# Service difficulty reports: N8546V

A list on [N8546V](https://openairdocs.org/aircraft/N8546V.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 · 59 reports

- [SDR SWAA2026090191566](https://openairdocs.org/sdr/SWAA2026090191566.md): Panel · delaminated · Aug 25, 2026 · N8546V · Boeing 7378H4 · Fuselage Structure (General)
  > PANEL 193CR LEADING EDGE HAS AREA OF EROSION AND DELAMINATION. R&R 193CR PER AMM 53-51-21. INSPECTED C/A 1. R&R 193CR PER AMM 53-51-21.
- [SDR SWAA2026090169727](https://openairdocs.org/sdr/SWAA2026090169727.md): Panel · delaminated · Aug 25, 2026 · N8546V · Boeing 7378H4 · Aerodynamic Fairings
  > PANEL 193CL LEADING EDGE HAS AREA OF EROSION AND DELAMINATION. R & R PANEL 193CL PER AMM 53-51-21.
- [SDR SWAA2026083109105](https://openairdocs.org/sdr/SWAA2026083109105.md): Battery Pack · inoperative · Aug 20, 2026 · N8546V · Boeing 7378H4 · Emergency Lighting
  > LEFT AFT BULL NOSE EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK AT UNIT M01673 OPS CHECK GOOD IAW AMM 33-51-06. INSPECTED WORK ABOVE.
- [SDR SWAA2026083119411](https://openairdocs.org/sdr/SWAA2026083119411.md): Battery Pack · inoperative · Aug 20, 2026 · N8546V · Boeing 7378H4 · Emergency Lighting
  > LEFT HAND OVER WING EMERGENCY LIGHTS INOP. R&R EMERGENCY LIGHTS BATTERY PACK OPS CHECK GOOD IAW AMM 33-55-02. INSPECTED WORK ABOVE
- [SDR SWAA2026083132563](https://openairdocs.org/sdr/SWAA2026083132563.md): Battery Pack · inoperative · Aug 20, 2026 · N8546V · Boeing 7378H4 · Emergency Lighting
  > LEFT FWD BULLNOSE EMERGENCY LIGHTS INOP. R&R EMERGENCY LIGHTS BATTERY PACK OPS CHECKED GOOD IAW AMM 33-55-02.
- [SDR SWAA2026083110976](https://openairdocs.org/sdr/SWAA2026083110976.md): Battery Pack · inoperative · Aug 20, 2026 · N8546V · Boeing 7378H4 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY DOOR LIGHTS INOP. R&R EMERGENCY LIGHTS BATTERY PACK OPS CHECK GOOD IAW AMM 33-55-02. INSPECTED WORK ABOVE
- [SDR SWAA2026083114525](https://openairdocs.org/sdr/SWAA2026083114525.md): Battery Pack · inoperative · Aug 20, 2026 · N8546V · Boeing 7378H4 · Emergency Lighting
  > R/H FWD BULLNOSE EMERGENCY LIGHTS INOP. R&R EMERGENCY LIGHTS BATTERY PACK OPS CHECK GOOD IAW AMM 33-55-02. INSPECTED WORK ABOVE
- [SDR SWAA2026090181278](https://openairdocs.org/sdr/SWAA2026090181278.md): Floor Panel · delaminated · Aug 19, 2026 · N8546V · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231 KF DELAMINATED REMOVED CABIN FLOORBOARD 231KF. REMOVED AND REPLACED CABIN FLOOR PANEL 231KF PER AMM 53-21-00-401-NG.
- [SDR SWAA2026090107154](https://openairdocs.org/sdr/SWAA2026090107154.md): Support Angle · corroded · Aug 18, 2026 · N8546V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO AFT BULKHEAD LOWER SUPPORT ANGLE STA 500I CORRODED. FWD CARGO AFT BULKHEAD LOWER SUPPORT ANGLE STA 500I 21LBL TO 21RBL CORRODED. REMOVED CORROSION PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.070") SUPPORT ANGLE IS OUT OF LIMITS IAW SRM 53-00-53-1A-2
- [SDR SWAA2026090102560](https://openairdocs.org/sdr/SWAA2026090102560.md): Angle · corroded · Aug 12, 2026 · N8546V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO PIT RT TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLE AT BS500C+11. REMOVED CORROSION PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.033" TRANSITION ANGLE (SIDEPLATE) IS OUT OF LIMITS IAW SRM 53-00-53-1A-2.
