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 WRLA2005035Spar Cap · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 36.SDR CA050203002Plate · failed(CAN) RT HORIZONTAL STABILIZER TO FIN SEAL SEPARATED FROM AIRCRAFT. UNABLE TO DETERMINE EXACT CAUSE. ALL AFFECTED PARTS REPLACED. REMAINING FLEET CHECKED, SERVICEABLE.SDR UPS05443724Stringer · crackedINSPECTION TYPE:C - LEFT BS 2658 STR 13 FOUND CRACKED. STRINGER REPLACED AS PER SRM 50-10-01.SDR IXXA0500040SPlate · corrodedDURING A ROUTINE C CHECK INSPECTION, RT HORIZONTAL STAILIZER OUTBOARD LEADING EDGE UPPER PLATING CORROSION DAMAGE BETWEEN STA XFS 172.000 AND XFS 335.000. REPAIR ACCOMPLISHED. REMOVED FASTENERS AND CORROSION. FOUND OUT OF LIMITS, REMOVED CORROSION, CLEANEDSDR SROM200400009Stringer · elongatedDURING D CHECK INSPECTION FOUND AFT CARGO PIT STRINGER 20L HAS SEVERAL ELONGATED FASTNER HOLES AND MULTIPLE CRACK INDICATIONS AROUND HOLES STA 747 TO 887. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR STRINGER AND SPLICES IAW SRM 53-10-3.SDR MWEA030488Skin · damagedRT HORIZONTAL STABILIZER ANTI-FLOAT TAB HAS LIGHT DAMAGE ON BOTTOM SIDE, 20 INCHES FROM OUTBOARD EDGE. FABRICATED AND INSTALLED DOUBLER.SDR C2XA03TY101Bearing · wornTHE LEFT AND RIGHT HORIZ STAB SPHERICAL BEARINGS FAILED WEAR CHECK. MAINTENANCE REPAIRED THE LEFT AND RIGHT VERTICAL STAB SPHERICAL BEARING HOUSINGS AND INSTALLED BOTH SPHERICAL BEARINGS IAW EC5510-01059 AND EMB-IC2003-145/2529. THE REPAIR WAS SATISFACTORY ASDR AUS20030593Brace · cracked(AUS) HORIZONTAL STABILIZER TRIM DIAGONAL BRACE CRACKED. SUSPECT BRACE WAS BENT OUT OF THE WAY FOR ACCESS. STABILIZER HINGE BOLTS HAD MISSING SPACER WASHERS. PERSONNEL/MAINTENANCE ERROR.SDR 125401Tab · delaminatedDURING SCHEDULED MX, FOUND LT ELEVATOR TRIM TAB INBOARD TOP AND BOTTOM SIDE DELAMINATED BEYOND LIMITS. REMOVED TRIM TAB, REPAIRED IAW CHAPTER 27-04-00 AND RE-INSTALLED TRIM TABSDR SWAA022883Bushing · wornDURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, BOTH LEFT AND RIGHT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH LEFT AND RT ELEVATOR TAB NR 1 HINGE BUSHINGS.SDR SWAA022563Tab · crackedDURING SCHEDULED A1 CHECK, FOUND RT ELEVATOR TAB CRACKED AT NR 1 HINGE CUT OUT. REMOVED AND REPLACEDR TAB ASSY PER MM.SDR SWAA021487Tab · vibrationLOW FREQUENCY AIRFRAME VIBRATION OCCURRED FOR ABOUT 2 MINUTES IN-FLIGHT. ACCOMPLISHED POST LCO (LIMIT CYCLE OSCILLATION) INSPECTION, REMOVED AND REPLACED BOTH LT AND RT ELEVATOR TABS PER MM.SDR IXXA0200073SStructure · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT HORIZONTAL STABILIZER LEADING EDGE STATION XFS 178 TO XFS 285. