N738CB

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 79,362 hrs · 47,107 cycles

EMERGENCY LIGHT BATTERY PACKS AT M1674, M1675, AND M1668 FAILED A CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACKS IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 79,362 hrs · 47,107 cycles

SUPPLEMENTAL INFORMATION: L/H HORIZONTAL FORWARD UPPER SLIDER SEAL IS CRACKED<[01] REMOVED AND REPLACED L/H HORIZONTAL STABILIZER FORWARD UPPER SLIDER SEAL PER AMM 53-31-31.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,362 hrs · 47,107 cycles

EMERGENCY LIGHT BATTERY PACKS AT M1674, M1675, AND M1668. REMOVED AND REPLACED EMERGENCY BATTERY PACKS IAW AMM 33-51-06. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 79,362 hrs · 47,107 cycles

EMERGENCY LIGHT BATTERY PACKS AT M1674, M1675, AND M1668. REMOVED AND REPLACED THE BATTERY PACKS IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 79,362 hrs · 47,107 cycles

EMERGENCY LIGHT BATTERY PACKS AT POSITION M1674; M1675; AND M1668 . BATTERY PACKS NEED ADD TO LIST. / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT POSITIONS M1674; M1675; AND M1668 IAW B737-700 AMM 33-51-06. OPS CHECK GOOD.

Part: FLOOR PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 79,241 hrs · 47,031 cycles

RAMP INFORMED US OF TWO CRACKS IN FLOOR OF AFT BAGGAGE COMPARTMENT. / [01] REMOVED AND REPLACE CARGO FLOOR LINER PER AMM. 25-52-01

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 77,681 hrs · 45,980 cycles

OVERWING EMERGENCY EXIT DOOR LIGHT LIGHT INOP / [01] RELAMPED RH OVERWING EMER EXIT DOOR LIGHT IAW AMM 33-51-01

Part: LIGHT — INOPERATIVE · airframe 76,939 hrs · 45,511 cycles

OVERHEAD LIGHT IN CENTER ISLE OVER LAST ROW 24 / [01] RELAMPED OVERHEAD LIGHT OVER ROW 24 IAW 33-21-12

Part: LIGHT — MISSING · airframe 76,607 hrs · 45,303 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING ; / [01] INSTALLED LENS PER SIP.

Part: SIGN — INCORRECT (CABIN) · airframe 76,114 hrs · 45,019 cycles

SUPPLEMENTAL INFORMATION: LEFT AFT ENTRY DOOR EMERGENCY EXIT SIGH POIN TO THE WRONG DIRECTION ; / [01] REMOVED AND REPLACED PER SIP; [02] ENTERED ON LOG PAGE 1714474; [03] CERTIFY CORRECTION

Part: PANEL — ELONGATED (FUSELAGE) · airframe 76,084 hrs · 45,002 cycles

ON PNL 193D AFT RIGHT O/B HOLE ELONGATED ; / [01] REFERENCE FAULT TTG8Q009BV54 AND EA 21-153-03397 FOR CORRECTIVE ACTION

Part: PANEL — ELONGATED (FUSELAGE) · airframe 76,084 hrs · 45,002 cycles

ON PNL 193D AFT LEFT O/B HOLE IS ELONGATED ; / [01] REPAIRED PANEL PER EA21-153-03397

Part: TRANSMITTER — FAULTY (E&E BAY) · airframe 75,839 hrs · 44,864 cycles

FLAPS WOULD NOT EXTEND BEYOND 25 DEGREES WHEN 30 DEGREES SELECTED FOR LANDING RAN FLAP DISAGREE AND BRAKE COOLING AND LANDED NORMALLY FLAPS CAME UP TO 15 AFTER LANDING ; / [01] INTERROGATED FSEU FOUND FAULT CODE 27 - 52259 L FLAP SENSOR FOUND NO EXISTING FAULTS PERFORMED FIM TASK 27 - 51 TASK 813 FOUND NO ABNORMALTIES

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 74,656 hrs · 44,175 cycles

CRACK ON SUPPORT ANGLE OF FRONT SPAR WEB FUEL BOOST PUMP IFSS 120 APPROX AND WBL 94.24 AT RT WING / REPLACED SUPPORT ANGLE OF FRONT SPAR WEB FUEL BOOST PUMP IFSS 120 APPROX AND WBL 94.24 AT RT WING IAW B737-700 SRM 51-42-02 AND DRAWING # 116A3001 REV 'A' AND 112A2004 REV A

Part: SCUFF PLATE — CRACKED (FWD GALLEY AREA) · airframe 74,656 hrs · 44,175 cycles

REPLACE SERVICE DOOR SCUFF PLATE FOR EXCESSIVE CRACK AT FWD GALLEY AREA / REPLACED SERVICE DOOR SCUFF PLATE AT FWD GALLEY AREA IAW DWG 141A8431 REV A AND AMM 53-11-01-420 -801

Part: STRAP — CORRODED (BS 727D-727E) · airframe 74,656 hrs · 44,175 cycles

CORROSION ON STRAP LOCATED FROM BS 727D TO BS 727E BETWEEN LBL 21.80 AND RBL 21.80 WL 156 AT AFT CARGO COMPARTMENT / REPLACED ON STRAP LOCATED FROM BS 727D TO 727E BETWEEN LBL 21.80 AND RBL 21.80 WL 156 AT AFT CARGO COMPARTMENT P/N NEW STRAP IS 146A9401-8 IAW DRAWING #146A7500 REV.'A'_SRM 51-10-02 ITEM 9

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 74,656 hrs · 44,175 cycles

CRACK CENTER SCUFF PLATE AT FWD CARGO COMPARTMENT / REPAIRED BY WELDING CENTER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30 -15-2R-1 REPAIR 1 PARAGRAPH 4 ITEM C STEP 4 AND BAC 5975

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 74,656 hrs · 44,175 cycles

CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT / REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4 ITEM B STEP (4) AND BAC 5975

Part: STRINGER — CRACKED (BS 540 S25L) · airframe 74,656 hrs · 44,175 cycles

CRACK STRINGER 25L LOCATED BS 540 AT FWD CARGO COMPARTMENT / PERFORMED PERMANENT REPAIR ON STRINGER 25L LOC BS 500D TO BS540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED IS: 7075T0.045' PO # 202113400800101 AND7075R0.50' PO # 202112114500103 CONVERTED FROM 7075T0 TO CONDITION 7075T6 IAW BAC5602

Part: STRINGER — CRACKED (BS 540 S26L) · airframe 74,656 hrs · 44,175 cycles

CRACK STRINGER 26L LOCATED BS 540 FWD CARGO COMPARTMENT / PERFORMED PERMANENT REPAIR ON STRINGER 26L LOC BS 500D+9' TO BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED IS: 7075-T0-0.050' PO # 202112114500103 AND 7075-0.045' PO #202113400800101 CONVERTED FROM 7075T0 TO CONDITION 7075T6 IAW BAC 5602

Part: STRINGER — CRACKED (BS 540 S25R) · airframe 74,656 hrs · 44,175 cycles

CRACK STRINGER 25R LOCATED BS 540 FWD CARGO COMPARTMENT / REPAIRED STRINGER 25R LOCATED BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 FIGURE 206-7 STRINGER SECTION MATERIAL CONDITION 7075T6 0.036'. -2 CHANNEL; -3 CHANNEL (2EA) MATERIAL CONDITION 7075T6 0.040' AND PERFORMED HEAT TREATMENT IAW BAC 5602 AND APPLIED PROTECTIVE TREATMENT ON REPAIR AREA AND REPAIR PART IAW B737-700 SRM 51-20-01

