# Service difficulty reports: N784SW, cancelled Oct 4, 2024

A list on [N784SW, cancelled Oct 4, 2024](https://openairdocs.org/deregistered/N784SW-2024-10-04.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 6 · 271 reports

- [SDR SWAA2023080384717](https://openairdocs.org/sdr/SWAA2023080384717.md): Light · unsecure · Aug 2, 2023 · N784SW · Boeing 7377H4 · Emergency Lighting
  > FWD CABIN FLOOR EMERGENCY LUMINESCENT STRIP NEEDS TO BE SECURED AT FWD RH BULKHEAD.<[01] SECURED FWD CABIN FLOOR EMERGENCY LUMINESCENT STRIP AT FWD RH BULKHEAD IAW AMM 25-00-00.
- [SDR SWAA2023050846629](https://openairdocs.org/sdr/SWAA2023050846629.md): Megaphone · failed · May 6, 2023 · N784SW · Boeing 7377H4 · Emergency Equipment
  > AFT MEGAPHONE WILL NOT TEST<[01] REPLACED BATTERIES FOR AFT MEGAPHONE PER AMM 25-64-00. OPS CHECK IS GOOD
- [SDR SWAA2023040322416](https://openairdocs.org/sdr/SWAA2023040322416.md): Lens · stained · Mar 31, 2023 · N784SW · Boeing 7377H4 · Passenger Compartment Equipment
  > BOTH OVER WING EXITS LIGHT LENSES ARE STAINED.<[01] REPLACED LENSES PER AMM 33-51-01
- [SDR SWAA2023040322418](https://openairdocs.org/sdr/SWAA2023040322418.md): Slide · loose · Mar 31, 2023 · N784SW · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR AFT SLIDE ISOLATOR LOOSE<[01] R&R FWD SERVICE DOOR AFT SLIDE ISOLATOR IAW AMM 20-50-11.;[02] INSPECTION C/W R&R FWD SERVICE DOOR AFT SLIDE ISOLATOR IAW AMM 20-50-11.
- [SDR SWAA2023030110296](https://openairdocs.org/sdr/SWAA2023030110296.md): Battery Pack · inoperative · Feb 26, 2023 · N784SW · Boeing 7377H4 · Emergency Lighting
  > THREE AFT EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED AFT RH EMERGENCY BATTERY PACK IN REF TO AMM 33-51-06. OPS CHECK GOOD
- [SDR SWAA2023020297768](https://openairdocs.org/sdr/SWAA2023020297768.md): Light · inoperative · Feb 2, 2023 · N784SW · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT AFT OF THE AFT SERVICE DOOR INOP<[01] RELAMP'ED EMER. LITE AFT OF THE AFT SERVICE DOOR REF M/M 33-51-22
- [SDR SWAA2023010588315](https://openairdocs.org/sdr/SWAA2023010588315.md): Megaphone · inoperative · Jan 4, 2023 · N784SW · Boeing 7377H4 · Emergency Equipment
  > FWD MEGA PHONE HANDLE LOOSE AND INOPERATIVE. REMOVED AND REPLACED FWD MEGA PHONE PER AMM 25-64-00.
- [SDR SWAA2022112875595](https://openairdocs.org/sdr/SWAA2022112875595.md): Megaphone · inoperative · Nov 25, 2022 · N784SW · Boeing 7377H4 · Emergency Equipment
  > FA WRITE UP - FWD MEGAPHONE NEEDS BATTERY / [01] REMOVED AND REPLACED BATTERIES PER AMM SIP
- [SDR SWAA2022111068411](https://openairdocs.org/sdr/SWAA2022111068411.md): Slide · out of adjust · Nov 6, 2022 · N784SW · Boeing 7377H4 · Escape Slide
  > AFT A/C LEFT: EMERGENCY ESCAPE SLIDE HAS MANUAL PULL HANDLE EXPOSED / [01] ATTACHED PULLHANDLE COVER TO VELCRO PER SIP
- [SDR SWAA2022062822651](https://openairdocs.org/sdr/SWAA2022062822651.md): Slide · out of position · Jun 24, 2022 · N784SW · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE PULLED OUT OF NORMAL / [01] SLIDE SKIRT DROOPING REFOLDED SLIDE SKIRT OK FOR SERVICE. SLIDE WAS NOT DEPLOYED IAW SIP
- [SDR SWAA2022041995225](https://openairdocs.org/sdr/SWAA2022041995225.md): Cover · loose · Apr 17, 2022 · N784SW · Boeing 7377H4 · Escape Slide
  > SLIDE PULL HANDLE COVERS- FWD ENTRY & BOTH REAR DOORS NEED TO BE RESECURED / [01] RESECURED SLIDE PULL HANDLE COVERS ON FWD ENTRY AND BOTH DOORS PER SIP.;[02] RESECURED SLIDE PULL HANDLE COVERS ON FWD ENTRY AND BOTH REAR DOORS PER SIP.
