# Service difficulty reports: Boeing 767-224

A list on [Boeing 767-224](https://openairdocs.org/model/boeing-767-224.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 224 reports

- [SDR CNMA202601230001](https://openairdocs.org/sdr/CNMA202601230001.md): Charger · odor · Jan 23, 2026 · N207AX · Boeing 767224 · Battery/Charger System
  > PILOTS REPORTED MAIN BAT CHARGER HAD A STRONG BURNING SMELL.
- [SDR CNMA2024050001](https://openairdocs.org/sdr/CNMA2024050001.md): Panel · dented · May 7, 2024 · N207AX · Boeing 767224 · Wing, Plate/Skin
  > PANEL 611 FB REMOVED FROM A/C DUE TO BIRDSTRIKE
- [SDR CNMA202404230001](https://openairdocs.org/sdr/CNMA202404230001.md): Gcu · failed · Apr 18, 2024 · N225AX · Boeing 767224 · AC Generator-Alternator
  > EICAS R AC BUS OFF. STATUS: WXR SYS / R ICE DETECTOR / HI FLOW INHIBIT
- [SDR CNMA](https://openairdocs.org/sdr/CNMA.md): Fuel Cap · leaking · Jan 30, 2021 · N207AX · Boeing 767224 · Fuel Storage
  > RIGHT WING SINGLE POINT FUEL CAP LEAKING. CORRECTIVE ACTION: REMOVED AND REPLACED SPR FUEL CAP IAW 767 AMM 28-11.
- [SDR MK1Y20200327001](https://openairdocs.org/sdr/MK1Y20200327001.md): Bulkhead · dented · Mar 26, 2020 · N430CJ · Boeing 767224 · Fuselage Main, Bulkhead
  > BULKHEAD FOUND DENTED AT STA 1702
- [SDR CNMA2019120310001](https://openairdocs.org/sdr/CNMA2019120310001.md): Radar · shorted · Nov 29, 2019 · N234AX · Boeing 767224 · Weather Radar System
  > SMOKE CENTER PEDESTAL AT TOC. CORRECTIVE ACTION: REMOVED AND REPLACED WEATHER RADAR CONTROL PNL DO TO SHORTING, SMOKE, AND HEAVY BURNT SMELL. IAW AMM 34-43
- [SDR CNMA201810100001](https://openairdocs.org/sdr/CNMA201810100001.md): Audio Control · failed · Oct 4, 2018 · N225AX · Boeing 767224 · VHF Communications System
  > LT VHF RADIO FAIL AND RT VHF RADIO FAIL CORRECTIVE ACTION: REMOVED AND REPLACED (CA'S) RADIO CONTROL PANEL IAW AMM 23-10. OPS CHECKED GOOD. AND REMOVED AND REPLACED AUDIO CONTROL PANEL (F/O'S) IAW AMM 23-51. OPS CHECKED GOOD.
- [SDR CNMA2018020001](https://openairdocs.org/sdr/CNMA2018020001.md): Clamp · loose · Feb 13, 2018 · N207AX · Boeing 767224 · Potable Water System
  > EICAS MESSAGES CABIN AUTO INOPERATIVE, CABIN ALT AUTO 1 AND CABIN ALT AUTO 2 SHOW AND AUTO INOP LIGHT IS ON. UNABLE TO CONTROL OUTFLOW VALVE IN MANUAL MODE. FOUND WATER LEAKING ONTO THE OUTFLOW VALVE. FOUND BROKEN CLAMP ON GALLEY LINE R & R CLAMP IAW AM
- [SDR CNMA201706020002](https://openairdocs.org/sdr/CNMA201706020002.md): Seal · broken · May 31, 2017 · N207AX · Boeing 767224 · Hydraulic System, Main
  > CENTER HYD QTY MESSAGE CAME ON IN FLIGHT. DRAINED TO 0.25 QTY. LANDING GEAR SELECTOR VALVE CTR HYD SYS SUPPLY LINE HAD A BROKEN SEAL. REPLACED BROKEN SEAL. LEAK & OPS CHECKED GOOD IAW AMM 32-31
- [SDR CNMA2017050001](https://openairdocs.org/sdr/CNMA2017050001.md): Charger · inoperative · May 4, 2017 · N207AX · Boeing 767224 · Emergency Lighting
  > DURING MILITARY INSPECTION, R2 DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED THE CHARGER IAW AMM 33-51 AT M734. SYSTEM CHECKED NORMAL.
