# Service difficulty reports: N8646B

A list on [N8646B](https://openairdocs.org/aircraft/N8646B.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 · 132 reports

- [SDR SWAA2026100509772](https://openairdocs.org/sdr/SWAA2026100509772.md): Lamp · inoperative · Oct 1, 2026 · N8646B · Boeing 7378H4 · Emergency Lighting
  > R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IN THE EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHKD GOOD.
- [SDR SWAA2026062204623](https://openairdocs.org/sdr/SWAA2026062204623.md): Intercostal · cracked · May 20, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 344 - 360, RBL 12, WL 200. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02 AND DWG 141A5400, REV -.
- [SDR SWAA2026062204622](https://openairdocs.org/sdr/SWAA2026062204622.md): Intercostal · cracked · May 20, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 344 TO 360, BL 0, WL 200. REMOVED AND REPLACED THE INTERCOSTAL BS 344 - 360, BL 0 IAW SRM 51-40-02 AND DWG 141A5400, REV -.
- [SDR SWAA2026062204302](https://openairdocs.org/sdr/SWAA2026062204302.md): Floor Panel · pulled · May 19, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 231HF LOWER SKIN HAS AREAS OF PULLED STRANDS. FABRICATE REPLACEMENT FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026062204303](https://openairdocs.org/sdr/SWAA2026062204303.md): Floor Panel · pulled · May 19, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 231MF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026062204318](https://openairdocs.org/sdr/SWAA2026062204318.md): Floor Panel · pulled · May 19, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 241RF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241RF FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026062204311](https://openairdocs.org/sdr/SWAA2026062204311.md): Floor Panel · pulled · May 19, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, DWG 146A5810.
- [SDR SWAA2026062204315](https://openairdocs.org/sdr/SWAA2026062204315.md): Floor Panel · pulled · May 19, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 242EF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-0-B00275, REPAIR GENERAL.
- [SDR SWAA2026062204316](https://openairdocs.org/sdr/SWAA2026062204316.md): Floor Panel · pulled · May 19, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 242FF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, DWG 146A5810.
- [SDR SWAA2026062204317](https://openairdocs.org/sdr/SWAA2026062204317.md): Floor Panel · pulled · May 19, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242D UPPER SKIN HAS AN AREA OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-1-B00276, REPAIR 1.
- [SDR SWAA2026062204308](https://openairdocs.org/sdr/SWAA2026062204308.md): Floor Panel · pulled · May 19, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 222CF UPPER SKIN HAS PULLED STRANDS ALONG THE AFT EDGE. FWD FLOOR PANEL 222CF WITH UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026062204309](https://openairdocs.org/sdr/SWAA2026062204309.md): Floor Panel · pulled · May 19, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 222DF UPPER SKIN HAS PULLED STRANDS ALONG THE FWD EDGE. FWD FLOOR PANEL 222DF DAMAGE WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2026062204620](https://openairdocs.org/sdr/SWAA2026062204620.md): Shield · corroded · May 19, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB FWD SHIELD WEB BETWEEN BS 767 - 792, RBL 25, WL 156. REMOVED AND REPLACED THE SHIELD IAW SRM 51-40-02-0G-0, AND DWG 146A0081, REV A.
- [SDR SWAA2026062204523](https://openairdocs.org/sdr/SWAA2026062204523.md): Threshold Web · corroded · May 19, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FCB SUB THRESHOLD WEB BETWEEN BS 440 - 492, RBL 25, WL 156. P 5 REJECT DUE TO COMMON STRUCTURE TO SUB-THRESHOLD HAS BEEN COUNTERSINK. REMOVED AND REPLACED FCB THRESHOLD WEB IAW SRM 51-40-02-0G-0, DWG 143A8330, REV B.
- [SDR SWAA2026062204121](https://openairdocs.org/sdr/SWAA2026062204121.md): Floorbeam · corroded · May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON BS 947 FLOORBEAM UPPER FLANGE, LBL 49 AND LBL 53, WL 208. PERFORMED REPAIR ON THE FLOORBEAM IAW SRM 53-70-51-2R-5, REPAIR 5.
- [SDR SWAA2026062204124](https://openairdocs.org/sdr/SWAA2026062204124.md): Floorbeam · corroded · May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON BS 986.5 FLOORBEAM UPPER FLANGE AT NUTPLATE HOLE LBL 43, WL 208. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6, FIG 205.
