N752SW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2018-12-06 – 2018-12-06 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2018-12-06 – 2018-12-06 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AFT ENTRY DOOR SLIDE DEPLOY HANDLE NOT COVERED.<[01] REPOSITIONED SLIDE; DEPLOY HANDLE NOW COVERED PER MT 725-61-06.
L2 DOOR SLIDE FELL OUT OF CONTAINER<[01] ADJUSTED GIRT BAR REF AMM 25-66-01. SLIDE PACKED PROPERLY GIRT BAR STRAPS NEEDED ADJUSTMENT. AIRCRAFT OK FOR SERVICE.
AFT EXIT DOOR SLIDE NEEDS ADJUSTING<[01] SECURED GIRT BAR PER M/M 25-66-00.
SLIDE LOOSE ON RIGHT AFT SERVICE DOOR<[01] INSPECTED SLIDE ON A/C LEFT HAND SIDE NO DEFECTS NOTED PER AMM 25-66-01
BIRD STRIKE ON DEPARTURE LEFT ENGINE ;VIBRATION PEAKED AROUND 6 UNITS ; NO UNUSUAL SMELLS; VIBRATION DECREASED TO AROUND 3.5 UNITS WITH REDUCTION IN POWER. REMOVED AND REPLACED THE #1 ENGINE COMPLETE FAN BLADE SET INCLUDING ALL ELASTOMERS, SHIMS, AND PLATFORMS PER AMM 72-21-02. R&R #1 ENGINE COMPLETE SET OF FAN BLADES AND PLATFORMS PER MT 772-21-20. REPLACED #1 ENGINE ALL ELASTOMERS; SHIMS AND PLATFORMS PER AMM 72-21-02.
4 CABIN EMERGENCY BATTERIES PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT POSITIONS M10672, M10673, M10668, M10675 IAW AMM 33-51-06.
4 CABIN EMERGENCY BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT POSITIONS M10672, M10673, M10668. M10675 IAW AMM 33-51-06
4 CABIN EMERGENCY BATTERIES PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT POSITIONS M10672, M10673, M10668, M10675 IAW AMM 33-51-06.
4 CABIN EMERGENCY BATTERIES PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT POSITIONS M10672, M10673, M10668, M10675 IAW AMM 33-51-06
RIGHT HORIZONTAL STABILIZER UPPER AFT SLIDING SEAL FWD RETAINER DAMAGED. REMOVED AND REPLACED THE SLIDING SEAL IAW AMM 53-31-31 AND FWD TRACK IAW AMM 25-50-11.
LEFT NOSE WHEEL TREAD RECAP CAME LOOSE ON TAKEOFF AND DEPARTED THE AIRCRAFT. LANDED AT LAX WITH A SMOOTH TOUCHDOWN AND GENTLE BRAKING. AIRCRAFT DID NOT LAND OVERWEIGHT. / [01] REMOVED/ REPLACED LH NOSE WHEEL ASSEMBLY PER AMM 32-45-21.;[02] R&R'ED NOSE LANDING GEAR POSITION 2 (B) TIRE PER AMM 32-45-21; TIRE PRESSURE NORMAL.
LEFT NOSE WHEEL TREAD RECAP CAME LOOSE ON TAKEOFF AND DEPARTED THE AIRCRAFT. LANDED AT LAX WITH A SMOOTH TOUCHDOWN AND GENTLE BRAKING. AIRCRAFT DID NOT LAND OVERWEIGHT. / [01] REMOVED/ REPLACED LH NOSE WHEEL ASSEMBLY PER AMM 32-45-21.;[02] R&R'ED NOSE LANDING GEAR POSITION 2 (B) TIRE PER AMM 32-45-21; TIRE PRESSURE NORMAL.
POSIBLE CRACK IN AFT. LOWER DOOR STOP FITTING ON THE FWD. SERVICE DOOR. / [01] PERFORMED NDTM PART 6 51-00-00 PROCEDURE 23. FOUND PART TO BE CRACKED;[02] REMOVED AND REPLACED GALLEY SERVICE DOOR IAW 737 AMM 52-41-00
FORWARD ENTRY DOOR SLIDE HAS YELLOW CAUTION FLAP EXPOSED / [01] PLACED VELCRO COVER BACK OVER L1 DOOR ESCAPE SLIDE HANDLE PER SIP
FWD ENTRY DOOR EMERGENCY LIGHT LENS COVER LOOSE / [01] SECURED WITH TAPE. OK TO CONTINUE ON TLD PER EA M-21-133-00720.
FWD SERVICE DOOR HAS A LOOSE STRAP / [01] REMOVED FWD SVC DOOR ESCAPE SLIDE ASSY; ADJUSTED SLIDE MATERIAL FOR GIRT BAR ; INSTALLED SLIDE ASSY IAWMM 25-66-01
LOWER EXIT PLACARD AT FORWARD ENTRY DOOR LOOSE / [01] RESECURED LOWER EXIT SIGN COVER @ FWD ENTRY DOOR PER SIP
ROWS 8 THRU 11 DEF OVERHEAD BIN EMERGENCY LIGHTS INOP / [01] REPLACED BATTERY CHARGER AND PACK PER AMM 33-51-06. OPS GOOD.
ROWS 8 THRU 11 DEF OVERHEAD BIN EMERGENCY LIGHTS INOP / [01] REPLACED BATTERY CHARGER AND PACK PER AMM 33-51-06. OPS GOOD.
FWD ENTRY SLIDE NOT SEATED PROPERLY ON GIRT BAR ; / [01] REMOVED AND REPLACED GIRT BAR FASTENERS PER SRM 51-40-02-0G-0
SUPPLEMENTAL INFORMATION: LEFT WING TO BODY FAIRINGS 191AL-191FL; SUPPORT ASSEMBLY CRACKED ; / [01] R&R LEFT WING TO BODY FAIRINGS 191AL-191FL; SUPPORT ASSEMBLY PER SRM 51-10-02 & SRM 51-40-02.
CRACK SLAT 6 ON COVE CHORD (ANGLE) STA 202.45 MORE 4.5 INCH AT RT WING ; 2021-319881 / [01] REMOVED COVE CHORD (ANGLE) LOC ON SLAT 6 IAW SRM B737-700 51-40-02; [02] REMOVED COVE CHORD (ANGLE) LOC ON SLAT 6 IAW SRM B737-700 51-40-02; [03] REPLACED COVE CHORD ANGLE P/N : 114A8331-2 AND FASTENERS LOC. ON SLAT #6; BETWEEN STA 144.4500 AND STA 260.4500; RT WING. IAW B737-700 SRM 51-40-02 AND DWG 114A5030 REV: A AND IAW B737-700 SRM 51-10-02 PARAGRAPH 9. TOOL USED CALIPER P/N: 700-113-10; S/N :0019306; DUE DATE: 14-OCT-21; [04] REPLACED COVE CHORD ANGLE P/N : 114A8331-2 AND FASTENERS LOC. ON SLAT #6; BETWEEN STA 144.4500 AND STA 260.4500; RT WING. IAW B737-700 SRM 51-40-02 AND DWG 114A5030 REV: A AND IAW B737-700 SRM 51-10-02 PARAGRAPH 9. TOOL USED CALIPER P/N: 700-113-10; S/N :0019306; DUE DATE: 14-OCT-21 VERIFIED AS RII
CRACK ANGLE - SUPPORT LOCATED BS 400 AFT FACE STRINGER 26L FWD CARGO COMPARTMENT ; 2021-319856 / [01] REPLACED ANGLE - SUPPORT LOCATED BS 400 AFT FACE STRINGER 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 DWG 143A7505 REV.B PN USED 143A7502U155 PO 2020 212944; [02] CERTIFIED RII WORK PERFORMED.
CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727E AND BS 807 S-25L AT WL 156 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727E AND BS 807 S-25L AT WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DRAWING # 146A7502 REV A.
CORROSION SUPPORT ZEE LOACTED BETWEEN BS 767 AND BS 727 S-25R AT WL 156 AT AFT CARGO COMPARTMENT ; 2021-319853 / [01] TOOL USED P/N DIGITAL 150;S/N AE-412602;CAL DUE DATE 31 MAY-2022; [02] REPLACED SUPPORT ZEE LOACTED BETWEEN BS 727 AND BS 767 S-25R AT WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DWG 146A7500 SHEET 26 REV A; [03] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 AND BS 767 S-25R AT WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DWG 146A7500 SHEET 26 REV A; [04] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 AND BS 767 S-25R AT WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DWG 146A7500 SHEET 26 REV A. RII
CRACK SUPPORT ZEE LOCATED BS 400 AND BS 420 AND S-26R AT FWD CARGO COMPARTMENT ; 2021-319855 / [01] TOOL USED: DIGITAL 150 S/N: AE-412602 DUE DATE: 31-MAY-22; [02] REPLACED SUPPORT ZEE LOCATED BS 400 AND BS 420 AND STR 26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND SRM 53-30-53-0L-2 FIGURE 2 ITEM 1 TABLE 2 DWG 143A7500 REV. A MATERIAL USED BAC 1496-444 PO 2020 185898; [03] REPLACED SUPPORT ZEE LOCATED BS 400 AND BS 420 AND STR 26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND SRM 53-30-53-0L-2 FIGURE 2 ITEM 1 TABLE 2 DWG 143A7500 REV. A MATERIAL USED BAC 1496-444 PO 2020 185898<BR>RII
CRACK FRONT SPAR SUPPORT ANGLE LOCATED AT IFSS 120 AND WBL 94.24 AT RT WING ; 2021-319839 / [01] REPLACED FRONT SPAR SUPPORT ANGLE LOCATED AT IFSS 120 AND WBL 94.24 AT RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND B737-700 SRM 51-40-02 AND DWG # 116A3001 REV: --; [02] REPLACED FRONT SPAR SUPPORT ANGLE LOCATED AT IFSS 120 AND WBL 94.24 AT RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND B737-700 SRM 51-40-02 AND DWG # 116A3001 REV: --<BR>RII INSPECTION DONE.
