# Service difficulty reports: JASC 3213

A list on [JASC 3213](https://openairdocs.org/jasc/3213.md).

Reports filed under 3213 · Main Landing Gear Strut/Axle/Truck, newest first.

Page 1 of 45 · 2,210 reports

- [SDR 55YR202610130001](https://openairdocs.org/sdr/55YR202610130001.md): Strut · damaged · Oct 5, 2026 · N326KW · Beech B200
  > CAME IN FOR PHASE MAINTENANCE, AND THE OPERATOR REQUESTED AN EARLY LANDING GEAR REPLACEMENT. THE LANDING GEAR WAS DUE SOON FOR REPLACEMENT, AND REPRESENTATIVES FROM BERING AIR DECIDED TO HAVE IT CHANGED AHEAD OF SCHEDULE. AFTER INSTALLING NEW MLG ASSEMBLIES
- [SDR DXTA2026092509835](https://openairdocs.org/sdr/DXTA2026092509835.md): Strut · discharged · Sep 21, 2026 · N402QS · Emb EMB505
  > DURING GEAR RETRACTION AFTER TAKEOFF, THE NOSE GEAR INDICATED IN TRANSIT AND NEVER FULLY RETRACTED. LG LEVER DISAG CAS MESSAGE DISPLAYED. HYDRAULIC PRESSURE WAS NORMAL. ALL GEAR EXTENDED NORMALLY WHEN SELECTED DN. SERVICED NLG STRUT. OPS CHECK GOOD. IAW PHENO
- [SDR 2026F00210](https://openairdocs.org/sdr/2026F00210.md): Spacer · missing · Sep 11, 2026 · N603FX · Emb EMB550
  > AFTER GEAR RETRACTION LOW FREQUECY VIBRATION. WHEN READY TO TOWING OUR TECH NOTED TOO MANY THREADS VISIBLE ON LH NLG WHEEL AXLE. FURTER INSPECTION REVEALED MISSING SPACER UNDER WHEEL NU
- [SDR NI6R202608260068](https://openairdocs.org/sdr/NI6R202608260068.md): Strut · worn · Jul 29, 2026 · N115Z · Beech B200GT
  > RIGHT MLG SHOCK STRUT HAS DAMAGE FROM UPLOCK SWITCH, CHROME CHIPPED OFF TO BARE METAL. CHROME ON MLG STRUT ASSEMBLY HAS A DIVOT AT THE LOCATION WHERE UPLOCK PUSH BUTTON APPLIES FORCE TO PLUNGE THE BUTTON FOR GEAR UPLOCK NOTIFICATION. DIVOT BEYOND LIMITS PER C
- [SDR DXTA2026071508807](https://openairdocs.org/sdr/DXTA2026071508807.md): Axle · worn · Jul 13, 2026 · N303QS · Emb EMB505
  > DURING TAKEOFF AND LANDING ROLL AT HIGHER SPEEDS THERE IS A LOUD GRINDING/SQUEAKING NOISE COMING FROM THE NOSEWHEEL ACCOMPANIED BY A STRONG NOSEWHEEL SHIMMY. REPEAT WRITE UP. REMOVED AXEL P/N: 2310-1165-001 S/N: 3128269 ALONG WITH ALL TORQUE LINK HARDWARE. RE
- [SDR DALA2026070904018](https://openairdocs.org/sdr/DALA2026070904018.md): Sleeve · damaged · Jul 5, 2026 · N355NB · Airbus A319114
  > NR 3 AND 4 MLG AXLE SLEEVE DAMAGED. R & R NR 3 & 4 MLG AXLE ADAPTER SLEEVES PER AMM 32-42. OK FOR SVC. (LP: 8924695, AIRCRAFTT WAS GROUNDED)
- [SDR 2026FA0000574](https://openairdocs.org/sdr/2026FA0000574.md): Strut · broken · Jun 19, 2026 · N145WW · Piper PA44180
