# Service difficulty reports: N252WN

A list on [N252WN](https://openairdocs.org/aircraft/N252WN.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 7 · 323 reports

- [SDR SWAA2026052604849](https://openairdocs.org/sdr/SWAA2026052604849.md): Handle · loose · May 19, 2026 · N252WN · Boeing 7377H4 · Emergency Exits
  > EMERGENCY EXIT HANDLE INOP 15F<[01] REPLACED MISSING HARDWARE IN HANDLE TRIM IAW S.I.P.
- [SDR SWAA2026040786145](https://openairdocs.org/sdr/SWAA2026040786145.md): Slide · no discrepancy · Apr 3, 2026 · N252WN · Boeing 7377H4 · Escape Slide
  > L1 DOOR SLIDE FLAP HANGS OUT WHEN ARMED. INSPECTED L1 DOOR SLIDE AND FOUND SLIDE AND GIRT BAR ARM AND STOW NORMALLY IAW AMM 25-66-01 AND TEST OF GIRT BAR IN MT 725-61-06.
- [SDR SWAA2025121651907](https://openairdocs.org/sdr/SWAA2025121651907.md): Megaphone · inoperative · Dec 12, 2025 · N252WN · Boeing 7377H4 · Emergency Equipment
  > FWD MEGAPHONE INOPERATIVE. REPLACED MEGAPHONE IAW AMM 25-64-00, OPS CHKD GOOD. NEXT INSPECTION DUE 12-12-2026.
- [SDR SWAA2025102727283](https://openairdocs.org/sdr/SWAA2025102727283.md): Guard · disengaged · Oct 23, 2025 · N252WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN AFT FLIGHT ATTENDANT CONTROL PANEL EMERGENCY EXIT LIGHT SWITCH COVER CLOSE SPRINGS ARE DISENGAGED FROM ASSEMBLY. REMOVED AND REPLACED AFT ATTENDANT PANEL EMER LIGHT SWITCH GUARD REF SIP
- [SDR SWAA2025102427273](https://openairdocs.org/sdr/SWAA2025102427273.md): Seat Back · out of adjust · Oct 23, 2025 · N252WN · Boeing 7377H4 · Passenger Compartment Equipment
  > CABIN PASSENGER SEATBACK AT 11D RECLINES INTO EXIT ROW. ADJUSTED CABIN PASSENGER SEAT BACK ACTUATOR AT 11D TO PREVENT RECLINE PER CMM 25-21-42
- [SDR SWAA2025082708742](https://openairdocs.org/sdr/SWAA2025082708742.md): Tailpipe · fire · Aug 26, 2025 · N252WN · Boeing 7377H4 · Engine Collector/Tailpipe/Nozzle
  > FIRE REPORTED COMING OUT OF THE TAILPIPE BY ANOTHER SWA ACFT WHEN THE ACFT WAS ON THE TAXI SHORT OF THE RUNWAY. PERFORMED ENGINE VENTS AND DRAIN INSPECTIONS IAW AMM 71-71-00. NO LEAKS NOTED. PERFORMED ENGINE RUN IAW AMM 71-00-00. ENGINE OPERATES NORMAL.
- [SDR SWAA2025072293927](https://openairdocs.org/sdr/SWAA2025072293927.md): Slide · loose · Jul 21, 2025 · N252WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE LOOSE. REINSTALLED FWD ENTRY DOOR SLIDE PER AMM 25-66-01 AND MT 725-61-06. AC OK FOR SERVICE.
- [SDR SWAA2025071490461](https://openairdocs.org/sdr/SWAA2025071490461.md): Tailpipe · fire · Jul 11, 2025 · N252WN · Boeing 7377H4 · Engine Collector/Tailpipe/Nozzle
  > A/C BEHIND REPORTED TAIL PIPE FIRE NR 1 ENGINE. INSPECTED NR 1 ENG IAW FIM 71-05 TASK 811. NO ABNORMAL ACCUMULATION OF OIL IN EXHAUST PLUG AND NO ABNORMAL OIL CONSUMPTION RECORDED. A/C OK FOR SERVICE.