- [SDR SWAA2022041492842](https://openairdocs.org/sdr/SWAA2022041492842.md): Cover · loose · Apr 10, 2022 · N784SW · Boeing 7377H4 · Emergency Lighting
  > F/O OVER WING EXIT LIGHT FELL OFF / [01] RESECURE F/O OVERWING EXIT LIGHT COVER PER SIP
- [SDR SWAA2022032385654](https://openairdocs.org/sdr/SWAA2022032385654.md): Light · loose · Mar 19, 2022 · N784SW · Boeing 737* · Emergency Lighting
  > R/H OVERWING UPPER RIGHT EXIT/SALIDA SIGN COVER LOOSE. / [01] REPOSITION AND RE TIGHTEN SCREW ON R/H OVER WING UPPER RIGHT EXIT/SALIDA SIGN COVER; OPS CHECK GOOD REF AMM 33-51-01.
- [SDR SWAA2022031783218](https://openairdocs.org/sdr/SWAA2022031783218.md): Light · inoperative · Mar 13, 2022 · N784SW · Boeing 737* · Emergency Lighting
  > LOWER EMERGENCY EXIT LIGHT INOP LOWER EMERGENCY EXIT LIGHT INOP (F/O) SIDE CENTER DOOR / [01] R&R LOWER EMERGENCY EXIT LIGHT ASSY PER AMM 33-51-01. OPS CHECK GOOD.
- [SDR SWAA2022031582758](https://openairdocs.org/sdr/SWAA2022031582758.md): None · none · Mar 11, 2022 · N784SW · Boeing 737* · Engine Collector/Tailpipe/Nozzle
  > ON TAKEOFF ROLL TOWER OBSERVED FLAMES COMING OUT OF THE #2 ENGINE. ALL ENGINE PARAMETERS NORMAL. / [01] PERFORMED FIM TASK 71-05 TASK 811 WITH NO FAULTS FOUND. DETERMINED OIL PUDDLING IN OIL CENTER PLUG CAVITY CAUSED DUE TO BORESCOPE PRIOR TO FLIGHT AND DRY MO
- [SDR SWAA2022030379862](https://openairdocs.org/sdr/SWAA2022030379862.md): Light · broken · Mar 3, 2022 · N784SW · Boeing 737* · Emergency Lighting
  > AIRCRAFT RIGHT FO OVER WING FWD EXIT SIGN COVER BROKEN / [01] RESECURRED COVER PER SIP
- [SDR SWAA2022010457054](https://openairdocs.org/sdr/SWAA2022010457054.md): Light · inoperative · Dec 29, 2021 · N784SW · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT INOP AT OVERHEAD BIN SEAT 22 RH.; EMERGENCY LIGHT INOP AT OVERHEAD IN SEAT 22 RH. / [01] RELAMPED EMERGENCY LIGHT AT OVERHEAD BIN SEAT 22 RH PERFORMED OPERATIONAL TEST; TEST OK AS PER REF B737 AMM 33-51-03-960-801; [02] VERIFIED
- [SDR SWAA2022010555180](https://openairdocs.org/sdr/SWAA2022010555180.md): Floor Support · cracked · Dec 21, 2021 · N784SW · Boeing 737 · Fuselage Miscellaneous Structure
  > SUPPLEMENTAL INFORMATION: MAIN CABINE FLOOR SUPPORT CRACK AT STA.540 AND I/B OF SEAT TRACK RBL 24.75; / [01] LOCATED AND DRILLED NEW MAIN CABIN FLOOR SUPPORT PER B 737-700 SRM 51-40-05-0G-0; [02] VERIFIED 1.; [03] LATE ENTRY: REMOVED MAIN CABINE FLOOR SUPPORT
- [SDR SWAA2021122754661](https://openairdocs.org/sdr/SWAA2021122754661.md): Intercostal · cracked · Dec 18, 2021 · N784SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BILGE INTERCOSTAL CRACKED AT BS500B TO BS500C AND S25L. REMOVED INTERCOSTAL AT FWD CARGO BS 500B TO BS 500C IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED HOLES IAW SRM 51-40-05-0G-0. OK TO INSTALL INTERCOSTAL. INSTALLED INTERCOSTAL AT FWD CARGO I
- [SDR SWAA2021122754660](https://openairdocs.org/sdr/SWAA2021122754660.md): Angle · cracked · Dec 18, 2021 · N784SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BILGE BS500B AND S25R ANGLE CLIP CRACKED.; / [01] REMOVED AND REPLACED CLIP AT STA 500B AND STR 25R PER SRM 51-40-02-0G-0; [02] VERIFIED 1