- [SDR SWAA2026090131028](https://openairdocs.org/sdr/SWAA2026090131028.md): Fairing · cracked · Aug 12, 2026 · N8546V · Boeing 7378H4 · Trailing Edge Flaps
  > NR 6 TRAILING EDGE FLAP SUPPORT FAIRING CANOE HAS CRACK AT UPPER OUTBOARD CORNER SURFACE. REMOVED NR 6 TRAILING FLAP SUPPORT FAIRING IAW AMM 27-51-18 OBTAINED NEW CANOE FAIRING FROM STOCK AND INSTALLED TAIL CONE ASSEMBLY PER AMM 27-51-28
- [SDR SWAA2026083193382](https://openairdocs.org/sdr/SWAA2026083193382.md): Lens · cracked · Aug 8, 2026 · N8546V · Boeing 7378H4 · Emergency Lighting
  > FWD CABIN HORSESHOE CEILING PANEL - EPL LENSE IS CRACKED. REMOVED & REPLACED EPL LENSE IN REFERENCE TO AMM 33-51-03. INSPECTED WORK ACCOMPLISHED REMOVED & REPLACED EPL LENS IN REFERENCE TO AMM 33-51-03.
- [SDR SWAA2026083184227](https://openairdocs.org/sdr/SWAA2026083184227.md): Lens · cracked · Aug 8, 2026 · N8546V · Boeing 7378H4 · Emergency Lighting
  > AFT CABIN HORSESHOE CEILING PANEL - EPL LENSE IS CRACKED. REMOVED & REPLACED EPL LENSE IN REFERENCE TO AMM 33-51-03. INSPECTED WORK ACCOMPLISHED REMOVED & REPLACED EPL LENS IN REFERENCE TO AMM 33-51-03.
- [SDR SWAA2026083136129](https://openairdocs.org/sdr/SWAA2026083136129.md): Stringer · cracked · Aug 7, 2026 · N8546V · Boeing 7378H4 · Fuselage Main, Longeron/Stringer
  > LEFT STR 18A STA 727 INNER CHORD UPPER FASTENER HOLE STILL HAS A CRACK DEFECT INDICATIOIN IN UPPER FWD FASTENER HOLE PER HFEC HOLE PROBE INSP NDT PART 6, 51-00-00 PROCEDURE 16 USING A.020" NOTCH. PER 26-153-02116-WIP1 (AD - N8546V - L/H STR 18A STA 727 INNER
- [SDR SWAA2026090142229](https://openairdocs.org/sdr/SWAA2026090142229.md): Stringer · cracked · Aug 4, 2026 · N8546V · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > STRINGER18AL BS 727 UPPER FASTENER HOLE COMMON TO INNER CHORD INDICATES A CRACK DEFECT IN STR.18A PER BOEING NDT MANUAL PART6, 51-00-00 PROC.16. L/H STR.18A STA.727 UPPER FASTENER HOLE COMMON TO INNER CHORD INDICATES A CRACK DEFECT IN STR.18A PER BOEING NDT MA
- [SDR SWAA2026082737942](https://openairdocs.org/sdr/SWAA2026082737942.md): Skin · damaged · Aug 3, 2026 · N8546V · Boeing 7378H4 · Nacelle/Pylon, Plate/Skin
  > NR 2 ENGINE INLET HAS PULLING FASTENERS AT 3 AND 9 O'CLOCK POSITIONS REMOVED AND REPLACED #2 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE TTG8Q01DHKKQ FOR PARTS INFORMATION AND WORK PERFORMED.
