# Service difficulty reports: N763SW, cancelled Oct 29, 2024 A list on [N763SW, cancelled Oct 29, 2024](https://openairdocs.org/deregistered/N763SW-2024-10-29.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 8 · 357 reports - [SDR SWAA2024022053497](https://openairdocs.org/sdr/SWAA2024022053497.md): Girt Bar · loose · Feb 17, 2024 · N763SW · Boeing 7377H4 · Emergency Equipment > FWD SERVICE DOOR GIRT BAR LOOSE WHEN STOWED<[01] SECURED GIRT BAR HOLDER TABS RETAINING CLIPS REF AMM 25-66-01 - [SDR SWAA2024011641093](https://openairdocs.org/sdr/SWAA2024011641093.md): Handle · missing · Jan 14, 2024 · N763SW · Boeing 7377H4 · Escape Slide > AFT SERVICE DOOR PULL HANDLE MISSING<[01] RESECURED AFT SERVICE DOOR SLIDE PULL HANDLE FLAP IAW AMM 25-66-01 - [SDR SWAA2024010437368](https://openairdocs.org/sdr/SWAA2024010437368.md): Slide · out of adjust · Jan 3, 2024 · N763SW · Boeing 7377H4 · Escape Slide > FWD SVC DOOR SLIDE FOLD COMING OUT OF HOLDER THIS IS HOW THE CREW RELAYED IT TO ME CONTRACT MX FOUND NOTHING WRONG.<[01] INSPECTED ALL 4 DOOR SLIDES; NO DEFECTS NOTED PER AMM 25-66-01. - [SDR SWAA2023112224041](https://openairdocs.org/sdr/SWAA2023112224041.md): Slide · out of adjust · Nov 21, 2023 · N763SW · Boeing 7377H4 · Escape Slide > FWD SERVICE DOOR EMERGENCY EXIT SLIDE VISIABLE UNDER DOOR<[01] READJUSTED SLIDE IN CONTAINER PER 25-66-01 - [SDR SWAA2023101610340](https://openairdocs.org/sdr/SWAA2023101610340.md): Battery Pack · failed · Oct 13, 2023 · N763SW · Boeing 7377H4 · Emergency Lighting > EMX BATT PACK M01668 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01668 PER AMM 33-51-06 - [SDR SWAA2023101610341](https://openairdocs.org/sdr/SWAA2023101610341.md): Battery Pack · failed · Oct 13, 2023 · N763SW · Boeing 7377H4 · Emergency Lighting > EMX BATT PACK M01669 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01669 PER AMM 33-51-06 - [SDR SWAA2023101610334](https://openairdocs.org/sdr/SWAA2023101610334.md): Battery Pack · failed · Oct 13, 2023 · N763SW · Boeing 7377H4 · Emergency Lighting > EMX BATT PACK M01670 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01670 PER AMM 33-51-06 - [SDR SWAA2023101610342](https://openairdocs.org/sdr/SWAA2023101610342.md): Battery Pack · failed · Oct 13, 2023 · N763SW · Boeing 7377H4 · Emergency Lighting > EMX BATT PACK M01673 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01673 PER AMM 33-51-06 - [SDR SWAA2023101610343](https://openairdocs.org/sdr/SWAA2023101610343.md): Battery Pack · failed · Oct 13, 2023 · N763SW · Boeing 7377H4 · Emergency Lighting > EMX BATT PACK M01672 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01672 PER AMM 33-51-06 - [SDR SWAA2023101610335](https://openairdocs.org/sdr/SWAA2023101610335.md): Battery Pack · failed · Oct 13, 2023 · N763SW · Boeing 7377H4 · Emergency Lighting > EMX BATT PACK M01675 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01675 PER AMM 33-51-06 - [SDR SWAA2023101610344](https://openairdocs.org/sdr/SWAA2023101610344.md): Battery Pack · failed · Oct 13, 2023 · N763SW · Boeing 7377H4 · Emergency Lighting > EMX BATT PACK M01674 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01674 PER AMM 33-51-06 - [SDR SWAA2022112173002](https://openairdocs.org/sdr/SWAA2022112173002.md): Girt Bar · out of adjust · Nov 18, 2022 · N763SW · Boeing 7377H4 · Emergency Equipment > RT FOWARD DOOR-FOWARD SIDE GIRT BAR HOLDER HOLDSIT LOOSLY. GIRT BAR COULD FALL OUT. / [01] ADJUSTED FWD R/H SERVICE