CRACK LEADING EDGE RIB AT LEADING EDGE STATION 86.66 AT LT HORIZONTAL STABILIZER ; 2021-319790 / [01] REPLACED RIB LOC LEADING EDGE STA 86.66 AT LT HORIZONTAL STABILIZER . I.A.W B737-700 SRM 51-10-02 ;SRM 51-40-02 AND DWG 186A1001 REV B.; [02] REPLACED RIB LOC LEADING EDGE STA 86.66 AT LT HORIZONTAL STABILIZER . I.A.W B737-700 SRM 51-10-02 ;SRM 51-40-02 AND DWG 186A1001 REV B.
CRACK LEADING EDGE RIB AT LEADING EDGE STATION 95.96 AT LT HORIZONTAL STABILIZER ; 2021-319791 / [01] TOOL USED CALIPER PN: DIGITAL 150 SN: AE 412599 DUE DATE 21-MAY 22; [02] REPLACED LEADING EDGE RIB AT LEADING EDGE STATION 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 DWG 186A1303 REV.A SRM 51-10-02 ITEM 9 AND SRM 51-40-02 P/N USED 186A1352-5 PO 2021-172982; [03] REPLACED LEADING EDGE RIB AT LEADING EDGE STATION 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 DWG 186A1303 REV.A SRM 51-10-02 ITEM 9 AND SRM 51-40-02 P/N USED 186A1352-5 PO 2021-172982
CRACK LEADING EDGE RIB AT LEADING EDGE STATION 105.25 AT LT HORIZONTAL STABILIZER ; 2021-319441 / [01] TOOL USED CALIPER PN: DIGITAL 150 SN: AE 412599 DUE DATE 21-MAY 22; [02] REPLACED LEADING EDGE RIB AT LEADING EDGE STATION 105.25 AT LT HORIZONTAL STABILIZER IAW B737-700 DWG 186A1001 REV. A SRM 51-10-02 AND SRM 51-10-02 ITEM 9 P/N USED 186A1304-1 PO 2021-172657; [03] REPLACED LEADING EDGE RIB AT LEADING EDGE STATION 105.25 AT LT HORIZONTAL STABILIZER IAW B737-700 DWG 186A1001 REV. A SRM 51-10-02 AND SRM 51-10-02 ITEM 9 P/N USED 186A1304-1 PO 2021-172657
CRACK CLOSURE ANGLE LOCATED BETWEEN BS1088 TO BS1121 RH SIDE AT UPPER FUSELAGE ; 2021-319799 / [01] TOOL USED PN: NORTEC 600D; SN: 210138503; CAL DUE DATE: 05-MAR-22; [02] PRECISION RADIUS P/N: 2204A3 S/N:AE-408651 DUE DATE: 02-FEB-22; [03] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22.; [04] REPAIRED CLOSURE ANGLE LOCATED BETWEEN BS1088 TO BS1121 RH SIDE AT UPPER FUSELAGE IAW B737-700 SRM 53-80-71-2R-6 REPAIR 6 MATERIAL USED 2024-T0 0.063 P.O. 2021-138368 REPAIR ANGLE (1 E/A) 2024T0/0.063 HEAT TREATED AND CONVERTED FROM 2024T0 TO 2024T42 IAW BAC5602; TABLE IV; TABLE X. TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22.; [05] REPAIRED CLOSURE ANGLE LOCATED BETWEEN BS1088 TO BS1121 RH SIDE AT UPPER FUSELAGE IAW B737-700 SRM 53-80-71-2R-6 REPAIR 6 MATERIAL USED 2024-T0 0.063 P.O. 2021-138368 REPAIR ANGLE (1 E/A) 2024T0/0.063 HEAT TREATED AND CONVERTED FROM 2024T0 TO 2024T42 IAW BAC5602; TABLE IV; TABLE X. TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22.AS RII.
CRACK ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 276 LT WING ; 2021-319810 / [01] REPLACED ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 276LT WING IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG 115A62 REV : A; [02] REPLACED ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 276LT WING IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG 115A6200 REV : A
CRACK ANGLE - SUPPORT LOCATED ON BS807 AND RBL 19 APPROX. AFT CARGO COMPARTMENT ; 2021-319750 / [01] REPLACED ANGLE-SUPPORT LOCATED ON BS807 AND RBL19 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ;51-10-02 AND DWG # 146A8120 REV A ;146A0081 REV C; [02] REPLACED ANGLE-SUPPORT LOCATED ON BS807 AND RBL19 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ;51-10-02 AND DWG # 146A8120 REV A ;146A0081 REV C AND TOOL USED: CALIPER 0-6; P/N: 700-113-10; S/N: 0019289; DUE DATE: 25-MAR-22; [03] REPLACED ANGLE-SUPPORT LOCATED ON BS807 AND RBL 19 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ;51-10-02 AND DWG # 146A8120 REV A ;146A0081 REV C AND TOOL USED: CALIPER 0-6; P/N: 700-113-10; S/N: 0019289; DUE DATE: 25-MAR-22<BR>RII ACCOMPLISHED
CRACK STIFFENER FLOOR STRUCTURE BS 540 AND BL0 TO RBL 24.5 CENTER SECTION ; 2021-319751 / [01] TOOL USED P/N: 500-197-20 S/N: 12141486 DUE DATE: 31-JAN-21; [02] REPLACED STIFFENER FLOOR STRUCTURE BS 540 AND BL0 TO RBL 24.5 CENTER SECTION I.A.W B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02-0G-0 AND DWG:143A0060 REV B; [03] REPLACED STIFFENER FLOOR STRUCTURE BS 540 AND BL0 TO RBL 24.5 CENTER SECTION I.A.W B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02-0G-0 AND DWG:143A0060 REV B<BR>RII
CRACK STRINGER 26L LOCATED BS 540 FWD CARGO COMPARTMENT ; 2021-319732 / [01] TOOL USED: UT EQUIPMENT P/N: 45MG; S/N: 130060401; DUE DATE: 22/APR/22; [02] TOOL USED P/N:NORTEC 500D; S/N:N500X1693P030456; CAL DUE DATE:30-NOV-21; [03] TOOL USED RADIUS GAUGE P/N S167C S/N AE-35943 CAL DUE DATE: 04 JAN 22.; [04] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE.; [05] REPAIRED STRINGER 26L LOCATED BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R 1 REPAIR 1 MATERIAL USED 7075-0.045 PO 2021 134008 AND 7075-T0-0.040 PO 2021 109926 STRINGER SECTION;CHANNEL AND REPAIR ANGLES (2EA) MATERIAL 7075-T0/0.040*/0.045* HEAT TREATED AND CONVERTED FROM 7075-T0 TO CONDITION T6 IAW BAC5602 TABLE IV PAGE 22 AND TABLE X PAGE 33. TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22; [06] TASK CARD COMPLETED. RII
CRACK STRINGER 24R LOCATED BS540 FWD CARGO COMPARTMENT ; 2021-319734 / [01] TOOL USED: P/N: 35 DL; S/N: 091419910; DUE DATE: 30-NOV-21.; [02] TOOL USED P/N: NORTEC 500D; S/N: N500X11290U021704; DUE DATE: 08-OCT-21; [03] TOOL USED : RADIUS GAUGE PN: S167C; SN: AE-27309 DUE DATE 05-AUG-21.; [04] PERFORMED PERMANENT REPAIR ON STR 24R LOCATED BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED 7075-T6.045 PO# 2021 152098 AND 7075-T6-0.050; PO# 2921 139514; [05] PERFORMED PERMANENT REPAIR ON STR 24R LOCATED BS 500D BTW BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED 7075-T6.045 PO# 2021 152098 AND 7075-T6-0.050; PO# 2921 139514; [06] PERFORMED PERMANENT REPAIR ON STR 24R LOCATED BS 500D BTW BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED 7075-T6.045 PO# 2021 152098 AND 7075-T6-0.050; PO# 2921 139514 <BR>RII INSPECTION DONE.
