIG 201 REPAIR 31.

Part: SKIN — DENTED (BS 1004-1016) · airframe 52,326 hrs · 29,609 cycles

RT FUSELAGE DENTED 19 INCHES AFT OF R2 DOOR CUTOUT. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER AND TRIPLER AND INSTALLED REPAIR IAW SRM 53-00-01 FIG 201 DETAIL 35.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 52,326 hrs · 29,609 cycles

FWD ENTRY DOOR BEAR STRAP IS CRACKED AT FASTENER HOLE UPPER HINGE CUTOUT. REPAIRED L! DOOR CUTOUT BEAR STRAP AT UPPER HINGE IAW AAR EA 13050 AND ASA EA 400 53EA 00289.

Part: SKIN — GOUGED (RT TE FLAP) · airframe 52,326 hrs · 29,609 cycles

RT WING INBD T/E AFT FLAP SEGMENT SMALL GOUGE ON T/E UPPER SURFACE 5 INCHES FROM OTBD END. REPAIRED RT WING INBD T/E AFT FLAP IAW SRM 51-70-10 REPAIR 4.

Part: SKIN — CHAFED (MID FLAP) · airframe 52,326 hrs · 29,609 cycles

LT OUTBOARD MID FLAP LOWER SURFACE HAS A CHAFED SPOT JUST ABOVE NR 2 FLAP TRACK FAIRING. REPAIRED LT OUTBOARD MID FLAP LOWER SURFACE SKIN IAW B737 400 SRM 51 70 10 PG 214 & IAW B737 400 SRM 51 70 10 PG 249-256.

Part: SKIN — DENTED (NR 9 SPOILER) · airframe 52,326 hrs · 29,609 cycles

RT WING NR 9 SPOILER UPPER SURFACE CLUSTER OF 5 DENTS 5 INCHES FROM END AND 15 INCHES FROM INBD END. DEEPEST DENT MEASURES A=.200 Y=.008 A/Y=25. REPAIRED NR 9 SPOILER UPPER SURFACE DENTS IAW SRM 51-70-10 REPAIR 4.

Part: SKIN — DENTED (NR 9 SPOILER) · airframe 52,326 hrs · 29,609 cycles

RT WING NR 9 SPOILER UPPER SURFACE DENTED CTR 3 INCH FROM 4E DENT. REPAIRED REMOVED DAMAGE FAB AND DRILLED DOUBLER AND INSTALLED REPAIR IAW B737 400 SRM 57 70 10 FIG 201.

Part: SKIN — DENTED (NR 3 SPOILER) · airframe 52,326 hrs · 29,609 cycles

NR 3 SPOILER HAS A SHARP DENT ON UPPER SURFACE 5 INCHES FROM T/E AND 6 INCHES FROM OUTBOARD END. PREPPED DAMAGED AREA, FABRICATED DOUBLER AND BONDED REPAIR IAW SRM 51-70-10.

Part: SKIN — DENTED (NR 8 SPOILER) · airframe 52,326 hrs · 29,609 cycles

RT WING NR 8 SPOILER HAS MULTIPLE PROTRUDING DENTS 8 INCHES FROM T/E HIGHEST DENT MEASURES A=.800 Y=.008 A/Y= 80 MARKED. REPAIRED DENT DAMAGE AT INBD AND OTBD UPPER SURFACE OF NR 8 SPOILER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 REPAIR DOUBLERS INBD END AT 2" ,12" FROM EDGE OTBD END 2", 12" FROM EDGE.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 52,326 hrs · 29,609 cycles

NR 5 SPOILER LOWER INBOARD SURFACE HAS A CLUSTER OF DENTS APPROX 20. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER AND BONDED REPAIR IAW SRM 51-70-10 REP 10.

Part: SKIN — GOUGED (MID FLAP) · airframe 52,326 hrs · 29,609 cycles

RT WING I/B AFT MID FLAP TRAILING EDGE IS GOUGED PREVIOUS REPAIR AT AFT FLAP I/B CONTROL ROD. REMOVED PREVIOUS REPAIR, FABBED REPAIR DOUBLER AND BONDED REPAIR PARTS IAW B737 400 SRM 51 70 10.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 52,326 hrs · 29,609 cycles

NR 5 SPOILER LOWER SURFACE DENTED OUTBOARD END 11 INCHES FROM T/E. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER AND BONDED IAW SRM 51-70-10 REP 4.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 52,326 hrs · 29,609 cycles

NR 5 SPOILER DENTED ON LOWER SURFACE CENTER AREA 9 IN FROM T/E. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER AND BONDED IAW SRM 51-70-10 REP 4.

Part: SKIN — DENTED (LT FOREFLAP) · airframe 52,326 hrs · 29,609 cycles

LT INBD FOREFLAP HAS 2 DENTS 18 INCHES FROM OTBD EDGE ON UPPER CAMBER. PREPPED DAMAGED AREA FABRICATED DOUBLER AND BONDED THE REPAIR IAW SRM 51-70-10 REP 2.

