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.
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
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 SWAA2026091494497Blade · crackedCRACK BLADE ACCESS PANEL 333AT ON LT HORIZONTAL STAB. REPLACED BLADE AND FASTENER FOR ACCESS PANEL 333AT IAW SRM 51-40-02.SDR JR2R202410120002Stringer · damagedRH HORIZ STRINGERS HAVE DRILL MARKSSDR 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 THISSDR 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.SDR 7C7A2023022000014Tab · crackedIN PROCESS OF REPAIRIND DENTED SKIN REAR SPAR OF ELEVATOR TRIM TAB FOUND CRACKEDSDR 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 CLOSDR 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 COMSDR 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 SUBSEQUSDR 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 SUBSEQUSDR 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 INSPSDR 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 FIRSSDR 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 SUBSEQSDR 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 COMPONENTSDR 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 INSPECTSDR 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 INSPSDR 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 INSPSDR 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 INSPSDR 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.SDR 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.SDR 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 JOBSDR 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.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) COMPLISDR 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 2022-01-20SDR 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 RSDR 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, SDR SWIA202161978None · damagedFORM M-337 REQUIRED DUE TO DAMAGE ON RH HORIZONTAL STABILIZER IAW REO 601R-55-11-701 (FILED CLOSED) COMPLIED WITH M-337SDR 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 SDR 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: .37SDR 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-SKYSDR MASA20200727056Tab · damaged(C-CHECK) HSTAB PIVOT FITTING LHS/RHS ANTI-ROTATION TABS DAMAGED. REPAIRED I/A/W SB 670BA-55-012 & 670BA-55-013.SDR 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 WASDR 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 (DSASDR 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.SDR DALA2017040702796Skin · delaminatedHORIZONTAL STABILIZER, DELAMINATION ON LT ANTI-FLOAT TAB UPPER/LOWER SURFACE. ANTI-FLOAT TAB WAS REPAIRED PER SRM 55-04 P 3.SDR 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.SDR 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.SDR 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.SDR 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.SDR DALA13034239205Mechanism · gougedRIGHT HORIZONTAL STABILIZER L/E FLOAT TAB MECHANISM GOUGED. REPAIRED IAW ERA 514984-14, REV O AND FINAL ERA 514894-14, REV O.SDR DALA13034249205Bracket · gougedLEFT HORIZONTAL STABILIZER FLOAT TAB BRACKET GOUGED. REPAIRED IAW ERA 514894-14, REV O.SDR 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.SDR A6WA201141101Pivot · damagedHORZONTAL STAB TRIM ACTUATOR PIVOT STRUCTURE DAMAGED ON LT OTBD FACE. BLENDED DAMAGED AREA NDT INSPECTION PRIMED IAW REO 601R-55-31-220.SDR DALA1119700916Skin · dentedDURING HMV A DENT WAS FOUND ON UPPER SKIN OF RT GEARED TAB. GEARED TAB WAS REPAIRED IAW SRM 55-04 PAR 3A.SDR DLM88091321Tab · corrodedDURING SHOP VISIT THE SUBJECT HORIZONTAL STABILIZER ELEVATOR ANTI-FLOAT TAB WAS FOUND WITH CORROSION. REPAIRED PER ERA 474926-14.SDR 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 SDR SWAA060864Tab · crackedDURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR TAB CRACKED AT NR 2 HINGE CUTOUT. REMOVED AND REPLACED TAB PER MM.SDR 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.SDR WRLA2005031Spar Cap · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 36.SDR WRLA2005032Spar Cap · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 01.SDR WRLA2005037Skin · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 31.
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