# Service difficulty reports: N8526W

A list on [N8526W](https://openairdocs.org/aircraft/N8526W.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 3 · 114 reports

- [SDR SWAA2026032381707](https://openairdocs.org/sdr/SWAA2026032381707.md): Girt Bar · loose · Mar 19, 2026 · N8526W · Boeing 7378H4 · Emergency Equipment
  > LEFT FWD ENTRY GIRT BAR AFT BRACKET LOOSE. REPOSITIONED GIRT BAR AND BRACKET WITH NO DEFECTS NOTED IAW AMM 25-66-01. AC OK FOR SERVICE
- [SDR SWAA2026012661825](https://openairdocs.org/sdr/SWAA2026012661825.md): Megaphone · damaged · Jan 15, 2026 · N8526W · Boeing 7378H4 · Emergency Equipment
  > AFT GALLEY EMERGENCY MEGAPHONE DAMAGED. R & R MEGAPHONE IAW AMM 25-64-00.
- [SDR SWAA2026012661012](https://openairdocs.org/sdr/SWAA2026012661012.md): Lamp · inoperative · Jan 14, 2026 · N8526W · Boeing 7378H4 · Emergency Lighting
  > FWD ENTRY DOOR ESCAPE SLIDE LIGHT (L731) INOPERATIVE. REPLACED THE LAMPS IAW MM 33-51-04. OPS CHECKED NORMAL.
- [SDR SWAA2026012760380](https://openairdocs.org/sdr/SWAA2026012760380.md): Access Panel · delaminated · Jan 12, 2026 · N8526W · Boeing 7378H4 · Aerodynamic Fairings
  > ACCESS PANEL 191CL HAS SMALL AREA OF DELAMINATION ON OUTSIDE OF PANEL APROX 22" FROM FWD END AND 15" FROM UPPER END. REMOVED THE AREA OF DELAMINATION IAW SRM 51-70-05-0G-0. ACCOMPLISHED A REPAIR TO AREA IAW SRM 51-70-05-2R-1.
- [SDR SWAA2026012659858](https://openairdocs.org/sdr/SWAA2026012659858.md): Crossbeam · cracked · Jan 9, 2026 · N8526W · Boeing 7378H4 · Fuselage Main, Structure
  > CABIN CROSSBEAM IS CRACKED. LOCATED BELOW FLOORBOARD 231UF, BS 540 FROM BL 0 - RBL 24. REPLACED CROSSBEAM IAW SRM 51-40-02.
- [SDR SWAA2026012758880](https://openairdocs.org/sdr/SWAA2026012758880.md): Rib · damaged · Jan 6, 2026 · N8526W · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT WING MAIN FLAP OTBD DEFLECTION RIB HAD TWO OBLONG HOLES IN THE END FITTING. REMOVED NR 1 FLAP TRACK CARRIAGE FROM UNSERVICEABLE FLAP & INSTALLED ON SERVICEABLE FLAP IAW MM 27-51-31. REMOVED NR 2 FLAP TRACK CARRIAGE FROM UNSERVICEABLE FLAP & INSTALLED O
- [SDR SWAA2026012658151](https://openairdocs.org/sdr/SWAA2026012658151.md): Floor Support · cracked · Jan 4, 2026 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT, BS 537.5, LBL 2 CRACKED. R & R THE FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR SWAA2026012757604](https://openairdocs.org/sdr/SWAA2026012757604.md): Angle · cracked · Dec 31, 2025 · N8526W · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > NR 1 SEAT TRACK GUSSET CRACKED ON BOTTOM INBD SIDE AT BS 727B. REMOVED OTBD VERTICAL ATTACH ANGLE IAW SRM 51-40-02. REMOVED THE GUSSET IAW SRM 51-40-02. LOCATED, & MATCH DRILLED HOLES ON NEW GUSSET IAW SRM 51-40-02. INSTALLED A NEW GUSSET IAW SRM 51-40-02.
