N434WN

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 65,938 hrs · 39,170 cycles

EVACUATION SLIDE SLIPPED OUT OF ITS CASE AFTER OPENING THE L-1 DOOR. / [01] INSTALLED SLIDE AT L-1 DOOR PER MT 725-61-06

Part: BATTERY — INOPERATIVE (AFT MEGAPHONE) · airframe 65,515 hrs · 38,883 cycles

AFT GALLEYS MEGA PHONE INOP / [01] REPLACED BATTERIES IN AFT GALLEY?S MEGA PHONE AS REQUIRED PER B 737 MM 25-64-00

Part: SENSOR — FALSE ACTIVATION (#2 ENGINE) · airframe 65,471 hrs · 38,849 cycles

ON START OF TAKEOFF ROLL; GOT A RIGHT WING TO BODY OVERHEAT INDICATION. REJECTED TAKEOFF. WING/ BODY OVERHEAT INDICATION FLICKERED ON INTERMITTENTLY ON TAXI BACK WITH BLEED AIR SYSTEM OFF/ ISOLATED / [01] OK TO CONTINUE PER MEL 26-13-01 SP#1 AUTH#91958;[02] REPLACED FWD #2 ENG PYLON STRUT SENSOR (M1763) IAW AMM 26-18-02

Part: BATTERY — INOPERATIVE (L/H OVERWING) · airframe 65,396 hrs · 38,799 cycles

LFT OVERWING EXIT EMERGENCY LIGHTS AND CENTER ISLE EMERGENCY EXIT SIGN INOP / [01] R&R?D BATTERY AND CHARGER 33-51-06

Part: CHARGER — INOPERATIVE (L/H OVERWING EXI) · airframe 65,396 hrs · 38,799 cycles

LFT OVERWING EXIT EMERGENCY LIGHTS AND CENTER ISLE EMERGENCY EXIT SIGN INOP / [01] R&R?D BATTERY AND CHARGER 33-51-06

Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 64,892 hrs · 38,450 cycles

LH OVERWING EXIT EMERGENCY LIGHT INOP / [01] RELAMPED PER AMM 33-51-04

Part: LIGHT — BROKEN (RH O/W EXIT) · airframe 64,641 hrs · 38,268 cycles

RT WING EMERGENCY EXIT LOWER EXIT INDICATOR LIGHT BROKEN. / [01] REPLACED RT. WING EMERGENCY EXIT LOWER EXIT INDICATOR LIGHT IAW AMM 33-51-01.

Part: PUMP — FAILED (#2 ENG) · airframe 63,455 hrs · 37,543 cycles

#2 ENGINE WOULD NOT MAKE CLIMB POWER. MAX POWER 87%. NO VIBRATIONS OR OTHER ANOMALIES NOTES. ; #2 ENGINE WOLD NOT MAKE CLIM THRST; MAXIMM N1 87%. NO VIRATIONS OR OTHER ANOMALIES NOTED. / [01] FOUND BAD ENG FUEL PUMP REMOVED AND REPLACED #2 ENG FUEL PUMP REF MT 773-11-00 OPS CHECK GOOD NO DEFECTS NOTED; [02] COMPLIED WITH ALL RII REQUIREMENTS PER MT 773-11-00; [03] COMPLIED WITH ALL RII REQUIREMENTS PER MT 773-11-00

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 61,434 hrs · 36,353 cycles

R1 DOOR LOWER EMERGENCY EXIT SIGN MISSING DIRECTIONAL ARROW. ; / REMOVED AND REPLACED R1 DOOR EMERGENCY EXIT SIGN COVER PER AMM 33-51-01; INSPECTED

Part: SIGN — CRACKED (OVERWING EXIT) · airframe 61,091 hrs · 36,156 cycles

OVER WING EMERGENCY EXIT AISEL SIGN CRACKED. REPLACED EMERGENCY EXIT AISEL SIGN ASSY IAW AMM 335101 OPS CHECK GOOD.

Part: STRUCTURE — BENT (R2 DOOR) · airframe 60,459 hrs · 35,793 cycles

AFT SERVICE DOOR; FO'S SIDE; BOTTOM RIGHT CORNER; METAL BENT OUT FROM SIDE OF AIRCRAFT / C/W EA 21-152-00099

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,441 hrs · 35,783 cycles

INOPERABLE BATTERY PACK M1672 AT PASSENGER CABIN. REPLACED BATTERY PACK M1672, IAW B737-700 AMM 33-51-06-960-805 TEST IS OK.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 60,441 hrs · 35,783 cycles

BROKEN EMERGENCY DOOR UPPER LIGHT LENS LH SIDE AT PASSENGER CABIN (1 EA) / REPLACED EMERGENCY DOOR UPPER LIGHT LENS LH SIDE AT PASSENGER CABIN (1EA) IAW B737-700 SRM 51-40-02 AND AMM 25-21-20-400-801

Part: REVEAL — CRACKED (SERVICE DOOR) · airframe 60,441 hrs · 35,783 cycles

CRACK SERVICE DOOR CUT OUT CORNER REVEAL UPPER AREA LOC BS 296 BTW STR8R TO STR 9R AT FWD GALLEY AREA / REPLACED CORNER REVEAL UPPER AREA LOC BS 296 BTW STR 8R TO STR9R AT SERVICE DOOR CUT OUT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8370 SHEET 2 REV C PART USED 141A8372U1 PO 2020-220637

Part: SUPPORT ANGLE — CRACKED (R/H WING) · airframe 60,441 hrs · 35,783 cycles

CRACK FRONT SPAR SUPPORT ANGLE ON FUEL BOOST PUMP AREA BETWEEN IFSS 110 AND IFSS 120 AT RT WING / REPLACED FRONT SPAR SUPPORT ANGLE ON FUEL BOOST PUMP AREA BTW IFSS 110 ON IFSS 120 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 51-40-02 57-20-10-1A-3 ALLOWABLE DAMAGE 3 AND DRAWING N. 112A2004 REV A AND 116A3939 REV B MACHINING FROM MATERIAL 7050T7451 BATCH 2020-1835

Part: STUB FRAME — CRACKED (DOOR FRAME) · airframe 60,441 hrs · 35,783 cycles

CRACK SERVICE DOOR CUT OUT STUD FRAME LOCATED BS 296 BETWEEN STR 8R TO STR 9R UPPER AREA AT FWD GALLEY AREA. REPLACED STUB FRAME LOCATED BS 296 BETWEEN STR 8R TO STR 9R UPPER AREA AT FWD GALLEY AREA, IAW B737-700 SRM 51-10-02 PAR 9 AND DRAWING 141A8370 REV 'F' FRAME PN INSTALLED 141A8371U7 DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS FOR THIS PART.

Part: WEB — CORRODED (CABIN) · airframe 60,441 hrs · 35,783 cycles

CORROSION WEB LOCATED BETWEEN BS 951 TO BS 992 AT LEVEL STR 17R RBL 54 WL 208 AT AFT GALLEY AREA. REPLACED WEB LOCATED BETWEEN BS 951 TO BS 992 AT LEVEL STR 17R RBL 54 WL 208 AT AFT GALLEY AREA, IAW B737-700 SRM 51-10-0G-0 ITEM 9 DUE TO WEB WAS EVALUATED. FOUND OUT LIMITS, IAW B737-700 SRM 53-70-15-1A-1. FABRICATED NEW WEB FROM MATERIAL 7075-TE 0.71' PO 2019577967, IAW B737-700 51-40-02 SRM AND DWG 147A8510 REV A.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 60,441 hrs · 35,783 cycles

BROKEN EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AND LAV (1 EA). REPLACED EMERGENCY LENS GALLEY 1 AT FWD GALLEY AND LAV (1 EA), IAW B737-700 AMM 33-51-01-960-801 STEP 2(C)(4).

