# Service difficulty reports: N8540V

A list on [N8540V](https://openairdocs.org/aircraft/N8540V.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 · 79 reports

- [SDR SWAA2026061107658](https://openairdocs.org/sdr/SWAA2026061107658.md): Shield · corroded · May 30, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > IN THE AFT CARGO BAY JUST FWD OF THE ENTRY DOOR. THE FLOOR STRUCTURE SHIELD ASSEMBLY HAS AREAS OF UPPER SURFACE CORROSION. REMOVED AFT CARGO TRANS ANGLE SHIELD PER SRM 51-40-02. INSTALLED FASTENER IAW SRM 51-40-02. APPLIED CORROSION INHIBITING COMPOUND I
- [SDR SWAA2026061106481](https://openairdocs.org/sdr/SWAA2026061106481.md): Frame · damaged · May 26, 2026 · N8540V · Boeing 7378H4 · Fuselage Main, Frame
  > FWD CARGO LT SIDE FRAME AT BS 500D, STR 25L HAS ELONGATED NR 13 HOLE.THE HOLE IS MEASURED 0.187 WIDE BY 0.262 LENGTH. WORK ACCOMPLISHED PER EA 26-153-01419.
- [SDR SWAA2026061106480](https://openairdocs.org/sdr/SWAA2026061106480.md): Frame · damaged · May 26, 2026 · N8540V · Boeing 7378H4 · Fuselage Main, Frame
  > FWD CARGO LT SIDE FRAME AT BS 500C, STR 25L HAS ELONGATED NR 13 HOLE. THE HOLE SIZE IS MEASURED 0.187 WIDE BY 0.277 LENGTH. WORK IS ACCOMPLISHED IAW EA 26-153-01416.
- [SDR SWAA2026061105657](https://openairdocs.org/sdr/SWAA2026061105657.md): Angle · cracked · May 23, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT BS 867, LBL 13, ANGLE BRACKET FOR PANEL 141QW PILLAR IS CRACKED. REMOVED AND REPLACED AFT CARGO COMPARTMENT BS 867, LBL 13.
- [SDR SWAA2026061104577](https://openairdocs.org/sdr/SWAA2026061104577.md): Lamp · inoperative · May 19, 2026 · N8540V · Boeing 7378H4 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT BY AFT LEFT SERVICE DOOR IS INOPERATIVE. REPLACED THE LAMPS EXTERIOR EMERGENCY LIGHT BY AFT LEFT SERVICE DOOR IAW AMM 33-51-04. OPS CHECKED GOOD.
- [SDR SWAA2026061104576](https://openairdocs.org/sdr/SWAA2026061104576.md): Lamp · inoperative · May 19, 2026 · N8540V · Boeing 7378H4 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT BY FWD SERVICE DOOR IS INOPERATIVE. REPLACED THE LAMPS EXTERIOR EMERGENCY LIGHT BY FORWARD SERVICE DOOR IAW AMM 33-51-04. OPS CHECKED GOOD.
- [SDR SWAA2026061104505](https://openairdocs.org/sdr/SWAA2026061104505.md): Fairing · cracked · May 19, 2026 · N8540V · Boeing 7378H4 · Trailing Edge Flaps
  > NR 6 CANOE FAIRING CRACKED. INSIDE CENTER BOTTOM. REPAIRED PER E/A M 21-157-01063. INSPECTION C/W FOR CORRECTIVE ACTION NR 1. REPAIRED IAW E/A M 21-157-01063.
- [SDR SWAA2026061004183](https://openairdocs.org/sdr/SWAA2026061004183.md): Baffle · cracked · May 19, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO RT TRANSITION ANGLE SUPPORT BAFFLE BETWEEN STA.500G TO 500H IS CRACKED. REMOVED AND REPLACED NEW FWD CARGO R/H TRANSITION ANGLE SUPPORT BAFFLE BETWEEN BS 500G TO 500H PER SRM 51-40-02.
- [SDR SWAA2026061103713](https://openairdocs.org/sdr/SWAA2026061103713.md): Battery Pack · inoperative · May 17, 2026 · N8540V · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS OVER LEFT FWD AND AFT OVERWING EXITS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT BS 659L IAW MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD IAW MM 33-51-06.
