# Service difficulty reports: JASC 3252

A list on [JASC 3252](https://openairdocs.org/jasc/3252.md).

Reports filed under 3252 · Shimmy Damper, newest first.

Page 1 of 2 · 79 reports

- [SDR AALA201907199010](https://openairdocs.org/sdr/AALA201907199010.md): Shimmy Dampener · broken · Jul 18, 2019 · N836NN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: CREW DECLARED AN EMERGENCY INTO IAH ON ACCOUNT OF HYDRAULIC ISSUE. ENG 1 HYD LOW PRESSURE LIGHT ILLUMINATED. MAINTENANCE FOUND BROKEN CONNECTION LINE ON THE LT MLG SHIMMY DAMPER. REMOVED AND REPLACED LT MLG SHIMMY DAMPER AND ALSO PERFORM
- [SDR AALA201907149014](https://openairdocs.org/sdr/AALA201907149014.md): Shimmy Dampener · excess play · Jul 13, 2019 · N945AN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: PILOT REPORTS BRAKES CHATTERING STRONGLY AT LOW SPEED DIFFICULT TO STOP WITHOUT VIOLENT SHAKING. TWO FLIGHTS IN A ROW. MAINTENANCE REMOVED AND REPLACED THE #3 BRAKE ASSEMBLY. REMOVED AND REPLACED THE RH SHIMMY DAMPER IAW AMM 32-11-81. R
- [SDR 2019FA0000079](https://openairdocs.org/sdr/2019FA0000079.md): Shimmy Dampener · failed · Mar 7, 2019 · Boeing 73737Q
  > DURING LANDING ROLL AFTER NOSE GEAR CONTACT WITH THE RUNWAY HIGH VIBRATION STARTED. (NOTE: LEFT MLG SHIMMY DAMPER EVENT CAUSED TORSION LINK FRACTURE). CORRECTIVE ACTION: REMOVED AND REPLACED SHIMMY DAMOER, TORSION LINK, TIRES 1 AND 2, BRAKE 1 AND 2.
- [SDR 2017FA0000192](https://openairdocs.org/sdr/2017FA0000192.md): Barrel · broken · May 16, 2017 · N6233A · Cessna 182
  > NOSE WHEEL SHIMMY DAMPENER BARREL ASSEMBLY. ATTACHMENT BOSS BROKE CAUSING SHIMMY DAMPENER TO LOSE ITS FLUID CAUSING LOSS OF STEERING CONTROL.
- [SDR ZP8R20160318002](https://openairdocs.org/sdr/ZP8R20160318002.md): Shimmy Dampener · jammed · Mar 9, 2016 · Pilats PC1247E
  > SHIMMY DAMPER WOULD NOT TEST PER CMM, INTERNALS JAMMED. UPON TEARDOWN INSPECTION SEVERAL DISCREPANCIES WERE DISCOVERED: MISSING PARTS WITHIN UNIT. DUE TO MISSING PARTS, ORFICE WAS JAMMED SIDEWAYS. INCORRECT RETAINER PIN INSTALLED. PREVIOUS REPAIR STATION USE
- [SDR CALA2015042300321](https://openairdocs.org/sdr/CALA2015042300321.md): Shimmy Dampener · unserviceable · Apr 23, 2015 · N25201 · Boeing 737824
  > UPON LANDING WITH MAIN WHEELS ON THE GND & PRIOR TO NOSE WHEEL TOUCHING GND, EXPERIENCED EXCESSIVE SHIMMY. SEVERAL CEILING PANEL CAME DOWN, 2 PSU FELL DOWN & LATCHES BROKE & TWO VIDEO MONITOR FELL DOWN & LATCHES BROKE. COMPLIED WITH AMM 05-51-08-210-802, INS
- [SDR GLBA2014110400463](https://openairdocs.org/sdr/GLBA2014110400463.md): Shimmy Dampener · faulty · Nov 2, 2014 · N202UX · Beech 1900D
  > DURING TAXI OUT, THE CREW NOTED THAT THE ACFT WOULD NOT STEER TO THE RT WITH MAX DIFFERENTIAL BRAKING POWER & NOSE WHEEL STEERING. TOWED THE ACFT BACK TO THE GATE & REPLACED THE NOSE SHIMMY DAMPER IAW BMM 32-50-00. AFTER RELEASE, THE ACFT FLEW & WHILE TAXIIN
- [SDR CA140903010](https://openairdocs.org/sdr/CA140903010.md): Damper · misoverhauled · Aug 29, 2014 · Cessna 560XL
