# Service difficulty reports: N952WN

A list on [N952WN](https://openairdocs.org/aircraft/N952WN.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 5 · 222 reports

- [SDR SWAA2026082178201](https://openairdocs.org/sdr/SWAA2026082178201.md): Handle · loose · Aug 16, 2026 · N952WN · Boeing 7377H4 · Passenger/Crew Doors
  > PAX CABIN FWD ENTRY DOOR LOWER ASSIST HANDLE LOOSE. INSTALLED THE ASSIST HANDLE CORRECTLY IAW AMM 52-11-31-400-802 STEP 3.G.(2).
- [SDR SWAA2026082179287](https://openairdocs.org/sdr/SWAA2026082179287.md): Access Panel · damaged · Jul 31, 2026 · N952WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > ELONGATED HOLES ON LEADING EDGE TIP STRUCTURE ACCESS PANEL 341B AT RT HORIZONTAL STAB. REPLACED LEADING EDGE TIP STRUCTURE LOCATED ON ACCESS PANEL 341B AT RT HORIZONTAL IAW SRM 51-40-01 SRM 51-10-02 ITEM 9 AND DWG 186A1001 SHEET 16 REV. A REPLACED LEADING ED
- [SDR SWAA2026082160911](https://openairdocs.org/sdr/SWAA2026082160911.md): Frame · cracked · Jul 30, 2026 · N952WN · Boeing 7377H4 · Nacelle/Pylon, Frame/Spar/Rib
  > CRACKED FRAME, OTBD FAN COWL AFT POSITION, NR 1 ENGINE. REPLACED THE FRAME & FASTENERS IAW SRM 51-40-02, AND 71-13-30, REV 34.
- [SDR SWAA2026081749181](https://openairdocs.org/sdr/SWAA2026081749181.md): Stringer · cracked · Jul 30, 2026 · N952WN · Boeing 7377H4 · Wing, Longeron/Stringer
  > CRACKED ON STRINGER 8. INTERNAL AREA FUEL TANK, RIB 19 - 20, UPPER SKIN, LOWER SURFACE AFT AREA, LT WING. IAW EA 26-157-02068, THE CONFIGURATION IS ACCEPTABLE. TASKCARD COMPLETED.
- [SDR SWAA2026081772706](https://openairdocs.org/sdr/SWAA2026081772706.md): Rib · cracked · Jul 24, 2026 · N952WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACKED LEADING EDGE RIB ACCESS PANEL 331B, HSS 95.96, LT HORIZONTAL STAB. REPLACED RIB IAW SRM 51-10-02, ITEM 9, DWG 186A1303, SHEET 1, REV A, AND DWG 186A1001, SHEET 19, REV -.
- [SDR SWAA2026082160196](https://openairdocs.org/sdr/SWAA2026082160196.md): Support · corroded · Jul 23, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED SUPPORT ZEE, BS 727 - 847, LBL 21, WL 156 (10 POINTS) IN THE AFT CARGO BAY. REPLACED SUPPORT AND FASTENERS IAW SRM 51-40-02-0G-0, DWG 146A7500, SHEET 173, REV - & SRM 53-00-53-2R-6.
- [SDR SWAA2026082174260](https://openairdocs.org/sdr/SWAA2026082174260.md): Web · corroded · Jul 23, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED WEB, BS 747 - 767, RBL 22, WL 156, IN THE AFT CARGO BAY. REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 146A7502, SHEET 49, REV-.
- [SDR SWAA2026082196517](https://openairdocs.org/sdr/SWAA2026082196517.md): Web · corroded · Jul 23, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED SHIELD WEB BTWN BS 767 & 794.3, WL 156, & RBL 22 IN THE AFT CARGO BAY, REPLACED THE SHIELD WEB IAW SRM 51-40-02-0G, AND DWG 146A0081, SHEET 43, REV-.
- [SDR SWAA2026082142009](https://openairdocs.org/sdr/SWAA2026082142009.md): Support · corroded · Jul 23, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED SUPPORT ZEE BTWN BS 727 & 767, RBL 21, WL 156. (7 POINTS) IN THE AFT CARGO BAY. REPLACED SUPPORT ZEE AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 53-00-53-2R-6, REPAIR 6, & DWG 146A7500, SHEET 173, REV-.
