# Service difficulty reports: N468WN

A list on [N468WN](https://openairdocs.org/aircraft/N468WN.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 · 309 reports

- [SDR SWAA2026101210725](https://openairdocs.org/sdr/SWAA2026101210725.md): Light · dirty · Oct 8, 2026 · N468WN · Boeing 7377H4 · Emergency Lighting
  > PHOTOLUMINESCENT STRIP AT MOST AFT L/H CENTER ISLE POSITION HAS INTERNAL MOISTURE. R & R PHOTOLUMINESCENT STRIP IAW AMM 33-51-15-400-802.
- [SDR SWAA2026101299102](https://openairdocs.org/sdr/SWAA2026101299102.md): Light · inoperative · Oct 8, 2026 · N468WN · Boeing 7377H4 · Emergency Lighting
  > EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE AT RT EMER EXIT DOOR. RELAMPED RT EMERGENCY EXIT SLIDE LIGHT IAW AMM 33-51-04.
- [SDR SWAA2026101218078](https://openairdocs.org/sdr/SWAA2026101218078.md): Skin · delaminated · Oct 8, 2026 · N468WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT WING INBD AFT FLAP HAS DELAMINATED 20 INCH FROM INBD EDGE AND 4" FROM T/E ON THE LOWER SIDE. 4.1" X 3.8". 01. REMOVED AND REPLACED IAW AMM 27-51-12-401.
- [SDR SWAA2026090715551](https://openairdocs.org/sdr/SWAA2026090715551.md): Megaphone · inoperative · Sep 3, 2026 · N468WN · Boeing 7377H4 · Emergency Equipment
  > AFT MEGAPHONE INOPERATIVE. REPLACED THE AFT MEGAPHONE IAW AMM 25-64-00.
- [SDR SWAA2026081035960](https://openairdocs.org/sdr/SWAA2026081035960.md): Strap · cracked · Jul 25, 2026 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > RIGHT STUB BEAM STRAP, LOWER AFT FASTENER HOLE FOUND CRACKED AT BS 639 OTBD LAYER. REMOVED AND REPLACED IAW SRM 51-40-02-0G-0-A00729.
- [SDR SWAA2026081095897](https://openairdocs.org/sdr/SWAA2026081095897.md): Strap · cracked · Jul 25, 2026 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > LEFT STUB BEAM STRAP, LOWER, FWD FASTENER HOLE FOUND CRACKED AT BS 639 AT INBD LAYER. OK TO CONTINUE IAW SRM 51-40-02-0G-0-A00729. FASTENER INSTALLATION AND REMOVAL. REPLACED RT STUB BEAM STRAP AT BS 639, LBL 45 & RESTORED FINISHES IAW SRM 51-40-02-0G-0, S
- [SDR SWAA2026061510387](https://openairdocs.org/sdr/SWAA2026061510387.md): Battery Pack · inoperative · Jun 9, 2026 · N468WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT ON LEFT OVER WING EXIT DOOR IS INOPERATIVE. REMOVED AND AND REPLACED THE BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2026052204892](https://openairdocs.org/sdr/SWAA2026052204892.md): Sign · out of adjust · May 20, 2026 · N468WN · Boeing 7377H4 · Emergency Lighting
  > FLIGHT ATTENDANTS REPORT OVERHEAD EMERGENCY EXIT SIGNS MISSING ARROWS. REPLACED CENTER ISEL EMERGENCY EXIT SIGN LENS REF AMM 33-51-01.
- [SDR SWAA2026052204472](https://openairdocs.org/sdr/SWAA2026052204472.md): Lens · wrong part · May 19, 2026 · N468WN · Boeing 7377H4 · Emergency Lighting
  > FLIGHT ATTENDANTS REPORT OVERHEAD EMERGENCY EXIT SIGNS MISSING ARROWS. REPLACED CENTER ISEL EMERGENCY EXIT SIGN LENS IAW AMM 33-51-01.
