# Service difficulty reports: N762SW, cancelled Oct 30, 2024

A list on [N762SW, cancelled Oct 30, 2024](https://openairdocs.org/deregistered/N762SW-2024-10-30.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 7 · 316 reports

- [SDR SWAA2024022755939](https://openairdocs.org/sdr/SWAA2024022755939.md): Battery Pack · inoperative · Feb 25, 2024 · N762SW · Boeing 7377H4 · Emergency Lighting
  > FWD EMERGENCY LIGHTS INOP<[01] R/R FWD LH EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06
- [SDR SWAA2024020848799](https://openairdocs.org/sdr/SWAA2024020848799.md): Fan · smoke · Feb 5, 2024 · N762SW · Boeing 7377H4 · Air Distribution Fan
  > BURN RUBBER SMELL DURING CRUISE ROWS 7-11. NO SMOKE NOTED BY FAS. TURNED R PACK OFF AND SMELL WENT AWAY.<[01] COMPLIED WITH CONDITIONAL INSPECTION OF SMOKE OR FUMES IN THE CABIN IN REFERENCE TO AMM 05-51-56. REFERENCE LOG PAGE 2665117 FOR R&R RECIRC FAN
- [SDR SWAA2024010938073](https://openairdocs.org/sdr/SWAA2024010938073.md): Floor Panel · cracked · Jan 5, 2024 · N762SW · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT AFT FLOOR LINER CRACKED OUT OF LIMITS PER SRM 53-00-53-1A-1<[01] OK TO CONTINUE PER MEL 25-5-02 SP1B AUTH 173964;[02] REMOVED AND REPLACED FWD CARGO COMPARTMENT AFT LINER FLOOR REFERENCE AMM25-52-10. NO FURTHER DEFECTS NOTED.
- [SDR SWAA2023101811056](https://openairdocs.org/sdr/SWAA2023101811056.md): Pitot System · failed · Oct 15, 2023 · N762SW · Boeing 7377H4 · Pitot/Static System
  > AIRSPEED DISAGREE AFTER T/O. F/O INDICATION APPEARED CORRECT.<[01] PERFORMED ADIRS BITE IAW FIM 34-21 TASK 801. NO INFLIGHT FAULT FOUND. 1 PREVIOUS LEG FAULT FOR TAT PROBE FAIL. 34-21022. SEE L/P#2514346 FOR FINAL REPAIR.;[02] REF LOGPAGE# 2514349 FOR FINAL RE
- [SDR SWAA2023062670970](https://openairdocs.org/sdr/SWAA2023062670970.md): Engine · hung start · Jun 23, 2023 · N762SW · Boeing 7377H4 · Engine (Turbine/Turboprop)
  > ENG #1 REQUIRED A RESTART AFTER A HUNG START. 2ND ENGINE START NORMAL INCLUDING ALL INDICATION. APPROX 5 MIN LATER PAX REPORTED FLAMES FROM #1<[01] C/W FIM TASK 71-05-811; NO DEFECTS NOTED. VERIFIED OIL CONSUMPTION WITHIN LIMITS. (.431/HR).