Part: STRINGER — CRACKED (BS 540 S26R) · airframe 74,656 hrs · 44,175 cycles

CRACK STRINGER 26R LOCATED BS 540 FWD CARGO COMPARTMENT / PERFORMED PERMANENT REPAIR ON STRINGER 26R LOC BS 500D TO BS 540 AT FWD CARGO COMPARTMENT IAW B737- 700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 205 MATERIAL USED 7075T0/0.045' PO # 2021-134008 BAC 1498-132PO #200826465 CONVERTED FROM 7075T0 TO CONDITION 7075T6 IAW BAC 5602

Part: ANGLE — CRACKED (LT WING) · airframe 74,656 hrs · 44,175 cycles

CRACK ANGLE TRAILING EDGE ACCESS PANEL 551FB LT WING (1 EA) / REPLACED ANGLE TRAILING EDGE ACCESS PANEL 551FB LT WING (1EA) IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 115A2710 REV 'B'

Part: ANGLE — CRACKED (RT WING) · airframe 74,656 hrs · 44,175 cycles

CRACK ANGLE TRAILING EDGE LOCATED IFSS 120 UPPER SIDE RT WING (1 EA) / REPLACED ANGLE LOC TRAILING EDGE 1FSS 120 UPPER SIDE RT WING (1EA) IAW B737-700 SRM 51-10-02 AND SRM 51-40-02

Part: STRINGER — CRACKED (BS 540 S24R) · airframe 74,656 hrs · 44,175 cycles

CRACK STRINGER 24R LOCATED BS540 FWD CARGO COMPARTMENT / REPAIRED STRINGER 24R LOCATED BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-02R-1 REPAIR 1 FIGURE 205 -7 STRINGER SECTION MATERIAL USED CONDITION 7075T6 0.050' HAT SECTION SPLICE MATERIAL USED BAC 1498-132 AND PERFORMED HEAT TREATMENT IAW BAC 5602 AND APPLIED PROTECTIVE TREATMENT ON REPAIR AREA AND REPAIR PART IAW B737-700 SRM 51-20-01

Part: SKIN — DAMAGED (BS 867 S27R/L) · airframe 74,656 hrs · 44,175 cycles

EXISTING RE-WORK EXTERNAL SKIN BS867 MORE 9 INCHES AT BETWEEN STR 27R TO STR 27 L AT LOWER FUSELAGE (1 EA) / REPAIRED EXTERNAL SKIN FROM BS 867 TO BS 888 BETWEEN STR 27L AND STR 26R I.A.W SRM B737-700 53-00-01-2R-3 REPAIR 3 FIG. 201 AT LOWER FUSELAGE. FOR REINSPECTION SEE TLD T080560 MATERAIL USED:2024T3 0.063' P.O #202022545200101 AND 2024T3 0.071' P.O #202111042100101

Part: LIGHT — BROKEN (LAVATORY) · airframe 74,656 hrs · 44,175 cycles

BROKEN LAVATORY EMERGENCY EXIT LIGHT ASSY FWD WALL AT AFT GALLEY AREA / REPLACED LAVATORY EMERGENCY EXIT LIGHT ASSY FWD WALL AT AFT GALLEY AREA IAW AMM 33-51-01-960-802 AND PERFORMED OPERATIONAL TEST OF THE NEW ASSEMBLY AND TEST IS OK

Part: STIFFENER — CRACKED (BS 540 BL0-RBL24) · airframe 74,656 hrs · 44,175 cycles

CRACK STIFFENER FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL0 AND RBL24.5 CENTER SECTION / REPLACED STIFFENER LOC BS 540 BTW BL0 AND RBL 24.5 CENTER SECTION IAW B737-700 SRM 51-40-02

Part: STIFFENER — CRACKED (BS 540 LBL 45-60) · airframe 74,656 hrs · 44,175 cycles

CRACK STIFFENER PLATE LOCATED BS 540 BETWEEN LBL 45 AND LBL 60 AT CENTER WING BOX / REPLACED STIFFENER PLATE LOCATED BS 540 BETWEEN LBL 45 AND LBL 60 AT CENTER WING BOX IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 143A5240 REV B

Part: SUPPORT ANGLE — CRACKED (BS 1016 S2L/R) · airframe 74,656 hrs · 44,175 cycles

CRACK FRONT SPAR SUPPORT ANGLE LOCATED AT BS 1016 BETWEEN STR 2R AND STR2L LOWER AT VERTICAL STABILIZER / REPLACED FRONT SPAR SUPPORT ANGLE LOCATED AT BS 1016 BTW STR 2R AND STR 2L LOWER AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 176A3001 REV 'E'

Part: WEB — CRACKED (NR 1 FAN) · airframe 74,656 hrs · 44,175 cycles

CRACK INBOARD FAN COWL WEB ON ENGINE 1 / REPLACED WEB ON INBOARD FAN COWL ON ENGINE 1 IAW B737-700 CMM 71-13-30 GOODRICH AEROSTRUCTURE PAGE 10064

Part: ACCESS PANEL — CRACKED (AFT CARGO) · airframe 74,656 hrs · 44,175 cycles

CRACK FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT / MADE NEW FLOOR ACCESS PANEL 140CF AT AFT CARGO COMPARTMENT IAW DWG # 453A2610-1 SHEET 009 AND SHEET 010 REV 'E' MATERIAL USED 2024T3 0.080' INCH PO 2021149583 AND B737-700 SRM 51-40-05 AND 51-40-08

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,656 hrs · 44,175 cycles

CRACK FRONT SPAR INSPAR RIB LOWER HORIZONTAL INBOARD FLANGE AT STAB STA 147.90 RT HORIZONTAL STAB / PERFORMED REPAIR RIB FRONT SPAR LOWER HORIZONTAL INBOARD FLANGE AT STAB STA 147.90 RT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 FIGURE 205 SHEET 3

Part: EEC — FAULTED (NR 2 ENGINE) · airframe 74,647 hrs · 44,170 cycles

DURING CLIMB PASSING 9000' #2 ENGINE EXPERIENCED A COMPRESSOR STALL (2 LOUD BANGS). ENGINE RECOVERED AT IDLE AND THEN RAN NORMALLY. PASSENGER WITNESSED 2 FIREBALLS EXIT THE #2 ENGINE DURING COMPRESSOR STALL. EEC BITE CODES: 75-20822 T25 SENSOR OUT OF RANGE 75-20802 T25SENSOR SIGNALS DISAGREE / R&R EEC PER MM 73-21-60 MPN 2042M67PO2 S/N LMDR4015. R&R T25 SENSOR PER 73-21-02. MPN RP236-00 S/N EM 398328-5. R&R J10 HARNESS PER MM 73-21-06. MPN 325-043-503-0 S/N N/S. PERFORMED FDR PER MM 71-00-00-200-801-F00 RAR# 96372 T25 RAR# 96370 EEC RAR 93672 P/N OFF/ON RP236-00 SN OFF YC069170-J SN ON EM398328-5 RAR 96370 P/N OFF 0748250CN1852M33P06 P/N ON 2042M67P02 SN OFF LMDN7145 SN ON LMDR4015

