# Service difficulty reports: N8684F

A list on [N8684F](https://openairdocs.org/aircraft/N8684F.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 3 · 101 reports

- [SDR SWAA2026032683505](https://openairdocs.org/sdr/SWAA2026032683505.md): Unknown · odor · Mar 26, 2026 · N8684F · Boeing 7378H4 · Air Distribution System
  > FLIGHT ATTENDANTS REPORTED BURNING WIRE SMELL IN AFT GALLEY NO VISIBLE SMOKE; SMELL PERSISTED THROUGHOUT FLIGHT<[01] PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-56; RAN BOTH PACKS; PERFORMED OPS TEST OF DOOR HEATERS PER 21-45-01; WITH ALL LIGHTS ILLUMINATED
- [SDR SWAA2026010557659](https://openairdocs.org/sdr/SWAA2026010557659.md): Tray · broken · Jan 2, 2026 · N8684F · Boeing 7378H4 · Passenger Compartment Equipment
  > TRAY TABLE BROKEN ROW 14A. RE-INSTALLED TRAY TABLE 14A OTBD ARM TO TABLE PER CMM 25-22-46.
- [SDR SWAA2025121652125](https://openairdocs.org/sdr/SWAA2025121652125.md): Lens · detached · Dec 12, 2025 · N8684F · Boeing 7378H4 · Emergency Lighting
  > OVERWING EXIT LIGHT LENS FELL OFF. INSTALLED THE LENS IAW 33-51-01.
- [SDR SWAA2025082708003](https://openairdocs.org/sdr/SWAA2025082708003.md): Lamp · inoperative · Aug 25, 2025 · N8684F · Boeing 7378H4 · Emergency Lighting
  > RIGHT AFT OVERWING EMERGENCY EXIT LIGHT LAMP OUT. RELAMPED RT AFT OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-51-04.
- [SDR SWAA2025062484547](https://openairdocs.org/sdr/SWAA2025062484547.md): Transmitter · inoperative · Jun 22, 2025 · N8684F · Boeing 7378H4 · Trailing Edge Flap Control System
  > TRAILING EDGE FLAP /DISAGREE /ASYMMETRY TRAILING EDGE FLAP DISAGREE / ASYMMETRY <1<[01] ALT FLAP SWITCH USED SWITCH TO DRIVE FLAPS DOWN;SWITCH IN COCKPIT NOT SAFTY WIRED;[02] CREW REPORTS PSEU LIGHT ILLUMINATED ON LANDING ( FAULT CODES 32-62009;32-62010) ON A
- [SDR SWAA2025061079867](https://openairdocs.org/sdr/SWAA2025061079867.md): Transmitter · malfunctioned · Jun 9, 2025 · N8684F · Boeing 7378H4 · Trailing Flap Position Indicating System
  > DURING APP AT MDW WHEN SELECTING FLAPS 5; WE GOT A SPLIT FLAP; RAN QRH PER OPPS T427 IS LAGGING ON AHM FSEU BITE FC 27-53279 CONFIRMED NO CB TRIPPED<[01] REMOVED AND REPLACED LT FLAP POSITION TRANSMITTER PER M/M 27-58-01
- [SDR SWAA2025051265576](https://openairdocs.org/sdr/SWAA2025051265576.md): Fairing · damaged · Apr 29, 2025 · N8684F · Boeing 7378H4 · Trailing Edge Flaps
  > #6 CANOE FAIRING HAS ELONGATED SEAL FASTENER HOLES.<[01] A NEW #6 CANOE FAIRING WAS ORDERED FOR A/C. NEW CANOE FAIRING WILL BE INSTALLED ON FAULT # TTG8Q00ZVLVW.;[02] C/W
- [SDR SWAA2025051265004](https://openairdocs.org/sdr/SWAA2025051265004.md): Seal · cracked · Apr 28, 2025 · N8684F · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > RT STAB UPPER FWD SLIDING SEAL ON FUSELAGE CRACKED.<[01] REMOVED RH HORIZONTAL UPPER FWD SLIDING SEAL PER AMM 53-31-31.;[02] REPLACED RH HORIZONTAL UPPER FWD SLIDING SEAL PER AMM 53-31-31.;[03] 02 - INSPECTED PER [AMM 53-31-31-401 CONFIG 2-NG (STABILIZER TO BO
- [SDR SWAA2025051264513](https://openairdocs.org/sdr/SWAA2025051264513.md): Battery Pack · inoperative · Apr 27, 2025 · N8684F · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT EXTERNAL OF AFT R/H OVERWING EXIT WILL NOT ILLUMINATE.<[01] REMOVED AND REPLACED BATTERY PACK M1671 PER AMM 33-51-06. NO FAULTS NOTED.;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR BATTERY PACK REPLACEMENT.