CRACK TIE CLIP LOCATED AT BS 277 LEVEL STR 10R AT PASSENGER CABIN ; 2021-319725 / [01] REPLACED TIE CLIP LOC. BS 277 AT LEVEL STRINGER 10R AT PASSENGER CABIN. IAW B737-700; SRM 51-10-02; SRM 51-40-02 AND DWG #141A1110 SHEET 18 REV -.; [02] TASK COMPLETED; VERIFIED AS RII.<BR><BR>INSTALLED NEW TIE CLIP AND FASTENERS LOC. BS 277 LEVEL STRINGER 10R AT PASSENGER CABIN. IAW B737-700; SRM 51-40-02 AND DWG #141A1110 SHEET 18 REV -.
CRACK STRINGER 25R LOCATED BS540 FWD CARGO COMPARTMENT ; 2021-319735 / [01] TOOL USED PN: 45MG; SN: 130064101; DUE DATE: 11 MAR 22.; [02] TOOL USED P/N: NORTEC 500D; S/N: N500X12101V022240; DUE DATE: 01-DEC-21.; [03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22.; [04] PERFORMED PERMANENT REPAIR ON STR 25R LOCATED BTW BS 500C TO BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 MATERIAL USED 7075-T6.036 PO# 2021 131796 AND 7075-T6-0.040; PO# 2921 108926; [05] PERFORMED PERMANENT REPAIR ON STR 25R LOCATED BTW BS 500C TO BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 MATERIAL USED 7075-T6.036 PO# 2021 131796 AND 7075-T6-0.040; PO# 2921 108926 <BR>RII INSPECTION DONE.
CRACK STRINGER 26R LOCATED BS540 FWD CARGO COMPARTMENT ; 2021-319736 / [01] TOOL USED: P/N: 35 DL; S/N: 091419910; DUE DATE: 30-NOV-21.; [02] TOOL USED P/N: NORTEC 500D; S/N: N500X11290U021704; DUE DATE: 08-OCT-21; [03] PERFORMED PERMANENT REPAIR ON STR 26R LOCATED BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED 7075-T6.045 PO# 2021 152098 AND 7075-T6-0.050; PO# 2921 139514; [04] PERFORMED PERMANENT REPAIR ON STR 26R LOCATED BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED 7075-T6.045 PO# 2021 152098 AND 7075-T6-0.050; PO# 2921 139514<BR>RII
CRACK STRINGER 27R LOCATED BS540 FWD CARGO COMPARTMENT ; 2021-319737 / [01] TOOL USED PN: 45MG; SN: 130064101; DUE DATE: 11 MAR 22.; [02] TOOL USED: P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 24-FEB-22; [03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22; [04] REPAIRED STRINGER 27R LOCATED BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; MATERIAL USED : STRINGER SECTION 7075/0.056/T0 PO# 2021 127971 ; CHANNEL(1E/A);ANGLE (2E/A) 7075/0.063/T0; PO# 2021 120486 STRINGER SECTION;CHANNEL AND REPAIR ANGLES (2EA) MATERIAL 7075-T0/0.056*/0.063* HEAT TREATED AND CONVERTED FROM 7075-T0 TO CONDITION T6 IAW BAC5602 TABLE IV PAGE 22 AND TABLE X PAGE 33. TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22; [05] TASK CARD COMPLETED. RII
CRACK STRINGER 24L LOCATED BS540 FWD CARGO COMPARTMENT ; 2021-319729 / [01] TOOL USED: UT EQUIPMENT P/N: 45MG; S/N: 130060401; DUE DATE: 22/APR/22; [02] TOOL USED P/N:NORTEC 500D; S/N:N500X1693P030456; CAL DUE DATE:30-NOV-21; [03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22; [04] REPAIRED STRINGER 24L LOCATED BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R 1 REPAIR 1 MATERIAL USED 7075-0.045 PO 2021 152098 STRINGER SECTION;CHANNEL AND REPAIR ANGLES (2EA) MATERIAL 7075-T0/0.045*/0.050* HEAT TREATED AND CONVERTED FROM 7075-T0 TO CONDITION T6 IAW BAC 5602 TABLE IV PAGE 22 AND TABLE X PAGE 33. TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22; [05] TASK CARD COMPLETED. RII
CRACK FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT ; 2021-319615 / [01] FABRICATED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 STEP 1 (C) (F) DWG 453A2310 SHEET 4 REV C. MATERIAL USED A90RG1W 48144 PO 2021-152338.; [02] CERTIFIED WORK PERFORMED.
CRACK FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT ; 2021-319616 / [01] FABRICATED FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 STEP 1 (C) (F) DWG 453A2610 SHEET 3 REV C MATERIAL USED A90RG1W 48144 PO 2021-152338.; [02] CERTIFIED WORK PERFORMED.
BROKEN EMERGENCY DOOR COVER HANDLE RH SIDE AT PASSENGER CABIN (1 EA) ; 2021-319518 / [01] REPLACED EMERGENCY DOOR COVER HANDLE RH SIDE AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 52-22-51-400-801; [02] REPLACED EMERGENCY DOOR COVER HANDLE RH SIDE AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 52-22-51-400-801 STEP 3; C; 2(H)
CRACK EXTERNAL SKIN SLAT 8 LOCATED AROUND THE FASTENER THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 451.97. AT RT WING ; 2021-319497 / [01] TOOL USED DIGITAL CALIPER P/N: 500-172-20;S/N: 12141486; DUE DATE: 31-JAN-22; [02] TOOL USED P/N: NORTEC500D; S/N: N500X12101V022236; DUE DATE: 02-JUN-22.; [03] RAISED NEW FAULT TTG8Q005QV50 TO REPLACE SLAT 8 DUE TO NOT FOUND ALLOWABLE DAMAGE FOR CRACK ON THE ACTUATOR RIB FITTING; [04] RAISED NEW FAULT TTG8Q005QV50 TO REPLACE SLAT 8 DUE TO NOT FOUND ALLOWABLE DAMAGE FOR CRACK ON THE ACTUATOR RIB FITTING
CRACK EXTERNAL SKIN SLAT 6 LOCATED AROUND THE FASTENER THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 202.45. AT RT WING ; 2021-319499 / [01] TOOL USED DIGITAL CALIPER P/N: 500-172-30; S/N: 15237811; DUE DATE: 11-MAY-22; [02] TOOL USED P/N: NORTEC500D; S/N: N500X12101V022236; DUE DATE: 02-JUN-22.; [03] PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN SLAT 6 LOCATED AROUND THE FASTENER THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 202.45. AT RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8.; [04] PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN SLAT 6 LOCATED AROUND THE FASTENER THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 202.45. AT RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8. VERIFIED AS RII.
CAPT. ASSIST HANDLE IS BROKEN. R&R CAPT. ASSIST HANDLE AMM 561111.
CRACK INDICATION S4R STA 500D + 10 APPROX 1/2' LONG. NDT REF PART 6 53-30-25; VERIFIED PART 6 53-30-09 / ACCOMPLISH REPAIR EA NO. 1-A53-10228 REV. 1 SEE SA-M A1308731
INDICATION OF CRACK S4R STA 500C +8 APPOX 1.5'LONG. NDT REF PART 6 53-30-25; VERIFIED PART 6 53-30-09 / ACCOMPLISHED REPAIR IAW EA 1-A53-10228 REV 1 SA-M 326:A1308728
CRACK INDICATOR STR STA 500 D & 7 APPROX 1' IN LENGTH NDT REF PART 6 53-30-25; VERIFIED PART 6 53-30-09 / ACCOMPLISHED REPAIR EA NO. 1-A53-10228 REV 1 SA-M 326:A1308730
PILOT REPORT RF SLIDE INSPECTION STICKER BLOCKS PRESSURE GUAGE / R&R'D SLIDE ASSY PER MT 725-61-06 RAR# 91643 P/N OFF/ON 63550-101; S/N OFF 0311F _____________________S/N ON 0177F
AFT ENTRY DOOR GUIDE ROLLER OUTER RACE BROKEN. / REMOVED AND REPLACED PER AMM 52-13-21.
SURFACE CORROSION FOUND ON CROWN SKIN AT ADF ANTENNA MOUNT HOLES 1-12 MARKED / REPAIRED PER EA #21-153-00299
FOUND 2 EACH CRACK INDICATIONS AT CHEM-MILL STEP AT STR 1 BETWEEN STA 675 AND STA 706 AT L/H SIDE OF ADF ANTENNA. DETECTED WITH PART 6; 53-30-09 AND VERIFIED WITH PART 4; 53-30-07. AFT CRACK MEASURES 2' IN LENGTH APPROX; FWD CRACK MEASURES APPROX 1' IN LENGTH / SA-M 326 #A1308443 COMPLIED WITH EA. 21-153-00299. PART 1;2;4;5;6 AND REV IR
9ABC AND 12ABC AISLE EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED M1670 BATTERY PACK. OPERATIONS CHECK GOOD, REF AMM 33-51-06.
