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 96ZZZX5890Reinforcement · crackedAT 50 HR INSP, NOTICED REINFORCEMENT CRACKED AT BOTTOM FLANGE WHERE HINGE BOLTS TO STABILIZER. INSTALLED NEW REINFORCEMENT FROM CESSNA. SUBMITTER STATED HINGE BOLTS WERE NOT LOOSE, SO CRACK MUST HAVE OCCURRED DUE TO FATIGUE.SDR AALA961520Beam · corrodedTUL - FOUND CORROSION UPPER HORIZONTAL TE BEAM 2 PLACES BEYOND LIMITS. CUT OUT AND BLENDED AREAS. TREATED AND PRIMED, REPAIRED PER ESO 11697 AND SRM 55-10-6 FIG 1. (M)SDR MWEA96543Stringer · crackedDURING D-CK, FOUND RT HORIZONTAL STAB UPPER STRINGER NR 3 CRACKED AT STA XHS50. INSTALLED REPAIR IAW SRM 55-02, FIG 16, SHEET 7.SDR HEEA968213Stabilizer Assy · mis mfgLH SIDE OF STABILIZER AT CENTER, MEASURES 1.778, ANGLES ON AUX FIN MEASURE 1.704 WHICH MAKES STABILIZER .074 TOO THICK. RH SIDE OF STABILIZER AT CENTER MEASURES 1.799 ANGLES ON AUX FIN MEASURES 1.708 WHICH MAKES STAB. .091 TOO THICK.SDR HEEA968114Bolt · wornBOLTS FOR HORIZONTAL STABILIZER WORN. REPLACED WITH SERVICEABLE HORIZONTAL STABILIZER.SDR 96ZZZX5103Bracket · crackedDURING ANNUAL INSPECTION, CRACKS WERE NOTED ON (3 OF THE 4) STABILATOR WEIGHT ARM MOUNT BRACKETS. CAUSE, NORMAL WEAR AND VIBRATION. SUBMITTER RECOMMMENDS CLOSER INSPECTION AND DYE CHECK. ALSO INCLUDES FORWARD MOUNT P/N 1732010-1 AND DASH 2.SDR 96ZZZX5102Bracket · crackedDURING ANNUAL INSPECTION, CRACKS WERE NOTED ON (3 OF THE 4) STABILATOR WEIGHT ARM MOUNT BRACKETS. CAUSE, NORMAL WEAR AND VIBRATION. SUBMITTER RECOMMMENDS CLOSER INSPECTION AND DYE CHECK. ALSO INCLUDES FORWARD MOUNT P/N 1732010-1 AND DASH 2.SDR 96ZZZX4990Bracket · crackedA CRACK WAS FOUND IN A BEND RADIUS OF THE LEFT HAND REAR SPAR ATTACHMENT REINFORCEMENT BRACKET ADJACENT TO THE BEND RADIUS HOLE. SUBMITTER RECOMMENDS THE MFG TO MAKE LARGER BRACKET EXTENDING PAST THE LIGHTNING HOLE.SDR N3VR96152Retainer · corrodedRIGHT HORIZ STAB T/E SEAL RETAINER, SEAL LOOSE AT ELEVATOR HINGES NR 2, NR 5 AND NR 7 POSITIONS, CRACKS FOUND RUNNING FROM LOOSE RIVET HEADS. BLENDED OUT DAMAGED AREAS, REMOVED CORROSION, RELOCATED FASTENERS IAW EO 96-1031, REF SRM 51-10-2, 51-30-2 AND 51-10-SDR UPS96821089Stabilizer · crackedON PRED. CHK FOUND 2 DENTS ON LEFT STAB L/E. DENT THAT IS APPROX. 46 INCHES OUT FROM STAB L/E ROOT AND HAS 2.6258 INCH CRACK. DENT INBOARD OF PREVIOUS MENTIONED IS 6 INCHES BY 2.50 INCHES. REMOVED DAMAGED L/E SKIN PER SRM 55-2-1. FABRICATED DOUBLERS FROM 7SDR CA961018010Stabilizer · out of bal(CAN) TAIL ROTOR ASSEMBLY HAS ALWAYS BEEN DIFFICULT TO DYNAMICALLY BALANCE USING THE CHADWICK 8500 SERIES STOBEX. OVER THE LIFE OF THE TAIL ROTOR SEVERAL SETS OF EXPENSIVE BEARINGS HAVE BEEN CHANGED. WHILE THIS PARTIALLY RESOLVED THE PROBLEM, IT STILL TOOK MANSDR TSAA9655066Beam · corrodedDURING HEAVY MAINTENANCE