N751SW

Part: BATTERY PACK — FAILED (CABIN) · airframe 75,335 hrs · 44,591 cycles

AFT L/H EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK ; / [01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,739 hrs · 44,231 cycles

CUSTOMER REQUEST: BLOWN LIGHT BULB BELOW R2 DOOR EMERGENCY EXIT SIGN ; / [01] RELAMPED LIGHT BULBS BELLOW R2 DOOR EMERGENCY EXIT SIGN AS PER REF B737 AMM 33-51-01-960-801.OPS CHECK FOUND NORMAL.; [02] INSPECTION COMPLETED.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 74,739 hrs · 44,231 cycles

FWD EMERGENCY LIGHTS (2 ON LT; CENTER SIGN AND L1 DOOR EXIT SIGN) LIGHT UP FOR ABOUT 30 SECONDS AND THEN TURN OFF. ; / [01] T/S FORWARD EMERGENCY LIGHT ISSUES AND FOUND EMERGENCY POWER SUPPLY AND BATTERY PACK AT POSITION M1675 (FWD ENTRY CEILING PANEL) INOPERATIVE AS PER REF B737 SSM 33-51-12.; [02] VERIFIED STEP 1.; [03] REMOVED AND REPLACED BATTERY PACK AND CHARGER ASSY AS PER B737 AMM 33-51-06-960-805 AND 33-51-06-960-806. PERFORMED OPS CHECK; TEST OK.<BR><BR>AAR TAG WN6140 FOR CHARGER ASSY<BR>AAR TAG A05071 FOR BATTERY PACK; [04] VERIFIED STEP 3

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,739 hrs · 44,231 cycles

SEVERAL EMERGENCY LIGHTS INOP BY AFT ENTRY/SERVICE DOOR AREA. / [01] PERFORMED T/S PER B737 FIN 33-50 TASK 801 AND FOUND BATTERY PACK M1672 PART# D717-01-100; S/N: 5570 DEFECTIVE.; [02] VERIFIED; [03] REMOVED AND REPLACED BATTERY PACK AND CHARGER ASSY AS PER B737 AMM 33-51-06-960-806 AND 33-51-06-960-805. PERFORMED OPS CHECK. TEST OK.<BR>AAR TAG WN6141 FOR CHARGER ASSY <BR>AAR TAG A05070 FOR BATTERY PARK; [04] VERIFIED STEP 3

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 74,739 hrs · 44,231 cycles

CRACK INDICATION NOTED ON SEAT TRACK FRAME BS 727B RBL24.75 HOLE 'A' AT 3 O'CLOCK POSITION ; CRACK LENGTH 0.030' / VERIFIED REMOVAL OF CORROSION AT SEAT TRACK STA. 727B RBL 24.75, I/B & O/B FLANGE. FOUND OUT OF LIMITS. PERFORMED REPAIR AT SEAT TRACK FROM STA. 727B TO STA. 727D,RBL 24.75, REF. : B737-7 SRM 51-10-02-0G-0,53-60-52-1A-0, & 53-00-52-2R-5 REPAIR 5, FIG. 202

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 74,739 hrs · 44,231 cycles

CRACK INDICATION NOTED ON SEAT TRACK FRAME BS727B RBL45.5 HOLE 'B' AT 2 O'CLOCK POSITION ; CRACK LENGTH 0.040' / CUT & REMOVED DAMAGE PART OF SEAT TRACK FROM STA. 727B TO STA. 727D PLUS 10.00'; REF : B737-7 SRM 53-00-52-2R-5 REPAIR 5;FIG. 102.; [03] PARTIALLY FABRICATED NEW SEAT TRACK P/N BAC1520-2789 7178T65 PO#1424478 REF B737-700 SRM 53-00-52-2R-5 REPAIR 5;FIG 202 FABRICATED REPAIR PARTS : 1EA. SEAT TRACK SECTION; MAT. USED BAC 1520-2789 7178-T76511; 2EA. ANGLES; MAT. USED BAC1503-100122 7075-T6; 1EA. STRAP MAT. USED 7075-T651 BARE PLATE 0.313';2EA. STRAPS MAT. USED 7075-T6 BARE SHEET 0.071'; REF. B737-7 SRM 53-00-52-2R-5 REPAIR 5 TABLE 201 & FIG. 202.; [07] LOCATED;TRIMMED & DRILLED REPAIR PARTS AT STA.727B

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 74,739 hrs · 44,231 cycles

PER CUSTOMER REQUEST...RT WING O/B T/E FLAP HAS AFT EDGE DELAMINATING AT I/B CORNER ; / [01] PERFORMED CUT OUT OF 3 3/8 ' BY 1 1/4' AT DAMAGED AREA; NO WATER FOUND; NO CORE DAMAGE FOUND AT RT WING O/B T/E FLAP I/B CORNER.; [02] PERFORMED CUT OUT OF 3 3/8 ' BY 1 1/4' AT DAMAGED AREA AS PER B737-700 SRM 51-70-10-2R-4; NO WATER FOUND; NO CORE DAMAGE FOUND AT RT WING O/B T/E FLAP I/B CORNER; [03] VERIFIED JOB IN STEP2.; [04] CLEANED DAMAGED AREA AND FABRICATED FILLERS AND DOUBLER REF B737-700 SRM 51-70-10-2R-4 REPAIR 4. APPLIED BONGEL AC 130; AND ADHESIVE PRIMER BMS 5-137 REF B737-700 SRM 51-70-10 PARAGRAPHS 14 AND 15.; [05] VERIFIED STEP 4; [06] INSTALLED REPAIR AT RT WING O/B T/E FLAP LOWER SURFACE I/B CORNER. REF B737-700 SRM 51-70-10-2R-4 REPAIR 4. PERFORMED A VISUAL INSPECTION AND TAP - TEST INSPECTION NO DAMAGES AND NO DELAMINATION FOUND REF B737 NDT PART 1 51-05-01.; [07] ACCOMPLISH TAP TEST ON REPAIR AREA FOUND NO DELAMINATION AS PER B737 NDTM 51-05-01 SECTION 5. RESTORE AREA TO ORIGINAL. FINISHES .; [08] VERIFIED STEP #7; [09] VERIFIED ALL STEPS ACCOMPLISHED

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 74,739 hrs · 44,231 cycles

LT I/B T/E FLAP AT O/B CORNER HAS PREVIOUS REPAIR DELAMINATING. ; / [01] REMOVED OLD REPAIR AT L/WING T/E FLAP O/B CORNER AS PER BOEING 737 SRM 51-70-10-2R-4 REPAIR 4; [02] VERIFIED STEP #1; [03] CUT- OUT DAMAGE AREA;NO WATER FOUND NO CORE DAMAGE AT L/T I/B T/E FLAP O/B CORNER AS PER BOEING 737 SRM51-70-10-2R-4 REPAIR4; [04] APPLIED BOEGEL C130 AT L/WING I/B FLAP O/B CORNER AS PER BOEING 737 SRM 51-70-10-2R-4 REPAIR4. CUT-OUT SIZE 7' BY 3'.; [05] VERIFIED STEP 1 THROUGHOUT STEP 4 ; AND OK TO APPLY REPAIR; [06] REPAIRED DAMAGE AREA AT L/WING I/B T/E FLAP O/B CORNER AS PER BOEING737 SRM 51-70-10-2R-4 REPAIR4.MATERIAL USED BR127 .;#1691047 PLUS HCS2404-10-05 PO#1698173 AND 2024T3.016' PO#1195957.RESTORED ORIGINAL FINISHED.; [07] VERIFIED STEP #6; [08] VERIFIED STEP 6; [09] ALL STEPS COMPLIED WITH

Part: SEAT TRACK — CORRODED (BS 727B) · airframe 74,739 hrs · 44,231 cycles

FOUND CORROSION AT CABIN SEAT TRACK STA. 727B RBL 24.75; I/B AFT. FLANGE. ; / REMOVED FASTNER FOR MATERIAL REMOVAL ORIGINAL MATERIAL OF SEAT TRACK FLANGE AT STA 727B RBL 24.75 I/B AFT IS 0.100' MATERIAL REMAINING IS 0.050' FOUND TO BE OUT OF LIMITS REF:SRM 51-40-02-0G-0; SRM 53-60-52-1A-0 FIG 103 DETAIL E; CUT SEAT TRACK AT STA. 727C + 1'; REMOVED DAMAGED PART OF SEAT TRACK FROM STA. 727B TO STA. 727D. REF. B737-7 SRM 53-00-52-2R-5 REPAIR 5. FIG202. SHEET 1.;] LOCATED AND DRILLED NEW SEAT TRACK SECTION AND REPAIR SPLICE AS PER B 737SRM53-00-52-2R-5 REPAIR 5; VERIFIED STEPS 1 & 2;] VERIFIED REMOVAL OF CORROSION AT SEAT TRACK STA. 727B RBL 24.75; I/B & O/B FLANGE. FOUND OUT OF LIMITS. PERFORMED REPAIR AT SEAT TRACK FROM STA. 727B TO STA. 727D;RBL 24.75; REF. : B737-7 SRM 51-10-02-0G-0;53-60-52-1A-0; & 53-00-52-2R-5 REPAIR 5; FIG. 202

