# Service difficulty reports: N8658A

A list on [N8658A](https://openairdocs.org/aircraft/N8658A.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 · 140 reports

- [SDR SWAA2026102180451](https://openairdocs.org/sdr/SWAA2026102180451.md): Angle · cracked · Oct 11, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK GUSSET ANGLE, BS 500I, STRINGER 19R TTG8Q01E8P5B STEP 1 COMPLETED PCW TTG8Q01E8P5B.
- [SDR SWAA2026102193644](https://openairdocs.org/sdr/SWAA2026102193644.md): Support Bracket · cracked · Oct 11, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT BRACKET, BS 540, LBL 6 IN THE LT AIR CONDITION ING BAY. FAULT RESOLVED ON OTHER FAULT TTG8Q01E9MWY.
- [SDR SWAA2026102139156](https://openairdocs.org/sdr/SWAA2026102139156.md): Intercostal · cracked · Sep 24, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL, BS 500G - 500H, STRINGER 26R, 0 REPLACED THE INTERCOSTAL AND FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHT 151, REV -, SHT 153, REV -.
- [SDR SWAA2026102120461](https://openairdocs.org/sdr/SWAA2026102120461.md): Rib · cracked · Sep 23, 2026 · N8658A · Boeing 7378H4 · Horizontal Stabilizer, Spar/Rib
  > CRACKED LT HORIZONTAL STAB LEADING EDGE RIB AT ACCESS PANEL 331B, REPLACED THE RIB & FASTENERS IAW SRM 51-40-02, & DWG 186A1001, SHEET 19, REV -.
- [SDR SWAA2026102102572](https://openairdocs.org/sdr/SWAA2026102102572.md): Rib · cracked · Sep 23, 2026 · N8658A · Boeing 7378H4 · Horizontal Stabilizer, Spar/Rib
  > CRACKED LEADING EDGE RIB, L/E STA 272.62 ON THE RT HORIZONTAL STAB. REPLACED THE RIB IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, STEP 9, AND DWG 186A1001, SHT 19, REV -.
- [SDR SWAA2026102158537](https://openairdocs.org/sdr/SWAA2026102158537.md): Support · no discrepancy · Sep 20, 2026 · N8658A · Boeing 7378H4 · Wing Miscellaneous Structure
  > CORROSION ON THE LT WING OTBD T/E ON RAIL SUPPORT. PERFORMED A DETAILED VISUAL INSPECTION ON THE LT WING OTBD T/E RAIL SUPPORT IAW SRM 51-10-04, & NO FOUND CORROSION ONLY MISSING PROTECTIVE TREATMENT. THE APPLICATION SEE TTG8Q01ERA8A.
- [SDR SWAA2026102154393](https://openairdocs.org/sdr/SWAA2026102154393.md): Stop Fitting · cracked · Sep 18, 2026 · N8658A · Boeing 7378H4 · Emergency Exits
  > CRACKED STOP PAD, EMERGENCY DOOR 833, FWD POSITION, LOWER SURFACE. REPLACED STOP PAD IAW SOPM 20-50-12, REV 58.
- [SDR SWAA2026102119544](https://openairdocs.org/sdr/SWAA2026102119544.md): Support Angle · cracked · Sep 18, 2026 · N8658A · Boeing 7378H4 · Wing Miscellaneous Structure
  > CRACKED SUPPORT ANGLE FOR RT WING ACCESS PANEL 651FB. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-20-01, & DWG 115A2710, SHT 9, REV A.
- [SDR SWAA2026102132055](https://openairdocs.org/sdr/SWAA2026102132055.md): Support Angle · cracked · Sep 18, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 500I, STRINGER 28R. REPLACED THE SUPPORT ANGLE & FASTENERS IAW SRM-51-40-02-0G-0, & DWG 143A7902, SHT 320, REV-.