  > (CAN) THE DAMPER WAS REPAIRED AT A VENDOR IN 2011, AND WAS REASSEMBLED INCORRECTLY. IT WAS THEN INSTALLED BACKWARDS TO MAKE UP FOR THE IMPROPER ASSEMBLY. IN 2013 VENDOR DID A PHASE 2 AND PHASE B ON THE AIRCRAFT AND DID NOT NOTE ANY DEFECTS. WE WERE CONDUCTING
- [SDR CA131125002](https://openairdocs.org/sdr/CA131125002.md): Nut · loose · Nov 21, 2013 · Emb ERJ190100IGW
  > (CAN) LT AND RT MLG SHIMMY DAMPERS BOTH FOUND WITH LOOSE JAM AND FLANGED NUTS. MPN 2225-0070 AND 2225-0069, RESPECTIVELY. REF IPC 32-11-03, FIG 01 ITEMS 60 AND 70. BOTH SHIMMY DAMPERS RETORQUED IAW AMM 32-11-03, SUBTASK 212-005-A.
- [SDR USAA2012051400030](https://openairdocs.org/sdr/USAA2012051400030.md): Shimmy Dampener · faulty · May 12, 2012 · N434US · Boeing 7374B7
  > CREW REPORTED THE RIGHT BRAKE ON BOTH CAPT'S AND F/O PEDALS PULSE WITH LITTLE TO NO BRAKING AVAILABLE. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR SHIMMY DAMPER PER AMM 32-11-81. CHECKED WIRING TO ALL WHEEL SPEED TRANSDUCERS AND ANTI SKID VALVES FOR SHO
- [SDR K5SR2012050123536](https://openairdocs.org/sdr/K5SR2012050123536.md): Shimmy Dampener · leaking · May 1, 2012 · N330VP · Cessna 560CESSNA
  > AFT WAS LANDING WHEN A VIOLENT SHIMMY AND VIBRATION OCCURRED BETWEEN 40 TO 50 KTS, EMANATING FROM THE NOSE LANDING GEAR. THE AIRCRAFT WAS BROUGHT INTO MAINTENANCE. FOUND SHIMMY DAMPER LEAKING FLUID. NOSE LANDING GEAR SHIMMY DAMPENER, PN 5543001-11, S/N 684,
- [SDR CA111107006](https://openairdocs.org/sdr/CA111107006.md): Piston · cracked · Nov 7, 2011 · Boeing 73776N
  > (CAN) DURING A ROUTINE OVERHAUL OF THE SHIMMY DAMPER ASSY, PISTON WAS NOTED AS REQUIRED AND SEVERAL SMALL CRACKS WERE FOUND, BOTH INSIDE AND ON THE OUTER EDGE OF THE PISTON O-RING GROOVE, AND THEY DIDN`T APPEAR TO BE IN AN AREA THAT IS SUBJECT TO EXCESSIVE S
- [SDR BSYA2010035](https://openairdocs.org/sdr/BSYA2010035.md): Shimmy Dampener · broken · Jul 21, 2010 · N35453 · Piper PA31350
  > AFTER TAKEOFF WHEN RETRACTING THE GEAR NOSE GEAR DID NOT GO UP ALL THE WAY, THE CAUSE WAS THE SHIMMY DAMPER ROD END BROKE CAUSING NOSE GEAR TO JAM IN WHEEL WELL. CYCLED GEAR BACK DOWN AND RETURNED TO EWN. REMOVED AND REPLACED SHIMMY DAMPER AND NOSE GEAR ASSY
- [SDR CA090331005](https://openairdocs.org/sdr/CA090331005.md): Shimmy Dampener · malfunctioned · Mar 17, 2009 · Piper PA31350
  > (CAN) BENT SHIMMY DAMPER ROD CAUSED NOSE WHEEL TO JAM TO MAX. RT DEFLECTION AND WHEN GEAR WAS RETRACTED CAUSED MISALIGNMENT OF THE ALIGNER ASSY AND THE GUIDE BRACKET. GEAR SELECTION UP OR DOWN WAS AFFECTED AND RESULTED IN AN EMERGENCY LANDING WITH A UNLOCKED N
- [SDR 2009FA0000096](https://openairdocs.org/sdr/2009FA0000096.md): Roll Pin · broken · Jan 23, 2009 · N3309Y · Cessna 182E
  > PILOT REPORT: ON LANDING SEVERE NOSE WHEEL SHIMMY. FOUND ROLL PIN THAT SECURES PISTON TO DAMPER ROD BROKEN AT PISTON THE DAMPER ROD. REPLACED ROLL PIN AND ALL O-RINGS. OPS NORMAL ON NEXT LANDING. (K)
- [SDR CA080812002](https://openairdocs.org/sdr/CA080812002.md): Clevis · broken · Aug 8, 2008 · Cessna 172RG
  > (CAN) DAMPER SHAFT CLEVIS BROKE AT NOSE STRUT ATTACHMENT ALLOWING UNRESTRAINED MOTION OF SHIMMY DAMPER.