Part: FRAME — CRACKED (R1 DOOR) · airframe 74,739 hrs · 44,231 cycles

FOUND CRACKED INTERNAL FRAME ASSY. AT R-1 DOOR FWD. UPPER CORNER. ; / [01] LOCATE AND STARTED DRILLING PROCESS OF NEW FRAME ASSEMBLY P/N 141A8370U13 P/O# 1617089 PER B737-700 SRM 51-40-02-0G-0; [02] VERIFIED STEP 1; [03] LATE ENTRY : REMOVED DAMAGED STUB FRAME AS PER B737-7 SRM 51-40-02-0G-0.; [04] STUB FRAME ASSY. FOUND OUT OF LIMITS(NO CRACKS PERMITED )AS PER B737-7 SRM 53-10-15-1A-2 FIG. 102.; [05] LOCATED & COMPLETED DRILLING OF NEW STUB FRAME AS PER B737-7 SRM 51-40-05-0G-0; & DWG. 141A8370.; [06] ACCOMPLISHED TOP COAT APPLICATION TO NEW STUB FRAME PER B737-700 AMM 51-21-73-370-803; [07] OK TO INSTALL NEW STUB FRAME; [08] MIXED BMS 5-95 SEALANT AT 7:30AM 7/16/2021 SQUEEZE OUT TIME BY 3:30 AM 7/17/2021; [09] INSTALLED NEW STUB FRAME AT R-1 DOOR FWD UPPER CORNER PER B737-700 SRM 51-40-02-0G-0 AND DRAWING #141A8370; [10] VERIFIED STEPS 8 & 9

Part: FITTING — CRACKED (R1 DOOR) · airframe 74,739 hrs · 44,231 cycles

FOUND CRACKED INTERNAL SEAL FITTING AT R-1 DOOR FWD. UPPER CORNER. ; / [01] REMOVED DAMAGE SEAL FITTING ( SEAL RETAINER ) FROM R-1 DOOR FWD UPPER CORNER PER B737-700 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW SEAL RETAINER P/N 141A8372U1 P/O #1684224 PER B737-700 SRM 51-40-02-0G-O AND DRAWING # 141A8370; [03] VERIFIED STEPS 1 & 2; [04] OK TO TREAT AND PRIME; [05] TREATED & PRIMED NEW SEAL RETAINER; REF. : B737-7 SRM 51-20-01-0G-0.; [06] OK TO INSTALL SEAL RETAINER; [07] MIXED BMS 5-95 SEALANT AT 7:30AM 7/16/2021 SQUEEZE OUT TIME BY 3:30 AM 7/17/2021; [08] INSTALLED NEW SEAL RETAINER AT R-1 DOOR FWD UPPER CORNER PER B737-700 SRM 51-40-02-0G-0 AND DRAWING #141A8370; [09] VERIFIED STEP 7 & 8

Part: DOUBLER — CRACKED (POWER CUTOUT) · airframe 74,739 hrs · 44,231 cycles

EXT. POWER RECEPTACLE CUT-OUT FWD EDGE DOUBLER CRACKED ABOVE AND BELOW THE LWR HINGE ; / [01] REMOVED POWER RECEPTACLE ACCESS DOOR #114AR PER B737-700 SRM 53-10-15-2R-5; [02] REMOVED ACCESS PANEL# 114AW AND 114AC FROM NOSE WHEEL WELL PER B737-700 SRM 51-40-02-0G-0; [03] PARTIALLY REMOVED FASTENER AT EXTERNAL POWER RECEPTACLE SKIN BETWEEN STA 219 AND STA 243 ; BETWEEN S-17R & S-24R PER SRM 51-40-02-0G-0 REMOVED INNER DOUBLER AT EXT. POWER RECEPTACLE CUT-OUT AS PER SRM 51-40-02; [06] LOCATED AND DRILLED NEW DOUBLER P/N 141A3722U12 AT EXTERNAL POWER RECEPTACLE AREA IRW B737-700 SRM 53-10-15-2R-5;] REMOVED & REPLACED INNER SKIN DOUBLER AROUND EXTERNAL POWER RECEPTACLE CUT OUT; REF. B737-7 SRM 51-40-02-0G-0; & DWG. 141A3702.;

Part: BEAR STRAP — CRACKED (BS 294) · airframe 74,739 hrs · 44,231 cycles

CRACK FOUND AT INTERNAL MAIN CABIN BEAR STRAP STA 294.5 JUST BELOW STR 8-R; CRACK LENGTH :2.362' / [01] STRIPPED PAINT AT THE REPAIR AREA OF R-1 UPPER FWD. CORNER; STA. 294.5; S-8R; CUT AND REMOVED DAMAGE PART OF THE BEAR STRAP PER B737-700 SRM 53-10-01-2R-6 PARAGRAPH 4.C; FIG 202; REPAIR 6; [18] VERIFIED STEPS 16AND STEP 17.; [19] CONTINUED FABRICATION OF REPAIR PARTS (DOUBLER &TRIPLER ) PER B737-700 SRM 53-10-01-2R-6 REPAIR 6; [20] VERIFIED STEP 19; [21] VERIFIED STEP 19; [22] OK TO TREAT AND PRIME BEARSTRAP AND FUSELAGE SKIN; [23] TREATED AND PRIMED BEARSTRAP TRIM OUT EDGES AND FUSELAGE SKIN PER B737-700 SRM 51-20-01-OG-0; [24] COMPLETED FABRICATION OF REPAIR PARTS DOUBLER MATERIAL USED 2024-T3 CLAD 0.100 IN; TRIPLER MATERIAL USED 2024-T3 CLAD 0.063 INSTARTED INSTALLATION OF REPAIR PARTS PER B737-700 SRM 53-10-01-2R-6; REPAIR 6 AND SRM 51-40-02-0G-0; [45] VERIFIED STEP 44; [46] CONTINUE INSTALLATION OF REPAIR PARTS PER B737-700 SRM 53-10-01-2R-6; REPAIR 6 AND SRM 51-

Part: CHANNEL — DAMAGED (BS 887) · airframe 74,739 hrs · 44,231 cycles

AFT CARGO BAY ZEE CHANNEL AT ST 887 ;RBL 20 RIVET HOLE IS ELONGATED. REMOVED Z CHANNEL SPLICE REPAIR AT STA 887 RBL 20 IAW 53-00-53-2R-5. INSTALLED NEW SPLICE REPAIR AT STA Z CHANNEL 887 RBL 20 ASPER B-737-700 SRM 53-00-53-2R-5 CERTIFIED INSTALLED NEW SPLICE REPAIR ASPER B-737 SRM 53-00-53-2R-5 VERIFIED SPLICE INSTALLATION INSTALLED NEW Z CHANNEL SPLICE REPAIR AT STA 887 RBL 20 AS PER B-737-700-SRM 53-00-53-2R-5 CORRECTION STEP#8 REMOVED AND INSTALLED NEW Z CHANNEL SPLICE REPAIR AT STA 887 RBL 20 ASPER B-737-700 SRM 53-00-53-2R-5 CERTIFIED CORRECTION AT STEP#8 VERIFIED REMOVAL AND INSTALLATION OF NEW Z CHANNEL SPLICE AT STA 887 RBL 20.

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 74,739 hrs · 44,231 cycles

CRACK FOUND AT NO. 4 BEAM IN THE FWD SERVICE DOOR INTERNAL STRUCTURE PN 141A6536-14 LOWER BEAM. ENSURE THAT EITHER EO 5241-C-14093-NG OR EO 5241-C-14344-NG IS IDENTIFIED IN THE REPAIR ORDER (RO) ; CRACK FOUND AT NO. 4 BEAM IN THE FWD SERVICE DOOR INTERNAL STRUCTURE PN 141A6536-14 LOWER BEAM. ENSURE THAT EITHER EO 5241-C-14093-NG OR EO 5241-C-14344-NG IS IDENTIFIED IN THE REPAIR ORDER (RO) OR ADDED TO AIRCRAFT WORK PACKAGE. / [01] PARTIALLY REMOVED FASTENERS AT NO.4 BEAM IN THE. R1 SERVICE DOOR INTERNAL STRUCTURE PER REF B737-700 SRM 51-40-02-0G-0; [02] PARTIAL CONTINUE REMOVED FASTENERS ON #4 BEAM R1 INTERNAL STRUCTURE REF B737-700 SRM 51-40-02; [03] COMPLETED REMOVED DAMAGE # 4 BEAM ON R/1 INTERNAL RESTRUCTURE REF B 737-700 SRM 51-40-02-0G-0; [04] LOCATED AND DRILLING NEW BEAM #4 REF B 737-700 SRM 51-40-05-0G-0; [05] VERIFIED STEPS 1 - 4; [06] (LATE ENTRY) STEP 4 IS RII; [07] OK TO INSTALL BEAM #4; [08] INSTALLED NEW BEAM #4 AT R-1 SERVICE DOOR INTERNAL STRUCTURE REF SRM 51-40-05-0G-0; CMM52-41-05 AND B/DRAWINGS 141A6516; [09] LATE ENTRY PARTIALL REMOVED WEB FOR ACCESS TO BEAM; [10] OK TO INSTALL PARTIALLY REMOVED WEB; [11] PARTIAL INSTALLED WEB ON R/1 SERVICE DOOR REF B737-700-0G-0; [12] MISSING REFERENCE ON STEP #11 SRM 51-40-05-0G-0; [13] COMPLETE INSTALLED WEB AT R/1 DOOR I TERROR AREA REF B 737-700 SRM 51-40-02-0G-0; [14] VERIFIED STEP #9; [15] VERIFIED STEP 8; [16] VERIFIED STEPS 11; 12 AND 13

