JASC 3211

Service difficulty reports · 1,177

Reports filed under 3211 · Main Landing Gear Attach Section, 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 = '3211'
  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.

SDR SWAA001194Fitting · corrodedDURING SCHEDULED D CHECK, FOUND LT MLG FITTING CORRODED AT TWO FASTENER HOLES, BS 706 STRINGER 18A L. REPAIRED FITTING PER ER NR 00-0667.Jul 1, 2000 · N104SW · Boeing 7372H4SDR 20000720SH005Bearing · crackedDURING REMOVAL OF BOTH LEFT AND RIGHT LANDING GEAR, FORWARD TRUNNION BEARINGS. FOUND THE OUTER HOUSING WAS CRACKED COMPLETELY THROUGH ON BOTH BEARINGS. OLD BEARINGS WERE BEING REMOVED BECAUSE OF LOOSE BALLS. LANDINGS, 6,570. (X)Jun 23, 2000 · N19RP · Lear 35ASDR 20000720SH033Bearing · crackedREMOVED FORWARD MAIN LANDING GEAR TRUNNIONS BEARINGS BECAUSE OF LOOSE BALLS. FOUND OUTER HOUSING OF BOTH BEARINGS CRACKED COMPLETE THROUGH. LANDINGS, 7,271. (X)Jun 21, 2000 · N435MS · Lear 35LEARSDR CA000621035Fitting · crackedTHE WING LOWER SKIN IN AREA OF MLG DRAG LINK FITTINGS IS TO BE INSPECTED EVERY 4000 FLT HRS. IN CASE OF ABOVE AC INSPECTIONS NEVER REVEALED ANY DISCREPANCIES. MLG DRAG LINK FITTINGS (UNDER INSP REQMT OF GENERAL DYNAMICS ALERT SB-57-51) REFERS TO ACCEPTANCE CJun 19, 2000 · Cvac 580SDR P5CA0000208Bushing · crackedRIGHT BODY LANDING GEAR INBOARD TRUNNION BUSHING CRACKED. REPLACED RT BODY LANDING GEAR INBOARD AND OUTBOARD TRUNNION FITTING. BORE REWORKED AND NEW REWORKED BUSHINGS INSTALLED PER SRM 53-10-08 FIG 1 & 2 AND POLAR CARD M3213-001.Jun 17, 2000 · N858FT · Boeing 747123SDR DL72W001158Trunnion · corrodedTHE I/B LUG OF THE LEFT MAIN LANDING GEAR TRUNNION SUPPORT BEAM WAS FOUND CORRODED. THE LUG BORE WAS OVERSIZED TO REMOVE THE CORROSION AND AN OVERSIZED REPAIR BUSHING WAS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 377531-14.Jun 14, 2000 · N296WA · Boeing 727247SDR 20001115SH008Damper · leakingKIN/MBJ - FLT JM 059 - PRIOR TO DEPARTURE, RIGHT PITCH DAMPER WAS FOUND SEEPING HYDRAULIC FLUID. IT WAS SERVICED AND AIRCRAFT DISPATCHED. DURING TAKEOFF, RIGHT MAIN LANDING GEAR WOULD NOT RETRACT BOTH IN SYSTEM 1 AND SYSTEM 2. DURING TROUBLESHOOTING, THE PIJun 7, 2000 · N840AB · Airbus A310324SDR AWXA0000368Beam · galledC-CHECK, RIGHT MLG INBOARD STABILIZER SUPPORT BEAM GALLED ON LUG FACES (BOTH ENDS). REMOVED AND REPLACED RIGHT MLG STABILIZER SUPPORT BEAM IAW 737 MM 57-15-0 PG 408.Jun 5, 2000 · N183AW · Boeing 737277SDR DLM88001079Fitting · dentedAN INTEGRAL STIFFENER ON THE LT NOSE LANDING GEAR TRUNNION SUPPORT FITTING WAS FOUND DENTED JUST AFT OF THE MAIN LUG. THE DENTED STIFFENER WAS REFORMED, HFEC INSPECTED TO ENSURE NO CRACKING, AND REINFORCED WITH TWO ALUMINUM REPAIR ANGLES PER ER/A 377424-14, RJun 2, 2000 · N977DL · Doug MD88SDR AALA20000930Trunnion · corrodedTUL - FOUND AFT MOUNT HOLE LEFT SIDE TRUNNION CASTING HAS CORROSION. INSTALLED BUSHING PER SRM 53-40-00-00 PAGE 69 LEFT AFT MOUNT HOLE. (M)Jun 1, 2000 · N1755 · Doug MD11SDR PLGA000525ABolt · shearedBOS-BGR - FLT 4844 - AFTER TAKEOFF, WHEN THE PILOT SELECTED THE GEAR UP, THE INTRANSIT LIGHT STAYED ON. THE CREW FOLLOWED THEIR CHECKLIST AND SELECTED THE GEAR DOWN. THE RIGHT MAIN GEAR WOULD NOT INDICATE DOWN AND LOCKED. THE CREW THEN FOLLOWED THE GEAR UNSMay 25, 2000 · N356BE · Saab 340BSDR GAIA00288Stiffener · crackedDURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, RIGHT NLG TRUNNION SUPPORT VERTICAL STIFFENER CRACKED. REPAIRED TRUNNION SUPPORT STIFFENER IAW TIMCO REO S00168. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M)May 24, 2000 · N854AA · Boeing 727223SDR GAIA00289Fitting · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, NLG RIGHT TRUNNION SUPPORT FITTING HAS PITTING CORROSION ON FLANGE. REPAIRED SUPPORT FITTING IAW TIMCO REO S00161. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M)May 24, 2000 · N854AA · Boeing 727223SDR USAA000732Fitting · crackedCLT - FOUND FITTING CRACKED .375 INCH, LEFT MLG SUPPORT FITTING REAR SPAR WALKING BEAM. REPAIRED PER TR 57-40-13. (M)May 23, 2000 · N563AU · Boeing 737301SDR USAA000725Fitting · crackedCLT - FOUND .5 INCH CRACK IN FITTING, OUTBOARD SUPPORT FITTING MLG BEAM AT CUTOUT, REMOVED AND REPLACED. (M)May 23, 2000 · N246US · Boeing 737201SDR AALA20000898Trunnion · corrodedTUL - FOUND LEFT AND RIGHT NLG TRUNNION FITTINGS (UPPER AND LOWER) AND CAPS CORRODED. REPAIRED TO FIRST OVERSIZE PER SRM 53-40-1 PAGE 1. (M)May 16, 2000 · N848AA · Boeing 727223SDR USAA000716Fitting · crackedCLT - Q-4, FITTING HAD .50 INCH CRACK. REPAIRED PER TR 57-40-10. (X)May 16, 2000 · N278AU · Boeing 7372B7SDR UPS00232610Trunnion · brokenINSPECTION TYPE:C, RT MLG TRUNNION BROKE WHILE AIRCRAFT WAS PARKED. *S/D* RIGHT MAIN GEAR REMOVED AND REPLACED.May 15, 2000 · N911UP · Boeing 72727CSDR 2000UALA00243Bolt · crackedON WALKAROUND, FOUND 1.125 INCH DIA H-11 BOLT BROKEN AT STATION 1480 BODY LANDING GEAR INBOARD TRUNNION SUPPORT FITTING. *S/D* CAUSE WAS DUE TO STRESS CORROSION. REPLACED BOLT (69B13682-1) AND PERFORMED ULTRASONIC INSPECTED ADJACENT (2) BOLTS COMMON TO FITTMay 11, 2000 · N179UA · Boeing 747422SDR AU001274Trunnion · cracked(AUS) MAIN LANDING GEAR FORWARD TRUNNION CRACKED IN THE TOP WEB ADJACENT TO THE GEAR ATTACHMENT BEARING. FOUND DURING FLUORESCENT DYE PENETRANT INSPECTION IAW MEB85-11 R4.May 4, 2000 · Cessna 402CSDR AU001272Trunnion · cracked(AUS) RT MAIN LANDING GEAR FORWARD TRUNNION CRACKED ON THE TOP WEB ADJACENT TO THE GEAR ATTACHMENT BEARING. FOUND DURING FLUORESCENT DYE PENETRANT INSPECTION IAW MEB85-11 R4.May 4, 2000 · Cessna 402CSDR 20000531SH007Pivot · crackedLEFT BRAKE KEPT BECOMING SOFT AND LOOSING HYDRAULIC FLUID WITH NO EXTERNAL LEAKS FOUND. REMOVAL AND DYE PENETRANT INSPECTION OF LEFT MAIN GEAR PIVOT REVEALED CRACK IN RADIUS OF SPLINES INTO BRAKE FLUID PASSAGE. (X)May 2, 2000 · N4802R · Cessna 172RGSDR 20010614CW001Bolt · brokenRIGHT GEAR LEG SPRING ROTATED IN MOUNTING (BOLT SHEARED) AFTER