# Service difficulty reports: N928WN

A list on [N928WN](https://openairdocs.org/aircraft/N928WN.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 · 238 reports

- [SDR SWAA2026090873210](https://openairdocs.org/sdr/SWAA2026090873210.md): Fairing · delaminated · Sep 3, 2026 · N928WN · Boeing 7377H4 · Trailing Edge Flaps
  > DURING WALKAROUND FOUND LH WING AFT FLAP FAIRING #3 DELAMINATED AND CRACKED FOUND DELAMINATION MEASURES LENGHT: 15 INCHES APPROX WIDTH: 3 INCHES APPROX. PER SRM 57-53-70-1A-1 DELAMINATION IS BEYOND ALLOWABLE LIMITS OK TO CONTINUE PER CDL 57-10-4. INSTALLED AFT
- [SDR SWAA2026082722091](https://openairdocs.org/sdr/SWAA2026082722091.md): Flashlight · inoperative · Aug 23, 2026 · N928WN · Boeing 7377H4 · Emergency Equipment
  > FRWD GALLEY FLASH LIGHT INOP (TOP POSITION)_ R&R FWD GALLEY UPPER FLASHLIGHT BATTERY PER AMM 25-64-00.
- [SDR SWAA2026082483248](https://openairdocs.org/sdr/SWAA2026082483248.md): Flashlight · inoperative · Aug 18, 2026 · N928WN · Boeing 7377H4 · Emergency Equipment
  > FLT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FWD F/A FLASHLIGHT IAW AMM 25-64-00. OPS CHECKED GOOD
- [SDR SWAA2026050593743](https://openairdocs.org/sdr/SWAA2026050593743.md): Skin · delaminated · Apr 28, 2026 · N928WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT OTBD AFT FLAP INBD AFT CORNER IS DELAMINATED. REMOVED & REPLACED, ADJUSTMENTS ARE GOOD OF THE LT OTBD AFT FLAP IAW AMM 27-51-22-000-801 & AMM 27-51-22-400-801.
- [SDR SWAA2026050587998](https://openairdocs.org/sdr/SWAA2026050587998.md): Attach Angle · cracked · Apr 9, 2026 · N928WN · Boeing 7377H4 · Wing, Attach Fittings
  > LEFT WING TRAILING EDGE ATTACH ANGLE FOR OTBD END OF TRANSVERSE WEB CRACKED. REMOVED AND REPLACED LEFT WING TRAILING EDGE ATTACH ANGLE FOR OTBD END OF TRANSVERSE WEB IAW SRM 51-40-02-0G-0.
- [SDR SWAA2026050587403](https://openairdocs.org/sdr/SWAA2026050587403.md): Floor Panel · pulled · Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026050587397](https://openairdocs.org/sdr/SWAA2026050587397.md): Floor Panel · pulled · Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS. 241YF AFT PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026050587402](https://openairdocs.org/sdr/SWAA2026050587402.md): Floor Panel · pulled · Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242VF UPPER SKIN PREVIOUS REPAIR IS DETERIORATED. 242VF AFT FLOOR PANEL UPPER AND LOWER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026050587398](https://openairdocs.org/sdr/SWAA2026050587398.md): Floor Panel · pulled · Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. 241ZF AFT PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026050587400](https://openairdocs.org/sdr/SWAA2026050587400.md): Floor Panel · pulled · Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241ABF UPPER SKIN PREVIOUS REPAIR IS DETERIORATED. REPAIRED IAW SRM 53-00-50-2R-1-A00939.
- [SDR SWAA2026050587714](https://openairdocs.org/sdr/SWAA2026050587714.md): Strap · corroded · Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS 767+6, RBL 11.5, WL 156. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED IAW SRM 51-10-02.
- [SDR SWAA2026050587713](https://openairdocs.org/sdr/SWAA2026050587713.md): Strap · corroded · Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS 727D+6, RBL 11.5, WL 156. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED PER SRM 51-10-02.
