N709AS

Part: SIGN — BROKEN (CABIN) · airframe 51,694 hrs · 34,331 cycles

EXIT SIGN ABOVE THE ENTRY TO FLIGHT DECK IS BROKEN. GROUNDED - YES. REMOVED AND REPLACED EXIT SIGN COVER THAT WAS BROKEN.

Part: TEE FITTING — CRACKED (DOOR FRAME) · airframe 51,381 hrs · 34,116 cycles

FWD GALLEY DOOR CUTOUT NR 1 DOOR STOP TEE CRACKED IN RADIUS BS 333, STRINGER 8. ACFT GROUNDED. REMOVED AND REPLACED THE TEE IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 727) · airframe 51,381 hrs · 34,116 cycles

RIGHT OTBD BS 727 FRAME CRACKED, STRINGER 18A. ACFT GROUNDED. ACCOMPLISHED A REPAIR IAW AD20122304-400-53-011R, AND AD20122304-400-53-8.

Part: GUIDE ARM — DAMAGED (L1 DOOR) · airframe 51,046 hrs · 33,861 cycles

RAMP REPORTED UNABLE TO OPEN THE L1 DOOR. ACFT GROUNDED. ATTEMPTED TO OPEN DOOR, NO LUCK. DOOR UNLATCHES, CRACKS OPEN MAKING A CRACKLING NOISE AND BINDS. FOUND BOTTOM RADIUS LINK KEY WASHER AND SCREW MISSING WHICH CAUSED BINDING ON L1 DOOR GUIDE ARM. REMOVED AND REPLACED PIN, KEYWASHER AND SCREW ON THE L1 DOOR GUIDE ARM, OPS CHECKED GOOD IAW AMM TASK 52-11-21-404-007-003, STEP 3.D. NO ADJUSTMENTS DISTURBED ON GUIDE ARM.

Part: SKIN — CRACKED (FWD CARGO DOOR) · airframe 51,038 hrs · 33,856 cycles

FORWARD CARGO DOOR SKIN CRACKED, UPPER AFT CORNER OF HANDLE CUT OUT. ACFT GROUNDED. INSTALLED A REPAIR DOUBLER IAW SRM 52-00-01-2R-2.

Part: STOP FITTING — GOUGED (FWD CARGO DOOR) · airframe 50,510 hrs · 33,442 cycles

FWD CARGO DOOR FWD LOWER FITTING DAMAGE IN PREVIOUS BLENDED AREA OUT OF LIMITS OF IAW SRM 52-30-02-1A-1. ACFT GROUNDED. REPLACED FWD LOWER STOP FITTING IAW SRM 51-40-02, AND DWG 65-46921.

Part: INTERCOSTAL — CRACKED (BS 420-440) · airframe 47,650 hrs · 31,218 cycles

FWD CARGO BAY INTERCOSTAL BS 420-440, STR 26R IS CRACKED, FOUND UPON REMOVAL OF TRANSITIION PANEL. ACFT GROUNDED. R & R CRACKED INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: STRINGER SPLICE — CORRODED (BS 907) · corrosion level 2 · airframe 47,649 hrs · 31,217 cycles

AFT CARGO BAY STRINGER SPLICE 21R AT BS 907 IS CORRODED. ACFT GROUNDED. R & R THE STRINGER SPLICE AT BS 907 IAW SRM 51-40-02-0G-0.

Part: STRAP — CRACKED (BS 312-344) · airframe 47,650 hrs · 31,218 cycles

FLOORBEAM STABILIZER STRAP BL0 IS CRACKED THROUGH AT BS 312. ACFT GROUNDED. R & R STRAP IAW SRM 51-40-02-0G-0.

Part: STRINGER — CORRODED (BS 907-1016) · corrosion level 2 · airframe 47,649 hrs · 31,217 cycles

STRINGER 21R HAS MULTIPLE AREAS OF CORROSION AT BS 986. ACFT GROUNDED. R & R THE STRINGER IAW SRM 51-40-02-0G-0.

Part: WEB — CORRODED (BS 810) · corrosion level 2 · airframe 47,650 hrs · 31,218 cycles

LATERAL TRACK AT BS 807, LBL 50 CORRODED ON LOWER SIDE. ACFT GROUNDED. REMOVED AND REPLACED WEB UNDERNEATH LATERAL TRACK AT BS 807, LBL 50 IAW SRM 51-40-02-0G-0, W 2, O .071", R 0.58", L 4, D .013".

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 47,650 hrs · 31,218 cycles

INTERCOSTAL BS 312 TO BS 328 AT LBL45, CRACKED. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: FRAME — CRACKED (BS 344) · airframe 47,649 hrs · 31,217 cycles

FRAME AT BS 344 HAS A CRACK INDICATION AT BS 4 RT LOWER FWD HOLE AT SPLICE. ACFT GROUNDED. REPAIRED DAMAGE TO FRAME IAW EA 400-53EA-17039. THIS REPAIR HAS A REINSPECT THRESHOLD OF 8,000 FLT. CYCLES AFTER MODIFICATION WITH A REPAIR INTERVAL OF 8,000 FLT. CYCLES. PERFORM THE INSPECTIONS SPECIFIED BY UJ-2 AT THE LAST 4 FASTENERS COMMON TO THE PD37-53-2526-1, REPAIR ANGLE AND THE FRAME WEB, LOCATE APPROXIMATELY AT BS 5.5R, FIG 4. ADDITIONALLY, PERFORM THE INSPECTION SPECIFIED BY UJ-2 AT THE LAST 2 FASTENERS COMMON TO THE PD37-53-2526-1. REPAIR ANGLE AND THE FRAME FLANGE LOCATED APPROXIMATELY AT STR 5.5R, FIG 4 OF EA 400-53EA-17039.

Part: CARGO TRACK — CORRODED (BS 870-947) · corrosion level 2 · airframe 47,649 hrs · 31,217 cycles

AFT PIT CARGO TRACK RBL 13 AT BS 945 IS CORRODED. ACFT GROUNDED. CORRODED TRACK IS FOUND OUT OF LIMITS. R & R DAMAGE SECTION OF TRACK IAW SRM 51-40-02-0G-0.

Part: STRAP — CRACKED (BS 460) · airframe 47,650 hrs · 31,218 cycles

MCD STRAP AT BS 460, STR 20L CRACKED. ACFT GROUNDED. R & R INNER WEB STRAP IAW SRM 51-40-02-0G-0.

Part: STRAP — CRACKED (BS 400) · airframe 47,650 hrs · 31,218 cycles

MCD STRAP AT BS 400, SR 20L CRACKED. ACFT GROUNDED. R & R INNER WEB STRAP IAW SRM 51-40-02-0G-0.

