# Service difficulty reports: N8657B

A list on [N8657B](https://openairdocs.org/aircraft/N8657B.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 SWAA2026101949061](https://openairdocs.org/sdr/SWAA2026101949061.md): Lamp · inoperative · Oct 13, 2026 · N8657B · Boeing 7378H4 · Emergency Lighting
  > RIGHT FWD OVERWING EXIT ESCAPE LIGHT IS INOPERATIVE. REPLACED THE LAMPS AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-04-960-801.
- [SDR SWAA2026101907588](https://openairdocs.org/sdr/SWAA2026101907588.md): Baffle Angle · cracked · Sep 22, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > BAFFLE ANGLE CRACKED, BS 400, WL 155, RBL 25, AFT SIDE OF FRAME. REMOVED AND REPLACED THE BAFFLE ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A7505 REV-.
- [SDR SWAA2026101961698](https://openairdocs.org/sdr/SWAA2026101961698.md): Door Frame · cracked · Sep 11, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Structure
  > FED UPPER DOOR SURROUND CUTOUT FRAME WAS CRACKED AT BS 312, STR 5L. THE DOOR FRAME WAS REPAIRED IAW EA M-22-153-01244 LBL 33 BETWEEN S5L & S6L.
- [SDR SWAA2026101953037](https://openairdocs.org/sdr/SWAA2026101953037.md): Crossbeam · cracked · Sep 11, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Structure
  > PASSENGER CABIN FLOOR CROSSBEAM CRACKED, TOP PLATE ONLY, AT BS 540, RBL 27, WL 208. REMOVED AND REPLACED THE CROSSBEAM IAW SRM 51-40-02-0G-0, 51-40-05-0G-0, AND DWG 143A0060, REV B.
- [SDR SWAA2026101929413](https://openairdocs.org/sdr/SWAA2026101929413.md): Attach Angle · cracked · Sep 10, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACK FOUND ON THE INTERCOSTAL ATTACH ANGLE AT BS 380+13, LBL 11, WL 208. R & R THE ATTACH ANGLE IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, & DWG 143A5400, REV-.
- [SDR SWAA2026101964468](https://openairdocs.org/sdr/SWAA2026101964468.md): Attach Angle · cracked · Sep 10, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACKED INTERCOSTAL ATTACH ANGLE AT BS 380+10, LBL 52, WL 208. R & R THE ATTACH ANGLE IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, AND DWG 143A5400, REV-.
- [SDR SWAA2026101973041](https://openairdocs.org/sdr/SWAA2026101973041.md): Floor Support · cracked · Sep 10, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON FLOOR SUPPORT AT BS 380+13, RBL 11, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT BTWN BS 380 - 400, RBL 11, WL 208 IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, AND DWG 143A5400 REV-.
- [SDR SWAA2026101929534](https://openairdocs.org/sdr/SWAA2026101929534.md): Floor Support · cracked · Sep 10, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON INTERCOSTAL ATTACH ANGLE, BS 380+11, RBL 41, WL 208. REMOVED & REPLACED THE INTERCOSTAL BS380-400 RBL 41 WL 208 IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, AND DWG 143A5400, REV -.
- [SDR SWAA2026101970924](https://openairdocs.org/sdr/SWAA2026101970924.md): Support Plate · corroded · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON THE AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAD MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 727B - 767, RBL 22, WL 156. REMOVED AND REPLACED THE RT FLOOR TO SIDEWALL SUPPORT PLATE IAW SRM 51-40-02-0G-0, AND DWG 146A7500, REV-.
- [SDR SWAA2026101993008](https://openairdocs.org/sdr/SWAA2026101993008.md): Support Plate · corroded · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B - 767, LBL 22, WL 156. REMOVED AND REPLACED AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE IAW SRM 51-40-02-0G-0, AND DWG 146A7500, REV-.
- [SDR SWAA2026101975908](https://openairdocs.org/sdr/SWAA2026101975908.md): Floor Support · corroded · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FWD WET AREA FLOOR STRUCTURE AT BS 328+11 LBL 45 WL 208. REMOVED AND INSTALLED REPLACEMENT INTERCOSTAL AT BS 328-BS 344 LBL 45 IAW SRM 51-40-02-0G-0 AND DWG 141A5730 REV:A.