- [SDR SWAA2026082198560](https://openairdocs.org/sdr/SWAA2026082198560.md): Web · cracked · Jul 23, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED WEB, BS 927 - 947.5, STR 25R IN THE AFT CARGO BAY. REPLACED THE WEB, NUTPLATES 5(E/A) AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 147A7500, SHEET 37, REV-.
- [SDR SWAA2026082152321](https://openairdocs.org/sdr/SWAA2026082152321.md): Fitting · cracked · Jul 23, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED FITTING, BS 947.5, STR 26L. REPLACED THE FITTING IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, & DRAWING 149A8103, SHEET 8, REV -.
- [SDR SWAA2026081761813](https://openairdocs.org/sdr/SWAA2026081761813.md): Support Angle · cracked · Jul 23, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED CARGO LINER SUPPORT ANGLE, BS 727E, LBL 51, IN THE AFT CARGO BAY. REPLACED LINER SUPPORT ANGLE IAW SRM 51-40-02-0G-0, DWG 149A9490, SHEET 21, REV-, AND DWG 146A7942, SHEET 39, REV-.
- [SDR SWAA2026081741374](https://openairdocs.org/sdr/SWAA2026081741374.md): Angle · cracked · Jul 23, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE BS 867, STR 26L - 27L. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, & DWG 149A8102, SHEET 19, REV A.
- [SDR SWAA2026081734883](https://openairdocs.org/sdr/SWAA2026081734883.md): Support Angle · cracked · Jul 23, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED CARGO LINER SUPPORT ANGLE, BS 887, RBL 53, AFT CARGO BAY. PERFORMED REPAIR ON CARGO LINER SUPPORT ANGLE IAW SRM 51-70-11-2R-0, SRM 51-10-02-0G, PARAGRAPH 9, & 51-40-02-0G-0.
- [SDR SWAA2026081786862](https://openairdocs.org/sdr/SWAA2026081786862.md): Support Angle · cracked · Jul 23, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK CARGO LINER SUPPORT ANGLE, BS 727D, LBL 51 IN THE AFT CARGO BAY. FAULT RESOLVED ON OTHER FAULT DOCUMENTED ON TTG8Q01DC1BT.
- [SDR SWAA2026081787560](https://openairdocs.org/sdr/SWAA2026081787560.md): Rib · cracked · Jul 23, 2026 · N952WN · Boeing 7377H4 · Vertical Stabilizer, Spar/Rib
  > CRACK ACCESS PANEL 321A LEADING EDGE RIB 8 VERTICAL STABILIZER 2026-443094 REPLACED RIB ASSY 8 AND FASTENERS OF THE ACCESS PANEL 321A AT VERTICAL STABILIZER FIN IAW B737-700 SRM 51-40-02 B737-700 SRM 51-10-02 AND DWG 174A1008 SHEET 2 REV C AND 174A0103 SHEET 1
- [SDR SWAA2026081791006](https://openairdocs.org/sdr/SWAA2026081791006.md): Support Angle · cracked · Jul 23, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED CARGO LINER SUPPORT ANGLE, BS 727B, LBL 51 IN THE AFT CARGO BAY. REPLACED THE LINER SUPPORT ANGLE IAW SRM 51-40-02-0G-0, DWG 149A9490, SHEET 21, REV-, & DWG 146A7942, SHEET 39, REV-.
- [SDR SWAA2026081769287](https://openairdocs.org/sdr/SWAA2026081769287.md): Seal · cracked · Jul 23, 2026 · N952WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > CRACKED SEAL BLADE ACCESS PANEL 333AT, LT HORIZONTAL STAB. REPLACED THE SEAL BLADE ACCESS PANEL 333AT IAW SRM 51-40-02, & DWG 186A3101, SHT 19, REV -.
- [SDR SWAA2026081760834](https://openairdocs.org/sdr/SWAA2026081760834.md): Light · inoperative · Jul 22, 2026 · N952WN · Boeing 7377H4 · Emergency Lighting
  > INOPERATIVE EMERGENCY LIGHT ON LAVATORY B. REPLACED EMERGENCY LIGHT IAW AMM 33-51-01-960-802. TESTED OK.