- [SDR SWAA2026061103387](https://openairdocs.org/sdr/SWAA2026061103387.md): Intercostal · cracked · May 15, 2026 · N8540V · Boeing 7378H4 · Wing Miscellaneous Structure
  > BRACKET INBOARD OF THE INBD RT WING DEFLECTION CONTROL RIB INBD INTERCOSTAL IS CRACKED. REMOVED AND REPLACED THE BRACKET ANGLE IAW SRM 5-40-02.
- [SDR SWAA2026061197975](https://openairdocs.org/sdr/SWAA2026061197975.md): Support · corroded · May 13, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO AFT BULKHEAD SUPPORT LT LOWER CURVED RAIL IS CORRODED. REMOVED AFTER BULKHEAD LH SUPPORT IAW SRM 51-40-02. LOCATED; DRILLED AND INSTALLED AFT BULKHEAD LH SUPPORT ANGLE.
- [SDR SWAA2026061197596](https://openairdocs.org/sdr/SWAA2026061197596.md): Support Angle · cracked · May 12, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO RT TRANSITION ANGLE SUPPORT BAFFLE BETWEEN STA 500D TO STA 500E IS CRACKED. REMOVED AND REPLACED FORWARD CARGO RH TRANSITION ANGLE SUPPORT BAFFLE BETWEEN STA 500D TO STA 500E PER SRM 51-40-02.
- [SDR SWAA2026061197971](https://openairdocs.org/sdr/SWAA2026061197971.md): Support Angle · cracked · May 12, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO RT TRANSITION ANGLE SUPPORT BAFFLE BETWEEN STA.500C TO 500D IS CRACKED. REMOVED AND REPLACED FORWARD CARGO RH TRANSITION ANGLE SUPPORT BAFFLE BETWEEN BS 500C TO 500D IAW SRM 51-40-02.
- [SDR SWAA2026061197309](https://openairdocs.org/sdr/SWAA2026061197309.md): Angle · corroded · May 11, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO R/H TRANSITION ANGLE HAS CORROSION AROUND SEVERAL FASTENER HOLES FROM BS 500B - BS 500I. WORK ACCOMPLISHED ON TASK CARD TTG8Q01C4A72 PER SRM 51-40-02.
- [SDR SWAA2026061197312](https://openairdocs.org/sdr/SWAA2026061197312.md): Angle · corroded · May 11, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO LT TRANSITION ANGLE HAS CORROSION AROUND SEVERAL FASTENER HOLES FROM BS 500C - BS 500I. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-00-53. REMOVED TRANSITION ANGLE FROM BS 500C+12 TO BS 500I IAW SRM 53-00-53-2R-5. FABRICATED REPAIR PARTS IAW SR
- [SDR SWAA2026061197112](https://openairdocs.org/sdr/SWAA2026061197112.md): Seal · cracked · May 10, 2026 · N8540V · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STAB FWD UPPER SLIDER SEAL IS CRACKED. REMOVED RT STAB TO BODY UPPR FRONT SPAR SLIDING SEAL IAW AMM 53-31-31. INSTALLED SLIDING SEAL FITTING ASSY TO SLIDING SEAL WITH FASTENERS IAW SRM 51-40-02. INSTALLED RT STAB TO BODY UPPR FRONT SPAR S
- [SDR SWAA2026061197115](https://openairdocs.org/sdr/SWAA2026061197115.md): Seal · cracked · May 10, 2026 · N8540V · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB FWD UPPER SLIDER SEAL IS CRACKED. REMOVED LT STAB TO BODY UPPER FRONT SPAR SLIDING SEAL IAW AMM 53-31-31. INSTALLED SLIDING SEAL FITTING ASSY TO SLIDING SEAL WITH FASTENERS IAW SRM 51-40-02. REMOVED LH STAB TO BODY UPPR FRONT SPAR SLI
- [SDR SWAA2026061197111](https://openairdocs.org/sdr/SWAA2026061197111.md): Rod End · corroded · May 9, 2026 · N8540V · Boeing 7378H4 · Ailerons
  > THE RIGHT WING AILERON TAB ATTACH (HINGE) ROD ENDS ALL HAVE EVIDENCE OF EXTERNAL SURFACE CORROSION.. REMOVED RT AILERON TRIM TAB PER AMM 27-11-21. R & R RIGHT WING AILERON TAB ATTACH ROD ENDS IAW CMM 57-50-26. REINSTALLED RT AILERON TRIM TAB IAW AMM 27-11-
- [SDR SWAA2026061196793](https://openairdocs.org/sdr/SWAA2026061196793.md): Rib · cracked · May 8, 2026 · N8540V · Boeing 7378H4 · Trailing Edge Flaps
  > FOUND CRACK INDICATION BY HFEC NDT PART 6, 51-00-00 PROCEDURE 23 OF LT WING TRAILING EDGE RIB WBL 413.18. IAW EA 26-157-01239-WIP1, STEP 7. DAMAGE LOCATION 1. LENGTH APPROXIMATELY.1'. REPAIRED PER EA 26-157-01239.
