# Service difficulty reports: N8320J

A list on [N8320J](https://openairdocs.org/aircraft/N8320J.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 · 139 reports

- [SDR SWAA2026092320213](https://openairdocs.org/sdr/SWAA2026092320213.md): Sign · broken · Sep 19, 2026 · N8320J · Boeing 7378H4 · Emergency Lighting
  > MID CABIN OVERHEAD EXIT SIGN BROKEN. SECURED THE OVERWING EXIT SIGN IAW AMM 33-51-01
- [SDR SWAA2026091473762](https://openairdocs.org/sdr/SWAA2026091473762.md): Hydraulic Line · leaking · Sep 10, 2026 · N8320J · Boeing 7378H4 · Hydraulic System, Main
  > NR 2 BRAKE SMOKING, POSIBLE HYD LEAK ON BRAKE. FOUND FITTING AT QUICK DISCONNECT LOOSE. TIGHTENED HYD LINE IAW AMM 32-41-11. OPS & LEAK CHKD GOOD.
- [SDR SWAA2026090807776](https://openairdocs.org/sdr/SWAA2026090807776.md): Battery Pack · inoperative · Sep 2, 2026 · N8320J · Boeing 7378H4 · Emergency Lighting
  > FOUND EMERGENCY LIGHTS ABOVE 10 ABC AND 14 ABC INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK IAW AMM 33-51-06. OPS CHKD GOOD.
- [SDR SWAA2026081085412](https://openairdocs.org/sdr/SWAA2026081085412.md): Light · detached · Aug 6, 2026 · N8320J · Boeing 7378H4 · Emergency Lighting
  > CEILING EXIT ROW LIGHT FELL OFF. REINSTALLED OVERHEAD EXIT LIGHT IAW AMM 33-51-01.
- [SDR SWAA2026080430775](https://openairdocs.org/sdr/SWAA2026080430775.md): Slide · low pressure · Aug 1, 2026 · N8320J · Boeing 7378H4 · Escape Slide
  > FWD GALLEY DOOR SLIDE READING LOW PRESSURE, REMOVED AND REPLACED FWD SERVICE DOOR ESCAPE SLIDE PER REF:725-61-06-FS. TTG8Q01DGQ32
- [SDR SWAA2026070216629](https://openairdocs.org/sdr/SWAA2026070216629.md): Handle · damaged · Jun 28, 2026 · N8320J · Boeing 7378H4 · Service Doors
  > FORWARD SERVICE DOOR ASSIST HANDLE DAMAGED. SWAPPED FWD LAV ASSIST HANDLE WITH FWD SERVICE DOOR HANDLE. OKAY TO CONTINUE PER MEL 25-10-01. SP 1 B. AUTH 326585. REPLACED LAV ASSIST HANDLE THAT WAS SWAPPED TO SERVICE DOOR POSITION IAW CMM 25-45-72.
- [SDR SWAA2026011461278](https://openairdocs.org/sdr/SWAA2026011461278.md): Starter · faulted · Jan 13, 2026 · N8320J · Boeing 7378H4 · Engine Starter
  > NR 2 ENGINE POSSIBLE HUNG START. NO LIGHT OFF. N2 AT APROX 20%. SMOKE OBSERVED BY GROUND CREW. NO SMOKE IN CABIN. GROUND CREW INFORMED PILOTS THAT SMOKE DISIPATED. NO OTHER ABNORMAL INDICATIONS OR ENG FIRE LIGHT OBSERVED IN COCKPIT. ENG START LEVER NR 2 NEVE
- [SDR SWAA2025121243813](https://openairdocs.org/sdr/SWAA2025121243813.md): Lens · loose · Dec 8, 2025 · N8320J · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT LENS AT CENTER OF AIRCRAFT CEILING, KNOCKED LOOSE. SECURED THE EMERGENCY LIGHT LENS IAW AMM 33-51-03.
- [SDR SWAA2025092316611](https://openairdocs.org/sdr/SWAA2025092316611.md): Panel · cracked · Sep 20, 2025 · N8320J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO PANEL 122AW HAS MULTIPLE CRACKS WITHIN 2 INCHES OF THE EDGE. REPAIRED CARGO PANEL 122AW IAW EA# M-21-125-00669.
