JASC 5532
Service difficulty reports · 1,753
Reports filed under 5532 · Vertical Stabilizer, Plate/Skin, 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 = '5532' 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 = '5532' 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 SIMA200216511Skin · dentedDURING MBV 1 INSPECTION FOUND LEFT SIDE OF VERTICAL STABILIZER TO HAVE 2 DENTS.SDR DL72S020624Panel · missingTOP CAP ON VERTICAL STABILIZER MISSING. REPLACED PANEL.SDR AWXA200200544Skin · chafedDURING C-8 INSPECTION TWO CHAFED AREAS OF SKIN WERE FOUND ON THE VERTICAL STAB LEADING EDGE AT FIN STATION 80 AND 90. MAINTENANCE BLENDED AND REMOVED CHAFED AREAS OF SKIN AT FSS STA.80 PER ASTM E797-95 PAGES 369-374 AND B757 SRM 55-30-01 FIG 101 PAGE 104. MASDR F3LA200200143Panel · crackedDURING C-1 CHECK, INSPECTION REPORTED LT VERTICAL PANEL 9507L INNER BRACE WORN AND CRACKED. FABRICATED PANEL RETAINER AND INSTALLED PER SRM 51-40-2, 51-30-50 AND SOPM 20-41-02.SDR 2002FA0000666Skin · crackedVERTICAL STABILIZER - ON BOTTOM TRAILING EDGE OF VERTICAL STABILIZER. THE SKIN APPEARED TORN, UPON REMOVAL OF RUDDER. THE STRUCTURE INSIDE THE VERTICAL STABILIZER APPEARED TO HAVE FATIGUE AND WAS CRACKED TO MIDPOINT OF VERTICAL WIDTH. NO DAMAGE TO RUDDER.SDR ASAA0280140Skin · chafedPAE - DURING 30K-CHECK, FOUND VERTICAL STABILIZER SKIN CHAFED FROM AFT TO CENTER AREA, WHERE BANANA FAIRING 3804A IS MOUNTED. REPAIRED VERTICAL STABILIZER SKIN PER EA 5530-01089. (M)SDR UPS02838279Skin · corrodedINSPECTION TYPE:N/A CORROSION AND PILLOWING OF SKIN ON VERTICAL STAB AFT LT SIDE. REMOVED PANEL AND ROUTED TO VENDOR FOR FABRICATION. TRIMMED AND INSTALLED NEW PANEL.SDR 02FDEA00246Flange · corrodedVERTICAL FIN MATING SURFACE FOR PANEL 9602 CORRODED (C55-391-30). REMOVED AND REPLACED FLANGE PER EA 7-5510-64063.SDR 2002UALA00630Panel · missingON ARRIVAL FOUND DORSAL FIN PANEL MISSING. THE DORSAL FIN PANEL WAS REPLACED. THE FUSELAGE SKIN IN THE AREA OF THE DORSAL FIN WAS VISUALLY AND HFEC INSPECTED TO ENSURE THAT NO DAMAGE TO THE FUSELAGE SKIN OCCURRED.SDR QXEA0201417Skin · dentedCKB - DENT ON RIGHT HAND SIDE OF VERTICAL STABILIZER BETWEEN RIBS 10 AND 11. REPAIRED IAW HORIZON AIR EA 9-55-149A AND WVAC EO DH8S-55-0357A.SDR P2EA2002V0026Service difficulty-DURING Q1 AND Q2 INSPECTION:-RUDDER STA 85 SKIN WITH DENT-REPAIRED IAW EO B737HC57-051/02. APPROVED 8110-3 DTD 03-06-02 BY FAA DER ROBERT MANASHI (DERT-71067-SW)-NOTE: SEE AEROMAN W/O No. 2002-90/1, VAM100 0579, SDA 239SDA030SDR TSAA0253059Skin · corrodedFOUND SKIN BULGE ON RIGHT SIDE VERTICAL FIN RIGHT SPAR AT FWL 112.356. FABRICATED REPAIR ANGLE, EXTERNAL DOUBLER, TWO FS 173.10 IN SPAR RIB CLIPS, REPLACEMENT FIN REAR SPAR WEB, SOLID SINGLE GUSSET, SKIN TRIM POUT FILLER AND FLAT FILLERS IAW FIGURES 2A THROUGSDR CA020308008Panel · cracked(CAN) VERTICAL STAB LEADING EDGE PANELS 322BL CRACKED. PANEL 322BL CRACKED.SDR CA020308007Panel · cracked(CAN) VERTICAL STAB LEADING EDGE PANEL 322AL AND 322BL CRACKED. PANEL 322AL APPEARS CRACKED ON BOTH LT AND RT SIDES APROX 4 INCHES BELOW UPPER EDGE. ALSO APPROX. 