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 FDEA2020082781818Spar · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013, PER DRAWING NUMBER SN10550000 REVISION C, ON LT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, CRACK INDICATION FOUND ON THIRD FASTENERS FROMAug 8, 2020 · N625FE · Doug MD11FSDR FDEA2020082781817Spar · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013, PER DRAWING NUMBER SN10550000 REVISION C, ON LT SIDE OF THE LOWER VERTICAL STABILIZER AFT FLANGE OF UPPER REAR SPAR CAP CRACK INDICATION FOUND BETWEEN FOURTH AND THIRD FASTENEAug 8, 2020 · N625FE · Doug MD11FSDR JGVR20200819001Spar · corrodedBLENDED AREA OF CORROSION ON RT SIDE OF VERTICAL STABILIZER AFT SPAR AT VFS 118.79. PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED AND TREATED BLENDED AREA THEN PRIMED, APPLIED TOP COAT, AND CORROSION INHIBITING COMPOUND PER TEXTRON FIELD REPAIR.Aug 7, 2020 · N397QS · Cessna 680ASDR JGVR20200807004Spar Cap · corrodedBLENDED 4 AREAS OF CORROSION ON THE VERTICAL STABILIZER AFT SPAR CAP ANGLES, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. TREATED BLENDED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLERS PER ENGINEERING ORDER.Aug 7, 2020 · Cessna 680CESDR R61A2020080800585Rib · crackedDURING HEAVY CHECK MAINTENANCE, FOUND THE VERTICAL STABILIZER TRAILING EDGE RIB 9/10 CRACKED. REPLACED THE RIB IAW SRM 51-41-01, AND SRM 51-41-02.Jul 22, 2020 · N641RW · Emb ERJ170100SESDR VNAA202007139995Drag Angle · crackedRH VERT STAB AFT DRAG ANGLE, POSSIBLE CRACK. INSTALLED NEW VERT DRAG ANGLE IAW CRJ900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01Jul 13, 2020 · N577NN · Bombdr CL6002D15SDR FDEA202007061446Spar · crackedEMPENNAGE, HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION FOUND ADDITIONAL FASTENER HOLES NR 4 & 6 CRACKED AT NR 4 BANJO FITTING RIGHT HAND AFT FLANGE AREA STATION 2164 & ONE FASTENER HOLE OVER-COUNTERSUNKED, UNABLE TO INSTALL HLT335-8-14 AS PER SRM 55-30-02Jul 6, 2020 · N605FE · Doug MD11FSDR FDEA202006261363Spar · crackedULTRASONIC INSPECTION FOUND CRACK INDICATION ON LOWER VERTICAL STABILIZER NR 4 BANJO FITTING RIGHT HAND SIDE FORWARD FLANGE. REPAIR AREA AND UNABLE TO DETERMINE THE CRACK LENGTH DUE TO REPAIR BLOCKAGE AT APPROXIMATE STATION Y = 2164. CRACK ON LOWER VERTICAL Jun 26, 2020 · N605FE · Doug MD11FSDR SWAA2020071595445Rib · crackedDORSAL FIN FWD RIB AT BS867.0 IS CRACKED. REMOVED & REPLACED DORSAL FIN FWD RIB AT BS 867 IAW SRM 51-40-02 STEP 4 & 6 & DWG 174A0103 ID 0003 REV A.Jun 23, 2020 · N486WN · Boeing 7377H4SDR FDEA2020071091163Frame · crackedEMPENNAGE - ACCESS PANEL 364QR FOUND CUT OUT CRACKED UPON PANEL REMOVAL. AT STATION 2164 RIGHT HAND ZID = 75.5 , XID = 9.0 . EMPENNAGE ACCESS PANEL 364QR AT STATION 2164 RIGHT HAND ZID = 75.5 , XID = 9.0 CRACKED SKIN PANEL REMOVED PER SRM 51-31-01-OG . NEWJun 9, 2020 · N617FE · Doug MD11FSDR FDEA2020071091162Frame · crackedEMPENNAGE - ACCESS PANEL 363ML FOUND CUT OUT CRACKED UPON PANEL REMOVAL. AT STATION 2164 LEFT HAND , ZID = 72.0 , XID = 9.0 . ACCESS PANEL 363ML AT STATION 2164 LEFT HAND ZID = 72.0 XID = 9.0 CRACK FRAME REMOVED AND REPLACED AS PER EA # 1-5500-T0354594P1.Jun 9, 2020 · N617FE · Doug MD11FSDR HYIA20200519001Spar Cap · corrodedDURING MAINTENANCE TWO SPOTS OF CORROSION WERE VISUALLY IDENTIFIED ON THE AFT LEFT HAND VERTICAL SPAR CAP (P/N: 5131007-5) OF THE  VERTICAL STABILIZER. THESE SPOTS EXIST AT APPROXIMATE W.L 156.52 AND W.L. 167.52, AND HAVE A MAXIMUM DEPTH OF .033 INCHES. THIS DMay 19, 2020 · N409BK · Cessna 402CSDR DALA2022010400051None · noneER/A 586819-14AD REV ORIGINAL HAS BEEN ISSUED FOR CRACKING DISCOVERED DURING ACCOMPLISHEMENT OF AMDS WC 5530-01048-02. THE SUBJECT SECTION I REPAIR IS TIME LIMITED. FOLLOW ON ACTION REQUIRED. ASSOCIATED ER/A 95-586819 ADDED FOR AC 9576. ERA 586819-14AD REV A IMay 11, 2020 · N608AT · Boeing 717200SDR DALA2020051202382Spar Cap · crackedDURING OPN 5530-01048-02 STEP 14, OPEN HOLE HFEC FOUND CRACK INDICATION IN BOLT HOLE ON RH VERT STAB FRONT SPAR CAP. 1ST HOLE UP FROM SPLICE. DISCONNECTED UPPER AND LOWER ANTENNA ON VERT STAB. ALL FURTHER MAINTENANCE COMPLIED WITH ON PRI / ER/A 586819-14AD ANDMay 11, 2020 · N608AT · Boeing 717200SDR 3WTR2020050400000Spar Web · crackedDURING GENERAL VISUAL INSPECTION (GVI) OF VERTICAL STABILIZER, THE VERTICAL STABILIZER REAR SPAR WEB WAS FOUND TO BE CRACKED IN TWO PLACES NEAR THE HORIZONTAL STABILIZER ATTACHMENT POINT. ONE CRACK WAS APPROXIMATELY 12MM LONG AND THE SECOND CRACK WAS APPROXIMAMay 4, 2020 · N998GC · Emb EMB505SDR FDEA2020051830879Spar · crackedULTRASONIC INSPECTION FOUND CRACK INDICATION ON LOWER VERTICAL STABILIZER # 4 BANJO FITTING LEFT HAND SIDE FORWARD FLANGE REPAIR AREA AND UNABLE TO DETERMINE THE CRACK LENGTH DUE TO REPAIR BLOCKAGE AT APPROXIMATE STATION Y = 2164 EXISTING CRACK FOUND DURMay 3, 2020 · N615FE · Doug MD11FSDR SWAA2020050145363Rib · crackedDORSAL FIN #8 RIB ASSY (P/N 174A1008-2) CRACKED AT LH AND R/H SIDES JUST OUTBD OF MOUNT BRACKETS / REMOVED AND REPLACED DORSAL FIN #8 RIB ASSY (P/N 174A1008-2) PER SRM 51-10-02;INSTALLED FASTENERS PER SRM 51-40-02.Apr 23, 2020 · N249WN · Boeing 7377H4SDR DALA2020040102111Spar · crackedTHE AUXILIARY SPAR WEB AROUND THE SCREW HOLE WHERE IT ABOVE THE LH SIDE AUX SPAR CHORD AT APPROXIMATELY FSS 193 FOUND CRACK. REPAIRED PER ERA 585991-14 (LP 15411190)Mar 28, 2020 · N825MH · Boeing 767432ERSDR SWIA2020040149887Bulkhead · damagedVERTICAL STAB. PANEL 321AL AFT BULKHEAD HAS COMPOSITE DAMAGE. (C CHECK) RO 3/30/2020 REMOVED AND REPLACED VERTICAL STAB PANEL 321AL AFT BULKHEAD/FRAME REF. EMB SRM.Mar 18, 2020 · N135SY · Emb ERJ170200LRSDR 2020F00104Rib · crackedBULLET FAIRING RIB CRACK. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ25104M1 DATED MARCH 12, 2020; 750-0158 (N958QS) BULLET FAIRING RIB REPAIR.Mar 13, 2020 · N958QS · Cessna 750SDR DALA2020031201819Spar · crackedMTC TASK-A CRACK FOUND ON VERTICAL STABILIZER AUXILIARY SPAR WEB AT LH FSS 65.75 LOG-PAGE UPDATED RII: Y W THE CRACKED AUXILIARY SPAR WEB REPAIRED AS PER PRI585644-14. REV.O THE PRI 585644-14 REV.O COMPARED AND COMPLIED WITH ERA585644-14 REV.ORIGINAL ASSOCIATEMar 12, 2020 · N839MH · Boeing 767432ERSDR JGVR20200224001Spar · corrodedMECHANICALLY BLENDED CORRODED AREA FROM THE VERTICAL STABILIZER LH SPAR CLIP, APPROXIMATELY FOUR INCHES BELOW THE MIDDLE RUDDER HINGE, PERFORMED EDDY CURRENT CRACK AND ULTRASONIC THICKNESS INSPECTIONS AND REPORTED TO TEXTRON FOR REPAIR DISPOSITION. CLEANED, TFeb 24, 2020 · N376QS · Cessna 680CESDR DALA2020022101313Spar Cap · crackedVERTICAL STABILIZER LEADING EDGE SPAR CAP CARCK. REPETITIVE INSPECTION NEEDS TO BE PERFORMED EVERY 3000 FLIGHT CYCLES, THIS IS INCORPORATED INTO ER/A 585429-14. (LP1497972)Feb 20, 2020 · N907DE · Doug MD88SDR JGVR202002192001Spar · corrodedVERTICAL STAB HAS 1 AREA OF VERIFIED CORROSION ON LH SPAR CLIP BELOW UPPER RUDDER HINGE. FOUND DURING 6 MONTH INSPECTION. REMOVED LEVEL 1 CORROSION FROM VERTICAL STAB LH SPAR CLIP BELOW UPPER RUDDER HINGE IAW CESSNA 680 SRM 51-70-02. FOUND BLENDED AREA TO BE BFeb 20, 2020 · N313QS · Cessna 680ASDR SWAA2020021241355Rib · crackedVERTICAL STABILIZER LEADING EDGE STA. 278.8 RIB CRACKED. / R&R RIB IAW SRM AND DWG.Feb 5, 2020 · N799SW · Boeing 7377Q8SDR SWAA2020021241354Rib · crackedVERTICAL STABILIZER LEADING EDGE STA. 288.2 RIB CRACKED. / R&R RIB IAW SRM AND DWG.Feb 5, 2020 · N799SW · Boeing 7377Q8SDR JGVR20200124001Spar Cap · corrodedFOUND ONE AREA OF VERIFIED CORROSION ON VERTICAL SPAR RH AFT SPAR CLIP. FOUND DURING 55-30-00-2200. SUBMIT HAND SANDED AREA TO ENGINEERING FOR FURTHER GUIDANCE. BLEND ONE AREA OF VERIFIED CORROSION ON VERTICAL SPAR RH AFT SPAR CLIP APPROXIMATELY 1.5 INCHES BELJan 24, 2020 · N362QS · Cessna 680CESDR FDEA2020012310193Spar · crackedVERTICAL STABILIZER FORWARD SPAR RIGHT CHORD/TORN FSS 330 REPAIRED PER EA# F-5530-T0351942A TITLE STABILIZERS-VERTICAL-FRONTSPAR-WEB AND CHORD SPLICE REPAIR- COVER E.A.Jan 21, 2020 · N922FD · Boeing 75723ASDR FDEA2020012310192Spar Web · tornVERTICAL STABILIZER FORWARD SPAR WEB TORN/DAMAGED FSS 320 TO FSS 350 REPAIRED ON EA# F-5530-T0351942A TITLE STABILIZER-VERTICAL-FRONT SPAR-WEB AND CHORD SPLICE REPAIR-COVER E.A. MAJOR REPAIRJan 21, 2020 · N922FD · Boeing 75723ASDR FDEA2020012310191Spar · bentVERTICAL STABILIZER FORWARD SPAR LEFT CHORD BENT FSS 330 REPAIRED PER EA# F-5530-T0351942A THE STABILIZER-VERTICAL-FRONT SPAR-WEB AND CHORD SPLICE REPAIR-COVER E.A.Jan 21, 2020 · N922FD · Boeing 75723ASDR JGVR20200150001Spar · corroded6 SPOTS OF CORROSION ON THE VERTICAL STAB AFT SPAR.Jan 15, 2020 · N397QS · Cessna 680CESDR DALA2019120907153Rib · cracked(AIRCRAFT 7006, L/P 1392582) OPEN HOLE HFEC INSPECTION SHOWS 7 EA CRACK INDICATIONS AT RIB ISS196 (2ND RIB O/B). 