# Service difficulty reports: N8545V

A list on [N8545V](https://openairdocs.org/aircraft/N8545V.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 SWAA2026092128425](https://openairdocs.org/sdr/SWAA2026092128425.md): Flashlight · inoperative · Sep 17, 2026 · N8545V · Boeing 7378H4 · Emergency Equipment
  > AFT CABIN FLASHLIGHT INOPERATIVE. OK TO CONTINUE IAW MEL 25-12-01, SP1B. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25-64-00. OP CHKD GOOD. MEL CLEARED.
- [SDR SWAA2026080310149](https://openairdocs.org/sdr/SWAA2026080310149.md): Web · cracked · Jul 22, 2026 · N8545V · Boeing 7378H4 · Wing Miscellaneous Structure
  > LEFT WING TRAILING EDGE TRANSVERSE WEB ABOVE NR 1 AFT PYLON TIP CRACKED. REMOVED AND REPLACED LT WING TRAILING EDGE TRANSVERSE WEB ABOVE NR 1 AFT PYLON TIP IAW SRM 51-40-02, AND AIPC 57-50-00-36A.
- [SDR SWAA2026080334290](https://openairdocs.org/sdr/SWAA2026080334290.md): Attach Angle · cracked · Jul 17, 2026 · N8545V · Boeing 7378H4 · Wing, Attach Fittings
  > LEFT WING TRAILING EDGE OTBD ATTACH ANGLE AT TRANSVERSE WEB ABOVE NR 1 AFT PYLON TIP CRACKED. REMOVED AND REPLACED LEFT WING TRAILING EDGE OTBD ATTACH ANGLE AT TRANSVERSE WEB ABOVE NR 1 AFT PYLON TIP IAW SRM 51-40-02 AND AIPC 57-42-51-03.
- [SDR SWAA2026073106687](https://openairdocs.org/sdr/SWAA2026073106687.md): Attach Angle · cracked · Jul 14, 2026 · N8545V · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > LEFT BS 663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER, LBL 13, WL 167.68, A CRACK FOUND TO BE OUT OF LIMITS IAW SRM 57-10-10-1A-2. REPAIRED THE LT BS 663 UPPER ATTACH ANGLE ON VAPOR BARRIER, WL167.68 IAW EA-M-157-01480.
- [SDR SWAA2026073149054](https://openairdocs.org/sdr/SWAA2026073149054.md): Attach Angle · cracked · Jul 14, 2026 · N8545V · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > RIGHT BS 663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL 8, WL 167.68 CRACK FOUND TO BE OUT OF LIMITS IAW SRM 57-10-10-1A-2. REPAIRED RT BS 663 UPPER ATTACH ANGLE ON VAPOR BARRIER WL167.68, IAW EA-M-157-01481.
- [SDR SWAA2026070719197](https://openairdocs.org/sdr/SWAA2026070719197.md): Lens · detached · Jul 6, 2026 · N8545V · Boeing 7378H4 · Emergency Lighting
  > OVERWING EMERGENCY SIGN COVER FELL OFF. REINSTALLED LENS IAW AMM 33-51-01.
- [SDR SWAA2026051396731](https://openairdocs.org/sdr/SWAA2026051396731.md): Battery Pack · inoperative · May 8, 2026 · N8545V · Boeing 7378H4 · Emergency Lighting
  > LEFT OVER WING EMERGENCY EXIT CABIN LIGHTS INOPERATIVE. REMOVED AND REPLACED 1 EA BATTERY PACK M1694 AND OPS CHECK GOOD IAW AMM 33-51-06-960-805.
- [SDR SWAA2026051396730](https://openairdocs.org/sdr/SWAA2026051396730.md): Battery Pack · inoperative · May 8, 2026 · N8545V · Boeing 7378H4 · Emergency Lighting
  > R/H OVER WING EMERGENCY EXIT CABIN LIGHTS INOPERATIVE. REMOVED AND REPLACED 1 EA BATTERY PACK M1695 AND OPS CHECK GOOD IAW AMM 33-51-06-960-805.
