# Service difficulty reports: N8535S

A list on [N8535S](https://openairdocs.org/aircraft/N8535S.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 · 81 reports

- [SDR SWAA2026092107806](https://openairdocs.org/sdr/SWAA2026092107806.md): Fitting · loose · Sep 16, 2026 · N8535S · Boeing 7378H4 · Emergency Equipment
  > FED AFT GIRT BAR FITTING LOOSE. TIGHTENED LOOSE SCREWS COMMON TO FED AFT GIRT BAR FITTING IAW AMM 25-66-02-400-801.
- [SDR SWAA2026092152602](https://openairdocs.org/sdr/SWAA2026092152602.md): Collar · missing · Sep 14, 2026 · N8535S · Boeing 7378H4 · Service Doors
  > G1 GALLEY ASSIST HANDLE MISSING 1 COLLAR. REPLACED THE G1 GALLEY ASSIST HANDLE COLLAR IAW AMM 52-41-31-400-802.
- [SDR SWAA2026070618318](https://openairdocs.org/sdr/SWAA2026070618318.md): Lens · dislodged · Jul 2, 2026 · N8535S · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN MID CABIN, LENS DISLODGED. SNAPPED EMERGENCY EXIT SIGN LENS BACK ON IAW SIP.
- [SDR SWAA2026062314178](https://openairdocs.org/sdr/SWAA2026062314178.md): Girt Bar · loose · Jun 19, 2026 · N8535S · Boeing 7378H4 · Emergency Equipment
  > F/A REPORTS FWD SERVICE DOOR GIRT BAR CAME LOOSE WHILE DOOR WAS BEING OPENED. INSPECTED FWD SERVICE DOOR GIRT BAR. ALL IS SECURE. OPENED AND CLOSED DOOR; NO DEFECTS NOTED. REF AMM 25-66-01. ACFT OK FOR SERVICE.
- [SDR SWAA2026061510533](https://openairdocs.org/sdr/SWAA2026061510533.md): Battery · no test · Jun 9, 2026 · N8535S · Boeing 7378H4 · Emergency Equipment
  > FWD INBD EMERGENCY FLASHLIGHT WILL NOT TEST. REPLACED FWD INBD FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS TESTED GOOD.
- [SDR SWAA2026051397822](https://openairdocs.org/sdr/SWAA2026051397822.md): Slide · loose · May 11, 2026 · N8535S · Boeing 7378H4 · Escape Slide
  > AFT ENTRY DOOR SLIDE LOOSE IN CASE. REPOSITIONED SLIDE PER MT 725-61-06
- [SDR SWAA2026042490006](https://openairdocs.org/sdr/SWAA2026042490006.md): Battery Pack · failed · Apr 16, 2026 · N8535S · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY BATTERY PACK M01670 WILL NOT TAKE CHARGE. REMOVED; REPLACED; AND OP CHECKED M01670 BATTERY PACK IAW SWA AMM 33-51-06-960-805. NEW BATTERY PACK OP CHECKS GOOD.
- [SDR SWAA2026042490007](https://openairdocs.org/sdr/SWAA2026042490007.md): Battery Pack · failed · Apr 16, 2026 · N8535S · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY BATTERY PACK M01671 WILL NOT TAKE CHARGE. REMOVED; REPLACED; AND OP CHECKED M01671 BATTERY PACK IAW AMM 33-51-06-960-805. NEW BATTERY PACK OP CHECKS GOOD.
- [SDR SWAA2026042490008](https://openairdocs.org/sdr/SWAA2026042490008.md): Battery Pack · failed · Apr 16, 2026 · N8535S · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY BATTERY PACK M01676 WILL NOT TAKE CHARGE. REMOVED; REPLACED; AND OP CHECKED M01676, BATTERY PACK IAW AMM 33-51-06-960-805. NEW BATTERY PACK OP CHECKS GOOD.
