# Service difficulty reports: N8511K

A list on [N8511K](https://openairdocs.org/aircraft/N8511K.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 · 89 reports

- [SDR SWAA2026072334302](https://openairdocs.org/sdr/SWAA2026072334302.md): Flashlight · no test · Jul 19, 2026 · N8511K · Boeing 7378H4 · Life Raft
  > ONE FWD F/A FLASHLIGHT WILL NOT TEST REPOSITION FLASHLIGHT ON CRADLE OPS CHECK GOOD PER AMM 25-64-00
- [SDR SWAA2026060809143](https://openairdocs.org/sdr/SWAA2026060809143.md): Lens · damaged · Jun 4, 2026 · N8511K · Boeing 7378H4 · Emergency Lighting
  > PASSENGER CABIN OVERHEAD BIN EMERGENCY LIGHT LENS AT 27ABC DAMAGED. R & R PASSENGER CABIN OVERHEAD BIN EMERGENCY LIGHT LENS AT 27ABC IAW AMM 33-51-03.
- [SDR SWAA2026040986888](https://openairdocs.org/sdr/SWAA2026040986888.md): Flashlight · inoperative · Apr 7, 2026 · N8511K · Boeing 7378H4 · Emergency Equipment
  > FWD GALLEY FLASHLIGHT (RIGHT SIDE) INOP. FLASHLIGHT W/N TEST<[01] OK TO CONT PER MEL 25-12-01 SP1B AUTH #313849;[02] R&R FWD GALLEY RIGHT SIDE PER AMM 25-64-00 OPS CHECK GOOD CLEARS MEL
- [SDR SWAA2026010556733](https://openairdocs.org/sdr/SWAA2026010556733.md): Sign · dislodged · Dec 30, 2025 · N8511K · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN IN CENTER AISLE DISLODGED. SECURED AISLE EMERGENCY EXIT SIGN IAW AMM 33-51-00.
- [SDR SWAA2025122953763](https://openairdocs.org/sdr/SWAA2025122953763.md): Access Panel · damaged · Dec 19, 2025 · N8511K · Boeing 7378H4 · Wing, Plate/Skin
  > ACCESS PANEL 553ET FASTENER HOLE ELONGATED. LOCATED, DRILLED, AND INSTALLED A NEW ACCESS PANEL IAW SRM 51-40-02.
- [SDR SWAA2025122953304](https://openairdocs.org/sdr/SWAA2025122953304.md): Power Supply · inoperative · Dec 17, 2025 · N8511K · Boeing 7378H4 · Emergency Lighting
  > LEFT EMERGENCY EXIT LIGHT INOP IN CABIN AT BS639. R&R BATTERY PACK FOR POWER SUPPLY M1670 IAW AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2025122947265](https://openairdocs.org/sdr/SWAA2025122947265.md): Angle · cracked · Dec 9, 2025 · N8511K · Boeing 7378H4 · Wing Miscellaneous Structure
  > LEFT WING UPPER TRAILING EDGE ANGLE CRACKED, INBD OF MID SPAN DEFLECTION RIB. REMOVED THE CRACKED ANGLE IAW SRM 51-40-02. LOCATED, DRILLED, AND DEBURRED REPLACEMENT ANGLE IAW SRM 51-40-05.
- [SDR SWAA2025121844050](https://openairdocs.org/sdr/SWAA2025121844050.md): Angle · cracked · Dec 9, 2025 · N8511K · Boeing 7378H4 · Wing Miscellaneous Structure
  > LEFT WING UPPER TRAILING EDGE ANGLE FOUND CRACKED, INBD OF MID SPAN DEFLECTION RIB. REMOVED THE CRACKED ANGLE IAW SRM 51-40-02.
- [SDR SWAA2025122954889](https://openairdocs.org/sdr/SWAA2025122954889.md): Fitting · worn · Dec 2, 2025 · N8511K · Boeing 7378H4 · Wing Main, Frame Structure
  > LEFT WING TRAILING EDGE DEFLECTION RIB FITTING UPPER ATTACH POINTS HAS EXCESSIVE WARE AT BOLT HOLES. INSPECTED DEFLECTION CONTROL RIB UPPER TAB AND FOUND TO BE OUT-OF-LIMITS. CUT AND REMOVED DAMAGE ALL WORK IAW PER SRM 57-51-02-1A-1. NO CRACK INDICATIONS F
- [SDR SWAA2025122641508](https://openairdocs.org/sdr/SWAA2025122641508.md): Floor Panel · delaminated · Dec 2, 2025 · N8511K · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241AF TOP SURFACE DELAMINATED. R & R IAW AMM 53-21-00-400-801.
