N406WN

Part: SENSOR — FAULTY (ZN 200 FUS TOP) · airframe 74,343 hrs · 44,406 cycles

SPLIT FLAP INDICATOR AT FLAPS 25; FLAPS WOULD NOT MOVE ALTERNATE; UPON LANDING FLAPS BOTH INDICATOR 25<[01] -FSEU BITE TEST SHOWS; FLAP 4 SKEW AND MAINT MSG # 27-53253;[02] IAW FIM 27-59 TASK 804; NIL NOTED FAULT OF MEASURED DISTANCE FROM THE BALLSCREW NUT TO THE YOKE ON TRANSMISSSION NO4 AND NO 5;[03] FSEU BITE TEST SHOWED FLAP 4 SKEW. R&R #4 SKEW SENSOR PER AMM 27-59-01. PERFORMED FLAP SKEW DETECTION SYSTEM FUNCTIONAL TEST PER AMM 27-59-00. OPS CHECK GOOD

Part: PANEL — ELONGATED (ZN 100 FUS LOWER) · airframe 74,123 hrs · 44,261 cycles

193B FAIRING PANEL HAS SEVERAL ELONGATED HOLES<[01] REMOVED AND REPLACED WING TO BODY FAIRING PANEL 193B IAW AMM 53-51-21.

Part: POWER SUPPLY — INOPERATIVE (ZN 200 FUS TOP) · airframe 73,554 hrs · 43,914 cycles

EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1675 INOP WHEN SELECTED ON<[01] REMOVED AND REPLACED M1675 BATTERY POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD.

Part: SIGN — BROKEN (ZN 200 FUS TOP) · airframe 73,114 hrs · 43,620 cycles

RIGHT SIDE OVERWING EXIT SIGN (LOWER) BROKEN<[01] R-R RIGHT SIDE OVERWING EMERGENCY EXIT SIGN & OPS GOOD PER AMM 33-51-01

Part: LIGHT — INOPERATIVE (ZN 800 DOOR) · airframe 73,097 hrs · 43,607 cycles

FWD ENTRY DOOR EXTERIOR EMERGENCY EGRESS LIGHT INOP<[01] RELAMPED PER MM 33-51-04

Part: COVER — LOOSE (ZN 200 FUS TOP) · airframe 72,741 hrs · 43,377 cycles

AFT GALLEY EXIT SIGN FELL APART<[01] RE-INSTALLED EXIT SIGN COVER PER AMM 33-51-01. AIRCRAFT OK FOR SERVICE.

Part: SIGN — LOOSE (ZN 200 FUS TOP) · airframe 72,238 hrs · 43,049 cycles

FA REPORT:EMER EXIT ROW SIGN IN MIDDLE OF CABIN COVER IS LOOSE. AFT FACING SIGN COVER / [01] REINSTALLED EMER EXIT SIGN PER SIP; OK TO SERVICE

Part: SENSOR — OUT OF LIMITS (TE FLAP SYS) · airframe 72,194 hrs · 43,025 cycles

WHEN SELECTING FLAPS 15 FOR LANDING FLAPS STAYED AT 5. PERFORMED QRH PROCEDURE LANDED FLAPS 15. FOUND THE NR 4 SKEW SENSOR OUT OF LIMITS. R & R THE NR 4 SKEW SENSOR IAW AMM 27-59 00. FLAPS OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,194 hrs · 43,025 cycles

PASSENGER CABIN EMERGENCY BATTERY PACK AT POSITION M1670 INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805. TESTED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,192 hrs · 43,024 cycles

EMERGENCY LIGHTS 3DEF; 6DEF, 8DEF, 11DEF, AND RT OVERWING HATCH INOPERATIVE. REMOVED AND REPLACED BATTERY PACK M1669 IAW AMM 33-51-06-960-805. TESTED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,192 hrs · 43,024 cycles

EMERGENCY LIGHTS AT POSITIONS L1 DOOR EXIT SIGN, R1 FLOOR PROXIMITY AND R1 ESCAPE SLIDE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805. TESTED OK.

Part: CARGO TRACK — CORRODED (BS 947) · airframe 72,192 hrs · 43,024 cycles

CARGO TRACK, BS 947, RBL 10, CORRODED. REMOVED THE CARGO TRACK IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW CARGO TRACK IAW SRM 51-40-05-02-0G-0. TREATED AND PRIMED IAW AMM 51-21-41-370-803 AND AMM 51-21-72-370-804. INSTALLED THE NEW CARGO TRACK IAW SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 72,192 hrs · 43,024 cycles

CABIN FLOOR SUPPORT CRACKED AT BS 540, RBL. 1, WL 208. REMOVED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0. LOCATED & DRILLED A NEW FLOOR SUPPORT IAW SRM 51-40-05-0G-0. INSTALLED THE NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 72,192 hrs · 43,024 cycles

FLOORBEAM CRACKED AT BS 540, LBL 1, WL 208. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-02-0G-0.

Part: NONE — MISSING · airframe 71,876 hrs · 42,807 cycles

R1 DOOR LOWER EXIT SIGN IS NOT MULTI LANGUAGE. / [01] REMOVED AND REPLACED R1 DOOR LOWER EXIT SIGN PER AMM 33-51-01;[02] INSPECTED

Part: SLIDE — DISLODGED (AFT ENTRY DOOR) · airframe 71,805 hrs · 42,761 cycles

LEFT AFT EMERGENCY EXIT SLIDE PARTIALLY STICKING OUT BOTTOM OF CONTAINER. / [01] SECURED LEFT AFT EMERGENCY EXIT SLIDE IAW AMM 25-66-01.

Part: SENSOR — FAILED (E&E BAY) · airframe 71,045 hrs · 42,262 cycles

ON DEPARTURE MOVED FLAP LEVER FROM 5 TO 1 AND RECIEVED A SPLIT FLAP CONDITION ACMS SHOWS #4 SKEW SENSOR FAILED. / [01] R&R #4 FLAP SKEW SENSOR PER AMM 27-59-01 OPS CHECK GOOD AT THIS TIME AND NO FAULT NOTED.

Part: LIGHT — LOOSE (L1 DOOR) · airframe 70,563 hrs · 41,928 cycles

L-1 DOOR ; EMERGENCY EXIT LIGHT LENS IS LOOSE. / [01] REPLACED L-1 DOOR; EMERGENCY EXIT LIGHT ASSEMBLY IAW AMM 33-51-01-960-802<BR>OPS CK GOOD;[02] VERIFIED STEP 1<BR>AUDIT C/W

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,486 hrs · 41,875 cycles

EXTERNAL AFT ENTRY EMERGENCY LIGHT INOP. / [01] RE-LAMP NO HELP; FOUND BATTERY PACK AT FAULT; R+R AFT TOP LEFT BATTERY PACK PER AMM 33-51-06; OPS CK?D GOOD.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 69,797 hrs · 41,429 cycles

194E PANEL FWD EDGE HAS TWO HOLES ELONGATED 9 EACH TOTAL ON FWD EDGE. BOTH LH AND RH LEADING EDGE 3RD ONE BOTH SIDE COMING INDRD IF COUNTING LH TO RH 3RD HOLE AND 7TH HOLE ELONGATED MARKED PANEL ; 194E PANEL FWD EDGE HAS TWO HOLES ELONGATED 9 EACH TOTAL ON FWD EDGE. BOTH LH AND RH LEADING EDGE 3RD ONE OTH SIDE COMING INDRD IF CONTING LH TO RH 3RD HOLE AND 7TH HOLE ELONGATED MARKED PANEL / [01] REMOVED AND REPLACED 194E PANEL REF M/M 53-51-21

Part: GIRT BAR — OUT OF POSITION (R2 DOOR) · airframe 68,659 hrs · 40,723 cycles

FLIGHT ATTENDANT UNABLE TO ARM AFT GALLEY SERVICE DOOR SLIDE ; / [01] INSTALLED CORRECT GIRT BAR REFERENCE B737 AMM CH 25-66-01. OPS CHECK GOOD. ENTERED FOR E143284 AFTER DEPARTURE

Part: RETAINER — CRACKED (RT WING) · airframe 67,161 hrs · 39,858 cycles

RIGHT WING UPPER AFT FIXED PANEL TRAILING EDGE ABOVE NACELLE STRUT FAIRING SEAL RETAINER CRACKED / REMOVED AND REPLACED NACELLE STRUT FAIRING SEAL RETAINER PER SRM 51-40-02

Part: LIGHT — FAULTY (CABIN) · airframe 67,100 hrs · 39,826 cycles

FO SIDE EMERGENCY EXIT DOOR WHITE LIGHT DIM. (OVERWING DOOR). / CLOSING DMA #0371359 RELAMPED; REF AMM 33-21-00 CLOSING # 72357

Part: HANDLE — OUT OF ADJUST (FWD CARGO) · airframe 66,898 hrs · 39,718 cycles

FDW CARGO COMPARTMENT DOOR HANDLE HARD TO_CLOSE / PERFORMED ADJUSTMENT ON FWD CARGO COMPARTMENT DOOR IAW B737-700 AMM 52-31-00-820-801 STEP 2.K(1) TOOL USED: DIGITAL CALIPER P/N:500-197- 30 S/N:A18135097 DUE DATE:03 JAN 22; FEELER GAUGE P/N:2ZVEG S/N:AE-37272 DUE DATE:05 OCT 21; AND PERFORMED LUBRICATION IAW B737-700 AMM 12-25-31-640-801

