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 DALA2015010800279Skate Angle · crackedFUSELAGE EXTERIOR VERTICAL STABILIZER SKATE ANGLE CRACKED AND RIVET POPPED, CANTED BS 1531, RT SIDE. COMPLIED WITH PRI 531878-14, REV O.SDR DALA2015012100427Attach Angle · crackedLT INTERNAL VERTICAL STABILIZER ATTACH ANGLE IS CRACKED IN RADIUS. REMOVED ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW DWG 5912188.SDR REXA2014121701215Fitting · crackedRT VENTRAL FIN FWD MOUNT FITTING IS CRACKED. MECH EMP R & R RT VENTRAL FIN TO FOM IAW AMM 53-87-90-000-801-A01, STEP 4 AND 53-87-90-400-801-A01, STEP 4. R & R RH VENTRAL FIN FWD MOUNT FITTING IAW AMM 53-87-90-000-802-A01, STEP 4 AND 53-87-90-400-802-A01, STSDR AALA20141208004Skate Angle · crackedFUSELAGE TO VERTICAL STABILIZER RT SKATE ANGLE IS CRACKED AT FUSELAGE STATION 1463. REPAIRED SKATE ANGLE IAW SRM 53-05-00-001 SHEET 3.SDR ASAA2014111709679Attach Fitting · corrodedAFTER REMOVAL OF RT HORIZONTAL STABILIZER, FOUND THE FWD UPPER LUG CORRODED. ACFT GROUNDED. REPAIRED RT HORIZONTAL STABILIZER FWD UPPER LUG IAW EA COMPT-55EA-13723 REV NEW ISSUED 7NOV14 ASSOCIATED FAA FORM 8100-9 PROVIDES FIRST STAGE APPROVAL FOR STATIC STRENSDR ASOA20141029309Drag Angle · crackedDURING C-CHECK, RT FWD VERTICAL TO FUSELAGE DRAG ANGLE CRACKED. MAINTENANCE R & R RT FWD VERTICAL TO FUSELAGE DRAG ANGLE CRACKED. MAINTENANCE R & R NEW DRAG ANGLE ON RT FWD VERTICAL TO FUSELAGE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASAA2014101309656Attach Fitting · corrodedRT HORIZONTAL STABILIZER FWD LOWER LUG HAS CORROSION. ACFT GROUNDED. REPAIRED RT HORIZONTAL STABILIZER FWD LOWER LUG IAW EA COMPARTMENT 55 EA, 13726 REV NEW ISSUED 07NOV14 ASSOCIATED FAA FORM 8100-9 PROVIDES FIRST STAGE APPROVAL FOR STATIC STRENGTH. SECOND STSDR ASOA2014102411488Attach Angle · crackedVERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED LT SIDE AT APPROX STR DATUM 55.62 PERCENT. FOUND TO BE OUT OF LIMITS IAW SRM 55-00-00-101-001. INSTALLED NEW SERVICEABLE ATTACH ANGLE IAW DWG JBA 670-23103, & SRM 51-42-06-001-001-A01 & 51-42-21-001-001-SDR ASOA2014102411487Attach Angle · crackedVERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED RT SIDE AT APPROX STG DATUM 55.62 PERCENT. EVALUATED DAMAGES TO BE OUT OF LIMITS IAW SRM 55-00-00-101-001. SUMITTED TO ENGINEERING FOR PERMANENT REPAIR DISPOSITION. THIS REPAIR IS CLASSIFIED AS A MAJOR RESDR ASOA20140821257Fitting · corrodedDURING C-CHECK, THE VERTICAL STABILIZER FITTING AT FRAME 75 BETWEEN STRINGERS 2R-2L WAS FOUND TO HAVE FRETTING CORROSION. MAINTENANCE REMOVED THE CORROSION AND REPAIRED THE FITTING IAW EC5330-02931. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SWAA2014100632685Attach Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING ON ACFT FUSELAGE AFT SPAR RT OTBD FITTING FWD LUG CORRODED. REPAIRED FITTING IAW EA.SDR SWAA2014100632684Attach Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING ON ACFT FUSELAGE AFT SPAR LT OTBD FITTING AFT LUG CORRODED. REPAIRED FITTING IAW EA.SDR SWAA2014100632683Attach Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING ON ACFT FUSELAGE AFT SPAR LT OTBD FITTING FWD LUG CORRODED. REPAIRED FITTING IAW EA.SDR SWAA2014100632682Attach Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING ON ACFT FUSELAGE FWD SPAR RT FITTING AFT LUG CORRODED. REPAIRED FITTING IAW EA.SDR DALA2014062003723Attach Fitting · crackedCRACK .125 INCHES, ON LT DORSAL FIN ATTACH FITTING LOCATED ON UPPER AFT SIDE OF BS 1437 BULKHEAD. LEFT DORSAL FITTING WAS REPLACE IAW SRM 51-30-5.SDR