- [SDR SWAA2026101975411](https://openairdocs.org/sdr/SWAA2026101975411.md): Floorbeam · corroded · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON FWD WET AREA FLOORBEAMS AT BS 344, RBL 9, & BS 344, RBL 17, WL 208. CORROSION EVALUATED AND REMOVED FLOORBEAM UPPER FLANGE RBL9 WL208 AND RBL17 1"X1" AREA ORIGINAL MATERIAL THICKNESS IS 0.175" LOWEST MATERIAL THICKNESS IS 0.170" CORROSION
- [SDR SWAA2026101921248](https://openairdocs.org/sdr/SWAA2026101921248.md): Baffle Angle · cracked · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY BAFFLE ANGLES WERE CRACKED, AFT SIDE OF FRAMES BS 500G & BS 500H, RBL 25, WL 156. REMOVED AND REPLACED THE FWD CARGO BAFFLE ANGLES IAW SRM 51-40-02-0G-0, & DWG 145A7505, REV B.
- [SDR SWAA2026101920953](https://openairdocs.org/sdr/SWAA2026101920953.md): Attach Bracket · cracked · Sep 9, 2026 · N8657B · Boeing 7378H4 · Passenger/Crew Doors
  > AFT ENTRY DOOR PANEL 834DZ AFT ATTACH BRACKET WAS CRACKED. REMOVED AND REPLACED THE ATTACH BRACKET IAW SRM 51-40-02-0G-0, & AIPC 52-13-21-10.
- [SDR SWAA2026101992331](https://openairdocs.org/sdr/SWAA2026101992331.md): Floor Support · corroded · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON AFT WET AREA FLOOR SUPPORT, BS 947+1, RBL 52, WL 208. LOCATED AND DRILLED A NEW FLOOR SUPPORT BS 947 - 967, RBL 52 WL 208 IAW SRM 51-40-05-0G-0, & DWG 147A5650, REV A INSTALLED ON CCN TTG8Q01E78KV, STEP 8.
- [SDR SWAA2026101984460](https://openairdocs.org/sdr/SWAA2026101984460.md): Baffle Angle · cracked · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY BAFFLE ANGLES WERE CRACKED, FWD SIDE OF FRAMES BS 500G AND BS 500H, RBL 25, WL 156. REMOVED AND REPLACED FWD CARGO BAY BAFFLE ANGLES IAW SRM 51-40-02-0G-0, AND DWG 145A7505, REV B.
- [SDR SWAA2026101916199](https://openairdocs.org/sdr/SWAA2026101916199.md): Floor Panel · debonded · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 231JF UPPER SKIN HAS A LARGE DEBOND NEAR THE FWD EDGE. REPLACED THE FLOOR PANEL 231JF IAW SRM 51-10-02-0G-0, PARA 9, AND AIPC 53-21-51-58B, ITEM 205.
- [SDR SWAA2026101970639](https://openairdocs.org/sdr/SWAA2026101970639.md): Floor Panel · debonded · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 232HF UPPER SKIN HAD A LARGE DISBONDED AREA NEAR FWD EDGE. REPLACED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-B00275.
- [SDR SWAA2026101934106](https://openairdocs.org/sdr/SWAA2026101934106.md): Shield · corroded · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON THE AFT CARGO BAY SHIELD, FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES, BS 767+3 - 794, RBL 22, WL 156. THE SHIELD WAS REMOVED AND REPLACED IAW SRM 51-40-02-0G-0, AND DWG 146A0081, REV A.
- [SDR SWAA2026101993415](https://openairdocs.org/sdr/SWAA2026101993415.md): Shield · corroded · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON THE FWD CARGO BAY AFT SHIELD, BS 500+1 - 500+19, RBL 22, WL 156 HAD MULTIPLE AREAS AROUND NUT PLATE HOLES. THE FWD CARGO AFT SHIELD WAS REMOVED AND REPLACED BS 494 - 500A, RBL 22, WL 156 IAW SRM 51-40-02-0G-0, AND DWG 143A0080, REV-.