Part: DOOR — OUT OF ADJUST (AFT CARGO) · airframe 66,898 hrs · 39,718 cycles

AFT CARGO COMPARTMENT DOOR HANDLE HARD TO CLOSE / PERFORMED ADJUSTMENT ON AFT CARO COMPARTMENT DOOR IAW B737-700 AMM 52-31-00-820-801 STEP 2.K(1); AND PERFORMED LUBRICATION IAW B737-700 AMM 12-25- 31-640-801 TOOL USED:CALIPER PART NUMBER:800-197-30 S/N:A18135097 DUE DATE:03 JAN 22; FEELER GAUGE PART NUMBER:2ZVE6 S/N:AE-37272 DUE DATE:05 OCT 21

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 66,898 hrs · 39,718 cycles

CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT / REPAIRED BY WELD SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737- 700 SRM 53-60-15-2R-1; REPAIR 1 AND BAC 5975

Part: STRINGER SPLICE — CRACKED (E/E BAY) · airframe 66,898 hrs · 39,718 cycles

CRACK STRUCTURE ON STRINGER SPLICE LOCATED ON BST 360 STR 28RH AT EQUIPMENT ELECTRONIC COMP / REPLACED STRINGER SPLICE LOCATED ON BS360 STR28RH AT EQUIPMENT ELECTRONIC COMPARTMENT IAW B737-700 SRM 51-40-02 MATERIAL USED PN 7075 TO +0.036' PO 2020-214270

Part: STRINGER SPLICE — CORRODED (EE BAY) · airframe 66,898 hrs · 39,718 cycles

CORROSION STRUCTURE ON STRINGER SPLICE BST 360 STR 27RH WL 148.5 AT EQUIPMENT ELECTRONIC COMP / REPLACED STRINGER SPLICE LOC ON BS360 STR27RH WL WL 148.5 AT EQUIPMENT ELECTRONIC COMP IAW SPM B737-700 51-40-02 AND DWG140A9101 SHEET 17 REV 51-10-02 ITEM 9 NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM B737-700 FABRICATED FROM 7075-0.045' HEAT TREATED AND CONVERTED FROM T0 AND T6 IAW BAC 5602

Part: STRINGER SPLICE — CORRODED (EE BAY) · airframe 66,898 hrs · 39,718 cycles

CORROSION STRUCTURE ON STRINGER SPLICE BST 360 STR 23RH WL 130 AT EQUIPMENT ELECTRONIC COMP / REPLACED STRINGER SPLICE BS 360; STR.23R WL 160.5 EQUIPMENT ELECTRONIC COMPARTMENT IAW B737-700 SRM 51-10-02 ABD DRAWING #140A9101 REV. R FABRICATED FROM 70-75-01 0.045' HEAT TREATED AND CONVERTED 7075T6. P.O#2020203305; AFFECTED P/N 141A3340-34

Part: STRINGER — CORRODED (E/E BAY) · airframe 66,898 hrs · 39,718 cycles

CORROSION STRUCTURE STRINGER 23RH AT BST 360 MORE 4 INCH AT EQUIPMENT ELECTRONIC COMP WL 165.00 / EVALUATION CORROSION ON STRUCTURE STRINGER 23RH AT BS360 MORE 4 INCH AT EQUIPMENT ELECTRONIC COMPARTMENT AND FOUND OUT OF ALLOWABLE DAMAGE LIMITS I.A.W B737-700SRM 53-00-03-1A-1 ALLOWABLE DAMAGE 1 AND PERFORMED PERMANENT REPAIR ON STRINGER 23RH BTW BS 360 TO BS 400 I.A.W B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIG. 206 REPAIR PARTS STRINGER SECTION MADE FROM 7075 TO 0.036 PO 2020 214270 AND CHANNEL AND ANGLES (2 E/A) MADE FROM 7075 - TO /0.040 PO 2015 506435 REPAIR PARTS HEAT TREATED AND CONVERTED 7075 T6.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 66,898 hrs · 39,718 cycles

WEAR ON TRACK RAIL-ASSY CAPTAIN RAIL AFT LT SIDE AT COCKPIT (1 EA) / REPLACED TRACK RAIL-ASSY CAPTAIN RAIL AFT LT SIDE AT COCKPIT (1EA) IAW B737-700 AMM 25-11-11-400-801

Part: SEAT TRACK — WORN (COCKPIT) · airframe 66,898 hrs · 39,718 cycles

WEAR ON TRACK RAIL-ASSY FIRST OFFICER RAIL AFT LT AND RT SIDE AT COCKPIT (2 EA) / REPLACED TRACK RAIL-ASSY FIRST OFFICER RAIL AFT LT AND RT SIDE AT COCKPIT (2EA) IAW B737-700 AMM 25-11-11-400-801

Part: ANGLE — CRACKED (AFT CARGO) · airframe 66,898 hrs · 39,718 cycles

CRACK ANGLE - SUPPORT LOCATED BS 947.5 AND STR 26L AT AFT CARGO COMPARTMENT / REPLACED ANGLE SUPPORT LOCATED BS947.5 AND STR 26L AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG #149A8103 REV.-

Part: RIVET — BROKEN (FUSELAGE SKIN) · airframe 66,898 hrs · 39,718 cycles

BROKEN EXTERNAL SKIN HEAD RIVETS (6E/A) LOC S-23R BTW BS 360 MORE 5 INCH AT LOWER FUSELAGE / REPLACED RIVETS (6EA) LOC S-23R BTW BS 360 MORE 5' AT LOWER FUSELAGE IAW SRM B737-700 51-40-02. THIS WORK IS DOCUMENTED ON NRC L190893

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 66,898 hrs · 39,718 cycles

CORROSION SUPPORT ZEE LOC BTW BS727 TO BS767 AND STR 25R WL 156.5 AFT CARGO COMPARTMENT / REPLACED SSUPORT ZEE LOCATED BTW BS 727 TO BS 767 AND STR 25-R WL 156.5 AFT CARGO COMPARTMENT DUE TO FOUND OUT LIMITS MEASURE ARE: L=1.813' W=1.404' D=0.013' TOOL USED DIGITAL CALIPER PN: 500-197-30 SN: B16144236 DUE DATE: 18NOV21 ; PART NUMBER USED BAC1496-377 7075 T62 P.O 2020-186462 IAW B737-700 DWG 146A7502 REV- AND SRM 51-10-02 ITEM 9; AND SRM 51-40-02

Part: STRINGER — CORRODED (E/E BAY) · airframe 66,898 hrs · 39,718 cycles

CORROSION STRINGER LOCATED BS 360 TO BS 380 STR 28R WL 148.5 AT EQUIPMENT ELECTRONIC COMP / PERFORMED PERMANENT REPAIR ON STRINGER LOCATED BS 360 TO BS 400 STR 28R WL 148.5 AT EQUIPMENT ELECTRONIC COMPARTMENT I.A.W EA #21-153-00190 REV. IR AND 53-0023-21 REV 0. MATERIAL USED ON STRINGER SECTION 7075-T6 0.036' PO:2020-214270; CHANNEL ANGLE 7075-T6 0.040' P.O:2015-506435. EVALUATED DAMAGE AND FOUND OUT LIMITS I.A.W B737-700 SRM 53-00-03-1A-1 AD1 PARAGRAPH 4 (A;1;B) FIG. 103 DETAIL L

Part: STRINGER — CORRODED (E/E BAY) · airframe 66,898 hrs · 39,718 cycles

CORROSION STRINGER LOCATED BS 360 TO BS 380 STR 27R WL 148.5 AT EQUIPMENT ELECTRONIC COMP / PERFORMED PERMANENT REPAIR ON STRINGER 27R BS 360 TO BS 380 W/148.5 AT EQUIPMENT ELECTRONIC COMP IAW SRM B737-700 53-00-03-2R REPAIR 1 FIG 206 MATERIAL USED ON STRINGER SECTION (-7) 7075-T6 0.032' CHANEL (-2) AND ANGLES (-3) 7075-T6 0.036' AND EVALUATED ALLOWABLE DAMAGE LIMITS AND FOUND OUT LIMITS DUE TO EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM B737-700 53-00-03-1A-1 AD1 PARAGRAPH 4A(1)(B) FIGURE 103 DETAIL C P/O MATERIAL 2020-203301

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 66,898 hrs · 39,718 cycles

CORROSION SUPPORT ZEE LOC BS727 TO BS847 STR 25L WL 156.5 AFT CARGO COMPARTMENT / EVALUATED SUPPORT ZEE LOC BS 727 TO BS847 STR25L WL 156.5 AFT CARGO COMPARTMENT AND FOUND OUT LIMITS IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 STEP 4A(2)(A) FIGURE 103 DETAIL D REPAIRED SUPPORT ZEE IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 FIGURE 203 SHEET 1 AND DWG 146A7500 REV- SRM 51-10-02 FABRICATED SUPPORT ZEE MATERIAL USED BAC 1496-377 7075-T62 PO 2020186462

