# Service difficulty reports: N783SW

A list on [N783SW](https://openairdocs.org/aircraft/N783SW.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 · 363 reports

- [SDR SWAA2023091901688](https://openairdocs.org/sdr/SWAA2023091901688.md): Floor Panel · cracked · Sep 16, 2023 · N783SW · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT FLOOR PANEL IS CRACKED<[01] OKAY TO CONTINUE PER MEL 25-16-01 SP1B FWD BIN TO REMAIN EMPTY;[02] REMOVED AND REPLACED CRACKED FLOOR PANEL FROM FWD CARGO COMPATMENT PER 25-52-10. MEL CLEARED SP1B.
- [SDR SWAA2023061959937](https://openairdocs.org/sdr/SWAA2023061959937.md): Girt Bar · out of position · Jun 16, 2023 · N783SW · Boeing 7377H4 · Escape Slide
  > GIRT BART LOCATED AT THE R2 AFT GALLEY DOOR IS HANGING OUT OF POSITION<[01] REPOSITIONED GIRT BAR AS REQD. AMM 25-66-01<BR>R2 DOOR
- [SDR SWAA2023061658972](https://openairdocs.org/sdr/SWAA2023061658972.md): Handle · loose · Jun 14, 2023 · N783SW · Boeing 7377H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR UPPER ASSIST HANDLE LOOSE<[01] ADJUSTED FWD ENTRY DOOR ASSIST HANDLE PER AMM 52-11-31-000-802
- [SDR SWAA2023060956455](https://openairdocs.org/sdr/SWAA2023060956455.md): Battery Pack · inoperative · Jun 6, 2023 · N783SW · Boeing 7377H4 · Emergency Lighting
  > FWD LH EMERGENCY LIGHT BATTERY INOP.<[01] REMOVED AND REPLACED FWD LH EMERGENCY LIGHT BATTERY PACK REF: AMM 33-51-06.
- [SDR SWAA2023042730410](https://openairdocs.org/sdr/SWAA2023042730410.md): Floor Panel · cracked · Apr 23, 2023 · N783SW · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CARGO AFT FLOOR PANEL HAS A CRACK 9.5 INCHES IN LENGTH<[01] REMOVED AND REPLACED FWD CARGO AFT FLOOR PANEL IAW AMM 25-52-10.
- [SDR SWAA2023021502479](https://openairdocs.org/sdr/SWAA2023021502479.md): Tailpipe · fire · Feb 13, 2023 · N783SW · Boeing 7377H4 · Engine (Turbine/Turboprop)
  > ENGINE TAILPIPE FIRE @ 75KTS DURING T/O ON NO 1 ENG REJECTED T/O; PERFORMED QRH PROCEDURES.FLAMES WERE REPORTED FROM ANOTHER A/C AND TOWER RAN BRAKE COOLING ON PWB TAXI TO GATE NORMALLY FIRE TRUCKS CLEARED US TO GATE RAN COOLING FOR APPROX 3 MINUTES PRIOR TO
- [SDR SWAA2022120979977](https://openairdocs.org/sdr/SWAA2022120979977.md): Slide · out of position · Dec 8, 2022 · N783SW · Boeing 7377H4 · Escape Slide
  > STBD AFT A/C SERVICE DOOR SLIDE PULL HANDLE VISIBLE AND EXPOSED WHEN DOOR IS ARMED. REPOSITIONED MANUAL HANDLE COVER FOR AFT SERVICE DOOR ESCAPE SLIDE IAW AMM 25?66-01. OPS CHECKS NORMAL.