- [SDR SWAA2026101988789](https://openairdocs.org/sdr/SWAA2026101988789.md): Floorbeam · corroded · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON AFT WET AREA FLOORBEAM AT BS 987, RBL 42, WL 208. REPAIRED THE UPPER TEE ON THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.
- [SDR SWAA2026101971602](https://openairdocs.org/sdr/SWAA2026101971602.md): Floor Panel · pulled · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-B00275.
- [SDR SWAA2026101909350](https://openairdocs.org/sdr/SWAA2026101909350.md): Floor Panel · pulled · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 232EF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1.
- [SDR SWAA2026100872963](https://openairdocs.org/sdr/SWAA2026100872963.md): Floorbeam · corroded · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON AFT WET AREA FLOORBEAM, BS 947, RBL 52, WL 208. REMOVED DAMAGED UPPER FLANGE ON THE FLOORBEAM FROM RBL 30 - RBL 58, WL 208 AND REPAIRED IAW SRM 53-70-51-2R-5, REPAIR 5, ALTERNATIVE 2.
- [SDR SWAA2026100465784](https://openairdocs.org/sdr/SWAA2026100465784.md): Floorbeam · corroded · Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE AT BS 987 LBL 42 WL 208 \CORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE AT BS 987 LBL 42 WL 208 REMOVED CORROSION FOUND OUT OF LIMIT AND AREA WAS REPAIRED IAW SRM 53-70-51-2R-6 REPAIR 6 VERIFIED ACTION 1
- [SDR SWAA2026101954042](https://openairdocs.org/sdr/SWAA2026101954042.md): Floor Support · corroded · Sep 8, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE AT BS 987 RBL 42, BS 947 RBL 52, BS 987 LBL 42 WL 208 CORRODED.
- [SDR SWAA2026101901663](https://openairdocs.org/sdr/SWAA2026101901663.md): Threshold · cracked · Sep 7, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY, FWD CORNER THRESHOLD WAS CRACKED. REPAIRED THRESHOLD IAW SRM 53-30-15-2R-1.
- [SDR SWAA2026101967807](https://openairdocs.org/sdr/SWAA2026101967807.md): Plate · cracked · Sep 4, 2026 · N8657B · Boeing 7378H4 · Wing Main, Frame Structure
  > WIGGLE PLATE COMMON TO ACCESS PANEL 651EB FOUND CRACKED. REMOVED AND REPLACED THE WIGGLE PLATE IAW SRM 51-40-02-0G-0, AND DWG 115A2001, REV A.
- [SDR SWAA2026100809422](https://openairdocs.org/sdr/SWAA2026100809422.md): Plate · cracked · Sep 4, 2026 · N8657B · Boeing 7378H4 · Wing Main, Frame Structure
  > WIGGLE PLATE INBD OF NR 7 FLAP TRACK, COMMON TO ACCESS PANEL 661AB WAS CRACKED. THE WIGGLE PLATE WAS REMOVED AND REPLACED WIGGLE PLATE AT INBD OF NR 7 FLAP TRACK IAW SRM 51-40-02-0G-0, AND DWG. 115A2001, REV A.
- [SDR SWAA2026100856519](https://openairdocs.org/sdr/SWAA2026100856519.md): Drip Tray · cracked · Sep 4, 2026 · N8657B · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STAB, FWD CABLE DRUM DRIP SHIELD CRACKED.
- [SDR SWAA2026101900859](https://openairdocs.org/sdr/SWAA2026101900859.md): Rib · cracked · Sep 3, 2026 · N8657B · Boeing 7378H4 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STAB L/E 5TH FROM INBD RIB IS CRACKED. REMOVED AND REPLACED THE NR 5 RIB IAW SRM 51-40-02-0G-0, AND DWG 186A1001, REV B.
- [SDR SWAA2026101916761](https://openairdocs.org/sdr/SWAA2026101916761.md): Rib · cracked · Sep 3, 2026 · N8657B · Boeing 7378H4 · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STAB L/E, THIRD FROM INBD RIB CRACKED. R & R THE RIB IAW SRM 51-40-02-0G-0, & DWG 186A1001, REV B.