Part: STRINGER — CRACKED (FWD CARGO) · airframe 66,898 hrs · 39,718 cycles

CRACK STRINGER 26L AT BS 540 FWD CARGO COMPARTMENT / EVALUATED ALLOWABLE DAMAGE LIMITS ON STR 26L BS 540 FWD CARGO COMPARTMENT AND FOUND OUT LIMITS DUE TO CRACK IAW SRM B737-700 53-00-03-1A-1 AND PERFORMED PERMANENT REPAIR ON STRINGER 26L BTW BS500D TO BS 540 IAW B737-700 SRM 53-00-03-2R REPAIR 1 FIGURE 206 MATERIAL USED 7075-T6 0.050' PO MATERIAL 2020-193A61

Part: PANEL — CRACKED (APU AIR INLET) · airframe 66,898 hrs · 39,718 cycles

CRACK AIR INLET PLENUM I/B PANEL ASSEMBLY ON APU COMPARTMENT (1 EA) / REPLACED ANGLE LOC. ON AIR INLET PLENUM I/B PANEL ASSEMBLY ON APU COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DRAWING #353A2010 REV. 'B' PART NUMBER USED 353A2010-18 PO #2021 107162

Part: STRINGER — CRACKED (FWD CARGO) · airframe 66,898 hrs · 39,718 cycles

CRACK STRINGER 25L AT BS 540 FWD CARGO COMPARTMENT / PERFORMED PERMANENT REPAIR ON STRINGER 25L AT BS 540 FWD CARGO COMPARTMENT BTW BS 500D TO BS 540 IAW B737-700 SRM 53-00-03-2R REPAIR 1 FIGURE 206 MATERIAL USED ON STRINGER SECTION (-7) 7075-T6 0.045' CHANNEL (-2) 7075-T6 0.050' ANGLES (-3) 7075-T6 0.050' AND PERFORMED EVALUATED ALLOWABLE DAMAGE LIMITS AND FOUND OUT DUE TO CRACK IAW B737-700 SRM 53-00-03-1A-1 PO MATERIAL 2015-506435

Part: SIDEWALL PANEL — SCRATCHED (CABIN) · airframe 66,898 hrs · 39,718 cycles

SCRATCH ON INNER PANE SIDEWALL PANEL 241 YAW (1EA) AND 241 YEW (2EA) AT PASSENGER CABIN (3 EA) / PERFORMED PERMANENT REPAIR ON STRINGER 25R BTW BS500L TO BS540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIG 206 MATERIAL USED ON STRINGER SECTION (-7) 7075-T6 0.040' CHANNEL (-2) 7075-T6 0.045' ANGLES (-3) 7075-T6 0.045' AND PERFORMED EVALUATE ALLOWABLE DAMAGE DUE TO CRACK AND FOUND OUT OF ALLOWABLE DAMAGE LIMITS IAW B737-700 SRM 53-00-03- 1A-1 PO MATERIAL 2015-506435

Part: SUPPORT ANGLE — CRACKED (AFT CARGO) · airframe 66,898 hrs · 39,718 cycles

CRACK ANGLE - SUPPORT BS 500 D AT LEVEL STRINGER 28L FWD CARGO COMPARTMENT / REPLACED SUPPORT ANGLE LOC. BS 500D AT LEVEL STRINGER 28L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 REV.A FABRICATED FROM ALUMINUM SHEET 2024T3.040

Part: STRINGER — CRACKED (FWD CARGO) · airframe 66,898 hrs · 39,718 cycles

CRACK STRINGER 23L BS 540 FWD CARGO COMPARTMENT / PERFORMED PERMANENT REPAIR ON STRINGER 23L BS540 FWD CARGO COMPARTMENT BTW 500D TO BS 540 IAW B737- 700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED ON STRINGER SECTION (-7) 7075-T6 0.040' CHANNEL (-2) 7075-T6 0.045' ANGLES (-3) 7075-T6 0.045' AND PERFORMED EVALUATED ALLOWABLE DAMAGE LIMITS AND FOUND OUT DUE TO CRACK IAW B737-700 SRM 53-00-03-1A-1 PO MATERIAL 2015-506435

Part: FRAME — CRACKED (CABIN) · airframe 66,898 hrs · 39,718 cycles

CRACK FRAME LOCATED ON BS867 BETWEEN STR8R AND STR9R AT PASSENGER CABIN / REPAIRED FRAME LOCATED ON BS 867 AND BETWEEN STR 8R TO STR 9R AT PASSENGER CABIN IAW EA # 1-A53-12114 REV 5 PARTS NUMBER USED SWA 53100010-003 PO # 2020 -136748 AND SWA 53100010-006 PO# 2020-136749

Part: FRAME — CRACKED (CABIN) · airframe 66,898 hrs · 39,718 cycles

CRACK FRAME LOCATED ON STA312 AND STR5L AT PASSENGER CABIN / PERFORMED REPAIR ON FRAME LOCATED ON STA 312 AND STR 5L AT PASSENGER CABIN IAW SRM B737-700 53-10-07-2R-1 REPAIR 1. DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700 ANGLE FABRICATED FROM 7075-T0 -0.063' PO #2020206794 HEAT TREATED AND CONVERTED FROM T0 TO T62 IAW BAC5602 TEMPERATURE CONTROLED PN P301566300000 SN 112031023 DUE DATE 23/FEB/21 FOR INSPECTION REQUIREMENT SEE TLD #T080633

Part: STRINGER CLIP — CRACKED (PAX CABIN) · airframe 66,898 hrs · 39,718 cycles

CRACK TIE CLIP LOCATED ON STA277 AND STR10R AT PASSENGER CABIN / EVALUATED ALLOWABLE DAMAGE LIMITS OF TIE CLIP LOCATED ON STA STA277 AND STR 10R AT PASSENGER CABIN AND NO FOUND ALLOWABLE FOR CRACK ON SRM MADE TIE CLIP FROM BAC/493-852 P/N 2016 557447 IAW DWG 141A1252 REV - AND REPLACED IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 141A8380 SHEET 2 REV AND DRAWING 141A1110 SHEET 6 REV B

Part: FRAME — CRACKED (CABIN) · airframe 66,898 hrs · 39,718 cycles

CRACK FRAME LOCATED ON BS827 BETWEEN STR8L AND STR9L AT PASSENGER CABIN / REPAIRED FRAME LOCATED ON BS827 BETWEEN STR 8L TO STR 9L AT PASSENGER CABIN IAW EA # 1-A53-12114 REV 5 PARTS NUMBER USED SWA 53100010-003 PO # SW202000865

Part: SUPPORT — CRACKED (BS 400 S26L) · airframe 66,898 hrs · 39,718 cycles

CRACK ANGLE - SUPPORT BS 400 S-26L AFT FACE FWD CARGO COMPARTMENT / REPLACED ANGLE - SUPPORT BS400 S-26L AFT FACE FWD CARGO COMPARTMENT IAW SM B737-700 51-10-02SRM 51-40-02 AND DRAWING #143A7505

Part: GUSSET — CRACKED (BS 500D S21L) · airframe 66,898 hrs · 39,718 cycles

CRACK GUSSET LOCATED BS 500D S-21L FWD CARGO COMPARTMENT / REPLACED GUSSET LOC BS500D -21L FWD CARGO COMPARTMENT IAW B737-700 SPM 51-40-02 AND DWG 143A7902 REV E PART USED 143A9481-9 REPLACED DUE TO NOT FOUND DAMAGE IN SRM B737-700

Part: ANGLE — CRACKED (FWD CARGO) · airframe 66,898 hrs · 39,718 cycles

CRACK ANGLE - SUPPORT BS 440 STR -26L AFT FACE FWD CARGO COMPARTMENT / REPLACED ANGLE-SUPPORT BS440 STR26L AFT FACE FWD CARGO COMPARTMENT IAW SM B737-700 51-10-02 SRM 51-40-02 AND DRAWING #143A7505

Part: SUPPORT ANGLE — CRACKED (VERTICAL STAB) · airframe 66,898 hrs · 39,718 cycles

CRACK LEADING EDGE SUPPORT ANGLE LOCATED INTERNAL AREA AT VERTICAL STABILIZER (1 EA) / REPLACED SUPPORT ANGLE LOCATED INTERNAL AREA AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 176A3001; MATERIAL USED P/N 2024-T0/0.040' P.O 2012-545964. CONVERTED FORM T0 TO T42

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 66,898 hrs · 39,718 cycles

CRACK GUSSET LOCATED BS 500D STR19L FWD CARGO COMPARTMENT / REPLACED GUSSET LOCATED BS 500D STR.19L FWD CARGO COMPARTMENT DUE TO CRACK NOT ALLOWABLE DAMAGE PART NUMBER USED 143A9481-6; P.O 2020 202231 IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG 143A7902 SHEET 21 REV.E MEASURE OF CRACK IS L=1.08'

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 66,898 hrs · 39,718 cycles

CRACK GUSSET LOCATED BS 500D STR 19R FWD CARGO COMPARTMENT / REPLACED GUSSET LOC BS 500 STR 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV E DUE TO NO FOUND ALLOWABLE DAMAGE B737 PART NUMBER USED 143A9481-5

Part: RIB — CRACKED (VERTICAL STAB) · airframe 66,898 hrs · 39,718 cycles

CRACK DORSAL FIN RIB BST 867 AT VERTICAL STABILIZER / REPLACED RIB ON DORSAL FIN BS867 AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DRAWING # 174A0103 REV A

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 66,898 hrs · 39,718 cycles

BROKEN EMERGENCY EXIT COVER ASSEMBLY LOCATION ON LOWERED CELING PANEL AT FWD GALLEY AREA (1 EA).