- [SDR SWAA2022102765082](https://openairdocs.org/sdr/SWAA2022102765082.md): Flashlight · inoperative · Oct 26, 2022 · N783SW · Boeing 7377H4 · Emergency Equipment
  > FA FOUND FWD GALLEY UPPPER EMER FLASHLIGHT NOT BLINKING / [01] R&R EMER FLASHLIGHT PER AMM 25-64-00
- [SDR SWAA2022090649795](https://openairdocs.org/sdr/SWAA2022090649795.md): Slide · low · Sep 2, 2022 · N783SW · Boeing 737 · Escape Slide
  > FORWARD RIGHT SERVICE DOOR SLIDE INDICATOR GAUGE SHOWING LOW. SLIDE PART REQUEST IS BUILT INTO THE SUBTASK / [01] R&R?D FWD SERVICE (R1)DOOR EMERGENCY ESCAPE SLIDE PER MT 725-61-06-FS
- [SDR SWAA2022060111139](https://openairdocs.org/sdr/SWAA2022060111139.md): Web · cracked · May 24, 2022 · N783SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL SUPPORT WEB CRACKED AT OUTBOARD ATTACH FASTENER HOLE. REMOVED DAMAGE WEB ANGLE AT R/H WING TRAILING EDGE DEFLECTION CONTROL PANEL PER REF B737-700 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW PART WED ANGLE
- [SDR SWAA2022060111136](https://openairdocs.org/sdr/SWAA2022060111136.md): Support Angle · cracked · May 24, 2022 · N783SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL SEAL SUPPORT ANGLE CRACKED AT WEB ATTACH POINT. REMOVED DAMAGE SEAL SUPPORT ANGLE AT R/H WING TRAILING EDGE DEFLECTION CONTROL PANEL PER REF B737-700 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW PART WEB ANGL
- [SDR SWAA2022060111137](https://openairdocs.org/sdr/SWAA2022060111137.md): Support Angle · cracked · May 24, 2022 · N783SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > LEFT WING DEFLECTION CONTROL RIB PANEL VERTICAL SEAL SUPPORT ANGLE CRACKED AT THE FORWARD SIDE OF WEB. / [01] REMOVED AND REPLACED SEAL SUPPORT ANGLE AT FWD SIDE OF WEB ON L/W DEFLECTION CONTROL PANEL PER REF B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.
- [SDR SWAA2022030279163](https://openairdocs.org/sdr/SWAA2022030279163.md): Light · missing · Mar 2, 2022 · N783SW · Boeing 737* · Emergency Lighting
  > EMERGENCY EXIT LIGHT LENS NOT INSTALLED AT R2 DOOR / [01] REMOVED & REPLACED EMERGENCY EXIT LIGHT ASSY; AT R2 DOOR; PER AMM 33-51-01.
- [SDR SWAA2022021472148](https://openairdocs.org/sdr/SWAA2022021472148.md): Sensor · faulty · Feb 11, 2022 · N783SW · Boeing 7377H4 · Leading Edge Slat Position Indicating System
  > CREW REPORTED FLAP LOCK OUT ON LANDING; / [01] REPLACED SLAT #1 INBOARD PROXIMITY SENSOR PER AMM 27-88-11; OPS CHECK GOOD.
