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 Q2SA201930000046Structure · dentedDENT FOUND ON HORIZONTAL INNER FUSELAGE LOWER DECK STRUCTURE DURING LH HORIZONTAL SLIDER REMOVAL.SDR SWAA2022030105705Seal · crackedRIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / R&R RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31.SDR SWAA2019010927898Stabilizer · corrodedLT HORIZONTAL STABILIZER CORRODED BETWEEN BS 265 TO APPROXIMATELY BS 245. R&R LEADING EDGE STABILIZER PER AMM.SDR SWAA2022022429700Slider · crackedLEFT HAND HORIZONTAL STABILIZER UPPER FORWARD SLIDER SEAL CRACKED / R AND R SLIDER PER M/M REF. 53-31-31.SDR CALA2018111902401Structure · damagedL/H LOWER HORIZONTAL STABILIZER INSPAR SKIN @ STA. 101.9 REQUIRE S CUTOUT TO FACILITATE REPAIR OF INTERNAL STRUCTURE REF. FLEET C YCLE L/P9633418. FABRICATED AND INSTALLED REPAIR PER SRM 55-10-01,REPAIR 11.INITI ATED DIP TO PERFORM A DETAIL EXTERNAL VISUAL ANDSDR SWAA2022022870198Retainer · corrodedL/H HORIZONTAL STABILIZER PIVOT HINGE BUSHING IS WORN INTO BUSHING RETAINER WITH EVIDENCE OF FRETTING. REF AMM 27-41-31 FIG 402 ITEMS [1] AND [17] / FACT AS A RESULT OF POST REPAIR INSPECTION. REF. AMM 27-41-31 FIG 402 ITEMS 1 & 17. REPAIRED PER EA 1-753-33635SDR 6MXR201811050473Reinforcement · crackedSTAB HINGE BOXES DAMAGED. REPLACED BOTH STABILIZER HINGE REINFORCEMENT BOXES.SDR CA190412004Screw · broken(CAN) IN 2018, REPAIR SHOP HAS IDENTIFIED THREE (3) CASES OF BROKEN BULL GEAR SCREW FROM CRJ PLATFORM ON THE LATEST HSTA BULL-GEAR ASSEMBLY CONFIGURATION. FOLLOWING THESE FINDINGS, HAS ISSUED A DISCLOSURE LETTER SAE/2018/017-FT IN NOV 2018. IN APRIL 2019, ASDR ABXA201811263121Beam · corrodedCORROSION ON THE RIGHT HORIZONTAL STABILIZER FIXED TRAILING EDGE BEAM UPPER CHORD BETWEEN ELEVATOR STATIONS 237 AND 261. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201811213107Structure · corrodedCORROSION ON LOWER FLANGE ON RIGHT HORIZONTAL STABILIZER CHORD 17. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR SWAA2022022420295None · bulgedRIGHT STAB UPPER SKIN BULGING ABOVE TAB TRIM MECHANISM UPPER ATTACH BRACKET. STAB STA 57.9. LOCATED 62.5 INCHES AFT OF THE FWD SPAR. (MARKED) / NEW R/H STAB. WAS ORDERED OUT OF STOCK AND INSTALLED ON N/R G597708. TAG NO: 364699 PN ON: 186A2000-41 SN ON: SAIC03SDR CA180822005Splice · corroded(CAN) DURING THE 48M-72M INSPECTION CHECK, CORROSION DAMAGE WAS FOUND. (TC# 20180822005)SDR FOTR20180814007Bushing · corrodedRT STAB FORWARD LOWER SPAR JOINT LUG HAS CORROSION ON FWD. FACESDR FOTR20180814006Bushing · corrodedRH STAB. FWD. SPAR FITTING LOWER CLEVIS AFT FACE HAS CORROSION (AIRCRAFT SIDE)SDR FOTR20180814005Bushing · corrodedRIGHT STAB FORWARD SPAR FITTING LOWER, FWD, CLEVIS, FWD FACE HAD CORROSION (AIRCRAFT SIDE)SDR FOTR20180814004Bushing · corrodedRIGHT STAB FORWARD SPAR FITTING AFT, UPPER CLEVIS-AFT FACE HAS CORROSION (AIRCRAFT SIDE).SDR FOTR20180814003Bushing · corrodedRIGHT STAB FORWARD SPAR FITTING UPPER FWD. CLEVIS FACE HAS CORROSION (AIRCRAFT SIDE)SDR FOTR20180814002Bushing · corrodedRH STABILIZER, FORWARD UPPER SPAR JOINT LUG HAS CORROSION ON FWD. FACE OF BUSHINGSDR FOTR20180814001Bushing · corrodedLEFT HORIZONTAL STABILIZER FWD ATTACH LUG, UPPER BUSHING, HAD CORROSION.SDR 2019F00051Bushing · corrodedLEFT STABILIZER, CENTER SECTION FRONT SPAR UPPER AFT CLEVIS, HAS CORROSION (AIRCRAFT SIDE)SDR 2019F00050Bushing · corrodedLEFT STAB. CENTER SECTION FRONT SPAR UPPER FWD CLEVIS HAS CORROSION (AIRCRAFT SIDE)SDR 2019F00049Bushing · corrodedLEFT HORIZONTAL STABILIZER, FWD. ATTACH LUG, LOWER BUSHING HAS CORROSION (STABILIZER SIDE)SDR 2019F00048Bushing · corrodedLH STAB. FORWARD SPAR FITTING, FWD FACE OF LOWER CLEVIS, HAS CORROSION (AIRCRAFT SIDE)SDR SWAA2019082636210Support · crackedR/H HORIZONTAL STABILIZER #4 BALANCE BAY PANEL, BALANCE PANEL SUPPORT INBOARD CORNER CRACKED. R&R SUPPORT IAW SRM AND DWG.SDR IPXA2018092734447Structure · crackedCRACKS WERE FOUND ON THE LT HORIZONTAL STABILIZER TRAILING EDGE AT HSS BL 421.5. REPAIRED IAW SRID 3-4281233668, AND EO B747-5510-69998-A.SDR 2018FA0000435Hinge · corrodedDURING PREFLIGHT A SECTION OF STAB (R) INBOARD HINGE WAS MISSING DUE TO HEAVY CORROSION. ALL OTHER HINGES WERE INSPECTED AND NO DEFECTS NOTED. SEE ATTACHED PHOTO. WE ARE STARTING TO SEE A TREND WITH CORROSION ON ALUMINUM ON LATE MODEL AIRCRAFT AND RE-PLACEMSDR ASOA201809107152Spherical Bearin · wornHORIZONTAL STABILIZER BACKLASH FAILED (LEFT HAND SIDE). INSTALLED SPHERICAL BEARING INTO VERTICAL STABILIZER, LEFT HAND SIDE, IN ACCORDANCE WITH AMM 55-37-00.SDR 2018FA0000279Lug · corrodedRIGHT STAB AFT CENTER SPAR JOINT LUG HAS CORROSION ON FWD FACESDR 2018FA0000278Clevis · corrodedRIGHT STAB AFT SPAR FITTING FWD CENTER CLEVIS FWD FACE HAD CORROSIONSDR 2018FA0000277Clevis · corrodedRT STAB AFT SPAR FITTING AFT CENTER CLEVIS AFT FACE HAS CORROSION.SDR 2018FA0000276Clevis · corrodedLEFT STAB REAR SPAR UPPER FWD CLEVIS HAS CORROSION (AIRCRAFT SIDE)SDR 2018FA0000275Lug · corrodedLEFT HORIZONTAL STABILIZER AFT ATTACH LUG UPPER BUSHING AFT FACE HAS CORROSION.SDR 2018FA0000274Clevis · corrodedLEFT STABILIZER REAR SPAR UPPER AFT CLEVIS HAS CORROSION.SDR 2018FA0000273Clevis · corrodedLEFT STAB. REAR SPAR FWD LOWER CLEVIS HAD CORROSION.SDR 