4 INCHES UP FROM LOWER EDGE ON LT SIDE APPEARS TO BE A THIRD CRACK. 322BL APPEARS TOBE DELAMINATEDSDR DL72S020231Skin · crackedA .9375 INCH CRACK WAS FOUND FROM FASTENER HOLE AT THE STRINGER 7L SKIN SPLICE TO THE EDGE OF THE SKIN. THE CRACK WAS VERIFIED TO BE CONTAINED IN THE FASTENER HOLE THROUGH HFEC INSPECTION. THE CRACKED AREA WAS REPAIRED WITH AN EXTERNAL TITANIUM DOUBLER.SDR QXEA0200357Flange · crackedPDX - NUT PLATE FLANGE IS CRACKED AT TOP AFT CORNER OF APERTURE FOR PANEL 57P. REPAIRED IAW FOKKER SRM 55-02-05, PAGE 8, FIGURE 4 AND SRM 51-31-01.SDR QXEA0200356Skin Panel · crackedPDX - THREE CRACKS IN SKIN PANEL BENEATH THE LEADING EDGE OF THE RUDDER ON THE LT SIDE AT THE STIFFENER. REPAIRED IAW FOKKER SRM 53-02-05, PAGE 10, FIGURE 5 AND SRM 51-31-01.SDR CA020228005Panel · cracked(CAN) VERTICAL STAB LEADING EDGE PANELS 322AL AND 322CL CRACKED. PANEL 322AL CRACKED APPROXIMATELY 4 INCHES FROM LOWER EDGE LT SIDE. PANEL 322CL CRACKED APPROXIMATELY 4 INCHES FROM LOWER EDGE LT SIDE.SDR CA020308010Panel · sheared(CAN) FLAPS EXTENDED FOR SERVICE CHECK INSPECTION. UPON RETRACTION RT CLOSURE PANEL AT INBOARD FLAPS HUNG UP AT 10 UNITS.FOUND RT INBOARD CLOSURE PANEL SHEARED CAUSING FLAPS TO JAM. CLOSURE PANEL REMOVED. AIRCRAFT OPERATED PER CDL 57-52-01. AIRCRAFT FERRIED FSDR CA020215005Structure · cracked(CAN) VERTICAL STAB LEADING EDGE PANEL 322B1 CRACKED APPROXIMATELY 5 INCHES UP FROM LOWER EDGE. LT SIDE. THE DAMAGE IS WITHIN REPAIR LIMITS WILL BE REPAIRED AS PER SRM 55-30-00, PA 200, OR REPLACED.SDR 02FDEA00082Skin · damagedDRILL START DAMAGE IN VERTICAL STAB SKIN STR 5 LT, NR 2 RIB. R&R SKIN.SDR AUS20011450Skin · delaminated(AUS) VERTICAL STABILISER LEADING EDGE SKIN DELAMINATED.SDR QXEA0102155Skin · chafedPDX - TOP LT SIDE OF VERTICAL STABILIZER AT LOWER FORWARD CORNER OF PANEL 55 OPENING HAS THREE CHAFE AREAS TO STAB SKIN. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-01.SDR QXEA0102040Rivet · loosePDX - VERTICAL STABILIZER LOWER RT SIDE SKIN HAS THREE LOOSE/SMOKING RIVETS. REPAIRED IAW FOKKER SRM 51-30-00.SDR CA011210017Skin · cracked(CAN) DURING INSPECTION OF THE AIRCRAFT, CRACKS WERE NOTED ON THE VERTICAL STABILIZER SKIN. THE CRACKS WERE LOCATED AT THE FIRST FASTENER ABOVE THE DOUBLER AT THE CENTRE SPAR. THE LONGEST CRACK MEASURED .75 INCHES IN LENGTH. A