- [SDR SWAA2021110832157](https://openairdocs.org/sdr/SWAA2021110832157.md): Girt Bar · out of position · Oct 20, 2021 · N783SW · Boeing 737* · Agricultural Spray System
  > L-1 DOOR GIRT BAR HITTING AFT DOOR CUTOUT (WHEN OPENING DOOR); / [01] REMOVED R1 DOOR SLIDE REF MT 725-61-06; [02] REPOSITIONED GIRT BAR FOR L1 DOOR REF B737 MM 25-66-01-400-803; [03] REMOVED L1 DOOR SLIDE REF MT 725-61-06; [04] EDIT WORK CAPTURE STEP 1 (& 3)
- [SDR SWAA2021110832154](https://openairdocs.org/sdr/SWAA2021110832154.md): Girt Bar · out of position · Oct 20, 2021 · N783SW · Boeing 737* · Escape Slide
  > R-1 DOOR GIRT BAR HITTING DOOR CUTOUT WHEN CLOSING ON AFT CORNER; / [01] REMOVED R1 DOOR SLIDE REF MT 725-61-06; [02] REPOSITIONED GIRT BAR FOR R1 DOOR REF B737 MM 25-66-01-400-803; [03] OK TO INSTALL R1 DOOR SLIDE.; [04] REINSTALLED R1 DOOR SLIDE REF MT 725-
- [SDR SWAA2021102832155](https://openairdocs.org/sdr/SWAA2021102832155.md): Bulb · inoperative · Oct 20, 2021 · N783SW · Boeing 7377H4 · Oxygen System
  > L-1 DOOR UPPER EMERGENCY LIGHT WITH 2EA BULBS INOP; / [01] RECITED BULBS (2EA) AT L-1 DOOR UPPER EMERGENCY LIGHT AS PER REF B737 AMM 33-51-01-960-801 PERFORMED OPERATIONAL TEST FOUND NORMAL; [02] VERIFIED STEP 1
- [SDR SWAA2021110831031](https://openairdocs.org/sdr/SWAA2021110831031.md): None · popped · Oct 17, 2021 · N783SW · Boeing 737* · Emergency Lighting
  > PASSENGER CABIN LIGHTING EMERGENCY CHARGER FWD C/B POPPING AT P18.; PASSENGER CAIN LIGHTING EMERGENCY CHARGER FWD CB POPPING AT P18. / [01] PERFORMED TROUBLESHOOTING PASSENGER CABIN LIGHTING CHARGER FWD C/B AS PER WDM 33-51-11; FOUND BATTERY CHARGER M1875 AT
- [SDR SWAA2021110831030](https://openairdocs.org/sdr/SWAA2021110831030.md): Light · inoperative · Oct 17, 2021 · N783SW · Boeing 737* · Emergency Lighting
  > OVERHEAD BIN EMERGENCY LIGHT INOP BY ROW 4 LH; OVERHEAD IN EMERGENCY LIGHT INOP Y ROW 4 LH / [01] RE-SECURED CONNECTOR D11090 IN AISLE LIGHT L1065; AS PER REFERENCE B737 WDM 33-51-12; PERFORMED OPERATIONAL TEST AS PER REFERENCE B737 AMM 33-51-00-710-801; NORM
- [SDR SWAA2021110929830](https://openairdocs.org/sdr/SWAA2021110929830.md): Scuff Plate · cracked · Oct 14, 2021 · N783SW · Boeing 737* · Fuselage Miscellaneous Structure
  > FWD CARGO FWD SCUFF PLATE CRACKED; / [01] RECEIVED WELDED SCUFF PLATE ON TAG #397070; ISSUE TAG #HZ896; P.O.#1734696. WILL BE INSTALLED ON CARD 3 # TTG8Q004G7HY; [02] VERIFIED STEP 1
- [SDR SWAA2021110826978](https://openairdocs.org/sdr/SWAA2021110826978.md): Floor Panel · delaminated · Oct 5, 2021 · N783SW · Boeing 737* · Fuselage Floor Panel
  > FOUND PANEL 212DC DELAMONATE AT CORNER; / [01] PREPARED FOR REPAIR AT PANEL 212 DC AS PER B737-700-SRM 51-70-06-2R-6; [02] VERIFIED STEP 1. OK TO INSTALL REPAIR.; [03] ACCOMPLISHED REPAIR OF DELAMINATION OF THE EDGEBAND OF HONEYCOMB OF FLIGHT DECK CEILING PAN