- [SDR SWAA2023061256855](https://openairdocs.org/sdr/SWAA2023061256855.md): Doubler · cracked · Jun 7, 2023 · N762SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER HAS CRACK DAMAGE ON FORWARD LOWER CORNER THAT EXTENDS UNDERNEATH AIRCRAFTS FUSELAGE SKIN THEREFORE BEING OUT OF LIMITS PER ALLOWABLE DAMAGE LIMITS. ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER HAS CRAC
- [SDR SWAA2023051546898](https://openairdocs.org/sdr/SWAA2023051546898.md): Fairing · delaminated · May 9, 2023 · N762SW · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > LH ENGINE AFT STRUT FAIRING 431ER PANEL DELAMINATED.<[01] REMOVED AND REPLACED PANEL 431ER REF AMM 54-53-01
- [SDR SWAA2023020297050](https://openairdocs.org/sdr/SWAA2023020297050.md): Girt Bar · loose · Jan 31, 2023 · N762SW · Boeing 7377H4 · Escape Slide
  > AFT SERVICE DOOR GIRT BAR IS LOOSE<[01] RE-SECURED AFT SERVICE DOOR GIRT BAR PER S.I.P
- [SDR SWAA2022102865554](https://openairdocs.org/sdr/SWAA2022102865554.md): Megaphone · inoperative · Oct 27, 2022 · N762SW · Boeing 7377H4 · Emergency Equipment
  > F/A REPORTS MEGAPHONE INOP / [01] REMOVED AND REPLACED FORWARD GALLEY MEGAPHONE AMM 25-64-00
- [SDR SWAA2022101258601](https://openairdocs.org/sdr/SWAA2022101258601.md): None · loose · Oct 12, 2022 · N762SW · Boeing 7377H4 · Wing, Control Surfaces
  > LEFT WING LOWER T/E PANEL NOT SECURE AT BRACKET I/B OF PYLON FAIRING / [01] REMOVED AND REPLACED LOWER ATTACHMENT BRACKET ASSY FOR THE LEFT WING LOWER T/E PANEL I/B OF PYLON FAIRING PER AMM 57-50-02
- [SDR SWAA2022101258597](https://openairdocs.org/sdr/SWAA2022101258597.md): Support · cracked · Oct 12, 2022 · N762SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT WING #8 SLAT I/B AUX TRACK SKIN TAB I/B TAB SUPPORT IS CRACKED. / [01] R&R RIGHT WING #8 SLAT I/B AUX TRACK SKIN TAB I/B SUPPORT AS PER AMM 27-81-00 AND AMM 20 50-11.
- [SDR SWAA2022082947157](https://openairdocs.org/sdr/SWAA2022082947157.md): Slide · out of position · Aug 27, 2022 · N762SW · Boeing 7377H4 · Escape Slide
  > RH AFT SERVICE SLIDE HANGING LOOSE / [01] REPOSTIONED R2 SLIDE PER MM25-66-01
- [SDR SWAA2022082243976](https://openairdocs.org/sdr/SWAA2022082243976.md): Girt Bar · out of position · Aug 19, 2022 · N762SW · Boeing 7377H4 · Passenger/Crew Doors
  > FWD ENTRY GIRT BAR NEEDS ADJUSTMENT / [01] PROPERLY STOWED ESCAPE SLIDE GIRT BAR FLAP MATERIAL IAW AMM 25-66-01.
- [SDR SWAA2022050200284](https://openairdocs.org/sdr/SWAA2022050200284.md): Handle · out of position · Apr 27, 2022 · N762SW · Boeing 7377H4 · Escape Slide
  > R-1 DOOR SLIDE; MANUAL INFLATION HANDLE COVER NOT SECURED R-1 DOOR SLIDE MANUAL INFLATION HANDLE COVER NOT SECURED / [01] SECURED FLAP IAW AMM 25-66-00
- [SDR SWAA2022050200285](https://openairdocs.org/sdr/SWAA2022050200285.md): Handle · out of position · Apr 27, 2022 · N762SW · Boeing 7377H4 · Escape Slide
  > R-2 DOOR SLIDE; MANUAL INFLATION HANDLE COVER NOT SECURED R-2 DOOR SLIDE MANUAL INFLATION HANDLE COVER NOT SECURED / [01] SECURED FLAP IAW AMM 25-66-00