Part: STRAP — CRACKED (BS 420) · airframe 47,650 hrs · 31,218 cycles

MCD STRAP AT BS 420, STR 20L CRACKED. ACFT GROUNDED. R & R INNER WEB STRAP IAW SRM 51-42-02-0G-0.

Part: INTERCOSTAL — CRACKED (BS 277-294) · airframe 47,650 hrs · 31,218 cycles

INTERCOSTAL CRACKED IN RADIUS AT STR 14 RT AT BS 277. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: FRAME — CRACKED (BS 500E) · airframe 47,649 hrs · 31,217 cycles

LEFT FRAME, STA 500E IS CRACKED AT .50 HOLE BETWEEN STR 20 AND 21 LT. ACFT GROUNDED. REPAIRED DAMAGE TO FRAME IAW SRM 53-00-07-2R-13, REPAIR 13. THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 66,000 TOTAL ACFT CYCLES REFER TO SRM 53-00-07-2R-13, REPAIR 13, TABLE V FOR INSPECTION METHODS AND INTERVALS.

Part: FITTING — CORRODED (BS 303) · corrosion level 2 · airframe 44,832 hrs · 29,045 cycles

L1 DOOR LWR HINGE, UPPER BEARING PLATE SUPPORT STRUCTURE CORRODED AT FASTENERS, FOUND OK TO INSTALL. ACFT GROUNDED. R & R LOWER HINGE SUPPORT FITTING IAW SRM 51-40-02 0G 0, W 1, O .100, R 0, L 1, D 100 PERCENT.

Part: ANGLE — CRACKED (BS 277-291) · airframe 44,832 hrs · 29,045 cycles

INTERNAL ANGLE ABOVE STRINGER 10 ON FWD SIDE OF RT GALLEY DOOR CUT OUT IS CRACKED NDT VERIFIED. ACFT GROUNDED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02-0G-0.

Part: ANGLE — CRACKED (BS 277-291) · airframe 44,832 hrs · 29,045 cycles

INTERNAL ANGLE BELOW STRINGER 12 ON FWD SIDE OF RT GALLEY DOOR IS CRACKED NDT VERIFIED. ACFT GROUNDED. R & R INTERNAL ANGLE BELOW STRINGER 12 ON FWD SIDE OF RT GALLEY DOOR IAW SRM 51-40-02-0G-0.

Part: ANGLE — CRACKED (BS 277-291) · airframe 44,832 hrs · 29,045 cycles

INTERNAL ANGLE BELOW STRINGER 11 ON FWD SIDE OF RT GALLEY DOOR CUTOUT IS CRACKED, NDT VERIFIED. ACFT GROUNDED. R & R THE ANGLE IAW SRM 51-40-02-0G-0.

Part: CHANNEL — CORRODED (BS 986-1006) · corrosion level 2 · airframe 44,832 hrs · 29,045 cycles

AFT WASTE WATER DRAIN MAST MIDDLE ATTACH FASTNER HOLE HAS LIGHT SURFACE CORR ON INTERNAL SIDE. REF AD 20122314-400-53 STE4P 14 CORR WAS FOUND CONTACT ENG TO OBTAIN AMOC REPAIR. GROUNDED - YES. REMOVED AND REPLACED AFT WASTE WATER DRAIN MAST MIDDLE SUPPORT CHANNEL IAW AD20122314, 400-53-103 R, W .25 O .040 R .037 L 1.0 D .003.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 44,656 hrs · 28,915 cycles

L1 DOOR FLOOR EMERGENCY EXIT LIGHT COVER LENS BROKEN. ACFT GROUNDED. REPLACED L1 DOOR FLOOR EMERGENCY EXIT LIGHT COVER LENS REF AMM 33-51-81-962-011. OPS CHECK GOOD.

Part: WEB — CRACKED (APU BAY) · airframe 41,765 hrs · 26,672 cycles

APU UPPER SHROUD RT SIDE EDGE HAS A CRACK BY AFT LATCH FITTING. ACFT GROUNDED. REPAIRED APU UPPER SHROUND RT SIDE EDGE IAW EA 400-49EA-11534.

Part: WEB — CRACKED (APU BAY) · airframe 41,765 hrs · 26,672 cycles

APU UPPER SHROUD AIR INLET CUTOUT WEB EDGE BENT AND CRACKED. ACFT GROUNDED. REPAIRED APU UPPER AIR INLET CUTOUT WEBS IAW EA 400-49EA-11524.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 41,765 hrs · 26,672 cycles

LEFT WING, NR 2 SLAT INBD T/E IS DELAMINATED. ACFT GROUNDED. REPAIRED NR 2 SLAT INBD T/E IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: SKIN — CRACKED (LT WING) · airframe 41,765 hrs · 26,672 cycles

LEFT WING FIXED L/E IS CRACKED AT NR 2 SLAT ACTUATOR CUTOUT. ACFT GROUNDED. REMOVED ACTUATOR CURTAIN, REPAIRED CRACK IAW SRM 57-41-01-2R-7 AND REINSTALLED ACTUATOR CURTAIN ALSO SRM 57-41-01-2R-7.

Part: SKIN — CRACKED (LT WING) · airframe 41,765 hrs · 26,672 cycles

LEFT WING FIXED L/E CRACKED AT NR 3 SLAT ACTUATOR CUTOUT. ACFT GROUNDED. REPAIRED NR 3 SLAT ACTUATOR CUTOUT IAW SRM 51-70-14-06-0 AND 57-41-01-2R-7, FIG 201.

Part: FLOORBEAM — CRACKED (BS 639) · airframe 41,765 hrs · 26,672 cycles

MAIN CARGO DECK FLOOR SUPPORT STRUCTURE RT BS 639, STUB BEAM INNER CHORD EVIDENCE OF BEING CRACKED AT LWR ATTACHMENT REPAIRED RT STUB BEAM INNER CHORD BS 639 IAW DWG A-5310025284.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 40,520 hrs · 25,657 cycles

L1 DOOR HARD TO CLOSE. ADJUSTED L-1 DOOR GUIDE ARM REF AMM 52-11-21. ACCOMPLISHED FWD ENTRY DOOR TEST REF AMM 52-11-00. OPS CK GOOD.

Part: DOOR — LACK OF LUBE (L1) · airframe 40,126 hrs · 25,341 cycles

L1 DOOR HARD TO CLOSE. RETORQUED UPPER SNUBBER DOOR ATTACH BRACKET. CLEANED AND LUBED L1 DOOR LATCH CRANK, GUIDE PLATES, GUIDE ARM ROLLER PIN, COUNTER BALANCE BEARING, SNUBBER ABD GUIDE PIN, AND LOWER HINGE REF AM 12-25-21. OPS NORMAL.