Part: DOOR — STIFF (L1) · airframe 47,101 hrs · 26,737 cycles

L1 DOOR HARD TO CLOSE. CONFIRMED L1 DOOR HANGS UP WHEN AFT LATCH ROLLERS ENTER THE LATCH CAM FITTINGS (AFT). LUBED ALL FOUR LATCH ROLLER TORQUE TUBE BEARINGS PER AMM. ACCOMPLISHED FWD ENTRY DOOR OPS TEST PER AMM, ALL NORMAL.

Part: STRINGER CLIP — CORRODED (BS 500D) · corrosion level 2 · airframe 45,075 hrs · 25,527 cycles

FOUND FRAME TIE CLIP CORRODED. REPLACED TIE CLIP IAW SRM 53 00 03 AND 51 40 02.

Part: FRAME — CORRODED (BS 787 S27R-27L) · corrosion level 2 · airframe 45,075 hrs · 25,527 cycles

FOUND FRAME CORRODED. REPAIRED CORRODED FRAME IAW SRM 53 00 07.

Part: SHEAR TIE — CRACKED (BS 500-500A) · airframe 45,075 hrs · 25,527 cycles

FOUND SHEAR TIE CRACKED. REPLACED SHEAR WEB IAW SRM 51 40 05 AND 51 40 02.

Part: STRINGER — CRACKED (BS 500 S16R) · airframe 45,075 hrs · 25,527 cycles

FOUND STRINGER CRACKED. REPAIRED PER SRM 53 00 03.

Part: SKIN — CRACKED (BS 500-500A) · airframe 45,075 hrs · 25,527 cycles

INSURANCE CLAIM DAMAGED FROM BS 500 TO BS 500A STR 16R TO 18R. DAMAGED SKIN REPAIRED IAW SRM 53 00 01 REPAIR 32.

Part: STRINGER — CORRODED (BS 727C S26R) · corrosion level 2 · airframe 45,075 hrs · 25,527 cycles

FOUND STRINGER 16R CORRODED. REPAIRED CORRODED STRINGER IAW SRM 53 00 03 FIG 201.

Part: STRINGER CLIP — CRACKED (BS 500A S16R)

FOUND TIE CLIP CRACKED. REPLACED CRACKED TIE CLIP IAW SRM 51 40 02.

Part: SHEAR TIE — CRACKED (BS 500 S17R) · airframe 45,075 hrs · 25,527 cycles

FRAME TO SKIN ATTACH ANGLE CRACKED. REPLACED FRAME TO SKIN ATTACH ANGLE IAW SRM 53 00 07.

Part: STRINGER CLIP — CRACKED (BS 500A S18R) · airframe 45,075 hrs · 25,527 cycles

FOUND TIE CLIP CRACKED. REPLACED TIE CLIP IAW SRM 51 40 02.

Part: STRINGER CLIP — CORRODED (BS 907 S26R) · airframe 45,075 hrs · 25,527 cycles

FOUND TIE CLIP CORRODED. REPLACED TIE CLIP IAW SRM 51 40 02.

Part: STRINGER — CRACKED (BS 500) · airframe 45,075 hrs · 25,527 cycles

FOUND STRINGER CRACKED. REPAIRED IAW SRM 51 70 13.

Part: BRACKET — CRACKED (BS 500 S16-17R) · airframe 45,075 hrs · 25,527 cycles

FOUND AFT FRAME TO SKIN ATTACH ANGLE CRACKED. REPAIRED AFT FRAME TO SKIN ATTACH ANGLE IAW SRM 53 00 07.

Part: STRINGER — CRACKED (BS 500 S18R) · airframe 45,075 hrs · 25,527 cycles

STRINGER CRACKED. REPAIRED CRACKED STRINGER IAW SRM 53-00-03.

Part: BRACKET — CRACKED (BS 500) · airframe 45,075 hrs · 25,527 cycles

FWD FRAME TO SKIN ATTACH ANGLE CRACKED. FWD FRAME TO SKIN ATTACH ANGLE REPAIRED IAW SRM 53-00-07.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 44,590 hrs · 25,277 cycles

GOUGE IN EXISTING DOUBLER JUST AFT OF THE FWD CARGO DOOR OPENING IN FUSELAGE. REMOVED EXISTING DOUBLER AND INSTALLED NEW REPAIR PER ASA EA 5330 02104.

Part: SEAL DEPRESSOR — CRACKED (GALLEY DOOR)

AFT GALLEY DOOR CUTOUT SEAL DEPRESSOR CRACKED BELOW LOWER HINGE CUTOUT. REMOVED AND REPLACED IAW SRM. NOTE: REVISION 1 DUE TO MODEL NUMBER, SERIAL NUMBER, AND REFERENCE MATERIAL CORRECTIONS. (K)

Part: FRAME — DENTED (FUSELAGE)

FWD CARGO BAY, BSTA 440, RBL 22, WL 156, FRAME IS DENTED AT FASTENER. TRIMMED OUT DAMAGE AND INSTALLED REPAIR IAW EA. (K)

Part: BULKHEAD — CORRODED (FUSELAGE)

CORROSION ON AFT PRESSURE BULKHEAD C-CHANNEL. REMOVED DAMAGED SECTION OF AFT PRESSURE BULKHEAD AND VERTICAL STIFFENER, FABRICATED REPAIR PARTS AND INSTALLED IAW EA. (K)