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 74,739 hrs · 44,231 cycles

CRACK FOUND AT NO. 5 BEAM IN THE FWD SERVICE DOOR INTERNAL STRUCTURE PN 141A6536-15 UPPER BEAM. ENSURE THAT EITHER EO 5241-C-14093-NG OR EO 5241-C-14344-NG IS IDENTIFIED IN THE REPAIR ORDER (RO) OR AD ; CRACK FOUND AT NO. 5 BEAM IN THE FWD SERVICE DOOR INTERNAL STRUCTURE PN 141A6536-15 UPPER BEAM. ENSURE THAT EITHER EO 5241-C-14093-NG OR EO 5241-C-14344-NG IS IDENTIFIED IN THE REPAIR ORDER (RO) OR ADDED TO AIRCRAFT WORK PACKAGE. / REMOVED R1 DOOR HANDLE BOX ASSEMBLY AS PER B737 CMM 52-41-05;PARTIALLY REMOVED FASTENERS AT NO.5BEAM IN THE. R1 SERVICE DOOR INTERNAL STRUCTURE PER REF B737-700 SRM 51-40-02-0G-0; COMPLETE REMOVED FASTENERS AT FWD SERVICE DOOR #5 BEAM UPPER AREA INTERNAL STRUCTURE REF B737-700 SRM 51-40-02-0G-0;PARTIAL LOCATED AND DRILLING NEW BEAM AT FWD SERVICE DOOR # 5 BEAM UPPER AREA REF B 737-700 SRM 51-40-05-0G COMPLETE LOCATED AND DRILLING NEW BEAM REF B-737-700 SRM 51-40-05-0G-0; VERIFIED STEPS 1-5 BEAM OUTER SKIN AREA OF R-1 DOOR; REF. B737-7 SRM 51-40-02-G-0 & DWG. 141A6516.; INSTALLED #5 BEAM IN R 1 SERVICES DOOR REF B737 -700 SRM 51-40-02-0G-0 INSTALLED WEB AT R/1 DOOR INTERIOR AREA REF B737-700 SRM 51-40-02-0G-0; INSTALLED NEW #5 BEAM IN THE FWD. SERVICE DOOR INTERNAL AREA REPAIR ORDER : EO 5241-C-14093-NG OR EO 5241-C-14344-NG. R-1 DOOR HANDLE BOX ASSY. WILL BE INSTALLED ON TTG8Q005WGHK;

Part: TAIL CONE — DELAMINATED (AFT) · airframe 74,739 hrs · 44,231 cycles

TAIL CONE HAS TWO AREAS OF DELAM ON THE RIGHT SIDE ; DELAMINATION / [01] MEASUREMENTS; [02] CLEANSED DAMAGE AREA AND PREPARED AREA FOR REPAIR ON R/H SIDE OF OUTER SKIN OF TAIL CONE AS PER B737 SRM 51-70-04-2R-1 OK TO INSTALL REPAIR; [03] ON STEP 2 DAMAGE LOCATION IS AT STA. 1167 ;11 INCHES FROM FWD. EDGE OF TAIL CONE AND 17 INCHES FROM BOTTOM CENTER THIS REPAIR WILL BE CALLED REPAIR A; [04] SECOND DAMAGE AREA IS AT STA. 1179 ;23 INCHES FROM FWD. EDGE OF TAIL CONE AND 12 INCHES FROM BOTTOM CENTER . PERFORMED TAP TEST FOUND NO DELAMINATION ONLY DETERIORATED OUTER PAINT AS PER B737 NDTM 51-05 -01 THIS REPAIR WILL BE CALLED REPAIR B; [05] VERIFIED STEPS # 1; 2; 3 AND 4; [06] OK TO INSTALL REPAIR A; [07] REPAIRED DAMAGE A ON R/H SIDE OUTER SKIN OF TAIL CONE AS PER B737 SRM 51-70-04-2R-1 MATERIALS USED PO# 1150387 & PO# 1715972 PERFORMED TAP TEST ON REPAIRED AREA FOUND NO DELAMINATION AD PER NDTM 51-05-01 SECTION 5; [08] VERIFIED STEP 7; [09] PAINTED AREA AT STA 1179; 23 INCHES FROM FWD EDGE OF TAIL AND 12 INCHES FROM BOTTON CENTER AND AREA AT STA 1167 11 INCHES FROM FWD EDGE OF TAIL CONE AND 17 INCHES FROM BOTTOM CENTER REF B 737-700 AMM 51-21-73-370-803; [10] PAINT WORK WAS ACCOMPLISHED BY TECHNICIAN VICTORINO ANASTACIO MENDOZA EMPLOYEE # 2381; [11] VERIFIED PAINT STEP 9 AND 10.

Part: STRAP — CORRODED (BS 727D) · airframe 74,739 hrs · 44,231 cycles

AFT CARGO COMP. FLOOR SPLICE STRAP AT ST 727D IS CORRODED (228-001) ; / [01] RECEIVED NEW STRAP AND REPLACED AT AFT CARGO FLOOR SPLICESTRAP STA 727D AS PER AIPC -53-42-11-30<BR>NOTE:NEW PART WILL BE INSTALL ON TASK CARD#TTG8Q004FAR0; [02] VERIFIED NEW STRAP FOR STA 727D; [03] REF. B737-700 SRM 53-00-53-2R-5

Part: STRAP — CORRODED (B 773) · airframe 74,739 hrs · 44,231 cycles

AFT CARGO FLOOR SPLICE STRAP AT ST 773 IS CORRODED IN MANY PLACE (228-003) ; / [01] RECEIVED NEW STRAP AND REPLACED AT AFT CARGO FLOOR SPLICE STRAP STA 773 AS PER AIPC 53-42-11-30<BR>NOTE: NEW PART WILL BE INSTALL ON TASK CARD#TTG8Q004FAR0; [02] VERIFIED NEW STRAP FOR STA 773; [03] REF. : B737-700 SRM 53-00-53-2R-5.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 74,739 hrs · 44,231 cycles

CABIN SEAT TRACK L/H I/B TRACK WITH CORROSION SPOTS BETWEEN SEATS 20 AND 21. REMOVED CORROSION IAW SRM 51-10-02-0G-0. FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIGURE 103 DETAIL (A). TREATED & PRIMED REWORKED AREA OF SEAT TRACK IAW SRM 51-20-01-0G-0.

Part: BRACKET — CRACKED (LT WING) · airframe 74,739 hrs · 44,231 cycles

LT WING CONTROL RIB CENTER AFT SEAL BRACKET CRACKED. [200-005] ; / [01] REMOVED & REPLACED SEAL BRACKET FITTING AT L/W CONTROL RIB AFT POSITION; AS PER B737-7 SRM 51-40-02-0G-0.; [02] VERIFIED REPLACEMENT OF SEAL BRACKET FITTING AT L/W CONTROL RIB AFT POSITION.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 74,739 hrs · 44,231 cycles

MAIN CABIN CENTER WING BOX FLOOR SUPPORT BREAK CRACKED AT STA 540 AND RBL 1 ; / [01] REMOVED DAMAGED FLOOR SUPPORT BREAK AT MAIN CABIN CTR. WING STA. 540 & RBL 1; REF. : B737-7 SRM 51-40-02-0G-0.; [02] OK TO INSTALL FLOOR SUPPORT; [03] INSTALLED NEW PANEL SUPPORT BRAKE P/N : 143A5240-36;ISSUE TAG A05025; PO # 1617089. REF. : 51-40-02-0G-0.; [04] REF. : B737-700 SRM 51-40-02-0G-0.; [05] REMOVED SUPPORT BREAK IN STEP # 1 PART REMOVED P/N : 143AA5240; REF. : B737-7000 SRM 51-40-02-0G-0.; [06] REMOVED DAMAGED FLOOR SUPPORT BREAK AT MAIN CABIN CTR. WING STA. 540 & RBL 1; REF. : B737-7 SRM 51-40-02-0G-0INSTALLED NEW PANEL SUPPORT BRAKE P/N : 143A5240-36;ISSUE TAG A05025; PO # 1617089. REF. : 51-40-02-0G-0. .

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 74,739 hrs · 44,231 cycles

L2 DOOR EMERGENCY LIGHT LENS CRACKED ; / [01] REMOVED AND REPLACED L2 DOOR EMERGENCY LIGHT LENS AS PER BOEING AMM 33-51-01-960-801.; [02] CERTIFIED REMOVED AND REPLACED L2 DOOR EMERGENCY LIGHT LENS AS PER BOEING AMM 33-51-01-960-801; [03] VERIFIED

Part: BRACKET — CRACKED (BS 500C S25R) · airframe 74,739 hrs · 44,231 cycles

FWD CARGO COMPT RIGHT HAND STA 500C STR 25 BRACKET UNDER ZEE ANGLE CRACKED ; / [01] REMOVED DAMAGED CLIP BRACKET P/N 143A7502-14;AT FWD. CARGO COMPT. R/H STA. 500C S-25R;UNDER 'Z' ANGLE. REF. :: B737-700 SRM 51-40-02-0G-0.; [02] VERIFIED STEP 1; [03] INSTALLED BRACKET AT FWD CARGO COMPART. RH STA 500 C STRG 25 PERB737-700 SRM 51-40-02-0G-0; [04] REMOVED & REPLACED BRACKET AT FWD CARGO COMPT.;UNDER Z ANGLE;AS PER B737-700 SRM 51-40-02-0G-0.; [05] VERIFIED STEPS 3 & 4

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 74,739 hrs · 44,231 cycles

O/W EMERGENCY DOORS HEADER PANELS LIGHT LENS DAMAGED ; / [01] REPLACED O/W EMERGENCY DOORS HEADER PANELS LIGHTS LENS AS PER B737 AMM 33-51-01-960-801.; [02] VERIFIED; [03] REPLACED O/W EMERGENCY DOORS HEADER PANELS LIGHTS LENS AS PER B737 AMM 33-51-01-960-801.; [04] VERIFIED STEPS 1 & 3

Part: BRACKET — CRACKED (BS 500D S18L) · airframe 74,739 hrs · 44,231 cycles

FWD CARGO COMPT LEFT HAND STA 500D STR18 BRACKET CRACKED ; / [01] REMOVED CRACKED GUSSET BRACKET AT FWD. CARGO COMPT. L/H STA. 500D; S-18R; REF : B737-700 SRM 51-40-02-0G-0.; [02] RECEIVED NEW GUSSET BRACKET P/N : 143A9481-6; ISSUE TAG E26842; PO # 1698442.; [03] VERIFIED STEP 1; [04] OK TO INSTALL GUSSET; [05] INSTALLED NEW GUSSET BRACKET AT FWD. CARGO COMPT. L/H STA. 500D; S-18R;AS PER B737-700 SRM 51-40-02-0G-0.; [06] VERIFIED STEP 5; [07] STEP # 5;INSTALLATION REF. : PER BOEING DWG. 143A9481.