- [SDR SWAA2026012756879](https://openairdocs.org/sdr/SWAA2026012756879.md): Access Panel · cracked · Dec 31, 2025 · N8526W · Boeing 7378H4 · Aerodynamic Fairings
  > ACCESS PANEL 191CL HAS 1 FASTENER HOLE CRACKED & THE COUNTER SINK IS DAMAGED. REMOVED THE DAMAGE IAW SRM 51-70-05-2R-0. INSPECTED REMOVED DAMAGE TO AREA IAW SRM 51-70-05-2R-0. ACCOMPLISHED A REPAIR TO FASTENER HOLE IAW SRM 51-70-05-2R-8.
- [SDR SWAA2026012756860](https://openairdocs.org/sdr/SWAA2026012756860.md): Seal · cracked · Dec 31, 2025 · N8526W · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB UPPER FWD SLIDING SEAL CRACKED ON FWD EDGE. R & R LT HORIZONTAL STAB UPPER FWD SLIDING SEAL IAW AMM 53-31-31. INSPECTED IAW AMM 53-31-31-401, CONFIG 2-NG.
- [SDR SWAA2026012655787](https://openairdocs.org/sdr/SWAA2026012655787.md): Handle · loose · Dec 26, 2025 · N8526W · Boeing 7378H4 · Passenger/Crew Doors
  > FORWARD ENTRY DOOR GRAB HANDLE IS LOOSE. SECURED L1 DOOR GRAB HANDLE IAW AMM 52-11-31.
- [SDR SWAA2025093019184](https://openairdocs.org/sdr/SWAA2025093019184.md): Battery · no test · Sep 28, 2025 · N8526W · Boeing 7378H4 · Emergency Equipment
  > FWD LEFT FLASHLIGHT WILL NOT TEST. REMOVED & REPLACED FWD OTBD FLASHLIGHT BATTERY IAW AMM 25-64-00.
- [SDR SWAA2025100118818](https://openairdocs.org/sdr/SWAA2025100118818.md): Flashlight · inoperative · Sep 27, 2025 · N8526W · Boeing 7378H4 · Emergency Equipment
  > FWD F/A FLASHLIGHT INOPERATIVE AND SEAL BROKEN. REMOVED AND REPLACED FWD FLIGHT ATTENDANT FLASHLIGHT AND SEALED IAW AMM 25-64-00.
- [SDR SWAA2025091514448](https://openairdocs.org/sdr/SWAA2025091514448.md): Glowstrip · loose · Sep 12, 2025 · N8526W · Boeing 7378H4 · Emergency Equipment
  > PHOTOLUMINESCENT STRIP COMMING UP AT ROW 12 FO SIDE. RESECURED STRIP PER AMM 33-51-15. NO DAMAGED NOTED, ACFT OK FOR SVC.
- [SDR SWAA2025081403148](https://openairdocs.org/sdr/SWAA2025081403148.md): Flashlight · no test · Aug 11, 2025 · N8526W · Boeing 7378H4 · Emergency Equipment
  > CREW REPORTS AFTER F/A FLASHLIGHT WILL NOT TEST. REMOVED AND REPLACED AFT F/A FLASHLIGHT ASSY IAW AMM 25-64-00.
- [SDR SWAA2025080798516](https://openairdocs.org/sdr/SWAA2025080798516.md): Flashlight · no test · Aug 4, 2025 · N8526W · Boeing 7378H4 · Emergency Equipment
  > FWD GALLEY FLASH LIGHT WONT TEST. REPLACED FLASH LIGHT IAW AMM 25-64-00.
- [SDR SWAA2025080698124](https://openairdocs.org/sdr/SWAA2025080698124.md): Light · unsecure · Aug 3, 2025 · N8526W · Boeing 7378H4 · Emergency Lighting
  > PHOTO ILLUMIN.STRIP PULLED UP ON FOS SIDE NEAR ROWS 12-13. SECURED PHOTO LUMINESCENT LIGHTING STRIP AT ROW 12 IAW AMM 33-51-15.
- [SDR SWAA2025070186568](https://openairdocs.org/sdr/SWAA2025070186568.md): Flashlight · no test · Jun 29, 2025 · N8526W · Boeing 7378H4 · Emergency Equipment
  > FLIGHT ATT FLASHLIGHT TEST INOP.<[01] OPS TESTED PER AMM 25-64-00. OPS TEST GOOD. RE-SEALED PER AMM 25-64-00.
