# Service difficulty reports: N7868K

A list on [N7868K](https://openairdocs.org/aircraft/N7868K.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 5 · 231 reports

- [SDR SWAA2026100762237](https://openairdocs.org/sdr/SWAA2026100762237.md): Battery Pack · inoperative · Oct 1, 2026 · N7868K · Boeing 73779P · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INOPERATIVE. REMOVED, REPLACED, AND PERFORMED SATISFACTORY OPS CHECK OF EMERGENCY LIGHT BATTERIES LOCATION M1675, M01669, M01672, AND M01673 IAW AMM 33-51-06.
- [SDR SWAA2026100714266](https://openairdocs.org/sdr/SWAA2026100714266.md): Battery Pack · inoperative · Oct 1, 2026 · N7868K · Boeing 73779P · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INOPERATIVE. REMOVED, REPLACED, & PERFORMED A SATISFACTORY OPS CHECK OF THE BATTERIES, M1675, M01669, M01672, & M01673 IAW IAW AMM 33-51-06.
- [SDR SWAA2026100791478](https://openairdocs.org/sdr/SWAA2026100791478.md): Battery Pack · inoperative · Oct 1, 2026 · N7868K · Boeing 73779P · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INOPERATIVE. REMOVED, REPLACED, & PERFORMED SATISFACTORY OPS CHECK OF EMERGENCY LIGHT BATTERIES, M1675, M01669, M01672, & M01673 IAW AMM 33-51-06.
- [SDR SWAA2026100774168](https://openairdocs.org/sdr/SWAA2026100774168.md): Battery Pack · inoperative · Oct 1, 2026 · N7868K · Boeing 73779P · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE. REMOVED, REPLACED, & PERFORMED A SATISFACTORY OPS CHECK OF THE EMERGENCY LIGHT BATTERIES, M1675, M01669, M01672, & M01673 IAW AMM 33-51-06.
- [SDR SWAA2026100754271](https://openairdocs.org/sdr/SWAA2026100754271.md): Battery Pack · inoperative · Oct 1, 2026 · N7868K · Boeing 73779P · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INOPERATIVE. REMOVED, REPLACED AND PERFORMED SATISFACTORY OPS CHECK OF EMERGENCY LIGHT BATTERIES M1675, M01669, M01672, & M01673 IAW AMM 33-51-06.
- [SDR SWAA2026080320505](https://openairdocs.org/sdr/SWAA2026080320505.md): Lamp · inoperative · Jul 30, 2026 · N7868K · Boeing 73779P · Emergency Lighting
  > LEFT OVERWING EXIT WINDOW LIGHT INOPERATIVE. RELAMPED IAW 33-51-01.
- [SDR SWAA2026070618272](https://openairdocs.org/sdr/SWAA2026070618272.md): Girt Bar · out of adjust · Jul 3, 2026 · N7868K · Boeing 73779P · Emergency Equipment
  > L1 DOOR LT GIRT BAR CLIP LOST TENSION AND GIRT BAR SLIPS OUT. ADJUSTED GIRT BAR CLIPS ON L1 DOOR IAW SIP. OPS CHECKED GOOD.
- [SDR SWAA2026070618013](https://openairdocs.org/sdr/SWAA2026070618013.md): Slide · out of position · Jul 2, 2026 · N7868K · Boeing 73779P · Escape Slide
  > L1 DOOR EMERGENCY ESCAPE SLIDE NOT IN STOWED POSITION. SECURED FWD ENTRY DOOR SLIDE PER MT 725-61-06.
- [SDR SWAA2026062415020](https://openairdocs.org/sdr/SWAA2026062415020.md): Hook · loose · Jun 22, 2026 · N7868K · Boeing 73779P · Emergency Equipment
  > GIRT BAR STOWAGE HOOKS AT FWD SERVICE DOOR LOOSE. ADJUSTED THE HOOKS IAW MM SIP.
- [SDR SWAA2026060808621](https://openairdocs.org/sdr/SWAA2026060808621.md): Sensor · out of range · Jun 2, 2026 · N7868K · Boeing 73779P · Engine Temperature Indicating System
  > MAX T/O THRUST MTJ 97.1 N1 ON CLIMB NR 2 EGT INDICATED 966. REDUCED NR 2 THRUST BELOW REDLINE. INDICATIONS NORMAL AFTER - NO MASTER CAUTION LIGHTS. CW FIM 77-21 TASK 801 FOUND J9 HARNESS AND/OR PROBE OUT OF RANGE. REMOVED AND REPLACED PROBE T49.5 S4 SENSOR
- [SDR SWAA2025120339727](https://openairdocs.org/sdr/SWAA2025120339727.md): Fuse · blown · Nov 26, 2025 · N7868K · Boeing 73779P · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS SURROUNDING RT OVERWING EXIT INOPERATIVE. REPLACED THE FUSE AND PERFORMED A GOOD OPS TEST OF EMERGENCY LIGHTS SURROUNDING RT OVERWING EXIT IAW AMM 33-51-06-960-804.