ON 5 MILE FINAL HAD TO SLOW FOR PRECEEDING AIRCRAFT, WENT FROM FLAPS 30 TO FLAPS 40. FLAPS STOPPED SYMMETRICALLY AT 35 DEGREES W/FLAP HANDLE IN THE 40 DEGREE POSITION. WENT AROUND RAN TRAILING EDGE FLAP DISAGREE QRH. DECLARED EMERGENCY LANDED. AFTER LANDING FLAPS MOVED TO 40 DEGREES ON THEIR OWN. AT THE GATE 'B' SYSTEM HYD READ 68%. LEFT GEG 'B' SYST HYD READ 91%, FOUND BAD LEFT TRAILING EDGE FLAP POSITION FAILED, PER FSCU. REMOVED LEFT TRAILING EDGE FLAP POSITION TRANSMITTER AND INSTALLED SERVICEABLE UNIT, PER AMM 27-58-01. C/W TRAILING EDGE FLAPS AND LEADING EDGE FLAPS/SLAT SYSTEM LOCKOUT, PER 727-PRD-01-03 RAR 78726 POS LT P/N OFF/ON 18-1738-10 S/N OFF 3152 S/N ON 3919.
AFT SCREW, HOLDING ESCAPE SLIDE ON AFT ENTRY DOOR, STRIPPED. SECURED COVER IAW AMM.
L2 DOOR MANUAL ESCAPE SLIDE PULL HANDLE COVER MISSING. / REPOSITIONED PULL HANDLE IAW AMM.
R/H EMERGENCY EXIT OVER WING COVER VELCRO WORN. / R&R VELCRO PER SIP.
G1 GALLEY EMERGENCY EXIT LIGHT ASSEMBLY DAMAGED. / R&R LIGHT ASSEMBLY IAW AMM.
R/H FORWARD SLIDE LIGHT INOP. R&R LAMP PER AMM.
ACB AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED ACB AFT CORNER SCUFF PLATE PER REF EA 1-A53-2076 REV 11
FORWARD CARGO BAY; FORWARD CORNER SCUFF PLATE IS CRACKED. / RECIEVED FCB FORWARD CORNER SCUFF PLATE (P/N 7530406). TO BE INSTALLED ON CUSTOMER CARD # 753-646-63-01. 59577U 09AUG19
AFT CARGO BAY; FORWARD CORNER SCUFF PLATE IS CRACKED. / REPLACED FWD CORNER SCUFF PLATE PER REF AMM 53-11-02-420-801
FORWARD CARGO BAY; AFT CORNER SCUFF PLATE IS CRACKED. / RECIEVED ACB AFT CORNER SCUFF PLATE (P/N 7530065). TO BE INSTALLED ON CUSTOMER CARD # 753-646-63-01. 59577U 09AUG19
R/W T/E WIGGLE PLATE BROKEN COMMON TO FORWARD EDGE OF PANEL 651BB / REMOVED AND REPLACED WIGGLE PLATE ASSY R/W T/E COMMON TO FORWARD EDGE OF PANEL 651BB IAW SRM 51-40-02-0G-0; DWG 115A2781 AND IPC 57-50-00-27 83802U 10AUG19
FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS. 400 TO BS. 420, LBL 22. / R&R INTERCOSTAL IAW SRM AND DWG.
FUSELAGE CROWN DOUBLER PLATE CORRODED BETWEEN BS. 1036 TO BS. 1043, BETWEEN STR. 2L TO STR. 2R. / R&R DOUBLER PLATE IAW SRM AND DWG.
***CORROSION*** ANGLE ON FUSELAGE CROWN; AT BS1036; STR-2L TO STR-2R / REMOVED AND REPLACED ANGLE ON FUSELAGE CROWN; AT BS 1036; STR-2L TO STR-2R IAW SRM 51-40-02-0G-0 AND DWG 148A3110 83802U 05AUG19
***CORROSION*** UNDER VERTICAL STABILIZER; ALONG PERIMETER OF LH AND RH REAR SPAR STRUCTURAL SUPPORT ANGLES; APPROX. STA 1035-1076; LBL 11-RBL 9 (UPPER CROWN) - MARKED / CORROSION ALONG PERIMETER OF LH & RH REAR SPAR STRUCTURAL SUPPORT ANGLES AT BS 1035-1076; LBL 11- RBL 9 WAS REPAIRED IAW ATS ER 19-04138 REV IR DATED 12AUG19 AND EA 1-753-35388 REV IR
L/H WING FIXED LEADING EDGE STRINGER CRACKED JUST INBOARD OF PYLON. R&R STRINGER IAW SRM & DWG.
FLOOR SUPPORT ANGLE DAMAGED AT BS. 685+4, LBL 9. / R&R ANGLE IAW SRM AND DWG.
PANEL 194GR HAS A DELAMINATED DENT ON THE EXTERNAL SKIN / PANEL 194GR HAD DELAMINATED DENT ON THE EXTERNAL SKIN WERE REPAIRED IAW SRM 51-70-05-2R-2 AND SRM 51-70-05-2R-11
FLOOR SUPPORT STRUCTURE CRACKED AT BS. 540, LBL 1. R&R FLOOR SUPPORT STRUCTURE IAW SRM & DWG.
MAIN E-BAY DOOR CUTOUT LT VERTICAL WEB DAMAGED AT BS. 335, LBL 5. R&R WEB IAW SRM AND DWG.
***CORROSION*** ON FWD BULKHEAD AT APU COMPARTMENT JUST UNDER FUEL SUPPLY LINE BS1088 LBL14 WL215. MARKED. / CORROSION ON FWD BULKHEAD AT APU COMPARTMENT AT BS 1088 LBL 14 WL 215 WAS REPAIRED IAW ATS ER 19-04139 REV IR DATED 29JUL19 AND EA 1-753-35316 REV IR
PANEL 192AL HAS A DELAMINATED DENT ON THE EXTERNAL SURFACE; 9' FROM THE AFT EDGE; 8' FROM THE LOWER EDGE / REPAIRED DELAMINATED DENT ON EXTERNAL SURFACE OF PANEL 192AL IAW SRM 51-70-05-2R-2. 59049U 07-20-19
CRACKED RADIUS OF FRAME ABOVE ENTRY DOOR AT BS. 313, STR. 5L. / REPAIRED FRAME IAW ER AND EA.
LOWER COMPOSITE BULKHEAD SUPPORT ANGLE CRACKED AT BS. 663, RBL 27. R&R ANGLE IAW SRM AND DWG.
REAR SPAR WING CENTER SECTION SEAL RETAINER ASSY AT RH SIDE IS CRACKED / REPLACED REAR SPAR WING CENTER SECTION SEAL RETAINER ASSY AT RH SIDE BS 663 I.A.W SRM 51-40-02-0G-0 AND DRAWING # 111A1000.
FORWARD CARGO BAY ON LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 500 TO BS. 500D, LBL 22. R&R SUPPORT PER SRM AND DWG.
CRACKED INTERCOSTAL TO FRAME ANGLE SUPPORT AT BS. 400, LBL 24. / R&R SUPPORT IAW SRM AND DWG.
FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 420 TO BS. 440, RBL 22. R&R SHIELD IAW SRM AND DWG.
FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 492 TO BS. 500A, RBL 22. R&R SHIELD IAW SRM AND DWG.
FRAME TO STRINGER INTERCOSTAL SUPPORT CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET PER SRM AND DWG.
LT WING FWD FAIRING 542AB O/B SEAL RETAINER CRACKED. / REMOVED CRACKED LT WING FWD FAIRING 542AB O/B SEAL RETAINER IAW 20-50-01 AND INSTALLED NEW SERVICEABLE LT WING FWD FAIRING 542AB O/B SEAL RETAINER IAW SOPM 20-50-01 59617U 19JUL19
AFT CARGO BAY STRINGER SPLICE FITTING CORRODED AT BS. 1016, RBL 21. / R&R FITTING PER DWG AND SRM.
AFT CARGO BAY AFT SHIELD AT CORRODED BETWEEN BS. 847 TO BS. 867, RBL 21. R&R SHIELD IAW SRM & DWG.
AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727C TO BS. 847, LBL 20. R&R SUPPORT IAW SRM AND DWG.
AFT CARGO BAY ON FORWARD SHIELD CORRODED BETWEEN BS. 767 TO BS. 787, RBL 22. R&R SHIELD IAW SRM AND DWG.
AFT CARGO BAY RAIL CORRODED AT BS. 767+6, LBL 3. REPAIRED RAIL IAW EA.
AFT CARGO BAY RAIL CORRODED AT BS. 767+6, RBL 8. / REPAIRED RAIL IAW EA.
AFT CARGO BAY ON LOWER BULKHEAD TO FLOOR PANEL SUPPORT CORRODED BETWEEN BS. 847 TO BS. 867, LBL 20. / R&R SUPPORT PER SRM & DWG.
AFT CARGO BAY RAIL CORRODED AT BS. 767+6, RBL 3. / REPAIRED FLOOR BEAM IAW EA.