Part: ANGLE — CORRODED (BS 500D) · airframe 74,739 hrs · 44,231 cycles

CORROSION FWD CARGO COMP STA 500D FLOOR SUPPORT BETWEEN LEFT AND RIGHT ZEE ANGLE ; / [01] REMOVED SURFACE CORROSION AT FLOOR SUPPORT Z ANGLE ON FWD CARGO COMPONENT BETWEEN LEFT AND RIGHT REF B737-700 SRM 51-10-02-0G-0; [02] ORIG. MAT. : 0.071'; MAT. REMOVED : 0.003'; REMAINING MAT. : 0.068'.FOUND WITHIN LIMITS ASPER B737-700 SRM 53-30-08-1A-1; DETAIL C. TOOL USED : MICROMETER : B/C : 165542; DUE : 30-NOV.-2021.; [03] VERIIFIED STEPS 1 & 2; [04] OK TO TREAT; [05] TREATED AREAS AT FLOOR SUPPORT ZEE ANGLE REF B737-700 SRM 51-20-01-0G-0; [06] APPLICATION OF PRIMER & WHITE ENAMEL PRIMER OF ALL FWD. CARGO COMPT. FLOOR STRUCTURES WILL BE PERFORMED AT CARD 5330-E-16461-NG. TASK CARD : TTG8Q004FATS.; [07] VERIFIED STEP 5 & 6

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 74,739 hrs · 44,231 cycles

AFT CARGO COMPARTMENT FLOOR BOARD 140AF HAS PROMINENT BURRS AND EXCESSIVELY WORN. ; / [01] FABRICATED FLOOR PANEL 140AF AT AFT CARGO COMP AS PER B-737 AMM 25-52-01-201-801-NG; [02] CERTIFIED FABRICATION FLOOR PANEL #140AF; [03] FABRICATED FLOOR PANEL #140AF IWA B-737 AMM 25-52-01-201-801

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 74,739 hrs · 44,231 cycles

AFT CARGO COMPARTMENT FLOOR BOARD 140BF HAS PROMINENT BURRS AND EXCESSIVELY WORN. ; / [01] FABRICATED FLOOR PANEL 140BF AT AFT CARGO COMP AS PER B 737 REF AMM25-53-01-201-801-NG; [02] CERTIFIED FABRICATION FLOOR PANEL #140BF; [03] FABRICATED FLOOR PANEL #140BF IWA B-737 AMM-25-52-01-201-801

Part: HINGE — BROKEN (ACCESS DOOR) · airframe 74,702 hrs · 44,210 cycles

EXTERNAL POWER UNIT ACCESS DOOR LOWER HINGE BROKEN ; EXT POWER ACCES DOOR. LOWER HINGE BROKEN / REMOVED AND REPLACED EXTERNAL RECEPTACLE ACCESS DOOR LOWER HINGE PER AMM 51-49-02.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 74,631 hrs · 44,170 cycles

FWD ENTRY DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW / REMOVED AND REPLACED SIGN IAW AMM 33-51-01; INSPECTED

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 73,729 hrs · 43,650 cycles

EMERGENCY EXIT SIGN FELL OFF @ FWD ENTRY DOOR. / INSTALLED NEW EXIT SIGN COVER PER AMM 33-51-04.

Part: HANDLE — DETACHED (PAX DOOR ASSIST) · airframe 72,759 hrs · 43,054 cycles

MAIN ENTRY DOOR ASSIST HANDLE DETATCHED AT BOTTOM OF HANDLE. SECURED FWD ENTRY DOOR ASSIST HANDLE IAW CMM 52-11-00.

Part: DOOR — OUT OF ADJUST (L1 DOOR) · airframe 72,619 hrs · 42,967 cycles

L1 DOOR HARD TO CLOSE / ACCOMPLISHED ADJUSTMENT OF L1 DOOR PER AMM 52-11-00 OPERATION NO NORMAL.

Part: STIFFENER — CRACKED (RT WING) · airframe 72,362 hrs · 42,809 cycles

RIGHT WING T/E UPPER FIXED PANEL SUPPORT STIFFENER IS CRACKED / REMOVED AND REPLACED PANEL STIFFENER PER SRM 51-40-02

Part: COVER — LOOSE (EXIT SIGN) · airframe 72,214 hrs · 42,709 cycles

FORWARD GALLEY OVERHEAD EXIT SIGN COVER LOOSE. REPLACED LIGHT ASSEMBLY IAW AMM 33-51-03.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 70,688 hrs · 41,727 cycles

R/H OVERWING EXIT BATTERY FAILED CAPACITY CHECK. / R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,415 hrs · 41,556 cycles

EMERGENCY LIGHTS GROUND ILLUMINATION LIGHT L547 INOP. R&R M1670 BATTERY PACK PER AMM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,415 hrs · 41,556 cycles

EMERGENCY LIGHTS GROUND ILLUMINATION LIGHT L547 INOP. / R&R CHARGER PER AMM.

Part: CONTROL PANEL — INOPERATIVE (COCKPIT) · airframe 69,692 hrs · 41,060 cycles

AIR TURNBACK, #1 COMM RADIO WORKS ON GROUND, DURING CLIMB & CRUISE ITS INOP. R&R THE #1 RADIO TUNING PANEL PER AMM.

Part: AUDIO PANEL — INOPERATIVE (E&E BAY) · airframe 69,692 hrs · 41,060 cycles

AIR TURNBACK, #1 COMM RADIO WORKS ON GROUND, DURING CLIMB & CRUISE ITS INOP. R&R THE #1 AUDIO CONTROL PANEL PER AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,684 hrs · 41,054 cycles

AFT CARGO BILGE FLOOR SUPPORT CORRODED AT BS. 947, STR. 26R. R&R TRACK PER SRM.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 69,684 hrs · 41,054 cycles

FOUND CRACK ON UPPER SEAL PLATE AT LEFT HORIONTAL STAB.-TO-BODY FRONT SPAR / REMOVED AND REPLACED UPPER SEAL PLATE AT LEFT HORIZONTAL STAB. TO-BODY FRONT SPOR AS PER REF B737-700 AMM 53-31-31-400-801.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,684 hrs · 41,054 cycles

LH HORIZONTAL STABILIZER RIB #4 FAILED (NDT) ROTO INSPECTION FINDING A CRACK FROM FWD LOWER SECTION 15' ON AOPEN HOLE / REPAIRED L/H HORIZONTAL STABILIZER R/B #4 @ FWD LOWER SECTION @ OPEN ROLE 15' FROM FWD SPAIR AS PER B737-700 SRM 55-10-09-2R-5

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,684 hrs · 41,054 cycles

LT HORIZONTAL STABILIZER RIB #4 FAILED (NDT) ROTO INSPECTION FINDING A CRACK FROM FORWARD LOWER SECTION. REPAIRED RIB #4 PER EA.

Part: SUPPORT — CRACKED (LOWER EXT FUSELA) · airframe 69,684 hrs · 41,054 cycles

LEFT WING TO BODY FAIRING SUPPORT CRACKED AT STA 500D; S18L TO S-19L / REMOVED AND REPLACED / LEFT. WING BODY FAIRING SUPPORT AT STA 500D; S18L TO S-19L IN REF B737-700 SRM 51-40-05-0G-0; SRM 51-20-01-0G-0

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,684 hrs · 41,054 cycles

LT HORIZONTAL STAB INTERIOR RIB #4 CRACKED AT LOWER VERTICAL STIFFENER. REPAIRED RIB #4 PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,684 hrs · 41,054 cycles

SPLICE ANGLE CORRODED AT BS. 364, STR 28L. R&R STRINGER SPLICE PER SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,684 hrs · 41,054 cycles

FLOOR INTERCOSTAL WEB CORRODED AT BS. 351 STR 28L. R&R WEB PER SRM & DWG.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 69,684 hrs · 41,054 cycles

LOWER FUSELAGE INNER DOUBLER CORODED BETWEEN BS.360 TO BS. 384, STR 28. REPAIRED PER SRM, AMM, & DWG.

