N731SA

Part: GIRT BAR — OUT OF POSITION (R2 DOOR) · airframe 75,916 hrs · 44,783 cycles

AFT SERVICE DOOR SLIDE UNSEATED ; / [01] REPOSITIONED GIRT BAR IAW SIP

Part: BRACKET — CRACKED (L/H MLG W/W) · airframe 74,252 hrs · 43,809 cycles

CRACK ACCESS DOOR 551DB BRACKET ON LT MAIN LANDING GEAR / REPLACED ACCESS DOOR 551DB BRACKET ON LT MAIN LANDING GEAR IAW B737-700 SRM 51-10-02; SRM 51-40-02

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,252 hrs · 43,809 cycles

CRACK STRINGER 24L LOCATED AT BS 540 FWD CARGO COMPARTMENT / REPAIRED STRINGER 24L LOCATED AT BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 PARAGRAPH 4 TABLE 202;203 FIG 206. MATERIAL USED 7075-T0-0-050 PO-2020 172955 1; 7075T0-0-0-056 PO-2020-205766 1. HEAT TREATED AND CONVERTED FROM T0 TO T6 IAW BAC 5602. TOOL USED TEMPERATURE CONTROLLER P/N P3015606300000 S/N U2820025 DUE DATE 25FEB21

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,252 hrs · 43,809 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BS695 AND RBL24.75 CENTER SECTION / INSTALLED NW REPAIR ANGLE LOC BS695 AND RBL 24.75 CENTER SECTION AND FASTENER IAW B737-700 SRM 51-40-02 AND DWG 111A6000 REV DATE 2-15-99 REV ITEM 4

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 74,252 hrs · 43,809 cycles

(CRACK ON LEADING EDGE RIB 95.96 LT HORIZONTAL LEADING EDGE.) _________________N / REMOVED AND REPLACED RIB 95.96 LT HORIZONTAL LEADING EDGE IAW SRM B737-700 51-40-02 AND DRAWING #186A1001 REV B

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 74,252 hrs · 43,809 cycles

(CRACK ON LEADING EDGE RIB 105.26 AT LT HORIZONTAL LEADING EDGE.) / REMOVED AND REPLACED RIB 105.26 AT LT HORIZONTAL LEADING EDGE IAW SRM B737-700 51-40-02 AND DRAWING # 186A1001 REV B

Part: BRACKET — BROKEN (FUSELAGE) · airframe 74,252 hrs · 43,809 cycles

BROKEN UPPER BRACKET SIDEWALL PANEL 232 YCW(2EA); 241 YKW(1EA); 242 YDW(1EA); 241 YEW(1EA);241YGW(1EA) AT PASSENGER CABIN (6 EA) / REPLACED UPPER BRACKET SIDEWALL PANEL 232 YCW(2EA); 241 YKW(1EA); 242 YDW(1EA); 241 YEW(1EA); 241 YGW(1EA) AT PASSENGER CABIN (6EA) IAW B737-700 SRM 51-10-02-0G-0 STEP 9

Part: GUSSET — CRACKED (FUSELAGE) · airframe 74,252 hrs · 43,809 cycles

CRACK GUSSET LOCATED AT BS 500D STRINGER 19 R FWD CARGO COMPARTMENT / REMOVED AND INSTALLED NEW GUSSET AND FASTENERS LOCATED AT BS 500D STRINGER 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG #143A7902 REV - AND SRM 51-10-02 ITEM 9

Part: PANEL — CRACKED (R/H WING) · airframe 74,252 hrs · 43,809 cycles

CRACK ACCESS PANEL 651GB TRAILING EDGE ANGLE SUPPORT RT WING (1 EA) / REPLACED ANGLE SUPPORT ON ACCESS PANEL 651GB AT RH WING (1EA) IAW B737-700 51-10-02 ITEM 9 AND SRM 51-40-02 PART NUMBER USED 115A2752-18 (SEAL RETAINER)

Part: BEAM — CRACKED (R1 DOOR) · airframe 74,252 hrs · 43,809 cycles

CRACK INDICATION ON FWD SERVICE DOOR LOC. ON BEAM #4 AND 14 INCH AFT FWD LEADING EDGE DOOR INTERNAL AREA I/B SIDE AT PASSENGER CABIN (1 EA) (LENGTH = 1.750 INCH APPROX.) / REPLACED BEAM ON FWD SERVICE FOOR LOC AT 14 INCH AFT OF FWD LEADING EDGE DOOR INTERNAL AREA I/B SIDE AT PASSENGER CABIN IAW DWG 141A6535 REV B AND WORK INSTRUCTION # 5241-C-14093-NG ITEM 2(B) AND SRM 51-40-02 PART NUMBER USED 141A6536U20 BATCH 2020001281 PO-000

Part: PRESSURE DECK — CRACKED (PASS CABIN) · airframe 74,252 hrs · 43,809 cycles

CRACK WEB HORIZONTAL PRESSURE DECK LOCATED ON STA 663 AT LEVEL LBL 30.5 AT PASSENGER. CABIN PERFORMED PERMANENT REPAIR ON WEB HORIZONTAL PRESSURE DECK LOCATED ON STA 663 AT LEVEL LBL 30 TO LBL 60 AT PASSENGER CABIN IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 FIGURE 203 MATERIAL USED IS BAC1505-100052 PO#2019607303 2024T3/0.080' PO# 2020213281 2024T3/0.063' PO#2020221732 2021T3/0.020' PO #2018567508.-

Part: PANEL — CRACKED (FWD CARGO) · airframe 74,252 hrs · 43,809 cycles

CRACK CEILING PANEL 122YCC (SHOURD PANEL) FWD CARGO COMPARTMENT /

Part: FASTENER — BROKEN (#1 ENGINE) · airframe 74,252 hrs · 43,809 cycles

BROKEN FASTENER LIP INLET COWL ON ENGINE 1 / REPLACED BORKEN FASTENER LOC ON LIP INLET COWL ON ENGINE 1 IAW B737-700 SRM 51-40-02 AND CMM 71-11-22

Part: PANEL — CRACKED (FWD CARGO) · airframe 74,252 hrs · 43,809 cycles

CRACK CEILING PANEL 121YAC (SHOURD PANEL) FWD CARGO COMPARTMENT /

Part: PANEL — CRACKED (FWD CARGO) · airframe 74,252 hrs · 43,809 cycles

CRACK CEILING PANEL 120YAC (SHOURD PANEL) FWD CARGO COMPARTMENT /

Part: SKIN — DELAMINATED (R/H WING) · airframe 74,252 hrs · 43,809 cycles

DEBONDED OB AFT FLAP SKIN I/B SIDE AT RT WING / REPAIRED AFT FLAP SKIN I/B SIDE AT RT WING ASPER B737-700 SRM 57-53-01-2R-16 REPAIR 16 TOOL USED CALIPER PN 500-197-30 SN A18229508 DUE DATE 09-AUG-21 HOT BONDER PN HCS9200B SN 16122983 DUE DATE 16-DEC-21 CALIPER PN 500-197-30 SN AE18229497 DUE DATE 27-JUL-21. THIS IS AN INTERIM REPAIR FOR INSPECTIONS REQUIREMENTS SEE TLD SN T080519

Part: CONTROL UNIT — ARCED (WINDSHEILD HEAT) · airframe 74,112 hrs · 43,724 cycles

L1 WINDOW ARCED FOR 20 SECONDS AND CRACKED OUTER PANE. REMOVED AND REPLACED LT NR 1 WINDOW AND LT FWD WINDOW HEAT CONTROL UNIT, REF AMM 56-11-11 AND 30-41-11. LEAK AND OPERATIONS CHECK GOOD FOR CAT III UPGRADE SEE LOG PAGE #1238649POS LT 1 PN OFF/ON 5-89354-319 SN OFF 18288H1888 SN ON 18319H5082 POS LT FWD PN OFF/ON 231-5 SN OFF 8006 SN ON 8081.