- [SDR SWAA2025122641510](https://openairdocs.org/sdr/SWAA2025122641510.md): Floor Panel · delaminated · Dec 2, 2025 · N8511K · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 232RF TOP SURFACE HAS SEVERAL DENTS AND DELAMINATION. R & R CABIN FLOOR PANEL 232RF IAW AMM 53-21-00.
- [SDR SWAA2025122641511](https://openairdocs.org/sdr/SWAA2025122641511.md): Floor Panel · delaminated · Dec 2, 2025 · N8511K · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231ZF DELAMINATED; TOP SURFACE HAS SEVERAL DENTS. R & R IAW AMM 53-21-00-400-801.
- [SDR SWAA2025122641512](https://openairdocs.org/sdr/SWAA2025122641512.md): Floor Panel · delaminated · Dec 2, 2025 · N8511K · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231XF TOP SURFACE HAS SEVERAL DENTS AND DELAMINATION. R & R IAW AMM 53-21-00-400-801.
- [SDR SWAA2025122641513](https://openairdocs.org/sdr/SWAA2025122641513.md): Floor Panel · delaminated · Dec 2, 2025 · N8511K · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 242AF DELAMINATED WITH SEVERAL DENTS TO TOP SURFACE. R & R CABIN FLOOR PANEL 242AF PER AMM 53-21-00.
- [SDR SWAA2025122641518](https://openairdocs.org/sdr/SWAA2025122641518.md): Floor Panel · delaminated · Dec 2, 2025 · N8511K · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241DF TOP SURFACE DELAMINATED. R & R THE FLOOR PANEL IAW AMM 53-21-00-400-801.
- [SDR SWAA2025122641519](https://openairdocs.org/sdr/SWAA2025122641519.md): Floor Panel · delaminated · Dec 2, 2025 · N8511K · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241FF DELAMINATED, TOP SURFACE HAS SEVERAL DENTS. R & R THE FLOOR PANEL IAW AMM 53-21-00-400-801.
- [SDR SWAA2025122641531](https://openairdocs.org/sdr/SWAA2025122641531.md): Floor Panel · delaminated · Dec 2, 2025 · N8511K · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 242CF DELAMINATED; TOP SURFACE HAS SEVERAL DENTS. R & R IAW AMM 53-21-00-400-801.
- [SDR SWAA2025122641532](https://openairdocs.org/sdr/SWAA2025122641532.md): Floor Panel · delaminated · Dec 2, 2025 · N8511K · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241BF TOP SURFACE DELAMINATED WITH SEVERAL DENTS. R & R THE CABIN FLOOR PANEL 241BF IAW AMM 53-21-00-401.
- [SDR SWAA2025121841964](https://openairdocs.org/sdr/SWAA2025121841964.md): Panel · damaged · Dec 2, 2025 · N8511K · Boeing 7378H4 · Wing, Plate/Skin
  > PANEL 551CB AFT SCREW HOLES HAVE PULL THROUGH DAMAGE.
- [SDR SWAA2025121841963](https://openairdocs.org/sdr/SWAA2025121841963.md): Panel · damaged · Dec 2, 2025 · N8511K · Boeing 7378H4 · Wing, Plate/Skin
  > PANEL 551BB AFT SCREW HOLES HAVE PULL THROUGH DAMAGE.