AFT CARGO BAY RAIL CORRODED AT BS. 767+6, LBL 8. REPAIRED FLOOR BEAM IAW EA.
CHAFING ON FRAME STA 294.5 STR 3 LT HAND LOWER FLANGE (MARKED) / BS 294.5. STR 3L FRAME CHAFING WAS REPAIRED IAW ATS ER 19-04127 REV IR DATED 07AUG19 AND EA 1-753-35370 REV IR
FRAME CRACKED AT BS. 440, STR 8L BIN RAIL SUPPORT. REPAIRED FRAME PER EA.
AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727C TO BS. 767, RBL 20. / R&R SUPPORT IAW SRM AND DWG.
***CORROSION*** ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS927+8 RBL13 WL176. / REMOVED AND REPLACED ACB FLOOR TRACK AT BS 887-947 RBL 13 WL 176 IAW SRM 53-00-53-1A-2 SRM 51-40-02; SRM 51-40-05 AND DWG # 147A7500. 59647U 29JUL19
***CORROSION*** ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS927+8 LBL3 WL176. / REMOVED CORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS 927+8 LBL 3 I.A.W SRM 51-10-02-0G-0 AND ELEVAULATED MAX. MATERIAL REMOVED. L=2.5' X W=1.0' X MINIMUM REMAINING THICKNESS 0.073' FROM ORIGINAL THICKNESS=0.080' AND FOUND TO BE WITHIN LIMITS I.A.W. SRM 53-00-53-1A-2 PARAGRAPH 4.B.(2) FIGURE 103 DETAIL 'G'; APPLIED CHEMICAL CONVERSION COATING AND PRIMER I.A.W. SRM 51-20-01-0G-0 ON BLENDED AREA.
CABIN FRAME CRACKED AT BS. 727D, STR. 8R BIN RAIL SUPPORT. / REPAIRED FRAME IAW EA.
***CORROSION*** ON FLOOR PANEL SUPPORT SPLICE AT AFT CARGO BAY BS767+6 LBL20 - RBL19 WL156. / RECIEVED NEW REPLACEMENT SUPPORT SPLICE TO REPLACE CORRODED SPLICE AT ACB BS 767+6 LBL20-RBL19 IAW SRM 51-10-02-0G-0; SUPPORT SPLICE TO BE INSTALLED ON CUSTOMER CARD # JPANEL-141-CLOSE BETWEEN FLOOR PANEL 140BF & 140CF
AFT CARGO BAY FLOOR PANEL SUPPORT SPLICE CORRODED AT BS. 887, BETWEEN RBL 20 TO LBL 7. / R&R SPLICE IAW SRM.
HORIZONTAL PRESSURE DECK CRACKED BETWEEN BS. 663 TO BS. 675, LBL 32. REPAIRED PRESSURE DECK IAW ER AND EA.
AFT BULKHEAD AFT STR END FITTING HOLE OUT OF LIMITS MEASURES .319 AT 8L STR 3L / REAMED HOLE 8L AT STR 3L TO A HOLE DIAMETER OF 0.3286' AND INSTALLED BOLT IAW SI# 12107-53
R1 DOOR NR 4 LOWER BEAM WAS CRACKED IN THE RADIUS ON THE OUTBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. R & R THE LOWER BEAM.
RT WING TRAILING EDGE SUPPORT ANGLE CRACKED BELOW PROGRAM ROLLER SUPPORT ARM JUST O/B OF #2 PYLON AFT TIP. R&R ANGLE IAW SRM.
LT WING TRAILING EDGE COVE SEAL SUPPORT ANGLE CRACKED ABOVE #1 PYLON AFT TIP. R&R ANGLE IAW SRM.
RT WING TRAILING EDGE COVE SEAL SUPPORT ANGLE CRACKED ABOVE #2 PYLON AFT TIP. R&R ANGLE IAW SRM.
LOWER COMPOSITE BULKHEAD CRACKED AT BS. 663, RBL 10. R&R BULKHEAD IAW SRM & DWG.
AFT BULKHEAD VERTICAL FIN ATTACHMENT FITTING HOLE OUT OF LIMITS MEASURES .384' AT 6L STR 2L / REAMED HOLE 6L AT STR 2L TO A HOLE DIAMETER OF 0.4067' AND INSTALLED BOLT IAW SI#12107-53
AFT BULKHEAD VERTICAL FIN ATTACHMENT FITTING HOLE OUT OF LIMITS MEASURES .384' AT 5L STR 2L / REAMED HOLE 5L AT STR 2L TO A HOLE DIAMETER OF 0.4067' AND INSTALLED BOLT IAW SI#12107-53
AFT CARGO CENTER SCUFF PLATE HAS A CRACK MEASURING 5' LONG FROM FWD EDGE OF SCUFF PLATE AND DENT 6' FWD FROM AFT EDGE MEASURING 1.25' LONG .055' DEEP AND .25' WIDE MOD / RECEIVED NEW PART 146A8342-8 OK TO INSTALL WAS ACCOMPLISHED ON CUSTOMER CARD NBR 753-140-00-02Y STEP 3 INSTALLED AFT CARGO CENTER SCUFF PLATE. PER REF. AMM 53-11-02-420-801
RT SIDE AFT OF COCKPIT DOOR EMERGENCY BATTERY PACK M1674 WILL NOT CHARGE. R&R BATTERY PACK IAW AMM.
LT FWD EMERGENCY BATTERY FAILED TEST. R&R BATTERY ASSY PER MM.
AFT GALLEY EMERGENCY EXIT SIGN LENS MISSING. REPLACED THE LENS IAW SIP.
LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER AMM.
LT OVERWING EMERGENCY EXIT LOWER HANDLE BEZEL CRACKED. R&R HANDLE BEZEL PER AMM.
EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01673. R&R BATTERY PACK PER MM.
EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01675. R&R BATTERY PACK PER MM.
EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01670. R&R BATTERY PACK PER MM.
EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01672. R&R BATTERY PACK PER MM.
LT WIND SCREEN EMERGENCY FLASHLIGHT OUT OF POSITION. R&R BATTERY PER AMM.
CENTER OVERWING CEILING EMERGENCY EXIT SIGN LIGHT BROKEN. R & R THE SIGN ASSEMBLY IAW AMM.
AFT CARGO BAY FLOOR TEE SPLICE CORRODED AT BS 772. R & R THE TEE SPLICE IAW SRM & DWG.
AFT CARGO BAY FLOORBEAM TEE CORRODED AT BS 727D+5.6. R & R THE TEE IAW SRM AND DWG.
AFT CARGO BAY BULKHEAD SUPPORT CORRODED AT BS 947 RT. R&R SUPPORT PER SRM.
ACB; CARGO TIE DOWN TRACK; BS 727+4 TO BS 887; RBL 18; WL 155; REQUIRES REPLACEMENT DUE TO THE EXTENT OF DAMAGE. / ACB; CARGO TIE DOWN TRACK; B.S. 727+4 TO BS 887; RBL 18; WL 155 REQUIRES REPLACEMENT DUE TO THE EXTENT OF DAMAGE. REMOVED DAMAGED SECTION OF TIE DOWN TRACK PER SRM 51-40-02. RECIEVED NEW TIE DOWN TRACK; LOCATED; DRILLED AND INSTALLED PER SRM 53-00-53-2R-3 AND PER DWG 146A7500.
LT HORIZ. STAB UPPER FWD SLIDE SEAL IS CRACKED. / REPLACED LT HORIZ. STAB UPPER FWD SLIDE SEAL IAW SRM 51-40-02-0G-0 STEP 4.
FORWARD CARGO BAY CRACKED GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM AND DWG.
FLOOR SUPPORT CORRODED BETWEEN BS. 1006 TO BS. 1016, LBL 36. R & R THE FLOOR SUPPORT IAW SRM AND DWG.
AFT CARGO BAY FRAME SPLICE CORRODED AT BS 787, STRINGER 25R. R & R THE FRAME SPLICE IAW SRM & DWG.
AFT CARGO DOOR CUTOUT SUB WEB THRESHOLD CORRODED AREAS. R & R THE SUB WEB THRESHOLD PER SRM & DWG.
AFT CARGO BAY SIDEWALL SHIELD CORRODED BETWEEN BS. 847 TO BS. 867, RBL 21. R & R THE SHIELD IAW SRM & DWG.
AFT CARGO BAY DOOR CUTOUT STRAP CORRODED BETWEEN BS 781 TO 847, RBL 21. R & R STRAP IAW SRM & DWG.
AFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO 807, LBL 21. R & R THE SIDEWALL SUPPORT IAW SRM & DWG.
AFT CARGO BAY SHIELD CORRODED BETWEEN BS 767 - 787, RBL 21. R & R THE SHIELD IAW SRM.
SHEAR WEB CORRODED AT BS 1016, RBL 36. R & R THE SHEAR WEB IAW SRM AND DWG.
AFT CARGO BAY BULKHEAD PANEL SUPPORT CORRODED AT BS 947, WL 155. R&R SUPPORT PER SRM.
