# Service difficulty reports: N288WN A list on [N288WN](https://openairdocs.org/aircraft/N288WN.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 · 272 reports - [SDR SWAA2026031879789](https://openairdocs.org/sdr/SWAA2026031879789.md): Light · inoperative · Mar 15, 2026 · N288WN · Boeing 7377H4 · Emergency Lighting > EXTERIOR EMERGENCY LIGHT ON L1 DOOR INOPERATIVE. R&R THE LIGHT ASSEMBLY IAW AMM 33-51-04. OPS CHECKED GOOD. - [SDR SWAA2026021068112](https://openairdocs.org/sdr/SWAA2026021068112.md): Isolation Mount · cracked · Feb 6, 2026 · N288WN · Boeing 7377H4 · Escape Slide > AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATOR CRACKED. R & R AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATORS IAW SRM 51-40-02. - [SDR SWAA2026012965618](https://openairdocs.org/sdr/SWAA2026012965618.md): Battery · inoperative · Jan 29, 2026 · N288WN · Boeing 7377H4 · Emergency Equipment > FWD AND AFT GALLEYS EMERGENCY FLASHLIGHTS REQUIRES REPLACEMENT. REPLACED FWD AND AFT GALLEY EMERGENCY FLASHLIGHT BATTERIES AND PLACARDS IAW AMM 25-64-00. - [SDR SWAA2025112438033](https://openairdocs.org/sdr/SWAA2025112438033.md): Lens · broken · Nov 20, 2025 · N288WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHT LENS BROKEN AT ROW 1C (BULLNOSE). INSTALLED MISSING LENS ON EMERGENCY LIGHT AT 1C PER AMM 33-51-03. - [SDR SWAA2025060373647](https://openairdocs.org/sdr/SWAA2025060373647.md): Light · broken · May 21, 2025 · N288WN · Boeing 7377H4 · Emergency Lighting > AFT ENTRY LOWERED CEILING PANEL EXIT LIGHT HOUSING IS BROKEN.<[01] REMOVED AND REPLACED AND PERFORMED OPS CHECK GOOD ON AFT ENTRY LOWERED CEILING PANEL EXIT LIGHT HOUSING IAW AMM 33-51-01-960-802;[02] VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2025060268965](https://openairdocs.org/sdr/SWAA2025060268965.md): Floor Panel · deformed · May 8, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 221EF HAS SOFT EDGE AT L/H AFT CORNER.<[01] FLOOR PANEL 221EF WITH SOFT EDGE AT L/H AFT CORNER WAS REPAIRED PER SRM 53-00-50-2R-10.;[02] VERIFIED CORRECTIVE ACTION #1 - [SDR SWAA2025060368418](https://openairdocs.org/sdr/SWAA2025060368418.md): Stiffener · elongated · May 7, 2025 · N288WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > STIFFENER AT BS663 LBL40 WL160 HAS ELONGATED FASTENER HOLE<[01] REMOVED AND REPLACED STIFFENER AT BS663 LBL40 WL160 IAW SRM 51-40-02-0G-0 AND DWG 111A7000 REV:-.;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE. - [SDR SWAA2025060366068](https://openairdocs.org/sdr/SWAA2025060366068.md): Frame · cracked · Apr 30, 2025 · N288WN · Boeing 7377H4 · Fuselage Main, Frame > CRACK ON BS 312 FRAME COMMON TO STR 5L ABOVE FWD ENTRY DOOR UPPER SILL WEB.<[01] REPAIRED BS 312 FRAME COMMON TO STR 5L ABOVE FWD ENTRY DOOR UPPER SILL WEB IAW EA 22-153-01244.;[02] VERIFIED ACTION 1 - [SDR SWAA2025060365870](https://openairdocs.org/sdr/SWAA2025060365870.md): Seat Track · corroded · Apr 30, 2025 · N288WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON PAX CABIN SEAT TRACK LBL 45 WL 208 FROM BS 495 TO BS 520 ON TOP MARKED<[01] REMOVED AND REPLACED SEAT TRACK AT LBL 45 WL 208 FROM BS 480-520 IAW SRM 51-40-02; DWG 143A5300; SH42; REV A AND 25-153-01221-WIP1; TOOL USED ID:ATS2889; DUE:12/2025;[02] - [SDR SWAA2025060365868](https://openairdocs.org/sdr/SWAA2025060365868.md): Seat Track · corroded · Apr 30, 2025 · N288WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON PAX CABIN SEAT TRACK LBL 25 WL 208 FROM BS 495 TO BS 520 ON TOP MARKED.