- [SDR COMA0770040](https://openairdocs.org/sdr/COMA0770040.md): Shimmy Dampener · worn · Jul 18, 2007 · N378CA · Cndair CL6002C10
  > MLG SHIMMY ON TAKEOFF AND GEAR RETRACTION. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED RIGHT MLG SHIMMY DAMPENER.
- [SDR COMA0770039](https://openairdocs.org/sdr/COMA0770039.md): Shimmy Dampener · worn · Jul 18, 2007 · N378CA · Cndair CL6002C10
  > FLIGHT 5058 - MLG SHIMMY ON TAKEOFF AND GEAR RETRACTION. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LEFT MLG SHIMMY DAMPENER.
- [SDR GLBA20060914](https://openairdocs.org/sdr/GLBA20060914.md): Shimmy Dampener · missing · Feb 19, 2007 · N220GL · Beech 1900D
  > UPON PRE-FLIGHT INSPECTION, PILOT REPORT OF SHIMMY DAMPENER DAMAGE/MISSING AND SUSPECTED DAMAGE TO STRUCTURE IN SURROUNDING AREA WAS ALSO REPORTED. MAINTENANCE REMOVED AND REPLACED THE SHIMMY DAMPER IAW B1900D MM 32-20. MAINENANCE REMOVED AND REPLACED STEERIN
- [SDR KBM2006F00185](https://openairdocs.org/sdr/KBM2006F00185.md): Bearing · worn · May 6, 2006 · N53SH · Snias AS350B1
  > DAMPERS, BEARINGS ARE WORN, REMOVED AND REPLACED. (K)
- [SDR SAI030603](https://openairdocs.org/sdr/SAI030603.md): Roll Pin · sheared · Mar 21, 2006 · N1119V · Cessna 208B
  > DURING TAKE-OFF PILOT NOTED VIBRATION AND ABORTED TAKE-OFF. AIRCRAFT RETURNED TO RAMP. AIRCRAFT WAS INSPECTED AND FOUND FAULTY SHIMMY DAMPNER. ROLL PIN, P/N NAS561P5-18, SHEARED.