Part: SENSOR — FAULTED (NR 2 ENGINE) · airframe 74,647 hrs · 44,170 cycles

DURING CLIMB PASSING 9000' #2 ENGINE EXPERIENCED A COMPRESSOR STALL (2 LOUD BANGS). ENGINE RECOVERED AT IDLE AND THEN RAN NORMALLY. PASSENGER WITNESSED 2 FIREBALLS EXIT THE #2 ENGINE DURING COMPRESSOR STALL. EEC BITE CODES: 75-20822 T25 SENSOR OUT OF RANGE 75-20802 T25SENSOR SIGNALS DISAGREE / R&R EEC PER MM 73-21-60 MPN 2042M67PO2 S/N LMDR4015. R&R T25 SENSOR PER 73-21-02. MPN RP236-00 S/N EM 398328-5. R&R J10 HARNESS PER MM 73-21-06. MPN 325-043-503-0 S/N N/S. PERFORMED FDR PER MM 71-00-00-200-801-F00 RAR# 96372 T25 RAR# 96370 EEC RAR 93672 P/N OFF/ON RP236-00 SN OFF YC069170-J SN ON EM398328-5 RAR 96370 P/N OFF 0748250CN1852M33P06 P/N ON 2042M67P02 SN OFF LMDN7145 SN ON LMDR4015

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 74,045 hrs · 43,819 cycles

2 EACH EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST. REMOVED AND REPLACED 2 EACH EMERGENCY LIGHTING BATTERY PACKS AT LOCATIONS MM01672 AND M01673, PER AMM 33-51-06 AND ENG DWG 33500005.

Part: SCREW — MISSING (L1 DOOR) · airframe 72,554 hrs · 42,939 cycles

FORWARD ENTRY DOOR ASSIST HANDLE MISSING SCREW / RESECURED FWD ENTYR DOOR ASSIST HANDLE AS REQ'D S.I.P.

Part: COVER — OUT OF POSITION (CABIN) · airframe 72,272 hrs · 42,753 cycles

FLT ATTENDANT REPORTS MANUAL INFLATION HANDLE COVER NOT IN VIEW REPOSITIONED MANUAL INFLATION HANDLE COVER PER SIP

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 72,153 hrs · 42,668 cycles

AFT CARGO COMPARTMENT CENTER SCUFF PLATE HAS 2 EA. CRACKS AT DENTS 6.5' AND 9.5' FROM EDGES AS MARKED. /

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,103 hrs · 42,637 cycles

EMERGENCY LIGHT AT FORWARD ENTRY DOOR HAD 2 EACH LAMP INOPERATIVE. / RELAMPED LIGHT PER AMM.

Part: COFFEEMAKER — FIRE (GALLEY) · airframe 71,049 hrs · 41,966 cycles

SUPPLEMENTAL INFORMATION, DIVERSION/DECLARED EMERGENCY. FORWARD FA REPORTED FIRE AND SMOKE IN THE FORWARD GALLEY COFFEE MAKER. DIRECTED FA TO PULL CIRCUIT BREAKERS AND FIRE AND SMOKE STOPPED. NO FIRE EXTINGUISHER USED. THE FIRE REMAINED OUT WITH NO SMOKE. R&R COFFEE MAKER PER AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 70,988 hrs · 41,930 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. / R&R BATTERY PER AMM.

Part: COVER — OUT OF POSITION (L1 DOOR SLIDE) · airframe 70,162 hrs · 41,364 cycles

L1 DOOR SLIDE INFLATION HANDLE COVER OUT OF POSITION. REPOSITIONED SLIDE INFLATION HANDLE COVER TO THE HOOK AND LOOP IAW MT.

Part: PANEL — DELAMINATED (LT WING) · airframe 69,974 hrs · 41,246 cycles

PNL 431 ER DELAMINATED / REMOVED AND REPLACED LT PYLON 431 ER IAW SRM REF 51-40-02

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,957 hrs · 41,234 cycles

LT EMERGENCY FLOOR LUMINESCENT STRIPS INOP BETWEEN ROW 9 TO ROW 13. R&R BATTERY PACK PER AMM.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 69,957 hrs · 41,234 cycles

R1 DOOR EMERGENCY SLIDE LIGHT INOP. R&R LAMP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,957 hrs · 41,234 cycles

RT OVERWING EMERGENCY LIGHT INOP. R&R EMERGENCY LIGHT SUPPLY PER AMM.

Part: INTERCOSTAL — CRACKED (FWD FUSELAGE) · airframe 69,957 hrs · 41,234 cycles

WHILE INSTALLING THE FRAME SPLICE REPAIR AT STA 303 FOUND INTERCOSTAL AT STA 294 STR 15 CRACKED AT FASTENER HOLE P/N 141A8181-37 REV A. / REMOVED DAMAGE ON INTERCOSTAL AT STA 294 STR 15L. INSTALLED REPAIR ANGLE AND FILLER IAW AAR EA 190559 IR AND SWA EA 1-753-35139 REV IR A-TAG # A34815 P/N 7075-0-090

Part: PAN — DAMAGED (BS 986) · airframe 69,957 hrs · 41,234 cycles

R/H CREASE BEAM AT BS. 986, FOUND AFT LAV PAN CREASED AND BENT. / R&R WEB IAW SRM & DWG.

Part: WEB — CORRODED (BS 867) · airframe 69,957 hrs · 41,234 cycles

UPPER SURFACE OF CREASE BEAM WEB HAD CORROSION AT BS. 867+16, STR. 17L. / R&R WEB PER SRM.

Part: ANGLE — CRACKED (CABIN) · airframe 69,957 hrs · 41,234 cycles

PASSENGER CABIN. STA 259+2; STR 10L; CIRCUIT BREAKER ATTACH ANGLE IN STRINGER IS CRACKED IN RADIUS / REMOVED AND REPLACED ATTACH ANGLE AT PASSENGER CABIN STA 259 + 2; STR 10L IAW BOEING DRAWING: 141A9502 REV. A AND B737-700 SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (BS 227) · airframe 69,957 hrs · 41,234 cycles

STRINGER CLIP CRACKED AT BS. 227, STR. 10R. / R&R STRINGER CLIP IAW DWG.

Part: NONE — DENTED (FLIGHT DECK) · airframe 69,957 hrs · 41,234 cycles

FLIGHT DECK. STA 251.6 TO 251.6+6; RBL 6 TO LBL 16; FLIGHT DECK FOOR HAS DENT GOING ACROSS STRUCTURE / EVALUATED DENT ON FLIGHT DECK STA 251.8 TO 251.6+6' RBL6 TO LBL 16 & FOUND TO BE OUT OF LIMIT I.A.W B737-700 SRM 53-10-51-1A-1R REPLACED I.A.W. B737-700 SRM 53-10-51-2R-2; HG 203. APPLIED TOPCOAT I.A.W AMM 51-21-73-370-801.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,957 hrs · 41,234 cycles

L/H HORIZONTAL STABILIZER RIB CRACKED AT STA. 120.3, STIFFENER LOWER FLANGE, 4TH FROM THE FRONT. / REPAIRED RIB IAW SRM.