Part: SEAL DEPRESSOR — CRACKED (FWD GALLEY DR)

FWD GALLEY DOOR CUTOUT FWD UPPER SEAL DEPRESSOR CRACKED. REMOVED AND REPLACED IAW EA. (K)

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2

CORROSION ON FLOORBEAM. REMOVED TOP SECTION OF FLOORBEAM, FABRICATED AND INSTALLED REPAIR PARTS AND INSTALLED. (K)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

WHILE WORKING FOUND FLOOR SUPPORT IN AFT CARGO BAY TO BE DAMAGED AT BSTA 727E+14 INCH, LBL 13. TRIMMED OUT DAMAGED AREA IN FLOOR SUPPORT IN AFT CARGO BAY AT BSTA 727E + 14 INCH LBL 13 AREA, REMOVED .5 INCH X 6 INCH SECTION, THEN FABRICATED AND INSTALLED REPAIR. ALL WORK PERFORMED IAW EA. (K)

Part: SKIN — DAMAGED (RUDDER)

RUDDER SKIN DAMAGED AT 3 LOCATIONS. LWR LT SIDE AT BOTTOM CORNER EDGE 1 INCH, 2 INCH, AND 7 INCH AFT OF L/E. REPAIRED DAMAGE IAW EA. (K)

Part: SILL — CORRODED (BS 947-1000) · corrosion level 2

CORROSION ON AFT GALLEY MOP SILL BSTA947-1000, RBL 49, WL 206. REMOVED AND REPLACED AFT GALLEY MOP SILL. (K)

Part: SILL — CORRODED (BS 937-1000) · corrosion level 2

CORROSION ON AFT ENTRY MOPSILL, BS 937 TO 1000. REMOVED AND REPLACED AFT ENTRY MOPSILL. (K)

Part: WEB — MISDRILLED (FUEL CELL)

CENTER FUEL CELL, AFT CELL, DRILL START DAMAGE ON UPPER CHORD AND SPANWISE BEAM WEB. REPAIRED DRILL START ON UPPER CHORD AND SPANWISE BEAM. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON FLOORBEAM BSTA 947.5, LBL 16, RBL 16, WL 208. REPAIRED FLOORBEAM IAW SRM AND EA. (K)

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

CORROSION ON FLOORBEAM BSTA 1076, RBL 25-30, WL 208. BLENDED CORROSION, DETERMINED TO BE OUT OF LIMITS, REPAIRED FLOORBEAM IAW SRM. (K)

Part: SEAL DEPRESSOR — CRACKED (AFT GALLEY DOOR)

AFT GALLEY DOOR CUTOUT SEAL DEPRESSOR CRACKED BELOW LWR HINGE CUTOUT. REMOVED AND REPLACED IAW SRM. (K)

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

CORROSION ON FRAME WEB BSTA 796, STR 24R. REMOVED CORROSION, OUT OF LIMITS AND REPAIRED IAW SRM. (K)

Part: SEAT TRACK — CORRODED (FS 907)

PAE - FOUND SEAT TRACK CORRODED AT BS 907 RBL 25 WL 208. REMOVED REPLACED SEAT TRACK. (M)

Part: FRAME — CRACKED (FUSELAGE)

CRACKED FRAME AT BIN RAIL STA 440. REPAIRED CRACKED FRAME AT BIN RAIL BSTA 440, STR 8L-9L IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE)

CRACKED FRAME AT BIN RAIL STA 440. REPAIRED CRACKED FRAME AT BIN RAIL BSTA 440, STR 8L - 9L IAW SRM. (K)

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

CORROSION ON FWD ENTRY DOOR MOPSILL WEB DOUBLER. REMOVED AND REPLACED IAW SRM. (K)

Part: FRAME — CRACKED (FS 787)

PAE - FOUND CRACKED FRAME. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW 737-400 SRM 53-00-07. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

CORROSION ON U-CHANNEL, BSTA 312 - 344, LBL 59, WL 208. REMOVED AND REPLACED IAW SRM. (K)

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

CORROSION ON FWD ENTRY DOOR MOPSILL BSTA 300-344, LBL 58, WL 208. REMOVED AND REPLACED IAW SRM. (K)

Part: FRAME — CRACKED (BS 360)

CRACKED FRAME AT BIN RAIL BSTA 360, BETWEEN STR 7L AND 8L. REPAIRED IAW SRM. (K)

Part: FRAME — CRACKED (BS 400)

PAE - FOUND CRACKED FRAME AT BIN RAIL STATION 400 BETWEEN STRINGER 8R-9R. REPAIRED CRACKED FRAME AT BIN RAIL STATION 400 BETWEEN STRINGER 8R-9R IAW 737-400 SRM 53-00-07. (M)

Part: FRAME — CRACKED (FUSELAGE)

CRACKED FRAME AT BSTA 480 BIN RAIL, STR 8R-9R. REPAIRED IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE)

CRACKED FRAME AT BIN RAIL STA 400. REPAIRED CRACKED FRAME AT BIN RAIL BSTA 400, STR 8L- 9L IAW SRM. (K)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON SEAT TRACK FLANGE, BSTA 344, LBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK IAW SRM. (K)

