# Service difficulty reports: N8532S

A list on [N8532S](https://openairdocs.org/aircraft/N8532S.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 · 77 reports

- [SDR SWAA2026101230130](https://openairdocs.org/sdr/SWAA2026101230130.md): Fastener · missing · Oct 6, 2026 · N8532S · Boeing 7378H4 · Emergency Equipment
  > PER M-23-125-01839-TLD ACCOMPLISH A PERMANENT REPAIR TO LT AFT ENTRY DOOR GIRT BAR RETAINER. INSTALLED MISSING FASTENER IAW SRM 51-40-02.
- [SDR SWAA2026100540509](https://openairdocs.org/sdr/SWAA2026100540509.md): Rivet · sheared · Oct 1, 2026 · N8532S · Boeing 7378H4 · Emergency Equipment
  > CA SIDE AFT SLIDE GIRT BAR RETAINING HOOK RIVET SHEARED C/W EA M-23-125-01839
- [SDR SWAA2026082721009](https://openairdocs.org/sdr/SWAA2026082721009.md): Flashlight · not seated · Aug 23, 2026 · N8532S · Boeing 7378H4 · Emergency Equipment
  > PORTABLE FLASHLIGHT LIGHT FWD GALLEY INOP RESEATED FWD GALLEY FLASHLIGHT IN REFERENCE WITH AMM 25-64-00.
- [SDR SWAA2026061110938](https://openairdocs.org/sdr/SWAA2026061110938.md): Flashlight · inoperative · Jun 10, 2026 · N8532S · Boeing 7378H4 · Emergency Equipment
  > FWD GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FWD GALLEY EMER FLASHLIGHT IAW AMM 25-64-00.
- [SDR SWAA2026022671958](https://openairdocs.org/sdr/SWAA2026022671958.md): Battery Pack · inoperative · Feb 19, 2026 · N8532S · Boeing 7378H4 · Emergency Lighting
  > PASSENGER OVHD EMERGENCY LIGHT INOPERATIVE AT 25DEF. REMOVED AND REPLACED M1672 BATTERY PACK, OPS CHECKED GOOD IAW AMM 33-51-06-960-805-NG.
- [SDR SWAA2026030267995](https://openairdocs.org/sdr/SWAA2026030267995.md): Mount · corroded · Feb 5, 2026 · N8532S · Boeing 7378H4 · Engine Mount Section
  > NR 1 ENGINE FWD MOUNT HAD EVIDENCE OF FRETTING AT THE OTBD LINK ASSEMBLY UPPER AND LOWER ATTACH BOLTS. R & R THE NR 1 ENGINE FWD ENGINE MOUNT ASSEMBLY IAW AMM 71-21-01.
- [SDR SWAA2026022670876](https://openairdocs.org/sdr/SWAA2026022670876.md): Panel · damaged · Feb 3, 2026 · N8532S · Boeing 7378H4 · Passenger Compartment Equipment
  > PASSENGER CABIN CEILING BULL NOSE COVE PANEL IS DAMAGED, OR PRIOR REPAIRS ARE PEELING OFF AT 6/7 ABC AND 17/18 ABC. REMOVED AND REPLACED THE BULL NOSE PANELS AT POSITION 6/7 ABC AND 17/18ABC PER AMM 33-51-01. INSPECTED IAW AMM 33-51-01-960-802-NG.
- [SDR SWAA2026030266698](https://openairdocs.org/sdr/SWAA2026030266698.md): Bracket · cracked · Feb 2, 2026 · N8532S · Boeing 737824 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 1 ENGINE INBD FAN COWL VERTICAL BRACKET JUST AFT OF OIL SERVICE DOOR IS CRACKED. NR 1 ENGINE FAN COWL REPLACED ON TTG8Q00S5HD9.
- [SDR SWAA2026030266699](https://openairdocs.org/sdr/SWAA2026030266699.md): Bracket · cracked · Feb 2, 2026 · N8532S · Boeing 7378H4 · Nacelle/Pylon, Main Frame
  > NUMBER 2 ENGINE OTBD FAN COWL VERTICAL BRACKET, JUST BEHIND OIL SERVICE DOOR, CRACKED. NR 2 ENGINE FAN COWL REPLACED ON TTG8Q00S5HD9.