DALA2014062003706Attach Angle · crackedCRACKS ON DORSAL FIN ATTACH ANGLE OF BS 1406 - 1435 LONGERONS 1- 2L. ATTACH ANGLE WAS REPLACED IAW DWG 591288, REV BD AND SRM 51-30-5.SDR DALA2014062003704Attach Angle · crackedCRACKED ANGLE TO ATTACH TOP FUSELAGE TO VERTICAL STAB RT SIDE STA Y=1405 AND Y=1437 APPROXIMATELY, H1L1-SM, CARD 168, ZONE 100. ANGLE WAS REPLACE IAW DWG 5912188, REV BD AND SRM 51-30-5. RETAIN FOR RECORDS BY PRIMARY STRUCTURE.SDR AALA20140501012Skate Angle · crackedTAIL VERTICAL STABILIZER SKATE ANGLE CRACKED AT FASTENER STATION 1463. INSTALLED FILLER, CONICAL WASHERS & REPAIR ANGLE IAW AARD 53-10-00-2.SDR ASOA20140428065Attach Angle · crackedDURING 4A INSPECTION, THE RT VERTICLE STAB TO FUSELAGE ATTACH ANGLE WAS FOUND TO HAVE A CRACK EXTENDING 22.43MM. MAINTENANCE R & R THE AFFECTED ANGLE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA2014052210558Drag Angle · crackedRT VERTICAL STAB TO FUSELAGE ATTACH DRAG ANGLE IS CRACKED. COMPLIED WITH EC/TC REO 670-55-31-018 IAW REO 670-55-31-018. MAJOR REPAIR.SDR ASOA2014051610503Drag Angle · crackedLEFT VERTICAL STAB TO FUSELAGE ATTACH DRAG ANGLE IS CRACKED. REPAIRED IAW REO 670-55-31-018.SDR DALA14027220960Attach Angle · looseRIGHT FUSELAGE SKIN HAS TWO LOOSE FASTENERS ON LOWER FLANGE OF VERTICAL TO FUSELAGE ATTACH ANGLE WITH POSSIBLE CRACKS FROM FASTENER HOLES "MARKED" APPROXIMATELY CANT STA 1225, I-34 NR 55. IDENTIFIED CRACK, CUT-OUT DAMAGED AREA DIM: 1.8" X 1.7", FABRICATED, LOSDR CALA2014040390762Fitting · damagedHORIZONTAL STAB LT OTBD INTERMEDIATE PIVOT PIN FITTING PN 148T2708-6 FOUND WITH ELONGATED HOLES & TOOLING MARKS. INCORRECT ATTACH FASTENERS IDENTIFIED. REPAIRED FITTING IAW REO G17299 REV A & ECRA 5380-01106. THIS IS A CAT A MINOR REPAIR, DTE APPROVAL STATUSDR AALA20140313019Attach Angle · crackedTHE LT HAND VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE WAS FOUND TO BE CRACKED, APPROXIMATELY 6 INCHES FWD OF THE AFT EDGE. INSTALLED VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE REPAIR IAW AARD 53-10-00-2.SDR SWAA2014031726104Attach Angle · crackedRT HORIZONTAL STABILIZER CTR SECTION LOWER CHORD ATTACH ANGLE CRACKED AT BS 1121. R & R ANGLE IAW SRM & DWG.SDR IPXA2014022182004Seat Track · corrodedMAIN DECK CARGO TRACK CORRODED AT FRAMES 80-82, Y1137.1. REPAIRED SEAT TRACK IAW SRM 53-10-16, PARA 4, FIG 201.SDR SWAA2013121623329Skate Angle · damagedLT SKATE ANGLE DAMAGED AT BS 1060 INBD. R & R SKATE ANGLE IAW SRM.SDR QMLA2013112013168Attach Fitting · crackedDURING THE SCHEDULED MAINTENANCE AMC EC130B4 AAIP A 1040 300 HOUR - 12 MONTH AIRFRAME INSPECTION, FOUND RT LOWER HORIZONTAL STABILIZER ATTACH FITTING CRACKED. THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION AWAITING A MOBILE REPAIR TEAM FRSDR CA131113008Strut · corroded(CAN) DURING ANNUAL INSPECTION, IT WAS FOUND THAT THE LT STABILIZER STRUT ASSY. LOWER ATTACH FORK AND BUSHINGS WERE HEAVILY CORRODED.SDR SWAA2013121623328Skate Angle · corrodedLT VERTICAL STABILIZER SKATE ANGLE CORRODED BETWEEN BS 1016 & BS 1130. R & R SKATE ANGLE IAW SRM.SDR SIMA20131105003Drag Angle · crackedRT FWD VERTICAL STAB TO FUSELAGE DRAG ANGLE CRACKED. REPAIR TO RT FWD VERT TO FUSELAGE DRAG ANGLE IAW PART A OF EO CR-53MR-038R1.SDR SIMA20131030001Drag Angle · crackedRIGHT AFT VERTICAL TO FUSELAGE DRAG ANGLE CRACKED. REPAIRED IAW EO CR-53MR-164R1 PART B.SDR SIMA20131030003Drag Angle · crackedLEFT FORWARD VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED. REPAIRED IAW EO CR-55MR-038 PART A.SDR SIMA20131030002Drag Angle · crackedRT FORWARD VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED. REPAIRED IAW EO CR-55MR-038R19805.SDR SIMA20131030004Drag Angle · crackedLEFT AFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED.SDR DALA13050389207Attach Angle · brokenTHE RT FUSELAGE TO DORSAL FIN ATTACH ANGLE WAS CUT AT STA 1520, COMPLETELY SEVERED. OEM APPROVED REPAIR AS PERMANENT, ERA 518618-14. REQUIRES GVI AT 3000 CYCLES OR CHECK THRESHOLD.SDR AALA20130819003Plate · corrodedHORIZONTAL STABILIZER PLATE RT LOWER PLATE CORRODED. R&R WITH A NEW PIVOT PLATE IAW EA B757-53-031040.SDR AALA20130820004Plate · corrodedRT STABILIZER LOWER PIVOT SPLICE PLATE CORRODED. REPLACED STABILIZER PLATE IAW SRM 51-10-02-0G.SDR QMLA2013080613111Carrier Assy · crackedDURING A ROUTINE AIRWORTHINESS CHECK, MECHANIC PERFORMED A VISUAL INSPECTION OF THE ACFT. ON INSPECTING THE HORIZONTAL STABILIZER AREA, A CRACK WAS NOTICED ON THE RT LOWER CARRIER ATTACH FITTING. REPLACED CRACKED CARRIER.SDR 39LA2013072400074Attach Fitting · crackedWHILE PERFORMING EDDY CURRENT INSPECTION, SUPPLEMENTAL INSPECTION DOCUMENT 20,000 /2,800 FLIGHT SUPPLEMENTAL INSPECTION OF HORIZONTAL STABILIZER, FOUND THAT LT HORIZONTAL STABILIZER UPPER AAFT ATTACH FITTING HAS CORROSION AND CRACK INDICATION AROUND MOUNT BUSHSDR ASOA20130709111Drag Angle · crackedDURING 3A INSPECTION THE LT FWD VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE (SHAPE L ATACHMENT) WAS FOUND TO BE CRACKED APPROX 1.75" FROM THE AFT END. MX R & R THE AFFECTED DRAG ANGLE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/12/13.SDR AALA20130702007Skate Angle · crackedTAIL VERTICAL STABILIZER SKATE ANGLE IS CRACKED ON LT SIDE OF FS 1463. INSTALLED SKATE ANGLE REPAIR DOUBLER IAW EA.SDR SIMA20130425008Drag Angle · damagedDURING MAINTENANCE INSPECTION FOUND THE RIGHT VERTICAL STABLIZER TO FUSELAGE DRAG ANGLE DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DRAG ANGLE IAW AEA EO EM-53MR-1281. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130420012Angle · crackedRT FWD VERTICAL TO FUSELAGE ANGLE CRACKED. REPAIRED ANGLE IAW AEA EM-53MR-1281.SDR SIMA20130117012Drag Angle · crackedDURING MAINTENANCE INSPECTION FOUND THE RIGHT FORWARD FUSELAGE TO VERTICAL DRAG ANGLE HAS 2 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-53MR-1281 PART B. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130114010Angle · crackedDURING MAINTENANCE CHECK FOUND THE FORWARD LEFT VERTICAL STAB TO FUSELAGE ANGLE HAS A CRACK APPROX 1" LONG. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD VERTICAL STAB TO FUSELAGE ANGLE IAW EO EM-53MR-2062. THE AIRCRAFT WAS RETURNEDSDR WVER2013010550102Drag Angle · crackedLEFT AND RIGHT FUSELAGE TO VERTICAL STABILIZER ATTACHMENT DRAG ANGLES ARE CRACKED AT REAR SPAR DATUM 67.5 PERCENT.SDR USAA2012112900020Attach Bolt · corrodedQ3 CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT OUTBOARD AFT VERTICAL STABILIZER ATTACH BOLT AT BS 1085, BL 0. REPLACED RIGHT OUTBOARD AFT VERTICAL STABILIZER ATTACH BOLT AT BS 1085, BL 0 IAW JOB CARD 03C70655019.SDR USAA2012112900019Attach Bolt · corrodedQ3 CHECK - CORROSION ON LEFT FORWARD VERTICAL STABILIZER ATTACH BOLT AT BS 1016, S4L. REPLACED LEFT FORWARD VERTICAL STABILIZER ATTACH BOLT AT BS 1016, S4L IAW JOB CARD 03C70655019.SDR ASOA20121014113Fitting · crackedDURING C-CHECK THE VERTICAL STABILIZER FITTING AT FRAME 75 WAS ORIGINALLY REMOVED FOR EVIDENCE OF FRETTING AND THEN FOUND TO BE CRACKED AROUND AN UPPER BOLT HOLE. MX R & R THE FITTING IAW EC5310-01317. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
Back to JASC 5342