JASC 5551
Service difficulty reports · 672
Reports filed under 5551 · Horizontal Stabilizer, Attach Fittings, 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 = '5551' 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 = '5551' 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 96ZZZX2775Doubler · rivets defectiveTOP RIVET ABOVE PLATE. NUT POPPED ON RIGHT SIDE AND WORKING ON LEFTSIDE. RECOMMEND PERIODIC INSPECTION.SDR 96ZZZX2774Doubler · rivets defectiveTOP RIVET ABOVE PLATE. NUT POPPED ON RIGHT SIDE AND WORKING ON LEFTSIDE. RECOMMEND PERIODIC INSPECTION.SDR DLL16960968Fitting · out of positionTHE UPPER STABILIZER POWER SERVO FITTINGS ATTACHED TO THE 1860 BULKHEAD WERE ORIGINALLY MISPLACED. AFTER REALIGNMENT, THE FITTINGS' INBOARD ATTACH FASTENERS DID NOT HAVE E.D. THIS ER/A AUTHORIZES PLUGGING THE DISCREPANT HOLES AND RELOCATING THEM PER DL ERA 2SDR AU960492Fitting · loose(AUS) HORIZONTAL STABILISER WAS REMOVED DUE TO EXCESSIVE MOVEMENT - INVESTIGATION FOUND THAT EACH OF THE TWO FORWARD ATTACHMENT FITTINGS HAD FOUR OF THE FIVE RIVETS SHEARED - SUSPECT INCORRECT GROUND HANDLING TECHNIQUESDR 96ZZZX3513Stabilizer · bolts looseWHILE REMOVING THE HORIZONTAL STABILIZER TO FACILITATE REPAIRS, NOTED THAT 6 OF THE 8 FORWARD ATTACH BOLTS WERE LOOSE. TWO OF THE SPACERS USED BETWEEN THE VERTICAL AND HORIZONTAL ATTACHMENT SHOWED SIGNS OF RUBBING. SUBMITTER RECOMMENDS THAT A ONE-TIME INSPECTSDR 96ZZZX1246Bracket · crackedDURING ROUTINE INSPECTION, LT HORIZONTAL STABILIZER ATTACH BRACKET REINFORCEMENT WAS FOUND CRACKED .50 INCH IN THE LOWER LT RADIUS. CESSNA SERVICE INFORMATION LETTER SE84-17R1 CALLS FOR A REPETITIVE 100-HOUR INSPECTION OF THIS AREA, BUT IT DOES NOT LIST THE 'SDR AU960307Fitting · corroded(AUS) TOP RH STABILATOR ATTACHMENT FITTING CORRODED - STABILATOR AND ALL FOUR FITTINGS REMOVED FOR FURTHER INSPECTION - INSPECTION OF TOP RH POSITION REVEALED EXTENSIVE CORROSION TO SKIN FLANGE AND CRACKING - CRACK LENGTH 19.05MM (0.75IN) - FOUND DURINGINSPECSDR 96ZZZX168Bracket · corrodedDURING INSPECTION, FOUND FORWARD HORIZONTAL STABILIZER BRACKETS EXFOLIATED. PIPER SB 962, WHICH PERTAINS TO THIS AREA, HAD BEEN PREVIOUSLY C/W. THESE BRACKETS ARE HARD TO SEE WITHOUT A MIRROR AND, LIKEWISE, ARE HARD TO CLEAN. SUBMITTER STATED THIS PROBLEM (SDR 96ZZZX167Bracket · corrodedDURING INSPECTION, FOUND FORWARD HORIZONTAL STABILIZER BRACKETS EXFOLIATED. PIPER SB 962, WHICH PERTAINS TO THIS AREA, HAD BEEN PREVIOUSLY C/W. THESE BRACKETS ARE HARD TO SEE WITHOUT A MIRROR AND, LIKEWISE, ARE HARD TO CLEAN. SUBMITTER STATED THIS PROBLEM (SDR 96ZZZX41Bracket · crackedUPON INSPECTION OF RIGGING OF THE RUDDER AND ELEVATOR CONTOL SURFACES FOR A MODIFICATION OF AIRCRAFT, FOUND LEFT HORIZONTAL STABILIZER ATTACH BRACKET CRACKED AT THE BOTTOM OUTBOARD SIDE OF BRACKET. INSTALLED NEW BRACKETS, P/N 1232624-1 IAW SE 84-17, REV. 1.SDR 95ZZZX7030Spar Tube · crackedTHE FUSELAGE REAR SPAR TUBE FOR THE HORIZONTAL STABILIZER WAS FOUND CRACKED THREE-FOURTHS THROUGH ON LT SIDE AND ONE-HALF THROUGH ON RT SIDE. THIS DEFECT WAS FOUND ON 2 ACFT IN A FLEET OF 3. THIS DEFECT APPEARS