- [SDR SWAA2026051394870](https://openairdocs.org/sdr/SWAA2026051394870.md): Battery Pack · inoperative · May 2, 2026 · N8545V · Boeing 7378H4 · Emergency Lighting
  > FWD LT BIN EMERGENCY AISLE LIGHTS 3 EA INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK OPS CHECK GOOD IAW AMM 33-51-06-960-805 AND 33-51-00-710-801.
- [SDR SWAA2026051394977](https://openairdocs.org/sdr/SWAA2026051394977.md): Handle · loose · May 2, 2026 · N8545V · Boeing 7378H4 · Passenger/Crew Doors
  > L1 DOOR ASSIST HANDLE NEEDS SECURED. SECURED L1 DOOR ASSIST HANDLE PER AMM 52-11-31400-802.
- [SDR SWAA2026051394980](https://openairdocs.org/sdr/SWAA2026051394980.md): Handle · loose · May 2, 2026 · N8545V · Boeing 7378H4 · Passenger/Crew Doors
  > L2 DOOR / AIRFRAME SIDE ASSIST HANDLES NEED SECURED. SECURED L2 DOOR AIRFRAME SIDE ASSIST HANDLES PER AMM 25-21-25-420-801;
- [SDR SWAA2026042492282](https://openairdocs.org/sdr/SWAA2026042492282.md): Flashlight · no test · Apr 23, 2026 · N8545V · Boeing 7378H4 · Emergency Equipment
  > AFT FLIGHT ATTENDANT FLASHLIGHT NOT TESTING. REMOVED AND REPLACED AFTER F/A FLASHLIGHT BATTERY IAW AMM 25-64-00.
- [SDR SWAA2026033184082](https://openairdocs.org/sdr/SWAA2026033184082.md): Bracket · inoperative · Mar 28, 2026 · N8545V · Boeing 7378H4 · Emergency Equipment
  > FWD ENTRY DOOR GIRT BAR NOT IN POSITION. REMOVED AND REPLACED RIVET AT GIRT BAR BRACKET IAW SRM 51-40-02
- [SDR SWAA2026032080862](https://openairdocs.org/sdr/SWAA2026032080862.md): Slide · out of adjust · Mar 18, 2026 · N8545V · Boeing 7378H4 · Escape Slide
  > FWD SERVICE DOOR ESCAPE SLIDE FWD MOUNTING SCREW STRIPPED. R & R SCREW IAW AMM 25-66-01 AND MT 725-61-06-FS
- [SDR SWAA2026031980188](https://openairdocs.org/sdr/SWAA2026031980188.md): Sign · loose · Mar 16, 2026 · N8545V · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN LOOSE. RESECURED EMERGENCY EXIT SIGN PER AMM 33-51-01.
- [SDR SWAA2025102225627](https://openairdocs.org/sdr/SWAA2025102225627.md): None · smoke · Oct 19, 2025 · N8545V · Boeing 7378H4 · Standard Practices/Structures
  > DUE TO PASSENGER LI-ION BATTERY HIGH CAPACITY DISCHARGE IN FLIGHT. PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-56. NO SMOKE OR FUMES NOTED.
- [SDR SWAA2025100821741](https://openairdocs.org/sdr/SWAA2025100821741.md): Battery Pack · inoperative · Oct 6, 2025 · N8545V · Boeing 7378H4 · Emergency Lighting
  > OVERWING AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED OVERWING AFT EMERGENCY LIGHT BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-51-06.
- [SDR SWAA2025052975235](https://openairdocs.org/sdr/SWAA2025052975235.md): Slide · out of adjust · May 26, 2025 · N8545V · Boeing 7378H4 · Escape Slide
  > L2 DOOR SLIDE IS SAGGING <[01]. VERIFIED CORRECT INSTALLATION OF L2 DOOR SLIDE NO DEFECTS NOTED NO MAINTENANCE ACTION REQUIRED AT THIS TIME AMM 25-66-01.