- [SDR SWAA2026051296765](https://openairdocs.org/sdr/SWAA2026051296765.md): Slide · out of adjust · May 8, 2026 · N468WN · Boeing 7377H4 · Emergency Equipment
  > R1 DOOR SLIDE OUT OF POSITION. SECURED R1 DOOR SLIDE PER MM 25-66-01
- [SDR SWAA2026050695263](https://openairdocs.org/sdr/SWAA2026050695263.md): Light · broken · May 4, 2026 · N468WN · Boeing 7377H4 · Emergency Lighting
  > OVERHEAD EMERGENCY EXIT SIGN AT ROW 15 BROKEN ON AFT SIDE. REMOVED AND REPLACED BROKEN OVERHEAD EXIT SIGN LIGHT ASSEMBLY AT ROW 15 WITH NEW IAW AMM 33-51-01, OPS CHECKED GOOD.
- [SDR SWAA2026021163584](https://openairdocs.org/sdr/SWAA2026021163584.md): Angle · cracked · Jan 22, 2026 · N468WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACKED ANGLE, ORSS 271, RT WING T/E. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2930, SHEET 8, REV -.
- [SDR SWAA2026021163587](https://openairdocs.org/sdr/SWAA2026021163587.md): Plate · cracked · Jan 22, 2026 · N468WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACKED CORRUGATED PLATE, ORSS 261, LT WING T/E. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02, AND DWG 115A2001, SHEET 29, REV-. CRACK LENGTH: 0.830'.
- [SDR SWAA2026021163588](https://openairdocs.org/sdr/SWAA2026021163588.md): Angle · cracked · Jan 22, 2026 · N468WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACKED ANGLE, T/E ORSS 271, LT WING. REPLACED THE ANGLE ON LT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2930, REV-, SHEET 7.
- [SDR SWAA2026021163583](https://openairdocs.org/sdr/SWAA2026021163583.md): Plate · cracked · Jan 22, 2026 · N468WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE ORSS 241, RT WING. REPLACED THE CORRUGATED PLATE T/E ORSS 241, RT WING AND FASTENER IAW SRM 51-40-02, & DWG 115A2001, SHEET 30, REV A, AND SRM 51-10-02, ITEM 9.
- [SDR SWAA2026021163589](https://openairdocs.org/sdr/SWAA2026021163589.md): Support Bracket · cracked · Jan 22, 2026 · N468WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK TRAILING EDGE SUPPORT BRACKET ORSS 271 AT LT WING. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02-0G-0, & SRM 51-10-02-0G-0 ITEM 9. MEASUREMENT OF CRACK: L: 0.475 INCHES.
- [SDR SWAA2026021163586](https://openairdocs.org/sdr/SWAA2026021163586.md): Web · cracked · Jan 22, 2026 · N468WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACKED WEB LOCATED ORSS269 TRAILING EDGE FIXED PANEL RT WING. REPLACED THE WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 115A2512, SHEET 9, REV B.
- [SDR SWAA2026021163579](https://openairdocs.org/sdr/SWAA2026021163579.md): Angle · cracked · Jan 21, 2026 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FLOOR ANGLE, BS 695, BL 0 IN THE AFT PAX CABIN. REPLACED THE FLOOR ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV-.
- [SDR SWAA2026021163423](https://openairdocs.org/sdr/SWAA2026021163423.md): Cover · out of adjust · Jan 21, 2026 · N468WN · Boeing 7377H4 · Escape Slide
  > AFT SERVICE DOOR SLIDE RUBBING AGAINST WITH DOOR SCUFF PLATE. PROPERLY PACKED SLIDE LOWER COVER IAW AMM 25-66-01-400-803, & MT-725-61-06.
- [SDR SWAA2026021163427](https://openairdocs.org/sdr/SWAA2026021163427.md): Cover · out of adjust · Jan 21, 2026 · N468WN · Boeing 7377H4 · Escape Slide
  > AFT ENTRY DOOR SLIDE RUBBING AGAINST WITH DOOR SCUFF PLATE. PROPERLY PACKED THE SLIDE LOWER COVER IAW AMM 25-66-01-400-803, MT-725-61-06.
- [SDR SWAA2026021163425](https://openairdocs.org/sdr/SWAA2026021163425.md): Nut · deteriorated · Jan 21, 2026 · N468WN · Boeing 7377H4 · Passenger/Crew Doors
  > DETERIORATED WHITE NUTS ON ASSIST HANDLE AT FWD ENTRY DOOR CUT OUT SIDEWALL PANEL. REPLACED THE NUTS ON ASSIST HANDLE IAW AMM 25-21-31-420-801, STEP 2.B, & AMM 25-21-31-420-802, STEP 3.B (6).
