# Service difficulty reports: N8525S

A list on [N8525S](https://openairdocs.org/aircraft/N8525S.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 2 · 72 reports

- [SDR SWAA2026072457953](https://openairdocs.org/sdr/SWAA2026072457953.md): Battery · discharged · Jul 20, 2026 · N8525S · Boeing 7378H4 · Emergency Equipment
  > AFTER FAS FLASHLIGHT LOW BATTERY REMOVED AND REPLACED AFT FAS FLASHLIGHT BATTERY PER AMM 25-64-00. OPS CHECK GOOD.
- [SDR SWAA2026070718520](https://openairdocs.org/sdr/SWAA2026070718520.md): Flashlight · no discrepancy · Jul 3, 2026 · N8525S · Boeing 7378H4 · Emergency Equipment
  > AFT LEFT F/A EMERGENCY FLASHLIGHT INOPERATIVE. OPS CHK OF FLASHLIGHT WAS GOOD. IAW AMM 25-64-00.
- [SDR SWAA2026042391460](https://openairdocs.org/sdr/SWAA2026042391460.md): Sign · detached · Apr 20, 2026 · N8525S · Boeing 7378H4 · Emergency Lighting
  > PAX HIT EMERGENCY EXIT SIGN WITH BAG. REINSTALLED EM EXIT SIGN COVER REFERENCE MM 33-51-01.
- [SDR SWAA2026031174711](https://openairdocs.org/sdr/SWAA2026031174711.md): Battery Pack · inoperative · Feb 27, 2026 · N8525S · Boeing 7378H4 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ON M1695 EMERGENCY LIGHT POWER SUPPLY. OPS CHECK GOOD IAW AMM 33-51-06.
- [SDR SWAA2026031173957](https://openairdocs.org/sdr/SWAA2026031173957.md): Seal · cracked · Feb 25, 2026 · N8525S · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STAB, FWD UPPER SLIDING SEAL CRACKED. REMOVED THE CRACKED RT HORIZONTAL STAB SLIDING SEAL & REPLACED WITH A NEW UPPER SEAL PLATE. C/W STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL INSTALLATION IAW AMM 53-31-31-400-802 UP TO STEP 3.F(20).
- [SDR SWAA2026031173563](https://openairdocs.org/sdr/SWAA2026031173563.md): Seal · cracked · Feb 24, 2026 · N8525S · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB FWD UPPER SLIDER SEAL CRACKED. ATTACHED THE TIE- BAR AND CORNER PLATES TO REPLACEMENT UPPER SEAL IAW SRM 51-40-02 & AMM 53-31-31.
- [SDR SWAA2026031170228](https://openairdocs.org/sdr/SWAA2026031170228.md): Bulkhead Web · cracked · Feb 13, 2026 · N8525S · Boeing 7378H4 · Fuselage Main, Bulkhead
  > RIGHT BS 663, RBL 38, WEB CRACKED AT FASTENER HOLE. REMOVED & FABRICATED RT WEB IAW SRM 57-10-10-01-3; SRM 51-40-02. REPLACEMENT WEB IAW SRM 57-10-10-01-3. INSTALLED REPLACEMENT WEB IAW SRM 51-40-02. REF DWG 111A1141 APPROVED THRU BAC SMAL FOR 111A1141-30
- [SDR SWAA2026022569194](https://openairdocs.org/sdr/SWAA2026022569194.md): Seal · cracked · Feb 9, 2026 · N8525S · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STABILIZER PANEL 343AB SLIDING FIN IS WORN & STARTING TO CRACK. REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER PANEL 343AB SLIDING SEAL IAW SRM 51-40-02..
- [SDR SWAA2026022569195](https://openairdocs.org/sdr/SWAA2026022569195.md): Panel · cracked · Feb 9, 2026 · N8525S · Boeing 7378H4 · Horizontal Stabilizer Structure
  > RIGHT HORIZONTAL STABILIZER PANEL 343AT SLIDING FIN IS WORN AND CRACKED. REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER PANEL 343AT SLIDING SEAL IAW SRM 51-40-02.
