JASC 5510
Service difficulty reports · 5,966
Reports filed under 5510 · Horizontal Stabilizer Structure, 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 = '5510' 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 = '5510' 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 AALA20021328Plate · corrodedTUL - FOUND RIGHT OUTBOARD HORIZONTAL STAB PIVOT BEARING LUG PLATES ARE CORRODED. REPLACED RIGHT OUTBOARD LUG PLATE AND MACHINED PIVOT BORE PER FCO KF0488A, 9, D/E. (M)SDR SIMA200227916Pin · corrodedTHIS A LEVEL 2 FINDING, HORIZONTAL STABILIZER PINS ARE CORRODED. REMOVED AND REPLACED PINS IAW EMB 145 AMM 55-10-00. (M)SDR AUS20021023Structure · bird strike(AUS) BIRDSTRIKE ON RH HORIZONTAL STABILISER. EXTENSIVE DAMAGE CAUSED TO LEADING EDGE AND UPPER AND LOWER SKINS.SDR SWAA022095Rib · crackedDURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STABILIZER UPPER RIB CHORD CRACKED (2 EA) AT STA 166.30 AND STA 193.9. REPAIRED UPPER RIBS PER SRM.SDR SWAA022033Stabilizer · crackedDURING SCHEDULED C2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED ALONG REAR SPAR, NEAR MID POINT. REPAIRED STABILIZER PER SRM.SDR AUS20021007Structure · cracked(AUS) HORIZONTAL STABILIZER CRACKED.SDR UIEA200200034Skin · corrodedDURING CURRENT (C) CHECK AT SIAEC FOUND RIGHT HORIZONTAL STABILIZER BOTTOM SKIN AT STA 343 OUTER SURFACE CORRODED (LEVEL 2). FASTENERS REMOVED IN THE AFFECTED AREA. ALL HOLES CHECKED FOR CORROSION, OVER-SIDED AND HFEC INSPECTED FOR CRACKS. NO ADDITIONAL CORRSDR SWAA021819Rib · crackedDURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STABILIZER LOWER RIB CHORD CRACKED AT STA 120.3, 24 AFT OF FWD LOWER SPAR. REMOVED AND REPLACED LOWER RIB CHORD PER SRM.SDR 02FDEA00557Structure · corrodedNR 1 TAIL FUEL TANK FIFTH BARREL NUT BORE FWD OF REAR SPAR IS CORRODED AT HORIZ STAB UPPER AFT PLANK COMMON TO LT OPERATING BLKHD AND CONSTANT SECTION JOINT.SDR CA020829005Bracket · cracked(CAN) AIRCRAFT LANDED IN ROUGH WATER, CAUSING THE BATTERY TO CRACK AT THE BATTERY POSTS. A COMPLETE INSPECTION OF THE AIRCRAFT WAS CARRIED OUT, AND THE CRACK IN THE REINFORCEMENT BRACKET WAS DISCOVERED. NO OTHER DEFECTS WERE FOUND.SDR QXEA0201419Structure · crackedCKB - HORIZONTAL STABILIZER HAS CRACK INDICATION. COMPLIED WITH SERVICE BULLETIN 8-55-22.SDR SWAA021611Skin · crackedDURING SCHEDULED SPECIAL VISIT, FOUND LOWER SKIN CRACKED ON RT HORIZ STAB AFT SPAR AT NR 1 BALANCE BAY. REPAIRED SKIN PER SWA EA.SDR CA020729001Tip Cap · cracked(CAN) WHILE IN A STEEP DESCENT THE PILOT OBSERVED THE RIGHT HAND TIP CAP (WINGLET) GO PAST HIM AND HIT THE GROUND IN THE LANDING / WORKSITE. THE AIRCRAFT WAS LESS THAN 300 FEET