VISIT, EXFOLIATION NOTED ON RIGHT HORIZONTAL STABILIZER T/E SUPPORT BEAM (TOP) BETWEEN BS 66.54-94.07. REPAIRED PER ECO2306 PART 1 WITH DEVIATION D. AIRCRAFT RETURNED TO SERVICE. (M)SDR HEEA967751Stabilizer Assy · mis repair2 EACH INSERTS ON R//H FORWARD BOTTOM SIDE MISLOCATED AND 4 EACH INSERTS ON L/H AFT BOTTOM SIDE MISLOCATED. TIME SINCE REPAIR 0:00.SDR 96ZZZX5222Stabilizer · loose rivetsFOUND LOOSE RIVETS ON LEADING EDGE OF HORIZONTAL STABILIZER ON THE FIRST TWO RIBS OUT FORM THE FUSELAGE. REMOVED AND REPLACED RIVETS WITH NEW. AIRCRAFT EQUIPPPED WITH DE-ICE BOOTS.SDR P5CA9601232Tip Fairing · damagedRT STABILIZERS T/E TIP IS TORN. INSTALLED NEW FAIRING TIP (P/N 65B03521-34) AND RIVETED PER SRM 51-30-02.SDR CA960826021Reinforcement · cracked(CAN) HORIZONTAL STAB REINFORCEMENT BRACKET REPLACED WITH HEAVIER REPLACEMENT PART SUPPLIED THROUGH CESSNA.SDR CALA9601182Hinge Plates · corrodedINSPECTION FOUND INBOARD AND OUTBOARD HINGE PLATES FOR LT HORIZONTAL STABILIZER CORRODED. THE HINGE PLATES WERE REMOVED AND NEW PLATES WERE INSTALLED IAW SRM 51-30-5.SDR MWEA96309Stringers · crackedDURING D-CHECK, LOWER STRINGERS 5, 6 WERE FOUND CRACKED AT STATION XHS 50 IN LT HORIZ STAB. REPAIRED THE CRACKED STRINGERS IAW SRM 55-02, FIG 16.SDR 96ZZZX4852Longeron · corrodedDURING SCHEDULED MAINTENANCE, FOUND LT STABLIZER LONGERON WITH EXCESSIVE CORROSION.SDR 96ZZZX4851Doubler · corrodedDURING SCHEDULED MAINTENANCE, FOUND STABILIZER DOUBLER WITH EXCESSIVE CORROSION. COMPONENT P/N 7600006003011.SDR 96ZZZX4850Tip Cap · corrodedDURING SCHEDULED MAINTENANCE, FOUND STABILIZER INSTALLATION WITH EXCESSIVE CORROSION.SDR 96UAL900536Bolt · shearedDURING REPLACEMENT OF HORIZONTAL STAB PIVOT BEARINGS, FOUND ANTI-ROTATION PLATE CROSS BOLT SHEARED ON LT STAB FITTING. ANTI-ROTATION PLATES DISLODGED AND PIVOT BUSHING ROTATED IN HINGE FITTING BORE CREATING GOUGE IN OUTBOARD FACE OF LT PIVOT FITTING. ROTATIONSDR HEEA967579Stabilizer Assy · mis mfgSTABILIZER INSERTS FOR L/H AND R/H TAILBOOM ATTACHMENT SUPPORTS MISLOCATED. (INSTALLED TOO FAR OFF)SDR HEEA967578Stabilizer Assy · mis mfgSTABILIZER IS TOO THICK. WILL NOT ALIGN TO STABILIZER SUPPORTS THAT ATTACH TO TAILBOOM.SDR AALA960987Beam · corrodedTUL - LEFT HORIZONTAL STABLIZER TRAILING EDGE BEAM CORRODED INBOARD OF NR 4 ELEVATOR HINGE BEARING. REMOVED CORROSION, REPAIRED PER SRM ESO 11697, DATED 6-20-96. TST: 64,997 HOURS. CYCLES, 44,491. (X)SDR CA960708006Stabilizer · cut(CAN) DAMAGE FOUND ON LEADING EDGE OF RIGHT HAND HORIZONTAL STABILIZER AT STATION 120. FURTHER INVESTIGATION FOUND UPPER AND LOWER EXHAUST CLAMP ASSEMBLIES ON CYLINDER 16 AND 17 HAD COME OFF DURING FLIGHT AND CUT LEADING EDGE STABILIZER 2.5".SDR CA960703003Horizontal Stab · delaminated(CAN) MOMENTARY CONTROL FLUTTER IN FLIGHT. UPON LANDING AN INSPECTION