- [SDR SWAA2025062785338](https://openairdocs.org/sdr/SWAA2025062785338.md): Flashlight · inoperative · Jun 25, 2025 · N8526W · Boeing 7378H4 · Emergency Equipment
  > AFT EMERGENCY FLASHLIGHT INOP. OK TO CONTINUE PER MEL 25-12-01; SP1B; AUTHORIZAT AFT EMERGENCY FLASHLIGHT INOP. OK TO CONTINUE PER MEL 25-12-01 SP1B AUTHORIZATION #<[01] PERFORMED AFT EMERGENCY FLASH LIGHT OPERATIONAL CHECK IAW AMM 25-64-00.OPS CHECK NORMAL
- [SDR SWAA2025061079518](https://openairdocs.org/sdr/SWAA2025061079518.md): Light · unsecure · Jun 7, 2025 · N8526W · Boeing 7378H4 · Emergency Lighting
  > FLOOR LIGHTING IS A TRIP HAZARD AT ROW 12<[01] RESECURED PHOTOLUMINESCENT STRIP PER [AMM 33-51-15-201-NG (FLOOR PROXIMITY LIGHTS; PHOTOLUMINESCENT - MAINTENANCE PRACTICES - PERMANENT)]
- [SDR SWAA2025043064642](https://openairdocs.org/sdr/SWAA2025043064642.md): Light · loose · Apr 26, 2025 · N8526W · Boeing 7378H4 · Emergency Lighting
  > FA REPORTS FLOOR LIGHTING AT ROW 12 FO SIDE IS LOOSE AND IS A TRIPPING HAZARD<[01] RESECURED FLOOR PROXIMITY LIGHT (SAF-T-GLO) STRIP PER AMM 33-51-15
- [SDR SWAA2025031304863](https://openairdocs.org/sdr/SWAA2025031304863.md): Girt Bar · out of adjust · Mar 13, 2025 · N8526W · Boeing 7378H4 · Emergency Equipment
  > AFT SERVICE DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] ADJUSTED IAW AMM 25-66-01
- [SDR SWAA2025031304864](https://openairdocs.org/sdr/SWAA2025031304864.md): Girt Bar · out of adjust · Mar 13, 2025 · N8526W · Boeing 7378H4 · Emergency Equipment
  > AFT ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] ADJUSTED GERT BAR REF AMM 25-66-01
- [SDR SWAA2025031003227](https://openairdocs.org/sdr/SWAA2025031003227.md): Strip · buckled · Mar 7, 2025 · N8526W · Boeing 7378H4 · Emergency Lighting
  > PHOTO-LUMINESCENT FLOOR STRIP BETWEEN ROWS 12 & 14 AIRCRAFT RIGHT BUCKLED AND CAME OFF <[01]. RE INSTALLED STRIP; SECURE CHECK GOOD PER AMM33-51-15.
- [SDR SWAA2025012788128](https://openairdocs.org/sdr/SWAA2025012788128.md): Mount · damaged · Jan 21, 2025 · N8526W · Boeing 7378H4 · Fuselage, Equipment Attach Fittings
  > FWD ENTRY GIRT BAR FLOOR MOUNT FOR FLOOR BRACKET DAMAGED ON AFT SIDE POSITION<[01] R/R FLOOR MOUNT BRACKET(LOWER) PER AMM 25-66-02
- [SDR SWAA2025012787759](https://openairdocs.org/sdr/SWAA2025012787759.md): Seal · cracked · Jan 20, 2025 · N8526W · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > FUSELAGE TO LT. HORIZONTAL STAB UPPER FWD METAL SLIDING SEAL CRACKED.<[01] REMOVED LH HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31.;[02] REPLACED LH HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31. OPS CHECKS GOOD.