- [SDR SWAA2025122941322](https://openairdocs.org/sdr/SWAA2025122941322.md): Attach Angle · cracked · Dec 1, 2025 · N8511K · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACK FOUND ON BS 663 VAPOR BARRIER UPPER ATTACH ANGLE AT RBL 34. REMOVED THE VAPOR BARRIER ATTACH ANGLE IAW SRM 51-40-02. COMPLIED WITH OPEN HOLE INSPECTION FOR THE REMOVED ATTACH ANGLE IAW NDT MANUAL PART 6, 51-00-00, PROC 16. NO FAULTS FOUND. THE ATTACH A
- [SDR SWAA2025122947178](https://openairdocs.org/sdr/SWAA2025122947178.md): Attach Angle · cracked · Dec 1, 2025 · N8511K · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACK FOUND ON BS 663 VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 9. CUT OUT AND REMOVED CRACKED SECTION OF VAPOR BARRIER ANGLE IAW SRM 57-10-10-2R-5. COMPLIED WITH OPEN HOLE INSPECTION FOR THE REMOVED ATTACH ANGLE IAW NDT MANUAL PART 6; 51-00-00 PROC.16. NO F
- [SDR SWAA2025122941499](https://openairdocs.org/sdr/SWAA2025122941499.md): Attach Bracket · cracked · Dec 1, 2025 · N8511K · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > SEAT TRACK NR 1 ATTACH BRACKET HAD POSSIBLE CRACK AT RADUIS BS 727B. VERIFIED CRACK INDICATION PER NDT PART 6 51-00-00 PROCEDURE 23. REMOVED THE SEAT TRACK NR 1 ATTACH BRACKET IAW SRM 51-40-02. MATCHED DRILLED FASTENER HOLES IN SPLICE STRAP IAW SRM 51-40-0
- [SDR SWAA2025122941502](https://openairdocs.org/sdr/SWAA2025122941502.md): Attach Bracket · cracked · Dec 1, 2025 · N8511K · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > SEAT TRACK NR 4 ATTACH BRACKET HAS POSSIBLE CRACK AT RADUIS BS 727B. VERIFIED CRACK INDICATION PER NDT PART 6 51-00-00 PROCEDURE 23. REMOVED SEAT TRACK NR 4 ATTACH BRACKET SPLICE STRAP IAW SRM 51-40-02. MATCHED DRILLED FASTENER HOLES FOR THE NR 4 ATTACH BRA
- [SDR SWAA2025122941324](https://openairdocs.org/sdr/SWAA2025122941324.md): Angle · cracked · Dec 1, 2025 · N8511K · Boeing 7378H4 · Fuselage Main, Structure
  > CRACK FOUND ON BS 663 VAPOR BARRIER UPPER ATTACH ANGLE AT RBL 9. CUT OUT AND REMOVED CRACKED PORTION OF VAPOR BARRIER ANGLE PER SRM 57-10-10-2R-5. COMPLIED WITH OPEN HOLE INSPECTION FOR REMOVED ATTACH ANGLE IAW NDT MANUAL, PART 6, 51-00-00, PROC 16. NO FAUL
- [SDR SWAA2025121841323](https://openairdocs.org/sdr/SWAA2025121841323.md): Attach Angle · cracked · Dec 1, 2025 · N8511K · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACK FOUND ON BS 663 VAPOR BARRIER UPPER ATTACH ANGLE, LBL 9. CUT OUT AND REMOVED THE CRACKED SECTION OF THE ATTACH ANGLE IAW SRM 57-10-10-2R-5. COMPLIED WITH OPEN HOLE INSPECTION FOR THE REMOVED ATTACH ANGLE IAW NDT MANUAL, PART 6, 51-00-00, PROC 16. NO
- [SDR SWAA2025110630690](https://openairdocs.org/sdr/SWAA2025110630690.md): Slide · unpacked · Oct 31, 2025 · N8511K · Boeing 7378H4 · Escape Slide
  > FWD SERVICE DOOR SLIDE NEEDS TO BE REPACKED. REPACKED FSD SLIDER PER MT 725-61-06 FS ON CARD TTG8Q01758XW.
- [SDR SWAA2025110329991](https://openairdocs.org/sdr/SWAA2025110329991.md): Light · inoperative · Oct 29, 2025 · N8511K · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE AT LT SIDE AFT EMERGENCY EXIT DOOR LOWER SIDE. RELAMPED AND PERFORMED GOOD TEST OF EMERGENCY LIGHT AT LH SIDE AFT EMERGENCY EXIT DOOR LOWER SIDE IAW AMM 33-51-01-960-801.
- [SDR SWAA2025103129658](https://openairdocs.org/sdr/SWAA2025103129658.md): Lamp · inoperative · Oct 29, 2025 · N8511K · Boeing 7378H4 · Emergency Lighting
  > AFT ENTRY DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. RELAMPED AFT ENTRY DOOR EMERGENCY SLIDE LIGHT AND PERFORMED A GOOD OPERATIONAL TEST OF NEWLY INSTALLED LAMP IAW AMM 33-51-04-960-801.