- [SDR SWAA2025092316610](https://openairdocs.org/sdr/SWAA2025092316610.md): Panel · cracked · Sep 20, 2025 · N8320J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > 141FW HAS MULTIPLE CRACKS WITHIN 2 INCHES OF THE EDGE. REMOVED AFT CARGO PANEL 141FW IAW AMM 25-52-10. FOUND MULTIPLE BROKEN NUT PLATES. REMOVED AND REPLACED AFTER CARGO PANEL 141FW IN REF TO AMM 255-52-06.
- [SDR SWAA2025092316609](https://openairdocs.org/sdr/SWAA2025092316609.md): Floor Panel · cracked · Sep 20, 2025 · N8320J · Boeing 7378H4 · Fuselage Floor Panel
  > 142FW HAS CRACK WITHIN 2 INCHES OF THE EDGE. ALONG WITH WRONG SCREWS INSTALLED IN CAP STRIP. REMOVED AFT CARGO PANEL IAW AMM 25-52-10. FOUND MULTIPLE BROKEN NUT PLATES. REMOVED AND REPLACED AFT CARGO PANEL 142FW IN REF TO AMM 25-52-06.
- [SDR SWAA2025092316607](https://openairdocs.org/sdr/SWAA2025092316607.md): Floor Panel · cracked · Sep 20, 2025 · N8320J · Boeing 7378H4 · Fuselage Floor Panel
  > FWD CARGO PANNEL 122EW HAS MULTIPLE CRACKS WITHIN 2 INCHES OF THE EDGE. REPAIRED CARGO PANEL 122EW IAW EA# M-21-125-00669.
- [SDR SWAA2025072192999](https://openairdocs.org/sdr/SWAA2025072192999.md): Sign · detached · Jul 18, 2025 · N8320J · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT MID CABIN FELL OFF. SECURED EMERGENCY EXIT SIGN AT MID CABIN IAW AMM 33-51-01;LIGHT OPS CHECK NORMAL.
- [SDR SWAA2025070186381](https://openairdocs.org/sdr/SWAA2025070186381.md): Sign · loose · Jun 28, 2025 · N8320J · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN AT MID-CABIN IS LOOSE.<[01] RESECURED EMERGENCY EXIT SIGN MID-CABIN IN REFERENCE TO AMM 33-51-01. OPS CHECKS GOOD.
- [SDR SWAA2025050566004](https://openairdocs.org/sdr/SWAA2025050566004.md): Battery Pack · inoperative · Apr 30, 2025 · N8320J · Boeing 7378H4 · Emergency Lighting
  > CUSTOMER WALK ITEM: EMERGENCY LIGHT INOP AFT R2 DOOR<[01] RECHARGED R2 DOOR EMERGENCY LIGHT BATTERY PACK REF. B737NG AMM 33-51-06-610-802. OPERATIONAL TEST GOOD REF. B737NG AMM 33-51-00-710-801.;[02] VERIFIED RECHARGED R2 DOOR EMERGENCY LIGHT BATTERY PACK REF.
- [SDR SWAA2025050566003](https://openairdocs.org/sdr/SWAA2025050566003.md): Battery Pack · inoperative · Apr 30, 2025 · N8320J · Boeing 7378H4 · Emergency Lighting
  > CUSTOMER WALK ITEM: CABIN OVER R2 DOOR EMERGENCY LIGHT INOP<[01] RECHARGED R2 DOOR EMERGENCY LIGHT BATTERY PACK REF. B737NG AMM 33-51-06-610-802. OPERATIONAL TEST GOOD REF. B737NG AMM 33-51-00-710-801.;[02] VERIFIED RECHARGED R2 DOOR EMERGENCY LIGHT BATTERY PA
- [SDR SWAA2025050565665](https://openairdocs.org/sdr/SWAA2025050565665.md): Lens · missing · Apr 29, 2025 · N8320J · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT LENS MISSING AT MID COVE BULLNOSE APPROX. SEAT 17FED<[01] INSTALLED LIGHT LENS ON EMERGENCY AISLE LIGHT AT SEAT 17DEF IAW SWA 737-800 AMM 33-51-03-960-803. PO# 1120695.1;[02] INSTALLED LIGHT LENS ON EMERGENCY AISLE LIGHT AT SEAT 17DEF IAW SWA 7
- [SDR SWAA2025050557510](https://openairdocs.org/sdr/SWAA2025050557510.md): Handle · loose · Apr 21, 2025 · N8320J · Boeing 7378H4 · Passenger/Crew Doors
  > CR VB ASSIST HANDLE ON L1 AND R1 DOOR BOTH LOOSE<[01] SECURED ASSIST HANDLES ON L1 AND RI DOORS IAW B737-800 AMM 52-11-31-400-802;[02] SECURED ASSIST HANDLES ON L1 AND RI DOORS IAW B737-800 AMM 52-11-31-400-802
- [SDR SWAA2025040922236](https://openairdocs.org/sdr/SWAA2025040922236.md): Bulb · inoperative · Apr 7, 2025 · N8320J · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN @ ROW 15CB EXIT SIGN HAS 3 INOP BULBS. <[01] REMOVED AND REPLACED 3 BULBS AT ROW 15CB EXIT SIGN PER AMM 33-51-01. OPS TEST GOOD.