- [SDR SWAA2026022666682](https://openairdocs.org/sdr/SWAA2026022666682.md): Tail Cone · delaminated · Feb 1, 2026 · N8532S · Boeing 7378H4 · Aerodynamic Fairings
  > DELAMINATION LOCATED ON AFT TAIL CONE RT SIDE APROX 25 FROM APU EXHAUST AND 19 FROM BOTTOM OF RUDDER. REMOVED DAMAGE TO AREA IAW SRM 51-70-05-2R-0. C/W INSPECTION OF DAMAGE REMOVAL TO AREA PER 51-70-05-2R-0. PERFORMED TAP TEST IAW 51-10-06. NO DELAMINATION
- [SDR SWAA2026022666683](https://openairdocs.org/sdr/SWAA2026022666683.md): Fairing · damaged · Feb 1, 2026 · N8532S · Boeing 7378H4 · Trailing Edge Flaps
  > NR 3 CANOE FAIRING HAS ELONGATED HOLES WHERE THE TAIL CONE ATTACHES. REMOVED FAIRING FROM ACFT AND REMOVED DRIVE LINKAGE FROM FAIRING ON BENCH IAW AMM 27-51-18. INSTALLED AFT LINK ASSEMBLY IN NEW AFT FLAP SUPPORT FAIRING IAW AMM 27-51-18. R & R THE AFT TAI
- [SDR SWAA2026030265791](https://openairdocs.org/sdr/SWAA2026030265791.md): Attach Angle · no discrepancy · Jan 30, 2026 · N8532S · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > THE LT A/C BAY VAPOR BARRIER ATTACH ANGLE AT BS 663, LBL 34 WAS CRACKED. ACCOMPLISHED HFEC INSPECTION OF THE DAMAGED AREA AND VERIFIED THE CRACK IAW NDT MANUAL PART 6; 51-00-00, PROCEDURE 23. ACCOMPLISHED HFEC HOLE PROB INSPECTION OF LT VAPOR BARRIER ANGLE
- [SDR SWAA2026030265788](https://openairdocs.org/sdr/SWAA2026030265788.md): Attach Angle · cracked · Jan 30, 2026 · N8532S · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > THE RT A/C BAY VAPOR BARRIER ATTACH ANGLE, BS 663, RBL 9 CRACKED. ACCOMPLISHED HFEC INSPECTION OF THE DAMAGED AREA & VERIFIED THE CRACK IAW NDT MANUAL PART 6, 51-00-00, PROCEDURE 23. REMOVED & REPLACED THE VAPOR BARRIER ATTACH ANGLE IAW SRM 51-40-02. TANK S
- [SDR SWAA2026030265789](https://openairdocs.org/sdr/SWAA2026030265789.md): Attach Angle · cracked · Jan 30, 2026 · N8532S · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > THE RT A/C BAY VAPOR BARRIER ATTACH ANGLE AT BS 663, RBL 34 CRACKED. ACCOMPLISHED HFEC INSPECTION OF THE DAMAGED AREA AND VERIFIED THE CRACK IAW NDT MANUAL PART 6, 51-00-00, PROCEDURE 23. PERFORMED HOLE PROBE INSPECTION ON FUEL TANK FASTENERS HOLES PER HFE
- [SDR SWAA2026030265790](https://openairdocs.org/sdr/SWAA2026030265790.md): Attach Angle · cracked · Jan 30, 2026 · N8532S · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > THE LEFT A/C BAY VAPOR BARRIER ATTACH ANGLE AT BS 663, LBL 9 IS CRACKED. ACCOMPLISHED HFEC INSPECTION OF THE DAMAGED AREA & VERIFIED THE CRACK IAW NDT MANUAL PART 6; 51-00-00, PROCEDURE 23. REMOVED THE LT A/C BAY VAPOR BARRIER ATTACH ANGLE IAW SRM 51-40-02.
