# Service difficulty reports: N8698B

A list on [N8698B](https://openairdocs.org/aircraft/N8698B.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 · 82 reports

- [SDR SWAA2026090829296](https://openairdocs.org/sdr/SWAA2026090829296.md): Bulb · inoperative · Sep 1, 2026 · N8698B · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY SIGN ON LAV D HAS INOPERATIVE BULBS. REPLACED THE BULBS AND PERFORMED GOOD FUNCTIONAL TEST IAW AMM 33-51-01-960-801.
- [SDR SWAA2026090814511](https://openairdocs.org/sdr/SWAA2026090814511.md): Lamp · inoperative · Sep 1, 2026 · N8698B · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT R/H GROUND ILLUM LIGHT INOP. REPLACED LAMP AND PERFORMED GOOD FUNCTIONAL TEST IAW AMM 33-51-04-960-801.
- [SDR SWAA2026040786320](https://openairdocs.org/sdr/SWAA2026040786320.md): Cover · loose · Apr 3, 2026 · N8698B · Boeing 7378H4 · Escape Slide
  > R1 SLIDE COVER APPEARS LOOSE<[01] SECURED R1 DOOR SLIDE COVER IN REFERENCE TO AMM 70-20-02.
- [SDR SWAA2026032782691](https://openairdocs.org/sdr/SWAA2026032782691.md): Crossbeam · cracked · Mar 24, 2026 · N8698B · Boeing 7378H4 · Fuselage Main, Structure
  > FWD CARGO BAY BS 540 AT FLOOR LEVEL AND RIGHT OF BL 0, EXPANSION JOINT BREAK PANEL ASSEMBLY CRACKED. REMOVED AND REPLACED BREAK PANEL ASSEMBLY IAW SRM 51-40-02-0G-0-B00069.
- [SDR SWAA2025092416430](https://openairdocs.org/sdr/SWAA2025092416430.md): Nut · cracked · Sep 19, 2025 · N8698B · Boeing 7378H4 · Service Doors
  > FWD SERVICE DOOR ASSIST HANDLE NUT IS CRACKED. REMOVED AND REPLACED FWD SERVICE DOOR ASSIST HANDLE NUT IAW AMM 52-41-31.
- [SDR SWAA2025092411425](https://openairdocs.org/sdr/SWAA2025092411425.md): Battery Pack · inoperative · Sep 5, 2025 · N8698B · Boeing 7378H4 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK AT BS 659 FOUND INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW MM 33-51-06. ACCOMPLISHED OPS CHECK IAW AMM 33-51-06. NO FAULTS NOTED.
- [SDR SWAA2025092411423](https://openairdocs.org/sdr/SWAA2025092411423.md): Angle · cracked · Sep 4, 2025 · N8698B · Boeing 7378H4 · Wing Miscellaneous Structure
  > LEFT WING ANGLE ASSY INBD OF MIDFLAP DEFLECTION RIB IS CRACKED. REMOVED THE LT WING ANGLE ASSY IAW SRM 51-40-02. LOCATED AND DRILLED FASTENER HOLES IN THE NEW ANGLE IAW SRM 51-40-05. INSTALLED THE NEW ANGLE ASSY IAW SRM 51-10-02 & SRM 51-40-02.
- [SDR SWAA2025091609400](https://openairdocs.org/sdr/SWAA2025091609400.md): Cover · damaged · Aug 29, 2025 · N8698B · Boeing 7378H4 · Emergency Lighting
  > LENS ASSY OVER RT AFT WING EXIT SCREW HOLE ELONGATED. REMOVED AND REPLACED LENS ASSY COVER IAW AMM 33-21-00-960-805-NG.
- [SDR SWAA2025092409233](https://openairdocs.org/sdr/SWAA2025092409233.md): Seal · cracked · Aug 28, 2025 · N8698B · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB UPPER FWD SLIDING SEAL CRACKED. REMOVED AND REPLACED LT HORIZONTAL STAB UPPER FWD SLIDING SEAL IAW AMM 53-31-31.
- [SDR SWAA2025092409234](https://openairdocs.org/sdr/SWAA2025092409234.md): Seal · cracked · Aug 28, 2025 · N8698B · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STAB UPPER FWD SLIDING SEAL CRACKED. REMOVED AND REPLACED RT HORIZONTAL STAB UPPER FWD SLIDING SEAL IAW AMM 53-31-31.