Part: WINDOW — ARCED (L1) · airframe 74,112 hrs · 43,724 cycles

L1 WINDOW ARCED FOR 20 SECONDS AND CRACKED OUTER PANE. REMOVED AND REPLACED LT NR 1 WINDOW AND LT FWD WINDOW HEAT CONTROL UNIT, REF AMM 56-11-11 AND 30-41-11. LEAK AND OPERATIONS CHECK GOOD FOR CAT III UPGRADE SEE LOG PAGE #1238649POS LT 1 PN OFF/ON 5-89354-319 SN OFF 18288H1888 SN ON 18319H5082 POS LT FWD PN OFF/ON 231-5 SN OFF 8006 SN ON 8081.

Part: PRESSURE BLKHD — CRACKED (BS 1016) · airframe 73,579 hrs · 43,395 cycles

AFT PRESSURE BULKHEAD WEB SKIN HAS A CRACK INDICATION RADIATING TOWARD THE CENTER OF THE APB AT THE MOST CENTERED FASTENER COMMON TO THE RADIAL STIFFENER ALIGNED WITH STRINGER 22L. FOUND DURING HFEC INSPECTION OF NDT PART 6; 53-10-64, PER TASK CARD 5311-I-11681. APB WEB CRACK HAS BEEN REPAIRED, AS PER EA 20-153-01881 REF SA-M 326 - A1131890.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 73,139 hrs · 43,109 cycles

DVI OF EGPR PER EA 20-153-01146 FOUND NO DAMAGE GEYOND THAT NOTED GVI OF AREA AROUND EGPR HAS POSSIBLE CRACK ON LOWER DOUBLER / REPAIRED LOWER DOUBLER REF SRM 53-10-15-2R-4

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 73,139 hrs · 43,109 cycles

ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER IS CRACKED ON FWD SIDE BETWEEN DOOR HINGES. TRIMED OUT DAMAFED OFTHE EGPR DOUBLER PER EA 20-153-01146 PART 1.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,787 hrs · 42,906 cycles

EMERGENCY LIGHTS ON ROW 16 & 19 DEF, REMOVED AND REPLACED BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-51-21. PN OFF AND ON D717-01-100, PN OFF 46969 AND SN ON 25797.

Part: ROPE — OUT OF POSITION (LT OVRWING EXIT) · airframe 71,456 hrs · 42,057 cycles

L/H OVERWING EMERGENCY EXIT ROPE NOT STOWED PROPERLY. / INSTALLED ROPE PER AMM.

Part: SEAL — DAMAGED (LH HOR STAB) · airframe 71,456 hrs · 42,057 cycles

LEFT HORIZONTAL STAB UPPER FWD SLIDER IS DAMAGED. / REMOVED AND REPLACED LEFT HORIZONTAL STAB UPPER FWD SLIDER REF. AMM 53-31-31. OPS CHECK GOOD.

Part: ROPE — OUT OF POSITION (RT OVRWING EXIT) · airframe 71,456 hrs · 42,057 cycles

R/H OVERWING EMERGENCY EXIT ROPE NOT STOWED PROPERLY. / INSTALLED ROPE PER AMM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 71,418 hrs · 42,032 cycles

L2 DOOR SLIDE MATERIAL LOOSE. REPOSITIONED SLIDE IN CONTAINER PER MT.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 70,374 hrs · 41,340 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. R&R SIGN PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 69,857 hrs · 41,016 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY OPS CHECK AT M1675. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 69,857 hrs · 41,016 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY OPS CHECK AT M1668. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 69,857 hrs · 41,016 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY OPS CHECK AT M1673. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,857 hrs · 41,016 cycles

EMERGENCY LIGHTS CONTROLLED BY BATTERY PACK M1670 INOP. REMOVED AND INSTALLED BATTERY PACK M1670 IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,857 hrs · 41,016 cycles

LT OVERWING ESCAPE HATCH EXTERNAL EMERGENCY LIGHT IS INOP. REPLACED LT OVERWING ESCAPE HATCH EXTERNAL EMERGENCY LIGHT IAW AMM 3.

Part: LENS — CRACKED (CABIN) · airframe 69,857 hrs · 41,016 cycles

LT OVERWING ESCAPE LIGHT LENS CRACKED. R&R LENS IAW SRM.

Part: HOUSING — CRACKED (CABIN) · airframe 69,857 hrs · 41,016 cycles

CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT HOUSING CRACKED. R&R LIGHT HOUSING IAW AMM.

Part: INTERCOSTAL — CRACKED (FWD CARGO LH) · airframe 69,857 hrs · 41,016 cycles

LH 'Z' ANGLE INTERCOSTAL CRACKED AT STA 420- 440 LBL 22 / REMOVED AND REPLACED INTERCOSTAL P/N 143A7810-9 FROM STA 440 TO 460 IAW N737-700 SRM 51-10-02-0G-0 AND DWV 143A7505 REV A ATAGWN 6669

Part: INTERCOSTAL — CRACKED (FWD CARGO LH) · airframe 69,857 hrs · 41,016 cycles

LH 'Z' ANGLE INTERCOSTAL CRACKED AT STA 500-500A LBL 22 / REMOVED AND REPLACED L/H Z ANGLE INTERCOSTAL AT STA 500-500A LBL 22 IAW SRM 51-40-02-0G-0 AND DWG 143A7505 REV -

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 69,857 hrs · 41,016 cycles

RT WING TRAILING EDGE SUPPORT BRACKET ATTACHED TO DEFLECTION CONTROL RIB CRACKED. R&R BRACKET IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 69,857 hrs · 41,016 cycles

DURING THE INSTALLATION OF FLOOR REPAIR OUTSIDE THE FLIGHT DECK; FOUND INTERCOASTAL CRACKED BETWEEN STA. 270 TO STA. 291 AT BL0. / REMOVED OLD PART IAW 737 SRM 51-40-02-0G-0. VERIFIED NEW PART IAW BOEING DOCUMENT # 141A5400; REV-. PART#141A5410-3. DRILLED UP NEW PART IAW 737 SRM 51-40-05-0G-0. INSTALED NEW PART IAW 737 SRM 51-40-02-0G-0. 'A' TAG# WN752?

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

FIRST OFFICER'S NR 3 WINDOW UPPER INTERCOSTAL CRACKED BETWEEN BS. 244 TO BS. 259, AT AFT LOWER FASTENER HOLE. R&R INTERCOSTAL IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

CENTER SECTION WING BOX AT STA 663, LBL 45, O/B SIDE OF THE FLOORBEAM FITTING HAS A CRACK ON THE LOWER ATTACH ANGLE. REPAIRED ANGLE PER SWA EA.

Part: FRAME — CORRODED (AFT CARGO COMPT) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO COMPARTMENT STA 947 FRAME CORRODED ON TOP FLANGE APPROX RBL 21 / STA 947 AFT CARGO FRAME SEGMENT REPLACED ON N/R 39149/1600/0087 DEFECT X925109.