- [SDR CNMA201704280001](https://openairdocs.org/sdr/CNMA201704280001.md): Battery Pack · discharged · Mar 3, 2017 · N225AX · Boeing 767224 · Emergency Lighting
  > EMERGENCY LIGHTS ROW 8 & ROW 29-35 RIGHT SIDE UNSERVICEABLE. REPLACED THE BATTERY PACK. OPS CHECKED NORMAL IAW MM 33-51.
- [SDR CNMA2016060001](https://openairdocs.org/sdr/CNMA2016060001.md): Static Line · loose · Jun 26, 2016 · N234AX · Boeing 767224 · Pitot/Static System
  > AFTER TAKEOFF, EICAS MESSAGE FOR AILERON LOCKOUT DISPLAYED AND RUDDER RATIO DISPLAYED. FOUND S1 STATIC LINE LOOSE AT CAPTAIN`S UPPER PITOT PROBE. AFTER CORRECTION THAT FAULT AILERON LOCK OUT, SYS TESTS GOOD IAW AMM 27-11
- [SDR CNMA2015090001](https://openairdocs.org/sdr/CNMA2015090001.md): Pitot Line · disconnected · Sep 28, 2015 · N234AX · Boeing 767224 · Pitot/Static System
  > IAS DISAGREE EICAS MESSAGE ALSO EICAS MESSAGE ELECTRONIC ENGINE CONTROL OFF RUDDER RATIO AND AILERON LOCKOUT. FOUND PITOT LINE AT LT ADC DISCONNECTED. RECONNECTED LINE AND PERFORMED LEAK CK IAW AMM 34-11 & OP CK GOOD IAW AMM 34-12.
- [SDR HN6R2014FA0000431](https://openairdocs.org/sdr/HN6R2014FA0000431.md): Spar · damaged · Jul 15, 2014 · N68160 · Boeing 767224 · Rudder, Spar/Rib
  > FRONT SPAR OF RUDDER DAMAGED AT RUDDER STATION 165.074. DAMAGE APPROXIMATELY 2"X 2".
- [SDR CALA2013011400038](https://openairdocs.org/sdr/CALA2013011400038.md): Control Panel · failed · Jan 12, 2013 · N69154 · Boeing 767224 · Entertainment System
  > THE ENTERTAINMENT CONTROL CENTER MS201 OPPOSITE DOOR 1R AFTER LANDING BEGAN MAKING A VIBRATING SOUND THEN SMELLED OF ELECTRICAL BURNING. ISOLATED TO IFE CONTROL PANEL. R & R IAW AMM 23-35-45-024-001, IFE OPS GOOD. NO ODOR OF SMOKE OR ELESTRICAL BURNING AT
- [SDR CALA2012112800826](https://openairdocs.org/sdr/CALA2012112800826.md): Lamp · broken · Nov 28, 2012 · N73152 · Boeing 767224 · Emergency Lighting
  > R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPS CHECKED OK.
- [SDR CALA2012112000812](https://openairdocs.org/sdr/CALA2012112000812.md): Fuse · inoperative · Nov 20, 2012 · N73152 · Boeing 767224 · Emergency Lighting
  > ROW 1D, 2D CTR SEATS AISLE PATH LIGHTING INOPERATIVE. FOUND BAD FUSE AT RT FWD PACK RW 1 KICK PNL, FUNCTIONAL CKS NORMAL.
- [SDR CALA2012110100717](https://openairdocs.org/sdr/CALA2012110100717.md): Skin · dented · Nov 1, 2012 · N76153 · Boeing 767224 · Cargo/Baggage Doors
  > FWD CARGO DOOR FWD LOWER CORNER DAMAGED. PERFORMED INTERIM REPAIR IAW PART 1 OF ECRA 5230-01794, REV A.
