N760SW

Part: GIRT BAR — OUT OF ADJUST (PAX DOOR) · airframe 76,779 hrs · 45,798 cycles

GIRT BAR WILL NOT ENGAGE AFT ENTRY DOOR ON CA SIDE / [01] R/R AFT ENTRY SIDE GIR BAR PER AMM 25-66-01. OPS CHK GOOD

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 76,573 hrs · 45,667 cycles

R/H HORIZONTAL FWD UPPER SLIDING SEAL CRACKED. / [01] REMOVED AND REPLACED R/H HORIZONTAL FWD UPPER SLIDING SEAL PER AMM 53-31-31

Part: ROPE — OUT OF ADJUST (ZN 900 LAV/GALLE) · airframe 76,573 hrs · 45,667 cycles

CABIN RH OVERWING EXIT EMERGENCY ROPE NOT SECURED PROPERLY / [01] RE-SECURED CABIN RH OVERWING EXIT EMERGENCY ROPE; PER AMM 25-61-10

Part: GIRT BAR — LOOSE (ZN 800 DOOR) · airframe 76,573 hrs · 45,667 cycles

FWD ENTRY DOOR SLIDE GIRT BAR AFT RETAINER CLIP FASTENERS ARE LOOSE / [01] ADJUSTED FWD ENTRY DOOR SLIDE GIRT BAR AFT RETAINER CLIP PER MT725-61-06 AND AMM 25-66-00

Part: GIRT BAR — OUT OF ADJUST (ZN 800 DOOR) · airframe 76,573 hrs · 45,667 cycles

FWD ENTRY SLIDE GIRT REQUIRES ADJUSTMENT / [01] ADJUSTED FWD ENTRY SLIDE GIRT PER MT725-61-06 AND AMM 25-66-00

Part: GIRT BAR — OUT OF POSITION (ZN 800 DOOR) · airframe 76,573 hrs · 45,667 cycles

AFT ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT / [01] AFT ENTRY DOOR SLIDE GIRT PER MT725-61-06 AND AMM 25-66-00;[02] ADJUSTED AFT ENTRY DOOR SLIDE GIRT PER MT725-61-06 AND AMM 25-66-00

Part: GIRT BAR — OUT OF POSITION (ZN 800 DOOR) · airframe 76,573 hrs · 45,667 cycles

AFT ENTRY DOOR SLIDE GIRT BAR RETAINER CLIPS REQUIRE ADJUSTMENT / [01] ADJUSTED AFT ENTRY DOOR SLIDE GIRT BAR RETAINER CLIPS PER MT 725-61-06 AND AMM 25-66-01

Part: GIRT BAR — OUT OF POSITION (ZN 800 DOOR) · airframe 76,573 hrs · 45,667 cycles

AFT SERVICE DOOR SLIDE GIRT BAR RETAINING CLIP NEEDS TO BE ADJUSTED / [01] ADJUSTED AFT SERVICE DOOR SLIDE GIRT BAR RETAINING CLIP PER MT725-61-06 AND AMM 25-66-00

Part: GIRT BAR — OUT OF ADJUST (ZN 800 DOOR) · airframe 76,573 hrs · 45,667 cycles

AFT SERVICE DOOR SLIDE GIRT REQUIRES ADJUSTMENT / [01] ADJUSTED AFT SERVICE DOOR SLIDE GIRT PER MT725-61-06 AND AMM 25-66-00

Part: BATTERY — FAILED (ZN 900 LAV/GALLE) · airframe 76,573 hrs · 45,667 cycles

TWO EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY CHECK. FWD LEFT AREA AND MID RIGHT CABIN. / [01] REPLACED RT OVER WING BATTERY PACK; DEEP. CYCLED FRONT LEFT BATTERY PACK AND REPLACED RT EMERGENCY EXIT LIGHT LENS PER AMM 33-51-06

Part: BATTERY — INOPERATIVE (ZN 900 LAV/GALLE) · airframe 76,573 hrs · 45,667 cycles

EMERGENCY CABIN LIGHT AT ROW 6 ABC IS INOP. / [01] REMOVED AND REPLACED EMERGENCY CABIN LIGHT ASSY AT ROW 6ABC REFERENCING AMM 33-51-03 WITH NO HELP. NON-ROUTINE STILL OPEN.;[02] REPLACED BATTERY PACK AND CHARGER BASE M1674 AT LEFT OVER WING EXIT DOOR PER AMM 33-51-06

Part: NONE — CRACKED · airframe 76,536 hrs · 45,641 cycles

FUSELAGE CRACK INDICATIONS AT BS 782 AND BS 778 BELOW STR 1 USING 737 NDT PART 6; 53-30-18 AND 737 NDT PART 4; 53-30-07 FUSELAGE CRACK INDICATIONS AT BS 782 AND BS 778 BELOW STR 1 USING 737 NDT PART 6 53-30-18 AND 737 NDT PART 4 53-30-07.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 76,272 hrs · 45,452 cycles

GIRT BAR ON FWD SVC DOOR REQUIRES ADJUSTMENT / [01] ADJUSTED R1 DOOR GIRT BAR PER SIP

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 75,339 hrs · 44,847 cycles

L1 ENTRY GIRT BAR LOOSE / [01] TIGHTENED GIRT BAR RETAINERS PER SIP

Part: NONE — INOPERATIVE (CABIN) · airframe 73,729 hrs · 43,861 cycles

RH EMERGENCY HATCH LIGHT IS INOP ; / [01] R&RED R/H EMERGENCY HATCH LIGHT BALLAST ASSY PER MM 33-21-00. OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,637 hrs · 43,807 cycles

RIGHT EMERGENCY EXIT WINDOW LIGHT INOP ; / [01] RELAMPED RIGHT EMERGENCY EXIT WINDOW LIGHT PER AMM 33-21-00 OPS CHECK GOOD

Part: SUPPORT BRACKET — CRACKED (L/H HORIZ. STAB.) · airframe 73,521 hrs · 43,731 cycles

BROKEN SUPPORT BRACKET ON LEFT HORIZONTAL STABILIZER(WHERE SLIDDING PANEL RUNS) AT UPPER FUSELAGE. ; 2021-418287 / [13] REPLACED UPPER FORWARD TRACK SUPPORT BRACKET LOCATED ON LEFT HORIZONTAL STABILIZER(WHERE SLIDDING PANEL RUNS) AT UPPER FUSELAGE . I.A.W B737-700 SRM 51-10-02 ITEM 9 .; [14] CERTIFIED STEP 12 AND COMPLETED TASK CARD WITH STEP 13

Part: DOOR — CRACKED (L/H MLG W/W) · airframe 73,521 hrs · 43,731 cycles

CUSTOMER REQUEST CRACK ON LT MAIN LANDING GEAR CENTER DOOR ; 2021-418213 / [23] REPAIRED LT MAIN LANDING GEAR CENTER DOOR IAW EA 21-152-02872 WIP 1 REV B AND SUMMARY EA 21-152-02872; [24] REPAIRED LT MAIN LANDING GEAR CENTER DOOR IAW EA 21-152-02872 WIP 1 REV B AND SUMMARY EA 21-152-02872

Part: NONE — CRACKED (R2 DOOR) · airframe 73,521 hrs · 43,731 cycles

CUSTOMER REQUEST CRACK SERVICE DOOR ON SUPPORT ANGLE PANEL 844DZ (FWD) AT AFT GALLEY AREA (1 EA) ; 2021-418203 / [01] REPLACED SERVICE DOOR SUPPORT ANGLE PANEL 844DZ (FWD) AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; [02] JOB TASK CARD COMPLETED.

Part: NONE — CRACKED (R2 DOOR) · airframe 73,521 hrs · 43,731 cycles

CUSTOMER REQUEST CRACK SERVICE DOOR ON SUPPORT ANGLE PANEL 844DZ (AFT) AT AFT GALLEY AREA (1 EA) ; 2021-418204 / [01] REPLACED SERVICE DOOR SUPPORT ANGLE PANEL 844DZ (AFT) AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; [02] JOB TASK CARD COMPLETED.

Part: NONE — DETERIORATED (R2 DOOR) · airframe 73,521 hrs · 43,731 cycles

DETERIORATED GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA ; 2021-418115 / [01] REPLACED GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA I.A.W B737-700 AMM 25-66-02-400-801; [02] STEP 1 COMPLETE. <BR><BR>TASK CARD COMPLETE.

Part: NONE — CRACKED · airframe 73,521 hrs · 43,731 cycles

CRACK DORSAL FIN FWD RIB ON PANEL 321A AT LEVEL STA 867.0 AT VERTICAL STABILIZER. REMOVED DORSAL FIN FWD RIB ON PANEL 321A IAW 51-40-02 AND PERFORMED VISUAL INSPECTION ON AREA. A NEW RIB INSTALLED DORSAL FIN FWD RIB IAW SRM 51-40-02 AND DWG 174A1008.

Part: NONE — BROKEN (R1 DOOR) · airframe 73,521 hrs · 43,731 cycles

BROKEN SERVICE DOOR CUT OUT DEPRESSOR SEAL RETAINER AT FWD GALLEY AREA ; 2021-418137 / [01] REPLACED SERVICE DOOR CUT OUT DEPRESSOR SEAL RETAINER AT FWD GALLEY AREA IAW B737-700 AMM 52-09-16-400-803 STEP 5.D.(1).(B).; [02] REPLACED SERVICE DOOR CUT OUT DEPRESSOR SEAL RETAINER AT FWD GALLEY AREA IAW B737-700 AMM 52-09-16-400-803 STEP 5.D.(1).(B).

Part: NONE — DETERIORATED (R1 DOOR) · airframe 73,521 hrs · 43,731 cycles

SUPPLEMENTAL INFORMATION: DETERIORATED GIRT BAR FITTING HARDWARE AT FWD GALLEY AREA ; 2021-418114 / [01] REPLACED GIRT BAR FITTING HARDWARE AT FWD GALLEY AREA I.A.W B737-700 AMM25-66-02-400-801; [02] JOB COMPLETE

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 73,521 hrs · 43,731 cycles

CORRODED SUPPORT ZEE, BS 500A - 500D, WL 154.5, LBL 21.8. REMOVED THE SUPPORT ZEE IAW SRM 51-10-02. REPLACED THE SUPPORT ZEE IAW 51-40-02, 51-10-02, ITEM 9, AND DWG 143A7500 REV Y.

Part: ANGLE — CRACKED · airframe 73,521 hrs · 43,731 cycles

CRACK ON SUPPORT ANGLE LOC ON FRONT SPAR WEB UPPER AREA FUEL BOOST PUMP IFSS 120 RT WING ; 2021-418014 / [01] REMOVED SUPPORT ANGLE LOC ON FRONT SPAR WEB UPPER AREA FUEL BOOST PUMP IFSS 120 RT WING IAW B737-700 SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE FOR CRACK. SUPPORT ANGLE MUS BE REPLACED; [02] STEP 1 COMPLETE; [03] MACHINED NEW ( 1 E/A ) SUPPORT ANGLE; MATERIAL USED 7050T7451 P.O 148288 IAW DWG 116A3939 AND BOEING 737-700 SRM 57-20-10-0I-1 IDENTIFICATION 1; ITEM 4.A TABLE 2 (1) TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: B20189334 DUE DATE 23-NOV-21.; [04] STEP 3 COMPLETED; [05] PERFORMED PENETRANT INSPECTION ON MACHINED SUPPORT ANGLE IAW BAC 5423 AND BSS7039; CRACK INDICATIONS NOT FOUND.;

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 73,521 hrs · 43,731 cycles

CORRODED SUPPORT ZEE, BS 500A - 500D, WL 154.5, RBL 21.80. REMOVED THE SUPPORT ZEE IAW SRM 51-10-02. REPLACED THE SUPPORT ZEE IAW SRM 51-40-02, 51-10-02, ITEM 9, AND DWG 143A7500 REV Y.

