N323AS

Part: BULB — INOPERATIVE (EXTERIOR LIGHT) · airframe 57,728 hrs · 23,362 cycles

EMERGENCY LIGHT EXTERIOR GROUND ILLUMINATION LIGHT ON LEFT AFT FUSELAGE INOP. GROUNDED - YES. RELAMPED AND TESTED PER B737-900 AMM 33-51-04-960-801 - OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,728 hrs · 23,362 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN ON #4 GALLEY ADJACENT TO L-2 DOOR IS INOP. GROUNDED - YES. RELAMPED AND TESTED PER B737-900 AMM 33-51-01-960-801 - OPS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,731 hrs · 23,363 cycles

EMERGENCY LIGHT OVERWING ESCAPE LIGHT ADJACENT TO LEFT AFT OVERWING EXIT ON AIRCRAFT EXTERIOR IS INOP. GROUNDED - YES. REFERENCE SSM 33-51-13-102 SHEET 2 - RELAMPED L6 OVERWING ESCAPE LIGHT PER MM 33-51-04-960-801 - NO HELP. REMOVED, REPLACED, AND TESTED M1670 POWER SUPPLY PER MM 33-51-06-960-806 - OPS NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 57,641 hrs · 23,328 cycles

ROW 16F EXIT SIGN MISSING. GROUNDED - YES. INSTALLED NEW LENS FOR 16F EMERGENCY EXIT SIGN (LIGHT).

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,448 hrs · 22,707 cycles

AFT LEFT EXTERIOR EMERGENCY EXIT BULB DID NOT TURN ON WHEN LIGHTS SELECTED ON. GROUNDED-YES. RELAMPED & OPERATIONS CHECKED GOOD L2 DOOR SLIDE EXT LIGHT, IAW B737-900 AMM 33-51-04-960-801.

Part: WINDOW POST — CRACKED (L1 WINDOW) · airframe 56,448 hrs · 22,707 cycles

LT NR 1 WINDOW POST IS CRACKED UPPER OUTBOARD CORNER MARKED. GROUNDED-YES. REPAIRED LT NR 1 WINDOW POST, IAW ALASKA AIRLINES TASK CARD SB737-53-1336-NG-2L. WORK ACCOMPLISHED ON ALASKA AIRLINES TASK CARD SB737-53-1336-NG-2L, 1018825 2000-0172.

Part: FLOORBEAM — CORRODED (BS 270) · corrosion level 2 · airframe 56,448 hrs · 22,707 cycles

FLIGHT DECK FLOOR PANEL 211AF LANDING IS CORRODED ALL THE WAY AROUND. GROUNDED-YES. REMOVED CORROSION ON STA 270 FLOOR PANEL 211AF LANDING AND FOUND HOLE OUT OF LIMITS, IAW 737-900 SRM 53-10-51-A. REPAIRED STA 270 LATERAL INTERCOSTAL, IAW ALASKA AIRLINES EA NO 900-53EA-22936 REV 00 9/24/2020.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 56,448 hrs · 22,707 cycles

ALL EMERGENCY LIGHTS AT R2 SERVICE DOOR INOPERABLE. GROUNDED-YES. REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD, IAW B737-900 AMM 33-51-06-960-805.

Part: FLOORBEAM — CORRODED (BS 270) · corrosion level 2 · airframe 56,448 hrs · 22,707 cycles

FLIGHT DECK FLOOR PANEL 211AF LANDING IS CORRODED ALL THE WAY AROUND. GROUNDED-YES. REMOVED CORROSION ON STA 270 FLOOR PANEL 211AF LANDING AND FOUND HOLE OUT OF LIMITS, IAW 737-900 SRM 53-10-51-A. REPAIRED STA 270 LATERAL INTERCOSTAL, IAW ALASKA AIRLINES EA NO 900-53EA-22936 REV 00 9/24/2020.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 56,448 hrs · 22,707 cycles

RT HORIZONTAL LOWER SKIN IS CRACKED STA 129, 9 INCHES FROM LEADING EDGE. GROUNDED-YES. REMOVED DAMAGED AREA OF SKIN BY TRIM OUT AND INSTALLED FILLER AND DOUBLER REPAIR, IAW B737-900 SRM 55-10-01-2R-11.

Part: RETAINER — BROKEN (EMERGENCY LIGHT) · airframe 56,077 hrs · 22,545 cycles

ON PREFLIGHT, F/A REPORTS L2 EXIT/SALIDA SIGN MISSING. GROUNDED - YES. INSPECTED AND FOUND EXIT SIGN COVER RETENTION TAB BROKEN OFF, REMOVED AND REPLACED L2 FLOOR LEVEL EMERGENCY LIGHT ASSY REF B737-900 AMM 33-51-14, OPS CHECK GOOD.

Part: SLIDING WINDOW — BINDING (R2) · airframe 56,018 hrs · 22,525 cycles

UNABLE TO CLOSE FIRST OFFICERS R2 SLIDING WINDOW. GROUNDED - YES. AT FIRST OFFICER R2 WINDOW, FOUND LOWER ROLLER BEARING LOOSE. REMOVED R2 WINDOW, TIGHTENED LOWER ROLLER BEARING, THEN RE-INSTALLED R2 WINDOW. OPERATIONAL CHECKS GOOD, HEAT CHECK OF WINDOW HEAT GOOD. REF B737-900 AMM 56-12-11-300-802, 56-12-00-000-801/-400-801, AND 56-12-11-710-803.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 53,343 hrs · 21,285 cycles

FOR TRACKING PURPOSES ONLY FOR SB737 57 1330 NG 2 RIGHT WING REAR SPAR VERTICAL PRESSURE DECK WEB-INPSECTION REPAIR AND MODIFICATION. GROUNDED - YES. C/W TRACKING FOR RT WING REAR SPAR VERTICAL PRESSURE DECK WEB INSPECTION AND MOD FOR MAJOR REPAIR FOR SB737 57 1330 NG 2.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 53,343 hrs · 21,285 cycles

RT HORIZ LOWER SKIN HAS A CRACK AT STA 138 APPROX 18 IN. FROM T/E. GROUNDED - YES. REPAIRED HORIZ STAB LOWER SKIN IAW SRM 55 10 01 2R 4 THIS REPAIR IS A CAT B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 TOTAL FLT. CYCLES AND REPEAT INSPECTION INTERVALS OF 9,000 FLT. CYCLES TOTAL AC CYCLES AT TIME OF REPAIR 21,273.NOTE: DTI REINSPECTION REQUIREMENTS ENTERED INTO FILEMAKER PRO FOR TRACKING REQUIREMENTS 74711.

