# Service difficulty reports: N248WN A list on [N248WN](https://openairdocs.org/aircraft/N248WN.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 · 269 reports - [SDR SWAA2026033184022](https://openairdocs.org/sdr/SWAA2026033184022.md): Frame · debonded · Mar 28, 2026 · N248WN · Boeing 7377H4 · Rudder Miscellaneous Structure > RUDDER LT CONDUCTIVE FRAME DEBONDED. REMOVED DAMAGED CONDUCTIVE FRAME PER SRM 51-10-02 GENERAL; AND FASTENERS PER SRM 51-40-02. ACCOMPLISHED PERMANENT REPAIR OF CONDUCTIVE FRAME ZONE 3. IAW SRM 55-40-01-1A-3 ALLOWABLE DAMAGE 3. RUDDER BALANCE ACCOMPLISHED ON - [SDR SWAA2026031178471](https://openairdocs.org/sdr/SWAA2026031178471.md): Lamp · dim · Mar 11, 2026 · N248WN · Boeing 7377H4 · Emergency Lighting > LEFT AND RIGHT OVER-WING-EXIT LIGHTS DIM. REPLACED THE LAMP IAW AMM 33-21-00. - [SDR SWAA2026011360058](https://openairdocs.org/sdr/SWAA2026011360058.md): Battery Pack · inoperative · Jan 10, 2026 · N248WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHTS ASSOCIATED WITH AFT BATTERY PACK M1672 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER M1672 IAW AMM 33-51-06. OPS CHKD GOOD - [SDR SWAA2025081198825](https://openairdocs.org/sdr/SWAA2025081198825.md): Lamp · inoperative · Aug 6, 2025 · N248WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHTS / BIN OVHD AREA LAMP INOP AT SEAT 16 FED AND 19 FED. REMOVED AND REPLACED LAMP BULBS FOR EMERGENCY LIGHTS / BIN OVHD AREA LAMP AT SEAT 16 FED AND 19 FED IAW AMM 33-51-03. OPS CHECK GOOD. - [SDR SWAA2025051970291](https://openairdocs.org/sdr/SWAA2025051970291.md): Lamp · inoperative · May 13, 2025 · N248WN · Boeing 7377H4 · Emergency Lighting > AFT GALLEY ENTRANCE DOOR (R2) EMERGENCY LIGHT IS INOP.<[01] REMOVED AND REPLACED AFT GALLEY ENTRANCE DOOR SLIDE LIGHT LAMP IN REF TO AMM 33-51-04. OPS CEHCK GOOD AT THIS TIME. - [SDR SWAA2025051269123](https://openairdocs.org/sdr/SWAA2025051269123.md): Unknown · odor · May 8, 2025 · N248WN · Boeing 7377H4 · Air Distribution System > ODD ODOR NEAR EMER EXIT ROW<[01] ACCOMPLISHED FIM TASK 21-00 TASK 806. CUSTOMER REPORTED DRY CLEANNG SMELL. INSPECTED AREA. NO SMELLS AT THIS TIME - [SDR SWAA2025013090686](https://openairdocs.org/sdr/SWAA2025013090686.md): Slide · jammed · Jan 29, 2025 · N248WN · Boeing 7377H4 · Escape Slide > WHILE PERFORMING SAMPLE OF AFT SERVICE DOOR ESCAPE SLIDE; DOOR BECAME JAMMED BECAUSE SLIDE COMPARTMENT DID NOT OPEN WITH LOWER LATCH RELEASED. WHEN DOOR WAS FORCED OPEN; SLIDE DROPPED AND DEPLOYED<[01]. INSPECTED DOOR AND ESCAPE SLIDE ENCLOSURE; NO DEFECTS N - [SDR SWAA2024102350941](https://openairdocs.org/sdr/SWAA2024102350941.md): Retainer · loose · Oct 20, 2024 · N248WN · Boeing 7377H4 · Emergency Equipment > FWD ENTRY FWD GIRT BAR RETAINER CLIP FASTENERS LOOSE<[01] SECURED FWD ENTRY FWD GIRT BAR RETAINER CLIP FASTENERS AS REQUIRED PER SRM 51-40-02 - [SDR SWAA2024071611564](https://openairdocs.org/sdr/SWAA2024071611564.md): Battery Pack · inoperative · Jul 12, 2024 · N248WN · Boeing 7377H4 · Emergency Lighting > INOP BATTERY PACK ON POWER SUPPLY UNIT M1670 AT PASSENGER CABIN 1 E/A. 2024-345852<[01] REPLACED EMERGENCY POWER SUPPLY BATTERY M1670 AND
PERFORMED TEST IAW B737-700 AMM 33-51-06-960-805. TEST