- [SDR SWAA2026102139371](https://openairdocs.org/sdr/SWAA2026102139371.md): Angle · cracked · Sep 17, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, AFT FACE OF FRAME BS 500G, STRINGER 26R IN THE FWD CARGO BAY. REPLACED ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHT 152, REV-.
- [SDR SWAA2026102119703](https://openairdocs.org/sdr/SWAA2026102119703.md): Support Angle · cracked · Sep 17, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, ON THE FWD FACE OF FRAME BS 500G, STRINGER 26L, IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHT 152, REV -.
- [SDR SWAA2026102180577](https://openairdocs.org/sdr/SWAA2026102180577.md): Angle · corroded · Sep 17, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORRODED ANGLE, BS 500I, BTWN STRINGERS 26L - 26R, WL 152, IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, & DWG 143A7902, SHT 257, REV B.
- [SDR SWAA2026102113404](https://openairdocs.org/sdr/SWAA2026102113404.md): Tie Clip · cracked · Sep 17, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK TIE CLIP ON BS 500H, STRINGER 26L AT FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED ON STA 500H AND STR 26L AT FWD CARGO COMPARTMENT IAW SRM 51-40-02, & DWG 143A7505 SHT 151, REV -.
- [SDR SWAA2026102193787](https://openairdocs.org/sdr/SWAA2026102193787.md): Tie Clip · cracked · Sep 17, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED TIE CLIP ON STA 500H AND STRINGER 26R AT FWD CARGO COMPARTMENT 2026-572636 REPLACED TIE CLIP ON STA 500H AND STR 26R AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9 AND DRAWING# 143A1233 REV-.
- [SDR SWAA2026102191183](https://openairdocs.org/sdr/SWAA2026102191183.md): Support Angle · cracked · Sep 17, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE ON THE FWD FACE OF THE FRAME AT BS 500G, STRINGER 26R. REPLACED THE SUPPORT ANGLE, & FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 152, REV -.
- [SDR SWAA2026102111786](https://openairdocs.org/sdr/SWAA2026102111786.md): Tie Clip · cracked · Sep 17, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED TIE CLIP, BS 500I, STRINGER 26R IN THE FWD CARGO BAY. REPLACED THE TIE CLIP IAW SRM 51-10-02, ITEM 9, & DWG 143A1234, REV A.
- [SDR SWAA2026102158399](https://openairdocs.org/sdr/SWAA2026102158399.md): Plate · damaged · Sep 16, 2026 · N8658A · Boeing 7378H4 · Wing Miscellaneous Structure
  > ELONGATED HOLE ON LT WING CORRUGATED PLATE T/E, IRSS 199 + 15. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02, SRM 51-10-02, DWG 115A171327, SHT 6, REV A, & DWG 115A2001, SHT 78, REV A.
- [SDR SWAA2026102100402](https://openairdocs.org/sdr/SWAA2026102100402.md): Support Angle · cracked · Sep 16, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 380 - 400, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, DWG-143A5400, SHEET 154 REV-, & DWG 143A5400, SHT 201, REV -.
- [SDR SWAA2026102118304](https://openairdocs.org/sdr/SWAA2026102118304.md): Plate · damaged · Sep 16, 2026 · N8658A · Boeing 7378H4 · Wing Miscellaneous Structure
  > ELONGATED HOLE ON THE SUPPORT OF CORRUGATED PLATET RAILING EDGE, ORSS 297 + 25, RT WING. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02, SRM 51-10-02, & DWG 115A3700, SHT 96, REV-.
- [SDR SWAA2026102171174](https://openairdocs.org/sdr/SWAA2026102171174.md): Support Angle · cracked · Sep 16, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, DWG-143A5400, SHT 154, REV -, & DWG 143A5400, SHT 201, REV -.
- [SDR SWAA2026102117802](https://openairdocs.org/sdr/SWAA2026102117802.md): Support Angle · cracked · Sep 16, 2026 · N8658A · Boeing 7378H4 · Wing Miscellaneous Structure
  > CRACKED RT WING SUPPORT ANGLE FIXED T/E, ORSS 261 + 16. REPLACED THE SUPPORT ANGLE & FASTENERS IAW SRM 51-40-02, & DWG 115A6200, SHT 17, REV A.