Part: ATTACH ANGLE — CORRODED (LT HORIZ STAB) · airframe 69,857 hrs · 41,016 cycles

LH HORIZONTAL STAB. #2 BALANCE BAY. FWD BALANCE PANEL HINGE ATTACH ANGLE COMMON TO HORIZONTAL STAB HAS CORROSION ON UPPER SURFACE. FROM I/B END OF BAY TO O/B END OF BAY / L/H HORIZONTAL STAB #2 BALANCE BAY; REMOVED CORROSION ON ATTACH ANGLE (CHANNEL) IAW. SRM 51-1-02-0G-0; REMOVED 0.010; ORIGINAL TH. 0.040; REMAINING 0.030; NO SRM. REFERENCE FOR THE LIMITS; REMVOED AND REPLACED -1 CHANNEL PN 185A1112-1; FABRICATED ON BACK SHOP W/O. 39151.3400-0001 IAW. DWG. 185A1112 REV. C INSTALLED IAW. SRM. 51-40-02-0G-0 AND BOEING. DWG. 185A11101 REV C.

Part: INTERCOSTAL — CORRODED (AFT CARGO) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO COMP.FWD OF DOOR CUTOUT;TOP OF FLOOR INTERCOSTAL CORRODED STA 787-794 RBL 20' / REMOVED CORROSION AND EVALUATED AFT CARGO FLOOR INTERCOASTAL STA 787-794 RBL 20; ORIG 'T' .045; REMAINING .043 LOSS .002

Part: DRAG ANGLE — CORRODED (VERTICAL STAB) · airframe 69,857 hrs · 41,016 cycles

AFT L/H UPPER FUSELAGE AT STA 1088 LEFT VERTICAL PRIMARY ATTACH FITTING ON AIRCRAFT SIDE FORWARD DRAG ANGLE FITTING CORRODED IN BORE. / R&R DRAG ANGLE IAW DWG.

Part: SEAL — BUCKLED (L/H HORIZ. STAB.) · airframe 69,857 hrs · 41,016 cycles

LH HORIZONTAL STABILIZER FRONT SPAR LOWER SLIDING SEAL PLATE IS BUCKLED AT TIE BAR ATTACHMENT. / REMOVED AND REPLACED SLIDING SEAL ON L/H HORIZONTAL STAB I/A/W AMM 53-31-31-400-803. A TAG WN 9285.

Part: NONE — BUCKLED (AFT CARGO) · airframe 69,857 hrs · 41,016 cycles

AFT PIT DOOR CUT OUT LOWER SILL BEAM INBOARD CLIP UPPER FLANGE IS BUCKLED BS 860; RBL 18. / REMOVED CLIP FROM STA 860 RBL 18. RECIEVED NEW CLIP FROM BACKSHOP ON W/O 39151-1600-0002 P/N 146A8125-45. LOCATED AND DRILLED NEW CLIP IAW DWG 146A0081 REV AND SRM 51-40-05-0G-0. TREATED AND PRIMED AND ACCOMPLISHED CONFORMITY INSTALLED NEW CLIP IAW B737-700 SRM 51-40-02-0G-0 AND DWG 146A0081 REV C

Part: BAFFLE — CRACKED (BS 945) · airframe 69,857 hrs · 41,016 cycles

AFT PIT BILGE BODY FRAME INTERCOSTAL BAFFLE UPPER FLANGE CRACKED AT BS. 945, RBL 21. / R&R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — BUCKLED (AFT CARGO) · airframe 69,857 hrs · 41,016 cycles

AFT PIT DOOR CUT OUT LOWER SILL BEAM UPPER FLANGE IS BUCKLED BS 860; RBL 18. / REMOVED LOWER SILL BEAM 'INTERCOSTAL' AT STA 860 RBL 18 RECEIVED NEW INTERCOSTAL FROM BACKSHOP ON W/O 39151-1600-0003 P/N 146A8123-5. LOCATED AND DRILLED NEW INTERCOSTAL IAW B737-700 SRM 51-40-05-0G-0 AND DWG 146A0081 REV B. TREATED AND PRIMED AND ACCOMPLISHED CONFORMITY BULKHEAD IAW B737 NEW INTERCOSTAL IAW B737-700 SRM 51-40-02-0G-0 AND DWG 146A0081 REV B

Part: PLATE — CRACKED (L/H HORIZ. STAB.) · airframe 69,857 hrs · 41,016 cycles

LH HORIZONTAL STABILIZER FRONT SPAR UPPER SLIDING SEAL PLATE IS CRACKED AT TIE BAR ATTACHMENT. / REMOVED CRACKED TIE BAR ASSY. IAW 737 SRM 51-40-02-0G-0. RECEIVED AND VERIFIED NEW ASSY P/N 181A80-3 IAW 737 IPC 53-31-31-03 ITEM 75 LOCATED DRILLED IAW 737 SRM 51-40-05-0G-0 INSTALLED NEW PART IAW 737 SRM 51-40-02-0G-0

Part: STRIP — CRACKED (AFT CARGO BAY) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO PIT FWD BULKHEAD PANEL 142NW LOWER CAP STRIP CRACKED / REPLACED AFT CARGO PIT FWD BULKHEAD PNL 142NW'S LOWER CAPSTRIP 'ON BENCH' W / P/N 453A2511-2 ATAG # WN8438 I/A/W BOEING DWG 453A2500 SHEET 6 REV A.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

FWD CARGO STA 500+18" STR 26R IS CORRODED. REPAIRED STRINGER PER SWA EA.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO COMPARTMENT FLOOR PANEL #140CF HAS A SECTION OF CORROSION ON THE TOP OF THE PANEL. / AFT CARGO PNL 140CF REPLACED ON N/R 39149/1600/0079 DEFECT #X924955. REMOVED CORROSION IN 4EA AREA; VERIFIED REMOVAL OF CORROSION ON OLD PNL 140LF USING 19X MAG I/A/W SRM 51-10-02-0G-0.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO COMPARTMENT FLOOR PANEL #140CF HAS SEVERAL SPOTS OF CORROSION NOTED ON THE BACK OF THE PANEL. / AFT CARGO FLOOR PANEL 140CF REPLACED ON N/R 39149/1600/0079 DEFECT #X924955

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

RT LOWER FUSELAGE STA 500 + 17", STR 26R SKIN CORRODED. REPAIRED STRINGER PER EA.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 69,857 hrs · 41,016 cycles

PASSENGER CABIN FLOOR PANEL 241AF UPPER SURFACE HAD FIBER DAMAGED, BETWEEN BS 537.45 TO 727B. REPAIRED THE FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 69,857 hrs · 41,016 cycles

PASSENGER CABIN FLOOR PANEL 231ZF EDGE DAMAGED, (BETWEEN BS. 537.45 TO BS. 727B). / REPAIRED PANEL IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

FLIGHT DECK LEFT WINDOW POST CRACKED AT BS. 225, BETWEEN #2 AND #3 WINDOW CRACKED AT TOP FASTENER ON AFT SIDE. R&R LT #3 WINDOW FRAME IAW EA, SRM, & DWG.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

FLIGHT DECK RIGHT WINDOW POST CRACKED AT BS. 225, BETWEEN #2 AND #3 WINDOW AT TOP FASTENER ON AFT SIDE. R&R RT #3 WINDOW FRAME IAW EA, SRM, DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

FUSELAGE SKIN FASTENER HOLE CORRODED AT BS. 360, STR. 28R. REPAIRED SKIN IAW SRM AND EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

ELECTRONIC & EQUIPMENT COMPARTMENT AT BS. 360+6, STR. 27R BELOW VALVE INBOARD SIDE CRACKED FORWARD OF SPLICE. REPAIRED STRINGER SPLICE IAW SRM AND EA.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 69,857 hrs · 41,016 cycles

BS 663 BULKHEAD VERTICAL WEB CRACKED AT LBL 34. REPAIRED WEB PER SRM.

Part: SKIN — BULGED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

EMERGENCY AND EQUIPMENT COMPARTMENT EXTERNAL SKIN BULGED AT BS. 259, STR. 28R. REPAIRED SKIN IAW EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,857 hrs · 41,016 cycles

L/H HORIZONTAL STABILIZER INSPAR RIB AT STA. 120.3 CRACKED ON 4TH VERTICAL FROM FRONT SPAR. / REPAIRED RIB IAW DWG.