IS OK.;[02] CERTIFIED WORK PERFORMED. - [SDR SWAA2024071611932](https://openairdocs.org/sdr/SWAA2024071611932.md): Web · incorrect · Jun 6, 2024 · N248WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > REJECT - IMPROPERLY WEB REPAIR PROCEDURE AT RT HORIZONTAL STABILIZER (TRIMMED OUT WEB INSTEAD STOP DRILL PROCEDURE) 2024-345807<[01] FOR STEP 2; TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N:190023010; DUE DATE: 24-JUL-24;[02] REPAIRED FRONT SPA - [SDR SWAA2024071697034](https://openairdocs.org/sdr/SWAA2024071697034.md): Angle · cracked · Jun 1, 2024 · N248WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON ANGLE LOCATED BTW BS 380 UP TO 400 RBL 43 WL 208.1 2024-345758<[01] REPLACED ANGLE
LOCATED BTW BS 380 UP TO BS400 RBL 43 WL 208.1
IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02
DWG: 143A5400 SHEET: 38 REV: A
SEE INDIVIDUAL SIGN OFFS BE - [SDR SWAA2024071691769](https://openairdocs.org/sdr/SWAA2024071691769.md): Spar Web · cracked · May 30, 2024 · N248WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > (CUSTOMER REQUEST) CRACK ON FRONT SPAR WEB LOCATED BETWEEN STAB STA 138.70 TO STAB STA 147.90 AT RT HORIZONTAL STABILIZER 2024-345743<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[02] REFER TO FAULT TTG8Q00TT24M WHERE - [SDR SWAA2024071691377](https://openairdocs.org/sdr/SWAA2024071691377.md): Support Angle · cracked · May 29, 2024 · N248WN · Boeing 7377H4 · Wing Miscellaneous Structure > CRACK ON SUPPORT ANGLE LOCATED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING 2024-345719<[01] REPLACED SUPPORT ANGLE LOCATED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G-2;SRM 51-10-02-0G-0 PARAGRAPH 9 CHECK CLARENCE BETWEEN SKIN F - [SDR SWAA2024071690935](https://openairdocs.org/sdr/SWAA2024071690935.md): Mount · cracked · May 29, 2024 · N248WN · Boeing 7377H4 · Fuselage Main, Structure > CRACK ON WEATHER RADAR MOUNT SUPPORT STRUCTURE 2024-345680<[01] REPLACED SUPPORT OF WEATHER RADAR MOUNT STRUCTURE IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02 AND DWG# 141A9194 REV D. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT OF WEATHER R - [SDR SWAA2024071691143](https://openairdocs.org/sdr/SWAA2024071691143.md): Access Panel · cracked · May 29, 2024 · N248WN · Boeing 7377H4 · Doors > CRACK LOWER EDGE ACCESS PANEL 211B AT CONTROL CABIN 2024-345710<[01] REPAIRED LOWER EDGE ACCESS PANEL 211B AT CONTROL CABIN IAW B737-700 AMM 25-00-00-340-801 PROCEDURE 8.E MEASURED DAMAGE AREA IS (24IN2) TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A23218437; - [SDR SWAA2024071690937](https://openairdocs.org/sdr/SWAA2024071690937.md): Fitting · deteriorated · May 29, 2024 · N248WN · Boeing 7377H4 · Emergency Equipment > DETERIORATED AFT SERVICE DOOR GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA 2024-345681<[01] REPLACED AFT SERVICE DOOR GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801;[02] REPLACED AFT SERVICE DOOR GIRT BAR FITTING HARDWARE AT AFT - [SDR SWAA2024071190938](https://openairdocs.org/sdr/SWAA2024071190938.md): Fitting · deteriorated · May 29, 2024 · N248WN · Boeing 7377H4 · Escape Slide > DETERIORATED ENTRY DOOR GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA 2024-345684<[01] REPLACED ENTRY DOOR GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801.;[02] REPLACED ENTRY DOOR GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA IAW - [SDR SWAA2024071690667](https://openairdocs.org/sdr/SWAA2024071690667.md): Plate · cracked · May 28, 2024 · N248WN · Boeing 7377H4 · Wing Main, Frame Structure > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 AT RT WING 2024-345621<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 AT RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 115A3700 SHEET: 41 REV: - TOOL USED DIGITAL CA - [SDR SWAA2024071690668](https://openairdocs.org/sdr/SWAA2024071690668.md): Plate · cracked · May 28, 2024 · N248WN · Boeing 7377H4 · Wing Main, Frame Structure > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 305 AT RT WING 2024-345622<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 305 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02 AND DWG # 115A3700 REV-;[02] COMPLETED TASK CERTIFIED - [SDR SWAA2024071690670](https://openairdocs.org/sdr/SWAA2024071690670.md): Bracket · cracked · May 28, 2024 · N248WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON BRACKET LOCATED BS 540 AIR CONDITIONING BLEED DUCT RT SIDE 2024-345627<[01] REPLACED BRACKET LOCATED BS 540 AIR CONDITIONING BLEED DUCT RT SIDE IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02-0G-0;DWG 212A1101 SHEET 3 REV -.TOOL USED DIGIT - [SDR SWAA2024071690377](https://openairdocs.org/sdr/SWAA2024071690377.md): Support Angle · cracked · May 27, 2024 · N248WN · Boeing 7377H4 · Wing Miscellaneous Structure > CRACK ON SUPPORT ANGLE LOCATED ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING 2024-345585<[01] REPLACED SUPPORT ANGLE (FITTING) LOCATED ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING (1 E/A) IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 PARAGRAPH 9 DW - [SDR SWAA2024071690458](https://openairdocs.org/sdr/SWAA2024071690458.md): Angle · cracked · May 27, 2024 · N248WN · Boeing 7377H4 · Wing Miscellaneous Structure > CRACK ON ANGLE LOCATED ON ACCESS PANEL 551FB TRAILING EDGE AT LT 2024-345592<[01] REPLACED ANGLE LOCATED ON ACCESS PANEL 551FB TRAILING EDGE AT LT IAW B737-700 SRM 51-10-02 ITEM 9 AND B737-700 SRM 51-40-02.;[02] COMPLETED TASK CERTIFIED - [SDR SWAA2024071690379](https://openairdocs.org/sdr/SWAA2024071690379.md): Panel · corroded · May 27, 2024 · N248WN · Boeing 7377H4 · Wing Main, Frame Structure > CORROSION ON REFUELING PANEL ON LEADING EDGE AT RT WING 2024-345588<[01] ON STEP 4. TOOL USED: THICKNESS GAGE. P/N: 45MG. S/N: 221859911. DUE DATE: 17-NOV-24.

ON STEP 5. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 60009161631. DUE DATE: 11-MAR-25. - [SDR SWAA2024071690378](https://openairdocs.org/sdr/SWAA2024071690378.md): Fitting · corroded · May 27, 2024 · N248WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > CORROSION ON LOWER LUG FITTING LOCATED AFT FACE POSITION LT HORIZONTAL STABILIZER 2024-345584<[01] FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION LT HORIZONTAL STABILIZER SEE FAULT TTG8Q00TL6U8;[02] FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION LT H - [SDR SWAA2024071690381](https://openairdocs.org/sdr/SWAA2024071690381.md): Fitting · corroded · May 27, 2024 · N248WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > CORROSION ON LOWER LUG FITTING LOCATED AFT FACE POSITION RT HORIZONTAL STABILIZER 2024-345586<[01] FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION LT
HORIZONTAL STABILIZER SEE FAULT TTG8000TL5VX.;[02] CORRECTED CORRECTIVE ACTIONS 1.
