# Service difficulty reports: N8534Z

A list on [N8534Z](https://openairdocs.org/aircraft/N8534Z.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 · 74 reports

- [SDR SWAA2026050895380](https://openairdocs.org/sdr/SWAA2026050895380.md): Battery · inoperative · May 5, 2026 · N8534Z · Boeing 7378H4 · Emergency Equipment
  > FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERIES ARE BAD. REMOVED AND REPLACED FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERIES 2 EACH IAW AMM 25-64-00.
- [SDR SWAA2026050895381](https://openairdocs.org/sdr/SWAA2026050895381.md): Battery · inoperative · May 5, 2026 · N8534Z · Boeing 7378H4 · Emergency Equipment
  > AFT FLIGHT ATTENDANT LT INBD EMERGENCY FLASHLIGHT BATTERY ARE BAD. REMOVED AND REPLACED AFT LT INBD EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00.
- [SDR SWAA2026050893604](https://openairdocs.org/sdr/SWAA2026050893604.md): Battery Pack · inoperative · Apr 28, 2026 · N8534Z · Boeing 7378H4 · Emergency Lighting
  > BATTERY BAD ON EMERGENCY LIGHT BATTERY PACK M01694. REMOVED AND REPLACED IAW AMM 33-51-06-960-805. EMERGENCY LIGHTS OPS CHECKED GOOD IAW AMM 33-51-06.
- [SDR SWAA2026051192311](https://openairdocs.org/sdr/SWAA2026051192311.md): Attach Angle · cracked · Apr 23, 2026 · N8534Z · Boeing 7378H4 · Wing, Attach Fittings
  > RIGHT WING TRAILING EDGE PANEL 651FB FWD ATTACH 'L' ANGLE CRACKED.<[01] REMOVED AND REPLACED RIGHT WING T/E PANEL 651FB FWD ATTACH 'L' ANGLE PER SRM 51-40-02; AND IPC 57-50-00-38.;[02] VERIFIED
- [SDR SWAA2026051190480](https://openairdocs.org/sdr/SWAA2026051190480.md): Skin · delaminated · Apr 17, 2026 · N8534Z · Boeing 7378H4 · Trailing Edge Flaps
  > LH OB AFT FLAP; HAS AN AREA OF DELAM IN LOWER TRAILING EDGE WEDGE SKIN AT THE IB END. AREA MEASURES APPROXIMATELY 8.5 X 14 IN SIZE. NEW LEFT WING OUTBOARD AFT FLAP INSTALLED.
- [SDR SWAA2026051187621](https://openairdocs.org/sdr/SWAA2026051187621.md): Web · cracked · Apr 8, 2026 · N8534Z · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENG INBD FAN COWL VERTICAL WEB CRACKED FWD OF ACCESS DOOR 414AR. SEE REFERENCED TASK CARD TTG8Q00S5H9B FOR REPLACEMENT.
- [SDR SWAA2026051187259](https://openairdocs.org/sdr/SWAA2026051187259.md): Attach Angle · cracked · Apr 7, 2026 · N8534Z · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > H.F.E.C. VERIFIED BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED APPROX. LBL 9.<[01] REMOVED ALL FASTENERS ON L/H VAPOR BARRIER ATTACH ANGLE IN FUEL TANK PER SRM 57-10-10-2R-5. REMOVED ALL FASTENERS ON VERTICAL FLANGE OF THE VAPOR BARRIER ATTACH ANGLE FROM APPROX
- [SDR SWAA2026051187260](https://openairdocs.org/sdr/SWAA2026051187260.md): Attach Angle · cracked · Apr 7, 2026 · N8534Z · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > HFEC VERIFIED BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED APPROX. LBL 34. REMOVED AND REPLACED VAPOR BARRIER ATTACH ANGLE AT STA. 663 FROM LBL 5 TO LBL 65 PER SRM 51-40-02; EA-M-24-157-02340 AND DRAWING 111A1000.