- [SDR SWAA060316](https://openairdocs.org/sdr/SWAA060316.md): Damper · sheared · Jan 26, 2006 · N370SW · Boeing 7373H4
  > SEVERE VIBRATION FELT FROM RIGHT MLG. FOUND RIGHT MLG SHIMMY DAMPER BOLT SHEARED BETWEEN TORSION LINKS. REMOVED AND REPLACED RIGHT MLG SHIMMY DAMPER ASSY, NR 3 & NR 4 BRAKE LINES, NR 3 & NR 4 MAIN BRAKE ASSY, NR 3 & NR 4 MAIN TIRE/WHEEL ASSY AND RT MLG UPPER
- [SDR CA051020002](https://openairdocs.org/sdr/CA051020002.md): Nut · loose · Oct 19, 2005 · Cndair CL600*
  > (CAN) CREW REPORTED MAINWHEEL SHIMMY ON LANDING. MAINTENANCE FOUND BOLT (ITEM 45)FROM THE RT MLG TORQUE LINK TO THE SHIMMY DAMPER HAD BACKED OUT AND THE TORQUE LINKS SEPARATED 1.2500 INCHES. THE SAFTEY BOLT (ITEM 35) AND LOCKING PLATE (ITEM 60) WERE FOUND LAYI
- [SDR DJFA2005147](https://openairdocs.org/sdr/DJFA2005147.md): Shimmy Dampener · worn · Oct 6, 2005 · N783TA · Beech 400A
  > UPON ARRIVAL AFTER APPROACH AND NORMAL LANDING WITH NORMAL DECELERATION USING THRUST REVERSERS, AND AFTER ACHIEVING TAXI SPEED OF A FAST PACED WALK, THE AIRCRAFT EXPERIENCED A SEVERE NOSEWHEEL VIBRATION. NORMAL BRAKING APPEARED TO BE LOST, AND EMERGENCY BRAKI
- [SDR 2005FA0000913](https://openairdocs.org/sdr/2005FA0000913.md): Cap · cracked · May 25, 2005 · Doug MD900
  > CAP IS CRACKED ON PORT SIDE. CATASTROPHIC FAILURE. MANFACTURE CAP FROM SOLID BLOCK OF MATERIAL INSTAD OF CASTING PART. (K) (REF: 195920/JMG)
- [SDR 2005FA0000912](https://openairdocs.org/sdr/2005FA0000912.md): Cylinder · delaminated · May 25, 2005 · Doug MD900
  > CHROME HAS DELAMINATED IN CYLINDER BORE. IMPROPER PLATING. IMPROVE CHROME PLATING METHOD TO IMPROVE ADHESION TO CYLINDER. (K) (REF: 195920/JMG)
- [SDR CA050405003](https://openairdocs.org/sdr/CA050405003.md): Shimmy Dampener · failed · Mar 21, 2005 · Cessna 150L
  > (CAN) SHIMMY DAMPNER FAILED AT TAKEOFF CAUSING A VIBRATION. AIRCRAFT CAME TO REST WITH ONLY MINIMAL DAMAGE. SHIMMY DAMPNER REPLACED.
- [SDR 2005FA0000143](https://openairdocs.org/sdr/2005FA0000143.md): Bolt · misinstalled · Jan 26, 2005 · N249PM · Piper PA34200T
  > DURING RAMP INSPECTION, INSPECTOR NOTICED BOLT ATTACHING NOSE GEAR CENTERING DEVICE WAS INSTALLED INCORRECTLY, HEAD OF BOLT AT TOP OF HARDWARE STACK. AD 92-13-05 AND SB 893 REQUIRE BOLT TO BE INSTALLED WITH HEAD DOWN AND A CAUTIONARY PLACARD TO BE AFFIXED. P
- [SDR CA040810005](https://openairdocs.org/sdr/CA040810005.md): Shimmy Dampener · broken · Jul 19, 2004 · Cessna 208B
  > (CAN) SHIMMY DAMPENER BARREL END ENTIRELY BROKE OFF AT CIRCLIP GROOVE. ALL FLUID LOST,CIRCLIP MISSING, BROKEN PIECE MISSING. NO EVIDENCE OF PRIOR OVERSTEER.
- [SDR AUS20040056](https://openairdocs.org/sdr/AUS20040056.md): Damper · faulty · Jan 23, 2004 · Beech 76
  > (AUS) NOSE WHEEL SHIMMY DAMPER END CAP RETAINING CIRCLIP MISSING.
- [SDR 1B](https://openairdocs.org/sdr/1B.md): Shimmy Dampener · misinstalled · Dec 20, 2002 · N6506R · Cessna U206C
  > SHIMMY DAMPENER SLIDING SHAFT INSTALLED 180 DEGREES OUT. UNIT WAS OVERHAULED.