FOR REPAIR OF LUG - [SDR SWAA2024071690385](https://openairdocs.org/sdr/SWAA2024071690385.md): Fitting · corroded · May 27, 2024 · N248WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > CORROSION ON REAR SPAR CENTER SECTION LOWER AFT CLEVIS LOCATED FWD FACE RT HORIZONTAL STABILIZER 2024-345590<[01] FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION RT
HORIZONTAL STABILIZER SEE FAULT TTG8000TL5VX.;[02] CORRECTED CORRECTIVE ACTIONS 1.
FO - [SDR SWAA2024071690031](https://openairdocs.org/sdr/SWAA2024071690031.md): Tie Clip · cracked · May 26, 2024 · N248WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN 2024-345554<[01] REPLACED TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 REV-; DWG 141A8380 SHEET 21 REV-. SEE INDIVIDUA - [SDR SWAA2024071690247](https://openairdocs.org/sdr/SWAA2024071690247.md): Support Angle · cracked · May 26, 2024 · N248WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK SUPPORT ANGLE LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN 2024-345574<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN IAW DRAWING # 146A7901-1 SHEET 66 REV: A; B737-700 SRM 51-40-02- - [SDR SWAA2024071690029](https://openairdocs.org/sdr/SWAA2024071690029.md): Angle · cracked · May 26, 2024 · N248WN · Boeing 7377H4 · Wing Miscellaneous Structure > CRACK ON SUPPORT ANGLE LOCATED ORSS 251 AREA OF DEFLECTION CONTROL RIB AT LT TRAILING EDGE 2024-345552<[01] REPLACED SUPPORT ANGLE LOCATED ORSS 251 AREA OF DEFLECTION CONTROL RIB AT LT TRAILING EDGE IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING - [SDR SWAA2024071690030](https://openairdocs.org/sdr/SWAA2024071690030.md): Support Beam · cracked · May 26, 2024 · N248WN · Boeing 7377H4 · Wing Main, Frame Structure > CRACK ON SUPPORT BEAN ON DEFLECTION CONTROL RIB TRAILING EDGE AT LT WING 2024-345553<[01] TOOL USED STEP 8: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 21 JUL 24.;[02] PERFORMED PERMANENT REPAIR ON DEFLECTION CONTROL RIB AREA LH WING IA - [SDR SWAA2024071290028](https://openairdocs.org/sdr/SWAA2024071290028.md): Light · deteriorated · May 26, 2024 · N248WN · Boeing 7377H4 · Emergency Lighting > DETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA). 2024-345547<[01] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) IAW B737-700 AMM 33-51-15-400-802;[02] TASK CARD COMPLETE. - [SDR SWAA2024071689687](https://openairdocs.org/sdr/SWAA2024071689687.md): Scuff Plate · cracked · May 25, 2024 · N248WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON CENTER SCUFF PLATE AT FWD SERVICE DOOR. 2024-345515<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B23272782; DUE DATE: 06-MAR-25.;[02] EQUIPMENT P/N XRP-3000; S/N 1859843; DUE DATE 24-JUL-24 WAS USED ON STEP 4;[03] REPAIRED CENTER SCUFF PLATE A - [SDR SWAA2024071690021](https://openairdocs.org/sdr/SWAA2024071690021.md): Strap · corroded · May 25, 2024 · N248WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON STRAP LOCATED BTW BS1016 TO BS1040 WL208.1 RBL4 AFT GALLEY AREA 2024-345534<[01] REPLACED STRAP LOCATED BTW BS1016 TO BS1040 WL208.1 RBL4 AFT GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DRAWING# 147A5730 SHEET 23 R - [SDR SWAA2024071690022](https://openairdocs.org/sdr/SWAA2024071690022.md): Strap · corroded · May 25, 2024 · N248WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON STRAP LOCATED