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,343 hrs · 21,285 cycles

FWD CARGO RT STA 500H FWD BAFFLE CLIP CRACKED. GROUNDED - YES. REMOVED CRACKED BAFFLE CLIP IN FWD CARGO RT AT STA 500H ON FWD SIDE AND REPLACED IAW SRM 51 40 02 0G 0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,343 hrs · 21,285 cycles

FWD CARGO STA RT 500K FWD BAFFLE CLIP CRACKED. GROUNDED - YES. REMOVED FWD CARGO STA RT 500K FWD BAFFLE CLIP REPLAED WITH NEW BAFFLE CLIP IAW SRM 51 40 02 0G 0.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · airframe 53,343 hrs · 21,285 cycles

AFT PIT LT TRANSITION PANEL HAS AREAS OF CORR FROM STA 727+8 TO STA 760. GROUNDED - YES. REMOVED CORR FROM AFT PIT LT TRANSITION PANEL FROM STA 727+8 TO 760, FOUND TO BE OUT OF LIMITS IAW SRM 53 00 53 1A 2, REPAIRED AFT PIT LT TRANSITION PANEL FROM STA 727+8 TO 760 IAW SRM 53 00 53 2R 5 REPAIR 5 W 1 O .040 R .000 L 6 D .040.

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,343 hrs · 21,285 cycles

FWD CARGO LT STA 440 AFT BAFFLE CLIP CRACKED. GROUNDED - YES. REMOVED FWD CARGO LT STA 440 AFT BAFFLE CLIP AND REPLACED WITH NEW ONE IAW SRM 51 40 02 0G 0.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,343 hrs · 21,285 cycles

FWD CARGO RT TRANSITION BETWEEN STA 500 AND 500A HAS MULTIPLE AREAS OF CORR. GROUNDED - YES. REMOVED DAMAGED AREA OF RT TRANSITION PANEL BETWEEN STA 500 AND STA 500A IN FWD CARGO FOUND TO BE OUT OF LIMITS IAW SRM 53 30 53 1A 2 REMOVED AND REPLACED THE TRANSITION PANEL WITH A NEW ONE IAW SRM 51 40 02 0G 0 W 4 O .040 F .029 L 1.5 D .011.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 53,343 hrs · 21,285 cycles

LEFT WING VERTICAL PRESSURE DECK WEB NDT REVEAL CRACK AT STA 663 LBL35. GROUNDED - YES. REPAIRED LT WING VERTICAL PRESSURE DECK WEB STA 663 IAW SRM 57 10 10 2R 3 REPAIR 3 ALTERNATIVE 1, THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 56000 FLT. CYCLES AN INSPECTION INTERVAL OF 36,000 FLT. CYCLES IAW SRM 57 10 10 2R 3 REPAIR 3 ALTERNATIVE 1 NOTE: DTI REQUIREMENTS ENTERED INTO FILEMAKER PRO FOR TRACKING PURPOSES.

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,343 hrs · 21,285 cycles

FWD CARGO LT STA 400 AFT BAFFLE CLIP CRACKED. GROUNDED - YES. REMOVED CRACKED BAFFLE CLIP IN FWD CARGO LT AT STA 400 AND REPLACED WITH A NEW BAFFLE CLIP IAW SRM 51 40 02 0G 0.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · airframe 53,343 hrs · 21,285 cycles

AFT PIT RT TRANSITION PANEL HAS AREAS OF CORR FROM STA 727C+10 TO 767. GROUNDED - YES. REMOVED CORR FROM AFT PIT RT TRANSITION PANEL STA 727C+10 TO 767, FOUND TO BE OUT OF LIMITS IAW SRM 53 00 53 1A 2 REPAIRED AFT PIT RT TRANSITION PANEL STA 727C+10 TO 767 IAW SRM 53 00 53 2R 5 REPAIR 5 W 1 O .040 R 000 L 3 D .040.

Part: WEB — CORRODED (BS 807-840) · airframe 53,343 hrs · 21,285 cycles

AFT CARGO LOWER DOOR SILL WEB HAS INTERGRANULAR CORR. GROUNDED - YES. REMOVED CORR AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW B737 900 SRM 53 60 15 1A 1, REMOVED AND REPLACED SILL WEB IAW B737 900 SRM 51 40 02 0G 0 W 1.25 O .050 R .043 L 1.75 D .007.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,343 hrs · 21,285 cycles

FWD WET AREA INTERCOSTAL BETWEEN BS 312-328 LBL50 HAS A CRACK AROUND FASTENER HOLE. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51 40 02 0G 0.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,343 hrs · 21,285 cycles

AFT WET AREA BS 986 FLOORBEAM HAS AREA OF LIGHT CORR AROUND GIRT BAR ATTACH HOLE RBL 50. GROUNDED - YES. REPAIRED BS 986 FLOORBEAM AT GIRT BAR ATTACH HOLE RBL 50 IAW EA NR 900 53EA 21366.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,343 hrs · 21,285 cycles

AFT WET AREA R2 MOPSILL HAS AREAS OF CORR ON UPPER FLANGE. GROUNDED - YES. REMOVED CORR ON AFT WET AREA MOPSILL UPPER FLANGE AND FOUND TO BE OUT OF LIMITS IAW SRM 53 70 15 1A 1 REMOVED MOPSILL AND REPLACED WITH NEW PART IAW SRM 51 40 02 0G 04 AND 7 W 2.0" O .080 R .044 L 3.0" D .036.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 53,343 hrs · 21,285 cycles

LT MLG BAY VERTICAL ANGLE IS CRACKED AT STA 661.95 O/B OF PACK EXHAUST. GROUNDED - YES. REMOVED AND REPLACED ANGLE IAW SRM 51 40 02 0G 0.

Part: FUEL LINE — FAILED (NR 1 ENGINE) · airframe 53,119 hrs · 21,181 cycles

ON CLIMBOUT AT = FL215 THE AIRPLANE EXPERIENCE A MODERATE JOLT SIMILAR TO AN ENGINE STALL / SURGE. THE NR 1 N1 DROPPED FROM = 88% TO 79% W/ASSOCIATED DROP IN EGT. SOON AFTER NR 1 STABILIZED WITH NR 2 AT = 81%. IT WAS AT THIS POINT THE "IMBAL" ALERT WAS ILLUMINATED UNDER THE NR 1 MAIN TANK QTY GAUGE. BOTH ENGINE FUEL FLOWS WERE MATCHED AND THE IMB REMAINED AND CONTINUED TO WORSEN. THE ENGINE LIMIT, SURGE STALL CHECKLIST WAS DISCONTINUED AND THE ENGINE FIRE, SEV DAMAGE, SEPARATION CHECKLIST WAS COMPLETED. SUCCESSFUL UNDER MAX LANDING WEIGHT BACK AT PHX. GROUNDED - YES. UPON INSPECTION OF NR 1 ENG FOUND INBD FUEL LINE ON TOP OF HMU FAILED. REF IPC 73-11-00-02, P/N 340-138-901-0 ITEM 130. REPLACED FUEL LINE, IDLE LK CK GOOD. FUEL IMBALANCE EXCEEDANCE CONDITIONAL INSPECTION NOT REQ'D REF AMM 05-51-48-211-801, ITEM D, TABLE 101 & 102. PERFORMED GVI OF AIRCRAFT EXTERIOR, LANDING GEAR, AND ENGS. ALL CKS GD.