- [SDR SWAA2025120338522](https://openairdocs.org/sdr/SWAA2025120338522.md): Light · damaged · Nov 21, 2025 · N7868K · Boeing 73779P · Emergency Lighting
  > FWD OF RT OVERWING EXIT DOOR EXIT LIGHT DAMAGED. INSTALLED NEW RT OVERWING EXIT DOOR LIGHT ASSY IAW AMM 33-51-01-960-802, STEPS 3, (C).(9).(10). PERFORMED SUCCESSFUL OPS TEST ON RT OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-51-00-720-801.
- [SDR SWAA2025120336818](https://openairdocs.org/sdr/SWAA2025120336818.md): Glowstrip · damaged · Nov 19, 2025 · N7868K · Boeing 73779P · Emergency Equipment
  > CABIN PHOTOLUM, SHIP SET FOUND DAMAGED REQUIRE REPLACEMENT. INSTALLED PHOTOLUMINESCENT STRIPS EXCEPT SEGMENTS AP AND AN PER SWA DWG 33500007 REV 2, AND AMM 33-51-15-400-802.
- [SDR SWAA2025121534525](https://openairdocs.org/sdr/SWAA2025121534525.md): Rib · cracked · Nov 13, 2025 · N7868K · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > FOUND ONE CRACK RADIATING FROM FASTENER HOLE AT LT HORIZONTAL STAB RIB 5, HSS 129.50, LOWER FLANGE ADJACENT TO THE NR 1 VERTICAL STIFFENER.
- [SDR SWAA2025120334898](https://openairdocs.org/sdr/SWAA2025120334898.md): Stiffener · cracked · Nov 13, 2025 · N7868K · Boeing 73779P · Horizontal Stabilizer Miscellaneous Structure
  > FOUND CRACK RADIATING FROM ONE FASTENER HOLE, LT HORIZONTAL STAB RIB 5 HSS 129.50 LOWER FLANGE ADJACENT TO NR 4 VERTICAL STIFFENER. REPAIRED LWR FLANGE NR.4 STIFFENER; IAW SRM 55-10-09-2R-5.
- [SDR SWAA2025120334113](https://openairdocs.org/sdr/SWAA2025120334113.md): Attach Angle · cracked · Nov 12, 2025 · N7868K · Boeing 73779P · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT FCB BS 500B AFT SIDE, RBL 25, WL 154. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-05, & DWG 143A7505 REV A.
- [SDR SWAA2025120334515](https://openairdocs.org/sdr/SWAA2025120334515.md): Seal · cracked · Nov 12, 2025 · N7868K · Boeing 73779P · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED. REMOVED AND REPLACED THE HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-000-802, & AMM 53-31-31-400-802.
- [SDR SWAA2025120334112](https://openairdocs.org/sdr/SWAA2025120334112.md): Stiffener · cracked · Nov 12, 2025 · N7868K · Boeing 73779P · Horizontal Stabilizer Structure
  > NUMBER 2 VERTICAL STIFFENER AT LT HORIZONTAL STAB, RIB 5, HSS 129.50 IS CRACKED. REPAIRED THE STIFFENER; IAW SRM 55-10-09-2R-4.
- [SDR SWAA2025120333713](https://openairdocs.org/sdr/SWAA2025120333713.md): Web · chafed · Nov 11, 2025 · N7868K · Boeing 73779P · Fuselage Miscellaneous Structure
  > E/E BAY DOOR SURROUND STRUCTURE LONGITUDINAL CLOSE-OUT WEB HAS CHAFING DAMAGE ON THE TOP EDGE, BS 337.5, RBL 11.5. REMOVED, FABRICATED, & REPLACED THE CLOSE-OUT WEB IAW SRM 51-40-02-0G-0, & DWG 141A85110002, REV -, SRM 53-10-15-0I-3, TABLE 3, ITEM 8.
