JASC 3222
Service difficulty reports · 2,074
Reports filed under 3222 · Nose/Tail Landing Gear Strut/Axle, newest first.
Query with SQL
duckdb -csv -c "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 = '3222' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = '3222' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DXTA2011120804817Strut · dischargedAFTER TAKEOFF, RETRACTING LANDING GEAR, RECEIVED AN UNUSUALLY LONG NOSE GEAR IN TRANSIT FOLLOWED BY A RED GEAR STUCK INTRANSIT FOR APPROX 15 SECONDS. THE GEAR RETRACTED FULLY AND RECEIVED LT & RT PITOT AND TAT HEAT FAIL, TCAS FAIL MESSAGES AND THE FLIGHT CLOCSDR SWIA201128729Strut · lowNOSE GEAR WOULD NOT RETRACT. (FLT 6250) PERFORMED FULL SERVICE OF NOSE STRUT PER AMM.SDR DXTA2011120104806Strut · dischargedGEAR WOULD NOT RETRACT AFTER TAKEOFF. GEAR HANDLE WAS LOCKED IN DOWN POSITION. 3 GREEN GEAR DOWN LIGHTS WERE ILLUMINATED, NO RED UNSAFE LIGHTS ILLUMINATED. FOUND NOSE GEAR DID NOT FULLY EXTEND. PUSHED NOSE GEAR INTO POSITION. FOUND UPPER AND LOWER CHAMBERS SDR CA111125003Strut · low(CAN) AFTER TAKEOFF LG WOULD NOT RETRACT, THERE WAS A WEIGHT ON WHEELS, WOW, MIS-COMPARE MSG. ACFT RETURNED TO MX. THE NOSE GEAR WAS SERVICED & GEAR SWINGS COMPLETED WITHOUT FAULT. THIS FAULT APPEARS TO BE THAT THE NOSE GEAR IS NOT EXTENDING ALL THE WAY AFTSDR V0DR20111123019Strut · damagedNLG LEAKING. DURING DISASSEMBLY, NOTED SIGNIFICANT SCRATCHES IN THE CHROME PLATING OF THE PISTON TUBE. FURTHER DISASSEMBLY REVEALED THAT THE INTERNAL BEARING COATING OF THE NOSE CYLINDER WAS DETERIORATED TO THE POINT THE MATERIAL WAS FLAKING OFF. THE TECH SDR AALA20111117ORD01Bungee Cylinder · malfunctionedORD - CREW REPORTED UPON GEAR EXTENSION, NO NOSE GEAR DOWN INDICATION AND NO NOSE LANDING GEAR PIN EXTENSION INDICATION. FLIGHT ACCOMPLISHED GO AROUND AND CONFIRMED GEAR DOWN. FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NOSESDR CA111117002Strut · corroded(CAN) DURING MAINTENANCE, A SHOCK STRUT FLUID LEAK WAS NOTED ON THE NOSE GEAR OF A SN UE79. THE LOWER SHOCK ABSORBER TUBE WAS REMOVED TO FACILIATE SEAL REPLACEMENT. DURING THE PROCESS TO REPLACE THE SEAL, SEVERE CORROSION WAS NOTED AT THE LOWER END OF THE UPSDR REXA201100843Torque Link · disconnectedNOSE GEAR DISAGREE AFTER GEAR RETRACTION AFTER GEAR HANDLE PUT IN UP POSITION; NOSE WHEEL STEERING INOP CAUTION; WOW INPUT CAUTION. FOUND TORQUE LINKS TO BE DISCONNECTED. INTERROGATED PSEU-CODES WERE- S03, S11, S23, S35, S21, S22, S32. AFT NOSE LANDING GEARSDR AALA20111107STL01Bungee Cylinder · inoperativeSTL - CREW REPORTED NOSE GEAR WOULD NOT EXTEND WHEN GEAR HANDLE MOVED TO THE DOWN POSITION. UNSAFE NOSE GEAR WARNING LIGHT INDICATED. PERFORMED EMERGENCY GEAR EXTENSION PROCEDURE AND NOSE GEAR LOWERED AND GREEN LIGHT SAFE ILLUMINATED WITH