Part: NONE — CORRODED (FWD CARGO BAY) · airframe 73,521 hrs · 43,731 cycles

CORRODED WEB, BS 492.4 - 500A, WL 154.5, RBL 21.80, REMOVED WEB IAW SRM 51-40-02. FABRICATED IAW SRM 51-40-05, & APPLIED PROTECTIVE TREATMENT IAW SRM 51-20-01. INSTALLED THE WEB IAW SRM 51-40-02, AND DWG 143A0080, 143A8126. REPLACED THE WEB IAW SRM 51-40-02, 51-10-02, ITEM 9, & DWG 143A0080, REV P & 143A8126 REV A.

Part: NONE — CORRODED (FWD CARGO BAY) · airframe 73,521 hrs · 43,731 cycles

CORRODED WEB, BS 420 - 440, WL 154.5, RBL 21.80. NO ALLOWABLE DAMAGE IN SRM. REMOVED THE WEB IAW SRM 51-40-02. DRILLED A NEW WEB IAW SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT IAW SRM 51-20-01. INSTALLED THE NEW WEB IAW SRM 51-40-02, AND DWG 143A0080 REV-. REPLACED THE WEB IAW SRM 51-40-02, 51-10-02, ITEM 9 AND DWG 143A0080 REV-.

Part: NONE — CRACKED (AFT CARGO BAY) · airframe 73,521 hrs · 43,731 cycles

CRACKED SUPPORT ANGLE, BS 827, S25 - 26R. REMOVED THE SUPPORT ANGLE IAW SRM 51-40-02. DRILLED A NEW SUPPORT ANGLE IAW SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT IAW SRM 51-20-01. INSTALLED THE NEW SUPPORT ANGLE IAW SRM 51-40-02 AND DWG 146A8120, REV A. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DRAWING 146A8120, REV A.

Part: ANGLE — CRACKED (EXTERNAL FUSELAG) · airframe 73,521 hrs · 43,731 cycles

CRACKED ANGLE BS 1016. EVALUATED AND FOUND NO ALLOWABLE DAMAGE LIMITS IN SRM. CUT OUT AND REMOVED FASTENERS IAW SRM 53-80-71-2R-6, REPAIR 6, & SRM 51-40-02. PERFORMED A PERMANENT REPAIR IAW SRM 53-80-71-2R-6, REPAIR 6, PARA 4.

Part: NONE — CORRODED (FUSELAGE) · airframe 73,521 hrs · 43,731 cycles

CUSTOMER REQUEST CORROSION ON PLATE LOWER SIDE OF TOILET SERVICE DOOR CUT OUT ; 2021-417970 / [17] REPLACED PLATE LOWER SIDE OF TOILET SERVICE DOOR CUT OUT IAW B737-700 SRM 51-10-02 ITEM 9 ;SRM 51-40-02 VERIFIED PART NUMBER AFFECTED IS 146A7401-7 IAW DWG 146A7401 REV:-

Part: TRACK — CRACKED (FUSELAGE) · airframe 73,521 hrs · 43,731 cycles

CRACK TRACK RBBL 13.84 LOCATED BS747 AFT CARGO COMPARTMENT ; 2021-418057 / [23] REPAIRED CARGO TRACK LOC BETWEEN BS 727C TO BS767 AND RBL 13.84 AT AFT CARGO COMPARTMENT.I.A.W B737-700 SRM 53 -00-53-2R-3 REPAIR 3 .; [24] REPAIRED CARGO TRACK LOC BETWEEN BS 727C TO BS767 AND RBL 13.84 AT AFT CARGO COMPARTMENT.I.A.W B737-700 SRM 53 -00-53-2R-3 REPAIR 3 .<BR>COMPLETED STEP 23<BR>RII

Part: FITTING — CORRODED (AFT FUSELAGE) · airframe 73,521 hrs · 43,731 cycles

CUSTOMER REQUEST CORROSION ON FWD FITTING AT TOILET SERVICE DOOR LOWER FUSELAGE ; 2021-417971 / [01] REPLACED FWD FITTING AT TOILET SERVICE DOOR LOWER FUSELAGE (HINGE ASSY) IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 PART NUMBER USED IS NEW HINGE ASSY 146A7414-7 PO: 2021 199410 1; [02] JOB COMPLETED.

Part: STUB FRAME — CRACKED (FWD SERVICE DOOR) · airframe 73,521 hrs · 43,731 cycles

CRACKED SERVICE DOOR STUB FRAME LOCATED AT BS 291.5 STR 8R AT FWD GALLEY AREA. REMOVED STUB FRAME IAW SRM 51-40-02. PERFORMED VISUAL INSPECTION NO ADDITIONAL DAMAGE FOUND. REMOVED STOP FITTING, DEPRESOR, FITTING ASSY. PERFORMED DRILL NEW STUB FRAME IAW SRM 51-40-05. REPLACED SERVICE DOOR STUB FRAME IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 141A8370 REV D.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 73,521 hrs · 43,731 cycles

MISSING MATERIAL FLOOR PANEL 231XF AT PASSENGER CABIN ; 2021-417852 / [18] REPAIRED FLOOR PANEL 231XF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [19] REPAIRED FLOOR PANEL 231XF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII INSPECTION

Part: NONE — MISSING (FUSELAGE) · airframe 73,521 hrs · 43,731 cycles

MISSING MATERIAL FLOOR PANEL 242AF AT PASSENGER CABIN ; 2021-417854 / [22] REPAIRED FLOOR PANEL 242AF AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [23] COMPLETED STEP 21. ITEM RII.; [24] FINAL ACTION COMPLETED. RII COMPLETED.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 73,521 hrs · 43,731 cycles

CRACK FLOOR PANEL 242AF AT PASSENGER CABIN ; 2021-417853 / [22] REPAIRED FLOOR PANEL 242AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [23] COMPLETED STEP 21. ITEM RII.; [24] FINAL ACTION COMPLETED. RII COMPLETED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,521 hrs · 43,731 cycles

SUPPLEMENTAL INFORMATION: CRACK FRAME LOCATED BS787 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN ; 2021-417874 / [01] EVALUATED CRACK IS NOT PERMITTED ON FRAME LOC BS 787 BTW STR 8RH TO STR 9RH IAW B737-700 SRM 53-00-07-1A-1 FIGURE 102. FRAME MUST BE REPAIRED.; [02] CERTIFIED STEP 1; [03] TOOK MEASURE OF CRACK ON FRAME LOC BS 787 BTW STR 8RH TO STR 9RH LENGTH IS: 0.425 . TOOL USED: CALIPER P/N 500-752-20; S/N ; B16101265 ; DUE DATE 20-APR-22.; [04] STEP 3 COMPLETE; [05] MARKED HAND LAYOUT ON REPAIR AREA OF FRAME LOC AT BS 787 BTW STR 8RH TO STR 9RH AT PASSENGER CABIN I.A.W EA 1-A53-12114 FIGURE 1 SHEET 2. TOOL USED: CALIPER P/N 500-752-20; S/N ; B16101265 ; DUE DATE 20-APR-22.; [06] STEP 5 COMPLETE; [07] VERIFIED ANGLES A (PN:53100010-006) AND B (PN:53100010-03) IAW OF DWG#53100010 REV 2 MEET REQUIREMENTS OF EA#1-A53-12114 STEP 13 TO 18; MPM 17.10.01 OPP; [08] STEP 7 COMPLETE; [09] OK TO INSTALL RETAINED SUPPORT BRACKET AND FASTENERS LOC ON REPAIR AREA FRAME BS 787 BTW STR 8R TO STR 9R; [10] OK TO INSTALL GRANTED.. RII ITEM<BR>STEP 9 COMPLETE.. RII ITEM; [11] PERFORMED REPAIR FRAME IAW EA# 1-A53-12114 REV 7.; [12] TASK COMPLETED <BR><BR>PERFORMED REPAIR FRAME IAW EA# 1-A53-12114 REV 7.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 73,521 hrs · 43,731 cycles

MISSING MATERIAL FLOOR PANEL 241FF AT PASSENGER CABIN. EVALUATED FLOOR PANEL 241FF AND FOUND WITHIN LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1, PARAGRAPH 1 A. REMOVED DAMAGED SKIN AND INSERTS IAW SRM 53-00-50-2R-1, REPAIR 1, PARAGRAPH 3 B - D. INSTALLED REPAIR PLIES IAW SRM 53-00-50-2R-1, REPAIR 1, PARAGRAPH 3 K 1 & L 1.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 73,521 hrs · 43,731 cycles

DAMAGED FLOOR PANEL 232SF. EVALUATED & FOUND IN LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1, PARA 1 A. REMOVED DAMAGED SKIN & INSERTS IAW SRM 53-00-50-2R-1, REPAIR 1, PARA 3 B - D. FILLED AREA WITH POTTING COMPOUND IAW SRM 53-00-50-2R-1, REPAIR 1, PARA 3 G. INSTALLED REPAIR IAW SRM 53-00-50-2R-1, REPAIR 1, PARA 3 K & L. CURED REPAIR & DRILLED IAW SRM 53-00-50-2R-1, REPAIR 1, PARA 3 M, N & SRM 53-00-50-2R-0, REPAIR GENERAL, PARA 5 R & S. INSTALLED & CURED INSERTS IAW SRM 53-00-50-2R-1, REPAIR 1, PARA 3 N & SRM 53-00-50-2R-0, REPAIR GENERAL, PARA 5 S. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-1, REPAIR 1.

Part: NONE — CRACKED (CABIN) · airframe 73,521 hrs · 43,731 cycles

CRACK FLOOR PANEL 242BF AT PASSENGER CABIN . EVALUATED FLOOR PANEL 242BF AND FOUND WITHIN LIMITS TO REPAIR IAW SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 1.A. INSTALLED REPAIR PLIES ON FLOOR PANEL 242BF IAW SRM 53-00-50-2R-1, REPAIR 1, PARAGRAPH 3.K. 1 AND L. 1.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 73,521 hrs · 43,731 cycles

DAMAGED FLOOR PANEL 241AF IN CABIN. EVALUATED & FOUND IN LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1, PARA 1A. REMOVED DAMAGED SKIN & INSERT IAW SRM 53-00-50-2R-1, REPAIR 1, PARA 3 B - D. DRIED & CLEANED AREA IAW SRM 53-00-50-2R-1, REPAIR 1, PARA 3 E & F. FILLED REPAIR AREA WITH POTTING COMPOUND IAW SRM 53-00-50-2R-1, REPAIR 1, PARA 3 G. INSTALLED REPAIR PLIES IAW SRM 53-00-50-2R-1, REPAIR 1, PARA 3 K & L. CURED PLIES & DRILLED IAW SRM 53-00-50-2R-1, REPAIR 1, PARA 3 M, N, & SRM 53-00-50-2R-0, REPAIR GENERAL, PARA 5 R & S. INSTALLED & CURED INSERTS IAW SRM 53-00-50-2R-1, REPAIR 1, PARA 3 N & SRM 53-00-50-2R-0, REPAIR GENERAL, PARA 5. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R-1, REPAIR 1.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 73,521 hrs · 43,731 cycles

DAMAGED FLOOR PANEL 241DF IN CABIN. EVALUATED & FOUND WITHIN LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1, PARAGRAPH 1 A. REMOVED DAMAGED SKIN AND INSERTS IAW SRM 53-00-50-2R-1, REPAIR 1, PARAGRAPH 3 B - D. DRIED AND CLEANED REPAIR IAW SRM 53-00-50-2R-1, REPAIR 1, PARAGRAPH 3 E & F. FILLED REPAIR AREAS WITH POTTING COMPOUND IAW SRM 53-00-50-2R-1, REPAIR 1, PARAGRAPH 3G. CURED REPAIR PLIES AND DRILLED FASTENER HOLES ON REPAIR AREAS AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3.M (1); N. AND B737-700 SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 5 R AND 5 S. INSTALLED AND CURED INSERTS ON REPAIR AREAS IAW SRM 53-00-50-2R-1, REPAIR 1, PARAGRAPH 31. REPAIRED FLOOR PANEL 241DF IAW SRM 53-00-50-2R-1 REPAIR 1.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 73,521 hrs · 43,731 cycles