- [SDR SWAA2026082715244](https://openairdocs.org/sdr/SWAA2026082715244.md): Skin · damaged · Aug 3, 2026 · N8546V · Boeing 7378H4 · Nacelle/Pylon, Plate/Skin
  > #1 ENGINE INLET HAS PULLING FASTENERS AT THE 3 O'CLOCK POSITION REMOVED AND REPLACED NR 1 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE TTG8Q00S71UU FOR PARTS INFORMATION AND WORK PERFORMED. REMOVED AND REPLACED #1 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE
- [SDR SWAA2026083108860](https://openairdocs.org/sdr/SWAA2026083108860.md): Vapor Barrier · cracked · Jul 31, 2026 · N8546V · Boeing 7378H4 · Fuselage Main, Bulkhead
  > RH B.S 663 VAPOR BARRIER UPPER ATTACH ANGLE FASTENER HOLE AT APPX RBL 31" HAS INDICATION OF A CRACK. REPAIRED PER EA M-26-157-01481 (REPAIR OF RH B.S. 663 VAPOR BARRIER UPPER ATTACH L-ANGLE) VERIFIED C/A #1 IS COMPLIED WITH. ENTRY MADE TO CLOSE LABOR ROW ONLY
- [SDR SWAA2026082736697](https://openairdocs.org/sdr/SWAA2026082736697.md): Mount · corroded · Jul 31, 2026 · N8546V · Boeing 7378H4 · Engine Mount Section
  > #2 ENGINE FWD ENGINE MOUNT HAS EXTENSIVE FRETTING CORROSION ON THE HANGAR FITTING AND FAN CASE FITTING AT THE OUTBOARD SIDE LINK UPPER AND LOWER ATTACH BOLTS. REMOVED AND REPLACED #2 ENG FWD MOUNT IAW 771-021-00-01 REFERENCE TTG8Q01DJXC4 FOR PARTS INFORMATION
- [SDR SWAA2026083149380](https://openairdocs.org/sdr/SWAA2026083149380.md): Vapor Barrier · cracked · Jul 28, 2026 · N8546V · Boeing 7378H4 · Fuselage Main, Bulkhead
  > BS 663 VAPOR BARRIER ATTACH ANGLE APPROXIMATELY RBL 34 CRACKED AT O/B FASTENER. SEE ATTACHMENT FOR PIC. REPAIRED PER EA M-26-157-01481 (REPAIR OF RH B.S. 663 VAPOR BARRIER UPPER ATTACH L-ANGLE). INSPECTED WORK PERFORMED
- [SDR SWAA2026083193655](https://openairdocs.org/sdr/SWAA2026083193655.md): Panel · cracked · Jul 24, 2026 · N8546V · Boeing 7378H4 · Wing, Plate/Skin
  > PANEL 561AB NUMEROUS SCREW HOLES CRACKED. REMOVED DAMAGE PER SRM 51-70-05-2R-8 INSPECTED WORK PERFORMED ON C/A #1 APPLIED REPAIR PLIES AND COOKED REPAIR PER SRM 51-70-05-2R-8. INSPECTED WORK PERFORMED ON C/A #3 RESIN SEALED REPAIR PER SRM 51-70-08-0G-0 AND REF
- [SDR SWAA2026083113537](https://openairdocs.org/sdr/SWAA2026083113537.md): Panel · cracked · Jul 24, 2026 · N8546V · Boeing 7378H4 · Wing, Plate/Skin
  > PANEL 561CB HAS NUMEROUS SCREW HOLES CRACKED. REMOVED DAMAGE PER SRM 51-70-05-2R-8. REPAIRED DAMAGED FASTENER HOLES IAW SRM 51-70-05-2R-8. RESIN SEALED REPAIR IAW SRM 51-70-08-0G-0 AND REFINISHED PER AMM 51-21-99. REPAIRED DAMAGED FASTENER HOLES IAW SRM 51-
- [SDR SWAA2026083164633](https://openairdocs.org/sdr/SWAA2026083164633.md): Skin · delaminated · Jul 23, 2026 · N8546V · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT OUTBOARD AFT FLAP HAS A 4 INCH DELAMINATION ON LOWER SURFACE(MARKED) RII - OK TO INSTALL LEFT OUTBOARD AFT FLAP. REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22. RII: VERIFIED REPLACEMENT AND INSTALLATION OF THE L/H O/B AFT FLAP PER AMM 27-51-22. R
- [SDR SWAA2026083187376](https://openairdocs.org/sdr/SWAA2026083187376.md): Skin · delaminated · Jul 23, 2026 · N8546V · Boeing 7378H4 · Trailing Edge Flaps
  > RIGHT OUTBOARD AFT FLAP HAS A LARGE DELAMINATION ON UPPER SURFACE. REMOVED AND REPLACED RT OTBD AFT FLAP IAW AMM 27-51-22.
- [SDR SWAA2026082796842](https://openairdocs.org/sdr/SWAA2026082796842.md): Skid Shoe · damaged · Jul 23, 2026 · N8546V · Boeing 7378H4 · Nacelle/Pylon, Plate/Skin
  > #2 ENGINE INLET COWL LIP SKIN HAS 4 FASTENERS PULLING AT 3 O'CLOCK POSITION. REMOVED AND REPLACED #2 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE TTG8Q01DHKKQ FOR PARTS INFORMATION AND WORK PERFORMED.
