JASC 5552

Service difficulty reports · 222

Reports filed under 5552 · Elevator Tab, 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 = '5552'
  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.

SDR CALA0100265Attach Fitting · wornWHEN PERFORMING WORK CARD 99-5550-1-0006 MAINTENANCE FOUND THE LT ELEVATOR TAB MECHANISM O/B TAB ROD ATTACH FITTING WORN AND I/B WAS STARTING TO WEAR. THE LT ELEVATOR TAB MECHANISM ASSEMBLY WAS REMOVED AND REPLACED IAW MM 27-31-34.Mar 29, 2001 · N16217 · Boeing 737824SDR UPS01235104Bracket · crackedINSPECTION TYPE:C+SI, LT ELEV POSITION SENSOR BRACKET ON FRONT SPAR CRACKED. REPLACED IAW MM 20-80-01.Feb 16, 2001 · N941UP · Boeing 72722CSDR CA010112013Hinge Fitting · cracked(CAN) DURING INSPECTION MAINTENANCE FOUND R/H MID ELEVATOR HINGE FITTING CRACKED. FITTING REPLACED.Dec 5, 2000 · Cvac 340CVACSDR DHL200180239CTab · damagedDURING C CHECK FOUND RT ELEVATOR T/E DEFORMED AT STA.XE.168.REMOVED RT ELEVATOR T/E PER SRM 51-1-21A.FABRICATE T/E PER SRM 55-2-1.CLEANED ,TREATED ,AND PRIMED PER SRM 51-1-8B.INSTALLED T/E AS REQUIRED PER SRM 51-1-21ANov 25, 2000 · N802DH · Doug DC873FSDR USAASB00201Fitting · wornCLT - FLT 532 - ON CLIMB-OUT FROM SRQ, EN ROUTE TO CLT, A/C BEGAN TO EXPERIENCE AN AIRFRAME VIBRATION. VIBRATION BECAME ABNORMALLY PRONOUNCED WITH CONSTANT INTENSITY REGARDLESS OF AIRSPEED OR POWER SETTING. VIBRATION WAS MOST EVIDENT IN THE AFT GALLEY AND TAJul 29, 2000 · N408US · Boeing 737401SDR AU000612Bracket · cracked(AUS) ELEVATOR BRACKET CRACKED ALONG THE BEND RADII OF ONE SIDE.Jul 20, 2000 · Bnorm BN2A21SDR AU000319Hinge · corroded(AUS) RIGHT ELEVATOR CENTER HINGE CORRODED.Apr 13, 2000 · Emb EMB110P1SDR AU000314Fitting · worn(AUS) ELEVATOR TRIM FITTING AND HINGE HAD EXCESSIVE PLAY. FURTHER INVESTIGATION FOUND THE TRIM FITTING CRACKED.Mar 13, 2000 · Emb EMB110P1SDR AU000178Bracket · corroded(AUS) ELEVATOR ATTACHMENT BRACKETS CORRODED.Mar 3, 2000 · Doug DC3CS1C3GSDR 2000ZZZX672Fitting · crackedRIGHT ELEVATOR NR 2 A-FRAME CRACKED. REMOVED AND REPLACED NR 2 POSITION A-FRAME RT ELEVATOR IAW DC-8 OHM 27-30-1. (X)Sep 23, 1999 · N812TC · Doug DC8F55SDR 2000ZZZX698Fitting · gougedNR 1 RT ELEVATOR A-FRAME TRAILING EDGE BOLT HOLE BOSS GOUGED. BLENDED GOUGE SMOOTH. TREATED AND PRIMED. ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATD 8-19-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)Aug 23, 1999 · N812TC · Doug DC8F55SDR 2000ZZZX693Fitting · gougedNR 4 RIGHT ELEVATOR A-FRAME AFT MOUNT GOUGED. GOUGE IS A MAXIMUM OF .091 INCH DEEP. BLENDED GOUGE SMOOTH. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-136 WITH APPROVED 8110-3 DATED 8-20-99. REF: ZANTOP INTERNATIONAL AIRLINES, IAug 23, 1999 · N812TC · Doug DC8F55SDR 2000ZZZM212Fitting · gougedNR 4 RIGHT ELEVATOR 'A' FRAME AFT MOUNT GOUGED. GOUGE IS A MAXIMUM OF .019 INCHES DEEP. BLENDED GOUGE SMOOTH. