# Service difficulty reports: N8683D

A list on [N8683D](https://openairdocs.org/aircraft/N8683D.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 · 124 reports

- [SDR SWAA2026022072042](https://openairdocs.org/sdr/SWAA2026022072042.md): Lamp · burned · Feb 19, 2026 · N8683D · Boeing 7378H4 · Emergency Lighting
  > AFT SERVICE DOOR UPPER PROXIMITY LIGHT; BELOW THE EMERGENCY EXIT SIGN; HAS BURNT OUT BULB. AFT SERVICE DOOR UPPER PROXIMITY LIGHT BELOW THE EMERGENCY EXIT SIGN HAS BURNT OUT BULB. REPLACED THE BULB IAW AMM 33-51-00-710-801, OPS TESTED IAW AMM 33-51-01-960-80
- [SDR SWAA2026022071912](https://openairdocs.org/sdr/SWAA2026022071912.md): Battery Pack · inoperative · Feb 18, 2026 · N8683D · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT'S RELATED TO BATTERY PACK M1695 ARE INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY BATTERY PACK M1695; OPS TESTED GOOD IAW AMM 33-51-06-960-805.
- [SDR SWAA2026022071277](https://openairdocs.org/sdr/SWAA2026022071277.md): Handle · cracked · Feb 16, 2026 · N8683D · Boeing 7378H4 · Passenger/Crew Doors
  > FED UPPER DOOR ASSIST HANDLE IS CRACKED. REMOVED AND REPLACED FED UPPER DOOR ASSIST HANDLE IAW AMM 52-11-31-000-802 STEPS 2. F. (3) AND AMM 52-11-31-400-802 STEPS 3. G. (2).
- [SDR SWAA2026022369309](https://openairdocs.org/sdr/SWAA2026022369309.md): Battery Pack · failed · Feb 9, 2026 · N8683D · Boeing 7378H4 · Emergency Lighting
  > FUNCTIONAL CHECK ALL EMERGENCY LIGHTS PERFORMED IAW AMM 33-51-00-710-801. BATTERY PACK M1695 FAILED TEST. WILL BE REPLACE AND TESTED ON CARD ID TTG8Q01AH7R7.
- [SDR SWAA2025062584326](https://openairdocs.org/sdr/SWAA2025062584326.md): Sign · broken · Jun 22, 2025 · N8683D · Boeing 7378H4 · Emergency Lighting
  > CENTER AISLE OVERWING EXIT LIGHT BROKEN<[01] RE-PLACED CENTER EMERGENCY EXIT SIGN PER AMM 33-51-01;OPS CHECK GOOD.
- [SDR SWAA2025041418969](https://openairdocs.org/sdr/SWAA2025041418969.md): Battery Pack · failed · Mar 28, 2025 · N8683D · Boeing 7378H4 · Emergency Lighting
  > M1671 BATTERY PACK REQUIRES R&R. R/H AFT OVERWING EMERGENCY EXIT LIGHT FAILS TO ILLUMINATE.<[01] REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06. NO FAULTS NOTED.;[02] VERIFIED
- [SDR SWAA2025041006014](https://openairdocs.org/sdr/SWAA2025041006014.md): Floor Panel · delaminated · Mar 17, 2025 · N8683D · Boeing 7378H4 · Fuselage Floor Panel
  > PANEL 242GF HAS UPPER SURFACE DELAMINATION. <[01] -R&R FLOOR PANEL IAW AMM 53-21-00.;[02] 02 - INSPECTED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)].