- [SDR SWAA2025012787758](https://openairdocs.org/sdr/SWAA2025012787758.md): Seal · cracked · Jan 20, 2025 · N8526W · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > FUSELAGE TO RT. HORIZONTAL STAB UPPER FWD METAL SLIDING SEAL CRACKED.<[01] REMOVED RH HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31.;[02] REPLACED RH HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31. OPS CHECK GOOD.
- [SDR SWAA2025012787544](https://openairdocs.org/sdr/SWAA2025012787544.md): Battery Pack · inoperative · Jan 19, 2025 · N8526W · Boeing 7378H4 · Emergency Lighting
  > FWD CABIN EMERGENCY LIGHT BATTERY PACK INOP AT STA 527C L/H<[01] REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06;[02] 1. CHRISTOPHER KENNEDY (TECHNICIAN); 20-JAN-2025 15:17 UTC<BR>REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06<BR>INSPECTED AS REQUIRED;[03
- [SDR SWAA2025012787542](https://openairdocs.org/sdr/SWAA2025012787542.md): Battery Pack · inoperative · Jan 19, 2025 · N8526W · Boeing 7378H4 · Emergency Lighting
  > FWD CABIN EMERGENCY LIGHT BATTERY PACK INOP AT STA 527C R/H<[01] REMOVED AND REPLACED BATTERY PACK PER MM33-51-06;[02] 1. CHRISTOPHER KENNEDY (TECHNICIAN); 20-JAN-2025 15:26 UTC<BR>REMOVED AND REPLACED BATTERY PACK PER MM33-51-06<BR>INSPECTED AS REQUIRED;[03]
- [SDR SWAA2025012787543](https://openairdocs.org/sdr/SWAA2025012787543.md): Battery Pack · inoperative · Jan 19, 2025 · N8526W · Boeing 7378H4 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK INOP AT STA 565 R/H<[01] REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06;[02] 1. CHRISTOPHER KENNEDY (TECHNICIAN); 20-JAN-2025 15:37 UTC<BR>REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06<BR>INSPECTED AS REQUIRED
- [SDR SWAA2025012787191](https://openairdocs.org/sdr/SWAA2025012787191.md): Fairing · elongated · Jan 18, 2025 · N8526W · Boeing 7378H4 · Wing Miscellaneous Structure
  > #3 CANOE FAIRING HAS MULTIPLE FASTENERS HOLES ELONGATED.<[01] #3 CANOE FAIRING TO BE REPLACED ON TASK CARD TTG8Q00Y4C4E;[02] PARTS UPDATED;[03] ADDED SELECT REFERENCE ONLY
- [SDR SWAA2025012786838](https://openairdocs.org/sdr/SWAA2025012786838.md): Scuff Plate · cracked · Jan 17, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO THRESHOLD FORWARD CORNER SCUFF PLATE IS CRACKED.<[01] LOCATED AND DRILLED NEW THRESHOLD PER SRM 51-40-02;[02] LOCATED AND DRILLED NEW THRESHOLD FORWARD CORNER SCUFF PLATE PER <BR>SRM 51-40-02;[03] INSTALLED FORWARD CARGO THRESHOLD FORWARD CORNER
- [SDR SWAA2025012786839](https://openairdocs.org/sdr/SWAA2025012786839.md): Scuff Plate · cracked · Jan 17, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO THRESHOLD AFT CORNER SCUFF PLATE IS CRACKED.<[01] LOCATED AND DRILLED NEW THRESHOLD CORNER SCUFF PLATE PER SRM 51-40-;[02] INSTALLED FORWARD CARGO THRESHOLD AFT CORNER SCUFF PLATE PER AMM 53-11-02.;[03] INSPECTION COMPLETE ON CORRECTIVE ACTION #2
- [SDR SWAA2025012784286](https://openairdocs.org/sdr/SWAA2025012784286.md): Seat Track · out of limits · Jan 9, 2025 · N8526W · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings
  > CAPTAINS AFT; INBOARD SEAT TRACK IS OUT OF LIMITS.<[01] 01 - REMOVED AND REPLACED PER [AMM 25-11-11-400-801-NG (FLIGHT COMPARTMENT SEAT TRACKS - INSTALLATION AND ALIGNMENT - PERMANENT)];[02] INSPECTION C/W FOR CORRECTIVE ACTION #1 AND STEP 1 FOR INSTALLATION O
