JASC 5532
Service difficulty reports · 1,753
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 JR2R20160923116Skin · chafedVERTICAL STAB CAP FAIRING RT LOWER SKIN CHAFED. REMOVED AND REPLACED SKIN IAW EA 25-2016-245.SDR CALA2016092200676Skin · damagedDAMAGED FASTENER ON RT VERTICAL STAB IN SPAR SKIN VSS 224, 11TH FASTENER FROM FWD EDGE. PERFORMED PART 1-INTERIM REPAIR STEPS 1-6 OF ECRA 5530-01770.SDR DALA2016091206542Skin · dentedDURING INSPECTION, FOUND VERTICAL LEADING EDGE HAS A DENTED 36 INCHES FROM EPPER END LT SIDE. MAINTENANCE REPAIRED THE DENT ON VERTICAL STAB LEADING EDGE BY INSTALLING EXTERNAL DOUBLER IAW SRM 53-30-01 REPAIR 1.SDR DALA2016090206361Structure · damagedDURING INSPECTION, FOUND ALL HOLES IN BOTH FASTENER ROWS BELOW ZFS 52.267 ELONGATED. REPAIRED ELONGATED HOLES IAW SECTION I: PERMANENT REPAIR OF ER/A 550371-14AD, REV ORIGINAL.SDR DALA2016090206351Structure · damagedDURING INSPECTION, FOUND ALL HOLES IN BOTH FASTENER ROWS BELOW ZFS 52.267 ELONGATED. REPAIRED ELONGATED HOLES IAW SECTION I, PERMANENT REPAIR OF ER/A 550371-14AD, REV ORIGINAL.SDR DALA2016082806253Skin · damagedLOOSE FASTENERS ON VERTICAL STABILIZER LEADING EDGE UPPER/LOWER SPLICE VSS 52.267. HOLES ON VERTICAL STABILIZER LEADING EDGE WERE REPAIRED IAW SRM 55-03D PAR. 28 FIGURE 30 AND PAR. 27 FIGURE 29.SDR DALA2016082806252Skin · damagedLOOSE FASTENERS ON VERTICAL STABILIZER LEADING EDGE UPPER/LOWER SPLICE VSS 52.267. HOLES ON VERTICAL STABILIZER LEADING EDGE WERE REPAIRED IAW SRM 55-03D PAR. 28 FIGURE 30 AND PAR. 27 FIGURE 29.SDR DALA2016081906087Skin · damagedVERTICAL STAB RIGHT SIDE BELOW AND FORWARD OF LOWER RIGHT VOR ANTENNA SEVERAL SCREWS PULLED THROUGH SKIN. REPAIR WAS ACCOMPLISHED IAW ER/A 549263-14AD REV. ORIGINAL.SDR CWQR20160725026Skin · corrodedCORROSION WAS DISCOVERED ON THE VERTICAL STABILIZER SKIN. THE CORROSION WAS REMOVED AND VERTICAL STABILIZER SKINS WERE REPAIRED IAW ERO-850036, REV IR.SDR CWQR20160725025Skin · corrodedCORROSION WAS DISCOVERED ON THE VERTICAL STABILIZER SKIN. THE CORROSION WAS REMOVED AND VERTICAL STABILIZER SKINS WERE REPAIRED IAW ERO-850036, REV IR.SDR DALA2016110108049Access Panel · corrodedCORROSION ON DORSAL FIN JUST ON SETTLEMENT AREA OF ACCESS PANEL 370 AL. FABRICATED NEW AND REPLACED IAW SRM 51-41-02, 51-20-09, 51-10-04 PAR 15 AND 21, AND DWG 5911432 REV "CF".SDR DALA2016070705237Fastener · looseFOUND FASTENER LOOSE FROM THE APEX OF BS 2FS 52.267, 4 ROWS DOWN. OUT OF LIMITS. REPAIRED IAW DWG SG 9550004 AND SRM 55-03.SDR DALA2016070705236Fastener · looseFOUND FASTENERS LOOSE FROM THE APEX OF STATION 2FS 52.267, 2 ROWS DOWN. OUT OF LIMITS. REPAIRED IAW DWG SG09550004 AND SRM 55-03.SDR DALA2016070705234Fastener · looseFOUND FASTENER LOOSE FROM THE APES OF STA 2FS 52.267. OUT OF LIMITS. REPAIRED IAW DWG SG 9550004 AND SRM 55-03.SDR