- [SDR SWAA2026022666031](https://openairdocs.org/sdr/SWAA2026022666031.md): Battery Pack · inoperative · Jan 30, 2026 · N8532S · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE, RT SIDE ON OVERHEAD VALANCE FROM SEAT ROW 2DEF- 13DEF. RESTORED AIRCRAFT POWER AND RECHARGED EMERGENCY LIGHT BATTERY PACKS IAW AMM 33-51-06. EMERGENCY LIGHTS OPS TESTED GOOD IAW AMM 33-51-00. INSPECTED IAW AMM 33-51-06-201-NG.
- [SDR SWAA2026022665787](https://openairdocs.org/sdr/SWAA2026022665787.md): Battery Pack · inoperative · Jan 30, 2026 · N8532S · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE, L/H SIDE ON OVERHEAD VALANCE FROM SEAT ROW 2ABC - 13ABC. R & R LT EMERGENCY LIGHT POWER PACK ASSY AND OPS CHECKED GOOD IAW AMM 33-51-06-201.
- [SDR SWAA2026030265786](https://openairdocs.org/sdr/SWAA2026030265786.md): Plate · cracked · Jan 29, 2026 · N8532S · Boeing 7378H4 · Wing Main, Frame Structure
  > LEFT WING WAFFLE PLATE CRACKED I/B OF NR 3 FLAP TRACK. REMOVED CRACKED WAFFLE PLATE IAW SRM 51-40-02. LOCATED AND DRILLED FASTENER HOLES IN A NEW WAFFLE PLATE IAW SRM 51-40-05. REMOVED AND INSTALLED THE NEW WAFFLE PLATE WITH FASTENERS IAW SRM 51-40-02.
- [SDR SWAA2026030265785](https://openairdocs.org/sdr/SWAA2026030265785.md): Plate · cracked · Jan 29, 2026 · N8532S · Boeing 7378H4 · Wing Main, Frame Structure
  > RIGHT WING INBD OF NR 6 FLAP TRACK, WAFFLE PLATE CRACKED. REMOVED CRACKED WAFFLE PLATE IAW SRM 51-40-02. LOCATED & DRILLED FASTENER HOLES IN NEW WAFFLE PLATE IAW SRM 51-40-05. REMOVED AND INSTALLED A NEW WAFFLE PLATE WITH FASTENERS IAW SRM 51-40-02.
- [SDR SWAA2026030264282](https://openairdocs.org/sdr/SWAA2026030264282.md): Cowling · pulled · Jan 24, 2026 · N8532S · Boeing 7378H4 · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE OUTER LIP SKIN FOUR FASTENERS LOOSE & PULLED. REMOVED AND REPLACED THE NR 2 ENGINE INLET COWL IAW AMM 71-11-01 AND TASK TTG8Q01A4JPY.
- [SDR SWAA2026010557000](https://openairdocs.org/sdr/SWAA2026010557000.md): Battery Pack · inoperative · Dec 31, 2025 · N8532S · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY AISLE LIGHT AT SEAT 17 AND 21 DEF; AT RIGHT OVER WING SCAPE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2025112438283](https://openairdocs.org/sdr/SWAA2025112438283.md): Strap · degraded · Nov 21, 2025 · N8532S · Boeing 7378H4 · Emergency Equipment
  > FWD SERVICE DOOR SAFETY STRAP DEGRADED.<[01] R&R FWD SERVICE DOOR SAFETY STRAP PER SIP.
- [SDR SWAA2025091915617](https://openairdocs.org/sdr/SWAA2025091915617.md): Battery Pack · no test · Sep 17, 2025 · N8532S · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT RELATED TO BATTERY PACK (M1673) FAIL TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1673 AND TESTED GOOD PER AMM 33-51-06-960-805.
- [SDR SWAA2025060977447](https://openairdocs.org/sdr/SWAA2025060977447.md): Handle · loose · Jun 3, 2025 · N8532S · Boeing 7378H4 · Service Doors
  > FWD SERVICE DOOR ASSIST HANDLE IS LOOSE. SECURED FWD SERVICE DOOR ASSIST HANDLE REF AMM 20-50-11.