- [SDR SWAA2025012782829](https://openairdocs.org/sdr/SWAA2025012782829.md): Angle · corroded · Jan 3, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE STA 787-807 HAS CORROSION.<[01] REMOVED CORROSION IN AFT CARGO L/H TRANSITION ANGLE STA 787-807; FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.;[02] CORRECTED CORRODED ELEMENT PART NUMBER;[03] TRANSITION ANGLE WAS R/R ON TTG8Q00
- [SDR SWAA2025012782830](https://openairdocs.org/sdr/SWAA2025012782830.md): Angle · corroded · Jan 3, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE STA 767-787 HAS CORROSION.<[01] REMOVED CORROSION IN AFT CARGO L/H TRANSITION ANGLE STA 767-787; FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.;[02] CORRECTED CORRODED ELEMENT PART NUMBER;[03] PARTS DATA UPDATE ONLY;[04] TRANSIT
- [SDR SWAA2025012782831](https://openairdocs.org/sdr/SWAA2025012782831.md): Angle · corroded · Jan 3, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO SMALL TRANSITION ANGLE JUST FWD OF DOOR CUTOUT HAS CORROSION.<[01] LOCATED AND DRILLED FASTENER HOLES. IAW SRM 51-40-05;[02] CORRECTED CORRODED PART INFO;[03] REMOVED AND REPLACED AFT CARGO SMALL TRANSITION ANGLE JUST FWD OF DOOR CUTOUT IAW SRM 51-40
- [SDR SWAA2025012782832](https://openairdocs.org/sdr/SWAA2025012782832.md): Angle · corroded · Jan 3, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE STA 747-767 HAS CORROSION.<[01] REMOVED CORROSION IN AFT CARGO L/H TRANSITION ANGLE STA 747-767; FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.;[02] CORRECTED CORRODED ELEMENT PART NUMBER;[03] REMOVED AND REPLACED AFT CARGO L/H
- [SDR SWAA2025012782833](https://openairdocs.org/sdr/SWAA2025012782833.md): Angle · corroded · Jan 3, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE STA 727J- 747 HAS CORROSION.<[01] REMOVED CORROSION IN AFT CARGO L/H TRANSITION ANGLE STA 727J- 747; FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.;[02] CORRECTED CORRODED ELEMENT PART NUMBER;[03] REMOVED AND REPLACED AFT CARGO
- [SDR SWAA2025012782839](https://openairdocs.org/sdr/SWAA2025012782839.md): Angle · corroded · Jan 3, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE STA 727I-727J HAS CORROSION.<[01] REMOVED CORROSION IN AFT CARGO L/H TRANSITION ANGLE STA 727I-727J FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.;[02] CORRECTED CORRODED ELEMENT PART NUMBER;[03] REMOVED AND REPLACED AFT CARGO L
- [SDR SWAA2025012782834](https://openairdocs.org/sdr/SWAA2025012782834.md): Angle · corroded · Jan 3, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE STA 727A-727B HAS CORROSION.<[01] REMOVED CORROSION IN AFT CARGO L/H TRANSITION ANGLE STA 727A-727B FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.;[02] CORRECTED CORRODED ELEMENT PART NUMBER;[03] REMOVED AND REPLACED AFT CARGO L
- [SDR SWAA2025012782835](https://openairdocs.org/sdr/SWAA2025012782835.md): Angle · corroded · Jan 3, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE STA 727D-727E HAS CORROSION.<[01] REMOVED CORROSION IN AFT CARGO L/H TRANSITION ANGLE STA 727D-727E FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.;[02] CORRECTED CORRODED ELEMENT PART NUMBER;[03] REMOVED AND REPLACED AFT CARGO L