- [SDR SWAA2026031168722](https://openairdocs.org/sdr/SWAA2026031168722.md): Angle · cracked · Feb 7, 2026 · N8525S · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > WEB ANGLE CRACKED ON BACK SIDE JUST INBD OF DEFLECTION RIB. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02.
- [SDR SWAA2026031168497](https://openairdocs.org/sdr/SWAA2026031168497.md): Attach Angle · cracked · Feb 6, 2026 · N8525S · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > LEFT SIDE 663 VAPOR BARRIER ATTACH ANGLE HAS TWO CRACKS AT APPROXIMATELY LBL 9 AND LBL 34. REMOVED TANK FASTENERS COMMON TO THE 663 VAPOR BARRIER ATTACH ANGLE REPAIR/REPLACEMENT IAW SRM 57-10-10-2R-5.
- [SDR SWAA2026031168498](https://openairdocs.org/sdr/SWAA2026031168498.md): Attach Angle · cracked · Feb 6, 2026 · N8525S · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > RIGHT SIDE BS 663 VAPOR BARRIER ATTACH ANGLE HAD 2 CRACKS, RBL 9 & RBL 34. REMOVED TANK FASTENERS COMMON TO THE VAPOR BARRIER ATTACH ANGLE. REPAIRED & REPLACEMENT IAW SRM 57-10-10-2R-5.
- [SDR SWAA2026031170227](https://openairdocs.org/sdr/SWAA2026031170227.md): Mount · corroded · Feb 5, 2026 · N8525S · Boeing 7378H4 · Engine Mount Section
  > NR 2 ENGINE AFT MOUNT HAS EVIDENCE OF FRETTING ON THE OUTBOARD LINK AT TRF ATTACHMENT. REMOVED AND INSTALLED NEW AFT ENGINE MOUNT IAW MT 771-021-00-03.
- [SDR SWAA2025091513848](https://openairdocs.org/sdr/SWAA2025091513848.md): Battery Pack · inoperative · Sep 12, 2025 · N8525S · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. RT SIDE ROWS 1 - 24; LT SIDE 1 - 14. R & R THE BATTERY PACKS IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2025091612536](https://openairdocs.org/sdr/SWAA2025091612536.md): Seal · cracked · Sep 8, 2025 · N8525S · Boeing 7378H4 · Aerodynamic Fairings
  > NOSE RADOME BOOT HAS CRACKING<[01] REMOVED AND REPLACED RADOME PROTECTIVE BOOT IAW AMM 53-52-00;[02] VERIFIED THE FOLLOWING:<BR>REMOVED AND REPLACED RADOME PROTECTIVE BOOT IAW AMM 53-52-00
- [SDR SWAA2025081198860](https://openairdocs.org/sdr/SWAA2025081198860.md): Lens · detached · Aug 5, 2025 · N8525S · Boeing 7378H4 · Emergency Lighting
  > CABIN CEILING EXIT LIGHT COVER POPPED OFF. INSTALLED COVER PER AMM 33-51-01
- [SDR SWAA2025041423032](https://openairdocs.org/sdr/SWAA2025041423032.md): Lens · unsecure · Apr 8, 2025 · N8525S · Boeing 7378H4 · Emergency Lighting
  > MID CABIN EXIT SIGN LENS UNSECURED<[01] RESECURED LENS PER AMM 33-51-02
- [SDR SWAA2025021996839](https://openairdocs.org/sdr/SWAA2025021996839.md): Charger · inoperative · Feb 17, 2025 · N8525S · Boeing 7378H4 · Emergency Lighting
  > LH OVERWING EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED CHARGER ASSY AND BATTERY PACK FOR LH OVERWING EMERGENCY EXIT LIGHTS IAW AMM 33-51-06. OPS CHECK GOOD;[02] REMOVED AND REPLACED CHARGER ASSY AND BATTERY PACK (POS. M1670) FOR LH OVERWING EMERGENCY
- [SDR SWAA2025021997682](https://openairdocs.org/sdr/SWAA2025021997682.md): Battery Pack · inoperative · Feb 17, 2025 · N8525S · Boeing 7378H4 · Emergency Lighting
  > LH OVERWING EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED CHARGER ASSY AND BATTERY PACK FOR LH OVERWING EMERGENCY EXIT LIGHTS IAW AMM 33-51-06. OPS CHECK GOOD;[02] REMOVED AND REPLACED CHARGER ASSY AND BATTERY PACK (POS. M1670) FOR LH OVERWING EMERGENCY
- [SDR SWAA2024123181985](https://openairdocs.org/sdr/SWAA2024123181985.md): Battery · discharged · Dec 30, 2024 · N8525S · Boeing 7378H4 · Emergency Equipment
  > AFT GALLEY MEGAPHONE BATTERY LOW.<[01] REPLACED AFT MEGAPHONE PER S.I.P.