REVEALED THE MYLAR STRIP WHICH IS TAPED TO THE UPPER SKIN AND EXTENDS OVER THE ELEVATOR CONTROL SURFACE WAS MISSING. THE UPPER SKIN LAMINATE DIRECTLY OVER THE TWO CENTRE HINGES FOR THE ELEVASDR UPS96220457Support · corrodedINSPECTION TYPE SI, LT HORIZONTAL STABILIZER SIDE RUB PAD IS PILLOWING. REMOVED RUB PLATE FROM SUPPORT AND FOUND CORROSION TO BE OUT OF LIMITS PER SRM 55-50-01. INSTALLED NEW RUB PLATE AND SUPPORT PER SRM 51-30-02 MATERIAL LOSS WAS 100 PERCENT OF SUPPORT.SDR UPS96220456Support · corrodedINSPECTION TYPE SI, RT HORIZONTAL STABILIZER SIDE RIB PAD IS PILLOWING. REMOVED RUB PLATE FROM SUPPORT AND FOUND CORROSION TO BE OUT OF LIMITS PER SRM 55-50-01. INSTALLED NEW RUB PLATE AND SUPPORT PER SRM 51-30-02, MATERIAL LOSS WAS 1OO PERCENT OF SUPPORT.SDR 96ZZZX3226Flange · crackedTHE TAILPLANE STRUCTURE MAIN RIB FORWARD FLANGES AT THE TAILPLANE LOWER RIB ATTACHMENT FITTING FOUND CRACKED. THE CRACKING IS FATIGUE RELATED. SUBMITTER STATED TO CORRECT PROBLEM, INSTALL MOD. 3/935 IAW DHC-3 SB 3/50. NOTE: THE DYE PENETRANT METHOD PER SB SDR ABXA9600563Scraper · wornDURING C-CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE ICE SCRAPER HAD A HOLE IN IT. REPAIRED IAW DC-9 SRM 55-01 FIGURE 2, SHEET 2.SDR MZZA96054Beam · corrodedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON LEFT HORIZONTAL STABILIZER TE BEAM AT ELEV STATION 17. THE CORRODED TRAILING EDGE BEAM WAS TREATED AND REPAIRED PE B727 SRM 51-10-6 AND 55-10-6. REF: HANGAR NON ROUTINE SDR HEEA967210Stabilizer Assy · separatedSEPARATED ON L/H AND R/H SIDE AT BOTTOM EDGE.SDR AU960605Fairing · damaged(AUS) RH HORIZONTAL STABILISER TIP DAMAGED BY COLLISION WITH TOWED 747 AIRCRAFT - DAMAGE TO THE FOLLOWING AREAS:- 1. END TIP CLOSURE FAIRING FIBREGLASS PANEL SEVERED 2. LOWER FIBREGLASS PANEL SEVERED AT OUTBOARD EDGE 3. END CLOSURE TIP ASSEMBLY TORN AND DISTOSDR AWXA960312Clevis · corrodedPAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION ON LEFT UPPER CHORD ATTACH CLEVIS AND BOTTOM CHORD ATTACH LUG OF HINGE HOUSING. REMOVED CORROSION FROM LEFT UPPER/LOWER LUG CLEVIS .018 INCH, .005 INCH, .013 INCH AND .006 INCH SDR AU960697Beam · corroded(AUS) LH HORIZONTAL STABILISER LOWER TRAILING EDGE BEAM COVER PLATE CONTAINED SEVERE EXFOLIATION CORROSIONSDR 96FDEA00779Angle · crackedTHE RT HORIZ STAB CENTER L/E SECTION O/B RIB UPPER CHORD ANGLE IS CRACKED IN 3 PLACES ON IN FLANGE BETWEEN RADIUS AND FASTENERS HOLES. REMOVED AND REPLACED UPPER CHORD ANGLE PER SRM 55-00-01.SDR AWXA960182Beam · damagedPAE - FLT 3710 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND DAMAGE AROUND NUTPLATE FASTENER HOLES IN RT HORIZONTAL LOWER T/E BEAM AT STABILIZER STA 119, STA 144, AND STA 158. REPAIRED DAMAGED AREA AROUND NUTPLATE FASTENER HOLES IAW ER 3-55-12-04. SDR AALA960598Upper