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.

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 3RDFeb 12, 2020SDR 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 3RDFeb 12, 2020SDR 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 Dec 6, 2019 · N204NN · Emb ERJ170200LRSDR 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 RJun 20, 2019 · N233SW · Emb EMB120ERSDR 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 FRJun 20, 2019 · N233SW · Emb EMB120ERSDR JJBA201906031022Panel · damagedUPON REMOVAL OF EROSION TAPE FOUND COMPOSITE DAMAGE ON PANEL 333DL. REPAIRED COMPOSITE DAMAGE AND RESTORED SURFACE PROTECTION ON PANEL 333DL.May 31, 2019 · N27190 · Emb EMB145XRSDR 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.Apr 1, 2019 · N961SW · Cndair CL6002B19SDR 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.Mar 29, 2019 · N961SW · Cndair CL6002B19SDR 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.Nov 6, 2018 · N769US · Airbus A319112SDR 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.Aug 28, 2018 · N260SW · Boeing 7377H4SDR 2019F00047Bushing · corrodedLEFT LOWER AFT, FWD. STAB CLEVIS HAS CORROSION AROUND BUSHINGAug 14, 2018 · N480VX · Boeing 73748ESDR 2018FA0000285Clevis · corrodedRT STAB AFT SPAR FITTING AFT LOWER CLEVIS FACE HAS CORROSION.Jul 24, 2018 · Boeing 737400SDR 2018FA0000284Lug · corrodedRT STAB AFT LOWER SPAR JOINT LUG HAS CORROSION ON FWD FACE.Jul 24, 2018 · Boeing 737400SDR 2018FA0000282Clevis · corrodedRIGHT STAB AFT FITTING FWD LOWER CLEVIS FWD FACE HAD CORROSION.Jul 24, 2018 · Boeing 737400SDR 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.Jan 4, 2018 · N139UP · Airbus A300F4622RSDR 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.Nov 22, 2017 · N995AT · Boeing 717200SDR 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.Oct 14, 2017 · N981AT · Boeing 717200SDR EPUA20170810001Bulkhead · crackedDURING SCHEDULED INSPECTION, NOTE THAT BULKHEAD WAS CRACKED. REPLACED THE BULKHEAD.Aug 11, 2017 · N734OU · Cessna 207ASDR DALA2017062405009Support Bracket · corrodedDURING INSPECTION, FOUND STAB TORSION BOX MAIN SUPPORT BRACKET HAD SIGNS OF CORROSION. MAINTENANCE COMPLIED WITH ER/A 559757-14 REV. A.Jun 23, 2017 · N3738B · Boeing 737832SDR JGVR20170531001Strake · corrodedLT AND RT STRAKES WERE CORRODED, BEYOND LIMITS OF SRM. REPLACED BOTH STRAKES.May 31, 2017 · N669QS · Cessna 560XLSDR SWIA201642492Structure · dented2 DENTS JUST BELOW APU OIL COOLER INLET. REPAIRED IAW SRM.Aug 3, 2016 · N948SW · Cndair CL6002B19SDR SWIA201642403Panel · defectiveRIGHT LOWER STABILIZER VISOR PANEL FAILED GAP CHECK. RIGHT LOWER VISOR PANEL REPLACED.Jul 6, 2016 · N863AS · Cndair CL6002B19SDR SWIA201642402Panel · defectiveRIGHT UPPER STABILIZER VISOR PANEL FAILED GAP CHECK. RT UPPER VISOR PANEL REPLACED. GAP CHECK GOOD.Jul 6, 2016 · N863AS · Cndair CL6002B19SDR SWIA201642401Panel · defectiveLEFT LOWER STABILIZER VISOR PANEL FAILED GAP CHECK. LT LOWER VISOR PANEL REPLACED. GAP CHECK GOOD IAW AMM.Jul 6, 2016 · N863AS · Cndair CL6002B19SDR COEA2016043011908Panel · corrodedDURING HEAVY CHECK, PANEL 323AL LE INNER SURFACE HAS AREAS OF CORROSION ON THE 2ND FROM BOTTOM RIB. REPLACED PANEL WITH OEM PART.Apr 30, 2016 · N908FX · Aerosp ATR42300SDR COEA2016043010908Panel · corrodedDURING HEAVY CHECK, PANEL 323AL LE INNER SURFACE HAS AREAS OF CORROSION ON THE BOTTOM RIB. REPLACE PANEL WITH OEM PART.Apr 30, 2016 · N908FX · Aerosp ATR42300SDR 2016FA0000115Rib · damaged2 ASYMMETRICAL HOLES IN BOTTOM RUDDER RIB. FWD HOLE 1.5X1" AFT HOLE 1.375 X .875". 