- [SDR SWAA2025012782836](https://openairdocs.org/sdr/SWAA2025012782836.md): Angle · corroded · Jan 3, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE STA 727E-727F HAS CORROSION.<[01] REMOVED CORROSION IN AFT CARGO L/H TRANSITION ANGLE STA 727E-727F FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.;[02] CORRECTED CORRODED ELEMENT PART NUMBER;[03] REMOVED AND REPLACED AFT CARGO L
- [SDR SWAA2025012782840](https://openairdocs.org/sdr/SWAA2025012782840.md): Angle · corroded · Jan 3, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE STA 727F-727G HAS CORROSION.<[01] REMOVED CORROSION IN AFT CARGO L/H TRANSITION ANGLE STA 727F-727G FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.;[02] CORRECTED CORRODED ELEMENT PART NUMBER;[03] REMOVED AND REPLACED AFT CARGO L
- [SDR SWAA2025012782837](https://openairdocs.org/sdr/SWAA2025012782837.md): Angle · corroded · Jan 3, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE STA 727G THRU 727H HAS CORROSION.<[01] REMOVED CORROSION IN AFT CARGO L/H TRANSITION ANGLE STA 727G THRU 727H; FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.;[02] CORRECTED CORRODED ELEMENT PART NUMBER;[03] REMOVED AND REPLACED
- [SDR SWAA2025012782841](https://openairdocs.org/sdr/SWAA2025012782841.md): Angle · corroded · Jan 3, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE STA 727H THRU 727I HAS CORROSION.<[01] REMOVED CORROSION IN AFT CARGO L/H TRANSITION ANGLE STA 727H THRU 727I; FOUND TO BE OUT OF LIMIT PER SRM 53-00-52-1A-2.;[02] CORRECTED CORRODED ELEMENT PART NUMBER;[03] REMOVED AND REPLACED
- [SDR SWAA2025012782545](https://openairdocs.org/sdr/SWAA2025012782545.md): Scuff Plate · cracked · Jan 3, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT; CARGO DOOR CUTOUT; AFT CORNER SCUFF PLATE CRACKED.<[01] REMOVED AND REPLACED AFT CARGO COMPARTMENT; CARGO DOOR CUTOUT; AFT CORNER SCUFF PLATE IAW AMM 53-11-02.;[02] PARTS DATA UPDATE ONLY;[03] C/W;[04] C/W LEAK CHECK; NO DEFECT NOTED.
- [SDR SWAA2025012882540](https://openairdocs.org/sdr/SWAA2025012882540.md): Intercostal · corroded · Jan 2, 2025 · N8526W · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT L/H LAV; BEHIND AFT OUTBOARD MOUNT; HAS FLOORBOARD SCREW/INSERT; ON SUPPORT BRACKET AT STA. 947 +8.<[01]. REMOVED AND REPLACED SUPPORT INTERCOSTAL PER SRM 51-10-02.;[02] INSPECTION VERIFIED CORRECTIVE ACTION TAKEN IN STEP 1.
- [SDR SWAA2025012782538](https://openairdocs.org/sdr/SWAA2025012782538.md): Support Bracket · corroded · Jan 2, 2025 · N8526W · Boeing 7378H4 · Fuselage, Equipment Attach Fittings
  > AFT L/H LAV; AFT OUTBOARD MOUNT; HAS EVIDENCE OF CORROSION ON SUPPORT BRACKET AT STA. 947.<[01] REMOVED AND REPLACED SUPPORT FITTING PER SRM 51-10-02.;[02] INSPECTION VERIFIED CORRECTIVE ACTION TAKEN IN STEP 1.
- [SDR SWAA2025012782534](https://openairdocs.org/sdr/SWAA2025012782534.md): Vapor Barrier · cracked · Jan 2, 2025 · N8526W · Boeing 7378H4 · Fuselage Main, Bulkhead
  > STA 663 VAPOR BARRIER UPPER ATTACH ANGLE HAS CRACK AT LBL 33<[01] REJECTION INITIATED ON STEP #3 DUE TO: STEP #1 SHOWS PANEL REMOVED TO FOM INSTEAD OF CREATING A FOUND FAULT AS REQUIRED BY MPM 52.2.1.;[02] COMPLETED NDT STEP 4 IAW NDT MANUAL PART 6 PROCEDURE 1

Next page: https://openairdocs.org/aircraft/N8526W/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 = 'N8526W' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8526W/reports

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