- [SDR SWAA2026050587715](https://openairdocs.org/sdr/SWAA2026050587715.md): Plate · corroded · Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B TO BS 767, LBL 22, WL 156. REMOVED AND REPLACED AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG 146A750
- [SDR SWAA2026050587716](https://openairdocs.org/sdr/SWAA2026050587716.md): Plate · corroded · Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B TO BS 767, RBL22, WL156. EVALUATED; REMOVED; DRILLED AND INSTALLED NEW RT FLOOR TO SIDEWALL SUPPORT PLATE IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, A
- [SDR SWAA2026050587386](https://openairdocs.org/sdr/SWAA2026050587386.md): Floor Support · cracked · Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT IS CRACKED AT BS 320, LBL 44, WL 208. R & R THE FLOOR SUPPORT BS 312 - 328, LBL 44, WL 208 IAW SRM 51-40-02-0G-0, AND DWG 141A5400, REV -. NO LIMITS GIVEN ON SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1, PAR 4.B FOR SPECIFIC CRACK LOCATION, SRM 51-10-
- [SDR SWAA2026050587208](https://openairdocs.org/sdr/SWAA2026050587208.md): Cargo Track · cracked · Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO BAY CARGO TRACK CRACKED BS 767, 747, & 727E, RBL 13, WL 156. REPLACED THE CARGO TRACK, BS 727+4 - 887, RBL 13, WL156 IAW SRM 51-40-02 AS SHOWN IN DWG 146A0061 AND DWG 146A7500. SPLICED AT BS 755 PER SRM 53-00-53-2R-3, REPAIR 3, & EA 26-153-01000.
- [SDR SWAA2026050587384](https://openairdocs.org/sdr/SWAA2026050587384.md): Floor Support · corroded · Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORRODED FLOOR SUPPORT AROUND FLOORBOARD HOLE AT BS 273, LBL 12, WL 208. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02-0G-0, DWG 141A5600, SHEET 2, REV N, & DWG 141A5600, SHEET 1, REV N.
- [SDR SWAA2026050587388](https://openairdocs.org/sdr/SWAA2026050587388.md): Floorbeam · corroded · Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORRODED FLOORBEAM, BS 328, RBL 25, WL 208. REMOVED DAMAGE PART OF THE UPPER TEE FITTING ON THE FLOORBEAM, REPAIRED IAW SRM 53-10-51-2R-7, REPAIR 7.
- [SDR SWAA2026050587390](https://openairdocs.org/sdr/SWAA2026050587390.md): Skin · cracked · Apr 7, 2026 · N928WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON THE RT HORIZONTAL STAB LOWER SKIN AT HSS 193.90, 24 5/8 FROM L/E; L: 0.200. REMOVED AND REPAIRED THE CRACKED RT HORIZONTAL STAB LOWER SKIN IAW SRM 55-10-01-2R-11, REPAIR 11.
- [SDR SWAA2026050587387](https://openairdocs.org/sdr/SWAA2026050587387.md): Strap · corroded · Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT BS 1023 AND 1030, LBL 3, WL 208. REMOVED AND REPLACED REINFORCEMENT STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5600, SHEET 32, REV B.
- [SDR SWAA2026050587710](https://openairdocs.org/sdr/SWAA2026050587710.md): Crease Beam · corroded · Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage Main, Structure
  > CORRROSION WAS FOUND ON CREASE BEAM WEBS AT BS 807-827, WL 208, L69. REMOVED AND REPLACED CREASE BEAM AT BS 807-827, WL 208 IAW SRM 51-40-02-0G-0 AND DWG 146A5900, REV-.
- [SDR SWAA2026050586839](https://openairdocs.org/sdr/SWAA2026050586839.md): Pressure Deck · cracked · Apr 6, 2026 · N928WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK FOUND ON HORIZONTAL PRESSURE DECK AT MID PASSENGER CABIN BS 664, RBL 41, L: 0.6'. REMOVED DAMAGE PART OF THE BEADED PRESSURE DECK WEB AND REPAIRED BS 663- 674, RBL 38-60, WL 202, RESTORED FINISHES, APPLIED CIC IAW SRM 53-40-51-2R-2, REPAIR 2.
- [SDR SWAA2026050486433](https://openairdocs.org/sdr/SWAA2026050486433.md): Rivet · loose · Apr 4, 2026 · N928WN · Boeing 7377H4 · Emergency Equipment
  > FORWARD ENTRY DOOR SLIDE FORWARD GIRT BAR ATTACHMENT LOOSE. REMOVED AND REPLACED RIVETS ON FORWARD ENTRY DOOR SLIDE FORWARD GIRT BAR ATTACHMENT IAW SRM 51-40-02-0G-0 STEP 4.
- [SDR SWAA2025121652128](https://openairdocs.org/sdr/SWAA2025121652128.md): Girt Bar · no discrepancy · Dec 13, 2025 · N928WN · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR GIRT BAR CAUGHT UPON OPENING. INSPECTED FWD SERVICE DOOR GIRT BAR IAW AMM 25-66-01, NO DEFECTS FOUND.
