JASC 5342
Service difficulty reports · 578
Reports filed under 5342 · Fuselage, 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 = '5342' 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 = '5342' 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 SWIA2020031049194Drag Angle · crackedLH FWD VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED. (C-CHECK) RO 3/6/2020 REMOVED DAMAGED ANGLE AND FILLER REF CRJ-900 SRM FABRICATED NEW PICES REF CRJ-900 SRM INSTALLED NEW FABRICATED PARTS REF CRJ-900 SRM RESTORED FINISH TO INSTALLED PARTS CRJ-SDR SWIA2020031049192Drag Angle · crackedRH AFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED. (C-CHECK) RO 3/6/2020 REMOVED DAMAGED ANGLE AND FILLER REF CRJ-900 SRM. FABRICATED NEW PICES REF CRJ-900 SRM. INSTALLED NEW FABRICATED PARTS REF CRJ-900 SRM RESTORED FINISH TO INSTALLED PARTS CRSDR SWIA2020031049191Drag Angle · crackedLH AFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED. (C-CHECK) RO 3/6/2020 REMOVED DAMAGED ANGLE AND FILLER REF CRJ-900 SRM FABRICATED NEW PICES REF CRJ-900 SRM INSTALLED NEW FABRICATED PARTS REF CRJ-900 SRM RESTORED FINISH TO INSTALLED PARTS CRJ-SDR VNAA2020012299902Drag Angle · crackedRH AFT FUSELAGE TO VERTICAL STAB DRAG ANGLE CRACKED. REMOVED RT AFT FUSELAGE TO VERTICAL STAB CRACKED DRAG ANGLE IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01. LOCATED AND DRILLED NEW SERVICABLE RT AFT FUSELAGE TO VERTICAL STAB SDR SIMA20200118003Drag Angle · crackedLEFT AFT VERT STAB TO FUSELAGE DRAG ANGLE HAS A 1" CRACK ON LEADING EDGE.-C/A-REPAIRED LEFT DRAG ANGLE IAW 55-31-00-201-001-A01SDR VNAA2019121299902Drag Angle · crackedLEFT VERTICAL STAB DRAG ANGLE CRACKED. L/H VERTICAL STAB DRAG ANGLE REQUIRES REPAIR IAW CRJ900 SRM 55-31-00-201-001-A01. UPON FURTHER INVESTIGATION, FOUND LH AFT DRAG ANGLE TO REQUIRE REPLACEMENT IAW CRJ900 SRM 55-31-00-201-001-A01. REMOVED LH AFT DRAG ANGLESDR VNAA2019121299901Drag Angle · crackedRIGHT VERTICAL STAB DRAG ANGLE CRACKED. R/H VERTICAL STAB DRAG ANGLE REQUIRES REPAIR IAW CRJ900 SRM 55-31-00-201-001-A01. UPON FURTHER INVESTIGATION, FOUND RH AFT DRAG ANGLE TO REQUIRE REPLACEMENT IAW CRJ900 SRM 55-31-00-201-001-A01. REMOVED RH AFT DRAG ANGSDR SIMA2019102415002Drag Angle · crackedRIGHT SIDE, VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE HAS A 1 1/2" CRACK ALONG LEADING EDGE.-C/A-REPAIRED IAW SRM 55-31-00-995-801SDR SIMA2019102415001Drag Angle · crackedLEFT SIDE, VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE HAS A 1 1/2" CRACK ALONG LEADING EDGE.