- [SDR SWAA2025092408975](https://openairdocs.org/sdr/SWAA2025092408975.md): Fuel Tank · cracked · Aug 27, 2025 · N8698B · Boeing 7378H4 · Fuel Storage
  > BS 663 RIGHT, THE INBD FWD FUEL TANK FASTENER HOLE HAS CRACK INDICATION AT SECOND LAYER. CLEANED HOLE IAW SRM 51-10-02. PERFORMED HOLE PROBE INSPECTION IAW NDT 51-00-00, PART 6, PROC 16 CRACKED INDICATION STILL PRESENT. REPAIRED FASTENER HOLE IAW SRM 51-40
- [SDR SWAA2025092408526](https://openairdocs.org/sdr/SWAA2025092408526.md): Angle · cracked · Aug 27, 2025 · N8698B · Boeing 7378H4 · Wing Miscellaneous Structure
  > RIGHT WING ANGLE ASSY, INBD OF MID FLAP DEFLECTION RIB IS CRACKED. REMOVED ANGLE ASSY IAW SRM 51-40-02. LOCATED AND DRILLED FASTENER HOLES IN NEW ANGLE PER SRM 51-40-05. INSTALLED ANGLE PER SRM 51-10-02, & SRM 51-40-02.
- [SDR SWAA2025092408527](https://openairdocs.org/sdr/SWAA2025092408527.md): Angle · cracked · Aug 27, 2025 · N8698B · Boeing 7378H4 · Wing Miscellaneous Structure
  > RIGHT WING CLIP BETWEEN MID FLAP DEFLECTION RIB AND ANGLE IS CRACKED. REMOVED CLIP PER SRM 51-40-02. LOCATED AND DRILLED FASTENER HOLES IN NEW CLIP PER SRM 51-40-05. INSTALLED THE CLIP PER SRM 51-10-02, & SRM 51-40-02.
- [SDR SWAA2025092408976](https://openairdocs.org/sdr/SWAA2025092408976.md): Wedge · delaminated · Aug 27, 2025 · N8698B · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT INBD T/E MAIN FLAP AFT WEDGE DELAMINATED. LOCATED AND DRILLED FASTENER HOLES IN NEW MAIN FLAP T/E WEDGE REF SRM 51-40-02-0G-0. REPLACED THE WEDGE IAW SRM 51-10-02 & SRM 51-40-02-0G-0.
- [SDR SWAA2025092408973](https://openairdocs.org/sdr/SWAA2025092408973.md): Wedge · delaminated · Aug 27, 2025 · N8698B · Boeing 7378H4 · Trailing Edge Flaps
  > RIGHT INBD T/E MAIN FLAP AFT WEDGE DELAMINATED. LOCATED AND DRILLED NEW WEDGE IAW SRM 51-40-02. INSTALLED NUTPLATES IAW SRM 51-40-02. INSTALLED THE NEW WEDGE 113A2550-604 IAW SRM 51-40-02.
- [SDR SWAA2025092408416](https://openairdocs.org/sdr/SWAA2025092408416.md): Channel · cracked · Aug 26, 2025 · N8698B · Boeing 7378H4 · Wing Miscellaneous Structure
  > RIGHT WING TRAILING EDGE FIXED PANEL SUPPORT CHANNEL ATTACH BRACKET WAS CRACKED. REMOVED SUPPORT CHANNEL WEB IAW SRM 51-40-02. LOCATED & DRILLED FASTENER HOLES IN NEW CHANNEL IAW SRM 51-40-05. INSTALLED THE CHANNEL IAW SRM 51-10-02, & SRM 51-40-02.
- [SDR SWAA2025092408417](https://openairdocs.org/sdr/SWAA2025092408417.md): Skin · delaminated · Aug 26, 2025 · N8698B · Boeing 7378H4 · Trailing Edge Flaps
  > R WING OTBD TRAILING EDGE AFT FLAP LOWER INBD SURFACE HAS DELAMINATION.