- [SDR SWAA2025060978769](https://openairdocs.org/sdr/SWAA2025060978769.md): Tab · cracked · Jun 6, 2025 · N252WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > EXTERNAL POWER DOOR CUTOUT LOWER TAB CRACKED APPROX 1 AT FWD SIDE. REMOVED AND REPAIRED PER SRM 53-10-15-2R-4-A00964, REPAIR 4.
- [SDR SWAA2025051469258](https://openairdocs.org/sdr/SWAA2025051469258.md): Bracket · cracked · May 10, 2025 · N252WN · Boeing 7377H4 · Wing, Attach Fittings
  > RIGHT WING UPR I/B PANEL SUPPORT FWD ATTACH BRACKET (Z BRACKET) CRACKED.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]
- [SDR SWAA2025013091062](https://openairdocs.org/sdr/SWAA2025013091062.md): Engine · fire · Jan 29, 2025 · N252WN · Boeing 7377H4 · Engine (Turbine/Turboprop)
  > FLAMES REPORTED FROM #1 ENG EXITING TAILPIPE ALL ENGINE PARAMETERS WERE NORMAL.<[01] PERFORMED FIM 71-05 TASK 811; FOUND DEBRIS IN CHIP DETECTER FWD SUMP[ AND AFT SUMP. SENT TO LAB FOR ANALYSIS. WAITING RESULTS AND INSTRUCTIONS.;[02] LAB RESULTS CAME BACK AS R
- [SDR SWAA2024110155368](https://openairdocs.org/sdr/SWAA2024110155368.md): Cover · missing · Oct 31, 2024 · N252WN · Boeing 7377H4 · Emergency Lighting
  > CAPT SIDE EXIT ROW LIGHT COVER MISSING<[01] INSTALLED CAPT SIDE OVER WING LOWER EMERGENCY EXIT COVER PER AMM 33-51-02.
- [SDR SWAA2024093042471](https://openairdocs.org/sdr/SWAA2024093042471.md): Battery Pack · failed · Sep 27, 2024 · N252WN · Boeing 7377H4 · Emergency Lighting
  > EMX BATTERY PACK M01675 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATTERY PACK M01675 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024072414136](https://openairdocs.org/sdr/SWAA2024072414136.md): Charger · damaged · Jul 19, 2024 · N252WN · Boeing 7377H4 · Emergency Lighting
  > BATTERY CHARGER M1675 FRAME DAMAGED AT CIRCULAR CONNECTOR.<[01] REPLACED AND TESTED M1675 BATTERY CHARGER PER AMM 33-51-06-960-806; NO DEFECTS NOTED.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024072414132](https://openairdocs.org/sdr/SWAA2024072414132.md): Battery Pack · failed · Jul 18, 2024 · N252WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS RELATED WITH M1675 FAIL TEST<[01] REPLACED M1675 BATTERY PACK AND TESTED PER AMM 33-51-06-960-805; NO DEFECTS NOTED.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024072414130](https://openairdocs.org/sdr/SWAA2024072414130.md): Light · disconnected · Jul 18, 2024 · N252WN · Boeing 7377H4 · Emergency Lighting
  > EXIT LOCATOR SIGN L1070 AT LEFT OVERWING EXIT DO NOT ILLUMINATE DURING TEST<[01] PERFORMED TROBLEHOOTING EXIT LOCATOR SIGN L1070 AT LEFT OVERWING EXIT DO NOT ILLUMINATE DURING TEST; FOUND LIGHT NO CONNECT; CONNECTED EMERGENCY LIGHT AND PERFORMED GOOD TEST PER
- [SDR SWAA2024072413991](https://openairdocs.org/sdr/SWAA2024072413991.md): Scuff Plate · incorrect · Jul 18, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD GALLEY DOOR SCUFF PLATE AT AFT CORNER SIDE WITH SEVERAL GAP.<[01] REMOVED AND REINSTALLED KICK PLATE IN THE FWD GALLEY DOOR SCUFF PLATE AT AFT CORNER SIDE AND WAS APPLIED ADHESIVE SEALANT IAW AMM 25-27-21-400-801.;[02] REJECT: REFERENCE FOR INSTALL SCUFF P