Part: PANEL — ELONGATED (VERTICAL STABILI) · airframe 69,857 hrs · 41,016 cycles

VERT STAB PNL 323CR HAS OVERSIZED AND ELONGATED FASTENER HOLE AT LWR AFT CORNER. / REMOVED CHANNEL ON VERTICAL STAB PANEL 323CR. FABRICATED NEW PANEL; TREATED; PRIMED AND APPLIED TOP COAT. REINSTALL CHANNEL TO NEW PANEL IAW EA 190252 REV IR; AND S/W EA 1-755-4370 REV IR

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO COMPARTMENT AFT BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS. 947. R&R ANGLE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO COMPARTMENT FLOOR LT SIDE Z-ANGLE CORRODED BETWEEN BS. 727 TO BS. 847. R&R Z-ANGLE PER SRM AND DWG.

Part: STRIP — CRACKED (VERTICAL STABILI) · airframe 69,857 hrs · 41,016 cycles

VERT STAB PNL 323CL RETAINER STRIP CRACKED AND WORN THRU. / REMOVED AND INSTALLED NEW RETAINER AT VERT. STAB. PANEL #323CL IAW SRM 51-40-02-0G-0; VERIFED NEW RETAINER IAW DWG 172A6124 P/N 172A6124Y7; LOCATED AND DRILLED NEW RETAINER IAW SRM 51-40-05-0G-0 TAG#A33585

Part: ANGLE — CORRODED (BS 787) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO COMPARTMENT SIDEWALL SUPPORT ANGLE CORRODED AT BS. 787 BETWEEN STR. 23L TO STR. 25L. / R&R ANGLE IAW SRM.

Part: CHANNEL — CORRODED (BS 773) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED AT BS. 773, RBL 8. / REPAIRED CHANNEL IAW SRM & EA.

Part: TRACK — CORRODED (AFT CARGO COMPT) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO COMPARTMENT FLOOR TRACK STA 945 LBL3 HAS CORROSION / REMOVED AND EVALUATED CORROSION; ORIGINAL THICKNESS .070' LOSS OF .070'. FOUND 100%. MATERIAL LOSS. BLENDED FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED -13 CARGO TRACK STA 947 TO FACTORY SPLICE AT STA 887 PER SRM 51-40-2-0G-0 AND DWG 147A7500 REV-

Part: TRACK — CORRODED (AFT CARGO COMPT) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO COMPARTMENT FLOOR TRACK STA 907 TO 947 RBL 13 HAS CORROSION / REMOVED CORROSION ON AFT CARGO FLOOR TRACK STA 907-947 RBL 13 FOUND TO BE OUT OF LIMITS ORG T .070; REMAINING .050; LOSS OF .020' I/A/W SRM 53-00-53-1A-2. LOCATED DRILLED AND INSTALLED NEW FLOOR TRACK FROM 907-947 RBL 13 I/A/W SRM 51-40-02-0G-0 & DWG 147A7500 REV -

Part: TRACK — CORRODED (BS 773) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED AT BS. 773, RBL 3. / R&R FLOOR TRACK IAW SRM & EA.

Part: CHANNEL — CORRODED (BS 773) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO COMPARTMENT FLOOR TRACK CORRODED AT BS. 773, LBL 3. / R&R CHANNEL IAW SRM & EA.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO COMPARTMENT FLOOR R/H SIDE Z-ANGLE IS CORRODED STA 727 TO 767 / EVALUATED CORROSION ORIGINAL THICKNESS .040' LOSS OF .012' WITH 028' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED RH 2-ANGLE STA 727-767 PER SRM 51-40-02-0G-0 STEP 4 AND DWG 146A7502 REV A

Part: RETAINER — CRACKED (LEFT WING) · airframe 69,857 hrs · 41,016 cycles

LEFT WING TRAILING EDGE MIDSPAN BULKHEAD AFT SEAL RETAINER IS CRACKED / REMOVED AND INSTALLED NEW RETAINER SEAL AT LEFT WING T/E MID SPAN BULK HEAD AFT IAW SRM 51-40-02-0G VERIFIED NEW PART # 1152953-1 IAW DWG 115A2980 REV - LOCATED AND DRILLED NEW PART IAW SRM 51-40-05-0G-0 AND DWG 115A2930 REV - A65653 # TAG

Part: FLOOR SUPPORT — CORRODED (BS 767-867) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO BAY FLOOR TRACK CORRODED BETWEEN BS. 767+14 TO BS. 867, RBL 13. / R&R FLOOR TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (BS 500B-500C) · airframe 69,857 hrs · 41,016 cycles

PASSENGER CABIN SEAT TRACK CHANNEL CORRODED BETWEEN BS. 500B+8 TO BS. 500C+10, RBL 45.5. / R&R SEAT TRACK IAW SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO BAY LOWER DOOR CUTOUT THRESHOLD WEB CORRODED BETWEEN BS. 847 TO BS. 787+6.50, STR. 25R. R&R WEB IAW SRM AND DWG.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 69,857 hrs · 41,016 cycles

LH HORIZ STAB; STAB STA 120.30 RIB VERT STIFFENER IS CRACKED 18' AFT OF FRONT SPAR NEAR LWR END. / CUTOUT CRACK ON L/H HORIZ STAB STA 120.30 RIB VERT STIFFNER 18' AFT OF FRONT SPAR AND LWR CHORD FASTENER HOLE. IAW 737 SRM 55-10-09-2R-5 STEP 4.B. HFEC VERT STIFFNER NO DEFECTS NOTED; HFEC RIB WEB FOR CRACKS NO DEFECTS NOTED; HFEC ALL IAW 737 NDT PT. 6; 51-00-00 PROC 23. HFEC OPEN HOLES NO DEFECTS NOTED IAW 737 NDT PT. 6; 51-00-00 PROC 16. VERIFIED REPAIR MATERIAL KIT P/N 55100003-01 AND REPAIR ANGLE -2 ANGLE MATERIAL P/N BAC1490-2793 7075-T6 ALL MATERIAL IAW BOEING DWG 55100003 REV B AND 737 SRM 55-10-09-2R-5 TABLE 201. FABRICATED REPAIR ANGLE -2 AND LOCATED AND DRILLED REPAIR MATERIAL IAW 737 SRM 51-40-05-0G-0.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO BAY STA 847 RBL 19' NUTPLATE STRIP UNDER LOWER TRESHOLD STRAP HAS INTERGRAINULAR CORROSION ON THE BOTTOM SIDE / 100% DETERIORATION ON LOWER THRESHOLD STRAP FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. ORIGINAL THICKNESS .090' MAT LOSS .090'. AAR TOOL 36306 DUE 20-JAN-19. REMOVED + REPLACED STRAP AT STA 847 RBL 19 IAW B737-700 SRM 51-40-02-0G-0; 51-40-05-0G-0 AND DWG 146A0081 REV E

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO BAY BETWEEN STA 787 +6.50' AND 767 FWD FLOOR SHIELD IS CORRODED TOP AND BOTTOM SIDES IN SEVERAL AREAS / REMOVED CORROSION AND EVALUATED AFT CARGO FLOOR SHIELD FWD OF DOOR STA 767-787+6.5' ORIG 'T' .050; REMAINING .030'; LOSS OF .020' FOUND TO BE OUT OF LIMITS I/A/W SRM 53-00-53-1A-2 USING AAR TOOL # 36308 CAL DUE 04/18/19. REPLACED FLOOR SHIELD I/A/W SRM 51-40-02-0G-0 & DWG 146A0081 REV C.

