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 FDEA2021083042114Rib · crackedVERTICAL STAB L/E - PNL #371CLE HAS CRACKED RIB - 7TH FROM BOTTOM L/H SIDE TRIMMED OUT DAMAGE AND INSTALLED REPAIR ANGLE AND FILLER REFERENCE SRM 55-00-01 FIG. 7 SHEET 1 VOL. 1. "MAJOR REPAIR"Aug 24, 2021 · N321FE · Doug MD1030FSDR SWIA202161847None · cracked* RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FORWARD DRAG ANGLE CRACKED (MARKED) (C-CHECK RO 10/22/2021) REPAIRED RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FORWARD DRAG ANGLE REF CRJ900 SRM 55-31-00-201-001-A01. COMPLIED WITH 51-900-1002-SKY.Aug 13, 2021 · N554CA · Cndair CL6002D24SDR SWAA2021091003819Rib · crackedCRACK DORSAL FIN RIB FWD POSITION AT VERTICAL STABILIZER ; 2021-368570 / [01] REMOVED RIB LOC. DORSAL FIN FWD POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 DUE TO NOT FOUND ALLOWED DAMAGE ON SRM ; RIB MUST BE REPLACED CRACK LENGTH IS : 0.625 TOOL UAug 5, 2021 · N754SW · Boeing 7377H4SDR DALA2021072904291Rib · damagedSHIP 5645 RIB 1 OF VERT STAB DAMAGED. CORRECTIVE ACTION: REMOVED DAMAGED RIB AND MADE NEW RIB PER B757 SRM AND BOEING DRAWING 175N3001. INSTALLED RIB 1 ON VERT STABILIZER PER DRAWING 175N3001 AND B757 SRM. (1889815)Jul 27, 2021 · N545US · Boeing 757251SDR DALA2021070803798Spar · delaminatedDURING INSPECTION MAINTENANCE FOUND LEFT VERT STAB FROM FSS95 TO FSS145 FROM FRONT SPAR TO AUX SPAR FOUND DELAMINATION. AREA REPAIRED PER SRM 55-30-01 AND 51-70-10. (LP 1865369)Jul 6, 2021 · N191DN · Boeing 767332SDR DALA2021070803797Spar · delaminatedDURING INSPECTION MAINTENANCE FOUND LEFT INTERNAL VERT STAB FROM FSS92.25 TO FSS145 FROM FRONT SPAR TO AUX SPAR FOUND DELAMINATION. AREA REPAIRED PER SRM 55-30-01 AND 51-70-10. (LP 1865361)Jul 6, 2021 · N191DN · Boeing 767332SDR DALA2021070803796Spar · delaminatedDURING INSPECTION MAINTENANCE FOUND RIGHT INTERNAL VERT STAB FROM FSS92.25 TO FSS145 FROM FRONT SPAR TO AUX SPAR FOUND DELAMINATION. AREA REPAIRED PER SRM 55-30-01 AND 51-70-10. (LP 1865357)Jul 6, 2021 · N191DN · Boeing 767332SDR R61A2021063000519Rib · crackedWHILE AC WAS IN FOR HVY CK CRACK FOUND ON VERTICAL STABILIZER TRAILING EDGE RIB 9/10. REPLACED RIB 9/10 PN 170-63629-005 IAW SRM 51-41-01, 51-41-02. SEE AAR NRC# 4500917-3000-0037 FOR DETAILS OF WORK PERFORMED. AC RTS'ED.Jun 14, 2021 · N865RW · Emb ERJ170100SESDR FDEA202105251391Spar Cap · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NO. SN10550000 REVISION C ON LEFT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FROM May 25, 2021 · N598FE · Doug MD11FSDR JGVR20210520006Spar · corrodedMECHANICALLY REMOVED CORROSION LOCATED ON VERTICAL STAB, AFT SPAR, LH SPAR CLIP JUST BELOW LOWER CROSS MEMBER. FOUND CORROSION EXCEEDING C680 SRM 