# Service difficulty reports: N241WN

A list on [N241WN](https://openairdocs.org/aircraft/N241WN.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 · 293 reports

- [SDR SWAA2026092111237](https://openairdocs.org/sdr/SWAA2026092111237.md): Screw · missing · Sep 15, 2026 · N241WN · Boeing 7377H4 · Passenger Compartment Equipment
  > TRAY TABLE AT 14C BROKEN. REPLACED TRAY TABLE SCREW IAW SIP
- [SDR SWAA2026081364358](https://openairdocs.org/sdr/SWAA2026081364358.md): Warning Message · false activation · Aug 9, 2026 · N241WN · Boeing 7377H4 · Central Warning
  > NR 2 ENG OVERHEAT IND WITH NO FUEL APPLIED. INSPECTED NR 2 ENG INLET AND EXHAUST AREA NO DEFECTS NOTED. PERFORMED NORMAL ENG START PER AMM 71-00-00. NO DEFECTS NOTED
- [SDR SWAA2026011561698](https://openairdocs.org/sdr/SWAA2026011561698.md): Lens · loose · Jan 12, 2026 · N241WN · Boeing 7377H4 · Emergency Lighting
  > FWD GALLEY OVERHEAD LIGHT ANNUNCIATOR LENS LOOSE INDICATOR LIGHTS WORKS NORMAL AT THIS TIME. OK TO CONTINUE IAW MEL 25-10-01, SP-1B, 301789. LENS COVER SECURED IN PLACE. REPLACED FWD GALLEY EMERGENCY EXIT SIGN ASSY IAW AMM 33-51-01. OPS CHECKED OKAY.
- [SDR SWAA2026010954929](https://openairdocs.org/sdr/SWAA2026010954929.md): Web · cracked · Dec 23, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB LOCATED BTW BS 400 TO 420 AND AT LEVEL STRINGER 26L, FWD CARGO COMPARTMENT. REPLACED WEB AND FASTENERS LOCATED BTW BS 400 - 420, STRINGER 26L FWD CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 143A7505, SHEET 2, REV B.
- [SDR SWAA2026011248340](https://openairdocs.org/sdr/SWAA2026011248340.md): Web · corroded · Dec 8, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED WEB, BS 1016, RBL 32, REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, PARAGRAPH 9, AND DWG 148A0922, SHEET 20, REV -.
- [SDR SWAA2026010948341](https://openairdocs.org/sdr/SWAA2026010948341.md): Web · corroded · Dec 8, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB, ON BS 1016, LBL 26, AFT GALLEY. REPLACED WEB AND FASTENERS, BS 1016, LBL 2 IAW SRM 51-40-02, 51-10-02, & DWG 148A0922, SHEET 20, REV -.
- [SDR SWAA2026010844137](https://openairdocs.org/sdr/SWAA2026010844137.md): Web · corroded · Dec 8, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB BS 1016, RBL 32 IN AFT GALLEY AREA.
- [SDR SWAA2026010844138](https://openairdocs.org/sdr/SWAA2026010844138.md): Web · corroded · Dec 8, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB, BS 1016, LBL 26 IN AFT GALLEY.
- [SDR SWAA2026011243640](https://openairdocs.org/sdr/SWAA2026011243640.md): Support Angle · cracked · Dec 7, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 663.5, LBL 41, REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, DWG 111A1322, SHEET 5, REV-, AND DWG 111A1000, SHEET 202, REV -.
- [SDR SWAA2026011243639](https://openairdocs.org/sdr/SWAA2026011243639.md): Access Panel · cracked · Dec 7, 2025 · N241WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACKED LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA 114.55 AT LT HORIZONTAL STAB. REPLACED LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA 114.55 AT LT HORIZONTAL STAB AND FASTENERS IAW SRM 51-10-02-0G ITEM 9, SRM 51-40-02-0G, AND DWG 186A1001, SHEET
- [SDR SWAA2026011243314](https://openairdocs.org/sdr/SWAA2026011243314.md): Scuff Plate · cracked · Dec 6, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK CENTER SCUFF PLATE AT FWD SERVICE DOOR. REPAIRED THE CENTER SCUFF PLATE IAW SRM 53-10-15-2R-2, REPAIR 2. AND BAC 5975.
- [SDR SWAA2026011243548](https://openairdocs.org/sdr/SWAA2026011243548.md): Support Angle · cracked · Dec 6, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 294.5, S13L. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, STEP 9, AND DRAWING 141A1311, SHEET 1, REV C.
- [SDR SWAA2026011243547](https://openairdocs.org/sdr/SWAA2026011243547.md): Stringer · cracked · Dec 6, 2025 · N241WN · Boeing 7377H4 · Wing, Longeron/Stringer
  > CRACKED STRINGER U-8 INTERNAL AREA FUEL TANK UPPER POSITION LOC BTW RIB 19 AND RIB 20 AT RT WING. ACCOMPLISHED EA 25-157-03409-WIP1.