NOSE PIN EXTENDED. SDR SWIA201128472Torque Link · disconnectedNOSE GEAR WOULD NOT RETRACT. (FLT 3471) FOUND NOSE GEAR TORQUE LINKS DISCONNECTED AND NOSE TIRES DAMAGED, INSPECTED NOSE GEAR FOR DAMAGE REF AMM 32-21-00 WITH NO DAMAGE NOTED, REPLACED BOTH NOSE TIRES. / PN: 5010598 SN OFF: OCT00-3032 / PN: 5010598 SN OFF:SDR SWIA201128500Piston · failedGEAR DISAGREE WARNING MESSAGES. (FLT 4810) INSTALLED PISTON AXLE ASSEMBLY NEW CENTERING CAM LOCK PINS AND SERVICED STRUT.SDR REXA201100797Torque Link · disconnectedNOSE DOOR MASTER WARNING. NOSE WHEEL STEERING INOP MASTER CAUTION. UNABLE TO TAXI - IN W/STEERING ENGAGED. INSPECTED A/C, FOUND NOSE TQ LINKS DISCONNECTED, INSPECTED FOR DAMAGE. NO DAMAGE NOTED. CONNECTED TQ LINKS. OP CHECKED STEERING IAW AMM 32-50-00. SDR CA111103013Fork · cracked(CAN) DURING A ROUTINE 100 HR INSPECTION, SUBJECT NOSE FORK, PN 0442503-497 (LATER STYLE) WAS FOUND TO BE CRACKED ON BOTH SIDES OF THE UPPER AREA APPROX 2" BELOW THE TOP. AFTER EXAMINING THE FORK, IT DOES NOT APPEAR TO HAVE BEEN CAUSED BY A SINGLE INCIDENT ASSDR CA111021009Fork · cracked(CAN) ON LANDING, THE TAIL WHEEL FORK DEPARTED THE ACFT AS IT CRACKED THE CAST ALUMINUM FORK THAT THE TAIL WHEEL AXLE GOES THROUGH. THE ACFT LANDED WITH NO FURTHER DAMAGE BEYOND THE TAIL WHEEL ASSY.SDR REXA201100767Strut · low pressureNOSE DOOR OPEN WARNING MSG AFTER T/O. GEAR DISAGREE WARNING AFTER SELECTING GEAR UP AFTER T/O. SERVICED NOSE LANDING GEAR IAW AMM 12-12-32. PSEU CODES 511, 523, 521, 535, 522, 530, 532, DI14, DI15. C/W FULL GEAR SWING IAW AMM 32-30-00. OPS CHECKS GOOD. NSDR C2XA11CL227Strut · wornCLE FLT 5850 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL, AND A ENGINE 1/2 REV DISAGREE MESSAGE DURING CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NOSE STRUT DEFLATED. DURING REPACK OF THE NOSE STSDR C2XA11IA233Strut · low pressureIAH - FLIGHT 4369 THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE ON CLIMB, WITH THE MESSAGE CLEARING AFTER THE GEAR WAS DOWN AND LOCKED. THE AIRCRAFT LANDED AT OAH WITHOUT INCIDENT WHERE MAINTENANCE SERVICED THE NOSE LANDING GEAR, OPERATIONALLY TESTEDSDR 2011FA0000658Pin · migratedDURING SPECIAL INSPECTION, ALL 4 LOCKING PINS WERE FOUND EXHIBITING MOVEMENT AND ABOUT TO FALL OUT.SDR 2011FA0000645Pin · shearedNLG STRUT PINS SHEARED.SDR 2011FA0000643Tube · damagedNLG INNER TUBE SEPARATED.SDR 2011FA0000641Pin · shearedNLG PINS SHEARED ON INNER STRUT TUBE.SDR 2011FA0000640Tube · separatedNLG STRUT TUBE SEPARATED.SDR 2011FA0000642Tube · damagedNLG STRUT TUBE HAS PIN HOLES ELONGATED.SDR 2011FA0000649Pin · brokenNLG STRUT TUBE HAS A BROKEN PIN.SDR 2011FA0000647Pin · missingPINS MISSING.SDR MASA2011092863768Strut · overservicedWOW ANNUNCIATOR LIGHT ON & CONFIG BRAKE. FOUND NLG STRUT OVERSERVICED. DESERVICED.SDR