CREASE BEAM WEB CORRODED AT BS 380, RBL 68. REPAIRED WEB IAW EA & ER.
***CORROSION*** ACB BS 787 WL155 ABOVE STR25L FRAME SIDEWALL SUPPORT HAS CORROSION. / REMOVED & REINSTALLED NEW FRAME SIDEWALL SUPPORT DUE TO CORROSION PER SRM 51-40-02-0G-0 & DWG #146A1262
***CORROSION*** ACB BS 867-947 RBL21 WL155 SIDEWALL PANEL SUPPORT HAS NUMEROUS CORROSION. / REMOVED CORROSION ON SIDEWALL SUPPORT 807-847 RBL 21 - WL 155 MULTIPLE LOCATIONS 1' X 1' X 2' FOUND OUT OF LIMITS DUE TO GOING OVER MORE THAN 3 IN 10 FASTENERS REMOVED FLOOR TO SIDEWALL SUPPORT LOCATED; DRILLED USING BAC 1496-377 7075T6 LOT # 1283962 ALODINED PRIMED & INSTALLED PER SRM 51-40-02; SRM 51-20-01; SRM 53-00-53-1A-2; SRM 53-70-53-01-02 & DWG 147A7500
***CORROSION*** ACB BS 927 WL148 O/B STR27L FRAME WEB SURFACE HAS CORROSION. / ACB BS 927; WL 148; OB STR 27L FRAME WEB HAS SURFACE CORROSION REPAIRED PER ATS ESR 17-03115 REV IR AND SWA EA 1-753-31439 REV IR
ACB BS 947 RBL21 WL155 INTERCOSTAL BAFFLE IS CRACK. / ACB B.S 947 RBL 21 WL 155 INTERCOSTAL BAFFLE IS CRACKED & FOUND OUT OF LIMITS REMOVED & REPLACED PER DWG 147A7500 & SRM 51-40-02
***CORROSION*** ACB BS 947 RBL21 WL155 INTERCOSTAL BAFFLE CLIP HAS CORROSION. / CORROSSION ON ACB BAFFLE CLIP 947 RBL21 WL155 FOUND OUT OF LIMITS DUE TO NO LIMITS ESTABLISHED IN SRM REMOVED & REPLACED CLIP ON CUSTOMER CARD T671390. 56040C 03JUL17
AFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 727 & 767, RBL 21. R & R THE SIDEWALL SUPPORT IAW SRM & DWG.
FORWARD CARGO DOOR OPENING SUB WEB CORRODED. R & R THE SUB WEB PER SRM.
AFT CARGO BAY BULKHEAD BACKSIDE BRACKET CRACKED AT BS. 947, LBL 9. R & R THE BRACKET IAW SRM.
SHEAR WEB CORRODED AT BS 1016, LBL 36. R & R THE SHEAR WEB IAW SRM.
FLOORBEAM CORRODED AT BS 328, RBL 42. REPAIRED FLOORBEAM PER ER & EA.
CORROSION ON PRESSURE DOME SEAL DEPRESSOR ANGLE BS 1016 RBL 26 WL 210 / REMOVED AND REPLACED PRESSURE DOME SEAL DEPRESSOR ANGLE (INTERCOSTAL) AT BS 1016 RBL 26-RBL 49 WL 210 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 65-54862; 148A0922
***CORROSION*** FCB BILGE BETWEEN BS 500-500A BL0. ANTENNA INTERNAL BACE CORRODED / REMOVED AND REPLACED ANTENNA BASE ASSY FCB BILGE BETWEEN 500-500A BL0 PER DWG 143A3230 DWG 143A3233 SRM 51-40-02 .040 T6 CLAD LOT # 1252458
***CORROSION*** FCB BILGE BETWEEN BS500A AND 500B BL0 ANTENNA INTERNAL BASE CORRODED / REMOVED AND REPLACED ANTENNA BASE ASSY FCB BILGE BETWEEN B.S. 500A AND 500B BL0 PER DWG 143A3230 DWG 143A3233 SRM 51-40-02 .040 CLAD LOT # 1252458
***CORROSION*** FCB BS500A-500D RBL 25 SIDE PLATE HAS CORROSION IN SEVERAL AREAS / REMOVED AND REPLACED FCB BS 500A-500D RBL 25 SIDE PLATE IAW SRM 51-40-02 AND DWG 143A7500
INTERCOSTAL FLOOR SUPPORT CRACKED; BS 277 - 294; BL 0; WL 207. / REMOVED AND REPLACED INTERCOSTAL FLOOR SUPPORT AT BS. 277-294 BL0; WL 207 PER SRM 51-40-05-0G-0
FCB BS 500B -500C LBL 25 SIDE PLATE SUPPORT WEB CRACKED. / REMOVED AND REPLACED FCB B.S. 500B-500C LBL 25 SIDE PLATE SUPPORT WEB 143A7510-11/ NEW PER SRM 51-40-02 SRM 51-10-02 DWG 143A7505
FCBBS 500 LBL 25 SIDE PLATE SUPPORT WEB CRACKED / REMOVED AND REPLACED FCB BS 500 LBL 25 SIDE PLATE SUPPORT WEB ASSY 143A7510-15/ NEW FOR SRM 51-40-02 SRM 51-10-02 DWG 143A7505
(RIGHT WING) UPPER T/E PANEL U SUPPORT BEAM TO REAR SPAR ATTACH ANGLE IS CRACKED; RSS80 / REMOVED RT WING UPPER TE PANEL U SUPPORT BEAM TO SPAR ATTACH CLIP IAW SRM 51-40-02 56790 06/21/17 3074 C 21JUN17 INSTALLED A NEW T/E PANEL U SUPPORT BEAM TO SPAR ATTACH CLIP IAW SRM 51-40-02-0G-0 STEP 7
(RIGHT WING) T/E COVE SEAL SUPPORT ANGLE CRACKED ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED T/E CORE SEAL SUPPORT ANGLE ABOVE #2 PYLON AFT TIP IAW SRM 51-40-02-0G-0 84036_24JUN17
(RIGHT WING) UPPER T/E SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED UPPER T/E SUPPORT ANGLE AT THE TRANSVERSE WEB ABOVE #2 PYLON IAW SOPM 20-50-01 84036 24JUN17
(RIGHT WING) TRANSVERSE WEB IS CRACKED AT O/B END UPPER LEG JUST I/B OF PROGRAM ROLLER SUPPORT ARM ATTACH POINT / REMOVED AND REPLACED TRANSVERSE WEB FITTING OF O/B END AND I/B OF PROGRAM ROLLER ARM SUPPORT IAW SOPM 20-50-01 84036 22JUN17
ACB; FWD. CORNER SCUFF PLATE CRACKED. / REPAIRED AND INSTALLED ACB; FWD. CORNER SCUFF PLATE IAW EA 1-A53-2076 REV 11 AND AMM 53-11-02-420-801
FCB; AFT CORNER SCUFF PLATE CRACKED. / REPAIRED AFT CORNER SCUFF PLATE IAW EA 1-A53-2076 REV 11
***CORROSION*** ON FWD SERVICE DOOR THRESHOLD SUPPORT ANGLE; BS 298 - 330; RBL 57; WL 208. / REMOVED OUT OF LIMITS FWD SERVICE DOOR THRESHOLD SUPPORT ANGLE AT BS 298-330 RBL57 WL 208 AND INSTALLED NEW THRESHOLD SUPPORT ANGLE IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0; DWG 141A8310 REV.D
FORWARD CARGO BAY RT SIDE PLATE SUPPORT CORRODED BETWEEN BS 400 TO 420. R & R THE SUPPORT IAW SRM & DWG.
FORWARD CARGO BAY SIDE WALL PANEL SUPPORT CORRODED 500D RT BULKHEAD. R & R THE SIDEWALL SUPPORT IAW SRM.
FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, BL 0. R & R FLOOR SUPPORT IAW SRM.
LEFT WING UPPER TRAILING EDGE PANEL LOWER SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT. R & R THE ANGLE IAW SRM.
INTERCOSTAL FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, RBL 31. R & R THE FLOOR SUPPORT IAW SRM.
FORWARD CARGO BAY RT SIDE SHIELD ASSEMBLY CORRODED BETWEEN BS 420 & 440. R & R THE SHIELD ASSEMBLY IAW SRM AND DWG.
FORWARD CARGO BAY SHIELD ASSEMBLY CORRODED BETWEEN BS 492 & 500A, RBL 25. R & R THE SHIELD ASSEMBLY IAW SRM.
FORWARD CARGO BAY SIDE PLATE CORRODED BETWEEN BS 400 & 500D, LBL 25. R & R THE SUPPORT PLATE IAW SRM & DWG.
FORWARD CARGO BAY BOTTOM BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN LBL 25 RBL 25. R & R THE SUPPORT ANGLE IAW SRM.
CREASE BEAM CORRODED AT BS 706, LBL 55. REPAIRED THE CREASE BEAM IAW ER AND EA.