- [SDR SWAA2025103129408](https://openairdocs.org/sdr/SWAA2025103129408.md): Battery Pack · no test · Oct 28, 2025 · N8511K · Boeing 7378H4 · Emergency Lighting
  > ALL EMERGENCY LIGHTS RELATED TO BATTERIES PACK M1670 AND M1671 FAILED TO TEST. PERFORMED GOOD DEEP CYCLE AND FUNCTIONAL TEST OF EMERGENCY BATTERY PACK M1670 IAW AMM 33-51-06-600-802. REMOVED & REPLACED WITH SERVICEABLE UNIT AND PERFORMED GOOD INSTALLATION T
- [SDR SWAA2025051971535](https://openairdocs.org/sdr/SWAA2025051971535.md): Extinguisher · faulty · May 15, 2025 · N8511K · Boeing 737824 · Fire Bottle, Portable
  > SHARP ACRID SMELL IN FWD GALLEY FIRE EXT COMPARTMENT<[01] REMOVED FWD GALLEY FIRE EXT. CONTENTS AND CLEANED COMPARTMENT. REM & REP. FWD FIRE EXT. DUE TO POSSIBLE LEAKING PER AMM 26-26-02
- [SDR SWAA2025050266318](https://openairdocs.org/sdr/SWAA2025050266318.md): Flashlight · no test · May 1, 2025 · N8511K · Boeing 7378H4 · Emergency Equipment
  > AFT CABIN INBOARD FLASHLIGHT HAS NO GREEN LIGHT. DOES NOT TEST<[01] R/R AFT CABIN I/B FLASHLIGHT BATTERY IAW AMM 25-64-00 FUNCTIONAL CHECK OK. THIS CLEARS MEL
- [SDR SWAA2024112558850](https://openairdocs.org/sdr/SWAA2024112558850.md): Intercostal · cracked · Nov 11, 2024 · N8511K · Boeing 7378H4 · Fuselage Main, Structure
  > DOT A24-70 MID CABIN FLOOR INTERCOSTAL AT STATION 540 IS CRACKED AT RBL 3 AND RBL 22.<[01] REMOVED CRACKED MID CABIN FLOOR INTERCOSTAL AT STATION 540 AT RBL 3 AND RBL 22 AND REPLACED WITH NEW MID CABIN FLOOR INTERCOSTAL; PN 143A5240-64 ATAG WN48865; IAW SRM 51
- [SDR SWAA2024112158852](https://openairdocs.org/sdr/SWAA2024112158852.md): Floor Panel · pulled · Nov 11, 2024 · N8511K · Boeing 7378H4 · Fuselage Floor Panel
  > DOT A24-71 MID CABIN FLOOR PANEL 231XF HAS MULTIPLE PULLED FIBERS ON UPPER SURFACE.<[01] REPLACED BY FABRICATION MID CABIN FLOOR PANEL 231XF IAW SRM 53-00-50-2R-0; REPAIR GENERAL AND DWG 144A5810-126. INSTALLED INSERTS IAW BAC5085 CHAPTER 8.4 AND SAMPLE.;[02]
- [SDR SWAA2024112158853](https://openairdocs.org/sdr/SWAA2024112158853.md): Floor Panel · pulled · Nov 11, 2024 · N8511K · Boeing 7378H4 · Fuselage Floor Panel
  > DOT A24-72 MID CABIN FLOOR PANEL 241DF HAS MULTIPLE PULLED FIBERS ON UPPER SURFACE.<[01] REPLACED BY FABRICATION MID CABIN FLOOR PANEL 241DF IAW SRM 53-00-50-2R-0 REPAIR GENERAL; DWG 144A5810-128; BAC5085 AND SAMPLE.;[02] AUDIT
- [SDR SWAA2024112557853](https://openairdocs.org/sdr/SWAA2024112557853.md): Scuff Plate · cracked · Nov 7, 2024 · N8511K · Boeing 7378H4 · Cargo Compartments
  > AFT CARGO DOOR FWD CORNER SCUFF PLATE IS CRACKED<[01] CRACK ON AFT CARGO DOOR CUTOUT; FWD CORNER SCUFF PLATE WAS REPAIRED ON BACK SHOP W/O 46206/1600/0001 SERIAL NO. 9468658 IAW SRM 53-60-15-2R-1;[02] VERIFIED ITEM 1<BR>AUDIT C/W