- [SDR SWAA2025051264670](https://openairdocs.org/sdr/SWAA2025051264670.md): Battery Pack · inoperative · Apr 27, 2025 · N8684F · Boeing 7378H4 · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHTS BATTERY PACK INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1694 AT STA 565L PER MM 33-51-06;[02] LEFT OVERWING EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[03] 02 - INSPECTED PER [AMM 33-51-06-960-805-NG (POW
- [SDR SWAA2025051264671](https://openairdocs.org/sdr/SWAA2025051264671.md): Battery Pack · inoperative · Apr 27, 2025 · N8684F · Boeing 7378H4 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK M1695 AT STA 565R IS INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1695 AT STA 565R PER MM33-51-06;[02] RIGHT OVERWING EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[03] 02 - INSPECTED PER [AMM 33-
- [SDR SWAA2025051251405](https://openairdocs.org/sdr/SWAA2025051251405.md): Support Angle · cracked · Apr 22, 2025 · N8684F · Boeing 7378H4 · Wing Miscellaneous Structure
  > R/H WING TRAILING EDGE UPPER SHELF PANEL SUPPORT ANGLE INBD OF DEFLECTION CONTROL RIB CRACKED<[01] LOCATED AND DRILLED NEW FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05.;[02] INSPECTED LOCATION AND DRILLING OF NEW FASTENER HOLES IN NEW SUPPORT ANGLE PER
- [SDR SWAA2025050526851](https://openairdocs.org/sdr/SWAA2025050526851.md): Angle · cracked · Apr 22, 2025 · N8684F · Boeing 7378H4 · Wing Miscellaneous Structure
  > R/H WING TRAILING EDGE UPPER SHELF PANEL SUPPORT ANGLE INBD OF DEFLECTION CONTROL RIB CRACKED<[01] LOCATED AND DRILLED NEW FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05.;[02] INSPECTED LOCATION AND DRILLING OF NEW FASTENER HOLES IN NEW SUPPORT ANGLE PER
- [SDR SWAA2025050535622](https://openairdocs.org/sdr/SWAA2025050535622.md): Support Angle · cracked · Apr 22, 2025 · N8684F · Boeing 7378H4 · Wing Miscellaneous Structure
  > R/H WING TRAILING EDGE UPPER SHELF PANEL SUPPORT ANGLE INBD OF DEFLECTION CONTROL RIB CRACKED<[01] LOCATED AND DRILLED NEW FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05.;[02] INSPECTED LOCATION AND DRILLING OF NEW FASTENER HOLES IN NEW SUPPORT ANGLE PER
- [SDR SWAA2025050751397](https://openairdocs.org/sdr/SWAA2025050751397.md): Attach Bracket · cracked · Apr 19, 2025 · N8684F · Boeing 7378H4 · Wing, Attach Fittings
  > RIGHT WING CONDUIT BRACKET ABOVE AND AFT OF MLG MAIN RETRACT ACTUATOR LOWER ATTACH POINT MOUNT IS CRACKED.<[01] INFO: WORK WITH FAULT ID TTG8Q00ZUZDG AS THIS IS WHERE THE OTHER HALF OF THE SAME BRACKET IS WRITTEN UP.;[02] REFERENCE TASK CARD LINE # 1177; R/H W