- [SDR SWAA2026082758386](https://openairdocs.org/sdr/SWAA2026082758386.md): Skin · damaged · Jul 23, 2026 · N8546V · Boeing 7378H4 · Nacelle/Pylon, Plate/Skin
  > #2 ENGINE INLET COWL LIP SKIN HAS 2 FASTENERS PULLING AT 9 O'CLOCK POSITION. REMOVED AND REPLACED #2 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE TTG8Q01DHKKQ FOR PARTS INFORMATION AND WORK PERFORMED.
- [SDR SWAA2026082780829](https://openairdocs.org/sdr/SWAA2026082780829.md): Skin · damaged · Jul 23, 2026 · N8546V · Boeing 7378H4 · Nacelle/Pylon, Plate/Skin
  > #1 ENGINE INLET COWL LIP SKIN HAS 1 FASTENER PULLING AT 3 O'CLOCK POSITION. REMOVED AND REPLACED #1 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE TTG8Q00S71UU FOR PARTS INFORMATION AND WORK PERFORMED. REMOVED AND REPLACED #1 ENGINE INLET COWL PER AMM 71-11-01.
- [SDR SWAA2026082746627](https://openairdocs.org/sdr/SWAA2026082746627.md): Mount Bracket · cracked · Jul 23, 2026 · N8546V · Boeing 7378H4 · Nacelle/Pylon, Main Frame
  > #1 ENGINE HIGH STAGE REGULATOR MOUNT BRACKET IS CRACKED AT ATTACH POINT. REMOVED AND REPLACED #1 ENGINE HIGH STAGE REGULATOR MOUNT BRACKET PER AMM 70-20-02. INSPECTED WORK PERFORMED
- [SDR SWAA2026042992301](https://openairdocs.org/sdr/SWAA2026042992301.md): Lamp · inoperative · Apr 23, 2026 · N8546V · Boeing 7378H4 · Emergency Lighting
  > LEFT AFT ENTRY EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE LAMPS LEFT AFT ENTRY EXTERIOR EMERGENCY LIGHT AND PERFORMED GOOD OPS CHECK IAW AMM 33-51-04-960-801.
- [SDR SWAA2026042991178](https://openairdocs.org/sdr/SWAA2026042991178.md): Cartridge · cracked · Apr 20, 2026 · N8546V · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT WING OTBD AFT FLAP INBD END ROLLER CARTRIDGE CRACKED AT LOWER FWD RADIUS. LT WING OTBD AFT FLAP; CARTRIDGE WAS REMOVED AND REPLACED IAW SRM 51-40-02-0G-0. TASK COMPLETED.
- [SDR SWAA2026020265956](https://openairdocs.org/sdr/SWAA2026020265956.md): Battery Pack · inoperative · Jan 30, 2026 · N8546V · Boeing 7378H4 · Emergency Lighting
  > AFT RT MULTIPLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE RT EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2025080596966](https://openairdocs.org/sdr/SWAA2025080596966.md): Battery Pack · inoperative · Jul 30, 2025 · N8546V · Boeing 7378H4 · Emergency Lighting
  > ALL RH BIN EMERGENCY LIGHTS AFT OF OVERWING; AND R2 EMERGENCY LIGHTS INOP.<[01] TWO BATTERY PACKS (M1671 AND M1672) WERE FOUND TO BE AT FAULT. CHARGED AND OP CHECKED M1672 BATTERY PACK IAW SWA 737-800 AMM 33-51-06-610-802 AND AMM 33-51-06-960-805. REMOVED; REP
- [SDR SWAA2025080598529](https://openairdocs.org/sdr/SWAA2025080598529.md): Battery Pack · inoperative · Jul 30, 2025 · N8546V · Boeing 7378H4 · Emergency Lighting
  > ALL RH BIN EMERGENCY LIGHTS AFT OF OVERWING; AND R2 EMERGENCY LIGHTS INOP.<[01] TWO BATTERY PACKS (M1671 AND M1672) WERE FOUND TO BE AT FAULT. CHARGED AND OP CHECKED M1672 BATTERY PACK IAW SWA 737-800 AMM 33-51-06-610-802 AND AMM 33-51-06-960-805. REMOVED; REP
- [SDR SWAA2025080595836](https://openairdocs.org/sdr/SWAA2025080595836.md): Handle · unsecure · Jul 27, 2025 · N8546V · Boeing 7378H4 · Galley Doors
  > CR RR R2 DOOR ASSIST HANDLE NEEDS SECURED<[01] SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 52-41-31-400-802;[02] SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 52-41-31-400-802
- [SDR SWAA2025080595837](https://openairdocs.org/sdr/SWAA2025080595837.md): Handle · unsecure · Jul 27, 2025 · N8546V · Boeing 7378H4 · Galley Doors
  > CR RR R2 DOOR AIRFRAME SIDE ASSIST HANDLE NEEDS SECURED<[01] SECURED R2 DOOR AIRFRAME SIDE ASSIST HANDLE IAW B737-800 AMM 25-21-25-420-801;[02] SECURED R2 DOOR AIRFRAME SIDE ASSIST HANDLE IAW B737-800 AMM 25-21-25-420-801
- [SDR SWAA2024080722081](https://openairdocs.org/sdr/SWAA2024080722081.md): Cover · missing · Aug 3, 2024 · N8546V · Boeing 7378H4 · Escape Slide
  > L-1 DOOR SLIDE COVER IS MISSING (NO SEAT AND SLIDE INSIDE) PLACARDS<[01] RE APPLIED ?NO SEAT AND SLIDE INSIDE? PLACARDS AT L1 DOOR PER AMM 11-32-01.