- [SDR SWAA2025040922235](https://openairdocs.org/sdr/SWAA2025040922235.md): Bulb · inoperative · Apr 7, 2025 · N8320J · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN @ ROW 14FED EXIT SIGN HAS 3 INOP BULBS <[01]. PERFORMED TEST OF EMERGENCY LIGHTING PER AMM 33-51-00. FOUND 2 BULBS INOP. REMOVED AND REPLACED 2 BULBS AT ROW 14FED EXIT SIGN PER AMM 33-51-01. OPS TEST GOOD.
- [SDR SWAA2025031906540](https://openairdocs.org/sdr/SWAA2025031906540.md): Lens · missing · Mar 17, 2025 · N8320J · Boeing 7378H4 · Emergency Lighting
  > AFT LH LAV EMERGENCY EXIT LIGHT MISSING <[01]. INSTALLED LENS IAW AMM 33-51-01.
- [SDR SWAA2025021094619](https://openairdocs.org/sdr/SWAA2025021094619.md): Cover · missing · Feb 9, 2025 · N8320J · Boeing 7378H4 · Emergency Lighting
  > ROW 15 DEF EMERGENCY EXIT SIGN MISSING COVER<[01] REPLACED ROW 15 DEF EMERGENCY EXIT LIGHT COVER REF B737 AMM 33-51-01
- [SDR SWAA2024112561529](https://openairdocs.org/sdr/SWAA2024112561529.md): Sign · out of adjust · Nov 19, 2024 · N8320J · Boeing 7378H4 · Emergency Lighting
  > OVER-WING EMERGENCY EXIT SIGN ROW 15 DISLODGED FROM CEILING. OVER-WING EMERGENCY EXIT SIGN.<[01] RESECURED EXIT SIGN ASSEMBLY REF AMM 33-51-01. OPS CHECK GOOD.
- [SDR SWAA2024091135125](https://openairdocs.org/sdr/SWAA2024091135125.md): Retainer · loose · Sep 7, 2024 · N8320J · Boeing 7378H4 · Emergency Equipment
  > R1 DOOR GIRT BAR PLASTIC FITTING LOOSE.<[01] INSPECTED R1 DOOR ESCAPE SLIDE GIRT BAR PER AMM 25-66-01. NO FAULTS FOUND. RESECURED GIRT BAR RETAINER CLIP FOR THE L1 DOOR PER AMM 25-66-01.
- [SDR SWAA2024060397054](https://openairdocs.org/sdr/SWAA2024060397054.md): Cover · loose · Jun 1, 2024 · N8320J · Boeing 7378H4 · Emergency Lighting
  > SEAT ROW 15 DE AFT EMERGENCY EXIT LIGHT COVER LOOSE<[01] REMOVED AND REPLACED LIGHT ASSEMBLY AT ROW 15DE PER AMM 35-51-01 OPS CHECK GOOD
- [SDR SWAA2024022153795](https://openairdocs.org/sdr/SWAA2024022153795.md): Lamp · burned out · Feb 19, 2024 · N8320J · Boeing 7378H4 · Emergency Lighting
  > BURN EMERGENCY LIGHT AT LOWER FUSELAGE RH SIDE BTW STA 727F TO 727G 2024-61418<[01] LAMP ON HOUSING WAS PLACED CORRECTLY IAW B737-800 AMM 33-51-04-960-801 TEST OK;[02] TASK COMPLETED<BR><BR>OPERATIONAL TEST GOOD; NO DEFECTS NOTED.