- [SDR SWAA2025092408045](https://openairdocs.org/sdr/SWAA2025092408045.md): Attach Angle · cracked · Aug 25, 2025 · N8698B · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > BS 663 VAPOR BARRIER ATTACH ANGLE HAS CRACK AT APPROXIMATELY RBL 9. REPLACED THE ATTACH ANGLE IAW SRM 51-40-02 & DWG 111A1000.
- [SDR SWAA2025092408046](https://openairdocs.org/sdr/SWAA2025092408046.md): Attach Angle · cracked · Aug 25, 2025 · N8698B · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT APPROXIMATELY RBL 34. REMOVED THE ATTACH ANGLE IAW SRM 51-40-02. C/W HOLE PROBE INSP IAW NDT 51-00-00, PART 6, PROC. 16. MATCH DRILLED AND DEMURRED A NEW ATTACH ANGLE IAW SRM 51-40-05. INSTALLED THE NEW ATTAC
- [SDR SWAA2025092407618](https://openairdocs.org/sdr/SWAA2025092407618.md): Cover · cracked · Aug 24, 2025 · N8698B · Boeing 7378H4 · Emergency Exits
  > OVERWING ESCAPE, LOWER BEZELS BROKEN & CRACKED AT POSITIONS RF, LF, LA. R & R BEZELS COVERS IAW SIP.
- [SDR SWAA2025031704092](https://openairdocs.org/sdr/SWAA2025031704092.md): Handle · broken · Mar 11, 2025 · N8698B · Boeing 7378H4 · Service Doors
  > AFT SERVICE DOOR ASSIST HANDLE BROKEN<[01] R&R'D AFT SERVICE DOOR ASSIST HANDLE REF AMM 25-21-25-401-NG (AFT ENTRY AND AFT SERVICE DOORWAYS SIDEWALL LINING PANELS - REMOVAL/INSTALLATION - PERMANENT)
- [SDR SWAA2024121878895](https://openairdocs.org/sdr/SWAA2024121878895.md): Battery Pack · inoperative · Dec 18, 2024 · N8698B · Boeing 7378H4 · Emergency Lighting
  > LH INTERIOR OVER WING EMERGENCY ESCAPE HATCH LIGHTS INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M1694 PER AMM 33-51-06.
- [SDR SWAA2024082828567](https://openairdocs.org/sdr/SWAA2024082828567.md): Battery Pack · inoperative · Aug 21, 2024 · N8698B · Boeing 7378H4 · Emergency Lighting
  > FWD CABIN EMERGENCY LIGHT BATTERY PACK IS INOP AT STA 500C L/H<[01] REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06;[02] INSPECTED THE WORK PERFORMED ON CORRECTIVE ACTION #1; NO DEFECTS NOTED.
- [SDR SWAA2024082828568](https://openairdocs.org/sdr/SWAA2024082828568.md): Battery Pack · inoperative · Aug 21, 2024 · N8698B · Boeing 7378H4 · Emergency Lighting
  > FWD CABIN EMERGENCY LIGHT BATTERY PACK INOP AT STA 500C R/H<[01] R&R BATTERY PACK AND OPS CHECK GOOD PER AMM 33-51-06;[02] INSPECTED THE WORK PERFORMED ON CORRECTIVE ACTION #1; NO DEFECTS NOTED.
- [SDR SWAA2024082828569](https://openairdocs.org/sdr/SWAA2024082828569.md): Battery Pack · inoperative · Aug 21, 2024 · N8698B · Boeing 7378H4 · Emergency Lighting
  > AFT CABIN EMERGENCY LIGHT BATTERY PACK INOP AT STA 727C R/H<[01] REMOVED AND REPLACED BATTERY PACK. OPS CHK GOOD PER MM.33-51-06;[02] INSPECTED THE WORK PERFORMED ON CORRECTIVE ACTION #1; NO DEFECTS NOTED.