- [SDR SWAA2022042596123](https://openairdocs.org/sdr/SWAA2022042596123.md): Light · inoperative · Apr 21, 2022 · N762SW · Boeing 7377H4 · Emergency Lighting
  > L1 DOOR EMERGENCY EXIT LIGHT 1 BULB INOP / [01] RESECURED EMERGENCY EXIT LIGHT DOOR L1 AS PER B737-AMM 33-51-01-960-801.PERFORMED EMERGENCY LIGHT TEST FOUND NORMAL.;[02] VERIFIED STEP 1
- [SDR SWAA2022042095340](https://openairdocs.org/sdr/SWAA2022042095340.md): Light · inoperative · Apr 18, 2022 · N762SW · Boeing 737* · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INSIDE CABIN AND OUTSIDE INOPS / [01] REMOVED AND REPLACED BATTERY PACK AT M1670;M1674;M1672 AND M1668 POSITIONS AS PER REF B737; AMM 33-51-06-960-805.PERFORMED BATTERY PACK SYSTEM TEST AND FOUND NORMAL. REMOVED AND REPLACED BATTERY
- [SDR SWAA2022042095916](https://openairdocs.org/sdr/SWAA2022042095916.md): Light · inoperative · Apr 18, 2022 · N762SW · Boeing 737* · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INSIDE CABIN AND OUTSIDE INOPS / [01] REMOVED AND REPLACED BATTERY PACK AT M1670;M1674;M1672 AND M1668 POSITIONS AS PER REF B737; AMM 33-51-06-960-805.PERFORMED BATTERY PACK SYSTEM TEST AND FOUND NORMAL.
- [SDR SWAA2022042095917](https://openairdocs.org/sdr/SWAA2022042095917.md): Light · inoperative · Apr 18, 2022 · N762SW · Boeing 737* · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INSIDE CABIN AND OUTSIDE INOPS / [01] REMOVED AND REPLACED BATTERY PACK AT M1670;M1674;M1672 AND M1668 POSITIONS AS PER REF B737; AMM 33-51-06-960-805.PERFORMED BATTERY PACK SYSTEM TEST AND FOUND NORMAL.
- [SDR SWAA2022042095918](https://openairdocs.org/sdr/SWAA2022042095918.md): Light · inoperative · Apr 18, 2022 · N762SW · Boeing 737* · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INSIDE CABIN AND OUTSIDE INOPS / [01] REMOVED AND REPLACED BATTERY PACK AT M1670;M1674;M1672 AND M1668 POSITIONS AS PER REF B737; AMM 33-51-06-960-805.PERFORMED BATTERY PACK SYSTEM TEST AND FOUND NORMAL.
- [SDR SWAA2022042593740](https://openairdocs.org/sdr/SWAA2022042593740.md): Baffle · cracked · Apr 13, 2022 · N762SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAFFLE AT STA.400-STA.420; STR.26L; WL 206; CRACKED / [01] REMOVED BAFFLE AT FWD CARGO COMPARTMENT BETWEEN FS 400-420 STR 26L WL 206 IN REF B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED BAFFLE AT FWD CARGO COMPARTMENT BETWEEN FS 400-420 STR 26L
- [SDR SWAA2022042093513](https://openairdocs.org/sdr/SWAA2022042093513.md): Panel · corroded · Apr 12, 2022 · N762SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION.....AFT CARGO COMPARTMENT AFT BULKHEAD PANEL 141UW HAS EXFOLIATED CORROSION. / [01] RECEIVED NEW AFT CARGO PANEL 141 UW; NEW PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00ASNPF;[02] VERIFIED STEP 1.
- [SDR SWAA2022042590886](https://openairdocs.org/sdr/SWAA2022042590886.md): Strip · elongated · Apr 3, 2022 · N762SW · Boeing 7377H4 · Cargo/Baggage Doors
  > AFT CARGO L/H CAP STRIP P/N 453A2611-8 WITH HOLES ELONGATED / [01] RECEIVED NEW AFT CARGO CAP STRIP P/N 453A2611-8; NEW STRIP TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004GEP0; T/C 5360-E-16462-NG;[02] VERIFIED STEP 1.