<[01] REMOVED CORROSION ON CROWN AT BS 519. BLEND WAS.9'X.4'X.028' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1 PARAGRAPH 4. A. (2) (A) FIGURE 103 DETAIL A-A. DEPTH GAUGE I - [SDR SWAA2025060366062](https://openairdocs.org/sdr/SWAA2025060366062.md): Skin · cracked · Apr 30, 2025 · N288WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin > CRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE;.3' IN LENGTH (MARKED)<[01] REPAIRED LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90 IAW SRM 55-10-01-2R-11 REPAIR 11; TABLE 201; TABLE 202; FIG. 204; DETAIL B AND SRM - [SDR SWAA2025060366066](https://openairdocs.org/sdr/SWAA2025060366066.md): Skin · cracked · Apr 30, 2025 · N288WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin > CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 17.5' FROM FWD EDGE;.55' IN LENGTH (MARKED)<[01] REPAIRED RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90 IAW SRM 55-10-01-2R-11 REPAIR 11; TABLE 201; TABLE 202; FIG. 204; DETAIL B AND - [SDR SWAA2025060266067](https://openairdocs.org/sdr/SWAA2025060266067.md): Frame · cracked · Apr 30, 2025 · N288WN · Boeing 7377H4 · Fuselage Main, Frame > CRACKED FRAME BS 259.5 AT CUTOUT RBL 40 WL 260.<[01] THE DAMAGE WAS REPAIRED WITH A WEB SEGMENT SPLICE PER EA 25-153-01133. AN INSPECTION THRESHOLD IS DEFINED IN EA 25-153-01133-DTI.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE. - [SDR SWAA2025060266057](https://openairdocs.org/sdr/SWAA2025060266057.md): Vapor Barrier · cracked · Apr 30, 2025 · N288WN · Boeing 7377H4 · Fuselage Main, Bulkhead > BS 663 VAPOR BARRIER CRACKED BEHIND HYDRAULIC SYSTEM B GROUND SERVICE DISCONNECT MODULE - RBL 52; WL 184.<[01] BS 663 VAPOR BARRIER CRACK AT RBL 52 WL 184 WAS REPAIRED IAW SRM 51-70-04-2R-10. - [SDR SWAA2025060365706](https://openairdocs.org/sdr/SWAA2025060365706.md): Support Plate · corroded · Apr 29, 2025 · N288WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] CORROSION ON AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE FOUND TO BE OUT OF LIMITS. REMOVED; REPLACED AND INSTALLED NEW - [SDR SWAA2025060365705](https://openairdocs.org/sdr/SWAA2025060365705.md): Sidewall Support · corroded · Apr 29, 2025 · N288WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE FOUND TO BE OUT OF LIMITS. REMOVED; REPLACED AND INSTALLED NEW L/H - [SDR SWAA2025060365704](https://openairdocs.org/sdr/SWAA2025060365704.md): Scuff Plate · cracked · Apr 29, 2025 · N288WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED AFT CARGO BAY AFT CORNER SCUFF PLATE PER SRM 53-60-15-2R-1;[02] VERIFIED CORRECTIVE ACTION - [SDR SWAA2025060365366](https://openairdocs.org/sdr/SWAA2025060365366.md): Skin · debonded · Apr 29, 2025 · N288WN · Boeing 7377H4 · Fuselage Main, Plate/Skin > PANEL 194E OUTER SKIN HAS 2 DISBONDS. (MARKED)<[01] PANEL 194E OUTER SKIN WITH 2 DISBONDS AS MARKED PLUS ONE ADDITIONAL UNMARKED UPPER SKIN DISBOND WERE ALL REPAIRED PER SRM 51-70-05-2R-2. - [SDR SWAA2025060265707](https://openairdocs.org/sdr/SWAA2025060265707.md): Cargo Track · cracked · Apr 29, 2025 · N288WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > AFT CARGO BAY CARGO TRACK IS CRACKED BS767 RBL13 WL156<[01] REMOVED AND REPLACED AFT CARGO BAY CARGO TRACK BS 727+4 - BS 887 RBL 13 WL 156 IAW SRM 51-40-02-0G-0; DWG 146A7500 REV:- AND EA 25-153-01136 REV.A.;[02] VERIFIED CORRECTIVE ACTION - [SDR SWAA2025060365360](https://openairdocs.org/sdr/SWAA2025060365360.md): Floor Panel · delaminated · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 221AF IS DELAMINATED<[01] FLOOR PANEL 221AF WITH UPPER SKIN DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1 - [SDR SWAA2025060365347](https://openairdocs.org/sdr/SWAA2025060365347.md): Floor Panel · delaminated · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 221FF IS DELAMINATED<[01] FLOOR PANEL 221FF UPPER SKIN WITH DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE. - [SDR SWAA2025060365352](https://openairdocs.org/sdr/SWAA2025060365352.md): Floor Panel · delaminated · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 221GF IS DELAMINATED; CORNER CRACKS AND 1 BAD INSERT<[01] FLOOR PANEL 221GF WITH UPPER SKIN DELAMINATIONS; CORNER CRACKS AND 1 BAD INSERT WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE. - [SDR SWAA2025060365346](https://openairdocs.org/sdr/SWAA2025060365346.md): Floor Panel · delaminated · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 231AF IS DELAMINATED<[01] FLOOR PANEL 231AF WITH UPPER SKIN DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE. - [SDR