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-136 WITH APPROVED 8110-3 DATED 8/20/99. (M)Aug 23, 1999 · N812TC · Doug DC8F55SDR AU990867Hinge · cracked(AUS) RIGHT ELEVATOR HINGE CRACKED FROM ATTACHMENT BOLT HOLE.Mar 26, 1999 · Socata TB10TOBAGOSDR CALA9801974Bracket · wornINSPECTION FOUND LOOSE BOLTS AND WORN BOLT HOLES IN LT ELEVATOR TAB NR 1,3, AND 4 SUPPORT BRACKETS. THE TAB SUPPORT BRACKETS WERE REMOVED AND REPLACED IAW MM 27-30-11.Oct 17, 1998 · N79748 · Boeing 727224SDR 98ZZZX3144Lock Nut · failedGLIDER LANDED SHORT OF RUNWAY DUE TO NO ELEVATOR CONTROL. INVESTIGATION REVEALED THE BOLT AND LOCKING NUT WERE MISSING FROM BELLCRANK FOR ELEVATOR AT AFT FUSELAGE. ACFT HAD JUST COME OUT OF FACTORY WITH APPROX 4 HRS FLIGHT TIME. NOTE: BOLT WAS FOUND IN FUSJun 26, 1998 · N98NL · Glsdks DG800ASDR CA980608011Bolts · worn(CAN) DURING THE 750 HR FLIGHT CONTROL INSPECTION, IT WAS DISCOVERED THAT 3 OUT OF 6 HINGE BOLTS HOLDING LEFT ELEVATOR TAB IN PLACE WERE SEVERELY WORN. THE ELEVATOR TAB WAS REMOVED AND INSPECTED. HARDWARE WAS REPLACED AS REQUIRED. FURTHER INVESTIGATION IS INMay 22, 1998 · Cvac 340CVACSDR 97ZZZM1069Tab Hinge · wornVIBRATION FELT IN CONTROL YOKE AS WELL AS THROUGHOUT THE AIRCRAFT F/A'S STATE VIBRATION WAS MORE PROMINENT IN AFT OF AIRCRAFT, MORE PROMINENT ON RIGHT SIDE. INSPECTED AND FOUND INBOARD TAB BEARING BLOCK AND FWD HINGE BRACKET WORN, PER MM 27-31-31A. INSPECTEDSep 11, 1997 · N220US · Boeing 7372H5SDR CA970325008Bracket · cracked(CAN) DURING INSPECTION OF LEFT AND RIGHT ELEVATOR ATTACH BRACKETS, THEY WERE BOTH FOUND SEVERELY CRACKED. UNITS EXHIBITED NO DAMAGE DURING PREVIOUS INSPECTION. PROBLEM BELIEVED CAUSED BY EXCEEDING FLAP EXTEND SPEEDS IN AN EFFORT TO SLOW AIRCRAFT.Mar 7, 1997 · Bnorm BN2A27SDR 9605659611Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN A LEFT ELEVATOR GEARED TAB HINGE FITTING. REPLACED FITTING (P/N 3918075-509) PER SRM 51-30-2.Mar 5, 1996 · N611NA · Doug DC932SDR AWXA9500289Hinge Bracket · wornIND-CMH - FLT 280 - CREW REPORTED AIRFRAME VIBRATION AT HIGH SPEED. AIRCRAFT LANDED IN CMH WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND LEFT ELEVATOR TRIM TAB ATTACH BEARINGS WORN. REMOVED AND REPLACED LT TAB NR 1 HINGE BRACKET AND HARDWARE, AND REINSTALLED May 12, 1995 · N166AW · Boeing 73733ASDR MRKA9540Attach Plate · looseDURING C-INSPECTION, THE LEFT OUTBOARD ELEVATOR HINGE ATTACH PLATES WERE FOUND LOOSE AND FRETTING, WHERE THEY ATTACH TO THE AFT END OF THE STABILIZER RIB AT STATION 213.32. THE HINGE ATTACH PLATES WERE REPLACED AND THE RIB END FITTING REPAIRED PER S/B 737-55-Mar 21, 1995 · N2FOR · Boeing 7374Y0
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