- [SDR SWAA2026061097969](https://openairdocs.org/sdr/SWAA2026061097969.md): Angle · corroded · May 8, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT, LT TRANSITION ANGLE, LBL 21, BS 727I - 847 HAD AREAS OF CORRSOSION. BLENDED AREAS OF CORROSION. BLENDS FOUND TO OUT OF LIMITS ALL IAW SRM 53-00-53-1A-2. BLENDED AREAS OF CORROSION ON AFT CARGO COMPARTMENT LT TRANSITION ANGLE FABRICAT
- [SDR SWAA2026061196057](https://openairdocs.org/sdr/SWAA2026061196057.md): Support · corroded · May 7, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO AFT BULKHEAD LOWER SUPPORT STRUCTURE AT BS 500I, LBL 24, HAS CORROSION. REMOVED AFT BULKHEAD LOWER SUPPORT ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED NEW SUPPORT ANGLE. SRM 51-40-02. INSTALLED NEW SUPPORT ANGLE. SRM 51-21-02.
- [SDR SWAA2026061103710](https://openairdocs.org/sdr/SWAA2026061103710.md): Seal · worn · May 7, 2026 · N8540V · Boeing 7378H4 · Fuselage Main, Structure
  > RIGHT MAIN WHEEL WELL BLADE SEALS (8) ON THE AFT SIDE ARE WORN. REMOVED AND REPLACED RT MAIN WHEEL WELL, WORN BLADE SEALS AS REQUIRED. WORK PERFORMED IAW AMM 32-12-12-401-NG.
- [SDR SWAA2026050494327](https://openairdocs.org/sdr/SWAA2026050494327.md): Control Valve · leaking · Apr 29, 2026 · N8540V · Boeing 7378H4 · Aircraft Fuel System
  > NR 1 ENGINE FUEL LEAK AFTER PUSHBACK. CONTINUE AFTER 5 MINUTES. REMOVED AND REPLACED NR 1 ENGINE HPTACC IAW AMM 75-21-01; PERFORMED IDLE TEST 3A AND ACTUATORS TEST. TEST PASSED AND NO LEAKS FOUND. REF MT# 727-PRD-01-03.
- [SDR SWAA2026042793343](https://openairdocs.org/sdr/SWAA2026042793343.md): Drive System · out of adjust · Apr 23, 2026 · N8540V · Boeing 7378H4 · Trailing Edge Flap Control System
  > AFTER LANDING ROLL WHEN FLAPS WERE RETRACTED LEFT GUAGE INDICATOR STOPPED AT 5 RIGHT INDICATOR STOPPED AT 2.<[01] FOUND LH FLAP TORQUE TUBE SUPPORT P/N: 256A3750-3 DAMAGED. REMOVED LH FLAP TORQUE TUBE SUPPORT P/N: 256A3750-3 PER. AMM 27-51-59.;[02] INSTALLED L
- [SDR SWAA2026042792133](https://openairdocs.org/sdr/SWAA2026042792133.md): Torque Tube · damaged · Apr 23, 2026 · N8540V · Boeing 7378H4 · Trailing Edge Flap Control System
  > AFTER LANDING ROLL WHEN FLAPS WERE RETRACTED LEFT GUAGE INDICATOR STOPPED AT 5 RIGHT INDICATOR STOPPED AT 2.<[01] FOUND LH FLAP TORQUE TUBE SUPPORT P/N: 256A3750-3 DAMAGED. REMOVED LH FLAP TORQUE TUBE SUPPORT P/N: 256A3750-3 PER. AMM 27-51-59.;[02] INSTALLED L
- [SDR SWAA2025120943954](https://openairdocs.org/sdr/SWAA2025120943954.md): Slide · dislodged · Dec 8, 2025 · N8540V · Boeing 7378H4 · Escape Slide
  > R1 DOOR SLIDE DISLODGED. INSTALLED R1 DOOR ESCAPE SLIDE IAW MT 725-61-06 AND AMM 25-66-01.
