JASC 5524
Service difficulty reports · 324
Reports filed under 5524 · Elevator Miscellaneous 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 = '5524' 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 = '5524' 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 P762004F00002Bracket · crackedLT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT.SDR P762004F00001Bracket · crackedLT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT.SDR P762004F00000Bracket · crackedLT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT.SDR ARWA20040105Attach Fitting · looseDURING PREFLIGHT FOUND ELEVATOR STARBOARD SIDE UP SLIGHTLY AND PORT SIDE SLIGHTLY DOWN, SLIGHT DIFFERENCE IN TRAVEL BETWEEN PORT AND STARBOARD SIDE ELEVATORS. FOUND LOOSE ATTACHMENT AT PORT SIDE ELEVATOR ATTACHMENT TO TORQUE TUBE. PERFORMED ELEVATOR INSPECTISDR COMA0360581Hinge Fitting · chafedRIGHT ELEVATOR NR 1 HINGE POINT ON THE HORIZONTAL IS CHAFED. REPAIRED BY BLENDING CHAFED AREA SMOOTH, PERFORMED LIQUID PENETRANT INSPECTION, ROTO/FLAP PEEN REWORKED AREA IAW CNDAIR SRM 51-24-11, AND TREATED AREA WITH ALODINE, ALL WORK PERFORMED IAW WVAC EO 60SDR AUS20031258Stud · corroded(AUS) LT ELEVATOR FORWARD CONTROL CABLE FAILED. CABLE LOCKING STUD CORRODED. CONTROL WHEEL HAD BEEN RESTRAINED WITH SEAT BELT AND CABLE LOCK STUD FAILED DUE TO WIND GUSTS.SDR ASAA0340343Fitting · gougedGYR - DURING SI CHECK, FOUND LEFT ELEVATOR HINGE FITTING WORN AT STAB STA 213.43. REPAIRED IAW EA. (M)SDR CA031031005Hinge · worn(CAN) RT ELEVATOR OB HINGE ASSY BOLT HOLE IS WORN AND OBLONGED IN SHAPE AS WELL AS THE HINGES INNER FACES ARE GROOVED FROM BUSHING. NOTE THAT BUSHING IS NOT SE IZED IN THE BEARING ASSY ON THE ADJOINING HORIZONTAL STAB HINGE.SDR A6WA200360041Bracket · improperLEFT ELEVATOR NR 2 HINGE 'A' FRAME TOP MOUNTING BOLT HAS AN IMPROPER SAFETY BRACKET, POORLY MANUFACTURED. REPLACED WITH NWE PART NR HC551B0098-000. (M)SDR C2XA03TY090Fitting · lightning strikeA/C 962 WAS FERRIED TO TYS AFTER A PRELIMIARY INSPECTION FOUND A/C SATISFACTORY FOR A FERRY FLIGHT. MAINTENANCE REMOVED AND REPLACED THE RT ELEVATOR TRAILING EDGE FITTING; CUT OUT THE DAMAGED AREA AND FAB A DOUBLER, FILLER AND INSTALLED; ALODINED PRIMED AND PSDR MWEA030147Access Panel · damagedRIGHT ELEVATOR UPPER ACCESS PANEL 3632 DOUBLER DAMAGED AT INBOARD SCREW HOLE. FABRICATED AND INSTALLED DOUBLER AND FILLER AND BALANCED ELEVATOR.SDR 2002FA0001367Skin · will not balanceAIRCRAFT REPORTED AS NOT HAVING ENOUGH NOSE DOWN TRIM IN CRUISE FLIGHT. AFTER INSPECTION IT WAS NOTED THAT THE TRAILING EDGE OF THE LT ELEVATOR WAS CONTOURED DOWN AND A CHECK OF THE BALANCE SHOWED IT TO BE 'UNDERBALANCED' BY ALMOST TWO INCH POUNDS. THE TRAILINSDR SWAA022636Bearing · wornDURING SCHEDULED C4 CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR CONTROL PUSH ROD AFT