51-70-02 LIMITATIONS AND SUBMITTED TO TEXTRON ENGINEERING FOR REPAIRS. REPAIRED CORROSION IAW TEXTRON ENGINEERING May 20, 2021 · N323QS · Cessna 680CESDR JGVR20210520002Spar · corrodedMECHANICALLY BLENDED CORROSION FROM RUDDER COVE ON VERTICAL STAB AFT SPAR RH CLIP IAW CESSNA 680 SRM 51-70-02. REFER TO SQK 103-2 OF THIS WO FOR NDT. EVALUATED REMAINING THICKNESS AND FOUND TO BE OUT OF LIMITS. SUBMITTED INFO TO ENGINEERING. COMPLIED WITH TEXTMay 20, 2021 · N323QS · Cessna 680CESDR DALA2021052102835Spar Cap · crackedDURING CRACK CONFIRMATION STEP 10 OF 5530-01048-02 VERIFIED CRACK INDICATIONS IN LH VERTICAL STAB FRONT SPAR CAP FORWARD FLANGE AT HOLES 1,2,3,4, AND 7 BELOW ZFS=52.267. HOLES ARE NUMBERED FROM TOP TO BOTTOM REF AA 5530-01048-02 STEP 10 AND AD 2018-10-08. COMPMay 19, 2021 · N717JL · Boeing 717200SDR SWAA2021061769589Rib · crackedDORSAL FIN PANEL 321A FIRST RIB CRACKED AT LH LWR CORNER ; / CERTIFIED STEP #1 (1ST RIB REMOVAL) AND #2 (1ST RIB FABRICATION).;FABRICATED DORSAL FIN PANEL#321 FIRST RIB;MAT USED 2024-0 CLAD .040 PO#1679582 PER REF DWG#174A1108.;FINAL INSPECTED; REMOVED AND REPMay 4, 2021 · N416WN · Boeing 7377H4SDR R61A2021050600384Rib · crackedWHILE AC WAS IN FOR HVY CK FOUND VERTICAL STAB REAR SPAR AFT FACE CRACK FOUND AT RIB 9/10. REPLACED V-STAB AFT RIB 9/10 PN 170-63629-005. IAW SRM 51-41-02, 51-41-01. SEE AAR NRC # 4500889-3000-0034 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.Apr 23, 2021 · N213JQ · Emb ERJ170200LRSDR R61A2021042400360Rib · crackedWHILE AC WAS IN FOR HVY CK FOUND CRACK FOUND ON VERTICAL STABILIZER TRAILING EDGE RIB 9/10. AAR MX REPLACED RIB PN 170-63629-001 IAW SRM 51-41-01, 51-41-02. SEE AAR NRC# 4500895-3000-0016 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.Apr 14, 2021 · N855RW · Emb ERJ170100SESDR DALA2025060704356Spar Cap · crackedAIRCRAFT 9507, STABILIZERS / VERTICAL / APPROX. ZFS =62 - 44 / RH SPAR CAP, AND FORWARD SPAR WEB / CRACKS / AMOC 21-151. CORRECTIVE ACTION: COMPLIED WITH ER/A 561912-14AD SECTION III. (LP 1776790)Apr 8, 2021 · N947AT · Boeing 717200SDR SWAA2021042661226Rib · crackedVERTICAL STAB DORSAL FIN FORWARDMOST RIB CRACKED. REMOVED AND REPLACED VERTICAL STAB DORSAL FIN FORWARDMOST RIB AS PER B737700 NDT PART 6 510000 PROC 23. BC 166317; SRM 5140020G0.Apr 3, 2021 · N734SA · Boeing 7377H4SDR SWAA2021042664410Rib · crackedCRACK ON RIB AT LEVEL OF STA 867 ON ACCESS PANEL 321A DORSAL FIN. REPLACED RIB LOC AT LEVEL OF STA 867 ON ACCESS PANEL 321A DORSAL FIN IAW B737 700 SRM 511002 ITEM 9 AND DWG #174A1008 AND DWG #174A0101 REVApr 2, 2021 · N737JW · Boeing 7377H4SDR DALA2021030101128Skin · crackedCRACK DETECTED ON OPEN HOLE BY HFEC ROUTINE CARD 5530-01048-02, STEP 14, VERT STAB L/E SKIN AND FRONT SPAR