Part: PLATE — CRACKED (PAX DOOR) · airframe 60,441 hrs · 35,783 cycles

CRACK ENTRY DOOR FWD CORNER PLATE AT FWD GALLEY AREA. REPLACED ENTRY DOOR FWD CORNER PLATE AT FWD GALLEY AREA, IAW B737-700 AMM 53-11-01-420-801.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 60,441 hrs · 35,783 cycles

CRACK WEB, INTERCOSTAL FLOOR STRUCTURE LOCATED ON BS 312 TO BS 328 AT LEVEL RBL 32 FWD GALLEY AND LAV. REPLACED INTERCOSTAL ON FLOOR STRUCTURE LOCATED ON BS 312 TO BS 328 AT LEVEL RBL 32 FWD GALLEY, IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DRAWING NR 141A5400 REV. PART USED 141A5410U-12. PO 202022090600101 AND REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE IN SRM.

Part: FLOORBEAM — CORRODED (FWD GALLEY) · airframe 60,441 hrs · 35,783 cycles

CORROSION FLOOR BEAM ON BS 328 AT EVEL RBL 48 WL 208 AT FWD GALLEY AREA. REPAIRED FUSELAGE TRANSVERSAL FLOOR BEAM AT BSTA 328 AND BL 0 TO RBL 60 (WL 208)-UPR REPAIR CHORD, IAW EA 53-0816-20 REVISION 0 AND EA NO 21-153-00034 REV IR.

Part: STRUCTURE — CRACKED (FWD GALLEY) · airframe 60,441 hrs · 35,783 cycles

CRACK INNER CHORD LOCATED BS 303.9 AT LEVEL STR 17L AT FWD GALLEY AREA. REPLACED INNER CHORD LOCATED BS 303.9 AT LEVEL STR 17L AT FWD GALLEY AREA, IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 AND DRAWING 141A8310 REV: D. REPLACED INNER CHORD DUE TO DAMAGE FOUND OUT LIMITS, IAW B737-700 SRM 53-10-15-1A-1 ALLOWABLE DAMAGE 1 FIG 108 DETAIL A. P/N 654A0004-1073; BATCH: SW2020002018.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 60,441 hrs · 35,783 cycles

CRACK STRINGER 26L LOCATED BS 540 FWD CARGO COMPARTMENT. REPAIRED STRINGER 26L LOCATED BS 540 FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY A CRACK IS BEYOND THE ALLOWABLE DAMAGE LIMITS. REPAIR PERFORMED FROM BS 500D TO BS 540 MATERIAL USED ALUMINUM SHEETS PN: 7075-T0-0.050 AND 7075-0.045 AND HEAT TREATED AND CONVERTED FROM T0 TO T6.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 60,441 hrs · 35,783 cycles

CRACK STRINGER 25L LOCATED BS 540 FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER 25L BETWEEN BS 500D TO BS 540 FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIG 206 MATERIAL USED STRINGER SECTION 7075-T6 0.045' INCHES. CHANNEL 7075-T6 0.050' INCHES; ANGLES 7075-T6 0.050' INCHES.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 60,441 hrs · 35,783 cycles

CRACK STRINGER 27L LOCATED BS 540 FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER 27L BETWEEN BS 500D TO BS 540 FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIG 206 MATERIAL USED STRINGER SECTION 7075-T6 0.056' INCHES. CHANNEL 7075-T6 0.063' INCHES, ANGLES 7075-T6 0.063' INCHES.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 60,441 hrs · 35,783 cycles

CRACK STRINGER 26R LOCATED BS 540 FWD CARGO COMPARTMENT. EVALUATED STRINGER 26R LOCATED BS 540 FWD CARGO COMP AND CRACK IS BEYOND OF ALLOWABLE DAMAGE LIMITS, IAW SRM B737-700 53-00-03-1A-1 FIG 103 DETAIL A. PERFORMED PERMANENT REPAIR, IAW SRM B737-700 53-00-03-2R-1. FABRICATED REPAIR PARTS CHANNEL 7075-T0 0.050' PO 2020 193461 ANGLES (2 EA) FROM 7075T0 0.050 PO 2020 193461. REPLACEMENT STRINGER SECTION FROM 7075T0 0.045' PO 2020 203305 HEAT TREATMENT REPAIR PARTS AND CONVERTED FROM T0 TO T6, IAW BAC 5602 TABLE X TEMPERATURE CONTROLLED P/N P3015G0E500000 S/N 112820025 DUE DATE 25FEB21.

Part: ANGLE — CRACKED (FWD GALLEY) · airframe 60,441 hrs · 35,783 cycles

CRACK ON ANGLE LOCATED OF BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. REPLACED ANGLE LOCATION OF BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA, IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 AND SRM 53-10-15-2R-7.

Part: ANGLE — WORN (FUSELAGE) · airframe 60,441 hrs · 35,783 cycles

WEAR CLOSURE ANGLE LOCATED ON BS 1088 TO BS 1156 AT LEVEL STR 2L AT UPPER FUSELAGE. PERFORMED PERMANENT REPAIR CLOSURE ANGLE LOCATED ON BS 1088 TO BS 1156 AT LEVEL STR 2L AT UPPER FUSELAGE, IAW B737-700 SRM 53-80-71-2R-6 REPAIR 6 MATERIAL USED: ANGLE 0.063' 2024-T'0' TO CONDITION T42 PO NR 2020-171541 STRAP 0.080' 2024-T3 PO NR 2020-140514.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 60,441 hrs · 35,783 cycles

CRACK ACCESS DOOR 323AL PLATE AT VERTICAL STABILIZER (1 EA) / REPLACED ACCESS DOOR 323AL PLATE AT VERTICAL STABILIZER IAW SRM B737-700 51-40-02 AND 51-10-02; DWG#172A6122 REV.B PLATE (RETAINER) P/N 172A6125-16 IAW DWG#172A6122 SHEET 1 REV.B

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,441 hrs · 35,783 cycles

INOPERABLE EMERGENCY LIGHT BATTERY LOCATED BETWEEN BS 727C TO 727D LT SIDE AT PASSENGER CABIN (1 EA). REPLACED EMERGENCY LIGHT BATTERY LOCATED BETWEEN BS 727C TO 727D LT SIDE AT PASSENGER CABIN (1 EA) SERVICEABLE CONDITION, IAW B737-700 AMM 33-51-06-960-805 AND TEST IS OK.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 60,441 hrs · 35,783 cycles

CORROSION FLOOR STRUCTURE FLOOR BEAM LOCATED BS 986.5 AT LEVEL RBL 43 AND LBL 43 WL 208 AT AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON FLOOR BEAM 986.5 UPPER HORIZONTAL TEE CAP SPLICE AFT GALLEY AREA, IAW EA NR 1-A53-7848 REV: KIT USED P/N 53100011-01. DUE TO REWORK EXCEEDED ALLOWABLE DAMAGE LIMITS, IAW SRM B737-700 53-70-51-1A-1 ALLOWABLE DAMAGE 1 PARAGRAPH 4H. MRT ON P1 TO P6 IS: 0.010' TOOL USED CALIPER P/N 500-193 S/N 1116081 DUE DATE 24SEP21.