- [SDR SWAA2026042490009](https://openairdocs.org/sdr/SWAA2026042490009.md): Battery Pack · failed · Apr 16, 2026 · N8535S · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY BATTERY PACK M01694 WILL NOT TAKE CHARGE. REMOVED; REPLACED; AND OP CHECKED M01694 BATTERY PACK IAW AMM 33-51-06-960-805. NEW BATTERY PACK OP CHECKS GOOD.
- [SDR SWAA2026042490005](https://openairdocs.org/sdr/SWAA2026042490005.md): Battery Pack · failed · Apr 16, 2026 · N8535S · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY BATTERY PACK M01695 WILL NOT TAKE CHARGE. REMOVED; REPLACED; AND OP CHECKED M01695 BATTERY PACK IAW AMM 33-51-06-960-805. NEW BATTERY PACK OP CHECKS GOOD.
- [SDR SWAA2026042490010](https://openairdocs.org/sdr/SWAA2026042490010.md): Battery Pack · failed · Apr 16, 2026 · N8535S · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY BATTERY PACK M02335 WILL NOT TAKE CHARGE. REMOVED AND REPLACED M02335 EMERGENCY BATTERY PACK REF B737-800 AMM 33-51-06-960-805
- [SDR SWAA2026042487547](https://openairdocs.org/sdr/SWAA2026042487547.md): Seal · cracked · Apr 8, 2026 · N8535S · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL CRACKED AND WORN. REMOVED AND REPLACED LEFT STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL IAW AMM 53-31-31.
- [SDR SWAA2026042487548](https://openairdocs.org/sdr/SWAA2026042487548.md): Seal · cracked · Apr 8, 2026 · N8535S · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL CRACKED. REPLACED RT STABILIZER- TO-BODY UPPER FRONT SPAR SLIDING SEAL IAW AMM 53-31-31.
- [SDR SWAA2026042486809](https://openairdocs.org/sdr/SWAA2026042486809.md): Handle · unsecure · Apr 6, 2026 · N8535S · Boeing 7378H4 · Passenger/Crew Doors
  > L1 DOOR ASSIST HANDLE LOOSE NEEDS SECURED. SECURED L1 DOOR ASSIST HANDLE IAW B737-800 AMM 52-11-31-400-802 SUB TASK 52-11-31-420-007.
- [SDR SWAA2026042486807](https://openairdocs.org/sdr/SWAA2026042486807.md): Attach Angle · cracked · Apr 6, 2026 · N8535S · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACKS FOUND RT VAPOR BARRIER ATTACH ANGLE. REMOVED AND REPLACED CRACKED R/H VAPOR BARRIER ATTACH ANGLE IAW DWG 111A1000 REV -, SRM 51-40-02..
- [SDR SWAA2026042486808](https://openairdocs.org/sdr/SWAA2026042486808.md): Attach Angle · cracked · Apr 6, 2026 · N8535S · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKS FOUND LT VAPOR BARRIER ATTACH ANGLE. REMOVED AND REPLACED NEW VAPOR ANGLE IAW SRM 51-40-02 AND BOEING DWG 111A1000 REV: B AND BOEING DRW 111A1000 REV -.
- [SDR SWAA2026042486577](https://openairdocs.org/sdr/SWAA2026042486577.md): Slide · out of adjust · Apr 5, 2026 · N8535S · Boeing 7378H4 · Escape Slide
  > L2 DOOR SLIDE GIRT MATERIAL HANGING OUT OF BUSTLE. REMOVED AND INSTALLED SLIDE IAW AMM 25-66-01-000-802; AMM 25-66-01-400-801 AND MT 725-61-06.
