# Service difficulty reports: N488WN

A list on [N488WN](https://openairdocs.org/aircraft/N488WN.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 8 · 352 reports

- [SDR SWAA2026101946866](https://openairdocs.org/sdr/SWAA2026101946866.md): Slide · out of position · Oct 12, 2026 · N488WN · Boeing 7377H4 · Escape Slide
  > AE ESCAPE SLIDE FLAP NEEDS READJUSTED_ REPOSITIONED AFT ENTRY SLIDE REF MT #725-61-06.
- [SDR SWAA2026080379245](https://openairdocs.org/sdr/SWAA2026080379245.md): Light · inoperative · Jul 29, 2026 · N488WN · Boeing 7377H4 · Emergency Lighting
  > L1 DOOR OUTSIDE EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IN THE EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHKD GOOD.
- [SDR SWAA2026072736731](https://openairdocs.org/sdr/SWAA2026072736731.md): Slide · partial deploy · Jul 22, 2026 · N488WN · Boeing 7377H4 · Escape Slide
  > FRONT PROVISIONING DOOR EMERGENCY SLIDE PARTIALLY DEPLOYED. REINSTALLED FS (R1) DOOR SLIDE PER AMM 25-66-01 AND MT#725-61-06.
- [SDR SWAA2026070112804](https://openairdocs.org/sdr/SWAA2026070112804.md): Support Bracket · cracked · Jun 16, 2026 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FOUND IN THE UPPER SUPPORT BRACKET ON THE BULKHEAD AT BS 663, RBL 52, WL 165. REMOVED AND REPLACED VAPOR BARRIER SUPPORT CHANNEL BS 663 RBL 54 TO RBL 70 IAW SRM 51-40-02-0G-0 AND DWG 111A1001 REV-.
- [SDR SWAA2026070112429](https://openairdocs.org/sdr/SWAA2026070112429.md): Crossbeam · cracked · Jun 15, 2026 · N488WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK FOUND ON PANEL BREAK ANGLE AT STA 540 FROM LBL45.57-LBL24.82. NO ALLOWABLE DAMAGE PARTS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9C<BR>REMOVED AND REPLACED PANEL BREAK ON DISCREPANCY AREA IAW SRM 51-40-05; SRM
- [SDR SWAA2026070112430](https://openairdocs.org/sdr/SWAA2026070112430.md): Intercostal · cracked · Jun 15, 2026 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON INTERCOSTAL CLIP AT STA 690 FROM RBL.07. REMOVED AND REPLACED INTERCOSTAL CLIP AT BS 690 RBL.07 IAW SRM 51-40-02 AND DWG 273A9110, REV A.
- [SDR SWAA2026070112426](https://openairdocs.org/sdr/SWAA2026070112426.md): Crossbeam · cracked · Jun 15, 2026 · N488WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK FOUND ON PANEL BREAK ANGEL AT STA 540 FROM RBL45.57-RBL24.82. NO ALLOWABLE DAMAGE PARTS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9C. REMOVED AND REPLACED PANEL BREAK ON DISCREPANCY AREA IAW SRM 51-40-05; SRM
- [SDR SWAA2026070112428](https://openairdocs.org/sdr/SWAA2026070112428.md): Crossbeam · cracked · Jun 15, 2026 · N488WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK FOUND ON PANEL BREAK ANGLE AT STA 540 FROM LBL 24.82 - LBL.07. NO ALLOWABLE DAMAGE PARTS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9C. REMOVED AND REPLACED PANEL BREAK ON DISCREPANCY AREA ITEM 143A5240-63 LOT#1
- [SDR SWAA2026070112427](https://openairdocs.org/sdr/SWAA2026070112427.md): Crossbeam · cracked · Jun 15, 2026 · N488WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK FOUND ON PANEL BREAK ANGLE AT BS 540 FROM RBL24.82-RBL.07. NO ALLOWABLE DAMAGE PARTS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9C. REMOVED AND REPLACED PANEL BREAK ON DISCREPANCY AREA IAW SRM 51-40-05; SRM 51-
- [SDR SWAA2026070111439](https://openairdocs.org/sdr/SWAA2026070111439.md): Seat Track · corroded · Jun 11, 2026 · N488WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 45 AT BS480+18; BS500A+7; BS500C+10: BS500D+10. SEAT TRACK WILL BE REPLACED ON FAULT TTG8Q01CP3X6.