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND REPAIR DOUBLER IN ACCOURDSDR CA020205007Hinge Pin · corroded(CAN) DURING INSPECTION OF HORIZONTAL STABILIZER HINGE PINS, FOUND THE RT SIDE OUTER PIN THREADS AND THREAD RELIEF AREA CORRODED. THE OUTER AND INNER PINS WILL BE REPLACED PRIOR TO NEXT FLIGHT.SDR AUS20011211Bearing · corroded(AUS) RT HORIZONTAL STABILISER HINGE BEARING CORRODED IN BEARING BORE CAUSING CHAFING ON THE HINGE PLATE.SDR CA020523014Bracket · cracked(CAN) CRACKS FOUND WHERE STABILATOR TRIM BRACKET MEETS THE STABLATOR TRIM TAB DURING UNRELATED INSPECTION. AREA REINFORCED BY AMO.SDR SWAA011948Bushing · wornDURING SCHEDULED SERVICE CHECK SWA SI 11075-55, FOUND LT ELEVATOR TAB HINGE BUSHINGS WORN AT HINGE'S NR 2, 3 & 4. REMOVED AND REPLACED HINGE BUSHINGS PER MM.SDR RRXA10767Skin · damagedDURING A MAINTENCE VISIT FOUND HOLE DAMAGE TO HORZ STAB RT. ELEVATOR AT STA. XE 228.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8110-3 DATED 02/SDR SWAA010793Fitting · elongatedDURING SCHEDULED C4 CHECK, FOUND LT ELEVATOR TAB ATTACH FITTING MAST OUTBD INPUT ROD LUG BOLT HOLE ELONGATED. REMOVED AND REPLACED ELEVATOR TAB PER MM.SDR RRXA10812Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H I/B HORZ. STAB. L/E AT STA. XFS 178, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-006 SDR P2EA00451Fitting · crackedSJO - DURING Q-CHECK, FOUND LEFT ELEVATOR HINGE SUPPORT AT BS 1156 ELEVATOR STA ZERO WITH CRACK L = 2.00 INCHES. W = 0.002 INCH. REPLACED THE LEFT ELEVATOR HINGE SUPPORT AT BS 1156 ELEVATOR STA ZERO IAW BOEING SRM 51-10-1 PAGE 8 AND SRM 51-30-2. (X)SDR 20001109SH039Skin · crackedDURING ROUTINE INSPECTION, A CRACK WAS FOUND ON THE LEFT STABILATOR LOWER SKIN. (X)SDR 20001102SH022Spring · crackedSPRINGS, PN 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM CAUSING THE UNIT TO BOND AND JAM. IMPROPER HEAT-TREATING, AUSTENITE, FATIGUE AND INCREASED SPRING COIL STRESSES. SUBMITTER STATED SPRINGS PN 69-77855-1 ARE TO BE REPLACED WITH PN 69-77855-2 SPRSDR 20001106SH053Structure · corrodedCORROSION IN LOWER RIGHT HORIZONTAL STABILIZER BARREL NUT HOLES. (X)SDR 20001106SH052Structure · corrodedCORROSION IN UPPER LEFT HORIZONTAL STABILIZER BARREL NUT HOLES. (X)SDR AWXA0000366Track · crackedC-CHECK, RT HORIZ STAB UPPER AFT SLIDING SEAL TRACK CRACKED. REMOVED AND REPLACED RT