- [SDR SWAA2026081771897](https://openairdocs.org/sdr/SWAA2026081771897.md): Angle · cracked · Jul 22, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, BS 500D, STR 28L, FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A7902, SHEET 126, REV A.
- [SDR SWAA2026082134945](https://openairdocs.org/sdr/SWAA2026082134945.md): Gusset · cracked · Jul 21, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED GUSSET ANGLE, BS 500D, STR 19L IN THE FWD CARGO BAY. REPLACED THE GUSSET ANGLE AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 143A7902, SHEET 259, REV-.
- [SDR SWAA2026081700759](https://openairdocs.org/sdr/SWAA2026081700759.md): Tie Clip · cracked · Jul 21, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED TIE CLIP, BS 500C, STR 19L IN THE FWD CARGO BAY. REPLACED THE TIE CLIP IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, & DWG 143A1224, SHT 49, REV-.
- [SDR SWAA2026081782335](https://openairdocs.org/sdr/SWAA2026081782335.md): Gusset · cracked · Jul 21, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK GUSSET ANGLE, BS 500D, STRINGER 19R IN THE FWD CARGO BAY. REPLACED THE GUSSET ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, & DWG 143A7902, SHT 259, REV-.
- [SDR SWAA2026081755543](https://openairdocs.org/sdr/SWAA2026081755543.md): Crossbeam · cracked · Jul 21, 2026 · N952WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED FLOOR BRAKE PANEL, BS 540, LBL 1 IN PAX CABIN. REPLACED THE FLOOR BRAKE PANEL IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A0060, SHEET 58, REV A.
- [SDR SWAA2026081784126](https://openairdocs.org/sdr/SWAA2026081784126.md): Threshold · cracked · Jul 21, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SCUFF PLATE AFT CORNER, AFT CARGO BAY. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4. B, STEPS 2 - 7, FIGURE 203.
- [SDR SWAA2026081786778](https://openairdocs.org/sdr/SWAA2026081786778.md): Angle · cracked · Jul 21, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, BS 400, LBL 25 IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM-51-10-02, ITEM (9), SRM-51-40-02, & DWG:143A7505, SHEET 117, REV-.
- [SDR SWAA2026081716148](https://openairdocs.org/sdr/SWAA2026081716148.md): Tie Clip · cracked · Jul 21, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK TIE-CLIP LOCATED BS500D, STR 26R IN THE FWD CARGO BAY. PERFORMED DETAIL VISUAL INSPECTION ON TIE-CLIP AND DID NOT FIND A CRACK IAW SRM 51-00-06-0G-0, & APPLIED PROTECTIVE TREATMENT ON HEAD FASTENERS OF TIE-CLIP IAW SRM 51-20-01-0G-0,
- [SDR SWAA2026081769113](https://openairdocs.org/sdr/SWAA2026081769113.md): Crossbeam · cracked · Jul 21, 2026 · N952WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED FLOOR STRUCTURE BRAKE PANEL BS 540 AND RBL 1. REPLACED FLOOR STRUCTURE BRAKE PANEL BS 540 AND RBL 1 TO RBL 24.75 IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A0060, SHT 58, REV A.
- [SDR SWAA2026081784221](https://openairdocs.org/sdr/SWAA2026081784221.md): Angle · cracked · Jul 21, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, BS 440, LBL 21 IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A7505, SHT 118, REV-.
- [SDR SWAA2026081763623](https://openairdocs.org/sdr/SWAA2026081763623.md): Web · cracked · Jul 21, 2026 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED WEB BTW BS 500B - 500C, LBL 21 FWD CARGO BAY. REPLACED WEB BS 500B - 500C, LBL 21 IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHT 117, REV-.
- [SDR SWAA2026082131133](https://openairdocs.org/sdr/SWAA2026082131133.md): Light · deteriorated · Jul 20, 2026 · N952WN · Boeing 7377H4 · Emergency Lighting
  > DETERIORATED PHOTOLUMINESCENT STRIP (5EA) LT & RT SIDES, ALONG PAX CABIN. REPLACED PHOTOLUMINESCENT STRIP (5EA) IAW AMM-33-51-15-400-802.