SWAA2025060365345](https://openairdocs.org/sdr/SWAA2025060365345.md): Floor Panel · delaminated · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 232FF IS DELAMINATED. DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 232FF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025060365344](https://openairdocs.org/sdr/SWAA2025060365344.md): Floor Panel · delaminated · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 231JF IS DELAMINATED<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 231JF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025060365060](https://openairdocs.org/sdr/SWAA2025060365060.md): Floor Panel · delaminated · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241VF DELAMINATED<[01] FLOOR PANEL 241VF WITH UPPER SKIN AREAS OF DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE. - [SDR SWAA2025060365057](https://openairdocs.org/sdr/SWAA2025060365057.md): Web · corroded · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON L/H SHEAR WEB AT BS 1026 LBL 7 AND LBL 13 WL 208<[01] REMOVED AND REPLACED L/H SHEAR WEB BS1006-1029 BL0-LBL33 WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 REV: B;[02] VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2025060365340](https://openairdocs.org/sdr/SWAA2025060365340.md): Angle · cracked · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE ON INTERCOSTAL AT BS 380-400 RBL 40 WL 208<[01] REPLACED A NEW ANGLE ON INTERCOSTAL AT BS 380-400; RBL40; WL208 IAW SRM 51-40-02 AND BOEING DWG 143A5400 SH 38 REV A.;[02] VERIFIED CORRECTIVE ACTION - [SDR SWAA2025060365339](https://openairdocs.org/sdr/SWAA2025060365339.md): Floorbeam · corroded · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CORROSION ON FILLER OF FLOOR BEAM AT BS 986 RBL 45 WL 208 MARKED<[01] REMOVED; FABRICATED AND REPLACED FILLER AS SHOWN PREVIOUS REPAIR RECORD ON CCN TTG8Q00L09BK SRM 53-70-51-2R-6 FIG 205 I.A.W SRM 51-40-02-0G-0 WITHOUT ANY DEVIATION. - [SDR SWAA2025060265061](https://openairdocs.org/sdr/SWAA2025060265061.md): Floor Panel · delaminated · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241XF DELAMINATED<[01] FLOOR PANEL 241XF DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1. - [SDR SWAA2025060265063](https://openairdocs.org/sdr/SWAA2025060265063.md): Floor Panel · delaminated · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241YF DELAMINATED<[01] 241YF FLOOR PANEL DELAMINATION DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025060265062](https://openairdocs.org/sdr/SWAA2025060265062.md): Floor Panel · delaminated · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241ABF DELAMINATED<[01] FLOOR PANEL 241ABF WITH DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1. - [SDR SWAA2025060265064](https://openairdocs.org/sdr/SWAA2025060265064.md): Floor Panel · delaminated · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 242UF DELAMINATED AND 5EA BAD INSERTS<[01] FLOOR PANEL 242UF WITH DELAMINATION WAS REPAIRED AND REPLACE DAMAGED INSERTS IAW SRM 53-00-50-2R-1. - [SDR SWAA2025060265358](https://openairdocs.org/sdr/SWAA2025060265358.md): Floor Panel · delaminated · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 221EF IS DELAMINATED<[01] FLOOR PANEL 221EF UPPER SKIN WITH DELAMINATIONS AS MARKED WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1 - [SDR SWAA2025060265359](https://openairdocs.org/sdr/SWAA2025060265359.md): Floor Panel · delaminated · Apr 28, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 221CF IS DELAMINATED<[01] FLOOR PANEL 221CF WITH DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1. - [SDR SWAA2025060364397](https://openairdocs.org/sdr/SWAA2025060364397.md): Floor Panel · pulled · Apr 26, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241DF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025060364396](https://openairdocs.org/sdr/SWAA2025060364396.md): Floor Panel · pulled · Apr 26, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241BF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025060364392](https://openairdocs.org/sdr/SWAA2025060364392.md): Floor