- [SDR SWAA2024070107271](https://openairdocs.org/sdr/SWAA2024070107271.md): Tire · punctured · Jun 29, 2024 · N8546V · Boeing 7378H4 · Tire
  > NOSE GEAR CAME IN CONTACT WITH FOD ON TAKEOFF IN AUS. NORMAL ENGINE PARAMETERS OBSERVED.<[01] PERFORMED TIRE TREAD LOSS OR TIRED BURST CONDITIONAL INSPECTION IAW AMM 05-51-54. FOUND NOSE TIRE (R/H) TO BE PUNCTURED. NO FURTHER DEFECTS FOUND. R&R NOSE TIRES IAW
- [SDR SWAA2024061099664](https://openairdocs.org/sdr/SWAA2024061099664.md): Cover · detached · Jun 7, 2024 · N8546V · Boeing 7378H4 · Emergency Lighting
  > ROW 14 FWD EMERGENCY EXIT SIGN COVER FELL OFF<[01] RAR ROW 14 DEF EMERGENCY EXIT SIGN COVER PER AMM 33-51-01. OPS CHECK GOOD.
- [SDR SWAA2024050782788](https://openairdocs.org/sdr/SWAA2024050782788.md): Flashlight · inoperative · May 5, 2024 · N8546V · Boeing 7378H4 · Emergency Equipment
  > ONE AFT GALLEY FLASHLIGHT INOP<[01] R&R THE #1 AFT GALLEY FLASHLIGHT & BATTERY REF. AMM 25-64-00; OPS CHECK GOOD. THIS CLEARS MEL 25-12-01; SPECIAL PROCEDURES REVERSED.
- [SDR SWAA2024050682461](https://openairdocs.org/sdr/SWAA2024050682461.md): Slide · dislodged · May 4, 2024 · N8546V · Boeing 7378H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE FELL OUT OF THE SHELL AND SHELL IS ALSO DAMAGED<[01] REMOVED AND REPLACED FWD ENTRY DOOR SLIDE CONTAINER AND FWD ENTRY DOOR SLIDE REF MT 725-61-06-FE
- [SDR SWAA2024011139585](https://openairdocs.org/sdr/SWAA2024011139585.md): Light · inoperative · Jan 10, 2024 · N8546V · Boeing 7378H4 · Emergency Lighting
  > AFT ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP<[01] RELAMPED AFT ENTRY EMERGENCY EXIT SLIDE LIGHT PER AMM 33-51-04
- [SDR SWAA2023100507425](https://openairdocs.org/sdr/SWAA2023100507425.md): Slide · loose · Oct 4, 2023 · N8546V · Boeing 7378H4 · Escape Slide
  > FWD SVC DOOR EMER ESCAPE SLIDE PARTIALLY DROPPED OUT OF STOWAGE COMPARTMENT<[01] REPACKED FS DOOR ESCAPE SLIDE IN REF TO MT 725-61-06
- [SDR SWAA2023081587963](https://openairdocs.org/sdr/SWAA2023081587963.md): Slide · out of position · Aug 10, 2023 · N8546V · Boeing 7378H4 · Escape Slide
  > L-1 DOOR GIRT BAR MATERIAL HANGING TOO LOW<[01] CORRECTION OF MATERIAL HANGING ON L-1 DOOR GIRT BAR WILL BE PERFORMED IN TC MT-725-61-06 TTG8Q00MRGXV.;[02] VERIFIED STEP 1
- [SDR SWAA2023081585104](https://openairdocs.org/sdr/SWAA2023081585104.md): Battery Pack · inoperative · Aug 3, 2023 · N8546V · Boeing 7378H4 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INOP THROUGH OUT PASSENGER CABIN.<[01] PERFORMED TROUBLESHOOTING FOR EMERGENCY LIGHTS AS PER WDM 33-51-11; AND FOUND EMERGENCY BATTERY PACKS AT POSITION: M2816; M1675; AND M1670 DEFECTIVE.<BR>REMOVED AND REPLACED EMERGENCY BATTERY PACK