AIRCRAFT LOCKED UP WHEEL FROM HARD BRAKING. GEAR ROTATED 180 DEGREES. AIRCRAFT SUFFERED BELLY DAMAGE AND ELEVATOR DAMAGE.May 1, 2000 · N6360D · Cessna 172NSDR L1GA200000062Attach Fitting · corrodedLEVEL 2 CORROSION RT MLG FITTING AFT FACE OF FIXED BRACE BOLT HOLE.Apr 28, 2000 · N14534 · Doug DC932SDR L1GA200000061Attach Fitting · corrodedLEVEL 2 CORROSION LT MLG FIXED BRACE BUSHING ATTACH LUG AT THE MLG ATTACH FITTING.Apr 28, 2000 · N14534 · Doug DC932SDR USAA000584Support Fitting · crackedCLT - FOUND SUPPORT FITTING CRACKED .250 INCH, MLG BEAM SUPPORT FITTING OUTBOARD BOLT HOLE RT WING. REPAIRED PER TR 57-40-13. (M)Apr 24, 2000 · N351US · Boeing 737301SDR USAA000592Support Fitting · crackedCLT - FOUND SUPPORT FITTING CRACKED .25 INCH, LEFT MLG BEAM SUPPORT FITTING. REPAIRED PER TR 57-40-13. (M)Apr 24, 2000 · N351US · Boeing 737301SDR USAA000598Fitting · crackedCLT - FOUND FITTING CRACKED .375 INCH, LT MLG BEAM OUTBOARD ATTACH FITTING AT UPPER BOLT ON L/B. REPAIRED PER TR 57-40-13. (M)Apr 24, 2000 · N562AU · Boeing 737301SDR RRXA001948Boss · corrodedDURING A MAINTENANCE VISIT FOUND THE MLG STRUT ASSY RETRACT PIN BOSS AND RETRACT PIN NEEDED REWORK PER MA-AI-3210-01:03, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-05Apr 15, 2000 · N961R · Doug DC873FSDR 20000626SH007Bolt · misinstalledGOUGE IN NOSE WHEELWELL BAY CAUSED BY PREVIOUSLY INCORRECT INSTALLATION OF BOLT IN THE NOSE GEAR. (X)Apr 12, 2000 · N45UF · Lear 31ASDR CA000501033Fitting · corroded(CAN) ON HEAVY MAINTENANCE L DRAG STRUT SIDE BRACE FITTING BUSHING FOR SPINDLE PIN FOUND WITH EVIDENCE OF HAVING ROTATED, SEALENT CUT AROUND PERIPHERY OF BUSHING FLANGE. DRAG STRUT BUSHING REMOVED AND HEAVY CORROSION FOUND ON BOTH FLANGE SEAT AND BORE SURFACE Apr 11, 2000 · Boeing 767209SDR CA000501032Fitting · corroded(CAN) ON HEAVY MAINTENANCE LT DRAG STRUT SIDE BRACE FITTING BUSHING FOR SPINDLE PIN FOUND WITH EVIDENCE OF HAVING ROTATED, SEALENT CUT AROUND PERIPHERY OF BUSHING FLANGE. DRAG STRUT BUSHING REMOVED AND HEAVY CORROSION FOUND ON BOTH FLANGE SEAT AND BORE SURFACEApr 11, 2000 · Boeing 767209SDR 20000619SH001Fitting · crackedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CRACKED MLG SIDE BRACE STRUCTUAL FITTING IN RT MLG SIDE BRACE, UPPER ATTACH POINT. (X)Apr 10, 2000 · N260FA · Lkheed 1011385114SDR AU000115Bolt · cracked(AUS) LEFT LANDING GEAR INBOARD ATTACHMENT BOLT FAILED. LEFT LANDING GEAR COLLAPSED.Apr 5, 2000 · Piper PA38112SDR AU000276Fitting · corroded(AUS) MLG STRUT SUPPORT FITTING CORRODED IN BEARING BORES.Mar 28, 2000 · Saab 340BSDR AU000275Fitting · corroded(AUS) DRAG BRACE SUPPORT FITTING CORRODED IN BEARING BORES.Mar 28, 2000 · Saab 340BSDR AU000274Fitting · corroded(AUS) DRAG BRACE SUPPORT FITTING CORRODED IN BEARING BORES.Mar 28, 2000 · Saab 340BSDR AU000273Fitting · corroded(AUS) MLG STRUT SUPPORT FITTING CORRODED IN BEARING BORES.Mar 28, 2000 · Saab 340BSDR CA000328008Support Bracket · cracked(CAN) DURING