CREASE BEAM CORRODED AT BS 706, RBL 55. REPAIRED THE CREASE BEAM IAW ER AND EA.
CORROSION ON CABIN FLOORPANEL INSERTS 242WF / REPAIRED DAMAGE AND REPLACED CORRODED INSERTS ON CABIN FLOOR PANEL 242WF IAW SRM 53-00-50-2R-9 56749U 26JUN17
CORROSION BS 986 BEAM UPPER CHORD PREVIOUS REPAIR LBL55-RBL55 WL 208 / REMOVED AND REPLACED UPPER CHORD PER ATSER-07-3558 AND REMOVED AND REPLACED REPAIR FASTENERS PER 737-700 SRM 51-40-02 AS SHOWN IN ATS ER 07-3558 (REFERENCE. ESR #17-03029)
CORROSION ON INNER CHORD 'MOPSILL' BS 947-986 RBL57 WL 208 SEE SA-M 326 FOR REJECTIONS A1111758 ATS340INSP 6-28-17 / REMOVED AND REPLACED INNER CHORD 'MOPSILL' AT AFT SERVICE DOOR IAW SRM 51-40-02 AND DWG 147A8501 SHT 69 & 70. COMPLETED REJECTED ITEMS ON SAM326 A1111758 INSTALLED CORRECT FASTENERS IN FRAMES BS 907; 927; 951 & 992 PER DWG 147A8501 SHT 69 & 70. 7138C 6/28/17
CORROSION ON CABIN FLOORPANEL INSERTS 242UF / REPAIRED DAMAGE AND REPLACED CORRODED INSERTS ON CABIN FLOOR PANEL 242UF IAW SRM 53-00-50-2R-9. 56749U 26JUN17
CORROSION ON CABIN FLOORPANEL INSERTS 241ADF / REPAIRED DAMAGE AND REPLACED CORRODED INSERTS ON CABIN FLOOR PANEL 241ADF IAW SRM 53-00-50-2R-1. 56749U 26JUN17
CORROSION ON CABIN FLOORPANEL INSERTS 241ABF / REPAIRED DAMAGE AND REPLACED CORRODED INSERTS ON CABIN FLOOR PANEL 241ABF IAW SRM 53-00-50-2R-9. 56749U 26JUN17
CORROSION ON FLOORPANEL INSERTS 222BF / REPAIRED DAMAGE ON FLOOR PANEL 222BF; INSTALLED NEW INSERTS PER SRM 53-00-50-2R-9 AND SRM 53-00-50-2R-0.
CORROSION ON FLOORPANEL INSERTS 221BF / DAMAGE FOUND ON UPPER AND LOWER SKINS OF FLOOR PANEL 221BF AT INSERT LOCATION P45; AND ALL CORRODED INSERTS; WERE REPLACED IAW SRM 53-00-50-2R-1; SRM 53-00-50-2R-2; AND DWG 141A5810-56 56563U 26JUN17
CORROSION ON INNER CHORD 'MOPSILL' BS 947-986 LBL57 WL 208 / REMOVED AND REPLACED INNER CHORD 'MOPSIL' ON AFT ENTRY DOOR LOWER MAINSILL 1.D.W. SRM 51-40-20-0G-0 AND BOEING DWG 147A8501.
CORROSION ON FLOORPANEL INSERTS 221DF / REPAIRED DAMAGE AND REPLACED CORRODED INSERTS ON FLOOR PANEL 221DF IAW SRM 53-00-50-2R-1. 56749U 27JUN17
CORROSION ON FLOORPANEL INSERTS 221GF / REPAIRED DAMAGE AND REPLACED CORRODED INSERTS ON FLOOR PANEL 221GF IAW SRM 53-00-50-2R-9. 56749U 27JUN17
CORROSION ON FLOORPANEL INSERTS 222CF / REPAIRED DAMAGE AND REPLACED CORRODED INSERTS ON FLOOR PANEL 222CF IAW SRM 53-00-50-2R-1 56749U 27JUN17
LT WING UPPER TRAILING EDGE PANEL LOWER U SUPPORT BEAM REAR SPAR ATTACH ANGLE CRACKED AT RSS 80. R&R ANGLE IAW SRM.
INTERCOSTAL FLOOR SUPPORT CRACKED BETWEEN BS 312 TO BS 328, LBL 46. R&R SUPPORT IAW SRM.
INTERCOSTAL FLOOR SUPPORT CRACKED BETWEEN BS 328 TO BS 344, LBL 46. R&R SUPPORT IAW SRM.
FORWARD CARGO BAY SIDEWALL PANEL SUPPORT CORRODED AT BS 500, LBL 28. R & R THE SIDEWALL SUPPORT IAW SRM AND DWG.
L1 DOOR AFT GIRT BRACKET SUPPORT CORRODED AT BS 344, LBL 59. R & R THE SUPPORT IAW SRM AND DWG.
FAIRING FRAME CORRODED AT BS 727C, BETWEEN RBL 4 TO RBL 11. R & R THE FRAME IAW SRM.
L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY LENS RETAINER CLIP BROKEN. R & R THE LIGHT ASSEMBLY IAW AMM.
INTERCOSTAL ANGLE CRACKED AT BS 528 AIRCRAFT DISTRIBUTION AREA. R&R ANGLE PER SRM.
RIGHT MLG WHEEL WELL PRESSURE DECK, CRACKED AT BS 665, RBL 43. REPAIRED THE BULKHEAD WEB IAW EA.
L1 DOOR UPPER AFT CORNER DOOR SKIN CRACKED. R & R THE DOOR IAW AMM.
L1 DOOR EMERGENCY SLIDE GIRT BAR HOLDING ANGLE FOUND OUT OF ADJUST. ADJUSTED THE ANGLE IAW SIP.
DIVERSION, DECLARED EMERGENCY FUEL FLOW ON NR 2 ENGINE DROPPED 100 POUNDS N1 DECREASED 5 PERCENT. ENGINE RECOVERED. MINUTE LATER THE FUEL FLOW DROPPED AGAIN OVER 100 POUNDS WITH N1 & N2 DROP. R & R NR 2 ENGINE HYDRO MECHANICAL UNIT IAW MAINTENANCE.
FORWARD GALLEY EXIT SIGN HOUSING LOWER CLIP BROKEN. R & R SIGN IAW AMM.
DIVERSION, FUEL CROSS FEED CB POPPED. R & R FUEL CROSS FEED VLV ACTUATOR IAW AMM.
EXTERNAL EMER LIGHT INOPERATIVE, BETWEEN BS 986.5 - 1006, BETWEEN STRINGER 11R - 12R. R & R LIGHT IAW AMM.
RIGHT HORIZONTAL STABILIZER, RIB CRACKED AT STAB STATION 92.70 & 38" OF FRONT SPAR. REPAIRED RIB IAW SRM.
WEB CRACKED AT BS 663.75, LBL 10. REPAIRED WEB IAW SRM.
RIGHT HORIZONTAL STABILIZER CRACKED AT STAB STATION 92.70, 29" OF FRONT SPAR. REPAIRED RIB IAW EA.
FORWARD CARGO DOOR CUT OUT CTR SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.
RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STAB STATION 101.90, 10" OF FRONT SPAR. REPAIRED RIB IAW EA.
SUPPORT ANGLE CRACKED AT BS 663.75, LBL 10. R & R ANGLE IAW SRM & DWG.
LEFT WING TE INBD FLAP DELAMINATED. REPAIRED FLAP IAW SRM.
FRAME CRACKED AT BS 907, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
VERTICAL PRESS WEB CRACKED AT BS 663, LBL 29. REPAIRED WEB IAW EA.
RIGHT WING OTBD AFT FLAP TE DELAMINATED. REPAIRED AFT FLAP IAW SRM.
VERTICAL PRESS WEB CRACKED AT BS 663, LBL 34. REPAIRED WEB IAW EA.
LEFT HORIZONTAL STABILIZER RIB CRACKED AT 92.70, 29" OF FRONT SPAR. REPAIRED RIB IAW EA.
LEFT HORIZONTAL STABILIZER RIB CRACKED AT 92.70, 19" OF FRONT SPAR. REPAIRED RIB IAW EA.
LEFT HORIZONTAL STABILIZER RIB CRACKED AT 92.70, LOCATED 10" FRONT SPAR. REPAIRED RIB IAW EA.
LEFT WING OTBD AFT FLAP DELAMINATED ON TE AREA. R & R AFT FLAP IAW AMM.
FRAME CRACKED AT BS 500C, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 500A, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 867, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 400, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 827, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 480, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 440, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 360, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 500C, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 787, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 747, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
VERTICAL PRESS WEB CRACKED AT BS 663, RBL 28.5. REPAIRED WEB IAW EA.
VERTICAL PRESS WEB CRACKED AT BS 663, RBL 40. REPAIRED WEB IAW EA.
VERTICAL PRESS WEB CRACKED AT BS 663, RBL 41. REPAIRED WEB IAW EA.