- [SDR SWAA2026032481715](https://openairdocs.org/sdr/SWAA2026032481715.md): Unknown · odor · Mar 20, 2026 · N8535S · Boeing 7378H4 · Air Distribution System
  > ACRID SMELL IN COCKPIT WITH APU RUNNING. CREW HAD MENTIONED THIS SMELL WAS NOT PRESENT UNTIL THE APU WAS RUNNING WHILE TAXIING IN. THEY SEEMED TO OF ALREADY ISOLATED IT TO THE APU FOR IS SAYING THEY COULD DUPLICATE IT WITH THE APU RUNNING AND HOW IT WOULD GO A
- [SDR SWAA2026030275725](https://openairdocs.org/sdr/SWAA2026030275725.md): Girt Bar · detached · Mar 1, 2026 · N8535S · Boeing 7378H4 · Emergency Equipment
  > FWD SVC DOOR SLIDE SHROUD; GIRT BAR CLIP PULLED FROM RIVET. PERFORMED MT 725-61-06-FS TO FACILITATE FASTENER REPLACEMENT ON FWD GIRT BAR CLIP PER SRM 51-40-02. SLIDE REINSTALLED; CHECKS GOOD.
- [SDR SWAA2026021771243](https://openairdocs.org/sdr/SWAA2026021771243.md): Holder · loose · Feb 15, 2026 · N8535S · Boeing 7378H4 · Emergency Equipment
  > FWD SERVICE DOOR GIRT BAR HOLDER LOOSE. TIGHTENED FWD SERVICE DOOR AFT GIRT BAR STOWAGE HOLDER IAW SIP.
- [SDR SWAA2025122654640](https://openairdocs.org/sdr/SWAA2025122654640.md): Battery Pack · inoperative · Dec 22, 2025 · N8535S · Boeing 7378H4 · Emergency Lighting
  > FWD ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE AT L1 DOOR. R & R THE BATTERY PACK AND CHARGER IAW AMM 33-51-06-960-805.
- [SDR SWAA2025122354639](https://openairdocs.org/sdr/SWAA2025122354639.md): Skin · cracked · Dec 22, 2025 · N8535S · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > EXTERNAL POWER RECEPTACLE DOOR SURROUND STRUCTURE IS CRACKED AT BOTTOM OF OPENING. PERFORMED HFEC OF DAMAGE REMOVAL AND INTERIOR STRUCTURE PER NDT PART 6; 51-00-00 PROCEDURE 23 NO DEFECTS NOTED. ACCOMPLISHED PERMANENT REPAIR PER SRM53-10-15-2R-4, REPAIR 4,
- [SDR SWAA2025121143815](https://openairdocs.org/sdr/SWAA2025121143815.md): Sign · detached · Dec 7, 2025 · N8535S · Boeing 7378H4 · Emergency Lighting
  > OVERHEAD ISLE EXIT ROW SIGN PLACARD DETACHED. ATTACHED EMERGENCY EXIT SIGN TO OVERWING SIGN IAW SIP.
- [SDR SWAA2025092417065](https://openairdocs.org/sdr/SWAA2025092417065.md): Hook And Loop · detached · Sep 22, 2025 · N8535S · Boeing 7378H4 · Escape Slide
  > RIGHT AFTER SERVICE OOR EVACUATIONS SLIDE NEED TO BE REINSERTED TO DOOR. INSPECTED SLIDE PACKING; FOUND HOOK AND LOOP STRIPS ON THE GIRT NOT ATTACHED TO THE BACK PAN HOOK AND LOOP STRIP. REATTACHED HOOK AND LOOP STRIP IAW AMM 25-66-01. NO FURTHER DEFECTS NO
- [SDR SWAA2025090812041](https://openairdocs.org/sdr/SWAA2025090812041.md): Girt Bar · out of adjust · Sep 5, 2025 · N8535S · Boeing 7378H4 · Emergency Equipment
  > RIGHT AFT SLIDE GIRT BAR NOT SITTING CORRECTLY<[01] RE ADJUSTED R/H AFT SLIDE GIRT BAR AS REQUIRED PER AMM 25-66-01
- [SDR SWAA2025082908383](https://openairdocs.org/sdr/SWAA2025082908383.md): Lamp · inoperative · Aug 26, 2025 · N8535S · Boeing 7378H4 · Emergency Lighting
  > RT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP RT AFT EMERGENCY OVERWING LIGHT PER AMM 33-51-04. OPS CHECK NORMAL.