- [SDR SWAA2026011243308](https://openairdocs.org/sdr/SWAA2026011243308.md): Plate · corroded · Dec 5, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED BILGE AREA SHIELD PLATE BTW BS 767 & 787, RBL 13, WL 156. REPLACED THE SHIELD PLATEPARTMENT IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 146A0081, SHEET 31, REV -.
- [SDR SWAA2026010943304](https://openairdocs.org/sdr/SWAA2026010943304.md): Plate · corroded · Dec 5, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION BILGE AREA SHIELD PLATE BTW BS 847 - 867, S25R, WL 156, IN THE AFT CARGO BAY. REPLACED THE SHIELD PLATE IAW SRM 51-40-02, & DWG 146A0081, SHEET 31, REV -. <
- [SDR SWAA2026011242700](https://openairdocs.org/sdr/SWAA2026011242700.md): Stringer · cracked · Dec 4, 2025 · N241WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 25L, BS 540. PERFORMED A PERMANENT REPAIR ON STRINGER 25L, BTWN BS 500D & 540 IAW SRM 53-00-03-2R-1, REPAIR 1.
- [SDR SWAA2026011242702](https://openairdocs.org/sdr/SWAA2026011242702.md): Stringer · cracked · Dec 4, 2025 · N241WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 26L, BS 540. PERFORMED A PERMANENT REPAIR ON STRINGER 26L BTWN BS 500D & 540 IAW SRM 53-00-03-2R-1, REPAIR 1.
- [SDR SWAA2026011242703](https://openairdocs.org/sdr/SWAA2026011242703.md): Stringer · cracked · Dec 4, 2025 · N241WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 25R, BS 540. PERFORMED PERMANENT REPAIR ON STRINGER 25R BTW BS 500C - 540 IAW SRM 53-00-03-2R-1, REPAIR 1.
- [SDR SWAA2026011242705](https://openairdocs.org/sdr/SWAA2026011242705.md): Support Bracket · cracked · Dec 4, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT BRACKET, BS 867 BTW S2 & 3R. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02, AND DWG 146A7901, SHEET 66, REV A.
- [SDR SWAA2026011242946](https://openairdocs.org/sdr/SWAA2026011242946.md): Bracket · corroded · Dec 4, 2025 · N241WN · Boeing 7377H4 · Vertical Stabilizer Miscellaneous Structure
  > CORROSION GROUND PLATE LOCATED BTW HINGE 7A TO HINGE 8 AT VERTICAL STABILIZER. REPLACED BRACKET PLATE LOCATED BTW HINGE 7A TO HINGE 8 AT VERTICAL STAB IAW SRM 51-10-02 PARAGRAPH 9, SRM 51-40-02, AND DWG 175A1601, SHEET 18, REV A.
- [SDR SWAA2026010942699](https://openairdocs.org/sdr/SWAA2026010942699.md): Intercostal · cracked · Dec 4, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BS 500D - 520, S28R, FWD CARGO BAY. REPLACED INTERCOSTAL IAW SRM-51-10-02, ITEM 9, & DWG 143A7902, SHEET 126, REV A.
- [SDR SWAA2026010942701](https://openairdocs.org/sdr/SWAA2026010942701.md): Intercostal · cracked · Dec 4, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BS 500D TO BS 520 AND S-28L FWD CARGO BAY. REPLACED WEB - INTERCOSTAL BS 500D - 520, S28L IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7902, SHEET 126, REV A.
- [SDR SWAA2026011242281](https://openairdocs.org/sdr/SWAA2026011242281.md): Retainer · missing · Dec 3, 2025 · N241WN · Boeing 7377H4 · Fuselage Main, Structure
  > MISSING RETAINER AT UPPER SILL DOOR CUT OUT IN THE FWD CARGO BAY. INSTALLED THE RETAINER IAW SOPM 20-50-12.
- [SDR SWAA2026010941830](https://openairdocs.org/sdr/SWAA2026010941830.md): Angle · cracked · Dec 2, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE AT BS 400, S26L IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 2, REV B.
- [SDR SWAA2026011241671](https://openairdocs.org/sdr/SWAA2026011241671.md): Skin Panel · cracked · Dec 1, 2025 · N241WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND ON LT HORIZONTAL STAB LOWER SKIN PANEL. HSS 193.9, AND 16 INCHES FROM FRONT SPAR. INBD SIDE OF RIB. CRACK LENGTH = 0.950 INCH. PERFORMED REPAIR ON LT HORIZONTAL STAB LOWER SKIN PANEL IAW SRM 55-10-01-2R-11, REPAIR 11.
