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 DL72K000925Spar · crackedAT HMV2 FROM N/R 794 - FABBED PER PRI 334389-14 4-27-00/1900, INSTALLED, FABBED ACCESS DOUBLER AND PANEL PER OPN 7951, R/C 994. REMOVED FASTENERS ON STRINGER 6 BELOW ACCESS HOLE TO FOM, FABBED ACCESS PANEL/DOUBLER PER OPN 7951/R/C994.SDR AU000147Rib · cracked(AUS) VERTICAL STABILIZER RIB CRACKED. FORWARD SPAR RIVETS LOOSE. DRAG ANGLE PN 71059-06 CRACKED. CRACK LENGTH 20 MM (0.787 INCH).SDR 00FDEA00261Stringer · crackedVERTICAL STABILIZER STR 9 RT IS CRACKED WHERE IT ATTACHES TO RIB NR 7. *S/D* REMOVED AND REPLACED NEW STRINGER PER FEDEX SRM 55-30-04 PG 5.SDR AALA20000677Skin · crackedTUL- VERTICAL STABILIZER SKIN CRACKED AT STA 1340, LEFT SIDE. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER BOEING SB 727-55-82. (X)SDR UPS00232258Frame · corrodedINSPECTION TYPE:C, CORROSION ON VERT STAB ON T-CHORD AFT OF FEEL COMPUTER. REPLACED T-CHORD IAW SRM 51-30-2. REF IPC 55-30-00, FIG 2.SDR CALA0000387Spar · crackedINSPECTION FOUND A .5 INCH CRACK IN REAR SPAR VERTICAL STABILIZER RT LOWER ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-3, 51-10-3, AND 51-30-2.SDR UPS00832411Rib · crackedINSPECTION TYPE:C123 STA 1746 LONG 4L-4R CANTED CENTER SUPPORT RIB IS CRACKED AT BOTH ENDS. REMOVED, FABRICATED AND REPLACED RIB IAW DWG 56144140 AND SRM 51-1-20D.SDR ASAA0080232Skin · gougedSEA - DURING INSPECTION, A GOUGE DAMAGE WAS NOTED ON THE LEFT SKIN OF THE VERTICAL STABILIZER TIP. REPAIRED SKIN PER EA 5530-01055. (M)SDR RRXA000695Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE VERTICAL STABILIZER LWR L/E RIB NR 11 FROM TOP LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 55-5-1 FIG 2.SDR RRXA000694Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE VERTICAL STABILIZER LOWER L/E RIB NR 12 TOP LT DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 55-5-1 FIG 2.SDR RRXA000686Rib · crackedDURING A MAINTENANCE VISIT FOUND 2 CRACKS AT THE VERTICAL STABILIZER L/E RIB NR13 FROM TOP (1 LT AND 1 R/H) ON END OF RIBS, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DSDR QXEA0000646Rib · crackedPDX - VERTICAL STAB RIB 3.2 HAS A CRACKED LEFT LOWER FLANGE AT AFT END, SEVERAL CRACKS EXTEND THROUGH AND CONNECT APPROXIMATELY FOUR RIVET HOLES. REPAIRED IAW HORIZON AIR EA 4-55-194.SDR UPS00831918Rib · crackedINSPECTION TYPE:C123, LOWER VERTICLE STAB L/E RIB IS CRACKED RIGHT SIDE AT ZFS 111.00. REPAIRED IAW SRM 55-2-0 FIG 2.SDR CA000307007Spar · cracked(CAN) INSPECTION REQUIRED BY CF91-42 FOUND FRONT SPAR AND GUSSET PLATES CRACKED. P/N''S C2TP57 AND C2TP171 WERE REPLACED.SDR P2EA00063Frame · corrodedSJO - DURING Q-CHECK, FOUND CORROSION ON VERTICAL STABILIZER AT RIGHT SIDE CHORD AT FIN STATION 77.77. REPAIRED