Part: SEAL DEPRESSOR — CRACKED (FWD GALLEY DOOR)

FWD GALLEY DOOR CUTOUT SEAL DEPRESSOR ABOVE UPPER HINGE CUTOUT IS CRACKED. REMOVED AND REPLACED FWD GALLEY DOOR CUTOUT SEAL DEPRESSOR ABOVE UPPER HINGE CUTOUT. (K)

Part: ANGLE — DAMAGED (BS 309)

DAMAGED MOPSILL REINFORCEMENT ANGLE. REMOVED AND REPLACED IAW SRM. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON FLOORBEAM. REPAIRED IAW SRM. (K)

Part: WEB — CORRODED (FUSELAGE)

CORROSION ON WEB UNDER FWD ENTRY DOOR MOPSILL AT BSTA 333-342, LBL 58, WL 208. REPLACED WEB UNDER FWD ENTRY DOOR MOPSILL. (K)

Part: SILL — CORRODED (FUSELAGE)

CORROSION ON FWD GALLEY MOPSILL. REMOVED AND REPLACED FWD GALLEY MOPSILL. (K)

Part: FRAME — CRACKED (FS 907)

PAE - FOUND CRACKED FRAME. REPAIRED CRACKED FRAME IAW 737-400 SRM 53-00-07. (M)

Part: FRAME — CRACKED (BS 747, STR 4L)

CRACKED FRAME AT BIN RAIL BSTA 747, STR 4L AND BL 0. REPAIRED SRM. (K)

Part: INTERCOSTAL — MISDRILLED (FUSELAGE)

FWD CARGO BAY, BSTA 509, RBL 22, WL 154, INTERCOSTAL HAS A DRILL START. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM. (K)

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2

CORROSION ON CREASE BEAM WEB BSTA 336-344, RBL 62, WL 208. REPAIRED CREASE BEAM WEB IAW SRM. (K)

Part: SKATE ANGLE — CHAFED (VERTICAL FIN)

RT FWD SKATE ANGLE FOR VERTICAL FIN CHAFED 3 INCHES FROM FWD END ON IB SIDE. REMOVED AND REPLACED FWD SKATE ANGLE FOR VERTICAL FIN. (K)

Part: FRAME — CRACKED (FUSELAGE)

CRACKED FRAME. REPAIRED CRACK IAW SRM. (K)

Part: SKATE ANGLE — CHAFED (VERTICAL FIN)

RT AFT SKATE ANGLE FOR VERTICAL FIN CHAFED 18 INCH FROM AFT END ON OB SIDE. REMOVED AND REPLACED AFT SKATE ANGLE FOR VERTICAL FIN. (K)

Part: FITTING — CORRODED (STOP PAD) · corrosion level 2

CORROSION ON AFT CARGO DOOR FWD LWR STOP PAD FITTING. REMOVED, BLENDED AND FOUND TO BE (OUT OF LIMITS). REPLACED AFT CARGO DOOR FWD LWR STOP PAD FITTING. (K)

Part: SKATE ANGLE — CHAFED (VERTICAL FIN)

RT FWD SKATE ANGLE FOR VERTICAL FIN CHAFED 3 INCHES FROM FWD END ON IB SIDE. REMOVED AND REPLACED FWD SKATE ANGLE FOR VERTICAL FIN. (K)

Part: SKATE ANGLE — CHAFED (VERTICAL FIN)

RT AFT SKATE ANGLE FOR VERTICAL FIN CHAFED 18 INCHES FROM AFT END ON OB SIDE. REMOVED AND REPLACED AFT SKATE FOR VERTICAL FIN. (K)

Part: RIB — GOUGED (HORIZ STAB)

OKC- RT HORIZONTAL STAB T/E NR3 RIB IS GOUGED ON THE OB SIDE. PREPARED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM. (K)

Part: SKIN — DENTED (NR 6 SPOILER)

OKC - NR 6 SPOILER HAS 2 SHARP DENTS IN AREA OF ACTUATOR ATTACH. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM. (K)

Part: BALANCE ARM — DAMAGED (RUDDER)

OKC - RUDDER BALANCE ARM HAS DAMAGE TO TOP SKIN UPON REMOVAL. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR SKIN SECTION AND DOUBLER IAW AS EA. CRACK-(Y SHAPE 3.7 X 3.75 X 2.75). (K)

Part: FRAME — CORRODED (FUSELAGE)

OKC - AFT CARGO COMPARTMENT B-STA 727E FRAME IS CORRODED ON THE FORWARD SIDE BETWEEN STR 25R AND 25L. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER, ANGLE, AND SHEAR TIE IAW SRM. (K)

Part: FRAME — MISDRILLED (FUSELAGE)

OKC - AFT CARGO COMPARTMENT FRAME 947 HAS A MISDRILLED HOLE STRINGER 26 R. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER AND SHIMS IAW SRM. (K)

Part: SKIN — DENTED (NR 7 SPOILER)

OKC - NR 7 SPOILER HAS 2 SHARP DENTS IN AREA OF ACTUATOR ATTACH. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM. (K)

