N8540V

Service difficulty reports · 79

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWAA2026061107658Shield · corrodedIN 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 IMay 30, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061106481Frame · damagedFWD 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.May 26, 2026 · N8540V · Boeing 7378H4 · Fuselage Main, FrameSDR SWAA2026061106480Frame · damagedFWD 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.May 26, 2026 · N8540V · Boeing 7378H4 · Fuselage Main, FrameSDR SWAA2026061105657Angle · crackedAFT CARGO COMPARTMENT BS 867, LBL 13, ANGLE BRACKET FOR PANEL 141QW PILLAR IS CRACKED. REMOVED AND REPLACED AFT CARGO COMPARTMENT BS 867, LBL 13.May 23, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061104577Lamp · inoperativeEXTERIOR 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.May 19, 2026 · N8540V · Boeing 7378H4 · Emergency LightingSDR SWAA2026061104576Lamp · inoperativeEXTERIOR 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.May 19, 2026 · N8540V · Boeing 7378H4 · Emergency LightingSDR SWAA2026061104505Fairing · crackedNR 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.May 19, 2026 · N8540V · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2026061004183Baffle · crackedFWD 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.May 19, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061103713Battery Pack · inoperativeEMERGENCY 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.May 17, 2026 · N8540V · Boeing 7378H4 · Emergency LightingSDR SWAA2026061103387Intercostal · crackedBRACKET INBOARD OF THE INBD RT WING DEFLECTION CONTROL RIB INBD INTERCOSTAL IS CRACKED. REMOVED AND REPLACED THE BRACKET ANGLE IAW SRM 5-40-02.May 15, 2026 · N8540V · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2026061197975Support · corrodedFORWARD 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.May 13, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061197596Support Angle · crackedFORWARD 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.May 12, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061197971Support Angle · crackedFWD 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.May 12, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061197309Angle · corrodedFWD 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.May 11, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061197312Angle · corrodedFWD 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 SRMay 11, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061197112Seal · crackedRIGHT 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 SMay 10, 2026 · N8540V · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026061197115Seal · crackedLEFT 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 SLIMay 10, 2026 · N8540V · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026061197111Rod End · corrodedTHE 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-May 9, 2026 · N8540V · Boeing 7378H4 · AileronsSDR SWAA2026061196793Rib · crackedFOUND 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.May 8, 2026 · N8540V · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2026061097969Angle · corrodedAFT 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 FABRICATMay 8, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061196057Support · corrodedFWD 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.May 7, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061103710Seal · wornRIGHT 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.May 7, 2026 · N8540V · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2026050494327Control Valve · leakingNR 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.Apr 29, 2026 · N8540V · Boeing 7378H4 · Aircraft Fuel SystemSDR SWAA2026042793343Drive System · out of adjustAFTER 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 LApr 23, 2026 · N8540V · Boeing 7378H4 · Trailing Edge Flap Control SystemSDR SWAA2026042792133Torque Tube · damagedAFTER 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 LApr 23, 2026 · N8540V · Boeing 7378H4 · Trailing Edge Flap Control SystemSDR SWAA2025120943954Slide · dislodgedR1 DOOR SLIDE DISLODGED. INSTALLED R1 DOOR ESCAPE SLIDE IAW MT 725-61-06 AND AMM 25-66-01.Dec 8, 2025 · N8540V · Boeing 7378H4 · Escape SlideSDR SWAA2025120141084Unknown · odorLIGHT 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, INSPECNov 