DOOR FWD GIRT BAR HOLDER PER S.I.P.. IT CAN HOLD GIRT BAR NOW. - [SDR SWAA2022092830289](https://openairdocs.org/sdr/SWAA2022092830289.md): Panel · delaminated · Sep 25, 2022 · N763SW · Boeing 7377H4 · Nacelle/Pylon, Plate/Skin > #1ENG PLYON PANEL 431ER IS DELAM'ED LOWER FWD PORTION OF THE PANEL / [01] REMOVED AND REPLACED #1 ENGINE FWD STRUT FAIRING PANEL 431ER PER AMM 54-53-02 - [SDR SWAA2022033187606](https://openairdocs.org/sdr/SWAA2022033187606.md): None · cracked · Mar 24, 2022 · N763SW · Boeing 737 · Cargo Compartments > AFT CARGO BAY R/H CAP STIP SPLICE PLATE CRACKED BS 767 / [01] INSTALLED NEW ACB RH CAPSTRIP SPLICE PLATE IAW AMM 25-52-10-400-801 STEP 3. F. (10);[02] INSPECTION COMPLETE - [SDR SWAA2022033187608](https://openairdocs.org/sdr/SWAA2022033187608.md): None · inoperative · Mar 24, 2022 · N763SW · Boeing 737 · Emergency Lighting > AFT SERVICE DOOR EMERGENCY EXIT LOCATOR HAS 1 EA. LAMP INOP / [01] RELAMPED AFT SERVICE DOOR EXIT LOCATOR AND PERFORMED SATISFACTORY OPERATIONAL TEST PER AMM 33-51-01-960-801.;[02] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2022033183705](https://openairdocs.org/sdr/SWAA2022033183705.md): Track · cracked · Mar 14, 2022 · N763SW · Boeing 7377H4 · Fuselage Internal Mounting Structure > CRACK FWD CARGO TRACK AT STA 460; RBL 14. / [01] REMOVED FWD CARGO TRACK BS 395 TO BS 500D RBL14 WL 156 IAW SRM 51-40-02.;[02] REMOVED TO FOM FLOOR SUPPORT BS 395 RBL AND LBL P/N 284A3603-116 IAW SRM 51-40-02;[03] REMOVED FWD CARGO TRACK BS 395 TO BS 500D RBL1 - [SDR SWAA2022033182972](https://openairdocs.org/sdr/SWAA2022033182972.md): Panel · delaminated · Mar 12, 2022 · N763SW · Boeing 7377H4 · Aerodynamic Fairings > PANEL 193AR HAS DELAMINATION TO OUTER SKIN OVER CORE AREA (MARKED) / [01] IDENTIFIED PANEL 193AR IAW SRM 53-40-70-0I-1 FIGURE 2; SHEET 1; TABLE 2; ITEM 18. DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4A(6). REPAIR TO BE ACCOMPLISHE - [SDR SWAA2022033181481](https://openairdocs.org/sdr/SWAA2022033181481.md): Intercostal · corroded · Mar 8, 2022 · N763SW · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTAL BS 847 TO 850 RBL 18 W/L 153 / [01] APPLICABILITY STATEMENT: ALLOWABLE DAMAGE IAW SRM 53-60-15-1A-1;[02] REMOVED WEB AT ACB BS 847 TO BS 855; RBL 18; IAW SRM 51-40-02-0G-0. REMOVED CORROSION AT WEB L-3'; W-2'; D-0.007'; FOUND OUT OF LI - [SDR SWAA2022033180288](https://openairdocs.org/sdr/SWAA2022033180288.md): Skin · cracked · Mar 4, 2022 · N763SW · Boeing 737 · Horizontal Stabilizer, Plate/Skin > RH HORIZONTAL STAB LWR SKIN CRACKED AT STAB STA 184.7; AFT END IB OF RIB; MARKED / [01] STRIPPED PAINT IN DISCREPANT AREA AT STAB STA 184.7 IN ROUGHLY A 2'X2' AREA PER AMM 51-21-11-150-801 PARA. 3D;[20] ' DAMAGE REPAIRED PER EA 22-155-00745. REPETITIVE INSPECT - [SDR SWAA2022032880286](https://openairdocs.org/sdr/SWAA2022032880286.md): Skin · corroded · Mar 4, 2022 · N763SW · Boeing 737* · Fuselage Main, Plate/Skin > CORROSION ON FUSELAGE SKIN BETWEEN STA 886 - STA 888; STRINGER 25L. / [01] VERIFIED APPLICABILITY IAW SRM 53-00-01-1A-5;[15] AS PER EA 22-153-00763; THE DAMAGE IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING A - [SDR SWAA2022033180051](https://openairdocs.org/sdr/SWAA2022033180051.md): Attach Angle · cracked · Mar 3, 2022 · N763SW · Boeing 737 · Cargo Compartments > CRACK ON AFT CARGO WATER SERVICE TO STRINGER ATTACH ANGEL AT RBL 12 BS 907+8. / [01] RECEIVED A NEW STIFFENER P/N 147A7221-32 FROM STORES. REF: PO 855759.