- [SDR SWAA2021110826221](https://openairdocs.org/sdr/SWAA2021110826221.md): Seat Track · corroded · Oct 4, 2021 · N783SW · Boeing 737* · Fuselage Miscellaneous Structure
  > FOUND FIRST OFFICER FWD I/B AND O/B SEAT TRACKS WITH CORROSION; / [01] 1ST OFFICER FWD I/B AND O/B SEAT TRACKS WERE REMOVED ON TASKCARD TTG8Q0036K60.; [02] VERIFIED STEP 1. OK TO INSTALL NEW FWD SEAT TRACKS.; [03] INSTALLED NEW 1ST OFFICER FWD I/B AND O/B SEA
- [SDR SWAA2021110826222](https://openairdocs.org/sdr/SWAA2021110826222.md): Seat Track · corroded · Oct 4, 2021 · N783SW · Boeing 737* · Fuselage Miscellaneous Structure
  > FOUND CAPTAIN FWD I/B AND O/B SEAT TRACKS WITH CORROSION; / [01] RECEIVED CAPTAIN FWD I/B AND O/B SET TRACKS TO BE INSTALLED ON CARD TTG8Q0036K4C; [02] RECEIVED CAPTAIN FWD I/B AND O/B SET TRACKS TO BE INSTALLED ON CARD TTG8Q0036K4C
- [SDR SWAA2021110924748](https://openairdocs.org/sdr/SWAA2021110924748.md): None · corroded · Sep 29, 2021 · N783SW · Boeing 737* · Vertical Stabilizer Miscellaneous Structure
  > CORROSION.>>>>>VERTICAL FIN FWD R/H ATTACHMENT FITTING LUGS STA 1016 INNER BORE EVIDENCE OF PITTI CORROSION.; / [01] REMOVED CORROSION ON VERTICAL FIN FWD R/H ATTACHMENT FITTING LUGS STA. 1016 PER REF. 737 SRM 51-10-02-0G-0; BY REAMING HOLE TO FINAL SIZE; 1.0
- [SDR SWAA2021110924747](https://openairdocs.org/sdr/SWAA2021110924747.md): None · corroded · Sep 29, 2021 · N783SW · Boeing 737* · Vertical Stabilizer Miscellaneous Structure
  > CORROSION >>>>>>>VERTICAL FIN FRONT SPAR R/H FITTING LUG HAVE SIGN OF PITTI CORROSION AT INNER BORE.; / [01] REMOVED CORROSION ON VERTICAL FIN FRONT SPAR R/H FITTING LUG; PER REF. 737 SRM 51-10-02-0G-0; BY REAMING HOLE TO FINAL SIZE; 1.040 (0N VERTICAL); [02
- [SDR SWAA2021110924746](https://openairdocs.org/sdr/SWAA2021110924746.md): None · corroded · Sep 29, 2021 · N783SW · Boeing 737* · Vertical Stabilizer Miscellaneous Structure
  > CORROSION >>>>>>>VERTICAL FIN FRONT SPAR L/H FITTING LUG HAVE SIGN OF PITTI CORROSION AT INNER BORE.; / [01] REMOVED CORROSION ON VERTICAL FIN FRONT SPAR L/H FITTING LUG; PER REF. 737 SRM 51-10-02-0G-0; BY REAMING HOLE TO FINAL SIZE; 1.040;( ON VERTICAL); [
- [SDR SWAA2021110919709](https://openairdocs.org/sdr/SWAA2021110919709.md): Skin · corroded · Sep 17, 2021 · N783SW · Boeing 737* · Fuselage Main, Plate/Skin
  > AFT UPPER FUSELAGE AT STA 1016 - STA 1088 STR 3L - STR 3R WL 308.5 HAS SURFACE CORROSION. REMOVED CORROSION ON UPPER FUSELAGE FROM BS 1016 TO 1088, BETWEEN STRINGER 3L AND 3R, WL 308.5 IAW SRM 51-10-02-0G-0. NO MATERIAL LOST AREAS WITHIN LIMITS IAW SRM 53-00
- [SDR SWAA2021110820614](https://openairdocs.org/sdr/SWAA2021110820614.md): Angle · cracked · Sep 17, 2021 · N783SW · Boeing 737* · Fuselage Main, Structure
  > CABIN PASSENGER STATION 616 LBL 60 CRACK AT FASTENER HOLE; / [01] INSTALLED EWIS PROTECTION AT LT SIDE BETWEDN STA 540 TO 639 REF B737-7 AMM 20-60-07-913-801; [02] REMOVED CABIN PASSENGER INNER CHORD CREASE BEAM AT LT SIDE LBL 60 FROM STA 530 TO STA671 REF B7
