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.

SDR DALA2015112307166Skin · wornDURING C-CHECK, FOUND VERTICAL STABILIZER LOWER FIXED L/E SKIN INTERNAL FINGER DOUBLER WORN. REPAIRED IAW DWG SG-95550001, SRM 55-30-01, AND ER/A 541681-14.Nov 22, 2015 · N979AT · Boeing 717200SDR DALA2015112307165Skin · damagedDURING CHECK VISIT, FOUND VERTICAL STABILIZER L/E LOWER 2 ROWS OF FASTENERS AT ZFS 66.6 PULLED THRU SKIN, APPROXIMATELY 12" IN LENGTH ON LT SIDE. REPAIRED IAW ER/A 541681-14.Nov 22, 2015 · N979AT · Boeing 717200SDR FDEA201511173669Skin Panel · delaminatedVERTICAL STAB RT SIDE, AUXILIARY PANEL HAS DELAMINATION, 26" FROM AUXILIARY SPAR & 120" FROM BOTTOM. REMOVED DAMAGED PANEL ASSEMBLY & INSTALLED NEW PANEL ASSEMBLY PN 175N2001-4, IAW SRM 51-40-02 & WG 175N2001, SHEET 1 AT RT SIDE VERTICAL STAB. MAJOR REPAIR.Nov 17, 2015 · N788FD · Boeing 757222SDR FDEA201511103547Skin · corrodedAFTER PREPARING THE REPAIR AREA ON THE VERTICAL STAB AUXILIARY PANEL DENT, FOUND A DISBONDED AREA OF APPROX 13" X 13" DUE TO CORROSION ON THE INNER SKIN. THIS DISBONDED AREA IS APPROX 14" FROM AUXILIARY SPAR & 56" FROM BOTTOM. REPAIRED LT VERTICAL STAB AUXILNov 10, 2015 · N788FD · Boeing 757222SDR DALA2015110706799Skin · crackedCRACK ON VERTICAL STABILIZER SKIN LT SIDE BETWEEN BS XFS=12 TO XFS=17, JUST UP TO RAM AIR DUCT. VERTICAL STABILIZER SKIN LT SIDE BETWEEN XFS=12-17 WAS REPAIRED IAW 55-01, FIG 2, 51-10-3, PARA 14, 21, 51-30-8.Nov 6, 2015 · N986DL · Doug MD88SDR DALA2015110506744Skin · crackedCRACK ON VERTICAL STABILIZER SKIN LT SIDE BETWEEN BS XFS=12 TO XFS=17, JUST UP TO RAM AIR DUCT, SM. VERTICAL STABILIZER SKIN LT SIDE BETWEEN XFS=12-17 WAS REPAIRED IAW SRM 55-01, FIG 2, 51-10-5, PARG 14, 21, AND 51-30-8. CRACK 0.156" AND 0.281".Nov 5, 2015 · N986DL · Doug MD88SDR DALA2015102506445Skin · gougedVERTICAL STABILIZER TIP MID SECTION RT AFT SKIN HAS 2 DEEP 3" LONG GOUGES, ABOVE HORIZONTAL STABILIZER HINGE. REPAIRED IAW PRI 540664-14, REV 0 AND C/W ERA 540664-14, REV A.Oct 23, 2015 · N997DL · Doug MD88SDR DALA2015102506446Skin · wornVERTICAL STABILIZER LT SIDE SKIN IS WORN AT HORIZONTAL STABILIZER SIDE LOAD ROLLER. REPAIRED IAW PRI 540677-14, REV 0 AND WAITING FOR FINAL ER/A.Oct 22, 2015 · N997DL · Doug MD88SDR COEA2015101220923Skin · corrodedHEAVY CHECK COE & MAJOR REPAIR. VERTICAL STABILIZER LE 323AL HAS AREAS OF LEVEL 2 CORROSION UNDER THE DE-ICE BOOT. REPAIR IAW SRAS ES-5185 15 9718 DATED 11 6 15.Oct 12, 2015 · N923FX · Aerosp ATR42300SDR WX0A2015092872893Skin · damagedACCOMPLISHED