Part: STRAP — CORRODED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO BAY LOWER CARGO DOOR CUTOUT STRAP CORRODED BETWEEN BS. 787 TO BS. 807+16, RBL 19. R&R STRAP IAW SRM & DWG.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 69,857 hrs · 41,016 cycles

L/H HORIZONTAL STABILIZER STAB. STA. 120.30 RIB VERTICAL STIFFENER CRACKED 27" AFT OF FRONT SPAR NEAR LOWER END. / REPAIRED STIFFENER IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 69,857 hrs · 41,016 cycles

L/H WING TRAILING EDGE AFT OF #1 SAILTAIL WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

AFT CARGO BAY AFT FLOOR SHIELD CORRODED BETWEEN BS. 847 TO BS. 867. R&R SHIELD IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

L1 DOOR WAY LOWER SILL CREASE BEAM INNER CHORD VERTICAL FLANGE CORRODED BETWEEN BS. 323 TO BS. 344, LBL 60. R&R L1 DOOR CREASE BEAM IAW DWG.

Part: SUPPORT BRACKET — CRACKED (RT WING TE) · airframe 69,857 hrs · 41,016 cycles

R/H WING TRAILING EDGE SUPPORT BRACKET ATTACHED TO DEFLECTION CONTROL RIB CRACKED. R&R BRACKET IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

FORWARD CARGO Z ANGLE CORRODED BETWEEN BS. 400 TO BS. 480, LBL 22. R&R Z-ANGLE PER SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

FORWARD CARGO SHIELD CORRODED BETWEEN BS. 500 TO BS. 500A, RBL 22. R&R SHIELD PER DWG AND SRM.

Part: BAFFLE — CRACKED (FWD CARGO) · airframe 69,857 hrs · 41,016 cycles

FWD CARGO INTERCOSTAL ATTACH CLIP CRACKED AT BS 400 LBL25' / REMOVED BAFFLE CLIP AT STA 400 LBL25 IAW SRM 51-40-02-0G-0. VERIFIED NEW BAFFLE P/N - 143A7502U5 ON ATAG#A17245 IAW BOEING DWG # 143A7505 REV B. LOCATED AND DRILLED NEW BAFFLE CLIP IAW BOEING DWG #143A7505 REV B A-D SRM 51-40-05-0G-0. INSTALLED NEW BAFFLE CLIP IAW BOEING DWG #143A7505 REV B. ATAG#A17245

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 69,857 hrs · 41,016 cycles

STRINGER CLIP CRACKED AT BS. 277, STR. 10R. / R&R STRINGER CLIP IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,857 hrs · 41,016 cycles

RT CREASE BEAM CORRODED AT BS 767+2, STR 17R. R&R CREASE BEAM IAW SRM.

Part: CAP — MISSING (R2 DOOR) · airframe 69,857 hrs · 41,016 cycles

R2 DOOR SLIDE COVER MISSING A BUMPER CAP. INSTALLED BUMPER CAP IAW SRM.

Part: FRAME — CRACKED (CABIN) · airframe 69,857 hrs · 41,016 cycles

MAIN CABIN STA. 312 LH FRAME JUST ABOVE THE L1 DOOR CUTOUT THERE IS A CRACK AT THE BOTTOM CORNER. MARKED WITH A DOT. / TRIMMED OUT CRACK IAW EA 190229 IR AND EA 1-753-34542 REV IR

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 69,857 hrs · 41,016 cycles

R/H O/B TRAILING EDGE AFT FLAP I/B LOWER SURFACE DELAMINATED / REPAIRED DELAMINATION ON I/B FLAP LOWER SURFACE I.A.W B737 SRM

Part: SKIN — CRACKED (SLAT) · airframe 69,857 hrs · 41,016 cycles

#4 SLAT ACTUATOR; 4 SKIN RIVETS WORKING; MARKED / REMOVED 4SKIN RIVETS FROM #4 SLAT ACTUATOR SKIN AT BOTTOM SIDE UNDER #4 SLAT ACTUATOR FITTING STEP HOLES UP TO 2N OVER. FOUND SIKIN CRACKED AT ONE OF THE HOLES IN SKIN I/A/W 737 NDTM PART 6 51-00-00 PRO 16. CUTOUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER AND FILLER I/A/W 737-700 SRM 57-42-01-2R-8 REPAIR8 ATAGS A14664 ABND A82380

Part: SKIN — CRACKED (SLAT) · airframe 69,857 hrs · 41,016 cycles

#5 SLAT ACTUATOR; 2 SKIN HI-LOK WORKING; MARKED / REMOVED 2 EA HI-LOI FASTENERS AT #5 SLAT I.A.W B737-700 SRM 51-40-02; AFTER FURTHER INSPECTION NDT FOUND A CRACK INDICATION I.A.W B-737 NDTM PART 6 51-00-00 PRO 16 TOOL # 36303; DUE:17 APR 19 CUT-OUT DAMAGE 4IN X 3IN AND PERFORMED AND ACCOMPLISHED REPAIR 8# FIG 202 IAW B737-700 SRM 57-42-01-2R8.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,177 hrs · 39,927 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,177 hrs · 39,927 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 67,691 hrs · 39,602 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. RESECURED SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 66,572 hrs · 38,881 cycles

L2 DOOR EMERGENCY LIGHTS LENS MISSING ARROW. R&R LENS IAW.

Part: SPRING — BROKEN (LIGHT PANEL) · airframe 66,572 hrs · 38,881 cycles

AFT EMERGENCY LIGHTS GUARDED SWITCH SPRING BROKEN. R&R LIGHT PANEL PER AMM.

Part: LENS — MISSING (CABIN) · airframe 66,572 hrs · 38,881 cycles

R2 DOOR EMERGENCY LIGHTS LENS MISSING ARROW. R&R LENS IAW.

Part: LENS — MISSING (EXIT SIGN) · airframe 66,572 hrs · 38,881 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER LENS MISSING RED ARROW. R&R LENS IAW AMM.

Part: LENS — FADED (CABIN) · airframe 66,572 hrs · 38,881 cycles

LT OVERWING EMERGENCY DOOR LIGHT LENS COVER FADED. R&R LENS IAW AMM.

Part: BRACKET — CRACKED (RIGHT WING) · airframe 65,507 hrs · 38,227 cycles

RIGHT WING FIXED TRAILING EDGE PANEL (LOCATED AT MID SPAN DEFLECTION CONTROL RIB) CENTER ATTACHING BRACKET IS CRACKED APPROX. 1 INCH. / REMOVED AND REPLACED BRACKET REF SRM 51-40-02 AND SIP.

Part: BRACKET — CRACKED (RIGHT WING) · airframe 65,507 hrs · 38,227 cycles

RIGHT WING FIXED TRAILING EDGE PANEL ATTACH BRACKET LOCATED AT MID SPAN DEFLECTION CONTROL RIB IS CRACKED APPROX. 2 INCHES. / REMOVED AND REPLACED BRACKET REF SRM 51-40-02 AND SIP.

Part: PANEL — DELAMINATED (RH PYLON) · airframe 64,671 hrs · 37,701 cycles

PANEL #441 EL IS DELAMINATING ON LOWER FWD EDGE / INSTALLED PANEL PER AMM 54-53-01 REF A1059786

Part: BRACKET — OUT OF ADJUST (R2 DOOR) · airframe 64,671 hrs · 37,701 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET OUT OF ADJUST. ADJUSTED BRACKETS IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,106 hrs · 36,770 cycles

RIGHT FORWARD CABIN STOW BIN BULLNOSE EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 1 & 2. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,106 hrs · 36,770 cycles

FORWARD LAVATORY MOUNTED EMERGENCY EXIT SIGN INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,106 hrs · 36,770 cycles

R1 DOOR EXTERIOR EMERGENCY EXIT SIGN INOP. R&R BATTERY PACK IAW AMM.