- [SDR CALA2012110100715](https://openairdocs.org/sdr/CALA2012110100715.md): Lamp · inoperative · Oct 31, 2012 · N73152 · Boeing 767224 · Emergency Lighting
  > EMERGENCY LIGHT AT L1 DOOR AFT UPPER SIDE INOPERATIVE (EXTERIOR). LAMPED, OPS CHECKED GOOD.
- [SDR CALA2012103100698](https://openairdocs.org/sdr/CALA2012103100698.md): Stiffener · cracked · Oct 31, 2012 · N69154 · Boeing 767224 · Fuselage Miscellaneous Structure
  > BS 246 FLOORBEAM FWD SIDE 1 STIFFENER FOUND CRACK AT LBL 40, MES - BS 246 FLOOR BEAM FWD SIDE LBL 40 STIFFENER REPAIRED IAW ECRA 5310-04828 PART 1 AND MX WORKSHEET FORM 44.0008 ITEM 1 TO ITEM 6 ACCOMPLISHED.
- [SDR CALA2012100400637](https://openairdocs.org/sdr/CALA2012100400637.md): Socket · loose · Oct 3, 2012 · N68159 · Boeing 767224 · Emergency Lighting
  > RT EXIT EMERGENCY LIGHT AFT OF CARGO DOOR INOPERATIVE. FOUND LIGHT SOCKET LOOSE IN REFLECTOR, REPLACED SOCKET AND REFLECTOR, OPS CK NORMAL.
- [SDR CALA2012100100634](https://openairdocs.org/sdr/CALA2012100100634.md): Terminal · loose · Sep 30, 2012 · N68160 · Boeing 767224 · Light System Wiring
  > EMERGENCY LIGHT CAME ON DURING CLIMBOUT AT SEATS 3, 4 AB AND 19A B KL, FLICKERED ON OND OFF REPEATEDLY. R & R TWO BATTERY PACKS AND CHARGER ASSY M730 AN D M736 REF MM 33-51-07/ UPON REMOVAL IT WAS NOTED THAT THE TERMINALS ON THE BATTERY PACK WERE LOOSE.
- [SDR CALA2012092500624](https://openairdocs.org/sdr/CALA2012092500624.md): Battery Pack · damaged · Sep 24, 2012 · N68160 · Boeing 767224 · Emergency Lighting
  > NUMEROUS EMERGENCY LIGHTS OUT IN CTR ROW F/C. R & R BATTERY PACK, OPS CHECKED GOOD. REF AMM 33-51-07-422-012.
- [SDR 2012F00178](https://openairdocs.org/sdr/2012F00178.md): Actuator · failed · Sep 7, 2012 · N76151 · Boeing 767224 · Escape Slide
  > LEFT SLIDE DID NOT DEPLOY WHILE PERFORMING CARD NR 25-031-00-01, OPS CHECK OF THE SLIDE SYS ON A SAMPLING BASIS. UPON FURTHER INVESTIGATION FOUND LT OVERWING SLIDE AUTO ARM AND FIRE SWITCHES DID NOT TRIP. MEASURED CLEARANCE BETWEEN ACTUATOR AND STRIKER PIN, B
- [SDR UALA2012F00145](https://openairdocs.org/sdr/UALA2012F00145.md): Skin · damaged · Aug 1, 2012 · N67158 · Boeing 767224 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN REPAIR PERFORMED IAW REO-G15199, REV A, AT FUSELAGE BS 368, AT STRINGER 31 LEFT.
- [SDR 2012FA0000521](https://openairdocs.org/sdr/2012FA0000521.md): Skin · dented · Aug 1, 2012 · N67158 · Boeing 767224 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT BS 1714 BETWEEN STRINGER 36 AND 37 RT. PERFORMED REPAIR IAW REO-G15177 REVB. REPAIR IS A CATEGORY A REPAIR AS DEFINED IN SRM 51-00-06.