INSPECTION OF DAMAGE ON VERTICAL STAB, LIGHT STRIKE, TOP AFT STAB END CAP CTR OF WELD RT SIDE 24"" FROM FWD. DAMAGE WIDTH .187"", DEPTH .125"" FOUND TO BE OUT OF LIMITS. ACCOMPLISHED EA 20-2015-260, ENSURE NO DEFECTS OR SIGNS OF DAMAGE TO ANY ADSep 25, 2015 · N875GA · Doug DC983SDR DALA2015091505663Skin · wornVERTICAL STABILIZER RT SIDE EXTERIOR HAS 7 X .3750" AREA OF DEEP WEAR APPROXIMATELY .10" ABOVE & FWD OF HORIZONTAL STABILIZER CTR AFT SPAR. NR FOR ADDITIONAL INFORMATION 001-0341:5300-2551/010 00141. REPAIRED IAW PRI 539282-14, REV "0" AND ER/A 539282-14, RESep 14, 2015 · N917DE · Doug MD88SDR FDEA201509092820Panel · damagedVERTICAL STAB LT SIDE EXTERNAL PANEL REQUIRES REMOVAL FOR REPAIR IAW NR N00231, FSS 95 - 271. R & R PANEL 175N2001-3, PANEL ON VERTICAL STAB, LT SIDE IAW SRM 51-40-02 & DWG 175N2001 SH 1 REV B. MAJOR REPAIR.Sep 9, 2015 · N787FD · Boeing 757222SDR CALA2015090394270Skin · crackedVERTICAL STAB LT & RT SKIN CRACKED AT APPROX FS 570, CARRIED FROM 10 17 2013. VERTICAL STAB CRACK REPAIRED IAW ECRA 5530-01728. SKIN PANEL REPAIR, BETWEEN FS 600 TO 612 FIRST STG APP. CONTACT EG AFTER 14 APR 15 & BEFORE 14 JUL 15.Sep 2, 2015 · N127UA · Boeing 747422SDR CALA2015082894246Skin · crackedVERTICAL STAB LT & RT SKIN CRACKED AT APPROX FS 570, CARRIED FROM 10 17 13. VERTICAL STAB CRACK REPAIRED IAW ECRA 5530-01728. SKIN PANEL REPAIR BETWEEN FIN STATION 600 TO 612.Aug 26, 2015 · N127UA · Boeing 747422SDR R61A20158210549Skin · dentedWHILE ACFT WAS IN FOR HEAVY CHECK, FOUND ON VERTICAL STABILIZER RT SIDE SKIN DAMAGED BETWEEN PANEL 323NR AND 323MR. MAINTENANCE CUTOUT DAMAGED SKIN AND REPAIRED IAW ETD2015-190-072480 DATED 8/7/15, PN 170-63700-411.Aug 21, 2015 · N163HQ · Emb ERJ190200IGWSDR AALA20150816004Skin · crackedTAIL UPPER VERTICAL LE HAS 1 EACH 1/4" FASTENER HOLE CRACKED & DAMAGED ABOVE ZFS=52.267 SPLICE, LT SIDE, 14TH FASTENER HOLE. INSTALLED DOUBLER REPAIR IAW SRM 55-03-00 FIG 30.Aug 16, 2015 · N964TW · Doug DC983SDR CALA2015072894167Skin · corrodedDURING HORIZONTAL STABILIZER INSPECTION, FOUND SKIN TO HAVE INTERGRANULAR CORROSION FORWARD OF DOOR 312AR AT APPROXIMATE STRINGER 25 RIGHT, STATION 3366 & FRAME 70 APB. ACCOMPLISHED REPAIR IAW ECRA 5330-05303 STEPS 1 A & B. AT TIME OF CF PERMANENT REPAIR IS Jul 27, 2015 · N431UA · Airbus A320232SDR CALA2015072700609Skin · crackedRIGHT HORIZONTAL STABILIZER LOWER SKIN STATION 101.90 IS CRACKED, 11 INCHES FROM TE & CRACK LENGTH ABOUT 1 INCH. REPAIRED IAW SRM 55-10-01 REPAIR 11.Jul 25, 2015 · N39418 · Boeing 737924ERSDR