- [SDR SWAA2024121777871](https://openairdocs.org/sdr/SWAA2024121777871.md): Sign · out of adjust · Dec 15, 2024 · N8525S · Boeing 7378H4 · Emergency Lighting
  > O-HEADEMERGENCY EXIT ROW SIGN FELL OFF ITS FRAME<[01] REINSTALLED OVERHEAD EXIT ROW SIGN LENS. REF AMM 33-51-01.
- [SDR SWAA2024110155194](https://openairdocs.org/sdr/SWAA2024110155194.md): Megaphone · inoperative · Oct 31, 2024 · N8525S · Boeing 7378H4 · Emergency Equipment
  > MEGAPHONE NOT AUDIBLE<[01] REMOVED AND INSTALLED MEGAPHONE. REPLACED BATTERIES ON NEW MEGAPHONE PER AMM 25-64-00. OP CHECK GOOD.
- [SDR SWAA2024103054504](https://openairdocs.org/sdr/SWAA2024103054504.md): Flashlight · inoperative · Oct 28, 2024 · N8525S · Boeing 7378H4 · Emergency Equipment
  > BOTH FA AFT FLASHLIGHTS INOP.<[01] RESEATED BOTH AFT FA FLASHLIGHTS AND TESTED OK REF AMM 25-64-00. INSTALLED TAMPER SEALS REF AMM 25-64-00.
- [SDR SWAA2024100745255](https://openairdocs.org/sdr/SWAA2024100745255.md): Cover · missing · Oct 4, 2024 · N8525S · Boeing 7378H4 · Emergency Lighting
  > EMEGENCY EXIT SIGN COVERS ON THE CEILING POINTING TO THE EXITS ARE MISSING.<[01] REPLACED CEILING EMERGENCY EXIT SIGN COVER AT STA.589; REF AMM 33-51-01
- [SDR SWAA2024100743930](https://openairdocs.org/sdr/SWAA2024100743930.md): Charger · faulty · Oct 1, 2024 · N8525S · Boeing 7378H4 · Emergency Lighting
  > M1673 POWER SUPPLY ONLY ILLUMINATES FOR 3-5 MINUTES<[01] REMOVED AND REPLACED M1673 (AFT LH) CHARGER ASSY AND BATTERY PACK REF AMM 33-51-06.
- [SDR SWAA2024100745847](https://openairdocs.org/sdr/SWAA2024100745847.md): Battery Pack · faulty · Oct 1, 2024 · N8525S · Boeing 7378H4 · Emergency Lighting
  > M1673 POWER SUPPLY ONLY ILLUMINATES FOR 3-5 MINUTES<[01] REMOVED AND REPLACED M1673 (AFT LH) CHARGER ASSY AND BATTERY PACK REF AMM 33-51-06.