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 63,106 hrs · 36,770 cycles

STRINGER CLIP CRACKED AT BS 277, STRINGER 12R. R & R THE STRINGER CLIP IAW DWG.

Part: ANGLE — CRACKED (BS 294) · airframe 63,106 hrs · 36,770 cycles

FORWARD GALLEY DOOR STUB FRAME LOWER EDGE CUTOUT CRACKED AT BS 294. REPAIRED THE ANGLE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,106 hrs · 36,770 cycles

R2 DOOR CREASE BEAM CORRODED BETWEEN BS 947 TO BS 987. R&R CREASE BEAM IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 294) · airframe 63,106 hrs · 36,770 cycles

FORWARD WET AREA FLOOR SUPPORT CRACKED AT BS 294.5-10, BL 0. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (BS 294) · airframe 63,106 hrs · 36,770 cycles

FORWARD GALLEY DOOR CUTOUT FORWARD SIDE CREASE BEAM SUPPORT ANGLE CRACKED AT BS 294.5, RBL 54. R & R THE SUPPORT ANGLE IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (BS 294-360) · airframe 63,106 hrs · 36,770 cycles

CREASE BEAM CORRODED BETWEEN BS 294.5-4 TO 360, RBL 59. R & R THE CREASE BEAM IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 987) · airframe 63,106 hrs · 36,770 cycles

FLOORBEAM TEE CORRODED AT BS 987, BETWEEN RBL 30 TO 45. R & R THE TEE IAW SRM.

Part: ATTACH ANGLE — CORRODED (GIRT BAR) · airframe 63,106 hrs · 36,770 cycles

L1 DOOR GIRT BAR ATTACH ANGLE CORRODED AT BS. 344, LBL 62. R & R ATTACH ANGLE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (BS 328) · airframe 63,106 hrs · 36,770 cycles

CREASE BEAM THRESHOLD SUPPPORT ANGLE CORRODED BETWEEN BS 328.4 - 328, RBL 60. R & R THE SUPPORT ANGLE IAW SRM AND DWG.

Part: WEB — CORRODED (BS 987-1016) · airframe 63,106 hrs · 36,770 cycles

FLOOR WEB CORRODED BETWEEN BS 987 TO 1016, RBL 45. R & R THE WEB IAW DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,106 hrs · 36,770 cycles

FORWARD CARGO COMPARTMENT FLOOR STRUCTURE RT SIDE SHIELD Z-ANGLE CORRODED BETWEEN BS 420 TO BS 440. R&R SHIELD IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 727E-807) · airframe 63,106 hrs · 36,770 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT ANGLE CORRODED BETWEEN BS 727E+9 - 807. R & R THE ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 794-813) · airframe 63,106 hrs · 36,770 cycles

AFT CARGO FLOOR SUPPORT CORRODED AT BS 794 TO 813, RBL 13.5. REPAIRED THE FLOOR SUPPORT IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,106 hrs · 36,770 cycles

FWD CARGO FLOOR LT Z-ANGLE CORRODED AT STA 460 TO STA 500A. REPAIRED ANGLE PER SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,106 hrs · 36,770 cycles

AFT CARGO COMPARTMENT SHIELD CORRODED BETWEEN BS 767 TO BS 787, RBL 22. R&R SHIELD IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (BS 794) · airframe 63,106 hrs · 36,770 cycles

AFT CARGO BAY FLOORBEAM TEE CORRODED AT BS 794, BETWEEN RBL 15 TO 19. R & R THE FLOORBEAM TEE IAW SRM & DWG.

Part: LIGHT — DAMAGED (CABIN) · airframe 63,106 hrs · 36,770 cycles

FORWARD LAV EMERGENCY EXIT LIGHT LENS ON AFT WALL DAMAGED. R&R LIGHT ASSEMBLY IAW AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 62,731 hrs · 36,547 cycles

RT FORWARD SIDE OVERWING LOWER EXIT SIGN LENS COVER MISSING. INSTALLED COVER PER AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 62,274 hrs · 36,253 cycles

FWD GALLEY LOWER EXIT LIGHT COVER LENS MISSING. INSTALLED EXIT SIGN LENS IAW MM.

Part: DOOR — CRACKED (CABIN) · airframe 61,660 hrs · 35,896 cycles

R1 DOOR UPPER AND LOWER DOOR HANDLE MECHANISM MOUNTING MACHINED BEAMS CRACKED AT THE UPPER AND LOWER FORWARD INBD FASTENERS. R & R DOOR IAW AMM.

Part: SLAT — DAMAGED (LT WING) · airframe 61,660 hrs · 35,896 cycles

LEFT WING NR 2 SLAT ACTUATOR ATTACH POINT ON THE SLAT HAD DISPLACED. R & R NR 2 L/E SLAT IAW AMM.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 61,627 hrs · 35,873 cycles

R2 DOOR EXIT SIGN LIGHT LENS FELL OFF. R & R THE LENS ASSEMBLY IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 58,271 hrs · 33,957 cycles

R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: PLATE — CRACKED (TE FLAP) · airframe 57,595 hrs · 33,564 cycles

LEFT WING AFT FLAP TRACK FAIRING DOOR CUT OUT PLATE CRACKED. R & R PLATE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

TIE CLIP CRACKED AT BS 360, STRINGER 8R. R & R TIE CLIP IAW SRM & DWG.

Part: SUPPORT FRAME — CRACKED (FAIRING) · airframe 57,595 hrs · 33,564 cycles

LEFT WING TO BODY FAIRING STRUCTURE SUPPORT FRAME ANGLE CRACKED AT LEVEL OF BS 500D, WBL 76. R & R FRAME IAW SRM & DWG.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 57,595 hrs · 33,564 cycles

DAMAGED PHOTO LUMINESCENT STRIP AT FWD CABIN. R & R STRIP IAW AMM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 57,595 hrs · 33,564 cycles

DAMAGED PHOTO LUMINESCENT STRIP AT AFT CABIN. R & R STRIP IAW AMM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,595 hrs · 33,564 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT BS 92.70, 12" AFT OF LOWER CHORD FRONT SPAR. REPAIRED RIB IAW EO & EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,595 hrs · 33,564 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT BS 92.70, 21" AFT OF LOWER CHORD OF FRONT SPAR. REPAIRED RIB IAW EO & EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,595 hrs · 33,564 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT BS 92.70, 30.5" AFT OF LOWER CHORD OF FRONT SPAR. REPAIRED RIB IAW EO & EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,595 hrs · 33,564 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT STAB STATION 129.50, 27" AFT OF LOWER CHORD. REPAIRED RIB IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FUSELAGE FRAME CRACKED AT STATION 727B, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FUSELAGE FRAME CRACKED AT STATION 400, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FUSELAGE FRAME CRACKED AT STATION 787, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

LOWER WEB CRACKED AT BS 663, STRINGER 1L. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FUSELAGE FRAME CRACKED AT STATION 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FUSELAGE FRAME CRACKED AT STATION 747, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

LOWER WEB CRACKED AT BS 663, STRINGER 4L. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FUSELAGE FRAME CRACKED AT STATION 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

LOWER WEB CRACKED AT BS 663, STRINGER 2L. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FUSELAGE FRAME CRACKED AT STATION 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED FRAME IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FUSELAGE FRAME CRACKED AT STATION 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FUSELAGE FRAME CRACKED AT STATION 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FUSELAGE FRAME CRACKED AT STATION 440, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FUSELAGE FRAME CRACKED AT STATION 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FORWARD SEAT TRACK INBD FLANGE & OTBD FLANGE CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EO & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FORWARD SEAT TRACK OTBD FLANGE & INBD FLANGE CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EO & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

