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 UPS96805823Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT HORIZ STAB FITTING HAS CORROSION DAMAGE AT NR 4 STR, STA XFS 135 BOTTOM INSIDE SKIN. REPLACED FITTING PER SRM 51-1-20D.SDR AU960257Bracket · broken(AUS) HORIZONTAL STABILISER TRIM ACTUATOR MOUNT BRACKET BROKEN - AIRCRAFT IS USED FOR SKYDIVING WITH DOORS REMOVED AND DEFLECTORFITTED - SUSPECT TURBULANCE CAUSED BY DEFLECTORS CAUSES EXCESSIVETURBULANT AIRFLOW OVER EMPENNAGE - SEE MDR 96/0178 FOR FURTHER INFOSDR UPS96805964Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT HORIZONTAL STAB FITTING HAD CORROSION DAMAGE AT NR 4 STR STA XFS 135 BOTTOM INSIDE SKIN. REPLACED FITTING PER SRM 51-1-20D.SDR N3VR96012Chord · corrosionREF N/R 3642, RIGHT HORIZONTAL STABILIZER FRONT UPPER CHORD CORRODED STATION 170, 188, 195, 205 (INTERNAL). REMOVED CORROSION IAW SRM 51-10-6, FORWARD INFORMATION TO ENGINEERING MATERIAL. REMOVED DETERMINED TO BE ACCEPTABLE PER ENGINEERING, PREPARED AREA PERSDR 96ZZZX1351Bulkhead · crackedVERTICAL CRACKS FOUND INTERCONNECTING ALL FOUR BOLT HOLES DRILLED IN THE AFT STABILATOR BULKHEAD TO WHICH THE STABILATOR BEARING BRACKET ATTACHES TO ON THE RT SIDE. SUSPECT CAUSE: EXCESSIVE AIR LOADS ON THE STABILATOR DUE TO AEROBATIC MANEUVERS (HAMMER HEADSSDR IXXA9621Fitting · crackedDURING THE D-CHECK INSPECTION, FOUND CRACKED FITTING ON THE RIGHT HORIZONTAL STABILIZER L/E AT FS XFS 47. FITTING WAS MANUFACTURED PER DRAWING CF-N820BX-15/96, DATED 2/9/96 AND WAS APPROVED BY FAA FORM 8110-3 DATED 2/20/96. (M)SDR AU960221Bracket · cracked(AUS) HORIZONTAL STABILIZER AFT LH MOUNTING REINFORCING BRACKET CRACKED ALONG BEND RADIUS ADJACENT TO LOWER OUTBOARD BOLT - CRACK LENGTH 25MM (0.98IN)SDR AU960185Bracket · cracked(AUS) HORIZONTAL STABILISER REAR CENTRE SPAR REINFORCEMENT BRACKET CRACKED IN AREA OF LOWER LH FLANGE - INITIAL POINT OF CRACKAPPEARS TO BE AT THE BOLT HOLE WITH SECONDARY CRACKING IN BRACKETRADIUS - SUSPECT CAUSED BY PUSHING DOWN ON STABILISER DURING GROUND HSDR 96ZZZX1811Fitting · crackedINSPECTION FOUND FITTING CRACKED THROUGH UPPER RIVET HOLES.SDR CA960223005Reinforcement · cracked(CAN)LEFT HAND HORIZONTAL STABILIZER REINFORCEMENT PART #12326231 FOUND CRACKED.SDR SWAA960059Angle · crackedDURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION RT THRUST BEAM UPPER I/B ATTACH ANGLE CRACKED AT BS 1113. REPLACED PER BOEING SRM.SDR CAL960164Chord · crackedMIA - INSPECTION FOUND A 1 INCH CRACK IN INBOARD LOWER CHORD OF INBOARD LEFT HORIZONTAL STABILIZER LEADING EDGE FLANGE. THE CRACK WAS LOCATED AT ROLLER FITTING. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-30-2. (M)SDR 96FDEA00119Stringer · corrodedRT HORIZ STAB COMP STR 10 BETWEEN STAB STA 152.4 AND 184.80 FOUND CORRODED. MINOR SURFACE CORROSION REMOVED AND AREA REPROTECTED AS PER SRM FEDEX 51-10-01 AND 51-10-02 REV 76 WITHIN LIMITS AS PER SRM FEDEX 55-10-01 REV 76.SDR 9606699602Stringer · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE RIGHT HORIZONTAL STABILIZER UPPER STRINGERS 1 TO 9 BETWEEN XFS 15 TO 60. REPAIRED STRINGERS (P/N 5922578-501, 5922577-501 AND 5922576-501) PER EA 12-5510-9-C0705.SDR 96ZZZX967Bracket · crackedLEFT HORIZONTAL STABILIZER ATTACH FITTING ON STABILIZER SPAR FOUND CRACKED. INTERGRANULAR CORROSION EVIDENT ON THE COMPLETE LENGTH OF CRACK. PART IS HIGHLY LOADED AND SUBJECT TO STRESS CORROSION. SUBMITTER STATED THIS FITTING SHOULD BE EXAMINED CAREFULLY DUSDR UPS805411Fitting · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT HORIZ STAB CRACKED ON T-FITTING LOWER FWD I/B. REPLACED FITTING PER SRM 51-1-20D.SDR UPS805336Angle · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT HORIZ STAB LEADING EDGE I/B SUPPORT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-1-20D.SDR DL72W954776Beaded Doubler · crackedDURING C/V, FOUND RT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL BEADED DOUBLER LOWER PANEL CRACKED. REPAIRED PER SRM 55-20-3 FIG 3.SDR CA951204014Mounts · cracked(CAN)LH HORIZONTAL STABILIZER LEADING EDGE ASSEMBLY STA 156 AND STA 162 COMPENSATOR MOUNTS CRACKED. REPAIRED SRM 51-140-20.SDR 96ZZZX36Bracket · mismanufacturedAFTER RECEIVING PARTS FROM CESSNA PARTS DIVISION TO ACCOMPLISH SEB 89-1, 'STABILATOR BALANCE WEIGHT ATTACH BRACKETS' NOTICED THAT LT BRACKET WAS MANUFACTURED BACKWARDS TO RESEMBLE THE DASH 2 RT BRACKET. LATER, WAS NOTIFIED THE WHOLE BATCH FROM CESSNA WAS MADESDR HEEA956045Slat · deterioratedLT SLAT DETERIORATING.SDR CA951122014Horizontal Stab · cracked(CAN) LEFT HAND ATTACH POINT FOR HORIZONTAL STABILIZER FOUND CRACKED. REINFORCEMENT P/N 0712048-7 IS PART OF THE STABILIZER ATTACHMENT. SUBMITTER STATES THAT SUSPECT CAUSE IS USING THE HORIZONTAL STABILIZER TO PUSH THE AIRCRAFT.SDR DLL10954506Structure · crackedTHE RT HORIZ STAB L/E WAS FOUND WITH EXTENSIVE DAMAGE FWD OF THE FRONT SPAR BETWEEN STA-H LE 332.7 TO 455.2. THE DAMAGE CONSISTS OF CRACKED SKIN PANELS, CRACKED UPPER AND LWR AUXILIARY SPARS AND CRACKED RIBS ALONG WITH ATTACHED BRACES. ERA 272205 WILL AUTHORSDR A6WR95049Bracket · corrodedDURING ACCEPTANCE INSPECTION, FOUND EXFOLIATION CORROSION ON LT ELEVATOR NR 2 HINGE A-FRAME BRACKET. REPLACED BRACKET. (X)SDR 95ZZZX6840Support · crackedSUPPORT CRACKED AT END WHERE ELEVATOR ATTACHES. THIS CAUSES HINGE BEARINGS, PN BR4, TO BE LOOSE. THIS PART CAN ONLY BE SEEN BY REMOVING HINGE SUPPORT, PN 285-220401-7. RIGHT SUPPORT WAS FOUND BROKEN AND AS A PRECAUTION, LEFT SIDE WAS INSPECTED AND FOUND CRASDR 95UAL900191Channel · crackedHORIZONTAL STABILIZER CENTER SECTION, LEFT U-CHANNEL OF BOX WEB ASSEMBLY CRACKED. REPLACED LEFT U-CHANNEL OF BOX WEB ASSEMBLY.SDR 96ZZZX3664Chord · corrodedWHILE PERFORMING CPCP TASK CARD NR C55-300-10.01, FOUND INDICATION OF LEVEL 2 CORROSION. THIS CORROSION EFFECTED THE LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE CHORD AROUND FASTENERS FOR THE NR 2 ELEVATOR HINGE FITTING AT STABILIZER STA 118.65, ELEVATOR SSDR 96ZZZX3663Chord · corrodedWHILE PERFORMING CPCP TASK CARD NR C55-300-10.01, FOUND INDICATION OF LEVEL 2 CORROSION. THIS CORROSION EFFECTED THE LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE CHORD AROUND FASTENERS FOR THE NR 3 ELEVATOR HINGE FITTING AT STABILIZER STA 151, ELEVATOR STA SDR 95FDEA01528Beam · corrodedCORROSION (73C032-03), ON THE T/E AFT UPPER CHORD AT STAB STA 206 AND STA 161 RIGHT HORZ STAB. REMOVED AND REPLACED T/E AFT UPPER CHORD ON RIGHT HORZ STAB, ALL WORK DONE IAW.SDR C2XA95IA281Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR UPS804731Splice Beam · corrodedWHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND THE LT UPPER SPLICE BEAM AND THE UPPER AND LOWER SHEAR FITTINGS CORRODED AT APPROX RUDDER STA 212.87-220.870. MAINTENANCE REMOVED AND REPLACED SPLICE ASSY AND UPPER AND LOWER SHEAR FITTINGS IAW BOEING DRAWING 65SDR 95ZZZX6176Stabilizer · corrodedDURING THE ANNUAL INSPECTION, THE HORIZONTAL STABILIZER ASSEMBLY WAS FOUND CORRODED BEYOND ECONOMICAL REPAIR LIMITS. INTERNAL PORTION OF STABILIZER ASSY IS VERY DIFFICULT TO INSPECT WITH THE ELEVATOR ASSY INSTALLED. SUBMITTER RECOMMENDS EXTRA EFFORT TO THOROSDR CAL950881Horiz Stab · dentedIAH - INSPECTION FOUND THE HORIZONTAL STABILIZER RIB CORD AND SKIN DENTED ON INBOARD RT SIDE CAUSED BY A BIRD STRIKE. (X)SDR 95ZZZX6439Spar Assy · crackedFOUND 2 CRACKS AT LIGHTENING HOLE IN CENTER SECTION OF FRONT SPAR AND REINFORCEMENT SPAR OF HORIZONTAL STABILIZER. SUSPECT CAUSE - IMPROPER GROUND HANDLING. RECOMMENDATION - USE TOW BAR.SDR 96ZZZX729Fitting · rustedINSPECTION FOUND STAB FITTING RUSTED. PIPER SB 962 DATED SEPTEMBER 29, 1993, DOES NOT COVER RE-INSPECTION OF AREA AFFECTED SOON ENOUGH. RUST CANNOT BE SEEN UNDER FITTING AND BETWEEN AIRCRAFT SKIN. DISSIMILAR CORROSION SETS UP CAUSING ADDITIONAL DAMAGE. SUBSDR 95ZZZX5882Hinge · failedAFTER LANDING, AIRCRAFT EXPERIENCED A NOSE WHEEL SHIMMY. THE CONTROLS FOR THE STABILATOR FELT ABNORMAL FOLLOWING SHIMMY DURING ROLL-OUT. FURTHER INVESTIGATION REVEALED THE LEFT STABILATOR ATTACH BRACKET SHEERED OFF WITHOUT INDICATION OF WORKING - AD87-02-08 SDR UPS204487Beam · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT HORIZONTAL TRAILING EDGE BEAM EXTERIOR SURFACE AT STAB STATION 225.54 AND 182.5. MAINTENANCE CUTOUT THE DAMAGED SECTION AND SPLICED IN NEW SECTION IAW SRM 55-10-6.SDR UPS204480Stiffener · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE LEFT HORIZONTAL STABILIZER WEB STIFFENER AT STAB STATION 73 ON THE UPPER SIDE OF THE STIFFENER. MAINTENANCE