- [SDR SWAA2025120141084](https://openairdocs.org/sdr/SWAA2025120141084.md): Unknown · odor · Nov 30, 2025 · N8540V · Boeing 7378H4 · Air Distribution System
  > LIGHT ELECTRICAL ODOR DETECTED IN THE AFT GALLEY, FIRST OFFIER SIDE. GASPER VENT IN AFT GALLEY SEEMED TO HAVE AN ODOR. NO ISSUES OR ODORS DETECTED NEAR COFFEE POT. EARLY ONSET ODOR SEEMED RUBBER IN NATURE. USED FIM 21-00 TASK 806, AS A GUIDE FOR T/S, INSPEC
- [SDR SWAA2025103029074](https://openairdocs.org/sdr/SWAA2025103029074.md): Flashlight · not seated · Oct 27, 2025 · N8540V · Boeing 7378H4 · Emergency Equipment
  > FWD GALLEY FLASHLIGHT GREEN LIGHT NOT ILLUMINATED. RESEATED FWD GALLEY FLASHLIGHT AND OPS CHK NML PER AMM 25-64-00. APPLIED TAPER SEAL.
- [SDR SWAA2025102726831](https://openairdocs.org/sdr/SWAA2025102726831.md): Battery Pack · inoperative · Oct 22, 2025 · N8540V · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE AT ROW 7ABC AND AFT RH GALLEY. R & R EMERGENCY LIGHT BATTERY PACKS AT ROW 7ABC AND RH AFT GALLEY IAW AMM 33-51-06. OPS CHECK OK.;
- [SDR SWAA2025091614140](https://openairdocs.org/sdr/SWAA2025091614140.md): Flashlight · inoperative · Sep 13, 2025 · N8540V · Boeing 7378H4 · Emergency Equipment
  > FWD FLASHLIGHT INOPERATIVE. REPLACED FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 25-64-00; OPS CHECKED GOOD.
- [SDR SWAA2025090811243](https://openairdocs.org/sdr/SWAA2025090811243.md): Battery · inoperative · Sep 4, 2025 · N8540V · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS FROM LEFT O/W EXIT TO ROW 23 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER IAW AMM 33-51-06
- [SDR SWAA2025090812526](https://openairdocs.org/sdr/SWAA2025090812526.md): Charger · inoperative · Sep 4, 2025 · N8540V · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS FROM LEFT O/W EXIT TO ROW 23 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER IAW AMM 33-51-06
- [SDR SWAA2025062484251](https://openairdocs.org/sdr/SWAA2025062484251.md): Girt Bar · loose · Jun 21, 2025 · N8540V · Boeing 7378H4 · Emergency Equipment
  > GIRT BAR RETAINING BRACKET ON L1 DOOR LOOSE. INSTALLED NEW RIVET IN GIRT BAR HOLDER IN ACCORDANCE WITH SRM 51-40-02.
- [SDR SWAA2025060677663](https://openairdocs.org/sdr/SWAA2025060677663.md): Cabin Air Sys · odor · Jun 2, 2025 · N8540V · Boeing 7378H4 · Cabin Cooling System
  > LEFT PACK TRIP OFF LIGHT ILLUMINATED AT GATE FOLLOWED BY A HOT SMELL AND WHINNING NOISE <[01]. OK TO CONTINUE PER MEL 21-1-01; SP-1 AUTH# 256726; [02] 01 - REMOVED AND REPLACED PER [AMM 21-51-04-401 CONFIG 1-NG (AIR CYCLE MACHINE (ACM) - REMOVAL/INSTALLATION
- [SDR SWAA2025052774283](https://openairdocs.org/sdr/SWAA2025052774283.md): Battery Pack · inoperative · May 23, 2025 · N8540V · Boeing 7378H4 · Emergency Lighting
  > AISLE EMERGENCY LIGHTS BETWEEN STA 500B AND 578 RIGHT SIDE ARE INOP<[01] REPLACED BATTERY CHARGER AND BATTERY PACK M1676 IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 33-51-06 AND WDM 33-51-12. OPS CHECKED GOOD.