REMOVED CRACKED STIFFENER IAW SRM 51-40-02.;[02] LOCATED AND DRILLED NEW STIFFENER IAW SRM 51-40-05 A - [SDR SWAA2022033180052](https://openairdocs.org/sdr/SWAA2022033180052.md): Attach Angle · cracked · Mar 3, 2022 · N763SW · Boeing 737 · Cargo Compartments > CRACK ON AFT CARGO WATER SERVICE TO STRINGER ATTACH ANGEL AT RBL 12 BS 907+12. / [01] RECEIVED A NEW STIFFENER P/N 147A7221-32 FROM STORES. REF: PO 855759.
REMOVED CRACKED STIFFENER IAW SRM 51-40-02.;[02] LOCATED AND DRILLED NEW STIFFENER IAW SRM 51-40-05 - [SDR SWAA2022033179922](https://openairdocs.org/sdr/SWAA2022033179922.md): Stub Frame · cracked · Mar 3, 2022 · N763SW · Boeing 737 · Fuselage Main, Frame > FWD SERVICE DOOR FWD UPPER STUB FRAME IS CRACKED / [01] ACCOMPLISHED LOCATED AND DRILLED IN TASK CARD TTG8Q00B0AYZ STEP 13.;[08] INSTALLED FWD UPPER STUB FRAME WITH 100% TEMPORARY FASTENERS AND SEALANT BMS 5-95 C20; SQUEEZE OUT AT 3/19/2021 09:20 UTC.;[09] VER - [SDR SWAA2022033180055](https://openairdocs.org/sdr/SWAA2022033180055.md): Skin · corroded · Mar 3, 2022 · N763SW · Boeing 737 · Fuselage Main, Plate/Skin > CORROSION ON UPPER FUSELAGE SKIN AT BS 1016+20 LBL 3; BS 1016+23 LBL 3; BS 1016+23 LBL 5. ACCESS FROM 323BL / [01] REMOVED 17 FASTENERS; B.S. 1016+20-B.S. 1016+24 STR 1- LBL 5.5 TO FACILITATE CORROSION REMOVAL PER SRM 51-40-02-0G-0.;[02] REMOVED CORROSION; B.S - [SDR SWAA2022033180053](https://openairdocs.org/sdr/SWAA2022033180053.md): Skin · corroded · Mar 3, 2022 · N763SW · Boeing 737 · Fuselage Miscellaneous Structure > CORROSION ON UPPER FUSELAGE SKIN AT BS 1016+25 LBL 8; BS 1016+25 RBL 6; BS 1016+29 LBL 4; BS 1016+30 LBL 6. ACCESS FROM 232BL / [01] REMOVED CORROSION ON FUSELAGE CROWN SKIN; B.S. 1040+.5 TO B.S. 1064+13; STR2L TO STR2R PER SRM 51-10-02-0G-0.;[02] VERIFIED COR - [SDR SWAA2022033179735](https://openairdocs.org/sdr/SWAA2022033179735.md): None · cracked · Mar 2, 2022 · N763SW · Boeing 737 · Cargo Compartments > CRACK ON FWD CARGO BAY STRINGER AT BS 540 L/H STRINGER 25. / CRACK ON FCB STR 25 L/H BS 536; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103 REMOVED DAMAGE BY TRIMMING OUT STRINGER SECTION AT BS 500D+11' TO 536 STR 25L. IAW SRM 53-00-03-2 - [SDR SWAA2022033179726](https://openairdocs.org/sdr/SWAA2022033179726.md): None · cracked · Mar 2, 2022 · N763SW · Boeing 737 · Cargo Compartments > CRACK ON FWD CARGO BAY STRINGER AT BS 540 L/H STRINGER 23. / [01] EVALUATED CRACK ON FCB STR 23 L/H BS 536; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103;[02] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 1.;[03] VERIFIED APPLICABILITY FO - [SDR SWAA2022033179736](https://openairdocs.org/sdr/SWAA2022033179736.md): None · cracked · Mar 2, 2022 · N763SW · Boeing 737 · Cargo Compartments > CRACK ON FWD CARGO BAY STRINGER AT BS 540 L/H STRINGER 26. / CRACK ON FCB STR 26 L/H BS 536; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103;[02] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 1.;[03] VERIFIED APPLICABILITY FOR STR 26 L/H IA - [SDR SWAA2022033179727](https://openairdocs.org/sdr/SWAA2022033179727.md): Stringer · cracked · Mar 2, 2022 · N763SW · Boeing 7377H4 · Cargo Compartments > CRACK ON FWD CARGO