- [SDR SWAA2024022247078](https://openairdocs.org/sdr/SWAA2024022247078.md): Winglet · corroded · Jan 31, 2024 · N8320J · Boeing 7378H4 · Wing Main, Frame Structure
  > CORROSION ON SPLIT SCIMITAR TIP LOCATED WINGLET LT WING 2024-61372<[01] PERFORMED PERMANENT REPAIR ON SPLIT SCIMITAR TIP CAP LOCATED WINGLET LT WING IAW B737-800 SRM AP37.1-0632. 57-31-01 REPAIR 2; SEE INDIVIDUAL BELOW;[02] PERFORMED PERMANENT REPAIR ON SPLIT
- [SDR SWAA2024022245806](https://openairdocs.org/sdr/SWAA2024022245806.md): Support Web · cracked · Jan 28, 2024 · N8320J · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > CRACK INBOARD FAN COWL SUPPORT WEB ON ENGINE 1 2024-61365<[01] REPLACED INBOARD FAN COWL SUPPORT WEB ON ENGINE 1 IAW B737-800 SRM 51-40-02-0G-0.;[02] REPLACED INBOARD FAN COWL SUPPORT WEB ON ENGINE 1 IAW B737-800 SRM 51-40-02-0G-0.
- [SDR SWAA2024022245481](https://openairdocs.org/sdr/SWAA2024022245481.md): Angle · cracked · Jan 27, 2024 · N8320J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED BS500I AT LEVEL STR28R AT FWD CARGO COMPARTMENT 2024-61347<[01] REPLACED NEW ANGLE CLIP LOCATED BS500I AT LEVEL STR28R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7902 REV.B;[02] REPLACED NEW A
- [SDR SWAA2024022245480](https://openairdocs.org/sdr/SWAA2024022245480.md): Plate · corroded · Jan 27, 2024 · N8320J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION PLATE FLOOR STRUCTURE LOCATED BS259.5 TO BS270 AT LEVEL BL0 AND WL208.1 AT PASSENGER CABIN 2024-61346<[01] TOOL USED ON STEP 3 IS THICKNESS GAGE PN:45MG; SN: 130063701; DUE DATE: 24-JUL-24;[02] REPLACED PLATE FLOOR PANEL STRUCTURE LOCATED BS259.5 TO
- [SDR SWAA2024022245560](https://openairdocs.org/sdr/SWAA2024022245560.md): Rail · corroded · Jan 27, 2024 · N8320J · Boeing 7378H4 · Wing Main, Frame Structure
  > CORROSION INTERNAL CAVITY LEADING EDGE ON RAIL LOCATED ORSS336 AT RT WING 2024-61356<[01] REPLACED RAIL(GANG CHANNEL) LOCATED ORSS336 AT RT WING. IAW B737 800 SRM 51-40-02-0G-0; SRM 51-10-02 ITEM 9 AND DWG 112A4402 SHEET 41. SEE INDIVIDUAL SIGN OFF BELOW.;[02]
- [SDR SWAA2024022245558](https://openairdocs.org/sdr/SWAA2024022245558.md): Plate · cracked · Jan 27, 2024 · N8320J · Boeing 7378H4 · Wing Main, Frame Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS327 AT RT WING 2024-61353<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS327 AT RT WING IAW B737-800 SRM 51-40-02-0G-0;SRM 51-10-02-G-0 ITEM 9 AND DWG 115A3700 SHEET 61 REV.;[02] REPLACED CORRUGATED PL
- [SDR SWAA2024022245559](https://openairdocs.org/sdr/SWAA2024022245559.md): Retainer · corroded · Jan 27, 2024 · N8320J · Boeing 7378H4 · Wing Main, Frame Structure
  > CORROSION INTERNAL CAVITY TRAILING EDGE RETAINER SEAL UPPER AREA LOCATED ORSS360 AT RT WING 2024-61354 CORROSION INTERNAL CAVITY TRAILING EDGE RETAINER SEAL UPPER AREA LOCATED ORSS404 AT RT WING<[01] REPLACED INTERNAL CAVITY TRAILING EDGE RETAINER SEAL UPPER A
- [SDR SWAA2024022245145](https://openairdocs.org/sdr/SWAA2024022245145.md): Bracket · cracked · Jan 26, 2024 · N8320J · Boeing 7378H4 · Wing Miscellaneous Structure
  > CRACK BRACKET KEEL BEAM LOCATED BS540 AT LEVEL LBL4 AT LOWER FUSELAGE 2024-61344<[01] MEASURE OF CRACK IS: L:1.034 TOOL USED DIGITAL CALIPER PN:500-197-30 SN:A21042057; DUE DATE: 04-APR-24 AND REPLACED BRACKET KEEL BEAM LOCATED BS540 AT LEVEL LBL4 AT LOWER FUS
- [SDR SWAA2024022244363](https://openairdocs.org/sdr/SWAA2024022244363.md): Angle · cracked · Jan 24, 2024 · N8320J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS400 TO BS420 AT LEVEL LBL50 AT PASSENGER CABIN 2024-61327 CRACK ANGLE LOCATED BS380 TO BS400 AT LEVEL LBL50 AT PASSENGER CABIN<[01] REPLACED ANGLE LOCATED BS380 TO BS400 AT LEVEL LBL50 AT PASSENGER CABIN IAW B737 800 SRM 51-40-02-0G-01; D
- [SDR SWAA2024022144364](https://openairdocs.org/sdr/SWAA2024022144364.md): Angle · cracked · Jan 24, 2024 · N8320J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS400 TO BS420 AT LEVEL LBL13 AT PASSENGER CABIN 2024-61328 CRACK ANGLE LOCATED BS380 TO BS400 AT LEVEL LBL13 AT PASSENGER CABIN<[01] REPLACED ANGLE LOCATED BS380 TO BS400 AT LEVEL LBL13 AT PASSENGER CABIN IAW B737 800 RM 51-40-02-0G<BR>01.