Te Beam · corrodedTUL - FOUND CORROSION ON UPPER AND LOWER TRAILING EDGE BEAMS, HORIZ STAB UPPER FROM 196 TO 201 ELEVATOR STATION LOWER FROM ELEVATOR STATION 21 TO 29, RIGHT SIDE. REPAIRED PER ESO 11697, DATED 4/9/96. (M)SDR AALA960583Beam · corrodedTUL - FOUND CORROSION ON HORIZ STAB TRAILING EDGE BEAM, 8 INCHES INBOARD OF END OF TOP BEAM. REMOVED CORRODED AREA AND INSTALLED DOUBLER PER ESO 11697 DATED 4-9-96. (M)SDR 96ZZZM848Lower Te Beam · corrodedTUL - FOUND CORROSION ON UPPER AND LOWER TRAILING EDGE BEAMS, HORIZ STAB UPPER FROM 196 TO 201 ELEVATOR STATION LOWER FROM ELEVATOR STATION 21 TO 29, RIGHT SIDE. REPAIRED PER ESO 11697, DATED 4/9/96. REFERENCE AALA960598.SDR 96ZZZX3514Stringer · bentWHILE PERFORMING A PHASE 1-4 INSPECTION, NOTICED TOP CENTER SKIN OF THE HORIZONTAL STABILIZER WAS BUCKLED BEYOND LIMITS AS STATED IN THE SRM. WHEN SKIN WAS REMOVED FOR REPLACEMENT, A HIDDEN DAMAGE INSPECTION REVEALED UPPER AFT STRINGER WAS ALSO BENT AND DISTOSDR TSAA9655009Attach Lugs · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND CORROSION ON LEFT AND RIGHT HORIZONTAL STABILIZER ATTACH LUGS, FACE AND BORES. REPAIRED PER ECO 2689, PARTS I AND II. AIRCRAFT RETURNED TO SERVICE. TAT: 24,124.20 HOURS. TAC: 14,610.SDR MWEA96083Stringer · crackedFOUND LT HORIZ STAB NR 3 UPPER STRINGER CRACKED AT STA XHS32. INSTALLED REPAIR IAW SRM 55-03 FIG 16.SDR 96ZZZX2587Bolt · defectiveDURING C/W ARMY BULLETIN 95-ASAM-05 ON STABILIZER BAR PIVOT BOLTS, THE NUTS WERE FOUND BOTTOMED OUT ON THE BOLT SHANK. NEW PARTS IAW ARMY PART MANUAL DID NOT PROPERLY SOLVE THE PROBLEM, HOWEVER, INSTALLATION OF BELL'S COMMERCIAL 205 BOLTS 20-057-10S27D AND SPESDR 96ZZZX2383Balance Weight · bolts wornTHROUGH-BOLT HOLDING ELEVATOR BALANCE WEIGHT TO TUBE FOUND TO BE BADLY WORN FROM LOOSE FIT TO TUBE. AD 70-26-04 DOES NOT CALL FOR BOLT INSPECTION.SDR 96ZZZM778Stringer · damagedDURING SPECIAL CHECK, FOUND LOWER HORIZONTAL STABILIZER DAMAGE AT STATION 304, STRINGER 7L. REPAIRED PER SRM 55-10-03, PAGE 101, DETAIL NR 1 AND TWA STANDARD PRACTICES.SDR 96ZZZM776Stringer · crackedDURING SPECIAL CHECK, FOUND CRACK IN LOWER HORIZONTAL STABILIZER STRINGER 6L, STATION 290. REPAIRED PER SRM 55-10-03, FIGURE 101, DETAIL NR 1 AND TWA STANDARD PRACTICES.SDR 96ZZZM769Stringer · damagedDURING SPECIAL CHECK, FOUND LOWER HORIZONTAL STABILIZER STRINGER 5L DAMAGED AT STATION 300. REPAIRED PER SRM 55-10-03, FIGURE 101, DETAIL NR 1 AND TWA STANDARD PRACTICES.SDR CA960327012Bracket Stab · cracked(CAN)AT INSPECTION THE STABILIZER WAS REMOVED AND THE LEFT BRACKET STABILIZER HINGE WAS FOUND CRACKED FROM THE CENTRE DOWNWARDS. THE RIGHT STABILIZER HINGE WAS GROOVED TO THE POINT OF PART REJECTION AS WEL L AS THE RIGHT ANGLE REINFORCEMENT.
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