Panel · pulled · Apr 26, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 231XF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025060264393](https://openairdocs.org/sdr/SWAA2025060264393.md): Floor Panel · pulled · Apr 26, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241ZF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] CORRECTION TO ITEM #1. CORRECT PANEL IS 231ZF.;[03] VERIFIED CORRECTIVE ACTION ITEM 1 AND 2. - [SDR SWAA2025060264394](https://openairdocs.org/sdr/SWAA2025060264394.md): Floor Panel · pulled · Apr 26, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232SF WAS REPLACED IAW SRM 53-00-50-2R-0;[02] FLOOR PANEL 232SF WAS REPLACED IAW SRM 53-00-50-2R-0 PARA 1. A. NOTE:;[03] VERIFIED CORRECTIVE ACTION ITEM 1 AND 2. - [SDR SWAA2025060264395](https://openairdocs.org/sdr/SWAA2025060264395.md): Floor Panel · pulled · Apr 26, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241FF WAS REPLACED IAW SRM 53-00-50-2R-0 PARA 1.A. NOTE:;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025060264398](https://openairdocs.org/sdr/SWAA2025060264398.md): Floor Panel · pulled · Apr 26, 2025 · N288WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242CF WAS REPLACED IAW SRM 53-00-50-2R-0 PARA 1. A. NOTE:;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025060358379](https://openairdocs.org/sdr/SWAA2025060358379.md): Lamp · burned · Apr 25, 2025 · N288WN · Boeing 7377H4 · Emergency Lighting > LH #1 BIN EMERGENCY LIGHT IS BURNED OUT<[01] REPLACED LH#1 BIN EMERGENCY LIGHT AND PERFORMED GOOD FUNCTIONAL TEST IAW AMM 33-51-03-960-801.-;[02] VERIFIED - [SDR SWAA2025060264390](https://openairdocs.org/sdr/SWAA2025060264390.md): Vapor Barrier · cracked · Apr 25, 2025 · N288WN · Boeing 7377H4 · Fuselage Main, Bulkhead > L/H BS663 VAPOR BARRIER IS CRACKED AT LBL30 WL140<[01] L/H BS663 VAPOR BARRIER; CRACK AT LBL30 WL140; WAS REPAIRED IAW SRM 51-70-04-2R-10. - [SDR SWAA2025021996875](https://openairdocs.org/sdr/SWAA2025021996875.md): Light · inoperative · Feb 17, 2025 · N288WN · Boeing 7377H4 · Emergency Lighting > R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP<[01] R/R THE CHARGER ASSY. FOR M1674; THE R1 EMERGENCY SLIDE LIGHT OP?S CHECKS IAW AMM 33-51-06. - [SDR SWAA2025031094471](https://openairdocs.org/sdr/SWAA2025031094471.md): Compressor · stalled · Feb 8, 2025 · N288WN · Boeing 7377H4 · Turbine Engine Compressor Section > #1 ENG COMPRESSOR STALL ON TAKEOFF ROLL; PAX REPORT FLAMES OUT OF BACK OF ENGINE SMELL NOTED IN CABIN UNEVENTFUL LANDING (SMOOTH ROLLOUT) <[01]. PERFORMED COMPRESSOR STALL BORESCOPE INSPECTION AFTER ENGINE STALL EVENT. IAW AMM 71-00-00-210-801-FOO-NG. REF (T - [SDR SWAA2025011384163](https://openairdocs.org/sdr/SWAA2025011384163.md): Fairing · cracked · Jan 8, 2025 · N288WN · Boeing 7377H4 · Aerodynamic Fairings > LOWER BODY FAIRING 193D HAS DAMAGE. REMOVED PANEL 193D IAW AMM 53-51-21. INSTALLED PANEL 193D REF AMM 53-51-21. - [SDR SWAA2025010884161](https://openairdocs.org/sdr/SWAA2025010884161.md): Fairing · delaminated · Jan 8, 2025 · N288WN · Boeing 7377H4 · Aerodynamic Fairings > 194GL HAS TWO AREAS OF DELAMINATION ON PANEL. REF TTG8Q00Y1F7A AND TTG8Q00Y1HPD FOR REPLACEMENT OF PANEL 194GL - [SDR SWAA2025010884158](https://openairdocs.org/sdr/SWAA2025010884158.md): Fairing · delaminated · Jan 8, 2025 · N288WN · Boeing 7377H4 · Aerodynamic Fairings > WING TO BODY FAIRING 194CL 3EA AREAS OF DELAMINATION. R&R WING TO BODY FAIRING PER AMM 53-51-21 - [SDR SWAA2025010681968](https://openairdocs.org/sdr/SWAA2025010681968.md): Battery Pack · inoperative · Dec 31, 2024 · N288WN · Boeing 7377H4 · Emergency Lighting > EXTERIOR EMERGENCY LIGHT NEAR FWD SERVICE DOOR INOP.<[01] REMOVED AND REPLACED M1674 EMERGENCY LIGHT POWER SUPPLY PER AMM 33-51-06. OPS CHECK GOOD. Next page: https://openairdocs.org/aircraft/N288WN/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 = 'N288WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N288WN/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.