- [SDR SWAA2026051187258](https://openairdocs.org/sdr/SWAA2026051187258.md): Attach Angle · cracked · Apr 7, 2026 · N8534Z · Boeing 7378H4 · Wing, Attach Fittings
  > HFEC VERIFIED BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED APPROX. RBL 9. REMOVED ALL FASTENERS ON R/H VERTICAL FLANGE IN REPAIR AREA STA 663 RBL 5 TO RBL 16 IAW SRM 57-10-10-2R-5. CUT AND REMOVED DAMAGED SECTION OF RH VAPOR BARRIER ATTACH ANGLE FROM RBL 5 TO
- [SDR SWAA2026051186630](https://openairdocs.org/sdr/SWAA2026051186630.md): Cotter Pin · corroded · Apr 5, 2026 · N8534Z · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > ON THE LEFT STABILIZER FRONT SPAR LUGS; THE COTTER PINS FOR THE UPPER AND LOWER NUTS HAVE EVIDENCE OF CORROSION. PICTURE ATTACHED.<[01] REPLACED COTTER PINS ON LH HORIZONTAL STBILIZER FRONT SPAR; NO EVIDENCE OF CORROSION.
- [SDR SWAA2026051186627](https://openairdocs.org/sdr/SWAA2026051186627.md): Cotter Pin · corroded · Apr 5, 2026 · N8534Z · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > ON THE RIGHT HAND STABILIZER FRONT SPAR LUGS; THE COTTER PINS FOR THE UPPER AND LOWER NUTS HAVE EVIDENCE OF CORROSION. PICTURE ATTACHED.<[01] RH HORIZONTAL STABILIZER FRONT SPAR LUGS; REMOVED COTTER PINS NO MORE EVIDENCE OF CORROSION. REPLACED COTTER PINS.
- [SDR SWAA2026051185759](https://openairdocs.org/sdr/SWAA2026051185759.md): Skin · debonded · Apr 2, 2026 · N8534Z · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT WING OUTBD AFT FLAP INBD LOWER SKIN HAS A DISBONDED AREA. REMOVED AND REPLACED LEFT OUTBOARD AFT FLAP PER AMM 27-51-22.
- [SDR SWAA2025090508443](https://openairdocs.org/sdr/SWAA2025090508443.md): Floor Panel · peeling · Aug 26, 2025 · N8534Z · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 231ZF HAS PEELING STRANDS. NEW FLOOR PANEL INSTALLED ON TTG8Q014T1H8.
- [SDR SWAA2025090408442](https://openairdocs.org/sdr/SWAA2025090408442.md): Floor Panel · peeling · Aug 26, 2025 · N8534Z · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 231FF HAS PEELING STRANDS. FABRICATED 231FF FLOORBOARD PANEL IAW B737-800 SRM 53-00-50-2R-0 GENERAL REPAIR REV 85 AND PER BAC DWG 143A5810 SHT 515 REV: A.
- [SDR SWAA2025090408438](https://openairdocs.org/sdr/SWAA2025090408438.md): Floor Panel · peeling · Aug 26, 2025 · N8534Z · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 232SF HAS PEELING STRANDS. FABRICATED 232SF FLOORBOARD PANEL IAW B737-800 SRM 53-00-50-2R-0 GENERAL REPAIR AND PER DWG 144A5810 SHT 258 REV: -. INSPECTED PER SRM 53-00-50-2R-0-B00275 AND BAC DWG 144A5810 SHT 258 REV-.
- [SDR SWAA2025090408445](https://openairdocs.org/sdr/SWAA2025090408445.md): Floor Panel · pulled · Aug 26, 2025 · N8534Z · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241DF HAS PEELING STRANDS. FABRICATED 241DF FLOOR PANEL IAW B737-800 SRM 53-00-50-2R-0 GENERAL REPAIR REV 85 AND SWA TSR-2025007582. INSPECTED PER SRM 53-00-50-2R-0-B00275 AND SWA TSR-2025007582.
- [SDR SWAA2025090408444](https://openairdocs.org/sdr/SWAA2025090408444.md): Floor Panel · peeling · Aug 26, 2025 · N8534Z · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241AF HAS PEELING STRANDS. FABRICATED 241AF FLOORBOARD PANEL IAW B737-800 SRM 53-00-50-2R-0 GENERAL REPAIR REV 85 AND SWA TSR-2025007582. INSPECTED PER SRM 53-00-50-2R-0-B00275 AND SWA TSR-2025007582.