Part: SKIN — CRACKED (L/E SLAT)

OKC - NR3 SLAT LOWER SKIN CRACKED AT FASTENER OB END .6 INCHES LONG. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K)

Part: SKIN — CRACKED (L/E SLAT)

OKC - NR 2 SLAT LOWER SKIN CRACKED 2 PLACES IB END AT FASTENER (.73 INCH LONG) AND CENTER (1.6 INCHES LONG). REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K)

Part: SKIN — DENTED (AFT CARGO DOOR)

OKC - AFT CARGO DOOR DENTED IN MIDDLE, EXTERNAL SKIN. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM. (K)

Part: SKIN — DENTED (T/E FLAP)

OKC - LT WING IB AFT FLAP LOWER SKIN HAS 2 DENTS TOGETHER, 17 INCHES FROM THE IB EDGE AND 7.5 INCHES FROM THE TE A=5.3, Y=.075, A/Y= 70. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

OKC - STRINGER CLIP AT STA 947, STR 26R, CRACKED AND CORRODED. REMOVED DAMAGED CLIP, FABRICATED AND INSTALLED A REPLACEMENT CLIP IAW SRM. (K)

Part: SKIN — DENTED (NR 3 SPOILER)

OKC - NR 3 SPOILER UPPER SKIN IS DELAMINATED IN SEVERAL PLACES. UPON FURTHER INVESTIGATION NO DELAMINATION NOTED, AREAS HOWEVER DENTED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. (K)

Part: FRAME — CORRODED (FUSELAGE)

OKC - AFT CARGO COMPARTMENT STA B 927 FRAME IS CORRODED ON THE UPPER AND LOWER FLANGES, RBL 18 TO RBL 19. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND REPAIR ANGLE IAW SRM. (K)

Part: SKIN — PUNCTURED (NR 2 SPOILER)

OKC - NR 2 SPOILER UPPER SKIN IS DELAMINATED AND PUNCTURED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. (K)

Part: WEDGE — DELAMINATED (L/E SLAT)

OKC - RT WING NR 5 LE SLAT TRAILING EDGE WEDGE HAS SMALL AREA OF DELAMINATION AND DETERIORATED EDGE POTTING ON OB EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER AND REPORTED IAW SRM. (K)

Part: WEB — CORRODED (FUSELAGE)

OKC - AFT CARGO DOOR CUTOUT LOWER SILL WEB IS CORRODED AT B STA 794 TO 847, RBL 20 TO RBL 28. REMOVED DAMAGED WEB, ORDERED AND INSTALLED A NEW WEB IAW SRM. (K)

Part: TIE CLIP — CRACKED (FUSELAGE)

OKC - STA 460 FRAME TO STRINGER AT 27R TIE CLIP IS CRACKED. REMOVED DAMAGED CLIP, FABRICATED AND INSTALLED REPLACEMENT CLIP IAW SRM. (K)

Part: DOOR FRAME — GOUGED (FUSELAGE)

OKC - E AND E BAY DOOR CUTOUT FORWARD FRAME, WEB AT STA328, LBL 0 TO 3 IS GOUGED. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM. (K)

Part: ENGINE — MALFUNCTIONED (UNKNOWN)

EN ROUTE AT 31,000 FT, CREW FELT BUMP AND VIBRATION LASTING LESS THAN A MINUTE. ALL ENGINE GAUGED AND SYSTEMS WERE NORMAL. EVERYTHING SMOOTHED OUT. LATER, WHILE DESCENDING THROUGH 10,000 FT, ENGINE EXPERIENCED COMPRESSOR STALL WITH SEVERE VIBRATION. CREW SHUT DOWN ENGINE FOLLOWING QRC/QRH PROCEDURES AND ACCOMPLISHED SINGLE ENGINE LANDING. REMOVED AND REPLACED ENGINE. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C-CHECK FOUND CORROSION ON SHEAR TIE AT BS 727G BETWEEN STR 27 LT AND 26 LT. REMOVED AND REPLACED IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C-CHECK FOUND CORROSION ON SHEAR TIE AT BS 927 BETWEEN STR 26RT AND 27RT. REMOVED AND REPLACED IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C CHECK, FOUND CORROSION ON FRAME SHEAR TIE AT BS 500C BETWEEN STR 28L AND 28R. REMOVED AND REPLACED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 767 TO 727B+5, RBL20 AND WL156. REMOVED AND REPLACED IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C CHECK, FOUND CORROSION ON SHEAR TIE AT BS 927 BETWEEN STR 26 RT AND 25 RT. REMOVED AND REPLACED IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C CHECK FOUND CORROSION ON FRAME SHEAR TIE AT BS 500D BETWEEN STR 27L AND 28L. REPAIRED IAW SRM.

Part: FRAME — CORRODED (FUSELAGE)

DURING -C- CHECK FOUND CORROSION ON FRAME AT BS 727G BETWEEN STR 26L AND 25L. REMOVED AND REPLACED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING "C" CHECK FOUND CORROSION ON FLOOR TO BULKHEAD SUPPORT AT BS 947 RBL 21 AND WL 156. REMOVED AND REPLACED IAW SRM.