- [SDR SWAA2021110819715](https://openairdocs.org/sdr/SWAA2021110819715.md): Angle · cracked · Sep 17, 2021 · N783SW · Boeing 737* · Fuselage Main, Structure
  > CABIN PASSENGER STATION 616 LBL 60 CRACK AT FASTENER HOLE; / [01] INSTALLED EWIS PROTECTION AT LT SIDE BETWEDN STA 540 TO 639 REF B737-7 AMM 20-60-07-913-801; [02] REMOVED CABIN PASSENGER INNER CHORD CREASE BEAM AT LT SIDE LBL 60 FROM STA 530 TO STA671 REF B7
- [SDR SWAA2021110920599](https://openairdocs.org/sdr/SWAA2021110920599.md): None · corroded · Sep 16, 2021 · N783SW · Boeing 737* · Vertical Stabilizer, Spar/Rib
  > >>> CORROSION >> VERTICAL STABILIZER; RIGHT FRON SPAR FITTING PITTING CORROSION; / [01] REMOVED BUSHING AT VERTICAL STABILIZER RIGHT FRONT SPAT FITTING AS PER B737-700 SOPM 20-50-03; [02] REMOVED CORROSION AT VERTICAL STABILIZER RIGHT FROM SPAR FITTING REF B7
- [SDR SWAA2021110920598](https://openairdocs.org/sdr/SWAA2021110920598.md): None · corroded · Sep 16, 2021 · N783SW · Boeing 737* · Vertical Stabilizer, Spar/Rib
  > >>> CORROSION >> VERTICAL STABILIZER; LEFT FRON SPAR FITTING CORROSION; / [01] REMOVED BUSHING AT VERTICAL STABILIZER LEFT FRONT SPAR FITTING AS PER B737-700 SOPM 20-50-03; [02] REMOVED CORROSION AT VERTICAL STABILIZER LEFT FROM SPAR FITTING REF B737-7 SRM 5
- [SDR SWAA2021110920597](https://openairdocs.org/sdr/SWAA2021110920597.md): None · corroded · Sep 16, 2021 · N783SW · Boeing 737* · Vertical Stabilizer
  > >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT FRON SPAR FITTINGS CORROSION; / [01] REMOVED BUSHINGS AT VERTICAL STABILIZER CENTER SECTION LEFT FRONT SPAR AS PER B737-700 SOPM 20-50-03; [02] REMOVED CORROSION AT VERTICAL FIN LT FITTING REF B737-7 S
- [SDR SWAA2021110919708](https://openairdocs.org/sdr/SWAA2021110919708.md): Fitting · corroded · Sep 16, 2021 · N783SW · Boeing 737* · Empennage Structure
  > >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; RIGHT O/B REAR SPAR FITTINGS PITTING CORROSION; /
- [SDR SWAA2021110919702](https://openairdocs.org/sdr/SWAA2021110919702.md): Fitting · corroded · Sep 16, 2021 · N783SW · Boeing 737* · Empennage Structure
  > >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT O/B REAR SPAR FITTINGS CORROSION; /
- [SDR SWAA2021110919701](https://openairdocs.org/sdr/SWAA2021110919701.md): Fitting · corroded · Sep 16, 2021 · N783SW · Boeing 737* · Vertical Stabilizer Miscellaneous Structure
  > >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT I/B REAR SPAR FITTINGS CORROSION; /
- [SDR SWAA2021110919700](https://openairdocs.org/sdr/SWAA2021110919700.md): Fitting · corroded · Sep 16, 2021 · N783SW · Boeing 737* · Vertical Stabilizer Miscellaneous Structure
  > >>> CORROSION >> VERTICAL STABILIZER; RIGHT FRON SPAR FITTING PITTING CORROSION; /
- [SDR SWAA2021110919699](https://openairdocs.org/sdr/SWAA2021110919699.md): Fitting · corroded · Sep 16, 2021 · N783SW · Boeing 737* · Vertical Stabilizer Miscellaneous Structure