- [SDR SWAA2025112538725](https://openairdocs.org/sdr/SWAA2025112538725.md): Floor Panel · cracked · Nov 22, 2025 · N928WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL CRACKED. REMOVED AND FABRICATED NEW FLOOR PANEL IAW AMM 25-52-10. INSTALLED NEW FLOOR PANEL IAW EA M-25-125-02433.
- [SDR SWAA2025082206519](https://openairdocs.org/sdr/SWAA2025082206519.md): Handle · loose · Aug 20, 2025 · N928WN · Boeing 7377H4 · Emergency Exits
  > RIGHT SIDE OVERWING ASSIST HANDLE BEZEL IS LOOSE.<[01] SECURED IAW AMM 52-22-51.
- [SDR SWAA2025042426798](https://openairdocs.org/sdr/SWAA2025042426798.md): Handle · loose · Apr 21, 2025 · N928WN · Boeing 7377H4 · Galley Doors
  > R2 DOOR ASSIST HANDLE NEEDS SECURED <[01]. RESECURED ASSIST HANDLE R2 DOOR IAW B737 AMM 52-41-31-400-802; [02] RESECURED ASSIST HANDLE R2 DOOR IAW B737 AMM 52-41-31-400-802.\ VERIFIED.
- [SDR SWAA2025042326799](https://openairdocs.org/sdr/SWAA2025042326799.md): Fitting · out of adjust · Apr 21, 2025 · N928WN · Boeing 7377H4 · Emergency Equipment
  > R2 DOOR AFT GIRT BAR FITTING NEEDS SECURED <[01]. RESECURED AFT GIRT BAR FITTING IAW B737 AMM 25-66-02-400-801 TORQUE WRENCH: T8353K DUE: 12/SEP/25;[02] RESECURED AFT GIRT BAR FITTING IAW B737 AMM 25-66-02-400-801 TORQUE WRENCH: T8353K DUE: 12/SEP/25.
- [SDR SWAA2024052990589](https://openairdocs.org/sdr/SWAA2024052990589.md): Sensor · inoperative · May 28, 2024 · N928WN · Boeing 7377H4 · Trailing Flap Position Indicating System
  > ON APPROACH SELECTED FLAPS 5 WITH NO FLAP MOVEMENT OBSERVED FC-27-53257. TE FLAP SUPPORT NO. 8 SKEW PROBLEM<[01] R&R #8 FLAP SKEW SENSOR PER AMM 27-59-01 AND <BR>CLEANED CONNECTOR D0034P PER <BR>SWPM 20-60-01;[02] R&R # 8 FLAP SKEW SENSOR PER AMM 27-59-01 AND
- [SDR SWAA2024052385905](https://openairdocs.org/sdr/SWAA2024052385905.md): Skin · cracked · May 15, 2024 · N928WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FOUND SMALL CRACK @ L/H FUS INT FRAME CUTOUT FLANGE ABOVE L-1 DOOR CUTOUT STA 312 MKD DOT<[01] ACCOMPLISHED REPAIR AS PER SWA EA M-22-153-01244 (TTG8Q00TCSP5);[02] VERIFIED STEP 1
- [SDR SWAA2024052385493](https://openairdocs.org/sdr/SWAA2024052385493.md): Battery Pack · inoperative · May 14, 2024 · N928WN · Boeing 7377H4 · Emergency Lighting
  > FOUND SEVERAL EMERGENCY LIGHTS INOP THRU THE CABIN.<[01] REPLACED EMERGENCY LIGHT BATTERY PACKS AT POWER SUPPLY M1668 AND M1670 AS PER REF AMM TASK 33-51-06-960-805. INSTALLATION TEST FOUND NORMAL.;[02] VERIFIED STEP 1.
- [SDR SWAA2024052381717](https://openairdocs.org/sdr/SWAA2024052381717.md): Strip · corroded · May 2, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMP. LEFT FLOOR CAP STRIP HAS CORROSION.<[01] RECEIVED NEW AFT CARGO COMP. LEFT FLOOR CAP STRIP REF INSTALLATION TO TASK CARD TTG8Q00T4LDX;[02] VERIFIED STEP 1.
- [SDR SWAA2024052379691](https://openairdocs.org/sdr/SWAA2024052379691.md): Floorbeam · cracked · Apr 26, 2024 · N928WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR STRUCTURE PANEL BREAK ASSY AT STA 537 LBL 24.75 TO BL 0 IS CRACKED<[01] REMOVED AND REPLACED MAIN CABIN FLOOR STRUCTURE PANEL BREAK ASSY AT STA 537 LBL 24.75 TO BL 0 AS PER REF SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION.