  > DURING TAXI, FAILURE OF THE LEFT MAIN LANDING GEAR OCCURRED AROUND THE OLEO STRUT PISTON TUBE BOLT HOLE. PIPER AIRCRAFT SERVICE LETTER 1263 RECOMMENDS ROUTINE INSPECTION OF THIS FAILURE POINT EVERY 700 HOURS TIS ON AIRCRAFT WITH OVER 6,500 TOTAL HOURS IN SERV
- [SDR IPXA2026062555305](https://openairdocs.org/sdr/IPXA2026062555305.md): Swivel Fitting · corroded · Jun 7, 2026 · N322UP · Boeing 76734AF
  > AFTER REMOVAL RT MLG STRUT SWIVEL FITTING FOUND OUTER SHAFT OF INBOARD CRANK AND DRIVE ARMS WITH CORROSION IN THE TEETH, FLL-023, ATA 57. NEW SHAFT ASSEMBLY PROCURED AND ACCOMPLISHED INSTALLATION ON TASK CARD "T3F18E008YJ8T" LINE # 50. NO FURHTER ACTION IS R
- [SDR CALA2026052516512](https://openairdocs.org/sdr/CALA2026052516512.md): Strut · discharged · May 23, 2026 · N452UA · Airbus A320232
  > LEFT MAIN SHOCK STRUTAPPEARS TO BE ALMOSTFULLY COMPRESSED FOUND H DIMENTION WITHIN LIMIT REF AMM 12-14-32-200-001-A, BUT DIFFERENCE BETWEEN LEFT AND RIGHT MLG H DIMENTIONS IS MORE THAN 1.7 IN. REQUEST DIP OF FUNCTIONAL CHECK OF MLG SHOCK ABSORBER FLUID LEVEL B
- [SDR AALA202604299403](https://openairdocs.org/sdr/AALA202604299403.md): Strut · collapsed · Apr 28, 2026 · N929NN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: DURING LANDING ROLLOUT MANUAL BRAKING DECELERATION THE AIRCRAFT FELT AS THOUGH THE BRAKES STOPPED WORKING MOMENTARILY. DURING POST FLIGHT INSPECTION, LEFT MAIN STRUT IS COLLAPSED. COMPLETED FULL STRUT SERVICE. PER AMM 12-15-31. NO DEFEC
- [SDR CALA2026042815790](https://openairdocs.org/sdr/CALA2026042815790.md): Axle · failed · Apr 27, 2026 · N17331 · Boeing 7378
  > BRAKES APPEAR TO BE TO BE LOCKING UPON TOUCHDOWN & EXIT FROM R WY GRABING...UPON TAXI INTO RAMP, ACFT EXPERIENCED NR 4 MAIN TIRE DEFLATION. NR 4 BRAKE FOUND DISINTEGRATED. HUB CAP WAS FOUND ON A TAXIWAY PARTIALLY SHAVED OFF & ALSO DISINTEGRATED. ACFT TOWED TO
- [SDR VNAA202606120060](https://openairdocs.org/sdr/VNAA202606120060.md): Axle · corroded · Apr 9, 2026 · N649NN · Cndair CL6002D24
  > LEFT RUSTED AND MISSING TOPCOAT ON ROOT RADIUS INBD AND OTBD SECTIONS PISTON, PISTON AXLE LT MLG. ROOT RADIUS INBD AND OTBD SECTIONS PISTON, PISTON AXLE LT MLG. WERE REPAIRED AND ATTENDED PER REO 670-32-11-361 REV. A.
- [SDR VNAA202606120059](https://openairdocs.org/sdr/VNAA202606120059.md): Axle · corroded · Apr 9, 2026 · N649NN · Cndair CL6002D24
  > EXPOSED MATERIAL ON ROOT SETTLEMENT AREA AT RH MLG PISTON AXLE. EXPOSED MATERIAL ON ROOT SETTLEMENT AREA AT RH MLG PISTON AXLE WAS ATTENDED PER REO 670-32-11-361 REV A.