FDEA201109264125Drag Strut · failedDURING ROUTINE NORMAL GEAR EXTENTION AND RETRACTION POST REINSTALLATION OF MLG ACTUATORS. THE NLG TELESCOPIC DRAG STRUT WITH THE PIN INSTALLED, BEGAN TO RETRACT AND SHEARED THE PIN AND THE DOWN LOCK VALVE. R & R NLG TELESCOPIC STRUT IAW AMM 32-31-24-04. PSDR REXA201100597Strut · low pressureGEAR DISAGREE UPON GEAR RETRACTION. MSG CLEAR AFTER FLAPS RETRACTED. SVCD NOSE STRUT IAW AMM 12-12-32 COMPLIED WITH PA05-018B GEAR DISAGREE EVENT PROCEDURE AND AMM 32-30-00. NO DEFECTS NOTED OK FOR SVC.SDR UALA2011092205117Seal · leakingAT GATE, FOUND NLG STRUT LEAKING OIL & LOW, CLEANED, TOWED ACFT TO HANGAR, NLG STRUT CONTINUES TO LEAK OIL. REPLACED NLG STRUT SEALS PER MM. FOUND LEAKING TO CEASE WITH NO DECREASE TO DIMENSION X. CHECKED EXTENSION AND FOUND IT 1.5" LOW. SERVICED STRUT WITHSDR 2011FA0000639Tube · separatedNLG INNER STRUT TUBE PIN MIGRATING LOOSE.SDR 2011FA0000606Strut · separatedDURING SPECIAL INSPECTION INNER STRUT TUBE FOUND SEPARATED AT CAP AND TUBE CONNECTION.SDR 2011FA0000605Strut · separatedINNER STRUT TUBE FOUND SEPARATED AT CAP AND TUBE CONNECTION.SDR 2011FA0000604Shim · damagedDURING PHASE INSP NOSE GEAR SHIMS WERE FOUND TO BE TORN AND COMPRESSED. INTERIOR INSP OF STRUT FOUND THE INNER STRUT TUBE CAP WAS SEPARATED FROM THE METERING TUBE. UPON DISASSEMBLY THE 4 PIN HOLES WERE FOUND TO BE ELONGATED AND THE SECURING PINS WERE FOUND ISDR 2011FA0000603Strut · separatedINNER STRUT TUBE FOUND SEPARATED DURING SPECIAL INSPECTION. OTHER ACFT IN FLEET HAVE BEEN FOUND. MFG AND LOCAL FSDO HAVE BEEN MADE AWARE OF ISSUE.SDR 2011FA0000602Pin · looseDURING HARD LANDING INSPECTION, INNER STRUT TUBE CAP PINS WERE FOUND TO BE LOOSE AND ELONGATING. THIS HAS BEEN FOUND IN NUMEROUS ACFT IN OUR FLEET OF 62 ACFT RANGING FROM LOOSE PINS TO PIN DISPLACEMENT CAUSING CAP AND TUBE SEPERATION. MFG AND LOCAL FSDO HAVE SDR 2011FA0000601Strut · separatedDURING INSP, NOSE GEAR INNER STRUT TUBE WAS FOUND TO BE SEPARATED AT CAP AND TUBE CONNECTION. NO LEAKS WERE NOTED BUT A SPONGY STRUT WAS REPORTED DURING PRE-INSPECTION RUN-UP.SDR 2011FA0000648Tube · separatedINNER TUBE SEPARATED.SDR 2011FA0000646Tube · separatedNLG STRUT INNER TUBE SEPARATING.SDR NOCA08911Strut · overservicedA/C HAD AN AIR TURNBACK INTO MSP DUE TO NOSE GEAR AIR GROUND DISAGREE DISPLAYED ON EICAS AFTER GEAR RETRACTION. REPLACED S10067 SWITCH, A/C TAKEOFF A/C HAD A SECOND AIR TURNBACK INTO MSP DUE TO STATUS MSG AIR GROUND DISAGREE. PERFORMED INDUCTANCE CHECK ON THSDR DXTA2011091204722Strut · dischargedRAISED LANDING GEAR AFTER TAKEOFF AND RED UNLOCK LIGHT STAYED ON. ALL GREEN INDICATORS WENT OUT. IN ADDITION THE HYD PRESSURE STAYED ON AND STAB MISCOMPARE LIGHT CAME ON. PERFORMED COMPLETE NOSE GEAR STRUT SERVICING IAW MM 