Part: SKIN — CRACKED (NR 8 SLAT) · airframe 53,343 hrs · 21,285 cycles

#8 SLAT LWR SURFACE @ ACT. ATTACH POINT HAS CRACK EMANATING FROM FASTNER. GROUNDED - YES. (RESOLVED ON W/O: 419922 TASKCARD: N/R-00043 ) REPAIRED #8 SLAT LOWER SURFACE AT ACTUATOR ATTACH POINT IAW 737 900 SRM 57 42 01 2R 8 REPAIR 8 RAY SEAMC NOTIFIED.

Part: CONTROL CABLE — BROKEN (STAB TRIM) · airframe 51,471 hrs · 20,403 cycles

DURING PREFLIGHT, ATTEMPTED TO ACTUATE PITCH- TRIM WHEEL VIA ELECTRIC SWITCHES, AND FOUND NO MOVEMENT. TRIED BOTH FO'S (RIGHT) AND CAPTAINS (LEFT) SWITCHES, STILL NO MOVEMENT. GROUNDED - YES. FOUND STABILIZER CONTROL CABLE BROKEN. INIT MIG-2C 40-0009409, REF L/P 11776961 FOR HORIZ STAB ACTUATOR CHANGE. REMOVED AND REPLACED THE HORIZONTAL STAB TRIM CONTROL CABLES REF B737-900 AMM 27-41-82/401, ALL ASSOCIATED OPS TESTS PASS AND TRIM SWITCHES OPERATE NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,840 hrs · 20,098 cycles

L2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: SIGN — UNSECURE (CABIN) · airframe 50,177 hrs · 19,770 cycles

EXIT SIGN IN AFT GALLEY HANGING DOWN. GROUNDED - YES. REMOVED AND REPLACED AFT GALLEY CEILING EXIT SIGN PER AMM 33-51-01. OPS TEST GOOD.

Part: SKIN — CRACKED (NR 7 SLAT) · airframe 53,343 hrs · 21,285 cycles

#7 SLAT LWR SKIN @ ACT ATTACH POINT APPEARS TO BE CRACKED. GROUNDED - YES. (RESOLVED ON W/O: 419922 TASKCARD: N/R-00001 ) REPAIRED SLAT SKIN IAW 737 900 SRM 57 42 01 2R 8 CONTACTED JIM SEAMC.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 47,140 hrs · 18,369 cycles

MAIN CABIN FLOORBEAM BS 947 LBL 24 ,UPPER FLANGE HAS CORROSION. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 51-10-51-1A-1 FIG 103. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-5.

Part: INTERCOSTAL — CORRODED (BS 947) · corrosion level 2 · airframe 47,140 hrs · 18,369 cycles

MAIN CABIN BS 947, LBL 24.75 HAS CORROSION ON INTERCOSTAL. ACFT GROUNDED. FOUND TO BE OUT OF LIMTS IAW SRM 51-10-51-1A-1. LOCATED AND DRILLED A NEW INTERCOSTAL IAW SRM 51-40-05.

Part: BATTERY PACK — FAILED (CABIN) · airframe 46,543 hrs · 18,089 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1671 FAILED TASK CARD 78233001. GROUNDED - YES. REMOVED AND REPLACED M1671 POWER SUPPLY BATTERY PACK PER AMM TASK 33-51-06.

Part: BATTERY PACK — FAILED (CABIN) · airframe 46,543 hrs · 18,089 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1670 FAILED TASK CARD 78233001. GROUNDED - YES. REPLACED PACK BATTERIES FOR M1670. OPS CHECK NORMAL, REF B737-900 AMM 33-51-06-960-805.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 46,532 hrs · 18,083 cycles

DURING CRUISE, THE NR 1 ENGINE LOW PRESSURE LIGHT CAME ON FOLLOWED BY LOSS OF SYS A. RAN QRH FOR BOTH. ACFT GROUNDED. EMERGENCY LANDING. INSPECTED SYSTEM A FOUND EDP LEAKING. REMOVED SYSTEM A EDP IAW AMM 29-11-21-000-801-001. INSPECTED CASE DRAIN FILTER. NO METAL CONTAMINATION FOUND. R & R CASE DRAIN FILTERS ELEMENT IAW AMM 29-11-41-00/400-801. INSTALLED SYSTEM A EDP IAW AMM 29-11-27, LEAK CHECKED GOOD. REMOVED AND REPLACED ACOUSTIC FOR THE A SYSTEM IAW AMM 29-11-21, LEAK CHECKED GOOD. ACCOMPLISHED NR 1 ENG START IAW AMM 71-00-00-800-808-F00. NO PROBLEMS NOTED. LEAK CHECKED A SYSTEM CASE DRAIN FILTER. OP'S CHECKED GOOD IAW AMM 29-11/400-801. REPLACED NR 1 ENG HYD PUMP IAW AMM 29-11-11-400-801-001, OPS & LEAK CHECKED GOOD.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 45,849 hrs · 17,782 cycles

EMERGENCY EXTERIOR SLIDE LIGHT AT THE R 2 DOOR WAS INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS AND TESTED IAW AMM 33-51-04-960-801. OPS NORMAL.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 45,849 hrs · 17,782 cycles

EMERGENCY LIGHT EXIT SIGN ADJACENT TO LEFT FORWARD OVERWING EXIT HAS MULTIPLE LAMPS INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS AND TESTED IAW AMM 33-51-01-960-801, OPS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,223 hrs · 17,488 cycles

WHILE PERFORMING TASK CARD 78233008, FOUND EMERGENCY AREA LIGHT AT 26ABC INOPERATIVE. ACFT GROUNDED. RELAMPED AREA LIGHT, NO HELP. REPLACED BATTERY PACK. ALL OPS NORMAL REF AMM 33-51-06.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 44,704 hrs · 17,277 cycles

L1 DOOR HARD TO CLOSE FROM THE INSIDE. ACFT GROUNDED. GUIDE ARM OUT OF ADJUSTMENT. UNABLE TO ADJUST, FROZEN ADJUSTER. REPLACED L1 DOOR GUIDE ARM ASSY IAW AMM 52-11-21. OPS CHECK GOOD.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 44,585 hrs · 17,227 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN ADJACENT TO RT AFT OVERWING EXIT HAS MULTIPLE LAMPS INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMP AND TESTED IAW AMM 33-51-01-960-801. OPS NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 43,889 hrs · 16,920 cycles

EXIT SIGN 17F MISSING. ACFT GROUNDED. REINSTALLED EXIT SIGN COVER AT ROW 17F LOWER SIDEWALL AS REQUIRED.