- [SDR 2026FA0000264](https://openairdocs.org/sdr/2026FA0000264.md): Axle · out of tolerance · Apr 8, 2026 · N424CW · Cessna 525B
  > DURING THE 1ST TIRE CHANGE ON THIS AIRCRAFT SINCE PRODUCTION, IT WAS FOUND THAT BOTH MLG AXLE NUTS HAD JUST FINGER TIGHT TORQUE. THE MAINTENANCE MANUAL CALLS OUT 550 IN LBS INTIAL TORQUE, BACK TO ZERO, THEN 265 -275 IN LBS FINAL TORQUE. IT WAS FOUND AFTER INSP
- [SDR AALA202604081377](https://openairdocs.org/sdr/AALA202604081377.md): Shock Absorber · collapsed · Apr 4, 2026 · N407AN · Airbus A321253NX
  > AIRCRAFT WAS GROUNDED: UPON LANDING GEAR RETRACTION RECEIVED A NOSE LANDING GEAR SHOCK ABSORBER FAULT. FAULT CLEARED WHILE READING ECAM ACTIONS. THEN LANDING GEAR DOOR NOT CLOSED. FOLLOWED ECAM RECYCLED GEAR HANDLE, GEAR RETRACTED NORMALLY. THE FAULT REOCCURE
- [SDR 2026FA0000476](https://openairdocs.org/sdr/2026FA0000476.md): Strut · fractured · Mar 3, 2026 · N1532V · Piper PA18
  > PIPER PA-18 EXPERIENCED RIGHT HAND LANDING GEAR COLLAPSE AFTER LANDING ROLLOUT CAUSING DAMAGE TO MAIN LANDING GEAR AND RIGHT WING ASSEMBLY. DETAIL INSPECTION FOUND 2 EACH FRACTURES ON RIGHT HAND LANDING GEAR ASSEMBLY. RIGHT SHOCK STRUT HYDRASORB (PN 487 558) F
- [SDR 2026FA0000149](https://openairdocs.org/sdr/2026FA0000149.md): Bushing · missing · Mar 2, 2026 · N808TC · Gulstm GVSP
  > DURING A RECENT LANDING GEAR INSPECTION AT STANDARD AERO VNY IT WAS NOTED THAT BOTH LH AND RH AXLES WERE MISSING BUSHINGS FOR STRUT ATTACH PINS TO AXLES, RESULTING IN DAMAGE REQUIRING REPLACEMENT OF BOTH AXLES AND THE RH STRUT PISTON SPHERICAL BEARING. BOTH
- [SDR CVGA20260216002](https://openairdocs.org/sdr/CVGA20260216002.md): Strut · overserviced · Feb 13, 2026 · N453TM · Beech 400A
  > ON LANDING, REVERSERS WOULD NOT DEPLOY. BELOW 60 K LOST BRAKES. USED EMERGENCY BRAKES TO STOP ACFT. AFTER TAXIING OFF RUNWAY, PLACED BRAKES IN ANTI SKID OFF POSITION. BRAKES WERE RESTORED. AIRSPEED INDICATOR SPEED LOW BAR WAS VISUAL. AFTER ACFT PARKED MAIN WH
- [SDR SIMA20260123001](https://openairdocs.org/sdr/SIMA20260123001.md): Strut · underserviced · Jan 23, 2026 · N329DD · Emb ERJ170200LR
  > LG WOW SYS FAIL AFTER TAKEOFF RETURN TO ORD. EMERGENCY DECLARED. PERFORMED LT MAIN LANDING GEAR SHOCK STRUT SERVICNG IAW AMM 12-12-07. LEAK CHECK PASSED NO FAULT DETECTED OPS CHECK GOOD.