- [SDR SWAA2026021163582](https://openairdocs.org/sdr/SWAA2026021163582.md): Angle · cracked · Jan 21, 2026 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR ANGLE BS 695, BL 0, FWD PAX CABIN. REPLACED THE FLOOR ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.
- [SDR SWAA2026021163428](https://openairdocs.org/sdr/SWAA2026021163428.md): Access Panel · damaged · Jan 21, 2026 · N468WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 661AB AT RT WING. REPAIRED THE ACCESS PANEL 661AB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026021163429](https://openairdocs.org/sdr/SWAA2026021163429.md): Access Panel · damaged · Jan 21, 2026 · N468WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 561CB AT LT WING. REPAIRED ACCESS PANEL 561CB AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026021163580](https://openairdocs.org/sdr/SWAA2026021163580.md): Light · deteriorated · Jan 21, 2026 · N468WN · Boeing 7377H4 · Emergency Lighting
  > DETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA). REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) IAW IAW AMM 33-51-15-400-802;
- [SDR SWAA2026021163088](https://openairdocs.org/sdr/SWAA2026021163088.md): Pressure Deck · cracked · Jan 20, 2026 · N468WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION FOUND ON THE HORIZONTAL PRESSURE DECK WEB, RBL 41 BTWN BS 663 - 675 IN THE MAIN WHEEL WELL. REPAIRED THE PRESSURE DECK IAW SRM 53-40-51-2R-2, REPAIR 2.
- [SDR SWAA2026021163258](https://openairdocs.org/sdr/SWAA2026021163258.md): Scuff Plate · cracked · Jan 20, 2026 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED AFT CORNER OF THE FWD CARGO SCUFF PLATE. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1.
- [SDR SWAA2026021163259](https://openairdocs.org/sdr/SWAA2026021163259.md): Scuff Plate · cracked · Jan 20, 2026 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED CENTER SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1.
- [SDR SWAA2026021163257](https://openairdocs.org/sdr/SWAA2026021163257.md): Support Beam · cracked · Jan 20, 2026 · N468WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACKED TRAILING EDGE DEFLECTION CONTROL RIB SUPPORT BEAM, RT WING. PERFORMED PERMANENT REPAIR ON TRAILING EDGE DEFLECTION CONTROL RIB SUPPORT BEAM AT RT WING IAW SRM 57-51-02-2R-3, REPAIR 3.
- [SDR SWAA2025081404048](https://openairdocs.org/sdr/SWAA2025081404048.md): Megaphone · inoperative · Aug 13, 2025 · N468WN · Boeing 7377H4 · Emergency Equipment
  > MEGAPHONE FORWARD CABIN. INOPERATIVE. R & R FWD CABIN MEGAPHONE IAW MM 25-64-00.
- [SDR SWAA2025051268000](https://openairdocs.org/sdr/SWAA2025051268000.md): Lens · loose · May 6, 2025 · N468WN · Boeing 7377H4 · Emergency Lighting
  > FO SIDE EMERGENCY EXIT SIGN LOOSE OVER WING EXIT<[01] REPLACED EMERGENCY LIGHT SIGN LENS PER AMM 33-51-01
- [SDR SWAA2025050767588](https://openairdocs.org/sdr/SWAA2025050767588.md): Cover · dislodged · May 5, 2025 · N468WN · Boeing 7377H4 · Emergency Lighting
  > RT OVERWING SIGN DISLODGED (COVER). REINSTALLED RT OVERWING EXIT COVER SIGN PER SIP.