Part: CHANNEL — CORRODED (VHF ANTENNA)

DURING -C- CHECK, FOUND CORROSION ON LOWER VHF ANTENNA SUPPORT CHANNEL. REMOVED AND REPLACED IAW SRM

Part: FRAME — CORRODED (FUSELAGE)

DURING C-CHECK FOUND CORROSION ON FRAME AT BS 727F BETWEEN STR 26LF AND 25LF. REPAIRED IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING-C- CHECK FOUND CORROSION ON SHEAR TIE AT BS 727D BETWEEN STR 25R AND 26R. REMOVED AND REPLACED IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C CHECK FOUND CORROSION ON SHEAR TIE AT STA 500E BETWEEN STR 27R AND 28R. REMOVED AND REPLACED IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C CHECK FOUND CORROSION ON SHEAR TIE AT BS 727C BETWEEN STRINGER 25R AND 26R. REMOVED AND REPLACED IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C CHECK FOUND CORROSION ON SHEAR TIE AT BS 768 BETWEEN STR 26L AND 27L. REMOVED AND REPLACED IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING -C- CHECK FOUND CORROSION ON SHEAR TIE AT BS 807 LBL 12 BETWEEN STR 26 LT AND 27 LT. REMOVED AND REPLACED IAW SRM.

Part: KEELBEAM — CORRODED (FUSELAGE)

DURING -C- CHECK FOUND CORROSION ON LT KEELBEAM AT BS 500G+4. REPAIRED IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C CHECK, FOUND CORROSION ON FRAME SHEAR TIE AT BS 500B BETWEEN STR 28L AND 28R REPAIRED IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL. REMOVED AND REPLACED IAW SRM. (M)

Part: DOUBLER — GOUGED (APU DOOR)

PAE - DURING C-CHECK, FOUND APU COMPARTMENT DOOR REPAIR IS GOUGED 16 INCHES FROM AFT END AND 7 INCHES FROM LEFT EDGE. REMOVED AND REPLACED DOUBLER IAW SRM. (M)

Part: STIFFENER — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON UPPER SURFACE OF FORWARD CARGO DOOR THRESHOLD WEB STIFFENER AT BS 460, RBL 29, WL 156. REMOVED AND REPLACED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 747 BETWEEN STRINGER 26 LEFT AND 27 LEFT. REMOVED AND REPLACED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 768 BETWEEN STRINGER 26 RT AND 27 RT. REMOVED AND REPLACED SHEAR TIE PER SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 837 TO 947 AND LBL 21 AND WL 156. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 727 PLUS 10 INCHES LBL 21 AND WL 156. REMOVED AND REPLACED IAW SRM. (M)

Part: SKIN — GOUGED (FUSELAGE)

DURING C-CHECK, FOUND GOUGE ON EXTERIOR SKIN AT BS 500 PLUS 1.5 AND 2.5 INCHES BELOW STRINGER 22R. REMOVED AND REPLACED IAW SRM. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON SUB THRESHOLD WEB AT BS 840 TO BS 794 RBL 19.5 TO 27.5 AND WL 156. REMOVED AND REPLACED THRESHOLD WEB IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT. REMOVED AND REPLACED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 787 RBL 17 BETWEEN STRINGER 25 RT AND 26 RT. REMOVED AND REPLACED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDE WALL SUPPORT AT BS 767 TO 794 RBL 20 AND WL 156. REMOVED AND REPLACED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON SIDEWALL SUPPORT AT BS 727E PLUS 10 TO 835, LBL 21 AND WL 156. REMOVED AND REPLACED SUPPORT IAW SRM. (M)

Part: DOOR FRAME — CORRODED (CARGO DOOR)

DURING C-CHECK, FOUND FORWARD CARGO DOOR FRAME AFT CLOSURE WEB LOWER FORWARD CORNER DAMAGED. REPAIRED IAW SRM. (M)

Part: THRESHOLD — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON LOWER SURFACE OF FORWARD CARGO DOOR THRESHOLD WEB AT NUT PLATED AT BS 445-490, RBL 29 AND WL 156. REMOVED AND REPLACED IAW SRM. (M)

Part: DOOR FRAME — CORRODED (CARGO DOOR)

PAE - DURING C-CHECK, FOUND FORWARD CARGO DOOR FRAME AFT CLOSURE WEB LOWER FORWARD CORNER IS DAMAGED. REMOVED DAMAGED LOWER FORWARD CORNER OF FORWARD CARGO DOOR FRAME AFT CLOSURE WEB AND REPAIRED PER SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDE WALL SUPPORT BS 847 TO 867, RBL 20 WL 156. REMOVED AND REPLACED WITH NEW SUPPORT PER SRM. (M)

Part: WIRE — DISCONNECTED (CABIN)

FAI - FOUND FLOOR TRACK LIGHTING INOPERATIVE FROM ROW 18-20. RECONNECTED TRACK LIGHT WIRING, OPS CHECKED NORMAL. (M)

Part: WIRE — DISCONNECTED (CABIN)

FAI - FLOOR TRACK LIGHTING INOPERATIVE FROM ROW 22-25. RECONNECTED TRACK LIGHT WIRING, OPS CHECKED NORMAL. (M)