- [SDR SWAA2025050266215](https://openairdocs.org/sdr/SWAA2025050266215.md): Flashlight · inoperative · May 1, 2025 · N8540V · Boeing 7378H4 · Emergency Equipment
  > FWD CABIN EMERGENCY FLASHLIGHT INOP.<[01] FLASHLIGHT CAME LOOSE FROM MOUNT. RESECURED AND REPLACED SECURITY SEAL PER AMM 25-64-00
- [SDR SWAA2024121777613](https://openairdocs.org/sdr/SWAA2024121777613.md): Battery Pack · inoperative · Dec 15, 2024 · N8540V · Boeing 7378H4 · Emergency Lighting
  > FWD SVC DOOR EMERGENCY LIGHTS INOP ON INTERIOR CEILING AND OUTSIDE OF DOOR.<[01] R/R?D M2816 EMERGENCY LIGHTS BATTERY PACK FOR FWD SVC DOOR EMERGENCY LIGHTS REF AMM 33-51-06. OPS CHECK NORMAL.
- [SDR SWAA2024050983615](https://openairdocs.org/sdr/SWAA2024050983615.md): Battery Pack · inoperative · May 8, 2024 · N8540V · Boeing 7378H4 · Emergency Lighting
  > FWD ENTRY DOOR EMERGENCY LIGHT AND FWD GALLEY EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED FWD ENTRY DOOR EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06
- [SDR SWAA2024041774868](https://openairdocs.org/sdr/SWAA2024041774868.md): Girt Bar · loose · Apr 15, 2024 · N8540V · Boeing 7378H4 · Emergency Equipment
  > GIRT BAR BRACKET IS LOOSE ON SLIDE MAIN CABIN DOOR (AFT BRACKET)<[01] PERFORMED INSPECTION OF AFT CAPT SIDE GIRT BAR AND FOUND SPRING PIN LOOSE FROM THE BAR LOCK ASSY. REATTACHED THE SPRING PIN IAW AMM 25-66-01. NO DEFECTS NOTED.
- [SDR SWAA2024011039011](https://openairdocs.org/sdr/SWAA2024011039011.md): Handle · broken · Jan 6, 2024 · N8540V · Boeing 7378H4 · Service Doors
  > FORWARD SERVICE DOOR ASSIST HANDLE BROKEN.<[01] REPLACED DOOR ASSIST MOUNT PER AMM. 52-41-31.
- [SDR SWAA2023091499924](https://openairdocs.org/sdr/SWAA2023091499924.md): Handle · loose · Sep 13, 2023 · N8540V · Boeing 7378H4 · Passenger/Crew Doors
  > LH FWD EMER EXIT PULL COVER LOOSE<[01] RESECURED ASSIST HANDLE AND COVER FOR LH FWD EMER EXIT REF MM 52-22-51
- [SDR SWAA2023060955508](https://openairdocs.org/sdr/SWAA2023060955508.md): Battery Pack · inoperative · Jun 2, 2023 · N8540V · Boeing 7378H4 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INOP THRU CABIN AREA AND EXTERIOR<[01] REMOVED AND REPLACED BATTERY PACK (M1671 AND M1673) AS PER REF. B737 AMM 33-51-06-960-805 AND PERFORMED OPERATIONAL TEST PER REF. B737 AMM 33-51-06-960-805. FOUND NORMAL.;[02] VERIFIED STEP # 1; R
- [SDR SWAA2023061250614](https://openairdocs.org/sdr/SWAA2023061250614.md): Channel · corroded · May 22, 2023 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FABRICATE AFT CARGO COMPARTMENT LEFT 'Z' CHANNEL FROM STA 727I +3 TO STA 847 SINCE SEVERAL CORROSION NUTPLATE HOLES WERE FOUND OUT OF LIMITS.<[01] REMOVED AFT CARGO LEFT Z CHANNEL; FABRICATED AND DRILLED L/H Z CHANNEL FROM STA 727I+3 TO STA 847; FABRICATED AFT
- [SDR SWAA2023061250942](https://openairdocs.org/sdr/SWAA2023061250942.md): Angle · cracked · May 22, 2023 · N8540V · Boeing 7378H4 · Wing, Control Surfaces