Part: FLOOR SUPPORT — CORRODED (AFT GALLY) · airframe 60,441 hrs · 35,783 cycles

CORROSION FLOOR STRUCTURE INNER CHORD BS 947/BS 987 AT LEVEL RBL 54 WL 208 AFT GALLEY AND LAVATORY. REPLACED INNER CHORD LOCATED BETWEEN BS 887 TO 1006 AT LEVEL RBL 54 WL 208 AFT GALLEY AREA, IAW SRM B737-700 51-40-02 AND DRAWING 147A8501 REV B PART NUMBER USED 147A8540U8. DUE TO REWORK ARE P1=L=11.270' W=2.350' MRT=0.00 P2=L=11.140 W=2.350' MRT=0.00 INNER CHORD AND FOUND OUT LIMITS, IAW B737-700 SRM 53-70-15-1A-1 A/D 1 DETAIL D FIG 103 TOOL USED CALIPER PN 500-193 SN 1116081 DUE DATE 24-SEP-21.

Part: BOLT — DETERIORATED (L1 DOOR GIRT BAR) · airframe 60,441 hrs · 35,783 cycles

DETERIORATED ENTRY AND SERVICE DOOR GIRT BAR FITTING HARDWARE AT FWD GALLEY AREA. REPLACED ENTRY AND SERVICE DOOR GIRT BAR FITTING HARDWARE AT FWD GALLEY AREA INSTALLATION IS DOCUMENTED IN MT 725-025-00-01Y.

Part: ANGLE — CRACKED (BS 727B-727E) · airframe 60,441 hrs · 35,783 cycles

CRACK ANGLE - SUPPORT LOCATED BS727B TO BS727E AT LEVEL LBL51 CEILING STRUCTURE AREA AFT CARGO COMPARTMENT / REPLACED ANGLE - SUPPORT LOC BS 727B TO BS727E AT LEVEL LBL51 CEILING STRUCTURE AREA AFT CARGO COMPARTMENT MATERIAL USED ALUMINUM SHEET 2024T3 040' P/O 2020207935 IAE B737-700 SRM 51-40-02 AND DWG 149A9491 SHEET 38

Part: ANGLE — CRACKED (LT WING TE) · airframe 60,441 hrs · 35,783 cycles

CRACK ANGLE TRAILING EDGE AT LEVEL WS 278.50 LT WING / REPLACED ANGLE LOCATED ON TRAILING EDGE AT LEVEL WS 278.50 AT LT WING IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02 AND DWG 115A3712 SHEET 3. REV.- P/N USED 115A3757425

Part: PLATE — DETERIORATED (L1 DOOR GIRT BAR) · airframe 60,441 hrs · 35,783 cycles

DETERIORATED GIRT BAR ADAPTER PLATE ON FWD ENTRY AND SERVICE DOOR AT FWD GALLEY AREA (4 EA). REPLACED GIRT BAR ADAPTER PLATE ON FWD ENTRY AND SERVICE DOOR AT FWD GALLEY AREA (4 EA), IAW B737-700 SRM 51-10-02-REV 72 ITEM 9.

Part: BOLT — DETERIORATED (R1 DOOR GIRT BAR) · airframe 60,441 hrs · 35,783 cycles

DETERIORATED ENTRY AND SERVICE DOOR GIRT BAR FITTING HARDWARE AT FWD GALLEY AREA. REPLACED ENTRY AND SERVICE DOOR GIRT BAR FITTING HARDWARE AT FWD GALLEY AREA INSTALLATION IS DOCUMENTED IN MT 725-025-00-01Y.

Part: SPAR — CORRODED (RT WING) · airframe 60,441 hrs · 35,783 cycles

CORROSION FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APPROXIMATELY AT RT WING AND WBL 94.24. REPAIRED RT WING, FRONT SPAR WEB LOCATED AT 120.0 IFSS AT FUEL BOOST PUMP FAYING SURFACE, IAW EA NO 20-157-02589 REV IR AND EA NR 57-0819-20 REV 0 EWIS PROTECTION. REMOVED IAW AMM 20-60-07.

Part: ANGLE — CRACKED (BS 500B S26L) · airframe 60,441 hrs · 35,783 cycles

CRACK ANGLE - CLIP LOCATED ON BS 500B FWD FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT / REPLACED ANGLE-CLIP LOC. ON BS 500B AND ANGLE-CLIP 500A FWD FACE AT LEVEL STR.26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 ITEM 4 AND DWG #143A7505 REV.B; REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700 P/N USED 143A7502 U159

Part: FLOORBEAM — CRACKED (CABIN) · airframe 60,441 hrs · 35,783 cycles

CRACK ANGLE FLOOR STRUCTURE AT BS 693 AND BL 0 CENTER SECTION. REPLACED ANGLE LOCATED FLOOR STRUCTURE AT BS 693 AND BL 0 CENTER SECTION, IAW SRM B737-700 51-40-02 AND DWG 273A9111 SHEET 4 REV A DUE TO NO FOUND ALLOWABLE DAMAGE LIMITS IN SRM B737-700. FABRICATED ANGLE FROM BAC1490-2883 PO 2020195975.

Part: PLATE — DETERIORATED (R1 DOOR GIRT BAR) · airframe 60,441 hrs · 35,783 cycles

DETERIORATED GIRT BAR ADAPTER PLATE ON FWD ENTRY AND SERVICE DOOR AT FWD GALLEY AREA (4 EA). REPLACED GIRT BAR ADAPTER PLATE ON FWD ENTRY AND SERVICE DOOR AT FWD GALLEY AREA (4 EA), IAW B737-700 SRM 51-10-02-REV 72 ITEM 9.

Part: ANGLE — CRACKED (BS 400 S26L) · airframe 60,441 hrs · 35,783 cycles

CRACK ANGLE - CLIP LOCATED ON BS 400 AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT / REPLACED ANGLE-CLIP LOCATED ON BS400 AFT FACE AT LEVEL STR.26L AT FWD CARGO COMP. IAW SRM B737-700 51-40-02; 51-10-02 AND DWG#143A7505 REV.'B'; REPLACED ANGLE DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM B737-700 P/N USED: 143A7502U155

Part: FITTING — DETERIORATED (R1 DOOR GIRT BAR) · airframe 60,441 hrs · 35,783 cycles

DETERIORATED ENTRY AND SERVICE DOOR HARDWARE OF GIRBART FITTING AT AFT GALLEY AREA. REPLACED ENTRY AND SERVICE DOOR HARDWARE OF GIRT BAR FITTING AT AFT GALLEY AREA INSTALLATION IS DOCUMENT IN MT 725-025-00-02Y.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 60,441 hrs · 35,783 cycles

CRACK INDICATION FOUND ON BEAR STRAP AREA (INTERNAL) AROUND TO FASTENER LOCATED AT BS 294.5 BETWEEN S-8R TO S-9R NEAR TO FITTING LATCH FWD GALLEY DOOR (R1) CRACK LENGTH: 0.750 INCH APPROXIMATE. REPAIRED FUSELAGE SKIN BETWEEN BS 277 TO BS 312 STR 6R TO STR 10R, IAW B737-700 SRM 53-10-01-2R-6 REPAIR 6 FIGURE 202. FOR INSPECTION REQUIREMENTS SEE TLD T080514.

Part: SPAR — CORRODED (LT WING) · airframe 60,441 hrs · 35,783 cycles

CORROSION FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APPROXIMATELY AT LT WING AND WBL 94.24. REPAIRED LT WING FRONT SPAR WEB AT IFSS 120.00 AT FUEL BOOTS PUMP FAYING SURFACE, IAW EA NR 20-157-02599 REV IR AND EA 57-0854-20 REV 0 MEASURES OF THE REWORK AREA L=6.493'; W=3.901' MAX DEPTH=0.102' MATERIAL USED: ALUMINUM SHEET P/N 2024-T3 0.125' PO=2020 129976.