Part: LIGHT — FAILED (CABIN) · airframe 41,528 hrs · 15,968 cycles

WHILE PERFORMING TC 78233008, EMERGENCY LIGHTS OPS, FOUND EMERGENCY LIGHT AT OVERHEAD BIN 29 ABC BURNED OUT. ACFT GROUNDED. SEVERAL ATTEMPTS AT REPLACING LAMPS UNSUCCESSFUL. REPLACED LIGHT ASSY. OPS CK GOOD. REF AMM 33-51-03.

Part: FLOOR SUPPORT — CRACKED (BS 500J-500K) · airframe 40,910 hrs · 15,722 cycles

FWD CARGO COMPARTMENT, RT FLOOR SUPPORT BAFFLE STA 500J TO STA 500K IS CRACKED. ACFT GROUNDED. R & R RT FLOOR SUPPORT BATTLE FS 500J TO 500K IAW SRM 51-40-02 AND 51-10-02, PARA 9.

Part: INTERCOSTAL — CORRODED (BS 737-787) · corrosion level 2 · airframe 40,910 hrs · 15,722 cycles

AFT CARGO RT BAFFLE, PN 1146A7505-8, UNDER SIDE PLATE AT FS 787 IS CORRODED. ACFT GROUNDED. R & R THE AFT CARGO RT INTERCOSTAL, BAFFLE, PART NR 1146A7505-8, UNDER SIDE PLATE AT FS 787 IAW DWG NR 146A7502 AND SRM 51-40-02. .

Part: FLOOR SUPPORT — CRACKED (BS 500H-500I) · airframe 40,910 hrs · 15,722 cycles

FWD CARGO COMPARTMENT, LT FLOOR SUPPORT BAFFLE STA 500H TO STA 500I IS CRACKED. ACFT GROUNDED. REMOVED LT FLOOR SUPPORT BAFFLE IAW SRM 51-40-02. THEN INSTALLED IAW SRM 51-40-02.

Part: ANGLE — CORRODED (BS 312-344) · airframe 40,910 hrs · 15,722 cycles

L1 DOORWAY O/B ANGLE UNDER SCUFF PLATE CORROSION. ACFT GROUNDED. REMOVED DAMAGE AND FOUND TO BE WITHIN LIMITS IAW SRM 53-10-15. ALODINED AND PRIMED IAW SRM 51-20-01. RESTORED SURFACE FINISH IAW AMM 51-05-01. ORIGINAL THICKNESS 0.063", REMOVED 0.002" REMAINING 0.061" .

Part: SUPPORT ANGLE — CORRODED (BS 312-348) · airframe 40,910 hrs · 15,722 cycles

L1 DOORWAY UNDER SCUFF PLATE INBD SUPPORT ANGLE SEVERAL SPOTS CORROSION BS 312-BS 348. ACFT GROUNDED. BLENDED CORROSION AT L1 DOOR LOWER SILL INBD SUPPORT ANGLE, FOUND TO BE IN LIMITS IAW SRM 53-10-15, ALODINED & PRIMED IAW SRM 51-20-01, MARKED BLENDED AREAS IAW AMM 51-05-01. ORG MAT THICKNESS .080, REMOVED .002, .078 REMIANS BLEND OUTS (A) 3.4 X .800 (B) 3.5 X .850 (C) 1.2 X .450.

Part: SUPPORT — CORRODED (BS 727-787) · corrosion level 2 · airframe 40,910 hrs · 15,722 cycles

AFT CARGO BAY BS 787 TO 727 RT TRANSITION STRIP CORRODED. ACFT GROUNDED. R & R TRANSITION STRIP IAW DWG 143A7502.

Part: SUPPORT — CORRODED (BS 727-787) · corrosion level 2 · airframe 40,910 hrs · 15,722 cycles

AFT CARGO PIT, STA 787 TO 727 LT TRANSITION STRIP CORRODED. ACFT GROUNDED. R & R TRANSITION STRIP IAW DWG 143A7502.

Part: STRUCTURE — CORRODED (BS 767-787) · airframe 40,910 hrs · 15,722 cycles

AFT CARGO BAY BS 767 - 787 RT TRANSITION STRIP CORRODED. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MAT 0.050, REMAINING 0.047, REMOVED 0.003, FOUND IN LIMITS IAW SR, 53-00-53, TOOL T8225M, ALODINED & PRIMED IAW SRM 51-20-01, TOP COATED AREA IAW 51-21-73 PART MARKED BLENDED AREAS IAW AMM 51-05-01, DOT REMOVED.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 40,910 hrs · 15,722 cycles

MAIN CABIN STA 312-328, LBL 48 FLOORBOARD SUPPORT CRACKED. ACFT GROUNDED. R & R INTERCOSTAL IAW BAC DWG 141A5400 AMD SRM 51-40-02. DOT REMOVED.

Part: INTERCOSTAL — CRACKED (BS 277-294) · airframe 40,910 hrs · 15,722 cycles

MAIN CABIN INTERCOSTAL CRACKED STA 277-294.5 RBL 1. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02. PO 836637.3. DOT REMOVED.

Part: INTERCOSTAL — CRACKED (BS 328-344) · airframe 40,910 hrs · 15,722 cycles

MAIN CABIN STA 328-344, LBL 50 FLOORBOARD SUPPORT CRACKED. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02 AND DWG 141A5400. DOT REMOVED.

Part: SUPPORT — CORRODED (BS 500K-500L) · corrosion level 2 · airframe 40,910 hrs · 15,722 cycles

FORWARD CARGO BAY BS 500L LT AT TRANSITION STRIP CORRODED. ACFT GROUNDED. REMOVED CORROSION AT STA 500K TO 500K+ TO 500KH2 REMAINING .0.38". FOUND TO BE WITH IN LIMITS IAW SRM 53-00-53-14-2. REMOVED CORROSION AT STA 500KH3 TO 500K+19. ORIG THICKNESS .040" LOSS 0.009" REMAINING 0.03" TO 500K"19 ORIG THICKNESS 0.04"LOSS 0.009" REMAINING REMAINING 0.03" FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 REPAIRED AREA IAW SRM 53-00-53-2R-5 ALODINED AND PRIMED IAW SRM 51-20-01. PAINTED IAW SRM 51-20-01.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 40,910 hrs · 15,722 cycles

MAIN CABIN STA 312-328, RBL 35 FLOORBOARD SUPPORT CRACKED. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02. DOT REMOVED.