Part: FRAME SPLICE — DAMAGED (BS 328) · airframe 38,726 hrs · 24,252 cycles

FRAME SPLICE AT BS 328, STR 1 HAS ONLY 3 FASTENERS ENGAGED, THE 4TH HAS BEEN TRIMMED AROUND. REPAIRED IAW EA 400-53EA-08424.

Part: MODULE — FAILED (MLG WW) · airframe 35,956 hrs · 22,051 cycles

RIGHT MAIN LANDING GEAR SLOW TO EXTEND. RIGHT GEAR RED REMAINED RED FOR 30 SECONDS AFTER OTHER GEAR SHOWED GREEN. DURING GO AROUND A "KLUNK" WAS HEARD AND FELT THEN INDICATED DOWN. GEAR WAS DOWN DURING RETURN TO AIRPORT. HYDRAULIC PRESSURE WAS NORMAL. SELECTOR VALVE REPLACED REF MIG 2A 6754750. REPLACED RT MLG MODULAR PACKAGE IAW AMM 32 32 00 501. REPLACED RIGHT MLG UPLOCK ACTUATOR IAW AMM 32 32 41. BOTH MLG OPERATED SIMULTANEOUSLY UP AND DOWN WITH NO DELAY OR UNUSUAL NOISE.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 35,855 hrs · 21,974 cycles

LT HORIZONTAL STABILIZER LEADING EDGE UPPER SKIN CHAFED AND PUNCTURED AT L/E STA 133.15. REMOVED DAMAGED LEADING EDGE REPAIRED IAW B737 400 SRM 55 10 01 REPAIR 12 FIG 202 AND INSTALLED IAW B737 400 AMM 20 50 11 912 202.

Part: SKIN — DENTED (FOREFLAP) · airframe 35,855 hrs · 21,974 cycles

RIGHT WING I/B FORE FLAP LOWER SURFACE HAS DENT WITH CREASE 21 INCHES FROM I/B EDGE AND 3.25 INCHES FROM TRAILING EDGE. REPAIRED DAMAGE AREA OF THE RIGHT WING I/B FORE FLAP LOWER SURFACE IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,855 hrs · 21,974 cycles

FOUND HOLE IN EXISTING FRAME LOWER FLANGE FORWARD CARGO BAY STA 500G FRAME CORRODED BETWEEN STR 27L- 26L. REMOVED OLD REPAIR, FABRICATED NEW REPAIR AND INSTALLED IAW B737 400 SRM 51 40 02 AND SRM 53 00 07 FIG 201.

Part: BAFFLE — CRACKED (CARGO BAY) · airframe 35,855 hrs · 21,974 cycles

FORWARD CARGO COMPARTMENT BAFFLE CRACKED BETWEEN BS 400 AND 420 STR 26L. REMOVED AND REPLACED DAMAGED BAFFLE IAW B737 400 SRM 51 40 02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,855 hrs · 21,974 cycles

FORWARD CARGO BAY STA 500G FRAME CORRODED BETWEEN STR 26R AND 27R. REPAIRED THE 500G FRAME IAW B737 400 SRM 53 00 07 FIG 201. REPAIR IS CATEGORY "B" REPAIR AND REQUIRES INSPECTION AT 66000 TOTAL FLIGHT CYCLES.

Part: INTERCOSTAL — BROKEN (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

INTERCOSTAL AT BS 460 TO BS 480 STR 26L BROKEN. REMOVED INTERCOSTAL FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,855 hrs · 21,974 cycles

WHILE CLEANING FORWARD SIDE OF AFT PRESSURE BULKHEAD FOR THE RESTORATION CARD FOUND CORROSION AROUND THE RIVETS JUST TO THE LEFT OF BL 0. REMOVED CORROSION, CUTOUT LOWER SKIN FOR WEB ACCESS REMOVED STRINGER END FITTING. FABRICATED SKIN DOUBLER AND WEB DOUBLER INSTALLED REPAIR PARTS AND STRINGER END FITTINGS IAW ASA EA 400 53EA 05300.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

CORROSION ON BL 0 STIFFENER AT BS 1016 (AFT PRESSURE BULKHEAD). REMOVED CORRODED STIFFENER AND INSTALLED REPAIR PARTS IAW ASA EA 400 53EA 5300.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

MAIN CABIN FLOORBOARD SUPPORT IS CORRODED AT LBL 65 BS 797. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 51 70 12.

Part: ATTACH ANGLE — CRACKED (BS 727A) · airframe 35,855 hrs · 21,974 cycles

AFT CARGO COMPARTMENT LEFT BS 727A FRAME TO INTERCOSTAL ATTACH ANGLE IS CRACKED BETWEEN STR 25L AND 26L. REMOVED ANGLE FABRICATED REPLACEMENT PART AND INSTALLED IAW SRM 51-40-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,855 hrs · 21,974 cycles

LEFT CUSP WEB AT BS 767 TO BS 787 CORRODED. REMOVED CUSP WEB FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 30 01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,855 hrs · 21,974 cycles

LEFT CUSP WEB AT BS 867 TO BS 887 CORRODED. REMOVED CUSP WEB FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02 AND 51 30 01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,855 hrs · 21,974 cycles

MAIN CABIN FLOORBOARD SUPPORT IS CORRODED AT BS 847 LBL 28. REMOVED DAMAGED BEAM STRAP AND INSTALLED REPLACEMENT PART IAW B737 SRM 51 40 02.

Part: TRANS PANEL — GOUGED (CARGO BAY) · airframe 35,855 hrs · 21,974 cycles

FORWARD CARGO BAY LEFT FORWARD TRANSITION PANEL BS 420 HAS 3 GOUGES FABRICATED REPLACEMENT TRANSITION PANEL AND INSTALLED IAW B737 400 SRM 51 40 05 AND 51 40 02.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

AFT CARGO COMPARTMENT CENTER FLOOR SUPPORT HAS 2 EA DRILLED HOLES AT RADIUS BS 727E BETWEEN STR 27L AND 27R. REMOVED DAMAGE FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 53 00 53.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 35,855 hrs · 21,974 cycles

AFT CARGO COMPARTMENT CENTER FLOOR LEFT CARGO TRACK IS CORRODED AT BS 787 ABOVE STR 26L. REMOVED AND REPLACED TRACK SECTION IAW B737 400 SRM 51 40 02.

Part: TRANS PANEL — CORRODED (CARGO BAY) · airframe 35,855 hrs · 21,974 cycles

FORWARD PIT RIGHT AFT TRANSITION PANEL CORRODED BS 500D 500G. REMOVED TRANSITION PANEL FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,855 hrs · 21,974 cycles

MAIN CABIN FLOORBOARD SUPPORT IS CORRODED AT BS 867 LBL 22. REMOVED DAMAGED BEAM STRAP AND INSTALLED REPLACEMENT PART IAW B737 SRM 51 40 02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

AFT PIT RIGHT TRANSITION PANEL ATTACH ANGLE CRACKED BS 947. REMOVED CRACKED ANGLE, FABRICATED REPLACEMENT PART AND INSTALLED IAW BOEING DWG 69 33359.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

AFT CARGO COMPARTMENT CENTER FLOOR SUPPORT HAS CORROSION AROUND FASTENER HOLES AT BS 860 BETWEEN STR 25L AND 25R BLENDED AREA FOUND TO BE OUT OF LIMITS IAW B737 400 SRM 53 60 53 FIG 101. FABRICATED REPLACEMENT PART AND INSTALLED IAW BOEING DWG 65 45269.