- [SDR SWAA2024112155765](https://openairdocs.org/sdr/SWAA2024112155765.md): Baffle · cracked · Nov 1, 2024 · N8511K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > DOT#18 A-043 FWD CARGO COMPARTMENT BAFFLE; BETWEEN STA 500B / 500C LBL 22 WL 156 CRACKED<[01] REMOVED AND REPLACED BAFFLE ON FWD CARGO COMPARTMENT BETWEEN STA 500B / 500C LBL 22 WL 156 I.A.W. DWG NO. 143A7505 REV:- AND SRM 51-40-02-0G-0;[02] AUDIT C/W
- [SDR SWAA2024112155764](https://openairdocs.org/sdr/SWAA2024112155764.md): Baffle · cracked · Nov 1, 2024 · N8511K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > DOT#19 A-043 FWD CARGO COMPARTMENT BAFFLE; BETWEEN STA 500C / 500D RBL 22 WL 156 CRACKED<[01] REMOVED AND REPLACED (INSTALLED) ON FWD CARGO COMPARTMENT BAFFLE; BETWEEN STA 500C / 500D RBL 22 WL 156 I.A.W SRM 51-40-02-0G-0 AND DWN: 143A7505 REV: -;[02] VERIFIED
- [SDR SWAA2024112156004](https://openairdocs.org/sdr/SWAA2024112156004.md): Baffle · cracked · Nov 1, 2024 · N8511K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT BAFFLE; BETWEEN STA 500D / 500E LBL 22 WL 156 CRACKED<[01] REMOVED AND REPLACED BAFFLED ON FWD CARGO COMPARTMENT BETWEEN STA 500D / 500E LBL 22 WL 156 I.A.W. SRM 51-40-02-0G-0 AND DWG NO. 143A7505 REV:-;[02] AUDIT C/W
- [SDR SWAA2024112155337](https://openairdocs.org/sdr/SWAA2024112155337.md): Angle · corroded · Oct 31, 2024 · N8511K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > DOT#17 A-043 AFT CARGO COMPARTMENT INTERCOSTAL CORRODED UNDER 'Z' ANGLE AT STA 747 TO 767 RBL 22 WL 156<[01] 01 - REMOVED AND REPLACED PER [SRM 53-00-53-1A-2-B00297 (PERMANENT (NON-DENT DAMAGE TYPES))];[02] VERIFIED STEP 1<BR>AUDIT CW
- [SDR SWAA2024112155615](https://openairdocs.org/sdr/SWAA2024112155615.md): Retainer · missing · Oct 31, 2024 · N8511K · Boeing 7378H4 · Escape Slide
  > G4 GALLEY DOOR OUTBD SLIDE RETAINER MISSING.<[01] INSTALLED NEW SLIDE RETAINER ON G-4 GALLEY; 4B-26 IAW CMM 25-31-76 IPL FIG. 24 PG. 10029-1 <BR><BR> A-TAGS: A272008; A35210;[02] VERIFIED TASK COMPLETE<BR><BR>AUDIT C/W
- [SDR SWAA2024112155616](https://openairdocs.org/sdr/SWAA2024112155616.md): Retainer · missing · Oct 31, 2024 · N8511K · Boeing 7378H4 · Escape Slide
  > G4 GALLEY DOOR 4B-24 INBD SLIDE RETAINER MISSING.<[01] INSTALLED NEW INBD SLIDE RETAINER IAW CMM 25-31-76 IPL FIG. 24 PG. 10029-1 <BR><BR> A-TAGS: A35210; A272007;[02] VERIFIED TASK COMPLETE<BR><BR>AUDIT C/W
- [SDR SWAA2024112155169](https://openairdocs.org/sdr/SWAA2024112155169.md): Floor Panel · corroded · Oct 30, 2024 · N8511K · Boeing 7378H4 · Fuselage Floor Panel
  > (A125) CARGO FLOOR PANEL 140CF CORRODED AROUND PERIMETER<[01] UPON FURTHER INVESTIGATION FOUND THERE TO BE 48 INCHES OF CORROSION WITH A MAX ALLOWED LENGTH OF 3 INCHES PERMITTED FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 RECEIVED REPLACEMENT MATERIAL PART
- [SDR SWAA2024112155170](https://openairdocs.org/sdr/SWAA2024112155170.md): Floor Panel · corroded · Oct 30, 2024 · N8511K · Boeing 7378H4 · Fuselage Floor Panel
