JASC 5523

Service difficulty reports · 1,033

Reports filed under 5523 · Elevator, Tab 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 = '5523'
  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 EISA20010010Skin · damagedDURING ROUTINE C-CHECK INSPECTION FOUND HOLE IN LT ELEVATOR TAB UPPER SURFACE. CLEANED PREPPED AND POTTED .250 DIAMETER AREA, ALODINED, PRIMED, AND PAINTED. WEIGHT AND BALANCE IAW SRM 51-40-6 FIG 35, 51-10-2, 51-80-9 PG 1, 51-80 FIG 2, AND M/M 27-30-1.Feb 2, 2001 · N314NE · Boeing 727223SDR DHL2001367504Structure · damagedC-CHECK, LT ELEVATOR TIP OUTBOARD DAMAGE TO AFT 3 FASTENERS DUE TO POSSIBLE LIGHTNING STRIKE. DAMAGE TO ELEVATOR TIP REPAIRED IAW SRM 51-42-20. NR 78820Jan 26, 2001 · N367DH · Airbus A300B4203SDR 20001219SH011Attach Fitting · crackedSTEEL HORN WITH BRAZED IN BUSHING CRACK ON HORN ONLY NOT INTO BUSHING. CAUSE UNKNOWN. (X)Dec 1, 2000 · N1025T · Beech E55SDR 20001206SH019Attach Fitting · crackedSTEEL HORN WITH BRAZED BUSHING CRACK ON HORN ONLY, NOT INTO BUSHING. CAUSE UNKNOWN. (X)Dec 1, 2000 · N1025T · Beech E55SDR AU001085Trim Tab · cracked(AUS) ELEVATOR TRIM TAB CRACKED AND FAILED IN THE AREA AROUND THE HORN. (X)Nov 9, 2000 · Cessna U206ASDR SWAA002231Structure · wornDURING SCHEDULED C2 CHECK, FOUND RT ELEVATOR TRIM TAB INBOARD ATTACH HINGE WORN. REMOVED AND REPLACED TRIM TAB PER MM.Nov 5, 2000 · N687SW · Boeing 7373Q8SDR SWAA002012Tab · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT ELEVATOR TAB DELAMINATED ON T/E. REMOVED AND REPLACED TAB ASSY PER MM.Oct 13, 2000 · N654SW · Boeing 7373H4SDR CALA0001518Panel · corrodedINSPECTION FOUND LT ELEVATOR O/B GEAR TAB MECHANISM PANEL CORRODED AROUND DIMPLED FASTENER HOLES AND ONE FASTENER HOLE WAS CRACKED. THE PANEL WAS REMOVED AND A REPLACEMENT WAS INSTALLED IAW 51-30-2.Oct 8, 2000 · N35888 · Doug DC982SDR SWAA001649Fitting · crackedDURING SCHEDULED C1 CHECK, FOUND LT ELEVATOR TAB MAST ATTACH FITTING CRACKED. REMOVED AND REPLACED ELEVATOR TAB PER MM.Aug 31, 2000 · N706SW · Boeing 7377H4SDR USAASB00230Bolt · wornCLT - FLT 309 - ON CLIMB-OUT FROM CLT, ACCELERATING ABOVE 280 KNOTS, CREW NOTED A FLUTTER IN FLIGHT CONTROLS. FLIGHT ATTENDANT REPORTED A STRONGER VIBRATION IN TAIL AREA. AS AIRSPEED INCREASED, FREQUENCY AND INTENSITY OF VIBRATION INCREASED. CREW SLOWED AIRAug 26, 2000 · N434US · Boeing 7374B7SDR COMA0060659Bushing · wornTHE VERTICAL STABILIZER LEFT HAND AND RIGHT HAND BUSHINGS WERE FOUND WORN DURING ACCOMPLISHMENT OF COMAIR EO 55-007. PERFORMED A MAJOR REPAIR BY INSTALLING BUSHINGS (P/N 60-21061-7) IN LEFT HAND AND RIGHT HAND VERTICAL STABILIZER LUGS IAW WVAC EO 601R-55-1608Aug 19, 2000 · N805CA · Cndair CL6002B19SDR COMA0060666Bushing · wornLEFT HAND AND RIGHT HAND VERTICAL STABILIZER FITTING BUSHINGS WERE FOUND TO BE WORN. PERFORMED A MAJOR REPAIR BY REPLACING LEFT HAND AND RIGHT HAND VERT STAB FITTING BUSHING WITH P/H 600-21061-7 IAW WVAC EO 601R-55-1594 AND CRJ AMM 20-26-00-910-803.Aug 15, 2000 · N804CA · Cndair CL6002B19SDR CALA0001260Tab · delaminatedINSPECTION FOUND RT ELEVATOR ANTI-FLOAT TAB DELAMINATED AT O/B UPPER SIDE. THE DELAMINATED AREA WAS CUT OUT IAW SRM 51-70-2. REPAIR CORE AND WEDGE DOUBLER WERE BONDED IAW SRM 51-70-2. DEFLASHED BOND AND APPLIED FILLET SEAL IAW SRM 51-70-2. BALANCED TAB IAWAug 14, 2000 · N35832 · Doug DC982SDR COMA0060675Bushing · damagedTHE RIGHT HAND VERTICAL STABILIZER HINGE BUSHING LVG WAS FOUND TO BE OVERSIZED 1.7025 INCH. PERFORMED A MAJOR REPAIR BY INSTALLING OVERSIZED BUSHING IN VERTICAL STABILIZER RIGHT HAND LVG IAW CRJ REO 601R-55-31-017.Aug 11, 2000 · N978CA · Cndair CL6002B19SDR COMA0060667Bushing · scoredTHE LEFT HAND VERTICAL STABILIZER HINGE BUSHING WAS FOUND DAMAGED. REPLACED DAMAGED VERTICAL STABILIZER HINGE BUSHING (LT) IAW WVAC EO 601R-55-1579A.Aug 11, 2000 · N978CA · Cndair CL6002B19SDR CA000720005Tab · loose(CAN) WHILE CARRYING OUT THE 100 HOUR INSPECTION OF THE SERVO TAB, THE ENGINEER NOTICED THAT THERE WAS EXCESSIVE PLAY IN THE ELEVATOR SERVO TAB OPERATING LEVER. UPON FURTHER INVESTIGATION, FOUND THE SERVO TAB HAD TO BE REPLACED DUE TO WEAR ON THE OPERATING LEJul 14, 2000 · Dhav DHC3SDR USAA001147Skin · crackedPIT - FOUND LEFT TAB SKIN CRACKED IN 3 PLACES .25 INCH, .5 INCH AND .25 INCHES LONG, LEFT ELEV TAB 3 MOST OUTBOARD HINGE CUTOUTS. RADIUS OUT CRACKS PER SRM 55-20-01. (M)Jul 12, 2000 · N517AU · Boeing 7373B7SDR USAASB00181Structure · crackedPIT - FLT 9234 - EN ROUTE FROM ROC-CMH, CAPTAIN REPORTED AN AIRFRAME VIBRATION WHICH WAS FELT IN THE AFT GALLEY/LAVATORY AREA. VIBRATION WAS OF HIGH FREQUENCY AND MODERATE FROM 5,000 TO 31,000 FEET BETWEEN 220 TO 300 KNOTS. CAPTAIN ACCOMPLISHED TROUBLESHOOTIJun 29, 2000 · N562AU · Boeing 737301SDR 20001005AP002Bushing · wornBUF - FLT 1804 - DURING CLIMB-OUT FROM BUF, AT FL100 AND ACCELERATING THROUGH 260 KNOTS, THE AIRCRAFT BEGAN EXPERIENCING AND AIRFRAME VIBRATION. CREW SLOWED AIRCRAFT TO 230 KNOTS BUT VIBRATION CONTINUED. CREW THEN RAISED SPOILERS AND VIBRATION LESSENED. FLIJun 15, 2000 · N412US · Boeing 737401SDR USAASB00168Bolt · wornBUF - FLT 1804 - DURING CLIMB-OUT FROM BUF, AT FL100 AND ACCELERATING THROUGH 260 KNOTS, THE AIRCRAFT BEGAN EXTERIENCING AND AIRFRAME VIBRATION. CREW SLOWED AIRCRAFT TO 230 KNOTS BUT VIBRATION CONTINUED. CREW THEN RAISED SPOILERS AND VIBRATION LESSENED. FLIJun 15, 2000 · N412US · Boeing 737401SDR SWAA001011Tab · delaminatedDURING SCHEDULED 1/2D CHECK, FOUND RT ELEVATOR TAB DELAMINATED AT T/E. REMOVED AND REPLACED TAB ASSY PER MM.Jun 2, 2000 · N606SW · Boeing 7373H4SDR AU000423Trim Tab · distorted(AUS) RIGHT ELEVATOR TRIM TAB DISTORTED, SPLIT AND BULGED. INVESTIGATION FOUND THAT THE CORE HAD BEEN FILLED WITH EXPANDABLE FOAM WHICH HAD CONTINUED TO EXPAND AFTER FILLING THE AVAILABLE SPACE. UNAPPROVED PART.May 31, 2000 · Cessna U206FSDR SWAA000710Skin · crackedDURING SCHEDULED 1/2 D CHECK, FOUND LT ELEVATOR TAB LOWER SKIN CRACKED AROUND NR 3 AND NR 4 HINGE BEARING CUTOUTS. R & R TAB ASSY PER MM.Apr 13, 2000 · N662SW · Boeing 7373H4SDR SWAA000588Hinge · wornDURING SCHEDULED C2 CHECK, FOUND BOTH LT AND RT ELEVATOR TABS INBD HINGES WITH EXCESSIVE PLAY. R&R BOTH ELEVATOR TABS PER MM.Mar 29, 2000 · N332W · Boeing 7373H4SDR ABXA000146Skin · crackedFOUND RIGHT ELEVATOR CONTROL TAB SKIN CRACKED AT NR 4 BEARING ASSY BRACKET. REPLACED CONTROL TAB IAW DC9 MM 27-30-03.Mar 13, 2000 · N983AX · Doug DC932SDR SWAA000433Bearing · wornDURING SCHEDULED D-CHECK, FOUND BOTH LT AND RT ELEVATOR TRIM TAB INBD AND OUTBD ACTUATOR ROD END BEARINGS WORN. REMOVED AND REPLACED ROD ENDS AND BEARINGS PER MM.Mar 7, 2000 · N82SW · Boeing 7372H4SDR F3LA00016Trim Tab · out of toleranceDEN - DURING C-5 CHECK, INSPECTION REPORTED LT ELEVATOR TRIM TAB OUT OF TOLERANCE AT ELEVATOR HINGE LOCATION. REPLACED LT ELEVATOR TRIM TAB PER MM 27-31-31 AND BOEING SERVICE BULLETIN 737-55-1049. (M)Mar 1, 2000 · Boeing 737317SDR F3LA00017Bearing · out of toleranceDURING C-5 CHECK, INSPECTION REPORTED RIGHT ELEVATOR TRIM TAB OUTBOARD BEARING OUT OF TOLERANCE. REPLACED RIGHT ELEVATOR TRIM TAB PER MM 27-31-31 AND BOEING SERVICE BULLETIN 737-55-1049. (M)Feb 6, 2000 · Boeing 737317SDR SWAA000051Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR TAB CRACKED ON UPPER SKIN AT INBOARD HINGE FITTING CUT OUT. REMOVED AND REPLACED RT ELEVATOR TAB ASSY PER MM.Jan 7, 2000 · N331SW · Boeing 7373H4SDR 99ZZZX4696Screw · corrodedSCREWS (P/N'S MS35206-251 AND MS35206-333) SECURING ELEVATOR TRIM TAB HORN, SEVERELY CORRODED AND RUSTED AWAY TO A THICKNESS NO LARGER THAN A PENCIL LEAD. THE SPANNER BLOCK THEY PASS THROUGH WAS CRACKED AND IN TWO PIECES WHEN REMOVED.Dec 20, 1999 · N5338C · Cessna 310RSDR 99ZZZX4695Screw · corrodedSCREWS (P/N'S MS35206-251 AND MS35206-333) SECURING ELEVATOR TRIM TAB HORN, SEVERELY CORRODED AND RUSTED AWAY TO A THICKNESS NO LARGER THAN A PENCIL LEAD. THE SPANNER BLOCK THEY PASS THROUGH WAS CRACKED AND IN TWO PIECES WHEN REMOVED.Dec 20, 1999 · N5338C · Cessna 310RSDR MWEA99812Skin · dentedLEFT HAND ELEVATOR GEARED TAB HAS SMALL DENT ON TOP SURFACE. MTC FABRICATED AND INSTALLED DOUBLER FOR THE LEFT HAND ELEVATOR GEARED TAB.Nov 16, 1999 · N300ME · Doug DC915SDR SWAA991819Bushing · failedAIRCRAFT VIBRATION AT 295 KNOTS AND ABOVE DURING LEVEL FLIGHT AND NO BANKS. REMOVED AND REPLACED RT ELEVATOR TAB ASSY AND HINGE ATTACH FITTING BUSHINGS PER MM.Oct 29, 1999 · N700GS · Boeing 7377H4SDR 99ZZZX4300Bracket · failedTENSION BRACKET FOR ELEVATOR TRIM INDICATOR CABLE BROKE AND CAUSED TRIM SYSTEM TO BIND COMPLETELY, MAKING TRIM SYSTEM UNMOVABLE.Oct 25, 1999 · N48RK · Beech F33ASDR 2000ZZZX709Gear Tab · dentedRT ELEVATOR GEAR TAB DAMAGED DENT/CREASE. REPAIRED RT ELEVATOR GEAR TAB PER EO 99-136 WITH APPROVED 8110-3 DATED 10-15-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)Oct 25, 1999 · N812TC · Doug DC8F55SDR F3LA99165Bracket · crackedDEN - DURING C-7 CHECK, INSPECTION REPORTED RT ELEVATOR TOP OUTBOARD HINGE COVER BRACKET CRACKED. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2 AND 51-40-3. (M)Oct 24, 1999 · N1PC · Boeing 7372P6SDR TWAA0000204Skin · delaminatedDURING OP 16 MAINT CHECK, FOUND LT ELEVATOR CONTOL TAB WITH DELAMINATION AT THE INBD AREA. CONTROL TAB SENT TO SHOP FOR OVERHAUL. DELAMINATION REPAIRED PER SRM 55-04, PAGE 5 TO 7.Oct 5, 1999 · N950U · Doug DC982SDR CA991007082Servo Tab · cracked(CAN) DURING INSPECTION, ELEVATOR SERVO TAB WAS FOUND CRACKED. TAB REPLACED.Sep 24, 1999 · Dhav DHC3SDR UPS99230710Skin · dentedINSPECTION TYPE:C SMALL DENT ON LWR SKIN OF LT ELEV TAB AT OUTBOARD END. REPAIRED IAW SRM 51-40-6 FIG 39.Sep 14, 1999 · N924UP · Boeing 72731CSDR SWAA991466Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND LEFT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED ELEVATOR TAB PER MM.Sep 1, 1999 · N693SW · Boeing 737317SDR CALA9901106Skin · dentedINSPECTION FOUND THE LT ELEVATOR GEAR TRIM TAB DENTED AT I/B TRAILING EDGE. THE TRIM TAB WAS REMOVED, REPAIRED AND REINSTALLED IAW MM 27-30-04.Aug 30, 1999 · N69826 · Doug DC982SDR MWEA99542Skin · damagedLEFT ELEVATOR GEARED TAB CENTER ATTACHMENT BEARING IS EXCESSIVELY WORN. MTC REPLACED BEARING, FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR ON TAB SURFACE SKIN.Aug 26, 1999 · N600ME · Doug DC914SDR CALA9900862Fitting · crackedINSPECTION FOUND A .75 INCH CRACK IN LT ELEVATOR TAB MAST ARM FITTING. THE LT ELEVATOR TAB WAS REMOVED AND REPLACED IAW MM 27-31-00 AND 27-31-31. THE TAB WAS RIGGED AND OPERATION WAS NORMAL.Jul 26, 1999 · N23707 · Boeing 737724SDR AU990753Tab · disbonded(AUS) ELEVATOR TRIM TAB TRAILING EDGES DISBONDED.Jul 26, 1999 · Beech 76SDR SWAA991222Tab · crackedDURING SCHEDULED BC4 CHECK, FOUND LT ELEVATOR TAB CRACKED. REMOVED AND REPLACED LT ELEVATOR TAB ASSY PER MM.Jul 21, 1999 · N670SW · Boeing 7373Q8SDR DHL9970218CWeight · crackedC CHECK, LT ELEVATOR TAB HAS BALANCE WEIGHTS CRACKED. REMOVED AND REPLACED LEFT ELEVATOR TAB WEIGHTS BALANCE AS PER S/B 727-55-0040 FIG NR 1, N/R 4004.Jun 20, 1999 · N702DH · Boeing 72730CSDR DHL9970217CWeight · crackedC-CHECK, RT ELEVATOR TAB HAS BALANCE WEIGHT CRACKED. REPLACED RT ELEVATOR TAB BALANCE WEIGHTS PER B727 SRM 51-10-1 PAR 5 AND B727 SRM 51-30-2 AND S/B 727 55-0040 FIG 1, N/R4005.Jun 20, 1999 · N702DH · Boeing 72730CSDR SWAA991037Tab · crackedDURING SCHEDULED SERVICE CHECK, FOUND LT AND RT ELEVATOR TABS WITH NUMEROUS CRACKS AROUND ATTACH POINT CUTOUTS. REMOVED AND REPLACED ELEVATOR TABS PER MM.Jun 16, 1999 · N709SW · Boeing 7377H4SDR SWAA991024Hinge · crackedDURING SCHEDULED SPECIAL CHECK, FOUND RT ELEVATOR TAB MAST FITTING HAS A .125 INCH LONG CRACK ON UPPER OUTBD FLANGE RADIUS. REMOVED AND REPLACED RT ELEVATOR TAB ASSY.Jun 14, 1999 · N707SA · Boeing 7377H4SDR SWAA991025Bushing · wornDURING SCHEDULED SPECIAL CHECK, RT ELEVATOR TAB FAILED BEARING FREEPLAY CHECK. REMOVED AND REPLACED BUSHINGS PER MM.Jun 13, 1999 · N708SW · Boeing 7377H4
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