Part: STRINGER CLIP — CORRODED (BS 500K) · corrosion level 2 · airframe 40,910 hrs · 15,722 cycles

FORWARD CARGO PIT STA. 500K, RBL 24 INTERCOSTAL CLIP CORRODED. ACFT GROUNDED. R & R FWD CARGO STA 500K, RBL 24 INTERCOASTAL CLIP FWD SIDE IAW SRM 51-40-02. REMOVED DOT L990.

Part: FLOORBEAM — BROKEN (BS 540) · airframe 40,910 hrs · 15,722 cycles

MAIN CABIN STA 540, LBL 10 FLOORBOARD SUPPORT BROKEN. ACFT GROUNDED. R & R FLOOR SUPPORT IAW SRM 51-40-02. DOT REMOVED.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · corrosion level 2 · airframe 40,910 hrs · 15,722 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT STA 952.5, LBL 16. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51, DETAIL "C". ORIGINAL THICKNESS .075", REMAINING THICKNESS .060", REMOVED .015". R & R FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 147A5650.

Part: ANGLE — CORRODED (L1 DOORWAY) · corrosion level 2 · airframe 40,910 hrs · 15,722 cycles

L1 DOORWAY INNER CHORD ANGLE UNDER SCUFF PLATE AND FLOORBOARD SEVERAL SPOTS CORROSION BS 312-BS 348. ACFT GROUNDED. R & R INNER CHORD FROM BS 277-BS 364 AT L1 DOOR IAW DWG 141A8112 & 141A8110, NEW PN 141A811241, PO 836853. 1 DOT REMOVED.

Part: FRAME — CRACKED (BS 540 BULKHEAD) · airframe 40,910 hrs · 15,722 cycles

RIGHT LOWER BULKHEAD CHORD AT STA 540 HAS 1 EA FASTENER HOLE CRACK, BS 540-BS 540, STR 22R-STR 23R. ACFT GROUNDED. REPAIRED IAW EA 900-57EA-14971 AND REO-G18873, REV A.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · corrosion level 2 · airframe 34,275 hrs · 13,100 cycles

AFT CARGO BAY AT BS 887 FLOOR PANEL IS CORRODED. R & R FLOOR SPLICE IAW SRM 51-40-02.

Part: TRANSITION PANEL — CORRODED (BS 727-770) · airframe 34,275 hrs · 13,100 cycles

AFT PIT RT TRANSITION PANEL SIDE PLATE UPPER SURFACE HAS CORROSION FROM BS 727 TO BS 770. REMOVED AND FABRICATED NEW TRANSITION PANEL.

Part: PLATE — CORRODED (BS 727-770) · corrosion level 2 · airframe 34,275 hrs · 13,100 cycles

AFT CARGO BAY LT TRANSITION SIDEPLATE CORRODED FROM BS 727 TO 770. REPAIRED IAW SRM 53-00-53, REPAIR 5.

Part: CHANNEL — CORRODED (BS 500-500D) · corrosion level 2 · airframe 34,275 hrs · 13,100 cycles

FWD CARGO SIDE PLATE CHANNEL CORRODED BS 500 -BS 500D, RBL 21. ACFT GROUNDED. REMOVED CORROSION ON RT TRANSITION PANEL FROM 500-500A IAW SRM 51-10-02. ORIG MAT FOUND TO BE .032 IAW SRM 53-30-15, FIG 5, TABLE 4, ORIG.032. REMOVED .001 REMAIL .031, LEG 2.6 WID 2.5 FOUND TO BE WITHIN LIMITS IAW SRM 53-30-15, FIG 5, 103 DETAIL D. REMOVED CORROSION ON RT TRANSITION PANEL STA 500A-500 B7 IAW SRM 51-10-02. ORIG MAT FOUND TO BE .040 IAW BAC1496-444, ORIG .040. REMOVED .001 REMAIN .039 LEG 4.1 WIDTH 1.1. FOUND TO BE WITHIN LIMITS IAW MM 5-21-99. MARKED BLENDOUT ID IAW MM 51-05-01. REMOVED CORROSION AT RT TRANSITION PANEL STA 500 B7- 500D IAW SRM 51-10-02, ORIG MAT 040, REMOVED R017, REMAIN .023 LENGTH 4 WIDTH 2.2 FOUND TO BE OUT OF LIMITS IAW MM 51-05-01. REMOVED LENGTH 4 WIDTH 2.2 FOUND TO BE OUT OF LIMITS IAW SRM 53-0053, FIG 103, DETAIL D. TOOL T8225P. R & R RT TRANSITION PANEL FROM STA500B7-500D IAW SRM 51-40-02.

Part: FRAME — WORN (BS 727) · airframe 34,275 hrs · 13,100 cycles

DAMAGED NUTPLATE HOLES AT STA 727+2.7. R & R FRAME ASSYS.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · corrosion level 2 · airframe 34,275 hrs · 13,100 cycles

FWD CARGO FLOOR STRUCTURE HAS CORROSION AROUND FASTENER HOLE REPAIRED IAW SRM 53-00-53, REPAIR 3.

Part: CHANNEL — CORRODED (BS 500D-500I) · airframe 34,275 hrs · 13,100 cycles

FORWARD CARGO COMPARTMENT SIDE PLATE CHANNEL CORRODED BS 500D - 500I, RBL 21. REMOVED CORROSION ON RT TRANSITION PANEL FROM STA 500-500I IAW SRM 51-10-02. ORIG MAT FOUND TO BE .040 IAW BAC1496-444, ORIG 040, REMOVED .020, REMAIN .020 LEG.6, WIDTH 3. FOUND TO BE OUT OF LIMITS SRM 53-00-53, FIG 103. REMOVED TRANSITION PANEL FROM STA 500D-500I IAW SRM 51-40-02. LOCATED, DRILLED AND DEBURRED TRANSITION ZEE AND SPLICE IAW SRM 53-00-53-212-5. ALODINED AND PRIMED NEW PARTS IAW SRM 51-20-01. INSTALLED REPAIR PARTS IAW IAW SRM 53-00-53-212-5.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 34,275 hrs · 13,100 cycles

MAIN CABIN FLOOR SUPPORT CRACKED BS 312 - 328, LBL 48. R & R MAIN CABIN FLOOR SUPPORT IAW SRM 51-40-02.

Part: RELAY — FAILED (E&E BAY) · airframe 28,026 hrs · 10,839 cycles

AT CRUISE ALTITUDE 1.5 HOURS INTO FLIGHT F/A'S SMELLED HOT ELEC ODOR AT ROW 21 23 COINCIDENTAL TO F/A'S ADJUSTING WINDOW LIGHTING. REMOVED AND REPLACED R427 RELAY IAW B737 900 WDM 33 21 11 OPS CHECK NORMAL. ACCOMPLISHED SMOKE OR FUMES IN THE CABIN SOURCE UNKNOWN FAULT ISOLATION IAW B737 900 FIM TASK 21 00 00 810 806 PARA J, NO FUMES NOTED.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 22,117 hrs · 8,587 cycles

EMERGENCY AISLE LIGHTS AND EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 22,117 hrs · 8,587 cycles

EMERGENCY AISLE LIGHTS AND EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY.