- [SDR SWAA2024072310837](https://openairdocs.org/sdr/SWAA2024072310837.md): Splice Plate · corroded · Jul 10, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR PANEL SPLICE PLATE AT APPROXIMATELY BS 727D HAS CORROSION.<[01] REMOVED CORRODED SPLICE PLATE IAW AMM 51-40-02;[02] NEW SPLICE PLATE IS PRIMED AND REQUIRES TOPCOAT. APPLIED BAC 702 WHITE TOPCOAT; BMS TYPE 10-11 IAW AMM 51-21-73-370-
- [SDR SWAA2024072310836](https://openairdocs.org/sdr/SWAA2024072310836.md): Splice Plate · corroded · Jul 10, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR PANEL SPLICE PLATE AT APPROXIMATELY BS 767 HAS CORROSION.<[01] REMOVED CORRODED SPLICE PLATE.;[02] NEW SPLICE PLATE IS PRIMED AND REQUIRES TOPCOAT. APPLIED BAC 702 WHITE TOPCOAT; BMS TYPE 10-11 IAW AMM 51-21-73-370-804;[03] UPDATE T
- [SDR SWAA2024072310835](https://openairdocs.org/sdr/SWAA2024072310835.md): Floorbeam · corroded · Jul 9, 2024 · N252WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > DUE TO INTERFERENCE WITH BL 0 INTERCOSTAL ON FWD SIDE OF FLOOR BEAM; REPAIR AT BS 294.5 FLOOR BEAM AT BL 0 REQUIRES RE-MAKING REPAIR PARTS AND INSTALLING ON UPPER SIDE OF FLOOR BEAM.<[01] REPAIRED FLOOR BEAM BS 294.5; BL-0; PER SRM 53-10-51-2R-14 ALTERNATIVE 2
- [SDR SWAA2024072410141](https://openairdocs.org/sdr/SWAA2024072410141.md): Scuff Plate · cracked · Jul 8, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD GALLEY DOOR SCUFF PLATE CRACKED AT UPPER AFT SIDE<[01] STEPS 1;2;&3 VERIFIED COMPLETED.;[02] VERIFIED STEP 5.;[03] VERIFIED STEP 14 COMPLETE.;[04] REMOVED; REPAIRED AND INSTALLED FWD GALLEY DOOR SCUFF PLATE TOOL USED SCREW GUN ID:1698; S/N1505370; DUE:05/2
- [SDR SWAA2024072309512](https://openairdocs.org/sdr/SWAA2024072309512.md): Floor Panel · debonded · Jul 6, 2024 · N252WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT WET AREA FLOOR PANEL 242TF FWD RH CORNER LOWER PLIES DISBONDED<[01] 242TF AFT FLOOR PANEL FWD RH CORNER DAMAGED LOWER SURFACE PLIES HAVE BEEN REPAIRED IAW SRM 53-00-50-2R-1 AND BOEING DWG: 147A5810 ID: 0094.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02]
- [SDR SWAA2024072406473](https://openairdocs.org/sdr/SWAA2024072406473.md): Web · corroded · Jun 28, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOT WITH CORROSION ON FCB DOOR CUTOUT SURROUND THRESHOLD BS460+5; 480+4;480+10 RBL29;WL156<[01] REMOVED AND REPLACED SUBTHRESHOLD WEB BS440 TO BS492.4 RBL29 WL156 IAW SRM 5 1-40-02-0G-0 AND DWG 143A8330 REV A;[02] VERIFIED RII ITEMS COMPLETE
- [SDR SWAA2024072406471](https://openairdocs.org/sdr/SWAA2024072406471.md): Web · corroded · Jun 28, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOT WITH CORROSION ON ACB DOOR CUTOUT SURROUND THRESHOLD AT BS794 TO 847 RBL 29; WL 158.<[01] COMPLETED STEP 7 AND PARTIAL STEP 4;[02] REMOVED AND REPLACED ACB DOOR CUTOUT SURROUND THRESHOLD WEB AT BS 794 TO BS 847 RBL 29 WL 158 IAW SRM 51-40-02 AND
- [SDR SWAA2024072308160](https://openairdocs.org/sdr/SWAA2024072308160.md): Sidewall Support · mechanic error · Jun 28, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > REJECT: DURING LOCATED AND DRILLED FOR NEW SIDEWALLED SUPPORT FOUND SEVERAL MISDRILLED HOLES AT THE LOWER FLANGE MARKED (AT THE NEW PART)<[01] VERIFIED STEP 3 COMPLETE; STEP 5 IN PARTIAL.;[02] MADE REPAIR PARTS ITEM (1) ZEE CHANNEL BAC1496-377 LOT#1554641-1 IT