- [SDR SWAA2025051268438](https://openairdocs.org/sdr/SWAA2025051268438.md): Flashlight · no test · May 7, 2025 · N8545V · Boeing 7378H4 · Emergency Equipment
  > FLIGHT ATTENDANT REPORTS FLASH LIGHT AFT GALLEY FLASHING RED (GREEN)<[01] REMOVED AND REPLACED AFT GALLEY FA FLASHLIGHT. OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME FLASH IS GREEN REF AMM 25-64-00
- [SDR SWAA2025033109685](https://openairdocs.org/sdr/SWAA2025033109685.md): Coffeemaker · odor · Mar 27, 2025 · N8545V · Boeing 7378H4 · Buffet/Galleys
  > FWD COFFEE MAKER SMELLED DURING AND AFTER OPERATION.<[01] OK TO CONT. PER MEL 25-10-01 SP-1 AUTH# 244280;[02] REMOVED AND REPLACED FWD COFFEE MAKER IN REF TO AMM 25-30-01.
- [SDR SWAA2025030401276](https://openairdocs.org/sdr/SWAA2025030401276.md): Cover · loose · Mar 2, 2025 · N8545V · Boeing 7378H4 · Emergency Lighting
  > MID- CABIN-EXIT SALIDA- SIGN COVER FELL OFF<[01] INSTALLED MID- CABINET EXIT SIGN COVER IAW AMM 33-51-02.
- [SDR SWAA2025012889174](https://openairdocs.org/sdr/SWAA2025012889174.md): Battery Pack · inoperative · Jan 23, 2025 · N8545V · Boeing 7378H4 · Escape Slide
  > AFT LEFT(L732) AND RIGHT(L733) ESCAPE SLIDE LIGHTS ARE INOP. FUTHER INVESTIGATION ALL AFT AREA EMERGENCY LIGHT INOP SUSPECTED BATTERY PACK M1673 M1672 M1671 NEED TO BE REPLACE. REPLACED POWER SUPPLY - BATTERY PACKS TO M1673; M1672 AND M1671 PER AMM 33-51-0
- [SDR SWAA2024121778476](https://openairdocs.org/sdr/SWAA2024121778476.md): Lens · missing · Dec 16, 2024 · N8545V · Boeing 7378H4 · Emergency Lighting
  > OVERHEAD CABIN EXIT SIGN LENS WAS MISSING<[01] INSTALLED OVER WING EXIT SIGN LENS PER MM 33-51-01.
- [SDR SWAA2024120974592](https://openairdocs.org/sdr/SWAA2024120974592.md): Lens · detached · Dec 6, 2024 · N8545V · Boeing 7378H4 · Emergency Lighting
  > CABIN CENTER EMERGENCY EXIT LIGHT LENS FELL OFF<[01] REINSTALLED CABIN CENTER EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01
- [SDR SWAA2023081487878](https://openairdocs.org/sdr/SWAA2023081487878.md): Light · broken · Aug 9, 2023 · N8545V · Boeing 7378H4 · Emergency Lighting
  > FWD EXIT CALL LIGHT CLIP ON HOUSING BROKEN<[01] O.K. TO CONTINUE. PER MEL 25-10-01 SP#1B. AUTH# 149439.;[02] REMOVED AND REPLACED FWD EXIT SIGN CALL LIGHT ASSEMBLY REF AMM 33-51-01
- [SDR SWAA2023080182212](https://openairdocs.org/sdr/SWAA2023080182212.md): Angle · cracked · Jul 26, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ANGLE FOR 141PW AFT STANCHION CRACKED AT LWR END.<[01] REMOVED AND REPLACED WITH NEW ANGLE PER SRM 51-40-02
- [SDR SWAA2023073183475](https://openairdocs.org/sdr/SWAA2023073183475.md): Battery Pack · inoperative · Jul 20, 2023 · N8545V · Boeing 7378H4 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INOP IN THE CABIN<[01] REMOVED AND REPLACED 2 EACH EMERGENCY POWER SUPPLY BATTERY PACKS IN FWD GALLEY AND FWD RIGHT CABIN BULLNOSE IAW AMM 33-51-06.;[02] OPS CHECKED GOD PER AMM 33-51-06