- [SDR SWAA2024082926891](https://openairdocs.org/sdr/SWAA2024082926891.md): Fairing · delaminated · Aug 16, 2024 · N8698B · Boeing 7378H4 · Trailing Edge Flaps
  > L/H WING #3 CANOE FAIRING; AFT CONE; OUTBOARD SIDE; HAS SEVERAL AREAS OF DELAMINATION INDICATED BY BULGING FACE SHEET.<[01] REMOVED AND REPLACED THE #3 CANOE FAIRING; AFT FAIRING ASSEMBLY PER AMM 27-51-18;[02] C/W INSPECTION
- [SDR SWAA2024082824241](https://openairdocs.org/sdr/SWAA2024082824241.md): Angle · cracked · Aug 9, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO; FOUND CRACK ON AFT FLOOR CLIP AT STA 500H.<[01] REMOVED AND REPLACED CLIP PER SRM 51-40-02.;[02] 02 - INSPECTED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]
- [SDR SWAA2024082824240](https://openairdocs.org/sdr/SWAA2024082824240.md): Angle · cracked · Aug 9, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO; FOUND CRACK ON FWD FLOOR CLIP AT STA 500H.<[01] REMOVED AND REPLACED CLIP PER SRM 51-40-02.;[02] 02 - INSPECTED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]
- [SDR SWAA2024082923292](https://openairdocs.org/sdr/SWAA2024082923292.md): Skin · delaminated · Aug 6, 2024 · N8698B · Boeing 7378H4 · Trailing Edge Flaps
  > L/H O/B TRAILING EDGE FLAP I/B LOWER SURFACE IS DELAMINATED.<[01] OK TO INSTALL NEW L/H O/B AFT FLAP S/N 001118;[02] INSTALLED NEW L/H O/B AFT FLAP PER AMM 27-51-22;[03] RII INSPECTED AS REQUIRED. CORRECTIVE ACTION #2; VERIFIED TORQUES AND SAFETIES.
- [SDR SWAA2024082826890](https://openairdocs.org/sdr/SWAA2024082826890.md): Panel · loose · Aug 6, 2024 · N8698B · Boeing 7378H4 · Wing Miscellaneous Structure
  > L/H SHELF PANEL LOOSE AT L/H DEFLECTION RIB<[01] REMOVED HARDWARE AND FASTENERS PER SRM 57-51-02-2R-4.;[02] REMOVED DAMAGE FROM UPPER CONTROL RIB TAB PER SRM 57-51-02-2R-4 AND DAMAGE FROM TRAILING EDGE SUPPORT BEAM PER SRM 57-51-02-2R-1.;[03] C/W DAMAGE REMOVA
- [SDR SWAA2024082922314](https://openairdocs.org/sdr/SWAA2024082922314.md): Panel · cracked · Aug 3, 2024 · N8698B · Boeing 7378H4 · Nacelle/Pylon, Main Frame
  > #1 ENGINE INBD FAN COWL DEFLECTOR WEB PANEL CRACKED JUST INSIDE OF OIL SERVE DOOR (MARKED)<[01] REMOVED AND REPLACED #1 ENG INBD FAN COWL PER AMM 71-11-02<BR>REF TTG8Q00S5GN8 FOR WORK ACCOMPLISHED.;[02] C/W INSPECTION
- [SDR SWAA2024082822018](https://openairdocs.org/sdr/SWAA2024082822018.md): Floor Support · corroded · Aug 3, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON INTERCOSTAL BETWEEN STA 947 TO STA 967 AT LBL 50.<[01] REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL IS OUT OF MANUAL LIMITS PER SRM 53-70-51-1A-1. MAX MATERIAL REMOVED 0.030?.;[02] RII- C/W INSPECTION AS REQUIRED C/A #1. RICHARD BLACKB
- [SDR SWAA2024082821571](https://openairdocs.org/sdr/SWAA2024082821571.md): Mount · corroded · Aug 2, 2024 · N8698B · Boeing 7378H4 · Fuselage, Equipment Attach Fittings
  > THE AFT LAVATORY MOUNT STRUCTURE IS CORRODED AT STA 947 RBL 51<[01] REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.14] FABRICATED AND DRILLED REPLACEMENT T-CHORD; REPAIR ANGLES; REPAIR STRAPS; FILLERS; AND DR
- [SDR SWAA2024082821572](https://openairdocs.org/sdr/SWAA2024082821572.md): Mount · corroded · Aug 2, 2024 · N8698B · Boeing 7378H4 · Fuselage, Equipment Attach Fittings
  > THE AFT LAVATORY MOUNT STRUCTURE IS CORRODED AT STA 947 RBL 27<[01] REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. ENTIRE LENGTH OF FLOOR BEAM UPPER FLANGE TO BE REMOVED AND REPAIRED ON FAULT #TTG8Q00UYZC6.;