- [SDR SWAA2022011254145](https://openairdocs.org/sdr/SWAA2022011254145.md): Cap · corroded · Dec 16, 2021 · N784SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H CAP STRIPS WITH CORROSION; / [01] ORDERED NEW PARTS; [02] REMOVED DAMAGED AS PER B737-7 SRM 51-10-02-0G-0. CORROSION THROUGH MATERIAL FOUND OUT OF LIMITS; [03] FOR INSTALLATION REFERENCE TASK TTG8Q004ERCP; [04] RECEIVED NEW CAP STRIPS 7EA TO REP
- [SDR SWAA2022011254146](https://openairdocs.org/sdr/SWAA2022011254146.md): Cap · corroded · Dec 16, 2021 · N784SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H CAP STRIPS WITH CORROSION; / [01] RECIEVED NEW PARTS; [02] REMOVED DAMAGED AS PER B737-7 SRM 51-10-02-0G-0. CORROSION THROUGH MATERIAL FOUND OUT OF LIMITS; [03] FOR INSTALLATION REFERENCE TASK TTG8Q004ERCP; [04] VERIFIED STEPS 1; 2 AND 3
- [SDR SWAA2022011253499](https://openairdocs.org/sdr/SWAA2022011253499.md): Support Beam · elongated · Dec 15, 2021 · N784SW · Boeing 7377H4 · Wing, Control Surfaces
  > RIGHT WING ACCESS PANEL 651GB UPPER SUPPORT BEAN FASTENER HOLE ELONGATED ( MARKED); / [01] PERFORMED HFEC INSP. IAW B737 NDT<BR>PART 6; 51-00-00; PROCEDURE 23. NO CRACKS <BR>TOOL: NORTEC 600 B/C: 166316 DUE: 10/08/22; [22] REPAIR ACCOMPLISHED PER EA-22-157-00
- [SDR SWAA2022010552363](https://openairdocs.org/sdr/SWAA2022010552363.md): Shield · cracked · Dec 11, 2021 · N784SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO AFT SHIELD IS CRACK; / [01] RECEIVED NEW SHIELD LOCATED AND DRILL HOLES NEW SHIELD INSTALLED NUTPLATES AS PER SRM 51-40-05 AND 51-40-02; [02] VERIFIED 1
- [SDR SWAA2022011051936](https://openairdocs.org/sdr/SWAA2022011051936.md): Skin · delaminated · Dec 10, 2021 · N784SW · Boeing 7377H4 · Spoilers
  > L/H WING SPOILER #6 HAS A DELAMINATED DENT LOCATED AT 9.75' FROM I/B EDGE AND 6.5' FROM AFT EDGE MEASURES L=0.5';W=O.5';Y=0.004';W/Y=125; / [01] PREPARED THE DAMAGED AREA TO EXAMINE THE DAMAGE IN THE REPAIR AREA. REF B737-700 SRM 57-70-01-2R-2 AND SRM 51-70-1
- [SDR SWAA2022011249854](https://openairdocs.org/sdr/SWAA2022011249854.md): Rib · cracked · Dec 3, 2021 · N784SW · Boeing 737 · Vertical Stabilizer, Spar/Rib
  > SUPPLEMENTAL INFORMATION: VERTICAL DORSAL FIN FWD RIB CRACKED; / [01] REMOVED AND REPLACED VERTICAL DORSAL FIN FWD RIB AS PER B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING 174A0103; [02] VERIFIED STEP 1
- [SDR SWAA2022011249442](https://openairdocs.org/sdr/SWAA2022011249442.md): None · cracked · Dec 2, 2021 · N784SW · Boeing 737 · Horizontal Stabilizer, Spar/Rib
  > SUPPLEMENTAL INFORMATION: R/H STAB INSPAR RIB ASSY NO. 5 AT STAB STA 129.50 STIFFENER NO.4 CRACKED; / [01] TRIMMED OUT DAMAGED AREA ON RH STAB INSPAR RIB ASSY NO. 5 AT STAB STA 129.5 STIFFENER 4 AS PER B737-700 SRM 55-10-09-2R-4; [06] FABRICATED REPAIR PARTS