AGL. THE AIRCRAFT CONTINUED DESCENT AND MADE A NORMAL POWER ON LANDING. RECOVERY ANSDR SWAA021564Skin · crackedDURING SCHEDULED D CHECK, FOUND RT HORIZ STAB SKIN CRACKED ON LOWER SURFACE AT STAB STA 125. REPAIRED SKIN PER BFG ER.SDR QXEA0201034Frame · crackedPDX - LEFT HAND SIDE FRAME 4 STRINGER 3, LOOK UP FROM PANEL 331AB OVER SUPPORT BRACKET, HAS .5 INCH CRACK. REPAIRED IAW RD 8-55-199.SDR SWAA021515Rib · crackedDURING SCHEDULED D CHECK, FOUND RT HORIZ STABILIZER RIB CRACKED AT STAB STA 120.3. REMOVED AND REPLACED RT HORIZ STAB LOWER RIB CHORD.SDR SWAA021435Skin · crackedDURING SCHEDULED C4 CHECK, FOUND RT HORIZ STAB LOWER SKIN CRACKED AT THE AFT SPAR. REPAIRED SKIN PER SRM.SDR USAA020313Frame · corrodedPIT - FOUND X-FRAME CORRODED .5 INCH BY 2 INCH AREA, FORWARD SPAR UPPER RIGHT BOLT HEAD TERMINAL FITTING. CORROSION LEVEL 1. CLEANED CORROSION, TREATED, AND PRIMED PER SRM 51-20-04 AND 51-10-02. (M)SDR UPS02238740Rib · crackedINSPECTION TYPE:C+SI INSPECT REMOVED STAB.RIBS. FOR CRACKS AND FORWARD FINDING TO ENGINEE RING(RETAIN CRACKED RIBS) DVI INSPECTION PERFORMED IAW CUSTOMER REQUEST :CRACKS NOTED @ L/H RI BS 17:20 AND 136:50 AND R/H RIBS 17:20 AND 66:50 AND 99:79.SDR 2002FA0000790Bracket · brokenAIRCRAFT UNDERGOING ANNUAL INSPECTION. HORIZONTAL STABILIZER FOUND LOOSE. INSPECTED AND FOUND REAR MOUNTING REINFORCEMENT BRACKET BOTH SIDES BROKEN AND THE FORWARD ATTACHMENT FITTINGS LOOSE. INSTALLED REAR BRACKETS AND PN SK210-126.SDR SWAA021182Skin · crackedDURING SCHEDULED C4 CHECK, FOUND LT STABILIZER LOWER SKIN CRACKED AT FWD EDGE OF AFT SPAR. REPAIRED SKIN PER SRM.SDR AALA20020804Structure · crackedTUL - FOUND RIGHT HORIZONTAL STABILIZER, MID LOWER SECTION, MIDDLE PLANK HAS APPROX 6 INCHES DAMAGED AREA WITH CRACK. REPAIRED PER ESO 80559 DATED 5/20/02. (M)SDR 2002FA0000660Terminal · brokenLEFT LOWER FORWARD TAIL STRUT THREADED ROD DISCOVERED BROKEN ON PREFLIGHT. (NO ADVERSE FLIGHT CHARACTERISTICS NOTED ON PREVIOUS FLIGHT.) ROD BROKEN AT END OF 5/16 INCH X 24 THREADS NEXT TO 5/16 INCH HEX SHAFT.SDR TOX2002F00000Support · crackedDURING A ROUTINE INSPECTION, NOT RELATED TO MFG, THE LOWER LEFT FOLDED TAB WAS FOUND BROKEN OUTBOARD OF THE BOLT HOLE. UPON REMOVAL, A CRACK WAS DISCOVERED ACROSS ABOUT 80 PERCENT OF THE FORWARD FLANGE. THE EFFECTIVE SUPPORT OF THE LEFT STABILIZER WAS REDUCESDR C2XA02TY080Hinge Fitting · wornTYS DURING A SCHEDULED 1C/2C INSPECTION THE HORIZ. STAB HINGE PIN LOCKING BRACKETS ON THE LT. AND RT. SIDE HAD WEAR STEPS IN THEM. MAINT. BLENDED THE WEAR STRIPS,PERFORMED NDT INSPECTION,ALLODINED,PRIMED AND PAINTED IAW WITH GST#1391/02-EMB 135/145 CPM 51-21SDR UPS02238304Beam · corrodedINSPECTION TYPE:C CORROSION ON RH STAB TE UPPER BEAM AT STAB STA. 115 TO 145 CORROSION REMOVED IAW SRM 51-10-06 FOUND TO BE OUTSIDE LIMITS HFEC C/O IAW B727 NDTM PT 6 51-00-00 - NDF BEAM REPAIRED IAW SMRO EO 2002-027-003 UPS ENGINEERING FILE NO. 727-53-200SDR O9I2002F00001Tip Cap · delaminatedTHE TRAILING EDGE OF THE RIGHT HORIZONTAL STABILIZER TIP CAP (PN 24W45002050251) WAS FOUND TO BE DELAMINATING ON THE TRAILING EDGE . THIS IS A COMPOSITE ASSEMBLY AND THE DELAMINATION WAS EASILY SEEN BY VISUAL INSPECTION. THE DEFECTIVE PART WAS REPLACED. THISDR ABXA010847Fitting · crackedRIGHT UPPER HORIZONTAL STABILIZER FITTING HAD INBOARD FORWARD FASTENER HOLE CRACKED. REPAIRED AREA IAW B767 REA B655-43116MR.SDR ABXA010846Fitting · crackedLEFT UPPER HORIZONTAL STABILIZER FITTING HAD 2 EACH FORWARD FASTENER HOLES CRACKED. REPAIRED AREA IAW B767 SRM 57-40 AND REA B655-43116MR.SDR ABXA010845Fitting · crackedLEFT HORIZONTAL, LOWER HORIZONTAL STABILIZER FITTINGS HAD 3 EACH FORWARD FASTENER HOLES CRACKED. REPAIRED AREA IAW B767 SRM 51-40-05 AND REA B766-43116MR.SDR AALA20020478Hinge · corrodedTUL - FOUND CORROSION IN LEFT STAB HINGE BORE OUTBOARD SIDE BETWEEN LUG AND BUSHING. REMOVED CORROSION PER ESO 80559 DATED 4-11-02 AND INSTALLED OVERSIZE BUSHING. (M)SDR 200200233Balance Weight · chippedLEFT HAND HORIZONTAL STABILIZER ELEVATOR BALANCE WEIGHTS FROM STA. 206.8 - 331.8 HAS CHIPPED PAINT UPPER AND LOWER SURFACES. REMOVED LOOSE AND FLAKING PAINT ON LEFT HORIZONAL STABILIZER BALANCE WEIGHTS AND PRIMED.SDR CA020411008Bracket · cracked(CAN) BRACKET WAS FOUND TO BE CRACKED. AIRCRAFT IS BEING REBUILT AFTER AN ACCIDENT.SDR COOSDR02077Rub Strip · wornFUSELAGE TAIL SECTION, HORIZONTAL STABILIZER FIXED FAIRINGS (RUB PLATES) WITH WEAR IN SEVERAL PLACES.SDR USAA020145Hinge Fitting · wornPIT - FOUND SUPPORT FITTING WORN BEYOND LIMITS, HINGE PLATE MOUNTING HOLES WORN, LEFT HORIZONTAL NR 6 HINGE, HORIZ STATION 213.32. REMOVED AND REPLACED PART. (M)SDR AALA20020393Web · puncturedTUL - FOUND PUNCTURE IN WEB OF RIGHT HORIZONTAL BETWEEN AFT SPARS. INSTALLED DOUBLER REPAIR PER ESO 80559 3/21/02. (M)SDR CALA0200138Fitting · corrodedINSPECTION FOUND RT HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR UPPER FORWARD LUG CORRODED. AN OVERSIZED BUSHING WAS INSTALLED IAW MM 55-10-06.SDR CALA0200137Fitting · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR UPPER FORWARD AND AFT LUGS CORRODED. OVERSIZED BUSHINGS WERE INSTALLED AT EACH LOCATION IAW CMM 55-10-06.SDR DHL2002807557FittingDURING C CHECK FOUND L/H HORIZTAL STABILIZER ATTACH FITTING OF UPPER FAIRING,FWD PART CRACKED 5 IN.REMOVED DAMAGED FITTING PER SRM 51-3-0 PG 1.