- [SDR SWAA2024092541180](https://openairdocs.org/sdr/SWAA2024092541180.md): Lens · loose · Sep 23, 2024 · N8525S · Boeing 7378H4 · Emergency Lighting
  > OVERHEAD FORWARD FACING EMERGENCY EXIT ROW SIGH FELL OFF<[01] RESECURED OVER WING EMERGENCY EXIT LIGHT LENS PER MM 33-51-01
- [SDR SWAA2024091236155](https://openairdocs.org/sdr/SWAA2024091236155.md): Seal · cracked · Sep 11, 2024 · N8525S · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB UPPER FWD SLIDING SEAL CRACKED.<[01] R&R LH HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL REF. AMM 53-31-31.
- [SDR SWAA2024062504889](https://openairdocs.org/sdr/SWAA2024062504889.md): Lens · detached · Jun 23, 2024 · N8525S · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN OVERHEAD MID CABIN LENSE FELL OUT<[01] RESECURED EMER EXIT SIGN PER AMM 33-51-01
- [SDR SWAA2024061100575](https://openairdocs.org/sdr/SWAA2024061100575.md): Unknown · unknown · Jun 7, 2024 · N8525S · Boeing 7378H4 · Fuselage Structure (General)
  > DURING CLIMB PASSING FL340; POP / THUD FELT RIGHT SIDE OF AIRCRAFT. ALL ENG INDICATIONS AND CONTROL NORMAL. PERFORMED AIRCRAFT WALKAROUND INSPECTION; OBSERVING ALL FLIGHT CONTROLS; ENGINES; PANELS; OPENING; FUSELAGE AND WHEEL WELL AREAS. NOTHING ABNORMAL FOUN
- [SDR SWAA2024060497507](https://openairdocs.org/sdr/SWAA2024060497507.md): Battery · inoperative · Jun 2, 2024 · N8525S · Boeing 7378H4 · Emergency Equipment
  > FORWARD FA JUMPSEAT FLASHLIGHT INOP. R & R EMER FLASHLIGHT BATTERY FWD GALLEY O/B POSITION IAW AMM 25-64-00. TEST NORMAL.
- [SDR SWAA2024052990317](https://openairdocs.org/sdr/SWAA2024052990317.md): Jumpseat · fod · May 27, 2024 · N8525S · Boeing 7378H4 · Passenger Compartment Equipment
  > CAPT SIDE AFT FLIGHT ATTENDANT JUMP SEAT DOES NOT STOW PROPERLY BLOCKS AFT EMERGENCY EXIT PATH<[01] REMOVED FOD FROM AFT FLIGHT ATTENDANT JUMPSEAT IAW SIP.
- [SDR SWAA2024011039415](https://openairdocs.org/sdr/SWAA2024011039415.md): Motor · failed · Jan 9, 2024 · N8525S · Boeing 7378H4 · Elevator Control System
  > PRIMARY STAB TRIM FAILURE<[01] R AND R STAB TRIM MOTOR PER AMM 27-41-71.
- [SDR SWAA2023051849427](https://openairdocs.org/sdr/SWAA2023051849427.md): Lens · missing · May 17, 2023 · N8525S · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT OVERHEAD SIGN ABOVE ROW 14 MISSING ONE LENS<[01] INSTALLED LENS PER AMM 33-51-01
- [SDR SWAA2023040724283](https://openairdocs.org/sdr/SWAA2023040724283.md): Slide · out of adjust · Apr 5, 2023 · N8525S · Boeing 7378H4 · Escape Slide
  > FORWARD ENTRY GERT BAR FALLING OFF HOOK WHEN OPENING DOOR<[01] ADJUSTED BSLIDE ON FWD ENTRY DOOR REF AMM 25-66-01
- [SDR SWAA2023031309687](https://openairdocs.org/sdr/SWAA2023031309687.md): Angle · corroded · Feb 24, 2023 · N8525S · Boeing 7378H4 · Fuselage Structure (General)
  > REJECT: FAULT TTG8Q00HGSR7 (AFT CARGO DOOR SILL PLATE HAS SEVERAL AREAS OF CORROSION) REQUIRES INSPECTION BUYBACK.<[01] FAULT TTG8Q00HGSR7 HAD NO INSPECTION BUY BACK. NEW FAULT RAISED ON TTG8Q00HJ4X0 FOR INSPECTION AND MEASUREMENTS ARE FROM THAT FAULT.;[02] LI
- [SDR SWAA2023031309685](https://openairdocs.org/sdr/SWAA2023031309685.md): Floor Panel · faulty · Feb 23, 2023 · N8525S · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR BOARD 231DF HAS A BAD SCREW INSERT.<[01] REMOVED AND REPLACED 231DF AS PER AMM 53-21-00.;[02] VERIFIED INSTALLATION OF FLOOR PANEL 231DF AS PER AMM 53-21-00.