-C/A-REPAIRED IAW SRM 55-31-00-995-801SDR SWAA2022031183705Attach Fitting · out of toleranceAFT BULKHEAD VERTICAL FIN ATTACHMENT FITTING HOLE OUT OF LIMITS MEASURES .384' AT 5L STR 2L / REAMED HOLE 5L AT STR 2L TO A HOLE DIAMETER OF 0.4067' AND INSTALLED BOLT IAW SI#12107-53SDR SWAA2022031183706Attach Fitting · out of toleranceAFT BULKHEAD VERTICAL FIN ATTACHMENT FITTING HOLE OUT OF LIMITS MEASURES .384' AT 6L STR 2L / REAMED HOLE 6L AT STR 2L TO A HOLE DIAMETER OF 0.4067' AND INSTALLED BOLT IAW SI#12107-53SDR A6WA201904196566Angle · crackedRH OVER WING BL 45 FS 473 REINFORCING ANGLE CRACKED. REPLACEDSDR V0XD201811240004Drag Angle · crackedRT, AFT FUSELAGE TO VERTICAL DRAG ANGLE HAS SIGNS OF CRACKING AT FS 1200. REPAIRED RT AFT FUSELAGE TO VERTICAL DRAG ANGLE AT FS 1200 IAW REO 670-55-31-018, REV A, 2016-11-10.SDR V0XD201811240003Drag Angle · crackedLT FWD FUSELAGE TO VERTICAL DRAG ANGLE HAS SIGNS OF CRACKING AT FS 1200. REPAIRED LT FWD FUSELAGE TO VERTICAL DRAG ANGLE AT FS 1200 IAW REO 670-55-31-018, REV A, 2016-11-10 AND REO 670-55-31-098, 2017-06-28.SDR U2RA201809270001Doubler · crackedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2651 REVISION 1 STATION 2403.6 TO STATION 2524.4, UPPER LOBE DOUBLER AT THE FUSELAGE VERTICAL STABILIZER ATTACH FITTINGS INSPECTION, A 2 INCH CRACK WAS DISCOVERED ON THE RIGHT HAND SIDE, FROM STATION 2519 TO 252SDR 2A6R08232018Attach Fitting · crackedTO COMPLETE INSPECTIONS OF THE TAIL BOOM AND HORIZONTAL STAB ASSEMBLY. THE HORIZONTAL WAS REMOVED AND IT WAS THEN FOUND DURING A VISUAL INSPECTION OF THE ATTACHMENT FITTINGS THAT THE UPPER LEFT HAND HAD CRACKED COMPLETELY IN HALF.SDR SIMA20180819009Drag Angle · crackedRIGHT FWD VERTICAL STAB TO FUSELAGE DRAG ANGLE WAS CRACKED AT THE AFT END FASTENER. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-40-02.SDR EE4Y2018070906892Attach Angle · crackedDURING THE CURRENT MAINTENANCE PROCESS IT WAS FOUND AT THE EMPENNAGE, VERTICAL STABILIZER TO FUSELAGE LEFT ATTACHMENT SUPPORT ANGLE CRACKED AT THE BS 1121 FIN WL 0.0. DUE TO THIS SITUATION THE AFFECTED SUPPORT ANGLE WAS REPAIRED AS PER SRM 53-80-71 REPAIR 1, FSDR DALA2018060603846Attach Angle · crackedCRACK IN THE LT & RT INTERNAL VERTICAL STABILIZER ATTACH ANGLES BS 1458 TO 1486. REPLACED THE ATTACH ANGLES IAW SRM 51-30-02, VOL II, AND 51-30-05.SDR ASAA2018051624957Lug · corrodedLEFT HORIZONTAL STAB AFT ATTACH FITTING, LOWER LUG STAB SIDE, AFT SIDE HAS EVIDENCE OF CORROSION. ACFT GROUNDED. REPAIRED THE ATTACH FITTING LOWER LUG IAW EA EA 20332.SDR DALA2017100707362Skin · dentedDENT ON THE LT SIDE NEAR THE T/E OF THE RUDDER. THE RUDDER WAS REPAIRED IAW SRM 51-70-13-2R-1 PAR 4B.SDR DALA2017072405709Attach Angle · crackedLEFT HAND VERTICAL STABILIZER ATTACH ANGLE CRACKED. REPLACED ANGLE IAW SRM 51-30-02 AND 51-30-05.SDR ASOA201707221798Drag Angle · crackedRT VERTICAL TO FUSELAGE DRAG ANGLE HAS A CRACK. REMOVED AND REPLACED DRAG ANGLE P/N AV670-71186-003 IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, AND DRAWING BA670-30100.SDR ASOA201707221797Drag Angle · crackedLT VERTICAL TO FUSELAGE DRAG ANGLE HAS A CRACK. REMOVED AND REPLACED DRAG ANGLE P/N AV670-71186-003 IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, AND DRAWING BA670-30100.SDR AALA20170710005Attach Fitting · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON VERTICAL STABILIZER FORWARD SPAR ATTACHMENT CLEVIS FITTING AT LBL11.55, AFT FACE OF AFT LUG. REPAIRED PER EA 271389.SDR SWAA2017072715288Fitting · corrodedLEFT OTBD AFT VERTICAL STABILIZER ATTACH LUG FORWARD AND AFT BOLT HOLES CORRODED AT BS 1088. R & R FITTING IAW SRM AND DWG.SDR DALA2017070205147Attach Angle · crackedVERTICAL STABILIZER RIGHT HAND INTERNAL ATTACH ANGLE CRACKED. REMOVED AND REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 5912188.SDR DALA2017070205146Attach Angle · crackedVERTICAL STABILIZER LEFT HAND INTERNAL ATTACH CRACKED. REMOVED AND REPLACED VERTICAL STABILIZER LEFT HAND INTERNAL ATTACH ANGLE IAW SRM 51-30-02, 51-30-05 AND DWG 5912188.SDR DALA2017061304811Angle · crackedCRACKED LEFT DORSAL FIN JOINT ANGLE BS 1460. REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 5912188.SDR WVER2017021051213Drag Angle · crackedDURING SCHEDULED HEAVY MAINT CHECK, DISCOVERED BOTH THE LEFT HAND AND RIGHT HAND VERTICAL STAB FORWARD ATTACH ANGLES TO BE CRACKED. REPLACED BOTH LEFT HAND AND RIGHT HAND VERTICAL STAB FORWARD ATTACH ANGLES IAW REO 670-55-31-018, REV -A, DATED 2016-11-10.SDR DALA2017012800708Fastener · shearedSHEARED FASTENER ON DORSAL FIN ANGLE STA Y=1152 BTW LONGS: 2-3 (STA). REPAIR WAS ACCOMPLISHED PER ETI-17-17-005 R2 AND ER/A 554078-14 REV ORIGINAL.SDR SIMA20170122004Drag Angle · crackedVERTICAL STAB LT DRAG ANGLE CRACKED AFT OF FR 75 PREVIOUS REPAIR. PERFORMED PERMANENT REPAIR OF VERTICAL STAB LT DRAG ANGLE AFT OF FR 75 IAW SRM 51-40-02.SDR WVER2016113092103Drag Angle · crackedLT VERTICAL STABILIZER FORWARD DRAG ANGLE IS CRACKED.SDR V0XD20161003182Drag Angle · crackedRT AFT FUSELAGE TO VERTICAL AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-090, DATED 21 SEPT 2016. NDT PERFORMED.SDR V0XD20161003181Drag Angle · crackedRT AFT FUSELAGE TO VERTICAL FWD DRAG ANGLE IS CRACKED. CUT AWAY DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-018, DATED 16 APR 2007. NDT PERFORMED.SDR V0XD20161003180Drag Angle · crackedLT AFT FUSELAGE TO VERTICAL FWD DRAG ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-018, DATED 16 APR 2016. NDT PERFORMED.SDR DALA2016062304859Skate Angle · deformedRT SIDE VERTICAL STABILIZER ATTACH SKATE ANGLE IS DEFORMED. REPAIRED IAW ER/A 547541-14, REV ORIGINAL ER/A MATCHES ALL PRIS.SDR REXA2016061601119Drag Angle · crackedRIGHT FORWARD