- [SDR SWAA2026011241661](https://openairdocs.org/sdr/SWAA2026011241661.md): Floorbeam · cracked · Dec 1, 2025 · N241WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED FLOORBEAM, BS 540, BETWEEN BL 0 TO LBL 24.75. REPLACED THE FLOORBEAM IAW SRM 51-10-02, PARAGRAPH 9, AND DRAWING 143A0060, SHEET 46, REV -.
- [SDR SWAA2026011241662](https://openairdocs.org/sdr/SWAA2026011241662.md): Floorbeam · cracked · Dec 1, 2025 · N241WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED FLOORBEAM, BS 540, BL 0 TO RBL 24.75. REPLACED FLOORBEAM IAW SRM 51-10-02, PARAGRAPH 9, AND DRAWING 143A0060, SHEET 46, REV -.
- [SDR SWAA2026011241668](https://openairdocs.org/sdr/SWAA2026011241668.md): Support Angle · cracked · Dec 1, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 695, RBL 24.75. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 111A6000, SHEET, 246, REV-.
- [SDR SWAA2026011241663](https://openairdocs.org/sdr/SWAA2026011241663.md): Support Angle · cracked · Dec 1, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 695, BL 0. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 271A9110, SHEET 6, REV A.
- [SDR SWAA2026010941384](https://openairdocs.org/sdr/SWAA2026010941384.md): Stub Frame · cracked · Dec 1, 2025 · N241WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK INDICATION ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5, BTW S8 - 9R AT FWD GALLEY DOOR AREA. REPLACED THE STUB FRAME BETWEEN BS 294.5 - 296.5, BTW S8 - 9R IAW SRM 51-40-02, SRM 51-10-02, DWG 141A8380, SHEET 20, REV -, AND DWG 141A8370, SHEET 10,
- [SDR SWAA2026010941667](https://openairdocs.org/sdr/SWAA2026010941667.md): Gusset · cracked · Dec 1, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED GUSSET, BS 500D, S19R IN THE FWD CARGO BAY. REPLACED GUSSET BS 500D S19R IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 143A7902, SHEET 174, REV -.
- [SDR SWAA2026010940918](https://openairdocs.org/sdr/SWAA2026010940918.md): Light · deteriorated · Nov 30, 2025 · N241WN · Boeing 7377H4 · Emergency Lighting
  > DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ON ALONG PASSENGER CABIN. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN IAW AMM 33-51-15-400-802 INSTALLATION IS DOCUMENTED WHIT TTG8Q0022SA4 AND TTG8Q0022TU0.
- [SDR SWAA2026010948328](https://openairdocs.org/sdr/SWAA2026010948328.md): Pressure Deck · cracked · Nov 30, 2025 · N241WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB, LBL 30, BS 663. PERFORMED PERMANENT REPAIR ON PRESSURE DECK WEB, BS 663.75 - 675, LBL 25 - 60 IN THE MAIN WHEEL WELL IAW SRM 53-40-51-2R-2, REPAIR 2, STEP 4.
- [SDR SWAA2026010740916](https://openairdocs.org/sdr/SWAA2026010740916.md): Pressure Deck · cracked · Nov 30, 2025 · N241WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 30 STA 663 AT PASSENGER CABIN. CRACK LENGTH 0.200 INCH.
- [SDR SWAA2026010940625](https://openairdocs.org/sdr/SWAA2026010940625.md): Scuff Plate · cracked · Nov 29, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK CENTER SCUFF PLATE AT FWD CARGO BAY. REPAIRED CENTER SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1.
- [SDR SWAA2026010940624](https://openairdocs.org/sdr/SWAA2026010940624.md): Scuff Plate · cracked · Nov 29, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED CENTER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1.
- [SDR SWAA2026010940622](https://openairdocs.org/sdr/SWAA2026010940622.md): Scuff Plate · cracked · Nov 28, 2025 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SCUFF PLATE ON FWD CORNER OF AFT CARGO DOOR CUTOUT. REPAIRED SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1.
- [SDR SWAA2025050565629](https://openairdocs.org/sdr/SWAA2025050565629.md): Floor Panel · corroded · Apr 30, 2025 · N241WN · Boeing 7377H4 · Fuselage Floor Panel
  > CORROSION FOUND ON AFT LAV THRESHOLD COMPISITE FLOOR.<[01] C/W EA 25-124-01104;[02] CORRECTED FOR C/W EA 25-125-01104
- [SDR SWAA2025032608826](https://openairdocs.org/sdr/SWAA2025032608826.md): Sign · missing · Mar 24, 2025 · N241WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN MID CABIN IS MISSING<[01] FOUND AND RE-INSTALLED MID CABIN OVERHEAD EMERGENCY EXIT DIRECTIONAL SIGN COVERS AS NEEDED REF AMM 33-51-03
- [SDR SWAA2025021997634](https://openairdocs.org/sdr/SWAA2025021997634.md): Sign · detached · Feb 19, 2025 · N241WN · Boeing 7377H4 · Emergency Lighting
  > AFT GALLEY (RT SIDE) EXIT SIGN FELL OFF<[01] REMOVED AND REPLACED AFT RH SERVICE DOOR EXIT SIGN LIGHT ASSY IAW AMM 33-51-01.