30, 2025 · N8540V · Boeing 7378H4 · Air Distribution SystemSDR SWAA2025103029074Flashlight · not seatedFWD GALLEY FLASHLIGHT GREEN LIGHT NOT ILLUMINATED. RESEATED FWD GALLEY FLASHLIGHT AND OPS CHK NML PER AMM 25-64-00. APPLIED TAPER SEAL.Oct 27, 2025 · N8540V · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025102726831Battery Pack · inoperativeEMERGENCY 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.;Oct 22, 2025 · N8540V · Boeing 7378H4 · Emergency LightingSDR SWAA2025091614140Flashlight · inoperativeFWD FLASHLIGHT INOPERATIVE. REPLACED FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 25-64-00; OPS CHECKED GOOD.Sep 13, 2025 · N8540V · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025090811243Battery · inoperativeEMERGENCY LIGHTS FROM LEFT O/W EXIT TO ROW 23 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER IAW AMM 33-51-06Sep 4, 2025 · N8540V · Boeing 7378H4 · Emergency LightingSDR SWAA2025090812526Charger · inoperativeEMERGENCY LIGHTS FROM LEFT O/W EXIT TO ROW 23 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER IAW AMM 33-51-06Sep 4, 2025 · N8540V · Boeing 7378H4 · Emergency LightingSDR SWAA2025062484251Girt Bar · looseGIRT BAR RETAINING BRACKET ON L1 DOOR LOOSE. INSTALLED NEW RIVET IN GIRT BAR HOLDER IN ACCORDANCE WITH SRM 51-40-02.Jun 21, 2025 · N8540V · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025060677663Cabin Air Sys · odorLEFT 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 Jun 2, 2025 · N8540V · Boeing 7378H4 · Cabin Cooling SystemSDR SWAA2025052774283Battery Pack · inoperativeAISLE 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.May 23, 2025 · N8540V · Boeing 7378H4 · Emergency LightingSDR SWAA2025050266215Flashlight · inoperativeFWD CABIN EMERGENCY FLASHLIGHT INOP.<[01] FLASHLIGHT CAME LOOSE FROM MOUNT. RESECURED AND REPLACED SECURITY SEAL PER AMM 25-64-00May 1, 2025 · N8540V · Boeing 7378H4 · Emergency EquipmentSDR SWAA2024121777613Battery Pack · inoperativeFWD 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.Dec 15, 2024 · N8540V · Boeing 7378H4 · Emergency LightingSDR SWAA2024050983615Battery Pack · inoperativeFWD ENTRY DOOR EMERGENCY LIGHT AND FWD GALLEY EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED FWD ENTRY DOOR EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06May 8, 2024 · N8540V · Boeing 7378H4 · Emergency LightingSDR SWAA2024041774868Girt Bar · looseGIRT 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.Apr 15, 2024 · N8540V · Boeing 7378H4 · Emergency EquipmentSDR SWAA2024011039011Handle · brokenFORWARD SERVICE DOOR ASSIST HANDLE BROKEN.<[01] REPLACED DOOR ASSIST MOUNT PER AMM. 52-41-31.Jan 6, 2024 · N8540V · Boeing 7378H4 · Service DoorsSDR SWAA2023091499924Handle · looseLH FWD EMER EXIT PULL COVER LOOSE<[01] RESECURED ASSIST HANDLE AND COVER FOR LH FWD EMER EXIT REF MM 52-22-51Sep 13, 2023 · N8540V · Boeing 7378H4 · Passenger/Crew DoorsSDR SWAA2023060955508Battery Pack · inoperativeSEVERAL 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; RJun 2, 2023 · N8540V · Boeing 7378H4 · Emergency LightingSDR SWAA2023061250614Channel · corrodedFABRICATE 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 AFTMay 22, 2023 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023061250942Angle · crackedR/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 1May 22, 2023 · N8540V · Boeing 7378H4 · Wing, Control SurfacesSDR SWAA2023061248216Shield · corrodedAFT 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.May 13, 2023 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023061248196Channel · corrodedAFT 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 AMay 13, 2023 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023061248197Channel · corrodedAFT 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 FMay 13, 2023 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023061248175Channel · corrodedAFT 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 FMay 13, 2023 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023061248198Channel · corrodedAFT 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 FMay 13, 2023 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023061248177Channel · corrodedAFT 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 ARMay 13, 2023 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous Structure
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