X-RAY INSPECTION WAS ACCOMPLISSDR QXEA0102015Rivet · loosePDX - VERTICAL STABILIZER SMOKING RIVETS LT SIDE JUST BELOW RIB 5 ON 50 PERCENT SPAR. REPAIRED IAW HORIZON AIR EA 4-55-299.SDR QXEA0102014Rivet · loosePDX - VERTICAL STABILIZER SMOKING RIVET JUST BELOW RIB 5 ON 50 PERCENT SPAR RT SIDE. REPAIRED IAW HORIZON AIR EA 4-55-299.SDR F3LA200100121Skin · dentedDURING C-1 CHECK, INSPECTION REPORTED SEVERAL DENTS IN SKIN OF DORSAL FIN FWD OF VERTICAL STABILIZER. FABRICATED AND INSTALLED EXTERNAL REPAIR PER SRM 55-30-6 AND 51-20-1.SDR P2EA2001V0013Skin · dentedC CHECK, VERTICAL FIN WITH DENTS BETWEEN FIN STA 191.5 - 180.3. REPAIRED SKIN IAW SRM 55-30-6 FIG 2.SDR DHL2001801527Skin · dentedVERTICAL STABILIZER LEFT OUTER SKIN DENTED 3 INCHES AT 2 R 159.961. REMOVED DAMAGED SKIN FROM VERTICAL STABILIZER AND FABRICATED NEW ONE PER SRM 55-2-0 PG 1-2 AND SRM 55-51 FIG 1. INSTALLED NEW SKIN PER SRM 55-2-0 PG 1-2.SDR DHL2001742510Skin · erodedAT C-CHECK, VERTICAL STAB L/E PANEL NR 9502 AT LOWER SECTION HF ANTENNA IS ERODED.SDR 2001F00465Rub Strip · bulgedVERTICAL STABILIZER UPPER FORWARD RUB STRIPS, FOR HORIZONTAL STABILIZER PATH, HAS BULGED AREAS ON BOTH RIGHT AND LEFT SIDES. (M)SDR DHL2001727511Skin Panel · damagedREPLACE TEMP REPAIR LT VERT FIN BELOW RUDDER. REMOVED ACCESS PANEL BETWEEN FWD ENG MOUNT FOR SHEET METAL ACCESS PER SRM 51-30-2. REMOVED SKIN PANEL AT LT OF HORIZ STABILIZER PER SRM 51-30-2. SENT TO COMPOSITE SHOP FOR REPAIR. INSTALLED NEW SKIN PANEL PER SSDR 2002F00704Skin · bulgedFOUND VERTICAL STAB BS 1342 RIGHT SIDE STRINGER 10R HAS BULGING SKIN. (M)SDR QXEA0101285Skin · dentedYYC-VERTICAL STABILIZER SKIN PANEL HAS 2 MINOR DENTS. REPAIRED IAW FOKKER SRM 51-00-00, PAGE 1B AND HORIZON AIR EA 4-55-297.SDR DL72L011163Skin · crackedTHE LT VERTICAL STABILIZER SKIN WAS FOUND WITH A 1 INCH CRACK EMANATING FROM A FASTENER HOLE NEAR THE REAR SPAR JUST ABOVE THE STAB-TO-FUSELAGE SKIN ATTACH ANGLE.SDR B652001F00000Skin · crackedFOUND FATIGUE CRACK IN RIGHT VERTICAL STABILIZER FIN DURING PREFLIGHT. CRACK STARTED AT FORWARD AND TOP ATTACH POINTS AND RAN AFT FOR APPROXIMATELY 8 INCHES. CRACK WAS ON INSIDE SURFACE AT MOUNTING POINTS TO HORIZONTAL STABILIZER.SDR AWXA0001931Skin · dentedVERT STAB L/E STA 137 DENT FOUND OUT OF LIMITS PER SRM 55-30-01. CUT OUT DAMAGED AREA HFEC NO CRACK NOTED CAL 0692, FABRICATED DOUBLER FROM .063 2024T3 PO X95024189 AND FILLER FROM 2024T3 .040 PO X95025244 TREATED AND PRIMED. INSTALLED DOUBLER AND FILLER PERSDR ZW0A0104403Panel · dentedON THE RT SIDE OF THE VERTICAL STABILIZER, THE FWD ALUMINUM HONEYCOMB PANEL AT STA 92.250 HAD 24 GROUPS OF DENTS TOO CLOSE TOGETHER AND OUT OF LIMITS PER SRM 55-30-01. ALL DENTS DEPTH WITHIN