MISSING MATERIAL FLOOR PANEL 231ZF AT PASSENGER CABIN ; 2021-417839 / [17] REPAIRED FLOOR PANEL 231ZF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [18] REPAIRED FLOOR PANEL 231ZF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII INSPECTION

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 73,521 hrs · 43,731 cycles

CRACK FLOOR PANEL 241FF AT PASSENGER CABIN. EVALUATED FLOOR PANEL 241FF AND FOUND WITHIN LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1, PARAGRAPH 1.A. NSTALLED REPAIR PLIES ON REPAIR AREA IAW SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3.K 1, L 1.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 73,521 hrs · 43,731 cycles

CRACK FLOOR PANEL 231ZF AT PASSENGER CABIN ; 2021-417837 / [18] REPAIRED FLOOR PANEL 231ZF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII INSPECTION

Part: FLOOR PANEL — PULLED (CABIN) · airframe 73,521 hrs · 43,731 cycles

DAMAGED FLOOR PANEL 232RF IN CABIN, EVALUATED AND FOUND WITHIN LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1, PARAGRAPH 1.A. REMOVED DAMAGED SKIN AND INSERTS IAW SRM 53-00-50-2R-1, REPAIR 1, PARAGRAPH 3. B - D. DRIED AND CLEANED REPAIR AREA IAW SRM 53-00-50-2R-1, REPAIR 1, PARAGRAPH 3. E & F. INSTALLED REPAIR IAW SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3.K. & L.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 73,521 hrs · 43,731 cycles

CRACK INDICATION FOUND AROUND FASTENER LOCATED BEAR STRAP AT LEVEL FITTING-LATCH; STA 294.5 BETWEEN S-8R AND S-9R. LENGTH CRACK IS 0.188 INCH. ; 2021-417776 / REPAIRED BEAR STRAP AT LEVEL FITTING-LATCH, STA 294.5 BETWEEN S-8R AND S-9R IAW EA 21-153-02753 RII

Part: NONE — CRACKED (RH WING) · airframe 73,521 hrs · 43,731 cycles

CRACK FLAP TRACK FAIRING 642AB RETAINER SEAL AT RT WING ; 2021-417759 / [01] REPLACED FLAP TRACK FAIRING 642AB RETAINER SEAL AT RT WING. IAW B737-700 SRM 51-40-02.; [02] REPLACED FLAP TRACK FAIRING 642AB RETAINER SEAL AT RT WING. IAW B737-700 SRM 51-40-02.

Part: NONE — CRACKED (R1 DOOR) · airframe 73,521 hrs · 43,731 cycles

CRACK INDICATION FOUND ON BEAM # 4 FWD SERVICE DOOR ; 2021-417766 / [14] REPLACED BEAM #4 OF FWD SERVICE DOOR IAW B737-700 SRM 51-10-02 ITEM 9. SEE TASK 5241-C-14093-NG (R1 FORWARD SERVICE DOOR - CRACKED BEAM REPLACEMENT AND REIDENTIFICATION) [TTG8Q002VFZ7]<BR>COMPLETED STEP 13<BR>RII

Part: THRESHOLD — CRACKED (CARGO DOORWAY) · airframe 73,521 hrs · 43,731 cycles

CRACK AFT CARGO DOOR AREA ON THRESHOLD AT AFT CARGO COMPARTMENT ; 2021-417734 / [01] EVALUATED MIDDLE SCUFF PLATE CARGO DOOR AREA ON THRESHOLD LOCATED AT AFT CARGO COMPARTMENT FOUND CRACK ( 1 EA ) MEASURE AS FOLLOW:L=0.2140 INCH. CRACK MUST BE REPAIRED BY WELDING IN ACCORDANCE WITH BOEING 737-700 SRM 53-60-15-2R-1; REPAIR 1 PARAGRAPH 4.C. TOOL USED; DIGITAL CALIPER P/N:500-197-30 S/N:B20189531 DUE DATE 22/NOV/21; [02] STEP 1 COMPLETED; [03] WELDED THE MIDDLE SCUFF PLATE CARGO DOOR AREA ON THRESHOLD OF AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1; REPAIR 1 PARAGRAPH 4.C. STEP ( 4 ) AND BAC 5975. WELD ROD USED:P/N:AMS4951 P.O.2021-149033; [04] STEP 3 COMPLETED; [05] PENETRANT INSPECTION DONE ON WELDED CARGO DOOR AREA ON THRESHOLD AFT C.C. IAW SPM 20-20-02. CRACK INDICATION NOT FOUND; [06] APPLIED PRIMER ON MIDDLE SCUFF PLATE CARGO DOOR AREA ON THRESHOLD OF AFT CARGO COMPARTMENT IAW B737-700 SRM 53-60-15-2R-1 REPAIR 1; 4.C. (5) TO (7). AND SOPM 20-41-02.; [07] COMPLETED STEP 6.; [08] REPAIRED THRESHOLD PLATE OF AFT CARGO COMPARTMENT DOOR AREA BY WELD PROCESS IAW B737-700 SRM 53-60-15-2R-1.; [09] REPAIRED THRESHOLD PLATE OF AFT CARGO COMPARTMENT DOOR AREA BY WELD PROCESS IAW B737-700 SRM 53-60-15-2R-1. SIGNED MEASUREMENTS; [10] CORRECT STEPS 8.AND 9. REPAIRED THRESHOLD PLATE OF AFT CARGO COMPARTMENT DOOR AREA BY WELD PROCESS IAW B737-700 SRM 53-60-15-2R-1; [11] REPAIRED THRESHOLD PLATE OF AFT CARGO COMPARTMENT DOOR AREA BY WELD PROCESS IAW B737-700 SRM 53-60-15-2R-1

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 73,521 hrs · 43,731 cycles

CRACKED SCUFF PLATE AFT CORNER IN THE AFT CARGO WELDED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4.B. STEP 4, AND BAC 5975.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 73,521 hrs · 43,731 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT WELDED THE FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1 PARAGRAPH 4.B. STEP ( 4 ) AND BAC 5975.

Part: SUPPORT — CRACKED · airframe 73,521 hrs · 43,731 cycles

CRACK SUPPORT BRACKET TRAILING EDGE ORSS 269 APPROX AT RT WING. REMOVED SUPPORT BRACKET IAW SRM 51-40-02. PERFORMED VISUAL INSPECTION ON AREA AND FOUND NO ADDITIONAL DAMAGE. DRILLED A NEW SUPPORT BRACKET IAW SRM 51-40-05. APPLIED PROTECTIVE TREATMENT ON HOLE SUPPORT BRACKET IAW SRM 51-20-01. INSTALLED SUPPORT BRACKET IAW SRM 51-40-02 AND DWG 115A2982.

Part: ACCESS PANEL — DELAMINATED (RH WING) · airframe 73,521 hrs · 43,731 cycles

DELAMINATED ACCESS PANEL 621FB, RT WING EVALUATED AND FOUND WITHIN LIMITS IAW SRM 57-41-01-2R-1, REPAIR 1, TABLE 202, PARA 4.D. REMOVED DAMAGE, PREPARED AND DRIED REPAIR AREA AND REMOVED STRIP IAW SRM 51-70-04-2R-6 PAR.4 A TO D AND SRM 57-41-01-2R-6 REPAIR 6 PAR.4.B. REPAIRED ACCESS PANEL 621FB IAW SRM 51-70-04-2R-6, REPAIR 6.

Part: PANEL — CRACKED (LH WING) · airframe 73,521 hrs · 43,731 cycles

CRACK ACCESS PANEL 561BB AROUND HOLE AT LT WING ; 2021-417652 / [01] EVALUATED ACCESS PANEL 561BB AT LT WING AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 SRM 57-41-01-2R-1 REPAIR 1 PARA 2.B ITEM (2) AND SRM 51-70-04-2R-9 REPAIR 9 DAMAGE FASTENER HOLE 1) L=0.41 IN W=0.22 IN; 2) L=0.48 IN W=0.24 IN; 3) L=0.5 IN W=0.22 IN; 4) L=0.47 IN W=0.22 IN; 5) L=0.5 IN W=0.23 IN; 6) L=0.49 IN W=0.22 IN; 7) L=0.49 IN W=0.3 IN; 8) L=0.46 IN W=0.34 IN; 9) L=0.5 IN W=0.33 IN TOOL USED CALIPER P/N: 500-197-30 S/N: 15121550 DUE DATE 03-AUG-22; [02] STEP 1 COMPLETED; [03] REMOVED DAMAGE AND PREPARED THE REPAIR AREA AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9 PARA.4.A TO C AND B737-700 SRM 51-70-04-2R-0 REPAIR GENERAL PARA.4.D;E; [04] STEP 3 COMPLETED.; [05] STARTED DRY PROCESS ON THE REPAIR AREA AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9 PARA.4.B AND B737-700 SRM 51-70-04-2R-0 REPAIR GENERAL PARA.4.D.] REPAIRED ACCESS PANEL 561BB IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.; [28] TASK CARD COMPLETED

Part: ANGLE — CRACKED · airframe 73,521 hrs · 43,731 cycles

CRACK ANGLE BS 540 BTWN BL 0 TO RBL 24. REMOVED ANGLE IAW SRM 51-40-02-0G-0. REPLACED ANGLE IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02.

Part: BRACKET — CRACKED (LH WING) · airframe 73,521 hrs · 43,731 cycles

CRACKED SUPPORT BRACKET LOCATED TRAILING EDGE ORSS 269 APPROX AT LT WING. REMOVED SUPPORT BRACKET IAW SRM-51-40-02 AND PERFORMED VISUAL INSPECTION ON AREA AND NO ADDITIONAL DAMAGE FOUND. INSTALLED A NEW SUPPORT BRACKET IAW SRM 51-40-02-0, AND DWG 115A2930.

Part: PANEL — CRACKED (LH WING) · airframe 73,521 hrs · 43,731 cycles

CRACK ACCESS PANEL 561AB AROUND HOLES AT LT WING ; 2021-417651 / [01] EVALUATED ACCESS PANEL 561AB AT RT WING AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 SRM 57-41-01-2R-1 REPAIR 1 PARA 2.B ITEM (2) AND SRM 51-70-04-2R-9 REPAIR 9 DAMAGE FASTENER HOLE 1) L=0.36 IN W=0.26 IN; 2) L=0.42 IN W=0.4 IN; 3) L=0.44 IN W=0.32 IN; 4) L=0.45 IN W=0.39 IN; 5) L=0.46 IN W=0.35 IN; 6) L=0.39 IN W=0.34 IN; 7) L=0.47 IN W=0.43 IN; 8) L=0.41 IN W=0.32 IN; 9) L=0.42 IN W=0.28 IN TOOL USED CALIPER P/N: 500-197-30 S/N: 15121550 DUE DATE 03-AUG-22; [02] STEP 1 COMPLETED; [03] REMOVED DAMAGE AND PREPARED THE REPAIR AREA AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9 PARA.4.A TO C AND B737-700 SRM 51-70-04-2R-0 REPAIR GENERAL PARA.4.D;E; [04] STEP 3 COMPLETED; [05] STARTED DRY PROCESS ON THE REPAIR AREA AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9 PARA.4.B AND B737-700 SRM 51-70-04-2R-0 REPAIR GENERAL PARA.4.D. REPAIRED ACCESS PANEL 561AB IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9. COMPLETED

Part: PANEL — CRACKED (RH WING) · airframe 73,521 hrs · 43,731 cycles

CRACKED ACCESS PANEL 661BB RT WING. FOUND WITHIN LIMITS IAW SRM 57-41-01-2R-1, REPAIR 1, PARA 2.B ITEM 2 AND SRM 51-70-04-2R-9 REPAIR 9. REMOVED DAMAGE AND PREPARED IAW SRM 51-70-04-2R-9, REPAIR 9, PARA 4.A - C AND SRM 51-70-04-2R-9 REPAIR 9.