Part: WIRE — DAMAGED (CABIN)

JNU - FLOOR TRACK LIGHTING INOPERATIVE FROM ROW 14-17. REPLACED DAMAGED TRACK LIGHT WIRING, OPS CHECKED NORMAL. (M)

Part: TERMINAL — DISCONNECTED (CABIN)

FAI - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROWS 17-23 INOPERATIVE. RECONNECTED WIRE TERMINAL ENDS. LIGHTS THEN FUNCTIONED PROPERLY. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND TRACK LIGHTS INOPERATIVE AT ROW 20. RECONNECTED LIGHTS, OPS CHECKED NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FAI - DURING LINE CHECK, FOUND NUMEROUS TRACK LIGHTS INOPERATIVE. RELAMPED AND RECONNECTED LIGHTS, OPS CHECKED NORMAL. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND FLOOR TRACK LIGHTS DISCONNECTED AT ROW 22. RECONNECTED WIRES. TRACK LIGHTS THEN OPERATED NORMALLY. (M)

Part: WIRE — DAMAGED (CABIN)

PDX - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTING AT ROW 16 INOPERATIVE. RESTORED WIRING TO ORIGINAL CONDITION, OPS CHECKED GOOD. (M)

Part: WIRE — DISCONNECTED (CABIN)

JNU - DURING PREFLIGHT, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROWS 21 AND 22. RECONNECTED FLOOR TRACK LIGHTING WIRE, OPS CHECKED GOOD. (M)

Part: BALLAST — FAILED (CABIN)

OAK - DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHT AT OVERWING EXIT INOPERATIVE. REMOVED AND REPLACED LIGHT BALLAST, OPERATIONAL CHECK NORMAL. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROWS 16ABC TO 19ABC INOPERATIVE, WIRE BROKEN. REPAIRED BROKEN WIRE. OPS CHECK NORMAL. (M)

Part: STRAP — CHAFED (HORIZONTAL STAB)

PAE - DURING SCHEDULED SI CHECK, THE RIGHT HORIZONTAL STABILIZER L/E WAS FOUND TO BE CHAFED ON THE INTERNAL STRAP AT INBOARD END, L/E STATION 86.88. REPAIRED PER EA 5510-01098. (M)

Part: LIGHT — BROKEN (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD THREE EMERGENCY EIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BROKEN LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

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

Part: ENGINE — MALFUNCTIONED (NR 2 ENGINE)

PDX-ATB - FLT 95, DUE TO REPORT OF SMOKE IN THE CABIN AFTER TAKEOFF. PACKS WERE TURNED OFF AND THE SMOKE DISSIPATED. AIRCRAFT RETURNED TO PDX AND LANDED WITHOUT INCIDENT. PDX MAINTENANCE INSPECTED AIRCRAFT AND RELEASED FOR FERRY FLIGHT TO SEA FOR REPAIR. SEA MAINTENANCE INSPECTED AIRCRAFT AND FOUND THE NR 2 ENGINE TO BE THE SOURCE OF CABIN SMOKE ODOR. REPLACED NR 2 ENGINE. SUBSEQUENTLY REPLACED THE NR 3 BEARING AIR/OIL SEAL AND OVERHAULED 7 FUEL NOZZLES ON THE ENGINE. THE ENGINE WAS THEN REASSEMBLED, TESTED, AND RETURNED TO SERVICE. (M)

Part: WIRE — FAILED (CABIN)

PDX - PRIOR TO FLT 440 SEVERAL EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE MID-CABIN AREA. REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — FAILED (CABIN)

YVR - PRIOR TO FLT 684, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 14-15. CONTRACT MAINTENANCE REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: GUIDE ARM — FAILED (R1 DOOR)

PDX - DURING A-CHECK, THE R-1 DOOR HOLD OPEN LEVER WOULD NOT FUNCTION PROPERLY. REPLACED UPPER GUIDE ARM AND DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT 2 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS, LIGHTS OPERATED NORMALLY. (M)

Part: SIGN — MISSING (CABIN)

ANC - PRIOR TO FLIGHT 534, THE LEFT FLOOR 'EXIT' SIGN AT ROW 14 WAS FOUND TO BE MISSING. REPLACED 'EXIT' SIGN. (M)

Part: STIFFENER — WORN (LT TE FLAP)

SEA - DURING C-CHECK, FOUND WEAR ON A STIFFENER ON THE LEFT WING NR 3 FLAP TRACK FAIRING INBOARD SKIN. REPAIRED PER EA 5720-01134. (M)

Part: FITTING — CORRODED (RT ELEVATOR)

SEA - DURING C-CHECK, FOUND CORROSION IN THE TWO AFT HOLES OF THE RT OUTBOARD ELEVATOR HINGE FITTING. REPAIRED PER EA 5520-01052 AND BOEING TELEX ASA-SEA-98-0029RR. (M)

Part: TR UNIT — GOUGED (NR 1 ENGINE)

SEA - DURING C-CHECK, THE NR 1 ENGINE INBOARD T/R BLOCKER DOORS WERE FOUND RIDING THE BULLNOSE IN SEVERAL PLACES. REPAIRED PER EA 5430-01027 AND BOEING TELEX ASA-SEA-98-0028RR. (M)