- [SDR SWAA2025041404586](https://openairdocs.org/sdr/SWAA2025041404586.md): Stiffener · cracked · Mar 12, 2025 · N8683D · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > PANEL 414 COWL ASSY - FAN - #1 ENGINE INBOARD - STIFFENER AT OIL SERVICE DOOR CRACKED<[01] FAN COWL TO BE REPLACED ON TTG8Q00S5HJN
- [SDR SWAA2025041404181](https://openairdocs.org/sdr/SWAA2025041404181.md): Attach Angle · cracked · Mar 11, 2025 · N8683D · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > STA 663 R/H VAPER BARRIER UPPER ATTACH ANGLE CRACKED AT RBL 10 & RBL35.<[01] REMOVED CRACKED ATTACH ANGLE PER SRM 51-10-02.;[02] MATCH DRILLED REPLACEMENT ANGLE PER SRM 51-10-02 AND DWG 111A1000. VERIFIED MATCH DRILLED REPLACEMENT ANGLE PER SRM 51-10-02 AND DW
- [SDR SWAA2025041404184](https://openairdocs.org/sdr/SWAA2025041404184.md): Stiffener · cracked · Mar 11, 2025 · N8683D · Boeing 7378H4 · Wing Miscellaneous Structure
  > R WING FIXED UPPER TRAILING EDGE PANEL SUPPORT STIFFENER AT WBL 198.6 HAS CRACK.(MARKED)<[01] REMOVED CRACKED SUPPORT STIFFENER PER SRM 51-40-02.;[02] VERIFIED WORK PERFORMED ON C/A #1;[03] LOCATED;DRILLED AND DEBURRED THE NEW SUPPORT ANGLE PER SRM 51-40-05.;[
- [SDR SWAA2025041404185](https://openairdocs.org/sdr/SWAA2025041404185.md): Angle · cracked · Mar 11, 2025 · N8683D · Boeing 7378H4 · Wing Miscellaneous Structure
  > L/H WING UPPER FIXED T/E PANEL ABOVE #1 ENGINE PYLON AFT FAIRING HAS CRACKED ANGLE ON I/B END (MARKED)<[01] REMOVED CRACKED ANGLE.;[02] REMOVED AND REPLACED PER SRM 51-40-02.;[03] 02 - INSPECTED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AN
- [SDR SWAA2025041404294](https://openairdocs.org/sdr/SWAA2025041404294.md): Support Beam · damaged · Mar 11, 2025 · N8683D · Boeing 7378H4 · Wing Miscellaneous Structure
  > R WING FIXED UPPER TRAILING EDGE PANEL SUPPORT BEAM AT WBL.198.6 HAS 2EA ELONGATED FASTENER HOLES.(MARKED)<[01] REMOVED DAMAGE FROM UPPER SUPPORT BEAM AND FOUND TO BE OUT-OF-LIMITS PER SRM 57-51-02-2R-1.;[02] VERIFIED WORK ACCOMPLISHED IN C/A #1;[03] REMOVED D
- [SDR SWAA2025041404182](https://openairdocs.org/sdr/SWAA2025041404182.md): Rib · damaged · Mar 11, 2025 · N8683D · Boeing 7378H4 · Wing, Rib/Bulkhead
  > R WING DEFLECTION CONTROL RIB HAS 2EA ELONGATED FASTENER HOLES.(MARKED)<[01] INSPECTED DEFLECTION CONTROL RIB UPPER TAB ELONGATED FASTENER HOLES AND FOUND TO BE OUT-OF-LIMITS PER SRM 57-51-02-1A-1;[02] VERIFIED DEFLECTION CONTROL RIB UPPER TAB FOUND BE OUT OF
- [SDR SWAA2025041403931](https://openairdocs.org/sdr/SWAA2025041403931.md): Skin · delaminated · Mar 10, 2025 · N8683D · Boeing 7378H4 · Trailing Edge Flaps
  > L/H MAIN FLAP T/E WEDGE HAS 2 SMALL AREAS OF DELAMINATION<[01] REMOVED DAMAGE TO AREA PER SRM 57-53-01-2R-7.;[02] 02 - INSPECTED PER [SRM 57-53-01-2R-7-B00269 (REPAIR 7 - INBOARD MAIN FLAP TRAILING EDGE WEDGE - PERMANENT)];[03] PART TOOLING UPDATE.;[04] REPAIR