1 EA HOLE HAS CRACK APPROX. 1.25". OTHER 6 CRACKS ARE APPROX. 0.5".*MARKED*. CORRECTIVE ACTION: REPAIRED PER B777 SRM 57-43-01.Dec 8, 2019 · N865DA · Boeing 777232SDR FDEA2019120183140Spar Cap · crackedHIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION CARRIED OUT ON LOWER VERTICAL STABILIZER REAR SPAR CAP, STATION Y=2164, CRACK FOUND ON LEFT HAND FORWARD FLANGE. LOWER VERTICAL STABILIZER REAR SPAR CAP STATION Y=2164 LEFT HAND FORWARD FLANGE CARRIED OUT REPAIR ANov 28, 2019 · N610FE · Doug MD11FSDR 2TJR201910210001Spar Cap · corrodedCORROSION WAS FOUND AT THREE LOCATIONS ON THE 6931012-1 LH AFT SPAR CAP OF THE VERTICAL STABILIZER. ALL CORROSION WAS REMOVED BY BLENDING IAW CESSNA FIELD REPAIR - CORROSION, VERTICAL STABILIZER, LH REAR SPAR CAP, VFS 115 TO 163 DWG NO. FR-680-0245-7226 DATEOct 21, 2019 · N382QS · Cessna 680SOVSDR FDEA2019101762656Spar · crackedHFEC INSPECTION CARRIED OUT AT PSE SPAR, LOWER VERTICAL STABILIZER AND FOUND CRACK INDICATION AT LEFT HAND FORWARD FLANGE OF THE REAR UPPER SPAR LEFT HAND REAR SPAR CAP FORWARD FLANGE LOCATED AT UPPER SECTION OF THE #4 BANJO FITTING OF LOWER VERTICAL STABIOct 16, 2019 · N587FE · Doug MD11FSDR FDEA2019101762655Spar · crackedHFEC INSPECTION CARRIED OUT AT PSE, LOWER VERTICAL STABILIZER SPAR. FOUND A CRACK INDICATION AT THE RIGHT FORWARD FLANGE OF THE REAR UPPER SPAR. THE RIGHT REAR SPAR CAP FORWARD FLANGE LOCATED AT UPPER SECTION OF THE NR 4 BANJO FITTING OF LOWER VERTICAL STABIOct 16, 2019 · N587FE · Doug MD11FSDR SWAA2022041941919Rib · delaminatedVERTICAL FIN L/E RIB P/N 176A1310-13 HAS DELAMINATION ON BULLNOSE. / VERTICAL FIN L/E RIB P/N 176A1310-13 WAS REPLACED WITH SERVICEABLE VERTICAL FIN L/E ASSEMBLY ON CARD #T984182.Oct 9, 2019 · N421LV · Boeing 7377H4SDR FDEA201909172267Spar · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT PRINCIPAL STRUCTURAL ELEMENT SPAR, LOWER VERTICAL STABILIZER AND FOUND CRACK INDICATION AT RIGHT HAND STATION 2164 FORWARD FLANGE OF THE REAR UPPER SPAR. LOWER VERTICAL STABILIZER AT RIGHT HAND STATION 2164Sep 17, 2019 · N586FE · Doug MD11FSDR FDEA201909172266Spar · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT PRINCIPAL STRUCTURAL ELEMENT SPAR, LOWER VERTICAL STABILIZER AND FOUND CRACK INDICATION AT LEFT HAND STATION 2164 FORWARD FLANGE OF THE REAR UPPER SPAR. LOWER VERTICAL STABILIZER AT LEFT HAND STATION 2164 FSep 17, 2019 · N586FE · Doug MD11FSDR JGVR20190912001Fitting · corrodedREPAIRED CORROSION ON VERTICAL STABILIZER AFT SPAR, LT SPAR CLIP APPROXIMATELY 11 INCHES ABOVE LOWER RUDDER HINGE BY MECHANICAL BLENDING, PERFORMING NDT, TREATING, PRIMING, AND TOP COATING PER REPAIR MEMO.Sep 13, 2019 · N306QS · Cessna 680CESDR FDEA201908282033Spar · crackedON REMOVAL