JASC 5520
Service difficulty reports · 5,421
Reports filed under 5520 · Elevator 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 = '5520' 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 = '5520' 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 PCAA9600329Plate · looseELEVATOR GUST LOCK PLATE HAS SEVERAL WORKING JO-BOLTS. REPAIRED GUST LOCK PLATES IAW DHC REPAIR DRAWING 8-55-099. AIRCRAFT RETURNED TO SERVICE. (M)SDR MZZA96161Elev Tabs · req'd repaintTNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, PER CUSTOMER REQUEST ITEMS TO REPAINT LT/RT ELEVATORS AND TABS. THE LT/RT ELEVATORS AND TABS WERE REPAINTED AND REBALANCED PER CONTINENTAL DRAWING NR 5100D8465 ADN B727 SRM 51-80-7 AND -9 RESPECTIVESDR ABXA9700428Hat Channel · crackedINNER HAT CHANNELS CRACKED. REPLACED 3 HAT CHANNELS IAW SRM 51-30-2.SDR 96ZZZX5626Elevator · flutterELEVATOR FLUTTER CAUSED MULTIPLE FRACTURES AND DELAMINATIONS IN ELEVATOR SKINS INCLUDING SEPARATION OF INBOARD HINGES ON HORIZONTAL STABILIZER. PILOT REPORTED A VIBRATION AT 120 KTS AND 10,000 FEET IN SMOOTH AIR. REDLINE AT 10,000 FEET IS 128 KTS. POST-INSPSDR HEEA968325Elevator Asy · crackedELEV CRACKED AT PIVOT HOLES.SDR HEEA968323Elevator Asy · corrodedELEV ASSY CORRODED BEYOND LIMITS.SDR HEEA968321Elevator Asy · corrodedELEV ASSY CORRODED BEYOND LIMITS.SDR CALA9601584Bracket · crackedINSPECTION FOUND A .75 INCH CRACK IN LT ELEVATOR NR 3 HINGE ATTACH BRACKET AT HORIZONTAL STABILIZER TRAILING EDGE. THE CRACKED AREA WAS CUT OUT. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-10-4.SDR CA961018001Hinge Fitting · hole elongated(CAN) PILOT INDICATED INTERMITTENT VIBRATION AT LOWER SPEEDS. UPON INSPECTION, THE LEFT ELEVATOR WAS FOUND TO HAVE EXCESSIVE PLAY AT OUTBOARD HINGE. BOTH FITTING AND HINGE ARM WERE REPLACED AS THE BOLT HOLE WAS ELONGATED.SDR HEEA968094Stabilizer Assy · mis mfgINSTALLED STABILIZER AND TRIED TO INSTALL ELEVATOR ASSEMBLY. THE LEFT ELEV PIVOT PIN HAD BEEN INSTALLED 5/16" INBOARD TOO FAR. UNABLE TO INSTALL ELEVATOR.SDR 96ZZZX5129Hinge Half · failedELEVATOR BROKE LOOSE FROM THE OUTBOARD HINGE BOLT. THE REMAINING INBOARD BRACKET BROKE OUT OF THE SPAR.SDR 96ZZZX5128Bushing · failedELEVATOR BROKE LOOSE FROM THE OUTBOARD HINGE BOLT. THE REMAINING INBOARD BRACKET BROKE OUT OF THE SPAR.SDR P5CA9600708Fairing · pulled rivetsRIVET HEADS SUNK INTO UPPER FIXED FAIRING MID SECTION ON LEFT HORIZONAL STABLIZER. MADE FIBERGLASS REPAIR PER BAC SRM 51-40-09.SDR CALA9601309Cover Plate · crackedRT ELEVATOR TRAILING EDGE IN BETWEEN BOTH TABS, GEAR TAB INBOARD END ROD COVER UPPER PLATE WAS FOUND CRACKED. THE OLD DOUBLER WAS REMOVED AND A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR 96ZZZX4983Hinge · bushing wornDURING AN ANNUAL INSPECTION, THE LT INBD ELEVATOR HINGE BUSHING WAS FOUND TO HAVE ITS INNER RACE WORN TO THE POINT THAT IT ALLOWED THE ELEVATOR ADDITIONAL MOVEMENT PAST THE NORMAL TRAVEL. BUSHING WAS REPLACED WITH NEW. WHEN QUESTIONING THE PILOT ABOUT THE AISDR EISA96142Cover · crackedLEFT ELEVATOR TAB BOB WEIGHT COVERS CRACKED. REPLACED LEFT ELEVATOR. (M)SDR EISA96139Cover · crackedRIGHT ELEVATOR TAB, BOB WEIGHT COVERS CRACKED. RIGHT