LIMITS. APPROX 125 DENTS TOTAL. REPAIRED PER ARA 17707. NO CHECK-SDR DHL2001803508Skin · dentedVERTICAL STABILIZER L/E SHOWS 3.52 IN DENT AT ZFS 123.500. CUT OUT DAMAGED AREA PER SRM 55-2-1 PG 17. FABRICATED FILLER (ALCLAD 7075 T6,0.050) PER SRM 55-2-1. FABRICATED DOUBLER (ALCLAD 7075-T6 0.050) PER SRM 55-2-1 PG 17. CLEANED, TREATED AND PRIMED PER SSDR AT0100212Spar · crackedFOUND RIGHT HORIZONTAL STABILIZER SPAR CRACKED. CORRECTIVE ACTION: FABRICATED AND INSTALLED SPLICE ANGLES AND REPLACEMENT SECTION OF SPAR IAW 51-30-01, 51-30-05, AND 55-01 FIG 2.SDR DL72L010930Skin · crackedA 0.5 INCH CRACK WAS FOUND IN THE VERTICAL STABILIZER SKIN ON THE LT SIDE, AT S-11. CRACK RUNS FROM A FASTENER HOLE AT S-11 AND EXTENDS FWD FOR APPROXIMATELY 0.5 INCH. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER INSTALLED.SDR ABXA010564Skin · corrodedCORROSION ON EXTERNAL SKIN OF THE VERTICAL STABILIZER, JUST ABOVE THE FUSELAGE TO VERTICAL ATTACHING ANGLE REPAIR DOUBLER. REPAIRED AREA AND INSTALLED NEW SKIN IAW DC-8 SRM 55-2-0, 51-1-21, 51-3-0, 51-1-22, 51-9-0, 51-1-26, 51-1-20D, 51-1-15, 51-1-16, AND DC-8SDR CA010529013Skin · cracked(CAN) SMOKING WAS NOTICED AT THE ETOP R/H VERTICAL STAB SKIN. FURTHER INSPECTION REVEALED THAT THE REPAIR PATCH PREVIOUSLY INSTALLED IAW PILATUS TECH MEMO EC-12-TM-540 WAS CRACKED AT APPROXIMATELY THE SAME LOCATION AS THE ORIGINAL SKIN CRACKED. THE FIRST REPAISDR DL72S010749Skin · crackedTHE LT SKIN OF THE VERTICAL STABILIZER WAS FOUND WITH A .75 INCH CRACK EMANATING FROM AN ATTACHMENT TO THE REAR SPAR. THE CRACK WAS LOCATED JUST ABOVE THE FUSELAGE SKIN INTERFACE. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. SDR AALA20010899Skin Panel · damagedTUL - FOUND VERTICAL STAB SKIN WORN 50 PERCENT THROUGH BY DAMAGED SEAL BRACKET JUST AFT OF RIGHT ROLLER TRACK. PART REPLACEMENT. REMOVED AND REPLACED STAB SKIN PANEL WITH NEW TREATED PRIMED AND PAINTED PER SRM 51-10-3. (M)SDR MWEA010557Skin · chafedVERTICAL STABILIZER SKIN JUST AFT OF LEFT LEADING EDGE SIDE ROLLER TRACK HAS A CHAFE MARK. FABRICATED AND INSTALLED HORIZONTAL STAB CUTOUT PANEL.SDR AALA20010692Skin · scratchedTUL - FOUND DEEP SCRATCH 3 INCHES BY .25 INCH IN LOWER LEFT VERTICAL STABILIZER SKIN BETWEEN TAIL NR. INSTALLED DOUBLER PER SRM 55-30-3, FIG 1. (M)SDR AALA20010691Skin · scratchedTUL - FOUND DEEP SCRATCH 3 INCHES BY .5 INCH IN LOWER LEFT VERTICAL STABILIZER SKIN JUST ABOVE AIRCRAFT TAIL NR. INSTALLED DOUBLER PER SRM 55-30-3, FIG 1. (M)SDR AALA20010690Skin · scratchedTUL - LOWER LEFT VERTICAL STABILIZER HAS DEEP SCRATCH 3 INCHES BY .25 INCH JUST ABOVE TAIL NR. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)
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