- [SDR SWAA2026063010909](https://openairdocs.org/sdr/SWAA2026063010909.md): Skin · cracked · Jun 10, 2026 · N488WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK ON RT LOWER HORIZONTAL STABILIZER SKIN AT STAB STA 193.90; 17.5' FROM FWD EDGE. REMOVED THE DAMAGED PART ON RH HORIZONTAL STAB LOWER SKIN STA 193.9 17.5' FROM FWD EDGE AND INSTALLED REPAIR PARTS IAW SRM 55-10-01-2R-11.
- [SDR SWAA2026070110468](https://openairdocs.org/sdr/SWAA2026070110468.md): Pressure Deck · cracked · Jun 9, 2026 · N488WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK NOTED ON LH HORIZONTAL PRESSURE DECK BS 663+9.5; LBL 37.5; WL 202.5; L: 0.3'. PERFORMED REPAIR AT HORIZONTAL PRESSURE DECK BETWEEN BS 663 TO BS 675 LBL 30 TO LBL 60 PER SRM 53-40-51-2R-2 REP 2.
- [SDR SWAA2026041388306](https://openairdocs.org/sdr/SWAA2026041388306.md): Handle · broken · Apr 10, 2026 · N488WN · Boeing 7377H4 · Service Doors
  > AFT SERVICE DOOR HANDLE BROKEN. R&R THE ASSIST ENTRY NUT ON THE ASSIST HANDLE REF AMM 52-13-31
- [SDR SWAA2026030976690](https://openairdocs.org/sdr/SWAA2026030976690.md): Battery Pack · no test · Mar 5, 2026 · N488WN · Boeing 7377H4 · Emergency Lighting
  > BATTERY PACK AT 14DEF FAILED A TIME CHECK. REMOVED & REPLACED THE BATTERY PACK 14DEF IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2026030976691](https://openairdocs.org/sdr/SWAA2026030976691.md): Plate · cracked · Mar 5, 2026 · N488WN · Boeing 7377H4 · Wing Main, Frame Structure
  > RIGHT WING LOWER SHELF PANEL WAFFLE PLATE CRACKED OTBD NR 6 FLAP TRACK. REMOVED AND REPLACED THE WAFFLE PLATE OTBD OF NR 6 FLAP TRACK IAW SRM 51-40-02, AMM 54-52-04, AND SECURED PANEL 651GB IAW SOPM 20-50-01.
- [SDR SWAA2026021270216](https://openairdocs.org/sdr/SWAA2026021270216.md): Filter · fumes · Feb 11, 2026 · N488WN · Boeing 7377H4 · Air Distribution System
  > AFTER TAKEOFF, ACRID FUMES. APPARENT SOURCE COULD NOT BE IDENTIFIED. FLIGHT ATTENDANTS REPORTED IT WAS NOTICIABLE THROUGH THE CABIN. STRONG FUMES NOTICIABLE IN THE COCKPIT. PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-56. PERFORMED FIM 21-31, TASK 806.
- [SDR SWAA2026021270217](https://openairdocs.org/sdr/SWAA2026021270217.md): Water Separator · fumes · Feb 11, 2026 · N488WN · Boeing 7377H4 · Humidity Control System
  > AFTER TAKEOFF, ACRID FUMES. APPARENT SOURCE COULD NOT BE IDENTIFIED. FLIGHT ATTENDANTS REPORTED IT WAS NOTICIABLE THROUGHT THE CABIN. STRONG FUMES NOTICIABLE IN THE COCKPIT. PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-56. PERFORMED FIM 21-31,TASK 806.