RIGHT WING LE NR 5 SLAT SKIN CRACKED ON LOWER SURFACE AT ACTUATOR RIB STATION 85.19. REPAIRED SLAT SKIN IAW SRM.
LEFT WING LE SLAT, NOSE SKIN CRACKED ON LOWER SURFACE AT THE ACTUATOR RIB, SLAT STATION 451.97. REPAIRED SKIN IAW SRM.
LEFT EMER EXIT BULLNOSE LIGHT LENS LOOSE BETWEEN ROW 11 TO 12. R & R LENS IAW AMM.
BULKHEAD CHORD CRACKED AT BS 540 BETWEEN STRINGER 22R TO 23R. REPAIRED CHORD IAW EA.
RT EMERGENCY EXIT BULLNOSE LIGHT INOPERATIVE AT ROW 18. R & R LIGHT IAW MM.
LT NR 3 FWD WINDOW POST FASTENER HOLE NR 4 FROM BOTTOM CRACKED AT 3 O'CLOCK POSITION. REPAIRED POST IAW SWA EA.
LT NR 3 FWD WINDOW POST FASTENER HOLE NR 3 FROM BOTTOM CRACKED AT 3 O'CLOCK & 9 O'CLOCK POSITION. REPAIRED POST IAW SWA EA.
SEAT TRACK CRACKED AT BS 727B RBL 45.5 FWD OTBD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.
SEAT TRACK CRACKED AT BS 727B RBL 45.5, FWD INBD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.
RT NR 3 FWD WINDOW POST CRACKED FASTENER HOLE NR 2 FROM BOTTOM, AT 3 & 9 O'CLOCK POSITION. REPAIRED POST IAW EA.
LT NR 3 FWD WINDOW POST CRACKED FASTENER HOLE NR 2 FROM BOTTOM, AT 3 & 9 O'CLOCK POSITION. REPAIRED POST IAW EA.
LT NR 3 FWD WINDOW POST FASTENER HOLE NR 5 FROM BOTTOM CRACKED AT 3 O'CLOCK POSITION. REPAIRED POST IAW SWA EA.
RT NR 3 FWD WINDOW POST CRACKED FASTENER HOLE NR 3 FROM BOTTOM, AT 3 O'CLOCK POSITION. REPAIRED POST IAW EA.
LT HORIZONTAL STABILIZER SKIN CRACKED AT OTBD STAB BS 92.70. REPAIRED SKIN IAW SRM.
LT EMERGENCY EXIT LIGHT BATTERIES FAILED TEST. R&R BATTERY PACKS IAW AMM.
RT EMERGENCY EXIT LIGHT BATTERIES FAILED TEST. R&R BATTERY PACKS IAW AMM.
L1 DOOR EMERGENCY EVAC SLIDE COVER AFT ATTACH BOLT DAMAGED. REMOVED & REPLACED MOUNT ASSY PER MM.
RIGHT AC BAY AFT BULKHEAD HORIZONTAL STIFFENER IS CRACKED. REMOVED AND REPLACED PER SRM 51-40-02.
E&E COMPT LEFT FLOOR SUPPORT BRACKET CRACKED AT FASTENER LOCATED LEFT OF CENTER BETWEEN BS 312 TO 328. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02.
RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.
NR 1 TR I/B TRANSLATING SLEEVE TRAILING EDGE OUTER SKIN DAMAGED/DELAMINATED 3/4" X 2 1/2 " MOD. REPAIRED NR 1 ENGINE I/B T/R TRANSLATING SLEEVE AS PER SEM 51-70-05-2R-1.
L1 DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER M/M.
DECLARED EMERGENCY -- FLAP INDICATION UP (WITH SPLIT) FLAPS DID NOT EXTEND FOR APPROACH OR LANDING. REMOVED AND REPLACED NR 3 SENSOR AND NR 2, 3, 4, 5, 6, 7 AND 8 SKEW SENSOR CONNECTORS PER MM.
RIGHT HORIZONTAL STABILIZER CRACKED AT STA 101.9 9. REPAIRED STABILIZER IAW SRM.
L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MM.
L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.
DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED CHARGER PER MM.
DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED CHARGER PER MM.
DURING SCHEDULED 12Y CHECK, FOUND FWD LAV EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW MM.
DURING SCHEDULED 12Y CHECK, FOUND FLIGHT DECK FIRST OFFICERS FWD I/B SEAT TRACK CRACKED. REMOVED AND REPLACED TRACK IAW MM.
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME IAW EA.
DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE VIEWER COVER CRACKED. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE COVER LENS CRACKED. REMOVED AND REPLACED LENS PER MM.
FWD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.
AIR TURNBACK / DECLARED EMERGENCY. AFTER TAKEOFF GEAR WOULD NOT COME UP. RECYCLED MANUAL GEAR. HORN WOULD NOT SILENCE WITH FLAPS RETRACTED. FOUND WHEEL WELL CONNECTOR NOT SECURED. SECURED CONNECTOR PER MM.
DURING SCHEDULED MV3 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 15. RELAMPED PER MM.
DURING SCHEDULED HC1 CHECK, FOUND EEPLS WORN AT ROW 9. REMOVED AND REPLACED EEPLS PER MM.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS CORRODED BETWEEN ROW 22 TO ROW 23. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 548, RBL 15. REMOVED AND REPLACED FITTING PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 548, LBL 15. REMOVED AND REPLACED FITTING PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND RT WING OB/ AFT FLAP I/B AFT CORNER DELAMINATED. REPAIRED AFT FLAP PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING SECTION REAR SPAR WEB CRACKED AT BS 663, LBL 41. REPAIRED WEB PER AAR EA.
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING SECTION REAR SPAR WEB CRACKED AT BS 663, RBL 34. REPAIRED WEB PER AAR EA.
DURING SCHEDULED 10Y CHECK, FOUND BULKHEAD SUPPORT CRACKED AT BS 727, RBL 4, WL 163.
DURING SCHEDULED 10Y CHECK, FOUND EMERGENCY LIGHT INOP AT 12 DEF. RELAMPED PER MM.
FWD EMERGENCY EXIT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED MV3 CHECK, FOUND LT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.
DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.
AN ODOR WAS PRESENT IN CABIN, SMELLED ELECTRIC/BURNT COFFEE ODOR. SHUTOFF RECIR/GASPER FAN, SMELL WENT AWAY IMMEDIATELY. NO REOCCURRENCE OF SMELL. REMOVED AND REPLACED GASPER FAN PER MM.
DURING SCHEDULED HC1 CHECK, FOUND RT WING NR 4 SLAT UPPER T/E WEDGE INBD CORNER BROKEN. REMOVED AND REPLACED SLAT PER MM.
DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER MM.
DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM.
DURING SCHEDULED HC2 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
DURING SCHEDULED HC2 CHECK, RIGHT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 15 TO RBL 25. REPAIRED FLOORBEAM PER ER.
DECLARED EMERGENCY, NR 2 ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED ALONG WITH "B" SYSTEM HYDRAULIC FAILURE. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 6 ABC. RELAMPED LIGHT PER MM.
R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.
DURING SCHEDULED 5Y CHECK, FOUND LT WING INBOARD AFT T/E FLAP CRACKED. REPAIRED LT WING INBOARD AFT FLAP PER SRM.
AIRTURN BACK, AFTER TAKEOFF FAILED TO PRESSURIZE AND THERE WAS A LOUD AIR NOISE AROUND L1 DOOR AREA. DOOR HANDLE WAS DOWN AND L1 DOOR LIGHT WAS OUT. ADJUSTED L1 DOOR PER MM.
FWD ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATION OUT OF LIMITS. REMOVED AND REPLACED FWD ENTRY DOOR SLIDE ASSY PER MM.
DURING SCHEDULED C2 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.
DURING SCHEDULED A1 CHECK, FOUND EEPLS COVERS BROKEN AT ROW NR 1 AND 11. REMOVED AND REPLACED COVERS PER MM.
AIR TURNBACK, L/E FLAP TRANSIT LIGHT REMAINED ON WITH ALL L/E DEVICES EXTENDED. REMOVED AND REPLACED NR 1, 6, 7 AND 8 L/E SLAT ACTUATORS PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND AFT PRESS BULKHEAD OIL CANNED, BS 1016, FIRST CIRCUMFERENTIAL STRAP. MX FERRY TO PAE, REPAIRED BULKHEAD PER SRM.
EEPLS WIRING EXPOSED AT OVERWING EXIT. SECURED EEPLS WIRING PER MM.
EEPLS WIRING EXPOSED AT OVERWING EXIT. SECURED WIRING PER MM.
AIR TURNBACK - DURING TAKEOFF, RECEIVED T/O CONFIG WARNING, GEAR HANDLE WOULD NOT RETRACT AND A/C WOULD NOT PRESSURIZE. MX FERRY TO PHX. REMOVED AND REPLACED SPOILER INTERLOCK VALVE ROD ASSY PER MM.
DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUSTMENT. REINSTALLED SLIDE ASSY PER MM.