- [SDR SWAA2024100844998](https://openairdocs.org/sdr/SWAA2024100844998.md): Hook And Loop · detached · Oct 4, 2024 · N241WN · Boeing 7377H4 · Escape Slide
  > AFT SERVICE DOOR SLIDE (R2) HOOK AND LOOP STRIPS ON THE GIRT ARE NOT ATTACHED TO HOOK AND LOOP STRIPS ON THE BACKING PAN SHELF<[01] RESECURED AFT SERVICE DOOR (R2) HOOK AND LOOP STRIPS ON THE GIRT TO THE BACKING PAN PER AMM 25-66-00.
- [SDR SWAA2024100845000](https://openairdocs.org/sdr/SWAA2024100845000.md): Hook And Loop · detached · Oct 4, 2024 · N241WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE (L1) HOOK AND LOOP STRIPS ON THE GIRT ARE NOT ATTACHED TO HOOK AND LOOP STRIPS ON THE BACKING PAN SHELF<[01] RESECURED FWD ENTRY DOOR SLIDE (L1) HOOK AND LOOP STRIPS ON THE GIRT TO THE BACKING PAN PER AMM 25-66-00.
- [SDR SWAA2024100845001](https://openairdocs.org/sdr/SWAA2024100845001.md): Hook And Loop · detached · Oct 4, 2024 · N241WN · Boeing 7377H4 · Escape Slide
  > AFT ENTRY DOOR SLIDE (L2) HOOK AND LOOP STRIPS ON THE GIRT ARE NOT ATTACHED TO HOOK AND LOOP STRIPS ON THE BACKING PAN SHELF<[01] RESECURED AFT ENTRY DOOR (L2) HOOK AND LOOP STRIPS ON THE GIRT TO THE BACKING PAN PER AMM 25-66-00.
- [SDR SWAA2024072214201](https://openairdocs.org/sdr/SWAA2024072214201.md): Battery Pack · failed · Jul 19, 2024 · N241WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK AT LOCATION M1672 (AFT RIGHT) FAILED CAPACITY TEST<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION M1672; OPS CHECK GOOD PER AMM 33-51-06
- [SDR SWAA2024072214208](https://openairdocs.org/sdr/SWAA2024072214208.md): Slider · cracked · Jul 19, 2024 · N241WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STABILIZER UPPER AFT SLIDER CRACKED.<[01] R&R RIGHT HORIZONTAL STABILIZER UPPER AFT SLIDER. IAW SRM 51-40-02
- [SDR SWAA2024061299697](https://openairdocs.org/sdr/SWAA2024061299697.md): Seat · out of adjust · Jun 8, 2024 · N241WN · Boeing 7377H4 · Passenger Compartment Equipment
  > EXIT ROW SEAT 11B RECLINES AND SEAT 23F DOES NOT RECLINE. ADJUSTED 11B RECLINE PER SIP AND PERFORMED OPERATIONAL TEST OF 23F PER SIP. NO DEFECTS NOTED.
- [SDR SWAA2024042577954](https://openairdocs.org/sdr/SWAA2024042577954.md): Cover · missing · Apr 22, 2024 · N241WN · Boeing 7377H4 · Emergency Lighting
  > CREW REPORTS OVERWING EMERGENCY EXIT FLOOR SIGN COVER MISSING. INSTALLED OVERWING EMERGENCY EXIT FLOOR EXIT SIGN COVER PER AMM 33-51-01.
- [SDR SWAA2024022355266](https://openairdocs.org/sdr/SWAA2024022355266.md): Tray · broken · Feb 23, 2024 · N241WN · Boeing 7377H4 · Passenger Compartment Equipment
  > TRAY TABLE ROW 11ABC BROKEN<[01] SECURED TRAY TABLE ARM PER CMM 25-23-46
- [SDR SWAA2024011633608](https://openairdocs.org/sdr/SWAA2024011633608.md): Support Angle · cracked · Dec 19, 2023 · N241WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STAR 17R AT FWD GALLEY AREA 2023-756880<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STAR 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 141A8310; SHEET
- [SDR SWAA2024011633609](https://openairdocs.org/sdr/SWAA2024011633609.md): Tie Clip · cracked · Dec 19, 2023 · N241WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2023-756881<[01] REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING # 141A1110 SHEET 17 REV.-.. SEE INDIVIDUAL

Next page: https://openairdocs.org/aircraft/N241WN/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 = 'N241WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N241WN/reports

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