- [SDR SWAA2025050526424](https://openairdocs.org/sdr/SWAA2025050526424.md): Bracket · cracked · Apr 19, 2025 · N8684F · Boeing 7378H4 · Wing Miscellaneous Structure
  > RIGHT WING CONDUIT BRACKET ABOVE AND AFT OF MLG MAIN RETRACT ACTUATOR LOWER ATTACH POINT MOUNT IS CRACKED.<[01] INFO: WORK WITH FAULT ID TTG8Q00ZUZDG AS THIS IS WHERE THE OTHER HALF OF THE SAME BRACKET IS WRITTEN UP.;[02] REFERENCE TASK CARD LINE # 1177; R/H W
- [SDR SWAA2025050535614](https://openairdocs.org/sdr/SWAA2025050535614.md): Bracket · cracked · Apr 19, 2025 · N8684F · Boeing 7378H4 · Wing Miscellaneous Structure
  > RIGHT WING CONDUIT BRACKET ABOVE AND AFT OF MLG MAIN RETRACT ACTUATOR LOWER ATTACH POINT MOUNT IS CRACKED.<[01] INFO: WORK WITH FAULT ID TTG8Q00ZUZDG AS THIS IS WHERE THE OTHER HALF OF THE SAME BRACKET IS WRITTEN UP.;[02] REFERENCE TASK CARD LINE # 1177; R/H W
- [SDR SWAA2025051251345](https://openairdocs.org/sdr/SWAA2025051251345.md): Bracket · cracked · Apr 14, 2025 · N8684F · Boeing 7378H4 · Wing, Attach Fittings
  > LT WING CONDUIT BRACKET ABOVE AND AFT OF MLG MAIN RETRACT ACTUATOR CRACKED. SEE ATTACHED PICS.<[01] REMOVED AND REPLACED CONDUIT BRACKET. IAW SRM 51-40-02;[02] 02 - INSPECTED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME
- [SDR SWAA2025051251332](https://openairdocs.org/sdr/SWAA2025051251332.md): Support Bracket · corroded · Apr 12, 2025 · N8684F · Boeing 7378H4 · Wing Miscellaneous Structure
  > R/H WING L/E FUELING GAUGES SUPPORT BRACKET HAS SEVERAL AREAS OF SURFACE CORROSION. MRKD<[01] REMOVED AND REPLACED R/H WING L/E REFUELING GAUGES SUPPORT BRACKET (P15 PANEL) PER AMM 28-21-00.;[02] INSPECTION C/W C/A #1;[03] REQUIRES INSTALLATION TEST PER AMM 28
- [SDR SWAA2025050523404](https://openairdocs.org/sdr/SWAA2025050523404.md): Attach Angle · cracked · Apr 10, 2025 · N8684F · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT RBL 34<[01] REMOVED BS 63 R/H VAPOR BARRIER ANGLE PER SRM 51-40-02.;[02] MATCH DRILLED NEW ANGLE PER SRM 51-40-02. NEED OK TO INSTALL.;[03] C/W INSPECTION OF CA # 1-2. OK TO INSTALL;[04] INSTALLED FASTENERS COMMON T
- [SDR SWAA2025050535537](https://openairdocs.org/sdr/SWAA2025050535537.md): Attach Angle · cracked · Apr 10, 2025 · N8684F · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT RBL 34. REMOVED BS 63 R/H VAPOR BARRIER ANGLE PER SRM 51-40-02. MATCH DRILLED NEW ANGLE PER SRM 51-40-02. INSTALLED FASTENERS COMMON TO FUEL TANK ON VAPOR BARRIER ATTACH ANGLE PER SRM 51-40-02 & DWG 111A1000.