- [SDR SWAA2025050666550](https://openairdocs.org/sdr/SWAA2025050666550.md): Lamp · inoperative · May 2, 2025 · N468WN · Boeing 7377H4 · Emergency Lighting
  > FWD EMERGENCY EXIT SIGN; BETWEEN FWD LAV AND G1; LIGHTS INOP<[01] REPLACED DAMAGED FRONT EMERGENCY EXIT SIGN LAMPS I.A.W AMM 33-51-01-960-801 <BR>OPS CHECKS:GOOD<BR>ATAG:A31161;[02] REPLACED DAMAGED FRONT EMERGENCY EXIT SIGN LAMPS I.A.W AMM 33-51-01-960-801 <B
- [SDR SWAA2025050540505](https://openairdocs.org/sdr/SWAA2025050540505.md): Skin · corroded · Apr 25, 2025 · N468WN · Boeing 7377H4 · Fluid Service Doors
  > DOT A24-1 WATER SERVICE DOOR 146AR OUTER SKIN CORRODED JUST FORWARD OF FORWARD LATCH.<04 - REPAIRED PER [SRM 52-40-01-1A-5-A00193 (PERMANENT (NON-DENT DAMAGE TYPES))]
- [SDR SWAA2025042858100](https://openairdocs.org/sdr/SWAA2025042858100.md): Battery Pack · no test · Apr 23, 2025 · N468WN · Boeing 7377H4 · Emergency Lighting
  > AFT L/H EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025021896662](https://openairdocs.org/sdr/SWAA2025021896662.md): Slide · dislodged · Feb 15, 2025 · N468WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR ESCAPE SLIDE DISLODGED.<[01] REMOVED AND REPLACED SAME FWD SVC DOOR ESCAPE SLIDE IAW MT 725-61-06-FS.
- [SDR SWAA2024102953886](https://openairdocs.org/sdr/SWAA2024102953886.md): Handle · loose · Oct 26, 2024 · N468WN · Boeing 7377H4 · Emergency Equipment
  > MEGAPHONE IN AFT GALLEY HANDLE LOOSE. MISSING SCREW.<[01] REMOVED AND REPLACED AFT MEGAPHONE IAW AMM 25-64-00.
- [SDR SWAA2024042668639](https://openairdocs.org/sdr/SWAA2024042668639.md): Strut · corroded · Mar 29, 2024 · N468WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > CUSTOMER REQUEST-CORROSION ON AFT STRUT FAIRING INBOARD SIDE AT LT PYLON 2024-195942<[01] TOOL USED IN STEP 4: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 130064101 DUE DATE: 13-DIC-24;[02] TOOL USED IN STEP 5: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 210
- [SDR SWAA2024042668638](https://openairdocs.org/sdr/SWAA2024042668638.md): Strut · corroded · Mar 29, 2024 · N468WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > CUSTOMER REQUEST-CORROSION ON AFT STRUT FAIRING INBOARD SIDE AT RT PYLON 2024-195943<[01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN: 45MG; SN:221861811; DUE DATE: 30-NOV-24;[02] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 210138503; DUE DATE: 21-JU
- [SDR SWAA2024042667365](https://openairdocs.org/sdr/SWAA2024042667365.md): Girt Bar · worn · Mar 25, 2024 · N468WN · Boeing 7377H4 · Emergency Equipment
  > WEAR HARDWARE OF ESCAPE SLIDE FLOOR BRACKETS AT AFT SERVICE DOOR AND AFT ENTRY DOOR 2024 195924<[01] REPLACED HARDWARE OF ESCAPE SLIDE FLOOR BRACKETS AT AFT SERVICE DOOR AND AFT ENTRY DOOR IAW B737-700 AMM 25-66-02-400-801;[02] REPLACED HARDWARE OF ESCAPE SLID
- [SDR SWAA2024042667077](https://openairdocs.org/sdr/SWAA2024042667077.md): Angle · cracked · Mar 23, 2024 · N468WN · Boeing 7377H4 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ANGLE LOCATED BS1016 BETWEEN STR3L TO STR3R AT VERTICAL STABILIZER 2024-195913<[01] REPLACED ANGLE LOCATED BS1016 BETWEEN STR3L TO STR3R AT VERTICAL STABILIZER I.A.W. B737-700 SRM 51-40-02 AND DRAWING # 176A7101 REV ? AND DRAWING 176A3001 REV ?D? SEE IND