AFT SEAT TRACK OTBD FLANGE FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED CHORD IAW EO & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FORWARD SEAT TRACK INBD & OTBD FLANGE CRACKED. REPAIRED SEAT TRACK IAW EO & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

AFT SEAT TRACK INBD FLANGE CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EO & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

AFT SEAT TRACK OTBD FLANGE FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EO & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,595 hrs · 33,564 cycles

FORWARD SEAT TRACK, OTBD FLANGE CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EO & EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,595 hrs · 33,564 cycles

LEFT WING LE, NR 3 SLAT NOSE SKIN CRACKED AT STATION 202.45. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,595 hrs · 33,564 cycles

RIGHT WING NR 7 SLAT NOSE SKIN CRACKED AT STATION 322.71. REPAIRED SKIN IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 57,595 hrs · 33,564 cycles

MAIN WW VERTICAL SPAR PRESS WEB CRACKED AT BS 663, RBL 40. REPAIRED WEB IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,206 hrs · 32,771 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 3. RELAMPED LIGHT IAW AMM.

Part: COVER — LOOSE (R2 DOOR) · airframe 56,031 hrs · 32,670 cycles

R2 DOOR SLIDE COVER LOOSE. SECURED COVER IAW MM.

Part: WIRE — DAMAGED (CABIN) · airframe 55,351 hrs · 32,271 cycles

EMERGENCY LIGHT INOPERATIVE AT 16 DEF. REPAIRED LIGHT ASSEMBLY WIRING IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,607 hrs · 31,845 cycles

FUSELAGE SKIN CRACKED AT BS 540 STRINGER 22R. REPAIRED SKIN IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,607 hrs · 31,845 cycles

LOWER BULKHEAD CHORD CRACKED AT BS 540 BELOW STRINGER 22R. REPAIRED CHORD IAW EA & ACO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,607 hrs · 31,845 cycles

LOWER BULKHEAD CHORD CRACKED AT BS 540 BETWEEN STRINGER 22L TO 23L. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,607 hrs · 31,845 cycles

FUSELAGE SKIN CRACKED AT BS 540 BELOW STRINGER 22L. REPAIRED SKIN IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,607 hrs · 31,845 cycles

RIGHT LOWER BULKHEAD CHORD CRACKED AT BS 540 BELOW STRINGER 22R. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,607 hrs · 31,845 cycles

LEFT LOWER BULKHEAD SKIN CRACKED AT BS 540 BELOW STRINGER 22L. REPAIRED SKIN IAW EA.

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 54,537 hrs · 31,806 cycles

RIGHT CTR WING FUEL PUMP LOW PRESS LIGHT ILLUMINATED. PRIMED RT PUMP. OPERATIONS CHECKED GOOD IAW MM.

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 54,537 hrs · 31,806 cycles

LEFT CTR WING FUEL PUMP LOW PRESS LIGHT ILLUMINATED. PRIMED LT PUMP. OPERATIONS CHECKED GOOD IAW MM.

Part: FITTING — LOOSE (R2 DOOR) · airframe 52,407 hrs · 30,597 cycles

R2 DOOR EMERGENCY EVAC SLIDE COVER RETAINING SCREW LOOSE. SECURED CLIP IAW SIP.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 51,339 hrs · 29,958 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOW PRESSURE. R&R SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 51,008 hrs · 29,755 cycles

L1 DOOR EMERGENCY EXIT SIGN INTERIOR NR 1 LED INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 51,008 hrs · 29,755 cycles

L2 DOOR EMERGENCY EXIT SIGN NR 2 LED INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,008 hrs · 29,755 cycles

RT INTERIOR OVERWING EMERGENCY EXIT HANDLE AFT LIGHT INOPERATIVE. RELAMPED IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,692 hrs · 29,579 cycles

LEFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,692 hrs · 29,579 cycles

LEFT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,692 hrs · 29,579 cycles

RIGHT FWD EMERGENCY LIGHT FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 50,692 hrs · 29,579 cycles

LEFT BULLNOSE EMERGENCY LIGHT LOOSE AT ROW 9. R & R LIGHT IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,692 hrs · 29,579 cycles

LEFT AFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 50,692 hrs · 29,579 cycles

LEFT MLG WHEEL WELL REAR SPAR TO UPPER SHELF VERTICAL STIFFENER CRACKED 1" BELOW UPPER SHELF AT IRSS 140. R & R SHELF BRACKET IAW SRM.

Part: STRUCTURE — DELAMINATED (CARGO BAY) · airframe 50,692 hrs · 29,579 cycles

LT AFT CARGO BAY BULKHEAD FIBERGLASS DELAMINATED AT BS 663, LBL 10. REPAIRED FIBERGLASS IAW EA.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 50,692 hrs · 29,579 cycles

RIGHT MLG WHEEL WELL REAR SPAR TO UPPER SHELF VERTICAL STIFFENER CRACKED 1" BELOW UPPER SHELF AT IRSS 140. R & R SHELF BRACKET IAW SRM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 50,692 hrs · 29,579 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD ATTACH HOOK LOOSE ON CONTAINER. SECURED HOOK IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,692 hrs · 29,579 cycles

FLIGHT DECK LT NR 1 WINDOW FRAME CRACKED AT OTBD UPPER CORNER. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,692 hrs · 29,579 cycles

LEFT NR 3 FLIGHT DECK WINDOW FRAME SECOND LOWER FASTENER HOLE CRACKED. R & R FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,692 hrs · 29,579 cycles

RIGHT NR 3 FLIGHT DECK WINDOW FRAME SECOND LOWER FASTENER HOLE CRACKED. R & R FRAME IAW EA.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 50,342 hrs · 29,368 cycles

DIVERSION - LEFT ELEC HYD OVERHEAT PUMP ILLUMINATED. LOW PRESSURE LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED "A" SYSTEM ELEC PUMP, "A" SYS CONNECTOR & PINS IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 48,419 hrs · 28,204 cycles

LEFT EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 48,419 hrs · 28,204 cycles

RIGHT EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,364 hrs · 26,995 cycles

EMERGENCY LIGHT INOP AT ROW 19. REMOVED AND REPLACED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,418 hrs · 26,458 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING LOWER AFT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: PCU — FAULTY (AILERON) · airframe 44,813 hrs · 26,081 cycles

DURING SCHEDULED MV2 CHECK, FOUND BINDING FLIGHT CONTROL ON PREFLIGHT AILERON CHECK TO RIGHT SIDE. REMOVED AND REPLACED "A" SYSTEM AILERON PCU PER MM.

Part: LENS — MISSING (CABIN) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD EMERGENCY EXIT SIGN LENS MISSING. REMOVED AND REPLACED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT EMERGENCY EXIT SIGN LENS MISSING. REMOVED AND REPLACED LENS PER MM.

Part: ANGLE — PUNCTURED (FUSELAGE) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO COMPARTMENT Z-ANGLE PUNCTURED BETWEEN BS 500B TO BS 500C. REPAIRED Z-ANGLE PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLIGHT DECK SUPPORT ANGLE CORRODED AT BS 270, LBL 10. REPAIRED ANGLE PER EA.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 40.87. REMOVED AND REPLACED FITTING PER SRM.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE CONTAINER WILL NOT BREAK OVER TO ALLOW CLOSURE. REMOVED AND REPLACED SLIDE PER MT.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 40.87. R&R FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 32.40. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 6.14. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 15.04. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 54.60. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 6.14. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 32.40. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 15.04. REMOVED AND REPLACED FITTING PER SRM.