- [SDR SWAA2024121777031](https://openairdocs.org/sdr/SWAA2024121777031.md): Sign · broken · Dec 13, 2024 · N8684F · Boeing 7378H4 · Emergency Lighting
  > OVERHEAD EMERGENCY EXIT SIGN AT OVERNIGHT EXITS BROKEN.<[01] REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT SIGN ASSY AT OVERWING EXITS IAW AMM 33-51-01. OP CHECKS GOOD.
- [SDR SWAA2024101748765](https://openairdocs.org/sdr/SWAA2024101748765.md): Cover · missing · Oct 14, 2024 · N8684F · Boeing 7378H4 · Emergency Lighting
  > CENTER AISLE FORWARD EXIT LOCATOR SIGN MISSING<[01] INSTALLED MISSING LENSE COVER PER SIP
- [SDR SWAA2024100744089](https://openairdocs.org/sdr/SWAA2024100744089.md): Sign · broken · Oct 1, 2024 · N8684F · Boeing 7378H4 · Emergency Lighting
  > CENTER EMERGENCY EXIT SIGN BROKEN<[01] REPLACED CENTER EMER EXIT SIGN LENS PER M/M 33-51-01.
- [SDR SWAA2024081325122](https://openairdocs.org/sdr/SWAA2024081325122.md): Cover · detached · Aug 10, 2024 · N8684F · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT CEILING MOUNTED COVER FELL OFF<[01] REINSTALLED COVER PER SIP
- [SDR SWAA2024071814095](https://openairdocs.org/sdr/SWAA2024071814095.md): Lens · loose · Jul 18, 2024 · N8684F · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT ROW SIGN ON OVHD LENS FELL OFF<[01] REINSTALLED OVERWING EXIT SIGN LENS IAW AMM 33-51-01. A/C OK FOR SERVICE
- [SDR SWAA2024070106909](https://openairdocs.org/sdr/SWAA2024070106909.md): Bracket · broken · Jun 28, 2024 · N8684F · Boeing 7378H4 · Emergency Lighting
  > MID CABIN EXIT SIGN BRACKET BROKEN<[01] RESECURED MID CABIN EXIT SIGN LENS PER MM 33-51-03; OPS CK GOOD
- [SDR SWAA2024050279621](https://openairdocs.org/sdr/SWAA2024050279621.md): Light · broken · Apr 27, 2024 · N8684F · Boeing 7378H4 · Emergency Lighting
  > FWD LAV A EXIT LIGHT IS BROKEN.<[01] REMOVED AND REPLACED FWD LAV A EXIT LIGHT PER SOPM 20-50-01.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024050276757](https://openairdocs.org/sdr/SWAA2024050276757.md): Floorbeam · corroded · Apr 18, 2024 · N8684F · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON AFT WET AREA FLOOR BEAM AT BS 947; RBL 23; WL 208.<[01] REMOVED DAMAGED SECTION AND ACCOMPLISHED REPAIR OF FLOOR BEAM AT BS 947 RBL 8.5' TO RBL 41.7' WL 208; PER SRM 53-70-51-2R-5; REPAIR 5.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED ME
- [SDR SWAA2024050776755](https://openairdocs.org/sdr/SWAA2024050776755.md): None · none · Apr 17, 2024 · N8684F · Boeing 7378H4 · Standard Practices/Structures
  > REMOVE AND REINSTALL RIGHT ELEVATOR FOR PAINT<[01] REMOVED AND REINSTALLED RH ELEVATOR IAW AMM 27-31-11-400-801. SEE PREVIOUS STEPS TO VERIFY.
- [SDR SWAA2024050776754](https://openairdocs.org/sdr/SWAA2024050776754.md): None · none · Apr 17, 2024 · N8684F · Boeing 7378H4 · Ailerons
  > REMOVE AND REINSTALL LEFT ELEVATOR FOR PAINT<[01] REMOVED AND REINSTALLED LH ELEVATOR IAW AMM 27-31-11-400-801. SEE PREVIOUS STEPS TO VERIFY.
