JASC 5500
Service difficulty reports · 490
Reports filed under 5500 · Empennage 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 = '5500' 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 = '5500' 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 2020FA0000142Aneroid · mismanufacturedWE HAVE ORDERED 4 NEW PARTS FROM VARIOUS VENDORS AND WITH VARIOUS ORIGIN 8130-3S THAT ALL ARE NOT MEETING MANUFACTURER`S SPEC. THERE PARTS WERE ALL ORDERED BTW 10/5/18 AND 10/20/18. WE HAVE HAD THE PARTS IN QUESTION TESTED BY TWO INDEPENDENT VENDORS AS A 3RDSDR 2020FA0000141Aneroid · mismanufacturedWE HAVE ORDERED 4 NEW PARTS FROM VARIOUS VENDORS AND WITH VARIOUS ORIGIN 8130-3S THAT ALL ARE NOT MEETING MANUFACTURER`S SPEC. THERE PARTS WERE ALL ORDERED BTW 10/5/18 AND 10/20/18. WE HAVE HAD THE PARTS IN QUESTION TESTED BY TWO INDEPENDENT VENDORS AS A 3RDSDR C77A202002190008Support · damagedDURING BASIC CHECK AT EAMS TOOLING DAMAGE WAS SUSTAINED ON THE #3 HINGE FITTING SUPPORT P/N 170-62826-410. REFERENCE ETD2019-170-158838, FIGURE 1 FOR THE DAMAGE LOCATIONS AND DETAILS. EAMS REQUESTED AND RECEIVED RELIEF IN THE FORM OF ETD2019-170-158838, WHICH SDR HKGA201906260025Rib · chafedRIB FLANGE CHAFED AND CORRODED. REMOVED CORROSION AND CHAFFING IAW CPM 51-14-00 REV DATE 6/30/17. MATCH DRILLED NEW LEADING EDGE RIB FLANGE IAW SBM 51-5-00 REV 58. INSTALLED THE RIB FLANGE IAW SRM 51-40-02 REV 58. APPLIED PRIMER AND TOP COAT IAW CPM 512106 RSDR HKGA201906250019Doubler · corrodedDOUBLER CORROED. MATCH DRILLED REPAIR PARTS IAW SRM 51-70-04, AND 51-40-02, REV 58. INSTALLED DOUBLER AND FILLER IAW STEP 2 OF ETD 2019-120-055992 AND SRM 51-40-02, REV 58. REMOVED REPAIRED DOUBLER IAW SRM 51-40-02, REV 58, CONFIRMED AFFECTED AREA CRACK FRSDR JJBA201906031022Panel · damagedUPON REMOVAL OF EROSION TAPE FOUND COMPOSITE DAMAGE ON PANEL 333DL. REPAIRED COMPOSITE DAMAGE AND RESTORED SURFACE PROTECTION ON PANEL 333DL.SDR SWIA2019050845857Skin · chafedRIGHT HAND SIDE AFT EXTERIOR SKIN HAS CHAFING AND CORROSION WHERE APU EXHAUST SHEILD ATTACHES TO AIRCRAFT. (C-CHECK) RO: 05/07/2019 BLENDED CHAFING AND CORROSION WHERE APU EXHAUST SHEILD ATTACHES TO AIRCRAFT IAW SRM AND REO.SDR SWIA2019050845859Fairing · damagedFAIRING 326CL IS CHAFED/GOUGED WHERE IT INTERFACES WITH THE VISOR PANEL. (C-CHECK) RO: 05/07/2019 REMOVED DAMAGE ON PANEL 326CL AND COMPLIED WITH ALL STEPS OF REO.SDR AALA2018121049012Hinge Fitting · excess playEXCESSIVE PLAY FOUND ON THE HINGE FITTING. REPLACED THE HINGE FITTING IAW SRM 51-72-11, AND AMM 55-36-41-400-001-A.SDR SWAA2022021818936Mount · corrodedRUDDER WEIGHT CORRODED AND HAS EXCESSIVE GAP BETWEEN MATING SURFACE. / REMOVED RUDDER BALANCE WEIGHT;FOUND MATING SURFACE ON MOUNT ARM TO HAVE EXCESSIVE CORROSION.RUDDER TO BE REPLACED ON WORK CARD #G588896.SDR 2019F00047Bushing · corrodedLEFT LOWER AFT, FWD. STAB CLEVIS HAS CORROSION AROUND BUSHINGSDR 2018FA0000285Clevis · corrodedRT STAB AFT SPAR FITTING AFT LOWER CLEVIS FACE HAS CORROSION.SDR 2018FA0000284Lug · corrodedRT STAB AFT LOWER SPAR JOINT LUG HAS CORROSION ON FWD FACE.SDR 2018FA0000282Clevis · corrodedRIGHT STAB AFT FITTING FWD LOWER CLEVIS FWD FACE HAD CORROSION.SDR IPXA2018012625897Rod · crackedINSPECTION TYPE: C-1, LOWER LEFT SUPPORT STRUT HAS A CRACK AT THE BOTTOM END, MEASURING .388" IN LENGTH. REMOVED AND REPLACED ROD ASSY IAW AMM 53-10-47.SDR DALA2017112208316Structure · corrodedCORROSION ON BARREL NUTS WAS FOUND. THE BARREL NUT HOLES WERE REPAIRED IAW ETI-17-17-231, REV 5, AND ER/A 562391-14, REV ORIG. BOLTS AND NUTS WERE REPLACED IAW AMM 20-20-22.SDR DALA2017101507511Structure · corrodedAFTER A CORRODED NUT WAS REMOVED, CORROSION AND SCRATCHES AT BORES WERE FOUND. BORE OF BARREL NUT NR 27 WAS REPAIRED IAW ETI-17-17-190, REV 1, AND ER/A 562336-14, REV ORIGINAL.SDR EPUA20170810001Bulkhead · crackedDURING SCHEDULED INSPECTION, NOTE THAT BULKHEAD WAS CRACKED. REPLACED THE BULKHEAD.SDR DALA2017062405009Support Bracket · corrodedDURING INSPECTION, FOUND STAB TORSION BOX MAIN SUPPORT BRACKET HAD SIGNS OF CORROSION. MAINTENANCE COMPLIED WITH ER/A 559757-14 REV. A.SDR JGVR20170531001Strake · corrodedLT AND RT STRAKES WERE CORRODED, BEYOND LIMITS OF SRM. REPLACED BOTH STRAKES.SDR SWIA201642492Structure · dented2 DENTS JUST BELOW APU OIL COOLER INLET. REPAIRED IAW SRM.SDR SWIA201642403Panel · defectiveRIGHT LOWER STABILIZER VISOR PANEL FAILED GAP CHECK. RIGHT LOWER VISOR PANEL REPLACED.SDR SWIA201642402Panel · defectiveRIGHT UPPER STABILIZER VISOR PANEL FAILED GAP CHECK. RT UPPER VISOR PANEL REPLACED. GAP CHECK GOOD.SDR SWIA201642401Panel · defectiveLEFT LOWER STABILIZER VISOR PANEL FAILED GAP CHECK. LT LOWER VISOR PANEL REPLACED. GAP CHECK GOOD IAW AMM.SDR COEA2016043011908Panel · corrodedDURING HEAVY CHECK, PANEL 323AL LE INNER SURFACE HAS AREAS OF CORROSION ON THE 2ND FROM BOTTOM RIB. REPLACED PANEL WITH OEM PART.SDR COEA2016043010908Panel · corrodedDURING HEAVY CHECK, PANEL 323AL LE INNER SURFACE HAS AREAS OF CORROSION ON THE BOTTOM RIB. REPLACE PANEL WITH OEM PART.SDR 2016FA0000115Rib · damaged2 ASYMMETRICAL HOLES IN BOTTOM RUDDER RIB. FWD HOLE 1.5X1" AFT HOLE 1.375 X .875". 2 HOLES CONNECTED BY A CRACK.SDR 7C7A201602135Structure · damagedTWO DENTS & SCRATCHES BEYOND MFG SRM LIMITS.SDR DALA2015091605668Structure · crackedAFT LT EMPENNAGE, JUST ABOVE NR 1 PYLON. PACK EXIT FLANGE IS CRACKED. REPAIRED IAW ERA 539229-14, REV ORIGINAL.SDR 9EKA2015060322Structure · crackedFOUND CRACKED STABILIZER AT INBD LOCATION. CRACK IS 2 INCHES IN LENGTH, CRACKED THROUGH MATERIAL.SDR DALA1503050978Structure · unknownVERTICAL STAB FRONT SPAR AND SKINS REPAIRED IAW AA 5530-01045.SDR FDEA201501200450Structure · unknownSTABILIZER LT UPPER SPAR CAP & SKIN REPAIR. SHORING COMPLY WITH EA 8-5510-T0315116 REV NR A POS P1.SDR ASAA2014100709366Skin · crackedCRACK INDICATION FOUND RT STABILIZER LOWER SKIN STA 138.70,16' FWD OF AFT SPAR. MARKED .830' LONG AT INBD LOCATION. ACFT GROUNDED. REPAIRED RT LWR STAB SKIN STA 138.70 IAW SRM 55-10-01-28-11. REMOVED AND REINSTALLED PANELS 341B AND 345B IAW AMM 27-41-21.SDR ASAA2014100709365Skin · crackedCRACK INDICATION FOUND LT LOWER STAB SKIN STA 138.70,16' FWD OF AFT SPAR MARKED .670' LONG. ACFT GROUNDED. REPAIRED