JASC 5531
Service difficulty reports · 1,234
Reports filed under 5531 · Vertical Stabilizer, Spar/Rib, 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 = '5531' 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 = '5531' 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 DL72L953309Rib · crackedFOUND ON CV2 CHECK, CRACK FOUND INSIDE VERTICAL STABILIZER, 2 BULKHEADS UP FROM ACCESS HOLE ON RT SIDE 2ND RIB UP. CRACKED AT RIB TO BULKHEAD ATTACH POINT. REPAIRED PER M/M 55-30-0 FIG 803.SDR DL72L953308Rib · crackedFOUND ON CV2 CHECK, CRACK FOUND INSIDE VERTICAL STABILIZER, 4 BULKHEADS UP FROM ACCESS HOLE ON LT SIDE 5TH RIB UP. CRACKED AT RIB TO BULKHEAD ATTACH POINT. REPAIRED PER M/M 55-30-0 FIG 803.SDR DL72L953307Rib · crackedFOUND ON CV2 CRACK, FOUND INSIDE VERTICAL STABILIZER, 5 BULKHEADS UP FROM ACCESS HOLE 4TH RIB UP. CRACKED AT RIB TO BULKHEAD ATTACH POINT RT SIDE. REPAIRED PER M/M 55-30-O.SDR DL72L953306Rib · crackedFOUND ON CV2 CHECK, CRACK FOUND INSIDE VERTICAL STABILIZER, 5 BULKHEADS UP FROM ACCESS HOLE 4TH RIB UP. CRACKED AT RIB BULKHEAD ATTACH POINT LT SIDE. REPAIRED PER M/M 55-30-0 FIG 803.SDR ABXA9500648Rib · crackedDURING C - CHECK INSPECTION, SEVERAL RIBS WERE FOUND CRACKED IN THE VERTICAL STABILIZER LEADING EDGE. REPAIRED OR REPLACED RIBS IAW DC-9 SUPP., SRM DRAWING K05159, AND DC-9 SRM 51-30-5, 51-30-2 AND 51-30-3.SDR TSAA9555132Rear Spar · corrodedDURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON LEFT VERTICAL STABILIZER REAR SPAR AT FS 132. REPAIRED PER ECO2509 PART 2. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA9555131Rear Spar · corrodedDURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON LEFT VERTICAL STABILIZER REAR SPAR AT FS 158. REPAIRED PER ECO2509 PART 2. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA9555130Rear Spar · corrodedDURNG HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON LEFT VERTICAL STABILIZER REAR SPAR AT FS 195. REPAIRED PER ECO2509 PART 2. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA9555129Rear Spar · corrodedDURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON LEFT VERTICAL STABILIZER REAR SPAR AT FS 201. REPAIRED PER ECO 2509 PART II. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA9555128Rear Spar · corrodedDURING HEAVY MAINTENACNE VISIT, DISCOVERED EXFOLIATION CORROSION ON RT VERTICAL STABILIZER REAR SPAR AT FS 86. REPAIRED PER ECO2509 PART II. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA9555127Rear Spar · corrodedDURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON RT VERTICAL STABILIZER REAR SPAR AT FS 81. REPAIRED PER ECO2509 PART II. AIRCRAFT RETURNED TO SERVICE. (M)SDR 96ZZZX1866Rib · crackedDURING C-CHECK, FOUND FIXED VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPLACED RIB, PN 9911881-9. AIRCRAFT TT: 35,252. AIRCRAFT TC: 51,897.SDR 96ZZZX1864Spar · corrodedDURING C-CHECK, FOUND VERTICAL STABILIZER REAR SPAR CORRODED ABOVE UPPER RUDDER HINGE FITTING. REPAIRED IAW DC9 SRM CH 55. AIRCRAFT TT: 35,252. AIRCRAFT TC: 51,897.SDR USAA950880Rib · crackedPIT - DURNIG Q-3/CX-2 INSPECTION, FOUND 1 INCH CRACK AT VERTICAL STABILIZER LEADING EDGE LOWER RT RIB. INSTALLED DOUBLER REPAIR PER SRM 52-01. (M)SDR UPS203520Spar Chord · crackedWHILE IN C-CHECK, MAINTENANCE FOUND RT VERTICAL FIN REAR SPAR CHORD CRACKED AT STA 22.5, F.S. 1342. REPAIRED IAW E.O. B727-5530-4601.SDR UPS203519Spar Chord · crackedWHILE IN C-CHECK, MAINTENANCE FOUND LT VERTICAL FIN REAR SPAR CHORD CRACKED STA 22.5, F.S. 1342. REPAIRED IAW SRM 51-10-3.SDR USAA950658Rib · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND .1250 INCH CRACK AT VERTICAL STAB L.E. BOTTOM 7TH RIB. INSTALLED NESTED DOUBLER