- [SDR SWAA2026062204122](https://openairdocs.org/sdr/SWAA2026062204122.md): Support Angle · corroded · May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON RT ZEE SUPPORT ANGLE AT BS 986.5+6, RBL 37, WL 208. REMOVED AND REPLACED RT ZEE SUPPORT ANGLE AT BS 986.5, RBL 37, WL 208 IAW SRM 51-40-02-0G-0, AND DWG 147A5700, REV A.
- [SDR SWAA2026062204270](https://openairdocs.org/sdr/SWAA2026062204270.md): Support Angle · corroded · May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON RT ZEE SUPPORT ANGLE AT BS 986.5+6, RBL 32, WL 208. REMOVED AND REPLACED RT ZEE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 147A5700, REV A.
- [SDR SWAA2026062204271](https://openairdocs.org/sdr/SWAA2026062204271.md): Sill Drain · corroded · May 18, 2026 · N8646B · Boeing 7378H4 · Emergency Exits
  > CORROSION ON ASD MOP SILL AT BS 947+8, RBL 56, WL 208. REMOVED & INSTALLED NEW AFT SERVICE DOOR MOP SILL FROM 887+10 -1006 IAW SRM 51-40-02; DWG 147A8501 REV:A,; & DWG 147A0000 REV A.
- [SDR SWAA2026062204268](https://openairdocs.org/sdr/SWAA2026062204268.md): Support Strap · corroded · May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SHEAR WEB SUPPORT STRAP AT BS 1016+3, RBL 3, WL 208. REMOVED AND REPLACED SHEAR WEB SUPPORT STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5700, REV A.
- [SDR SWAA2026062204272](https://openairdocs.org/sdr/SWAA2026062204272.md): Support Strap · corroded · May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SHEAR WEB SUPPORT STRAP AT BS 1016+3 AND 1016+12, LBL 3, WL 208. REMOVED AND REPLACED THE SHEAR WEB STRAP IAW SRM 51-40-02-0G-0, AND DWG 147A5700, REV A.
- [SDR SWAA2026062204281](https://openairdocs.org/sdr/SWAA2026062204281.md): Support Bracket · cracked · May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > LOWER BULKHEAD SUPPORT BRACKET AT BS 867, LBL 3, WL 156 CRACKED. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02-0G-0.
- [SDR SWAA2026062204273](https://openairdocs.org/sdr/SWAA2026062204273.md): Support Bracket · cracked · May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ACB FWD BULKHEAD SUPPORT BRACKET AT BS 731, BL 0, WL 160 IS CRACKED. REMOVED AND REPLACED ACB FWD BULKHEAD BRACKET ASSY IAW SRM 51-40-02 AND DWG 144A2600, REV -.
- [SDR SWAA2026062204297](https://openairdocs.org/sdr/SWAA2026062204297.md): Access Panel · debonded · May 18, 2026 · N8646B · Boeing 7378H4 · Aerodynamic Fairings
  > ACCESS PANEL 191FL L/E IS DISBONDED. REPAIRED DISBONDED L/E ON ACCESS PANEL 191FL IAW SRM 53-30-70-2R-1 AND SRM 51-70-05-2R-6.
- [SDR SWAA2026062204269](https://openairdocs.org/sdr/SWAA2026062204269.md): Support Angle · corroded · May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON LT ZEE SUPPORT ANGLE AT BS 986.5+6, LBL 37, WL 208. REMOVED AND REPLACED RT ZEE SUPPORT ANGLE BS 986.5+6, LBL 37, WL 208 IAW SRM 51-40-02, SRM 51-40-02-0G-0, AND DWG 147A5700, REV A;
- [SDR SWAA2026062203781](https://openairdocs.org/sdr/SWAA2026062203781.md): Sidewall Support · corroded · May 17, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON RT AFT CARGO FLOOR TO SIDEWALL SUPPORT, BS 727 - 747, RBL 21, WL 156. REMOVED AND REPLACED SIDEWALL SUPPORT IAW SRM 51-40-02, AND DWG 146A7500, REV-.
- [SDR SWAA2026062203782](https://openairdocs.org/sdr/SWAA2026062203782.md): Sidewall Support · corroded · May 17, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT BS 867 - 927, RBL 21, WL 157. REMOVED AND REPLACED SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV-.