Part: ACCESS PANEL — ELONGATED (WTB FAIRING) · airframe 73,521 hrs · 43,731 cycles

ELONGATED HOLE ON ACCESS PANEL 193D FOR WING TO BODY FAIRING. EVALUATED AND FOUND WITHIN LIMITS IAW SRM 53-40-70-2R-1, REPAIR 1, PARAGRAPH 2.B(1)(B). INSTALLED FILLER PLIES ON REPAIR AREA IAW SRM 51-70-05-2R-8 PAR 4D TO F. DRILLED AND COUNTERSUNK FASTENER HOLES AND PERFORMED POST REPAIR INSPECTION AND FOUND SATISFACTORY IAW SRM 51-70-05-2R-8, REPAIR 8, PAR 4.H.I. AND SRM 51-70-05-2R-0, REPAIR GENERAL, PAR 4.N. REPAIRED ACCESS PANEL 193D WING TO BODY FAIRING LOWER FUSELAGE IAW SRM 51-70-05-2R-8, REPAIR 8.

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 73,521 hrs · 43,731 cycles

CRACKED ANGLE LOCATED BS 693 AND RBL 24. REMOVED ANGLE IAW SRM 51-40-02. FORMED ANGLE IAW SRM 51-30-01, AND DWG 273A9112. HEAT TREATED TO 7075T73 IAW BAC5602, TABLE IV, AND TABLE XI. DRILLED THE NEW ANGLE IAW SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT IAW SRM 51-20-01. INSTALLED THE NEW ANGLE IAW SRM 51-40-02 AND DWG 273A9110, REV-.

Part: PANEL — CRACKED (LH WING) · airframe 73,521 hrs · 43,731 cycles

CRACK ACCESS PANEL 571 DB AT LT WING ; 2021-417650 / [PERFORMED VISUAL INSPECTION ON REPORTED AREA AND NO CRACK FOUND ONLY HOLE THROUGH THE PANEL. EVALUATED ACCESS PANEL 571DB AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 SRM 57-51-01-2R-1 REPAIR 1. TABLE 201. DAMAGE SIZE ARE: L= 0.25 W= 0.20 TOOL USED: CALIPER P/N 500-197-30 S/N 15121550 DUE DATE: 03-AUG-22.; [02] STEP 1 VERIFIED AND COMPLETED.; [03] REMOVED DAMAGE; DRIED AND PREPARED AREA ON ACCESS PANEL 571DB AS PER B737-700 SRM 51-70-04-2R-4 REPAIR 4 PARAGRAPH 4.B AND C. AND B737-700 SRM 51-70-04-2R-0 REPAIR GENERAL PARAGRAPH 4. C AND E; REPAIRED ACCESS PANEL 571DB AT LT WING IAW B737-700 SRM 51-70-04-2R-4 REPAIR 4;

Part: PANEL — CRACKED (LH WING) · airframe 73,521 hrs · 43,731 cycles

CRACK ACCESS PANEL 561CB AROUND HOLES AT LT WING ; 2021-417654 / [01] EVALUATED ACCESS PANEL 561CB AT LT WING AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 SRM 57-41-01-2R-1 REPAIR 1 PARA 2.B ITEM (2) AND SRM 51-70-04-2R-9 REPAIR 9 DAMAGE FASTENER HOLE 1) L=0.36 IN W=0.25 IN; 2) L=0.44 IN W=0.28 IN; 3) L=0.34 IN W=0.26 IN; 4) L=0.48 IN W=0.34 IN; 5) L=0.42 IN W=0.3 IN; 6) L=0.45 IN W=0.29 IN; 7) L=0.44 IN W=0.33 IN; 8) L=0.42 IN W=0.34 IN; 9) L=0.43 IN W=0.37 IN TOOL USED CALIPER P/N: 500-197-30 S/N: 15121550 DUE DATE 03-AUG-22; [02] STEP 1 COMPLETED; [03] REMOVED DAMAGE AND PREPARED THE REPAIR AREA AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9 PARA.4.A TO C AND B737-700 SRM 51-70-04-2R-0 REPAIR GENERAL PARA.4

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 73,521 hrs · 43,731 cycles

CRACKED ANGLE, BS 693, LBL 24. REMOVED ANGLE IAW SRM 51-40-02. FORMED A NEW ANGLE IAW SRM 51-30-01 & DWG 273A9112, REPAIR ANGLE HEAT TREATED TO 7075-T73 IAW BAC5602 TABLE IV AND TABLE XI. DRILLED THE NEW ANGLE IAW SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT IAW SRM 51-20-01. INSTALLED THE NEW ANGLE IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 273A9112, REV- AND DWG 273A9110, REV.

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 73,521 hrs · 43,731 cycles

CRACK ANGLE, BS 540 BTWN BL 0 TO LBL 24. REMOVED ANGLE IAW SRM 51-40-02-0G-0. REPLACED ANGLE IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02.

Part: PANEL — CRACKED (RH WING) · airframe 73,521 hrs · 43,731 cycles

SUPPLEMENTAL INFORMATION: CRACK ACCESS PANEL 661CB TRAILING EDGE AROUND HOLES RT WING ; 2021-417656 / EVALUATED ACCESS PANEL 661CB TRAILING EDGE AT RT WING AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 SRM 57-41-01-2R-1 REPAIR 1 PARA 2.B ITEM (2) AND SRM 51-70-04-2R-9 REPAIR 9 DAMAGE FASTENER HOLE 1) L=0.43 IN W=0.28 IN; 2) L=0.46 IN W=0.31 IN; 3) L=0.48 IN W=0.34 IN; 4) L=0.49 IN W=0.33 IN; 5) L=0.47 IN W=0.39 IN; 6) L=0.48 IN W=0.4 IN; 7) L=0.42 IN W=0.35 IN; 8) L=0.49 IN W=0.38 IN; 9) L=0.47 IN W=0.35 IN TOOL USED CALIPER P/N: 500-197-30 S/N: 15121550 DUE DATE 03-AUG-22 REMOVED DAMAGE AND PREPARED THE REPAIR AREA AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9 PARA.4.A TO C AND B737-700 SRM 51-70-04-2R-0 REPAIR GENERAL PARA.4.D;E;] INSTALLED THE REPAIR PLIES ON REPAIR AREA OF ACCES PANEL 661CB AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9 PARA. 4(J) TO (L) AND SRM 51-70-04-2R-0 REPAIR GENERAL PARA. 4(L) AND (M). MATERIAL USED: ADHESIVE P/N: EA9390AB; P/O: 2021-180215/001. TOOL USED: SCALE P/N: SCA-301; S/N: AE-412120; DUE DATE: 24-FEB-22 COMPLETED; [18] CURED; DRILLED; COUNTERSUNK FASTENER HOLES AND PERFORMED POST REPAIR INSPECTION AND FOUND SATISFACTORY AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9 PARAGRAPH 4.M TO O. TOOL USED: HOT BONDER P/N HCS9200B S/N 18175478 DUE DATE: 05-AUG-22; .REPAIRED ACCESS PANEL 661CB AT RT WING IAW B737-7,NG,NRC,2021-10-04 21:10:27,22Y,N,MX,0,0,,CRACK ACCESS PANEL 661CB TRAILING EDGE AROUND HOLES RT WING ; 2021-417656"

Part: NONE — BROKEN (FUSELAGE) · airframe 73,521 hrs · 43,731 cycles

BROKEN EXTERNAL GROUND ELECTRICAL POWER SKIN CUT OUT AT LOWER FUSELAGE ; 2021-417559 / [16] OK TO INSTALL REPAIR PARTS DOUBLER; FILLER; RUBBING BLOCK; LAMINATED SHIM; FASTENERS AND WASHER ON EXTERNAL GROUND ELECTRICAL POWER SKIN CUT OUT AT LOWER FUSELAGE; [17] STEP 16 COMPLETED RII ITEM; [18] INSTALLED REPAIR PARTS DOUBLER; FILLER; RUBBING BLOCK; LAMINATED SHIM; FASTENERS AND WASHER ON EXTERNAL GROUND ELECTRICAL POWER SKIN CUT OUT AT LOWER FUSELAGE IAW B737-700 SRM 53-10-15-2R-4 REPAIR 4 PARAGRAPH 4 AND SRM 51-40-02; [19] PERFORMED PERMANENT REPAIR ON EXTERNAL GROUND ELECTRICAL POWER SKIN CUT OUT AT LOWER FUSELAGE IAW B737-700 SRM 53-10-15-2R-4 REPAIR 4; [20] CERTIFIED STEP 18 & 19 RII

Part: NONE — CRACKED · airframe 73,521 hrs · 43,731 cycles

CRACKED LOWER SURFACE SLAT 4 NOSE SKIN, LT WING. NO FOUND ALLOWABLE DAMAGE ON SRM. REMOVED NR 4 SLAT SKIN, ACCESS PANEL 522DB, AND FASTENERS IAW SRM 51-40-02. ROTOTEST INSPECTION ACCOMPLISHED IAW NDT MANUAL PART 6 51-00-00, PROCEDURE 16. CRACK INDICATIONS WERE FOUND (3 E/A) CRACK 1 ON HOLE AT NOSE SKIN LAYER ONLY, CRACK 2 ON HOLE AT RIB LAYER ONLY CRACK 3 ON HOLE NOSE SKIN LAYER ONLY. REPLACED SLAT 4 DUE TO NO FOUND ALLOWABLE DAMAGE IN SRM.

Part: WEB — CORRODED · airframe 73,521 hrs · 43,731 cycles

CORROSION FUEL BOOST PUMP, RT WING REMOVED BRACKET AND BONDING JUMPER IAW SRM 51-40-02, DAMAGE FOUND OUT LIMITS IAW SRM 57-20-10-1A-3 ALLOWABLE DAMAGE 3 TABLE 101; ZONE 1 AND PARAGRAPH 4.D. APPLIED PROTECTIVE TREATMENT ON REWORKED AREA FUEL BOOST PUMP IAWSRM 51-20-01.

Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 73,521 hrs · 43,731 cycles

CUSTOMER REQUEST CRACK ON VAPOR BARRIER BS 663 LOCATED AT LBL 50 MAIN WHEEL WELL COMPARTMENT ; 2021-417560 / [24] REPAIRED VAPOR BARRIER BS 663 LOCATED AT LBL 50 MAIN WHEEL WELL COMPARTMENT AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10; [25] STEP 16 RII; [26] JOB TASK CARD COMPLETED

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 72,661 hrs · 43,234 cycles

RIGHT WING EMERGENCY EXIT LIGHT LENS BROKE ; / REPLACED RIGHT WING EMERGENCY EXIT LENS PER AMM 33-51-01

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 72,499 hrs · 43,133 cycles

REAR SERVICE DOOR ON A/C RIGHT SLIDE PACK IS FALLING OUT. ; / SECURED EXCESS SLIDE MATERIAL TO CASE VELCRO. CASE REMAINED SECURED AND CLOSED. NO DEFECTS PER AMM 20-00-00

Part: SKIN — ERODED (HF ANTENNA) · airframe 72,372 hrs · 43,055 cycles

EROSION DAMAGE ON HF ANTENNA ; ACCOMPLISHED EA 1-A55-3992 REV 3 AND EA 1-A55-3775REV 2. REPETITIVE ACTIN REMOVE PPT TAPE AND PERFORMDVI PER SRM 51-10. TO INSPECT FOR ADDITIONAL DAMAGE.ALSO ACCOMPLISH TAP TEST IAW SRM 51-10-06. IFDEFECTS ARE FOUND CONTACT SERVICE ENGINEERING; IFNO DEFECTS ARE FOUND REAPPLY PPT TAPE IAWEA 1-A55-3775. PERMANENT REPAIR DUE 30 DAYS; PERFORMINTERIM REPAIR OF HF ANTENNA PANEL IAW 1-A55-3777OR R&R VERTICAL STABL LEADING EDGE.REMOVABLE COMPONENT: PN 176A1001-6 SN WN0020PERMANENT ACTION REQUIRED / COMPLIED WITH EA 1-A55-3777

Part: SKIN — ERODED (HF ANTENNA) · airframe 72,372 hrs · 43,055 cycles

EROSION DAMAGE ON HF ANTENNA ; ACCOMPLISHED EA 1-A55-3992 REV 3 AND EA 1-A55-3775REV 2. REPETITIVE ACTIN REMOVE PPT TAPE AND PERFORMDVI PER SRM 51-10. TO INSPECT FOR ADDITIONAL DAMAGE.ALSO ACCOMPLISH TAP TEST IAW SRM 51-10-06. IFDEFECTS ARE FOUND CONTACT SERVICE ENGINEERING; IFNO DEFECTS ARE FOUND REAPPLY PPT TAPE IAWEA 1-A55-3775. PERMANENT REPAIR DUE 30 DAYS; PERFORMINTERIM REPAIR OF HF ANTENNA PANEL IAW 1-A55-3777OR R&R VERTICAL STABL LEADING EDGE.REMOVABLE COMPONENT: PN 176A1001-6 SN WN0020PERMANENT ACTION REQUIRED / COMPLIED WITH EA 21-155-01195

Part: YOKE — SMOKE (FLIGHT DECK) · airframe 72,055 hrs · 42,870 cycles

SMOKING FROM NUMBER WHEEL ON CA YOKE. SMOKE/GLOWING WENT AWAY WHEN LIGHTS WERE TURNED DOWN. / PERFORMED CONDITION INSPECTION PER MM 05-51-56. VERIFIED CAPT'S YOKE MEMORY DEVICE (TRIP COUNTER). R&R CAPTS MEMORY DEVICE PER MM 33-11-00. CKS OK

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 71,389 hrs · 42,487 cycles

PASSENGER CABIN RT OVERWING EMERGENCY EXIT DOOR. EMERGENCY EXIT LIGHT WIRES ON FWD SIDE LOOSE. SECURED EMERGENCY EXIT LIGHT WIRES ON FWD SIDE OF RT OVERWING EMERGENCY EXIT DOOR, PER SIP.

Part: STOP FITTING — BROKEN (L1 DOOR) · airframe 70,169 hrs · 41,709 cycles

FWD ENTRY DOOR PRESSURE STOP FITTING BROKE / (REF LP 0263529) REPLACED BROKEN AFT MID-PRESSURE DOOR STOP TO L1 PASSENGER DOOR PER SRM 51-40-02; SRM 51-40-05 REF DWG 141A6260 CLOSING # 35399

Part: BRACKET — BROKEN (FWD FLASHLIGHT) · airframe 69,787 hrs · 41,468 cycles

EMERGENCY FLASHLIGHT BRACKET IN FORWARD ENTRY BULKHEAD BROKEN. / R&R BRACKET PER SIP.

Part: FAIRING — DELAMINATED (RT NACELLE) · airframe 69,540 hrs · 41,308 cycles

STRUT THRUST REVERSER FAIRING PANEL R/H (431ER) HAS DELAM ON FWD EDGE. DELAM IS L= 2 1/4'; W = 3/4'; DAMAGE IS INTO 2 PLYS. / CLOSING DMA #0263513 R&R #1 ENG T/R STRUT FAIRING PANEL 431ER PER M/M 54-53-02 CLEARING #22759

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,656 hrs · 40,762 cycles

R/H EMERGENCY LIGHT INOP AT OVERHEAD BIN ROW 11. / RELAMPED LIGHT PER AMM.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 68,656 hrs · 40,762 cycles

EMERGENCY LIGHTS INOP AT G1 GALLEY. SECURED CONNECTOR PER AMM.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,656 hrs · 40,762 cycles

L/H EMERGENCY OVERHEAD BIN LIGHTS INOP AT ROW 4. SECURED CONNECTOR PER AMM.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 68,656 hrs · 40,762 cycles

FWD CARGO DOOR CUTOUT AFT SCUFF PLATE CRACKED / REPAIRED FWD CARGO DOOR CUT OUT AFT SCUFF PLATE CORNER BY OUTSIDE (JL WELDING INC. W.O 15762) IRW SOUTHWEST EA # 1-A53-2076 REV. 11

Part: SCUFF PLATE — CRACKED (R1 DOOR) · airframe 68,656 hrs · 40,762 cycles

R1 DOOR MID SCUFF PLATE HAS CRACK / R-1 DOOR MID SCUFF PLATE REPAIRED AS PER EAF 1-A53-2076 REV 11 / W124004

Part: LENS — CRACKED (CABIN) · airframe 68,656 hrs · 40,762 cycles

L/H EMERGENCY LIGHT LENS CRACKED AT POSITION 4. / R&R LENS IAW AMM.

Part: STRINGER — OUT OF TOLERANCE (AFT FUSELAGE) · airframe 68,656 hrs · 40,762 cycles

BS 1016 APB AT 5R AT STR-2R HOLE OUT OF TOLERANCE MEASURES 0.381' / REPAIRED FASTENER HOLE AT BS 1016 STRINGER 2R; HOLE 5R AS PER SOUTH WEST SPECIAL ITEM (SI # 12107-53) STEP 13 REF. FIG 5

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 68,656 hrs · 40,762 cycles

LT HORIZONTAL STABILIZER IN SPAR RIB ASSEMBLY 4, STA 120.30, CRACKED AT STIFFENER #3. INSPAR STIFFENER CRACK REPAIR IAW SRM.

Part: STRINGER — OUT OF TOLERANCE (AFT FUSELAGE) · airframe 68,656 hrs · 40,762 cycles

WHILE ACCOMPLISHING SI#12107-53 FOUND HOLE 9R AT STR-3R OUT OF THE 0.3745-0.3755' TOLERANCE REQUIRED PER STEP 36D (EXISTING HOLE SIZE 0.3780 / REPAIRED FASTENER HOLE AT BS 1016 STRINGER 3R HOLE 9R AS PER SOUTHWEST SPECIAL ITEM (SI # 12107-53) STEP 38 FIG 15

Part: STRINGER — OUT OF TOLERANCE (AFT FUSELAGE) · airframe 68,656 hrs · 40,762 cycles

WHILE ACCOMPLISHING SI#12107-53 FOUND HOLE 9L AT STR-3L OUT OF THE 0.3745-0.3755 TOLERANCE REQURED FOR STEP 29.D. EXISTING WHOLE DIAMETER 0.380. / REPAIRED FASTNER HOLE AT BS 1016; STRINGER 3L; HOLE 9L AS PER SOUTHWEST SPECIAL ITEM (SI # 12107 # 53) STEP 31 REF. FIG 15

Part: STRINGER — OUT OF TOLERANCE (CABIN) · airframe 68,656 hrs · 40,762 cycles

WHILE ACCOMPLISHING SI#12107-53 FOUND HOLE 8L AT S-3L OUT OF THE .0312- 0.3130 TOLERANCE REQUIRED PER THE SI ON STEP 19F. (EXISTING HOLE DIAMETER 0.319) / REPAIRED FASTENER HOLE AT BS 1016 STRINGER 3L; HOLE 8L AS PER SOUTHWEST SPECIAL ITEM (SI # 12107 # 53) STEP 20; REF. FIG 10

Part: STRINGER — OUT OF TOLERANCE (CABIN) · airframe 68,656 hrs · 40,762 cycles

WHILE ACCOMPLISHING SI#12107-53 FOUND HOLE 7L AT S-3L OUT OF THE 0.312-0.3130' TOLERANCE REQUIRED PER THE SI ON STEP 19D. (EXISITING HOLE DIAMETER 0.317) / REPAIRED FASTENER HOLE AT BS 1016 STRINGER 3L HOLE 7L AS PER SOUTH WEST SPECIAL ITEM (SI # 12107-53) STEP 20; REF. FIG 10

Part: STRINGER — OUT OF TOLERANCE (CABIN) · airframe 68,656 hrs · 40,762 cycles

WHILE ACCOMPLISHING SI#12107-53 FOUND HOLE 7R AT S-3R OUT OF THE 0.312- 0.3130' TOLERANCE REQUIRED PER STEP 24D. (EXISTING HOLE DIAMETER .315) / REPAIRED FASTENER HOLE AT BS 1016 STRINGER 3R HOLE 7R AS PER SOUTH WEST SPECIAL ITEM (SI # 12107-53) STEP 25 REF. FIG 10

Part: STRINGER — OUT OF TOLERANCE (CABIN) · airframe 68,656 hrs · 40,762 cycles

WHILE ACCOMPLISHING SI#12107-53 FOUND HOLE 8R AT S-3R OUT OF THE 0.312- 0.3130' TOLERANCE REQUIRED PER THE SI ON STEP 24F. (EXISTING HOLE DIAMETER .315) / REPAIRED FASTENER HOLE AT BS 1016 STRINGER 3R; HOLE 8R AS PER SOUTHWEST SPECIAL ITEM (SI # 12107 # 53) STEP 25 REF. FIG 10

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,656 hrs · 40,762 cycles

R/H HORIZONTAL STABILIZER TRAILING EDGE, RIB AT STA. 66.54 CRACKED. / REPAIRED RIB IAW SRM.

Part: BULKHEAD — OUT OF TOLERANCE (AFT FUSELAGE) · airframe 68,656 hrs · 40,762 cycles

BS 1016 APB AT 6R STR-2R HOLE OUT OF TOLERANCE; MEASURES 0.380' / REPAIRED FASTENER HOLE AT BS 1016 STRINGER 2R; HOLE 6R AS PER SOUTHWEST SPECIAL ITEM (SI # 12107-53) STEP 13 REF. FIG 5

Part: STRINGER — CORRODED (BS 360) · airframe 68,656 hrs · 40,762 cycles

EQUIPMENT AND ELECTRONICS COMPARTMENT AT STRINGER CORRODED AT BS. 360+15, STR. 27L. / REPAIRED STRINGER IAW SRM AND EA.

Part: CHANNEL — CORRODED (BS 727-847) · airframe 68,656 hrs · 40,762 cycles

AFT CARGO COMPARTMENT L/H FLOOR SUPPORT ZEE CHANNEL CORRODED BETWEEN BS. 727 TO BS. 847, STR. 25L / R&R FLOOR SUPPORT ZEE CHANNEL PER SRM & DWG.

Part: SEAT TRACK — CORRODED (BS 400-480) · airframe 68,656 hrs · 40,762 cycles

L/H PASSENGER CABIN SEAT TRACKS UPPER CROWN SURFACE CORRODED BETWEEN BS. 400+10 TO BS. 480, LBL 45.50. / R&R SEAT TRACK SECTION IAW SRM.