Part: NONE — CORRODED (AFT CARGO COMPT) · airframe 69,684 hrs · 41,054 cycles

AFT CARGO COMPMT. BILGE STRINGER SUPPORT BRACKET CORRODED AT STA 847 ; S-27L MKD DOT 60-028 / REMOVED AND REPLACE STRINGER CLIP AT AFT CARGO BILGYE STRINGER 27L STA 847 IAW B737-700 SRM 51-40-02-0G-0 AND DWG 146A1281 REV B

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,684 hrs · 41,054 cycles

AFT CARGO COMPARTMENT BILGE FLOOR SUPPORTS CORRODED AT FASTENER WHOLES BETWEEN BS. 887 TO BS. 947, S27L AND S26R. REPAIRED FLOOR SUPPORTS PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,684 hrs · 41,054 cycles

LT HORIZONTAL STABILIZER INTERIOR RIB #5 CRACKED AT STIFFENER LOWER AREA. REPAIRED #5 RIB PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,684 hrs · 41,054 cycles

LT HORIZONTAL STABILIZER INTERIOR RIB #4 CRACKED ALONG THE LOWER AREAS OF THE STIFFENERS. REPAIRED RIB PER SRM.

Part: PRESSURE WEB — CRACKED · airframe 69,684 hrs · 41,054 cycles

CRACK INDICATION FOUND [1 EA.] AT HORIZONTAL PRESSURE WEB STA 663 ON FWD EDGE OF STIFFENING BEAD AT LBL 30. APPROXIMATE CRACK LENGTH: 1.200'' / REMOVED FASTENERS TO ACCESS. REMOVED CORROSION AT AFT CARGO DOOR LOWER SILL WEB UPPER SURFACE. PERFORMED THICKNESS MEASURE. ORIGINAL THICKNESS 0.056' MINIMUS THICKNESS NOTED 0.061'; MATERIAL LOST 0.005' FOUND WITHIN LIMITS. TREATED AND PRIMED REWORKED AREA AND INSTALLED NEW FASTENERS. IAW B737 SRM 51-40-02-0G-0; 51-10-02-0G-0; 53-60-15-01-1 FIG 6; 53-60-15-1A-1 PG 2; 7 FIG 103 F NDTM 51-00-00

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 69,684 hrs · 41,054 cycles

HORIZONTAL PRESSURE WEB CRACKED AT BS. 663, ON FORWARD EDGE OF STIFFENING BEAD AT LBL 30. REPAIRED WEB IAW SRM.

Part: RETAINER — CRACKED (RT WING) · airframe 69,684 hrs · 41,054 cycles

RIGHT WING REAR SPAR T/E O/B SPOILER NO-7 FIXED T/E PANEL UP MID SEAL RETAINER BRACKET CRACKS MKD DOT60-007 / REPLACED BRACKET ON LOWER ATTACHED WEB AT RIGHT WING REAR SPAR T/E O/B SPOILER NO.7 FIXED T/E PANEL THE INSTALLATION WILL BE ACCOMPLISHED ON N/ W104890 6000/0005/

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 69,684 hrs · 41,054 cycles

RIGHT WING REAR SPAR BETWEEN SPOILER # 7 & 8 T/E FIXED PANEL LWR ATTACHED WEB CRACKS AT FASTENER TAIL O/B END MKD DOT 60-009 / REMOVED AND INSTALLED AT R/W REAR SPAR BETWEEN SPOILER #7 & #8 T/E FIXED PNL LWR ATTACHED ANGLE AS PER 737-700 SRM 51-40-02-0G-0 SECT #4; A& B; & C;D&E AND REF DRW #115-A2156; REV.D

Part: SUPPORT ANGLE — CORRODED (RT WING) · airframe 69,684 hrs · 41,054 cycles

SUPPORT ANGLE AT RT WING REAR SPAR T/E LOWER PANEL CORRODED AT FASTENER HOLES. R&R RIGHT WING REAR SPAR T/E LOWER PANEL SUPPORT ANGLE PER SRM.

Part: HMU — FAULTY (NR 2 ENGINE) · airframe 69,088 hrs · 40,688 cycles

NR 2 ENGINE GAVE NORMAL INDICATIONS UNTIL ADDING POWER ABOVE 85%. ENGINE DID NOT GO MORE THAN 85%, BUT MATCHED ENGINE #1 IN ALL INDICATIONS WITH N1 RPM MATCHING. AIR TURNBACK THE DIFFERENCE BETWEEN THROTTLE POSITION AND ACTUAL N1 DECREASED AS WE CLIMBED. BEFORE LANDING AT 4000FT. MSL THE SAME ISSUE RETURNED. R&R HYDRO MECHANICAL UNIT IAW MM.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 69,088 hrs · 40,688 cycles

NR 2 ENGINE GAVE NORMAL INDICATIONS UNTIL ADDING POWER ABOVE 85%. ENGINE DID NOT GO MORE THAN 85%, BUT MATCHED ENGINE #1 IN ALL INDICATIONS WITH N1 RPM MATCHING. AIR TURNBACK. THE DIFFERENCE BETWEEN THROTTLE POSITION AND ACTUAL N1 DECREASED AS WE CLIMBED. BEFORE LANDING AT 4000FT. MSL THE SAME ISSUE RETURNED. R&R FUEL PUMP PACKAGE IAW MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 69,027 hrs · 40,653 cycles

1016 BULKHEAD WEB LAP SPLICE CRACKED AT BS 1016, STR 23L. REPAIRED WEB PER EA.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 69,027 hrs · 40,653 cycles

BULKHEAD WEB LAP SPLICE CRACKED AT BS 1016, STR 23R. REPAIRED WEB PER EA.

Part: BRACKET — CRACKED (WHEEL WELL LH) · airframe 69,027 hrs · 40,653 cycles

LH WHEEL WELL - BS 663 BULKHEAD U-SHAPE FITTING COMMON TO LH RAM AIR EXHAUST HOUSING IS CRACKED. / REMOVED AND REPLACED BRACKET PER SRM 51-40-02.

Part: RETAINER — CRACKED (LEFT WING) · airframe 69,027 hrs · 40,653 cycles

LT WING SEAL RETAINER CRACKED UPPER SHELF PANEL I/B OF DEFECTION RIB FWD SIDE / REMOVED AND REPLACED RETAINER PER SRM 51-40-02

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,027 hrs · 40,653 cycles

FORWARD ENTRY DOOR FUSELAGE EMERGENCY LIGHT INOP. R&R BULB IAW AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 68,792 hrs · 40,496 cycles

L1 DOOR SLIDE GIRT FLAP HANGING OUT OF SLIDE COVER DRAGGING ON THE FLOOR. R&R SLIDE PER MT.

Part: MODULE — FAULTY (COCKPIT) · airframe 68,705 hrs · 40,441 cycles

ON CLIMB OUT WHEN PLACING THE LANDING GEAR LEVER TO THE OFF POSITION. ALL GREEN AND RED LANDING GEAR INDICATOR LIGHTS ILLUMINATED STANDBY AND IT SOUNDED AS IF NOSE GEAR DOOR OPENED. PLACED HANDLE BACK UP AND LIGHTS EXTINGUISHED. R&R LANDING GEAR CONTROL LEVER MODULE PER AMM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,426 hrs · 40,264 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD (OUTER) FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,426 hrs · 40,264 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD (OUTER) FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,426 hrs · 40,264 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD (OUTER) FACE CORRODED. REPAIRED FITTING PER EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 68,426 hrs · 40,264 cycles

RT WING AFT OUTBOARD FLAP UPPER SKIN DELAMINATED. REPAIRED AFT FLAP PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,426 hrs · 40,264 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING-UPPER OUTBOARD (OUTER) FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG WW) · airframe 68,426 hrs · 40,264 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING BLOWER OUTBOARD (OUTER) FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,426 hrs · 40,264 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING ON LOWER OUTBOARD (OUTER) FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,426 hrs · 40,264 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING-UPPER OUTBOARD (OUTER) FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,426 hrs · 40,264 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING-UPPER INBOARD (OUTER) FACE CORRODED. REPAIRED FITTING PER EA.

Part: PRESSURE DECK — CRACKED (RT M LG WW) · airframe 68,058 hrs · 40,017 cycles

RT WHEEL WELL PRESSURE DECK CRACKED AT BS 663.75, BETWEEN RBL 38 TO RBL 40. REPAIRED DECK PER EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 67,922 hrs · 39,926 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 66,997 hrs · 39,361 cycles

EMERGENCY LIGHTS OVERWING FAILED CAPACITY CHECK. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 66,992 hrs · 39,358 cycles

LT AFT EMERGENCY BATTERY FAILED CAPACITY TEST. R&R BATTERY IAW MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 65,870 hrs · 38,622 cycles

L2 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: COVER — OUT OF ALIGNMENT (R2 DOOR SLIDE) · airframe 65,488 hrs · 38,382 cycles

R2 DOOR SLIDE COVER MISALIGNED. ALIGNED THE SLIDE COVER IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,365 hrs · 37,655 cycles

RIGHT EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 64,323 hrs · 37,626 cycles

FUSELAGE SKIN CORRODED BETWEEN BS 500 TO BS 500A. REPAIRED SKIN PER EA.

Part: SKIN — DAMAGED (UPPER FUSELAGE L) · airframe 64,004 hrs · 37,422 cycles

SUPPLEMENTAL INFORMATION: TRANSFERRED FROM LOG PAGE 0026722: INSPECTION FOUND DAMAGE TO SKIN AROUND RIVET MEASURING 0.045' DEEP BY 1/16' BY 1/16' WIDE AT STA 727 S-7L / REPAIRED SKIN DAMAGE AT BS 727 STR 7L PER ER 17-03880 REV IR AND EA 1-753-31647 REV IR

Part: LIGHT — BROKEN (CABIN) · airframe 63,761 hrs · 37,269 cycles

RT OVERWING EMERGENCY EXIT LIGHT BROKEN. R&R LIGHT ASSEMBLY PER AMM.