- [SDR 2002FA0001300](https://openairdocs.org/sdr/2002FA0001300.md): Bolt · misinstalled · Nov 6, 2002 · N6292H · Piper PA24250
  > BOLT WAS INSTALLED BACKWARDS ON SHIMMY DAMPNER. GEAR WAS LOWERED IN FLIGHT AND HUNG UP ON COWL LT V CHANNEL. SUBSEQUENT DAMAGE WAS CAUSE TO CHANNEL AND REAR SUPPORT. TIME SINCE LAST WORK TO SHIMMY DAMPENER MOUNT CLAMP UNKNOWN.
- [SDR 2002FA0001181](https://openairdocs.org/sdr/2002FA0001181.md): Computer · malfunctioned · Oct 13, 2002 · N10AH · Lear 35A
  > NOSE WHEEL STEERING WILL NOT ARM. FOUND NO OUTPUT VOLTAGE ON P224 PIN A. 1.0 VAC REQUIRED FROM THIS PIN.
- [SDR AUS20020788](https://openairdocs.org/sdr/AUS20020788.md): Barrel · broken · Jul 11, 2002 · Cessna 402B
  > (AUS) NOSE LANDING GEAR SHIMMY DAMPER BODY BROKEN AWAY FROM ATTACHMENTLUG.
- [SDR CA020619002](https://openairdocs.org/sdr/CA020619002.md): Shaft · sheared · Jun 18, 2002 · Cessna 172R
  > (CAN) INVESTIGATION OF A SEVERE NOSEWHEEL SHIMMY REPORT REVEALED THAT THE SHIMMY DAMPENER SHAFT HAD SHEARED. BOTH HALVES OF THE ASSEMBLY REMAINED ATTACHED BUT THE UNIT COULD NO LONGER FUNCTION AS DESIGNED. THE FAULTY UNIT WAS REMOVED FROM SERVICE AND REPLACED
- [SDR CA020619003](https://openairdocs.org/sdr/CA020619003.md): Shaft · sheared · May 8, 2002 · Cessna 172P
  > (CAN) SEVERE NOSEWHEEL SHIMMY REPORTED AFTER LANDING. INSPECTION OF THE DEFECT BY MAINTENANCE REVEALED THAT THE SHAFT WAS SHEARED. THE DAMPENER UNIT REMAINED ATTACHED BUT IN TWO SEPARATE PARTS PREVENTING IT FROM FUNCTIONING AS DESIGNED. NO FURTHER DAMAGE WAS F
- [SDR CA020513001](https://openairdocs.org/sdr/CA020513001.md): Rod End · separated · May 7, 2002 · Mtsbsi MU2B60
  > (CAN) ROD END SEPARATED FROM PISTON.UNIT RETURNED TO VENDOR AND WAS OVERHAULED. SERVICE BULLETIN NR 169B EMBODIED TO PRECLUDE FURTHER EVENTS.
- [SDR HEEA073107](https://openairdocs.org/sdr/HEEA073107.md): Damper · leaking · May 10, 2001 · N972AE · Snias AS350B
  > LEAKING AROUND SHAFT SEAL.
- [SDR 2002FA0000045](https://openairdocs.org/sdr/2002FA0000045.md): Shimmy Dampener · damaged · Apr 3, 2001 · N63GG · Cessna 310J
  > PILOT MADE A HARD LEFT TURN CAUSEING DAMAGE TO THE NOSE GEAR AREA. BENT ROD ON THE SHIMMY DAMPER CAUSING INTERNAL DAMAGE TO THE COMPONENT.
- [SDR CA010426003](https://openairdocs.org/sdr/CA010426003.md): Strap · broken · Mar 28, 2001 · Pilats PC1245
  > (CAN) NOSE GEAR BONDING STRAP P/N 532.20.12.262 WAS WRAPPED AROUND SHOCK STRUT P/N 571.10.12.353 AND HAD BENT THE STRUT SOME 70 DEGREES UP FROM ITS NORMAL POSITION. THE STRUT COULD NO LONGER OPEN AND CLOSE THE OIL COOLER DOOR UPON GEAR RETRACTION. BONDING STRA
- [SDR 20010323CW004](https://openairdocs.org/sdr/20010323CW004.md): Shimmy Dampener · defective · Feb 27, 2001 · N2048A · Beech B19
  > FOUND MULITUDE OF (AIR) POCKETS AND AIRCRAFT SHIMMIED EXCESSIVELY ON LANDING AND TAXI.