- [SDR SWAA2024052478210](https://openairdocs.org/sdr/SWAA2024052478210.md): Floor Panel · peeling · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Floor Panel
  > MAIN CABIN FWD WET AREA FLOOR PANEL 222DF TOP SKIN FIBERGLASS PEELING OFF SEVERAL AREAS<[01] REPLACED MAIN CABIN FWD WET AREA FLOOR PANEL 222DF REF. B737-700 AMM 53-21-00-400-801. FLOOR PANEL 222DF WILL BE INSTALL ON FAULT TTG8Q00SGX5S;[02] VERIFIED STEP 1
- [SDR SWAA2024052478580](https://openairdocs.org/sdr/SWAA2024052478580.md): Floor Support · cracked · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD WET AREA INTERCOSTAL BETWEEN STA 360 TO 400 AND LBL 13 IS CRACKED. DOT 82-003. FWD WET AREA INTERCOSTAL UPPER CHORD ANGLE BETWEEN STA 360 TO 380 AND LBL 13 IS CRACKED<[01] REMOVED AND REPLACED UPPER CHORD ANGLE BETWEEN STA 360 TO 380 AND LBL 13 PER REF SRM
- [SDR SWAA2024052478582](https://openairdocs.org/sdr/SWAA2024052478582.md): Floor Support · cracked · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD WET AREA INTERCOSTAL BETWEEN STA 312 AND 328 AND LBL 45.5 IS CRACKED. DOT 82-005.<[01] REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 312 AND 328 AND LBL 45.5 PER REF SRM 51-40-02-0G-0 SAND DWG:141A5400 SHEET:26;[02] VERIFIED STEP 1.
- [SDR SWAA2024052478583](https://openairdocs.org/sdr/SWAA2024052478583.md): Floor Support · cracked · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD WET AREA INTERCOSTAL BETWEEN STA 328 AND 344 AND LBL 45.5 IS CRACKED. DOT 82-006.<[01] REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 328 AND 344 AND LBL 45.5 PER REF SRM 51-40-02-0G-0 AND DWG:141A5400 SHEET:88;[02] VERIFIED STEP 1.
- [SDR SWAA2024052478221](https://openairdocs.org/sdr/SWAA2024052478221.md): Floor Support · cracked · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR SUPPORT IS CORRODED AT 767-787 24' RIGHT OF CENTER LINE.<[01] REMOVED AND REPLACED NEW FLOOR SUPPORT (SHIELD) AT AFT CARGO COMPT FROM STA 767 TO STA 787 PER REF SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.;[03] REMOVED AND REPLACED NEW FLOOR SUPPOR
- [SDR SWAA2024052478222](https://openairdocs.org/sdr/SWAA2024052478222.md): Channel · corroded · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO LEFT SIDE 'Z' CHANNEL IS CORRODED AT 807-747.<[01] REMOVED; FABRICATED AND INSTALLED NEW L/H SIDE Z CHANNEL AT AFT CARGO COMPT FROM STA 807 TO 747 PER REF SRM 51-40-02-0G-0.;[02] CORRECTION: REMOVED; FABRICATED AND INSTALLED NEW L/H SIDE Z CHANNEL AT
- [SDR SWAA2024052478367](https://openairdocs.org/sdr/SWAA2024052478367.md): Channel · corroded · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RIGHT 'Z' CHANNEL IS CORRODED AT 727E-767<[01] FOUND OUT OF LIMITS; FABRICATED NEW RIGHT SIDE Z CHANNEL AT AFT CARGO COMPT FROM STA 727 TO 767 PER REF SRM 53-00-53-1A-2 AND DWG# 146A7502.;[02] VERIFIED STEP 1.
- [SDR SWAA2024052478574](https://openairdocs.org/sdr/SWAA2024052478574.md): Channel · corroded · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RIGHT 'Z' CHANNEL IS CORRODED AT 727-727D<[01] REFERED TO TASK CARD# TTG8Q00SXNQG;[02] VERIFIED STEP 1.