Part: FAIRING — CRACKED (WING) · airframe 22,117 hrs · 8,587 cycles

FAIRING 542BB HAS CRACK IN THE FORWARD LOWER EDGE BAND. REPAIRED CRACK IN THE EDGE BAND.

Part: ANGLE — CHAFED (LT WING) · airframe 22,117 hrs · 8,587 cycles

LEFT WING FIXED T/E CHAFED LOCATED UNDER NR 6 SPOILER I/B EDGE. REPLACED CHAFED ANGLE.

Part: SCUFF PLATE — CRACKED (CARGO BAY) · airframe 22,117 hrs · 8,587 cycles

AFT CARGO BAY DOOR LOWER AFT CORNER SCUFF PLATE CRACKED. REMOVED, REPAIRED AND REPLACED AFT CARGO BAY DOOR LOWER CORNER SCUFF PLATE.

Part: SUPPORT ANGLE — CHAFED (WING) · airframe 22,117 hrs · 8,587 cycles

UPPER T/E PANEL SUPPORT ANGLE COMMON TO PROGRAM ROLLER FITTING IS CHAFED. REMOVED AND REPLACED SUPPORT ANGLE.

Part: WEDGE — CHAFED (LE SLAT) · airframe 22,117 hrs · 8,587 cycles

LEFT WING NR 4 SLAT LWR SIDE OF T/E WEDGE HAS AREAS THAT ARE CHAFED. REPAIRED PER EA.

Part: FLOOR SUPPORT — CRACKED (BS 847) · airframe 22,117 hrs · 8,587 cycles

AFT PIT FLOOR SUPPORT BRACKET CRACKED. REPLACED FLOOR SUPPORT BRACKET.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 22,117 hrs · 8,587 cycles

AFT PIT FLOOR SUPPORT BEAM HAS EVIDENCE OF A PREVIOUS BLENDOUT THAT IS KNIFE EDGED. BLEND AREA OUT OF LIMITS REMOVED AND FABRICATED FLOOR SUPPORT BEAM AND INSTALLED IN THE AFT PIT.

Part: SKIN — CHAFED (TE FLAP) · airframe 22,117 hrs · 8,587 cycles

LEFT O/B AFT FLAP UPPER SURFACE CHAFED 5 INCHES FROM T/E ON O/B END. REPAIRED PER SRM.

Part: SKIN — CHAFED (TE FLAP) · airframe 22,117 hrs · 8,587 cycles

LEFT O/B AFT FLAP LWR SURFACE CHAFED 12 INCHES FROM T/E AND 24 INCHES FROM I/B END. REPAIRED PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,117 hrs · 8,587 cycles

CRACKS IN FLOOR SUPPORT INTERCOSTAL.

Part: SKIN — CHAFED (TE FLAP) · airframe 22,117 hrs · 8,587 cycles

LEFT WING O/B AFT FLAP UPPER SURFACE I/B EDGE CHAFED 8 INCHES FROM T/E. REPAIRED PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,117 hrs · 8,587 cycles

CRACKS IN FLOOR SUPPORT INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,117 hrs · 8,587 cycles

CRACK IN FLOOR SUPPORT INTERCOSTAL AT NUT PLATE HOLE. REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,117 hrs · 8,587 cycles

CRACK IN FLOOR SUPPORT INTERCOSTAL NUT PLATE HOLE. REMOVED AND REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (BS 349-360) · airframe 22,117 hrs · 8,587 cycles

CRACKS IN FLOOR SUPPORT INTERCOSTAL AT NUT PLATE HOLE. REMOVED AND REPLACED WITH NEW INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,117 hrs · 8,587 cycles

CRACKS IN FLOOR SUPPORT INTERCOSTAL AT NUT PLATE HOLE. REPLACED INTERCOSTAL.

Part: FITTING — CRACKED (LT WING) · airframe 22,117 hrs · 8,587 cycles

LEFT WING T/E FIXED BULKHEAD AT RS 289 CRACKED AT AFT END OUT OF LIMITS. REMOVED AND REPLACED FITTING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 22,117 hrs · 8,587 cycles

CRACKED SUPPORT ANGLE. REMOVED FABRICATED AND INSTALLED SUPPORT ANGLE.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 22,117 hrs · 8,587 cycles

RIGHT WING I/B FIXED T/E SEAL BULKHEAD AT WING STA 289 HAS CRACKED SUPPORT ANGLE. REMOVED AND REPLACED SUPPORT ANGLE.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 22,117 hrs · 8,587 cycles

INTERCOSTAL CRACKED AT BS 312 TO BS 328 REMOVED AND REPLACED INTERCOSTAL.

Part: SUPPORT — CORRODED (BS 727-727C) · corrosion level 2 · airframe 22,117 hrs · 8,587 cycles

CORROSION AFT PIT RT FLOOR TO SIDEWALL SUPPORT ZEE HAS MULTIPLE SPOTS OF CORROSION. REPLACED SIDEWALL SUPPORT.

Part: SUPPORT SPLICE — CORRODED (BS 727C-727D) · corrosion level 2 · airframe 22,117 hrs · 8,587 cycles

CORROSION AFT PIT RT FLOOR TO SIDEWALL SUPPORT SPLICE. REPLACED SIDEWALL SUPPORT SPLICE.

Part: SUPPORT — CORRODED (BS 727I) · corrosion level 2 · airframe 22,117 hrs · 8,587 cycles

CORROSION ACB RIGHT FLOOR TO SIDEWALL SUPPORT SPLICE 7 TO 2. REMOVED AND REPLACED SIDEWALL SUPPORT SPLICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,117 hrs · 8,587 cycles

RT FLOOR TO SIDEWALL SUPPORT SHIELD HAS SPOTS OF CORROSION. REPLACED SUPPORT.

Part: SUPPORT — CORRODED (BS 767-787) · corrosion level 2 · airframe 22,117 hrs · 8,587 cycles

CORROSION ACB RT FLOOR TO SIDEWALL SUPPORT SHIELD INTERCOSTAL. REMOVED AND REPLACED SUPPORT SHIELD INTERCOSTAL.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,117 hrs · 8,587 cycles

CORROSION ACB LT FLOOR TO SIDEWALL SUPPORT HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED SIDEWALL SUPPORT.

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 22,117 hrs · 8,587 cycles

AFT CARGO BAY DOOR RT FLOOR TO SIDEWALL SUPPORT ZEE IS CORRODED BEYOND LIMITS. REPLACED SIDEWALL SUPPORT.