- [SDR SWAA2026081786772](https://openairdocs.org/sdr/SWAA2026081786772.md): Girt Bar · worn · Jul 20, 2026 · N952WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED GIRT BAR FITTINGS HARDWARE AND PLATE ON ENTRY AND SERVICE DOORS. REPLACED THE GIRT BAR FITTINGS HARDWARE AND PLATE IAW AMM 25-66-02-000-801, AND AMM 25-66-02-400-801. TESTED OK.
- [SDR SWAA2026081746157](https://openairdocs.org/sdr/SWAA2026081746157.md): Floor Panel · elongated · Jul 20, 2026 · N952WN · Boeing 7377H4 · Fuselage Floor Panel
  > ELONGATED HOLES ON FLOOR PANEL 120CF IN THE FWD CARGO BAY. FABRICATED A NEW FLOOR PANEL 120CF IAW AMM 25-52-01-201-801, & DWG 453A1610, SHEET 2, REV D.
- [SDR SWAA2026081716175](https://openairdocs.org/sdr/SWAA2026081716175.md): Fitting · deteriorated · Jul 20, 2026 · N952WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED GIRT BAR FITTINGS HARDWARE AND PLATE ON ENTRY AND SERVICE DOOR AT FWD GALLEY. REPLACED GIRT BAR FITTINGS HARDWARE AND PLATE ON ENTRY AND SERVICE DOOR AT FWD GALLEY AREA IAW AMM 25-66-02-000-801, AND AMM 25-66-02-400-801. TESTED OK.
- [SDR SWAA2026081717544](https://openairdocs.org/sdr/SWAA2026081717544.md): Pressure Deck · cracked · Jul 19, 2026 · N952WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB, LBL 31 BTWN BS 663 - 675 IN THE MAIN WHEEL WELL. PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB IAW SRM 53-40-51-2R-2, REPAIR 2, PARAGRAPH 4.L, FIGURE 203, & SRM 51-40-02-0G-0.
- [SDR SWAA2026081735919](https://openairdocs.org/sdr/SWAA2026081735919.md): Access Panel · cracked · Jul 19, 2026 · N952WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 561BB ON THE LT WING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2026081757257](https://openairdocs.org/sdr/SWAA2026081757257.md): Access Panel · damaged · Jul 19, 2026 · N952WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON RT WING ACCESS PANEL 661BB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2026082179296](https://openairdocs.org/sdr/SWAA2026082179296.md): Light · inoperative · Jul 18, 2026 · N952WN · Boeing 7377H4 · Emergency Lighting
  > INOPERATIVE BULLNOSE EMERGENCY LIGHT, OVERHEAD BIN 8R IN THE PAX CABIN. REPLACED THE BULB IN THE EMERGENCY LIGHT IAW AMM 33-51-03-960-801, AND TESTED OK.
- [SDR SWAA2026081747166](https://openairdocs.org/sdr/SWAA2026081747166.md): Access Door · damaged · Jul 18, 2026 · N952WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLE ON ACCESS PANEL 571BB TRAILING EDGE ON LT WING. REPAIRED THE ACCESS PANEL 571BB IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2025102928662](https://openairdocs.org/sdr/SWAA2025102928662.md): Fastener · missing · Oct 26, 2025 · N952WN · Boeing 7377H4 · Emergency Equipment
  > R1 GIRT BAR FASTENER TLD. INSTALLED FASTENER IN GIRT BAR ATTACHMENT PER AMM 25-66-01 AND SRM 51-40-02
- [SDR SWAA2025102326056](https://openairdocs.org/sdr/SWAA2025102326056.md): Girt Bar · out of adjust · Oct 20, 2025 · N952WN · Boeing 7377H4 · Emergency Equipment
  > R1 DOOR SLIDE COMPARTMENT GIRT BAR HOOK MISSING 1 RIVET. COMPLIED WITH EA M-23-125-01839 FOR INTERIM REPAIR. TLD ISSUED.
- [SDR SWAA2025063085335](https://openairdocs.org/sdr/SWAA2025063085335.md): Light · inoperative · Jun 25, 2025 · N952WN · Boeing 7377H4 · Emergency Lighting
  > CABIN EMERGENCY LIGHT INOP AT OVERHEAD BIN ROW 9ABC AND 13DEF. <[01] RELAMPED AND OPS CHECKED GOOD IAW MM 33-51-03.