CAP. CRACK INDICATION IS FIRST HOLE GOING UP R/H SIDE SKIN SPLICE L/E ZFS 52.267. MAINTENANCE REMOVED VOR #1 RH / LH AND VOR #2 RH / LH PER B717 AMM 34-3Mar 1, 2021 · N964AT · Boeing 717200SDR FDEA202102170381Spar · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NUMBER SN10550000 REVISION C ON RIGHT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FFeb 17, 2021 · N572FE · Doug MD11FSDR R61A2021031100239Rib · crackedVERTICAL STABILIZER AFT SPAR TRAILING EDGE RIB 9/10 CRACKED. REPLACED RIBS 9/10 IAW SRM 51-40-08Feb 8, 2021 · N237JQ · Emb ERJ170200LRSDR SWAA2021022346658Rib · crackedVERTICAL DORSAL FIN FWD RIB CRACKED / REMOVED AND INSTALLED NEW RIB FROM VERTICAL STRAP DORSAL FIN IAW B-737-700 SRM 51-40-02-0G-0Feb 2, 2021 · N733SA · Boeing 7377H4SDR SWAA2021021148025Rib · crackedDORSAL FIN FORWARD ATTACH ASSY WEB CRACKED AT LEFT AND RIGHT FLANGES; RIB #8 STATION 867. / REPLACED DAMAGED RIB PER SRM 51-40-02.Feb 1, 2021 · N267WN · Boeing 7377H4SDR DALA2021012900547Spar Cap · crackedONE EACH FASTENER HOLE WITH A BHEC CRACK INDICATION ON RT VERTICAL STABILIZER LEADING EDGE FRONT SPAR CAP FORWARD FLANGE. CRACK IS IN FIRST FASTENER HOLE BELOW ZFS=52.267, MARKED. REFERENCE: AA 5530-01048, AD 2018-10-08 STEP 16B. COMPLIED WITH PRI 589482-14Jan 28, 2021 · N988AT · Boeing 717200SDR SWAA2021011140557Rib · crackedCRACK DORSAL FIN RIB BST 867 AT VERTICAL STABILIZER / REPLACED RIB ON DORSAL FIN BS867 AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DRAWING # 174A0103 REV AJan 7, 2021 · N406WN · Boeing 7377H4SDR 2020FA0000558Spar Cap · corrodedVERTICAL STABILIZER AFT SPAR CAP DAMAGE (CORROSION). ENGINEERING MEMO DQ28088M1 DATED DECEMBER 7, 2020.Dec 20, 2020 · N308QS · Cessna 680SOVSDR SWAA2021011137201Rib · crackedDORSAL FIN FWD RIB STA 877 SEVERAL CRACKS NOTED (MKD DOT 016). REMOVED AND REPLACED DORSAL FIN RIB AT STA 877, IAW B737-700 SRM 51-40-02-0G-0 AND DWG 174A1103.Dec 17, 2020 · N550WN · Boeing 73776QSDR JGVR20201215001Spar · damagedBLENDED CORRODED AREA ON THE VERTICAL STABILIZER AFT SPAR, LT SPAR STIFFENER. PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. REPLACED BLENDED STIFFER WITH NEW TEXTRON P/N 6931012-36.Dec 15, 2020 · N368QS · Cessna 680CESDR DALA2020121104050Spar Cap · crackedTHE THIRD BOLT HOLE BELOW STA ZFS=52.267 ON LT VERTICAL STAB FRONT SPAR CAP HAS CRACK INDICATION, REF AA 5530-01048 AND AD 2018-10-08. MAINTENANCE COMPLIED WITH CRACK VERIFICATION, PER AMDS 5530-01048-02 AND CRACK INDICATION STILL PRESENT. VERIFIED CRACK IN Dec 10, 2020 · N997AT · Boeing 717200SDR DALA2020121004034Spar Cap · cracked4TH BOLT HOLE BELOW STA ZFS=52.267 ON LT SIDE OF VERTICAL STAB FRONT SPAR CAP HAS CRACK INDICATION, REF AA5530-01048 & AD 2018 -10-08. C/W CRACK VERIFICATION, PER