Part: SUPPORT BRACKET — CRACKED (BS 540) · airframe 66,898 hrs · 39,718 cycles

CRACK SUPPORT BRACKET BODY STATION 540 AT LEVEL LBL 7 KEEL BEAM / REMOVED AND REPLACED SUPPORT BRACKET BODY STATION 540 AT LEVEL LBL 7' KEEL BEAM IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02

Part: RETAINER — CRACKED (RT WG ACCESS PNL) · airframe 66,898 hrs · 39,718 cycles

CRACK ACCESS PANEL 642BB SEAL RETAINER RT WING (1 EA) / REPLACED SEAL RETAINER AND FASTENERS ON ACCESS PANEL 642BB IAW B737-700 SRM 51-10-02 PARAGRAPH 9 SRM 51-40-02 DRAWING 113A9350 SHEET 1 REV F MATERIAL USED RUB STRIP PN 113A9380-1 PO 2021-109727

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 66,898 hrs · 39,718 cycles

CRACK FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT / FABRICATED FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT DUE TO CRACK IS NOT PERMITTED IAW B737-700 AMM 25-52-00-200-806 MATERIAL USED A90RG1W-48144 P.O 2020-180530 IAW B737-700 DWG 453A2610 SHEET 3 REV C

Part: ACCESS PANEL — DAMAGED (BODY FAIRING) · airframe 66,898 hrs · 39,718 cycles

ELONGATED HOLE ACCESS PANEL 194E BODY FAIRING AT LOWER FUSELAGE / REPAIRED ACCESS PANEL 194E BODY FAIRING AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9. TOOLS USED:CALIPER P/N:500-197-30; S/N:A182295- 28; DUE DATE:03 AUG 21;HOT BONDER P/N:HCS9200B; S/N:16122983; DUE DATE:16 DEC 21; SCALE P/N:CL5000; S/N:AE-39883 DUE DATE:03 NOV 21; HOT BONDER P/N:HCS9200B; S/N:15102320; DUE DATE:19NOV21; SCALE P/N:CL5000;S/N:AE-407340;DUE DATE:23JUL21.

Part: POST — DAMAGED (BULKHEAD) · airframe 66,898 hrs · 39,718 cycles

ELONGATED HOLE BULKHEAD PANEL 141QW VERTIVAL POST ON BST 907 AT AFT CARGO COMPARTMENT / REPLACED BULKHEAD VERTICAL POST ON BST 907 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 PN 149A8113Y26 BATCH 202019608900101 (ON ACCESS PANEL 141QW)

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 66,898 hrs · 39,718 cycles

CRACK INSPAR RIB STAB STA 129.50 RIB 5 STIFFENER 3 TO 26.750 INCHES FROM FRONT SPAR LT HORIZONTAL STAB / REPAIRED INSPAR RIB STAB STA 129.50 RIB 5 STIFFENER 3 TO 26.75 INCHES. FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIG 202 SHEET 1. DETAIL A MATERIAL USED KIT 55100003-01; REPAIR DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700

Part: WEB — CRACKED (NR 1 FAN COWL) · airframe 66,898 hrs · 39,718 cycles

CRACK INTERNAL SKIN INBOARD FAN COWL VERTICAL WEB ON ENGINE 1 / REPLACED VERTICAL WEB INTERNAL SKIN FAN COWL ON ENGINE 1 IAW SRM B737-700 51-10-02 ITEM 9; 51-40-02. PART NUMBER USED 314-2259-4 P/O: 2021-100853 IAW CMM GOODRICH AEROSTRUCTURE 71-13-30

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 66,898 hrs · 39,718 cycles

CRACK LEADING EDGE RIB 1 LE STA 78.29 RT HORIZONTAL STAB / REPLACED LEADING EDGE RIB 1 LE STA 78.29 RT HORIZONTAL STAB DUE TO NOT FOUND ALLOWABLE DAMAGE PART NUMBER USED 186A1352-2 PO 2021- 101345 IAW B737-700 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 186A1001 REV B

Part: SLIDE — LOOSE (L1 DDOOR) · airframe 66,787 hrs · 39,652 cycles

FWD ENTRY SLIDE IS HANGING BELOW THE CASING. RE-SECURE FWD ENTRY SLIDE, PER MT-725-61-06. OPERATIONS CHECK GOOD, NO DEFECT NOTED AT THIS TIME.

Part: CHARGER — FAULTED (EMERGENCY LIGHTS) · airframe 66,767 hrs · 39,639 cycles

EMERGENCY EXIT LIGHTS AT AFT ENTRY OH, ONE ON EACH BACK DOOR AND 16 AND 18 RIGHT INOPERABLE. REMOVED AND REPLACED BATTERY CHARGER AND BATTERY PACK M1672, IAW DWG 33500005 & PER AMM 33-51-06.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 66,767 hrs · 39,639 cycles

EMERGENCY EXIT LIGHTS AT AFT ENTRY OH, ONE ON EACH BACK DOOR AND 16 AND 18 RIGHT INOPERABLE. REMOVED AND REPLACED BATTERY CHARGER AND BATTERY PACK M1672, IAW DWG 33500005 & PER AMM 33-51-06.

Part: HOUSING — LOOSE (EMEGENCY LIGHT) · airframe 66,271 hrs · 39,331 cycles

LWS CEILING ANNUNCIATOR LIGHTS FWD GALLEY LOOSE. / REPLACED EMERGENCY EXIT LIGHT HOUSING IN FWD GALLEY CEILING IAW AMM 33-51-01 CL# 49657

Part: BRACKET — LOOSE (R1 DOOR GIRT BAR) · airframe 66,246 hrs · 39,317 cycles

FWD PASSENGER DOOR SLIDE BOX RT GIRT STOW BRACKET LOOSE / SECURED PER SRM 51-40-02

Part: TRUNNION — CORRODED (RT MLG) · airframe 66,019 hrs · 39,159 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING LOWER I/B LUG INNER FACE HAS EVIDENCE OF CORROSION. / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 66,019 hrs · 39,159 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING LOWER O/B LUG BORE HAS EVIDENCE OF CORROSION. / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 66,019 hrs · 39,159 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING LOWER O/B LUG INNER FACE HAS EVIDENCE OF CORROSION. / REPAIRED PER EA 1-A57-3246 REV 11

Part: SIGN — LOOSE (CABIN) · airframe 64,844 hrs · 38,407 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT SIGN LOOSE. / SECURED SIGN IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,599 hrs · 36,950 cycles

RT EMERGENCY LIGHT INOP AT ROW 11. RELAMPED LIGHT PER AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 62,233 hrs · 36,719 cycles

R1 SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 62,089 hrs · 36,636 cycles

RT OVERWING EMERGENCY EXIT SIGN LENS FELL OFF. R&R LENS PER SIP.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 62,041 hrs · 36,607 cycles

EMERGENCY BATTERY PACK M1670 DOES NOT HOLD CHARGE. R&R BATTERY PACK PER AMM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

FORWARD SIDE OF PRESSURE BULKHEAD DOME WEB CORRODED AT BS 1016, BETWEEN BL 0 TO LBL 8.5. REPAIRED DOME WEB PER ER AND EA.

Part: STRIP — BROKEN (AFT CARGO COMPT) · airframe 62,041 hrs · 36,607 cycles

AFT CARGO BAY FLOOR CAPSTRIP IS BROKEN AT BS 947 / LOCATED; DRILLED; DEBURRED; CONVERSION COATED; PRIMERED AND PAINTED NEW AFT CARGO BAY FLOOR CAPSTRIP BS. 947 FROM BAC 1513-286; 2024T3511; LOT # 1325650-1 IAW DWG 453A2611; MM 51-21-99-300-801; MM 51-21-77-370-804; MM 51-21-41-701

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

L1 DOOR UPPER SILL WEB CORRODED BETWEEN BS 329 TO BS 332, LBL 31. REPAIRED SILL WEB IAW ER & EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

STRINGER END FITTING CORRODED AT BS 1016, STR 27R. R&R FITTING PER ER AND EA.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

FORWARD SIDE COMMON TO SPLICE CORRODED AT BS 1016, BETWEEN RBL 5 TO LBL 5. R&R SPLICE IAW SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

STRINGER END FITTING CORRODED AT BS 1016, STR 27L. R&R FITTING PER ER AND EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

L2 DOOR MOPSILL CORRODED BETWEEN BS 967 TO BS 986, LBL 58. R&R MOPSILL IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

R1 DOOR MOP SILL REINFORCEMENT STRAP CORRODED BETWEEN BS 296 TO BS 300, RBL 58. R&R STRAP IAW SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

SHEAR WEB REINFORCEMENT STRAP CORRODED AT BS 1016, RBL 3. R&R STRAP IAW SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

SHEAR WEB REINFORCEMENT STRAP CORRODED AT BS 1016, LBL 3. R&R STRAP IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

R1 DOOR MOP SILL CORRODED BETWEEN BS 318 TO BS 328, RBL 60. R&R MOPSILL IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

R2 DOOR MOP SILL CORRODED BETWEEN BS 947 TO BS 986, RBL 58. R&R R2 DOOR MOP SILL IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

L1 DOOR MOP SILL CORRODED BETWEEN BS 312 TO BS 346, LBL 60. R&R MOP SILL IAW SRM AND DWG.