- [SDR SWAA2022042590887](https://openairdocs.org/sdr/SWAA2022042590887.md): Strip · elongated · Apr 3, 2022 · N762SW · Boeing 7377H4 · Cargo/Baggage Doors
  > AFT CARGO L/H CAP STRIPS P/N 453A2611-10 AND 543A2611-4 HOLES ELONGATED / [01] RECEIVED NEW CAP STRIPS P/NS 453A2611-10 AND 453A2611-4; NEW CAP STRIPS TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004GEP0;[02] VERIFIED STEP 1.
- [SDR SWAA2022042090559](https://openairdocs.org/sdr/SWAA2022042090559.md): Cap Seal · elongated · Apr 1, 2022 · N762SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H CAP STRIPS WITH HOLES ELONGATED / [01] RECEIVED NEW AFT CARGO CAP STRIPS 2 EACH;P/N 453A2611-11 AND 453A 2611-9; NEWS CAP STRIPS TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004GEPO; 5360-E-16462-NG;[02] ORRECTION RECEIVED NEW AFT CARGO CAP STRIPS
- [SDR SWAA2022042589243](https://openairdocs.org/sdr/SWAA2022042589243.md): Channel · corroded · Mar 29, 2022 · N762SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT LH Z CHANNEL STA 400 TO STA 500D HAS SEVERAL SPOTS OF CORROSION AT HOLE SCREW. CORROSION AT HOLES AUTOMATICALLY OUT OF LIMITS / [01] LOCATED AND DRILLED L/H ZEE CHANNEL STA.400 TO STA.500D REF. B737-7 SRM 51-40-05-0G-0;[02] VERIFIED STEP
- [SDR SWAA2022042589244](https://openairdocs.org/sdr/SWAA2022042589244.md): Channel · corroded · Mar 29, 2022 · N762SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT RH Z CHANNEL STA 500A TO STA 500D HAS SEVERAL SPOTS OF CORROSION AT HOLE SCREW. CORROSION AT HOLES AUTOMATICALLY OUT OF LIMITS / [01] LOCATED AND DRILLED R/H ZEE CHANNEL REF. B737-7 SRM 51-40-05-0G-0;[02] VERIFIED STEP 1;[03] OK TO TREAT
- [SDR SWAA2022042589245](https://openairdocs.org/sdr/SWAA2022042589245.md): Channel · corroded · Mar 29, 2022 · N762SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT RH Z CHANNEL STA 400 TO STA 420 HAS SPOTS OF CORROSION AT HOLE SCREW. CORRODED AROUND HOLES AUTOMATICALLY OUT OF LIMITS / [01] LOCATED AND DRILLED R/H ZEE CHANNEL REF. B737-7 SRM 51-40-05-0G-0;[02] VERIFIED STEP 1;[03] OK TO TREAT AND PRI
- [SDR SWAA2022042589240](https://openairdocs.org/sdr/SWAA2022042589240.md): Strap · corroded · Mar 29, 2022 · N762SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT LH AFT STRAP SUPPORT HAS SEVERAL SPOTS OF CORROSION. / [01] LOCATED AND DRILLED L/H AFT STRAP REF. B737-7 SRM 51-40-05-0G-0;[02] VERIFIED STEP 1. OK TO TREAT AND PRIME.;[03] TREATED AND PRIMED STRAP FASTENER HOLES REF. B737-7 SRM 51-20-01
- [SDR SWAA2022042588760](https://openairdocs.org/sdr/SWAA2022042588760.md): Splice · corroded · Mar 28, 2022 · N762SW · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT STA 767 SPLICER HAS SURFACE CORROSION / [01] REMOVED CORROSION ON FLOOR SPLICE STRAP PER REF. 737SRM 51-10-02-0G-0;[02] CORROSION PASS THROUGH OUT OF LIMITS PER SRM 53-00-53-1A-2;[03] VALIDATED STEPS 1 & 2;[04] RECEIVED NEW FLOOR SPLICE '