AMDS 5530-01048-02 STEP 10. CRACK DETERMINED IN SKIN (QC1432). STEPPED SKIN HOLE TO .277. C/WDec 10, 2020 · N997AT · Boeing 717200SDR DALA2022092906387None · noneDAMAGE TOLERANCE EVALUATION ERA 5882955-14AD ISSUED FOR VERTICAL STABILIZER SKIN CRACK REPAIR. FOLLOW ON ACTION REQUIRED. ACCOMPLISH DAMAGE TOLERANCE EVALUATION PRIOR TO 24 MONTHS FROM SECTION I ACCOMPLISHMENT. ERA REVISION REQUIRED FOR A/C OPERATION BEYOND 24Dec 9, 2020 · N997AT · Boeing 717200SDR SWAA2021072935015Rib · crackedDORSAL FIN FWD RIB CRACKED / REMOVED AND REPLACED DORSAL FIN FWD RIB AS PER B737-700 SRM 51-40-02-0G-0 AND DWG# 174A1008.Dec 8, 2020 · N274WN · Boeing 7377H4SDR JGVR20201208001Spar · corroded2 AREAS OF CONFIRMED CORROSION ON VERTICAL STAB SPAR RT AFT SPAR CLIP. MECHANICALLY AND HAND SANDED 1 AREA OF CORROSION LOCATED ON VERTICAL STAB RT AFT SPAR CLIP ON UPPER END AT 1ST RIVET AND 1 AREA OF CORROSION LOCATED 3RD RIVET BELOW UPPER RUDDER HINGE ON RDec 8, 2020 · N389QS · Cessna 680ASDR R61A2020121500883Rib · crackedWHILE IN HEAVY CHECKCRACK FOUND ON VERTICAL STAB TRAILING EDGE RIB 9/10. REPLACED ON AAR NRC 4500812-3000-0039, PER SRM 51-41-01/02. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.Nov 30, 2020 · N806MD · Emb ERJ170100LRSDR R61A2020121500878Rib · crackedWHILE IN HEAVY CHECK A CRACK WAS FOUND ON VERTICAL STAB TRAILING EDGE AT RIB 11. REPAIR WAS COMPLETED BY AAR ON NRC 4500812-3000-0040, PER SRM 55-30-07 AND DWG 170-63630-001. THIS ARICRAFT HAS BEEN RETURNED TO SERVICE.Nov 30, 2020 · N806MD · Emb ERJ170100LRSDR R61A2020121500874Rib · crackedWHILE IN HEAVY CHECK A CRACK WAS FOUND ON THE VERTICAL STAB TRAILING EDGE RIB 8. AAR REPLACED RIB 8 ON NRC 4500812-3000-0041, PER SRM 51-41-01/02 AND ETD2020-170-034323. THIS AIRCRAFT HAS BEEN RETURNED TO SERVICE.Nov 30, 2020 · N806MD · Emb ERJ170100LRSDR JGVR20201123001Spar · corrodedCORROSION FOUND ON VERTICAL STAB AFT SPAR. FOUND DURING 1 ADDITIONAL AREA OF CORROSION FOUND ON RT SIDE OF VERTICAL STAB SPAR CLIP JUST BELOW RUDDER MIDDLE HINGE. PERFORM TEXTRON ENGINEERING FIELD REPAIR ON VERTICAL STAB SPAR. MECHANICALLY BLENDED 6 TOTAL ANov 23, 2020 · N311QS · Cessna 680SOVSDR 2020F00454Spar Cap · damagedVERTICAL FIN AFT SPAR CAP (LEFT SIDE) DAMAGE. ACCOMPLISHED TEXTRON AVIATION LETTER DQ27908M1 DATED NOV 19, 2020; 680-0126 (N359QS) VERTICAL FIN AFT SPAR CAP (LEFT SIDE) DAMAGE.Nov 23, 2020 · N359QS · Cessna 680ASDR R61A2020120800854Rib · crackedV-STAB RIBS 9 & 10 TRAILING EDGE IS CRACKED. REPLACED IAW SRM 51-41-01 AND 51-41-02.Nov 19, 2020 · N212JQ · Emb ERJ170200LRSDR SWAA2021072930141Rib · crackedDORSAL FIN RIB AT STA 867 ; RIB CRACK / REMOVED AND REPLACED DAMAGED RIB DORSAL FIN STA 867' PER REF B737 SRM 51-40-02-0G-0Nov 12, 2020 · N432WN · Boeing 7377H4SDR JGVR202001112001Spar · corrodedVERTICAL STAB AFT SPAR LT UPPER ANGLE HAS 2 AREAS OF VERIFIED INTERGRANULAR CORROSION. MECHANICALLY BLENDED CORROSION ON VERTICAL STAB AFT SPAR RT UPPER ANGLE, ABOVE RUDDER LOWER HINGE, IAW CESSNA 680 SRM 51-70-02. FOUND BLENDED AREA TO BE OUT OF LIMITS, PERNov 12, 2020 · N375QS · Cessna 680ASDR JGVR20201111002Spar Cap · corrodedFOUND CORRODED AREA ON LT SPAR CAP EXTRUSION OF THE VERTICAL STABILIZER REAR SPAR. REMOVED RIVET OR ACCESS, MECHANICALLY BLENDED CORRODED AREA, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED REPAIR AREA AND INSTALLED NEW RIVENov 11, 2020 · N369QS · Cessna 680ASDR JGVR20201104002Spar Cap · corrodedBLENDED MULTIPLE CORRODED AREAS ON THE LT AND RT SPAR CAPS AND WEB OF THE VERTICAL STABILIZER AFT SPAR, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED BLENDED AND/OR CORRODED FASTENERS AS REQUIRED, TREATED AND PRIMED REPAIR AREAS, PER TEXTRON REPNov 4, 2020 · N370QS · Cessna 680CESDR R61A2020111300759Rib · crackedDURING HEAVY MAINTENANCE FOUND CRACK ON VERTICAL STABILIZER TRAILING EDGE RIB 9/10. VERTICAL STABILIZER TRAILING EDGE RIB 9/10 REPLACED, IAW EMB 175 SRM 51-41-02. A/C REMAINS IN CHECK.Oct 30, 2020 · N214JQ · Emb ERJ170200LRSDR SWAA2021072923599Rib · crackedDORSAL FIN FWD SUPPORT ATTACH RIB CRACKED / REMOVED AND REPLACED 1 EACH RIB AT DORSAL FIN FWD SUPPORT PER B737-700 SRM 51-40-02-0G-0Oct 15, 2020 · N725SW · Boeing 7377H4SDR R61A2020102200691Rib · crackedDURING HEAVY CHECK MAINTENANCE FOUND CRACK FOUND ON VERTICAL STABILIZER TRAILING EDGE RIB 9/10. VERTICAL STABILIZER TRAILING EDGE RIB 9/10 REPLACED WITH NEW, IAW EMB 170 SRM 51-41-01 AND 51-41-02. A/C REMAINS IN CHECK.Oct 6, 2020 · N208JQ · Emb ERJ170200LRSDR FDEA202009172294Rib · crackedRT HORIZ INBOARD LEADING EDGE SECTION, THE LEADING EDGE CAP OUTBOARD FORMED RIB, IS CRACKED AT BOTTOM AREA, MARKED. REPAIRED FORMER, REFERENCE SRM 22-00-01 FIG 7 SH 1 VOL 1.Sep 17, 2020 · N383FE · Doug MD1010FSDR FDEA202009142197Spar Cap · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013, PER DRAWING NUMBER SN10550000 ON LEFT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION Y=2164, CRACK INDICATION FOUND ON THIRD FASSep 14, 2020 · N588FE · Doug MD11FSDR FDEA202009142196Spar · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013, PER DRAWING NUMBER SN10550000 ON RIGHT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION Y=2164, CRACK INDICATION FOUND ON THIRD FASep 14, 2020 · N588FE · Doug MD11FSDR R61A2020090411611Rib · crackedDURING HEAVY CHECK MAINTENANCE FOUND VERTICAL STABILIZER TRAILING EDGE RIB 10 CRACKED. REPAIRED VERTICAL STAB TRAILING EDGE RIB 9/10 IAW ETD2020-170-05653.Aug 15, 2020 · N640RW · Emb ERJ170100SE
Back to JASC 5531