REMOVED THE CRACKED STIFFENER AND REPLACED WITH NEW IAW SRM 57-30-2.SDR UPS204479Stiffener · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE LEFT HORIZONTAL STABILIZER WEB STIFFENER AT STAB STATION 64 ON THE UPPER SIDE OF STIFFENER. MAINTENANCE REMOVED THE CRACKED STIFFENER AND REPLACED WITH NEW PER SRM 57-30-2.SDR UPS204478Stiffener · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK ON THE LEFT HORIZONTAL STABLIZER WEB STIFFENER AT STATION 54 ON THE UPPER SIDE OF THE STIFFENER. MAINTENANCE REMOVED THE CRACKED STIFFENER AND REPLACED WITH NEW IAW SRM 57-30-2.SDR UPS204477Stiffener · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT HORIZONTAL STABILIZER AFT INTERSPAR WEB INBOARD ATTACHING BRACKET INSIDE ACCESS PANEL AREA 9206. MAINTENANCE FABRICATED NEW STIFFENER AND INSTALLED IAW SRM 51-30-2 AND 55-10-1.SDR UPS204476Stiffener · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE HORIZONTAL STABILIZER RIGHT INBOARD CLOSURE WEB INSIDE ACCESS PANEL 9205 AREA AT UPPER END OF WEB WHERE AFT INTERSPAR WEB ATTACHING BRACKET IS MOUNTED. MAINTENANCE FABRICATED NEW STIFFENER AND INSTALLESDR 95FDEA01340Chord · damagedRT LOWER T/E CHORD, HORIZONTAL STAB, 3 RUBSTRIP FASTENERS HAVE PULLED THROUGH BETWEEN ELEVATOR STATIONS. REPAIRED LOWER T/E CHORD IAW FEDEX EA 7-5510-25695.SDR CA960202021Spar · cracked(CAN)SUBMITTER FOUND THE BEGINNING OF CRACKS IN THE FILLET OF THE SPAR AT THE STABILATOR HINGE ATTACHMENT POINTS.SDR CA951010024Stabilizer · cracked(CAN)THE RIGHT HAND REINFORCEMENT BRACKET WAS FOUND TO BE CRACKED. REPLACED.SDR DL72S953885Beam · crackedTHE LOWER TRAILING EDGE BEAM ON THE RT HORIZONTAL STABILIZER WAS FOUND CRACKED APPROXIMATELY 2 INCHES FROM THE OUTBOARD END OF THE BEAM. ACCOMPLISHED REPAIRS PER ERA 302395-14.SDR ABXA9500832Fitting · crackedDURING COMPLIANCE OF AD 82-06-02, SB 55-32, FOUND A CRACK AT FORWARD UPPER RIGHT HAND HI-LOCK IN THE REAR SPAR FITTING. REPLACED CONSTANT SECTION IAW DC-9 SRM 51-30-1.SDR 95ZZZX5705Support Assy · crackedDEFECTS WERE FOUND DURING ROUTINE MAINTENANCE INSPECTION PER CAMP CARD NR 27013, ATA 274006, LT, AND ATA 274007, RT. THE LT INBD HORIZ SUPPORT WAS FOUND BROKEN AT THE BEARING (PN BR4) AND THE RT INBD HORIZ SUPPORT WAS CRACKED AT THE BEARING (PN BR4). THE BEASDR 95ZZZX5704Support Assy · crackedDEFECTS WERE FOUND DURING ROUTINE MAINTENANCE INSPECTION PER CAMP CARD NR 27013, ATA 274006, LT, AND ATA 274007, RT. THE LT INBD HORIZ SUPPORT WAS FOUND BROKEN AT THE BEARING (PN BR4) AND THE RT INBD HORIZ SUPPORT WAS CRACKED AT THE BEARING (PN BR4). THE BEASDR 95FDEA01141Beam · elongatedBOLT HOLE ON LT HORIZONTAL STAB TRAILING EDGE BEAM AT NR 2 RUB BLOCK IS ELONGATED. REMOVED HORIZONTAL STAB TRAILING EDGE BEAM, FABRICATED AND INSTALLED PARTS PER FEDEX EA 7-5510-25555.
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