Part: SHEAR WEB — CORRODED · airframe 62,041 hrs · 36,607 cycles

***CORROSION*** ON L/H 1016 SHEAR WEB LBL 10 WL 208. / SHEAR WEB REPALCED DUE TO R022 ON T895623.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

L1 DOOR LOWER SILL "Z" ANGLE CORRODED BETWEEN BS 317 TO BS 341, LBL 63. R&R "Z" ANGLE IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (COCKPIT) · airframe 62,041 hrs · 36,607 cycles

***CORROSION*** ON COCKPIT THRESHOLD STA 270 WL 208; COMMON TO FWD DURAMAT. / REMOVED AND REPLACED COCKPIT THRESHOLD AT STA 270 IAW AMM 25-27-21-400-801. 57887U 09MAR19 THRESHOLD REPAIRED BY REPLACEMENT OF PART IAW SRM 51-10-02 STEP 9 AND MM 25-27-21-000-801 STEP 2 E (1)(A) THRESHOLD FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02 STEP 4.C.3.

Part: SHEAR WEB — CORRODED · airframe 62,041 hrs · 36,607 cycles

***CORROSION*** ON R/H MOP SILL SHEAR WEB BS 990 AND 1013 RBL 44 WL 208. / LOCATED AND DRILLED R/H MOPSILL SHEAR WEB I.A.W BOEING DWG 147A5730 AND SRM 51-40-05-0G-0; PART TO BE INSTALLED ON COSTUMER CARD T895284.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS 540 TO BS 727B, RBL 45. R&R SEAT TRACK IAW SRM AND DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

R1 DOOR MOP SILL ATTACH ANGLE CORRODED BETWEEN BS 294 TO BS 325, RBL 60. R&R ANGLE IAW SRM & DWG.

Part: PLATE — CRACKED (L/H WING) · airframe 62,041 hrs · 36,607 cycles

LEFT WING TRAILING EDGE WIGGLE PLATE AT ORSS 261 CRACKED / REMOVED AND REPLACED WIGGLE PLATE ON LEFT WING TRAILING EDGE AT ORSS 261 PER SRM 51-40-02-0G-0 AND IPC 57-50-00-30

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS 540 TO BS 727B, LBL 25. R&R SEAT TRACK IAW SRM AND DWG.

Part: RETAINER — CRACKED (LH WING) · airframe 62,041 hrs · 36,607 cycles

LEFT WING TRAILING EDGE ABOVE #1 PYLON AFT TIP CURVED BULB SEAL RETAINER AT FWD. SIDE OF TRANSVERSE WEB CRACKED / REMOVED AND REPLACED LT/WING T/E ABOVE #1 PYLON AFT TIP CULVE BULB SEAL RETAINER AT FWD. SIDE OF TRANSVERSE WEB PER 51-40-02-0G-0. AND IPC 57-50-00-25A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 47 TO RBL 47. REPAIRED FLOORBEAM IAW EA & ER.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS 727D+7 TO BS 887, RBL 45. R&R SEAT TRACK IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS 540 TO BS 727B, RBL 25. R&R SEAT TRACK IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

FLOORBEAM CORRODED AT BS 328, RBL 41. R&R UPPER CHORD IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

L1 DOOR LOWER SILL "L" ANGLE CORRODED BETWEEN BS 317 TO BS 341, LBL 60. R&R "L" ANGLE IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

SHEAR WEB REINFORCEMENT STRAP CORRODED AT BS 1016, RBL 17. R&R STRAP IAW SRM & DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

SHEAR WEB CORRODED AT BS 1016, BETWEEN RBL 9 TO RBL 20. R&R SHEAR WEB IAW SRM AND DWG.

Part: PLATE — CRACKED (RT WING) · airframe 62,041 hrs · 36,607 cycles

RT WING TRAILING EDGE WIGGLE PLATE ABOVE NR 6 FLAP TRACK CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS 727B TO BS 887, LBL 45. R&R SEAT TRACK IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

CRACKED INTERCOSTAL BS 312-328 RBL31 WL208. / REMOVED CRACKED INTERCOSTAL; LOCATED & DRILLED REPLACEMENT INTERCOSTAL IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0. INTERCOSTAL AT BS 312-328 RBL 31 WL 208 WILL BE INSTALLED ON CARD # T895257 SA-M 326 A 1249608 ITEM #3.

Part: SKIN — DENTED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

FUSELAGE SKIN DENT AT BS 380+10, STR 27L. REPAIRED SKIN PER ER AND EA.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

AFT CARGO BAY SHIELD CORRODED BETWEEN BS 767 TO BS 794, RBL 23. R&R SHIELD IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 787 TO BS 807, RBL 6. R&R INTERCOSTAL PER SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

AFT CARGO BAY FLOOR SPLICE STRAP CORRODED AT BS 887, BETWEEN RBL 10 TO LBL 10. R&R SPLICE STRAP PER SRM.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 460 TO BS 500D, LBL 23. REPAIRED SUPPORT IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

AFT CARGO BAY INTERCOSTAL CORRODED AT BS 927+2, RBL 3. R&R INTERCOSTAL PER SRM & DWG.

Part: MOUNT — CORRODED (FWD CARGO BAY) · airframe 62,041 hrs · 36,607 cycles

FWD CARGO BAY AIR PHONE ANTENNA MOUNT TRAY BETWEEN BS500 AND BS500A BLO WL150 HAS CORROSION / REMOVED AND REPLACED FWD CARGO BAY AIR PHONE ANTTENNA MOUNT TRAY BETWEEN BS 500 AND 500A BL 0 WL 150 IAW SRM 51-40-02 AND DWG 143A3233.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 727 TO BS 847, LBL 23. R&R SUPPORT IAW SRM.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

FORWARD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 500A TO BS 500D, RBL 23. R&R SUPPORT PER SRM.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 727 TO BS 767, RBL 23. R&R SUPPORT PLATE PER SRM.

Part: SPLICE STRAP — CORRODED (AFT CARGO BAY) · airframe 62,041 hrs · 36,607 cycles

AFT CARGO BAY FLOOR SPLICE STRAP HAS CORROSION BS772 RBL10 TO LBL10 WL156 / RECEIVED NEW ACB FLOOR SPLICE STRAP FOR BS 772 ON PO # 728946. PART WILL BE INSTALLED ON CUST. CARD # JPANEL-141-CLOSE

Part: SPLICE STRAP — CORRODED (AFT CARGO BAY) · airframe 62,041 hrs · 36,607 cycles

AFT CARGO BAY FLOOR SPLICE STRAP HAS CORROSION BS727D RBL10 TO LBL10 WL156 / RECEIVED NEW ACB FLOOR SPLICE STRAP FOR B.S 727D ON PO# 724358 PART WILL BE INSTALLED ON CUST. CARD # JPANEL-141-CLOSE

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

FORWARD CARGO BAY SHIELD AFT OF CARGO DOOR CORRODED BETWEEN BS 492 TO BS 500A, RBL 23. R&R SHIELD PER SRM AND DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 62,041 hrs · 36,607 cycles

R1 DOOR NR 4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. R&R BEAM PER R.O.

Part: LIGHT — BROKEN (CABIN) · airframe 62,041 hrs · 36,607 cycles

EMERGENCY EXIT LIGHT BROKEN ON SIDEWALL PANEL 242YAW. R&R LIGHT IAW AMM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 62,041 hrs · 36,607 cycles

R1 DOOR NR 5 (UPPER) BEAM CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. R&R DOOR PER RO.

Part: LIGHT — BROKEN (CABIN) · airframe 62,041 hrs · 36,607 cycles

EMERGENCY EXIT LIGHT BROKEN ON SIDEWALL PANEL 231YHW. R&R LIGHT IAW AMM.

Part: HOUSING — CRACKED (EMERGENCY EXIT) · airframe 62,041 hrs · 36,607 cycles

RT OVERWING EXIT DOOR LOWER HANDLE STRAP HOUSING CRACKED. R&R HANDLE STRAP HOUSING IAW AMM.

Part: HOUSING — CRACKED (EMERGENCY EXIT) · airframe 62,041 hrs · 36,607 cycles

LT OVERWING EXIT DOOR LOWER HANDLE STRAP HOUSING CRACKED. R&R HANDLE STRAP HOUSING IAW AMM.

Part: HOUSING — DAMAGED (CABIN) · airframe 62,041 hrs · 36,607 cycles

EXIT LIGHT HOUSING DAMAGED COMMON TO CEILING PANELS ON OVERWING EMERGENCY AREA. R&R LIGHT HOUSING PER AMM.