- [SDR SWAA2025041403932](https://openairdocs.org/sdr/SWAA2025041403932.md): Skin · delaminated · Mar 10, 2025 · N8683D · Boeing 7378H4 · Trailing Edge Flaps
  > R/H MAIN FLAP T/E WEDGE HAS SMALL AREA OF DELAMINATION.<[01] REMOVED DELAMINATIOM DAMAGE PER SRM 57-53-01-2R-7.;[02] VERIFIED REMOVAL OF DAMAGE ONLY;;[03] REPAIRED PER SRM 57-53-01-2R-7.;[04] C/W INSPECTION OF REPAIR AREA NO DEFECTS NOTED.;[05] RESTORED FINISH
- [SDR SWAA2025040707423](https://openairdocs.org/sdr/SWAA2025040707423.md): Stop · worn · Mar 10, 2025 · N8683D · Boeing 7378H4 · Leading Edge Slat Control System
  > #2 SLAT; L/E WING UP-STOPS WORN ON INBD AND OUTBD SIDES OF ACTUATOR.<[01] REMOVED AND REPLACED UPSTOPS AS REQUIRED PER AMM 27-81-00;[02] C/W RII INSPECTION
- [SDR SWAA2025041403332](https://openairdocs.org/sdr/SWAA2025041403332.md): Wire · exposed · Mar 8, 2025 · N8683D · Boeing 7378H4 · Light System Wiring
  > PASSENGER CABIN OVERHEAD EMERGENCY EXIT LIGHT CENTER AISLE CEILING HAS WIRES EXPOSED AT SEATS 14-15ABC DEF<[01] REPOSITIONED THE EMERGENCY EXIT LIGHT PER AMM 33-51-01.OPS CHK GOOD.;[02] 02 - INSPECTED PER [AMM 33-51-01-960-802-NG (EXIT SIGN - LIGHT ASSEMBLY RE
- [SDR SWAA2025041403393](https://openairdocs.org/sdr/SWAA2025041403393.md): Light · out of adjust · Mar 8, 2025 · N8683D · Boeing 7378H4 · Emergency Lighting
  > PHOTOLUMINESCENT STRIP AT SEAT 2DEF IS LIFTING FROM THE FLOOR.<[01] PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING TO BE REPLACED N TASKCARD #TTG8R007LV56.;[02] PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING TO BE REPLACED ON TASKCARD #TTG8R007LV56.;[03] C/W INSPECTION.
- [SDR SWAA2025041403382](https://openairdocs.org/sdr/SWAA2025041403382.md): Light · out of adjust · Mar 8, 2025 · N8683D · Boeing 7378H4 · Emergency Lighting
  > PHOTOLUMINESCENT STRIPS AT SEAT 26ABC HAS AN EXCESSIVE END GAP BETWEEN THE PHOTOLUMINESCENT STRIPS<[01] PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING TO BE REPLACED ON TASKCARD #TTG8R007LV56.;[02] C/W INSPECTION.
- [SDR SWAA2025041403431](https://openairdocs.org/sdr/SWAA2025041403431.md): Handle · loose · Mar 8, 2025 · N8683D · Boeing 7378H4 · Passenger/Crew Doors
  > L1 FWD ENTRY DOOR PLASTIC PULL HANDLE APPEARS LOOSE TO DOOR STRUCTURE.<[01] SECURED DOOR LINER UPPER ASSIST HANDLE PER AMM 52-11-31.;[02] 1. TROY CLEMENS (TECHNICIAN); 11-MAR-2025 14:41 UTC<BR>SECURED DOOR LINER UPPER ASSIST HANDLE PER AMM 52-11-31<BR>INSPECTE
- [SDR SWAA2025041403403](https://openairdocs.org/sdr/SWAA2025041403403.md): Slide · out of adjust · Mar 8, 2025 · N8683D · Boeing 7378H4 · Escape Slide
  > R2 AFT GALLEY DOOR LINER HAS A CRACK ABOVE AFT SLIDE MOUNT BOLT.<[01] REPAIRED LINER PER AMM 25-00-00 AND RESTORED FINISH PER AMM 51-21-00.;[02] INSPECTION C/W FOR CORRECTIVE ACTION #1 FOR REPAIRED LINER PER AMM 25-00-00 AND RESTORED FINISH PER AMM 51-21-00.