Part: TR UNIT — GOUGED (NR 2 ENGINE)

SEA - DURING C-CHECK, THE NR 2 ENGINE INBOARD T/R BULLNOSE SECTION WAS FOUND GOUGED AT THE 10 AND 11 O'CLOCK POSITIONS. REPAIRED PER EA 5430-01027 AND BOEING TELEX ASA-SEA-98-0028RR. (M)

Part: FAIRING — WORN (RT TE FLAP)

SEA - DURING C-CHECK, THE RT WING NR 6 FLAP TRACK FAIRING TAILCONE WAS FOUND TO HAVE LOOSE RIVETS. REPAIRED PER EA 5750-01212 ADN BOEING TELEX ASA-SEA-96-0203RR. (M)

Part: ANGLE — CORRODED (L1 DOOR SILL)

SEA - DURING C-CHECK, FOUND CORROSION IN THE UPPER SURFACE OF THE L1 DOOR SILL ANGLE. REPAIRED PER EA 5310-01569 AND BOEING TELEX ASA-SEA-98-0030RR. (M)

Part: SKIN — CRACKED (RUDDER)

SEA - DURING C-CHECK, THE RUDDER LEFT AND RIGHT SIDES WERE FOUND TO HAVE ETCHED AND CRACKED PAINT. ON FURTHER EVALUATION IT WAS DETERMINED THAT THE OUTER PLIES OF GRAPHITE WERE FOUND TO BE PEELING AND SPLINTERING. REMOVED AND REPLACED RUDDER. REMOVED RUDDER WAS SENT TO NORDAM FOR EVALUATION AND REPAIR. THE RUDDER WAS SUBSEQUENTLY EXCHANGED BY NORDAM AND ALASKA AIRLINES RECEIVED A NEW RUDDER. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT 7 - PRIOR TO DEPARTURE, THE AFT FIVE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AT ROW 27 AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (OVERWING EXIT)

PHX - FLT 721 - PRIOR TO DEPARTURE, THE CREW REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT THE OVERWING EMERGENCY EXIT. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

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

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT 158 - DURING CREW PREFLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 15 THROUGH 19. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 15, 16, AND 17. REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT 441 - PRIOR TO DEPARTURE, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 19 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACKLIGHTS WERE FOUND TO BE INOPERATIVE BETWEEN ROWS 14 THROUGH 18. RECONNECTEDWIRING AT ROW 14 AND LIGHTS OPERATED NORMALLY.(M)

Part: LIGHT — DEFECTIVE (CABIN)

ANC - FLT 88 - PRIOR TO DEPARTURE THE EMERGENCY EXIT FLOOR TRACK LIGHT AT ROW 23 WAS FOUND INOPERATIVE. RELEASED PER MEL 33-19B. REPLACED LIGHT ASSEMBLY WITH HARNESS IN SEA ON 7/2/96, AND LIGHT OPERATED NORMALLY. REMOVED PLACARD. (M)

Part: BATTERY CHARGER — DEFECTIVE (CABIN)

JNU - DURING MAINTENANCE CHECK, SECTIONS OF THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPAIRED BROKEN WIRING, REPLACED LAMP BASE ASSEMBLIES, REPLACED BATTERY CHARGER AND ALL LIGHTS OPERATED NORMALLY. REFERENCE: OPERATOR CONTROL NR ASAA9640045.

Part: LAMP BASE ASSY — DEFECTIVE (CABIN)

JNU - DURING MAINTENANCE CHECK, SECTIONS OF THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPAIRED BROKEN WIRING, REPLACED LAMP BASE ASSEMBLIES, REPLACED BATTERY CHARGER AND ALL LIGHTS OPERATED NORMALLY. REFERENCE: OPERATOR CONTROL NR 96ZZZX3298. (X)

Part: WIRE — DISCONNECTED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 15-18. RECONNECTED LOOSE WIRES AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 15-18. RECONNECTED LIGHTS AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — SEPARATED (CABIN)

JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 15 THROUGH 18. RECONNECTED SEPARATED WIRES AND LIGHTS OPERATED NORMALLY. (M)

Part: SOCKET — DISCONNECTED (CABIN)

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

Part: WIRE — DISCONNECTED (CABIN)

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

Part: EEL WIRING — DISCONNECTED (CABIN)

OAK - FLT NR 486 - DURING PREFLIGHT, FOUND EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 15-17. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - FLT NR 486 - DURING PREFLIGHT, FOUND EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 15-18. FOUND SPLIT IN WIRE AT DISCONNECT, RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - FLOOR TRACK LIGHTS INOP ROWS 15-18. MAINTENANCE RECONNECTED WIRE HARNESS AT ROW 18. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - CHECK, LAST 2 FLOOR EMERGENCY LIGHTS INOP. MAINTENANCE RECONNECTED WIRES. (W)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - FLT 110 - CREW REPORTED EMERGENCY EXIT FLOOR TRACK LIGHTS INOP AT ROWS 15. FOUND WIRES DISCONNECTED AT ROW 15. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)