- [SDR SWAA2025090408439](https://openairdocs.org/sdr/SWAA2025090408439.md): Floor Panel · pulled · Aug 26, 2025 · N8534Z · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241GF HAS PEELING STRANDS. FABRICATED 241GF FLOORBOARD PANEL IAW B737-800 SRM 53-00-50-2R-0 GENERAL REPAIR REV 85 AND SWA TSR-2025007582. INSPECTED PER SRM 53-00-50-2R-0-B00275 AND SWA TSR-2025007582.
- [SDR SWAA2025090408440](https://openairdocs.org/sdr/SWAA2025090408440.md): Floor Panel · peeling · Aug 26, 2025 · N8534Z · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241MF HAS PEELING STRANDS. FABRICATED 241MF FLOORBOARD PANEL IAW B737-800 SRM 53-00-50-2R-0 GENERAL REPAIR REV 85 AND SWA TSR-2025007582. INSPECTED PER SRM 53-00-50-2R-0-B00275 AND SWA TSR-202500782.
- [SDR SWAA2025090408441](https://openairdocs.org/sdr/SWAA2025090408441.md): Floor Panel · peeling · Aug 26, 2025 · N8534Z · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 231RF HAS PEELING STRANDS. FABRICATED 231RF FLOOR PANEL IAW B737-800 SRM 53-00-50-2R-0 GENERAL REPAIR REV 85 AND SWA TSR-2025007582. INSPECTED PER SRM 53-00-50-2R-0-B00275 AND SWA TSR-2025007582.
- [SDR SWAA2025090408067](https://openairdocs.org/sdr/SWAA2025090408067.md): Doubler · cracked · Aug 25, 2025 · N8534Z · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > EGPR DOOR LOWER CUTOUT SURROUND DOUBLER IS CRACKED. ACCOMPLISHED REPAIR ON EGPR DOOR LOWER CUTOUT SURROUND DOUBLER IAW B737-800 SRM 53-10-15-2R-4. INSPECTED PER [SRM 53-10-15-2R-4-B00449, REPAIR 4.
- [SDR SWAA2025090807558](https://openairdocs.org/sdr/SWAA2025090807558.md): Handle · loose · Aug 23, 2025 · N8534Z · Boeing 7378H4 · Passenger/Crew Doors
  > CR RR L1 DOOR ASSIST HANDLE NEEDS SECURED. SECURED L1 DOOR ASSIST HANDLE IAW AMM SUBTASK 52-11-31-020-011.
- [SDR SWAA2025090407553](https://openairdocs.org/sdr/SWAA2025090407553.md): Handle · unsecure · Aug 23, 2025 · N8534Z · Boeing 7378H4 · Passenger/Crew Doors
  > L2 DOOR ASSIST HANDLE NEEDS SECURED CR RR L2 DOOR ASSIST HANDLE NEEDS SECURED. SECURED L2 DOOR ASSIST HANDLE IAW B737-800 AMM SUBTASK 52-13-31-020-008.
- [SDR SWAA2025090407559](https://openairdocs.org/sdr/SWAA2025090407559.md): Handle · unsecure · Aug 23, 2025 · N8534Z · Boeing 7378H4 · Service Doors
  > R1 DOOR ASSIST HANDLE NEEDS SECURED CR RR R1 DOOR ASSIST HANDLE NEEDS SECURED. SECURED R1 DOOR ASSIST HANDLE IAW B737-800 AMM 52-41-31.
- [SDR SWAA2025070788055](https://openairdocs.org/sdr/SWAA2025070788055.md): Flashlight · no test · Jul 3, 2025 · N8534Z · Boeing 7378H4 · Emergency Equipment
  > FWD INBD FA FLASHLIGHT WON'T TEST. OK TO CONTINUE PER MEL 25-12-01; SP1B. R& R FWD. FLASHLIGHT (INBD) IAW MM 25-64-00.