- [SDR SWAA2026021269514](https://openairdocs.org/sdr/SWAA2026021269514.md): Acm · fumes · Feb 11, 2026 · N488WN · Boeing 7377H4 · Cabin Cooling System
  > AFTER TAKEOFF, ACRID FUMES APPARENT, THE SOURCE COULD NOT BE IDENTIFIED. FLIGHT ATTENDANTS REPORTED IT WAS NOTICIABLE THROUGHT THE CABIN. STRONG FUMES NOTICIABLE IN THE COCKPIT. PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-56. PERFORMED FIM 21-31, TASK
- [SDR SWAA2025102025305](https://openairdocs.org/sdr/SWAA2025102025305.md): Handle · broken · Oct 17, 2025 · N488WN · Boeing 7377H4 · Passenger/Crew Doors
  > L1 DOOR ASSIST HANDLE BROKEN. SWAPPED ASSIST HANDLE FROM FWD LAV TO L1 DOOR PER AMM 52-11-31. L1 DOOR ASSIST HANDLE OPS NORMAL. OK TO CONTINUE PER MEL 25-10-01. REPLACED FWD LAV EXIT ASSIST HANDLE AND HARDWARE AS REQ?D REF CMM 25-42-39.
- [SDR SWAA2025102025460](https://openairdocs.org/sdr/SWAA2025102025460.md): Handle · unsecure · Oct 17, 2025 · N488WN · Boeing 7377H4 · Passenger/Crew Doors
  > CREW REPORTSL1 DOOR HANDLE UNSCREWED. SECURED HANDLE IAW SIP.OPS CHECKED GOOD
- [SDR SWAA2025072893950](https://openairdocs.org/sdr/SWAA2025072893950.md): Sensor · faulty · Jul 22, 2025 · N488WN · Boeing 7377H4 · Engine Indicating System
  > TWO POPS HEARD ON NR 1 ENGINE AT 41K FT.79 MACH TAT -32C N1 ROLLED BACK APPROX 5%.. AUTOTHROTTLES DID NOT DISCONNECT AND ENGINE STABILIZED. ALL ENGINE PARAMETERS NORMAL FOR REMAINDER OF FLIGHT. COMPLIED WITH FIM TASK 71-05-805. FOUND FAULT CODE 75-30801 T
- [SDR SWAA2025061179935](https://openairdocs.org/sdr/SWAA2025061179935.md): Battery Pack · failed · Jun 10, 2025 · N488WN · Boeing 7377H4 · Emergency Lighting
  > AFT L/H EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2024081525951](https://openairdocs.org/sdr/SWAA2024081525951.md): Light · inoperative · Aug 14, 2024 · N488WN · Boeing 7377H4 · Emergency Lighting
  > AED EMERGENCY EXIT LIGHT HAS A BULB BURNT OUT<[01] RE-LAMPED AED EMERGENCY EXIT LIGHT PER AMM 33-51-01-960-801; OPS CHECK GOOD.<BR><BR>ALL ACTIONS COMPLETE;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024081525952](https://openairdocs.org/sdr/SWAA2024081525952.md): Button · inoperative · Aug 14, 2024 · N488WN · Boeing 7377H4 · Emergency Lighting
  > AFT FLIGHT ATTENDANT EMERGENCY EXIT LIGHT BUTTON DOSENT ILLUMINATE<[01] RE-LAMPED AFT FLIGHT ATTENDANT EMERGENCY EXIT LIGHT BUTTON PER SWPM 20-84-14; OPS CHECK GOOD PER AMM 33-51-00-710-801;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2024081524491](https://openairdocs.org/sdr/SWAA2024081524491.md): Battery Pack · inoperative · Aug 11, 2024 · N488WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT OUTSIDE R2 DOOR IS INOP<[01] FOUND BATTERY PACK M1672 INOPERATIVE IAW WDM 33-51-14. ORDERED BATTERY PACK; PENDING REPLACE.;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION STEP 1.;[04] REMOVED AND REPLACED BATTERY PACK M1672 ON CC#: TTG8Q00V4ZAG;