Part: CABLE ASSY — LOOSE (EVAC SLIDE) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE CABLE LOOSE. REPAIRED CABLE ASSY PER MT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR CREASE BEAM INNER CHORD FLOOR SUPPORT CORRODED. REMOVED AND REPLACED SUPPORT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME WEB ANGLE CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED FRAME CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME WEB ANGLE CRACKED AT BS 500B, STR 26L. REMOVED AND REPLACED FRAME CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME IAW EA.

Part: ATTACH BRACKET — CORRODED (GIRT BAR) · airframe 43,900 hrs · 25,535 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 41,524 hrs · 24,177 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS DAMAGED AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 39,683 hrs · 23,091 cycles

DURING SCHEDULED SPV CHECK, FOUND COCKPIT EMERGENCY EXIT DOME LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,683 hrs · 23,091 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,683 hrs · 23,091 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP AT ROW 11. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 38,986 hrs · 22,686 cycles

L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 37,981 hrs · 22,079 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REPAIRED LENS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,204 hrs · 21,593 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 772, LBL 2. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,204 hrs · 21,593 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 772, RBL 8. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,204 hrs · 21,593 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 772, RBL 2. REPAIRED FLOORBEAM PER EA.

Part: LUG — CORRODED (RT MLG) · airframe 35,297 hrs · 20,434 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION BEARING O/B LOWER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: LUG — CORRODED (LT MLG) · airframe 35,297 hrs · 20,434 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION BEARING I/B UPPER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: LUG — CORRODED (RT MLG) · airframe 35,297 hrs · 20,434 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION BEARING I/B LOWER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: LUG — CORRODED (RT MLG) · airframe 35,297 hrs · 20,434 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION BEARING O/B UPPER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: LUG — CORRODED (RT MLG) · airframe 35,297 hrs · 20,434 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION BEARING I/B UPPER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: LUG — CORRODED (LT MLG) · airframe 35,297 hrs · 20,434 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION BEARING O/B LOWER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: LUG — CORRODED (LT MLG) · airframe 35,297 hrs · 20,434 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION BEARING I/B LOWER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: LUG — CORRODED (LT MLG) · airframe 35,297 hrs · 20,434 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION BEARING O/B UPPER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,641 hrs · 20,063 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD RT SIDE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,526 hrs · 19,348 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 32,973 hrs · 19,019 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LENS — BROKEN (CABIN) · airframe 32,514 hrs · 18,759 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 32,370 hrs · 18,677 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 31,722 hrs · 18,272 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND BROKEN CONNECTOR. REMOVED AND REPLACED CONNECTOR PER MM.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 28,296 hrs · 16,247 cycles

INFLIGHT SHUTDOWN/AIR TURNBACK, ON LEVEL OFF AT 10,000 NR 1 ENGINE STARTED TO COMPRESSOR STALL. SECURED NR 1 ENGINE PER QRH. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 27,778 hrs · 15,964 cycles

DURING SCHEDULED HC1 CHECK, LT FWD EMERGENCY EXIT LIGHT BATTERY FAILED THE LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — LOOSE (CABIN) · airframe 26,986 hrs · 15,513 cycles

EEPLS LIGHT COVER LOOSE AT ROW 9 DEF. SECURED EEPLS COVER PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 26,954 hrs · 15,497 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 9 DEF. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: RIVET — LOOSE (L1 DOOR) · airframe 25,990 hrs · 14,953 cycles

FOUND L1 DOOR EMERGENCY EVAC SLIDE COVER HAS AFT HOOK LOOSE. REMOVED AND REPLACED EVAC SLIDE COVER RIVET PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 25,274 hrs · 14,546 cycles

DURING SCHEDULED HC2 CHECK, AFT GALLEY EMERGENCY EXIT LIGHT BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 25,274 hrs · 14,546 cycles

DURING SCHEDULED HC2 CHECK, CABIN OVERWING EMERGENCY EXIT LIGHTS BATTERIES FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 25,274 hrs · 14,546 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHT BATTERY AT ROW 16 FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,240 hrs · 13,982 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SIGN — MISSING (MID CABIN) · airframe 21,912 hrs · 12,665 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 21,200 hrs · 12,261 cycles

EEPLS COVER LOOSE AT ROW 6L. SECURED EEPLS COVER PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 18,360 hrs · 10,804 cycles

DURING SPV, FOUND FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 16,295 hrs · 94,492 cycles

RT OVERWING EXIT EMERGENCY EXIT LIGHT LENS LOOSE. REINSTALLED LENS COVER PER MM.

Part: SLIDE — OUT OF POSITION (FWD SVC DOOR) · airframe 15,394 hrs · 8,991 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: ENGINE — FAILED (NR 1) · airframe 14,828 hrs · 8,665 cycles

IN-FLIGHT SHUTDOWN, DECLARED EMERGENCY, AIR TURNBACK, NR 1 ENGINE FAILURE, AUTO SHUTDOWN IN-FLIGHT. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 14,423 hrs · 8,447 cycles

AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF POSITION. REPOSITIONED EVACUATION SLIDE ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 14,287 hrs · 8,371 cycles

AFT SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: INDICATOR — OUT OF POSITION (SERVICE DOOR) · airframe 14,318 hrs · 8,392 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 11,724 hrs · 6,943 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED THOUGHT OUT CABIN. REMOVED AND REPLACED COVERS PER MM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 10,578 hrs · 6,286 cycles

DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST AND RELAMPED LIGHT PER MM.

Part: ACTUATOR — FAILED (L/E SLAT) · airframe 8,006 hrs · 4,809 cycles

(AIR TURNBACK) AFTER TAKEOFF, L/E TRANSIT LIGHT STAYED ILLUMINATED. REMOVED AND REPLACED NR 4 & 7 L/E SLAT ACTUATORS PER MM.

Part: ACTUATOR — FAILED (L/E SLAT) · airframe 7,995 hrs · 4,798 cycles

AIR TURNBACK, AFTER TAKEOFF L/E EDGE TRANSIT LIGHT STAYED ILLUMINATED. REMOVED AND REPLACED NR 2 L/E SLAT ACTUATOR PER MM.

Part: FUSE — FAILED (MLG WW) · airframe 7,972 hrs · 4,779 cycles

DIVERSION, UPON FLAP RETRACTION ON DEPARTURE, L/E FLAP TRANSIT LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED L/E FLAPS SLAT HYD FUSE PER MM.

Part: BUSHING — WORN (ELEVATOR) · airframe 7,938 hrs · 4,751 cycles

DURING SCHEDULED A1 CHECK, LH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R ELEVATOR TAB BUSHING PER MM.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 3,715 hrs · 2,275 cycles

AIR TURNBACK. AFT CARGO DOOR LIGHT ILLUMINATED AFTER TAKE-OFF. FOUND BUNGEE CHORD INTERFERING WITH CARGO DOOR POSITION SWITCH. REPOSITIONED AFT CARGO DOOR BUNGEE CHORD PER MM.

Part: FUSE — CONTAMINATED (MLG WW) · airframe 3,533 hrs · 2,169 cycles

NLG WOULD NOT FULLY EXTEND ON FIRST ATTEMPT REOCCURRING AGAIN AT BNA FLIGHT NR 164. BLED MLG HYD RATE FUSE ON BOTH OCCASIONS PER BOEING LETTER.

Part: CHECK VALVE — INOPERATIVE (NLG) · airframe 3,450 hrs · 2,116 cycles

NLG WOULD NOT RETRACT AFTER FIRST ATTEMPT. REMOVED AND REPLACED NLG HYD RATE FUSE AND CHECK VALVE PER S/B.