SCHEDULED INSPECTION, A .25 INCH CRACK WAS FOUND IN THE LEFT LANDING GEAR LEG SUPPORT. THE CRACK WAS PROPAGATING FROM THE LOWER AFT RADIUS OF THE SLOT IN THE SUPPORT THAT RECEIVES THE LANDING GEAR LEG.Mar 9, 2000 · Cessna 172GSDR USAA000333Attach Fitting · crackedCLT - FOUND ATTACH FITTING CRACKED .25 INCH, RIGHT MLG TRUNNION SUPPORT BEAM OUTBOARD ATTACH POINT FIT. REPLACED RIGHT MIG BEAM SUPPORT FITTING PER TR 57-40-13. (M)Mar 7, 2000 · N512AU · Boeing 7373B7SDR CA000307001Structure · cracked(CAN) SECURING LUGS (P/N D2731) THAT SECURE THE HIGH SKID GEAR STEP ASSY FOUND CRACKED. SUBMITTER SUSPECTED CAUSE OF CRACKS IS IMPROPER TORQUE OF THE NUT AND BOLT WHICH SHOULD BE UP TO 60 INCH/POUNDS. MANUFACTURER HAS BEEN NOTIFIED.Mar 7, 2000 · Bell 206BSDR RRXA001691Boss · corrodedDURING A MAINTENANCE VISIT, FOUND THAT THE RT. MLG REQUIRES RE-WORK ON BOSS, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. C/W MAIN LANDING GEAR RETRACT PIN & BOSS REWORK IAW E.O. 99-236 WITH APPROVED 8110-3Feb 24, 2000 · N994CF · Doug DC862SDR RRXA001690Boss · corrodedDURING A MAINTENANCE VISIT, FOUND THAT THE LT MLG REQUIRES RE-WORK ON BOSS, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. C/W MAIN LANDING GEAR BOSS & RETRACT PIN PER E.O.99-236 WITH APPROVED 8110-3 DATED 2-2Feb 24, 2000 · N994CF · Doug DC862SDR 20000407SH034Fork · crackedCRACK INDICATION .75 INCH LONG IN SLOT 3. (X)Feb 23, 2000 · N585HV · Piper PA31350SDR 20000407SH032Trunnion · damagedPART IS MAIN LANDING GEAR REAR SIDE BRACE TRUNNION. A SMALL ERODE WAS FOUND IN THE WEB NEXT TO THE INBOARD LOWER BOLT HOLE ON BOTH RT AND LT MAIN GEAR. CRACK WAS DETECTED BY SMALL CRACK IN PAINT. CRACK WAS VERIFIED BY DYE PENETRANT. (X)Feb 21, 2000 · N531MC · Piper PA421000SDR 20000407SH020Trunnion · crackedPART IS MAIN LANDING GEAR REAR SIDE BRACE TRUNNION. A SMALL CRACK WAS FOUND IN THE WEB NEAR TO THE INBOARD LOWER BOLT HOLE ON BOTH RT AND LT MAIN GEAR. CRACK DETECTED FROM PREVIOUS EXPERIENCE. CRACK WAS VERIFIED BY DYE PENETRANT. (X)Feb 21, 2000 · N38AF · Piper PA421000SDR 20000407SH016Trunnion · crackedPART IS MAIN LANDING GEAR REAR SIDE BRACE TRUNNION. A SMALL CRACK WAS FOUND IN THE WEB NEXT TO THE INBOARD LOWER BOLT HOLE ON BOTH RT AND LT MAIN GEAR. CRACK WAS DETECTED BY PREVIOUS EXPERIENCE. CRACK WAS VERIFIED BY DYE PENETRANT. (X)Feb 21, 2000 · N325KW · Piper PA421000SDR AU000179Bolt · broken(AUS) MAIN LANDING GEAR STRUT TRUNNION PIN RETAINING BOLT CRACKED. TRUNNION PIN ALSO WORN.Feb 10, 2000 · Gulstm 114SDR 20000511SH008Trunnion · looseLEFT NOSE LANDING GEAR TRUNNION LOOSE. THIS IS THE THIRD OCCURRENCE IN A FLEET OF APPROXIMATELY 25 AIRCRAFT. (X)Feb 7, 2000 · N947QS · Cessna 750SDR 20000511SH007Trunnion · crackedNOSE GEAR TRUNNION MOUNT PLATES CRACKED OR MISSING FASTENERS. SUBMITTER STATED THIS IS THE THIRD OCCURRENCE OF THIS TYPE IN A FLEET OF APPROXIMATELY 25 AIRCRAFT. (X)Feb 7, 2000 · N926QS · Cessna 750
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