12-14-00. GEAR AND STAB OPS CHECKESDR 2011FA0000597Bolt · looseAN AN6-22A BOLT WITH AN AN365 NUT WAS USED TO HOLD THE FWD END OF THE TAIL WHEEL SPRING. THE NUT BACKED OFF ALLOWING THE TAIL WHEEL SPRING TO SIDE AFT IN THE TAIL POST SADDLE. SUGGEST THE INSTALLATION BE DONE USING AN AN6-22 BOLT WITH AN 310 NUT AND A COTTERSDR YENA20110825327Strut · dischargedFLT 73, AFTER TAKEOFF GEAR WOULD NOT RETRACT. "LG WOW SYS FAIL" - CAS MESSAGE. RETURN TO FIELD PER QRH. PLACED ON JACKS PER 07-10-01 AND DISCOVERED NLG STRUT WOULD NOT FULLY EXTEND. SERVICED STRUT PER AMM 12-12-09 AND PERFORMED SEVERAL GEAR SWINGS WITH NO FASDR MASA2011082503564Strut · lowWOW INPUT CAUTION W/ PX 1 FAULT STATUS. SERVICED NOSE STRUT.SDR CALA2011082400554Strut · overservicedDURING T/O A/C POWERED UP ON T/O ROLL. COULD NOT MAINTAIN DIRECTIONAL CONTROL WITH FULL RUDDER. BRAKE TEMP ZERO. A/C ABORTED AT 60 KTS FOUND NOSE STRUT OVERPRESSURE PER DIM "X" ADJUSTED PRESSURE IN NOSE STRUT TO PROPER DIM "X" AS OUTLINED IN 12-15-02-613-029SDR UALA2011082404531Strut · defectiveFOUND NOSE STRUT FLAT ON WALK AROUND. SERVICED WITH NITRO. TO BE RECHECKED WITHIN 4 TO 7 DAYS. SERVICED NOSE STRUT PER AMM. NOW NEED TO BE RECHECKED 4-7 DAYS. TIME CHANGED TO 22AUG PER SAMC CONTROLLER. REMOVED NLG STRUT INNER CYLINDER AND REPACK SHOCK ABSSDR CA110822006Link · broken(CAN) DURING GEAR RETRACTION AFTER TAKEOFF, THE GEAR IN-TRANSIT LIGHT DID NOT EXTINGUISH AND THE NOSE GEAR WAS VISUALLY VERIFIED AS PARTIALLY IN THE UP POSITION. THE GEAR WAS EXTENDED NORMALLY IN THE DOWN AND LOCKED POSITION AS INDICATED BY THE GEAR LIGHTS ANSDR 2012FA0000000Strut · debondedNOSE STRUT DISBONDED AT NOSE FORK BEARING SPINDLE. SPINDLE AND STRUT ARE BONDED VIA A HOT BOND AGENT WHILE IN AUTOCLAVE. SUSPECT DISBONDING OCCURED DUE TO UNREPORTED HARD LANDINGS AND EXTREME STRESS DUE TO IMPROPER GROUND HANDLING.SDR CA110829011Arm · wrong part(CAN) THE NOSE WHEEL CENTERING MECHANISM CONTAINS A CENTERING ARM WITH BEARING THAT ROTATES IN A CAM TO CENTER THE WHEELS. THE BEARING IS RETAINED IN THE ARM BY A PIN (OR IS SUPPOSED TO BE) THIS PARTICULAR ARM THAT WAS REMOVED, WAS NOT DRILLED TO ACCEPT THE PISDR 2011FA0000577Strut · failedDURING ROLLOUT AND AT APPROX 500' AFTER NOSE WHEEL TOUCHED DOWN AT LANDING, THE LOWER SECTION OF THE NOSE STRUT BROKE OFF. STRUT BROKE AT POINT WHERE THROUGH-BOLT IS INSTALLED. THIS BOLT HOLDS THE LOWER SECTION OF THE OLEO STRUT (PISTON) TO THE NOSE GEAR FOSDR A6WA201140673Strut · dischargedAFTER TAKEOFF, NOSE GEAR W/N RETRACT RECEIVED GEAR DISAGREE WARNING ALONG WITH WOW OUTPUT STATUS AND WOW INPUT CAUTION MSG. C/W QRH. PERFORMED AIR RETURN. LANDED AT 46,500 LBS, NORMAL LANDING. CORRECTLY SERVICED NLG SHOCK STRUT IAW AMM 12-12-32. PERFORMED
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