  > (A125) CARGO FLOOR PANEL 120CF CORRODED AROUND PERIMETER<[01] FOUND DAMAGE ON PNL # 120CF OUT OF LIMITS; FABRICATED NEW FLOOR PNL # 120CF USING 2024-T3-071; ATAG# A257728 ALODINED AND PRIMED. IAW AMM 25-52-01-201-801; AMM 51-21-41-370-802; AMM 51-21-72-370-804
- [SDR SWAA2024112155171](https://openairdocs.org/sdr/SWAA2024112155171.md): Floor Panel · corroded · Oct 30, 2024 · N8511K · Boeing 7378H4 · Fuselage Floor Panel
  > (A125) CARGO FLOOR PANEL 120AF CORRODED AROUND PERIMETER<[01] CORROSION EVALUATED; TOTAL ACCUMULATED CORROSOIN DAMAGE IS GREATER THAN THE ALLOWABLE 20'; OUT OF LIMITS IAW SRM 53-00-53-1A-1. MATERIAL FOR FABRICATION OF NEW PNL VERIFIED;.071' 2024-T3; IAW SRM 5
- [SDR SWAA2024112155172](https://openairdocs.org/sdr/SWAA2024112155172.md): Floor Panel · corroded · Oct 30, 2024 · N8511K · Boeing 7378H4 · Fuselage Floor Panel
  > (A125) CARGO FLOOR PANEL 120DF CORRODED AROUND PERIMETER<[01] UPON FURTHER INVESTIGATION FOUND A TOTAL OF 80 INCHES OF CORROSION WITH A MAX ALLOWED LENGTH OF 3 INCHES FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 RECEIVED REPLACEMENT MATERIAL PN 2024-T3-071
- [SDR SWAA2024112554560](https://openairdocs.org/sdr/SWAA2024112554560.md): Web · corroded · Oct 29, 2024 · N8511K · Boeing 7378H4 · Cargo Compartments
  > DOT#02 A-043 AFT CARGO COMPARTMENT DOOR CUTOUT SILL WEB CORRODED AT STA 787+10' TO 827+8' RBL 24 WL 156<[01] 01 - REMOVED AND REPLACED SILL WEB ON AFT CARGO COMPARTMENT DOOR CUTOUT PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AI
- [SDR SWAA2024112554764](https://openairdocs.org/sdr/SWAA2024112554764.md): Gusset · cracked · Oct 29, 2024 · N8511K · Boeing 7378H4 · Cargo Compartments
  > DOT#16 A-043 FWD CARGO COMPARTMENT GUSSET CRACKED AT STA 500I STR 18R<[01] REMOVED AND REPLACED (INSTALLED) ON FWD CARGO COMPARTMENT GUSSET AT STA 500I STR 18R I.A.W SRM 51-40-02-0G-0 AND DWG: 143A7902 REV.B AND APPLIED CIC I.A.W AMM 51-21-91-620-802.;[02] AUD
- [SDR SWAA2024112154761](https://openairdocs.org/sdr/SWAA2024112154761.md): Angle · corroded · Oct 29, 2024 · N8511K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > DOT#14 A-043 FWD CARGO COMPARTMENT LH 'Z' ANGLE CORRODED STA 500+4' TO 500H+7' LBL 22 WL 156<[01] REMOVED; FABRICATED AND INSTALLED REPAIR PARTS LH 'Z' ANGLE STA 480+8.5' TO 500I; WITH TWO SPLICE SIDEPLATE. THE FIRST LOCALIZED ON STA 480+8.5' AND THE SECOND ON
- [SDR SWAA2024112154757](https://openairdocs.org/sdr/SWAA2024112154757.md): Shield · corroded · Oct 29, 2024 · N8511K · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > DOT#11 A-043 FWD CARGO COMPARTMENT AFT SHIELD CORRODED STA 480+12' TO 500A RBL 22 WL 156<[01] FWD CARGO COMPARTMENT AFT SHIELD FROM STA 480+12' TO 500A AND RBL 22 WL 156 WAS REMOVED AND REPLACED I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 143A0080 REV:-;[02] VERIF

Next page: https://openairdocs.org/aircraft/N8511K/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 = 'N8511K' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8511K/reports

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