Part: FAIRING — CRACKED (LWR FUSELAGE) · airframe 62,041 hrs · 36,607 cycles

WING TO BODY FAIRING #195CL CRACKED AFT LOWER CORNER / REPAIRED DAMAGE TO WING TO BODY FAIRING #195CL LOWER CORNER IAW SRM 51-70-04-2R-6. 57885U 02-22-19

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,041 hrs · 36,607 cycles

RT OVERWING LOWER EMERGENCY EXIT LIGHT BULBS BURNED OUT. R&R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,041 hrs · 36,607 cycles

G4 GALLEY EXIT LIGHT BULBS BURNED OUT. R&R LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,041 hrs · 36,607 cycles

FORWARD LAV, EMERGENCY EXIT LIGHT BULBS BURNED OUT. R&R LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,041 hrs · 36,607 cycles

LT OVERWING EXIT, LOWER EMERGENCY EXIT LIGHT BULBS BURNED OUT. R&R BULB IAW AMM.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 60,709 hrs · 35,747 cycles

RT VAPOR BARRIER WEB CRACKED AT BS 663, RBL 18. REPAIRED BARRIER IAW SRM.

Part: STIFFENER — CRACKED (WHEEL WELL RH) · airframe 60,709 hrs · 35,747 cycles

REAR SPAR STIFFENER CRACKED AT STA.663 RBL 25 WL 145 (PART# 111A1308-9 SI#7531210) / REMOVED CRACKED REAR SPAR STIFFNER @ STA 663 RBL 25 WL 145 INSTALLED NEW STIFFNER P/N 7531949 PO# 703593 IAW SRM 51-40-02-G-0 DWG 111A1000 81146U 8/29/18

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 60,709 hrs · 35,747 cycles

VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, RBL 9. REPAIRED ANGLE IAW EA.

Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 60,709 hrs · 35,747 cycles

RT LOWER VAPOR BARRIER CRACKED AT BS 663. REPAIRED BARRIER IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 60,709 hrs · 35,747 cycles

LT MAIN LANDING GEAR UPPER BEADED PRESSURE DECK CRACKED BETWEEN BS 663.75 TO BS 675, BETWEEN LBL 38 TO LBL 60. REPAIRED DECK PER EA AND ER.

Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 60,709 hrs · 35,747 cycles

LT LOWER VAPOR BARRIER CRACKED AT BS 663. R&R BARRIER IAW SRM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 58,334 hrs · 34,230 cycles

AFT GALLEY EMERGENCY EXIT LIGHT SWITCH MISSING COVER. / INSTALLED COVER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 56,926 hrs · 33,349 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 55,523 hrs · 32,529 cycles

AFT CARGO COMPARTMENT TRACK CRACKED BETWEEN BS 727E TO BS 755, RBL 13.84. R&R TRACK IAW SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 55,523 hrs · 32,529 cycles

FORWARD GALLEY AREA EMERGENCY EXIT LENS BROKEN. R&R LENS IAW AMM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 55,523 hrs · 32,529 cycles

AFT CARGO COMPARTMENT TRACK CORRODED BETWEEN BS 787 TO BS 867, RBL 13.84. REPAIRED TRACK IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,523 hrs · 32,529 cycles

CENTER WING BOX LOWER BULKHEAD CHORD CRACKED AT BS 540, STR 22R. REPAIRED CHORD IAW EA.

Part: FAIRING — CRACKED (LT TE FLAP TRACK) · airframe 55,523 hrs · 32,529 cycles

LEFT WING FLAP TRACK FAIRING 544BB CRACKED. REPAIRED THE FAIRING IAW SRM AND EA.

Part: SKIN — CRACKED (LT WING) · airframe 55,523 hrs · 32,529 cycles

LT WING LEADING EDGE SKIN SLAT ACTUATOR RIB CRACKED AT SLAT STATION 202.45. REPAIRED SKIN IAW SRM.

Part: SIGN — FADED (EMERGENCY LIGHT) · airframe 55,344 hrs · 32,422 cycles

RIGHT OVERWING EXIT LENS FADED. R & R EXIT SIGN IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 54,753 hrs · 32,067 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW DWG.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 54,746 hrs · 32,060 cycles

FUEL CROSSFEED VALVE LIGHT DOES NOT DIM AFTER BEING POSITIONED TO OPEN. MANAGED 400LB FUEL IMBALANCE WITH THROTTLES. R&R CROSSFEED VALVE ACTUATOR IAW MM.

Part: HOOK — BROKEN (L1 DOOR) · airframe 54,501 hrs · 31,910 cycles

L1 DOOR ESCAPE SLIDE AFT GIRT BAR HOOK GIRT BROKEN. R & R GIRT BAR HOOK IAW SIP.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 54,068 hrs · 31,655 cycles

R2 DOOR EMERGENCY EVACUATION SLIDE APPEARS LOOSE. SECURED THE SLIDE IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 53,032 hrs · 31,028 cycles

CEILING OVERWING EMER EXIT SIGN LIGHT LOOSE. SECURED SIGN IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 50,309 hrs · 29,435 cycles

RIGHT EXIT LIGHT INDICATOR ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY AMM.

Part: PANEL — CRACKED (RT WING) · airframe 49,503 hrs · 28,987 cycles

RIGHT WING LOWER PANEL BEAM ASSEMBLY FOR PANEL 661AB CRACKED. REPAIRED PANEL IAW DWG & SRM.

Part: FRAME — CRACKED (LT HORIZ STAB) · airframe 49,503 hrs · 28,987 cycles

LEFT HORIZONTAL STABILIZER LOWER FRAME INBD FLANGE CRACKED AT STATION 101.90. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,503 hrs · 28,987 cycles

FORWARD SEAT TRACK FLANGE BOTH OTBD HOLES & INBD AFT HOLE CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,503 hrs · 28,987 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,503 hrs · 28,987 cycles

FORWARD SEAT TRACK FLANGE BOTH OTBD HOLES & INBD AFT HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,503 hrs · 28,987 cycles

AFT SEAT TRACK, OTBD FLANGE HOLE CRACKED AT BS 727B, RBL 24.75. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,503 hrs · 28,987 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,503 hrs · 28,987 cycles

FORWARD SEAT TRACK FLANGE OTBD AFT HOLE & BOTH INBD HOLES CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 49,503 hrs · 28,987 cycles

RIGHT NR 3 WINDOW FRAME E - F POST 2ND & 3RD HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 49,503 hrs · 28,987 cycles

RIGHT HORIZONTAL STABILIZER, LE, 3RD RIB FROM INBD END CRACKED. R & R RIB IAW SRM.

Part: DOUBLER — CRACKED (LT MLG WW) · airframe 49,503 hrs · 28,987 cycles

MAIN WW VERTICAL PRESS WEB DOUBLER CRACKED AT BS 663, BETWEEN LBL 34 - 41. REPAIRED DOUBLER IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 49,503 hrs · 28,987 cycles

RIGHT HORIZONTAL STABILIZER, LE, 4TH RIB FROM INBD END CRACKED. R & R RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 49,503 hrs · 28,987 cycles

RIGHT HORIZONTAL STABILIZER RIB STATION 92.7, THIRD SUPPORT RIB AFT FROM FRONT SPAR CRACKED. REPAIRED RIB IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 49,503 hrs · 28,987 cycles

LEFT NR 3 WINDOW FRAME E - F POST LOWER 3 HOLE CRACKED. REPAIRED POST IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 49,503 hrs · 28,987 cycles

RIGHT HORIZONTAL STABILIZER RIB STATION 92.7, SECOND SUPPORT RIB AFT FROM FRONT SPAR CRACKED. REPAIRED RIB IAW SRM.

Part: COVER — CRACKED (EMERGENCY EXIT) · airframe 49,379 hrs · 28,916 cycles

LEFT EMER EXIT HANDLE COVER CRACKED. R & R COVER IAW AMM.

Part: LENS — UNSECURE (CABIN) · airframe 49,261 hrs · 28,856 cycles

L1 DOOR LOWER EXIT IDENTIFIER LIGHT ASSEMBLY LENS FELL OFF. R & R LIGHT ASSEMBLY IAW MM.

Part: COVER — MISSING (EVAC SLIDE) · airframe 47,117 hrs · 27,663 cycles

R2 DOOR EMER EVAC SLIDE PULL HANDLE COVER MISSING. INSTALLED COVER IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 46,708 hrs · 27,433 cycles

FORWARD ENTRY EMER EXIT LIGHT BROKEN. R & R LIGHT IAW SIP.

Part: DOOR — DAMAGED (CABIN) · airframe 46,471 hrs · 27,290 cycles

L1 DOOR LOWER ACTUATOR BROKEN DOOR SKIN DAMAGED. REPAIRED DOOR IAW EA.

Part: PROXIMITY SENSOR — FAULTY (E&E BAY) · airframe 43,650 hrs · 25,623 cycles

IMMEDIATELY AFTER ROTATION & AFTER RAISING THE LANDING GEAR LEVER UP, NOTICED MIN SPEED TAPE. UPPER LIMIT INCREASE TO WITHIN 5 KNOTS OF CURRENT SPEED & V2 + 20 LIMITING PITCH TO 10 DEGREES & 12 DEGREES DUE TO PITCH LIMIT INDICATOR BETWEEN 12 DEGREES & 15 DEGREES. R&R NR 2 SLAT INBD PROX SENSOR IAW AMM.