Part: LIGHT — WORN (CABIN) · airframe 63,587 hrs · 37,169 cycles

FORWARD EMERGENCY LIGHT STRIP WORN. R & R THE LIGHT STRIP IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,364 hrs · 37,022 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,364 hrs · 37,022 cycles

RT FORWARD BULLNOSE EMERGENCY EXIT AISLE LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,364 hrs · 37,022 cycles

R1 DOOR EMERGENCY EXIT SLIDE LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: PLATE — CRACKED (RT WING) · airframe 63,364 hrs · 37,022 cycles

RT WING LOWER TRAILING EDGE WIGGLE PLATE INBOARD OF NR 2 PYLON TIP CRACKED. R&R WIGGLE PLATE PER SRM.

Part: RETAINER — ELONGATED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

FAIRING FRAME AT BS 663; LBL 15; HOLES COMMON TO SEAL DOUBLER ARE ELONGATED BEYOND 0.250'. / REMOVED; MADE FAIRING FRAME FROM BAC 1506-4475-7075-73511 LOT# 1292805; ANODIZED; PRIMED AND INSTALLED PER SRM 51-40-02-0G-0 AND DWG# 149A7214.

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 63,364 hrs · 37,022 cycles

FCB; LH; BAFFLE BS 500B TO 500C IS CRACKED. / REMOVED AND REPLACED FCB; LH; BAFFLE BS 500B TO 500C IAW SRM 51-40-02

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 63,364 hrs · 37,022 cycles

FWD FLOOR BOARD 221GF FWD O/B CORNER TAB IS BROKEN OFF. / REPAIRED FWD FLOOR BOARD 221GF WITH FWD O/B CORNER TAB BROKEN OFF IAW SRM 53-00-50-2R-6. 92420U 01JUN17

Part: WEB — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

AFT CARGO BAY VERTICAL WEB CORRODED BETWEEN BS 794 TO BS 847, RBL 21. R&R WEB ASSEMBLY PER SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,364 hrs · 37,022 cycles

AFT CABIN FLOOR PANEL 241ABF HAS 2 DISBONDS ON LOWER SURFACE (MARKED). / REPAIRED DAMAGE ON AFT CABIN FLOOR PANEL 241 ABF IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-9. 56749U 02JUN17

Part: STRAP — ELONGATED (AFT CARGO COMPT) · airframe 63,364 hrs · 37,022 cycles

AFT CARGO BAY BS 794-827 STR 25R WL 160 STRAP HAS ELONGATED HOLES / REMOVED AND REPLACED STRAP ASSY 146A8128U1/NEW B.S. 794-827 STR 25R WL 160 PER SRM 51-10-02 SRM 51-40-02 SRM 51-40-05 DWG 146A8120

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 63,364 hrs · 37,022 cycles

FWD CABIN FLOOR PANEL 222CF HAS A SMALL CRACK ON LOWER SURFACE 1' FROM I/B EDGE AND 23.2' FROM FWD EDGE. / FWD CABIN FLOOR PANEL 222CF SMALL CRACK ON LOWER SURFACE 1' FROM I/B EDGE AND 23.2' FROM FWD EDGE REPAIRED IAW SRM 53-00-50-2R-2 REPAIR 2 20549U 05/31/17

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,364 hrs · 37,022 cycles

FWD CABIN FLOOR PANEL 221BF HAS DAMAGE AT AFT O/B CORNER. / FWD CABIN FLOOR PANEL 221BF WITH DAMAGE AT AFT O/B CORNER WAS REPAIRED IAW SRM 53-00-50-2R-9.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,364 hrs · 37,022 cycles

AFT CABIN FLOOR PANEL 242RF HAS DAMAGE ON I/B EDGE 2' FROM L/E. / REPAIRED AFT CABIN FLOOR PANEL 242RF WHICH HAD DAMAGE ON I/B EDGE 2' FROM L/E IAW SRM 53-00-50-2R-2. 56371U 05/31/17.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,364 hrs · 37,022 cycles

AFT CABIN FLOOR PANEL 242UF HAS AREAS OF DELAM AND BROKEN/MISSING INSERTS. / DAMAGED FLOOR PANEL 242UF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PAR 9

Part: PANEL — ELONGATED (RIGHT WING) · airframe 63,364 hrs · 37,022 cycles

RIGHT HAND WING TRAILING EDGE DEFLECTION RIB TO PANEL ATTACH BOLTS HAVE ELONGATED BOTH ATTACH HOLES. / REPAIRED RIGHT HAND WING T/E DEFLECTION RIB TO PANEL ATTACH TAB PER SRM 57-51-02-2R-1; SRM 57-51-02-2R-4 AND EA 1-A57-3523 REV -.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 63,364 hrs · 37,022 cycles

PANEL 193AR HAS DELAMINATION ON INNER SURFACE. / REPAIRED PANEL 193AR WITH DELAMINATION ON INNER SURFACE IAW SRM 51-70-05-2R-2. 92420U 13JUN17

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

FLOORBEAM UPPER SURFACE AROUND FASTENER HOLE CORRODED AT BS 967, RBL 28. REPAIRED FLOOR BEAM IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 14. R&R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 47. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SILL DRAIN — CORRODED (FSD THRESHOLD) · airframe 63,364 hrs · 37,022 cycles

***CORROSION*** ON FORWARD SERVICE DOOR MOP SILL B.S 3294-360. / REMOVED CORRISION IN A AREA OF 1'X X 1' X .020. IAW SRM 51-10-02-0G-0; FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-2. REMOVED & REPLACED MOPSILL IAW SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; SRM 51-40-02-0G-0. 88952U 6/1/17

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 14. R&R INTERCOSTAL IAW SRM.

Part: SILL DRAIN — CORRODED (ASD THRESHOLD) · airframe 63,364 hrs · 37,022 cycles

***CORROSION*** ON AFT SERVICE DOOR MOP SILL B.S. 950-1000 / REMOVED AND REPLACED AFT SERCVICE DOOR MOPSILL I.A.W BOEING DWG 147A8501 AND SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

FLOORBEAM UPPER SURFACE AROUND FASTENER HOLES CORRODED BETWEEN BS 986.5, BETWEEN RBL 40 TO RBL 47. REPAIRED FLOOR BEAM IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 35. R&R INTERCOSTAL IAW SRM.

Part: SILL DRAIN — CORRODED (FED THRESHOLD) · airframe 63,364 hrs · 37,022 cycles

***CORROSION*** ON FORWARD ENTRY DOOR MOP SILL B.S 320-350. / REMOVED CORROSION AT FWD ENTRY DOOR MOPSILL AT BS 320-350 MAX MATERIAL LOSS L=1.5' X W= 1.2 X D= 0.15' FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-1. LOCATED AND DRILLED NEW MOPSILL PN #7530251 IAW SRM 51-40-05. INSTALLED IAW SRM 51-40-02 88324U 1JUN17

Part: BEAM — CRACKED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

R1 DOOR CUT OUT FORWARD LOWER STUB BEAM CRACKED AT BS 295, WL 209, LOWER CORNER. REPAIRED STUB BEAM PER ER & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

FLOORBEAM UPPER SURFACE AROUND FASTENER HOLE CORRODED AT BS 328, LBL 35. R&R FLOORBEAM IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294.5, BL 0. R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

FLOORBEAM UPPER SURFACE AROUND FASTENER HOLE CORRODED AT BS 328, LBL 25. R&R FLOORBEAM IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 747 TO BS 767, RBL 22. R&R INTERCOSTAL PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

AFT CARGO BAY CLIP CRACKED AT BS 807, RBL 20.5. R&R CLIP PER SRM & DWG.

Part: CHANNEL — CORRODED (AFT CARGO COMPT) · airframe 63,364 hrs · 37,022 cycles

***CORROSION*** ACB SIDEWALL SUPPORT CHANNEL B.S. 727D R/H RBL 23 HAS CORROSION / REMOVED AND REPLACED DAMAGED SIDEWALL SUPPORT CHANNEL AT BS 727D R/H PER SRM 51-40-02 AND DWG 146A9403

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED. R&R SUB-THRESHOLD IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

AFT CARGO BAY LAV PAN INTERCOSTAL CORRODED AT BS 847, LBL 25. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SKIN — CRACKED (LT WING) · airframe 63,364 hrs · 37,022 cycles

LT WING FAIRING 542BB INNER SKIN FORWARD OF A DRAIN HOLE CRACKED. REPAIRED SKIN PER EA.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,364 hrs · 37,022 cycles

***CORROSION*** ACB FLOOR STRAP 727D+4 RBL 23 - LBL22 HAS CORROSION / REPLACED ACB FLOOR SPLICE STRAP WITH NEW ONE 146A9401-8 WILL BE INSTALLED ON CUSTOMER CARD JPANEL-141-CLOSE AFT CARGO 56708U 6JUN17

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 847 TO BS 867, RBL 6. R&R INTERCOSTAL IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

AFT CARGO BAY BS 887 FLOOR STRAP CORRODED AT BS 887, BETWEEN LBL 13 TO RBL 16. R&R STRAP PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 440 TO BS 500D. R&R SUPPORT IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET PER SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

AFT CARGO BAY SHIELD CORRODED BETWEEN BS 767 TO BS 794, RBL 22. R&R SHIELD PER SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 794 TO BS 847, RBL 26. R&R SUB THRESHOLD ASSEMBLY PER SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 847 TO BS 867, LBL 23. R&R INTERCOSTAL PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

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

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, RBL 7. R&R INTERCOSTAL PER SRM & DWG.