- [SDR VNAA2026041500002](https://openairdocs.org/sdr/VNAA2026041500002.md): Sleeve · chafed · Jan 22, 2026 · N521AE · Cndair CL6002C10
  > LH MLG IB PISTON AXLE HAS CHIPPED METAL AT EDGE OF BRAKE UNIT ASSEMBLY BEARING SURFACE.
- [SDR VNAA2026041500003](https://openairdocs.org/sdr/VNAA2026041500003.md): Strut · scratched · Jan 21, 2026 · N521AE · Cndair CL6002C10
  > RH MLG STRUT HAS 3 SCRATCHES ON REAR SIDE, ONE SCRATCH SHOWING BARE METAL.
- [SDR SIMA20260119001](https://openairdocs.org/sdr/SIMA20260119001.md): Strut · discharged · Jan 19, 2026 · N205NN · Emb ERJ170200LR
  > AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT POSITIVE RATE CALL ATTEMPTED TO RETRACT GEAR. LEVER WOULD NOT MOVE, APPROX. 3 SECONDS LATER LG WOW SYS FAIL EICAS MESSAGE APPEARED. RAN QRH CHECKLIST. MESSAGE CLEARED UPON TOUCHDOWN. EMERGENCY DECLARED NOT OVER WT.
- [SDR DALA2026083104905](https://openairdocs.org/sdr/DALA2026083104905.md): Sleeve · corroded · Jan 9, 2026 · N820DX · Boeing 75726D
  > CORROSION ALONG THE BEVELED PART OF THE BEARING SLEEVE. FITTING REPLACED ON NR 18. (1393346)(AIRCRAFT GROUNDED)
- [SDR 2026FA0000010](https://openairdocs.org/sdr/2026FA0000010.md): Strut · misoverhauled · Jan 9, 2026 · N147X · Gulstm GIV
  > LANDING GEAR WOULD NOT RETRACT, CYCLED GEAR, ONCE GEAR WAS UP AND LOCKED, LEFT HYDRAULIC SYSTEM COMPLETE LOSS OF FLUID AND PRESSURE. UPON LANDING HAD TO SELECT THE LANDING GEAR DOWN, EMERGENCY BLEW LANDING GEAR DOWN FOLLOW EMERGENCY PRODUCERS. CONTACTED GULFST
- [SDR SCNA20260120038](https://openairdocs.org/sdr/SCNA20260120038.md): Strut · leaking · Jan 7, 2026 · N8059A · Boeing 73786J
  > DUE TO HISTORY OF LEFT MAIN LANDING GEAR STRUT LEAK- PERFORM REPLACEMENT OF THE ACTIVE AND SPARE SEALS IAW AMM 32-11-21-960-802. REMOVED AND REPLACED LT MAIN MANDING GEAR IAW CC 320400100.
- [SDR SIMA202512310001](https://openairdocs.org/sdr/SIMA202512310001.md): Strut · discharged · Dec 30, 2025 · N329DD · Emb ERJ170200LR
  > LANDING GEAR WOW SYS FAIL CAUTION MESSAGE, RETURNED TO THE FIELD, DECLARED EMERGENCY, NO INJURIES. SERVICED NITROGEN TO LT MLG SHOCK STRUT TO CORRECT HEIGHT IAW AMM 12-12-07. NO MLG WOW OR NO DISPATCH MESSAGE NOTED ON THE EICAS.
- [SDR AALA202512192290](https://openairdocs.org/sdr/AALA202512192290.md): Strut · low pressure · Dec 15, 2025 · N946NN · Boeing 737823
  > AIRCRAFT WAS NOT GROUNDED: AFTER TOUCHDOWN DURING MAX BRAKING CHECK AIRCRAFT PULLS SLIGHTLY LEFT. LEFT MAIN GEAR STRUT APPEARS LOW. SERVICED LEFT HAND MAIN LANDING GEAR SHOCK STRUT WITH NITROGEN. PER AMM12-15-31.
