JASC 5530
Service difficulty reports · 2,534
Reports filed under 5530 · Vertical Stabilizer, 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 = '5530' 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 = '5530' 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 QXEA9800748Angle · crackedLEFTHAND FUSE TO VERTICAL FIN CONNECTION ANGLE IS CRACKED AT THE 50 PERCENT SPAR LOCATION. REPAIRED IAW FOKKER SRM 55-31-01, PAGE 2 AND SRM 51-31-01.SDR QXEA9800762Angle · crackedLEFT VERTICAL STAB CONNECTION ANGLE AT INTERMEDIATE SPAR 1 (32 PERCENT) IS CRACKED. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1.SDR DL72S980965Stringer · crackedFOUND AT A2 LETTER CHECK, VERTICAL STAB STRINGER 6L CRACKED AT BOLT HOLE FIN STA 157.2. REPAIRED PER M/M 55-30-0.SDR CALA9800745Web · crackedVERT STAB INNER COMPARTMENT NR 1 CANTED STATION 1303 HAS CRACK (2.5) AT RT LOWER CORNER. ALSO, CRACK (1) AT RT UPPER CORNER. STOP DRILLED CRACKS, FABRICATED AND INSTALLED DOUBLERS PER SRM 51-40-2.SDR CALA9800744Stringer · crackedVERT STAB INNER COMPARTMENT NR 7 STRINGER NR 2 AND NR 3 CRACKED (2) AT ATTACH BOLT. REPAIRED NR 7 RT STRINGER NR 2 AND NR 3 ON VERTICAL STAB PER SRM 55-30-4.SDR DL72L980939Stringer · crackedFOUND ON C2 LETTER CHECK, VERTICAL FIN STRINGER CRACKED AT RIB ATTACH BOLT S-8 AT STA 157.200 RT SIDE. REPAIR PER M/M 53-30-0.SDR ABXA9800414Angle · crackedDURING C-CHECK, FOUND VERTICAL STABILIZER AFT SPAR, RIGHT VERTICAL Z ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-5 AND DACO DWG 5912123.SDR ABXA9800412Angle · crackedDURING C-CHECK, FOUND VERTICAL STABILIZER AFT SPAR LEFT VERTICAL Z ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-5 AND DACO DWG 5912123.SDR SWAA980703Skate Angle · chafedDURING SCHEDULED D-CHECK, FOUND CHAFED RIGHT VERTICAL STAB CLOSURE SKATE ANGLE. REMOVED AND REPLACED PER BOEING SRM.SDR MWEA98560Fairing · chafedFOUND THE BLEND OUT OF CHAFING ON UPPER VERTICAL STABILIZER FAIRING OUT OF LIMITS. MTC REPAIRED WITH DOUBLER.SDR CALA9800701Support · crackedINSPECTION FOUND A 2.5 CRACK IN VERTICAL STABILIZER STRINGER 4L SUPPORT WEB. THE SUPPORT WEB WAS REMOVED IAW SRM 51-30-2. A NEW SUPPORT WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9800700Support · crackedINSPECTION FOUND A 1 CRACK IN VERTICAL STABILIZER SUPPORT WEB AT STRINGER 3L AND STRINGER 3R. THE LT AND RT SUPPORT WEB WAS REMOVED. A NEW SUPPORT WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR TWAA9806507Angle · crackedMCI - DURING OVERNIGHT MAINTENANCE FOUND CRACK MIGRATING OUT OF FASTENER HOLE RT SIDE VERTICAL STABILIZER ATTACH ANGLE, FS 1388. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE PER SRM 51-10-0 AND TWA STD PRACTICES. CHECK-C 2-9-98 STL. ACFT TT: 33,526 HOURS.SDR TWAA9806506Angle · crackedMCI - DURING OVERNIGHT MAINTENANCE, FOUND LOWER ATTACH ANGLE FOR WRAP AROUND FAIRING AT VERTICAL STABILIZER CRACKED THROUGH FASTENER HOLE, 7 IN FORWARD OF PRODUCTION BREAK, LT SIDE FS 1421. REMOVED ATTACH ANGLE AND INSTALLED NEW ATTACH ANGLE PER SRM 51-10-0 ASDR TWAA9806505Angle · crackedMCI - DURING OVERNIGHT MAINTENANCE, FOUND LOWER ATTACH ANGLE FOR WRAP AROUND FAIRING AT VERTICAL STABILIZER CRACKED THROUGH FASTENER HOLE, 7 IN FORWARD OF PRODUCTION BREAK, RT SIDE FS 1421. REMOVED CRACKED ANGLE, INSTALLED NEW ANGLE PER SRM 51-10-0, AND TWA SSDR HALA9800106Tip Fairing · corrodedVERT STABILIZER AFT TIP FAIRING AREA LOWER WEB, DIRECTLY ABOVE TOP OF RUDDER) HAS CORROSION AT SEVERAL SIGHTS, FORWARD MOST AREA 10 INCH BY 8 INCH, LOCATION 2V113 FROM 8 INCH AFT OF AFT SPAR TO 48 INCHES AFT OF SPAR. REMOVED, FABRICATED, REPLACED WEB SECTIO NSDR C2XA98IA113Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEFT SIDE DRAG ANGLE CRACKED IN TWO PLACES AT FORWARD END. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED REPAIR ANGLES IAW CONTINTENTAL EXPRESS EC5530-01013. THE AIRCRAFT WAS APPROVED FOR RETURNSDR CA980421012Bracket · cracked(CAN) DURING 700 HOUR INSPECTION, VERTICAL STABILIZER FRONT FIN PICKUP AT STA 186.40 WAS FOUND CRACKED. CRACK EXTENDED ALONG BOTH WELDED JOINTS BETWEEN SIDE WEBS AND UPPER NUT FACE.SDR GTIA9800040Tie Fitting · crackedOKC - AIRCRAFT UNDERGOING A C-CHECK INSPECTION, THE VERTICAL TIE FITTING ATTACHING THE VERTICAL TO THE FUSELAGE WAS FOUND CRACKED IN HALF. (M)SDR CALA9800578Support · crackedINSPECTION FOUND A .375 INCH CRACK AT LOWER RIVET HOLE IN FORWARD LEFT VERTICAL STABILIZER SPAR SUPPORT AT 37.3 INCHES AFT OF STA 1089.3 IN TAIL COMPARTMENT ABOVE CATWALK. THE AREA WAS REPAIRED IAW SRM 55-02, FIGURE 26.SDR USAA980122Drag Angle · crackedPIT - DURING Q-1 CHECK, FOUND .5 INCH CRACK AT VERTICAL LEG OF LT VERTICAL STAB DRAG ANGLE AT STATION 1288 CANTED. INSTALLED NESTED ANGLE PER SRM 53-05 FIG 23B. (M)SDR SWAA980335Web · crackedDURING SCHEDULED D-CHECK, FOUND VERTICAL STAB WEB FIN AT BS 69.4 26 FWD OF RUDDER HINGE IS CRACKED. REMOVED AND REPLACED PER BOEING SRM.SDR HEEA0013451Fin Assy · damagedINSPECTED FIN, FOUND DAMAGE IN AREA WHERE NO STRUCTURAL DAMAGE ALLOWED TO VERTICAL FIN STRUCTURE AS PER BHT-206-SRM-1 SECTION 6-3-9. SCRATCH 2 3/4" LONG DEPTH .001-.004. STINGER HOLE OVERSIZED.SDR DL72S980662Skin · crackedSKIN CRACKED, PREVIOUSLY STOP DRILLED CRACK AT BASE OF VERTICAL STAB FRONT SPAR, RT SIDE. REMOVED FASTENERS. CUT OUT DAMAGED SECTION OF SKIN. E/C INSP OK. FABRICATED FILLER AND BEGAN FABRICATION OF DOUBLER PER SRM 55-30-3. OK TO INSTALL DOUBLER. STARTED SDR DL72S980640Web · crackedWEB CRACKED VERT STAB INTERIOR, VERTICAL WEB OVER S-DUCT IS CRACKED AT BOTH