Part: FITTING — DETERIORATED (L1 DOOR GIRT BAR) · airframe 60,441 hrs · 35,783 cycles

DETERIORATED ENTRY AND SERVICE DOOR HARDWARE OF GIRBART FITTING AT AFT GALLEY AREA. REPLACED ENTRY AND SERVICE DOOR HARDWARE OF GIRT BAR FITTING AT AFT GALLEY AREA INSTALLATION IS DOCUMENT IN MT 725-025-00-02Y.

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 60,441 hrs · 35,783 cycles

CRACK GUSSET LOCATED BS 500D AT LEVEL STR 19L FWD CARGO COMPARTMENT / REPLACED GUSSET LOC. BS 500D AT LEVEL STR.19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 ITEM 4 AND DWG 143A7902 REV.- REPLACED GUSSET DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM; P/N USED 143A9481-6

Part: ANGLE — CRACKED (BS 500C S26L) · airframe 60,441 hrs · 35,783 cycles

CRACK ANGLE - CLIP LOCATED ON BS 500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT / REPLACED ANGLE-CLIP LOC. ON BS500C AT LEVEL STR.26L AT FWD CARGO COMPARTMENT IAW SRM B737-700 51-40-02; 51-10-02 AND DWG#143A7505 REV. 'B' REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700; P/N USED 143A7502 U159

Part: PRESSURE DECK — CRACKED (PAX CABIN) · airframe 60,441 hrs · 35,783 cycles

CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK AT LEVEL STA 663 AND LBL 32 PASSENGER CABIN CENTER SECTION. CRACK LENGTH: 0.196 INCH APPROXIMATE. PERFORMED PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK WEB BETWEEN STA 663.75 TO STA 675 AND LBL 30.00 TO LBL 60.00, IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 REPAIR PARTS: -1 DOUBLER 2024-T3 0.080'; -2 STIFFENER (7 EA) BAC 1505-100052 7075-T6511; -3 WEB 2024T3 0.063'; -4 FILLER 2024T3 0.080'; -5 FILLER 2024T3 0.020' (3 EA); -6 FILLER 2024T3 0.090' AND 0.020'; -7 FILLER 2024T3 0.080'; -8 FILLER 2024T3 0.080'; -9 FILLER 2024T3 0.080'.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 60,441 hrs · 35,783 cycles

CRACK INSPAR RIB 129.50 AT 27 INCHES FRONT SPAR LT HORIZONTAL STAB (1 EA). PERFORMED PERMANENT REPAIR INSPAR RIB 129.50 LT HORIZONTAL STAB PART NUMBER USED OPP 55100003-01. NOT FOUND ALLOWABLE DAMAGE IN SRM. REPAIR IAW B737-700 SRM 55-10-09-2R-4.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 60,441 hrs · 35,783 cycles

CRACK INSPAR RIB 120.30 AT 27 INCHES FRONT SPAR AT RT HORIZONTAL STABILIZER (1 EA). REPAIRED INSPAR RIB 120.30 AT 27 INCHES FRONT SPAR AT RT HORIZONTAL STABILIZER, IAW B737-700 55-10-09-2R-5 REPAIR 5. PART USED PN SWA 55100003-01.

Part: SKIN — CRACKED (RT WING) · airframe 60,441 hrs · 35,783 cycles

CRACK OUTBOARD FIXED LEADING EDGE SKIN LOCATED AT OF SS 425 LEVEL AT RT WING (1 EA). REPAIRED OUTBOARD FIXED LEADING EDGE SKIN LOCATED AT SS 425 LEVEL AT RT WING, IAW B737-700 SRM 57-41-01-2R-1 REPAIR 1 AND SRM 57-41-01-2R-1 REPAIR 1 AND SRM 51-70-05-2R-10 REPAIR 10.

Part: SUPPORT BRACKET — BROKEN (LT WING TE) · airframe 60,441 hrs · 35,783 cycles

BROKEN SUPPORT BRACKET LOCATED BETWEEN WS 278.50 AND WS 253.00 TRAILING EDGE AT LT WING / REPLACED ANGLE (SUPPORT BRAKET) LOC BTW WS 278.50 AND WS 253.00 TRAILING EDGE IAW SRM B737-700 51-40-02; 51-10-02 AND DWG #115A2930 REV .- PN USED 115A2953-1

Part: ANGLE — CRACKED (LT WING) · airframe 60,441 hrs · 35,783 cycles

CRACK ANGLE TRAILING EDGE LOCATED AT LEVEL WS 278.50 LT WING / REPLACED ANGLE LOC. TRAILING EDGE AT LEVEL WS 278.50 LT WING P/N NEW ANGLE: 115A6260-1 IAW B737-700 SRM 51-10-02 DWG 115A6200-19 REV.A

Part: SUPPORT ANGLE — CRACKED (R/H WING) · airframe 60,441 hrs · 35,783 cycles

CRACK REAR SPAR SUPPORT ANGLE LOCATED BETWEEN SPOILER 5 AND 6 ORSS 271 AT RT WING (1 EA) / REPLACED SUPPORT ANGLE LOCATED BETWEEN SPOILER 5 AND 6 ORSS 271 AT RT WING (1EA) IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 AND DRAWING #115A2930 REV:- P/N 115A2953-2 BATCH 549524 REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 59,851 hrs · 35,415 cycles

EMERGENCY EXIT SIGN AT THE OVERWING IS LOOSE. SECURED OVERWING EXIT SIGN PER S.I.P.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,303 hrs · 35,069 cycles

EMERGENCY ASILE LIGHTS AT STATION 560-620 LBL AND BOTH OVER WING EXIT LIGHTS OUT AT STATION 747 ARE OUT. REMOVED AND REPLACED BATTERY PACK AT STATION 727C & B WL 212 LBL 68 SYSTEM OPS CHECKS GOOD POS M1670 P/N OFF/ON D-717-01-100SWA S/N OFF 81550 S/N ON 211234.

Part: HANDLE — DAMAGED (FWD CARGO DOOR) · airframe 59,282 hrs · 35,054 cycles

FWD CARGO DOOR HANDLE HOUSING DAMAGED. / R&R'D FWD CARGO DOOR HANDLE ASSY REF SRM 51-40-02 AND SRM 51-10-02

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,185 hrs · 33,066 cycles

LT EXTERIOR OVERWING LIGHT (L6) INOP. RELAMPED LIGHT PER AMM.