BTW BS1016 TO BS1040 WL208.1 LBL3 AFT GALLEY AREA 2024-345535<[01] REPLACED STRAP AND FASTENERS LOCATED BTW BS1016 TO BS1040 WL208.1 LBL3 AFT GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 147A5600 - [SDR SWAA2024071189898](https://openairdocs.org/sdr/SWAA2024071189898.md): Floorbeam · cracked · May 25, 2024 · N248WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CRACK FLOOR BEAM LOCATED STA328 AND RBL24.75 WL208.1 AT FWD GALLEY AREA 2024-345526<[01] TOOL USED EDDY CURRENT EQUIPMENT PN:NORTEC 600D;SN:60007161486;DUE DATE:28-JUL-24.;[02] REPAIRED FLOOR BEAM LOCATED STA328 BETWEEN LBL7 TO RBL 65 WL208.1 AT FWD GALLEY ARE - [SDR SWAA2024071689679](https://openairdocs.org/sdr/SWAA2024071689679.md): Intercostal · cracked · May 24, 2024 · N248WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV 2024-345503<[01] REPLACED WEB INTERCOSTAL AND FASTENERS LOC. FLOOR STRUCTURE BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV. IAW B737-700 SRM 51-10-02; 51-40-02 AND - [SDR SWAA2024071689680](https://openairdocs.org/sdr/SWAA2024071689680.md): Intercostal · cracked · May 24, 2024 · N248WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 312 TO BS 328 AND LBL 46 FWD GALLEY AND LAV 2024-345501<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BS 312 TO BS 328 AND LBL 46 FWD GALLEY AREA AND LAV; IAW BOEING 737-700 SRM 51-40-02; - [SDR SWAA2024071689681](https://openairdocs.org/sdr/SWAA2024071689681.md): Intercostal · cracked · May 24, 2024 · N248WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 328 TO BS 344 AND LBL 46 FWD GALLEY AND LAV 2024-345502<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED
BS 328 TO BS 344 AND LBL 46 FWD GALLEY AND LAV.
IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51 - [SDR SWAA2024071689682](https://openairdocs.org/sdr/SWAA2024071689682.md): Intercostal · cracked · May 24, 2024 · N248WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS344 TO BS 360 AND BL 0 FWD GALLEY AND LAV 2024-345505<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS344 TO BS 360 AND BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02-0G-0; 51-40-02-0G AND DWG 147A - [SDR SWAA2024071689683](https://openairdocs.org/sdr/SWAA2024071689683.md): Intercostal · cracked · May 24, 2024 · N248WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 312 TO BS328 AND RBL 31 FWD GALLEY AND LAV 2024-345504<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 312 TO BS328 AND RBL 31 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DRAWING - [SDR SWAA2024071689684](https://openairdocs.org/sdr/SWAA2024071689684.md): Intercostal · cracked · May 24, 2024 · N248WN · Boeing 7377H4 · Fuselage Main, Structure > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND LBL 11 FWD GALLEY AND LAV 2024-345506<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS360 AND LBL 11 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 - [SDR SWAA2024071689686](https://openairdocs.org/sdr/SWAA2024071689686.md): Support Plate · corroded · May 24, 2024 · N248WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON SUPPORT PLATE LOCATED BETWEEN BS 787 TO BS 790 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT 2024-345508<[01] REPLACED SUPPORT PLATE LOCATED BETWEEN BS 787 TO BS 790 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9.;[02] CO - [SDR