- [SDR SWAA2022042588870](https://openairdocs.org/sdr/SWAA2022042588870.md): Angle · corroded · Mar 28, 2022 · N762SW · Boeing 7377H4 · Fuselage Floor Panel
  > FLIGHT COMPARTMENT ENTRANCE; FLOOR AREA BS259.5 TO BS 270 BL 0 WL 208 AREA WITH CORROSION / [01] INSTALLED EWIS PROTECTION AT FLOOR STRUCTURE FLIGHT DECK ENTRANCE BETWEEN BS259.5 TO BS270 BL 0 WL208 AS PER B737-7 AMM 20-60-07-913-801.[21] FABRICATED AND DRILLE
- [SDR SWAA2022042588589](https://openairdocs.org/sdr/SWAA2022042588589.md): Stringer Splice · corroded · Mar 27, 2022 · N762SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > STRINGER 27L SPLICE AT STA. 370 CORRODED / [01] REMOVED CORROSION ON STR27L SPLICE STA. 370; REF. B737-7 SRM 51-10-02-0G-0;[02] ORIGINAL MATERIAL 0.045'; MATERIAL REMOVED 0.022'; MATERIAL REMAINING 0.023' FOUND OUT OF LIMITS REF. B737-7 SRM 53-00-03-1A-1;[03]
- [SDR SWAA2022042588590](https://openairdocs.org/sdr/SWAA2022042588590.md): Stringer · corroded · Mar 27, 2022 · N762SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > STRINGER 27L CORRODED FWD OF STA. 370 SPLICE / [01] FOUND CORR. ON STRINGER OUT OF LIMITS; CORRODED THRU; REF. B737-7 SRM 53-00-03-1A-1;[02] REMOVED FASTENERS BETWEEN STA 300 TO STA 326 STR 27L FORM AIRCRAFT SHORING ACCESS REF B737-7 SRM 51-40-02-0G-0;[03] VER
- [SDR SWAA2022042588592](https://openairdocs.org/sdr/SWAA2022042588592.md): Stringer Splice · corroded · Mar 27, 2022 · N762SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > STRINGER 26L SPLICE AT STA. 370 CORRODED / [01] REMOVED CORROSION ON STR26L SPLICE STA. 370; REF. B737-7 SRM 51-10-02-0G-0;[02] ORIGINAL MATERIAL 0.045'; MATERIAL REMOVED 0.020'; MATERIAL REMAINING 0.025' FOUND OUT OF LIMITS REF. B737-7 SRM 53-00-03-1A-1;[03]
- [SDR SWAA2022042588591](https://openairdocs.org/sdr/SWAA2022042588591.md): Stringer · corroded · Mar 27, 2022 · N762SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > STRINGER 26L CORRODED FWD OF STA. 370 SPLICE / [01] FOUND CORR. ON STRINGER 26L; OUT OF LIMITS; CORRODED THRU; REF. B737-7 SRM 53-00-03-1A-1;[15] INSTALLED NEW STRINGER SECTION 26 L; FROM STA. 294.4 TO STA. 360; PER REF 737-700 SRM 51-40-02-0G-0 AND DRAWING 1
- [SDR SWAA2022042088593](https://openairdocs.org/sdr/SWAA2022042088593.md): Stringer · corroded · Mar 27, 2022 · N762SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > STRINGER 25L SPLICE AT STA. 370 CORRODED / [01] REMOVED CORROSION ON STR25L SPLICE STA. 370; REF. B737-7 SRM 51-10-02-0G-0;[02] ORIGINAL MATERIAL 0.045'; MATERIAL REMOVED 0.018'; MATERIAL REMAINING 0.027' FOUND OUT OF LIMITS REF. B737-7 SRM 53-00-03-1A-1;[03]
- [SDR SWAA2022042586861](https://openairdocs.org/sdr/SWAA2022042586861.md): Channel · corroded · Mar 24, 2022 · N762SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H Z CHANNEL FROM STA 727 TO STA 767; RBL 33.5 AND WL 156.4 WITH DEEP CORROSION AT NUT PLATE HOLES / [01] REMOVED CORROSION ON AFT CARGO Z CHANNEL FROM STA 727 TO STA 767 I.A.W. SRM 51-10-02-0G-0; OUT OF LIMITS PASS THROUGH.;[02] CORRECTION TO STEP