- [SDR SWAA2024121675533](https://openairdocs.org/sdr/SWAA2024121675533.md): Battery Pack · inoperative · Dec 10, 2024 · N8532S · Boeing 7378H4 · Emergency Lighting
  > R1 DOOR EMERGENCY LIGHTS OUT AS WELL AS ROWS 8; 14 AND 20<[01] R&R POWER SUPPLY BATTER PACKS FOR R1 DOOR AND ROWS 8; 14 AND 20. OPS CHECK GOOD.
- [SDR SWAA2024121075008](https://openairdocs.org/sdr/SWAA2024121075008.md): Flashlight · failed · Dec 7, 2024 · N8532S · Boeing 7378H4 · Emergency Equipment
  > CREW REPORTS CAPT SIDE AFT OTBD EMERGENCY FLASHLIGHT TESTS RED<[01] R&R FLASHLIGHT AND BATTERY ASSY PER S.I.P.
- [SDR SWAA2024083031000](https://openairdocs.org/sdr/SWAA2024083031000.md): Handle · cracked · Aug 27, 2024 · N8532S · Boeing 7378H4 · Passenger/Crew Doors
  > EMERGENCY EXIT ROW AT 14A HAS A CRACKED ACCESS PANEL FOR THE DOOR ASSIST STRAP.<[01] R/R PANEL. REF MM 52-22-00.
- [SDR SWAA2024080924385](https://openairdocs.org/sdr/SWAA2024080924385.md): Megaphone · inoperative · Aug 8, 2024 · N8532S · Boeing 7378H4 · Emergency Equipment
  > FWD MEGAPHONE INOP<[01] REPLACED FWD MEGAPHONE IAW AMM 25-64-00. OPS TEST NML.
- [SDR SWAA2024053191854](https://openairdocs.org/sdr/SWAA2024053191854.md): Battery · inoperative · May 30, 2024 · N8532S · Boeing 7378H4 · Emergency Equipment
  > AFT GALLEY MEGAPHONE WON'T TEST<[01] 01 - REMOVED AND REPLACED PER [AMM 25-64-00-900-804-NG (MEGAPHONE BATTERY REPLACEMENT - PERMANENT)]
- [SDR SWAA2024052890135](https://openairdocs.org/sdr/SWAA2024052890135.md): Battery Pack · inoperative · May 26, 2024 · N8532S · Boeing 7378H4 · Emergency Equipment
  > FLIGHT CREW REPORTS AFT FLASHLIGHT NOT TESTING<[01] R&R?D AFT FLASHLIGHT BATTERY PACK AND OPS TESTED PER<BR>MM 25-64-00
- [SDR SWAA2024042579313](https://openairdocs.org/sdr/SWAA2024042579313.md): Megaphone · stuck · Apr 25, 2024 · N8532S · Boeing 7378H4 · Emergency Equipment
  > FWD MEGAPHONE SWITCH STICKING IN 'ON'<[01] R+R FWD MEGAPHONE PER AMM 25-64-00.
- [SDR SWAA2024042578328](https://openairdocs.org/sdr/SWAA2024042578328.md): Battery · discharged · Apr 23, 2024 · N8532S · Boeing 7378H4 · Emergency Equipment
  > AFT GALLEY MEGAPHONE BATTERY LOW<[01] 01 - REMOVED AND REPLACED PER [AMM 25-64-00-900-804-NG (MEGAPHONE BATTERY REPLACEMENT - PERMANENT)]
- [SDR SWAA2024031865002](https://openairdocs.org/sdr/SWAA2024031865002.md): Megaphone · inoperative · Mar 18, 2024 · N8532S · Boeing 7378H4 · Emergency Equipment
  > AFT MEGAPHONE INOP<[01] AFT MEGAPHONE OPS CHECK NORMAL PER AMM 25-64-00
- [SDR SWAA2024021251182](https://openairdocs.org/sdr/SWAA2024021251182.md): Lamp · inoperative · Feb 11, 2024 · N8532S · Boeing 7378H4 · Emergency Lighting
  > AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RE-LAMPED AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT REF 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2024011640681](https://openairdocs.org/sdr/SWAA2024011640681.md): Girt Bar · loose · Jan 13, 2024 · N8532S · Boeing 7378H4 · Emergency Equipment
  > L1 GIRT BAR LOOSE. REPORTED BY OPS<[01] INSPECTED AND REPOSITITIONED L1 DOOR GIRT BAR PER AMM 25-66-01.