Part: BATTERY PACK — DISCHARGED (EXTERIOR) · airframe 56,185 hrs · 33,066 cycles

R1 DOOR EMERGENCY LIGHT AFT ON THE EXTERIOR INOP. R&R BATTERY PACK M1674 PER AMM AND WDM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 56,185 hrs · 33,066 cycles

EMERGENCY LIGHT BATTERY PACK M1670 DISCHARGED. R&R CHARGER ASSEMBLY PER AMM AND WDM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,185 hrs · 33,066 cycles

EMERGENCY LIGHT BATTERY PACK M1674 DISCHARGED. R&R BATTERY PACK M1624 PER AMM AND WDM.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 56,185 hrs · 33,066 cycles

***CORROSION*** UPPER SURFACE OF AFT CARGO FLOOR 140CF STA 794 TO STA 868 WL 156 RB16. / FABRICATED AFT CARGO FLOOR PANEL 140CF IAW AMM 25-52-01-201-801. DRG # 453A2010-2 LOT # 5079180-1 THICKNESS .080 2024T3 CLAD. 57309U 5/2/19

Part: STRINGER SPLICE — DAMAGED (FUSELAGE) · airframe 56,185 hrs · 33,066 cycles

STRINGER SPLICE DAMAGED ATA BS. 351.2, STR. 28R. REPAIRED STRINGER SPLICE PER EA.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 56,185 hrs · 33,066 cycles

INSERT MISSING AND CORNER CRACKED I/B SIDE FWD PANEL 221GF / REPLACED AND REPAIRED MISSING INSERT AND CORNER CRACKED I/B SIDE FWD PANEL 221GF. VALIDATED APPLICABILITY OF REPAIR IAW SRM 53-00-50-2R-6. DAMAGE DETERMINED TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1; PARA 4F DELAMINATION NOT PERMITTED. 57795U 26APR19

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,185 hrs · 33,066 cycles

FUSELAGE SKIN CORRODED BETWEEN BS. 890 TO BS. 1006, BETWEEN STR. 2L TO STR. 2R. REPAIRED SKIN IAW ER AND EA.

Part: TRACK — CRACKED (HORIZONTAL STAB) · airframe 56,185 hrs · 33,066 cycles

RIGHT HAND HORIZONTAL STABILIZER PANEL 343AT FWD TRACK HAS A CRACK / REMOVE AND REPLACE RIGHT HAND HORIZONTAL STABILIZER PANEL 343AT FWD TRACK IAW SRM 51-40-02-0G-0 59710U 04/26/2019

Part: FLAP — DELAMINATED (R/H WING) · airframe 56,185 hrs · 33,066 cycles

RT WING O/B AFT FLAP LOWER SURFACE I/B LOWER CORNER HAS DELAMINATION / REPAIRED RT WING O/B AFT FLAP LOWER SURFACE I/B LOWER CORNER I.A.W 737 SRM 57-53-01-2R-4 & I.A.W 737 SRM 51-70-10-2R-4; DAMAGE WAS PAST ALLOWABLE LIMITS I.A.W 737 SRM 57-53-01-1A-4 PARA 4A(5)

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 56,185 hrs · 33,066 cycles

SIDE PANEL CRACKED AT 3RD FASTENER HOLE DOWN AT BS. 663, LBL 48. / R&R WEB IAW DWG & SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,185 hrs · 33,066 cycles

LOWER STRINGER SURFACE CRACKED AT BS. 372, STR. 28R. REPAIRED STRINGER IAW ER AND EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,185 hrs · 33,066 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS. 767 TO BS. 787, STR. 27R. R&R INTERCOSTAL IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 889-907) · airframe 56,185 hrs · 33,066 cycles

AFT CARGO ZEE ANGLE CORRODED BETWEEN BS. 889 TO BS. 907, RBL 21. / R&R ANGLE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,185 hrs · 33,066 cycles

ZEE ANGLE CORRODED BETWEEN BS. 727C TO BS. 807, LBL 21. R&R ZEE ANGLE PER SRM AND DWG.

Part: INTERCOSTAL — CORRODED (BS 795) · airframe 56,185 hrs · 33,066 cycles

INTERCOSTAL CORRODED AT BS 795, RBL 6, WL 150 / R&R INTERCOSTAL PER SRM.

Part: ANGLE — CORRODED (BS 727D-767) · airframe 56,185 hrs · 33,066 cycles

ZEE ANGLE CORRODED AT BS 727D - 767, RBL 21, WL 156. / R&R ANGLE PER SRM.

Part: SUPPORT — CORRODED (BS 500C-500D) · airframe 56,185 hrs · 33,066 cycles

FORWARD CARGO R/H FLOOR TO SIDEWALL Z CORRODED BETWEEN BS. 500C TO BS. 500D, RBL 24. / R&R ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FWD CARGO) · airframe 56,185 hrs · 33,066 cycles

***CORROSION*** FWD CARGO AFT BULKHEAD ATTACH ANGLE LBL22-RBL24 STA500D WL156 / CORROSION OUT OF LIMITS DUE TO NO LIMITS FOUND IN SRM. REMOVED AND REPLACED FWD CARGO AFT BULKHEAD ATTACH ANGLE LBL 2415 RBL 24 AT STA 500D. I-A-W SRM 51-40-02-0G-0. AND BDWG# 143A7902. PO# 731180

Part: SHIELD — CORRODED (BS 854-867) · airframe 56,185 hrs · 33,066 cycles

AFT CARGO AFT SHIELD CORRODED BETWEEN BS. 854 TO BS. 867, RBL 21. / R&R SHIELD IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 867-887) · airframe 56,185 hrs · 33,066 cycles

AFT CARGO ZEE ANGLE CORRODED BETWEEN BS. 867 TO BS. 887, RBL 21. / R&R ZEE ANGLE PER SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,185 hrs · 33,066 cycles

FORWARD CARGO FLOOR TO SIDEWALL Z CORRODED BETWEEN BS. 500A TO BS. 500B+10, LBL 24. REPAIRED Z ANGLE IAW SRM AND DWG.

Part: SHIELD — CORRODED (BS 767-787) · airframe 56,185 hrs · 33,066 cycles

AFT CARGO SHIELD BS 767-787, RBL 21, WL 156 IS CORRODED. REMOVED AND REPLACED SHIELD IAW SRM.

Part: SHIELD — CORRODED (BS 420-440) · airframe 56,185 hrs · 33,066 cycles

FORWARD CARGO SHIELD CORRODED FORWARD OF DOOR RBL24 STA420-440 WL156 / R&R SHIELD PER SRM AND DWG.

Part: SKIN — CRACKED (RT WING) · airframe 56,185 hrs · 33,066 cycles

FOUND #6 SLAT FLEX SKIN BROKEN DURING REMOVAL FOR REPAIR. / REPAIRED #6 FLEX SKIN I.A.W ATS E.R 19-02730 REV IR; I.A.W S.W.A E.A 1-757-16171 REV IR

Part: GUSSET — CRACKED (BS 500D) · airframe 56,185 hrs · 33,066 cycles

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

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,185 hrs · 33,066 cycles

VERTICAL PRESSURE WEB CRACKED AT BS. 663, LBL 40. REPAIRED WEB IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 56,185 hrs · 33,066 cycles

CRACK NOTED AT BS-663+10" RBL-43 WL-201 COMMON TO HORIZONTAL PRESSURE DECK WEB. / REPAIRED WEB PER SRM.

Part: GUSSET — CRACKED (BS 500D) · airframe 56,185 hrs · 33,066 cycles

FWD CARGO GUSSET CRACKED AT STA 500D STR 19R. R&R GUSSET PER SRM.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 56,185 hrs · 33,066 cycles

RT LOWER VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT BS. 663. REPAIRED ANGLE PER ER AND EA.

Part: PANEL — CRACKED (LOWER EXT FUSELA) · airframe 56,185 hrs · 33,066 cycles

ACCESS PANEL 195BL COMPOSITE CRACKED AROUND FASTENER HOLE. (MARKED) / REPAIRED CRACKS AROUND FASTENER HOLE ON ACCESS PANEL 195BL PER SRM 53-40-70-2R-1 AND SRM 51-70-05-2R-8

Part: PANEL — DEBONDED (LOWER EXT FUSELA) · airframe 56,185 hrs · 33,066 cycles

ACCESS PANEL 192BL FORWARD LOWER CORNER DISBANDED. (MARKED) / DISBANDED FORWARD LOWER CORNER ON ACCESS PANEL 192BL REPAIRED IAW SRM 53-40-70-2R-1 TABLE 202 AND IAW SRM 51-70-05-2R-10. DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PARA 4B(8). DAMAGE GREATER THAN 2 PLIES IN DEPTH.

