N928WN

Service difficulty reports · 238

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWAA2026090873210Fairing · delaminatedDURING 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 AFTSep 3, 2026 · N928WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2026082722091Flashlight · inoperativeFRWD GALLEY FLASH LIGHT INOP (TOP POSITION)_ R&R FWD GALLEY UPPER FLASHLIGHT BATTERY PER AMM 25-64-00.Aug 23, 2026 · N928WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2026082483248Flashlight · inoperativeFLT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FWD F/A FLASHLIGHT IAW AMM 25-64-00. OPS CHECKED GOODAug 18, 2026 · N928WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2026050593743Skin · delaminatedLEFT 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.Apr 28, 2026 · N928WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2026050587998Attach Angle · crackedLEFT 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.Apr 9, 2026 · N928WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2026050587403Floor Panel · pulledFLOOR 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.Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026050587397Floor Panel · pulledAFT 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.Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026050587402Floor Panel · pulledAFT 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.Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026050587398Floor Panel · pulledAFT 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.Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026050587400Floor Panel · pulledAFT FLOOR PANEL 241ABF UPPER SKIN PREVIOUS REPAIR IS DETERIORATED. REPAIRED IAW SRM 53-00-50-2R-1-A00939.Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026050587714Strap · corrodedCORROSION 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.Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026050587713Strap · corrodedCORROSION 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.Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026050587715Plate · corrodedCORROSION 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 146A750Apr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026050587716Plate · corrodedCORROSION 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, AApr 8, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026050587386Floor Support · crackedFLOOR 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-Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026050587208Cargo Track · crackedAFT 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.Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026050587384Floor Support · corrodedCORRODED 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.Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026050587388Floorbeam · corrodedCORRODED 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.Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2026050587390Skin · crackedCRACK 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.Apr 7, 2026 · N928WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2026050587387Strap · corrodedCORROSION 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.Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026050587710Crease Beam · corrodedCORRROSION 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-.Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026050586839Pressure Deck · crackedCRACK 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.Apr 6, 2026 · N928WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026050486433Rivet · looseFORWARD 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.Apr 4, 2026 · N928WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2025121652128Girt Bar · no discrepancyFWD SERVICE DOOR GIRT BAR CAUGHT UPON OPENING. INSPECTED FWD SERVICE DOOR GIRT BAR IAW AMM 25-66-01, NO DEFECTS FOUND.Dec 13, 2025 · N928WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2025112538725Floor Panel · crackedAFT 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.Nov 22, 2025 · N928WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2025082206519Handle · looseRIGHT SIDE OVERWING ASSIST HANDLE BEZEL IS LOOSE.<[01] SECURED IAW AMM 52-22-51.Aug 20, 2025 · N928WN · Boeing 7377H4 · Emergency ExitsSDR SWAA2025042426798Handle · looseR2 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.Apr 21, 2025 · N928WN · Boeing 7377H4 · Galley DoorsSDR SWAA2025042326799Fitting · out of adjustR2 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.Apr 21, 2025 · N928WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2024052990589Sensor · inoperativeON 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 May 28, 2024 · N928WN · Boeing 7377H4 · Trailing Flap Position Indicating SystemSDR SWAA2024052385905Skin · crackedFOUND 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 1May 15, 2024 · N928WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2024052385493Battery Pack · inoperativeFOUND 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.May 14, 2024 · N928WN · Boeing 7377H4 · Emergency LightingSDR SWAA2024052381717Strip · corrodedAFT 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.May 2, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052379691Floorbeam · crackedMAIN 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.Apr 26, 2024 · N928WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024052478210Floor Panel · peelingMAIN 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 1Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052478580Floor Support · crackedFWD 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 SRMApr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052478582Floor Support · crackedFWD 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.Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052478583Floor Support · crackedFWD 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.Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052478221Floor Support · crackedAFT 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 SUPPORApr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052478222Channel · corrodedAFT 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 ATApr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052478367Channel · corrodedAFT 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.Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052478574Channel · corrodedAFT CARGO RIGHT 'Z' CHANNEL IS CORRODED AT 727-727D<[01] REFERED TO TASK CARD# TTG8Q00SXNQG;[02] VERIFIED STEP 1.Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052478581Floor Support · corroded***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]Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052478578Fitting · corroded***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.Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052378573Floor Panel · corrodedPASSENGER 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 TTG8Q00SXMAQApr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052378368Angle · crackedCRACK 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 111A10Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052378211Floor Panel · crackedMAIN 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 TTG8Q0Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052378202Floor Panel · delaminatedMAIN 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 1Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052378207Floor Panel · delaminatedMAIN 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.Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024052378579Floor Support · crackedFWD 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.Apr 23, 2024 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024052482547Floor Panel · damagedAFT 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.Apr 22, 2024 · N928WN · Boeing 7377H4 · Fuselage Floor Panel
Back to N928WN