BEARING PER MM.SDR SWIA200211266Bushing · wornPILOT REPORTS OSCILLATIONS ON CLIMB AND IN THE PITCH AT AIR SPEED OF 284 KTS TO 290 KTS. REMOVED & REPLACED HARDWARE & BUSHINGS ON ALL 6 ELEVATOR PCU'S ROD END SIDE. OPS CHECK GOOD.SDR C2XA02IA186Hinge · wornLIT- THE CREW NOTED SEVERE VIBRATIONS IN BOTH YOKES IN FLIGHT. DECLARED EMERGENCY AND THE FLIGHT WAS DIVERTED TO LIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ELEVATOR IAW EMB145 AMM 27-30-00, OPS CHECK GOOD. THE AIRCRAFT WAS APSDR C2XA02IA187Hinge · wornLIT- THE CREW NOTED SEVERE VIBRATIONS IN BOTH YOKES IN FLIGHT. DECLARED EMERGENCY, THE FLIGHT WAS DIVERTED TO LIT, LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT ELEVATOR IAW EMB145 AMM 27-30-00, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVSDR C2XA02IA177Hinge Fitting · wornDURING UNSCHEDULED MAINTENANCE TO IDENTIFY A SOURCE OF INFLIGHT VIBRATION AT OR ABOVE 290 KTS, MAINTENANCE FOUND THE LEFT ELEVATOR TO HAVE WORN HINGE FITTINGS. THE FITTINGS WERE WORN TO THE POINT OF THAT ALLOWED MIGRATION OF A BUSHING INSERT CAUSING PLAY IN TSDR CA020610007Hinge · cracked(CAN) DURING POST FLIGHT WALKAROUND A CRACK WAS NOTICED IN THE ELEVATOR OUTBOARD-HINGE, INBOARD-BRACKET. THIS BRACKET IS THE SUBJECT OF A 100 HOUR REPETITIVE INSPECTION UNDER BN2/SB.259. THE PREVIOUS INSPECTION 90 HOURS EARLIER SHOWED NO PROBLEMS. THE CRACK ESDR MWEA020362Bracket · corrodedLEFT ELEVATOR HORN BALANCE WEIGHT ATTACH BRACKET IS HEAVILY CORRODED WHERE IT ATTACHES TO THE BALANCE WEIGHT. REMOVED AND REPLACED ATTACH BRACKET.SDR GAIA02046STAngle · crackedDURING A CPCP INSPECTION, IT WAS DISCOVERED THAT LEFT ELEVATOR INTERIOR Z ANGLE IS CRACKED AT ELEVATOR STATION 20.0. ACCOMPLISHED ELEVATOR Z ANGLE REPLACEMENT AT LEFT ELEVATOR STATION 20.0 IAW SRM.SDR GAIA02045STAngle · crackedDURING A CPCP INSPECTION, IT WAS DISCOVERED THAT RIGHT ELEVATOR INTERIOR Z ANGLE IS CRACKED AT ELEVATOR STATION 25. ACCOMPLISHED ELEVATOR Z ANGLE REPLACEMENT AT RIGHT ELEVATOR STATION 25.0 IAW SRM.SDR CA020429001Bracket · cracked(CAN) COMPLIED WITH CESSNA CUSTOMER LETTER NO 0423 DATED APRIL 23, 02. (INSPECTION OF LT AND RT ELEVATOR INBD HINGE BRACKETS) ONE BRACKET HAS TWO SURFACES: INBD AND OUTB.FOUND LEFT ELEVATOR INBD HINGE BRACKET CRACKED. INBD CRACK DIMENSION :. 062 INCH OUTB CRASDR CA020607001Hinge Bracket · cracked(CAN) A CRACK OF 0.30 INCHES WAS FOUND IN THE INBOARD SIDE OF THE HINGE BRACKET LOCATED IN THE FORWARD FROM THE TRAILING EDGE UNDER STIFFENER.SDR CA020311005Hinge Pin · loose(CAN) PILOT REPORTED ELEVATOR STICKING IN FLIGHT AND RETURNED TO POINT OF DEPARTURE. UPON INSPECTION IT WAS FOUND THAT LT ELEVATOR TRIM TAB HINGE PIN HAD WORKED OUT AND WAS RUBBING AGAINST TAILCONE. HINGE PIN WAS PUSHED BACK IN AND LOCKWIRED. AIRCRAFT WAS THE
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