ELEVATOR TAB REPLACED. (M)SDR CA960813005Fitting · worn(CAN) ON BOTH LEFT HAND AND RIGHT HAND ELEVATOR THE LOWER BOLT (P/N AN23-10A) COULD BE TURNED BY HANDSDR MWEA96355Angle · corrodedDURING D-CHECK, SEVERE CORROSION WAS FOUND ON LT ELEVATOR T/E 'TEE' ATTACH ANGLE BRACKET AT STA XE 171.5. FABRICATED A NEW TEE AND INSTALLED IAW SRM 51-10 AND 51-30.SDR AU961130Bolt · corroded(AUS) ELEVATOR HINGE BOLT CORRODED - FOUND DURING ELEVATOR BEARING CHANGE WHEN ELEVATORS REMOVEDSDR 96ZZZX4150Elevator · mismanufacturedRECEIVED 'NEW' PART, DROP SHIPPED FROM CESSNA AIRCRAFT. PREPPED AND PAINTED TO MATCH AIRCRAFT. PLACED CONTROL SURFACE ON BALANCING JIG. PART REQUIRED 6 OUNCES OF ADDITIONAL COUNTERWEIGHT TO BRING WITHIN PRESCRIBED LIMITS. REMOVED EXISTING LT ELEVATOR DUE TSDR 96ZZZX3917Fitting · crackedWHILE C/W CESSNA SB MEB 95-10, FOUND RT ELEVATOR FITTING CRACKED AT AREA WHERE THE TAPER PIN COMES THROUGH. SUBMITTER SUGGESTS THAT THESE FITTINGS ARE INSPECTED ANYTIME THE TAIL CONE IS REMOVED.SDR EISA96107Tip Filler · brokenLEFT ELEVATOR OUTBOARD AFT TIP IS BREAKING. REMOVED AND REPLACED TIP FILLER PER SRM 51-30-02. TT: 66,991:57 HOURS. TC: 45,084. (X)SDR EISA96106Tip Filler · brokenRIGHT ELEVATOR OUTBOARD T/E TIP IS BREAKING. REMOVED AND REPLACED ITP FILLER PER SRM 51-30-2. TT: 66,991:57 HOURS. TC: 45,084. (X)SDR DL72S961537Doubler · crackedPREVIOUS DOUBLER CRACKED 1.5 INCH AT FASTENER. LOWER RT ELEVATOR I/B END. REPAIRED PER SRM 55-20-3 FIG 4.SDR UPS96820510Mounting Flange · crackedINSPECTION TYPE CS2, RT ELEVATOR TOADSTOOL UPPER ACCESS PANEL MOUNTING FLANGE IS CRACKED. REPAIRED PER UPS EO.SDR AU960803Elevator · cracked(AUS) LH AND RH ELEVATORS CRACKED - FOUND DURING RADIOGRAPHIC INSPECTION IAW AD/PA31/126SDR 96ZZZX3362Hinge · crackedDURING PHASE 1 INSPECTION 'SMOKING' RIVETS WERE NOTED AT LEFT OUTBOARD ELEVATOR HINGE (ON HORIZONTAL STABILIZER). REMOVED ELEVATORS AND FOUND HINGE CRACKED APPROXIMATELY '.25 INCH' VERTICALLY. HINGE WAS REPLACED.SDR DL72W961308Doubler · crackedREPAIR DOUBLER CRACKED RT ELEV 3RD FROM O/B HINGE RIB. REPAIRED PER M/M 55-10-31.SDR DL72S961471Hinge Ftg · crackedTHE REAR SPAR OF THE LT ELEVATOR WAS FOUND CRACKED ON THE I/B SIDE OF THE THIRD FROM O/B HINGE FITTING. MODIFIED PER B727 S/B 727-55-0087, REV 1.SDR HEEA967123Elevator · chafedELEVATOR LEADING EDGE CHAFED BEYOND LIMITS AT OUTBOARD END. REPLACED WITH SERVICEABLE PART.SDR C2XA96IA109Fittings · wornIAH - DURING C-CHECK INSPECTION, THE ELEVATOR PITCH COUPLE FITTINGS WERE FOUND TO HAVE PLAY. MAINTENANCE REMOVED AND REPLACED THE BELLCRANK COUPLING AND SHEAR PIN, AND THE AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT TT: 18,278.2 HRS. CYCLES, 21,241. (X)SDR 96ZZZX2302Elevator · fabric missingTHE PILOT REPORTED AT APPROXIMATELY 100 MILES FROM BNA, EN ROUTE FROM CVG, THAT HE EXPERIENCED A HARD NOSE DOWN ELEVATOR CONDITION AND SOME AIRFRAME VIBRATION. THE PILOT ADJUSTED ELEVATOR TRIM TO HELP THE NOSE DOWN CONDITION AND TRIED TO ISOLATE THE VIBRATIONSDR HEEA967050Elevator Assy · flange crackedMOUNTING FLANGE THATS BONDED TO SPAR IS CRACKED FROM SPAR TOWARDS OUTER FLANGE. SCRAPPED ELEVATOR ASSEMBLY.SDR IXXA9667Hinge