Part: FRAME — CRACKED (BS 259) · airframe 69,957 hrs · 41,234 cycles

FRAME WEB CRACKED AT BS. 259, STR. 12L. / REPAIRED FRAME IAW EA.

Part: STRINGER — CORRODED (BS 360) · airframe 69,957 hrs · 41,234 cycles

ELECTRONICS AND EQUIPMENT COMPARTMENT STRINGER CORRODED BETWEEN BS. 360+15 TO BS. 360+18, STR. 27L. / REPAIRED STRINGER IAW EA.

Part: ANGLE — CORRODED (AFT FUSELAGE) · airframe 69,957 hrs · 41,234 cycles

EXTERNAL SKIN; LATERAL ANGLE HAS CORROSION ON UPPER SURFACE; STA 1016+20; RBL 7 TO LBL 7 / AFTER FURTHER EVALUATION OF LATERAL ANGLE AT STA 1016+20 AT RBL 7 TO LBL 7 WAS OUT ALLOWABLE REWORK LIMITS I.A.W B-737-700 SRM 53-00-01-1A-01 AAR TOOL #36646; DUE 02OCT19; REMOVED AND REPLACED LATERAL ANGLE AT EXTERNAL SKIN STA 1016+20; RBL 7 TO LBL7 AS PER: BOEING DRW #148A3110 FEV.- AND SRM 51-40-02 ORIGINAL THICKNESS .040 REMAINING .015 LOSS .025 P/N: BAC 1490-53-7075-T6 ISSUE TAG #A88404

Part: FLOOR PANEL — PULLED (CABIN) · airframe 69,957 hrs · 41,234 cycles

PASSENGER CABIN FLOORBOARD 242CF UPPER SURFACE HAS AREAS OF PULLED FIBERS. / REPAIRED FLOOR BOARD 242 CF UPPER SURFACE IAW SRM 53-00-50-2R-1; PG'S 1;2; STEPS 3(A-N)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,957 hrs · 41,234 cycles

AFT PIT BILGE LT FLOOR SUPPORT Z-ANGLE CORRODED BETWEEN BS. 727C TO BS. 787, LBL 20. R&R Z-ANGLE IAW SRM.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 69,957 hrs · 41,234 cycles

PASSENGER CABIN FLOORBOARD 241BF UPPER SURFACE HAS AREAS OF PULLED FIBERS. / REPAIRED FLOORBOARD PANEL 241 BF SURFACT SHEET IAW SRM 53-00-50-2R-1; PG'S 1;2; STEP 3(A-N)

Part: SEAT TRACK — CORRODED (BS 827-887) · airframe 69,957 hrs · 41,234 cycles

PASSENGER CABIN R/H OUTBOARD SEAT TRACK LOWER AND UPPER CROWN CORRODED BETWEEN BS. 827 TO BS. 887, RBL 45.5. / R&R SEAT TRACK IAW SRM.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 69,957 hrs · 41,234 cycles

PASSENGER CABIN FLOORBOARD 241DF UPPER SURFACE HAS AREAS OF PULLED FIBERS. / REPAIRED FLOORBOARD 241 DF FACE SHEET IAW SRM 53-00-50-2R-1; PG'S 1;7 STEPS 3(A-N).

Part: ANGLE — CORRODED (AFT FUSELAGE) · airframe 69,957 hrs · 41,234 cycles

APU COMPARTMENT; STA 1088+11; RBL 17; FWD APU DOOR HINGE; FWD ATTACH ANGLE HAS CORROSION AT BOLT HOLE / NO LIMITS IN SRM FOR APU DOOR HINGE FWD ATTACH ANGLE (GUSSET) OUT OF LIMITS. FABRICATED GUSSET AND INSTALLED; TREATED AND PRIMED I/A/W DWG 148A8540

Part: STRINGER CLIP — CORRODED (BS 847) · airframe 69,957 hrs · 41,234 cycles

AFT PIT BILGE BODY FRAME STRINGER CLIP CORRODED AT BS. 847, STR. 27L. / R&R STRINGER CLIP IAW SRM AND DWG.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 69,957 hrs · 41,234 cycles

PASSENGER CABIN FLOORBOARD 231YF UPPER SURFACE HAS AREAS OF PULLED FIBERS. / REPAIRED FLOORBOARD 231YF SURFACE SHEET IAW SRM 53-00-50-2R-1; PG'S 1.2; STEPS 3(A-N)

Part: FLOORBEAM — CORRODED (BS 986) · airframe 69,957 hrs · 41,234 cycles

AFT PIT EQUIPMENT BAY CABIN FLOOR BEAM UPPER CHORD EXISTING REPAIR CORRODED AT BS. 986, RBL 44. / R&R T-CAP SECTION IAW EA.

Part: FRAME — CRACKED (BS 312) · airframe 69,957 hrs · 41,234 cycles

ABOVE L1 DOOR FORWARD TOP CORNER FRAME CRACKED AT BS. 312. REPAIRED FRAME IAW EA.

Part: CHANNEL — BENT (AFT CARGO COMPT) · airframe 69,957 hrs · 41,234 cycles

AFT PIT BILGE FLOOR SUPPORT C-CHANNEL IS BENT BS 727E+10 TO 772; RBL 3. / AFT CARGO BILGE FLOOR SUPPORT AT 727E+10 TO 772 RBL 3. IS BENT. BEYOND ALLOWABLE LIMITS OF B737-700 SRM 53-00-53-1A-2; CUTOUT DAMAGED SECTION; FABRICATED AND INSTALLED REPAIR PARTS IAW B737-700 SRM 53-00-53-2R-4 AND EA 1-A53-4982

Part: FLOOR PANEL — PULLED (CABIN) · airframe 69,957 hrs · 41,234 cycles

PASSENGER CABIN FLOORBOARD 241AF UPPER SURFACE HAS A AREAS OF PULLED FIBERS. / REPAIRED FLOORBOARD 241AF SURFACE AREA IAW SRM 53-00-50-2R-1; PG'S 1;2; STEPS 3(A-N).

Part: FLOOR PANEL — PULLED (CABIN) · airframe 69,957 hrs · 41,234 cycles

PASSENGER CABIN FLOORBOARD 242AF UPPER SURFACE HAS AREAS OF PULLED FIBERS. / REPAIRED FLOORBOARD 242AF SURFACE SHEET IAW SRM 53-00-50-2R-1; PGS 1;2 STEPS 3(A-A)

Part: SKIN — CORRODED (BS 887-927) · airframe 69,957 hrs · 41,234 cycles

EXTERNAL SKIN CORRODED BETWEEN BS. 887+7 TO BS. 927, BETWEEN STR. 2R TO STR. 2L. REPAIRED SKIN IAW SRM.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 69,957 hrs · 41,234 cycles

PASSENGER CABIN FLOORBOARD 242AF LOWER SURFACE HAS MULTIPLE PUNCTURES. / REPAIRED FLOORBOARD 242 AF LOWER SURFACE IAW SRM 53-00-50-2R-1; PG'S 1;2; STEPS 3 (A - M).

Part: FLOOR PANEL — PULLED (CABIN) · airframe 69,957 hrs · 41,234 cycles

PASSENGER CABIN FLOORBOARD 232RF UPPER SURFACE HAS AREAS OF PULLED FIBERS. / REPAIRED FLOORBOARD 232 RF UPPER SURFACE IAW SRM 53-00-50-2R-1; PG'S 1;2; STEPS 3 (A-M).