- [SDR SWAA2023072880718](https://openairdocs.org/sdr/SWAA2023072880718.md): Battery Pack · inoperative · Jul 20, 2023 · N8545V · Boeing 7378H4 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INOP IN THE CABIN<[01] REMOVED AND REPLACED 2 EACH EMERGENCY POWER SUPPLY BATTERY PACKS IN FWD GALLEY AND FWD RIGHT CABIN BULLNOSE IAW AMM 33-51-06.;[02] OPS CHECKED GOD PER AMM 33-51-06
- [SDR SWAA2023073176967](https://openairdocs.org/sdr/SWAA2023073176967.md): Angle · corroded · Jul 10, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO; BELOW R/H SHIELD/SIDEPLATE STA.767-787 RBL 21 ANGLE HAS CORROSION AFT CARGO BELOW R/H SHIELD/SIDEPLATE STA.767-787 RBL 21 ANGLE HAS CORROSION<[01] REMOVED DAMAGED ANGLE PER SRM 51-40-02;[02] LOCATED AND DRILLED NEW ANGLE PER SRM 51-40-02;[03] INSTAL
- [SDR SWAA2023080176431](https://openairdocs.org/sdr/SWAA2023080176431.md): Intercostal · corroded · Jul 7, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT. CARGO R/H SIDE UNDER TRANSITION ANGLE (SIDE-PLATE) RBL. 21 WEB/INTERCOSTAL HAS CORROSION AROUND NUT-PLATE HOLES. AFT. CARGO R/H SIDE UNDER TRANSITION ANGLE (SIDE-PLATE) RBL. 21 WEB/INTERCOSTAL HAS CORROSION AROUND NUT-PLATE HOLES. STA.747-767<[01] REMOVED
- [SDR SWAA2023073176430](https://openairdocs.org/sdr/SWAA2023073176430.md): Intercostal · corroded · Jul 7, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT. CARGO R/H SIDE UNDER TRANSITION ANGLE (SIDE-PLATE) RBL. 21 WEB/INTERCOSTAL HAS CORROSION AROUND NUT-PLATE HOLES. STA. 747-767. AFT. CARGO R/H SIDE UNDER TRANSITION ANGLE (SIDE-PLATE) RBL. 21 WEB/INTERCOSTAL HAS CORROSION AROUND NUT-PLATE HOLES.<[01] REMOV
- [SDR SWAA2023073176433](https://openairdocs.org/sdr/SWAA2023073176433.md): Angle · corroded · Jul 7, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT. CARGO L/H TRANSITION ANGLE LBL. 21 STA.727H+10 TO STA.807+10 HAS CORROSION IN SEVERAL AREAS.<[01] CUT AND REMOVED DAMAGED SECTION PER SRM 53-00-53-2R-5. SECTION OUT OF LIMITS;[02] C/W INSPECTION.;[03] REJECT: IN THE MEASUREMENTS SECTION; THE FOLLOWING ERR
- [SDR SWAA2023073176432](https://openairdocs.org/sdr/SWAA2023073176432.md): Angle · corroded · Jul 7, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT. CARGO L/H TRANSITION ANGLE LBL. 21 STA.727H+10 TO STA.787+10 HAS CORROSION IN SEVERAL AREAS.<[01] CUT DAMAGED SECTION FROM STA.727H+10 TO 787+10 PER SRM 53-00-53-2R-5;[02] CUT DAMAGED SECTION FROM STA.727H+10 TO 787+10 PER SRM 53-00-53-2R-5 SECTION IS OUT
- [SDR SWAA2023073176191](https://openairdocs.org/sdr/SWAA2023073176191.md): Angle · corroded · Jul 6, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT. CARGO R/H TRANSITION ANGLE STA.727H TO STA.767 HAS CORROSION IN SEVERAL AREAS.<[01] TRANSITION ANGLE OUT OF LIMITS PER SRM 53-00-53-1A-2;[10] INSTALLED NUT PLATES PER SRM 51-40-10-2R-0 AND EA M-23-151-01545 ON 07-14-2030 @ 0100.;[11] VERIFIED C/A # 10: R
- [SDR SWAA2023073175402](https://openairdocs.org/sdr/SWAA2023073175402.md): Fairing · damaged · Jul 5, 2023 · N8545V · Boeing 7378H4 · Wing, Control Surfaces
  > #6 FLAP SUPPORT FAIRING 642BB (CANOE) HAS ELONGATED HOLES AT O/B CENTER BULB SEAL.<[01] CANOE FAIRING REPLACED ON FAULT # TTG8Q00M6D1H LINE 2523. REMOVED & REPLACED #6 FLAP SUPPORT FAIRING FOR COMPANY CONVENANCE.