STABILIZER CHORD BETWEEN STATION 67.44 AND STATION 105.5 IAW COOPESA EO COO=3=55-084-00 DATED 02/11/2000. FABRICATED SPAR SECTION IAW COOPESA COO-SDR DL72L000280Stringer · crackedSTRINGER 6 RT CRACKED VERT INTERIOR 4TH FRAME DOWN FROM 9504 RIB NR 2. BEGAN FABRICATED REPAIR PER M/M 55-30-0 PG 803. FINISHED FABRICATING REPAIR ANGLE PER M/M 55-30-0 FIG 803. OK TO TREAT AND PAINT. CHEM TREATED AS PER PS 900-2-4-1 NR 2. TREATED AND PAISDR UPS00431744Rib · crackedINSPECTION TYPE:C 44.TAIL.RIGHT HAND OUTBOARD ELEVATOR BALANCE WEIGHT SUPPORTS CRACKED AT STATIONS 261,285 AND 295.REPAIR SUPPORT STRUCTURE PER SRM. NEW SUPPORTS FABRICATED AND FITTED I.A.W SRM 51-10-01 AND 51-30-02.SDR GAIA99235Spar · corroded'NO FLIGHT', FOUND DURING 'HEAVY 2 MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (OSCODA MI). VERTICAL STABILIZER FORWARD SPAR CORRODED AT FS 55R. REMOVED DAMAGED AREA IAW ENGINEERING DEVIATION REQUEST B2-07305. PERFORMED HFEC AND LIGHT INSPECTION SDR CA000307013Spar · cracked(CAN) DURING INSPECTION, STABILIZER CENTER SECTION OF FRONT SPAR FOUND CRACKED. SECTION REPLACED COMPLETE WITH NEW SPLICE PLATE AND DOUBLERS.SDR DL72L992667Stringer · crackedAT HMV2, FOUND STRINGER 5R CRACKED AT RIB NR 9 VERT STAB INTERIOR. DYE CHECKED AND FOUND CRACK EXTENDS TO EDGE OF MATERIAL. CHEM TREATED PER PS 900-2-4-1 NR 2, FABRICATED REPAIR PER MM 55-30-0 PG 803, AND INSTALLED PER SAME.SDR 20000502AP003Stringer · crackedFOUND STRINGER CRACKED IN COMPARTMENT ABOVE FIN STATION 133.8, STRINGER IS FIFTH UP FROM BOTTOM OF COMPARTMENT. INSTALLED REPAIR PER SRM 55-30-1 FIG 1. (M)SDR F3LA99139Rib · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION ON RIGHT VERTICAL STABILIZER RIB CAPS AROUD NUTPLATES AT BS 58. MAINTENANCE REPLACED UPPER AND LOWER CHORDS PER SRM 51-30-2 AND 51-30-5. (M)SDR 9905082287Spar · crackedDURING H-CHECK, FOUND CRACKS EMITTING IN LEFT VERTICAL STABILIZER SKIN AT REAR SPAR CHORD. REPAIRED PER EA 22-170717, REV A.SDR 99UAL900515Spar · chafedTHE VERTICAL STABILIZER MID SPAR CHORD AT FIN STATION 215 ON BOTH THE RIGHT AND LEFT SIDES WERE FOUND CHAFED TO BELOW THE MINIMUM ALLOWABLE THICKNESS OF THE CHORD. THE DAMAGED AREAS WERE BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPASDR UPS99230636Spar · corrodedINSPECTION TYPE:C, RT VERTICAL MID SPAR FRETTING WHERE PANEL 9602 ATTACHES AT AFT END. REPAIRED LT VERTICAL MID SPAR WITH SPLICE REPAIR IAW ERN 99-5888.SDR 99UAL900474Spar · corrodedTHE VERTICAL STABLE MID SPAR CHORD AT FIN STATION 215 ON THE LEFT SIDE WAS FOUND CHAFED TO BELOW THE MINIMUM ALLOWABLE THICKNESS OF THE CHORD. THE DAMAGED AREA WAS BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THIS RSDR 2000ZZZX347Spar · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION ON VERTICAL FIN ON LT AND RT REAR SPAR AT STA ZR 45. REPAIRED CORROSION DAMAGE IAW FINE LINES EA NR G5531-01:00, SEMAN EO NR 990092 AND BOEING MESSAGE M-7200-99-08438.SDR 99UAL900429Spar · chafedTHE VERTICAL STABILIZER MID SPAR CHORD AT FIN STATION 215 ON THE LEFT SIDE WAS FOUND CHAFED TO BELOW THE MINIMUM ALLOWABLE THICKNESS OF THE CHORD. THE DAMAGED AREA WAS BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THSDR DL72L991852Rib · crackedAT HMV 2 FOUND VERT STAB INTERIOR-RIB CHORD HAS CRACK AT PREVIOUS STRINGER REPAIR-RT SIDE OF VERT AT STA 110.4 STR 10. STOP DRILLED CRACK PER MM 55-30-00 FIG 802. MADE REPAIR ANGLE PER SAME, INSTALLED.SDR 99UAL900406Spar · chafedTHE VERTICAL STABILIZER MID SPAR CHORD AT FIN STATION 215 ON THE LT SIDE WAS FOUND CHAFED TO BELOW THE MINIMUM ALLOWABLE THICKNESS OF THE CHORD. THE DAMAGED AREA WAS BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THISDR UPS99230635Spar · corrodedINSPECTION TYPE:C, LT VERTICAL MID SPAR FRETTING WHERE PANEL 9601 ATTACHES AT AFT END. REPAIRED LT VERTICAL MID SPAR WITH SPLICE REPAIR IAW ERN 99-5888.SDR 99ZZZX3711Spar · crackedAFTER REMOVAL OF THE VERTICAL STABILIZER LEADING EDGE, THE LEFT HORIZONTAL STABILIZER ATTACH FITTING ATTACHED TO THE VERTICAL STABILIZER FRONT SPAR WAS FOUND CRACKED. IT ORIGINATED FROM THE BOTTOM HUCK BOLT HOLE, UPWARD AND ALONG SIDE THE NEXT HUCK BOLT AND SSDR 99UAL900395Spar · chafedTHE VERTICAL STABILIZER MID SPAR CHORD AT FIN STATION 215 ON THE LEFT SIDE WAS FOUND CHAFED TO BELOW THE MINIMUM ALLOWABLE THICKNESS OF THE CHORD. THE DAMAGED AREA WAS CUT OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THIS SDR QXEA9901485Rib · chafedPDX - V STAB AT RIB 5.0 AND INTERMEDIATE SPAR II RIGHT SIDE HAS CHAFE DAMAGE FROM STAB. REPAIRED IAW HORIZON AIR EA 4-55-149.SDR UF6A990713Rib · crackedSBN - RIB AT STATION 351.75 IN VERTICAL FIN CRACKED. MAINTENANCE REPAIRED THE RIB IAW BAE SRM 51-60-03. (M)SDR TWAA9909910Rib · crackedDURING OP 16 MAINT CHECK, FOUND STA ZPS 52 RIB CRACKED LT LOWER CORNER, STA ZFS 52 RIB CRACKED LOWER CORNER, AND STA ZFS 45 RIB CRACKED IN THE LOWER CORNER. REPAIRED PER SSRM 55-30-02.SDR 99ZZZX2984Spar · separatedDURING A 100-HOUR INSPECTION, FOUND THAT THE VERTICAL TAIL SPAR HAD DISBONDED WITH FUSELAGE AND THE AREA BELOW WHERE THE TAIL SKID IS FORMED HAS CRACKED.SDR 99ZZZX2983Spar · sedparatedDURING A 100-HOUR INSPECTION, FOUND THE VERTICAL TAIL SPAR HAD DISBONDED WITH FUSELAGE AND THE AREA BELOW WHERE THE TAIL SKID IS FORMED HAS CRACKED.SDR CA990707021Frame · cracked(CAN) DURING SCHEDULED INSPECTION, A CRACK WAS LOCATED AT A RIVET HOLE ON FRAME NR 4 OF VERTICAL STABILIZER. REPAIRED BY DWG NR 8-55-199.SDR MZZA99122Spar Chord · corrosionTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON VERTICAL STABILIZER FRONT SPAR LEFT CHORD AT FS 54. THE CORRODED AREA IS TRIMMED OUT AND REPAIRED PER ECRA 5530-01250. ISSUE A NEW DIP NR CM 556 TO READ AS FOLLOWS WITHIN 11 MONTSDR CALA9900482Spar · crackedVERTICAL STAB UPPER RIGHT LEADING EDGE SPAR CRACKED (.25) AROUND RIVET AT STIFFENER PLATE JUST BELOW TENSION TIE FORWARD ATTACH BOLT. REMOVED FASTENERS. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR PER SRM 55-30-6 AND 51-1-20.SDR DL72E990992Rib · crackedLT STR TO RIB ATTACH FLANGE CRACKED INSIDE VERTICAL FIN AT RIB STA 179 STR 8L. FABRICATED REPAIR PER M/M 55-30-0 FIG 803. OK TO INSTALL. REPAIRED PER M/M 55-30-0 RIG 803.SDR AALA990559Spar Web · crackedTUL - FOUND CRACK IN VERTICAL SKIN REAR SPAR RIGHT JUST ABOVE FUSELAGE SKIN. INSTALLED DOUBLER IAW SRM 55-30-3. (M)SDR LR7A9917Web · crackedDURING C CHECK/BRIDGING INSPECTION, FOUND FS 1095 VERTICAL STABILIZER WEB CRACKED FROM VSS 9 TO 12. REPAIRED BY DOUBLER INSTALL IAW SPAR MPP L100-404-99-061, DWG R99-0002-08. LAC MEA 382-53-99-027.SDR CA990430036Spar · fractured(CAN) THE VERTICAL FIN REAR MAIN SPAR WEB BELOW THE UPPER RUDDER HINGE FOUND TO BE CRACKED IN SEVERAL PLACES. DISCUSSIONS WITH THE MANUFACTURER REVEALED THAT THE LATEST MODELS OF THIS AIRCRAFT HAVE A STRONGER REAR SPAR IN THE FIN.SDR 99ZZZX1609Bolt · wrong partDURING ANNUAL INSPECTION, FOUND INCORRECT HARDWARE INSTALLED ON AFT VERTICAL FIN SPAR ATTACH. BOLTS INSTALLED WERE STANDARD AN HARDWARE. BOLT SHOULD HAVE BEEN A NAS224-15. CONTACTED CESSNA PARTS DEPT AND FOUND THE PART NUMBER HAD BEEN SUPERCEDED TO MS27039-SDR 99T64R384ARSpar · corrodedNR 2569 - VERTICAL STABILIZER REAR SPAR LT TIP FAIRING ATTACH POINT ABOVE STA ZV299 HAS CORROSION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. DYE PENETRANT BLENDED AREA NO CRACKS EXIST, FLAP PEENED AND TREATED AREA PER EO 99-044 AND 99-061 WITH APPROVED FAA FORMSDR UPS99228916Spar · crackedINSPECTION TYPE-C, LT VERTICAL FIN REAR SPAR CHORD IS CRACKED AT INTERSECTION WITH BS 1342 BULKHEAD. STOP DRILLED CRACK, ALODINED AND PRIMED STOP DRILL HOLE, FABRICATED REPAIR ANGLE AND FILLER DRILLED UP AND INSTALLED REPAIR PARTS IAW SRM 51-10-1, 51-20-01, 5SDR AT9900147Spar · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE VERTICAL STABILIZER LEFT HAND AFT SPAR AT STA 183 TO 205.5 CORRODED. REMOVED TWO PANELS TO GAIN ACCESS, REMOVED ALL CORROSION, TREATED, PRIMED AND REINSTALLED PANEL AND SEAL PANELS IAW B737 SRM 51-10-2, 51-10-6SDR DL72K990260Rib · corrodedCORROSION FOUND ON THE INBD FACE OF THE INBD LUG ON THE LT FIN CLOSURE RIB CLEVIS. DAMAGE REMOVED WITH A 1.6 DIA SPOTFACE W/DEPTH OF 0.062. REWORKED PER ERA 332753-14.
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