Part: CUSP WEB — CORRODED (BS 807-827) · corrosion level 2 · airframe 35,855 hrs · 21,974 cycles

MAIN CABIN CUSP WEB IS CORRODED AT BS 807 TO BS 827. REMOVED WEB FABRICATED REPLACEMENT PART AND INSTALLED IAW SRM 51-30-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,855 hrs · 21,974 cycles

LEFT CUSP WEB BS 847 TO BS 867 CORRODED. REMOVED CORRODED WEB AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.

Part: CUSP WEB — CORRODED (BS 638) · corrosion level 2 · airframe 35,855 hrs · 21,974 cycles

LEFT CUSP WEB CORRODED AROUND RIVETS AT BS 638. REMOVED CORRODED WEB, FABRICATED REPLACEMENT PART AND INSTALLED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

FORWARD PIT FLOOR SUPPORT (TIE DOWN) CORRODED BS 500G ABOVE STRINGER 27R. REMOVED CORRODED SUPPORT AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 53 00 53 REPAIR 2.

Part: FITTING — GOUGED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

FORWARD CARGO BAY FRAME CLIP GOUGED FORWARD SIDE BS 440 BETWEEN STR 22L AND 23L. REMOVED AND REPLACED FRAME CLIP IAW B737 400 SRM 53 00 07.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,855 hrs · 21,974 cycles

MAIN CABIN FLOORBOARD SUPPORT IS CORRODED AT BS 827 RBL 19. REMOVED DAMAGED FLOORBEAM STRAP AND INSTALLED REPLACEMENT PART IAW B737 SRM 51 40 02.

Part: ATTACH ANGLE — CRACKED (BS 727A) · airframe 35,855 hrs · 21,974 cycles

AFT CARGO COMPARTMENT RIGHT BS 727A FRAME TO INTERCOSTAL ATTACH ANGLE IS CRACKED BETWEEN STR 25R AND 26R. REMOVED ANGLE FABRICATED REPLACEMENT PART AND INSTALLED IAW SRM 51-40-02.

Part: TRANS PANEL — CORRODED (CARGO BAY) · airframe 35,855 hrs · 21,974 cycles

FORWARD CARGO BAY LEFT AFT TRANSITION PANEL BETWEEN BS 500B AND 500G IS CORRODED IN MULTIPE AREAS. FABRICATED REPLACEMENT TRANSITION PANEL AND INSTALLED IAW B737 400 SRM 51 40 05 AND 51 40 02.

Part: PANEL — CORRODED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

AFT PIT LEFT TRANSITION PANEL CORRODED BS 727D TO BS 767. REMOVED CORRODED TRANSITION PANEL AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

RIGHT LATERAL FLOOR TRACK BS 559 CORRODED. REMOVED TRACK AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,855 hrs · 21,974 cycles

RIGHT CUSP WEB AT BS 698 RBL 68 CORRODED. REMOVED CUSP WEB FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 30 01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

MAIN CABIN FLOORBOARD SUPPORT CORRODED AT BS 727F LBL 50. REMOVED CORRODED SUPPORT FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,855 hrs · 21,974 cycles

LEFT CUSP WEB AT BS 767 LBL 70 CORRODED. REMOVED CUSP WEB FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 30 01.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

MAIN CABIN CUSP WEB CORRODED BS 727D+3 RBL 70. REMOVED AND REPLACED CUSP WEB IAW B737 400 SRM 51 40 02.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

T-CAP BS 312 CORRODED BETWEEN LBL 10 AND RBL 10. REMOVED CORRODED SECTION FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 53 10 51 REPAIR 5.

Part: FRAME — GOUGED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

TOP OF FRAME GOUGED AND RIVET PULLED THROUGH AT BS 480 STR 5R. REPAIRED FRAME IAW ASA EA 400 53EA O5312 REV NEW DATED 25 APR 2011.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

FRAME CRACKED AT BS 400 BETWEEN STR 8R AND 9R. REPAIRED FRAME IAW ASA EA AD20062609 400 53 119 REV 04/15/11.

Part: FRAME — GOUGED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

TOP OF FRAME GOUGED STA 420 AT STR 16R. REPAIRED FRAME AT STA 420 STR 16R IAW ASA EA 400 53EA 05277 ISSUED APRIL 19TH 2011.

Part: FRAME — GOUGED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

FORWARD SIDE OF FRAME AT BS 344 GOUGED JUST ABOVE STR 10R. REPAIRED FRAME IAW ASA EA 400 53EA 05315 REV NEW DATED.

Part: FRAME — GOUGED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

FORWARD SIDE OF FRAME AT BS 344 GOUGED JUST ABOVE STR 10R. CUT OUT DAMAGED SECTION FABRICATED REPAIR PARTS AND INSTALLED IAW ASA EA 400 53EA 05315.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 35,855 hrs · 21,974 cycles

RIGHT WING LEADING EDGE NR 6 SLAT UPPER SURFACE INBOARD END DELAMINATED. REPAIRED SLAT UPPER SURFACE INBOARD END IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: PANEL — CORRODED (THRUST REVERSER) · airframe 35,855 hrs · 21,974 cycles

NR 2 ENGINE RIGHT THRUST REVERSER UPPER AFT BIFURCATION PANEL CORRODED. REPAIRED PANEL IAW ASA EA 400 78EA 04303.

Part: SKIN — CHAFED (LE SLAT) · airframe 35,855 hrs · 21,974 cycles

RIGHT WING LEADING EDGE NR 4 SLAT LOWER SURFACE INBOARD AFT CORNER REPAIR DOUBLER CHAFED. REPAIRED SLAT LOWER SURFACE INBOARD AFT CORNER IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

SEAT TRACK AT BS 727G BL 0 CRACKED. REMOVED SEAT TRACK, FABRICATED REPLACEMENT PART AND INSTALLED IAW PEMCO DWG 0340 53 0010.