- [SDR REXA2026052700738](https://openairdocs.org/sdr/REXA2026052700738.md): Strut · corroded · Dec 13, 2025 · N921XJ · Cndair CL6002D24
  > PITTING WAS FOUND ON MLG SHOCK STRUT LH SIDE BELOW IDENTIFICATION PLACARD. MLG SHOCK STRUT WILL BE REPLACED BY CARD 900-32-730-705
- [SDR UIEA2025121101339](https://openairdocs.org/sdr/UIEA2025121101339.md): Flex Line · cracked · Dec 11, 2025 · N407KZ · Boeing 7474KZF
  > AFTER ROTATION, RECEIVED GEAR TILT EICAS MSG. GEAR SYNOPTIC PAGE SHOWED LEFT BODY GEAR TILT MSG. FOUND LT BODY GEAR POSITIONING ACTUATOR HYD LINE CRACKED. REPLACED THE LINE WITH TEMPORARY FLEX LINE IAW GMM 3.25.1 AND AMM 20-11-18.
- [SDR DXTA2025112605816](https://openairdocs.org/sdr/DXTA2025112605816.md): Packing · faulted · Nov 23, 2025 · N923QS · Cessna 680A
  > WHILE LEVEL AT FL410, HEARD A LOUD THUMP IN THE NOSE FOLLOWED BY GEAR DISAGREE N AMBER CAS MESSAGE. NOSE GEAR INDICATOR WAS ALSO SHOWING YELLOW HASH INDICATION. QRH PROCEDURES WERE ACCOMPLISHED. INDICATIONS REMAINED UNTIL DESCENDING THROUGH FL230, HEARD ANOTH
- [SDR 2025FA0000769](https://openairdocs.org/sdr/2025FA0000769.md): Bushing Sleeve · debonded · Nov 19, 2025 · N728FG · Cessna 172S
  > DURING ANNUAL INSPECTION IT WAS NOTED THAT THE LT MLG HAD A DISBONDED BUSHING LINER.
- [SDR AALA202512022587](https://openairdocs.org/sdr/AALA202512022587.md): Axle · failed · Nov 16, 2025 · N964AN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: DURING TAXI IN AIRCRAFT BEHIND US ADVISED THE TOWER WE HAD SMOKE COMING FROM LEFT MAIN NUMBER 1 TIRE. STOPPED THE AIRCRAFT AND CALLED FOR ARFF, WAS ADVISED TIRE WAS FLAT. WHILST PARKED AFTER 15 MINS ANTI-SKID INOPERATIVE LIGHT CAME ON.
- [SDR DALA2025111208280](https://openairdocs.org/sdr/DALA2025111208280.md): Strut · discharged · Nov 8, 2025 · N124DU · Airbus BD5001A10
  > DECLARED EMERGENCY FOR THE FLIGHT DUE TO WEIGHT ON WHEELS FAULT WITH POSSIBLE LOSS OF NOSE WHEEL STEERING. JACKED A/C. FOUND RT STRUT NOT FULLY EXTENDED. SERVICED RT STRUT, OPS CHECK GOOD. (LP# 8002764)
- [SDR DALA2025102007647](https://openairdocs.org/sdr/DALA2025102007647.md): Strut · out of limits · Oct 19, 2025 · N171DN · Boeing 767332
  > SHIP 171 RT MLG UPPER PISTON TORSION LINK ATTACHMENT POINT FOUND OUT OF LIMITS. CORRECTIVE ACTION: REPAIRED DIA II A+B PER LGCMM 32-00-00 (1259603)
- [SDR CALA2025100709749](https://openairdocs.org/sdr/CALA2025100709749.md): Spring · missing · Oct 3, 2025 · N210UA · Boeing 777222
  > PDA 2 REFRENCE LOG 6494784 FOUND LEFT HAND GEAR SIDE BRACE SPRING MISSING ON ARRIVAL..LANDING GEAR LEFT STRUT DOWNLINK SPRING MISSING FWD DRAG BRACE AFT SPRING INSTALLED NEW LEFT MLG DRAG BRACE AFT LOCK SPRING AND SPOOLHALF, REF AMM 32-32-07-400-802.