- [SDR SWAA2025071590632](https://openairdocs.org/sdr/SWAA2025071590632.md): Battery Pack · inoperative · Jul 12, 2025 · N8535S · Boeing 7378H4 · Emergency Lighting
  > FOUND MULTIPLE EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED R/H FWD AND AFT BATTERY PACK REF AMM 33-51-06. OPS CHECK GOOD
- [SDR SWAA2025052775436](https://openairdocs.org/sdr/SWAA2025052775436.md): Trim Motor · inoperative · May 26, 2025 · N8535S · Boeing 7378H4 · Stabilizer Control System
  > ELEC STAB TRIM INOP. R AND R STAB TRIM MOTOR PER AMM27-41-71. NO DEFECTS NOTED.
- [SDR SWAA2024071612499](https://openairdocs.org/sdr/SWAA2024071612499.md): Flashlight · inoperative · Jul 14, 2024 · N8535S · Boeing 7378H4 · Emergency Equipment
  > AFT GALLEY CAPTAIN SIDE FLSHLIGHT INOP<[01] R/R AFT GALLEY FLASHLIGHT BATTERY ON CAPT SIDE IAW AMM 25-64-00. OPS CHECK GOOD.
- [SDR SWAA2024071611892](https://openairdocs.org/sdr/SWAA2024071611892.md): Flashlight · inoperative · Jul 14, 2024 · N8535S · Boeing 7378H4 · Emergency Equipment
  > AC LEFT AFT FLASHLIGHT INOP<[01] R&R THE A/C LEFT AFT FLASHLIGHT ASSEMBLY AND BATTERY PER AMM 25-64-00.
- [SDR SWAA2024071511527](https://openairdocs.org/sdr/SWAA2024071511527.md): Light · inoperative · Jul 12, 2024 · N8535S · Boeing 7378H4 · Emergency Lighting
  > FO SIDEWALL LIGHTS INOP ROWS 9-13<[01] R&R ROW 14DEF SIDEWALL LIGHT IAW AMM 33-21-00
- [SDR SWAA2024020548299](https://openairdocs.org/sdr/SWAA2024020548299.md): Slide · out of adjust · Feb 2, 2024 · N8535S · Boeing 7378H4 · Escape Slide
  > FORWARD SERVICE DOOR GIRT BAR VERY HARD TO MOVE IN AND OUT OF BRACKETS<[01] REMOVED SLIDE AND ADJUSTED Z FOLD. REINSTALLED. OK FOR SERVICE. REF AMM 25-66-00
- [SDR SWAA2023122936127](https://openairdocs.org/sdr/SWAA2023122936127.md): Door · open · Dec 28, 2023 · N8535S · Boeing 7378H4 · Landing Gear Door Retract Section
  > LANDING GEAR DID NOT COME UP AFTER TAKEOFF; NO OVERWEIGHT LANDING.<[01] FOUND MANUAL EXTENSION DOOR OPEN; SECURED DOOR AND PERFORMED LANDING GEAR EXTENTION AND RETRACTION TEST IAW AMM 32-32-00 NO DEFECTES NOTED.;[02] C/W INSPECTION
- [SDR SWAA2023061659535](https://openairdocs.org/sdr/SWAA2023061659535.md): Battery · inoperative · Jun 15, 2023 · N8535S · Boeing 7378H4 · Emergency Equipment
  > THREE CABIN FLASHLIGHTS INOP 1 FWD AND 2 AFT RT<[01] R&R EMER FLASHLIGHT BATTERY @ FWD I/B AND BOTH AFT F/O SIDE FLASHLIGHT POSITIONS REF AMM 25-64-00. OPS CHECK GOOD. THIS ENTRY WAS DONE REMOTELY DUE TO TECHNICAL ISSUES WITH FAULT IN MXI. PLEASE SEE ATTACHED
- [SDR SWAA2023061558375](https://openairdocs.org/sdr/SWAA2023061558375.md): Lens · loose · Jun 12, 2023 · N8535S · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT LENS FWD OF THE R/H FWD OWE DOOR IS LOOSE.<[01] TIGHTENED SET SCREW ON EMERGENCY LIGHT LENS FWD OF THE R/H FWD OWE DOOR IAW SOPM 20-50-01;[02] CERTIFY ALL WORK WAS DONE AS PER SOPM 20-50-01;[03] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2023061654036](https://openairdocs.org/sdr/SWAA2023061654036.md): Door · out of adjust · May 30, 2023 · N8535S · Boeing 7378H4 · Passenger/Crew Doors
