JASC 5532
Service difficulty reports · 1,754
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 AT9900009Skin · chafedSCHEDULED INSPECTION AT AERO CORP, FL. VERTICAL STABILIZER UPPER LEADING EDGE SKIN CHAFED LEFT AND RIGHT. FABRICATED REPAIR AND INSTALLED IAW RES 982239, SRM DC9 51-10-20, 55-31-0, 51-10-4, 51-10-3, 51-30-5, AND 51-20-0.SDR VJ9800682Skin · chafedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE VERTICAL STAB PANEL (DOG HOUSE) CHAFFING AT THE LEFT HAND AFT SECTION. FABRICATED AND INSTALLED NEW PANEL IAW DC9 SRM 51-10-3, 51-30-3, 55-31-0, AND AIRTRAN RES 982127.SDR CALA9802117Panel · crackedINSPECTION FOUND A 4 INCH CRACK IN RT LOWER VERTICAL STABILIZER SLIDING PANEL. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01 FIGURE 2, 51-10-2A, 51-10-4, 51-10-3 AND 51-30-2.SDR 9810809926Skin · crackedDURING PERIODIC CHECK, FOUND CRACK IN VERTICAL STABILIZER SKIN ON LEFT SIDE ABOVE RUDDER. INSTALLED DOUBLER REPAIR PER EA 99-159482.SDR COMA9860319Panel · crackedRIGHT LOWER VISOR PANEL CRACKED. REPLACED PANEL.SDR DL72S982092Skin · crackedLT SIDE OF THE VERT STAB SKIN IS CRACKED AT THE INTERSECTIONOF S10 AND FUSE CREASE LINE. REPAIR PER ERA 332292-14.SDR WRLA98093Panel · chafedDURING C-CHECK, LOWER VERTICAL STABILIZER FIRE SEAL PANEL WAS FOUND CHAFED AND WORN THOUGH THE OUTER EDGE. MAINTENANCE PERSONNEL REPAIRED VIA WELDING PER DOUGLAS PROCESS SPECIFICATION. (X)SDR AALA981730Skin · crackedTUL - SKIN CRACKED PAST STOP DRILL, DOUBLER REPAIR AREA 5TH BAY ABOVE ACCESS OPENING, BELOW STRINGER 6 RT. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 55-30-3. (M)SDR TWAA9815306Skin · corrodedDURING CHECK-C MAINT, FOUND ON VERT STAB LT SIDE, A GROOVE BLENDED BEYOND LIMITS PER SRM 53-01, PG 6 FIG 1, IN SKIN BELOW LT HORIZ STAB. ACCOMP EDDY CURRENT OF AREA PER 51-00-03 AND NO CRACKS FOUND. REPAIRED PER ARA 15375.SDR ARWA981011Skin · corrodedCORROSION ON VERTICAL STAB AROUND AFT STATIC DISCHARGE BASE. REPAIR DONE IAW SRM 55-35-00. USING MAT (P/N 2024T3 050) (B/N 98/005851/5851) RIVETS NAS 1738E4-2 (B/N 95/040160/0160) CONS 118/98. DRAWING BW-L-15-55-A/4509. W/O JWM 24000 CCF 3139 MIN REPAIR.SDR CALA9801591Panel · crackedINSPECTION FOUND A .5 INCH CRACK IN LT VERTICAL STABILIZER SLIDER PANEL AND A .75 INCH CRACK IN RT VERTICAL STABILIZER SLIDER PANEL. BOTH PANELS WERE REPLACED IAW SRM 51-20-1, FIGURE 7, 51-10-2, AND MM 51-20-2.SDR CALA9801503Plate · crackedINSPECTION FOUND A 4 INCH CRACK IN VERTICAL STABILIZER INNER COMPARTMENT NR 1 RIB LOWER LT CORNER PLATE JUST AFT OF S-DUCT. THE RIVETS WERE REMOVED IAW SRM 51-30-2. A DOUBLER WAS INSTALLED IAW SRM 51-30-2.SDR QXEA9801302Skin · chafedVERTICAL STABILIZER RIGHT-HAND TOP SKIN IS CHAFED 7 INCHES WIDE UNDER ICE SCRAPER. REPAIRED IAW HORIZON AIR EA 4-55-81.SDR MWEA98934Skin · crackedVERTICAL STABILIZER APPROXIMATE STATION ZY 115 0 CRACK HAS CONTINUED TO CRACK PAST STOP DRILL LEFT SIDE APPROXIMATE 6 INCHES FROM TRAILING EDGE SEAM. MTC REMOVED AND REPLACED SPLICE.SDR CALA9801454Skin · crackedINSPECTION FOUND A 1 CRACK IN LOWER VERTICAL STABILIZER SKIN (NR 2 ENGINE INTAKE DUCT). THE AREA WAS REPAIRED IAW ECRA 5530-01213 AND A DIP WAS ISSUED TO PERFORM A VISUAL INSPECTION OF THE REPAIR IAW PART 2 OF ECRA 5530-01213 AT EVERY C CHECK.SDR CALA9801299Skin · crackedINSPECTION FOUND A .75 INCH CRACK THROUGH FASTENER HOLE OF SKIN AT LT SIDE OF VERTICAL STABILIZER AROUND ACCESS PANEL 9523 ABOVE BS 1215. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-0, 55-30-3, 51-10-2, 51-30-2, AND 51-00-SDR P5CA9801062Skin · corrodedLT HORIZONTAL STAB TOP SURFACE MINOR CORROSION ALONG STAB TORQUE BOX SKIN AREA FROM L/E TO T/E. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.SDR QXEA9800913Skin · chafedTOP EDGE RIGHTHAND SIDE OF VERTICAL STABILIZER SKIN HAS CHAFE DAMAGE FROM HORIZONTAL STABILIZER RUBBING AGAINST IT. REPAIRED IAW HORIZON AIR EA 4-55-72.SDR VJ9800185Skin · dentedREMOVED VERTICAL STABILIZER, FABRICATED DOUBLER AND FILLER FROM 7075 T6.063. CUT OUT DENTED AREA, TRIMMED, DRILLED AND INSTALLED REPAIR IAW EO 9-53-004, REINSTALLED VERTICAL STABILIZER LEADING EDGE.SDR QXEA9800915Skin · damagedVERTICAL STABILIZER PANEL 56G HAS 2 SCREW HOLES GOUGED AND REAMED OUT. REPAIRED IAW HORIZON AIR EA 4-55-66.SDR AU980991Skin · corroded(AUS) VERTICAL FIN ASSEMBLY SKIN CORRODED. PART TC: 7,193.SDR CALA9800908Skin · crackedINSPECTION FOUND INTERIOR CRACKS ON VERTICAL FIN LEADING EDGE FORWARD OF PITOT TUBE AROUND COUNTER SINK. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 55-01, FIGURE 2.SDR AALA981048Skin · crackedTUL - AN .25 INCH CRACK FROM SCREW HOLE IN VERT STAB SKIN AT BODY STATION 1213 LEFT SIDE. INSTALLED DOUBLER PER B 727 AARD/DC PAGE 55-30-03-1. (M)SDR 98ZZZX2112Skin · crackedSKIN OF LEFT VERTICAL STABILIZER CRACKED. REMOVED SKIN AND FOUND RIB P/N 33640000-11 WITH UNSHOT RIVETS AT ATTACH POINT TO REAR SPAR OF VERTICAL STABILIZER. IT APPEARS THAT THIS WAS THE FIRST TIME THIS SKIN WAS REMOVED SINCE DATE OF MANUFACTURE. RIVETS CAN SDR SWAA980785Skin · bird strikeBIRDSTRIKE INBOUND TO SMF. BIRDSTRIKE INSPECTION PERFORMED, FOUND DAMAGE TO VERTICAL STABILIZER L/E AT BS 1006, STA 57, RT WING LEADING EDGE AND PAX WINDOWS BADLY SCRATCHED. INSTALLED INTERIM REPAIRS FOR AERODYNAMIC SMOTHNESS. A/C FERRY TO TRAMCO FOR PERMANSDR MWEA98573Skin · chafedFOUND HEAVY CHAFING ON VERTICAL STABILIZER CANOE FAIRING AFT LEFT HAND SKIN. MTC REMOVED AND REPLACED FAIRING SKIN.SDR MWEA98572Skin · chafedFOUND HEAVY CHAFING ON VERTICAL STABILIZER CANOE FAIRING AFT RIGHT HAND SKIN. MTC REMOVED AND REPLACED FAIRING SKIN.SDR 98ZZZX2086Skin · damagedDEFECT WAS DISCOVERED DURING INSPECTION ASB 407-98-17. FOUND CUTS IN SKIN ON FORWARD AND AFT SIDES OF AFT LOWER INSERT AT ENDS OF FORMERS FOR COWLING. THE CAUSE IS THE SKIN WAS CUT DURING TRIMMING OF THE FORMERS DURING PRODUCTION. COMPONENT P/N 206020113323SDR IXXA9800106Panel · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LEFT VERTICAL STABILIZER PANEL BETWEEN STATIONS ZR 253 AND ZR 297. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH FAA DER APPROVED DRAWINSDR SWAA980723Skin · bird strikeON APPROACH, FOUND BIRD STRIKE DAMAGE TO VERTICAL STAB, RT INBD WING L/E, AND PAX CABIN WINDOW AT BS 747. AIRCRAFT MADE AN UNEVENTFUL LANDING. ACCOMPLISHED BIRD STRIKE INSP PER MM A/C FERRY TO TRAMCO. REPAIRED PER BOEING SRM.SDR MWEA98575Skin · gougedFOUND A DEEP GOUGE IN RIGHT SIDE VERTICAL STABILIZER UPPER AFT CANOE SKIN. MTC FABRICATED AND INSTALLED SKIN.SDR HEEA0014036Fin Assembly · damagedINSPECTED VERTICAL FIN AS PER ASB407-98-17 FOR CUTS AND SCRATCHES. THE ALLOWABLE DEPTH WAS .020. THE TWO CUTS FOUND WERE .017 AND .024 DEEP. SCRAPPED PART.SDR MWEA98559Skin · chafedFOUND VERTICAL STABILIZER CANOE SKIN ON RIGHT AFT SIDE CHAFED BEYOND LIMITS. MTC REPAIRED WITH DOUBLER.SDR P5CA9800831Panel · dentedVERTICAL STABILIZER PANEL 321D DENT FOUND. REPAIRED PANEL PER SRM 51-40-01.SDR P5CA9800869Skin · dentedVERT STAB T/E UPPER AREA HAS A DENT NEAR TOP OF UPPER RUDDER. REPAIRED PER SRM 51-40-15.SDR P5CA9800859Skin · dentedVERT STAB SKIN LEFT SIDE HAS DENT NEAR L/E STA 200-220 AT 2 LOCATIONS. DENT REPAIRED PER SRM 51-40-06 AND MM 51-26-11.SDR IXXA9800107Panel · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON RIGHT VERTICAL STABILIZER EXTERNAL PANEL BETWEEN STATIONS ZR 253 AND ZV 297. REPAIR ACCOMPLISHED REMOVAL OF AFFECTED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH FAA DER APPRSDR ARWA980492Skin · corrodedDURING D-CHECK, FOUND VERTICAL STABILIZER LEADING EDGE UPPER SECTION HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 55-2-1. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK SDR ARWA980491Skin · corrodedDURING D-CHECK, FOUND VERTICAL STABILIZER LEADING EDGE LOWER SECTION HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 55-2-1. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK OSDR DL72K980950Skin · crackedTHREE EACH .125 IN CRACKS IN VERTICAL STABILIZER OUTER SKIN RT SIDE FWD OF PANEL 9501 (MARKED). INSTALLED REPAIR PER MM 54-30-0.SDR DHL9870711CPanel · delaminatedAT C-CHECK, TAIL ACCESS PANEL 9705 SHOWS SIGNS OF DELAMINATION. INSTALLED REPAIR PER SRM 51-40-8, 24 X 15. N/R 4805SDR CALA9800564Skin · crackedINSPECTION FOUND A .1875 INCH CRACK IN LT SIDE OF VERTICAL STABILIZER LOWER SECTION AT STA 1343. A REPAIR WAS INSTALLED IAW ECRA 5530-01075.SDR CALA9800547Skin · crackedINSPECTION FOUND A 3 INCH CRACK IN LT VERTICAL STABILIZER AT STA 1253, JUST ABOVE AND AFT OF PANEL NR 9523. THREE 1 INCH CRACKS WERE FOUND IN THE LT VERTICAL STABILIZER AT STA 1264. THE CRACKED AREAS WERE CUTOUT IAW SRM 54-10-1. FILLER AND DOUBLER REPAIRS WSDR CALA9800504Skin · crackedINSPECTION FOUND A .25 INCH CRACK IN RT VERTICAL STABILIZER LOWER SECTION AT STA 1343. A REPAIR WAS INSTALLED IAW ECRA 5530-01075.SDR DHL9872689DPanel · damagedAT D CHECK, VERTICAL STAB PANEL 9607 DAMAGED. INSTALLED OVERLAY REPAIR PER SRM 51-40-8. N/R 4339.SDR DHL9872688DPanel · crackedAT D CHECK, VERTICAL STABILIZER ACCESS PANEL 9607 INTERM REPAIR CRACKED. INSTALLED OVERLAY REPAIR PER SRM 51-40-8. N/R 4340.SDR DHL9872687DPanel · damagedAT D CHECK, VERTICAL STABILIZER ACCEESS PANEL 4608 DAMAGED. INSTALLED OVERLAY REPAIR PER SRM 51-40-8. N/R 4341.SDR P5CA9800456Panel · debondedDEBONDING AND EROSION ON PREVIOUS REPAIR ON RIGHT EXTERIOR PANEL ON VERTICAL STABLIZER. REPAIRED PER BAC SRM 51-40-09.SDR DHL9872696DPanel · delaminatedAT D CHECK, ACCESS PANEL 9505 IS DELAMINATING. INSTALLED OVERLAY REPAIR PER SRM 51-40-8SDR DHL9872695DPanel · disbondedAT D CHECK, PANEL 9606 HAS DISBONDING AT SCREW HOLES. INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8. N/R 4237.
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