- [SDR SWAA2023073174200](https://openairdocs.org/sdr/SWAA2023073174200.md): Strap · corroded · Jul 2, 2023 · N8545V · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION FOUND AT STA.947 LBL25 UPPER AFT FLANGE AT FLOOR BEAM<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] ADDED TOOLS.;[03] VERIFIED 1. WILSON WHITT (TECHNICIAN); 02-JUL-2023 17:27 UTC<BR>REMOVED DAMAGE PER SRM
- [SDR SWAA2023073174201](https://openairdocs.org/sdr/SWAA2023073174201.md): Strap · corroded · Jul 2, 2023 · N8545V · Boeing 7378H4 · Fuselage Main, Floor Beam
  > IN THE AFT CABIN WET AREA THERE IS EVIDENCE OF CORROSION ON TOP OF THE FLOOR BEAM AT STATION 947; LBL 16.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] ADDED TOOLS;[03] VERIFIED 1. WILSON WHITT (TECHNICIAN); 02-JUL
- [SDR SWAA2023073173538](https://openairdocs.org/sdr/SWAA2023073173538.md): Floorbeam · cracked · Jun 30, 2023 · N8545V · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CABIN FLOOR STRUCTURE BREAK ASSY CRACKED STA 540 AT BL 0 TO RBL 24.<[01] REMOVED; AND REPLACED BREAK ASSY. REF. SRM. 51-40-02.;[02] INSPECTION VERIFIED CORRECTIVE ACTION STEP 1.
- [SDR SWAA2023073173540](https://openairdocs.org/sdr/SWAA2023073173540.md): Floorbeam · cracked · Jun 30, 2023 · N8545V · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CABIN FLOOR STRUCTURE BREAK ASSY CRACKED STA 540 AT BL 0 TO LBL 24.<[01] REMOVED; AND REPLACED BREAK ASSY. REF. SRM. 51-40-02.;[02] INSPECTION VERIFIED CORRECTIVE ACTION STEP 1.
- [SDR SWAA2023073173139](https://openairdocs.org/sdr/SWAA2023073173139.md): Angle · corroded · Jun 29, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR STRUCTURE RH TRANSITION ANGLE BETWEEN STA 727J-747 HAS CORROSION.(MARKED)<[01] ALL WORK TO BE PERFORMED ON NR#TTG8Q00M2JKA. INSTALLED R/H TRANSITION ANGLE REPAIR FROM BS727H+10 - 767 PER SRM 53-00-53-2R-5.
- [SDR SWAA2023073173154](https://openairdocs.org/sdr/SWAA2023073173154.md): Angle · corroded · Jun 29, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR STRUCTURE RH TRANSITION ANGLE BETWEEN STA 747-767 HAS CORROSION.(MARKED)<[01] ALL WORK TO BE PERFORMED ON NR#TTG8Q00M2JKA. INSTALLED R/H TRANSITION ANGLE REPAIR FROM BS727H+10 - 767 PER SRM 53-00-53-2R-5.
- [SDR SWAA2023073173124](https://openairdocs.org/sdr/SWAA2023073173124.md): Angle · corroded · Jun 29, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR STRUCTURE RH TRANSITION ANGLE BETWEEN STA 727I-727J HAS CORROSION.(MARKED)<[01] ALL WORK TO BE PERFORMED ON NR#TTG8Q00M2JKA. INSTALLED R/H TRANSITION ANGLE REPAIR FROM BS727H+10 - 767 PER SRM 53-00-53-2R-5.