LOWER CORNERS (2 PLACES). REMOVED FASTENERS DYE PEN'D STOP DRILL, NO CRACK NOTED AFTER STOP DRILL HOLES ON BOTH SIDES, FABRICATED NEW DOUBLERS AS PER SRM 53-10-4 FIG 17. INSTALLED DOSDR DL72S980595Stringer · crackedFOUND .75 INCH CRACK IN VERT STAB STRINGER 8R AT THIRD BULKHEAD ABOVE CRAWLWAY OPENING FIN STA 133.8. REPAIRED PER MM 55-30-0 FIG 803.SDR CALA9800446Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN VERTICAL STABILIZER FORWARD LEFT SPAR SUPPORT ANGLE AT APPROXIMATELY 37.5 INCHES AFT OF STA 1089.5 IN TAIL COMPARTMENT ABOVE CATWALK. REPAIRED ANGLE IAW SRM 55-02, FIGURE 26.SDR CALA9800445Angle · crackedINSPECTION FOUND A .375 INCH CRACK IN VERTICAL STABILIZER FORWARD RIGHT SPAR SUPPORT ANGLE AT APPROXIMATELY 37.5 INCHES AFT OF STA 1089.5 IN TAIL COMPARTMENT ABOVE CATWALK. THE ANGLE WAS REPAIRED IAW SRM 55-02, FIGURE 26.SDR CALA9800428Stringer · crackedINSPECTION FOUND VERTICAL STABILIZER INTERNAL COMPARTMENT NR 9 RT NR 3 STRINGER CRACKED 1 BEHIND ATTACH BOLT. REMOVED FASTENERS IAW SRM 51-30-2. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-2, AND 51-40-5.SDR CALA9800427Stringers · crackedINSPECTION FOUND VERTICAL STABILIZER INTERNAL COMPARTMENT NR 6 RT NR 3 STRINGER AND NR 5 STRINGER CRACKED 1 BEHIND ATTACH BOLT. REMOVED FASTENERS IAW SRM 51-30-2. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-2, AND 51-40-5.SDR P5CA9800583Nut Plate · damagedTWELVE DAMAGED NUT PLATE ON VERTICAL FIN. REMOVED AND REPLACED PER SRM 51-30-02.SDR DL72S980529Stringer · crackedFOUND AT C2 LETTER CHECK, .5 INCH CRACK IN VERT STAB S-7L, INSIDE VERT STAB CRAWLWAY THIRD BULKHEAD ABOVE OPENING. REPAIRED PER M/M 55-30-0 .SDR DL72S980528Stringer · crackedFOUND AT C2 LETTER CHECK, .75 INCH CRACK IN VERT STAB S-9L, INSIDE VERT STAB CRAWLWAY, FOURTH BULKHEAD ABOVE OPENING. REPAIRED PER M/M 55-30-0.SDR QXEA9800466Angle · crackedCRACKS AT BOTH ENDS OF TRANSVERSE ANGLE AT FWD BASE OF VERT STAB. REPAIRED IAW FOKKER SRM 51-10-05 PAGE 601.SDR SCNA98029Fastener · shearedDURING A SCHEDULED MAINTENANCE INSPECTION, THE AFT LOWER RIGHT HAND FASTENER WAS FOUND SHEARED OFF ON THE NUT SIDE FOR THE NUMBER FOUR BANJO FITTING ATTACHMENT. THE AREA WAS REWORKED IN ACCORDANCE WITH SERVICE BULLETIN DC10-55-023 REVISION TWO.SDR CALA9800273Skin · oversize holesINSPECTION FOUND OVERSIZED HOLES IN FUSELAGE SKIN AT OUTER DORSAL FIN ATTACH ANGLE ON LEFT AND RIGHT SIDES. REPAIRED IAW ECRA 5340-01312.SDR QXEA9800317Fairing · damagedVERTICAL STAB BULLET FAIRING HAS HOLE IN SKIN APPROXIMATELY 20 FORWARD OF STAY 26400, LEFTHAND SIDE MANUFACTURED DOUBLE. STOP DRILLED REPAIRED IAW FOKKER SRM 51-31-01, 55-02-03, PAGE 3, FIGURE 1.SDR CALA9800262Fitting · crackedINSPECTION FOUND A 0.160 INCH CRACK ON VERTICAL STABILIZER NR 4 BANJO FITTING. A REPAIR WAS PERFORMED IAW SRM 55-20-00, FIGURE2, PAGE 28-29 AND 55-20-00, FIGURE 7, PAGE 40.SDR CALA9800242Support · crackedINSPECTION FOUND A 1 CRACK IN CIRCUMFERENTIAL SUPPORT SIDE BRACE OF LT LOWER VERTICAL STABILIZER ABOVE NR 2 ENGINE DUCT. THE SUPPORT SIDE BRACE WAS REMOVED. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-00, 51-21-01, AND 51-31-01.SDR CALA9800213Angle · crackedINSPECTION FOUND VERTICAL FIN INNER ATTACH ANGLE ON RT AND LT SIDES CRACKED. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-30-5.SDR HEEA0012744Rib · damagedTAIL BOOM FIN RIB HAS SANDING MARKS BEYOND 10 PERCENT OF METAL.SDR CALA9800107Angle · crackedINSPECTION FOUND A 1.2 INCH CRACK IN RT LOWER VERTICAL STABILIZER DRAG ANGLE AT FORWARD CENTER SPAR POSITION. THE ANGLE WAS REPAIRED IAW SRM 53-20-00, FIGURE 3.SDR UPS98825831Bracket · corrodedINSPECTION TYPE:D CHECK, VERTICAL STAB FRONT SPAR ATTACH ANGLE IS CORRODED STA 1720 AT LONGERON 13 RIGHT. REMOVED CORROSION FROM VERTICAL STAB FRONT SPAR ATTACH ANGLE AT FS 1720 LONGERON 13 RIGHT IAW DC8 SRM 51-1-8 ALODINED AND PRIMED AREA IAW DC8 SRM 51-1-8SDR W8PA980032Angle · wornPAE- LT VERTICAL STABILIZER TO BODY CLOSURE ANGLE IS CHAFED AND WORN THROUGH ON AFT END. REMOVED ANGLE, INSTALLED NEW ANGLE.SDR DL72K980315Stringer · crackedAT MV2, FOUND STRINGER CRACKED FIN ATA 110.4 STR 10 LT STRINGER IS CRACKED INSIDE VERT STAB. FABRICATED REPAIR DOUBLER PER MM 55-30-00 FIG 803.SDR AALA980155Stringer · crackedTUL - STRINGER CRACKED AT BOLT HOLE INSIDE VERTICAL STABILIZER, BAY NR 10, RT SIDE, 4TH STRINGER FROM BOTTOM. INSTALLED DOUBLER ON CRACKED AREA OF STRINGER PER SRM 55-30-4 FIG 1 AND ESO 11697 DATED 1-14-98. TST: 56,192 HOURS. CYCLES: 34,665. (X)SDR AALA980088Web · crackedTUL - APPROX .75 INCH CRACK IN WEB RADIUS AT UPPER CORNER ATTACH TO VERTICLE FIN RT SIDE STATION 1363. STOP DRILLED CRACK, INSTALLED WEB ANGLE DOUBLER REPAIR PER SRM 51-40-2 FIG 1. (M)SDR CALA9800067Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN RT SIDE OF VERTICAL STABILIZER STRINGER NR 9 BETWEEN RIB NR 7 AND NR 8. THE CRACK WAS LOCATED AT ATTACH BOLT. THE FASTENERS WERE REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-2.SDR CALA9800066Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN LT SIDE OF VERTICAL STABILIZER STRINGER NR 8 BETWEEN RIB NR 8 AND NR 9. THE FASTENERS WERE REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-2.SDR CALA9800051Gusset · crackedINSPECTION FOUND A .5 INCH CRACK AT TOP CORNER AND A .5 INCH CRACK AT LOWER CORNER OF GUSSET ON RT SIDE OF VERTICAL STABILIZER AT STRINGER 9 BETWEEN RIB NR 6 AND NR 7. THE GUSSET PLATE WAS REMOVED, A NEW GUSSET PLATE WAS FABRICATED AND INSTALLED IAW SRM 55-30
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