- [SDR 2012FA0000518](https://openairdocs.org/sdr/2012FA0000518.md): Skin · dented · Jul 30, 2012 · N67158 · Boeing 767224 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT BS 1898.45 ON UPPER LEFT SURFACE. REPAIRED IAW SRM 53-00-01 FIG 201.
- [SDR CALA2012072400473](https://openairdocs.org/sdr/CALA2012072400473.md): Battery Pack · inoperative · Jul 24, 2012 · N68160 · Boeing 767224 · Emergency Lighting
  > EMERGENCY LIGHTS ROWS 3,4,5 DO NOT STAY ILLUMINATED WHEN TESTED (STAY ON FOR A FEW MINUTES THEN GO OUT). REPLACED BATTERY PACK AND POWER SUPPLY IAW AMM 33-51-07 (M730).
- [SDR 2012FA0000498](https://openairdocs.org/sdr/2012FA0000498.md): Skin · misrepaired · Jul 20, 2012 · N67158 · Boeing 767224 · Fuselage Main, Plate/Skin
  > SKIN AT BS 325 AT STRINGER 31 LT, MISREPAIRED. REPAIRED SKIN IAW SRM 53-00-01, FIG 201.
- [SDR 2012FA0000493](https://openairdocs.org/sdr/2012FA0000493.md): Skin · misrepaired · Jul 20, 2012 · N67158 · Boeing 767224 · Fuselage Main, Plate/Skin
  > DURING REPAIR ASSESSMENT IT WAS DETERMINED THAT SKIN AT BS 1793 BETWEEN STRINGERS 34 AND 35 LT WAS MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201.
- [SDR CALA2012070300425](https://openairdocs.org/sdr/CALA2012070300425.md): Megaphone · no test · Jul 2, 2012 · N68159 · Boeing 767224 · Emergency Equipment
  > AFT MEGAPHONE INTERMITENT. REPLACED AFT MEGAPHONE, CHECKED OK.
- [SDR CALA2012053100382](https://openairdocs.org/sdr/CALA2012053100382.md): Lamp · inoperative · May 22, 2012 · N69154 · Boeing 767224 · Emergency Lighting
  > CEILING EMERGENCY EXIT LIGHT ABOVE SEAT 1K INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT ABOVE SEAT 1K, CHECKED GOOD.
- [SDR CALA2012053100381](https://openairdocs.org/sdr/CALA2012053100381.md): Lamp · inoperative · May 22, 2012 · N69154 · Boeing 767224 · Emergency Lighting
  > LT OVERWING EMERGENCY EXIT LIGHT (AFT OF FLAP T/E) INOP. RELAMPED LT AFT OVERWING EMERGENCY EXIT LIGHT, CKS GOOD.
- [SDR CALA2012042000278](https://openairdocs.org/sdr/CALA2012042000278.md): Battery Pack · discharged · Apr 19, 2012 · N76156 · Boeing 767224 · Emergency Lighting
  > AISLE PATH LIGHTING INOP AT 3D, 4D, 5D LEFT AND RT HATCH. REPLACED BATTERY PACK AT M1209, CHECKS OK.
- [SDR CALA2012030500156](https://openairdocs.org/sdr/CALA2012030500156.md): Battery Pack · discharged · Mar 5, 2012 · N68159 · Boeing 767224 · Emergency Lighting
  > EMERGENCY LIGHTS AT ROWS 3, 4, 5 INOP. REPLACED BATTERY PACK AT ROW 19R, OPS CK NORMAL.