- [SDR SWAA2024082821577](https://openairdocs.org/sdr/SWAA2024082821577.md): Structure · corroded · Aug 2, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > LAV MOUNT SHOWS SIGNS OF CORROSION UNDER MOUNT AT STA 947 LBL 25<[01] FURTHER INVESTIGATION REVEALS THAT THERE IS NO CORROSION ON UNDERLYING STRUCTURE BENEATH LAV MOUNT PER SRM 51-10-02.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1;[03] TTG8Q00UYZC6 THE AF
- [SDR SWAA2024082821998](https://openairdocs.org/sdr/SWAA2024082821998.md): Floor Support · corroded · Aug 2, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON INTERCOSTAL BETWEEN STAS 947-967; RBL 50.<[01] REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] RII- C/W INSPECTION AS REQUIRED C/A #1. DAVID BELL (TECHNICIAN); 02-AUG-2024 22:26 UTC<BR
- [SDR SWAA2024082822001](https://openairdocs.org/sdr/SWAA2024082822001.md): Threshold · corroded · Aug 2, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR THRESHOLD PLATE HAS CORROSION IN MULTIPLE LOCATIONS. REMOVED SURFACE CORROSION ON AFT CARGO DOOR THRESHOLD PLATED. MATERIAL REMOVED.020 AND REMAINING THICKNESS IS.030. THRESHOLD PLATED FOUND TO BE OUT OF LIMITED REQUIRE REPLACEMENT. ALL WORK
- [SDR SWAA2024082821578](https://openairdocs.org/sdr/SWAA2024082821578.md): Mount · corroded · Aug 2, 2024 · N8698B · Boeing 7378H4 · Fuselage, Equipment Attach Fittings
  > THE AFT LAVATORY MOUNT STRUCTURE IS CORRODED AT STA 947 LBL 50<[01] REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL IS OUT OF MANUAL LIMITS PER SRM 53-70-51-1A-1. REMAINING THICKNESS IS 0.130?.;[02] RII-C/W INSPECTION AS REQUIRED C/A #1. RICHARD BLACKBURN (
- [SDR SWAA2024082821999](https://openairdocs.org/sdr/SWAA2024082821999.md): Floor Support · corroded · Aug 2, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE LOCATED BETWEEN STAS 927-947; RBL 25 CORRODED.<[01] REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] C/W INSPECTION AS REQUIRED C/A #1. DAVID BELL (TECHNICIAN); 02-AUG-2024 20:30 UTC<B
- [SDR SWAA2024082822008](https://openairdocs.org/sdr/SWAA2024082822008.md): Floor Support · cracked · Aug 2, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD PASSENGER COMPARTMENT FLOOR STRUCTURE WET AREA; INTERCOSTAL UPPER ANGLE HAS 2EA CRACKS AT FLOOR PANEL ATTACH HOLES STA. 380+7' AND STA. 380+14' LBL 13.<[01] REMOVED INTERCOSTAL UPPER ANGLE AT STA.380 - STA.400 PER SRM 51-40-02.;[02] C/W INSPECTION AS REQUI
- [SDR SWAA2024082822012](https://openairdocs.org/sdr/SWAA2024082822012.md): Floorbeam · corroded · Aug 2, 2024 · N8698B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > FWD PASSENGER COMPARTMENT FLOOR STRUCTURE WET AREA; FLOOR BEAM UPPER SURFACE HAS CORROSION AT FLOOR PANEL ATTACH HOLE STA. 328 RBL 39.<[01] REMOVED CORROSION. ORIG THICKNESS OF 0.130IN; REMOVED 0.052IN; REMAINING 0.078IN. FOUND TO BE OUT OF LIMITS PER SRM 53-1
- [SDR SWAA2024082821854](https://openairdocs.org/sdr/SWAA2024082821854.md): Panel · delaminated · Aug 2, 2024 · N8698B · Boeing 7378H4 · Aerodynamic Fairings
  > WING TO BODY FAIRING 191FR HAS DELAMINATION AT FWD LOWER CORNER<[01] DAMAGE REMOVAL ACCOMPLISHED FOR LAY UP OF REPAIR PLIES IAW SRM 51-70-05-2R-10 REPAIR #10.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1;[03] APPLIED REPAIR PLIES IAW SRM 51-70-05-2R-10 REP
