JASC 5513

Service difficulty reports · 97

Reports filed under 5513 · Horizontal Stabilizer, 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 = '5513'
  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 SWAA2026091494497Blade · crackedCRACK BLADE ACCESS PANEL 333AT ON LT HORIZONTAL STAB. REPLACED BLADE AND FASTENER FOR ACCESS PANEL 333AT IAW SRM 51-40-02.Aug 24, 2026 · N204WN · Boeing 7377H4SDR JR2R202410120002Stringer · damagedRH HORIZ STRINGERS HAVE DRILL MARKSOct 12, 2024 · N87306 · Emb ERJ170200LRSDR SWIA2023042700010Unknown · damagedRH HORIZONTAL STABILIZER UPPER SKIN HAS DAMAGE AT MULTIPLE AREAS AS MARKED. PN 170-62726-016 (C-CHECK RO 4/26/2023) PERFORMED REPAIRS ON NUMEROUS HOLES ON RH HORIZINTAL UPPER SKIN. REF ETD2023-170-009838 REV C. ADDITIONAL WEIGHT COMES OUT TO 304.2G THISApr 17, 2023 · N140SY · Emb ERJ170200LRSDR SWAA2023041024041Seal · cracked-LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] R&R LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL REF AMM 53-31-31.;[02] R&R LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL REF AMM 53-31-31.Apr 6, 2023 · N468WN · Boeing 7377H4SDR 7C7A2023022000014Tab · crackedIN PROCESS OF REPAIRIND DENTED SKIN REAR SPAR OF ELEVATOR TRIM TAB FOUND CRACKEDFeb 20, 2023 · N887EA · Dhav DHC8106SDR SWIA20230206Not Reported · dentedLEFT FUSELAGE STRUCTURE DENTED BY FS169.00 IN BETWEEN RADOME AND ACCESS PANEL 121 AL HAS BEEN EVALUATED AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-31. REFERENCE FOR CP 26143452 FOR INITAL DISCREPANCY. THIS IS A "MAJOR REPAIR". FORM M-337 INITIATED. (FILED CLOFeb 6, 2023 · N770SK · Cndair CL6002C10SDR GTIA2022072136545None · corrodedCORROSION FOUND ON LH ELEVATOR / ACTUATOR FITTING 1 CAT B. RAF-01 2907357-02 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED BORE OF HINGE FITTING #1 OF INBOARD ACTUATOR INBOARD LUG OF LH ELEVATOR IAW SRM 55-26-47-300-002. REPAIR INSPECTION THRESHOLD FROM COMJul 18, 2022 · N536NK · Airbus A319132SDR GTIA2022072136544None · corrodedCORROSION FOUND ON LH ELEVATOR FITTING 5 CAT B. RAF-01 2907359-02 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED BORES OF HINGE FITTING #5 OF LH ELEVATOR IAW SRM 55-26-41-300-004. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS AND SUBSEQUJul 18, 2022 · N536NK · Airbus A319132SDR GTIA2022072136543None · corrodedCORROSION FOUND ON LH ELEVATOR FITTING 3 CAT B. RAF-01 2907359-01 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED BORES OF HINGE FITTING #3 OF LH ELEVATOR IAW SRM 55-26-41-300-004. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS AND SUBSEQUJul 18, 2022 · N536NK · Airbus A319132SDR GTIA2022072136542None · corrodedCORROSION FOUND ON RH ELEVATOR FITTING 2 CAT B. RAF-01 2907361-01 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED HINGE FITTING #2 OF RH ELEVATOR IAW SRM 55-26-41-300-004. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS, AND SUBSEQUENT INSPJul 18, 2022 · N536NK · Airbus A319132SDR GTIA2022072136541None · corrodedCORROSION FOUND ON RH ELEVATOR / ACTUATOR FITTING 2 CAT B. RAF-01 2907358-01 OPENED. SDR REQUIRED.-REPAIRED BORES OF HINGE FITTING #2 OF OUTBOARD ACTUATOR INBOARD LUG OF ELEVATOR RH SIDE IAW SRM 55-26-47-300-002. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRSJul 18, 2022 · N536NK · Airbus A319132SDR GTIA2022072136540None · corrodedCORROSION FOUND ON LH ELEVATOR FITTING 6 CAT B. RAF-01 2907360-01 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED BORES OF HINGE FITTING #6 OF LH ELEVATOR IAW SRM 55-26-41-300-006. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS, AND SUBSEQJul 18, 2022 · N536NK · Airbus A319132SDR GTIA2022072136539None · corrodedCORROSION FOUND ON LH ELEVATOR FITTING #2 CAT B. RAF-01 2907358-02 OPENED. REFR TI 5513-1602. SDR REQUIRED.-REPAIRED BORE OF HINGE FITTING #1 OF INBOARD ACTUATOR INBOARD LUG OF LH LH ELEVATOR IAW SRM 55-26-47-300-002. REPAIR INSPECTION THRESHOLD FROM COMPONENTJul 18, 2022 · N536NK · Airbus A319132SDR GTIA2022072136538None · corrodedCORROSION FOUND ON RH ELEVATOR FITTING 3 CAT B. RAF-01 2907361-02 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED HINGE FITTING #3 OF RH ELEVATOR IAW SRM 55-26-300-004. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS, AND SUBSEQUENT INSPECTJul 18, 2022 · N536NK · Airbus A319132SDR GTIA2022072136537None · corrodedCORROSION FOUND ON RH ELEVATOR FITTING 5 CAT B. RAF-01 2907362-01 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED HINGE FITTING #5 OF RH ELEVATOR IAW SRM 55-26-41-300-004. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS, AND SUBSEQUENT INSPJul 18, 2022 · N536NK · Airbus A319132SDR GTIA2022072136536None · corrodedCORROSION FOUND ON RH ELEVATOR FITTING 6 CAT B. RAF-01 2907362-02 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED HINGE FITTING #6 OF RH ELEVATOR IAW SRM 55-26-41-300-006. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS, AND SUBSEQUENT INSPJul 18, 2022 · N536NK · Airbus A319132SDR GTIA2022072136535None · corrodedCORROSION FOUND ON RH ELEVATOR FITTING 1 CAT B. RAF-01 2907360-02 OPENED. REF TI 5513-1602. SDR REQUIRED.-REPAIRED HINGE FITTING #1 OF RH ELEVATOR IAW SRM 55-26-41-300-004. REPAIR INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT IS 6 YEARS, AND SUBSEQUENT INSPJul 18, 2022 · N536NK · Airbus A319132SDR AALA202207054259Bushing · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY, LEFT HAND HORIZONTAL STABILIZER ELEVATOR TAB, HINGE 6. REPLACED HINGE BUSHINGS PER AMM 27-31-31-000-801 AND AMM 27-31-31-400-801. ACCOMPLISHED SATISFACTORY FREE PLAY CHECK PER AMM 27-31-32-200-805.Jul 3, 2022 · N921NN · Boeing 737SDR AALA202207054025Bushing · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY, LEFT HAND HORIZONTAL STABILIZER ELEVATOR TAB, HINGE 5. REPLACED HINGE BUSHINGS PER AMM 27-31-31-000-801 AND AMM 27-31-31-400-801. ACCOMPLISHED SATISFACTORY FREE PLAY CHECK PER AMM 27-31-32-200-805.Jul 3, 2022 · N921NN · Boeing 737SDR UIEA2022042800413None · noneCORROSION DAMAGES ON RH HST CENTER SECTION UPPER SKIN TOP SURFACE BETWEEN STAB STA 143.6 AND 172.4, STRINGER 3 TO 12(<P>1) REMOVE THE AFFECTED FASTENERS IAW SRM 51.40.02 REV 94 2) BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 94 3) PFM NOT INSP REFER TO JOBApr 30, 2022 · N477MC · Boeing 74747UFSDR AALA202202231340Attach Fitting · gougedAIRCRAFT IN BASE MAINTENANCE: GOUGE IN OUTBD ATTACH FITTING OF LH ELEVATOR CONTROL TAB MECHANISM FROM PREVIOUSLY INSTALLED FASTENER AT STA 36.4, MEASURING D=0.012 IN. REPLACED FITTING WITH NEW IAW B737-NG SRM 55-20-90-1A.Feb 5, 2022 · N930AN · Boeing 737*SDR SWIA202165007None · damagedTOP PLATE FOR 1EA NUTPLATE ON THE RIGHT HORIZONTAL TIP HAS DAMAGE (MARKED) (C-CHECK RO 3/14/2022) REPAIRED TOP PLATE ON RIGHTHAND HORIZONTAL TIP IAW REO 601R-55-11-712 REV -- DATE 2022-02-01 STEPS. 