- [SDR SWAA2023031305632](https://openairdocs.org/sdr/SWAA2023031305632.md): Battery Pack · inoperative · Feb 21, 2023 · N8525S · Boeing 7378H4 · Emergency Lighting
  > AFT GALLEY R/H EMERGENCY LIGHTS BATTERY PACK INOP<[01] REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06;[02] AFT GALLEY EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[03] C/W.
- [SDR SWAA2023031005631](https://openairdocs.org/sdr/SWAA2023031005631.md): Battery Pack · inoperative · Feb 21, 2023 · N8525S · Boeing 7378H4 · Emergency Lighting
  > FWD GALLEY R/H EMERGENCY LIGHTS BATTERY PACK INOP<[01] REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06;[02] FWD GALLEY EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #2
- [SDR SWAA2023031398651](https://openairdocs.org/sdr/SWAA2023031398651.md): Angle · elongated · Feb 4, 2023 · N8525S · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FWD SHIELD SUPPORT ANGLE HAS ELONGATED HOLES<[01] REMOVED AFT CARGO FWD SHIELD SUPPORT ANGLE PER SRM 51-40-02;[02] LOCATED AND DRILLED ANGEL SHIELD SUPPORT # 146A8125U53; PER SRM.51-1002;[03] INSTALLED NEW SUPPORT ANGLE PER SRM 51-40-02.;[04] C/W IN
- [SDR SWAA2023031398649](https://openairdocs.org/sdr/SWAA2023031398649.md): Shield · corroded · Feb 4, 2023 · N8525S · Boeing 7378H4 · Fuselage Structure (General)
  > AFT CARGO RIGHT TRANSITION ANGLE767-787 HAS CORROSION AROUND MULTIPLE FASTNER HOLES. MARKED.<[01] REMOVED CORROSION RIGHT TRANSITION ANGLE STA 767-787. REMAINING THICKNESS 0.030?. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] VERIFIED C/A #1.;[03] REMOV
- [SDR SWAA2023031398650](https://openairdocs.org/sdr/SWAA2023031398650.md): Angle · corroded · Feb 4, 2023 · N8525S · Boeing 7378H4 · Fuselage Structure (General)
  > AFT CARGO LEFT TRANSITION ANGLE HAS AREAS OF CORROSION AROUND FASTNER HOLES STA 727I-747.<[01] REMOVED CORROSION AROUND FASTENER HOLES LEFT TRANSITION ANGLE STA 727I - 747. REMAINING THICKNESS IS 0.030. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] VERI
- [SDR SWAA2023031396392](https://openairdocs.org/sdr/SWAA2023031396392.md): Plate · corroded · Jan 29, 2023 · N8525S · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL PLATE HAS SEVERAL AREAS OF CORROSION; MARKED.<[01] REMOVED SURFACE CORROSION ON RH SILL PLATE FROM STATION 787+5 TO 847. MATERIAL REMAINING THICKNESS.043. SILLL PLATE REQUIRE TO BE REPALACE. ALL WORK REFERENCE TO SRM 53-60-15-1A-1;[02] VER
- [SDR SWAA2023031396386](https://openairdocs.org/sdr/SWAA2023031396386.md): Intercostal · cracked · Jan 29, 2023 · N8525S · Boeing 7378H4 · Wing, Center Box
  > IN THE MAIN CABIN FLOOR AREA AT STATION 540; THERE IS A CRACK AT THE FLEXIBLE INTERCOSTAL AT LBL 2. (SEE ATTACHED PICTURE)<[01] R/R INTERCOSTAL IAW SRM 51-40-02.;[02] C/W INSP