Part: SUPPORT — CORRODED (BS 761-847) · corrosion level 2 · airframe 22,117 hrs · 8,587 cycles

CORROSION ACB LT FLOOR TO SIDEWALL SUPPORT HAS SPOTS OF CORROSION. REMOVED AND REPLACED SIDEWALL SUPPORT.

Part: CHANNEL — CRACKED (CARGO BAY) · airframe 22,117 hrs · 8,587 cycles

ACB FLOOR SUPPORT CHANNEL CRACKED.

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 22,117 hrs · 8,587 cycles

CORROSION ACB RIGHT FLOOR TO SIDEWALL SUPPORT SHIELDS ANGLE. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT SHIELD ANGLE.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 22,117 hrs · 8,587 cycles

ACB FLOOR SUPPORT CHANNEL CRACKED BS 727I RBL WL 153. REPAIRED CHANNEL BEAM.

Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 22,117 hrs · 8,587 cycles

CORROSION ACB LT FLOOR TO SIDEWALL SUPPORT HAS MULTIPLE SPOTS OF CORROSION.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,117 hrs · 8,587 cycles

AFT CARGO BAY DOOR CUTOUT SUB THRESHOLD WEB IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED AFT CARGO BAY DOOR CUTOUT AND SUB THRESHOLD WEB.

Part: SKIN — DENTED (CARGO DOOR) · airframe 22,117 hrs · 8,587 cycles

AFT CARGO DOOR REQUIRES RESKIN. REMOVED AND REPLACED AFT CARGO DOOR SKIN.

Part: SKIN — CHAFED (TE FLAP) · airframe 22,117 hrs · 8,587 cycles

LEFT O/B AFT FLAP UPPER SURFACE O/B EDGE IS CHAFED BEYOND LIMITS. REPAIR ACCOMPLISHED.

Part: SUPPORT — CORRODED (BS 727I-761) · corrosion level 2 · airframe 22,117 hrs · 8,587 cycles

AFT CARGO BAY DOOR LT FLOOR TO SIDEWALL SUPPORT ZEE IS CORRODED BEYOND LIMITS. REPLACED SIDEWALL SUPPORT.

Part: SKIN — CHAFED (TE FLAP) · airframe 22,117 hrs · 8,587 cycles

LEFT O/B AFT FLAP LOWER SURFACE IS CHAFED BEYOND LIMITS. REPAIR ACCOMPLISHED.

Part: SKIN — DENTED (CARGO DOOR) · airframe 22,117 hrs · 8,587 cycles

FWD CARGO DOOR REQUIRES RESKIN. REMOVED AND REPLACED FWD CARGO DOOR SKIN.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,117 hrs · 8,587 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT ZEE CORRODED BEYOND LIMITS. REPLACED SIDEWALL SUPPORT.

Part: SUPPORT — CORRODED (BS 727-767) · corrosion level 2 · airframe 22,117 hrs · 8,587 cycles

AFT CARGO BAY DOOR RT FLOOR TO SIDEWALL SUPPORT ZEE IS CORRODED BEYOND LIMITS. REPLACED SIDEWALL SUPPORT.

Part: SKIN — CHAFED (TE FLAP) · airframe 22,117 hrs · 8,587 cycles

LEFT O/B AFT FLAP UPPER SURFACE I/B EDGE IS CHAFED BEYOND LIMITS. REPAIR ACCOMPLISHED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 19,734 hrs · 7,651 cycles

EMERGENCY LIGHTS WORKCARD 78233001 EMERGENCY LIGHTING FAILED TEST. REPLACED BATTERIES FORWARD GALLEY LT AND RT AFT GALLEY LT ROW 20 LT AND RT AND ROW 1R RT. WORKCARD 78233001 COMPLETED. CHECKED GOOD REF MM 33 51 06.

Part: ANGLE — CORRODED (BS 500F-500L) · corrosion level 2 · airframe 16,445 hrs · 6,395 cycles

FWD CARGO PIT LT FLOOR TO SIDEWALL ZEE ANGLE CORRODED STA 500 F + 10" TO 500 L LBL 23. CUT OUT DAMAGED SECTION, FABRICATED, LOCATED, DRILLED AND INSTALLED A REPLACEMENT SECTION IAW B737 900 SRM 53 00 53 FIG 201 202 REPAIR 5.

Part: ANGLE — CORRODED (BS 500H-508) · corrosion level 2 · airframe 16,445 hrs · 6,395 cycles

FWD CARGO PIT RT FLOOR TO SIDEWALL "Z" ANGLE CORRODED STA 500 H + 10" TO 506L (SIDEPLATE). CUT OUT DAMAGED AREA. FABRICATED, LOCATED, DRILLED AND INSTALLED IAW B737 900 SRM 53 00 53 PGS 204 205 REPAIR 5.

Part: FLOOR SUPPORT — CORRODED (BS 727I) · corrosion level 2 · airframe 16,445 hrs · 6,395 cycles

AFT CARGO PIT FLOOR SUPPORT CORRODED AT STA SPLICE 727 I LBL 8.1. REMOVED DAMAGED SPLICE, FABRICATED SPLICE CHANNEL IAW DRWG 146A7506 FIG 2. LOCATED DRILLED AND INSTALLED IAW B737 900 SRM 51 40 2 PG 6 ASA EA 5310 02779.

Part: FLOOR SUPPORT — CORRODED (BS 727) · corrosion level 2 · airframe 16,445 hrs · 6,395 cycles

AFT CARGO PIT FLOOR SUPPORT SPLICE CORRODED STA 727 I RBL 8.1. REMOVED DAMAGED SPLICE, FABRICATED SPLICE CHANNEL IAW DWG 146A7506 FIG 2. LOCATED DRILLED AND INSTALLED IAW B737 900 SRM 51 40 2 PG 6 ASA EA 5310 02779.

Part: FLOOR SUPPORT — CORRODED (BS 772-887) · corrosion level 2 · airframe 16,445 hrs · 6,395 cycles

AFT CARGO PIT FLOOR SUPPORT CORRODED STA 800 AREA RBL 13 CUT OUT DAMAGED SECTION OF FLOOR TRACK LOCATED. FABRICATED DRILLED AND INSTALLED A REPLACEMENT FLOOR TRACK AND SPLICE CHANNELS IAW SRM 53 00 53 VIA ASA EA 5310 02777.

Part: PANEL — CORRODED (BS 727B-727C) · corrosion level 2 · airframe 16,445 hrs · 6,395 cycles

AFT CARGO PIT RT FLOOR TO SIDEWALL TRANSITION PANEL MULTIPLE AREAS OF CORROSION FWD OF CARGO DOOR (SIDEPLATE). CUT OUT DAMAGED AREA OF SIDEPLATE LOCATED DRILLED. INSTALLED A REPLACEMENT SIDEPLATE AND SPLICE PARTS IAW B737 900 SRM 53 00 53 PG 202 FIG 202 PG 204 REPAIR 5 TABLE 201.