- [SDR SWAA2025041003072](https://openairdocs.org/sdr/SWAA2025041003072.md): Seat Back · out of adjust · Mar 8, 2025 · N8683D · Boeing 7378H4 · Passenger Compartment Equipment
  > EXIT ROW SEAT 14E RECLINES AND IT SHOULDN'T. <[01] SECURED SET RING PREVENTING HYDRAULIC LOCK FROM EXTENDING; OPS CK GOOD IAW CMM 25-22-46.; [02] SECURED EXIT ROW SEAT 14E RECLINE SET RING PREVENTING HYDRAULIC LOCK FROM EXTENDING; OPS CK GOOD IAW CMM 25-22-46
- [SDR SWAA2025022498836](https://openairdocs.org/sdr/SWAA2025022498836.md): Pump · failed · Feb 22, 2025 · N8683D · Boeing 7378H4 · Hydraulic Pump (Electric/Engine), Main
  > SYS A HYDRAULIC LOSS AFTER GEAR RETRACTION<[01] REPLACED #1 ENG CASE DRAIN FILTER AND ?A? ELEC CASE DRAIN FILTER; NO DEBRIS FOUND IN EITHER FILTER. REPLACED#1 ENG DRIVEN HYDRAULIC PUMP IAW AMM 29-11-11. RAN ENGINE TWICE; OPS AND LEAKS CHECKS GOOD. ALSO REF AMM
- [SDR SWAA2024111358314](https://openairdocs.org/sdr/SWAA2024111358314.md): Megaphone · broken · Nov 10, 2024 · N8683D · Boeing 7378H4 · Emergency Equipment
  > FOUND AFT MEGAPHONE BROKEN<[01] R+R REF AMM 25-64-00.
- [SDR SWAA2024080722478](https://openairdocs.org/sdr/SWAA2024080722478.md): Light · out of adjust · Aug 3, 2024 · N8683D · Boeing 7378H4 · Emergency Lighting
  > FLOOR STRIP LIGHTING ROW 12 CAPTAIN SIDE LOOSE<[01] UNABLE TO LIFT STRIP OFF FLOOR WORKING AS SHOULD IAW SIP
- [SDR SWAA2024041876193](https://openairdocs.org/sdr/SWAA2024041876193.md): Sign · missing · Apr 17, 2024 · N8683D · Boeing 7378H4 · Emergency Lighting
  > FA REPORTS EXIT SIGN MISSING OVER EMERGENCY EXIT ROW<[01] INSTALLED CENTER ISLE OVER-WING EMERGENCY EXIT LIGHT LENSE PER AMM 33-51-01
- [SDR SWAA2024041674313](https://openairdocs.org/sdr/SWAA2024041674313.md): Lens · missing · Apr 13, 2024 · N8683D · Boeing 7378H4 · Emergency Lighting
  > ROW 14/15 EMERGENCY LIGHT EXIT LENS MISSING<[01] INSTALLED ROW 14/15 EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01
- [SDR SWAA2024041173219](https://openairdocs.org/sdr/SWAA2024041173219.md): Lens · detached · Apr 10, 2024 · N8683D · Boeing 7378H4 · Emergency Lighting
  > OVERHEAD WING EXIT SIGN LENS DETACHED.<[01] INSTALLED BOTH LENS COVERS ON OVERHEAD EXIT IAW AMM 33-51-01.