Part: SLAT — DELAMINATED (NR 1) · airframe 35,855 hrs · 21,974 cycles

NR 1 SLAT OUTBOARD AFT CORNER DELAMINATED. REMOVED DAMAGED SECTION FABRICATED REPAIR PARTS AND BONDED IN IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — CHAFED (LE SLAT) · airframe 35,855 hrs · 21,974 cycles

NR 3 SLAT LOWER SURFACE CHAFED INBOARD AFT CORNER. REMOVED DAMAGED SKIN SECTION FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (FOREFLAP) · airframe 35,855 hrs · 21,974 cycles

RIGHT INBOARD FORE FLAP LOWER SURFACE HAS SEVERAL DENTS CLUSTERED 49 INCHES FROM INBOARD END 9 INCHES FROM TRAILING EDGE. REMOVED DAMAGED AREA AND PREVIOUS REPAIR. FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (FOREFLAP) · airframe 35,855 hrs · 21,974 cycles

RIGHT INBOARD FORE FLAP LOWER SURFACE DENTED 42 INCHES FROM INBOARD END 5 IN FROM TRAILING EDGE. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — CHAFED (TE FLAP) · airframe 35,855 hrs · 21,974 cycles

LEFT INBOARD FORE FLAP UPPER SURFACE CHAFED 30 INCHES FROM OUTBOARD EDGE. REMOVED DAMAGED SKIN FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — GOUGED (FOREFLAP) · airframe 35,855 hrs · 21,974 cycles

RIGHT INBOARD FORE FLAP UPPER SURFACE GOUGED 51 INCHES FROM INBOARD END 10 INCHES FROM LEADING EDGE. REMOVED DAMAGED SECTION FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — CHAFED (FOREFLAP) · airframe 35,855 hrs · 21,974 cycles

RIGHT INBOARD FORE FLAP UPPER SURFACE DOUBLER CHAFED. REMOVED DAMAGED DOUBLER FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — CHAFED (TE FLAP) · airframe 35,855 hrs · 21,974 cycles

LEFT INBOARD FORE FLAP UPPER SURFACE CHAFED ON EXISTING REPAIR 44 INCHES FROM INBOARD END. REMOVED DAMAGED SKIN FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — CHAFED (FOREFLAP) · airframe 35,855 hrs · 21,974 cycles

RIGHT INBOARD FORE FLAP OUTBOARD UPPER SURFACE CHAFED. REMOVED DAMAGED SKIN FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: STRIP — CORRODED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

AFT PIT NR 2 LEFT CAP STRIP CORRODED. REMOVED CORRODED CAP STRIP FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 05.

Part: STRIP — CORRODED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

AFT PIT RIGHT CAP STRIP CORRODED BS 727 TO BS 727D. REMOVED CORRODED CAP STRIP FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 05.

Part: STRIP — CORRODED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

AFT PIT NR 1 LEFT CAP STRIP CORRODED. REMOVED CORRODED CAP STRIP FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 05.

Part: STRIP — CORRODED (FUSELAGE) · airframe 35,855 hrs · 21,974 cycles

AFT PIT RIGHT NR 2 CAP STRIP CORRODED LOWER SIDE. REMOVED CORRODED SECTION FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 05.

Part: SEAT TRACK — NICKED (FUSELAGE) · airframe 19,699 hrs · 8,190 cycles

LATERAL SEAT TRACK HAS NICKS. REMOVED AND REPLACED SEAT TRACK.

Part: SEAT TRACK — NICKED (FUSELAGE) · airframe 19,699 hrs · 8,190 cycles

LATERAL SEAT TRACK HAS NICKS AND CHAFE MARKS. REMOVED AND REPLACED SEAT TRACK.

Part: FLAP TRACK — CHAFED (TE FLAP) · airframe 19,699 hrs · 8,190 cycles

LEFT O/B FLAP AFT FLAP TRACK FROM O/B END AREA OF MID FLAP SKIN CHAFED. REPAIRED BY INSTALLING DOUBLERS.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 19,699 hrs · 8,190 cycles

NR 5 SLAT UPPER SURFACE I/B AFT CORNER DELAMINATED. REPAIRED BY INSTALLING FILLER AND DOUBLER.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 19,699 hrs · 8,190 cycles

LEFT WING NR 3 SLAT O/B EDGE OF WEDGE DELAMINATED. INSTALLED FILLER AND DOUBLER.

Part: SKIN — DENTED (FUSELAGE) · airframe 19,699 hrs · 8,190 cycles

DENT UNDER L AT DOOR FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER AND TRIPLER.

Part: SKIN — DENTED (SPOILER) · airframe 19,699 hrs · 8,190 cycles

RIGHT WING NR 5 SPOILER LOWER SKIN HAS A CLUSTER OF DENTS WITHIN 2 INCHES T/E CRITICAL AREA. BONDED DOUBLER AND FILLER.

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 19,699 hrs · 8,190 cycles

CABIN FLOORBEAM IS CHAFED ON UPPER CHORD STRAP. REMOVED AND REPLACED STRAP.

Part: SKIN — DENTED (FUSELAGE) · airframe 19,699 hrs · 8,190 cycles

DENT ON FUSELAGE AT STA 949 1 INCH ABOVE STR 4 LT LESS THAN 3FT FROM LAP. REPAIRED SKIN.

Part: SKIN — DENTED (SPOILER) · airframe 32,895 hrs · 19,699 cycles

RIGHT WING NR 9 SPOILER UPPER SURFACE HAS 2EA PROTRUSIONS ABOVE SEAL MOUNT PLATE 1 I/B 1 CENTER. INSTALLED .016 2024 T3 DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: RIB — CRACKED (RT WING) · airframe 19,699 hrs · 8,190 cycles

RIGHT WING RIB CHORD AT STA 135 AFT OF STRINGER 2 IS CRACKED. REPAIRED LOWER CHORD.

Part: RIB — CRACKED (LT WING) · airframe 19,699 hrs · 8,190 cycles

LEFT WING RIB CHORD AT STA 135 AFT OF STRINGER 2 IS CRACKED. REPAIRED LOWER CHORD.

Part: SKIN — DENTED (SPOILER) · airframe 32,895 hrs · 19,699 cycles

RT WING NR 8 SPOILER UPPER SURFACE HAS PROTRUSION ABOVE SEAL MOUNT PLATE. INSTALLED .016 2024 T3 DOUBLER IAW B737 400 51 70 10 REPAIR 4.

Part: SKIN — DENTED (TE FLAP) · airframe 32,895 hrs · 19,699 cycles

RIGHT WING I/B AFT FLAP LEADING EDGE HAS A SHARP DENT 29 INCHES FROM I/B END .5 X .073 A/Y=6.8. SPLICED IN NEW SKIN SECTION .032 2024 T3 IAW B737 400 SRM 57 53 01 FIG 201.

Part: SKIN — DENTED (TE FLAP) · airframe 32,895 hrs · 19,699 cycles

DENT RIGHT T/E FLAP 15.5 INCHES FROM I/B EDGE LOWER SURFACE. INSTALLED .016 2024 T6 FILLER & DOUBLER IAW B737 400 SRM 51 70 10.