- [SDR SWAA2026102134422](https://openairdocs.org/sdr/SWAA2026102134422.md): Shield · corroded · Sep 15, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORRODED SHIELD PLATE, BTWN BS 767 - 787, STRINGER 25R FAULT WAS RESOLVED ON ANOTHER FAULT, SEE FAULT TTG8Q01ECET5.
- [SDR SWAA2026102120545](https://openairdocs.org/sdr/SWAA2026102120545.md): Pin · deformed · Sep 15, 2026 · N8658A · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > DEFORMED PLATING ON LOWER ATTACHMENT PIN CENTER SECTION REAR SPAR LUG AT RT HORIZONTAL STAB. REPLACED ONLY THE LOWER ATTACHMENT PIN CENTER SECTION REAR SPAR LUG IAW AMM 27-41-11-400-801, & AMM 27-41-11-400-801. FOR INSTALLATION LOWER PIN SEE TTG8R007BQES.
- [SDR SWAA2026102174565](https://openairdocs.org/sdr/SWAA2026102174565.md): Strap · corroded · Sep 15, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORRODED STRAP, BTWN BS 787 - 794.3, RBL 20, WL 156.1 IN THE AFT CARGO BAY. REPLACED THE STRAP IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 146A0081, SHT 49, REV A.
- [SDR SWAA2026102118881](https://openairdocs.org/sdr/SWAA2026102118881.md): Frame · cracked · Sep 14, 2026 · N8658A · Boeing 7378H4 · Fuselage Main, Frame
  > CRACKED FRAME, BS 312, STR 5 - 6L IN THE FWD GALLEY AREA. PERFORMED A REPAIR TO THE FRAME IAW M-22-153-01244.
- [SDR SWAA2026102164313](https://openairdocs.org/sdr/SWAA2026102164313.md): Light · deteriorated · Sep 14, 2026 · N8658A · Boeing 7378H4 · Emergency Lighting
  > DETERIORATED PHOTOLUMINESCENT STRIP ALONG PAX CABIN. REPLACED THE PHOTOLUMINESCENT STRIP IAW AMM 33-51-15-400-802, STEP 1.E.(2), & (5).
- [SDR SWAA2026102182814](https://openairdocs.org/sdr/SWAA2026102182814.md): Crossbeam · cracked · Sep 13, 2026 · N8658A · Boeing 7378H4 · Fuselage Main, Structure
  > CRACKED CROSSBEAM, BS 540, BTWN BL 0 - RBL 24.75, WL 208.1. REPLACED CROSSBEAM IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 146A0060, SHT 36, REV A.
- [SDR SWAA2026102142829](https://openairdocs.org/sdr/SWAA2026102142829.md): Skin · debonded · Sep 13, 2026 · N8658A · Boeing 7378H4 · Trailing Edge Flaps
  > DEBONDED LT WING, OTBD AFT FLAP. PERFORMED INTERIM REPAIR ON THE LT WING, OTBD AFT FLAP IAW SRM 57-53-01-2R-16, REPAIR 16. REQUIRED TAP-TEST INSPECTIONS EVERY 6875 FLIGHT CYCLES OR 30 MONTHS WHICHEVER COMES FIRST.
- [SDR SWAA2026102131160](https://openairdocs.org/sdr/SWAA2026102131160.md): Skin · debonded · Sep 13, 2026 · N8658A · Boeing 7378H4 · Trailing Edge Flaps
  > DEBONDED RT WING OTBD AFT FLAP. PERFORMED INTERIM REPAIR ON RT WING OTBD AFT FLAP IAW SRM 57-53-01-2R-16, REPAIR 16. REQUIRED TAP-TEST INSPECTIONS EVERY 6875 FLIGHT CYCLES OR 30 MONTHS WHICHEVER COMES FIRST.