Part: SHIELD — CORRODED (FWD CARGO RH) · airframe 63,364 hrs · 37,022 cycles

***CORROSION*** FCB; RIGHT HAND; BS 495 TO BS 500A; SHIELD CORRODED. / REMOVED AND REPLACED SHIELD ASSY IAW SRM 51-40-02 NO ALLOWABLE LIMITS GIVEN FOR THIS PART IN THE SRM. REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9

Part: FAIRING — CRACKED (TE FLAP) · airframe 63,364 hrs · 37,022 cycles

LT WING NR 6 FLAP TRACK FARING 642BB CRACKED JUST FORWARD OF TAIL CONE. REPAIRED FAIRING IAW ER AND EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,364 hrs · 37,022 cycles

AFT CARGO BAY SIDEWALL SUPPORT CHANNEL CORRODED AT BS 787, LBL 28. R&R CHANNEL PER SRM & DWG.

Part: FAIRING — CRACKED (LOWER EXT FUSELA) · airframe 63,364 hrs · 37,022 cycles

FAIRING PANEL 191FL IS CRACKED AT A FASTENER HOLE. / REPAIRED FAIRING PANEL 191FL WITH CRACK AT A FASTENER HOLE IAW SRM 57-70-05-2R-6; 92420U 13JUN17

Part: FAIRING — CRACKED (LOWER EXT FUSELA) · airframe 63,364 hrs · 37,022 cycles

FAIRING PANEL 191FL IS CRACKED AT A FASTENER HOLE. / REPAIRED FAIRING PANEL 191FL WITH CRACK AT A FASTENER HOLE IAW SRM 57-70-05-2R-6; 92420U 13JUN17

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,456 hrs · 35,896 cycles

RT OVERWING SIDEWALL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 60,569 hrs · 35,358 cycles

RIGHT EMERGENCY LIGHT LENS LOOSE BETWEEN BS 12 TO 20. R & R THE LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,494 hrs · 34,707 cycles

RIGHT EMER EXIT SIDEWALL LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,494 hrs · 34,707 cycles

ONE EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M01669. R & R BATTERY PACK IAW AMM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 57,942 hrs · 33,819 cycles

MID CABIN OVERHEAD EXIT SIGN LOOSE. SECURED LENS IAW MM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,663 hrs · 33,660 cycles

LEFT HORIZONTAL STABILIZER RIB AT STATION 92.7, CRACKED IN LOWER RADIUS, 29.0" FROM FRONT SPAR, LOCATION 3. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,663 hrs · 33,660 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STATION 92.7 CRACKED IN LOWER RADIUS, 29.0" AFT OF FRONT SPAR LOCATION 3. REPAIRED RIB IAW EA & SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,663 hrs · 33,660 cycles

RIGHT HORIZONTAL STABILIZER, RIB CRACKED IN LOWER RADIUS, 19.5" AFT OF FRONT SPAR AT STATION 92.7, LOCATION 2. REPAIRED RIB IAW SRM & EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,663 hrs · 33,660 cycles

LEFT HORIZONTAL STABILIZER RIB AT STATION 92.7, CRACKED AT LOWER RADIUS, 19.5" AFT OF FRONT SPAR, LOCATION 2. REPAIRED RIB IAW EA & SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,663 hrs · 33,660 cycles

LEFT HORIZONTAL STABILIZER RIB AT STATION 92.7 CRACKED IN LOWER RADIUS, 38.0" FROM FRONT SPAR LOCATION NR 4. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,663 hrs · 33,660 cycles

RIGHT HORIZONTAL STABILIZER, RIB CRACKED IN LOWER RADIUS, 38.25" AFT OF FRONT SPAR AT STATION 92.7, LOCATION 4. REPAIRED RIB IAW EA & SRM.

Part: STRINGER — CRACKED (RT WING) · airframe 57,663 hrs · 33,660 cycles

RIGHT WING FIXED LE STRINGER, CRACKED INBD OF NR 2 ENG PYLON. R & R STRINGER IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,663 hrs · 33,660 cycles

RIGHT HORIZONTAL STABILIZER, VERTICAL STIFFENER RIB CRACKED AT 92.70. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,663 hrs · 33,660 cycles

LEFT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT 92.70. REPAIRED RIB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,663 hrs · 33,660 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,663 hrs · 33,660 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,663 hrs · 33,660 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,663 hrs · 33,660 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,663 hrs · 33,660 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,663 hrs · 33,660 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,663 hrs · 33,660 cycles

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

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 57,663 hrs · 33,660 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,663 hrs · 33,660 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,663 hrs · 33,660 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,663 hrs · 33,660 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,663 hrs · 33,660 cycles

FUSELAGE FRAME CRACKED AT STATION 907, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,663 hrs · 33,660 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,663 hrs · 33,660 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 57,663 hrs · 33,660 cycles

LEFT WING NR 2 SLAT LE SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,663 hrs · 33,660 cycles

RIGHT WING NR 6 LE SLAT, SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED SLAT SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,663 hrs · 33,660 cycles

RIGHT WING NR 7 LE SLAT SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,663 hrs · 33,660 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 57,631 hrs · 33,640 cycles

EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1670. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 57,631 hrs · 33,640 cycles

EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1672. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 57,631 hrs · 33,640 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,630 hrs · 33,640 cycles

LEFT WING INBD FLAP DELAMINATED ON LOWER SKIN AT OTBD TE WEDGE. REPAIRED FLAP IAW EA.

Part: WEB — CRACKED (LT WING) · airframe 57,622 hrs · 33,635 cycles

LEFT WING TE UPPER FIXED PANEL WEB CRACKED INBD OF DEFLECTION CONTROL RIB. R & R WEB IAW SRM.

Part: LIGHT — MISSING (CABIN) · airframe 56,781 hrs · 33,177 cycles

RIGHT OVERWING EMER EXIT LIGHT MISSING. INSTALLED LIGHT IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 56,575 hrs · 33,061 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: LENS — LOOSE (CABIN) · airframe 56,427 hrs · 32,974 cycles

RIGHT OVERHEAD BIN EMER LIGHT LENS LOOSE AT ROW 3. SECURED LENS IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 55,368 hrs · 32,363 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: LIGHT — BROKEN (CABIN) · airframe 54,937 hrs · 32,103 cycles

L1 DOOR EMER EXIT LENS BASE BROKEN. R & R LIGHT IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,122 hrs · 31,625 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,122 hrs · 31,625 cycles

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

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 53,260 hrs · 31,125 cycles

DIVERSION, INFLIGHT SHUTDOWN & DECLARED EMERGENCY. NR 2 ENG OIL QTY DROPPED TO 0 PRESS. DROPPED & LOW OIL PRESS LIGHT CAME ON. OIL TEMP CLIMBED TO 120 DEGREES, SHUT DOWN ENG. R & R NR 2 ENG IAW MT.

Part: SIGN — BROKEN (CABIN) · airframe 52,498 hrs · 30,690 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. R & R SIGN IAW AMM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 52,381 hrs · 30,621 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.

Part: STRAP — CORRODED (FUSELAGE) · airframe 50,890 hrs · 29,765 cycles

AFT CARGO FLOOR SUPPORT STRAP CORRODED AT STATION 727D+6. REPAIRED STRAP IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 50,890 hrs · 29,765 cycles

AFT CARGO FLOOR SUPPORT STRAP CORRODED AT STATION 762. REPAIRED STRAP IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 50,890 hrs · 29,765 cycles

AFT CARGO FLOOR SUPPORT STRAP CORRODED AT STATION 887, BETWEEN RBL 13 TO LBL 13. REPAIRED STRAP IAW SRM.

Part: PANEL — CRACKED (R1 DOOR) · airframe 50,890 hrs · 29,765 cycles

R1 DOOR PANEL 844DZ FWD & AFT SUPPORT BRACKETS CRACKED. R&R PANEL IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,890 hrs · 29,765 cycles

RT WING NR 5 SLAT SKIN CRACKED AT FASTENER HOLE AT ACTUATOR ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: FITTING — LOOSE (EVAC SLIDE) · airframe 50,890 hrs · 29,765 cycles

R1 DOOR EMERGENCY EVAC SLIDE "S" CLIP LOOSE. SECURED CLIP IAW SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 50,890 hrs · 29,765 cycles

LT MLG WW FWD BULKHEAD CRACKED AT BS 663, LBL 30, BELOW WW CEILING. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (LT MLG WW) · airframe 50,890 hrs · 29,765 cycles

LT MLG WW VERTICAL WEB CRACKED AT BS 663, LBL 34. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,890 hrs · 29,765 cycles

LT WING NR 3 SLAT SKIN CRACKED AT FASTENER HOLE AT ACTUATOR ATTACHMENT POINT. REPAIRED SKIN IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,890 hrs · 29,765 cycles

LT NR 3 WINDOW FRAME NR 8 HOLE CRACKED. REPAIRED FRAME IAW SRM.

Part: PIN — LOOSE (EVAC SLIDE) · airframe 50,890 hrs · 29,765 cycles

R1 DOOR EMERGENCY EVAC SLIDE SAFETY PIN & BONDING JUMPER LOOSE. SECURED PIN & JUMPER IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 50,890 hrs · 29,765 cycles

LT EEPLS SIDEWALL LENS LOOSE. SECURED LENS IAW MM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 50,624 hrs · 29,616 cycles

R2 DOOR LOWER EXIT LEN BROKEN. R&R SIGN ASSEMBLY IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 48,600 hrs · 28,397 cycles

EMERGENCY EXIT LIGHT LENS LOOSE. REPLACED AFT RIGHT EMERGENCY EXIT LIGHT LENS REF M/M.