Part: FLAP — DENTED (LT WING) · airframe 32,895 hrs · 19,699 cycles

SMALL DENTS ON LOWER SURFACE OF LEFT I/B AFT FLAP. REPAIRED DAMAGED AREAS OF LEFT I/B AFT FLAP IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (SPOILER) · airframe 32,894 hrs · 19,699 cycles

LEFT I/B GROUND SPOILER CLUSTER OF DENTS I/B LOWER SURFACE. INSTALLED FILLER AND DOUBLER.

Part: SKIN — DENTED (TE FLAP) · airframe 32,894 hrs · 19,699 cycles

RIGHT O/B FLAP HAS A DENT ON UNDERSIDE CENTER OF PANEL APPROX I/B END. INSTALLED DOUBLER.

Part: SKIN — DENTED (TE FLAP) · airframe 32,894 hrs · 19,699 cycles

DENT ON LEFT O/B AFT FLAP LOWER SURFACE I/B OF NUMBER 1 FAIRING. REPAIRED LEFT O/B AFT FLAP LOWER SURFACE.

Part: SKIN — DENTED (TE FLAP) · airframe 32,894 hrs · 19,699 cycles

RIGHT I/B FOREFLAP LOWER SURFACE DENTED NEAR CENTER. INSTALLED FILLER AND DOUBLER.

Part: SKIN — DENTED (FOREFLAP) · airframe 32,894 hrs · 19,699 cycles

RIGHT WING I/B FOREFLAP LOWER SKIN HAS A DENT CLUSTER WITH OVERLAPPING DAMAGE WBL 80 TO WBL 95. INSTALLED FILLER AND DOUBLER.

Part: SKIN — DENTED (CARGO DOOR) · airframe 32,894 hrs · 19,699 cycles

DENT ON AFT CARGO DOOR SKIN 22 INCHES FROM TOP 37 INCHES FROM FWD EDGE OUT OF LIMITS. INSTALLED DOUBLER.

Part: SKIN — DAMAGED (SPOILER) · airframe 32,894 hrs · 19,699 cycles

NUMBER 2 SPOILER LOWER SURFACE DENTED AND GOUGED. INSTALLED FILLER AND DOUBLER.

Part: SKIN — DENTED (SPOILER) · airframe 32,894 hrs · 19,699 cycles

LEFT I/B GROUND SPOILER CLUSTER OF SMALL DENTS AFT OF I/B ACTUATOR LOWER SURFACE. INSTALLED FILLER AND DOUBLER.

Part: SKIN — DENTED (SPOILER) · airframe 32,894 hrs · 19,699 cycles

RIGHT WING INBOARD NR 5 SPOILER UPPER SKIN DENTED WITHIN CRITICAL AREA 3 INCHES FROM LEADING EDGE 19 INCHES FROM OUTBOARD END. REPAIRED DENT DAMAGE ON UPPER SURFACE OF SPOILER NR 5.

Part: SKIN — DENTED (SPOILER) · airframe 32,894 hrs · 19,699 cycles

RIGHT WING NR 5 SPOILER LWR SKIN HAS CLUSTER OF DENTS AT I/B END FROM LEADING EDGE TO TRAILING EDGE. REPAIRED DENT DAMAGE.

Part: SKIN — DENTED (TE FLAP) · airframe 32,894 hrs · 19,699 cycles

LEFT I/B MID FLAP T/E WEDGE HAS CLUSTER OF SMALL DENTS ON LOWER SURFACE. REPAIRED LEFT I/B MID FLAP T/E WEDGE.

Part: SKIN — CHAFED (MIDFLAP) · airframe 32,894 hrs · 19,699 cycles

LEFT I/B MID FLAP T/E WEDGE AFT END CHAFED LOWER SURFACE. REPAIRED CHAFED DAMAGE.

Part: SKIN — DAMAGED (SPOILER) · airframe 32,894 hrs · 19,699 cycles

RIGHT WING INBOARD NR 5 SPOILER UPPER SKIN HAS A PROTRUSION 14 INCHES FROM LEADING EDGE. REPAIRED UPPER SKIN PROTRUSION ON 35 SPOILER.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 32,894 hrs · 19,699 cycles

NR 5 SLAT UPPER SURFACE O/B CORNER DELAMINATED. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER.

Part: SKIN — CHAFED (LE SLAT) · airframe 32,894 hrs · 19,699 cycles

NR 4 SLAT LOWER SURFACE I/B AFT EDGE IS CHAFED. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER.

Part: SKIN — CHAFED (LE SLAT) · airframe 32,894 hrs · 19,699 cycles

NUMBER 4 SLAT LOWER SURFACE I/B AFT EDGE IS CHAFED. REMOVED DAMAGED ARE, FABRICATED REPAIR DOUBLER AND FILLER AND BONDED.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,895 hrs · 19,699 cycles

AT 727D+10 JUST BELOW STR 24R SKIN HAS 2 SMALL DENTS. FWD DENT MEASURES .012 DEEP X .500 WIDE A/Y=41. AFT DENT MEASURES .012 DEEP X .250 WIDE, ALSO 7 INCHES FROM EMERGENCY LIGHT CUTOUT = OUT OF LIMITS REPAIRED FUSELAGE SKIN IAW EA 400 53EA 02808 REV NEW ISSUED 28JAN10.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 19,699 hrs · 8,190 cycles

LEFT WING NR 2 SLAT OUTBOARD EDGE OF WEDGE DELAMINATED. REPAIRED THE DAMAGED AREA.

Part: RUB STRIP — CHAFED (NACELLE) · airframe 30,438 hrs · 17,819 cycles

RUBSTRIP MISSING AND STRUCTURE CHAFED AT PANEL 5729 IB AFT LATCH AREA. ACCOMPLISHED RUBSTRIP REPLACEMENT PER ER09 1229.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 30,438 hrs · 17,819 cycles

MISDRILLED HOLE IN FRAME IB FLANGE. REPAIRED MISDRILLED HOLE IN FRAME PER EA 400 53EA 00528.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 30,438 hrs · 17,819 cycles

MISDRILLED HOLE IN FRAME IB FLANGE. REPAIRED MISDRILLED HOLE IN FRAME PER EA 400 53EA 00528.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 30,438 hrs · 17,819 cycles

MISDRILLED HOLE IN FRAME IB FLANGE. REPAIRED MISDRILLED HOLE IN FRAME PER EA 400 53EA 00528.

Part: FLAP TRACK — CORRODED (MIDFLAP) · corrosion level 2 · airframe 30,438 hrs · 17,819 cycles

FOUND LT IB MIDFLAP CENTER FORE FLAP TRACK CORRODED. R&R LT IB MIDFLAP CENTER FORE FLAP TRACK.