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-3-0 PG 1SDR P2EA2002M016Hinge Fitting · vibratesINTERMITTENT VIBRATION OBSERVED AROUND THE AFT GALLEY FLOOR AREA. REMOVED AND REPLACED THE NR 4 HINGE FITTING ON THE LT HORIZONTAL STAB IAW MM 27-31-13. NO VIBRATION NOTED TO THIS DATE.SDR 2002FA0000671Bracket · crackedWHILE INSPECTING THE NUTPLATES IAW AD, WE FOUND THAT THE FORWARD UPPER WELD JOINT HAD CRACKED ADJACENT TO THE NUTPLATES THEMSELVES. THIS AIRCRAFT IS OPERATED IN A TRAINING ENVIRONMENT AND IS SUBJECTED TO A LOT OF ABRUPT MANEUVERS INCLUDING SPINS. DUE TO THE SDR 0200911211Stringer · crackedDuring "H" check found cracks on LH horizontal stabilizer outboard aft skin panel integral stringers, #1-7.5 inch crack at stations XE 77.100 and stringer #4-6.25 inch crack at station EX 77.100. Repaired per EA 12-162218.SDR 2002FA0000668Bracket · crackedWHILE INSPECTING THE NUTPLATES IAW AD. WE FOUND THAT THE FORWARD UPPER WELD JOINT HAD CRACKED ADJACENT TO THE NUTPLATES THEMSELVES. THIS AIRCRAFT IS OPERATED IN A TRAINING ENVIRONMENT AND IS SUBJECTED TO A LOT OF ABRUPT MANEUVERS INCLUDING SPINS. DUE TO THESDR 0200389873Fitting · corrodedDuring shop visit in ATl, corrosion damage was found on the LH side of the the Horizontal Stabilizer fitting 59180098-507. Fitting was removed and replaced. Repaired per EA 98-185483.SDR 2002F00160Web · crackedFOUND STATION 1125 W/L 250 SUBWEB UNDER HORIZONTAL STABILIZER SUPPORT FRAME, HAS SIX CRACKS EMANATING FROM THREE LIGHTENING HOLES IN THE SUB WEB. (M)SDR C2XA02TY011Fitting · chafedTYS DURING A SCHEDULED INSPECTION THE HORIZONTAL STABILIZER LEFT HAND FAIL SAFE PIN FITTING WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR INCLUDING DYE PENETRANT INSPECTION IAW EMBRAER GST-0045/02, THE REPAIR WAS SATISFACTORY. THE AIRSDR C2XA02TY010Fitting · chafedTYS DURING A SCHEDULED INSPECTION THE HORIZONTAL STABILIZER RIGHT HAND FAIL SAFE PIN FITTING WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMBRAER GST-0045/02 WHICH INCLUDED THE DYE PENETRANT INSPECTION. THE REPAIR WAS FOUND TO BESDR MWEA020048Skin · brokenHORIZONTAL STABILIZER LOWER FORWARD SKIN RIGHT HAND SIDE AT APPROXIMATELY XHS 2 SECOND BARREL NUT BACK IS BROKE OUT -- REMOVED BOLT AND REPAIRED HOLE. REINSTALLED BOLT.SDR SWAA020054Spar · crackedDURING SCHEDULED C4 CHECK, FOUND RT HORZ STAB LOWER SURFACE AFT SPAR CRACKED APPROX 3 INCHES FROM INBD END. REPAIRED SPAR PER SRM.SDR SWAA020043Stiffener · crackedDURING SCHEDULED D CHECK, FOUND LT HORIZ STAB MAIN BOX INTERIOR L/E STIFFENER ON INTERSPAR WEB CRACKED AT STA 95. REPAIRED STIFFENER PER SRM.
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