HORIZONTAL STAB UPPER AFT SLIDING SEAL TRACK IAW 737 SRM 51-30-02.SDR AT0000242Angle · wornFOUND BOTTON ANGLE LEFT AFT SIDE OF VERTICAL PANEL WORN BEYOND LIMITS. REMOVED AND REPLACED ANGLE IAW TIMCO SERVICE ORDER 151015-38274.SDR DHL200071729DPin · corrodedAT D CK, RT. OUTER HORIZONTAL STAB HINGE PIN IS CORRODED AT THREADS AND ON SHOULDER. REMOVED AND REPLACED HINGE PIN, PER B727 AD 84-21-05. REF: N/R 4675.SDR 99ZZZX3402Counterweight · crackedAT PRE-PURCHASE INSPECTION, FOUND MOVEMENT IN BALANCE TUBE AT FORWARD STABILATOR FITTING. REMOVED PAINT, INSPECTED. FOUND WHAT LOOKED LIKE CRACK. REMOVED FROM AIRCRAFT, MAGNAFLUXED, FOUND 1 INCH CRACK AROUND TUBE AND SECOND CRACK OPPOSITE SIDE OF TUBE. TUBSDR 99ZZZX1160Balance Weight · crackedDURING INSPECTION OF BALANCE WEIGHT TUBE PER AD NR 70-26-04, TUBE MOUNT ON STABILATOR FOUND CRACKED AT BOLT HOLES. FUSELAGE DOES NOT HAVE ACCESS PANEL FORWARD OF STABILATOR INSTALLED. PULLING BALANCE WEIGHT TUBE MUST BE DONE THROUGH TAILCONE REMOVING TUBE STSDR 99ZZZX533Balance Weight · crackedDURING 100-HOUR INSPECTION OF BALANCE WEIGHTS AND ARMS PER AD 78-02-03, FOUND BOTH ARMS CRACKED. REPLACED BOTH WITH SERVICEABLE PARTS. CAUSE UNKNOWN, POSSIBLE THAT ICE ACCUMULATION ON STABLIZER CAUSED SLIGHT FLUTTER.SDR ASAA9880241Fitting · chafedLCQ - DURING 30K CHECK, WEAR SPOT WAS FOUND ON LEFT ELEVATOR CONTROL TAB HINGE FITTING (4TH FROM INBOARD). REPAIRED IAW ASA EA 5520-01063. (M)SDR 98ZZZX3947Hinge Fitting · holes elongatedDURING INSPECTION. LT ELEVATOR OUTBOARD HINGE FOUND LOOSE. FOUND HOLES ELONGATED IN 115-620021-9 HINGE ASSEMBLY AND SURROUNDING STRUCTURE. BOLTS CALLED OUT FOR IN BEECH MSB 2132-R1 AND AD NOTE 87-03-06 HAD BEEN P/C/W. AD NOTE STATES THE RECURRING INSPECTIONSDR 98ZZZX823Rib · crackedDURING ANNUAL INSPECTION, THE LT STABILATOR TRIM TAB INBOARD RIB WAS FOUND CRACKED.SDR 99ZZZX501Trim Tab · crackedDURING ANNUAL INSPECTION, FOUND TRIM TAB CRACKED APPROXIMATELY 60 PERCENT AROUND BASE OF ATTACH ARM, P/N 65248-000. DAMAGE EXTENDED THROUGH INBOARD RIB, P/N 63887-01. SUBMITTER RECOMMENDED CLOSER PRE-FLIGHT AND MAINTENANCE INSPECTION OF THIS AREA AS IT CAN OSDR 99ZZZX500Trim Tab · crackedDURING ANNUAL INSPECTION, FOUND TRIM TAB CRACKED APPROXIMATELY 60 PERCENT AROUND BASE OF ATTACH ARM, P/N 65248-000. DAMAGE EXTENDED THROUGH INBOARD RIB, P/N 63887-01. SUBMITTER RECOMMENDED CLOSER PRE-FLIGHT AND MAINTENANCE INSPECTION OF THIS AREA AS IT CAN OSDR AU971465Trim Tab · cracked(AUS) STABILATOR TRIM TABS