Part: SKIN — CHAFED (FUSELAGE) · airframe 30,438 hrs · 17,819 cycles

SKIN CHAFED AT REAR SPAR STABILIZER SEAL. FABRICATED NEW SKIN AND REPLACED SKIN.

Part: BEAM — CRACKED (HORIZ STAB) · airframe 30,438 hrs · 17,819 cycles

LT HORIZONTAL STABILIZER LOWER TE BEAM CRACKED AT IB FWD. REMOVED DAMAGE.

Part: SKIN — DAMAGED (TE FLAP) · airframe 30,438 hrs · 17,819 cycles

RT OB MID FLAP SKIN DAMAGED AT IB END AT EXHAUST GATE CONTROL ROD CUTOUT AREA. REPAIRED RT OB MID FLAP.

Part: FRAME — DAMAGED (BS 847) · airframe 30,438 hrs · 17,819 cycles

OVERSIZED HOLES IN UPPER FRAME BS 847 STR 13R-18R. REMOVED AND REPLACED FRAME PER SRM 51-40-02.

Part: FAILSAFE — DAMAGED (FUSELAGE) · airframe 36,352 hrs · 18,419 cycles

OVERSIZED HOLES IN FAILSAFE CHORD BS 847 FROM STR 13R 18R. R&R FAILSAFE CHORD BS 847 FROM STR 13R 18R.

Part: ANGLE — GOUGED (BS 178) · airframe 30,438 hrs · 17,819 cycles

TEE ANGLE SUPPORT GOUGED. R&R T ANGLE SUPPORT.

Part: BULKHEAD — DAMAGED (BS 178) · airframe 30,438 hrs · 17,819 cycles

TOOLING DAMAGE ON BULKHEAD RT WEB. RECEIVED NEW RT WEB DRILLED AND INSTALLED ON TASK CARD.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 30,438 hrs · 17,819 cycles

DAMAGE 178 BULKHEAD LT WEB. RECEIVED NEW WEB DRILLED AND INSTALLED.

Part: WEB — CRACKED (FUSELAGE) · airframe 36,352 hrs · 18,419 cycles

WEB CRACKED AT AFT FASTENER HOLE BS 182 WL 207 RBL 17.1. REPAIRED WEB BS 182 WL 207 RBL 17.1 PER SRM 51 70 13 FIG 1.

Part: SEAL DEPRESSOR — CRACKED (FUSELAGE) · airframe 36,352 hrs · 18,419 cycles

MAIN CARGO DOOR DEPRESSOR ON FRAME CUTOUT UPPER EDGE IS CRACKED. REMOVED DEPRESSOR FABRICATED NEW AND INSTALLED FABRICATED PER PEMCO DWG 007 04402.

Part: SEAL DEPRESSOR — CRACKED (FUSELAGE) · airframe 30,438 hrs · 17,819 cycles

MAIN CARGO DOOR DEPRESSOR ON FRAME CUTOUT UPPER EDGE IS CRACKED. REMOVED DEPRESSOR FABRICATED NEW AND INSTALLED PER PEMCO DRAWING.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,438 hrs · 17,819 cycles

ANGLE SUPPORT CLIP BS 847 RBL 21-30 WL 155 CORRODED. REMOVED FABRICATED NEW SUPPORT AND INSTALLED NEW.

Part: WEB — CRACKED (FUSELAGE) · airframe 30,438 hrs · 17,819 cycles

WEB CRACKED AT AFT FASTENER HOLE BS 182 WL 207 RBL 17 REPAIRED WEB BS 182 WL 207 RBL 17 SRM 51 70 13.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,438 hrs · 17,819 cycles

SUPPORT BRACKET BS 847 RBL 21 WL 155 CORRODED. REMOVED FABRICATED NEW SUPPORT AND INSTALLED NEW.

Part: WEB — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,438 hrs · 17,819 cycles

AFT CARGO BAY WEB CORRODED IN SEVERAL AREAS BS 847 TO BS 792 WL 157 RBL 20 TO RBL 28. REMOVED RECEIVED NEW DRILLED AND INSTALLED WEB IAW SRM 53-60-15 DWG A-5330018186.

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 30,438 hrs · 17,819 cycles

SHIELD FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BS 847 867 RBL 21 WL 155. REMOVED FLOOR TO SIDEWALL SUPPORT RECEIVED NEW SUPPORT AND INSTALLED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 30,438 hrs · 17,819 cycles

INTERCOSTAL CRACKED BS 323 LBL 46 WL 208. REPLACED INTERCOSTAL BS 323 LBL 46 WL 208.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,438 hrs · 17,819 cycles

LOWER SILL WEB IS CORRODED STA 794-847. REMOVED SILL WEB DRILLED AND INSTALLED NEW WEB PER SRM 53-60-15 AND 51-40-02.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,438 hrs · 17,819 cycles

ANGLE SUPPORT STRAP CORROSION OUT OF LIMITS. REMOVED STRAP FABRICATED AND INSTALLED PER SRM 51-40-02.

Part: SUPPORT BRACKET — CORRODED (GIRT BAR) · corrosion level 2 · airframe 30,438 hrs · 17,819 cycles

FWD ENTRY DOOR AFT GIRT BAR SUPPORT BRACKET CORRODED. R&R BRACKET.

Part: SUPPORT BRACKET — CORRODED (GIRT BAR) · corrosion level 2 · airframe 30,438 hrs · 17,819 cycles

FWD ENTRY DOOR FWD GIRT BAR SUPPORT BRACKET CORRODED. R&R BRACKET.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,438 hrs · 17,819 cycles

INTERCOSTAL CORRODED BS 847 867 RBL 25. R&R INTERCOSTAL.

Part: FRAME — CORRODED (FUSELAGE) · airframe 30,438 hrs · 17,819 cycles

CORROSION ON FRAME STA 847 STR 22R 26R. R&R FRAME SECTION BS 847 STR 17R 27R.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 36,352 hrs · 18,419 cycles

AFT CARGO FLOOR TRACK CORROSION, BS 788 847, RBL 13.8, WL 155. REPAIRED PER SRM 53-00-53 FIG 201.

Part: STRAP — CRACKED (FUSELAGE) · airframe 30,438 hrs · 17,819 cycles

E BAY TENSION STRAP CRACKED BS 312 RBL 48 WL 200. REPAIRED TENSION STRAP PER SRM.

Part: PANEL — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 36,352 hrs · 18,419 cycles

CORROSION AFT CARGO BAY DOOR CUTOUT, AFT FRAME LOWER CLOSE OUT PANEL. R&R DAMAGED AFT CARGO BAY DOOR CUTOUT AFT FRAME LOWER CLOSE OUT PANEL REVEAL STRIP.

Part: STRAP — CRACKED (E&E BAY) · airframe 36,352 hrs · 18,419 cycles

E-BAY TENSION STRAP CRACKED BS 312 RBL 48 WL 200. REPAIRED TENSION STRAP PER SRM.