- [SDR SWAA2024072406057](https://openairdocs.org/sdr/SWAA2024072406057.md): Rib · cracked · Jun 27, 2024 · N252WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > RT HORIZONTAL STAB REMOVEABLE LEADING EDGE 5TH RIB FROM I/B; APPROX. L/E STA 114.5; IS CRACKED.<[01] REMOVED AND REPLACED RIB STA 114.5<BR>IAW SRM 51-40-02 & DWG 186A1001;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024072405244](https://openairdocs.org/sdr/SWAA2024072405244.md): Intercostal · cracked · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD WET AREA BS290 BL0 WL208.<[01] REMOVED AND INSTALLED NEW INTERCOSTAL BETWEEN BS 277 TO BS 294 BL 0 WL 208 PER SRM 51-40-05 AND DWG 141A5400;[02] VERIFIED ACTION 1.;[03] UPDATED MEASUREMENTS;[04] REJECT: DURING VERIFICATION OF INTERCO
- [SDR SWAA2024072405239](https://openairdocs.org/sdr/SWAA2024072405239.md): Intercostal · cracked · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD WET AREA BS317 RBL31 WL208.<[01] REMOVED AND REPLACE FLOOR INTERCOSTAL BETWEEN BS 312 TO BS 328 RBL 31 PER SRM 51-40-02 AND DWG 141A5400;[02] REMOVED AND REPLACED FLOOR INTERCOSTAL BETWEEN BS 312 TO BS 328 RBL 31 PER SRM 51-40-02 AND
- [SDR SWAA2024072405245](https://openairdocs.org/sdr/SWAA2024072405245.md): Intercostal · cracked · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD WET AREA BS344+9 LBL11 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL BETWEEN BS.344 - BS 360 LBL.11.10 WL 208.1 IAW SRM 51-40-02 & DWG# 141A5400. REV: A.;[02] VERIFIED RII ITEMS COMPLETE;[03] VERIFIED
- [SDR SWAA2024072405246](https://openairdocs.org/sdr/SWAA2024072405246.md): Intercostal · cracked · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD WET AREA BS344+5 BL0 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL BETWEEN BS.344 - BS 360 BL.0 WL 208 IAW SRM 51-40-02 & DWG# 141A5400.;[02] CUSTOMER CARD COMPLETE
- [SDR SWAA2024072405240](https://openairdocs.org/sdr/SWAA2024072405240.md): Intercostal · cracked · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD WET AREA BS344+5 RBL32 WL208.<[01] 01 - REMOVED AND REPLACED INTERCOSTAL P/N 141A5410U25; LOT 1541321-1 IAW SRM 51-40-05-0G-0 AND DWG141A5400.;[02] REMOVED AND REPLACED INTERCOSTAL P/N 141A5410U25; LOT 1541321-1 BETWEEN BS344 TO BS36
- [SDR SWAA2024072405241](https://openairdocs.org/sdr/SWAA2024072405241.md): Intercostal · cracked · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD WET AREA BS344+5 RBL51 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL BS344 TO BS360 RBL51 IAW SRM 51-40-02 DWG# 141A5400;[02] VERIFIED CARD COMPLETE;[03] VERIFIED RII ITEMS COMPLETE
- [SDR SWAA2024072405257](https://openairdocs.org/sdr/SWAA2024072405257.md): Angle · cracked · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD WET AREA BS387 BL0 WL208.<[01] REMOVED AND REPLACED ANGLE AT FWD. WET AREA BETWEEN BS-380 - BS 400 BL 0 WL 208 IAW B-737-700 SRM 51-40-02 AND DWG# 143A5400.;[02] VERIFIED ALL STEPS COMPLETE; MEASUREMENT FIELD AND CARD COMPLETE.