Part: FAN — FAULTY (AC BAY) · airframe 42,875 hrs · 25,162 cycles

IN DESCENT AROUND FL 200 SMELLED ACRID ODOR LIKE OVERHEATED ELEC EQUIP. REMOVED AND REPLACED LEFT WATER SEPARATOR BAG, HEPA FILTER, AND REPLACED RECIRCULATION FAN PER MM.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 42,747 hrs · 25,079 cycles

LEFT PACK OIL ODOR IN FLIGHT DECK. REMOVED AND REPLACED SOCKS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,733 hrs · 25,065 cycles

RIGHT OVERWING FWD EMERGENCY EXIT LIGHT BULB INOP. REMOVED AND REPLACED BULB PER AMM.

Part: LENS — BROKEN (CABIN) · airframe 42,733 hrs · 25,065 cycles

L2 DOOR AFT EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS IAW SOPM.

Part: PANEL — CRACKED (LT HORIZ STAB) · airframe 42,733 hrs · 25,065 cycles

LEFT HORIZONTAL STABILIZER UPPER GAP COVER PANEL ASSY 333 AT SHARK FIN CRACKED. REMOVED AND REPLACED PANEL ASSY IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 22 TO RBL 34. REPAIRED FLOORBEAM IAW SRM.

Part: STIFFENER — CRACKED (VERTICAL STAB) · airframe 42,733 hrs · 25,065 cycles

VERTICAL FIN TERMINAL FITTING ASSY LOWER CROSS STIFFENER CRACKED AT BS 1018 ON BOTH ENDS. REMOVED AND REPLACED STIFFENER IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

FLIGHT DECK RIGHT NR 1 WINDOW FRAME CRACKED IN UPPER OUTBOARD CORNER INTERNAL SURFACE. REPAIRED FRAME CRACK IAW ER & EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663.75, RBL 43. REMOVED AND REPLACED WEB IAW SRM.

Part: PANEL — CRACKED (RT HORIZ STAB) · airframe 42,733 hrs · 25,065 cycles

RIGHT HORIZONTAL STABILIZER UPPER GAP COVER PNL ASSY 343AT SHARK FIN CRACKED. REMOVED AND REPLACED PANEL ASSY IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

FORWARD CARGO BAY INTERCOSTAL ANGLE ON AFT SIDE OF FRAME CRACKED AT BS 500B, LBL 24. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LBL 22. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

VERTICAL INTERCOSTAL CORRODED BETWEEN BS 787 TO BS 792, RBL 19. REMOVED AND REPLACED STRIP IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

FLOOR SUPPORT UPPER SURFACE CORRODED BETWEEN BS 312 TO BS 328, LBL 12. REMOVED AND REPLACED FLOOR SUPPORT PER DWG.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 42,733 hrs · 25,065 cycles

R1 DOOR INNER SURFACE FRAME CRACKED AT BS 294, RBL 60. REPAIRED FRAME IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

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

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 42,733 hrs · 25,065 cycles

LEFT WING T/E COVE SEAL SUPPORT ANGLE CRACKED ABOVE NR 1 PYLON AFT TIP. REMOVED & REPLACED WEB ASSY IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 42,733 hrs · 25,065 cycles

LEFT WING UPPER T/E PANEL SUPPORT ANGLE CRACKED ABOVE NR 1 PYLON AFT TIP. REMOVED & REPLACED ANGLE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

SUPPORT ANGLE CORRODED BETWEEN BS 297 TO BS 324, RBL 63. REMOVED AND REPLACED ANGLE PER SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

FLOOR PANEL 242UF LOWER SKIN O/B EDGE DELAMINATED. REPAIRED FLOOR PANEL PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

FLOORBEAM CORRODED AT BS 294, BETWEEN LBL 7 AND LBL 11. REPAIRED BEAM IAW ER & EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 42,733 hrs · 25,065 cycles

CARGO TRACK CORRODED BETWEEN BS 787 TO BS 847, RBL 14. REPAIRED CARGO TRACK IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. REMOVED AND REPLACED INTERCOSTAL IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

GIRT BAR FWD FITTING CORRODED BS 312, LBL 60. REMOVED AND REPLACED FITTING IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

FLOORBEAM CORRODED AT BS 312, LBL 11. REPAIRED FLOORBEAM IAW ER AND EA.

Part: FLOOR PANEL — CRUSHED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

FLOOR PANEL 241ADF CRUSHED CORE ON I/B EDGE. REPAIRED FLOOR PANEL IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

GIRT BAR AFT FITTING CORRODED AT BS 344, LBL 63. REMOVED AND REPLACED FITTING IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

FRAME WEB CRACKED AT BS 440, STR 8R. REPAIRED FRAME IAW EA.

Part: SILL — CORRODED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

MOPSILL CORRODED BETWEEN BS 294 TO BS 340, BETWEEN RBL 57 TO RBL 63. REMOVED AND REPLACED MOPSILL PER SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

ANGLE CRACKED AT BS 500C, RBL 24. REMOVED AND REPLACED ANGLES IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

FWD CARGO BAY SUPPORT WEB AT BS 500D, STR 19R CRACKED. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

FLOORBEAM CORRODED BETWEEN BS 986, RBL 34-43. REPAIRED BEAM IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 42,733 hrs · 25,065 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED I/B SIDE OF RIB STAB STA 129.50 7.75 - 9 FROM REAR SPAR. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 42,733 hrs · 25,065 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT REAR SPAR STAB STA 96.50-98.75. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 42,733 hrs · 25,065 cycles

RIGHT WHEEL WELL CEILING PRESSURE DECK CRACKED AT BS 663, RBL 42. REPAIRED BULKHEAD IAW ATS ER.

Part: NUT PLATE — CORRODED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

NUT PLATE RETAINING STRIP BELOW FLOOR SUPPORT CORRODED AT BS 795, RBL 21. REMOVED AND REPLACED NUT PLATE STRIP DWG.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 42,733 hrs · 25,065 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED I/B SIDE OF RIB STAB STA 147.90 7.5 - 8.25 FROM REAR SPAR. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 30 TO LBL 41. REMOVED AND REPLACED FLOORBEAM PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

FWD CARGO BAY SUPPORT WEB AT BS 500D, STR 19L CRACKED. REMOVED AND REPLACED WEB IAW SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

STRAP CORRODED AT BS 1023, RBL 2. REMOVED AND REPLACED STRAP PER DWG AND SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 42,733 hrs · 25,065 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED I/B SIDE OF RIB STAB STA 138.70 15.5-16 FROM FRONT SPAR. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 42,733 hrs · 25,065 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT REAR SPAR STAB STA 97-99. REPAIRED SKIN PER SRM.

Part: FILLER — CRACKED (FUSELAGE) · airframe 42,733 hrs · 25,065 cycles

POWER DOOR 114 AR AFT LATCH STRIKER FILLER CRACKED. REMOVED & REPLACED FILLER IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 42,733 hrs · 25,065 cycles

LEFT WING NR 1 SLAT CRACKED ON LOWER SKIN AT ACTUATOR ATTACH POINT I/B SIDE. REPAIRED SKIN IAW SRM.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 41,720 hrs · 24,437 cycles

LEFT HORIZONTAL STABILIZER LOWER FORWARD SLIDING SEAL CRACKED. REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER LOWER FORWARD SLIDING SEAL REF SRM 51-40-02 AND M/M.

Part: CAP — MISSING (CABIN) · airframe 41,720 hrs · 24,437 cycles

CABIN EMERGENCY LIGHT TRACK AT ROW 1 END CAP MISSING. REPLACED CABIN EMERGENCY LIGHT TRACK END CAP AT ROW 1 PER M/M.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 41,720 hrs · 24,437 cycles

LEFT MLG W/W FWD BULKHEAD VAPOR BARRIER CRACKED DIAGONALLY 10 INCHES LONG BETWEEN LBL 45.64 AND LBL 31.83 ANGLES. REPAIRED CRACK IN MLG W/W FWD BULKHEAD VAPOR BARRIER PER EA 1-A53-3376.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 41,720 hrs · 24,437 cycles

LEFT MLG W/W FWD BULKHEAD WALL MOST LOWER ANGLE STIFFENER CRACKED AT THE LOWER END 3IN LONG AT LBL 24.92 (INBD AND BELOW A-SYS RETURN FILTER). REMOVED AND REPLACED THE LOWER ANGLE STIFFENER PER SRM 51-10-02

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,720 hrs · 24,437 cycles

PASSENGER CABIN FLOORBOARD SUPPORT BETWEEN BS 312-328 LEFT OF CENTER 50 INCHES IS CRACKED AT CENTER FASTNER HOLE. REMOVED AND REPLACED FLOOR INTERCOSTAL PER SRM 51-10-02 & 51-40-02.

Part: LENS — MISSING (CABIN) · airframe 41,720 hrs · 24,437 cycles

CABIN EMERGENCY LIGHT AT ROW 1 INOP AND LIGHT LENS MISSING. REPLACED CABIN EMERGENCY LIGHT AT ROW 1 AND LIGHT LENS PER M/M.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 41,720 hrs · 24,437 cycles

LEFT MLG W/W FWD BULKHEAD VAPOR BARRIER CRACKED 4 INCHES LONG BEHIND LOWER ANGLE STIFFENER LBL 24.92 (INBD AND BELOW A-SYS RETURN FILTER). REPAIRED CRACK IN FWD BULKHEAD VAPOR BARRIER PER EA 1-A53-3376.