Part: SKIN — GOUGED (E&E DOOR) · airframe 30,438 hrs · 17,819 cycles

E BAY DOOR INNER SKIN GOUGED FWD LT CORNER. OUT OF LIMITS.

Part: SKIN — GOUGED (E&E BAY DOOR) · airframe 36,352 hrs · 18,419 cycles

E BAY DOOR INNER SKIN GOUGED FWD LT CORNER OUT OF LIMITS. REPAIRED DOOR INNER SKIN.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 29,634 hrs · 17,205 cycles

L1 DOOR EXTREMELY DIFFICULT WILL NOT LATCH ADJUST FORWARD L1 DOOR GUIDE ARM. REF AMM 52 11 21 401, OPS CHECK NORMAL.

Part: SEAT TRACK — GOUGED (BS 420) · airframe 26,733 hrs · 15,044 cycles

CABIN RT LATERAL SEAT TRACK AT BS 420 IS GOUGED. REPLACED WITH FABRICATED REPAIR PART IAW PEMCO IPC SUPPLEMENT 53-21-01 FIG 11 & PEMCO ENGINEERING DWG 0340 53 0010 REV D & BOEING SRM 51-40-05 & 51-40-02.

Part: SEAT TRACK — GOUGED (BS 480) · airframe 26,733 hrs · 15,044 cycles

CABIN RT LATERAL SEAT TRACK AT BS 480 GOUGED. REPLACED WITH FABRICATED REPAIR PART IAW PEMCO IPC SUPPLEMENT 53-21-01 FIG 11 & PEMCO ENGINEERING DWG 0340 53 0010 REV D & BOEING SRM 51-40-05 & 51-40-02.

Part: FRAME — CRACKED (BS 616) · airframe 26,733 hrs · 15,044 cycles

RT OVERWING BODY FRAME AT BS 616 INNER CHORD IS CRACKED AT BTM FASTENER HOLE. REPAIRED IAW CASCADE ERO7243 & ALASKA EA5320 01814.

Part: SKIN — DENTED (CARGO DOOR) · airframe 26,733 hrs · 15,044 cycles

AFT CARGO DOOR EXTERNAL SKIN IS DENTED 6 INCHES AFT OF FWD EDGE. SKIN REPAIRED IAW BOEING SRM 52-30-01 PG 201 REPAIR 2.

Part: SKIN — DENTED (FORE FLAP) · airframe 26,733 hrs · 15,044 cycles

LEFT WING INBOARD FORE FLAP UPPER SURFACE HAS DENT. REPAIRED IAW BOEING SRM CHAPTER 51 70 10 REPAIR 3.

Part: SKIN — DENTED (MID FLAP) · airframe 26,733 hrs · 15,044 cycles

LEFT WING INBOARD MID FLAP TRAILING EDGE WEDGE LWR SURFACE HAS SEVERAL DENTS. WEDGE DENTS REPAIRED IAW BOEING SRM & ALASKA AIRLINES EA5750 02393 & CASCADE ERO7260.

Part: SKIN — GOUGED (VERTICAL STAB) · airframe 23,048 hrs · 12,512 cycles

LT UPPER VERTICAL STAB HAS A GOUGE 2.5 FEET LONG AT BSTA 220 LEADING EDGE. REPAIRED VERTICAL STAB PER EA 5530 01142.

Part: SKIN — DENTED (BS 870 S21-22R) · airframe 23,031 hrs · 12,506 cycles

FOUND FUSELAGE DENTED. CUT OUT DAMAGE AND INSTALLED REPAIR PER SRM 53 00 01 FIG 201.

Part: SKIN — DENTED (BS 500B S25-26L) · airframe 23,031 hrs · 12,506 cycles

DENTS BETWEEN STRINGERS 25 AND 26 LH. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW SRM 53 00 01 PAGE 232.

Part: PAN — CORRODED (BS 807-847) · corrosion level 2 · airframe 23,031 hrs · 12,506 cycles

AFT CARGO DOOR JAMB BOTTOM PAN CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED AND REPLACED WEB PER SRM 51 30 2 51 40 2 AND 53 30 53 PG 108 FIGURE 101.

Part: DOOR FRAME — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 23,031 hrs · 12,506 cycles

AFT CARGO DOOR JAMB BOTTOM PAN CORRODED. REPLACED PER SRM 51 40 02 PG 34 FIG 10.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 21,810 hrs · 11,822 cycles

L1 DOOR WAS REPORTED DIFFICULT TO CLOSE THROUGH LAST 4 INCHES OF TRAVEL. ADJUSTED GUIDE ARM. (K)

Part: GUIDE ARM — OUT OF ADJUST (R1 DOOR) · airframe 21,810 hrs · 11,822 cycles

R1 DOOR WAS REPORTED DIFFICULT TO CLOSE THROUGH LAST 4 INCHES OF TRAVEL. ADJUSTED GUIDE ARM. (K)

Part: SKIN — PUNCTURED (LT ELEVATOR)

OKC - LT ELEVATOR HAS A SMALL PUNCTURE IN THE UPPER SKIN. COMPLIED WITH A GRAPHITE WET LAY-UP REPAIR IAW SRM. (K)

Part: SKIN — DENTED (AFT CARGO DOOR)

OKC - AFT CARGO DOOR SKIN HAS A DENT WITH A CREASE 21 INCHES AFT OF THE FWD EDGE AND 38.5 INCH FROM TOP EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED A DOUBLER IAW SRM. (K)

Part: SKIN — GOUGED (E/E BAY DOOR)

OKC - E/E COMPARTMENT DOOR OUTER SKIN ON RT AFT SIDE HAS A DENT AND A GOUGE. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K)

Part: ENGINE — FAILED (NR 1 ENGINE) · airframe 19,842 hrs · 10,784 cycles

ENROUTE, AT 35,000 FT, APPROX .75 PWR, NR 1 ENG INDICATIONS BECAME ERRATIC (NO EXCESSIVE VIBRATION INDICATED ON VIB METER). F/A HEARD LOUD BANG JUST BEFORE FLT CREW HEAR A THUD. IN A FEW SECONDS, ENG OVERTEMPED (APPROX 982 DEGREES C) PERFORMED EMERGENCY SHUTDOWN AND DID NOT FIRE BOTTLES. ACCOMPLISHED SINGLE ENG LANDING. REMOVED AND REPLACED ENGINE.

Part: BATTERY — DISCHARGED (CABIN)

PHX - DURING LINE CHECK, THE EMERGENCY AISLE LIGHTS AT ROWS 18 AND 21 WERE INOPERATIVE. REPLACED EMERGENCY BATTERY ASSEMBLY. LIGHTS THEN OPERATED NORMALLY. (M)