- [SDR SWAA2024042667074](https://openairdocs.org/sdr/SWAA2024042667074.md): Support Bracket · cracked · Mar 23, 2024 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET LOCATED STA540 AND RBL7 AT CENTER WING BOX 2024-195912<[01] REPLACED SUPPORT BRACKET LOCATED STA540 AND RBL7 AT CENTER WING BOX IAW B737-700 SRM-51-40-02 AND SRM-51-10-02 ITEM 9. MEASUREMENTS CRACK IS: 1.230? TOOL USED: DIGITAL CALIPER P/
- [SDR SWAA2024042667073](https://openairdocs.org/sdr/SWAA2024042667073.md): Angle · cracked · Mar 23, 2024 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED STA663.75 AND LBL9 UPPER POSITION AT CENTER WING BOX. PERFORMED PERMANEN REPAIR ON STA663.75 BTW LBL15 TO LBL25 UPPER POSITION AT CENTER WING BOX IAW B737-700 SRM 57-10-10-2R-5 REPAIR 5 SEE INDIVIAL SIGN OFF BELOW;[03] CORRECTED STEP 2 <B
- [SDR SWAA2024042667076](https://openairdocs.org/sdr/SWAA2024042667076.md): Support Bracket · cracked · Mar 23, 2024 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET LOCATED STA540 AND LBL7 AT CENTER WING BOX 2024-195911<[01] REPLACED SUPPORT BRACKET LOCATED STA540 AND LBL7 AT CENTER WING BOX IAW B737-700 SRM 51-10-02 ITEM 9.;[02] REPLACED SUPPORT BRACKET LOCATED STA540 AND LBL7 AT CENTER WING BOX IAW
- [SDR SWAA2024042966768](https://openairdocs.org/sdr/SWAA2024042966768.md): Stringer · cracked · Mar 22, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK EWIS STR 10 L TIE CLIP BS 259.5 AT COCKPIT (1 EA) 2024 195900<[01] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00SA69T;[02] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00SA69T
- [SDR SWAA2024042666769](https://openairdocs.org/sdr/SWAA2024042666769.md): Bracket · cracked · Mar 22, 2024 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK BRACKET ANGLE (TIE CLIP) 10L BS259.5 AT UPPER FUSELAGE (1 EA). REPLACED BRACKET ANGLE (TIE CLIP) 1(EA) AND FASTENERS LOC. STR 10L BS 259.5 AT UPPER FUSELAGE IAW B737-700 SRM 51-40-02-0G-0 AND DWG #141A0720.;[03] REPLACED BRACKET ANGLE (TIE CLIP) 1(EA) A
- [SDR SWAA2024042566766](https://openairdocs.org/sdr/SWAA2024042566766.md): Lens · broken · Mar 22, 2024 · N468WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN LENS EXIT ON GALLEY 1 AT FWD GALLEY AREA 1EA 2024 195898<[01] REPLACED LENS EXIT ON GALLEY 1 AT FWD GALLEY AREA 1EA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C (10);[02] CERTIFIED WORK PERFORMED
- [SDR SWAA2024042566495](https://openairdocs.org/sdr/SWAA2024042566495.md): Pin · missing · Mar 21, 2024 · N468WN · Boeing 7377H4 · Escape Slide
  > MISSING SAFETY PIN ON ESCAPE SLIDE PACK AT FWD ENTRY DOOR. INSTALLED SAFETY PIN ON ESCAPE SLIDE PACK AT FWD ENTRY DOOR IAW BOEING AMM 25-66-01-000-801 NG AND MT 725-61-06 REM INST SLIDE STEP 3E.
- [SDR SWAA2024042665546](https://openairdocs.org/sdr/SWAA2024042665546.md): Frame · cracked · Mar 19, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FRAME ON BS 907 LOCATED BETWEEN S-25R TO S-26R AFT CARGO COMPARTMENT 2024-195833<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142820025; DUE DATE: 22-J
- [SDR SWAA2024042665547](https://openairdocs.org/sdr/SWAA2024042665547.md): Support Angle · cracked · Mar 19, 2024 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED AFT POSITION BS907 TO BS 927 BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT 2024-195834<[01] REPLACED ANGLE SUPPORT LOCATED AFT POSITION BS907 TO BS 927 BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG

Next page: https://openairdocs.org/aircraft/N468WN/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 = 'N468WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N468WN/reports

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