TO HAVE OCCURRED FROM HEAVY DOWNLOADS ON HORIZ SDR 95ZZZX7027Bracket · crackedBRACKET IS THE HORIZONTAL STABILIZER REAR ATTACH POINT. IT IS WELDED TO THE FUSELAGE TOP'S TWO TUBES. THE RIGHT SIDE BRACKET FLANGE IS CRACKED IN 3 PLACES AROUND WHERE THE STABILIZER CARRY-THROUGH TUBE ATTACHES TO THE FLANGE. AT THE POINT WHERE THE LEFT SIDSDR 96ZZZX142Fitting · crackedTHE HORIZONTAL STABILIZER UPPER SCISSOR MOUNT HAS TWO CRACKS, ONE AT EACH MOUNTING LUG. SUBMITTER SUSPECTS CAUSE A RESULTANT OF HEAVY TAIL-PLANE VIBRATIONS. RECOMMEND C/W SB 1124-55-124.SDR 95ZZZX6332Attach Fitting · corrodedCORROSION FOUND ON C-212 51D AT BEARING AREA. BEARING MATERIAL IS DISSIMILAR. SUBMITTER STATED THAT POSSIBLY A BEARING WAS INSTALLED DRY AT INSTALLATION BY MFG. OPERATORS SHOULD PERFORM CLOSE INSPECTION AT 1,600 FLIGHTS.SDR 95ZZZX6330Attach Fitting · corrodedCORROSION FOUND ON C-212 5ID AT BEARING AREA. BEARING MATERIAL IS DISSIMILAR. SUBMITTER STATED THAT POSSIBLY A BEARING WAS INSTALLED DRY AT INSTALLATION BY MFG. OPERATORS SHOULD PERFORM CLOSE INSPECTION AT 1,600 FLIGHTS.SDR 95ZZZX6329Attach Fitting · corrodedCORROSION FOUND ON C-212 51D AT BEARING AREA. BEARING MATERIAL IS DISSIMILAR. SUBMITTER STATED THAT POSSIBLY A BEARING WAS INSTALLED DRY AT INSTALLATION BY MFG. OPERATORS SHOULD PERFORM CLOSE INSPECTION AT 1,600 FLIGHTS.SDR 95ZZZX6207Splice Assy · cracked.25 INCH LONG WORKING CRACK .015 INCH DEEP. FOUND ON LOWER SPLICE ASSY HORIZONTAL STABILIZER, RT LOWER ATTACH FITTING. HORIZONTAL STABILIZER BEING REMOVED TO BE SENT OUT TO REPLACE SPLICE ASSY. AIRCRAFT TT, 5,392 HRS. LANDINGS, 4,280.SDR 95ZZZX3206Reinforcement · crackedACTT 3,957.8. OPERATOR DISCOVERD 1 INCH CRACK AT LEFT HORIZONTAL STABILIZER REAR SPAR ATTACH POINT REINFORCEMENT BRACKET, OUTBOARD HOLE IN BEND RADIUS (LOWER). DEFECT FOUND DURING PRE-FLIGHT. THIS IS THE SECOND OCCURRENCE AT 2202.1 TOTAL TIME. OPERATOR REPSDR 95ZZZX1750Attachment · crackedDURING 10,000-HOUR INSPECTION, CRACK FOUND AT HORIZONTAL STABILIER ATTACH BRACKET USING EDDY CURRENT INSPECTION. ZYGLO AND VISUAL INSPECTIONS SHOWED NO DEFECT. DEFECT TOO CLOSED UP FOR DETECTION. NEW PART OBTAINED FROM MANUFACTURER AND INSTALLED. REFER TO SDR 95ZZZX2262Fitting · crackedDURING AN INSPECTION, SLIGHT LOOSNESS NOTICED IN THE HORIZ STABILIZER. FURTHER DISASSEMBLY SHOWED FORWARD FITTING CRACKED COMPLETELY THROUGH NEAR RT BOLT HOLE. THE ACFT RECORDS SHOWED THAT EXTENSIVE REPAIRS HAD BEEN MADE TO THE EMPENNAGE AFTER A LANDING INCISDR 95ZZZX1771Nutplate · crackedALL EIGHT NUTPLATES FOUND CRACKED ON FORWARD HORIZONTAL SPAR ATTACH. SUSPECT CAUSE SITTING ON TAIL TO PARK AIRCRAFT. NUTPLATES WERE FOUND AFTER REMOVING STABILIZER FOR REPAIR AND CANNOT BE SEEN ON NORMAL INSPECTION. SUBMITTER WOULD RECOMMEND REMOVING STABILSDR 95ZZZX692Attach · looseDURING INSPECTION AND LOADING OF HORIZONTAL STABILIZER, STRUCTURAL NOISE IN FORM OF KNOCKS, SNAPPING, AND/OR CREAKING (OUTSIDE OF NORMAL SKIN OIL CANNING EVIDENT ON THIS MODEL A/C) EXISTING IN HORIZ STAB. NOISE HAS BEEN TRACED TO MOVEMENT AT HORIZ. STAB. FRON
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