- [SDR SWAA2023031396602](https://openairdocs.org/sdr/SWAA2023031396602.md): Intercostal · cracked · Jan 29, 2023 · N8525S · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > IN THE MAIN CABIN FLOOR AREA AT STATION 540; THERE IS A CRACK AT THE INTERCOSTAL AT RBL 2. (MARKED)<[01] R/R INTERCOSTAL IAW SRM 51-40-02.;[02] C/W INSP
- [SDR SWAA2023031396332](https://openairdocs.org/sdr/SWAA2023031396332.md): Web · cracked · Jan 28, 2023 · N8525S · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > PANEL 424 COWL ASSY - FAN - #2 ENGINE OUTBOARD OIL SERVICE DOOR OPENING; THE AFT REINFORCEMENT WEB IS CRACKED. (MARKED)<[01] REMOVED AND REPLACED REINFORCEMENT WEB PER SRM 51-40-02.;[02] OK
- [SDR SWAA2023031396075](https://openairdocs.org/sdr/SWAA2023031396075.md): Panel · elongated · Jan 28, 2023 · N8525S · Boeing 7378H4 · Standard Practices/Structures
  > PANEL 324BL PANEL ASSEMBLY - TRAILING EDGE - LH VERTICAL FIN HAS 1 FASTENER HOLE THAT IS ELONGATED.(MARKED)<[01] SANDED DAMAGED HOLE/REMOVED DAMAGE IN PREPARATION FOR REPAIR I/A/W SRM 51-70-05-2R-8.;[02] VERIFIED CORRECTIVE ACTION #1;[03] APPLIED REPAIR I/A/W
- [SDR SWAA2023031396039](https://openairdocs.org/sdr/SWAA2023031396039.md): Angle · corroded · Jan 27, 2023 · N8525S · Boeing 7378H4 · Fuselage Structure (General)
  > RH TRANS. ANGLE HAS CORROSION (EXFOLIATION) STA. 500A-500I<[01] REMOVED RH TRANSITION ANGLE FROM STATION 500A-500I FOR REPLACEMENT PER SRM 51-40-02;[02] DRILLED UP AND COUNTERSUNK NEW ANGLE PER SRM 51-40-05.;[03] REMOVED AND REPLACED ANGLE PER SRM 51-40-02.;[0
- [SDR SWAA2023031095768](https://openairdocs.org/sdr/SWAA2023031095768.md): Scuff Plate · cracked · Jan 27, 2023 · N8525S · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO AFT CORNER SCUFF PLATE IS CRACKED<[01] OK TO INSTALL C/W INSPECTION;[02] INSTALLED SCUFF PLATE PER AMM 53-11-02.;[03] VERIFIED INSTALLED SCUFF PLATE PER AMM 53-11-02.;[04] C/W INSPECTION
- [SDR SWAA2023031395748](https://openairdocs.org/sdr/SWAA2023031395748.md): Angle · corroded · Jan 26, 2023 · N8525S · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > R/H TRANSITION ANGLE 727H-727J HAS CORROSION AROUND MULTIPLE FASTNER HOLES. MARKED.<[01] REMOVE SURFACE CORROSION ON RH TRANSITION ANGLE FROM STATION 727H-727J. MATERIAL REMAINING THICKNESS.020. PART REQUIRE TO BE REPLACE. ALL WORK REFERENCE TO SRM 50-00-53-1

Next page: https://openairdocs.org/aircraft/N8525S/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 = 'N8525S' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8525S/reports

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