- [SDR SWAA2024072405258](https://openairdocs.org/sdr/SWAA2024072405258.md): Angle · cracked · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD WET AREA BS387 RBL9 WL208.<[01] REMOVED AND REPLACED ANGLE AT FWD. WET AREA BETWEEN BS-380 - BS 400 RBL9 WL 208 IAW B-737-700 SRM 51-40-02 AND DWG# 143A5400. REV: A.;[02] VERIFIED ALL STEPS COMPLETE; MEASUREMENT FIELD AND CARD COMPLE
- [SDR SWAA2024072405252](https://openairdocs.org/sdr/SWAA2024072405252.md): Angle · cracked · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD WET AREA BS387 LBL13 WL208.<[01] UPDATED MEASUREMENTS;[02] REMOVED AND REPLACED ANGLE AT INTERCOSTAL BS387 LBL13 WL208<BR>IAW SRM 51-40-02 & DWG 143A5400;[03] VERIFIED ACTION 2.<BR>JOB COMPLETE.
- [SDR SWAA2024072405256](https://openairdocs.org/sdr/SWAA2024072405256.md): Frame · cracked · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Main, Frame
  > PASSENGER CABIN FED UPPER FRAME BS 312 STR 5L CRACKED<[01] REPAIRED PASSENGER CABIN FED UPPER FRAME BS 312 STR 5L IAWS EA: M-22-153-01244;[02] VERIFIED RII ITEMS;[03] COMPLETE
- [SDR SWAA2024072405236](https://openairdocs.org/sdr/SWAA2024072405236.md): Sill Drain · corroded · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON L1 DOOR MOP SILL BS294+11 - BS344 LBL55 WL208. MARKED<[01] VERIFIED STEPS 1;3;4 COMPLETE; STEP 2 IN PARTIAL.;[02] REMOVED AND INSTALLED NEW L1 DOOR MOP SILL; PER SRM 51-40-02 AND DWG 141A8110; ID: 09 AND 10; REV: A;[03] ALL MAINTENANCE ACTIONS COM
- [SDR SWAA2024072405254](https://openairdocs.org/sdr/SWAA2024072405254.md): Sill Drain · corroded · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AED MOP SILL BS954 - BS986 LBL51 WL208. MARKED<[01] REMOVED AND REPLACED AED MOP SILL IAW SRM 51-40-02 AND DWG 147A8501 REV C;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2024072405255](https://openairdocs.org/sdr/SWAA2024072405255.md): Sill Drain · corroded · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ASD MOP SILL BS950 - BS993 RBL51 WL208. MARKED<[01] REMOVED AND REPLACED MOP SILL(INNER CORD) RBL 51;WL 208;IAW SRM 51-10-02-0G-0; SRM 51-40-02 AND DWG# 147A8501 REV B.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024072405237](https://openairdocs.org/sdr/SWAA2024072405237.md): Support · corroded · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON LATCH FITTING SUPPORT (141A5220-4) AT FWD WET AREA BS344 LBL59 WL208. MARKED<[01] REMOVED AND REPLACED TIEDOWN ASSY. LH FWD. ENTRY DOOR P/N 141A5220-4 LOT:1568438-1. IAW SRM 51-40-02 & DWG# 141A5220.;[02] VERIFIED;[03] VERIFIED
- [SDR SWAA2024072405248](https://openairdocs.org/sdr/SWAA2024072405248.md): Shield · corroded · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD. CARGO COMPARTMENT RH FWD. SHIELD HAS CORROSION AT BS 422; WL 156; RBL 25.<[01] REMOVED AND REPLACED FCB FWD SHIELD AT BS 420 TO BS 440 IAW SRM 51-40-02 AND DWG 143A0080 ID: 0023 REV: -;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024072405249](https://openairdocs.org/sdr/SWAA2024072405249.md): Tie Down · corroded · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Main, Structure
  > FWD. CARGO COMPARTMENT FLOOR TRACK HAS CORROSION ON 3EA TIE DOWN AT WL 156; LBL 18; BS 402/BS 436/BS 495.<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT FLOOOR TRACK TIE DOWN BS 396 TO BS 500D LBL 18 WL 146 IAW SRM 51-40-02 AND DWG 143A7500.;[02] VERIFIED COR
- [SDR SWAA2024072405259](https://openairdocs.org/sdr/SWAA2024072405259.md): Floor Support · corroded · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT AT AFT WET AREA BS947+4 RBL46 WL208.<[01] REMOVED AND REPLACED FLOOR SUPPORT ANGLE FROM BS 947 TO BS 967; RBL-46; WL-208 IAW SRM 51-40-02-0G-0 AND DWG# 147A5760;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024072305100](https://openairdocs.org/sdr/SWAA2024072305100.md): Floorbeam · cracked · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > FLOOR BEAM AT BS 294 RBL 54 WL 208 IS CRACKED<[01] PERFORMED REPAIR AT FLOOR BEAM BS 294 BETWEEN RBL 20 TO RBL 60 PER SRM 53-10-51-2R-16 REPAIR 16;[02] VERIFIED STEPS;2;3;16 COMPLETE.;[03] VERIFIED ALL STEPS AND MEASUREMENT FIEL COMPLETE; CARD COMPLETE.