- [SDR SWAA2024101547477](https://openairdocs.org/sdr/SWAA2024101547477.md): Handle · loose · Oct 11, 2024 · N952WN · Boeing 7377H4 · Passenger/Crew Doors
  > AFT ENTRY DOOR FWD HANDLE IS LOOSE<[01] TIGHTENED AFT ENTRY DOOR FWD ASSIST HANDLE PER AMM 25-21-25-420-801 STEP 3.B.(5);[02] VERIFIED ITEM 1
- [SDR SWAA2024101545987](https://openairdocs.org/sdr/SWAA2024101545987.md): Battery Pack · inoperative · Oct 8, 2024 · N952WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1669 INOP<[01] REPLACED EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1669; PERFORMED GOOD TEST PER AMM 33-51-06-960-805.<BR>TASK CARD COMPLETED;[02] VERIFIED ITEM 1
- [SDR SWAA2024101542425](https://openairdocs.org/sdr/SWAA2024101542425.md): Lens · broken · Sep 27, 2024 · N952WN · Boeing 7377H4 · Emergency Lighting
  > SEAT ROW 14ABC EMERGENCY LIGHT LENS BROKEN<[01] REMOVED AND REPLACED BROKEN EMERGENCY LIGHT LENS AT SEAT ROW 14ABC IAW AMM 33-51-03-960-801 STEP 2. D. (1)(2)(3)(A)(C).;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024101542248](https://openairdocs.org/sdr/SWAA2024101542248.md): Skin · delaminated · Sep 26, 2024 · N952WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT OUTBOARD AFT FLAP HAS AREA OF DELAMINATION AT LOWER O/B END<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22-000-801 AND AMM 27-51-22-400-801.;[02] VERIFIED RII ITEMS COMPLETE
- [SDR SWAA2024101540875](https://openairdocs.org/sdr/SWAA2024101540875.md): Seat Track · corroded · Sep 24, 2024 · N952WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK AT LBL 45; IN THE WELL AT STA STA 500D+6 TO STA 500D+9; AND ON THE CROWN AT STA 500D+6.<[01] CORRECTION TO FAULT DESCRIPTION: WATER LINE IS 208.3;[02] SEAT TRACK IS OUT OF LIMITS PER SRM 53-00-52-1A-1 FAULT WILL BE COMPLETED ON JOB CARD
- [SDR SWAA2024101441223](https://openairdocs.org/sdr/SWAA2024101441223.md): Stub Frame · cracked · Sep 24, 2024 · N952WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FOUND ON R1 DOOR STUB FRAME BS 291.5 + 7.5; WL266.5; L: 0.6' MARKED<[01] VERIFIED RII ITEMS COMPLETE;[02] REMOVED DAMAGED STUB FRAME AND INSTALLED NEW STUB FRAME ON R1 DOOR B 291.5 + 7.5; WL266.5 I.A.W. SRM 51-40-02-0G-0; DWG# 141A8370 REV. D;[03] TASK C
- [SDR SWAA2024101540712](https://openairdocs.org/sdr/SWAA2024101540712.md): Web · cracked · Sep 23, 2024 · N952WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT WING TRANSVERSE WEB UPPER O/B LEG IS CRACKED AT O/B ATTACH RIVET<[01] RIGHT WING TRANSVERSE WEB CRACK L = 0.900' AND IS FOUND OUT OF LIMITS PER SRM 57-51-02-1A-1 ALLOWABLE DAMAGE 1; PARR. 4.B.(1)(A); FIG 108.<BR>REMOVED AND REPLACED TRANSVERSE WEB IAW SR
- [SDR SWAA2024101440847](https://openairdocs.org/sdr/SWAA2024101440847.md): Floor Panel · delaminated · Sep 23, 2024 · N952WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241AF TOP SURFACE IS DELAMINATED.<[01] UPDATED MEASUREMENTS.;[02] UPDATED STEP 1;[03] REMOVED PANEL 241AF PER AMM 53-21-00-000-801. IDENTIFIED PANEL IAW SRM 53-00-50-0I-1 FIGURE 4. DAMAGE TO THE PANEL IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-

Next page: https://openairdocs.org/aircraft/N952WN/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 = 'N952WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N952WN/reports

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