JR2R20160705353Fairing · crackedVERTICAL STABILIZER UPPER FORWARD FAIRING AFT ATTACH FLANGE IS CRACKED. REPAIRED VERTICAL STABILIZER UPPER FORWARD FAIRING AFT FLANGE IAW SRM 55-01, FIGURE 2, SHEET 3.SDR DALA2016062304862Skin Panel · damagedVERTICAL STABILIZER, RT L/E LOWER MAIN SKIN PANELS DENTED AND GOUGED. REPAIRED SKIN IAW ER/A 547396-14, REV ORIGINAL, ER/A MATCHES ALL PRIS.SDR DALA2016062104810Skin · crackedCRACKED SKIN ON LT STA YV=160.688 APPROXIMATELY TIP FAIRING. AREA WAS REPAIRED IAW SRM 55-01, FIG 4, SHEET 2.SDR IPXA2016063005263Panel · delaminatedINSPECTION TYPE: C-13, FOUND MULTIPLE AREAS OF DELAMINATION ON THE VERTICAL STAB LT LOWER FORWARD TORQUE BOX PANEL. REMOVED AND REPLACED THE PANEL IAW SRM 51.40.02SDR JR2R20160615386Cover · crackedVERTICAL STABILIZER AFT SPAR PANEL NR 6404, 2 EA CRACKS .5" IN LENGTH AT FASTENER HOLES LT AND RT SIDES. REPAIRED VERTICAL STABILIZER PANEL 6404 BY SUBSTITUTING REPAIR MATERIAL .032" 2024-T3 IN PLACE OF .032" 2024-T42 IAW SRM 51-60-0, FIG 1, SHT 1 AND SRM 55-SDR DALA2016061604670Skin · crackedVERTICAL STABILIZER L/E HAS A 3" CRACK & FASTENERS PULLED INTO THE SKIN & ELONGATED HOLES BY LWR VOR ACCESS PANELS, REMOVED DAMAGE, FABRICATED FILLERS AND DOUBLERS USING 7075-0 HEAT TREATED TO 7075-T6 2090. INSTALLED REPAIR PARTS IAW ER/A 545681-14AD REPETITISDR DALA2016060604391Skin · crackedVERTICAL STAB L/E FWD OF RAM AIR SCOOP COMMON TO PANEL 370AL LOWER LT SIDE SKIN IS CRACKED AND UPPER AREA IS HEAVILY ERODED. REPLACED DOUBLER, PN 5910242-121, SKIN, ON VERT SLAB DORSAL FIN FWD OF RAM AIR SCOOP COMMON TO PANEL 370 AL IAW SRM 51-41-02, PG 1 PARSDR DALA2016062404927Skin · damagedDENT AND GOUGES IN RT VERTICAL STABILIZER SKIN APPROXIMATELY 12" ABOVE FUSELAGE BETWEEN CS 1103 AND CS 1131. BLEND AREA OF PAINT FOR HFEC. REF SRM 53-01-01. ACCOMPLISHED HFEC INSPECTION OF BLENDED AREA IAW NDT SPM 06-10-01.001. NO CRACKS NOTED. ALODINE ANDSDR SWIA201642175Skin · chafedVERTICAL STABILIZER PANEL 326CR HAS CHAFING. INSTALLED NEW VERTICAL STABILIZER PANEL 326CR IAW SRM.SDR DALA2016051303916Skin · gougedVERTICAL STABILIZER SKIN RT GOUGED UNDER PANEL 360AT. REPLACED NEW VERTICAL STABILIZER SKIN RT IAW DWG 5936143 AND 51-41-02, PARA 4 AND 51-41-05, PARA 2.SDR DALA2016042503246Skin · crackedCRACKED INTERNAL UPPER SKIN AT VERTICAL STABILIZER L/E, RT LOWER CORNER. SKIN REPAIRED IAW ER/A 483924-14MA, REV ORIGINAL.SDR DALA2016041502927Skin · damagedVERTICAL STABILIZER L/E ZFS 52.267, NUMEROUS FASTENERS LOOSE, SEVERAL FASTENERS PULLED THROUGH AND PARTIALLY PULLED THROUGH. REPAIRED VERTICAL STABILIZER L/W FASTENERS HOLES IAW SERVICE DWG SG 95550001, REPAIRED CRACK ON VERTICAL STABILIZER. FOUND DURING OPSDR FDEA201604051143Skin Panel · delaminatedVERTICAL STAB SKIN PANEL LT SIDE, BELOW THE ANTENNA COUPLER HAVE BULGING & DELAMINATED SECTION IAW SRM 55-30-01-1A FIG 101. NOT REPAIRABLE, FOUND OUT OF LIMITS. R & R WITH NEW PANEL, PN 175N2001-3, BATCH 0002920531 IAW SRM 51-40-02-0G & DWG 175N2001, PANEL ISDR EE4Y2016033100017Skin · dentedEMPENAGE VERTICAL STABILIZER LT SIDE WITH DENTS AT RIB 10+480MM AND RIB 10+515 MM BETWEEN STR 3 AND MID SPAR. DAMAGE HAS BEEN REPORTED UNDER NON ROUTINE ITEM A1E131, 3-4. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2016-190-028858, INSTRUCTION AND APPROVED.SDR C77A20160329001Skin · crackedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF THE RT VERTICAL STAB SKIN CRACK DAMAGE. REF FIGURE 1 FOR DAMAGE LOCATION & DIMENSIONS. REQUESTED PERMANENT REPAIR RELIEF & RECEIVED FROM ETD 2016-170-030649. BECAUSE THE VSDR DALA2016032602308Skin · wornWORN VERTICAL STABILIZER SKIN BS 170, LT SIDE. WORN VERTICAL STABILILZER SKIN BS 170, LT SIDE WAS ATTENDED WITH ER/A 543218-14, REV A.SDR DALA2016032302244Skin · wornLOOSE FASTENERS, 2 ROWS ABOVE AND BELOW BS ZFS=52 AT VERTICAL STABILIZER L/E REMOVABLE. DUE TO EXCESSIVE WEAR ON THE UPPER COUNTERSINK THE L/E SKIN WAS REPAIRED AND THE LOWER SKIN WAS FOUND WITHIN LIMITS IAW SRM 55-03D, PAR 28, 27 AND DWG SG09550004. REV D. SDR FDEA201603180952Skin Panel · delaminatedRIGHT VERTICAL STAB FIXED PANEL EXTERNAL SURFACE BETWEEN AUXILIARY SPAR & FRONT SPAR & APPROX BETWEEN FSS 220.521 & 245.652, HAS DELAMINATION. RT VERTICAL STABILIZER FXED PANEL FOUND DELAMINATED IAW SRM 55-30-01-1A FIG 101, NOT REPAIRABLE. FOUND TO BE OUT OFSDR C77A20160316001Skin · crackedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF THE RT VERTICAL STAB SKIN CRACK DAMAGE. REFERENCE FIGURE 1 FOR DAMAGE LOCATION & DIMENSIONS. REQUESTED PERMANENT REPAIR RELIEF & RECEIVED FROM ETD2016-170-024613B. BECAUSESDR DALA2016031501953Skin · dentedDENT AT VERTICAL STABILIZER TIP AT BS YV 215.200. DENT ON VERTICAL STABILIZER WAS REPAIRED IAW SRM 55-01, FIG 4, SHEET 2.SDR DALA2016031101868Skin · crackedVERTICAL STABILIZER HAS A CRACK ON TOP L/E. REMOVED DAMAGED SKIN BETWEEN STOP DRILLS. TRIMMED OUT DAMAGED AREA. HFEC IAW SPM 6-10-01.001. FABRICATED AND INSTALLED INTERNAL DOUBLER AND FILLER IAW PRI 544417-14, REV O. IDENTIFIED REPAIR IAW 900-5-1, NR 4. RSDR DXTR2016031002Skin · corrodedCORROSION FOUND AT MULTIPLE SITES ON THE LT & RT VERTICAL STABILIZER SKINS. REPAIRED IAW STRUCTURES REPORT NR: S-680-014/05RD.SDR DALA2016022401385Finger Doubler · crackedVERTICAL L/E SKIN LOWER FINGER DOUBLER CRACKED. FABRICATED AND INSTALLED REPAIR PART IAW DWG 5930609 AMD SG09550005.SDR DALA2016021601052Skin · damagedVERTICAL STABILIZER L/E WRAP AROUND SKIN PANEL JUST BELOW REMOVABLE PANELS 370DL 370GR HAS SEVERAL LOOSE SMOKING FASTENERS PULLING THROUGH SKIN. INSTALLED FABRICATED REPAIR DOUBLER AT VERTICAL STABILIZER WRAP AROUND SKIN PANEL IAW SRM 53-30-01, REPAIR (7) ANDSDR DALA2016020800922Skin · damagedSUNKEN FASTENERS 