BAY STRINGER AT BS 540 L/H STRINGER 27. / CRACK ON FCB STR 27 L/H BS 536; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103. REMOVED DAMAGE BY TRIMMING OUT STRINGER SECTION AT BS 500D+11' TO 536 STR 27L. IAW SRM 53-00-03- - [SDR SWAA2022033179737](https://openairdocs.org/sdr/SWAA2022033179737.md): Stringer · cracked · Mar 2, 2022 · N763SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CRACK ON FWD CARGO BAY STRINGER AT BS 540 R/H STRINGER 25. / [01] EVALUATED CRACK ON FCB STR 25 R/H BS 536; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103;[08] RECEIVED NEW STRINGER SECTION (1 EA) P/N: HFAB53-STR-011; LOT:1484566-1; P - [SDR SWAA2022033179728](https://openairdocs.org/sdr/SWAA2022033179728.md): Stringer · cracked · Mar 2, 2022 · N763SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CRACK ON FWD CARGO BAY STRINGER AT BS 540 R/H STRINGER 23. / [01] EVALUATED CRACK ON FCB STR 23 R/H BS 536; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103[17] INSTALLED NEW STRINGER SECTION AND HAT SECTION REPAIR BTW B/S 500D-540 STR 23R - [SDR SWAA2022033179729](https://openairdocs.org/sdr/SWAA2022033179729.md): Stringer · cracked · Mar 2, 2022 · N763SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > CRACK ON FWD CARGO BAY STRINGER AT BS 540 R/H STRINGER 26. / [01] EVALUATED CRACK ON FCB STR 26 R/H BS 536; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103;[08] RECEIVED NEW STRINGER SECTION ITEM: HFAB53-STR-011 LOT: 1484419-1 PO/N: 85906 - [SDR SWAA2022033179738](https://openairdocs.org/sdr/SWAA2022033179738.md): Stringer · cracked · Mar 2, 2022 · N763SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > DAMAGE ON FWD CARGO BAY STRINGER AT BS 540 R/H STRINGER 22. / [01] EVALUATED CRACK ON FCB STR 22 R/H BS 536; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103;[12] FABRICATED AND LOCATED AND DRILLED NEW REPAIR PARTS AT FCB BTW BS 500D+6' TO - [SDR SWAA2022033179739](https://openairdocs.org/sdr/SWAA2022033179739.md): Stringer · cracked · Mar 2, 2022 · N763SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer > DAMAGE ON FWD CARGO BAY STRINGER AT BS 540 R/H STRINGER 24. / [01] EVALUATED CRACK ON FCB STR 24 R/H BS 536; STRINGER DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A-1 FIG 103[07] RECEIVED; AND VERIFIED NEW STRINGER SECTION HFAB53-STS-011 FORMED; HEAT TREAT - [SDR SWAA2022033179741](https://openairdocs.org/sdr/SWAA2022033179741.md): Gusset · cracked · Mar 2, 2022 · N763SW · Boeing 737 · Fuselage Miscellaneous Structure > CRACK ON FWD CARGO BAY GUSSET AT BS 500D R/H STRINGER 19. / [01] NO ALLOWABLE DAMAGE FOUND IN B737-700 SRM FOR A CRACK ON FWD CARGO BAY GUSSET AT BS 500D R/H STRINGER 19. REPAIR BY REPLACEMENT IAW SRM 51-10-02.;[02] RECEIVED NEW GUSSET ASSY P/N 143A9481-5 FROM - [SDR SWAA2022033179732](https://openairdocs.org/sdr/SWAA2022033179732.md): Support · corroded · Mar 2, 2022 · N763SW · Boeing 737 · Fuselage Miscellaneous Structure > CORROSION ON FWD CARGO BAY LOWER BULKHEAD SUPPORT AT BS 395 LBL 23-RBL 22. / [01] REMOVED LOWER BULKHEAD SUPPORT IAW SRM 51-40-02.;[02] CORROSION ON FWD CARGO BAY LOWER BULKHEAD SUPPORT AT BS 395 LBL23 - RBL 22. NO ALLOWABLE DAMAGE PER SRM.