Part: CHANNEL — CORRODED (AFT CARGO) · airframe 68,656 hrs · 40,762 cycles

AFT CARGO COMPMT.R/H SIDE FLOOR SUPPORT ZEE CHANNEL SURFACE CORROSION S-25R STA 767 TO 787 MKD DOT 0-027 / ACCOMPLISHED VISUAL INSPECTION AT AFT CARGO COMP. FLOOR SUPPORT ZEE CHANNEL FOUND OUT OF LIMITS; REMOVED FLOOR SUPPORT ZEE CHANNEL AT CARGO COMP. R/H SIDE STA 25R BETWEEN STA 767 TO STA 787 LOCATED; DRILLED; AND INSTALLED NEW FLOOR SUPPORT ZEE CHANNEL AT AFT CARGO COMP. R/H SIDE STA 25R BETWEEN STA 767 TO STA 787 IAW B737 700 SRM 51-40-06-0 AND DRAWING 146 AB127

Part: FITTING — CORRODED (AFT FUSELAGE) · airframe 68,656 hrs · 40,762 cycles

AFT LWR FUS.INTERNAL S-27L TERMINAL END FITTING CORROSION AT STA 1016 MKD DOT / REMOVED CORROSION AT AFT CARGO STRINGS AND FITTING MEASURES: MATERIAL ORIGINAL THICKNESS .200'' MINIMUM MATERIAL FOUND .130' MATERIAL LOST .070'' FOUND OUT LIMITS AS PER REF B-737-700 SRM 53-70-07-01-1 AND DWG. 148A3450. REMOVED AND REPLACE STRINGE END FITTING AS PER REF B737-700 SRM 51-40.04-06-0 AND DWG 148A0933

Part: CHANNEL — CORRODED (BS 727-767) · airframe 68,656 hrs · 40,762 cycles

AFT CARGO COMPARTMENT R/H FLOOR SUPPORT ZEE CHANNEL SURFACE CORRODED BETWEEN BS. 727 TO BS. 767, STR. 25R. / R&R AFT CARGO FLOOR SUPPORT ZEE CHANNEL IAW SRM.

Part: DOUBLER — CORRODED (BS 727E-747) · airframe 68,656 hrs · 40,762 cycles

AFT CARGO COMPARTMENT SPOT CORRODED BETWEEN BS. 727E TO BS. 747, STR. 25R. / REPAIRED DOUBLER IAW SRM AND DWG.

Part: FITTING — CORRODED (AFT CARGO) · airframe 68,656 hrs · 40,762 cycles

AFT CARGO COMPMT. BILGE CARGO NET TIE DOWN FITTING PITTING CORROSION AT STA 787 S-24 L MKD DOT60-031 / REMOVED AND REPLACED CARGO NET TIE DOWN FITTING AT AFT CARGO STA 787 ; S-24L AS PER REF B737-700 AMM 25-52-06-400-801

Part: SUPPORT STRAP — CORRODED (AFT CARGO) · airframe 68,656 hrs · 40,762 cycles

AFT CARGO COMOMT BIGE FLOOR SUPPORT STRAP CORRODED AT STA 727D MKD DOT 60-025 FROM LBL 20.5 TO RBL 20.5 / REMOVED AND REPLACED SUPPORT STRAP AT AFT LAMP STA 727D RBL 205 TO LBL 205 IAW B737-700 SRM 51-40-02

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,656 hrs · 40,762 cycles

LT PASSENGER CABIN SEAT TRACKS;SHOW SIGNS OF UPPER CROWN SURFACE CORROSION AT B.S.520 LBL 45.50.(MKD 26-007) / CLEANED AND EVALUATED GAUGE AREA; MAT ORIGINAL .142; MAT LOST .023; MAT REMAINING .122. FOUND TO BE OUT LIMITS PER B737 SRM 53-00-52-1A. REMOVED SLOT TRACK DAMAGED FROM STA 520-500C+9' LBL 45.5 PER B737 SRM 53-00-52-2R-4. INSTALLED EWIS PROTECTION PER AMM 20-60-07-913-801. LOCATED AND DRILLED NEW SLOT TRACK AND CHANNEL REPAIR PER B737 SRM 53-00-52-2R-4; SEALED AND INSTALLED SLOT TRACK AND CHANNEL REPAIR PER B737 SRM 53-00-52-2R. REMOVE EWIS PROTECTION PER B737 AMM 20-60-07-913-801

Part: PANEL — ELONGATED (R/H WING) · airframe 68,656 hrs · 40,762 cycles

ELONGATED BOLT HOLE ON PANEL 621PB. 203-2 / CLEANED AREA OF DAMAGED OF PANEL #621 PB REF B737-700 SRM 51-70-06-2R-11 REPAIR 11-4(E) INSTALLED FIBERGLASS REPAIR CURED AND DRILL THE HOLES REF B737-700 SRM 51-70-06-2R-11 REPAIR 11-4-(N); MAT USED PO # 1150387; PO# 1624260; AND PO#1614988.

Part: PANEL — ELONGATED (R/H WING) · airframe 68,656 hrs · 40,762 cycles

ELONGATED BOLT HOLE ON PANEL 621LB. 203-3 / CLEARED AREA OF PANEL 621 LB REF B737-700 SRM 51-70-06-2R-11 A REPAIR 11-4(E); INSTALLED FIBERGLASS REPAIR CURED IT AND DRILL; THE HOLES REF B737-700 SRM 51-70-06-2R-11. REPAIR 11-4 (N) ; MAT USED PO# 1150387; PO# 1624260 AND PO # 1614988.

Part: BULKHEAD — OUT OF TOLERANCE (AFT FUSELAGE) · airframe 68,656 hrs · 40,762 cycles

BS 1016 APB AT 6L STR-2L HOLE OUT OF TOLERANCE MEASURES 0.381'. / REPAIRED FASTNER HOLE AT BS-1016 STR. 2 LEFT HOLE 6L AS PER BOEING S.I. # 12107-53 AND FIGURE 7 AND STEP 4 AND 5.

Part: PANEL — DELAMINATED (RH WING) · airframe 68,656 hrs · 40,762 cycles

DELAMINATION ON RIGHT WING LOWER PANEL 621DB CORNERS. 203-1 / CLEANED AND REPAIRED AT RIGHT WING LOWER PANEL 621DB PERB737-700 SRM 51-70-06-2R-6.MATERIAL USED P.O. #1150387; P.O. #1624260 AND P.O.#1614988. (FG 1257 09/26/19)

Part: BULKHEAD — OUT OF TOLERANCE (AFT FUSELAGE) · airframe 68,656 hrs · 40,762 cycles

BS 1016 APB AT 5L STR-2L HOLE OUT OF TOLERANCE MEASURES 0.380'. / REPAIRED FASTNER HOLE AT BS 1016 STR. 2 LEFT HOLE 5L AS PER BOEING S.I # 12107-53 AND FIGURE 7 AND STEP 4 AND 5.

Part: ATTACH ANGLE — CRACKED (CENTER WING) · airframe 68,656 hrs · 40,762 cycles

WING CENTER SECTION REAR SPAR LOWER CHORD CRACKED AT STA 663.75 LBL 24.92 AND WL 167.48. VIEWED THRU LEFT A/C BAY / ACCOMPLISHED PERMANENT REPAIR AT VAPOR BARRIER ATTACH ANGLE CRACK AT BS 663; LBL 24.92 AS PER SOUTHWEST EA # 1-757-16549 REV IR

Part: PANEL — DELAMINATED (R/H WING) · airframe 68,656 hrs · 40,762 cycles

RH WING PANEL 521DB HAS INSIDE CORNERS STARTING TO DELAMINATE. / CLEANED AREA OF DAMAGED OF R/W PANEL 521 DB REF B737-700 SRM 51-70-06-2R-6 REPAIRED 6-4 (B) PUT THE LAMINATED RESING CURED IT AND APPLIED FINISH ;REF B737-700 SRM 51-70-06-2R-6 REPAIRED 6-4-(G) MATERIAL USED EY3804AB PO#1624260

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 68,656 hrs · 40,762 cycles

RT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY 5, STAB STA 129.50, CRACKED AT STIFFENER #3. REPAIRED STIFFENER #3 PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,656 hrs · 40,762 cycles

HORIZONTAL ANGLE CRACKED AT BS 663.75, RBL 8. REPAIRED ANGLE IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 68,656 hrs · 40,762 cycles

LT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY 4, STAB STA 120.30, CRACKED AT STIFFENER #2. REPAIRED STIFFENER IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 68,656 hrs · 40,762 cycles

RT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY 3, STAB STA 111.10, CRACKED AT STIFFENER #3. REPAIRED RIB PER SRM.

Part: PRESSURE DECK — CRACKED (MAIN CABIN) · airframe 68,656 hrs · 40,762 cycles

EVIDENCE OF A CRACK AT THE HORIZONTAL PRESSURE DECK WEB (INTERNAL) STA. 663+2 AND LBL 33. / ACCOMPLISHED CATEGORY A REPAIR 2 AT MAIN CABIN HORIZONAL PRESSURE DECK WEB ON L/H SIDE BETWEEN STA 663.75 AND STA 675 FROM LBL 30 TO LBL 60 REF B737-700 SRM 53-40-51-2R-2 FIG 203

Part: FLOOR PANEL — CRACKED (FWD CARGO COMPT) · airframe 68,536 hrs · 40,690 cycles

FORWARD CARGO BAY AFT FLOOR PANEL CRACKED THROUGH. / REMOVED AND REPLACED FORWARD CARGO FLOOR AFT OF DOOR PER AMM 25-52-10

Part: CONNECTOR — LOOSE (CABIN) · airframe 68,106 hrs · 40,410 cycles

LT OVERWING EMERGENCY EXIT LIGHTS INOP. SECURED PLUG D12464 PER WDM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 67,512 hrs · 40,031 cycles

R2 DOOR EVAC SLIDE GIRT LOOSE. INSTALLED SLIDE PER MT AND AMM.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,457 hrs · 39,994 cycles

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

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,457 hrs · 39,994 cycles

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

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,457 hrs · 39,994 cycles

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

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,457 hrs · 39,994 cycles

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

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,457 hrs · 39,994 cycles

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

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,457 hrs · 39,994 cycles

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

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,457 hrs · 39,994 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,019 hrs · 39,712 cycles

LT EMERGENCY LIGHT INOP AT ROW 4. R&R BULB IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 66,527 hrs · 39,384 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 66,527 hrs · 39,384 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 66,527 hrs · 39,384 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 66,527 hrs · 39,384 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 66,527 hrs · 39,384 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R&R BATTERY PER AMM.

Part: NONE — CRACKED (R/H ENGINE) · airframe 66,527 hrs · 39,384 cycles

RIGHT ENGINE; RIGHT FAN COWL SKIN CRACK AT FWD BOTTOM CORNER. / R&R RIGHT ENGINE; RIGHT FAN COWL PER AMM 71-11-02. TAG NO: 460073 PN ON: 314-2200-18 SN ON: 8543001 PN OFF: SN OFF: 1900001

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 65,818 hrs · 38,918 cycles

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

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 65,283 hrs · 38,592 cycles

DURING WALK AROUND; FOUND CRACK IN FWD CARGO CENTER THRESHOLD SCUFF PLATE APPX 2.25' IN LENGTH MOD / REPAIRED FWD CARGO CENTER THRESHOLD SCUFF PLATE BY OUTSIDE VENDOR (J.L. WELDING INC W.O # 15759) IRW SOUTHWEST EA # 1-A53-2076 REV 11

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,459 hrs · 37,383 cycles

RIGHT EMERGENCY EXIT WINDOW LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,816 hrs · 36,986 cycles

LT OVERHEAD BIN EMERGENCY LIGHT INOP AT ROW 17. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,689 hrs · 36,897 cycles

RIGHT EMERGENCY LIGHT INOPERATIVE AT ROW 22. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: BRACKET — CRACKED (VERTICAL STAB) · airframe 62,307 hrs · 36,661 cycles

LT VERTICAL STABILIZER PANEL 323BL FORWARD SKATE ANGLE BRACKET CRACKED. R&R BRACKET PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,132 hrs · 36,555 cycles

GALLEY 4 EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: FRAME — CORRODED (BS 303.9) · airframe 62,132 hrs · 36,554 cycles

FRAME INBOARD FLANGE CORRODED AT BS 303.9, STRINGER 5L. REPAIRED THE FRAME IAW ER AND EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 62,132 hrs · 36,554 cycles

VAPOR BARRIER CRACKED AT BS 663, RBL 7. REPAIRED BARRIER IAW SRM.