- [SDR 20010328CW009](https://openairdocs.org/sdr/20010328CW009.md): Transponder · melted · Feb 24, 2001 · N705AL · Skrsky S76
  > IN CRUSE FLIGHT, SMOKE IN COCKPIT, ACRID SMELL IN COCKPIT. PHOTOCELL AND ADJACENT AREA OF CONTROL HEAD MELTED.
- [SDR AU000796](https://openairdocs.org/sdr/AU000796.md): Damper · faulty · Sep 4, 2000 · Cessna 150F
  > (AUS) SHIMMY DAMPER LOW ON FLUID. ON FURTHER INVESTIGATION THE FOLLOWING COMPONENTS WERE FOUND TO BE DAMAGED: 1. HEAD BEARING P/N 0542102-3. 2. ROLL PIN P/N NAS 561P4-143. RING RETAINER P/N MS16625-1118. DAMPER WAS ATTACHED BY TWO FULLY THREADED METRIC
- [SDR 20000609SH028](https://openairdocs.org/sdr/20000609SH028.md): Shimmy Dampener · failed · Apr 22, 2000 · N6331E · Cessna 172
  > AFTER LANDING, THE PIC WAS TAXIING TO THE RAMP WHEN THE NOSE WHEEL STARTED TO SHIMMY. HE APPLIED BRAKES AND THE AIRCRAFT MADE A HARD RIGHT TURN CAUSING THE AIRCRAFT TO TOP OVER TO THE LEFT/FRONT SIDE AND THE LEFT WING TIP AND PROPELLER MADE CONTACT WITH THE G
- [SDR 2000ZZZX614](https://openairdocs.org/sdr/2000ZZZX614.md): Shimmy Dampener · broken · Feb 24, 2000 · N35033 · Cessna 177B
  > AFTER REPLACING AN OLD SHIMMY DAMPENER WITH A NEW ONE AT APPROXIMATELY 100 HOURS IN SERVICE, THE NEW PART BROKE AT THE OUTER C-CLAMP RING SPLITTING THE OUTER CYLINDER CASE. THIS HAPPENED AS THE AIRCRAFT STOPPED SHIMMING. THE END PLUG, C-CLAMP AND ALL FLUID W
- [SDR AGQA065695](https://openairdocs.org/sdr/AGQA065695.md): Damper · discharged · Feb 4, 2000 · N5027P · Hughes 369D
  > MAIN LANDING GEAR DAMPER IS LOW.
- [SDR AGQA065694](https://openairdocs.org/sdr/AGQA065694.md): Damper · discharged · Feb 4, 2000 · N5027P · Hughes 369D
  > MAIN LANDING DAMPER IS LOW.
- [SDR AU990795](https://openairdocs.org/sdr/AU990795.md): Pin · wrong part · Jul 29, 1999 · Cessna 172N
  > (AUS) INCORRECT SHIMMY DAMPER PISTON ROLL PIN FITTED. A BRASS SCREW WAS USED INSTEAD OF THE CORRECT STEEL ROLL PIN. THE BRASS SCREW SHEARED CAUSING COMPLETE FAILURE OF THE DAMPER WITH ASSOCIATED NOSE WHEEL SHIMMY. UNAPPROVED PART.
- [SDR 20000508SH002](https://openairdocs.org/sdr/20000508SH002.md): Shimmy Dampener · failed · Jun 7, 1999 · N6639D · Beech C23
  > RETRIEVED SUBJECT SHIMMY DAMPENER FROM STOCK ROOM. ON FUNCTIONAL CHECK, DETERMINED MUCH WORSE THAN THE REMOVED UNIT.
- [SDR 20000508SH001](https://openairdocs.org/sdr/20000508SH001.md): Shimmy Dampener · leaking · Jun 7, 1999 · N6639D · Beech C23
  > SHIMMY DAMPENER HAS NUMEROUS DEAD SPOTS (AIR INSIDE) WHEN ACTUATED. CAUSES NOSE WHEEL TO SHIMMY READ BAD. (X)

Next page: https://openairdocs.org/jasc/3252/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 jasc_code = '3252'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/3252/reports

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