SWAA2024071689685](https://openairdocs.org/sdr/SWAA2024071689685.md): Support Angle · corroded · May 24, 2024 · N248WN · Boeing 7377H4 · Emergency Equipment > CORROSION ON SUPPORT ANGLE GIRT BAR FITTING LOCATED BS312 TO BS 344 AND LBL 56 WL 208.1 AT FWD GALLEY AREA 2024-345507<[01] REPLACED SUPPORT ANGLES 2 E/A GIRT BAR FITTING LOCATED BS312 AND BS344 AND LBL 56 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 - [SDR SWAA2024071288875](https://openairdocs.org/sdr/SWAA2024071288875.md): Scuff Plate · cracked · May 22, 2024 · N248WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-345451<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: B23272782; DUE DATE: 06-MAR-2024.;[02] CORRECTED STEP 1. TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: B23272782; DUE DATE: 06-MAR-25.;[03] T - [SDR SWAA2024071188500](https://openairdocs.org/sdr/SWAA2024071188500.md): Handle · deteriorated · May 21, 2024 · N248WN · Boeing 7377H4 · Emergency Exits > DETERIORATED NUT ASSIT HANDLE ON FWD ENTRY DOORWAY LINNING AT GALLEY AREA (2EA) 2024-345413<[01] REPLACED NUT ASSISTANT HANDLE ON FWD ENTRY DOORWAY LINNING AT GALLEY AREA (2EA) IAW SOPM-20-50-01 REV.38 AND DWG 411A2600-4B REV.A SHEET 2;[02] REPLACED NUT ASSIST - [SDR SWAA2024071187644](https://openairdocs.org/sdr/SWAA2024071187644.md): Vapor Barrier · cracked · May 19, 2024 · N248WN · Boeing 7377H4 · Wing Main, Frame Structure > (CUSTOMER REQUEST) CRACK ON VAPOR BARRIER LOCATED ON BS 663 RH SIDE AT WING CENTER SECTION 2024-345335<[01] TOOL USED: CALIPER: P/N:500-197-30 SN: B20189521; DUE DATE: 26-JAN-25.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 15-FEB-25.;[0 - [SDR SWAA2024071687149](https://openairdocs.org/sdr/SWAA2024071687149.md): Door · corroded · May 17, 2024 · N248WN · Boeing 7377H4 · Fluid Service Doors > CORROSION INTERNAL SKIN TOILET SERVICE DOOR 145AL AT LOWER FUSELAGE 2024-345277<[01] TOOL USED STEP 4 ULTRASONIC THICKNESS GAGE; P/N: 45 MG; S/ N: 221860711; DUE DATE: 21-NOV-24;[02] EQUIPMENT P/N 45MG; S/N 221861811; DUE DATE 30-NOV-24 WAS USED ON STEP 8;[03] - [SDR SWAA2024050883292](https://openairdocs.org/sdr/SWAA2024050883292.md): Battery Pack · no test · May 7, 2024 · N248WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHTS M1673 BATTERY PACK WILL NOT HOLD A CHARGE. - [SDR SWAA2024051380854](https://openairdocs.org/sdr/SWAA2024051380854.md): Battery Pack · failed · Apr 29, 2024 · N248WN · Boeing 7377H4 · Emergency Lighting > LEFT SIDE EXTERIOR WTB EMERGENCY LIGHT JUST AFT OF FLAP IS INOP<[01] PERFORMED EMERGENCY LIGHTS-OPERATIONAL TEST I.A.W AMM 33-51-00-710-801
OPS CHECK:GOOD;[02] PERFORMED EMERGENCY LIGHTS-OPERATIONAL TEST I.A.W AMM 33-51-00-710-801 FAILS OPS CHECK NEEDS BATT - [SDR SWAA2024051380856](https://openairdocs.org/sdr/SWAA2024051380856.md): Battery Pack · failed · Apr 29, 2024 · N248WN · Boeing 7377H4 · Emergency Lighting > RIGHT SIDE EXTERIOR WTB EMERGENCY LIGHT JUST AFT OF FLAPS IS INOP<[01] PERFORMED EMERGENCY LIGHTS-OPERATIONAL TEST I.A.W AMM 33-51-00-710-801
OPS CHECK:GOOD;[02] PERFORMED EMERGENCY LIGHTS-OPERATIONAL TEST I.A.W AMM 33-51-00-710-801 FAILS OPS CHECK NEEDS BA Next page: https://openairdocs.org/aircraft/N248WN/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 = 'N248WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N248WN/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.