- [SDR SWAA2023052450898](https://openairdocs.org/sdr/SWAA2023052450898.md): Bracket · out of position · May 21, 2023 · N8532S · Boeing 7378H4 · Emergency Equipment
  > AFT GALLEY MEGAPHONE BRACKET APPEARS INSTALLED UPSIDE DOW<[01] REPOSITIONED AFT GALLEY MEGAPHONE BRACKET REF CMM 25-40-42.
- [SDR SWAA2023032320207](https://openairdocs.org/sdr/SWAA2023032320207.md): Battery · inoperative · Mar 22, 2023 · N8532S · Boeing 7378H4 · Emergency Equipment
  > 1 FWD FLIGHT ATTENDANT FLASHLIGHT INOP<[01] R&R?D FWD CABIN FLASH LIGHT BATTERY REF AMM 25-64-00
- [SDR SWAA2023032118359](https://openairdocs.org/sdr/SWAA2023032118359.md): Flashlight · missing · Mar 19, 2023 · N8532S · Boeing 7378H4 · Emergency Equipment
  > FOUND FWD FLIGHT ATTENDANT FLASHLIGHTS AND BRACKETS MISSING<[01] INSTALLED FWD FLIGHT ATTENDANT FLASHLIGHT BRACKETS AND INBOARD FLASHLIGHT PER AMM 25-64-00. OPS CHECK GOOD. OUTBOARD FLIGHT ATTENDANT FLASHLIGHT MISSING. OK TO CONTINUE PER MEL 25-12-01 SP1B. MDD
- [SDR SWAA2023032016515](https://openairdocs.org/sdr/SWAA2023032016515.md): Megaphone · broken · Mar 14, 2023 · N8532S · Boeing 7378H4 · Emergency Equipment
  > MEGAPHONE; G2 GALLEY; HAS BROKEN TRIGGER MEGAPHONE G2 GALLEY HAS BROKEN TRIGGER<[01] R AND R MEGAPHONE PER AMM 25-64-00.
- [SDR SWAA2023031613875](https://openairdocs.org/sdr/SWAA2023031613875.md): Battery Pack · inoperative · Mar 8, 2023 · N8532S · Boeing 7378H4 · Emergency Lighting
  > FWD ENTRY DOOR EMERGENCY LIGHTS INOP<[01] REMOVED REPLACED AND OPS CHECKED FWD ENTRY BATTERY PACK PER AMM 33-511-06.;[02] REMOVED REPLACED AND OPS CHECKED FWD ENTRY EMERGENCY LIGHT BATTERY PER AMM 33-51-06;[03] C/W INSPECTION
- [SDR SWAA2023032011905](https://openairdocs.org/sdr/SWAA2023032011905.md): Intercostal · cracked · Mar 2, 2023 · N8532S · Boeing 7378H4 · Trailing Edge Flaps
  > INTERCOSTAL AT UPPER TRAILING EDGE PANEL INBOARD OF L/H WING DEFLECTION RIB IS CRACKED.<[01] REMOVED INTERCOSTAL AT UPPER TRAILING EDGE PANEL INBOARD OF L/H WING DEFLECTION RIB PER SRM 51-40-02;[02] INSTALLED NEW INTERCOSTAL AT UPPER TRAILING EDGE PANEL I/B OF
- [SDR SWAA2023032008682](https://openairdocs.org/sdr/SWAA2023032008682.md): Support · cracked · Feb 22, 2023 · N8532S · Boeing 7378H4 · Fuselage Internal Mounting Structure
  > FLOOR SUPPORT CRACKED STA. 540 BL-0 L/H SIDE FLOOR SUPPORT CRACKED STA. 540 BL-0 TO LBL-24<[01] REMOVED AND REPLACED PER SRM 51-40-02
- [SDR SWAA2023031605721](https://openairdocs.org/sdr/SWAA2023031605721.md): Angle · broken · Feb 21, 2023 · N8532S · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT T ANGLE BROKEN AT STATION 540 FOUND FLOOR SUPPORT T -ANGLE BROKEN AT STA 540 RIGHT OF BUTT LINE 0.<[01] REMOVED AND REPLACED PER SRM 51-40-02