DRAG ANGLE IS CRACKED, APPROXIMATELY 1" LEFT AT FUSE TO VERTICAL CONNECTION. REPAIRED RT FORWARD DRAG ANGLE IAW GREO 690-55-31-004, REV-A, SRM 51-21-11-001-001-A01 & 51-25-16-001-001-A01.SDR V0XD20160617131Drag Angle · crackedRIGHT DRAG ANGLE ON VERTICAL TO FUSELAGE IS CRACKED. REMOVED CRACKED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-53-31-087, DATED 10JUN2016. NDT PERFORMED.SDR V0XD2016617130Drag Angle · crackedLEFT AFT DRAG ANGLE ON VERTICAL TO FUSELAGE IS CRACKED. FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-53-31-087, DATED 10 JUN 2016. NDT PERFORMED.SDR REXA2016060601115Drag Angle · crackedRIGHT AFT DRAG ANGLE IS CRACKED APPROXIMATELY 1.5" LT AT FUSE TO VERTICAL CONNECTION. R & R RT AFT DRAG ANGLE IAW SRM 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.SDR AALA20160523009Attach Angle · crackedAIRCRAFT WAS NOT GNDED. LT DORSAL FIN TO FUSELAGE ATTACH ANGLE IS CRACKED IN RADIUS AT APPROX FS 1463. ACCOMPLISHED INTERIM REPAIR IAW AARD 53-10-00-2 & EA 260689.SDR V0XD20160511099Drag Angle · crackedLEFT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE IS CRACKED. CUT & REMOVED DAMAGED SECTION. FABRICATED & INSTALLED REPAIR IAW REO 670-55-31-083 REV A DATED 02 MAY 2016.SDR DALA2016042603307Fitting · crackedCRACKED RT LOWER DORSAL FITTING OF BS 1437 BETWEEN LONGERONS 1 TO 2 RT AT AFT ACCESSORIES COMPARTMENT. FITTING WAS REPLACED IAW SRM 51-30-5, 51-10-3 PAR 14 AND 21, ER/A 545086-14, REV ORIGINAL, AMM 20-30-01-201.SDR V0XD20160218036Drag Angle · crackedFUSELAGE TO VERTICAL STAB LT DRAG ANGLES CRACKED AT REAR DATUM 67.5%. CUT OUT CRACKED AREAS ON FWD & AFT DRAG ANGLES. FABRICATED FILLERS, DOUBLERS & INSTALLED IAW REO 670-51-00-095 REV A DATED 17 FEB 2016. FWD DRAG ANGLE, PN AV670-21186-XXX, AFT DRAG PN AV6SDR SWAA2015090943565Attach Angle · crackedFUSELAGE TO VERTICAL STABILIZER INNER ATTACH ANGLE CRACKED AT BS 1135, LONGERON 2L. R & R ANGLE IAW SRM & DWG.SDR AALA20150201005Attach Angle · crackedCRACK IN VERTICAL STABILIZER LE TO FUSELAGE FAIRING ATTACH ANGLE BELOW RAM AIR INTAKE. R & R ANGLE IAW AARD 55-30-00-7.SDR ASOA20150122012HDrag Angle · crackedDURING 2A INSPECTION THE RT FUSELAGE TO VERTICLE STAB DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE AFFECTED DRAG ANGLE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20150121005Support Angle · crackedRIGHT VERTICAL STAB TO FUSELAGE SUPPORT ANGLE IS CRACKED IN 2 AREAS NEAR FRAME 76 RT. REPLACED RT VERTICAL STAB TO FUSELAGE FWD SUPPORT ANGLE IAW EO EM-53MR-1281.SDR DALA2015012100420Attach Angle · crackedRIGHT VERTICAL FIN ATTACH ANGLE DOUBLER, AT FIN AFT SPAR, HAS 2 CRACKS. REPAIRED IAW PRI 510815-14, REV A, SEC II, FINAL ERA 510815-14.
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