2018FA0000272Clevis · corrodedLEFT STABILIZER AFT SPAR FITTING LOWER CLEVIS HAS CORROSION.SDR 2018FA0000271Bushing · corrodedLEFT HORIZONTAL STABILIZER AFT ATTACH LUG LOWER BUSHING AFT FACE HAD CORROSION, STAB SIDE.SDR AALA201807129019Hinge Arm · excess playTHE AIRCRAFT IS IN BASE MAINTENANCE. RIGHT HAND HORIZONTAL STABILIZER ELEVATOR HINGE ARM NR 6 HAS EXCESSIVE PLAY. REPLACED NR 6 HINGE ARM PER AMM 55-16-42-400-001-A.SDR AALA201807119004Hinge Arm · excess playTHE AIRCRAFT IS IN BASE MAINTENANCE. EXCESSIVE PLAY FOUND ON NR 6 HINGE ARM ON RIGHT HAND HORIZONTAL STABILIZER. REPLACED NR 6 HINGE ARM PER AMM 55-16-42-400-001-A.SDR VNAA2018062599905Fitting · crackedHORIZONTAL STABILIZER ANTI-ROTATION FITTING WAS CRACKED. INSTALLED A NEW ANTI-ROTATION FITTING IAW SB 601R-55-007.SDR AALA201806279003Hinge Fitting · wornEXCESSIVE PLAY ON HINGE ARM END FITTING ON THE RIGHT HORIZONTAL STABILIZER, BETWEEN HSS 1305 AND 1809, RIB 5. REPLACED HINGE ARM END FITTING IAW AMM 55-16-42-400-001-A.SDR ASOA201806077104Bushing · migratedRIGHT HORIZONTAL STAB HINGE INBD LUG BUSHING MIGRATED. REPAIRED IAW SRM 55-10-02.SDR ASOA201806077103Bushing · migratedLEFT HORIZONTAL STAB HINGE OTBD LUG BUSHING MIGRATED. REPAIRED IAW SRM 55-10-02.SDR ASOA201806077102Bushing · migratedRIGHT HORIZONTAL STAB HINGE OTBD LUG BUSHING MIGRATED. REPAIRED IAW SRM 55-10-02.SDR ASOA201806077101Bushing · migratedLEFT HORIZONTAL STAB HINGE, INBD LUG BUSHING MIGRATED. REPAIRED IAW SRM 55-10-02.SDR CALA2018060601424Fitting · crackedLEFT ELEVATOR OTBD ACTUATOR FITTING, ONE CRACK WAS FOUND, APPROXIMATELY 7/16 INCH IN LENGTH.SDR ASOA2018060217097Lug · displacedRIGHT OTBD HORIZONTAL HINGE MOUNT LUG HAS DISPLACED METAL. REPAIRED IAW SRM 55-10-02.SDR ASOA2018060217096Lug · displacedLEFT INBD HORIZONTAL HINGE MOUNT LUG HAD DISPLACED METAL. REPAIRED IAW SRM 55-10-02.SDR AALA201805295011Servo Valve · faultedCLIMBING 15,000 FEET AT 310 KNOTS, FELT A CONSTANT AIRFRAME VIBRATION. CONTINUED TO CLIMB TO 24,000 FEET WITH NO CHANGE. THEN SLOWED TO 280 KNOTS WITH STILL NO CHANGE. VIBRATION FELT LIKE LATERAL MOTION, SIDE TO SIDE. ACCOMPLISHED TSM 27-20-00-810-802-A, FOSDR SWAA2022021648025Seal · tornR/H STAB LOWER FWD SLIDER TORN/DEFORMED / REMOVED AND REPLACED R/H STAB LOWER FWD SLIDER PER MM 53-31-31SDR CA180423020Channel · cracked(CAN) DURING A SCHEDULED INSPECTION, THE HORIZONTAL CHANNEL PN C2FS535-5 ATTACHED THE 228 BULKHEAD WAS FOUND CRACKED AT THE RUDDER STOP ATTACHMENT BOLT HOLES. THE CHANNEL WAS REPLACED TO RECTIFY THE DEFECT. PART TOTAL TIME WAS 25, 344.9 HRS. ALL WORK WAS PE
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