- [SDR SWAA2022010549440](https://openairdocs.org/sdr/SWAA2022010549440.md): Floor Panel · delaminated · Dec 2, 2021 · N784SW · Boeing 737 · Fuselage Floor Panel
  > SUPPLEMENTAL INFORMATION: PAX CABIN FLOOR PANEL 222AF AFT O/B CORNER DELAMINATED; / [01] MEASUREMENTS; [02] PREPARED DAMAGED AREA FOR REPAIR AT CABIN FLOOR PANEL 222AF PER B737 SRM 53-00-50-2R-0; [03] VERIFIED STEPS 1 AND 2.; [04] REPAIRED DAMAGED AREA AT CAB
- [SDR SWAA2022010449061](https://openairdocs.org/sdr/SWAA2022010449061.md): Floor Panel · delaminated · Dec 1, 2021 · N784SW · Boeing 7377H4 · Fuselage Floor Panel
  > PAX CABIN FLOOR PANEL 221GF UPPER LAMINATE WITH SOME DELAMINATION; / [01] RECEIVED FLOOR PANEL 221GF P/N:141A5810-181 REF. TASK CARD TTG8Q006QHXA FOR PANEL INSTALLATION; [02] VERIFIED STEP 1
- [SDR SWAA2022010449065](https://openairdocs.org/sdr/SWAA2022010449065.md): Floor Panel · cracked · Dec 1, 2021 · N784SW · Boeing 7377H4 · Fuselage Floor Panel
  > PAX CABIN FLOOR PANEL 221BF AFT O/B CORNER CRACKED; / [01] PREPARED DAMAGED AREA AT FLOOR PANEL 221BF PER B737 SRN<BR>53-00-50-2R-0; [02] REPAIRED DAMAGED AREA AT FLOOR PANEL #221BF PER B737<BR>53-00-50-2R-0 MATERIAL USED RESIN 50-A PO# 1714421; [03] VERIFIED
- [SDR SWAA2022011247580](https://openairdocs.org/sdr/SWAA2022011247580.md): Angle · cracked · Nov 25, 2021 · N784SW · Boeing 737 · Fuselage Miscellaneous Structure
  > SUPPLEMENTAL INFORMATION: CABIN FLOOR ANGLE AT STA 540 LBL 64 IS CRACK (228-007); CAIN FLOOR ANGLE AT STA 540 LBL 64 IS CRACK (228-007) / [01] INSTALLED PARCIAL PROTECTION OF THE EWIS IN THE AREA AT CABIN FLOOR ANGLE STA. 540 LBL 64' IAW B737-700 AMM 20-60--0
- [SDR SWAA2022011247312](https://openairdocs.org/sdr/SWAA2022011247312.md): Support · corroded · Nov 24, 2021 · N784SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO, BS 727 TO 847 LBL 21, S25L SIDEPLATE SUPPORT ZEE CORROUDED. REMOVED CORROSION IAW SRM 51-10-02-0G-0. REMOVED CORROSION ON LT Z-CHANNEL BS 727-847 LBL 21 IAW SRM 51-10-02-0G-0. REMOVED THREE NUTPLATES AND ONE FASTENER TO REMOVE CORROSION ON LT Z-C
- [SDR SWAA2021112947308](https://openairdocs.org/sdr/SWAA2021112947308.md): Beam · corroded · Nov 24, 2021 · N784SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CABIN FLOORBEAM AT BS 986.5, RBL 30, AND RBL 34 HAS SURFACE CORROSION ON THE UPPER AND LOWER SURFACES. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP. ON REWORKED AREAS IAW NDT PART 4 51-00-00 PROCEDURE 3. PERFORMED A HFEC INSPECTIO
- [SDR SWAA2021112947309](https://openairdocs.org/sdr/SWAA2021112947309.md): Floorbeam · corroded · Nov 24, 2021 · N784SW · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CABIN FLOOR BEAM AT STA 986.5 LBL 32 AND LBL 35 HAS SURFACE CORROSION ON THE UPPER AND LOWER SURFACES OF THE FASTENER HOLE. REMOVED CORROSION IAW SRM 51-10-02-0G-0. NDT PERFORMED UT THICKNESS INSP. ON REWORKED AREAS IAW NDT PART 4 51-00-00 PROCEDURE 3. MIN