Part: RETAINER — CRACKED (RT WING) · airframe 48,600 hrs · 28,397 cycles

BULB SEAL RETAINER ON FIXED PANEL BETWEEN NR 5 AND 6 SPOILER IS CRACKED AT MOUNT BOLT HOLE. REMOVED AND REPLACED PER AMM.

Part: SLAT — CRACKED (RT WING) · airframe 48,600 hrs · 28,397 cycles

NR 8 SLAT ORIGINATING FROM A FASTENER HOLE CRACKED. REPLACED SLAT PER MM.

Part: FASTENER — DAMAGED (RT WING) · airframe 48,600 hrs · 28,397 cycles

THIRTEEN RIVETS ARE EITHER CRACKED OR THE HEADS ARE MISSING, RIGHT WING FIXED LEADING EDGE SKIN INBOARD OF NACELLE. REPLACED FASTENERS REF SRM 51-40-02.

Part: PANEL — CRACKED (RT WING) · airframe 48,600 hrs · 28,397 cycles

STRUCTURE BEHIND COVE SKIN OF RIGHT WING, ACCESSED VIA PANEL 621DB IS CRACKED. ACCOMPLISHED TIME LIMITED REPAIR REF EA: 1-757-7784.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 48,600 hrs · 28,397 cycles

RIGHT HORZ STAB LOWER SLIDER SEAL CRACKED. REMOVED AND REPLACED RIGHT LOWER SLIDER SEAL PER THE M/M.

Part: CAP — MISSING (L2 DOOR) · airframe 47,490 hrs · 27,700 cycles

L2 DOOR EMERGENCY EVAC SLIDE COVER BUMPER AFT ENDCAP MISSING. REMOVED AND REPLACED END CAP IAW SRM AND MT.

Part: ACTUATOR — BYPASSING (SPOILER) · airframe 45,018 hrs · 26,250 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING NR 3 FLIGHT SPOILER BYPASSING AND CHATTERING WHEN AILERONS ROLLED LEFT INTERMITTANTLY. REMOVED AND REPLACED NR 3 FLIGHT SPOILER ACTUATOR PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,404 hrs · 25,901 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,404 hrs · 25,901 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,404 hrs · 25,901 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,404 hrs · 25,901 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,404 hrs · 25,901 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,404 hrs · 25,901 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 44,342 hrs · 25,863 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 44,342 hrs · 25,863 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 41,146 hrs · 23,988 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 39,696 hrs · 23,135 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR LOWER FWD BEAM CRACKED AT I/B MOUNT. REMOVED AND REPLACED DOOR PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 39,696 hrs · 23,135 cycles

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

Part: SKIN — DELAMINATED (LE SLAT) · airframe 39,696 hrs · 23,135 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 4 SLAT UPPER WEDGE SKIN DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,821 hrs · 21,997 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,821 hrs · 21,997 cycles

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

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 37,430 hrs · 21,761 cycles

DIVERSION / INFLIGHT SHUT DOWN / DECLARED EMERGENCY. FUEL CROSS FEED VALVE FAILED, SHUT DOWN NR 1 ENGINE INDICATIONS WERE NORMAL, DECLARED EMERGENCY, DIVERTED TO MCI. INSPECTED A/C FOR LEAKS, FOUND NONE. REMOVED AND REPLACED CROSS FEED ACTUATOR PER MM.

Part: VALVE — FAULTY (CENTER TANK) · airframe 37,407 hrs · 21,742 cycles

INFLIGHT SHUTDOWN / DIVERSION / DECLARED EMERGENCY. AT ALTITUDE HAD A FUEL IMBALANCE OCCUR. UNABLE TO CROSSFEED. FUEL PUMPS ALL TANKS WORKED NORMAL, ENGINE PARAMETERS NORMAL. PRECAUTIONARY SHUT DOWN NR 1 ENGINE PER QRH OF POSSIBLE FUEL LEAK. INSPECTED AND OPERATED WINGS, FOUND NO EVIDENCE OF FUEL LEAK. FOUND CROSSFEED VALVE TO BE INTERMITTENT. REMOVED AND REPLACED P5-2 FUEL CONTROL PANEL AND FUEL CROSSFEED VALVE ACTUATOR PER MM.

Part: LINE — FRAYED (CABIN) · airframe 37,333 hrs · 21,695 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT EMERGENCY ESCAPE HATCH STRAP FRAYED. REMOVED AND REPLACED LIFE LINE PER MM.

Part: LINE — FRAYED (CABIN) · airframe 37,333 hrs · 21,695 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT EMERGENCY ESCAPE HATCH STRAP FRAYED. REMOVED AND REPLACED LIFE LINE PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,333 hrs · 21,695 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 12. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,333 hrs · 21,695 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 17. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,333 hrs · 21,695 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 8. REPAIRED BEAM PER SWA EA.

Part: LENS — LOOSE (CABIN) · airframe 36,557 hrs · 21,213 cycles

DURING SCHEDULED CV CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 21. SECURED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 36,557 hrs · 21,213 cycles

DURING SCHEDULED CV CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 3. SECURED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 36,557 hrs · 21,213 cycles

DURING SCHEDULED CV CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 13. REMOVED AND REPLACED LENS PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,989 hrs · 20,849 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,989 hrs · 20,849 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 35,558 hrs · 20,576 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. INSTALLED SLIDE PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,428 hrs · 20,495 cycles

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

Part: STRIP — WORN (CABIN) · airframe 35,428 hrs · 20,495 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP WORN BETWEEN ROW 11 TO ROW 12. REMOVED AND REPLACED EEPLS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,983 hrs · 19,008 cycles

DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,983 hrs · 19,008 cycles

DURING SCHEDULED HC1 CHECK, LEFT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 29,642 hrs · 17,038 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 27,748 hrs · 15,914 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROW 1 ABC AND ROW 4 ABC. REMOVED AND REPLACED EEPLS PHOTOLUMINESCENT STRIP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,675 hrs · 14,710 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD CABIN RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: WINDOW — MISSING (L1 DOOR SLIDE) · airframe 24,234 hrs · 13,918 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR VIEWER WINDOW MISSING. INSTALLED VIEWER WINDOW PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,560 hrs · 11,307 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: ANGLE — CRACKED (LT WING) · airframe 18,807 hrs · 10,887 cycles

DURING SCHEDULED 5Y CHECK, FOUND LT WING SUPPORT ANGLE AT REAR SPAR PANEL BETWEEN SPOILER NR 5 AND SPOILER NR 6, CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 18,432 hrs · 10,664 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHTS FAILED LONG TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 18,303 hrs · 10,589 cycles

R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED R1 DOOR EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,689 hrs · 9,173 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 14,222 hrs · 8,377 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED (12 EA) THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 13,009 hrs · 7,715 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB NR 1 HINGE ATTACH POINT BOLT BUSHING PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 12,382 hrs · 7,376 cycles

DURING SCHEDULED A2 CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB NR 2 AND NR 3 HINGE ATTACH POINTS WORN. REMOVED AND REPLACED HARDWARE AND BUSHINGS AT NR 2 AND NR 3 HINGE ATTACH POINTS PER MM.

Part: BUSHING — WORN (ELEVATORS) · airframe 12,118 hrs · 7,209 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, BOTH LEFT AND RIGHT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH LEFT AND RT ELEVATOR TAB NR 1 HINGE BUSHINGS.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 11,606 hrs · 6,914 cycles

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

Part: LENS — MISSING (CABIN) · airframe 11,409 hrs · 6,808 cycles

FWD OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: HINGE — WORN (RT ELEVATOR) · airframe 11,311 hrs · 6,750 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB NR 1, NR 2, NR 3 AND NR 4 HINGES PER BOEING SB.

Part: HINGE — WORN (LT ELEVATOR) · airframe 11,311 hrs · 6,750 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB NR 2, NR 3 AND NR 4 HINGES PER BOEING SB.

Part: COVER — MISSING (CABIN) · airframe 11,056 hrs · 6,612 cycles

EEPLS COVER MISSING IN CABIN. INSTALLED COVER PER MM.

Part: CAP — LOOSE (CABIN) · airframe 9,391 hrs · 5,641 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LOOSE AT ROW NR 1. REMOVED AND REPLACED END CAP AND SECURED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 9,191 hrs · 5,517 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — MISSING (CABIN) · airframe 7,074 hrs · 4,240 cycles

EEPLS COVER MISSING AT ROW 1. INSTALLED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 6,852 hrs · 4,107 cycles

EEPLS COVER CRACKED. R&R COVER PER MM.

Part: COVER — BROKEN (CABIN) · airframe 6,383 hrs · 3,829 cycles

EEPLS COVER BROKEN AT FWD CABIN. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 6,371 hrs · 3,822 cycles

EEPLS LIGHT COVER BROKEN AND WIRES EXPOSED AT FWD CABIN. REMOVED AND REPLACED EEPLS COVER AND SECURED EEPLS WIRES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,034 hrs · 3,639 cycles

EEPLS INOP AT FWD SECTION. REPAIRED EEPLS PER MM.

Part: COVER — MISSING (CABIN FLOOR) · airframe 4,397 hrs · 2,632 cycles

EEPLS COVER MISSING. INSTALLED TRACK COVER PER MM.