PART TO BE - [SDR SWAA2022033179742](https://openairdocs.org/sdr/SWAA2022033179742.md): Support · corroded · Mar 2, 2022 · N763SW · Boeing 737 · Fuselage Miscellaneous Structure > CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 420+5; BS 440+14; BS 460+10; BS 460+10; BS 460+14; BS 500+10; BS 500+14; BS 500+18. / [01] REMOVED CORROSION FWD CARGO BAY TO SIDEWALL SUPPORT AT LBL 24 BS 420+5;TO BS 500+18;IAW SRM 51-10-02; P - [SDR SWAA2022033179743](https://openairdocs.org/sdr/SWAA2022033179743.md): Support · corroded · Mar 2, 2022 · N763SW · Boeing 737 · Fuselage Miscellaneous Structure > CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 500A+2; BS 500A+10; BS 500A+14; BS 500A+18; BS 500B+7; BS 500B+10; BS 500C+2; BS 500C+10. / [01] REMOVED CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT;AT LBL 24;BTW BS500A+2 TO BS 500C+1 - [SDR SWAA2022033179745](https://openairdocs.org/sdr/SWAA2022033179745.md): None · corroded · Mar 2, 2022 · N763SW · Boeing 737 · Fuselage Miscellaneous Structure > CORROSION ON FWD CARGO BAY FWD DOOR SHIELD AT RBL 23 BS 420+7; BS 420+12; BS 420+19. / [01] REMOVED FWD DOOR SHIELD AT FCB RBL 23 BS420 - BS440. RECEIVED NEW SHIELD ASSY ITEM: 143A8126U21ATSMRO LOT: 1474950-1. LOCATED AND DRILLED NEW SHIELD IAW SRM 51-40-02; S - [SDR SWAA2022033179746](https://openairdocs.org/sdr/SWAA2022033179746.md): Shield · corroded · Mar 2, 2022 · N763SW · Boeing 737 · Fuselage Miscellaneous Structure > CORROSION ON FWD CARGO BAY AFT DOOR SHIELD AT RBL 23 BS 480+13; BS 500+6; BS 500+10; BS 500+14; BS 500+18. / [01] NOT ALLOWABLE DAMAGE FOUND ON SRM; PART MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] LOCATED AND DRILLED ON FWD CARGO BAY AFT DOOR NEW SHIE - [SDR SWAA2022033179747](https://openairdocs.org/sdr/SWAA2022033179747.md): Threshold Web · corroded · Mar 2, 2022 · N763SW · Boeing 737 · Fuselage Main, Structure > CORROSION ON FWD CARGO BAY DOOR THRESHOLD AT RBL 29 BS 460+12. / [01] SRM 53-30-15-1A-1 IS APPLICABLE

REMOVED CORROSION FROM FWD CARGO BAYI DOOR THRESHOLD WEB AT RBL29 BS460+12 N AREA OF 2.2'X1.2'X.005' ORIGINAL MATERIAL THICKNESS.045' FOUND TO BE OUT - [SDR SWAA2022033179734](https://openairdocs.org/sdr/SWAA2022033179734.md): Strap · corroded · Mar 2, 2022 · N763SW · Boeing 737 · Fuselage Miscellaneous Structure > CORROSION ON FWD CARGO BAY DOOR CUTOUT AFT STRAP AT BS 480+13 JUST ABOVE R/H STRINGER 24.(MARKED) CORROSION ON FWD CARGO BAY DOOR CUTOUT AFT STRAP AT BS 480+13 JUST ABOVE R/H STRINGER 24. / [01] SRM 53-30-15-1A-1 HAS BEEN FOUND TO BE APPLICABLE FOR THIS EVALUA - [SDR SWAA2022033179724](https://openairdocs.org/sdr/SWAA2022033179724.md): Panel · corroded · Mar 2, 2022 · N763SW · Boeing 737* · Fuselage Main, Structure > PANEL 113AC MATING SURFACE HAS MINOR FRETTING CORROSION AND BARE METAL / [01] REMOVED MINOR FRETTING CORROSION FROM PNL 113AC MEASURED 6'L X 1'W AND 0.003' DEEP FOUND IN LIMITS PER SRM 53-10-14-1A-2;[02] REMOVED MINOR FRETTING CORROSION FROM PNL 113AC MEASURED - [SDR SWAA2022033179733](https://openairdocs.org/sdr/SWAA2022033179733.md): Support · corroded · Mar 2, 2022 · N763SW · Boeing 737* · Fuselage Miscellaneous Structure > CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500A+2; BS 500A+7; BS 500A+12; BS 500A+16; BS 500B+6; BS 500B+10; BS 500B+14; BS 500B+18; BS 500C+1. CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500A+2 BS 500A+7 BS 500A+12 - [SDR SWAA2022033179333](https://openairdocs.org/sdr/SWAA2022033179333.md): Attach Angle · cracked · Mar 1, 2022 · N763SW · Boeing 7377H4 · Cargo Compartments > CRACK ON AFT CARGO BAY LOWER BULKHEAD ATTACH ANGLE AT LBL 11 BS 947+1. / [01] ENTERED MEASUREMENTS;[02] NO ALLOWABLE DAMAGE FOUND FOR THIS PART IN B737-700 SRM.