Part: PANEL — CORRODED (BS 727F-727I) · corrosion level 2 · airframe 16,445 hrs · 6,395 cycles

AFT CARGO PIT LT FLOOR TO SIDEWALL TRANSITION PANEL (SIDEPANEL) HAS MULTIPLE AREAS OF CORROSION STA 727G AREA. CUT OUT DAMAGED SECTION OF SIDEPANEL. LOCATED DRILLED INSTALLED A REPLACEMENT SIDEPLATE AND SPLICE PARTS IAW B737 900 SRM 53 00 53 PG 202 FIG 202 PG 204 REPAIR 5 TABLE 201.

Part: FLOOR SUPPORT — CORRODED (BS 727) · corrosion level 2 · airframe 16,445 hrs · 6,395 cycles

AFT CARGO PIT FLOOR SUPPORT SPLICE CORRODED AT STA 727 I RBL 3. REMOVED DAMAGED SPLICE, FABRICATED SPLICE CHANNEL IAW DWG 146A7506 FIG 2. LOCATED DRILLED AND INSTALLED IAW B737 900 SRM 51 40 2 PG 6 ASA EA 5310 02779.

Part: FLOOR SUPPORT — CORRODED (BS 727I) · corrosion level 2 · airframe 16,445 hrs · 6,395 cycles

AFT CARGO PIT FLOOR SUPPORT SPLICE CORRODED AT STA 727 I LBL 3. REMOVED DAMAGED SPLICE, FABRICATED SPLICE CHANNEL IAW DWG 146A7506 FIG 2. LOCATED DRILLED AND INSTALLED IAW B737 900 SRM 51 40 2 PG 6 ASA EA 5310 02779.

Part: FLOOR SUPPORT — CORRODED (BS 727I) · corrosion level 2 · airframe 16,445 hrs · 6,395 cycles

AFT CARGO PIT FLOOR SUPPORT CORRODED AT SPLICE STA 727 I LBL 12.5. REMOVED DAMAGED SPLICE, FABRICATED SPLICE CHANNEL IAW DRG 146A7506 FIG 2. LOCATED DRILLED AND INSTALLED IAW SRM 51-40-2 PG 6 AND ASA EA 5310 02779.

Part: FLOOR SUPPORT — CORRODED (BS 772-775) · corrosion level 2 · airframe 16,445 hrs · 6,395 cycles

AFT CARGO COMPT FLOOR SUPPORT CORRODED AROUND NUTPLATES AT STA 772 RBL 3. CUT OUT DAMAGED AREA OF FLOOR SUPPORT UPPER CAP ONLY. FABRICATED LOCATED DRILLED AND INSTALLED REF SRM 53-40-05 & 53-40-06 AND ASA EA 5310 02778.

Part: FLOOR SUPPORT — DAMAGED (BS 500C-500D) · airframe 16,445 hrs · 6,395 cycles

FWD CARGO BAY FLOOR SUPPORT TRACK BETWEEN STA 500C AND STA 500D RBL 5" TWO HOLES DRILLED THROUGH AT EDGE OF FLOOR SUPPORT. REMOVED DAMAGED SECTION OF FLOOR SUPPORT TRACK LOCATED DRILLED AND INSTALLED REPAIR ANGLES IAW SRM 53-00-53 PG 203 FIG 201.

Part: FLOOR SUPPORT — CORRODED (BS 727) · corrosion level 2 · airframe 16,445 hrs · 6,395 cycles

AFT CARGO PIT FLOOR SUPPORT SPLICE CORRODED AT STA 727 I RBL 13.84. REMOVED DAMAGED SPLICE. FABRICATED SPLICE CHANNEL IAW DWG 146A7506 FIG . 1 LOCATED, DRILLED AND INSTALLED IAW B737 900 SRM 51 40 02 PG 6 ASA EA 5310 02779.

Part: FLOORBEAM — CORRODED (BS 500) · corrosion level 2 · airframe 16,445 hrs · 6,395 cycles

FWD CARGO PIT AFT PANEL BULKHEAD LWR FLOORBEAM CORRODED STA 500 L RBL 24 TO LBL 24. REMOVED DAMAGED FLOORBEAM FABRICATED LOCATED DRILLED AND INSTALLED A REPLACEMENT PART IAW SRM 53-00-53 FIG 103 DWG 143A9485 & 5.0 P.M. 20 41 02 PGS 2 7.

Part: SKIN — DENTED (CARGO DOOR) · airframe 12,311 hrs · 4,655 cycles

FWD CARGO DOOR WAS FOUND TO HAVE THREE DENTS WITH GOUGES. REPAIRED IAW SRM 52-00-01 REPAIR NR 2.

Part: SKIN — GROUND DAMAGE (BS 450) · airframe 12,116 hrs · 4,568 cycles

RAMP HIT AIRCRAFT WITH BELT LOADER AT FWD CARGO DOOR AFT EDGE DAMAGED AT BS 450 AND WL 155. REPAIRED IAW SRM 53-00-01 REPAIR 25.

Part: SKIN — GROUND DAMAGE · airframe 12,116 hrs · 4,568 cycles

RAMP HIT AIRCRAFT WITH BELT LOADER AT FWD CARGO DOOR AFT EDGE DAMAGED AT BS 450 AND WL 155. REPAIRED IAW SRM 53-00-01 REPAIR 25.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 10,935 hrs · 4,041 cycles

LEFT HORIZONTAL STAB LEADING EDGE DAMAGED.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 10,935 hrs · 4,041 cycles

AFT PIT NR 4 PANEL HAS 2" CRACK AFT END OF PIT REPAIRED IAW SRM 51 40 05.

Part: SILL — CORRODED (BS 727E) · airframe 10,935 hrs · 4,041 cycles

CORROSION FOUND ON AFT CARGO RT FLOOR DUST SILL AT BS727E REPAIRED IAW SRM 51 40 05.

Part: SILL — CORRODED (BS 727E) · corrosion level 2 · airframe 10,935 hrs · 4,041 cycles

CORROSION FOUND ON AFT CARGO PIT LT FLOOR DUST SILL AT BS 727E REPARIED IAW SRM 53 00 53.

Part: SKIN — GOUGED (EMERGENCY EXIT) · airframe 10,935 hrs · 4,041 cycles

LT OVERWING EXIT DOOR SKIN GOUGED AT BS 578 REPAIRED IAW SRM 52 00 01 AND 52 20 04.

Part: SUPPORT — CHAFED (FUSLEAGE)

PAE - DURING C-CHECK, FOUND E/E CUTOUT AFT STOP FITTING CHAFED. REPAIRED IAW SRM 51-40-02. (M)