- [SDR SWAA2026101947890](https://openairdocs.org/sdr/SWAA2026101947890.md): Frame · punctured · Sep 3, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Frame
  > FRAME WEB, BS 380, WL 153, STRINGER 27R WAS PUNCTURED. REPAIRED IAW EA 26-153-02454.
- [SDR SWAA2026101985509](https://openairdocs.org/sdr/SWAA2026101985509.md): Stringer · severed · Sep 3, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT ARRIVED WITH STRINGER 27R SEVERED AT BS 360+13. STRINGER 27R REPAIRED IAW EA 26-153-02488.
- [SDR SWAA2026100888053](https://openairdocs.org/sdr/SWAA2026100888053.md): Rib · cracked · Sep 3, 2026 · N8657B · Boeing 7378H4 · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STAB L/E, 4TH FROM INBD RIB CRACKED. R & R LT HORIZONTAL STAB L/E 4TH RIB IAW SRM 51-40-02-0G-0, & DWG 186A1001, REV B.
- [SDR SWAA2026101961048](https://openairdocs.org/sdr/SWAA2026101961048.md): Pressure Deck · dented · Sep 2, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Structure
  > PREVIOUS REPAIR ON THE FLIGHT DECK FLOOR DENTED AT BS 255, RBL 4 - LBL 14, WL 207.54. REMOVED AND INSTALLED A REPLACEMENT FLIGHT DECK FLOOR WEB, BS 250 - 270, LBL 21- RBL 8 IAW SRM 51-40-02, AND EA 21-153-00734, REV A.
- [SDR SWAA2026082733898](https://openairdocs.org/sdr/SWAA2026082733898.md): Lamp · inoperative · Aug 27, 2026 · N8657B · Boeing 7378H4 · Emergency Lighting
  > RIGHT EMERGENCY LIGHT AFT OF WTB FAIRING INOP REMOVED AND REPLACED LAMP PER AMM 33-51-04
- [SDR SWAA2026082716876](https://openairdocs.org/sdr/SWAA2026082716876.md): Support Bracket · cracked · Aug 21, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > E&E COMPARTMENT SUPPORT BRACKET PN 143A9179-12 AT BS.374 STR.27R CRACKED REPAIRED IAW EA 26-153-02289 EA-26-153-02262 COMPLIED WITH. NO INSPECTION OR RII REQUIRED ON EA. EA SHOULD READ EA-153-02289
- [SDR SWAA2026082518189](https://openairdocs.org/sdr/SWAA2026082518189.md): Stringer · cracked · Aug 21, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Longeron/Stringer
  > STRINGER 27R WAS DAMAGED AT BS.378. REPAIRED IAW EA 26-153-02262. EA-26-153-02262 COMPLIED WITH. NO INSPECTION OR RII REQUIRED ON EA. REPAIRED IAW EA 26-153-02262.
- [SDR SWAA2026082555996](https://openairdocs.org/sdr/SWAA2026082555996.md): Skin · cracked · Aug 21, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > RIGHT FUSELAGE SKIN AT BS 380 WAS CRACKED, STRINGERS 24R - 28R.
- [SDR SWAA2026082534945](https://openairdocs.org/sdr/SWAA2026082534945.md): Stringer · damaged · Aug 21, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Longeron/Stringer
  > STRINGER 24R HAS DAMAGED AT BS 378. REPAIRED IAW EA 26-153-02262. EA-26-153-02262 COMPLIED WITH. NO INSPECTION OR RII REQUIRED ON EA. REPAIRED IAW EA 26-153-02262.
- [SDR SWAA2026082516305](https://openairdocs.org/sdr/SWAA2026082516305.md): Shear Tie · cracked · Aug 21, 2026 · N8657B · Boeing 7378H4 · Fuselage Internal Mounting Structure
  > BS.380 FRAME AT STRINGER 27R-28R SHEAR TIE CRACKED. REPAIRED IAW EA 26-153-02262. EA-26-153-02262 COMPLIED WITH. NO INSPECTION OR RII REQUIRED ON EA.