Part: COVER — BROKEN (CABIN) · airframe 41,381 hrs · 24,210 cycles

LEFT FWD EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,194 hrs · 24,095 cycles

LEFT EEPLS INOP AT ROW 2. RELAMPED EEPLS PER M/M.

Part: POST — CRACKED (FUSELAGE) · airframe 47,277 hrs · 27,754 cycles

L1 OTBD WINDOW POST CRACKED. REPAIRED POST IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 40,552 hrs · 23,694 cycles

LEFT WINDOW POST FRAME CRACKED BETWEEN L1 AND L2 WINDOW. REPAIRED FRAME PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 39,598 hrs · 23,117 cycles

EXIT SIGN NEXT TO R1 DOOR BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 38,936 hrs · 22,730 cycles

L1 DOOR EMERENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 38,392 hrs · 22,400 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,014 hrs · 22,158 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 5. RELAMPED PER MM.

Part: VALVE — LEAKING (LT WING) · airframe 36,572 hrs · 21,294 cycles

ABORTED TAKEOFF/DECLARED EMERGENCY. TOWER REPORTED FUEL STREAMING FROM RIGHT WING, FLIGHT ATTENDANTS CONFIRMED LEAK. COMPLIED WITH LEAK CHECKLIST, BY TURNING OFF CENTER FUEL PUMPS AND LEAK STOPPED. REMOVED AND REPLACED LT WING FUEL SHUTOFF VALVE AND CENTER TANK SCAVENGE JCT PUMP PER AEROSTREAM WORK CARD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,248 hrs · 21,126 cycles

DURING SCHEDULED OTS CHECK, FOUND EEPLS INOP BETWEEN ROW 11 TO ROW 12. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 36,248 hrs · 21,126 cycles

DURING SCHEDULED OTS CHECK FOUND, LT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED STABILIZER PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 36,246 hrs · 21,125 cycles

DURING SCHEDULED CV CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 193-90. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 36,246 hrs · 21,125 cycles

DURING SCHEDULED CV CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 184.70. REPAIRED SKIN PER EA.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,004 hrs · 20,981 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER NR 2 CRACKED. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,004 hrs · 20,981 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX HORIZONTAL STIFFENER NR 10 CRACKED. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,004 hrs · 20,981 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX HORIZONTAL STIFFENER NR 7 CRACKED. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,004 hrs · 20,981 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX HORIZONTAL STIFFENER NR 4 CRACKED. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,004 hrs · 20,981 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX HORIZONTAL STIFFENER NR 9 CRACKED. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,004 hrs · 20,981 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER NR 3 CRACKED. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,004 hrs · 20,981 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX HORIZONTAL STIFFENER NR 5 CRACKED. REMOVED AND REPLACED STIFFENER PER SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 35,148 hrs · 20,472 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — FRAYED (R2 DOOR) · airframe 35,148 hrs · 20,472 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT FRAYED. REMOVED AND REPLACED SLIDE PER MT.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 34,598 hrs · 20,148 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 34,598 hrs · 20,148 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,213 hrs · 19,311 cycles

EEPLS INOP AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 33,119 hrs · 19,255 cycles

R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 33,046 hrs · 19,210 cycles

EEPLS LOOSE AT ROW 1. SECURED PER MM.

Part: COVER — CRACKED (CABIN) · airframe 32,874 hrs · 19,102 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 8 AND ROW 9. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 32,228 hrs · 18,700 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,228 hrs · 18,700 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 31,840 hrs · 18,451 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED AT ROW 8. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 31,840 hrs · 18,451 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED AT ROW 9. REMOVED AND REPLACED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 31,745 hrs · 18,393 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,625 hrs · 18,325 cycles

FWD CABIN EEPLS INOP. RELAMPED PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 30,709 hrs · 17,776 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOLDER BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 30,709 hrs · 17,776 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 29,782 hrs · 17,183 cycles

L2 DOOR EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM.

Part: LENS — CRACKED (CABIN) · airframe 29,714 hrs · 17,144 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD LAV AFT FACE WALL, EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 28,118 hrs · 16,154 cycles

MID CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: COVER — MISSING (R2 DOOR) · airframe 27,404 hrs · 15,718 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT SLIDE VIEW WINDOW COVER MISSING. REMOVED AND REPLACED COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,075 hrs · 15,491 cycles

EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,744 hrs · 15,289 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — WORN (RT WING) · airframe 26,312 hrs · 15,004 cycles

DURING SCHEDULED 6Y CHECK, FOUND RT WING LOWER SKIN WORN OUTBOARD OF PYLON AFT END. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 26,291 hrs · 14,988 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 26,291 hrs · 14,988 cycles

DURING SCHEDULED HC2 CHECK, LEFT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 26,291 hrs · 14,988 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 26,291 hrs · 14,988 cycles

DURING SCHEDULED HC2 CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,295 hrs · 14,399 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 2 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 24,153 hrs · 13,699 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 22,538 hrs · 12,736 cycles

DURING SCHEDULED 6Y CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED. R&R SLAT PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,538 hrs · 12,736 cycles

DURING SCHEDULED 6Y CHECK, FOUND FLOORBEAM CORRODED BETWEEN BS 767 AND BS 787, RBL 14. REPAIRED FLOOR BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 22,538 hrs · 12,736 cycles

DURING SCHEDULED 6Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: COVER — LOOSE (CABIN) · airframe 21,983 hrs · 12,397 cycles

EEPLS COVER LOOSE AT ROW 3 ABC. SECURED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 21,896 hrs · 12,354 cycles

FWD CABIN EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,851 hrs · 12,331 cycles

DURING SCHEDULED SPV CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 DEF. REMOVED AND REPLACED LIGHT BULB ER MM.

Part: LENS — LOOSE (CABIN) · airframe 21,684 hrs · 12,234 cycles

EEPLS LENS LOOSE AT FWD END. SECURED LENS PER MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 21,662 hrs · 12,224 cycles

EEPLS LIGHT COVER BROKEN AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 18,540 hrs · 10,529 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 16,958 hrs · 9,490 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD LT EEPLS TRACK LENS COVER MISSING. INSTALLED LENS COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 16,695 hrs · 9,345 cycles

EEPLS TRACK COVER LOOSE AT FWD END. SECURED COVER PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 16,605 hrs · 9,298 cycles

FWD LOWER EMERGENCY EXIT LIGHT LENS COVER MISSING. INSTALLED LENS COVER PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 16,541 hrs · 9,262 cycles

EEPLS TRACK LENS MISSING AT FWD END. INSTALLED LENS PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 16,122 hrs · 9,006 cycles

EEPLS TRACK LENS COVER LOOSE AT FWD END. SECURED COVER PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 15,920 hrs · 8,891 cycles

EEPLS STRIP INOP AT ROW 11 TO ROW 17. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — BROKEN (CABIN) · airframe 14,178 hrs · 7,927 cycles

EEPLS TRACK LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 14,086 hrs · 7,873 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,377 hrs · 6,908 cycles

FWD RT EEPLS LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,866 hrs · 6,635 cycles

DURING SCHEDULED RON, FOUND EEPLS AT ROW 1 ABC, INOP. RELAMPED EEPLS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,844 hrs · 6,623 cycles

DURING SCHEDULED RON, FOUND EEPLS AT ROW 1 ABC INOP. RELAMPED EEPLS PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 11,788 hrs · 6,592 cycles

L1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 9,278 hrs · 5,218 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS FLOOR TRACK CRACKED AT ROWS 3, 12, 16 AND 17. REMOVED AND REPLACED EEPLS FLOOR TRACK PER MM.

Part: EEC — FAULTY (NR 1 ENGINE) · airframe 8,798 hrs · 4,975 cycles

NR 1 ENG WOULD NOT REACH CLIMB POWER, THROTTLE LEVER HAD 4 KNOBS AHEAD OF NR 2 ENG. RECYCLED NR 1 EEC AND NR 1 ENG OPERATED NORMALLY. C/W BITE CK AND REMOVED AND REPLACED NR 1 EEC PER MM.

Part: HMU — FAULTY (NR 1 ENGINE) · airframe 8,778 hrs · 4,963 cycles

DURING TAKEOFF, NR 1 ENG POWER SURGE INDICATION, REDUCED POWER AT CLIMB ALTITUDE OF 13000 FT, NR 1 ENG STABILIZED. REMOVED AND REPLACED NR 1 ENG HMU AND T12 SENSOR PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 8,170 hrs · 4,608 cycles

EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN ARMED POSITION. CHARGED BATTERY PACKS PER MM.

Part: SLIDE — DISLODGED (AFT SERVICE DOOR) · airframe 7,887 hrs · 4,444 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER WHEN OPENING THE DOOR. REINSTALLED SLIDE PER MM.

Part: STRAP — LOOSE (FLASHLIGHT) · airframe 3,829 hrs · 2,178 cycles

EMERGENCY FLASHLIGHT STRAP LOOSE IN FWD GALLEY. SECURED STRAP PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 2,360 hrs · 1,332 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM..

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 1,375 hrs · 788 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.