  > R/W TRAILING EDGE DEFLECTION CONTOL PANEL LOWER SUPPORT ANGLE CRACKED AT OUTBD END<[01] REMOVED AND REPLACED WITH NEW ANGLE SUPPORT AT R/W T/E STRUCTURE AT DEFLECTION CONTROL RIB AS PER SRM 51-40-02-0G-0; SRM 51-40-05.;[02] VERIFIED STEP 1
- [SDR SWAA2023061248216](https://openairdocs.org/sdr/SWAA2023061248216.md): Shield · corroded · May 13, 2023 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT FLOOR CARGO COMP R/H FWD SHIELD HAVE CORROSION IN 5 PLACE.(228-054)<[01] REMOVED AND REPLACED NEW R/H AFT CARGO FWD SHIELD PER REF SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.
- [SDR SWAA2023061248196](https://openairdocs.org/sdr/SWAA2023061248196.md): Channel · corroded · May 13, 2023 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMP. Z CHANNEL FROM STA 747 + 18' TO 767; LBL 21;WL 156.4 AROUND THE 2 NUTPLATES HOLE HAS CORROSION. (228-024)<[01] REMOVED CORROSION ON AFT CARGO Z CHANNEL FROM STA 747+18 TO STA 767; PERFORMED UT THICKNESS INSPECTION; CHECKED LIMITS OF REWORKED A
- [SDR SWAA2023061248197](https://openairdocs.org/sdr/SWAA2023061248197.md): Channel · corroded · May 13, 2023 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMP. Z CHANNEL FROM STA 767 + 3' TO 787; LBL 21;WL 156.4 AROUND THE NUTPLATE HOLE HAS CORROSION. (228-035)<[01] REMOVED CORROSION ON AFT CARGO Z CHANNEL FROM STA 767+3 TO STA 787; PERFORMED UT THICKNESS INSPECTION; CHECKED LIMITS OF REWORKED AREA F
- [SDR SWAA2023061248175](https://openairdocs.org/sdr/SWAA2023061248175.md): Channel · corroded · May 13, 2023 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMP. Z CHANNEL FROM STA 767 + 5' TO 787; LBL 21;WL 156.4 AROUND THE NUTPLATE HOLE HAS CORROSION. (228-036)<[01] REMOVED CORROSION ON AFT CARGO Z CHANNEL FROM STA 767+5 TO STA 787; PERFORMED UT THICKNESS INSPECTION; CHECKED LIMITS OF REWORKED AREA F
- [SDR SWAA2023061248198](https://openairdocs.org/sdr/SWAA2023061248198.md): Channel · corroded · May 13, 2023 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMP. Z CHANNEL FROM STA 767 + 6' TO 787; LBL 21;WL 156.4 AROUND THE NUTPLATE HOLE HAS CORROSION. (228-038)<[01] REMOVED CORROSION ON AFT CARGO Z CHANNEL FROM STA 767+6 TO STA 787; PERFORMED UT THICKNESS INSPECTION; CHECKED LIMITS OF REWORKED AREA F
- [SDR SWAA2023061248177](https://openairdocs.org/sdr/SWAA2023061248177.md): Channel · corroded · May 13, 2023 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMP. Z CHANNEL FROM STA 767 + 7.5' TO 787; LBL 21;WL 156.4 AROUND THE NUTPLATE HOLE HAS CORROSION. (228-040)<[01] REMOVED CORROSION ON AFT CARGO Z CHANNEL FROM STA 767+7.5 TO STA 787; PERFORMED UT THICKNESS INSPECTION; CHECKED LIMITS OF REWORKED AR

Next page: https://openairdocs.org/aircraft/N8540V/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 = 'N8540V' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8540V/reports

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