CRACKED AT INBOARD END ADJACENT TO THE ACTUATING ARM ATTACHMENT. CRACKING EVIDENT IN SKIN PANELS AND INBOARD RIB.SDR 97ZZZX1836Rib · crackedFIGHT TRIM TAB SKIN AND INBOARD SUPPORT RIB CRACKED AT ACTUATOR ATTACHMENT UNDER FLANGE FOOTPRINT.SDR BIER960039Trim Tab · crackedDURING REMOVAL OF HORIZONTAL STABILATOR TRIM TAB HINGES FOR REPLACEMENT, FOUND BOTH TRIM TABS CRACKED UNDER CONTROL HORN ATTACHMENT. CRACKS NOT VISIBLE WITH TABS ATTACHED. SUBMITTER SUGGEST REMOVAL OF HORN AT ANNUAL INSPECTION FOR ROUTINE INSPECTION.SDR 96ZZZX3543Trim Tab · crackedDURING 100-HOUR INSPECTION, THE TRIM TAB WAS DISCONNECTED TO ACCOMMODATE REPLACEMENT OF TRIM BARREL HARDWARE, THE TRIM TAB WAS FOUND CRACKED; UNDER THE ATTACH BRACKET, AT THE EDGE OF THE ATTACH BRACKET, INTO THE SUPPORTING RIBS, AND ON BOTH LEFT AND RIGHT TRIMSDR 96ZZZX3542Trim Tab · crackedDURING 100-HOUR INSPECTION, THE TRIM TAB WAS DISCONNECTED TO ACCOMMODATE REPLACEMENT OF TRIM BARREL HARDWARE, THE TRIM TAB WAS FOUND CRACKED; UNDER THE ATTACH BRACKET, AT THE EDGE OF THE ATTACH BRACKET, INTO THE SUPPORTING RIBS, AND ON BOTH LEFT AND RIGHT TRIMSDR 96FDEA00970Skin · delaminatedNR0402 AND 022, RT ELEVATOR TAB T/E O/B CORNER IS DELAMINATED. *S/D* REPAIRED RT ELEVATOR TAB IAW FEDEX SRM 51-40-06 AND 51-80-09.SDR 96ZZZX1785Nutplate · rustedNUT BODY OF ALL 4 NUTPLATES SECURING ARM ASSY STABILIZER TRIM, PN 65248-000, TO LEFT AND RIGHT STABILATOR TRIM TABS EATEN THROUGH WITH RUST AND SPLIT OPEN. SUSPECT MOISTURE. RECOMMENDATION - SPLIT TRIM TABS AND INSPECT NUTPLATES AT EACH ANNUAL INSPECTION.SDR 96ZZZX193Trim Tab · corrodedSKIN CORRODED AT NUTPLATE TO SKIN ATTACH POINTS. BOTH TABS BEYOND REPAIR. AIRCRAFT STRIPPED AND PAINTED 1 YEAR PRIOR. DRY, TRAPPED STRIPPER FOUND AROUND NUTPLATES. THIS MAY HAVE CONTRIBUTED OR WAS RESPONSIBLE FOR CORROSION.SDR 96ZZZX192Trim Tab · corrodedSKIN CORRODED AT NUTPLATE TO SKIN ATTACH POINTS. BOTH TABS BEYOND REPAIR. AIRCRAFT STRIPPED AND PAINTED 1 YEAR PRIOR. DRY, TRAPPED STRIPPER FOUND AROUND NUTPLATES. THIS MAY HAVE CONTRIBUTED OR WAS RESPONSIBLE FOR CORROSION.SDR TSAA9527045Skin · damagedDURING HEAVY MAINTENANCE VISIT, FOUND LEFT ELEVATOR TAB WITH TEAR IN SKIN AT INBOARD BEARING. REPAIRED PER ECO 2560. AIRCRAFT RETURNED TO SERVICE. (Z)SDR TSAA9527044Skin · crackedDURING HEAVY MAINTENANCE VISIT, FOUND RT ELEVATOR TAB SKIN CRACKED AT NR 2 HINGE TOP SIDE. REPAIRED PER ECO 2560. AIRCRAFT RETURNED TO SERVICE. (Z)
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