- [SDR SWAA2024050676437](https://openairdocs.org/sdr/SWAA2024050676437.md): Bracket · cracked · Apr 17, 2024 · N8684F · Boeing 7378H4 · Service Doors
  > BOTH BRACKETS CRACKED ON ASD PANEL 844DZ<[01] REPLACED BOTH FWD AND AFT BRACKETS ON ASD PANEL 844DZ PER SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
- [SDR SWAA2024050276423](https://openairdocs.org/sdr/SWAA2024050276423.md): Floor Panel · delaminated · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241GF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED FLOOR PANEL 241GF PER AMM 53-21-00-000-801;[02] REQUEST OK TO CLOSE;[03] INSTALLED PANEL 241GF PER AMM 53-21-00-400-801;[04] CAL TOOL 35 IN-LB SCREW GUN<BR>ID: ATS3017<BR>DUE DATE: 0
- [SDR SWAA2024050276424](https://openairdocs.org/sdr/SWAA2024050276424.md): Floor Panel · delaminated · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242HF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 242HF PER AMM 53-21-00-000-801;[02] REQUEST OK TO CLOSE;[03] OK TO CLOSE GRANTED;[04] INSTALLED PANEL 242HF PER AMM 53-21-00-400-801;[05] CAL TOOL 35 IN-LB SCREW GUN<BR>ID: ATS
- [SDR SWAA2024050276426](https://openairdocs.org/sdr/SWAA2024050276426.md): Floor Panel · delaminated · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242GF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 242GF PER AMM 53-21-00-000-801;[02] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242GF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[03] VERIFIED ITEM 2.;[04] REQUEST OK TO CLOSE;[0
- [SDR SWAA2024050276427](https://openairdocs.org/sdr/SWAA2024050276427.md): Floor Panel · delaminated · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242MF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 242MF PER AMM 53-21-00-000-801;[02] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242MF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[03] VERIFIED CORRECTIVE ACTION 2.;[04] REQUEST O
- [SDR SWAA2024050276425](https://openairdocs.org/sdr/SWAA2024050276425.md): Floor Panel · delaminated · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242NF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 242NF PER AMM 53-21-00-000-801;[02] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242NF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[03] VERIFIED CORRECTIVE ACTION 2.;[04] REQUEST O
- [SDR SWAA2024050276428](https://openairdocs.org/sdr/SWAA2024050276428.md): Floor Panel · delaminated · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241MF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 241MF PER AMM 53-21-00-000-801;[02] REQUEST OK TO CLOSE;[03] INSTALLED PANEL 241MF PER AMM 53-21-00-400-801;[04] INSTALLED PANEL 241MF PER AMM 53-21-00-400-801 <BR>CAL TOOL 35
- [SDR SWAA2024050276422](https://openairdocs.org/sdr/SWAA2024050276422.md): Floor Panel · delaminated · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231KF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 231KF PER AMM 53-21-00-000-801;[02] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 231KF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[03] VERIFIED CORRECTIVE ACTION ITEM 2.;[04] SELE
- [SDR SWAA2024050276080](https://openairdocs.org/sdr/SWAA2024050276080.md): Floor Support · cracked · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FWD FLOOR SUPPORT IS CRACKED AT BS 380-400; LBL 52; WL 208.<[01] REMOVED AND REPLACED FLOOR SUPPORT TOP ANGLE AT STA 380-400; LBL 52; WL 208 PER SRM 51-40-02-0G-0; PARAGRAPHS 4 AND 7; REFERENCING BOEING DWG 142A5400; SHEET 183; REV - DATED 03/2