- [SDR SWAA2024082821324](https://openairdocs.org/sdr/SWAA2024082821324.md): Plate · corroded · Aug 1, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO R/H SIDEPLATE HAS CORROSION RBL 24; STA. 500B-500C<[01] BLENDED AREAS; REMOVED.005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] THIS SECTION OF SIDE PLATE TO BE REPLACED ON NR#TTG8Q00UYKDB;[03] 02 - INSPECTED PER [REFERENCE]SRM 5
- [SDR SWAA2024082821325](https://openairdocs.org/sdr/SWAA2024082821325.md): Plate · corroded · Aug 1, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO R/H SIDEPLATE HAS CORROSION RBL 24; STA. 500C-500D<[01] BLENDED AREAS; REMOVED.005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] THIS SECTION OF SIDE PLATE TO BE REPLACED ON NR#TTG8Q00UYKDB;[03] 02 - INSPECTED PER [SRM 53-00-53-1A
- [SDR SWAA2024082821326](https://openairdocs.org/sdr/SWAA2024082821326.md): Plate · corroded · Aug 1, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO R/H SIDEPLATE HAS CORROSION RBL 24; STA. 500D-500E<[01] BLENDED AREAS; REMOVED.005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] THIS SECTION OF SIDE PLATE TO BE REPLACED ON NR#TTG8Q00UYKDB;[03] 02 - INSPECTED PER [SRM 53-00-53-1A-
- [SDR SWAA2024082821317](https://openairdocs.org/sdr/SWAA2024082821317.md): Plate · corroded · Aug 1, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO R/H SIDEPLATE HAS CORROSION RBL 24; STA. 500F-500G<[01] BLENDED AREAS; REMOVED.005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] THIS SECTION OF SIDE PLATE TO BE REPLACED ON NR#TTG8Q00UYKDB;[03] 02 - INSPECTED PER [SRM 53-00-53-1A
- [SDR SWAA2024082821328](https://openairdocs.org/sdr/SWAA2024082821328.md): Plate · corroded · Aug 1, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO R/H SIDEPLATE HAS CORROSION RBL 24; STA. 500H-500I<[01] BLENDED AREAS; REMOVED.005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] THIS SECTION OF SIDE PLATE TO BE REPLACED ON NR#TTG8Q00UYKDB;[03] 02 - INSPECTED PER [SRM 53-00-53-1A
- [SDR SWAA2024082821319](https://openairdocs.org/sdr/SWAA2024082821319.md): Angle · corroded · Aug 1, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO L/H SIDEPLATE HAS CORROSION LBL 24; STA. 500C-500D<[01] REMOVED SURFACE CORROSION AT L/H TRANSITION ANGLE FROM STA. 500C-500D PER SRM 51-10-02; FOUND TO BE OUT OF LIMITS. MATERIAL REMOVED.020 AND REMAINING THICKNESS.020. PER SRM 53-00-53-1A-2.;[02]
- [SDR SWAA2024082821322](https://openairdocs.org/sdr/SWAA2024082821322.md): Angle · corroded · Aug 1, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO L/H SIDEPLATE HAS CORROSION LBL 24; STA. 500B-500C<[01] REMOVED SURFACE CORROSION AT L/H TRANSITION ANGLE FROM STA. 500B-500C PER SRM 51-10-02; FOUND TO BE OUT OF LIMITS. MATERIAL REMOVED.007 AND REMAINING THICKNESS.033. PER SRM 53-00-53-1A-2.;[02]
- [SDR SWAA2024082821331](https://openairdocs.org/sdr/SWAA2024082821331.md): Angle · corroded · Aug 1, 2024 · N8698B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO L/H SIDEPLATE HAS CORROSION LBL 24; STA. 500A-500B<[01] REMOVED SURFACE CORROSION AT L/H TRANSITION ANGLE FROM STA. 500B-500C PER SRM 51-10-02; FOUND TO BE OUT OF LIMITS. MATERIAL REMOVED.005 AND REMAINING THICKNESS.035. PER SRM 53-00-53-1A-2.;[02]

Next page: https://openairdocs.org/aircraft/N8698B/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 = 'N8698B' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8698B/reports

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