FOR TH BANJO ACCESS, FOUND LEFT VERTICAL STABILIZER AT REAR CENTER SPAR PLANE AJC 7308 AT INTERNAL WEB BOX CRACKED. REPAIRED IAW SRM 55-30-02-2R, REPAIR 7 FIGURE 203, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 28, 2019 · N590FE · Doug MD11FSDR FDEA201907301741Spar · crackedDURING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION ON THE RIGHT HAND FORWARD FLANGE OF LOWER VERTICAL STABILIZER REAR SPAR CAP AT STATION Y = 2164 , FOUND 01EA CRACK WITH LENGTH APPROXIMATELY 1.5" BETWEEN THE FIRST AND THIRD FASTENER FROM BELOW. VERTIJul 30, 2019 · N529FE · Doug MD11FSDR SWAA2019080735697Support · crackedVERTICAL STABILIZER RIB LATERAL SUPPORT CRACKED AT BS. 1018, BETWEEN LBL 10 TO RBL 10. / R&R SUPPORT IAW DWG & SRM.Jul 18, 2019 · N568WN · Boeing 73776NSDR 2019FA0000215Spar · severedDURING ANNUAL INSPECTION DISCOVERED LEFT V-TAIL STABILIZER MAIN SPAR SEVERED IN TOTALITY AT THE FIRST-ORDER SPAR TO AIRFRAME FASTENERS. CRACK EXTENDED THROUGH BOTH MAIN SPAR -AND- FACTORY MAIN SPAR REINFORCEMENT PLATE VIA THE MIDDLE OF THE ATTACHMENT HOLES. AIJul 8, 2019 · N4223B · Beech 35BEECHSDR SWAA2019072535281Attach Fitting · damagedVERTICAL STABILIZER R/H REAR SPAR ATTACH FITTING, ON TOP OF FUSELAGE, FORWARD OUTBOARD FAILSAFE DRAG BRACE HAD A HOLE ON INBOARD OF LUG. REPAIRED FITTING PER SRM, ER, AND EA.Jun 8, 2019 · N737JW · Boeing 7377H4SDR FDEA201905161077Spar Cap · crackedDURING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION ON THE LEFT HAND FORWARD FLANGE OF LOWER VERTICAL STABILIZER REAR SPAR CAP, FOUND 01EACH CRACK WITH LENGTH APPROXIMATELY 1.2" BETWEEN THE LOWEST TWO FASTENERS AT STATION 2164 LEFT HAND REAR SPAR CAP FORWARDMay 16, 2019 · N522FE · Doug MD11FSDR ASAA2019060329568Fitting · corrodedVERT STAB L/H FRONT SPAR FITTING FWD FACE HAS CORR AND WEAR ON SURFACE WHERE WASHER RESTS. GROUNDED - YES. REPAIRED VERT. STAB LH FRONT SPAR FITTING FWD FACE IAW ASA EA 700 53EA 21672 W 2.5" O .502 R .485 L 2.5" D .017.May 13, 2019 · N622AS · Boeing 737790SDR ASAA201906039567Spar · corrodedVERT STAB R/H FWD SPAR FITTING HAS CORR AND WEAR ON FWD SIDE WHERE WASHER RESTS. GROUNDED - YES. REPAIRED VERT. STAB RH FWD SPAR FITTING FWD FACE IAW ASA EA 700 53EA 21672 W 3.5 O .500 R .481 L 3.5 D .019.May 13, 2019 · N622AS · Boeing 737790SDR DXTA201904230186Spar Cap · corrodedVERTICAL STAB. AFT SPAR CAP DAMAGE (CORROSION). REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ19154M1 DATED APRIL 12, 2019.Apr 23, 2019 · N305QS · Cessna 680SOVSDR DALA2019032701929Spar · crackedVERTICAL STABILIZER LT SIDE LEADING EDGE SPAR CHORD CRACK REPAIR / AMOC 17-088ER/A 557950-14AD REV A SUPPLEMENTAL INSPECTION RESTRICTION: ACCOMPLISH SECTION II: SUPPLEMENTAL INSPECTIONS, AT ACCRUEMENT OF 63,615 TOTAL AIRCRAFT FLIGHT CYCLES, AND EVERY 4,500 FLIMar 27, 2019 · N912DL · Doug MD88
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