1-9. (SEE CONTINUATION SHEET FOR FURTHER DETAILS) COMPLIDec 29, 2021 · N854AS · Cndair CL6002B19SDR SWIA202165005None · corrodedRH HORIZONAL STAB LE ERODED. (C-CHECK RO 3/14/2022) REMOVED EROSION ON RH HORIZONAL STAB LE, REF. CRJ200 SRM 51-12-00 / COMPLIED WITH REO 601R-55-12-716 REV -- DATE 2022-01-20Dec 29, 2021 · N854AS · Cndair CL6002B19SDR SWIA202163729None · mislocatedL/H HORZONAL STAB TIP PANEL HAS MISLOCATED NUTPLATE ON INBOARD EDGE, THIRD NUTPLATE FWD OF TRAILING EDGE OF STAB TIP. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RIB AND SPLICE WITH NEW FABRICATED PN: 600-23079-S0101 RIB AND PN: 600-23037-22 SPLICE IAW RDec 5, 2021 · N207PS · Cndair CL6002B19SDR A6WA202111187973None · corrodedPAX DOOR FWD ANCHO FITTING PLATE P/N600-38061-11 WAS FOUND CORRODED. THE EXPANSION CAUSED THE PAX DOOR FWD ANCHOR FITTING TO CRACK. ***AIRCRAFT REMOVED FROM SERVICE*** R&R PAX DOOR FWD ANCHOR PLATE AND ALL ATTACHING HARDWARE, FWD PAX DOOR SWIVEL CABLE END, Nov 13, 2021 · N426AW · Cndair CL6002B19SDR SWIA202161978None · damagedFORM M-337 REQUIRED DUE TO DAMAGE ON RH HORIZONTAL STABILIZER IAW REO 601R-55-11-701 (FILED CLOSED) COMPLIED WITH M-337Oct 30, 2021 · N472CA · Cndair CL6002B19SDR SWIA202161977Doubler · damagedINSPECTED R/H HORIZONTAL STABILATOR AND FOUND DAMAGE ON FRAME 9 (3/4 INCH HOLES WHERE TWO NUT PLATES BLEW OUT), SKIN IN RIGHT AFT CORNER (1/2 INCH HOLE) AND DAMAGE ON AFT SPAR (3/4 INCH HOLES WHERE ONE NUT PLATE BLEW OUT). (FILED CLOSED) REPAIRED DAMAGE Oct 30, 2021 · N472CA · Cndair CL6002B19SDR A6WA202110297941None · noneH/STAB PCU ACCESS PANEL #332AB (P/N: 601R23052-11) HAS 3EACH DAMAGED HOLES. DIMENSIONS: HOLE #1: .195" X .258"; HOLE #2: .310" X .220"; HOLE #3: .195" DIA ***AIRCRAFT REMOVED FROM SERVICE*** REAMED HOLES TO FOLLOWING DIMENSIONS: HOLE #1: .3685"; HOLE #2: .37Aug 27, 2021 · N439AW · Cndair CL6002B19SDR SWIA202161700None · dented* R/H HORIZONTAL STABILIZER UPPER SKIN HAS A DENT AT APPROX. HSS100, MARKED. (C-CHECK RO 10/8/2021) PERFORMED CUT OF R/H HORIZONTAL STABILIZER UPPER SKIN AT BETWEEN RIB 7 & RIB 6 AND STGR2 & STGR3 REF CRJ200 SRM 55-11-31. COMPLIED WITH 51-900-1003-SKYAug 10, 2021 · N946SW · Cndair CL6002B19SDR MASA20200727056Tab · damaged(C-CHECK) HSTAB PIVOT FITTING LHS/RHS ANTI-ROTATION TABS DAMAGED. REPAIRED I/A/W SB 670BA-55-012 & 670BA-55-013.Jul 27, 2020 · N927LR · Cndair CL6002D24SDR O2GA2020052801Panel · missingFROZEN STABILIZER TRIM FROZEN NOTICED AT TOP OF DESCENT. TRIM UNFROZE AT LOWER ALTITUDES. DIVERTED TO KVNY. LANDING WAS UNEVENTFUL. MAINTENANCE FOUND THE LEFT TRIM TAB ACTUATOR PANEL MISSING FROM THE TOP OF THE STAB. STAB TRIM ACTUATOR WAS LUBRICATED, PANEL WAMay 16, 2020 · N885UP · Beech B300SDR BIER2020042700000Balance Weight · rustedDURING ANNUAL INSPECTION BY CRS # BIER466C, FOUND BALANCE WEIGHT ASSEMBLY P/N 38398-005 RUSTED THROUGH. RECEIVED NEW PIPER PART NUMBER 38398-005 AS REPLACEMENT. THE NEW ASSEMBLY COMES CONSIDERABLY OVER-SIZED. ADDRESS THE ISSUE WITH PIPER DSA TOM PENTECOST (DSAApr 27, 2020 · N8187H · Piper PA44180TSDR DALA2017041302974Tab · dentedHORIZONTAL STABILIZER DENTED ON THE LT & RT ANTI FLOAT TAB UPPER SURFACE. THE ANTI FLOAT TABS WERE REPAIRED IAW SRM 55-04 P. 3.Apr 12, 2017 · N917DL · Doug MD88SDR