- [SDR SWAA2022042586847](https://openairdocs.org/sdr/SWAA2022042586847.md): Shield · corroded · Mar 23, 2022 · N762SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO;CARGO DOOR SURROUND STRUCTURE AFT SHIELD CORRODED AT TOP SURFACE. / [01] REMOVED CORROSION ON AFT SHIELD REF. B737-7 SRM 51-10-02-0G-0 FOUND SEVERAL CRACKS ON PANEL OUT OF LIMITS REF. B737-7 SRM 53-30-15-1A-1;[02] RECEIVED NEW SHIELD AT FWD CARGO COM
- [SDR SWAA2022042586859](https://openairdocs.org/sdr/SWAA2022042586859.md): Channel · corroded · Mar 23, 2022 · N762SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT L/H Z CHANNEL FROM STA. 727 TO STA 847 AT NUT PLATE HOLES WITH DEEP CORROSION / [01] REMOVED CORROSION ON AFT L/H CARGO Z CHANNEL FROM STA 727 TO STA 847 I.A.W. SRM 51-10-02-0G-0; OUT OF LIMITS PASS THROUGH I.A.W 53-00-53-1A-2.;[02] VERIF
- [SDR SWAA2022042585953](https://openairdocs.org/sdr/SWAA2022042585953.md): Strap · corroded · Mar 22, 2022 · N762SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > T FLOOR SPLICE AT STA 727D + 5 WITH DEEP CORROSION. / [01] FOUND EXFOLIATE CORROSION ON FLOOR SPLICE STRAP AT STA 727 D +5; OUT OF LIMITS PER REF 737 -700 SRM 53-00-53-1A-2;[02] VERIFIED STEP 1.;[03] RECEIVED NEW FLOOR SPLICE STRAP P/N 146A9401-8; NEW STRAP TO
- [SDR SWAA2022042090138](https://openairdocs.org/sdr/SWAA2022042090138.md): Panel · elongated · Mar 22, 2022 · N762SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > PANEL 193AR HAS SEVERAL HOLE SCREWS ELONGATED / [01] PREPARED FOR REPAIR AT PANEL 193 AR AS PER B 737-700 SRM 51-70-06-2R-9;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED AT PANEL 193AR;AS PER B737-700 SRM 51-70-06-2R-9 MATERIAL USED PO.1690463 AND P
- [SDR SWAA2022042086835](https://openairdocs.org/sdr/SWAA2022042086835.md): Handle · cracked · Mar 22, 2022 · N762SW · Boeing 7377H4 · Emergency Exits
  > MAIN CABIN R/H EMERGENCY EXIT DOOR HANDLE IS CRACK / [01] REMOVED AND REPLACED R/H EMERGENCY EXIT DOOR HANDLE ASPER B737-700 AMM 52-22-51-000-801;[02] VERIFIED STEP 1
- [SDR SWAA2022042086838](https://openairdocs.org/sdr/SWAA2022042086838.md): Stringer · corroded · Mar 22, 2022 · N762SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > STRINGER 25L CORRODED BETWEEN BS 360 & 380. REMOVED FASTENERS IAW SRM 51-40-02-0G-0. REMOVED STRINGER SPLICE IAW SRM 51-40-02-0G-0. FOUND S25L OUT OF LIMITS IAW SRM 53-00-03-1A-1. LOCATED & DRILLED A NEW STRINGER IAW SRM 51-40-02-0G-0. TREATED & PRIMED STR
- [SDR SWAA2022042086561](https://openairdocs.org/sdr/SWAA2022042086561.md): Stringer · corroded · Mar 22, 2022 · N762SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > FOUND STR27L WITH EXFOLIATING CORROSION BETWEEN STA.360 & STA.380 STRINGER 27L FROM STA 370 SPLICE TO AFT / [01] REMOVED FASTENERS AND EXISTING STRINGER SPLICE AT FUSELAGE SKIN S-27L BETWEEN STA 351.2 AND STA 380 REF B7373-700 SRM 51-40-02-0G-0.;[24] INSTALLED