2 HOLES CONNECTED BY A CRACK.Mar 5, 2016 · N369QS · Cessna 680CESDR 7C7A201602135Structure · damagedTWO DENTS & SCRATCHES BEYOND MFG SRM LIMITS.Feb 13, 2016 · N880EA · Dhav DHC8106SDR DALA2015091605668Structure · crackedAFT LT EMPENNAGE, JUST ABOVE NR 1 PYLON. PACK EXIT FLANGE IS CRACKED. REPAIRED IAW ERA 539229-14, REV ORIGINAL.Sep 15, 2015 · N955DL · Doug MD88SDR 9EKA2015060322Structure · crackedFOUND CRACKED STABILIZER AT INBD LOCATION. CRACK IS 2 INCHES IN LENGTH, CRACKED THROUGH MATERIAL.May 29, 2015 · N216VA · Snias AS332LSDR DALA1503050978Structure · unknownVERTICAL STAB FRONT SPAR AND SKINS REPAIRED IAW AA 5530-01045.Mar 4, 2015 · N978DL · Doug MD88SDR FDEA201501200450Structure · unknownSTABILIZER LT UPPER SPAR CAP & SKIN REPAIR. SHORING COMPLY WITH EA 8-5510-T0315116 REV NR A POS P1.Jan 20, 2015 · N396FE · Doug MD1010FSDR 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.Oct 7, 2014 · N533AS · Boeing 737890SDR 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.Oct 7, 2014 · N533AS · Boeing 737890SDR 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.Jul 22, 2014 · N968DL · Doug MD88SDR DALA14036489253Unknown · crackedCRACK REPAIRED IAW ERA 526678-14, SECTION I. COMPLIED WITH ERA 526678-14, SECTION II.Jun 13, 2014 · N953DN · Doug MD9030SDR COEA2014031111908Attach Angle · corrodedATTACH ANGLE FOR PANEL 325DL HAS LEVEL 2 CORROSION. REPLACED WITH OEM.Feb 14, 2014 · N908FX · Aerosp ATR42300SDR IXXA20141020024Stringer · corrodedCORROSION ON STRINGER 7 BETWEEN RIB 1L & 1R OUT OF LIMITS. REPAIRED IAW REQUEST FOR ENGINEERING ASSISTANCE DOCUMENT 47089REA02.Jan 3, 2014 · N763CX · Boeing 767232SDR 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.Oct 22, 2013 · N920DN · Doug MD9030SDR 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.Oct 18, 2013 · N920DN · Doug MD9030SDR 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.Sep 19, 2013 · N822MD · Emb ERJ170100SUSDR 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 SCREWJun 13, 2013 · N379DB · Cessna 525BSDR DALA1312393750Skin · crackedRT STABILIZER LOWER SURFACE SKIN CRACKED AT STAB STA 138.7 9" FROM AFT SPAR. REPAIRED IAW SRM 55-10-01, REPAIR 11.May 7, 2013 · N3750D · Boeing 737832SDR 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.Mar 28, 2013 · N413 · Cndair CL6002B19SDR SWAA2012121210557Seal · crackedLEFT LOWER STAB SLIDER SEAL IS CRACKED. REMOVED AND REPLACED PER AMM.Dec 10, 2012 · N771SA · Boeing 7377H4SDR AALA20121031023Spar Cap · crackedCRACK INDICATION IN SPAR CAP, NUMBER 1 HOLE BELOW 52.267, LEFT SIDE. INSTALLED DOUBLER/TRIPLER PER EA MD80-55-026866.Oct 31, 2012 · N16545 · Doug DC982SDR 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.Oct 30, 2012 · N801TJ · Boeing 7374B7SDR DALA1514290987Lug · not reportedHORIZONTAL STABILIZER HINGE RIB PIVOT BEARING LUG REPAIRED IAW AA 5500-01011.Sep 24, 2012 · N987DL · Doug MD88SDR 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.Sep 4, 2012 · Beech A100SDR 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.Jul 24, 2012 · N7543A · Doug DC982
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