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.

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.Jul 31, 1995 · N505DA · Boeing 727232SDR 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.Jul 31, 1995 · N505DA · Boeing 727232SDR 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.Jul 31, 1995 · N505DA · Boeing 727232SDR 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.Jul 31, 1995 · N505DA · Boeing 727232SDR 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.Jul 24, 1995 · N906AX · Doug DC931SDR 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)Jul 10, 1995 · N802AL · Boeing 7372S5CSDR 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)Jul 10, 1995 · N802AL · Boeing 7372S5CSDR 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)Jul 10, 1995 · N802AL · Boeing 7372S5CSDR 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)Jul 10, 1995 · N802AL · Boeing 7372S5CSDR 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)Jul 10, 1995 · N802AL · Boeing 7372S5CSDR 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)Jul 10, 1995 · N802AL · Boeing 7372S5CSDR 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.Jun 30, 1995 · N919PJ · Doug DC951SDR 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.Jun 30, 1995 · N919PJ · Doug DC951SDR 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)Jun 22, 1995 · N982VJ · Doug DC931SDR 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.Jun 13, 1995 · N942UP · Boeing 72722CSDR 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.Jun 13, 1995 · N942UP · Boeing 72722CSDR 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)Jun 1, 1995 · N983VJ · Doug DC931SDR 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.May 24, 1995 · N802UP · Doug DC873FSDR 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)May 23, 1995 · N420EA · Doug DC951SDR 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.May 4, 1995 · N611AW · Bag BAE146300ASDR 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.May 1, 1995 · N9033Y · Cessna 182ESDR 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.Apr 23, 1995 · N922UP · Boeing 72731CSDR 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.Apr 23, 1995 · N922UP · Boeing 72731CSDR 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.Apr 12, 1995 · N494DA · Boeing 727232SDR 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.Apr 1, 1995 · N928UP · Boeing 72722CSDR 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.Feb 22, 1995 · N933UP · Boeing 72725CSDR 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.Feb 22, 1995 · N933UP · Boeing 72725CSDR 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)Feb 17, 1995 · N971VJ · Doug DC931SDR 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.Feb 11, 1995 · N8921E · Doug DC931SDR 9502509928Rib · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON VERTICAL STABILIZER RIB ZRS 19. REPAIRED PER EA 99-092433.Feb 11, 1995 · N8921E · Doug DC931SDR 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.Feb 10, 1995 · N109RP · Agusta A109A2SDR DL72W950465Rib · crackedDURING HMV, FOUND RIB CHORD CRACKED AT FIN STA 110 AT STR 10 LEFT. REPAIRED PER MM 55-30-0 PG 802.Feb 1, 1995 · N293WA · Boeing 727247SDR 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 WIJan 11, 1995 · N3093M · Ayres S2RNORMALSDR 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 WIJan 11, 1995 · N3093M · Ayres S2RNORMAL
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