- [SDR SWAA2022042585933](https://openairdocs.org/sdr/SWAA2022042585933.md): Panel · delaminated · Mar 20, 2022 · N762SW · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > ACCESS PANEL 431ER SKIN CORNER SECTION DELAMINATED / [01] PREPARED FOR REPAIR AT PANEL 431ER AS PER B 737-700 SRM 51-70-04-2R-13;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED AT PANEL 431 ER AS PER B 737-700 SRM 51-70-04-2R-13 MATERIAL USED PO.169046
- [SDR SWAA2022042085937](https://openairdocs.org/sdr/SWAA2022042085937.md): Floor Panel · elongated · Mar 20, 2022 · N762SW · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT FLOOR PANEL 120AF; HOLES ENLONGATED / [01] FABRICATED FWD CARGO COMPARTMENT FLOOR PANEL 120AF AS PER B737-700 AMM 25-52-01-201-801;[02] VERIFIED STEP 1
- [SDR SWAA2022042593959](https://openairdocs.org/sdr/SWAA2022042593959.md): Panel · elongated · Mar 19, 2022 · N762SW · Boeing 7377H4 · Aerodynamic Fairings
  > ACCESS PANEL 193CL SCREW HOLES ENLONGATED / [01] PREPARED FOR REPAIR AT PANEL 193 CL AS PER B737- SRM 51-70-06-2R-9;[02] VERIFIED STEP #1.;[03] REPAIRED AT PANEL 193 CL AS PER B 737-700 SRM 51-70-06-2R-9 MATERIAL USED PO.1690463;PO. 1760049;[04] VERIFIED STEP
- [SDR SWAA2022042585903](https://openairdocs.org/sdr/SWAA2022042585903.md): Fitting · loose · Mar 19, 2022 · N762SW · Boeing 7377H4 · Emergency Exits
  > CABIN PASSENGER R1 DOOR GIRT BAR FWD FITTING LOOSE / [01] REMOVED AND REPLACED (2) SCREWS AT CABIN PASSENGER R1 DOOR GIRT BAR FWD FITTING ASPER B 737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP COMPLETED
- [SDR SWAA2022042585918](https://openairdocs.org/sdr/SWAA2022042585918.md): Floor Panel · frayed · Mar 19, 2022 · N762SW · Boeing 7377H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PNL 241DF;TOP SURFACE FRAYED ON GLASS FABRIC ALONG THE WHOLE PANEL. / [01] PERFORMED VISUAL INSPECTION AT FLOOR PANEL #241DF FOUND OUT LIMITS AS PER B-737 SRM53-00-50-1A-1;[02] VERIFIED STEP 1;[03] REMOVED CENTER PANEL 241 DF AS PER B737-700
- [SDR SWAA2022042585919](https://openairdocs.org/sdr/SWAA2022042585919.md): Floor Panel · frayed · Mar 19, 2022 · N762SW · Boeing 7377H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PNL 241AF;TOP SURFACE FRAYER ON GLASS FABRIC ALONG THE WHOLE PANEL. / [01] ACCOMPLISHED VISUAL INSPECTION AT FLOOR PANEL #241AF FOUND OUT LIMITS AS PER B-737 SRM 53-00-50-1A-1.;[02] VERIFIED STEP 1;[03] REMOVED CENTER PANEL 241 AF AS PER B737

Next page: https://openairdocs.org/deregistered/N762SW-2024-10-30/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 = 'N762SW' AND deregistration_id = 'N762SW-2024-10-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N762SW-2024-10-30/reports

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