- [SDR SWAA2025031705710](https://openairdocs.org/sdr/SWAA2025031705710.md): Battery · inoperative · Mar 15, 2025 · N8534Z · Boeing 7378H4 · Emergency Equipment
  > AFT OUTBOARD FLASHLIGHT WILL NOT TEST <[01]. 05 - OK TO CONTINUE PER [MEL 25-12-01; EMERGENCY FLASHLIGHT HOLDERS / FLASHLIGHTS - CABIN]. WITH SP __1B_______ AND AUTHORIZATION NUMBER _242483______; [02] R&R?D AFT RH OB FLASHLIGHT BATTERY. & RE-SEALED IAW AMM 25
- [SDR SWAA2025010783093](https://openairdocs.org/sdr/SWAA2025010783093.md): Battery Pack · inoperative · Jan 5, 2025 · N8534Z · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT BATTERY PACK M1670 WILL NOT CHARGE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK GOOD.
- [SDR SWAA2025010783090](https://openairdocs.org/sdr/SWAA2025010783090.md): Battery Pack · inoperative · Jan 5, 2025 · N8534Z · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT BATTERY PACK M1671 WILL NOT CHARGE<[01] REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK GOOD.
- [SDR SWAA2025010783091](https://openairdocs.org/sdr/SWAA2025010783091.md): Battery Pack · inoperative · Jan 5, 2025 · N8534Z · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT BATTERY PACK M1672 WILL NOT CHARGE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK AT POSITION M1672 IAW AMM 33-51-06-960-805. OPS CHECK GOOD.
- [SDR SWAA2025010783094](https://openairdocs.org/sdr/SWAA2025010783094.md): Battery Pack · inoperative · Jan 5, 2025 · N8534Z · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT BATTERY PACK M1673 WILL NOT CHARGE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK AT POSITION M1673 IAW AMM 33-51-06-960-805. OPS CHECK GOOD.
- [SDR SWAA2025010783092](https://openairdocs.org/sdr/SWAA2025010783092.md): Battery Pack · inoperative · Jan 5, 2025 · N8534Z · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT BATTERY PACK M1676 WILL NOT CHARGE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK GOOD.
- [SDR SWAA2025010783095](https://openairdocs.org/sdr/SWAA2025010783095.md): Battery Pack · inoperative · Jan 5, 2025 · N8534Z · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT BATTERY PACK M2335 WILL NOT CHARGE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK GOOD.
- [SDR SWAA2024101146424](https://openairdocs.org/sdr/SWAA2024101146424.md): Flashlight · inoperative · Oct 8, 2024 · N8534Z · Boeing 7378H4 · Emergency Equipment
  > FWD FLIGHT ATTENDANT FLASHLIGHT INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 25-64-00-900-806-NG (FLASHLIGHT BATTERY REPLACEMENT - PERMANENT)]
- [SDR SWAA2024072516315](https://openairdocs.org/sdr/SWAA2024072516315.md): Cover · loose · Jul 24, 2024 · N8534Z · Boeing 7378H4 · Emergency Equipment
  > 14A EMERGENCY EXIT DOOR RESTOW STRAP COVER BROKEN<[01] SECURED; REINSTALLED LOOSE COVER PER SIP
- [SDR SWAA2024021251410](https://openairdocs.org/sdr/SWAA2024021251410.md): Flashlight · out of position · Feb 11, 2024 · N8534Z · Boeing 7378H4 · Emergency Equipment
  > AFT RH EMERGENCY FLASHLIGHT WILL NOT TEST.<[01] RESEAT FLASHLIGHT AND RESEALED PER AMM. 33.55.00. OPS NORMAL.