- [SDR SWAA2026102131381](https://openairdocs.org/sdr/SWAA2026102131381.md): Support Angle · cracked · Sep 13, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 500I - 520, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, & DWG 143A5400, SHT 201, REV -.
- [SDR SWAA2026102189368](https://openairdocs.org/sdr/SWAA2026102189368.md): Access Panel · damaged · Sep 13, 2026 · N8658A · Boeing 7378H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON THE LT WING ACCESS PANEL 561BB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026102192801](https://openairdocs.org/sdr/SWAA2026102192801.md): Access Panel · damaged · Sep 13, 2026 · N8658A · Boeing 7378H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON THE LT WING ACCESS PANEL 561CB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026102100595](https://openairdocs.org/sdr/SWAA2026102100595.md): Tie Clip · cracked · Sep 12, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK TIE CLIP, BS 500H, STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE TIE CLIP & FASTENERS IAW SRM 51-40-02, & DWG 143A1233, SHT 29, REV -.
- [SDR SWAA2026102142780](https://openairdocs.org/sdr/SWAA2026102142780.md): Stub Frame · cracked · Sep 12, 2026 · N8658A · Boeing 7378H4 · Fuselage Main, Frame
  > CRACK INDICATION ON STUB FRAME BTWN BS 294.5 & 296.5, STRINGER 8R & 9R ON THE FWD GALLEY DOOR AREA. REPLACED THE STUB FRAME IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, DWG 141A8370, SHT 10, REV -, & DWG 141A8380, SHT 21, REV -.
- [SDR SWAA2026102193815](https://openairdocs.org/sdr/SWAA2026102193815.md): Web · corroded · Sep 12, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION SHIELD WEB LOCATED BTWN BS 767 - 794.3, WL 156, RBL 22 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB IAW SRM 51-10-02, ITEM 9, & DWG 146A0081, REV A,
- [SDR SWAA2026102141257](https://openairdocs.org/sdr/SWAA2026102141257.md): Cover · cracked · Sep 12, 2026 · N8658A · Boeing 7378H4 · Galley Doors
  > CRACKED COVER ON AFT SERVICE DOOR NEXT TO THE INTERNAL HANDLE. REPLACED THE COVER IAW AMM 52-41-31-401. THE INSTALLATION ACCOMPLISH ON TTG8Q01DTL16.
- [SDR SWAA2026102191104](https://openairdocs.org/sdr/SWAA2026102191104.md): Crossbeam · cracked · Sep 12, 2026 · N8658A · Boeing 7378H4 · Fuselage Main, Structure
  > CRACKED CROSSBEAM, BS 540, LBL 24.75 - 44.5. REPLACED THE CROSSBEAM IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A5240, SHT 12, REV-.
- [SDR SWAA2026102153730](https://openairdocs.org/sdr/SWAA2026102153730.md): Support Angle · cracked · Sep 12, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 500H, STRINGER 26R. REPLACED THE SUPPORT ANGLE, & FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHT 152, REV -.
- [SDR SWAA2026102180435](https://openairdocs.org/sdr/SWAA2026102180435.md): Crossbeam · cracked · Sep 12, 2026 · N8658A · Boeing 7378H4 · Fuselage Main, Structure
  > CRACKED CROSSBEAM, BS 540, BL 0 - LBL 24.75. REPLACED THE CROSSBEAM IAW SRM 51-10-02, ITEM 9, & DWG 143A0060, REV-. S
- [SDR SWAA2026102160553](https://openairdocs.org/sdr/SWAA2026102160553.md): Support Angle · cracked · Sep 11, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 663.75, LBL 36, WL 168, BLENDING PERFORMED WITH THE GRAIN DIRECTION INSTEAD OF CROSS GRAIN ON NEW ANGLE, PERFORMED BEND TO FORM NEW ANGLE IAW SRM 51-30-01, & DWG 111A1322, SHEET 14, REV A. PERFORMED CLEANING & REMOVED PROTECTIVE
- [SDR SWAA2026102117862](https://openairdocs.org/sdr/SWAA2026102117862.md): Access Panel · damaged · Sep 11, 2026 · N8658A · Boeing 7378H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON THE RT WING ACCESS PANEL 661AB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026102197527](https://openairdocs.org/sdr/SWAA2026102197527.md): Access Panel · elongated · Sep 11, 2026 · N8658A · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 193AR AT LOWER FUSELAGE. THE REPAIR REFERENCE OF PRE PREG SEND TO THE WET LAY UP REPAIR FOR THAT REASON WAS DOCUMENTED BOTH ON STEPS 3 AND 4. REPAIRED ACCESS PANEL 193AR AT LOWER FUSELAGE IAW SRM 51-70-05-2R-9 REPAIR 9.