Part: NONE — CORRODED (FWD CARGO COMPT) · airframe 62,132 hrs · 36,554 cycles

***CORROSION*** FWD. CARGO BAY; AFT BULKHEAD BS 500D; CENTER PANEL 121HW; LOWER PANEL EXTRUSION HAS CORROSION / REMOVED AND REPLACED PANEL 121HW LWR EXTRUSION PER DWG 453A1510

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

LT VAPOR BARRIER CRACKED AT BS 663. REPAIRED BARRIER IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

A/C EXHAUST DOUBLER CRACKED AT BS 663, LBL 20. R&R DOUBLER IAW SRM AND DWG.

Part: STIFFENER — CRACKED (BS 662) · airframe 62,132 hrs · 36,554 cycles

FORWARD SIDE OF VAPOR BARRIER WEB VERTICAL STIFFENER CRACKED AT BS 662, RBL 7. R & R THE STIFFENER IAW SRM & DWG.

Part: DOUBLER — CRACKED (WHEEL WELL RH) · airframe 62,132 hrs · 36,554 cycles

RIGHT HAND; A/C EXHAUST DOUBLER; AT BS663; RBL 20; WL 148; CRACKED. / LOCATED AND DRILLED A/C EXHAUST DOUBLER PER SRM 51-40-05 AT BS.663; RBL 20; WL 148. TO BE INSTALLED ON DEFECT #T694365. 84504U 29AUG17

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

LT CREASE BEAM WEB CORRODED BETWEEN BS 685 TO BS 695, LBL 65. R&R WEB IAW SRM AND DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

SHEAR WEB CORRODED BETWEEN BS 986 TO BS 1016, RBL 50. R&R SHEAR WEB IAW DWG AND SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

AFT CARGO BAY SUB THRESHOLD CORRODED BETWEEN BS 791 TO BS 847, RBL 18. R&R THRESHOLD ASSEMBLY PER SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (BS 887-947) · airframe 62,132 hrs · 36,554 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED BETWEEN BS 887 TO 947, RBL 3. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

LAV SUPPORT CHANNEL CORRODED BETWEEN BS 1006 TO BS 1016, LBL 55. R&R CHANNEL IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 328, BETWEEN RBL 43 TO RBL 50. R&R CHORD PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 15. R&R SUPPORT PER SRM & DWG.

Part: NONE — CORRODED (MAIN CABIN) · airframe 62,132 hrs · 36,554 cycles

CORROSION ON FSD MOPSILL INNER CHORD BS 301 AND 326 RBL55 WL208 / REMOVED CORROSION ON FSD MOPSILL AT BS 326 RBL 55 WL 208 IN AN ORDER OF 6' X 2' X .015' MAX MATERIAL LOSS ALLOWED IS .008' IAW SRM 51-10-02-0G-0 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-2 PARA 4.E. (2) FIG 103 CIRCLE NOTE D. REMOVED AND REPLACE FSD MOP SILL INNER CHORD IAW SRM 51-40-02-0G-0 AND DWG 141A8310 AND DWG 143A5900. 55860C 25AUG17

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 500D, LBL 22. R&R SUPPORT PER SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 772, RBL 8.1. REPAIRED SUPPORT PER EA.

Part: SUPPORT ANGLE — CORRODED (FWD CARGO BAY) · airframe 62,132 hrs · 36,554 cycles

***CORROSION*** FORWARD CARGO BAY BULKHEAD SUPPORT ANGLE BS500D RBL15-LBL15. / REMOVED AND REPLACED FORWARD CARGO BAY BULKHEAD SUPPORT ANGLE BS500D RBL 15-LBL 15 IAW DWG 143A9481 AND SRM 51-40-02

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 420, RBL 15. R&R SUPPORT IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 772, LBL 8.1. REPAIRED SUPPORT PER EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 21. R&R SUPPORT PER DWG & SRM.

Part: WEB — CORRODED (FWD CARGO BAY) · airframe 62,132 hrs · 36,554 cycles

***CORROSION*** FORWARD CARGO BAY SUB THRESHOLD BS440-496 RBL18. / REMOVED AND REPLACED FWD CARGO SUBTHRESHOLD WEB PER DWG 143A8330 AND SRM 51-40-02

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 62,132 hrs · 36,554 cycles

FWD CARGO BAY FWD CORNER THRESHOLD CRACKED. / FWD CARGO BAY FWD CORNER THRESHOLD REPAIRED PER SWA EA 1-A53-2076 REV 11

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LBL 15. R&R SUPPORT PER SRM & DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

SHEAR WEB CORRODED BETWEEN BS 986 TO BS 1013, LBL 50. R&R SHEAR WEB IAW DWG AND SRM.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 62,132 hrs · 36,554 cycles

***CORROSION*** AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT BS767-791 RBL21. / REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767-791 RBL21 IN AN AREA OF 2.0X0.25 PER SRM 51-10-02 ITEM IS. DUE TO NO SRM LIMITS PART TO BE REPLACED PER SRM 51-10-02 ITEM 9.REMOVED CORRODED FLOOR TO SIDEWALL SUPPORT PER SRM 51-40-02.RECIEVED NEW FLOOR TO SIDEWALL SUPPORT LOCATED;DRILLED AND INSTALLED;PER SRM 51-40-02 AND PER DWG 146A0081 BS 767-791 RBL 21.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986, BETWEEN LBL 50 TO RBL 50. R&R CHORD PER SRM & EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO BS 887, RBL 15. R&R SUPPORT PER SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 496 TO BS 500A, RBL15. R&R SUPPORT PER SRM & DWG.

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 62,132 hrs · 36,554 cycles

CRACKED INTERCOSTAL BS 344-360 LBL12 WL 208 / REMOVED AND REPLACED CRACKED INTERCOSTAL AT BS 344- 360 LBL 12 WL 208 IAW SRM 51-40-02-0G-0 SRM 51-40-05 -0G-0 AND BOEING DWG 141A5400 13656R 18AUG17

Part: STUB FRAME — CRACKED (BS 294.5) · airframe 62,132 hrs · 36,554 cycles

STUB FRAME CRACKED AT BS 294.5, RBL 50. REPAIRED THE STUB FRAME IAW ER & EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 847 TO BS 867, RBL 15. R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 420 TO BS 440, RBL 15. R&R SUPPORT PER SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED BETWEEN BS 887 TO BS 947, RBL 13.8. R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (MAIN CABIN) · airframe 62,132 hrs · 36,554 cycles

CORROSION ON THRESHOLD SUPPORT ANGLE ATTACHED TO MOPSILL BS 317-340 LBL60 / CORROSION ON THRESHOLD SUPPORT FOUND TO BE OUT OF LIMITS PER SRM 53-10-15-1A-1. REMOVED SUPPORT AND LOCATED AND INSTALLED NEW SUPPORT IAW SRM 51-40-02 AND DWG 141A8110.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

AFT CARGO BAY SUB THRESHOLD STRAP CORRODED BETWEEN BS 767 TO BS 867, RBL 15. R&R STRAP ASSEMBLY PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 31. R&R INTERCOSTAL IAW SRM & DWG.

Part: SCUFF PLATE — CORRODED (MAIN CABIN) · airframe 62,132 hrs · 36,554 cycles

CORROSION ON ASD MOPSILL INBD CHORD BS993 RBL60 WL 208 / REMOVED AND REPLACED ASD MOPSILL I.A.W BOEING DWG 147A8501 AND SRM 51-40-02-0G-0.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

MOPSILL INNER CHORD CORRODED BETWEEN BS 310 TO BS 357, LBL 50. R&R CHORD IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 935, LBL 3. R&R SUPPORT PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 62,132 hrs · 36,554 cycles

CRACKED INTERCOSTAL BS 344-360 BL 0 WL 208 / REMOVED AND REPLACED CRACKED INTERCOSTAL AT BS 344- 360 BL 0 WL 208 IAW SRM 51-40-02-0G-0 SRM 51-40-05- 0G-0 AND BOEING DWG 141A5400 13656R 18AUG17

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 62,132 hrs · 36,554 cycles

HORIZONTAL PRESSURE WEB CRACKED AT BS 663, RBL 40. / REPAIRED WEB PER ER & EA.

Part: SCUFF PLATE — CRACKED (MAIN CABIN) · airframe 62,132 hrs · 36,554 cycles

FWD SERVICE DOOR SCUFF PLATE CRACKED AT AFT END / REPAIRED FWD SERVICE DOOR THRESHOLD PER EA 1-A53-2076 REV 11

Part: PLATE — CRACKED (LT WING) · airframe 62,132 hrs · 36,554 cycles

LT WING LOWER TRAILING EDGE WIGGLE PLATE FOR PANEL 551GB CRACKED. R&R WIGGLE PLATE IAW SRM AND DWG.

Part: BRACKET — BROKEN (LT WING) · airframe 62,132 hrs · 36,554 cycles

BRACKET AT PANEL 551FB FWD EDGE 27' FROM O/B EDGE BROKEN / REMOVED AND REPAIRED BROKEN BRACKET AT PANEL 551FB FWD EDGE 27' FROM O/B END. IAW SRM 51-40-02-0G-0 PAR.4.51048U 17AUG17

Part: PLATE — CRACKED (RT WING) · airframe 62,132 hrs · 36,554 cycles

WIGGLE PLATE AT LOWER TRAILING EDGE PANEL 651GB CRACKED / REMOVED AND REPLACED WIGGLE PLATE AT LOWER TRAILING EDGE COMMON TO PANEL 65/GB IAW SRM 51-40-0-0G-0 15AUG17 84036U AND AIPC 57-50-00-30 84036U 15AUG17

Part: SKIN — CRACKED (LE SLAT) · airframe 62,132 hrs · 36,554 cycles

RT WING NR 8 SLAT NOSE SKIN CRACKED AT SLAT ACTUATOR ATTACH POINT. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

***CORROSION*** FUSELAGE SKIN; AROUND VENT BS 915; BETWEEN STR 21L AND 22L / FUSELAGE SKIN; AROUND VENT BS 915 BETWEEN STR 21L AND 22L REPAIRED PER ATS ER 17-03722 REV IR AND SWA EA 1-753-31633 REV IR INTERM REPAIR WITH INSPECTION TO FOLLOW

Part: SKIN — CRACKED (LE SLAT) · airframe 62,132 hrs · 36,554 cycles

LT WING NR 2 SLAT NOSE SKIN CRACKED AT SLAT ACTUATOR ATTACH POINT. REPAIRED SKIN PER SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 62,132 hrs · 36,554 cycles

EXTERNAL POWER CUTOUT DOUBLER AFT EDGE REPAIR PART CRACKED. REPAIRED DOUBLER PER SRM.

Part: HANDLE — OUT OF ADJUST (COCKPIT) · airframe 62,132 hrs · 36,554 cycles

RT NR 2 WINDOW EMERGENCY EXIT HANDLE OUT OF ADJUST. ADJUSTED HANDLE PER AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 61,774 hrs · 36,336 cycles

L1 DOOR SLIDE PRESSURE GAUGE OUT OF POSITION. REPOSITIONED THE SLIDE IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 61,607 hrs · 36,222 cycles

FORWARD EMERGENCY EXIT SIGN LENS CRACKED. R&R LENS IAW AMM.