- [SDR SWAA2023091198759](https://openairdocs.org/sdr/SWAA2023091198759.md): Slide · out of limits · Sep 9, 2023 · N8534Z · Boeing 7378H4 · Escape Slide
  > L2 DOOR SLIDE PRESSURE IN THE RED<[01] REMOVED AE SLIDE PER AMM 25-66-00 & MT 725-61-06;[02] R & R L2 DOOR SLIDE PER AMM 25-66-00 AND MT 725-61-06
- [SDR SWAA2023051641882](https://openairdocs.org/sdr/SWAA2023051641882.md): Web · cracked · Apr 26, 2023 · N8534Z · Boeing 7378H4 · Wing Miscellaneous Structure
  > THE LH UPPER FIXED TE PANEL TRANSVERSE WEB IS CRACKED AT APPROX ORSS 280.<[01] UPDATED MEASUREMENT SECTION; REMOVED CRACKED TRANSVERSE WEB LEFT HAND WING UPPER FIXED TRAILING EDGE PANEL AND INSTALLED NEW TRANSVERSE WEB PART NUMBER 115A2156-7 SAME LOCATION ABOV
- [SDR SWAA2023051530765](https://openairdocs.org/sdr/SWAA2023051530765.md): Panel · cracked · Apr 24, 2023 · N8534Z · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CRACKED BREAK PANEL STA 540; BL0- LBL 25; WL 208.<[01] UPDATED MEASUREMENTS. ON BS 540; BL0-LBL25; WL208; BREAK PANEL WILL BE A PART REPLACEMENT IAW SRM 51-10-02 STEP 9. REMOVED BREAK PANEL; AND RECEIVED A NEW BREAK PANEL; LOCATED HOLES; DRILLED; AND DEBURRED
- [SDR SWAA2023051530761](https://openairdocs.org/sdr/SWAA2023051530761.md): Support Angle · broken · Apr 24, 2023 · N8534Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > BROKEN WIRE SUPPORT ANGLE BS867 AT STR. 3R.<[01] REMOVED AND REPLACED WIRE SUPPORT ANGLE BS867 AT STR 3R PER SRM 51-40-02-0G-0 REF DWG 146A7901;[02] VERIFIED CORRETIVE ACTION 1.;[03] WORKSCOPE IS COMPLETE
- [SDR SWAA2023051630042](https://openairdocs.org/sdr/SWAA2023051630042.md): Fitting · corroded · Apr 21, 2023 · N8534Z · Boeing 7378H4 · Passenger/Crew Doors
  > CORROSION ON FWD ENRY DOOR (FWD) GIRT BAR FITTING SUPPORT UPPER SURFACE; STA 312; STA 314 LBL 54; WL 208.<[01] AFTER FURTHER INVESTIGATION NO CORROSION FOUND ON FWD ENTRY DOOR (FWD) GIRT BAR FITTING; ONLY BARE METAL APPLIED CHEMICAL CONVERSION COAT AND PRIMED
- [SDR SWAA2023051630025](https://openairdocs.org/sdr/SWAA2023051630025.md): Intercostal · corroded · Apr 21, 2023 · N8534Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL UPPER SURFACE STA 949; LBL 23; WL 208.<[01] EVALUATED DAMAGE ON INTERCOSTAL UPPER SURFACE STA 949; LBL 23; WL 208.AND FOUND TO BE OUT LIMITS DUE TO LOSS OF MATERIAL EXCEED LIMITS GIVEN ON SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 ORIGINAL M
- [SDR SWAA2023051630030](https://openairdocs.org/sdr/SWAA2023051630030.md): Floorbeam · corroded · Apr 21, 2023 · N8534Z · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON 947 FLOORBEAM UPPER SURFACE AT LBL 23; LBL 49; LBL 52; WL 208.<[01] VERIFIED THE APPLICABILY OF SRM 53-70-51-1A-1;[02] EVALUATED CORROSION ON 947 FLOORBEAM UPPER SURFACE AT LBL 23; LBL 49; LBL 52 AND FOUND TO BE OUT LIMITS DUE TO LOSS OF MATERIAL
- [SDR SWAA2023051630011](https://openairdocs.org/sdr/SWAA2023051630011.md): Floorbeam · corroded · Apr 21, 2023 · N8534Z · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON 947 FLOORBEAM UPPER SURFACE AT RBL 27; WL 208.<OUT LIMITS DUE TO LOSS OF MATERIAL EXCEED LIMITS GIVEN PER SRM LBL52 0.750'X0.600' ORIGINAL MATERIAL THICKNESS IS 0.180' REMAINING MATERIAL THICKNESS IS 0.110' ALL I.A.W SRM 53-70-51-1A-1REMOVED ADJAC