Part: SKIN — CRACKED (SLAT) · airframe 56,185 hrs · 33,066 cycles

LT WING; L/E #3 LOWER SURFACE OF L/E SLAT NOSE SKIN AT ACTUATOR RIBS HAS WORKING FASTENERS. / REMOVED WORKING FASTNERS; REMOVED DAMAGED AREA AND INSTALLE REPAIR ON L/H WING L/E #3 LOWER SURFACE L/E SLAT NOSE SKIN AT ACTUATOR SKIN IAW SRM 51-40-02-0G-0 AND SRM 57-42-01-2R-8

Part: DOOR — CORRODED (LOWER EXT FUSELA) · airframe 56,185 hrs · 33,066 cycles

***CORROSION*** TOILET SERVICE DOOR INNER SURFACE CORRODED STA860 WL160 STR25L / UPON EVALUATION OF THE WASTE TANK SERVICE DOOR FOUND DAMAGE OUT OF LIMITS; DAMAGE DIMENSIONS: L=2.2'; W=2.2'; D=0.08' I.A.W SRM 52-40-01-1A-4 FIG. 103; DETAIL 4; REMOVED AND REPLACED WASTE TANK SERVICE DOOR; BONDING TEST AND FIT CHECK COMPLIED WITH I.A.W AMM 52-49-07-400-801 AND AMM 52-9-07-000-802. 59600U 04-19-19 BONDING AND FIT CHECK GOOD STA 860 WL 16. STR 25L.

Part: SKIN — CRACKED (SLAT) · airframe 56,185 hrs · 33,066 cycles

LT WING; L/E #2 LOWER SURFACE OF L/E SLAT NOSE SKIN AT ACTUATOR RIBS HAS FASTENER HOLE CRACK. / REMOVED DAMAGED AREA AND INSTALLED REPAIR AT L/H WING L/E #W LOWER SURFACE OF L/E SLAT NOSE SKIN AT ACTUATOR RIB IAW SRM 51-40-02-0G-0 AND SRM 57-42-01-2R-8

Part: FLAP — DELAMINATED (RT WING) · airframe 56,185 hrs · 33,066 cycles

RT WING OUTBOARD TRAILING AFT FLAP DELAMINATED ON INBOARD EDGE ON TRAILING EDGE. REPAIRED AFT FLAP PER EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,185 hrs · 33,066 cycles

R/H FORWARD OVERWING EMERGENCY EXIT LIGHT ABOVE DOOR INOP. R&R LAMP IAW AMM.

Part: FLAP — DELAMINATED (L/H WING) · airframe 56,185 hrs · 33,066 cycles

L/H WING OUTBOARD TRAILING AFT FLAP HAS A 6' DELAMINATION 1/2' OF INBOARD EDGE ON THE TRAILING EDGE. DAMAGE IS IN BOTH ZONE 1 AND ZONE 2 PER SRM 57-53-01-1A-5 / ACCOMPLISHED EA #1-757-16107. SPEED TAPE AREA REQUIRES A VISUAL INSPECTION ONCE PER DAY FOR LOOSE OR MISSING SPEED TAPE. IF THE SPEED TAPE IS DAMAGED OR MISSING ACCOMPLISH A DETAILED VISUAL INSPECTION TO VERIFY DELAMINATION HAS NOT GROWN IN SIZE AND APPLY NEW SPEED TAPE PER STEP 4 AND 5 IN EA 1-757-16107. CONTACT SERVICE ENGINEERING IF NEW DAMAGES WERE FOUND. REPAIR OR REPLACE THE L/H AFT FLAP PER SRM 57-53-01-2R. WITHIN 20 CYCLES . CONTINUE ON LP#0943659

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 55,793 hrs · 32,819 cycles

R1 SLIDE WAS SLIGHTLY DISLODGED FROM ITS COMPARTMENT. SECURED SLIDE PER AMM & TC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,361 hrs · 31,878 cycles

RT EMERGENCY EXIT WINDOW LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 53,958 hrs · 31,629 cycles

R1 DOOR SLIDE GIRT BAR STUCK. CLEANED AND LOOSENED GIRT BAR PER SIP.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 53,164 hrs · 31,115 cycles

R1 DOOR EXIT SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: NONE — CRACKED (LT HORIZ STAB) · airframe 51,593 hrs · 30,119 cycles

SUPPLEMENTAL INFORMATION: LEFT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED. / REMOVED AND REPLACED LEFT HORIZ STAB UPPER FWD SLIDING SEAL PER MM 53-31-31

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 51,593 hrs · 30,119 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT LOCATION M01675. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 51,593 hrs · 30,119 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT LOCATION M01673. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 51,593 hrs · 30,119 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT LOCATION M01669. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 51,593 hrs · 30,119 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT LOCATION M01672. R & R THE BATTERY IAW AMM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 50,425 hrs · 29,381 cycles

L2 DOOR EMERGENCY EVAC SLIDE ATTACH BOLT LOOSE. SECURED SLIDE ASSEMBLY PER SIP.

Part: GLOWSTRIP — OUT OF ADJUST (CABIN) · airframe 49,530 hrs · 28,846 cycles

FORWARD GALLEY AREA PHOTOLUMINESCENT STRIP OUT OF ADJUST. ADJUSTED STRIP IAW DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,530 hrs · 28,846 cycles

FLOORBEAM SURFACE CORRODED AT BS 727D+7, RBL 8. REPAIRED FLOORBEAM PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,530 hrs · 28,846 cycles

FLOOR SUPPORT CORRODED AT BS 772, LBL 21. REPAIRED SUPPORT PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,530 hrs · 28,846 cycles

FLOORBEAM SURFACE CORRODED AT BS 727D+7, RBL 3. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,530 hrs · 28,846 cycles

FLOORBEAM SURFACE CORRODED AT BS 727D+7, LBL 3. REPAIRED FLOORBEAM PER SRM.

Part: CARGO TRACK — CORRODED (BS 727D) · airframe 49,530 hrs · 28,846 cycles

CARGO TRACK CORRODED AT BS 727D+7, RBL 14. R & R THE CARGO TRACK IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 49,530 hrs · 28,846 cycles

FLOOR STRAP CORRODED AT BS 767+5, BETWEEN LBL 21 TO RBL 19. R&R STRAP PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,530 hrs · 28,846 cycles

FLOOR SUPPORT CORRODED AT BS 772, LBL 8. REPAIRED SUPPORT PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,530 hrs · 28,846 cycles

FLOOR SUPPORT CORRODED AT BS 772, LBL 14. REPAIRED SUPPORT PER SRM.