- [SDR CNMA2012020003](https://openairdocs.org/sdr/CNMA2012020003.md): Lanyard · misrouted · Feb 15, 2012 · N67157 · Boeing 767224 · Escape Slide
  > DURING MINI-EVAC, SLIDE DEPLOYED PROPERLY AND WITHIN REQUIRED TIMES. THE SLIDE EMERGENCY LIGHTS DID NOT ILLUMINATE. REPLACED SLIDE ASSY IAW OAI W/C NR 25-029-01. POSSIBLE REASON FOR THE LIGHTS NOT ACTIVATING APPEARS TO BE THAT THE TRIGGER LANYARD TO THE BAT
- [SDR CNMA2012020002`](https://openairdocs.org/sdr/CNMA2012020002%60.md): Lanyard · misrouted · Feb 15, 2012 · N67157 · Boeing 767224 · Escape Slide
  > DURING MINI-EVAC, SLIDE DEPLOYED PROPERLY AND WITHIN REQUIRED TIMES, HOWEVER THE SLIDE EMERGENCY LIGHTS DID NOT ILLUMINATE. REPLACED SLIDE ASSY IAW W/C NR 25-029-01. POSSIBLE REASON FOR THE LIGHTS NOT ACTIVATING APPEARS TO BE THAT THE TRIGGER LANYARD TO THE
- [SDR CALA2012010300001](https://openairdocs.org/sdr/CALA2012010300001.md): Computer · failed · Dec 30, 2011 · N76156 · Boeing 767224 · Autopilot Computer
  > AFTER TAKEOFF, GOT "AUTOPILOT" EICAS MESSAGE & RED M/C LIGHT. SWITCHED AND TRIED ALL 3 AUTOPILOTS. ALL THE SAME, HAD NO STAB TRIM. PERF'D MCDP LAST FLT FAULT REVIEW, FOUND MULTIPLE CODES REFERENCING L FCC FAULT ACROSS MULTIPLE CHANNELS. R&R'D L FCC IAW AMM
- [SDR CNMA201111110049](https://openairdocs.org/sdr/CNMA201111110049.md): Threshold · corroded · Nov 11, 2011 · N234AX · Boeing 767224 · Fuselage Miscellaneous Structure
  > AFT LT LAVATORY LOWER TRESHOLD HAS SIGN OF CORROSION. FABRICATED REPAIR CHANNEL IAW 51-30-01, PAGE 1 THRU SRM 51-30-02 ALODINE PARTS IAW SRM 51-20-1, PAGE 3, PAINT PARTS IAW SRM 51-20-01, PAGE 1 AND INSTALLED. REPAIRED PARTS IAW SRM51-40-02, PAGE 2.
- [SDR CNMA20110036](https://openairdocs.org/sdr/CNMA20110036.md): Floorbeam · corroded · Oct 4, 2011 · N225AX · Boeing 767224 · Fuselage Main, Floor Beam
  > FLOORBEAM BS 325 AT LBL 20 CORRODED. CORROSION REMOVED IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101. HFEC PERFORMED IAW NDT, PT 6, 51-00-21. NO CRACK FOUND. FABRICATED TEE AND SPLICE AND INSTALLED IAW SRM 53-00-51 REPAIR 1.
- [SDR CNMA20110035](https://openairdocs.org/sdr/CNMA20110035.md): Seat Track · corroded · Sep 23, 2011 · N225AX · Boeing 767224 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SEAT TRACK BS 1208.45 -1428.45, RBL 88.5 CORRODED. CORROSION REMOVED IAW SRM 51-10-02 PG 7.
- [SDR CALA2011092100617](https://openairdocs.org/sdr/CALA2011092100617.md): Slide · out of position · Sep 21, 2011 · N76151 · Boeing 767224 · Escape Slide
  > DOOR 2R SLIDE PACK FELL DOWN WHEN DOOR WAS OPENED. FOUND SLIDE IN DISARM POSITION. DOOR 2R SLIDE PACK INSTALLED IAW AMM 25-66-01. INSTALLATION NEED RII INSPECTION. DEFERRED IAW MEL WITH DOOR 2R INOPERATIVE. MAINTENANCE PROCEDURE APPLIED. REMOVED, INSP, R
- [SDR CALA2011091900604](https://openairdocs.org/sdr/CALA2011091900604.md): Warning System · false activation · Sep 17, 2011 · N68159 · Boeing 767224 · Stabilizer Control System
  > UNSCHEDULED STAB TRIM EICAS LIGHT ILLUMINATED ON T/O ROLL APPROX 40 KTS ABORTED, LIGHT WENT OUT AS WE TAXIED OFF R/WAY PERFORMED UNSCHEDULED STAB TRIM TEST PER FIM 27-09-00 PG 167 STEPS 1 & 2 FAULT BALLS RESET, RAN TEST NO FAULTS NOTED. ACFT READY FOR SERVICE
- [SDR CALA2011081500541](https://openairdocs.org/sdr/CALA2011081500541.md): Floorbeam · corroded · Aug 16, 2011 · N68160 · Boeing 767224 · Fuselage Main, Floor Beam
  > FLOORBEAM UPPER TEE CORRODED AT BS 325 LBL 27-55. CORROSION REMOVED OUT IAW SRM 53-00 -51 1 FIG 101. REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201.