- [SDR SWAA2026082552272](https://openairdocs.org/sdr/SWAA2026082552272.md): Skin · cracked · Aug 21, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > RT FUSELAGE UPPER SKIN AT BS 380 STR 24R LAP JOINT HAD A 2 INCH CRACK. REPAIRED IAW EA 26-153-02262. EA-26-153-02262 COMPLIED WITH. NO INSPECTION OR RII REQUIRED ON EA.
- [SDR SWAA2026082590723](https://openairdocs.org/sdr/SWAA2026082590723.md): Stringer · cracked · Aug 21, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Longeron/Stringer
  > STRINGER 25R CRACKED AT BS 378. REPAIRED IAW EA 26-153-02262. EA-26-153-02262 COMPLIED WITH. NO INSPECTION OR RII REQUIRED ON EA. REPAIRED IAW EA 26-153-02262.
- [SDR SWAA2026082544578](https://openairdocs.org/sdr/SWAA2026082544578.md): Shear Tie · cracked · Aug 21, 2026 · N8657B · Boeing 7378H4 · Fuselage Internal Mounting Structure
  > BS.380 FRAME BETWEEN STRINGER 27R-28R SHEAR TIE CRACKED. REPAIRED IAW EA 26-153-02289 EA-26-153-02262 COMPLIED WITH. NO INSPECTION OR RII REQUIRED ON EA. CORRECTION SHOULD READ EA 26153-02289.
- [SDR SWAA2026082566239](https://openairdocs.org/sdr/SWAA2026082566239.md): Stringer · cracked · Aug 21, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R HAD DAMAGED AT BS 378. REPAIRED IAW EA 26-153-02262. EA-26-153-02262 COMPLIED WITH. NO INSPECTION OR RII REQUIRED ON EA. REPAIRED IAW EA 26-153-02262.
- [SDR SWAA2026082511056](https://openairdocs.org/sdr/SWAA2026082511056.md): Shear Tie · cracked · Aug 21, 2026 · N8657B · Boeing 7378H4 · Fuselage Internal Mounting Structure
  > E & E COMPARTMENT, BS 380, SHEAR TIE STR 27R WAS CRACKED. SAME AS BS.380 FRAME AT STRINGER 27R SUPPORT BRACKET SHEAR TIE CRACKED. BS.380 FRAME AT STRINGER 27R L SUPPORT SHEER TIE CRACKED. REPAIRED IAW EA 26-153-02289 EA-26-153-02262 COMPLIED WITH. NO INSPECT
- [SDR SWAA2026040987166](https://openairdocs.org/sdr/SWAA2026040987166.md): Engine · surges · Apr 6, 2026 · N8657B · Boeing 7378H4 · Engine (Turbine/Turboprop)
  > AT APPROX 14,000 FT NR 1 ENGINE BEGAN TO SURGE/STALL WITH VIBRATION. AT 70% N1 SURGE/STALL WENT AWAY. AT IDLE; VIBRATION CEASED. AFTER ENGINE SHUTDOWN; SMALL FIRE STARTED FIRE BRIGADE USED WATER EXTINGUISHING AGENT 2 TIMES. NO OVERWEIGHT LANDING.<[01] REF. TTG
- [SDR SWAA2026040284687](https://openairdocs.org/sdr/SWAA2026040284687.md): Light · abnormal · Mar 30, 2026 · N8657B · Boeing 7378H4 · Emergency Lighting
  > LEFT AFT OVERWING EXIT DOOR LIGHT STROBING. OK TO CONTINUE IAW MEL 33-2-04; SP1B; AUTH#312704. R & R AFT OWE LIGHT OPS CHECK GOOD PER AMM 33-21-00
- [SDR SWAA2026010758020](https://openairdocs.org/sdr/SWAA2026010758020.md): Battery Pack · inoperative · Jan 4, 2026 · N8657B · Boeing 7378H4 · Emergency Lighting
  > OWE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK REF AMM 33-51-06-960-806 AND OPS CHECK GOOD REF AMM 33-51-00-710-801.

Next page: https://openairdocs.org/aircraft/N8657B/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 = 'N8657B' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8657B/reports

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