- [SDR SWAA2024052478581](https://openairdocs.org/sdr/SWAA2024052478581.md): Floor Support · corroded · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION***FWD WET AREA INTERCOSTAL BETWEEN STA 294.5 AND 312 AND LBL 11 IS CORRODED. DOT 82-004.<[01] REMOVE AND REPLACE INTERCOSTAL AT FWD WET AREA BETWEEN STA 294.5 TO STA 312 LBL 11 AS PER B737-700 SRM 51-40-02-0G-0 AND BOEING DWG 141A5600 SHEET 1;[02]
- [SDR SWAA2024052478578](https://openairdocs.org/sdr/SWAA2024052478578.md): Fitting · corroded · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** FWD WET AREA FLOOR BEAM FITTING IS CORRODED AT STA 344 AND LBL 59. DOT 82-007<[01] REMOVED AND REPLACED TIEDOWN FITTING AT FWD WET AREA FLOOR AT STA 344 AND LBL 59 PER B737-700 REF SRM 51-40-02-0G-0.;[02] CERTIFIED WORK STEP ACCOMPLISHED.
- [SDR SWAA2024052378573](https://openairdocs.org/sdr/SWAA2024052378573.md): Floor Panel · corroded · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242UF HAS TWO INSERT WITH CORROSION (ONE INSERT GIRT BAR FITTING)<[01] CABIN FLOOR PANEL 242UF WILL BE REPLACED WITH NEW PANEL ON FAULT TTG8Q00SXMAQ;[02] VERIFIED TTG8Q00SXMAQ
- [SDR SWAA2024052378368](https://openairdocs.org/sdr/SWAA2024052378368.md): Angle · cracked · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FOUND AT FASTENER HOLE OF RT VAPOR BARRIER UPPER ATTACH ANGLE AT RBL 31.83.<[01] REMOVED AND REPLACED RT VAPOR BARRIER UPPER ATTACH ANGLE AT CENTER WING REAR SPAR STA 663 BETWEEN RBL 5.0 TO RBL 65.0 AS PER B737-700 SRM 51-40-02-0G-0 AND BOEING DWG 111A10
- [SDR SWAA2024052378211](https://openairdocs.org/sdr/SWAA2024052378211.md): Floor Panel · cracked · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Floor Panel
  > MAIN CABIN FWD WET AREA FLOOR PANEL 221GF HAS FWD CORNER CRACKED<[01] REPLACED MAIN CABIN FWD WET AREA FLOOR PANEL 221GF REF. B737-700 AMM 53-21-00-400-801. PANEL 221GF WILL BE INSTALL ON FAULT TTG8Q00SGX5X;[02] VERIFIED FLOOR PANEL # 221GF REPLACED AND TTG8Q0
- [SDR SWAA2024052378202](https://openairdocs.org/sdr/SWAA2024052378202.md): Floor Panel · delaminated · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Floor Panel
  > MAIN CABIN FWD WET AREA FLOOR BOARD #222CF WITH SIGNS OF DELAMINATION ON TOP OF FLOOR BOARD<[01] REPLACED MAIN CABIN FWD WET AREA FLOOR PANEL 222CF REF. B737-700 AMM 53-21-00-400-801. FLOOR PANEL 222CF WILL BE INSTALL ON FAULT TTG8Q00SGX5U;[02] VERIFIED STEP 1
- [SDR SWAA2024052378207](https://openairdocs.org/sdr/SWAA2024052378207.md): Floor Panel · delaminated · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Floor Panel
  > MAIN CABIN FWD WET AREA FLOOR BOARD #222AF WITH SIGNS OF DELAMINATION ON TOP OF FLOOR BOARD<[01] REPLACED MAIN CABIN FWD WET AREA FLOOR PANEL 222AF REF. B737-700 AMM 53-21-00-400-801. FLOOR PANEL WILL BE INSTALL ON FAULT #TTG8Q00SGWUW;[02] VERIFIED STEP 1.
- [SDR SWAA2024052378579](https://openairdocs.org/sdr/SWAA2024052378579.md): Floor Support · cracked · Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD WET AREA INTERCOSTAL AT STA 277 TO 284 AND RBL 1.5 IS CRACKED. DOT 82-002.<[01] REMOVED AND REPLACED INTERCOSTAL AT STA 277 TO 284 AND RBL 1.5 PER REF SEM 51-40-02-0G-0 AND DWG:141A5400 SHEET 85;[02] VERIFIED STEP 1.
- [SDR SWAA2024052482547](https://openairdocs.org/sdr/SWAA2024052482547.md): Floor Panel · damaged · Apr 22, 2024 · N928WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT WET AREA PANEL 241XF HAS SEVERAL LAYERS OF COMPOSITE MATERIAL LOSS.<[01] RECIEVED NEW FLOOR PANEL 241XF PO# 2059779 REF TASK CARD 'TTG8Q00SGWYT' FOR INSTALLATION;[02] VERIFIED STEP 1.

Next page: https://openairdocs.org/aircraft/N928WN/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 = 'N928WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N928WN/reports

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