Flange · bentDURING ROUTINE C-CHECK INSPECTION, THE LEFT ELEVATOR, NR 4 HINGE FLANGE WAS FOUND BENT. THE DAMAGED AREA WAS REMOVED IAW THE AIRCRAFT SERVICE REPAIR MANUAL. (X)SDR AU960685Pin · displaced(AUS) RH ELEVATOR TRIM TAB HINGE PIN MOVED INBOARDSDR MWEA96096Skin · lightning strikeFOUND LT ELEVATOR UPPER SKIN HAS LIGHTNING STRIKE DAMAGE ON FIBERGLASS TRAILING EDGE NEAR OUTBD END. INSTALLED REPAIR IAW SRM 55-03 FIG 15, WEIGHT AND BAL COMPLIED WITH.SDR 96ZZZX1982Elevator · crackedRIGHT SYNC ELEVATOR CRACKS SHOWED ALONG EDGE OF INBOARD RIB. RIB PN 109-8200-02-59 AND PN 109-0200-04-7. FURTHER DISASSEMBLY REVEALED CRACKS IN FORWARD SPAR AND SPAR DOUBLER PN 109-0200-02-49 AND AFT SPAR AND DOUBLER PN 109-0200-02-33. CRACKING APPEARS TO DSDR 96ZZZX1981Elevator · crackedLEFT SYNC ELEVATOR SHOWED CRACKS ALONG EDGE AND INTO ATTACH FITTING HOLES. RIB PN 109-0200-04-7 AND PN 109-0200-02-59. FURTHER DISASSEMBLY REVEALED CRACKS IN FORWARD SPAR AND SPAR DOUBLER PN 104-0200-02-49 AND AFT SPAR AND AFT SPAR DOUBLER PN 109-0200-02-33.SDR AU960395Elevator · deteriorated(AUS) LH ELEVATOR UNSERVICEABLE DUE TO POOR CONDITION AND FABRIC DETERIORATION - DRAIN HOLES WERE BLOCKED AND WATER WAS TRAPPED INSIDESDR AU960394Bracket · corroded(AUS) ELEVATOR STOP BRACKET AND INBOARD ELEVATOR ATTACHMENT BRACKET RIBS CORRODEDSDR AU960392Hinge · worn(AUS) LH ELEVATOR MID AND OUTBOARD HINGES EXCESSIVELY WORN - APPROXIMATELY 25.4MM (1IN) MOVEMENT FORWARD AND AFT - INBOARDELEVATOR ATTACHMENT BRACKET PNO 1115188 WAS FOUND WITH HEAVY EXFOLIATION CORROSION - BEARING WAS ALSO UNSERVICEABLESDR 96ZZZX1154Bolt · wrong lengthDURING A RECENT 2,400 HOUR-INSPECTION, THE LT ELEVATOR UPPER MID-ATTACH HINGE SEAL BOLTS WERE REPLACED WITH 5 EACH, DHS 1465-2DD, PER MOD 253410A DRAWING. AT 84 HRS FROM INSP DURING A PILOT PREFLT CHECK, A BINDING, AND SUBSEQUENT INSP REVEALED AT EXTREME AFT SDR 96ZZZM493Fittings · crackedDURING C-CHECK, FOUND RIGHT ELEVATOR HINGE SUPPORT FITTINGS ARE CRACKED AT STATION 50.5 AND 66.5 AS SEEN THROUGH ACCESS PANELS ON BOTTOM SIDE OF ELEVATOR AS PER MM CHAP 27-50-5. INSTALLED THE REPLACEMENT ELEVATOR AS PER MM CHAP 27-30-5. INSTALLED ELEVATOR BASDR P5CA9600037Elevator · crackedFOUND INBOARD AFT CORNER OF LEFT HAND INBOARD ELEVATOR CRACKED. REPAIRED IAW SRM 51-40-09.SDR MALA964832Clip · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK IN A CLIP FOR THE LEFT ELEVATOR CLOSE-OUT FAIRING END RIB. REPAIRS WERE COMPLETED BY REPLACING THE PART IAW FAC SRM 51-40-01 AND SRM 51-30-03. (X)SDR P5CA9600173Weight · corrodedFOUND LT OUTBOARD ELEVATOR WEIGHT AT STA 281.8 WITH LEVEL ONE CORROSION. REMOVED CORROSION, FOUND WITHIN LIMITS, REF SRM 51-20-03.SDR P5CA9600172Weight · corrodedBALANCE WEIGHT ON RT OUTBOARD ELEVATOR STA 306.8 HAD LEVEL 1 CORROSION. CORROSION REMOVED AND FOUND WITHIN LIMITS, REF SRM 51-20-03.SDR A6WR95055Bolt · corrodedDURING STRUCTURAL INSPECTION, FOUND RIGHT ELEVATOR NR 2 HINGE A-FRAME UPPER BOLT CORRODED. REPLACED BOLT. (X)SDR A6WR95054Bolt · corrodedDURING STRUCTURAL INSPECTION, FOUND RT ELEVATOR NR 1 HINGE A-FRAME LOWER BOLT CORRODED. REPLACED BOLT. (X)
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