- [SDR SWAA2024022244178](https://openairdocs.org/sdr/SWAA2024022244178.md): Intercostal · corroded · Jan 23, 2024 · N8320J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB - INTERCOSTAL LOCATED BS500 TO BS500A AT LEVEL STR26R FWD CARGO COMPARTMENT 2024-61318<[01] REPLACED WEB - INTERCOSTAL LOCATED BS500 TO BS500A AT LEVEL STR26R FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G-0 AND DWG 143A0080 SHEETS 39.SEE
- [SDR SWAA2024022243390](https://openairdocs.org/sdr/SWAA2024022243390.md): Support Angle · cracked · Jan 21, 2024 · N8320J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BS540 RBL 24.75 AT PASSENGER CABIN 2024-61307<[01] REPLACED SUPPORT ANGLE LOCATED BS540 RBL 24.75 AT PASSENGER CABIN IAW B737 800 SRM 51-40-02-0G-0; SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 64 REV -;[02] JOB COMPLETED.
- [SDR SWAA2024022243391](https://openairdocs.org/sdr/SWAA2024022243391.md): Support Angle · cracked · Jan 21, 2024 · N8320J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BS 540 LBL 24.75 AT PASSENGER CABIN 2024-61306<[01] REPLACED SUPPORT ANGLE LOCATED BS540 RBL 24.75 AT PASSENGER CABIN IAW B737 800 SRM 51-40-02-0G-0; SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 64 REV -;[02] JOB COMPLETED.
- [SDR SWAA2024022242807](https://openairdocs.org/sdr/SWAA2024022242807.md): Floor Panel · delaminated · Jan 19, 2024 · N8320J · Boeing 7378H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 231UF AT PASSENGER CABIN 2024-61275<[01] PERFORMED VISUAL INSPECTION AND TAP TEST ON FLOOR PANEL 231UF AT PASSENGER CABIN AND NOT FOUND DELAMINATION ONLY DAMAGE SLEEVE (2EA) IAW B737-800 NDT MANUAL 51-05-01. INSTALLED NEW SLEEVE (2EA)
- [SDR SWAA2024022242804](https://openairdocs.org/sdr/SWAA2024022242804.md): Plate · cracked · Jan 18, 2024 · N8320J · Boeing 7378H4 · Wing Main, Frame Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE ORSS 297 RT WING 2024-61271<[01] REPLACED CORRUGATED PLATE LOC. ON TRAILING EDGE ORSS 297 RT WING IAW B737-800 SRM 51-40-02-0G-0 AND DWG 115A3712 SHEET 7 REV A;[02] REPLACED CORRUGATED PLATE LOC. ON TRAILING EDGE ORSS 297 R
- [SDR SWAA2024022142797](https://openairdocs.org/sdr/SWAA2024022142797.md): A/C Pack · cracked · Jan 18, 2024 · N8320J · Boeing 7378H4 · Fuselage Main, Bulkhead
  > CRACK VAPOR BARRIER CENTER SECTION BS 663.75 AND RBL 28 WL 170 AT MAIN WHEEL WELL COMPARTME 2024-61255<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:15120589 DUE DATE:13-FEB-24;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18165044 DUE DATE: 26-MAR-24.;[03] TO
- [SDR SWAA2024022242289](https://openairdocs.org/sdr/SWAA2024022242289.md): Frame · cracked · Jan 17, 2024 · N8320J · Boeing 7378H4 · Fuselage Main, Frame
  > CRACK FRAME ON BS 312 AND STR6L AT FWD GALLEY AREA 2024-61199<[01] REPAIRED FRAME ON BS 312 AND STR6L AT FWD GALLEY AREA I.A.W EA M-22-153-01244;[02] CORRECTED STEP 1.<BR>REPAIRED FRAME ON BS 312 AND STR6L AT FWD GALLEY AREA I.A.W EA M-22-153-01244;DUE TO CRAC