REPAIR BY REPLACEMENT IAW SRM 51-10-02.
RECEIVED A NEW SUPPORT FITTING P/N 149A8113U6 FROM ST - [SDR SWAA2022033179334](https://openairdocs.org/sdr/SWAA2022033179334.md): Frame · cracked · Mar 1, 2022 · N763SW · Boeing 7377H4 · Cargo Compartments > CRACK ON AFT CARGO FRAME AT RBL 17 BS 907. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-07-1A-1 ALLOWABLE DAMAGE 1 AND SRM 53-70-07-0I-1 IDENTIFICATION 1;[02] EVALUATED FRAME; CRACK LENGTH: 1' FOUND OUT ALLOWABLE DAMAGE LIMITS IAW S - [SDR SWAA2022033179347](https://openairdocs.org/sdr/SWAA2022033179347.md): Rail · cracked · Mar 1, 2022 · N763SW · Boeing 737 · Cargo Compartments > CRACK ON AFT CARGO BAY RAIL AT LBL 17 BS 767. / [01] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS;[02] CRACK ON AFT CARGO BAY RAIL AT LBL 17; BS 767; L 0.500 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2;[03] VERIFIED CORRECTIVE ACTION STEP 1 AND 2.;[04] REMOVE - [SDR SWAA2022033179332](https://openairdocs.org/sdr/SWAA2022033179332.md): Bulkhead · corroded · Mar 1, 2022 · N763SW · Boeing 737 · Fuselage Main, Bulkhead > CORROSION ON AFT CARGO BAY LOWER BULKHEAD AT BS 947 RBL 21-LBL 10. / [01] LOCATED AND DRILLED NEW TRACK P/N149A8118 IAW SRM 51-40-02 OK TO INSTALL;[02] VERIFIED CORRECTIVE ACTION 1.;[03] INSTALLED 10 HI-LOCK IAW SRM 51-40-02 AND DWG 149A8110 ID:0013 REV:B;[04] - [SDR SWAA2022033179337](https://openairdocs.org/sdr/SWAA2022033179337.md): Support · corroded · Mar 1, 2022 · N763SW · Boeing 737* · Fuselage Miscellaneous Structure > CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 907+6; BS 907+10; BS 907+13; BS 907+17. / [01] REMOVED CORROSION FROM ACB FLOOR TO SIDEWALL SUPPORT RBL21 BS 907+6 MEASURED 1.3'L X 1'W AND 0.005' DEEP FOUND OUT OF LIMITS

REMOVED CORROSI - [SDR SWAA2022033179339](https://openairdocs.org/sdr/SWAA2022033179339.md): Rail · corroded · Mar 1, 2022 · N763SW · Boeing 737 · Fuselage Miscellaneous Structure > CORROSION ON AFT CARGO BAY RAIL AT LBL 3 BS 927. / [01] ENTERED MEASUREMENTS;[02] VERIFIED SRM 53-00-53-1A-2 ALLOWABLE DAMAGE IS APPLICABLE
REMOVED CORROSION IAW SRM 51-10-02.
BLENDED AREA MEASURES 0.75' X 1.00' X 0.018'
ORIGINAL MATERIAL THICKNESS 0 Next page: https://openairdocs.org/deregistered/N763SW-2024-10-29/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N763SW' AND deregistration_id = 'N763SW-2024-10-29' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N763SW-2024-10-29/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.