- [SDR SWAA2026102193853](https://openairdocs.org/sdr/SWAA2026102193853.md): Angle · cracked · Sep 11, 2026 · N8658A · Boeing 7378H4 · Leading Edge Devices
  > CRACK SLAT 3 OTBD ANGLE OF INBOARD AUXILIARY TRACKAT LT WING. REPLACED OUTBOARD ANGLE OF INBD AUXILIARY TRACK AT LT WING IAW SRM 51-40-02-0G-0 AND SKIN PAD ADJUSTMENT IAW AMM 27-81-00-820-803. ADJUSTMENT IS OK.
- [SDR SWAA2026102150779](https://openairdocs.org/sdr/SWAA2026102150779.md): Support Bracket · cracked · Sep 11, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT BRACKET, BS 540, LBL 6 IN THE LT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 212A1110, SHT 11, REV-, & PERFORMED GENERAL VISUAL INSPECTION ON AREA WHEN SUPPORT BRACKET WAS REMOVED AND NO FOUND D
- [SDR SWAA2026102141175](https://openairdocs.org/sdr/SWAA2026102141175.md): Angle · cracked · Sep 10, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, BS 500I, STRINGER 21L, IN THE FWD CARGO BAY. REPLACED WITH A NEW ANGLE IAW SRM 51-40-02-0G, SRM 51-10-02-0G, & DWG 143A7902, SHT 256, REV B.
- [SDR SWAA2026102180419](https://openairdocs.org/sdr/SWAA2026102180419.md): Support Angle · cracked · Sep 10, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 500H, STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 143A7505, SHT 152, REV -.
- [SDR SWAA2026102102907](https://openairdocs.org/sdr/SWAA2026102102907.md): Support Angle · cracked · Sep 10, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 500H, STR 26R IN THE FWD CARGO BAY. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A7505, SHT 152, REV -.
- [SDR SWAA2026102120424](https://openairdocs.org/sdr/SWAA2026102120424.md): Gusset · cracked · Sep 10, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED GUSSET ANGLE, BS 500I, STRINGER 19R IN THE FWD CARGO BAY. REPLACED WITH A NEW GUSSET ANGLE IAW SRM 51-40-02-0G, SRM 51-10-02-0G, AND DWG 143A7902, SHEET 256, REV B.
- [SDR SWAA2026102121247](https://openairdocs.org/sdr/SWAA2026102121247.md): Support · corroded · Sep 10, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE BTWN BS 500E - 500I, STR 26R IN THE FWD CARGO BAY. REMOVED CORROSION ON THE SUPPORT ZEE AND EVALUATED REWORKED AREA, & FOUND WITHIN LIMITS IAW SRM 53-00-53-1A-2, ALLOWABLE DAMAGE 2.
- [SDR SWAA2026102133742](https://openairdocs.org/sdr/SWAA2026102133742.md): Support Angle · cracked · Sep 10, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 695, RBL 1, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, & DWG 273A9110, SHT 8, REV-.

Next page: https://openairdocs.org/aircraft/N8658A/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 = 'N8658A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8658A/reports

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