- [SDR SWAA2024032567040](https://openairdocs.org/sdr/SWAA2024032567040.md): Power Supply · inoperative · Mar 23, 2024 · N8683D · Boeing 7378H4 · Emergency Lighting
  > L/H OVERWING LIGHTED EXIT SIGNS INOP.<[01] 01 - REMOVED AND REPLACED M1694 REF [AMM 33-51-06-960-806-NG (POWER SUPPLY - POWER SUPPLY REPLACEMENT - PERMANENT)]
- [SDR SWAA2024031261344](https://openairdocs.org/sdr/SWAA2024031261344.md): Battery · inoperative · Mar 9, 2024 · N8683D · Boeing 7378H4 · Emergency Equipment
  > L/H AFT F/A SEAT I/B FLASHLIGHT INOP<[01] R+R'D L/H AFT F/A I/B FLASHLIGHT BATTERY. OP'S CK GOOD. REF AMM 25-64-00;[02] 02 - INSPECTED PER [AMM 25-64-00-900-806-NG (FLASHLIGHT BATTERY REPLACEMENT - PERMANENT)]
- [SDR SWAA2024031360985](https://openairdocs.org/sdr/SWAA2024031360985.md): Battery Pack · inoperative · Mar 8, 2024 · N8683D · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK AT STA 500C R/H IS INOPERABLE<[01] REPLACED BATTERY PACK AND OPS CHECK GOOD PER AMM 33-51-06;[02] 02 - INSPECTED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024031360984](https://openairdocs.org/sdr/SWAA2024031360984.md): Battery Pack · inoperative · Mar 8, 2024 · N8683D · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS BATTERY PACK AT STA 727C L/H IS INOP<[01] REPLACED BATTERY PACK AND OPS CHECK GOOD PER AMM 33-51-06;[02] PARTS;[03] 02 - INSPECTED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024031360986](https://openairdocs.org/sdr/SWAA2024031360986.md): Battery Pack · inoperative · Mar 8, 2024 · N8683D · Boeing 7378H4 · Emergency Lighting
  > AFT GALLEY STA 952 L/H EMERGENCY LIGHT BATTERY PACK INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT STA 952 L/H PER MM 33-51-06;[02] 02 - INSPECTED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024031355229](https://openairdocs.org/sdr/SWAA2024031355229.md): Stringer Clip · cracked · Feb 23, 2024 · N8683D · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > FWD CARGO; STINGER CLIP CRACKED AT STA 500I STR 25L.<[01] REMOVED CRACKED STR. CLIP PER SRM 51-40-02;[02] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)] REPLACED STR. CLIP PER SRM 5
- [SDR SWAA2024031355228](https://openairdocs.org/sdr/SWAA2024031355228.md): Stringer · cracked · Feb 23, 2024 · N8683D · Boeing 7378H4 · Fuselage Main, Longeron/Stringer
  > FWD CARGO; STINGER CLIP CRACKED AT STA 500I STR 25R.<[01] REMOVED AND REPLACED PER SRM. 51-40-02;[02] C/W INSPECTION.<BR>01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]
- [SDR SWAA2024031454677](https://openairdocs.org/sdr/SWAA2024031454677.md): Plate · corroded · Feb 22, 2024 · N8683D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT: CORROSION ON THE UPPER SURFACE OF THE RIGHT SIDE PLATE. LOCATED AT RBL 21 STA 767+2 AND 767+12. MARKED<[01] REMOVED LIGHT SURFACE CORROSION ON SIDE PLATE AFT CARGO. MATERIAL REMAINING THICKNESS.034. BLENDED AREA FOUND TO BE OUT OF LIMIT