LT LWR STAB SKIN STA IAW SRM 55-10-01-2R-11. REMOVED AND REINSTALLED PANELS 331B AND 335A IAW AMM 27-41-21. STAB STA 138.7 LT.SDR DALA2014072704231Structure · corrodedCORROSION ON HORIZONTAL STABILIZER LT/RT HINGES PLATES INNER SURFACES AT VERTICAL STABILIZER. CORROSION WAS REMOVED IAW SRM 51-10-3, SRM 55-02, FIG 28, SRM 51-10-3, PAR. 14.SDR DALA14036489253Unknown · crackedCRACK REPAIRED IAW ERA 526678-14, SECTION I. COMPLIED WITH ERA 526678-14, SECTION II.SDR COEA2014031111908Attach Angle · corrodedATTACH ANGLE FOR PANEL 325DL HAS LEVEL 2 CORROSION. REPLACED WITH OEM.SDR IXXA20141020024Stringer · corrodedCORROSION ON STRINGER 7 BETWEEN RIB 1L & 1R OUT OF LIMITS. REPAIRED IAW REQUEST FOR ENGINEERING ASSISTANCE DOCUMENT 47089REA02.SDR DALA13054549220Structure · corrodedUPPER AFT HOLE ON CENTER SECTION, RT SIDE, CORRODED. OPENED HOLE. REMOVED CORROSION. NO CRACKS FOUND. FABRICATED AND INSTALLED BUSHING IAW PRI 519682-14, REV 4.SDR DALA13053559220Fitting · damagedDAMAGE AT UPPER AFT HOLE ON CENTER SECTION FITTING. REAMED AND REMOVED DAMAGE IAW SRM 55-10-03 HFEC. INSTALLED BUSHING. REPAIR COMPLETE IAW ERA 519682-14.SDR R61A201309190952Rib · crackedDURING HEAVY CHECK, RT L/E RIB CRACKED. MX CUT OUT DAMAGED AREA OF RIB AND FABRICATED REPAIR ANGLE IAW ETD 2013 170-041433, INSTALLED REPAIR ANGLE IAW ETD 2013-170-041433.SDR 2013F00132Screw · damagedDUAL AHRS FAILURE DURING CRUISE. MADE AN EMERGENCY DESCENT. AFTER TESTING, FOUND NO PROBLEM WITH AHRS BOXES. ON FURTHER INVESTIGATION, ORIGINAL SCREWS THAT HOLD THE INSPECTION PANEL TO THE FLUX VALVES BECAME MAGNETIZED. MFG RECOMMENDED INSTALLING NEW SCREWSDR DALA1312393750Skin · crackedRT STABILIZER LOWER SURFACE SKIN CRACKED AT STAB STA 138.7 9" FROM AFT SPAR. REPAIRED IAW SRM 55-10-01, REPAIR 11.SDR A6WA201304024893Skin · damagedC/W AWAC CARD 4DMI16663 REPAIR LEFT STAB LWR SKIN. REMOVED AND RE-INSTALLED NEW SERVICEABLE RIVET IAW CRJ 200 SRM 51-42-06.SDR SWAA2012121210557Seal · crackedLEFT LOWER STAB SLIDER SEAL IS CRACKED. REMOVED AND REPLACED PER AMM.SDR AALA20121031023Spar Cap · crackedCRACK INDICATION IN SPAR CAP, NUMBER 1 HOLE BELOW 52.267, LEFT SIDE. INSTALLED DOUBLER/TRIPLER PER EA MD80-55-026866.SDR EB1R20121030002Nut · looseDURING C-CHECK, FOUND THE NUT, WASHER AND COTTER PIN MISSING ON THE AFT UPPER THRUST LINK BOLT (BOLT WAS IN PLACE BUT LOOSE). INSPECTED THE SURROUNDING AREAS AND NO OTHER DEFECTS NOTED. INSTALLED THE WASHER, NUT AND COTTER PIN IAW MM 55-10-10.SDR DALA1514290987Lug · not reportedHORIZONTAL STABILIZER HINGE RIB PIVOT BEARING LUG REPAIRED IAW AA 5500-01011.SDR CA120904011Screw · wrong part(CAN) IMPROPER LENGTH OF SCREW WAS USED TO ATTACH, PN 115-440029-601, TAIL CONE ASSY CAUSING THE HORIZONTAL STABILIZER. HINGE BRACKET, PN 115-440031-4 TO BE DAMAGED BEYOND REPAIRABLE LIMITS.SDR AALA20120724015Skin Panel · damagedDUE TO NUMBER ON HOLES FOUND ON INSPECTION, DOUBLER IS REQUIRED ON UPPER LEADING EDGE PER SRM 55-03-00 FIGURE 29. INSTALLED REPAIR DOUBLER TO UPPER LEADING EDGE PANEL PER SRM 55-03-00 AND SRM 51-60-00.
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