- [SDR SWAA2024022242296](https://openairdocs.org/sdr/SWAA2024022242296.md): Plate · corroded · Jan 17, 2024 · N8320J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION INTERNAL STRUCTURE ZEE CHANEL SIDEPLATE LOCATED AT LEVEL OF STRINGER 25R AND BETWEEN STA 767 TO STA 794.37 AT AFT CARGO COMPARTMENT 2024-61214<[01] REPLACED ZEE CHANNEL SIDEPLATE LOCATED AT LEVEL OF STRINGER 25R AND BETWEEN STA 767 TO STA 794.37 AFT
- [SDR SWAA2024022242303](https://openairdocs.org/sdr/SWAA2024022242303.md): Floor Panel · delaminated · Jan 17, 2024 · N8320J · Boeing 7378H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 231ZF AT PASSENGER CABIN 2024-61221<[01] TOOL USED: CALIPER PN:500-197-30 SN:A21303945 DUE DATE: 04-DEC-24;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18175478; DUE DATE: 25-JAN-25;[03] TOOL USED: SCALE PN: CR5200 SN:8343110765 DU
- [SDR SWAA2024022242302](https://openairdocs.org/sdr/SWAA2024022242302.md): Floor Panel · delaminated · Jan 17, 2024 · N8320J · Boeing 7378H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 241EF AT PASSENGER CABIN 2024-61222<[01] TOOL USED: CALIPER PN: 500-197-30 SN: A21303945 DUE DATE: 04-DEC-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18175478; DUE DATE: 25-JAN-25;[03] TOOL USED: SCALE PN: CR5200 SN:8343110765
- [SDR SWAA2024022242304](https://openairdocs.org/sdr/SWAA2024022242304.md): Floor Panel · delaminated · Jan 17, 2024 · N8320J · Boeing 7378H4 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 231YF AT PASSENGER CABIN 2024-61220<[01] TOOL USED: CALIPER PN:500-197-30 SN: A21303945 DUE DATE: 04-DEC-24;[02] TOOL USED: CALIPER PN:500-196-30 SN:A23325549 DUE DATE: 03-JAN-25;[03] REPLACED FLOOR PANEL 231YF DUE TO WAS FOUND OUT LIMI
- [SDR SWAA2024022241925](https://openairdocs.org/sdr/SWAA2024022241925.md): Angle · cracked · Jan 17, 2024 · N8320J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP AT AFT FACE THE STA 500H AND STINGER 25LH AT FWD CARGO COMPARTMENT 2024-61194<[01] REPLACED NEW NEW ANGLE - CLIP AT AFT FACE THE STA 500H AND STINGER 25LH AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G-0 AND DWG 143A7505 SHEET 108 REV
- [SDR SWAA2024022242287](https://openairdocs.org/sdr/SWAA2024022242287.md): Angle · cracked · Jan 17, 2024 · N8320J · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP AT STA 500G AND STRG 25L AT FWD CARGO COMPARTMENT 2024-61198<[01] REPLACED NEW ANGLE - CLIP AT STA 500G AND STRG 25L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G-0 AND DWG 143A7505 REV.- SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED
- [SDR SWAA2024022242286](https://openairdocs.org/sdr/SWAA2024022242286.md): Stringer Clip · cracked · Jan 17, 2024 · N8320J · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACK CLIP AT STA 500I AND BETWEEN STRINGER 24R TO STRINGER 25R AT FWDCARGO COMPARTMENT 2024-61196 CRACK CLIP AT STA 500I AND BETWEEN STRINGER 25R TO STRINGER 26R AT FWDCARGO COMPARTMENT<[01] REPLACED NEW CLIP (SHEAR TIE) LOC. STA 500I AND BETWEEN STRINGER 25R

Next page: https://openairdocs.org/aircraft/N8320J/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 = 'N8320J' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8320J/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.