Part: CARGO TRACK — CORRODED (BS 772) · airframe 49,530 hrs · 28,846 cycles

AFT CARGO TRACK CORRODED AT BS 772, RBL 3. R & R THE CARGO TRACK IAW SRM.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 49,530 hrs · 28,846 cycles

FLOORBEAM CORRODED AT BS. 772, RBL 8. REPAIRED FLOORBEAM IAW EA.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 49,530 hrs · 28,846 cycles

FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED THE FLOORBEAM IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 49,530 hrs · 28,846 cycles

LT WING OUTBOARD AFT FLAP UPPER SKIN DELAMINATED AT INBOARD END. R&R AFT FLAP PER MM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 49,530 hrs · 28,846 cycles

LEFT WING NR 3 SLAT SKIN CRACKED AT ACTUATOR ATTACH FITTING, OTBD ROW SECOND AFT OF FORWARD HOLE. REPAIRED THE SKIN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 44,898 hrs · 26,105 cycles

LONGITUDINAL FLOORBEAM FLANGE FWD OF BS 727B, RBL 25, OTBD AFT HOLE CRACKED. REPAIRED FLANGE IAW ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 44,898 hrs · 26,105 cycles

LONGITUDINAL FLOORBEAM FLANGE FWD OF BS 727B, RBL 45, BOTH FWD HOLES CRACKED. REPAIRED FLANGE IAW ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 44,898 hrs · 26,105 cycles

LONGITUDINAL FLOORBEAM FLANGE CRACKED AT BS 727B, LBL 45, FWD OF BOTH AFT HOLES. REPAIRED FLANGE IAW EA & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 44,898 hrs · 26,105 cycles

LONGITUDINAL FLOORBEAM FLANGE FWD OF BS 727B, LBL 25, BOTH OTBD & INBD AFT HOLES CRACKED. REPAIRED FLANGE IAW ER & EA.

Part: POST — CRACKED (FUSELAGE) · airframe 44,898 hrs · 26,105 cycles

RIGHT NR 3 FLIGHT DECK WINDOW FRAME E - F POST, 2ND LOWER FASTENER HOLE CRACKED. REPAIRED POST IAW ER & EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,420 hrs · 25,240 cycles

LEFT HORIZONTAL LOWER IN SPAR SKIN CRACKED AT STATION 138.70 APPROX 26" AFT OF LE SPAR. REPAIRED SKIN IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,263 hrs · 25,151 cycles

LEFT DOOR EMER EXIT LIGHT SIGN BATTERY PACK INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: POST — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

LEFT FWD EXTERNAL FUSELAGE WINDOW POST CRACKED. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

LEFT NR 3 WINDOW FRAME E - F POST CRACKED AT SECOND LOWER FASTENER HOLE. REPAIRED POST IAW ACO.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 43,263 hrs · 25,151 cycles

RIGHT HORIZONTAL STABILIZER LE RIB CRACKED AT STATION 95.96. R & R RIB IAW SRM & DWG.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 43,263 hrs · 25,151 cycles

RIGHT PHOTO LUMINESCENT STRIPS CRACKED. R & R STRIP IAW AMM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 43,263 hrs · 25,151 cycles

LEFT PHOTO LUMINESCENT STRIPS CRACKED. R & R STRIP IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 43,263 hrs · 25,151 cycles

NUMBER 4 GALLEY EMER EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

STRINGER CRACKED AT BS 540, STRINGER 23R. REPAIRED STRINGER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 43,263 hrs · 25,151 cycles

LEFT WING SUPPORT BRACKET CRACKED ON LOCATED ON INTERNAL STRUCTURE OF TE BETWEEN ORSS 287 TO 329. R & R BRACKET IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

SUPPORT WEB INTERCOSTAL CRACKED BETWEEN BS. 312 - 328, RBL 34. R & R INTERCOSTAL IAW SRM & DWG.

Part: LENS — BROKEN (CABIN) · airframe 43,263 hrs · 25,151 cycles

FORWARD LAVATORY OUTSIDE WALL MOUNTED EMER LIGHT LENS ASSEMBLY BROKEN. R & R LENS ASSEMBLY IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 43,263 hrs · 25,151 cycles

LEFT WING LE SLAT NR 1 NOSE SKIN CRACKED ON LOWER SURFACE AT STATION 451.97. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,263 hrs · 25,151 cycles

RIGHT WING LE NR 6 SLAT SKIN CRACKED ON LOWER SURFACE AT STATION 202.45. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,263 hrs · 25,151 cycles

RIGHT WING LE NR 8 SLAT SKIN CRACKED ON LOWER SURFACE AT STATION 451.97. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,263 hrs · 25,151 cycles

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

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

RIGHT NR 1 WINDOW FRAME CRACKED ON INTERNAL SURFACE AT UPPER CORNER. REPAIRED FRAME IAW ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: FAIRING — CRACKED (RT WING) · airframe 43,263 hrs · 25,151 cycles

RIGHT WING AFT TRACK FAIRING NR 6 642BB CRACKED. R & R FAIRING IAW AMM.

Part: SKIN — CRACKED (LT WING FAIRING) · airframe 43,263 hrs · 25,151 cycles

LEFT WING AFT FAIRING SKIN AT FLAP SUPPORT NR 3 CRACKED ON INTERNAL AREA OF TE FLAP FAIRING 542BB. REPAIRED FAIRING IAW EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: FAIRING — CRACKED (LT WING) · airframe 43,263 hrs · 25,151 cycles

LEFT WING FWD EDGE OF FAIRING 542BB CRACKED. REPAIRED FAIRING IAW EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,263 hrs · 25,151 cycles

INTERCOSTAL SUPPORT CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24.5. R & R INTERCOSTAL IAW SRM & DWG.

Part: IDG — FAULTY (NR 2 ENGINE) · airframe 42,652 hrs · 24,814 cycles

AIR TURN BACK, SOURCE OFF LIGHT ILLUMINATED, DETERMINED THAT THE NR 2 GEN WAS LOST. TWO HIGH ALTITUDE APU STARTS WERE UNSUCCESSFUL, ALONE WITH A THIRD UNSUCCESSFUL APU START AT 241000 FT. THE APU FAULT LIGHT ILLUMINATED. R & R NR 2 IDG IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,265 hrs · 24,603 cycles

LEFT OVERWING EXTERNAL OVERWING EMER EXIT LIGHT INOPERATIVE. RE LAMPED LIGHT IAW AMM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 40,618 hrs · 23,630 cycles

DIVERSION, FIRST OFFICER`S NR 1 WINDOW CRACKED. R & R WINDOW IAW MM.

Part: ANGLE — BROKEN (L1 DOOR SLIDE) · airframe 39,827 hrs · 23,166 cycles

L1 DOOR EMERGENCY EVAC SLIDE MOUNTING ANGLE BROKEN. R & R SLIDE IAW MT.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 37,769 hrs · 21,920 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 37,489 hrs · 21,744 cycles

L2 DOOR EXIT LIGHT SIGN COVER LOOSE. R&R LIGHT ASSEMBLY IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 37,263 hrs · 21,612 cycles

R1 DOOR EMERGENCY EXIT SIGN BROKEN. R&R SIGN IAW AMM.

Part: ACM — FAULTY (AC BAY) · airframe 37,027 hrs · 21,481 cycles

DECLARED EMERGENCY. ACFT DEPRESSURIZED SLOWLY ON DECENT THROUGH FL380. PACKS WERE IN HIGH RECIRC FAN ON. CLIMB RATE FOR CABIN SHOWED ABOUT 2500 FPM AC DECENT INITIALLY 2400 FPM THEN INCREASED TO 4500 FPM. HIGHEST CABIN ALTITUDE NOTED WAS 10,500FT, CABIN WARNING HORN SOUNDED. CABIN ALT DROPPED BELOW 10,000FT FL330 OR THERE ABOUT. FWD POBS WERE USED BY F/A'S IN FWD AIRCRAFT. R & R RT PACK AIR CYCLE MACHINE IAW MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 36,364 hrs · 21,103 cycles

RIGHT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 129.5 RIB. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 36,364 hrs · 21,103 cycles

RIGHT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT REAR SPAR, BETWEEN STAB STA RIB 92.7-101.9. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 36,364 hrs · 21,103 cycles

LEFT HORIZONTAL STAB LOWER INSPAR SKIN CRACKED AT STAB STA 147.90. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 36,364 hrs · 21,103 cycles

LEFT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 157.10 RIB. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 36,364 hrs · 21,103 cycles

RIGHT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT REAR SPAR BETWEEN STAB STA RIB 92.7-101.9. REPAIRED SKIN IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 36,364 hrs · 21,103 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 92.70 CRACKED. REPAIRED RIB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 36,364 hrs · 21,103 cycles

LEFT WING COVE SEAL RETAINER SUPPORT ANGLE CRACKED ABOVE NR 1 PYLON AFT TIP. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 36,364 hrs · 21,103 cycles

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

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 36,364 hrs · 21,103 cycles

RIGHT WING T/E COVE SEAL RETAINER SUPPORT ANGLE CRACKED ABOVE NR 2 PYLON AFT TIP. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 36,016 hrs · 20,906 cycles

RIGHT FWD SERVICE DOOR SLIDE FELL OUT OF CASE. INSTALLED/REPOSITIONED SLIDE BACK INTO CASE IAW AMM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 34,511 hrs · 20,015 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER M/M.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 34,511 hrs · 20,015 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER M/M.