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 69,957 hrs · 41,234 cycles

AFT PIT BILGE BODY FRAME SIDEWALL SUPPORT ANGLE INBOARD END IS CORRODED BS 947; RBL 24. / REMOVED AND REPLACED AFT BILGE BODY FRAME SIDEWALL SUPPORT ANGLE IAW BOEING DWG 149A 8117 104 REV C AND SRM 51-40-02-0G-0 P/N REPLACED 149A8118-28- A TAG # AL4130

Part: RETAINER — CRACKED (VERTICAL STABILI) · airframe 69,957 hrs · 41,234 cycles

RH VERTICAL FIN TO BODY PANEL 324AR PANEL RETAINING CLIP CRACKED / REPLACED DAMAGE RETAINER ON PANNEL 324AR I.A.W SRM 51-40-02-0G & BOEING DWG # 172A6123 TY:DWG ID:0001 REV:A. A-TAG # SI1255.

Part: PANEL — CRACKED (HORIZONTAL STAB) · airframe 69,957 hrs · 41,234 cycles

RH HORIZONTAL STAB I/B DOOR ASSY. PANEL # 343AB IS CRACKED. / REMOVED AND REPLACE I/B DOOR ASSY. ON RH HORIZONTAL STAB PANEL # 343AB PER. 737 SRM 51-40-02-0G-0 STEP 9.

Part: PANEL — CRACKED (VERTICAL STABILI) · airframe 69,957 hrs · 41,234 cycles

RH VERTICAL FIN CLOSEOUT PANEL 323AR CRACKED UNDER RETAINER TAB / REPLACED CRACKED R/H VERTICAL FIN CLOSED OUT PANEL 323AR LOCATED + DRILLED NEW PANEL IAW DWG #172A6122 TRETAED + PRIMED + APPLIED EXTERIOR FINISH IAW SRM 51-20-01-0G-0 + AMM 51-21-99-300 ATAG WN9276

Part: BRACKET — BROKEN (LOWER EXT FUSELA) · airframe 69,957 hrs · 41,234 cycles

KEEL BEAM FWD PANEL 192E FORWARD RIGHT T BRACKET BROKEN. / REMOVED AND REPLACED KEEL BEAM FWD PANEL 192E FORWARD RIGHT BRACKET FITTING I/A/W BOEING DWG 149A7701 REV.A 737-700 SRM 51-40-02-0G-0 737-700 SRM 51-40-05-0G-0; AND 737 AMM AMM 51-21-91-620-802 ATAG A70762

Part: CHANNEL — BROKEN (VERTICAL STABILI) · airframe 69,957 hrs · 41,234 cycles

RH VERTICAL FIN TO BODY PANEL 324AR U-CHANNEL LOWER EDGE BROKEN OFF / REPLACED DAMAGE U-CHANNEL ON PANEL 324AR LWR EDGE I.A.W EDGE I.A.W B737-700 SRM 51-40-02-0G & BOEING DWG # 172A6134. TY:DWG; ID:0001; REV:4E

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,957 hrs · 41,234 cycles

FRAME CORRODED. REPAIRED FRAME IAW EA.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 69,957 hrs · 41,234 cycles

L/H HORIZONTAL STABILIZER RIB AT STA 120.3, THIRD STIFFENER AFT CRACKED. / REPAIRED STIFFENER IAW SRM AND DWG.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 69,957 hrs · 41,234 cycles

L\H HORIZONTAL STAB FWD TERMINAL FITTING UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED LH HORIZONTAL UPPER STAB SLIDING SEAL PER B737 AMM 53-31-31-000-802 AND B737 AMM 53-31-31-400-802. ATAG A69096; SI1279; A44532; A84335

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 69,957 hrs · 41,234 cycles

HORIZONTAL PRESSURE DECK FORWARD EDGE OF STIFFENING BEADS CRACKED BETWEEN BS. 663.75 TO BS. 675, BETWEEN RBL 39 TO RBL 60. / REPAIRED CUTOUT WEB IAW SRM.

Part: SKIN — CORRODED (DOOR) · airframe 69,957 hrs · 41,234 cycles

LOWER EXTERNAL FUSELAGE, POTABLE WATER DOOR SKIN CORRODED AROUND AFT LATCH. R & R SERVICE DOOR IAW SRM & DWG.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 69,957 hrs · 41,234 cycles

AFT CARGO PIT AFT CORNER SCUFF PLATE CRACKED / WORK ACCOMPLISHED ON W/O #39546-1600-0001.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 69,957 hrs · 41,234 cycles

L/H EMERGENCY LIGHT LENS STOW BIN LOOSE AT ROW 12. R&R LENS IAW AMM.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 68,711 hrs · 40,412 cycles

FUSELAGE WING TO BODY PNL 193B DELAMINATED AND ERODED AT FWD RT CORNER BETWEEN FASTENER LOCATION 20 AND 21 MOD / REPLACED FUSEALGE WING TO BODY PANEL 193B IAW SRM 51-40-02

Part: SIGN — UNSECURE (CABIN) · airframe 68,440 hrs · 40,229 cycles

R1 DOOR LOWER EMERGENCY EXIT SIGN COVER FELL OFF. R&R SIGN ASSEMBLY PER AMM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 68,349 hrs · 40,170 cycles

L2 DOOR ESCAPE SLIDE L GIRT BAR LOOSE. SECURED SLIDE IAW AMM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 68,258 hrs · 40,113 cycles

RT PHOTOLUMINESCENT STRIP DAMAGED AT 1ST SECTION. R&R STRIP IAW AMM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 67,893 hrs · 39,884 cycles

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

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,893 hrs · 39,884 cycles

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

Part: BLADE — CRACKED (NR 2 ENGINE) · airframe 67,162 hrs · 39,420 cycles

NR 2 ENG FAN BLADE NR 10 CRACKED AT CONVEX SIDE. R&R BLADE PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 67,162 hrs · 39,420 cycles

EMERGENCY LIGHT BATTERY M1675 FAILED TEST. R&R BATTERY PACK PER MM.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 67,162 hrs · 39,420 cycles

RIGHT WING VERTICAL BULB SEAL RETAINER AFT OF #2 ENGINE AFT STRUT CRACKED / REMOVED AND REPLACED BULB SEAL RETAINER ON RIGHT WING AFT OF #2 ENGINE AFT STRUT PER SRM 51-40-02 AND MM 20-50-11

Part: BATTERY PACK — FAILED (CABIN) · airframe 67,162 hrs · 39,420 cycles

EMERGENCY LIGHT BATTERY M1669 FAILED TEST. R&R BATTERY PACK PER MM.

Part: VALVE — INOPERATIVE (CROSSFEED) · airframe 65,881 hrs · 38,568 cycles

FUEL CROSSFEED CIRCUIT BREAKER TRIPPED, CROSSFEED LIGHT DID NOT TEST. R & R THE CROSSFEED VALVE IAW MM.

Part: STRAP — OUT OF ADJUST (R2 DOOR) · airframe 64,841 hrs · 37,887 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT STRAP OUT OF ADJUST. ADJUSTED STRAP PER AMM.