REPAIR PER SRM 55-01. (X)SDR UPS803305Ribs · crackedWHILE IN C CHECK, MAINTENANCE FOUND VERTICAL STAB LEADING EDGE, 4 RIBS CRACKED AT STA ZFS 217, ZFS 36, ZFS 104, AND ZFS 123. REPAIRED RIBS PER SRM 55-2-0.SDR HAL95067Fitting · crackedSBA - THE UPPER LEFT RUDDER HINGE AT THE REAR SPAR OF THE VERTICAL STABILIZER HAS SURFACE CORROSION AND FITTING IS CRACKED AT THE OUTBOARD SIDE OF THE FASTENER HOLE. REPLACED RUDDER HINGE 'A' ARM IAW MM 27-20-1. (W)SDR 95ZZZX4116Rib · crackedRIGHT SIDE OF VERTICAL STABILIZER, RIB 1, STABILIZER TO FUSELAGE CLOSURE ANGLE HAS 2 INCH CRACK THROUGH FASTENER AT FORWARD EDGE OF VERTICAL STABILIZER. REPAIRED IAW BAE REPAIR DRAWING HC550H9004 AND FAX REF KW/0863-91.SDR 95ZZZX2707Spar · crackedAT ANNUAL INSPECTION, FOUND RT ELEVATOR SPAR CRACKED WITH ONE INCH CRACK RADIATING AWAY FROM RIVET HOLE AT OUTBOARD HINGE ATTACH. POSSIBLE TAIL SECTION IMPACT WITH T-HANGAR MAY BE A CONTRIBUTING FACTOR. REPLACED ELEVATOR SPAR.SDR UPS203097Spar · crackedWHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE VERTICAL STABILIZER RIGHT HAND REAR SPAR CHORD AT STATION 0 TO 12. MAINTENANCE REPAIRED THE ONE INCH CRACK STOP AT FASTENER HOLE.SDR UPS203096Spar · crackedWHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE VERTICAL STABILIZER REAR SPAR LEFT HAND CHORD AT STATION 0 TO 12. MAINTENANCE STOP DRILLED AND INSTALLED THE REPAIR KIT.SDR DL72S951690Spar · crackedAT HMV, FOUND VERTICAL STAB RT FRONT SPAR HAS CRACK STOP DRILLED. MANF, REPAIR DOUBLER, REMOVED DAMAGE, AND INSTALLED PER SRM 55-30-3.SDR UPS202817Rib · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON RT UPPER RIB CHORD AT RBL 70.5, BS 760, FORWARD TWO FASTENER HOLES. INSTALLED REPAIR PER UPS EO B727-5710-1271F.SDR UPS202476Spar · corrodedDURING "C" CHECK MAINTENANCE FOUND CORR ON VERTICAL FIN, RT SIDE, MID SPAR CORRODED AND CHAFED AT AFT ATTACH POINT FOR ACCESS PNL 9602. INSTALLED REPAIR PER UPS EO 727-55-0277.SDR UPS202475Spar · corrodedDURING "C" CHECK MAINTENANCE FOUND CORR ON LT VERT. FIN MID SPAR AT AFT ATTACH POINT FOR ACCESS PNL 9601 PANEL SUPPORT. REPAIRED PER UPS EO 727-55-0276.SDR USAA950287Rib · crackedPIT - DURING SCHEDULED Q-1 INSPECTION, FOUND 1 INCH CRACK IN VERTICAL STAB STATION ZFS 52.3 5TH RIB, CRACK AT SIDE END. INSTALLED DOUBLER REPAIR PER SRM 55-02 FIG 27. (W)SDR 9502519928Beam · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK AND CORROSION IN VERTICAL STABILIZER BEAM ACROSS THE LOWER RUDDER 'A' BRACKET. REPAIRED SPAR ASSEMBLY PER EA 99-0924422.SDR 9502509928Rib · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON VERTICAL STABILIZER RIB ZRS 19. REPAIRED PER EA 99-092433.SDR 95ZZZX1086Spar · crackedDURING COMPLIANCE WITH MANDATORY B.T. 109-96, FOUND AFT VERTICAL FIN SPAR CRACKED AT LOWER END ABOVE HEAVY 'H' BRACKET ON REAR OF SPAR. THIS IS THE SECOND INSTANCE FOUND ON THIS SERIES ACFT. REPAIRED PER AGUSTA SUPPLIED DRAWINGS.SDR DL72W950465Rib · crackedDURING HMV, FOUND RIB CHORD CRACKED AT FIN STA 110 AT STR 10 LEFT. REPAIRED PER MM 55-30-0 PG 802.SDR 95ZZZX1162Stabilizer · mismanufacturedWHILE COMPLYING WITH SB 37 AND SB 38 ON THE HORIZONTAL AND VERTICAL STABILIZERS, FOUND THE VERTICAL STABILIZER FORWARD SPAR WAS INCORRECTLY INSTALLED DURING MANUFACTURE. EIGHTY-FIVE PERCENT OF RIVETS WERE KEY HOLED. THE HORIZONTAL HAD ONE LEADING EDGE RIB WISDR 95ZZZX1161Stabilizer · mismanufacturedWHILE COMPLYING WITH SB 37 AND SB 38 ON THE HORIZONTAL AND VERTICAL STABILIZERS, FOUND THE VERTICAL STABILIZER FORWARD SPAR WAS INCORRECTLY INSTALLED DURING MANUFACTURE. EIGHTY-FIVE PERCENT OF RIVETS WERE KEY HOLED. THE HORIZONTAL HAD ONE LEADING EDGE RIB WI
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