- [SDR SWAA2024081424489](https://openairdocs.org/sdr/SWAA2024081424489.md): Battery Pack · inoperative · Aug 11, 2024 · N488WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS ON PAX CABIN BINS 7 R/H AND 8 R/H ARE INOP<[01] FOUND BATTERY PACK M1672 INOPERATIVE IAW WDM 33-51-14. ORDERED BATTERY PACK; PENDING REPLACE.;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION STEP 1.;[04] UPDATED PARTS INFO;[05] REMOVED AND REPLAC
- [SDR SWAA2024081424490](https://openairdocs.org/sdr/SWAA2024081424490.md): Battery Pack · inoperative · Aug 11, 2024 · N488WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS ON AFT CEILING EXIT SIGN AND AFT ENTRY HEADER PANEL ARE INOP<[01] FOUND BATTERY PACK M1672 INOPERATIVE IAW WDM 33-51-14. ORDERED BATTERY PACK; PENDING REPLACE.;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION STEP 1.;[04] REMOVED AND REPLACED EME
- [SDR SWAA2024081622822](https://openairdocs.org/sdr/SWAA2024081622822.md): Skin · debonded · Aug 6, 2024 · N488WN · Boeing 7377H4 · Aerodynamic Fairings
  > FOUND AREA OF DISBOND ON TAILCONE; RT SIDE LOWER APPROX 10 INCHES AFT OF FWD EDGE. (MARKED)<[01] DISBONDED AREA ON TAIL CONE; RIGHT SIDE LOWER APPROX. 10 INCHES AFT OF FWD EDGE WAS REPAIRED IAW SRM 51-70-05-2R-2.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024081421220](https://openairdocs.org/sdr/SWAA2024081421220.md): Tear Strap · incorrect · Aug 1, 2024 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > REJECT: UPPER TEAR STRAP HAS INCORRECT FASTENER SPACING REFER TO FIGURE 1-2 AND SRM 53-00-01 FIGURE 201/REPAIR 35 DETAIL F<[01] REPAIR WAS FABRICATED IAW SRM 53-00-01-2R-35 REPAIR 35 TYPE 3.<BR>3.80 TO 4.30 INCH WIDE TEAR STRAP;[02] CORRETION ACTION ITEM 1: R
- [SDR SWAA2024081419914](https://openairdocs.org/sdr/SWAA2024081419914.md): Light · damaged · Jul 30, 2024 · N488WN · Boeing 7377H4 · Emergency Lighting
  > AFT LAV EXIT LIGHT INDICATOR IS DAMAGED<[01] REPLACED EXIT SIGN LIGHT ASSEMBLY IN THE AFT LAV IAW AMM 33-51-01-960-802 AND PENDING FOR EMERGENCY LIGHTS - OPERATIONAL TEST IAW AMM 33-51-00-710-801;[02] VERIFIED ITEM 1;[03] PERFORMED EMERGENCY LIGHTS - OPERATION
- [SDR SWAA2024081415739](https://openairdocs.org/sdr/SWAA2024081415739.md): Sign · damaged · Jul 23, 2024 · N488WN · Boeing 7377H4 · Emergency Lighting
  > G-1 GALLEY EXIT LIGHT INDICATOR IS DAMAGED<[01] REPLACED G1 EXIT LIGHT INDICATOR IAW AMM 33-51-14-960-802.;[02] LIGHT TEST WILL BE ACCOMPLISHED ON TASK CARD TTG8Q0034HP8;[03] VERIFIED CORRECTIVE ACTION 1 AND 2.
- [SDR SWAA2024081413091](https://openairdocs.org/sdr/SWAA2024081413091.md): Baffle · cracked · Jul 16, 2024 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB BAFFLE IS CRACKED BETWEEN BS500A TO BS500B RBL 23 WL156<[01] REMOVED AND REPLACED AT FCB BAFFLE BETWEEN BS500A TO BS500B RBL 23 WL156 IAW B-737-700 SRM 51-10-02; SRM 51-40-02.AND DWG#143A7505 REV:D.;[02] VERIFIED COMPLIED WITH AS PER TASK CARD AND COMPLETE
- [SDR SWAA2024081611811](https://openairdocs.org/sdr/SWAA2024081611811.md): Frame · cracked · Jul 12, 2024 · N488WN · Boeing 7377H4 · Fuselage Main, Frame
  > PASSENGER CABIN FED UPPER FRAME BS 312 STR 5L CRACKED<[01] VERIFIED COMPLIED WITH THE TASK CARD.;[02] ALL STEPS COMPLETED;[03] ALL STEPS COMPLETED/CARD COMPLETED.