- [SDR SWAA2023051630038](https://openairdocs.org/sdr/SWAA2023051630038.md): Attach Angle · cracked · Apr 21, 2023 · N8534Z · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-STA 400; LBL 13; WL 208.<[01] REMOVED INTERCOSTAL UPPER ATTACH ANGLE STA 380-STA 400; LBL 13; WL 208. PER. SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL UPPER ATTACH ANGLE BS380-400 LBL3 WL 208 PER S
- [SDR SWAA2023051530022](https://openairdocs.org/sdr/SWAA2023051530022.md): Intercostal · corroded · Apr 21, 2023 · N8534Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL UPPER SURFACE STA 949; RBL 26; WL 208.<[01] EVALUATED DAMAGE ON INTERCOSTAL UPPER SURFACE STA 949; LBL 49; WL 208.AND FOUND TO BE OUT LIMITS DUE TO LOSS OF MATERIAL EXCEED LIMITS GIVEN ON SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 ORIGINAL M
- [SDR SWAA2023051530023](https://openairdocs.org/sdr/SWAA2023051530023.md): Intercostal · corroded · Apr 21, 2023 · N8534Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL UPPER SURFACE STA 949; LBL 49; WL 208.<[01] EVALUATED DAMAGE ON INTERCOSTAL UPPER SURFACE STA 949; LBL 49; WL 208.AND FOUND TO BE OUT LIMITS DUE TO LOSS OF MATERIAL EXCEED LIMITS GIVEN ON SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 ORIGINAL M
- [SDR SWAA2023051629264](https://openairdocs.org/sdr/SWAA2023051629264.md): Vapor Barrier · cracked · Apr 19, 2023 · N8534Z · Boeing 7378H4 · Fuselage Main, Bulkhead
  > R/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL34 WL167.68<REMOVED DAMAGED SECTION OF VAPOR BARRIER UPPER ATTACH ANGLE BS 663 RBL38-RBL65 AND WL 167.68 IAW SRM 57-10-10-2R-5;[07] REMOVED DAMAGED SECTION OF VAPOR BARRIER UPPER ATTACH ANGLE AND PERF
- [SDR SWAA2023051728740](https://openairdocs.org/sdr/SWAA2023051728740.md): Door · out of adjust · Apr 18, 2023 · N8534Z · Boeing 7378H4 · Service Doors
  > FWD SERVICE DOOR REQUIRES ADJUSTMENT.<[01] ADJUSTED DORWARD SERVICE DOOR PER AMM 52-41-00-820-801 STEPS 2.G.(1);(2);(3)(A;C); I; L; N; Q; R. PERFORMED FORWARD SERVICE DOOR SYSTEM TEST PER AMM 52-41-00-700-801; PERFORMED FORWARD SERVICE DOOR INDICATION SENSOR A
- [SDR SWAA2023051728734](https://openairdocs.org/sdr/SWAA2023051728734.md): Fastener · sheared · Apr 18, 2023 · N8534Z · Boeing 7378H4 · Emergency Equipment
  > FWD ENTRY DOOR SLIDE COVER AFT GIRT BAR FITTING BRACKET HAS SHEARED FASTENER.<[01] REMOVED AND REPLACED FWD ENTRY DOOR SLIDE COVER AFT GIRT BAR FITTING BRACKET FASTENERS PER SRM 51-40-02-0G-0;[02] VERIFIED
- [SDR SWAA2023051728476](https://openairdocs.org/sdr/SWAA2023051728476.md): Panel · cracked · Apr 17, 2023 · N8534Z · Boeing 7378H4 · Wing, Control Surfaces
  > AT FWD O/B SIDE #3 FLAP TRACK AFT FAIRING PANEL (532CL) CRACKED CORRECTION TO PANEL: (542CL)<[01] REMOVED AND REPLACED AT FWD O/B SIDE #3 FLAP TRACK AFT FAIRING PANEL (532CL) IAW AMM 20-50-11-201-NG;[02] UPDATED MEASUREMENT TABLE;[03] PANEL REPLACED PER SRM 51

Next page: https://openairdocs.org/aircraft/N8534Z/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 = 'N8534Z' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8534Z/reports

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