Part: SHIELD — BROKEN (FLASHLIGHT) · airframe 64,114 hrs · 37,421 cycles

FORWARD EMERGENCY FLASHLIGHT SHIELD BROKEN. R&R SHIELD IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,280 hrs · 36,916 cycles

EXIT LIGHT INOP AFT OF L1 DOOR. R&R LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,280 hrs · 36,916 cycles

LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 63,280 hrs · 36,916 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1675 FAILED CAPACITY CHECK. R&R BATTERY PACK PER MM.

Part: TRACK — CRACKED (FLIGHT DECK) · airframe 63,280 hrs · 36,916 cycles

FLIGHT COMPARTMENT FIRST OFFICERS FORWARD LEFT SEAT TRACK IS CRACKED AS MARKED. / REMOVED AND REPLACED FLIGHT COMPARTMENT FIRST OFFICE RS FORWARD LEFT SEAT TRACK IAW AMM 25-11-11-400-801 ATAG WN8872

Part: INTERCOSTAL — CRACKED (FWD CARGO BAY) · airframe 63,280 hrs · 36,916 cycles

FWD CARGO BAFFLE AT STA 500-500A IS CRACKED / REMOVED DAMAGED BAFFLE OF FWD CARGO STA 500-500A AND LOCATED; DRILLED; AND INSTALLED NEW BAFFLE IAW SRM 51-40-02-0G-0 AND DWG 143A7505 REV. - RESTORED CIC IAW AMM 51-21-91-620-802.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

FUSELAGE STRINGER CLIP CRACKED AT STA 500D, STR 26L. R&R CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

FORWARD CARGO PIT STRINGER CRACKED BETWEEN BS 440+11 TO BS 460, STR 25L. R&R STRINGER IAW SRM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 63,280 hrs · 36,916 cycles

LEFT EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: SUPPORT — CORRODED (BS 1016) · airframe 63,280 hrs · 36,916 cycles

SUPPORT CORRODED AT BS 1016, BETWEEN RBL 18 TO 28. R & R THE SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 1016) · airframe 63,280 hrs · 36,916 cycles

SUPPORT CORRODED AT BS 1016 BETWEEN LBL 9 TO 16. R & R THE SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 1016) · airframe 63,280 hrs · 36,916 cycles

SUPPORT CORRODED AT BS 1016 BETWEEN LBL 18 TO 28. R & R THE SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 1016) · airframe 63,280 hrs · 36,916 cycles

SUPPORT CORRODED AT BS 1016, BETWEEN RBL 28 TO 45. R & R THE SUPPORT IAW SRM AND DWG.

Part: WEB — CORRODED (BS 807) · airframe 63,280 hrs · 36,916 cycles

AFT CARGO BAY FLOOR SUPPORT WEB CORRODED AT BS 807+1, RBL 10. R & R THE WEB IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (BS 1016) · airframe 63,280 hrs · 36,916 cycles

SUPPORT CORRODED AT BS 1016 BETWEEN LBL 28 TO 45. R & R THE SUPPORT IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (BS 663) · airframe 63,280 hrs · 36,916 cycles

BS 663 BULKHEAD, LT STIFFENER CRACKED ON THE INBOARD SIDE ABOVE THE LT AIR CONDITION PACK EXHAUST. R & R THE DOUBLER ASSEMBLY IAW SRM & DWG.

Part: WEB — CORRODED (BS 1016) · airframe 63,280 hrs · 36,916 cycles

FLOOR WEB CORRODED AT BS 1016+2, LBL 6. R & R THE WEB IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

LOWER STUB FRAME EXISTING REPAIR ANGLE CRACKED AT BS 294. R&R STUB FRAME IAW SRM AND DWG.

Part: ANGLE — CRACKED (BS 867 BULKHEAD) · airframe 63,280 hrs · 36,916 cycles

AFT CARGO BAY LT BULKHEAD STANCHION ANGLE CRACKED AT BS 867, STRINGER 27L. R & R THE ANGLE IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

R2 DOOR LOWER SILL WEB CORRODED BETWEEN BS 966 TO BS 986. R&R WEB IAW SRM AND DWG.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

RT KEEL BEAM FORWARD SIDE OF WHEEL WELL BULKHEAD CRACKED AT BS 663.75. REPAIRED LOWER LOBE IAW SRM.

Part: STIFFENER — CRACKED (LT WING) · airframe 63,280 hrs · 36,916 cycles

LT WING TRAILING EDGE FIXED UPPER PANEL INBOARD OF DEFLECTOR BEAM, MID SPAN TRIANGLE SHAPED STIFFENER CRACKED. R&R STIFFENER IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 727-727D) · airframe 63,280 hrs · 36,916 cycles

AFT CARGO BAY RT ZEE ANGLE CORRODED BETWEEN BS 727 - 727D. R & R ZEE ANGLE IAW DWG & SRM.

Part: ANGLE — CORRODED (BS 887-927) · airframe 63,280 hrs · 36,916 cycles

AFT CARGO BAY RT ZEE ANGLE CORRODED BETWEEN BS 887 TO 927+3. R & R THE ZEE ANGLE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

FUSELAGE FRAME CORRODED AT STA 727D, STR 25R TO STR 26R. REPAIRED FRAME PER EA.

Part: FRAME — CORRODED (BS 727D) · airframe 63,280 hrs · 36,916 cycles

AFT CARGO BAY FRAME CORRODED AT BS 727D, BETWEEN STRINGERS 25 - 26L. REPAIRED THE FRAME IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

AFT CARGO COMPARTMENT LT Z ANGLE CORRODED BETWEEN BS 727D TO BS 827. R&R Z ANGLE IAW SRM & DWG.

Part: ANGLE — CORRODED (BS 867-887) · airframe 63,280 hrs · 36,916 cycles

AFT CARGO BAY RT ZEE ANGLE CORRODED BETWEEN BS 867 TO 887. R & R THE ZEE ANGLE IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

FORWARD CARGO PIT GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

LT FUSELAGE Z-ANGLE CORRODED AT STA 430. R&R ANGLE PER SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

AFT CARGO COMPARTMENT DOOR THRESHOLD STRAP INBOARD OF LOWER DOOR THRESHOLD WEB CORRODED BETWEEN BS 827 TO BS 787. R&R STRAP IAW DWG & SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

AFT CARGO COMPARTMENT RT Z ANGLE FORWARD SHIELD CORRODED BETWEEN BS 847 TO BS 867. R&R SHIELD IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

FORWARD CARGO DOOR THRESHOLD WEB CORRODED. R&R WEB IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

FORWARD CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 480 TO BS 500, STR 28R. R&R INTERCOSTAL IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

FUSELAGE BULKHEAD ANGLE CORRODED AT STA 500D LT SIDE. R&R ANGLE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

L1 DOOR INNER CREASE BEAM CORRODED BETWEEN BS 294.5 TO BS 352. R&R CREASE BEAM IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 328, LBL 48. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 63,280 hrs · 36,916 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, LBL 48. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

R1 DOOR CREASE BEAM STRUCTURAL STRAP CORRODED BETWEEN BS 294 TO BS 302. R&R STRAP IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

R1 DOOR LOWER CUTOUT THRESHOLD SUPPORT ANGLE ATTACHED TO OUTBOARD SIDE OF CREASE BEAM CORRODED. R&R ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 312-344) · airframe 63,280 hrs · 36,916 cycles

L1 DOOR CREASE BEAM THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS 312 TO 344. R & R THE ANGLE IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

T-CAP TOP SURFACE CORRODED AT BS 328, RBL 45. R&R T-CAP IAW SRM.