- [SDR SWAA2021112446375](https://openairdocs.org/sdr/SWAA2021112446375.md): Track · corroded · Nov 20, 2021 · N784SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN L/H SEAT TRACK I/B TRACK AT ABOUT STA 500A +6' WITH CORROSION. REMOVED LIGHT CORROSION AT CABIN L/H SEAT TRACK I/B TRACK STA 500A +6' CORRECTION TO STEP 1: REMOVED LIGHT CORROSION AT CABIN L/H SEAT TRACK I/B TRACK STA 500A +6' AS PER B737-700 SRM 51-10-
- [SDR SWAA2021112446392](https://openairdocs.org/sdr/SWAA2021112446392.md): Seat Track · corroded · Nov 20, 2021 · N784SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN L/H SEAT TRACK AT ABOUT STA 500D +14' WITH CORROSION. FAULT FOUND AT OB TRACK. REMOVED SURFACE CORROSION ON L/H I/B TRACK STA 500D+14 PER B737-700 SRM 51-10-02-0G-0 VERIFIED 1 ORIGINAL MMATERIAL 0.230' MATERIAL LOSS 0.011' AND MATERIAL REMAINING 0.219
- [SDR SWAA2021112446397](https://openairdocs.org/sdr/SWAA2021112446397.md): Track · corroded · Nov 20, 2021 · N784SW · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN L/H SEAT TRACK O/B TRACK AT ABOUT STA 559+14' WITH CORROSION. REMOVED CORROSION ON SEAT TRACK STA 559B+14' LBL 45 AS PER B737-700 SRM 51-10-02-0G-0 VERIFIED STEP 1. MAXIMUM CLEANUP DEPTH 0.014'. FOUND WITHIN LIMITS AS PER B737-700 SRM 53-00-52-1A-1. TOO
- [SDR SWAA2022010545508](https://openairdocs.org/sdr/SWAA2022010545508.md): Stub Frame · cracked · Nov 17, 2021 · N784SW · Boeing 7377H4 · Fuselage Main, Frame
  > POSSIBLE CRACK AT CABIN R-1 DOOR FUSELAGE CUTOUT FWD EDGE BETWEEN S-8R AND S-9R. REMOVED SEALANT TO GAIN ACCESS FOR NDT INSPECTIONS TO CHECK FOR CRACK REF SRM 51-31-00-100-801. PERFORMED HFEC AT SUSPECTED CRACK IAW NDTM PART 6; 51-00-00 PROCEDURE 23.CRACK CO
- [SDR SWAA2022010444684](https://openairdocs.org/sdr/SWAA2022010444684.md): Floor Panel · delaminated · Nov 17, 2021 · N784SW · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241DF UPPER SURFACE DELAMINATED; / [01] RECEIVED NEW FLOOR PANEL 241DF P/N 144A5810-128 P/O:1728471 REF. TASK CARD TTG8Q006QHHG FOR PANEL INSTALLATION; [02] VERIFIED STEP 1
- [SDR SWAA2022010445113](https://openairdocs.org/sdr/SWAA2022010445113.md): Floor Panel · delaminated · Nov 17, 2021 · N784SW · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241DF UPPER SURFACE DELAMINATED; / [01] RECEIVED NEW FLOOR PANEL 241DF P/N 144A5810-128 P/O:1728471 REF. TASK CARD TTG8Q006QHHG FOR PANEL INSTALLATION; [02] VERIFIED STEP 1
- [SDR SWAA2022011244681](https://openairdocs.org/sdr/SWAA2022011244681.md): Fitting · cracked · Nov 16, 2021 · N784SW · Boeing 737 · Trailing Edge Flaps
  > SUPPLEMENTAL INFORMATION: L/H WING T/E AT LWR DEFLECTOR RIB SEAL BRACKET INNER SIDE CRACKED; / [01] REMOVED LWR DEFLECTOR RIB; FITTING AND SEAL; L/H WING T/E LOWER DEFLECTOR RIB REF B737-700 SRM 51-40-02-OG-0.. LOCATED AND DRILLED NEW FITTING PER. REF.B737-70
- [SDR SWAA2022011245110](https://openairdocs.org/sdr/SWAA2022011245110.md): Fitting · cracked · Nov 16, 2021 · N784SW · Boeing 737 · Trailing Edge Flaps
  > SUPPLEMENTAL INFORMATION: L/H WING T/E AT LWR DEFLECTOR RIB SEAL BRACKET INNER SIDE CRACKED; / [01] REMOVED LWR DEFLECTOR RIB; FITTING AND SEAL; L/H WING T/E LOWER DEFLECTOR RIB REF B737-700 SRM 51-40-02-OG-0.. LOCATED AND DRILLED NEW FITTING PER. REF.B737-70