- [SDR SWAA2024081511961](https://openairdocs.org/sdr/SWAA2024081511961.md): Support Angle · cracked · Jul 12, 2024 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MAIN EBAY OXYGEN BOTTLE SUPPORT ANGLE CRACKED BS362 RBL10 WL158. MARKED<[01] REMOVED AND REPLACED NEW OXYGEN CYLINDER SUPPORT RING ON BS362 RBL10 WL158 IAW SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2024081311958](https://openairdocs.org/sdr/SWAA2024081311958.md): Frame · cracked · Jul 12, 2024 · N488WN · Boeing 7377H4 · Fuselage Main, Frame
  > AFT CARGO BAY FRAME IS CRACKED ON INBOARD FLANGE; BS 747; RBL 20<[01] PARTIALLY COMPLETED STEP-9;[02] AFT CARGO BAY FRAME IS CRACK ON INBOARD FLANGE; BS 747; RBL 20 WAS REPAIRED IAW SRM 53-60-07-2R-2-A01771;[03] VERIFIED CORRECTIVE ACTION 2
- [SDR SWAA2024081511120](https://openairdocs.org/sdr/SWAA2024081511120.md): Support Angle · cracked · Jul 10, 2024 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > BS 727 BULKHEAD SUPPORT ANGLE IS CRACKED AT RBL 5; WL 164<[01] REMOVED AND REMPLACED BULKHEAD SUPPORT ANGLE<BR>BS 727 RBL5 WL164 IAW SRM 51-40-02 AND DWG 144A2600 REV A;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2024081411117](https://openairdocs.org/sdr/SWAA2024081411117.md): Support · corroded · Jul 10, 2024 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT IS CORRODED AT BS 874 AND 881; RBL 17 WL 156<[01] NO DAMAGE NOTED; CLEANED AND INSPECTED IAW SRM 51-10-02;[02] VERIFIED CORRECTIVE ACTION STEP 1.
- [SDR SWAA2024081411116](https://openairdocs.org/sdr/SWAA2024081411116.md): Support · corroded · Jul 10, 2024 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT IS CORRODED 727+5-767; RBL 21; WL 156<[01] REMOVED AND REPLACED NEW ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02 AND DWG 146A7500 ID:0085 REV:A;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024081311118](https://openairdocs.org/sdr/SWAA2024081311118.md): Support · corroded · Jul 10, 2024 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT IS CORRODED BS 727+5-847; LBL 21; WL 156<[01] AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT WITH CORROSION OUT OF LIMITS REMOVED AND REMPLACED IAW SRM 53-00-53-1A-2<BR>AND DWG 146A7500 REV A;[02] VERIFIED COMPLETION CORRECTI
- [SDR SWAA2024081610456](https://openairdocs.org/sdr/SWAA2024081610456.md): Panel · debonded · Jul 9, 2024 · N488WN · Boeing 7377H4 · Aerodynamic Fairings
  > PANEL 194DL OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL. (MARKED)<[01] 'PANEL 194DL OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL. (MARKED)' IS COMPLETED IAW SRM 51-70-05-2R-2.;[02] 'PANEL 194DL DISBOND' IS REPAIRED IAW SRM 51-70-05-2R-2.;[03] VERIFIED CORRECT
- [SDR SWAA2024081510856](https://openairdocs.org/sdr/SWAA2024081510856.md): Support · cracked · Jul 9, 2024 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED<[01] REMOVED AND INSTALLED NEW FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET BS500D S-19R WL 193 IAW SRM 51-40-02 DWG # 143A7902;[02] VERIFIED CORRECTIVE ACTION STEP 1.