- [SDR SWAA2026062203788](https://openairdocs.org/sdr/SWAA2026062203788.md): Floor Support · corroded · May 17, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB FLOOR PANEL TO FLOOR PANEL SUPPORT BS 887, RBL 3 - 12, WL 168. REMOVED AND REPLACED FLOOR PANEL SUPPORT IAW SRM 51-40-02 AND DWG 146A7500 REV-.
- [SDR SWAA2026062203783](https://openairdocs.org/sdr/SWAA2026062203783.md): Threshold Web · corroded · May 17, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB SUB THRESHOLD WEB AT BS 797 - 824, RBL 26, WL 157. REMOVED A REPLACED ACB SUB THRESHOLD WEB IAW SRM 51-40-02-0G-0, AND DWG:146A8340 REV-.
- [SDR SWAA2026062203786](https://openairdocs.org/sdr/SWAA2026062203786.md): Strap · corroded · May 17, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB THRESHOLD TRACK FASTENER HOLES AT BS 797 - 824, RBL 19, WL 158. REPLACED THE STRAP IAW SRM 51-40-02-0G-0.
- [SDR SWAA2026062203784](https://openairdocs.org/sdr/SWAA2026062203784.md): Support · corroded · May 17, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON LH AFT BODY TO SIDE WALL SUPPORT BS 736 - 799, LBL 21, WL 156. REMOVED AND REPLACED SIDEWALL SUPPORT IAW SRM 51-40-02 AND DWG 146A7500, REV-;
- [SDR SWAA2026062203785](https://openairdocs.org/sdr/SWAA2026062203785.md): Support · corroded · May 17, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB BODY TO AFT BULKHEAD SUPPORT BS 947, LBL 10, RBL 15, WL 179. REMOVED AND REPLACED BULKHEAD SUPPORT IAW SRM 51-40-02, AND DWG 149A8117, REV-.
- [SDR SWAA2026062204619](https://openairdocs.org/sdr/SWAA2026062204619.md): Sidewall Panel · corroded · May 16, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SIDEWALL FCB BS 500C+16.5; BS 500C+19; BS 500D+2.5; BS 500D+7; BS 500D+11 RBL 24.5. THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550'.;
- [SDR SWAA2026062203985](https://openairdocs.org/sdr/SWAA2026062203985.md): Shield · corroded · May 16, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SHIELD FCB BS 480+16, BS 500+14, RBL 24.5. REMOVED AND REPLACED FCB AFT SHIELD IAW SRM 51-40-02-0G-0, AND DWG 143A0080, REV -.
- [SDR SWAA2026062203777](https://openairdocs.org/sdr/SWAA2026062203777.md): Doubler · corroded · May 16, 2026 · N8646B · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > BS 727, BL 0, EXTERNAL SKIN AT PRESSURE DRAIN VALVE WAS CORRODED AT RIVETS. REMOVED AND REPLACED PRESSURE DRAIN VALVE DOUBLER BS 727, BL 0, WL 148 IAW SRM 51-40-02, AND DWG 146A3230 REV -.
- [SDR SWAA2026062203199](https://openairdocs.org/sdr/SWAA2026062203199.md): Floor Panel · pulled · May 15, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 & DWG 144A5810.
- [SDR SWAA2026062203201](https://openairdocs.org/sdr/SWAA2026062203201.md): Floor Panel · pulled · May 15, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 231ZF 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 SWAA2026062203200](https://openairdocs.org/sdr/SWAA2026062203200.md): Floor Panel · pulled · May 15, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, AND DWG 144A5810.
- [SDR SWAA2026062203204](https://openairdocs.org/sdr/SWAA2026062203204.md): Floor Panel · pulled · May 15, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, DWG 144A5810.
- [SDR SWAA2026062203202](https://openairdocs.org/sdr/SWAA2026062203202.md): Floor Panel · pulled · May 15, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 232SF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. THE FLOOR PANEL 232SF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1.
- [SDR SWAA2026062203203](https://openairdocs.org/sdr/SWAA2026062203203.md): Floor Panel · pulled · May 15, 2026 · N8646B · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-0-B00275,
- [SDR SWAA2026062203776](https://openairdocs.org/sdr/SWAA2026062203776.md): Scuff Plate · cracked · May 15, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ACD FWD CORNER SCUFF PLATE IS CRACKED. REMOVED AND REPLACED ACD FWD CORNER SCUFF PLATE IAW SRM 51-40-02, AND DWG 146A8341, REV A.