- [SDR 2025FA0000563](https://openairdocs.org/sdr/2025FA0000563.md): Bushing · debonded · Aug 21, 2025 · N561FG · Cessna 172S
  > DURING ANNUAL INSPECTION IT WAS NOTED THAT LEFT MLG HAS DISBONDED BUSHING LINER.
- [SDR 2025FA0000562](https://openairdocs.org/sdr/2025FA0000562.md): Bushing · debonded · Aug 21, 2025 · N239FG · Cessna 172S
  > DURING ANNUAL INSPECTION IT WAS NOTED THAT LEFT MLG HAS DISBONDED BUSHING LINER. IT WAS ALSO NOTED THE RIGHT BUSHING BEGINNING TO DISBOND.
- [SDR 2025FA0000618](https://openairdocs.org/sdr/2025FA0000618.md): Spring Strut · sheared · Aug 8, 2025 · N1950C · Cessna 195B
  > AIRCRAFT LH MAIN SPRING STRUT SHEARED AT THE FUSELAGE ATTACH POINT. THE SERIAL NUMBER OF THE FAILED STRUT IS 6L85, RETURNED TO SERVICE IN 2017. VISUAL INSPECTION OF THE SPRING STRUT SHOWS THAT THE CRACK HAD BEEN THERE FOR A LONG TIME, EVIDENCED BY IRON OXIDE A
- [SDR IPXA2028080700149](https://openairdocs.org/sdr/IPXA2028080700149.md): Strut · corroded · Aug 6, 2025 · N353UP · Boeing 76734AF
  > SUSPECTED CORROSION RH MLG UPPER STRUT BODY - APPROX 14€? X 0.75€? TOTAL AREA BLENDED CORROSION AREAS IAW CMM 20-10-01 STEP 2.F AND 2.H. PITTING STILL REMAINS. MAPPED AND SENT DAMAGE PHOTOS TO ENGINEERING OF PITTED AREAS AND ATTACHED TO FAULT. PITTED AREAS
- [SDR UIEA2025073001067](https://openairdocs.org/sdr/UIEA2025073001067.md): Bushing · gouged · Aug 2, 2025 · N471MC · Boeing 747412
  > LH BODY GEAR SIDE STRUT BUSHING (AIRCRAFT SIDE) IS GOUGED ON INSIDE.(<P>FABRICATED A NEW BUSHING PER BOEING SOPM 20-43-04 & EA 747-53-40-28-130537. NO FURTHER DEFECTS NOTED.</P>)
- [SDR DALA2025061004419](https://openairdocs.org/sdr/DALA2025061004419.md): Bearing · gouged · Jun 7, 2025 · N105DU · Airbus BD5001A10
  > R/H MLG ASSEMBLY, AFT SPHERICAL BEARING GOUGED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 211-0002:3210-4001-RH/001 00496 REMOVED AND REPLACED SPHERICAL BEARING REF A220 AMP 32-11-03. RH MLG ASSEMBLY INSTALLATION AND
- [SDR 4DPA2025041300001](https://openairdocs.org/sdr/4DPA2025041300001.md): Strut · underserviced · Apr 13, 2025 · N914JX · Emb EMB145LR
  > PILOT REPORTED- AFTER NORMAL TAKEOFF LG AIR/GND FAIL CAUTION MESSAGE PRESENTED MOMENTS AFTER GEAR FINISHED ITS RETRACT CYCLE. CYCLED GEAR IN AIR TO NO AVAIL. MX, OPS AND CREW ELECTED TO PERFORM AN AIR RETURN. LANDING WAS NORMAL AND SPOILERS, T/R'S DEPLOYED AND
- [SDR FXTA20250411001](https://openairdocs.org/sdr/FXTA20250411001.md): Strut · low pressure · Apr 9, 2025 · N703BA · Textrn 408
  > RH MLG STRUT LOW AND NEEDS SERVICED.