9 EA AT REMOVABLE L/E SECOND ROW ABOVE BS ZFS=52.267 VERTICAL STABILIZER. VERTICAL STABILIZER WAS REPAIRED IAW SRM 55-03D, PAR 28, FIG 30, 55-03, PAR 27, FIG 29, 51-10-3, PAR 14/21, 51-10-2, 51-10-4 AND 51-30-5 AND AMDS 55-30-01045-08.SDR IPXA2016021699462Panel · dentedINSPECTION TYPE: C10, VERTICAL STABILIZER RT LOWER FWD PANEL HAS 2 DENTS STREAMER ATTACHED, DENTS FOUND TO BE DISBOND. R & R PANEL IAW DWG 175N2001.SDR DALA2017072305663Skin · damagedDURING C CHECK, MAINTENANCE REPORTED DAMAGE TO THE UPPER EDGE OF THE LOWER FIXED LEADING EDGE PANEL COMMON TO THE ZFS=52 SPLICE STRAP. ON THE PANEL, ALL FASTENER LOCATIONS WERE BADLY OVERSIZED AND SKIN WASHERS HAD WORN INTO THE SURFACE ON THE LT UPPER AND LOWSDR FDEA201601010001Fairing · crackedRIGHT VERTICAL STAB AFT FAIRING SKIN HAS A .100 INCH CRACK INDICATION, PROPAGATING FWD OF A REPAIR WASHER AT STATION 2159. REPAIRED IAW EA 8-5530-T0322471. REPAIR CLASSIFIED AS MINOR.SDR DALA2015122807740Skin · crackedVERTICAL STABILIZER L/E, SKIN CRACKED AT EXISTING REPAIR, LONGERON 2R, BS 1418. CRACK PASSES THROUGH HI-LOC HOLE. REPAIR OF SKIN REPAIRED ON NR 167. L2R LONGERON REPAIRED BY SPLICE METHOD WITH SHIMMING TO ACCOMODATE SKIN REPAIR IAW SRM 53-02, FIG 18.SDR DALA2015122807739Skin · crackedVERTICAL STABILIZER L/E, SKIN CRACKED AT BS 1418, LONGERON 3R. NR 167, SKIN CRACK AT BS 1418 AND LONGERON 3R REPAIRED BY TRIMOUT, DOUBLER INSTALLATION AND LONGERON SPLICE WITH SHIMS. ALL WORK ACCOMPLISHED AND RECORDED ON PRI 542150-14AD, REV 0 THRU REV 03 SDR DALA2015121707644Skin · crackedLEFT BS 1155, EMPENNAGE SKIN CRACKED AT SHEAR TIE FASTENER BETWEEN STR 2L & 3L. REPAIRED SKIN CRACK AT STR 2L AND NR LT SHEAR TIE AT LT F/S 1155 IAW ER/A 541025-14 INSTRUCTIONS 1-11.SDR DALA2015121307581Skin · wornWEAR ON RT SKIN BETWEEN BS ZFS 180 AND ZFS 165 AT VERTICAL STABILIZER. RT SKIN WAS REPLACED DUE EXCESSIVE WEAR IAW SRM 55-32-0, FIG 3 AND DWG 5936143, REV.SDR AALA20151208005Skin · crackedCRACK IN RT STABILIZER SKIN AT STABILIZER STATION 92.7. PERFORMED SRM 55-10-01-2R-11 REPAIR.SDR DALA2015120807453Skin · crackedTWO INCH VISIBLE CRACK LT SIDE VERTICAL STABILIZER SKIN, BELOW ACCESS PANEL 6301A. NR 001-0283:5530-2595/003 00161. RECEIVED AND C/W WITH ERA 541996-14, REV ORIGINAL PERMANENT REPAIR. ALL REPAIR INSTRUCTIONS MATCH PRIS 541996-14, REV 0 THRU REV 4.SDR DALA2015113007353Skin · crackedVERTICAL STABILIZER L/E, SKIN CRACKED AT BS 1152, BETWEEN LONGERON 1 AND 2L. REPAIRED IAW ER/A 541498-14, SECTION 1.SDR FDEA201511253777Skin · dentedREWORK OF NR N00207, VERTICAL STAB LT SIDE AUXILIARY PANEL HAS DENT, 14" FROM AUXILIARY SPAR & 56" FROM BOTTOM, DUE TO PER NOTED SRM. A VISUAL & NDT INSPECTION OF DAMAGED AREA FOR DISBONDS, DELAMINATION, IS REQUIRED PRIOR TO APPLYING REPAIR. THIS WAS NOT DOC
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