  > >>> CORROSION >> VERTICAL STABILIZER; LEFT FRON SPAR FITTING CORROSION; /
- [SDR SWAA2021110919698](https://openairdocs.org/sdr/SWAA2021110919698.md): Fitting · corroded · Sep 16, 2021 · N783SW · Boeing 737* · Vertical Stabilizer Miscellaneous Structure
  > >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT FRON SPAR FITTINGS CORROSION; /
- [SDR SWAA2021110920602](https://openairdocs.org/sdr/SWAA2021110920602.md): Fitting · corroded · Sep 16, 2021 · N783SW · Boeing 737* · Vertical Stabilizer Miscellaneous Structure
  > >>> CORROSION >> VERTICAL STABILIZER; RIGHT I/B REAR SPAR FITTINGS PITTING CORROSION; / [01] REMOVED BUSHINGS AT RIGHT VERTICAL STABILIZER I/B REAR SPAR AS P[ER B737-700 SOPM 20-50-03; [02] AFTER BUSHING REMOVAL; INSPECTED AREA AT VERTICAL STABILIZER; RIGHT
- [SDR SWAA2021110920607](https://openairdocs.org/sdr/SWAA2021110920607.md): Fitting · corroded · Sep 16, 2021 · N783SW · Boeing 737* · Vertical Stabilizer Miscellaneous Structure
  > >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; RIGHT I/B REAR SPAR FITTINGS PITTING CORROSION; / [01] EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT); [02] EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT); [03] ISSUED SUMMARY EA 21-153-02759; [04] C/W
- [SDR SWAA2021110920604](https://openairdocs.org/sdr/SWAA2021110920604.md): Fitting · corroded · Sep 16, 2021 · N783SW · Boeing 7377H4 · Vertical Stabilizer
  > VERTICAL STABILIZER LEFT I/B REAR SPAR FITTINGS CORRODED. REMOVED BUSHINGS AT LEFT VERTICAL STABILIZER I/B REAR SPAR AS PER B737-700 SOPM 20-50-03, AFTER BUSHING REMOVAL, INSPECTED AREA, NO CORROSION FOUND. INSTALLED SERVICEABLE BUSHINGS SOPM 20-50-03 AND
- [SDR SWAA2021110920600](https://openairdocs.org/sdr/SWAA2021110920600.md): Fitting · corroded · Sep 16, 2021 · N783SW · Boeing 737* · Vertical Stabilizer
  > >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT I/B REAR SPAR FITTINGS CORROSION; / [01] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q006KMKF; [02] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q006KMKF
- [SDR SWAA2021110920601](https://openairdocs.org/sdr/SWAA2021110920601.md): Fitting · corroded · Sep 16, 2021 · N783SW · Boeing 737* · Horizontal Stabilizer, Spar/Rib
  > >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT O/B REAR SPAR FITTINGS CORROSION; / [01] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q006KMKF; [02] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q006KMKF
- [SDR SWAA2021110920606](https://openairdocs.org/sdr/SWAA2021110920606.md): Fitting · corroded · Sep 16, 2021 · N783SW · Boeing 737* · Vertical Stabilizer Miscellaneous Structure
  > >>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; RIGHT O/B REAR SPAR FITTINGS PITTING CORROSION; / [01] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q006KMKF; [02] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q0