Part: CREASE BEAM — CORRODED (BS 294-360) · airframe 63,280 hrs · 36,916 cycles

R1 DOOR INNER CREASE BEAM ANGLE CORRODED BETWEEN BS 294 TO 360. REPAIRED CREASE BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

AFT CABIN R2 DOOR CREASE BEAM ANGLE CORRODED. R&R CREASE BEAM IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 63,280 hrs · 36,916 cycles

AFT CABIN FLOORBEAM CORRODED AT BS 986, CAP AREA LT TO RT. REPAIRED THE FLOORBEAM TEE IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,280 hrs · 36,916 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R&R INTERCOSTAL IAW DWG AND SRM.

Part: ENGINE — WARNING MESSAGE (NR 2) · airframe 62,452 hrs · 36,428 cycles

THE OIL FILTER BYPASS ALERT FOR NR 2 ENGINE ILLUMINATED, REACHING FL390. RAN QRH, SHUTDOWN ENGINE, DECLARED AN EMERGENCY, AND RETURNED TO DEPARTURE. R & R THE NR 2 ENGINE IAW MT.

Part: SIGN — LOOSE (CABIN) · airframe 62,181 hrs · 36,271 cycles

R1 DOOR EMERGENCY EXIT LOWER LIGHT SIGN LOOSE. SECURED SIGN AMM.

Part: MOUNT — CRACKED (R2 DOOR SLIDE) · airframe 61,205 hrs · 35,674 cycles

R2 DOOR EMERGENCY SLIDE AFT MOUNT NUTPLATE CRACKED. R & R THE SLIDE MOUNT ASSEMBLY IAW SRM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 61,205 hrs · 35,674 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 61,205 hrs · 35,674 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 61,205 hrs · 35,674 cycles

EMERGENCY LIGHTS BATTERY PACKS FAILED CAPACITY CHECK. R & R BATTERY PACK IAW DWG.

Part: BATTERY PACK — NO TEST (CABIN) · airframe 61,205 hrs · 35,674 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 60,028 hrs · 34,982 cycles

RIGHT EMER EXIT ROW LOWER EXIT LIGHT COVER LOOSE. R & R COVER IAW SIP.

Part: WINDOW — ARCED (COCKPIT) · airframe 59,820 hrs · 34,858 cycles

FIRST OFFICERS NR 2 WINDOW ARCED. R & R NR 2 WINDOW IAW MT.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 58,554 hrs · 34,120 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,974 hrs · 33,760 cycles

LEFT STOW BIN EMER LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

SKIN CRACKED AT BS 294, BL0. REPAIRED SKIN IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

RIGHT SIDE FLIGHT DECK, BELOW NR 2 WINDOW VERTICAL FRAME, WEB CRACKED AT STATION 211.8. R & R WEB IAW EA.

Part: WEB — CRACKED (LT MLG WW) · airframe 57,974 hrs · 33,760 cycles

LEFT MAIN WW AFT WEB CRACKED. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

LEFT STUB FRAME CRACKED AT BS 235.8. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

FUSELAGE FRAME CRACKED AT BS 259, BETWEEN STRINGER 9L - 10L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

FUSELAGE FRAME CRACKED AT BS 259, BETWEEN STRINGER 9R - 10R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

FUSELAGE FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

FUSELAGE FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

FUSELAGE FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

FUSELAGE FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,974 hrs · 33,760 cycles

FUSELAGE FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,974 hrs · 33,760 cycles

LEFT WING NR 4 SLAT LOWER LE NOSE SKIN AT SLAT ACTUATOR CRACKED AT FASTENER HOLE. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,974 hrs · 33,760 cycles

RIGHT WING NR 7 SLAT LOWER LE NOSE SKIN AT SLAT ACTUATOR CRACKED. R & R SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,974 hrs · 33,760 cycles

RIGHT OVERWING EXIT LOWER FWD EXIT, LIGHT BULB INOPERATIVE. R & R LIGHT IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,974 hrs · 33,760 cycles

LEFT WING NR 1 SLAT SKIN LOWER LE AT SLAT ACTUATOR CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 57,730 hrs · 33,617 cycles

RIGHT WING OTBD AFT TE FLAP DELAMINATED AT INBD END. R & R FLAP ASSEMBLY IAW MM.

Part: BRACKET — MISSING (L1 DOOR) · airframe 56,821 hrs · 33,106 cycles

L1 DOOR EMER EVAC SLIDE LT BRACKET GIRT BAR MISSING. INSTALLED BRACKET IAW SRM & MT.

Part: BONDING STRAP — BROKEN (R2 DOOR) · airframe 54,662 hrs · 31,904 cycles

R2 DOOR EMER EVAC SLIDE BONDING STRAPS BROKEN. REPAIRED BONDING STRAPS IAW SRM.

Part: FITTING — BROKEN (CABIN) · airframe 53,240 hrs · 31,115 cycles

CENTER AISLE OVERWING EMERGENCY EXIT LIGHT CLIP BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — LOOSE (EXIT SIGN) · airframe 52,965 hrs · 30,960 cycles

MID CABIN OVERHEAD EMERGENCY EXIT SIGN LIGHT LOOSE. SECURED LIGHT IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,571 hrs · 30,723 cycles

LT NR 1 WINDOW FRAME OTBD END FWD & AFT FASTENER ROWS UPPER FASTENER HOLE IN EACH ROW CRACKED. R & R FRAME IAW ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,571 hrs · 30,723 cycles

SKIN CUTOUT CRACKED AT BS 540 RT SIDE FWD FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,571 hrs · 30,723 cycles

FUSELAGE SKIN CRACKED AT BS 540, BETWEEN STRINGER 22R TO STRINGER 23R. REPAIRED SKIN IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,571 hrs · 30,723 cycles

FLIGHT DECK LT NR 1 FIXED WINDOW FRAME UPPER OTBD CORNER OF WINDOW PANE CUTOUT CRACKED. R & R FRAME IAW ACO.

Part: BATTERY PACK — FAILED (CABIN) · airframe 52,466 hrs · 30,653 cycles

LT FWD EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 51,684 hrs · 30,197 cycles

EMERGENCY EXIT SIGN IN CENTER CABIN LOOSE. SECURED SIGN IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 51,418 hrs · 30,035 cycles

LT OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,063 hrs · 29,820 cycles

MAIN WW FWD BULKHEAD BEADED WEB VERTICAL WEB CRACKED AT STATION 663 RBL 47. R&R WEB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,063 hrs · 29,820 cycles

LT SKATE ANGLE CRACKED BETWEEN BS 1006 TO BS 1016. R&R ANGLE IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 51,063 hrs · 29,820 cycles

MAIN WW VERTICAL PRESSURE WEB CRACKED AT STATION 663 BETWEEN RBL 34 TO RBL 35. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 51,063 hrs · 29,820 cycles

MAIN WW VERTICAL PRESSURE WEB CRACKED AT STATION 663 BETWEEN RBL 40 TO RBL 41. REPAIRED WEB IAW SRM.