- [SDR SWAA2024031454853](https://openairdocs.org/sdr/SWAA2024031454853.md): Intercostal · corroded · Feb 22, 2024 · N8683D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT GALLEY AREA; INTERCOSTAL AT STA.947 HAS MINOR CORROSION. UPPER SURFACE.<[01] PRIOR TO BLENDING; DAMAGED MEASURES.040' DEEP AT INTERCOSTAL MACHINED STEP. MAXIMUM ALLOWABLE DAMAGE IS 10% OF THICKNESS. DAMAGE IS OUT OF LIMITS PER SRM 53-7051-1A-1.;[02] DAMAG
- [SDR SWAA2024031354680](https://openairdocs.org/sdr/SWAA2024031354680.md): Support Bracket · cracked · Feb 22, 2024 · N8683D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT: AFT VERTICAL FRAME SUPPORT FOR PANEL 141PW. THE LOWER AFT SUPPORT BRACKET IS CRACKED. LOCATED AT STA 867 LBL 9. MARKED.<[01] REMOVED AND REPLACED LOWER AFT SUPPORT BRACKET PER SRM 51-40-02.;[02] VERIFIED1. LIEM DANG (TECHNICIAN); 23-FEB-
- [SDR SWAA2024031354851](https://openairdocs.org/sdr/SWAA2024031354851.md): Floor Support · cracked · Feb 22, 2024 · N8683D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR SUPPORT INTERCOSTAL UPPER ANGLE CRACKED ADJACENT TO FLOORBOARD FASTENER HOLE; STA. 380 +7' LBL 13.<[01] REMOVED PASSENGER CABIN FLOOR SUPPORT INTERCOSTAL UPPER ANGLE AT STA. 380+7' LBL 13; IAW SRM 53-10-04.;[02] MATCH DRILLED NEW INTERCOS
- [SDR SWAA2024031254686](https://openairdocs.org/sdr/SWAA2024031254686.md): Plate · corroded · Feb 22, 2024 · N8683D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT RH SIDEPLATE HAS CORROSION ON AND AROUND FASTENER HOLES STA-727G-727H RBL21<[01] REMOVED SURFACE CORROSION IN AFT CARGO COMPARTMENT RH SIDEPLATE STA-727G-727H RBL21 PER SRM 51-10-02; FOUND TO BE OUT OF LIMITS. MATERIAL REMOVED 0.006 AND R
- [SDR SWAA2024031254687](https://openairdocs.org/sdr/SWAA2024031254687.md): Plate · corroded · Feb 22, 2024 · N8683D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT RH SIDEPLATE HAS CORROSION ON AND AROUND FASTENER HOLES STA-727H-727I RBL21<[01] REMOVED SURFACE CORROSION IN AFT CARGO COMPARTMENT RH SIDEPLATE STA-727H-727I RBL21 PER SRM 51-10-02; FOUND TO BE OUT OF LIMITS. MATERIAL REMOVED 0.005 AND R
- [SDR SWAA2024031254688](https://openairdocs.org/sdr/SWAA2024031254688.md): Plate · corroded · Feb 22, 2024 · N8683D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT RH SIDEPLATE HAS CORROSION ON AND AROUND FASTENER HOLES STA-727I-727J RBL21<[01] REMOVED SURFACE CORROSION IN AFT CARGO COMPARTMENT RH SIDEPLATE STA-727I-727J RBL21 PER SRM 51-10-02; FOUND TO BE OUT OF LIMITS. MATERIAL REMOVED 0.005 AND R
- [SDR SWAA2024031254689](https://openairdocs.org/sdr/SWAA2024031254689.md): Plate · corroded · Feb 22, 2024 · N8683D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT RH SIDEPLATE HAS CORROSION ON AND AROUND FASTENER HOLES STA-727J-747 RBL21<[01] REMOVED SURFACE CORROSION IN AFT CARGO COMPARTMENT RH SIDEPLATE STA-727J-747 RBL21 PER SRM 51-10-02; FOUND TO BE OUT OF LIMITS. MATERIAL REMOVED 0.005 AND REM