- [SDR SWAA2021110918244](https://openairdocs.org/sdr/SWAA2021110918244.md): None · broken · Sep 15, 2021 · N783SW · Boeing 737* · Horizontal Stabilizer Miscellaneous Structure
  > FOUND RIGHT UPPER STABILIZER-TO-BODY FRONT SPAR SLIDING SEAL BROKEN; / [01] REMOVED RIGHT UPPER STABLIZER -TO- BODY FRONT SPAR SLIDING SEAL AS PER BOEING 737 AMM 53-31-31-000-801; [02] REMOVED EXISTING HARDWARE AND LOCATED AND DRILLED NEW SLIDING PER REF. 737
- [SDR SWAA2021110918243](https://openairdocs.org/sdr/SWAA2021110918243.md): None · broken · Sep 15, 2021 · N783SW · Boeing 737* · Horizontal Stabilizer Miscellaneous Structure
  > FOUND LEFT UPPER STABILIZER-TO-BODY FRONT SPAR SLIDING SEAL BROKEN; / [01] REMOVED LEFT UPPER STABLIZER -TO- BODY FRONT SPAR SLIDING SEAL AS PER BOEING 737 AMM 53-31-31-000-801; [02] LOCATED AND DRILLED LEFT UPPER STABLIZER -TO- BODY FRONT SPAR SLIDING SEAL A
- [SDR SWAA2021110918242](https://openairdocs.org/sdr/SWAA2021110918242.md): Angle · cracked · Sep 15, 2021 · N783SW · Boeing 737* · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL FIN; FWD TERMINAL FITTING ASSY AFT FACE HORIZONTAL T ANGLE CRACKED 2 EA PLACES; / [01] PERFORMED HFEC INSP ON VERTICAL FIN FWD TERMINAL FITTING ASSY AFT FACE HORIZ T ANGLE IAW B737 NDT P6 51-00-00 PROC.23; CRACKS NOTED MARKED.<BR>TOOL USED: NORTEC 6
- [SDR SWAA2021110818245](https://openairdocs.org/sdr/SWAA2021110818245.md): Gusset · cracked · Sep 15, 2021 · N783SW · Boeing 737* · Fuselage Miscellaneous Structure
  > FWD CARGO COMP GUSSET IS CRACKED BETWEEN FRAME BS 500D AND STGR 19L; / [01] REMOVED GUSSET AT FWD CARGO COMPARTMENT AT FS 500D STRINGER 19L;FOUND OUT OF LIMITS IN REF B737-700 SRM 51-2=10-023-0G-0; LOCATED AND DRILLED NEW GUSSET IN REF B737-700 SRM 51-40-05-0
- [SDR SWAA2021110818246](https://openairdocs.org/sdr/SWAA2021110818246.md): Gusset · cracked · Sep 15, 2021 · N783SW · Boeing 737* · Fuselage Miscellaneous Structure
  > FWD CARGO COMP GUSSET IS CRACKED BETWEEN FRAME BS 500D AND STGR 21L; / [01] REMOVED CRACK GUSSET IN REF B737-700 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW GUSSET REF. B737-7 SRM #51-40-05-0G-0; [03] VEERIFIED STEP 1 AND 2; [04] OK TO TREAT AND PRIME HOL
- [SDR SWAA2021110818247](https://openairdocs.org/sdr/SWAA2021110818247.md): Gusset · cracked · Sep 15, 2021 · N783SW · Boeing 737* · Fuselage Miscellaneous Structure
  > FWD CARGO COMP GUSSET IS CRACKED BETWEEN FRAME BS 500D AND STGR 24L; / [01] REMOVED GUSSET AT FWD CARGO COMPARTMENT FS 500D;STRINGER 24L;IN REF B737-700 SRM 51-40-02-OG-0;LOCATED AND DRILLED GUSSET IN REF B737-700 SRM 51-40-05-0G-0; [02] VERIFIED STEP #1. OK

Next page: https://openairdocs.org/aircraft/N783SW/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 = 'N783SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N783SW/reports

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