- [SDR SWAA2024081510851](https://openairdocs.org/sdr/SWAA2024081510851.md): Shield · corroded · Jul 9, 2024 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SHIELD AT FCB BS500+10 - BS500A RBL24 WL156. MARKED<[01] REMOVED AND REPLACED AFT SHIELD ASSY BETWEEN BS 492.4 - BS500A RBL 24 WL 156 IAW B-737-700 SRM 51-40-02 & DWG# 143A0080.;[02] VERIFIED CORRECTIVE ACTION STEP 1.
- [SDR SWAA2024081510855](https://openairdocs.org/sdr/SWAA2024081510855.md): Attach Angle · cracked · Jul 9, 2024 · N488WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS400 LBL25 WL154.<[01] REMOVED AND REPLACED ANGLE AT FCB BS400 LBL 25 WL 154<BR>IAW SRM 51-40-02 AND DWG 143A7505 REV. B;[02] VERIFIED CORRECTION ACTION ITEM 1.;[03] VERIFIED STEP 5 COMPLETE; CORRECTION ACTION ITEM 1; M
- [SDR SWAA2024081410850](https://openairdocs.org/sdr/SWAA2024081410850.md): Stringer · cracked · Jul 9, 2024 · N488WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-23L WL164. MARKED<[01] REPAIRED CRACKED STRINGER AT AREA AFT OF FCB BS535 S-23L WL164 PER EA 24-153-01866.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024081410849](https://openairdocs.org/sdr/SWAA2024081410849.md): Stringer · cracked · Jul 9, 2024 · N488WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26L WL153. MARKED<[01] VERIFIED STEP 4 COMPLETED.;[02] VERIFIED STEP 5 COMPLETED.;[03] REPAIRED STR-26L WL 153 BETWEEN BS 510 TO BS 540 PER SRM 53-00-03-2R-1.;[04] VERIFIED CORRECTIVE ACTION STEP 3.;[05] VERIFIED COR
- [SDR SWAA2024081410848](https://openairdocs.org/sdr/SWAA2024081410848.md): Stringer · cracked · Jul 9, 2024 · N488WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26R WL153. MARKED<[01] REPAIRED STR-26R WL 153 BETWEEN BS 510 TO BS 540 PER SRM 53-00-03-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM AND STEPS; CARD COMPLETE.
- [SDR SWAA2024081410852](https://openairdocs.org/sdr/SWAA2024081410852.md): Shield · corroded · Jul 9, 2024 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD SHIELD AT FCB BS400 - BS409 RBL24 WL156. MARKED<[01] VERIFIED STEP 5 COMPLETED.;[02] REMOVED AND REPLACED FWD SHIELD AT FCB BETWEEN BS420 - BS440; RBL24; WL156. IAW B-737-700 SRM 51-40-02 & DWG# 143A0080.;[03] VERIFIED CORRECTIVE ACTION STEP 2
- [SDR SWAA2024081410853](https://openairdocs.org/sdr/SWAA2024081410853.md): Support · corroded · Jul 9, 2024 · N488WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS500A - BS500D RBL23 WL156. MARKED<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT FCB (ZEE CHANNEL) BETWEEN BS 500A - BS.500D RBL21 WL 156 IAW B-737-700 SRM 51-40-02 AND DWG# 143A7500;[02] VERIFIED CORRECT
- [SDR SWAA2024081310847](https://openairdocs.org/sdr/SWAA2024081310847.md): Stringer · cracked · Jul 9, 2024 · N488WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS535 S-25R WL155. MARKED<[01] 'REPAIRED PER EA 24-153-01875. THIS IS A CATEGORY A REPAIR AS DEFINED IN 737-700 SRM 51-00-06.'
- [SDR SWAA2024081610304](https://openairdocs.org/sdr/SWAA2024081610304.md): Seal · cracked · Jul 8, 2024 · N488WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RT HORIZONTAL STAB UPPER FWD SLIDE SEAL CRACKED.<[01] REMOVED RT HORIZONTAL STAB UPPER SLIDE SEAL IAW AMM 53-31-31-000-802. INSTALLED ATTACHING HARDWARE TO NEW RT STAB FWD UPPER SLIDE SEAL IAW SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] INST

Next page: https://openairdocs.org/aircraft/N488WN/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 = 'N488WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N488WN/reports

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