  > FORWARD ENTRY DOOR REQUIRES ADJUSTMENT.<[01] PARTIAL STEP 1-3;[02] TOOL USED; ID:ATS1782; S/N:1118389; DATE:10/2022-10/2023;[03] VERIFIED STEPS 1-3 AND CORRECTIVE ACTION 2
- [SDR SWAA2023061651361](https://openairdocs.org/sdr/SWAA2023061651361.md): Angle · cracked · May 23, 2023 · N8535S · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 13; WL 208.<[01] REMOVED DAMAGED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 13; WL 208 IAW SRM 51-40-02-0G-0;[02] NO CRACK LIMITS FOUND ON SRM; PART REPLACEMENT IAW SRM 51-10-02-0G-0 PAR.9.;[03] RECE
- [SDR SWAA2023061651507](https://openairdocs.org/sdr/SWAA2023061651507.md): Panel · cracked · May 23, 2023 · N8535S · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACKED BREAK PANEL STA 540; BL0-LBL 25; WL 208.<[01] REMOVED DAMAGED BREAK PANEL STA 540; BL0-LBL 25; WL 208 IAW SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW BREAK PANEL STA 540; BL0-RBL 25; WL 208 IAW SRM 51-40-05-0G-0 AND AIPC 53-42-11-66. OK TO INSTALL.
- [SDR SWAA2023061651508](https://openairdocs.org/sdr/SWAA2023061651508.md): Panel · cracked · May 23, 2023 · N8535S · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACKED BREAK PANEL STA 540; BL0-RBL 25; WL 208.<[01] REMOVED DAMAGED BREAK PANEL STA 540; BL0-RBL 25; WL 208 IAW SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW BREAK PANEL STA 540; BL0-RBL 25; WL 208 IAW SRM 51-40-05-0G-0 AND AIPC 53-42-11-66. OK TO INSTALL.
- [SDR SWAA2023061551070](https://openairdocs.org/sdr/SWAA2023061551070.md): Skin · damaged · May 23, 2023 · N8535S · Boeing 7378H4 · Passenger/Crew Doors
  > L1 DOOR AFT INTER SKIN HAS ONE BUSTED RIVET (MARKED WITH RED TAPE)<[01] DAMAGED RIVET ON L1 DOOR AFT INNER SKIN WILL BE REPLACED ON CUSTOMER CARD# TTG8Q00L78LT.;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2023061651060](https://openairdocs.org/sdr/SWAA2023061651060.md): Floor Panel · broken · May 22, 2023 · N8535S · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 221GF HAS A BROKEN TAB.<[01] IDENTIFIED FLOOR PANEL 221GF IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2 <BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR.4 F<BR><BR>DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-6 <BR><BR>REMOVED (2EA) T
- [SDR SWAA2023061651047](https://openairdocs.org/sdr/SWAA2023061651047.md): Floorbeam · corroded · May 22, 2023 · N8535S · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON 947 FLOORBEAM AT RBL 49-50; RBL 24; WL 208.<[01] EVALUATED CORROSION ON BS947 FLOORBEAM AT RBL 49-50 2'X1'ORIGINAL MATERIAL THICKNESS.180 REMAINING MATERIAL THICKNESS.090; RBL 24 1.5'X1.5' REMAINING MATERIAL THICKNESS.120; WL 208 ALL I.A.W SRM