COEA2015071912816Skin · damagedHEAVY CHECK COE & MAJOR REPAIR. LEFT VERTICAL STABILIZER SKIN HAS FRETTING DAMAGE, LEVEL 2, ABOVE THE UPPER VORTEX GENERATOR. REPAIRED IAW SRAS CE-4167/15 9528 DATED 8 13 15.Jul 19, 2015 · N816FX · Aerosp ATR72212SDR DALA2015070404133Skin · damagedVERTICAL STABILIZER L/E SPLICE AT ZFS=52.267, HAVE WORN COUNTER SINKS. FASTENERS ARE PULLED TO DEEP INTO THE SKIN; MARKED, RII: N ENTR 575200 W APPROVAL LEVEL ACCOMPLISHED BY INSPECTED BY FINAL, C/A 01045-08, VERTICAL L/E TO BE INSTALLED ON AMDS WC 5530-01045-Jul 3, 2015 · N913DE · Doug MD88SDR IPXA2015063090706Access Panel · damagedINSPECTION TYPE: 5YR, VERTICAL STAB INTERNAL ACCESS PANEL 311BZ HAS A MISDRILLED HOLE AT AFT LT NUTPLATE ACCOMPLISHED EO A300-5310-57892-A.Jun 30, 2015 · N128UP · Airbus A300F4622RSDR UHLA201506190516Skin · crackedRT VERTICAL STAB SKIN IS CRACKED AT RIB 12 BELOW AND AFT OF THE HOIST FITTING. REPAIRED THE VERTICAL STABILIZER SKIN IAW ETD2015-170-051804.Jun 19, 2015 · N653RW · Emb ERJ170100SESDR AALA20150617014Panel · delaminatedVERTICAL STABILIZER PANEL 332 FL FOUND DELAMINATED. REPAIRED PANEL IAW SRM 51-70-05 REPAIR 2 & REF HX PROCESS CARD CONTROL SFQ NO.LPH510382-01.Jun 18, 2015 · N771AN · Boeing 777223SDR CA150619015Skin · cracked(CAN) VISUAL INSPECTION WITH A FLASHLIGHT ABOVE THE TAIL CONE & AT THE LOWEST RIVET ROW OF THE FIN, THE AFT RT TOE CAP RIVET SHOP HEAD WAS MISSING. FIN ASSEMBLY REMOVED FROM ACFT & FURTHER INSPECTION REVEALED THE TWO OTHER RT TOE CAP RIVETS FWD OF THE SUSPECTJun 17, 2015 · Snias AS350B3SDR IPXA2015061690263Skin · corrodedCORROISON ON SKIN UNDER PANEL 364RR BOTTOM NEAR INTERCOSTAL. REMOVED DAMAGE IAW EO 5530-57772-A , FABRICATED DOUBLER AND FILLER IAW WITH EO 5530-57772-A AND INSTALL REPAIR IAW EO 5530-57772-A AND INSTALLED .Jun 15, 2015 · N259UP · Doug MD11FSDR 7C7A201505230035Skin Panel · dentedDENT DAMAGE TO LT VERTICAL STABILIZER LOWER SKIN PANEL FRONT SPAR AND MAIN SPAR AND RIB NR 7. REPAIRED WITH PERMANENT DENT ALLOWANCE IAW ECO 008-55-15.02May 23, 2015 · N891EA · Dhav DHC8106SDR 7C7A201505230029Skin Panel · dentedDENT DAMAGE TO RT SIDE OF VERTICAL STABILIZER SKIN PANEL 85530011. DENT ALLOWANCE REPAIRED IAW ECO 008.55-15.01May 23, 2015 · N891EA · Dhav DHC8106SDR DALA2015052403510Skin · crackedVERTICAL FIN SKIN HAS A FOUR INCH LONG CRACK AT RIVET LINE NEAR BS 1475. REPAIRED IAW ERA 516509-14MA, REV A.May 22, 2015 · N948DN · Doug MD9030SDR DALA2015052403509Skin · crackedVERTICAL FIN SKIN HAS ONE INCH LONG CRACK AT RIVET LINE NEAR BS 1475. REPAIRED IAW