- [SDR SWAA2025120334103](https://openairdocs.org/sdr/SWAA2025120334103.md): Gusset · cracked · Nov 11, 2025 · N7868K · Boeing 73779P · Fuselage Miscellaneous Structure
  > FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED, BS 500D, S19R, WL 193. REMOVED & REPLACED THE SUPPORT GUSSET IAW SRM 51-40-02, & DWG 143A79020259, REV -.
- [SDR SWAA2025120334102](https://openairdocs.org/sdr/SWAA2025120334102.md): Gusset · cracked · Nov 11, 2025 · N7868K · Boeing 73779P · Fuselage Miscellaneous Structure
  > FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED, BS 500D, S19L, WL 193. REMOVED & REPLACEDTHE SUPPORT GUSSET IAW SRM 51-40-02, & DWG 143A79020259, REV -.
- [SDR SWAA2025120334105](https://openairdocs.org/sdr/SWAA2025120334105.md): Attach Angle · cracked · Nov 11, 2025 · N7868K · Boeing 73779P · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT FCB BS 500C, FWD SIDE, LBL 25, WL 154. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-02, & DWG 143A75050005, REV -.
- [SDR SWAA2025120334108](https://openairdocs.org/sdr/SWAA2025120334108.md): Attach Angle · cracked · Nov 11, 2025 · N7868K · Boeing 73779P · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT FCB BS 500C, AFT SIDE, LBL 25, WL 154. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02, & DWG 143A75050005, REV-.
- [SDR SWAA2025120334106](https://openairdocs.org/sdr/SWAA2025120334106.md): Attach Angle · cracked · Nov 11, 2025 · N7868K · Boeing 73779P · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT FCB BS 500C, FWD SIDE, RBL 25, WL 154. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02, AND DWG 143A7505, REV D.
- [SDR SWAA2025120334109](https://openairdocs.org/sdr/SWAA2025120334109.md): Attach Angle · cracked · Nov 11, 2025 · N7868K · Boeing 73779P · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT FCB BS 500B, FWD SIDE, RBL 25, WL 154. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-05, AND DWG 143A7505, REV B.
- [SDR SWAA2025120334110](https://openairdocs.org/sdr/SWAA2025120334110.md): Attach Angle · cracked · Nov 11, 2025 · N7868K · Boeing 73779P · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT FCB BS 400, LBL 25, WL 154. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02, & DWG 143A75050012 REV -.
- [SDR SWAA2025120335209](https://openairdocs.org/sdr/SWAA2025120335209.md): Wire · pulled · Nov 11, 2025 · N7868K · Boeing 73779P · Light System Wiring
  > FOUND WIRES W3142-476-20 AND W3142-474-20 PULLED FROM GROUND BLOCK BS 986 LT. TERMINATED WIRES W3142-476-20 AND W3142-474-20 & INSTALLED ON GB3814 IAW SWPM 20-90-15, WDM 33-26-11, & 33-51-14.
- [SDR SWAA2025120334104](https://openairdocs.org/sdr/SWAA2025120334104.md): Support · cracked · Nov 11, 2025 · N7868K · Boeing 73779P · Aerodynamic Fairings
  > RIGHT WING TO BODY FORMER SUPPORT CRACKED JUST INBD OF FIXED L/E BS 500D, S19R, ACCESS PANEL 191FR. REMOVED AND REPLACED THE WING TO BODY FORMER SUPPORT IAW SRM 51-40-02, AND DWG: 116A3010 REV -.
- [SDR SWAA2025120333709](https://openairdocs.org/sdr/SWAA2025120333709.md): Stringer Clip · cracked · Nov 10, 2025 · N7868K · Boeing 73779P · Fuselage Main, Attach Fittings
  > ATTACH ANGLE BS 259.5 S8L CRACKED. REMOVED AND REPLACED STRINGER CLIP BS 259.5 S8L HEAT TREATED TO T6 CONDITION ON CARD RO 1065210-SWA IAW SRM 51-40-02-0G-0 AND DWG 141A0720 REV -.
- [SDR SWAA2025120333182](https://openairdocs.org/sdr/SWAA2025120333182.md): Attach Angle · corroded · Nov 9, 2025 · N7868K · Boeing 73779P · Fuselage Main, Attach Fittings
  > AFT CARGO BAY FRAME TO SIDEWALL SUPPORT ATTACH ANGLE HAS CORROSION ON UPPER FLANGE AT FASTENER HOLES, BS 727D, S19L - S25L. REMOVED AND REPLACED AFT CARGO BAY FRAME TO SIDEWALL SUPPORT ATTACH ANGLE IAW SRM 51-40-02, & DWG 146A12290073 REV -.