- [SDR SWAA2023073173183](https://openairdocs.org/sdr/SWAA2023073173183.md): Angle · corroded · Jun 29, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT LEFT SIDEPLATE HAS CORROSION AT STA 807 LBL 22<[01] SECTION TO BE REPLACED ON NR#TTG8Q00M31LY PER SRM 53-00-53-2R-5;[02] C/W INSPECTION. INSTALLED NEW SECTION OF TRANSITION ANGLE FROM STA 727H+11.5 TO 807+7 PER SRM 53-00-53-2R-5.
- [SDR SWAA2023073173156](https://openairdocs.org/sdr/SWAA2023073173156.md): Shield · corroded · Jun 29, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR STRUCTURE RH SHIELD (WEB) ANGLE BETWEEN STA 767-787 HAS CORROSION.(MARKED)<[01] SHIELD OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] VERIFIED CORRECTIVE ACTION STEP #1;[03] LOCATED AND DRILLED NEW SHIELD PER SRM 51-40-02;[04] REMOVED AND
- [SDR SWAA2023073173178](https://openairdocs.org/sdr/SWAA2023073173178.md): Plate · corroded · Jun 29, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD. CARGO BILGE; L/H TRANS. ANGLE FASTENER HOLES CORRODED FROM BS 500D-500E.<[01] CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] INSPECTED THE WORK PERFORMED ON C/A #1; NO DEFECTS NOTED.;[03] REMOVED DAMAGED SECTION OF L/H SIDEPLATE FROM STA 5
- [SDR SWAA2023073173142](https://openairdocs.org/sdr/SWAA2023073173142.md): Angle · corroded · Jun 29, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR STRUCTURE LH TRANSITION ANGLE BETWEEN STA 727I-727J HAS CORROSION.(MARKED)<[01] SECTION TO BE REPLACED ON NR#TTG8Q00M31LY PER SRM 53-00-53-2R-5;[02] C/W INSPECTION. INSTALLED NEW SECTION OF TRANSITION ANGLE FROM STA 727H+11.5 TO 807
- [SDR SWAA2023073173144](https://openairdocs.org/sdr/SWAA2023073173144.md): Angle · corroded · Jun 29, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR STRUCTURE LH TRANSITION ANGLE BETWEEN STA 727J-747 HAS CORROSION.(MARKED)<[01] SECTION TO BE REPLACED ON NR#TTG8Q00M31LY PER SRM 53-00-53-2R-5;[02] C/W INSPECTION. INSTALLED NEW SECTION OF TRANSITION ANGLE FROM STA 727H+11.5 TO 807+
- [SDR SWAA2023073173160](https://openairdocs.org/sdr/SWAA2023073173160.md): Angle · corroded · Jun 29, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR STRUCTURE LH TRANSITION ANGLE BETWEEN STA 747 TO 767 HAS CORROSION.(MARKED)<[01] SECTION TO BE REPLACED ON NR#TTG8Q00M31LY PER SRM 53-00-53-2R-5;[02] C/W INSPECTION. INSTALLED NEW SECTION OF TRANSITION ANGLE FROM STA 727H+11.5 TO 80
- [SDR SWAA2023073173146](https://openairdocs.org/sdr/SWAA2023073173146.md): Angle · corroded · Jun 29, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR STRUCTURE LH TRANSITION ANGLE BETWEEN STA 767 TO 787 HAS CORROSION.(MARKED)<[01] SECTION TO BE REPLACED ON NR#TTG8Q00M31LY PER SRM 53-00-53-2R-5;[02] C/W INSPECTION. INSTALLED NEW SECTION OF TRANSITION ANGLE FROM STA 727H+11.5 TO 80
- [SDR SWAA2023073173189](https://openairdocs.org/sdr/SWAA2023073173189.md): Web · corroded · Jun 29, 2023 · N8545V · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD. CARGO ENTRY THRESHOLD WEB HAS CORRODED AREA AT BS. 460-462.<[01] CORROSION OUT OF LIMITS PER SRM 53-30-15-1A-1;[02] INSPECTED THE WORK PERFORMED ON C/A #1; NO DEFECTS NOTED.;[03] REMOVED WEB PER SRM 51-40-02;[04] CORROSION OUT OF LIMITS PER SRM 51-30-15-1

Next page: https://openairdocs.org/aircraft/N8545V/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 = 'N8545V' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8545V/reports

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