- [SDR SWAA2024050276436](https://openairdocs.org/sdr/SWAA2024050276436.md): Floor Support · cracked · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FWD FLOOR SUPPORT IS CRACKED AT BS 380-400; LBL 1; WL 208.<[01] REMOVED AND REPLACED FLOOR SUPPORT TOP ANGLE AT STA 380-400; LBL 1; WL 208 PER SRM 51-40-02-0G-0; PARAGRAPHS 4 AND 7; REFERENCING BOEING DWG 143A5400; SHEET 154.;[02] VERIFIED CORR
- [SDR SWAA2024050276431](https://openairdocs.org/sdr/SWAA2024050276431.md): Floor Support · cracked · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FWD FLOOR SUPPORT IS CRACKED AT BS 380-400; LBL 13; WL 208.<[01] REMOVED AND REPLACE PASSENGER CABIN FWD FLOOR SUPPORT AT BS 380-400; LBL 13; WL 208 PER SRM 51-40-02; SRM 51-40-05; AND DWG#143A5400.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024050276064](https://openairdocs.org/sdr/SWAA2024050276064.md): Sidewall Support · corroded · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500A TO BS500I RBL22 WL156<[01] REMOVED FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE; LOCATED; DRILLED AND INSTALLED NEW FWD CARGO BAY R/H FLOOR TO SIDEWAL
- [SDR SWAA2024050276065](https://openairdocs.org/sdr/SWAA2024050276065.md): Shield · corroded · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY AFT SHIELD BS500+1 TO BS500+19 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] REMOVED FWD CARGO BAY AFT SHIELD; LOCATED; DRILLED AND INSTALLED NEW FWD CARGO BAY AFT SHIELD IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 143
- [SDR SWAA2024050276066](https://openairdocs.org/sdr/SWAA2024050276066.md): Sidewall Support · corroded · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500D+6' TO BS500I LBL22 WL156<[01] ' THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550'.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024050276434](https://openairdocs.org/sdr/SWAA2024050276434.md): Web · corroded · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS794 TO BS847 RBL 26 WL156<[01] REMOVED AFT CARGO BAY SUB THRESHOLD WEB; LOCATED; DRILLED AND INSTALLED NEW AFT CARGO BAY SUB THRESHOLD WEB IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-
- [SDR SWAA2024050276429](https://openairdocs.org/sdr/SWAA2024050276429.md): Sidewall Support · corroded · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727H+21' TO BS807+3' LBL22 WL156<[01] REMOVED DAMAGED SECTION OF FLOOR TO SIDEWALL SUPPORT; LOCATED AND DRILLED NEW SIDEWALL SUPPORT PLATE AND REPAIR PARTS (BS7
- [SDR SWAA2024050276435](https://openairdocs.org/sdr/SWAA2024050276435.md): Sidewall Support · corroded · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] REMOVED AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE; LOCATED; DRILLED AND INSTALLED NEW AFT CARGO BAY R/H FLOOR TO SIDE
- [SDR SWAA2024050276430](https://openairdocs.org/sdr/SWAA2024050276430.md): Shield · corroded · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] REMOVED AFT CARGO BAY SHIELD FWD OF CARGO DOOR; LOCATED; DRILLED AND INSTALLED NEW AFT CARGO BAY SHIELD FWD OF CARGO DOOR IAW SRM 51-40-05-0G-0;
- [SDR SWAA2024050276441](https://openairdocs.org/sdr/SWAA2024050276441.md): Strap · corroded · Apr 17, 2024 · N8684F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY FLOOR T STRAP BS 727I+5 RBL 16 TO LBL 16 WL 156<[01] RECEIVED NEW AFT CARGO BAY FLOOR T STRAP BS 727I+5 RBL 16 TO LBL 16 WL 156 ON PO # 968983 INSTALL WILL BE ON CARD # TTG8Q00S3YLY;[02] VERIFIED CORRECTIVE ACTION 1.

Next page: https://openairdocs.org/aircraft/N8684F/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 = 'N8684F' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8684F/reports

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