- [SDR SWAA2025120333187](https://openairdocs.org/sdr/SWAA2025120333187.md): Sidewall Support · corroded · Nov 9, 2025 · N7868K · Boeing 73779P · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY DOOR SURROUND STRUCTURE HAS CORROSION ON AFT FLOOR TO SIDEWALL SUPPORT AROUND FASTENER HOLES, BS 492 - 500A, RBL 24. REMOVED & REPLACED SIDWALL SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 143A0080 REV-.
- [SDR SWAA2025120333188](https://openairdocs.org/sdr/SWAA2025120333188.md): Sidewall Support · corroded · Nov 9, 2025 · N7868K · Boeing 73779P · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY DOOR SURROUND STRUCTURE FORWARD FLOOR TO SIDEWALL SUPPORT HAS CORROSION AROUND FASTENER HOLES; BS 420 - 440, RBL 24. REMOVED & REPLACED THE SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 143A0080, REV-.
- [SDR SWAA2025120333428](https://openairdocs.org/sdr/SWAA2025120333428.md): Panel · delaminated · Nov 9, 2025 · N7868K · Boeing 73779P · Aerodynamic Fairings
  > PANEL 194CR HAS DELAMINAION ON OUTER SURFACE. PANEL 194CR WITH DELAMINATION ON OUTER SURFACE WAS REPAIRED IAW SRM 51-70-05-2R-2, & SRM 53-60-70-2R-1.
- [SDR SWAA2025120333427](https://openairdocs.org/sdr/SWAA2025120333427.md): Panel · delaminated · Nov 9, 2025 · N7868K · Boeing 73779P · Aerodynamic Fairings
  > PANEL 194CL HAS DELAMINAION ON OUTER SURFACE. REPAIRED IAW AMM 51-21-99-300-802.
- [SDR SWAA2025120332952](https://openairdocs.org/sdr/SWAA2025120332952.md): Sidewall Support · corroded · Nov 8, 2025 · N7868K · Boeing 73779P · Fuselage Miscellaneous Structure
  > AFT CARGO BAY CORROSION ON LT FLOOR TO SIDEWALL SUPPORT AT FASTENER HOLES; BS 727 - 847. REMOVED AND REPLACED SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV A.
- [SDR SWAA2025120332951](https://openairdocs.org/sdr/SWAA2025120332951.md): Sidewall Support · corroded · Nov 8, 2025 · N7868K · Boeing 73779P · Fuselage Miscellaneous Structure
  > AFT CARGO BAY CORROSION ON RT FLOOR TO SIDEWALL SUPPORT AT FASTENER HOLES, BS 767 - 787. REMOVED AND REPLACED AFT CARGO BAY RT FLOOR TO SIDEWALL IAW SRM 51-40-02 AND DWG 146A0081 REV A.
- [SDR SWAA2025120332954](https://openairdocs.org/sdr/SWAA2025120332954.md): Sidewall Support · corroded · Nov 8, 2025 · N7868K · Boeing 73779P · Fuselage Miscellaneous Structure
  > AFT CARGO BAY CORROSION AT FASTENER HOLES ON R/H FLOOR TO SIDEWALL SUPPORT BS 727-767. REMOVED AND REPLACED THE SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV A.
- [SDR SWAA2025120332586](https://openairdocs.org/sdr/SWAA2025120332586.md): Scuff Plate · cracked · Nov 7, 2025 · N7868K · Boeing 73779P · Fuselage Miscellaneous Structure
  > FCB FWD CORNER SCUFF PLATE IS CRACKED. RECEIVED NEW FCB FWD CORNER SCUFF PLATE AND WILL BE INSTALLED ON TC TTG8Q00A5WT6.
- [SDR SWAA2025120332947](https://openairdocs.org/sdr/SWAA2025120332947.md): Scuff Plate · cracked · Nov 7, 2025 · N7868K · Boeing 73779P · Fuselage Miscellaneous Structure
  > ACD FWD CORNER SCUFF PLATE IS CRACKED. REPAIRED ACB FWD CORNER SCUFF PLATE PER SRM 53-60-15-2R-1. TASK CARD COMPLETED.
- [SDR SWAA2025120332826](https://openairdocs.org/sdr/SWAA2025120332826.md): Intercostal · cracked · Nov 7, 2025 · N7868K · Boeing 73779P · Fuselage Miscellaneous Structure
  > FED INTERCOSTAL FROM BS 294.5 - 303.9, S16L, WL 216 CRACKED. REMOVED AND REPLACED FED INTERCOSTAL IAW SRM 51-40-02 AND DWG 141A8180 REV: C.