ERA 516509-14MA, REV A. LP 1960283.May 22, 2015 · N948DN · Doug MD9030SDR DALA2015051103197Skin · crackedCRACKED DOUBLER ON DORSAL FIN LOWER SECTION BS 1474, AT VERTICAL STABILIZER. REMOVED DOUBLER. FABRICATED AND INSTALLED NEW DOUBLER IAW SRM 51-30-02 AND DWG 5910242, REV BV. LP 1941709.May 10, 2015 · N935DN · Doug MD9030SDR DALA2015042602921Skin · damagedLIGHTNING STRIKE ON RT VERTICAL STABILIZER B FS 1756, FS 101. REPAIRED IAW PRI 535398-14, REV 0. C/W ERA 535398-14, REV ORIGINAL SECTION 1.Apr 24, 2015 · N900PC · Boeing 75726DSDR DALA2015042602920Skin · damagedLIGHTNING STRIKE AT FASTENER ON RT VERTICAL STABILIZER REAR SPAR B, FS 1786 FS108. REPAIRED IAW PRI 535398-14, REV 0. C/W ERA 535398-14, REV ORIGINAL SECTION 1. Apr 24, 2015 · N900PC · Boeing 75726DSDR DXTR2015041002Skin · looseVERTICAL L/E HAS MULTIPLE LOOSE, WORKING FASTENERS. COMPLIED WITH STRUCTURES REPORT NO: S-560XL-5360/04 PRD1 REPAIR DEFINITION.Apr 3, 2015 · N615QS · Cessna 560XLSDR SWAA2015051139557Scoop · crackedVERTICAL STABILIZER, INLET SCOOP AT LT SIDE CRACKED. REPAIRED STABILIZER IAW SRM.Mar 16, 2015 · N942AT · Boeing 717200SDR UHLA2015030700191Skin · crackedRIGHT VERTICAL STAB SKIN, CRACK AFT OF UPPER HOIST POINT. SKIN HAS 2 CUTOUT AREAS TO REMOVE CRACK. 1ST CUTOUT AT REAR SPAR AND RIB 12 MEASURES 60MM, 120MM AND CUTOUT AFT SKIN EDGE 25MM-60MM. INSTALLED FILLERS AND DOUBLER IAW ETD2015-170-022174, REV C.Mar 7, 2015 · N647RW · Emb ERJ170100SESDR DALA2015030802000Skin · damagedFOUND 1 FASTENER MISSING ON VERTICAL STABILIZER L/E SKIN. REPLACED MISSING FASTENER IAW WC 5530-01044. LP 1851276.Mar 7, 2015 · N943DN · Doug MD9030SDR FDEA201503060705Skin · damagedVERTICAL STAB SKIN LT SIDE ONE EACH BUTTON HEAD FASTENER INSTALLED. BETWEEN BS 1790 & FSS 245.6. REPAIRED VERTICAL STAB SKIN LH FWD SIDE IAW SRM 51-70-10, PARAGRAPH 19, BS 1790, FSS 245.6. MAJOR REPAIR.Mar 6, 2015 · N771FD · Boeing 757222SDR DALA2015012800693Doubler · crackedCRACK ON INTERNAL DOUBLER BS 1429-1431, APPROXIMATELY 10 INCHES FROM LT DORSAL ANGLE AT SETTLEMENT AREA OF ACCESS PLATE 6301A AT VERTICAL STABILIZER FIXED L/E. INTERNAL DOUBLER WAS REPLACED IAW DWG 59140242, REV BV AND SRM 51-70-4 51-30-2.Jan 27, 2015 · N979DL · Doug MD88SDR DALA2015012800689Skin · crackedCRACK ON VERTICAL STABILIZER L/E RT SIDE BS 1401 BESIDE TO DORSAL ANGLE. CRACK WAS STOP DRILLED, DOUBLER WAS FABRICATED, TREATED AND PAINTED, AND INSTALLED IAW SRM 55-01.Jan 27, 2015 · N979DL · Doug MD88SDR SWAA2015022436862Access Panel · erodedVERTICAL STABILIZER LE ACCESS PANEL 