- [SDR CALA2011081500540](https://openairdocs.org/sdr/CALA2011081500540.md): Floorbeam · corroded · Aug 14, 2011 · N68160 · Boeing 767224 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM UPPER CHORD CORRODED AT BS 303 LBL 11-53. CABIN FLOOR UPPER CHORD CORROSION REMOVED AS PER SRM 51-10-02 AND BLENDED AREA D:0.042"X W:2"X L:3" (ORG 0.090") OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORRODED UPPER CHORD REPAIRED A
- [SDR CALA2011072000501](https://openairdocs.org/sdr/CALA2011072000501.md): Frame · cracked · Jul 19, 2011 · N68159 · Boeing 767224 · Nacelle/Pylon, Frame/Spar/Rib
  > SUPPORT TASK - NR 2 PYLON NAC STA 285 I/B FRAME CHORD AND UPPER CLIP FOUND CRACKED. NR 2 PYLON NAC STA 285 I/B FRAME CRACKED CHORD AND UPPER CRACKED CLIP. REPLACED AS PER SRM 51-10-02 AND NEW FRAME CHORD AND NEW CLIP INSTALLED AS PER SRM 51-40-02.
- [SDR CALA2011071100475](https://openairdocs.org/sdr/CALA2011071100475.md): Floorbeam · corroded · Jul 8, 2011 · N68159 · Boeing 767224 · Fuselage Main, Floor Beam
  > CABIN LT STA 325 LBL 22 TO 50 FLOORBEAM UPPER SURFACE FOUND CORROSION. CABIN LT STA 325 LBL 12 TO LBL 68 FLOORBEAM UPPER FLANGE REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND HFEC NIL CRACK FOUND.
- [SDR CALA2011071100474](https://openairdocs.org/sdr/CALA2011071100474.md): Floorbeam · corroded · Jul 8, 2011 · N68159 · Boeing 767224 · Fuselage Main, Floor Beam
  > CABIN LT STA 303 LBL 25-50 FLOORBEAM UPPER SURFACE FOUND CORROSION. CABIN LT STA 303 LBL 20 - LBL 68 FLOORBEAM UPPER FLANGE REPAIRED AS PER SRM 53-00-51 FIG 201 REPAIR 1 AND HFEC NIL CRACK FOUND.
- [SDR CALA2011070800469](https://openairdocs.org/sdr/CALA2011070800469.md): Fitting · cracked · Jul 7, 2011 · N68159 · Boeing 767224 · Nacelle/Pylon Miscellaneous Structure
  > SUPPORT TASK NR 2 PYLON NAC STA 285 TO STA 295 HORI TEE CHORD CRACKED. NR 2 PYLON NAC STA 285 TO STA 295 HORI TEE CHORD REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02.
- [SDR CALA2011062800452](https://openairdocs.org/sdr/CALA2011062800452.md): Oxygen Mask · damaged · Jun 24, 2011 · N67157 · Boeing 767224 · Crew Oxygen System
  > F/O OXYGEN MASK INFLATION HOSE DAMAGED. F/O OXYGEN MASK REPLACED AND TESTED NORMAL AMM 35-11-51. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1453953 S/N OFF 04885 MASK, OXYGEN, C OFF 99-3512-9-9001 4885 ON 99-3512-9-9001 4656.

Next page: https://openairdocs.org/model/boeing-767-224/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 aircraft_model_key = '767224'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-767-224/reports

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