- [SDR SWAA2023032004084](https://openairdocs.org/sdr/SWAA2023032004084.md): Angle · corroded · Feb 16, 2023 · N8532S · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > FWD CARGO COMPARTMENT RT TRANSITION ANGLE HAS AREAS OF CORROSION FROM STA 500C-500D<[01] R/H TRANSITION ANGLE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. REMOVED R/H TRANSITION ANGLE FROM STA 500A TO 500I. NEW TRANSITION ANGLE TO BE REPLACED ON NON ROUTINE
- [SDR SWAA2023032004134](https://openairdocs.org/sdr/SWAA2023032004134.md): Angle · corroded · Feb 16, 2023 · N8532S · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > FWD CARGO COMPARTMENT RT TRANSITION ANGLE HAS AREAS OF CORROSION FROM STA 500D-500E<[01] R/H TRANSITION ANGLE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. REMOVED R/H TRANSITION ANGLE FROM STA 500A TO 500I. NEW TRANSITION ANGLE TO BE REPLACED ON NON ROUTINE
- [SDR SWAA2023032004135](https://openairdocs.org/sdr/SWAA2023032004135.md): Angle · corroded · Feb 16, 2023 · N8532S · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > FWD CARGO COMPARTMENT RT TRANSITION ANGLE HAS AREAS OF CORROSION FROM STA 500E-500F<[01] R/H TRANSITION ANGLE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. REMOVED R/H TRANSITION ANGLE FROM STA 500A TO 500I. NEW TRANSITION ANGLE TO BE REPLACED ON NON ROUTINE
- [SDR SWAA2023032004086](https://openairdocs.org/sdr/SWAA2023032004086.md): Angle · corroded · Feb 16, 2023 · N8532S · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > FWD CARGO COMPARTMENT RT TRANSITION ANGLE HAS AREAS OF CORROSION FROM STA 500F-500G<[01] R/H TRANSITION ANGLE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. REMOVED R/H TRANSITION ANGLE FROM STA 500A TO 500I. NEW TRANSITION ANGLE TO BE REPLACED ON NON ROUTINE
- [SDR SWAA2023032004136](https://openairdocs.org/sdr/SWAA2023032004136.md): Angle · corroded · Feb 16, 2023 · N8532S · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > FWD CARGO COMPARTMENT RT TRANSITION ANGLE HAS AREAS OF CORROSION FROM STA 500G-500H<[01] R/H TRANSITION ANGLE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. REMOVED R/H TRANSITION ANGLE FROM STA 500A TO 500I. NEW TRANSITION ANGLE TO BE REPLACED ON NON ROUTINE
- [SDR SWAA2023032004087](https://openairdocs.org/sdr/SWAA2023032004087.md): Angle · corroded · Feb 16, 2023 · N8532S · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > FWD CARGO COMPARTMENT RT TRANSITION ANGLE HAS AREAS OF CORROSION FROM STA 500H-500I<[01] R/H TRANSITION ANGLE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. REMOVED R/H TRANSITION ANGLE FROM STA 500A TO 500I. NEW TRANSITION ANGLE TO BE REPLACED ON NON ROUTINE
- [SDR SWAA2023032004103](https://openairdocs.org/sdr/SWAA2023032004103.md): Angle · cracked · Feb 16, 2023 · N8532S · Boeing 7378H4 · Fuselage, Stabilizer Attach Fittings
  > AFT CARGO STA. 867; LAV POST ANGLE CRACKED.<[01] R&R?D ANGLE IAW SRM 51-40-02.

Next page: https://openairdocs.org/aircraft/N8532S/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 = 'N8532S' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8532S/reports

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