- [SDR SWAA2025120332827](https://openairdocs.org/sdr/SWAA2025120332827.md): Rib · cracked · Nov 7, 2025 · N7868K · Boeing 73779P · Horizontal Stabilizer, Spar/Rib
  > STIFFENER NR 3 AT LT HORIZONTAL STAB (RIB 5) HSS 129.50 CRACKED. REPAIRED THE STIFFENER; IAW SRM 55-10-09-2R-4, HSS 129.5.
- [SDR SWAA2025121532380](https://openairdocs.org/sdr/SWAA2025121532380.md): Drip Tray · cracked · Nov 6, 2025 · N7868K · Boeing 73779P · Fuselage Main, Structure
  > AFT RT DRIP SHIELD IS CRACKED.
- [SDR SWAA2025120332382](https://openairdocs.org/sdr/SWAA2025120332382.md): Battery Pack · no test · Nov 6, 2025 · N7868K · Boeing 73779P · Emergency Lighting
  > BATTERY PACK M1670 FAILED TEST. R & R BATTERY PACK M1670 IAW AMM 33-51-06-960-805 & PERFORMED GOOD OPS CHECK.
- [SDR SWAA2025120232381](https://openairdocs.org/sdr/SWAA2025120232381.md): Battery Pack · no test · Nov 6, 2025 · N7868K · Boeing 73779P · Emergency Lighting
  > BATTERY PACK M1668 FAILED TEST. R & R BATTERY PACK M1668 AND PERFORMED GOOD OPS CHECK IAW AMM 33-51-06-960-805.
- [SDR SWAA2025120332129](https://openairdocs.org/sdr/SWAA2025120332129.md): Scuff Plate · cracked · Nov 5, 2025 · N7868K · Boeing 73779P · Fuselage Miscellaneous Structure
  > FORWARD SERVICE DOOR AFT LOWER CORNER; SCUFF PLATE HAS A CRACK. WELDED CRACKED / DAMAGED AREA OF SCUFF PLATE IAW SRM 53-10-15-2R-2, STEP 4.B.(4). APPLIED TWO COATS OF PRIMER AT FSD SCUFF PLATE IAW AMM 51-11-01-420-801 STEP 3D (1) (B). FSD SCUFF PLATE WILL BE
- [SDR SWAA2025071791330](https://openairdocs.org/sdr/SWAA2025071791330.md): Scuff Plate · cracked · Jul 15, 2025 · N7868K · Boeing 73779P · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CENTER SCUFF PLATE HAS A LARGE CENTER DENT AND CRACK ON ITS RADIUS. REMOVED AND REPLACED PER AMM 53-11-02-401-NG (CARGO DOOR SCUFF PLATE - REMOVAL/INSTALLATION - PERMANENT) AFT CARGO DOOR CENTER SCUFF PLATE.
- [SDR SWAA2025030601928](https://openairdocs.org/sdr/SWAA2025030601928.md): Battery Pack · inoperative · Mar 4, 2025 · N7868K · Boeing 73779P · Emergency Lighting
  > EMERGENCY LIGHTS ABOVE L1 DOOR AND OUTSIDE THE R1 DOOR ARE INOP.<[01] 01 - REMOVED AND REPLACED M1674 BATTERY PACK PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024101446131](https://openairdocs.org/sdr/SWAA2024101446131.md): Battery Pack · no test · Oct 8, 2024 · N7868K · Boeing 73779P · Emergency Lighting
  > AFT R/H EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06
- [SDR SWAA2024080221385](https://openairdocs.org/sdr/SWAA2024080221385.md): Seat Back · out of adjust · Aug 1, 2024 · N7868K · Boeing 73779P · Passenger Compartment Equipment
  > SEAT 11D IN FRONT OF EXIT ROW RECLINES<[01] INSTALLED RECLINE LOCKS IAW AMM 25-22-00
- [SDR SWAA2024051585436](https://openairdocs.org/sdr/SWAA2024051585436.md): Seat Track · cracked · May 14, 2024 · N7868K · Boeing 73779P · Fuselage, Seat/Cargo Attach Fittings
  > CAPTS I/B FWD SEAT TRACK IS CRACKED<[01] R/R?D CAPTS I/B FWD SEAT TRACK IAW MM 25-11-11

Next page: https://openairdocs.org/aircraft/N7868K/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 = 'N7868K' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7868K/reports

---
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.