- [SDR SWAA2024031254691](https://openairdocs.org/sdr/SWAA2024031254691.md): Plate · corroded · Feb 22, 2024 · N8683D · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT RH SIDEPLATE HAS CORROSION ON AND AROUND FASTENER HOLES STA-747-767 RBL21<[01] REMOVED SURFACE CORROSION IN AFT CARGO COMPARTMENT RH SIDEPLATE STA-747-767 RBL21 PER SRM 51-10-02; FOUND TO BE OUT OF LIMITS. MATERIAL REMOVED 0.006 AND REMAI
- [SDR SWAA2024031254850](https://openairdocs.org/sdr/SWAA2024031254850.md): Floorbeam · corroded · Feb 22, 2024 · N8683D · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT GALLEY AREA; RH SIDE AT STA. 947 T-CAP HAS CORROSION AT VERY OUTBD SIDE NEXT TO INTERCOASTAL.<[01] PRIOR TO BLENDING; DAMAGE MEASURES.071' DEEP ON THE TRANSVERSE FLOOR BEAM ON STA. 947.5; UPPER FLANGE AT RBL 51'. MAXIMUM ALLOWABLE DAMAGE IS 15% OF MATERIA
- [SDR SWAA2024031454414](https://openairdocs.org/sdr/SWAA2024031454414.md): Seal · cracked · Feb 21, 2024 · N8683D · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > L/H HORIZONTAL STAB UPPER FWD SLIDING SEAL IS CRACKED.<[01] REMOVED AND REPLACED UPPER LH HORIZONTAL STAB UPPER FWD SLIDING SEAL PER AMM 53-31-31;[02] C/W INSPECTION
- [SDR SWAA2024031454423](https://openairdocs.org/sdr/SWAA2024031454423.md): Seal · cracked · Feb 21, 2024 · N8683D · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > R/H HORIZONTAL STAB UPPER FWD SLIDING SEAL IS CRACKED.<[01] REMOVED R/H HORIZONTAL STABILIZER TO BODY UPPER FRONT SPAR SLIDING SEAL PER AMM TASK 53-31-31-000-802.;[02] INSTALLED R/H HORIZONTAL STAB UPPER FWD SLIDING SEAL PER AMM 53-31-31.;[03] REMOVED AND REPL
- [SDR SWAA2024031354657](https://openairdocs.org/sdr/SWAA2024031354657.md): Floor Panel · damaged · Feb 21, 2024 · N8683D · Boeing 7378H4 · Fuselage Floor Panel
  > PANEL 221DF PANEL ASSEMBLY - LH PASSENGER CABIN FLOOR ACCESS FIBERS MISSING.<[01] REMOVED AND REPLACED WITH NEW FLOORBOARD. INSTALLATION AND TORQUE PERFORMED ON CARD #TTG8Q008JQFE.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
- [SDR SWAA2024031354670](https://openairdocs.org/sdr/SWAA2024031354670.md): Floor Panel · damaged · Feb 21, 2024 · N8683D · Boeing 7378H4 · Fuselage Floor Panel
  > PANEL 221EF PANEL ASSEMBLY - LH PASSENGER CABIN FLOOR ACCESS FIBERS MISSING.<[01] REMOVED AND REPLACED WITH NEW FLOORBOARD. INSTALLATION AND TORQUE PERFORMED ON CARD #TTG8Q008JQFE.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
- [SDR SWAA2024031354656](https://openairdocs.org/sdr/SWAA2024031354656.md): Floor Panel · damaged · Feb 21, 2024 · N8683D · Boeing 7378H4 · Fuselage Floor Panel
  > PANEL 221FF PANEL ASSEMBLY - LH PASSENGER CABIN FLOOR ACCESS FIBERS MISSING.<[01] REMOVED AND REPLACED WITH NEW FLOORBOARD. INSTALLATION AND TORQUE PERFORMED ON CARD #TTG8Q008JQFE.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1

Next page: https://openairdocs.org/aircraft/N8683D/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 = 'N8683D' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8683D/reports

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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.