Part: DOOR — BROKEN (MAIN CABIN) · airframe 61,607 hrs · 36,222 cycles

TRANSFERRED FROM NRC D144199. FWD ENTRY DOOR AFT UPPER STOP CASTING BROKEN. / R&R FWD ENTRY DOOR IAW AMM 52-11-00 LK& OPS CK GOOD CLEARING # 87526 POS ONLY: P/N OFF 141A6150-2M S/N OFF 000451 P/N ON 141A6100-678M S/N ON 000050

Part: LIGHT — BROKEN (CABIN) · airframe 58,573 hrs · 34,423 cycles

CENTER AISLE OVERHEAD EXIT LIGHT BROKEN. R & R THE LIGHT IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

FRAME CRACKED AT BS 520, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

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

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

SEAT TRACK SPLICE CRACKED, AT BS 727B, RBL 45.5. REPAIRED STRAP IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

FRAME CRACKED AT BS 480. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL 45.5. REPAIRED BEAM IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,795 hrs · 33,393 cycles

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

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,795 hrs · 33,393 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN RBL 35 - 45. REPAIRED WEB IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,579 hrs · 33,261 cycles

FORWARD CARGO COMPARTMENT FLOORBOARD SUPPORT CRACKED AT BS 540 RT. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,579 hrs · 33,261 cycles

FORWARD CARGO COMPARTMENT FLOORBOARD SUPPORT CRACKED AT BS 540 LT OF CTR. R & R SUPPORT IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 56,579 hrs · 33,261 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT M01675. R & R BATTERY PACK IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,735 hrs · 32,753 cycles

R1 DOOR EMER SLIDE LIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,735 hrs · 32,753 cycles

R1 DOOR EMER EXTERNAL SLIDE LIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 54,957 hrs · 32,313 cycles

R2 DOOR EXIT SIGN LENS MISSING. INSTALLED LENS IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 54,357 hrs · 31,966 cycles

AFT EMER EXIT SIGN LOOSE. R & R SIGN IAW AMM.

Part: TAB — CRACKED (LT AILERON) · airframe 54,803 hrs · 32,224 cycles

LEFT WING OTBD AFT WING OUTSIDE OF THE AILERON TAB CRACKED. REPAIRED TAB IAW SRM.

Part: SLIDE — UNWANTED DEPLOY (R2 DOOR) · airframe 53,280 hrs · 31,344 cycles

R2 DOOR EMER EVAC SLIDE INADVERTENTLY DEPLOYED. R & R SLIDE ASSEMBLY IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,355 hrs · 29,604 cycles

LT EMERGENCY EXIT LIGHT LAMPS INOPERATIVE. RELAMPED LAMPS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,355 hrs · 29,604 cycles

RT EMERGENCY EXIT LIGHT LAMPS INOPERATIVE. RELAMPED LAMPS IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 50,119 hrs · 29,464 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. R & R SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 50,013 hrs · 29,405 cycles

R1 DOOR EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 50,010 hrs · 29,403 cycles

RT HORIZONTAL STABILIZER IN SPAR RIB AT STABILIZER STATION 138.70 CRACKED AT LOWER END OF FWD VERTICAL STIFFENER. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 50,010 hrs · 29,403 cycles

RT HORIZONTAL STABILIZER IN SPAR RIB AT STABILIZER STATION 92.70 CRACKED AT ALL 4 VERTICAL STIFFENERS AT LOWER END. REPAIRED RIB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,010 hrs · 29,403 cycles

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

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 50,010 hrs · 29,403 cycles

LT WING AFT UPPER TE PANEL SUPPORT ANGLE CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT. R & R BRACKET IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,010 hrs · 29,403 cycles

LT NR 3 WINDOW FRAME CRACKED AT EF POST AT 2ND FASTENER FROM THE BOTTOM. REPAIRED POST IAW ACO.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 50,010 hrs · 29,403 cycles

MAIN WW VERTICAL PRESSURE WEB CRACKED AT BS 663 LBL 29. REPAIRED WEB IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,010 hrs · 29,403 cycles

RT NR 3 FLIGHT DECK WINDOW FRAME CRACKED AT EF POST AT 2ND FASTENER FROM BOTTOM. REPAIRED FRAME IAW EA & ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,010 hrs · 29,403 cycles

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

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 50,010 hrs · 29,403 cycles

LT WING TRANSVERSE WEB ATTACH ANGLE CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT. R & R ANGLE IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 50,010 hrs · 29,403 cycles

MAIN WW VERTICAL PRESSURE WEB CRACKED AT BS 663 LBL 35. REPAIRED WEB IAW EA.

Part: BATTERY — FAILED (CABIN) · airframe 49,894 hrs · 29,341 cycles

RT EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST. R & R BATTERIES IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 49,894 hrs · 29,341 cycles

LT EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST. R & R BATTERIES IAW MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 49,894 hrs · 29,341 cycles

LT EMERGENCY LIGHT POWER SUPPLY INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: SENSOR — FAULTY (TE FLAP) · airframe 49,618 hrs · 29,166 cycles

DIVERT, DECLARED EMERGENCY, TE FLAP ASSEMBLY. R & R NR 6 FLAP SKEW SENSOR IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 45,471 hrs · 26,642 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 44,631 hrs · 26,149 cycles

R2 DOOR EMERGENCY EVAC SLIDE NEEDS OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 43,234 hrs · 25,356 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT PRESSURE BULKHEAD OIL CAN AT STR 2R. REPAIRED BULKHEAD IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 43,234 hrs · 25,356 cycles

DURING SCHEDULED 12Y CHECK FOUND, L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,234 hrs · 25,356 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING NR 3 SLAT LOWER L/E SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,234 hrs · 25,356 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING L/E NR 7 SLAT LOWER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,234 hrs · 25,356 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT Z ANGLE CORRODED AT BS 767+3, LBL 18. REMOVED AND REPLACED Z-ANGLE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,234 hrs · 25,356 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 4L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,234 hrs · 25,356 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM CORRODED AT BS 986.5, LBL 48. REPAIRED BEAM IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,234 hrs · 25,356 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 7L TO STR 8L. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,234 hrs · 25,356 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 2L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 44,468 hrs · 25,493 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX BULKHEAD ATTACH ANGLE CRACKED AT BS 540, RBL 15. REMOVED AND REPLACED ANGLE PER ACO.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 44,468 hrs · 25,493 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX BULKHEAD ATTACH ANGLE CRACKED AT BS 540, RBL 8. REMOVED AND REPLACED ANGLE PER ACO.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 44,468 hrs · 25,493 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX BULKHEAD ATTACH ANGLE CRACKED AT BS 540, RBL 52. REMOVED AND REPLACED ANGLE PER ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 43,234 hrs · 25,356 cycles

DURING SCHEDULED 12Y CHECK, FOUND FIRST OFFICERS WINDOW FRAME POST CRACKED. REMOVED AND REPLACED WINDOW POST FRAME PER BAC DWG AND SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 43,205 hrs · 25,336 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 43,205 hrs · 25,336 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.70. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,234 hrs · 25,356 cycles

DURING SCHEDULED 12Y CHECK, FOUND CAPTAINS NR 1 WINDOW FRAME CRACKED AT UPPER O/B CORNER. REMOVED AND REPLACED SKIN IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,234 hrs · 25,356 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT WEB UPPER SURFACE CORRODED BETWEEN BS 807 TO BS 827, STR 25R. REPAIRED WEB IAW SRM AND DWG.

Part: ACTUATOR — MALFUNCTIONED (LE SLAT) · airframe 43,040 hrs · 25,244 cycles

AIR TURNBACK - ON TAKEOFF L/E FLAPS TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 4 SLAT ACTUATOR, ALL FOUR HYDRAULIC LINES FROM ACTUATOR OT SWIVELS, AFT MOUNTING BOLD, BUSHING, WASHER AND NUT IAW MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 40,781 hrs · 23,926 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 38,751 hrs · 22,718 cycles

DURING SCHEDULED BC1 CHECK, FOUND RT WING O/B AFT FLAP I/B CORNER DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,152 hrs · 21,804 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. REPAIRED SIGN PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT FWD EMERGENCY EXIT LIGHT BATTERY INOP. CHARGED BATTERY PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 40.87. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 15.04. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 6.14. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 40.87. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS BS 540, LBL 32.4. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REPLAMPED PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 15.04. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 54.6. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (BS 540) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 32.4. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS BS 540, LBL 6.14. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR FRAME LOWER FRAME COVER CRACKED. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING NR 1 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER AAR EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 54.6. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,393 hrs · 21,330 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 457, STR 16L. REPAIRED BEAM PER EA.

Part: LENS — BROKEN (CABIN) · airframe 36,346 hrs · 21,305 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 35,323 hrs · 20,667 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 35,323 hrs · 20,667 cycles

DURING SCHEDULED CV CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED COVER PER MM.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 35,138 hrs · 20,539 cycles

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

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 35,138 hrs · 20,539 cycles

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

Part: HOLDER — LOOSE (GIRT BAR) · airframe 34,185 hrs · 19,956 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER RT GIRT BAR HOLDER LOOSE. SECURED HOLDER PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 34,150 hrs · 19,938 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROW 6 TO ROW 9. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 34,150 hrs · 19,938 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 34,150 hrs · 19,938 cycles

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

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 30,960 hrs · 17,971 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,668 hrs · 17,200 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 43 TO LBL 43. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,668 hrs · 17,200 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 45 TO RBL 60. REPAIRED FLOORBEAM PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,668 hrs · 17,200 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, LBL 5. REPAIRED FLOORBEAM PER ER.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 29,472 hrs · 17,081 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 28,673 hrs · 16,618 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,618 hrs · 16,586 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 10 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,811 hrs · 16,083 cycles

DURING SCHEDULED SPV CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,696 hrs · 15,426 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,415 hrs · 14,681 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 24,826 hrs · 14,333 cycles

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

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 24,826 hrs · 14,333 cycles

DURING SCHEDULED HC2 CHECK, RT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 24,826 hrs · 14,333 cycles

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

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 24,826 hrs · 14,333 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 24,734 hrs · 14,278 cycles

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

Part: BATTERY — FAULTY (CABIN) · airframe 23,988 hrs · 13,848 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT LT EMERGENCY EXIT LIGHT BATTERY WILL NOT HOLD CHARGE. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,494 hrs · 12,439 cycles

DURING SCHEDULED RON CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 18,864 hrs · 10,881 cycles

DURING SCHEDULED 5Y CHECK, FOUND LOWER FUSELAGE SKIN BETWEEN BS 500 + 8 AND BS 500A + 12, AT AIRFONE ANTENNA, CORRODED. REPAIRED SKIN PER SRM.

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 14,223 hrs · 8,192 cycles

EEPLS WIRES EXPOSED THROUGH OUT CABIN FLOOR. REPOSITIONED WIRES PER MM.

Part: MOTOR — FAULTY (RT MLG W/W) · airframe 13,348 hrs · 7,738 cycles

FLAPS STAYED AT 0 WHEN SELECTED. ALTERNATE FLAPS WERE USED TO GET FLAPS TO 10, ALTERNATE T/E FLAP DRIVE CIRCUIT BREAKER TRIPPED. RESET CB, ATTEMPED MORE FLAPS AND CB CONTINUED TO TRIP. REMOVED AND REPLACED ALTERNATE FLAP DRIVE MOTOR PER MM. OPS CK'D FLAPS WITH HYDRAULICS AND WITH ALTERNATE FLAP DR MOTOR PER MM.

Part: BUSHING — WORN (BOTH ELEVATORS) · airframe 11,059 hrs · 6,490 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT ELEVATOR TAB HINGE ATTACH POINTS NR 3 AND NR 4 WORN. REMOVED AND REPLACED HARDWARE AND BUSHINGS AT NR 3 AND NR 4 HINGE ATTACH POINTS PER MM.

Part: RIVET — MISSING (SERVICE DOOR) · airframe 5,136 hrs · 3,126 cycles

DURING SCHEDULED BC1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK RETAINER MISSING RIVET. INSTALLED RETAINER RIVET PER SRM.

Part: CONTROL ROD — WORN (RT ELEVATOR TAB) · airframe 4,949 hrs · 3,017 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED OUTBOARD ELEVATOR TAB CONTROL ROD PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP ABOVE WING DOOR. REMOVED AND REPLACED LIGHT PER MM.