Part: ATTACH ANGLE — BROKEN (LT WING) · airframe 51,080 hrs · 29,832 cycles

LT WING ATTACH ANGLE BETWEEN SHELF PANELS 551DB AND 551EB FWD END ATTACH TO WING BROKEN. R&R ANGLE IAW SRM AND DWG.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,063 hrs · 29,820 cycles

LT NR 3 FLIGHT DECK WINDOW FRAME NR 3 HOLE CRACKED. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,063 hrs · 29,820 cycles

LT NR 3 FLIGHT DECK WINDOW FRAME NR 2 HOLE CRACKED. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,063 hrs · 29,820 cycles

RT NR 3 FLIGHT DECK WINDOW FRAME NR 1 HOLE CRACKED. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,063 hrs · 29,820 cycles

RT NR 3 FLIGHT DECK WINDOW FRAME NR 2 HOLE CRACKED. REPAIRED FRAME IAW EA.

Part: SIGN — LOOSE (CABIN) · airframe 49,134 hrs · 28,695 cycles

EMERGENCY "EXIT/SALIDA" SIGN CAP OFF. RE-SECURED EMERGENCY "EXIT/SALIDAA" SIGN PER MM, OPS CHECK GOOD.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 48,146 hrs · 28,089 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,570 hrs · 27,699 cycles

GALLEY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: HOOK — LOOSE (GIRT BAR) · airframe 47,005 hrs · 27,367 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT HOOK LOOSE. REMOVED AND REPLACED HOOK PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 47,005 hrs · 27,367 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,407 hrs · 27,017 cycles

RT SIDE OVERWING EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 44,369 hrs · 25,842 cycles

LT OVERWING EMERGENCY EXIT SIGN LENS LOWER RT SIDE BROKEN. REPAIRED SIGN ASSY PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,287 hrs · 25,787 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT EEPLS INOP BETWEEN ROW 10 TO ROW 15. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,287 hrs · 25,787 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT EEPLS INOP BETWEEN ROW 7 TO ROW 11. REMOVED AND REPLACED BULB PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,287 hrs · 25,787 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 40. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,287 hrs · 25,787 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 46. REPAIRED BEAM IAW SRM.

Part: SIGN — CRACKED (CABIN) · airframe 44,287 hrs · 25,787 cycles

DURING SCHEDULED 12Y CHECK, FOUND FORWARD LAV EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED SIGN IAW MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,287 hrs · 25,787 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 36. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,287 hrs · 25,787 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 32. REPAIRED BEAM IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,287 hrs · 25,787 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,287 hrs · 25,787 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,287 hrs · 25,787 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 827, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,287 hrs · 25,787 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,287 hrs · 25,787 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR STUB FRAME CRACKED AT BOTTOM END AT CREASE BEAM. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,287 hrs · 25,787 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,287 hrs · 25,787 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR CREASE BEAM CORRODED. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 43,947 hrs · 25,579 cycles

DURING SCHEDULED OTS CHECK, FOUND LT MAIN WHEEL WELL BULKHEAD SKIN CRACKED AT BS 663, LBL 31.83. REPAIRED SKIN IAW ER AND EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,944 hrs · 25,578 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT MAIN WHEEL WELL BULKHEAD SKIN CRACKED AT BS 663, LBL 31.83. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 43,944 hrs · 25,578 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT MAIN WHEEL WELL BULKHEAD SKIN CRACKED AT BS 663, LBL 31.83. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 43,944 hrs · 25,578 cycles

DURING SCHEDULE HC1 CHECK, RT EMERGENCY EXIT LIGHT FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 43,944 hrs · 25,578 cycles

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

Part: COVER — MISSING (CABIN) · airframe 43,295 hrs · 25,193 cycles

R2 DOOR EMERGENCY EXIT SIGN COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,132 hrs · 22,787 cycles

FWD GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EEPLS PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 37,937 hrs · 22,081 cycles

R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: ESCAPE ROPE — DAMAGED (COCKPIT) · airframe 37,298 hrs · 21,676 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT COCKPIT EMERGENCY ESCAPE ROPE DAMAGED. REMOVED AND REPLACED ROPE PER MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 37,298 hrs · 21,676 cycles

DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR WEB CORRODED BETWEEN BS 260 TO BS 270, BL 0. REPAIRED WEB PER SWA EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 37,298 hrs · 21,676 cycles

DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR WEB CORRODED AT BS 260, BETWEEN LBL 10 TO RBL 10. REPAIRED WEB PER SWA EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 37,298 hrs · 21,676 cycles

DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR WEB CORRODED AT BS 270, BETWEEN LBL 10 TO RBL 10. REPAIRED WEB PER SWA EA.

Part: STRIP — LOOSE (CABIN) · airframe 36,855 hrs · 21,431 cycles

LEFT EEPLS STRIP LOOSE. SECURED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 36,846 hrs · 21,426 cycles

LT EEPLS LOOSE. SECURED EEPLS PER MM.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 35,497 hrs · 20,610 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION SUPPORT FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 35,497 hrs · 20,610 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION SUPPORT FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,841 hrs · 18,966 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,831 hrs · 18,956 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,259 hrs · 17,435 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, STR 17. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,259 hrs · 17,435 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 35.5. REPAIRED FLOORBEAM PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 27,534 hrs · 15,869 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 27,534 hrs · 15,869 cycles

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

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,365 hrs · 14,058 cycles

DURING SCHEDULED RON CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,365 hrs · 14,058 cycles

DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 8 DEF AND ROW 10 DEF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,808 hrs · 13,772 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT ROW 8 DEF AND ROW 10 DEF. RELAMPED LIGHTS PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 22,197 hrs · 12,868 cycles

R2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED R2 COCKPIT WINDOW ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,957 hrs · 12,125 cycles

DURING SCHEDULED MV2 CHECK, FOUND SEVERAL EMERGENCY EXIT BULLNOSE LIGHTS INOP AT ROW 7 ABC TO ROW 18 ABC. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 19,128 hrs · 11,102 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 17,833 hrs · 10,354 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN AT BS 500+8, FWD AIR PHONE ANTENNA, CORRODED. REPAIRED SKIN PER SRM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 14,227 hrs · 8,326 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT ROW NR 1. RECONNECTED EEPLS WIRES PER MM.

Part: SENSOR — FAULTY (RT WING TE FLAPS) · airframe 13,595 hrs · 7,997 cycles

DECLARED EMERGENCY, DURING APPROACH T/E FLAPS STOPPED AT POSITION 2. REMOVED AND REPLACED NR 6 T/E FLAP SKEW SENSOR PER MM.

Part: ROD END — WORN (ELEVATOR TAB) · airframe 13,033 hrs · 7,685 cycles

DURING SCHEDULED C4 CHECK, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR TAB PUSH RODS HARDWARE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,033 hrs · 7,685 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: COVER — CRACKED (CABIN) · airframe 10,736 hrs · 6,360 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED COVERS PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 7,505 hrs · 4,504 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE PER MM.

Part: SLIDE — DEPLOYED (SERVICE DOOR) · airframe 7,426 hrs · 4,461 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT AND DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,875 hrs · 1,760 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW 6. RELAMPED PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE)

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY AND AFT SERVICE DOOR EVACUATION SLIDE GIRT ASSY'S OUT OF ADJUSTMENT. REPOSITIONED SLIDES PER MM.