- [SDR SWAA2025110731301](https://openairdocs.org/sdr/SWAA2025110731301.md): Fuse · failed · Nov 3, 2025 · N8646B · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS L01207 AND L01208 DO NOT ILLUMINATE. REMOVED AND REPLACED FUSE IN M1694 AND PERFORMED A GOOD TEST IAW AMM 33-51-06-960-804.
- [SDR SWAA2025081303565](https://openairdocs.org/sdr/SWAA2025081303565.md): Circuit Breaker · broken · Aug 12, 2025 · N8646B · Boeing 7378H4 · Light System Wiring
  > CABIN EMER LIGHTS C/B BROKEN OFF. R & R CABIN EMERGENCY LIGHT BREAKER IAW WDM #33-51-11. OPS CK GOOD. ALSO SWPM 20-30-00.
- [SDR SWAA2024082829711](https://openairdocs.org/sdr/SWAA2024082829711.md): Light · dim · Aug 24, 2024 · N8646B · Boeing 7378H4 · Emergency Lighting
  > IN THE PASSENGER CABIN; THE PHOTO LUMINESCENT LIGHT STRIP UPPER SURFACES HAVE PART NUMBER STICKERS IN NUMEROUS AREAS.<[01] CLEANED PHOTO LUMINESCENT LIGHT STRIP UPPER SURFACES IAW AMM 25-00-00.;[02] REJECT: CORRECTIVE ACTION #1 IS SIGNED OFF BUT TASK IS NOT CO
- [SDR SWAA2024082829180](https://openairdocs.org/sdr/SWAA2024082829180.md): Battery Pack · inoperative · Aug 22, 2024 · N8646B · Boeing 7378H4 · Emergency Lighting
  > R2 DOOR OVER-DOOR EMERGENCY EXIT SIGN LIGHT INOP.<[01] R/R BATTERY PACK(AFT R/H GALLEY) PER AMM 33-51-06. OPS CHECK GOOD.;[02] VERIFIED
- [SDR SWAA2024082826415](https://openairdocs.org/sdr/SWAA2024082826415.md): Intercostal · cracked · Aug 16, 2024 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > REMOVED FLOOR PANEL 231UF FOR 540 INTERCOSTAL CRACKED<[01] OK TO CLOSE PANEL.;[02] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.;[03] INSPECTED WORK PERFORMED
- [SDR SWAA2024082826413](https://openairdocs.org/sdr/SWAA2024082826413.md): Vapor Barrier · elongated · Aug 15, 2024 · N8646B · Boeing 7378H4 · Fuselage Main, Bulkhead
  > VAPOR BARRIER WEB UNDER VERTICAL LEG OF UPPER CHORD AT LBL 20 HAS TWO ELONGATED FASTENER HOLES<[01] REPAIRED PER EA 24-157-02249;[02] 1. DAVID BASTIAN (TECHNICIAN); 21-AUG-2024 15:59 UTC<BR>REPAIRED PER EA 24-157-02249 RII
- [SDR SWAA2024082823152](https://openairdocs.org/sdr/SWAA2024082823152.md): Beam · cracked · Aug 6, 2024 · N8646B · Boeing 7378H4 · Fuselage Main, Structure
  > R/H AC BAY LWR T CHORD CRACKED AT STA 663 RBL 42.<[01] DUPLICATE DISCREPANCY. SEE FAULT TTG8Q00V12TU FOR CHORD REPLACEMENT. MPM 52.02.05
- [SDR SWAA2024082823151](https://openairdocs.org/sdr/SWAA2024082823151.md): Vapor Barrier · cracked · Aug 6, 2024 · N8646B · Boeing 7378H4 · Fuselage Main, Bulkhead
  > R/H AC BAY STA 663 VAPOR BARRIER UPPER CHORD CRACKED AT RBL 37<[01] PARTS DATA UPDATE ONLY;[02] MATCH DRILLED AND DEBURRED NEW CHORD PER SRM 51-40-02/SRM51-10-02.;[03] OK TO INSTALL NEW CHORD (RII);[04] INSTALLED AND DOMED SEALED FASTENERS COMMON TO FUEL TANK

Next page: https://openairdocs.org/aircraft/N8646B/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 = 'N8646B' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8646B/reports

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