Part: COVER — BROKEN (CABIN) · airframe 34,323 hrs · 19,902 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 33,520 hrs · 19,405 cycles

R1 DOOR EMERGENCY EXIT LENS ASSY BROKEN. REMOVED AND REPLACED LENS ASSY PER M/M.

Part: SIGN — LOOSE (CABIN) · airframe 33,272 hrs · 19,266 cycles

CABIN CENTER AISLE O/H EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 33,272 hrs · 19,266 cycles

EEPLS COVERS CRACKED BETWEEN ROW 11 TO ROW 10. REMOVED AND REPLACED COVERS PER MM.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 32,821 hrs · 18,994 cycles

CROSSVALVE C/B TRIPPED FUEL IMBALANCE. REMOVED AND REPLACED CROSSFEED ACTUATOR PER AMM.

Part: LIGHT — CRACKED (CABIN) · airframe 32,123 hrs · 18,569 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS CRACKED BETWEEN ROW 1 TO ROW 13. REMOVED AND REPLACED EEPLS PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 32,090 hrs · 18,548 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 32,090 hrs · 18,548 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 31,041 hrs · 17,948 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 31,041 hrs · 17,948 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 31,041 hrs · 17,948 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 10. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 30,418 hrs · 17,588 cycles

LT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: FUSE — BLOWN (CABIN) · airframe 29,773 hrs · 17,212 cycles

DURING SCHEDULED HC1 CHECK FOUND, LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED FUSE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 29,773 hrs · 17,212 cycles

DURING SCHEDULED HC1 CHECK FOUND, EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 13. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 29,773 hrs · 17,212 cycles

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

Part: LENS — CRACKED (CABIN) · airframe 29,773 hrs · 17,212 cycles

DURING SCHEDULED HC1 CHECK FOUND, LT EEPLS LENS CRACKED AT ROW 14. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 29,773 hrs · 17,212 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 29,773 hrs · 17,212 cycles

DURING SCHEDULED HC1 CHECK FOUND, EEPLS COVER CRACKED BETWEEN ROW 14 TO ROW 21. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,688 hrs · 17,160 cycles

DURING SCHEDULED 8Y CHECK FOUND, FWD EMERGENCY FLOOR LIGHTING, LIGHTS INOP. REPAIRED EEPLS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 29,569 hrs · 17,086 cycles

DURING SCHEDULED 8Y CHECK FOUND, AFT LAV EMERGENCY EXIT SIGN LENS PLASTIC BOTTOM MOUNT CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LENS — DAMAGED (CABIN) · airframe 29,569 hrs · 17,086 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD LAV EMERGENCY EXIT LIGHT LENS DAMAGED. REMOVED AND REPLACED FWD LAV EMERGENCY LIGHT LENS PER AMM.

Part: LENS — BROKEN (CABIN) · airframe 29,569 hrs · 17,086 cycles

DURING SCHEDULED 8Y CHECK, FOUND BROKEN CABIN EMERGENCY EXIT EGRESS LIGHT LENS ON STOWAGE BIN BULLNOSE. REMOVED AND REPLACED LIGHT LENS PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,569 hrs · 17,086 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CENTER CABIN, LAST TWO FLOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY'S PER AMM.

Part: FASTENER — CORRODED (GIRT BAR) · airframe 29,569 hrs · 17,086 cycles

DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FASTENER CORRODED. REMOVED AND REPLACED FASTENER PER SRM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 29,569 hrs · 17,086 cycles

DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR BRACKET CORRODED. REMOVED AND REPLACED BRACKET PER SRM AND BAC DWG.

Part: LENS — BROKEN (CABIN) · airframe 29,510 hrs · 17,055 cycles

FWD EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: OUTFLOW VALVE — FAULTY (CARGO BAY) · airframe 28,856 hrs · 16,684 cycles

DIVERSION/DECLARED EMERGENCY. AT 40K AUTO FAIL IN PRESS THEN ALTN - FAIL ALL DASHES ON PANEL CABIN ALT NEVER ABOVE 13K. REMOVED AND REPLACED OUTFLOW VALVE AND NR 2 CABIN PRESSURE CONTROLLER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 27,934 hrs · 16,148 cycles

FWD EEPLS LOOSE. SECURED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,273 hrs · 15,764 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,046 hrs · 15,631 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 25,364 hrs · 14,622 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING I/B MID FLAP WEDGE DELAMINATED. REPAIRED WEDGE PER AAR EA.

Part: SLAT — CRACKED (LT WING) · airframe 25,364 hrs · 14,622 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 3 SLAT CRACKED. REMOVED AND REPLACED NR 3 SLAT PER MM.

Part: LENS — BROKEN (CABIN) · airframe 25,364 hrs · 14,622 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 23,990 hrs · 13,771 cycles

AFT GALLEY DOOR EGRESS LIGHT BASE BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 23,828 hrs · 13,669 cycles

AFT GALLEY LOWER EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 22,706 hrs · 13,000 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 22,706 hrs · 13,000 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 18,287 hrs · 10,248 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 17,256 hrs · 9,655 cycles

RIGHT FWD CABIN EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: COVER — LOOSE (CABIN) · airframe 16,057 hrs · 8,951 cycles

EEPLS COVER LOOSE AT ROW 2 ABC. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 15,918 hrs · 8,885 cycles

EEPLS COVER CRACKED AT ROW 1 ABC. R&R COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 15,730 hrs · 8,780 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 2 ABC AND ROW 4 ABC. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,730 hrs · 8,780 cycles

DURING SCHEDULED HC1 CHECK, FOUND LEFT FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 14,696 hrs · 8,213 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 14,480 hrs · 8,088 cycles

DURING SCHEDULED MV3 CHECK, FOUND EEPLS COVER CRACKED AT ROW 16 ABC. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,911 hrs · 7,203 cycles

EMERGENCY EXIT LIGHT INOP AT L2 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 11,205 hrs · 6,200 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 9,497 hrs · 5,269 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 8,918 hrs · 4,962 cycles

EEPLS TRACK LENS BROKEN AT MID CABIN. INSTALLED LENS PER MM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 7,530 hrs · 4,204 cycles

R2 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 6,541 hrs · 3,636 cycles

R2 DOOR EVAC SLIDE FELL, OUT DID NOT DEPLOY. REINSTALLED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 6,000 hrs · 3,333 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: LENS — BROKEN (EMERGENCY SIGN) · airframe 5,360 hrs · 2,960 cycles

DURING SCHEDULED MV3 CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 3,902 hrs · 2,147 cycles

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