322B ERODED. REPAIRED PANEL IAW EO & EA.Jan 24, 2015 · N433LV · Boeing 7377H4SDR IPXA2015012385426Skin · damaged.2500" HOLE IN OUTER SKIN OF VERTICAL STABILIZER PANEL. REPAIRED IAW EO 5530-56500-A.Jan 20, 2015 · N583UP · Boeing 7474R7FSDR IPXA2015012385425Skin · delaminatedDISBOND ON VERTICAL STABILIZER PANEL LT SIDE. REPAIRED IAW EO B747-5530-56500-A.Jan 20, 2015 · N583UP · Boeing 7474R7FSDR FDEA201501150175Skin · puncturedVERTICAL STAB RT SIDE PANEL INTERNAL SKIN FSS 125 & 5 INCHES FWD OF FRONT SPAR HONEYCOMB HAS SMALL PUNCTURE. REPAIRED VERTICAL STAB RT SIDE PANEL INTERNAL SKIN IAW SRM 51-70-10 REPAIR 2. TREATED & PRIMED AREA IAW SRM 51-20-01.Jan 15, 2015 · N770FD · Boeing 757222SDR ASOA2015020412145Skin · crackedVERTICAL STABILIZER TOP LT EDGE OF L/E IS CRACKED AT T/E. REPAIRED VERTICAL L/E IAW STS EA 12-2015-017, SECTION I, REPAIR 1, STEPS A THRU L. PAINTED VERTICAL L/E IAW STS EA 12-2015-017, STEP M, EA 12-2015-017 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCJan 12, 2015 · N908EV · Cndair CL6002B19SDR SWAA2015011635822Strap · crackedVERTICAL STABILIZER ACCESS PANEL 9501 STRAP CRACKED. R & R STRAP IAW SRM & DWG.Jan 11, 2015 · N527SW · Boeing 7375H4SDR C77A20150106002Skin · gougedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF THE RT VERTICAL STAB SKIN GOUGE DAMAGE IN TWO AREAS. THE DAMAGE IS LOCATED BELOW RIB 4 & BETWEEN STRINGER -2R TO -3R. THE GOUGE DAMAGE MEASURES APPROX THE FOLLOWING DIMENSJan 6, 2015 · N747CZ · Emb ERJ170100LRSDR DALA2014122806818Access Panel · crackedCRACKS ON ACCESS PANEL 6404A OF VERTICAL STABILIZER. (SM) (CARD 56 - ZONE 00). CRACK WAS STOPPED IAW SRM 55-01, FIG 2 AND 51-01, PAR 21. FABRICATED AND INSTALLED NEW DOUBLERS IAW SRM 55-01, FIG 2, 51-30-2, INSP WAS ACCOMPLISHED AFTER STOP DRILL AND NO CRACKS Dec 27, 2014 · N979DL · Doug MD88SDR REXA2014122500923Skin · dentedDENTS FOUND ON RT VERTICAL STABILIZER SKIN. FOUND TO BE WITHIN LIMITS IAW SRM 55-00-31. REPAIRED IAW EA 255-03171.Dec 25, 2014 · N8913A · Cndair CL6002B19SDR DALA2014120906510Fastener · looseLOOSE FASTENERS AT STA ZFS = 52.267 VERTICAL STABILIZER L/E. FOUND FIVE TOTAL HOLES OUT OF LIMITS AND REQUIRED BUSHING REPAIR IAW SG09550004-7003. INSTALLED DOUBLER IAW DW SR-09550004-7003, REV D.Dec 9, 2014 · N904DA · Doug MD9030SDR FDEA201412013992Access Panel · delaminatedVERTICAL STAB LT SIDE ACCESS PANEL 374EL HAS DELAMINATION. REPAIR DELAMINATION ON PANEL 374EL IAW SRM 51-71-00 VOL II.Dec 1, 2014 · N554FE · Doug MD1010F
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