- [SDR SWAA2024072305103](https://openairdocs.org/sdr/SWAA2024072305103.md): Frame · corroded · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Main, Frame
  > FRAME IS CORRODED AT BS 303.9 LBL 56 WL 211<[01] REMOVED CORROSION AND REWORKED AREA ON FRAME AT BS 303.9 LBL 56 WL 211 PER EA 24-153-01766.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] VERIFIED CORRECTIVE ACTION ENTRY 1.
- [SDR SWAA2024072305242](https://openairdocs.org/sdr/SWAA2024072305242.md): Floorbeam · cracked · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED FLOOR BEAM AT FWD WET AREA BS328 RBL20 WL208. MARKED.<[01] REPAIRED FLOOR BEAM AT FWD. WET AREA BS328 RBL20 WL208 SRM 53-10-51-2R-7 REPAIR AND SRM 51-40-02.;[02] CUSTOMER CARD COMPLETE;[03] APPLIED A FILLET SEAL AND CIC TO THE REPAIR AREA IAW SRM 53-10
- [SDR SWAA2024072305238](https://openairdocs.org/sdr/SWAA2024072305238.md): Floorbeam · corroded · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT FWD WET AREA BS328 RBL39 WL208. THE REPAIR OF FLOORBEAM AT FWD WET AREA BS328 RBL39 WL208 WAS ACCOMPLISHED ON FAULT [TTG8Q00U62RB];[02] STRUCTURAL REPAIR STILL OPEN [TTG8Q00U62RB];[03] THE CORROSION DAMAGE ON BS 328 FLOOR BEAM RBL 39
- [SDR SWAA2024072305253](https://openairdocs.org/sdr/SWAA2024072305253.md): Floorbeam · corroded · Jun 24, 2024 · N252WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM AT AFT WET AREA BS986 RBL43 WL208.<[01] RII REJECTED SUB-STEPS 5; 6 AND 8 DUE TO MAINTENIX FAULT NUMBER MISSING FOR THE EA 1-753-33056 REV IR. UNABLE TO PERFORM RII INSPECTION.;[02] REMOVED AND REPLACED BS 986 R/H PREVIOUS REPAIR IAW SR
- [SDR SWAA2024072304919](https://openairdocs.org/sdr/SWAA2024072304919.md): Floor Panel · delaminated · Jun 23, 2024 · N252WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242UF LOWER SURFACE IS DELAMINATED<[01] AFT FLOOR PANEL 242UF; LOWER SURFACE DELAMINATION; WAS REPAIRED WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
- [SDR SWAA2024072404688](https://openairdocs.org/sdr/SWAA2024072404688.md): Support · corroded · Jun 22, 2024 · N252WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > RH AFT CARGO FLOOR TO SIDEWALL SUPPORT HAS CORRODE NUT PLATE HOLES STA 787-807 CORRECTION TO FAULT DESCRIPTION: LH AFT CARGO FLOOR TO SIDEWALL SUPPORT HAS CORRODED NUT PLATE HOLES STA 787-807<[01] TASK FOR THIS FAULT WAS COMPLETED ON CUSTOMER CARD NR TTG8Q00U9

Next page: https://openairdocs.org/aircraft/N252WN/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 = 'N252WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N252WN/reports

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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.