- [SDR SWAA2023081589726](https://openairdocs.org/sdr/SWAA2023081589726.md): Battery Pack · inoperative · Aug 3, 2023 · N8546V · Boeing 7378H4 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INOP THROUGH OUT PASSENGER CABIN.<[01] PERFORMED TROUBLESHOOTING FOR EMERGENCY LIGHTS AS PER WDM 33-51-11; AND FOUND EMERGENCY BATTERY PACKS AT POSITION: M2816; M1675; AND M1670 DEFECTIVE.<BR>REMOVED AND REPLACED EMERGENCY BATTERY PACK
- [SDR SWAA2023081589727](https://openairdocs.org/sdr/SWAA2023081589727.md): Battery Pack · inoperative · Aug 3, 2023 · N8546V · Boeing 7378H4 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INOP THROUGH OUT PASSENGER CABIN.<[01] PERFORMED TROUBLESHOOTING FOR EMERGENCY LIGHTS AS PER WDM 33-51-11; AND FOUND EMERGENCY BATTERY PACKS AT POSITION: M2816; M1675; AND M1670 DEFECTIVE.<BR>REMOVED AND REPLACED EMERGENCY BATTERY PACK
- [SDR SWAA2023081580568](https://openairdocs.org/sdr/SWAA2023081580568.md): Skin · corroded · Jul 19, 2023 · N8546V · Boeing 7378H4 · Wing, Plate/Skin
  > DOOR 532JB FUEL ACCESS HOLE O/B LEFT WING LOWER AREA WITH CORROSION ON FLANGE OUTER SURFACE.<[01] REMOVED CORROSION FROM 532JB FUEL ACCESS HOLE O/B LEFT WING LOWER AREA ON FLANGE OUTER SURFACE PER SRM 57-20-01-2R-1.;[02] VERIFIED STEP 1;[03] REWORKED AREA TO 6
- [SDR SWAA2023081578915](https://openairdocs.org/sdr/SWAA2023081578915.md): Scuff Plate · cracked · Jul 16, 2023 · N8546V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT FWD DOOR SCUFF PLATE IS CRACK P/N 146A8341-7<[01] AFT CARGO DOOR COMPT FWD SCUFF PLATE P/N 146A8341-7 WAS REPAIRED BY J.L WELDING INC. CUSTOMER ORDER # 414134. INSTALLATION TO SCUFF PLATE TO BE ACCOMPLISH ON TASKCARD TTG8R007SXFW.;[02] VERIFIED
- [SDR SWAA2023081578912](https://openairdocs.org/sdr/SWAA2023081578912.md): Seal · cracked · Jul 15, 2023 · N8546V · Boeing 7378H4 · Horizontal Stabilizer Structure
  > LOWER LEFT HORIZONTAL LWR T/E GAP COVER ACCESS PANEL 333AB METAL AND RUBBER SEAL CRACKED; DETERIORATED.<[01] REMOVED AND REPLACED METAL AND RUBBER SEAL ON LOWER LEFT HORIZONTAL LWR T/E GAP COVER ACCESS PANEL 333AB AS PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1
- [SDR SWAA2023081578329](https://openairdocs.org/sdr/SWAA2023081578329.md): Support Angle · cracked · Jul 13, 2023 · N8546V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > L/H VAPOR BARRIER TO CENTER TANK LWR SKIN SUPPORT ANGLE CRACKED AT STA 663.75 AND LBL 10<[01] REMOVED FASTENERS AT L/H VAPOR BARRIER TO CENTER TANK LWR SKIN SUPPORT ANGLE STA 663.75 LBL 10 IRW SRM 51-40-02<BR><BR>CUT OUT DAMAGE AT L/H VAPOR BARRIER TO CENTER T

Next page: https://openairdocs.org/aircraft/N8546V/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 = 'N8546V' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8546V/reports

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