- [SDR ANCF20250331006](https://openairdocs.org/sdr/ANCF20250331006.md): Shock Absorber · corroded · Mar 31, 2025 · N800AV · Boeing 7878
  > ON MARCH 31, 2025, DURING THE EXECUTION OF THE PUT THE AIRPLANE BACK TO SERVICE. DEPRESERVING PROCEDURE (DMC-B787-A-10-11-07-03A-820A-A), CORROSION WAS DETECTED ON THE RH SHOCK STRUT (PN 51010-38, SN S00VC) DURING THE EXAMINE THE LANDING GEAR COMPONENTS FOR C
- [SDR FXTA20250408001](https://openairdocs.org/sdr/FXTA20250408001.md): Strut · leaking · Mar 15, 2025 · N408BA · Textrn 408
  > NO CHROME SHOWING ON RIGHT LANDING GEAR STRUT
- [SDR IPXA2025032270655](https://openairdocs.org/sdr/IPXA2025032270655.md): Cylinder · corroded · Mar 15, 2025 · N311UP · Boeing 76734AF
  > **SUPPLEMENTAL SDR** FAULT - CORROSION - FOUND CORROSION ON INNER SURFACE OF R/H MAIN LANDING GEAR OUTER CYLINDER. (REPAIR). ACCOMPLISHED JOB I.A.W UPS EO-93133-REQ1 REV1. REVIEW COMPLETE
- [SDR IPXA2025031870655](https://openairdocs.org/sdr/IPXA2025031870655.md): Cylinder · corroded · Mar 15, 2025 · N311UP · Boeing 76734AF
  > **SDR FILED OPEN** FOUND CORROSION ON INNER SURFACE OF R/H MAIN LANDING GEAR OUTER CYLINDER. (REPAIR) PERFORMED NDT/PT FOR THE REWORKED AREA I.A.W SOPM 20-20-02 REV.29.<BR>RESULT: NO CORROSION INDICATION WAS FOUND.
- [SDR 2025FA0000153](https://openairdocs.org/sdr/2025FA0000153.md): Strut · broken · Mar 5, 2025 · N1105 · Hughes 369D
  > LEFT HAND REAR LANDING GEAR STRUT ASSEMBLY BROKEN AT BRACE ASSEMBLY ATTACHMENT BOLT DURING LANDING. OTHER MINOR DAMAGE TO SURROUNDING AREA OCCURRED. TOTAL TIME ON PART IS UNKNOWN.
- [SDR DALA2025020700964](https://openairdocs.org/sdr/DALA2025020700964.md): Shock Absorber · discharged · Feb 7, 2025 · N348NW · Airbus A320212
  > SHIP 3248 - GEAR/ATB - DUE TO A L/G SHOCK ABSORBER FAULT THAT PREVENTED GEAR RETRACTION. CORRECTIVE ACTION: ACCOMPLISHED A FULL SERVICE OF THE NLG SHOCK STRUT. NLG 24GA AND 25GA PROXIMITY SENSORS REPLACED AS A PRECAUTION. (LP: 6821962)
- [SDR QXEA2025010600003](https://openairdocs.org/sdr/QXEA2025010600003.md): Strut · leaking · Jan 5, 2025 · N663QX · Emb ERJ170200LR
  > REJECTED TAKE OFF AT ROUGHLY 100 KNOTTS FO MAY HAVE ADVANCED THROTTLE A HAIR TOO FAR. REMOVED FROM SERVICE. NO SIGNS OF HIGH ENERGY STOP OR ANY SIGNS OF TIRE DAMAGE - REF AMM 05-50-12-200-801-A 1(B). FOUND LEAKING MLG STRUT ON INSPECTION AT LEFT SIDE. C/W MCN

Next page: https://openairdocs.org/jasc/3213/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 = '3213'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/3213/reports

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