DALA2017040702796Skin · delaminatedHORIZONTAL STABILIZER, DELAMINATION ON LT ANTI-FLOAT TAB UPPER/LOWER SURFACE. ANTI-FLOAT TAB WAS REPAIRED PER SRM 55-04 P 3.Apr 6, 2017 · N917DL · Doug MD88SDR DALA2017032302332Tab · dentedHORIZONTAL STABILIZER, DENT 1EA ON LT CONTROL TAB NEAR STA XHS= 68. LT CONTROL TAB NEAR STA XHS= 68 WAS REPAIRED PER SRM 55-04 FIGURE 2.Mar 22, 2017 · N912DE · Doug MD88SDR DALA2017032302331Tab · damagedHORIZONTAL STABILIZER, PROTUBERANCE ON LT CONTROL TAB NEAR STA XHS= 86. LT CONTROL TAB NEAR STA XHS= 86 WAS REPAIRED PER SRM 55-04 PAR 3 CLASS A.Mar 22, 2017 · N912DE · Doug MD88SDR WVER201503200003Tab · gougedRT HORIZONTAL ANTI-ROTATION TAB IS GOUGED FROM CONTACT WITH THE HORIZONTAL STABILIZER PIVOT PIN HARDWARE. REMOVED TAB IAW REO 670BA-55-012, PARTS A & B, REV D. NOTE: LT TAB HAS BEEN PREVIOUSLY REMOVED UNDER THE SAME REO.Mar 20, 2015 · N925FJ · Cndair CL6002D24SDR ASOA2014091611223Tab · chafedCHAFE DAMAGE ON LT AND RT ANTI-ROTATION TABS OF THE HORIZONTAL STABILIZER. COMPLIED WITH EC/TC SB 670BA-55-012 01,02,03.Sep 6, 2014 · N753EV · Cndair CL6002C10SDR DALA13034239205Mechanism · gougedRIGHT HORIZONTAL STABILIZER L/E FLOAT TAB MECHANISM GOUGED. REPAIRED IAW ERA 514984-14, REV O AND FINAL ERA 514894-14, REV O.Jul 9, 2013 · N905DA · Doug MD9030SDR DALA13034249205Bracket · gougedLEFT HORIZONTAL STABILIZER FLOAT TAB BRACKET GOUGED. REPAIRED IAW ERA 514894-14, REV O.Jul 7, 2013 · N905DA · Doug MD9030SDR A6WA201141102Fitting · damagedHORZONTAL STAB PIVOT FITTING DAMAGED ON LT INBD FWD FACE. BLENDED DAMAGED AREA NDT INSPECTION FLAP PEENED, ALODINED, PRIMED IAW REO 601R-55-11-392.Nov 3, 2011 · N470ZW · Cndair CL6002B19SDR A6WA201141101Pivot · damagedHORZONTAL STAB TRIM ACTUATOR PIVOT STRUCTURE DAMAGED ON LT OTBD FACE. BLENDED DAMAGED AREA NDT INSPECTION PRIMED IAW REO 601R-55-31-220.Nov 3, 2011 · N470ZW · Cndair CL6002B19SDR DALA1119700916Skin · dentedDURING HMV A DENT WAS FOUND ON UPPER SKIN OF RT GEARED TAB. GEARED TAB WAS REPAIRED IAW SRM 55-04 PAR 3A.Mar 17, 2011 · N916DL · Doug MD88SDR DLM88091321Tab · corrodedDURING SHOP VISIT THE SUBJECT HORIZONTAL STABILIZER ELEVATOR ANTI-FLOAT TAB WAS FOUND WITH CORROSION. REPAIRED PER ERA 474926-14.Aug 12, 2009 · N910DL · Doug MD88SDR QXEA2009051100321Tab · damagedDAMAGED LT AND RT ANTI ROTATION TABS OF THE HORIZ STAB PIVOT FITTING P/N AV670-23120, REMOVED PANELS 326CL AND 326CR. REMOVED HORIZ STAB PIVOT BOLT INNER PIN AND LT OUTER PIN, TRIMMED CHAFED LT LOCK TAB IAW TC REO 670-55-11-099 GENERAL NOTES 1-3. COMPLIED May 8, 2009 · N600QX · Cndair CL6002C10SDR SWAA060864Tab · crackedDURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR TAB CRACKED AT NR 2 HINGE CUTOUT. REMOVED AND REPLACED TAB PER MM.Mar 16, 2006 · N305SW · Boeing 7373H4SDR 05FDEA00499Splice · corrodedCORROSION ON STRINGER SPLICE AT BS 678 STRINGER 28L. INSTALLED NEW STRINGER SPLICE AT BS 678, STR 28L IAW SRM 51-30-2 & SRM 51-10-2.Mar 11, 2005 · N481FE · Boeing 727200SDR WRLA2005031Spar Cap · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 36.Feb 18, 2005 · N276 · Doug MD11FSDR WRLA2005032Spar Cap · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 01.Feb 17, 2005 · N276 · Doug MD11FSDR WRLA2005037Skin · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 31.Feb 11, 2005 · N276 · Doug MD11F
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