- [SDR SWAA2023061651046](https://openairdocs.org/sdr/SWAA2023061651046.md): Support · corroded · May 22, 2023 · N8535S · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT STA 951; RBL 27; RBL 47-48; WL 208.<[01] VERIFIED APPLICABILITY PER SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1;[02] EVALUATED CORROSION ON FLOOR SUPPORT STA951; RBL 27; RBL 47-48; WL 208 1'X0.600' INCH LOWEST MATERIAL REMOVED IS 0.040' ADJ
- [SDR SWAA2023061651044](https://openairdocs.org/sdr/SWAA2023061651044.md): Floorbeam · corroded · May 22, 2023 · N8535S · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON 947 FLOORBEAM AT LBL 26; LBL 44-46; WL 208.<[01] PARTIAL UPDATE STEP 1;16] FABRICATED REPAIR PARTS ITEM(1) T-CHORD 1EA FROM BAC1505-101045 7075T6 LOT #1522472-1;ITEM(2) ANGLE 2EA FROM BAC1490-2885 7075T62 LOT #1508729-1 AND ITEM 3 STRAPS 2EA FROM
- [SDR SWAA2023061651049](https://openairdocs.org/sdr/SWAA2023061651049.md): Intercostal · corroded · May 22, 2023 · N8535S · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL STA 950; RBL 23; RBL 26; WL 208.<[01] VERIFIED APPLICABILITY PER SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1;[02] EVALUATED CORROSION ON INTERCOSTAL STA 950; RBL 23; RBL 26; WL 208 2 PLACES 1'X1' INCH LOWEST MATERIAL REMOVED IS 0.015' ADJACEN
- [SDR SWAA2023061651050](https://openairdocs.org/sdr/SWAA2023061651050.md): Intercostal · corroded · May 22, 2023 · N8535S · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL STA 949; RBL 49; WL 208.<[01] VERIFIED APPLICABILITY PER SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1;[02] EVALUATED CORROSION ON INTERCOSTAL STA 949; RBL 49; WL 208 PLACES 1'X1' INCH LOWEST MATERIAL REMOVED IS 0.050' ADJACENT TO ORIGINAL MATE
- [SDR SWAA2023061650606](https://openairdocs.org/sdr/SWAA2023061650606.md): Floor Panel · delaminated · May 21, 2023 · N8535S · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 221BF IS DELAMINATED ON PANEL.<[01] IDENTIFIED PANEL 221BF MATERIAL IAW SRM 53-00-50-0I-1 FIG 2; TABLE 2.<BR><BR>FOUND DAMAGE TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4. F.<BR><BR>REPAIR TO BE ACCOMPLISHED IAW SRM 53
- [SDR SWAA2023061650608](https://openairdocs.org/sdr/SWAA2023061650608.md): Floor Panel · delaminated · May 21, 2023 · N8535S · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 221DF HAS DELAMINATION ON PANEL.<[01] IDENTIFIED PANEL 221DF MATERIAL IAW SRM 53-00-50-0I-1 FIG 2; TABLE 2.<BR><BR>FOUND DAMAGE TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4. F.<BR><BR>REPAIR TO BE ACCOMPLISHED IAW SRM
- [SDR SWAA2023061650613](https://openairdocs.org/sdr/SWAA2023061650613.md): Floor Panel · delaminated · May 21, 2023 · N8535S · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR PANEL 241E HAS DELAMINATION ON PANEL.<[01] IDENTIFIED FLOOR PANEL 241E MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6.<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. <BR><BR>DAMAGE IS REPAIRABLE IAW SR

Next page: https://openairdocs.org/aircraft/N8535S/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 = 'N8535S' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8535S/reports

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