- [SDR SWAA2022010443989](https://openairdocs.org/sdr/SWAA2022010443989.md): Battery Pack · inoperative · Nov 15, 2021 · N784SW · Boeing 737 · Emergency Lighting
  > SUPPLEMENTAL INFORMATION: FOUND EMERGENCY LIGHT POWER SUPPLY M1673 INOP;(AFT GALLEY CEILING).; / [01] REMOVED AND REPLACED BATTERY PACK AT AFT GALLEY CEILING PANEL M1693 POSITION.; [02] PERFORMED OPS OF BATTERY PACK M1693 CHECK FOUND PASS AS PER B737 AMM 33-
- [SDR SWAA2022010443983](https://openairdocs.org/sdr/SWAA2022010443983.md): Floor Panel · deteriorated · Nov 15, 2021 · N784SW · Boeing 737 · Fuselage Floor Panel
  > SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT;FLOOR PANEL 140AF IS DETERIORATED; / [01] FABRICATED AFT CARGO FLOOR PANEL 140AF AS PER B737-700 AMM 25-52-01-201-801; [02] STEP 1 VERIFIED
- [SDR SWAA2022010443428](https://openairdocs.org/sdr/SWAA2022010443428.md): None · out of tolerance · Nov 15, 2021 · N784SW · Boeing 737 · Escape Slide
  > SUPPLEMENTAL INFORMATION: L2 DOOR EMERGENCY ESCAPE SYSTEM; RETAINER CLIPS (BOTH); MEASUREMENTS OUT OF LIMITS; / [01] DUPLICATE. REF TASK CARD# TTG8Q009B258.; [02] VERIFIED
- [SDR SWAA2022010443427](https://openairdocs.org/sdr/SWAA2022010443427.md): Retainer Cup · out of tolerance · Nov 15, 2021 · N784SW · Boeing 7377H4 · Escape Slide
  > L1 DOOR EMERGENCY ESCAPE SYSTEM; RETAINER CLIPS (BOTH); MEASUREMENTS OUT OF LIMITS; / [01] REMOVED AND REPLACED BOTH FLOOR-MOUNTED ESCAPE SLIDE BRACKET/CLIP ON THE L1 ENTRANCE FLOOR IN REF. TO B737 AMM 25-66-02-000-801; 25-66-02-400-801. PENDING INSTALLATION
- [SDR SWAA2020020544161](https://openairdocs.org/sdr/SWAA2020020544161.md): Slide · dislodged · Jan 31, 2020 · N784SW · Boeing 7377H4 · Escape Slide
  > R1 DOOR SLIDE DISLODGED. / RESECURED SLIDE PER AMM.
- [SDR SWAA2020013040919](https://openairdocs.org/sdr/SWAA2020013040919.md): Fitting · corroded · Jan 25, 2020 · N784SW · Boeing 7377H4 · Wing, Landing Gear Attach Fittings
  > LT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG OUTBOARD FACE HAD CORROSION. REPAIRED PER WO SSR1207.
- [SDR SWAA2020013040918](https://openairdocs.org/sdr/SWAA2020013040918.md): Fitting · corroded · Jan 25, 2020 · N784SW · Boeing 7377H4 · Wing, Landing Gear Attach Fittings
  > LT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG INBOARD FACE HAD CORROSION. REPAIRED FACE PER WO 1207.
- [SDR SWAA2020013040917](https://openairdocs.org/sdr/SWAA2020013040917.md): Fitting · corroded · Jan 25, 2020 · N784SW · Boeing 7377H4 · Wing, Landing Gear Attach Fittings
  > LT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG OUTBOARD FACE HAD CORROSION. REPAIRED FACE PER WO SSR1207.

Next page: https://openairdocs.org/deregistered/N784SW-2024-10-04/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 = 'N784SW' AND deregistration_id = 'N784SW-2024-10-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N784SW-2024-10-04/reports

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