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 FDEA202210102527Frame · crackedEMPENNAGE: WHILE ACCOMPLISHING INSPECTION, ZONE 360 RIGHT SIDE FRAME FOUND CRACKED. FRAME REMOVED AND REPLACED PER MD-11 SRM 51-31-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. FRAME FABRICATED IAW DRAWING AJC7593 REVISION Z.SDR FDEA202210102526Frame · crackedEMPENNAGE: WHILE ACCOMPLISHING INSPECTION, ZONE 360 LEFT HAND SIDE FRAME FOUND CRACKED. FRAME REMOVED AND REPLACED IAW SRM 51-31-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. FRAME FABRICATED IAW DRAWING AJC7593 REVISION Z.SDR SWAA2022101322981Rib · crackedCRACK RIB LOCATED ON DORSAL FIN PANEL 321A AT LEVEL STA 867.95 AT VERTICAL STABILIZER 2022-529932 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23.;[02] REPLACED RIB LOCATED ON DORSAL FIN PANEL 321A AT LEVEL STA 867SDR SWAA2022101046554None · crackedCRACK ACCESS PANEL 321A RIB 8 ON INTERNAL AREA FWD POSITION AT VERTICAL STABILIZER 2022-466985 / [01] REPLACED RIB 8 LOC ACCES PANEL 321A INTERNAL AREA FWD POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02;[02] REPLACED RIB 8 LOC ACCES PANEL 321A INTERSDR AALA202208192262Rib · crackedAIRCRAFT IN BASE MAINTENANCE: 0.75 INCH CRACK FOUND ON RIB LOCATED AT RIGHT STABILIZER STA 92.7 AND 1 INCH FROM THE BOTTOM ON THE NUMBER 4 STIFFENER. INSTALLED INTERNAL DOUBLER REPAIR PER SRM 55-10-09-2R-4.SDR A6WA202207308301None · gougedL/H HSTAB Z BRACKET AT CANTED RIB 158.71 HAS TOOLING MARK DAMAGE MEASURING .600"L X .300"W X .030"D. EVALUATED DAMAGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-31-27 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** BLENDESDR SWAA2022081231546Rib Doubler · crackedDORSAL FIN STRUCTURE. FWD MOST RIB ASSY (STA 867) CRACKED AT TWO LOCATIONS (DOT 25-1). / [01] REMOVED CRACKED FWD RIB ASSY AT DORSAL FIN REF B737-700 ERM 51-40-02-0G-0;[02] VERIFIED STEP 1.;[03] OK TO INSTALL NEW RIB ASSY;[04] INSTALLED NEW DORSAL FIN FWD MOSTSDR FDEA202207041685Spar · 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 FROSDR SWAA2022072924961Rib · crackedVERTICAL FIN LEADING EDGE RIB #15 CRACKED / [01] EVALUATED CRACK AT VERTICAL FIN L/E RIB #15 FOUND OUT OF LIMITS NO CRACKS ALLOWED IAW B 737-7 SRM 55-30-09-1A-1;[02] FABRICATED NEW VERTICAL FIN RIB IAW B 737-7 SRM 55-30-09-01-1 DWG.176A1410 ID 0002 REV:D;[03] SDR FDEA202206301623Spar Cap · crackedDURING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION ON THE RIGHT HAND FORWARD FLANGE OF LOWER VERTICAL STABILIZER REAR SPAR CAP , FOUND 01 EACH CRACK WITH LENGTH APPROXIMATE 1.5 INCHES BETWEEN THE LOWEST TWO FASTENERS AT APPROXIMATE STATION 2164. RIGHTSDR SWAA2022070717598Rib · crackedCRACK DORSAL FIN RIB #8 AT VERTICAL STABILIZER 2022-316969 / [01] REPLACED RIB #8 AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 174A0101 SHEET: 5 REV: B<BR> SEE INDIVIDUAL SIGN-OFFS BELOW;[02] REPLACED RIB #8 AT VERTICAL STABILISDR SWAA2022070116743Rib · crackedCRACK FOUND ON DORSAL FIN FWD RIB FITTING. / [01] REMOVED DORSAL FIN FWD RIB AS PER REF B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW RIB AS PER REF B737-700 SRM 51-40-05-0G-0;[03] VERIFIED STEPS 1 AND 2. OK TO INSTALL NEW RIB.;[04] INSTALLED NEW RIBSDR 3EJA94206/2/22None · noneWHILE PERFORMING THE DOC 15 INSPECTION, FOUND A CRACK ON THE FRAME ON THE AFT SIDE OF THE VERTICAL STABILIZER AFT SPAR. CRACK IS APPROXIMATELY 6 INCH LONG ACROSS THE ENTIRE LENGTH OF THE FRAME. ALSO THE CLOSE OUT PANEL, BELOW THE RUDDER, ABOVE THE TAIL CONE, ISDR SWAA2022061613233Rib · crackedCRACK DORSAL FIN RIB #8 AT VERTICAL STABILIZER 2022-291513 / [01] REPLACED RIB 8 ON DORSAL FIN AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DRAWING 174A0103 REV -: AND MEASURES OF CRACK IS L: 0.260 INCH TOOK MECHANICALLY TOOL USED CALIPER P/N: 500-197-SDR SWIA202266079None · crackedR/H VERTICAL STAB AFT DRAG ANGLE IS CRACKED (C-CHECK RO 7/8/2022) REMOVED DAMAGED AND INSTALLED REPAIR DOUBLER AND FILLER ON R/H AFT DRAG ANGLE. REF: CRJ700 SRM 55-31-00-201-001-A01. / COMPLIED WITH TASKCARD 51-900-1002-SKYSDR SWIA202266066None · cracked*R/H VERTICAL STAB DRAG ANGLE IS CRACKED (MARKED) (C-CHECK RO 7/8/2022) REMOVED DAMAGED AND: INSTALLED REPAIR DOUBLER AND FILLER ON R/H FWD DRAG ANGLE. REF: CRJ700 SRM 55-31-00-201-001-A01. / COMPLIED WITH TASKCARD 51-900-1002-SKYSDR SWAA2022060707087Rib · crackedDORSAL FIN PANEL 321A FWD FITTING CRACK. DORSAL FIN PANEL 321A FWD RIB CRACK / [01] REMOVED DORSAL FIN 321A FWD RIB AS PER REF B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW RIB P/N 174A1108 AS PER REF B 737-700 SRM 51-40-05-0G-0;[03] VERIFIED STEPS 1SDR FDEA202205031103Frame · crackedVERTICAL STABILIZER RIGHT HAND ACCESS PANEL 364QR CUTOUT DOUBLER ASSEMBLY FOUND CRACK AT APPROXIMATELY STATION Y 2164 CRACKED FRAME DOUBLER AT VERTICAL STABILIZER APPROXIMATELY STATION Y 2164 RIGHT HAND ACCESS PANEL 364QR CUT OUT REMOVED AND REPLACED PER MSDR SWIA202265991None · cracked*SUSPECTED CRACK ON L/H DRAG ANGLE AT BASE OF VERTICAL STAB (MARKED) (C-CHECK RO 7/8/2022) REPAIRED L/H DRAG ANGLE AT BASE OF VERTICAL STAB REF CRJ700 SRM 55-31-00-201-001-A01.COMPLIED WITH 51-900-1002-SKY. SEE CONTINUATION CARD FOR MORE DETAILSSDR SWAA2022051196236Rib · crackedFOUND RIB #8 P/N 174A1008-2 OF DORSAL FIN ASSEMBLY CRACKED / [01] REMOVED RIB AT DORSAL FIN AS PER REF B737-700 SRM 51-40-02-0G-0. PERFORMED BY RS # 35463;[02] LOCATED AND DRILLED NEW RIB AS PER REF B737-700 SRM 51-10-05-0G-0. PERFORMED BY RS # 35463;[03] VERISDR DALA2022031601738None · noneSHIP 179 VERTICAL STABILIZER L/H AUXILIARY SPAR SKIN FOUND 2 BULGE BETWEEN FSS 170 AND FSS 245. CORRECTIVE ACTION: SKIN REPAIRED BETWEEN FSS 170 AND FSS 245 AS PER B767-300 SRM 55-30 & SRM 51-70 (2154047)SDR REXA2022032400493Spar · corrodedMULTIPLE GOUGES NEAR FASTNER HOLES UNDER PANEL 324AT (V-STAB LEADING BLENDED OUT MULTIPLE GOUGES NEAR FASTENERS HOLES UNDER PANEL 324AT AT V-STAB LEADING EDGE IAW CRJ/200 SRM 51-12-00.FOUND TO BE WITHIN LIMITS IAW CRJ/200 SRM 55-31-07SDR VNAA2022012899913Drag Angle · cracked(N0104) L/H AFT DRAG ANGLE, SUSPECT CRACK. ACCOMPLISHED REPAIR OF LH DRAG ANGLE IAW CRJ 700 SRM 55-31-00-201-001-A01.SDR DALA2022012600524None · noneSHIP 3209 CRACK INDICATION - FR 4 HORIZONTAL UPPER STIFFENER, HAS CRACK INDICATION IN LOWER FORWARD RADIUS ABOVE AND OUTBOARD OF HORIZONTAL BOLT IN UPPER FORWARD CORNER. CORRECTIVE ACTION: COMPLIED WITH ERA 596540-14AD REV. ORIGINAL. (2098512)SDR R61A2022011870037Rib · crackedWHILE AC WAS IN FOR HVY CK FOUND VERTICAL STAB CRACK FOUND ON TRAILING EDGE OF RIB 7 RH SIDE. MX REPAIRED RIB PN 170-24422-001 IAW ETD2022-170-000509SDR DALA2023030701656None · noneERA 586819-14AD INSTALLED A REPAIR STRAP COMMON TO RH SPAR CAP O N VERTIAL STABILIZER, ERA REVISION A IS CURRENT. ACCOMPLISH ERA 586819-14AD REV A SECTION II AT 4600 CYCLES AFTER SECTION I, THEN 2400 CYCLE INTERVALS THEREAFTER. ASSOCIATED AA 5530-01048 ADDED FSDR SWAA2022012054443Rib · crackedCRACK ACCESS PANEL 321A FWD RIB AT VERTICAL STABILIZER. REPLACED NEW RIB AT ACCESS PANEL 321A IAW B737-700 SRM 51-40-02 AND DRAWING # 174A1108 SHEET 2 REV C.SDR SWAA2022011249854Rib · crackedSUPPLEMENTAL INFORMATION: VERTICAL DORSAL FIN FWD RIB CRACKED ; / [01] REMOVED AND REPLACED VERTICAL DORSAL FIN FWD RIB AS PER B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING 174A0103; [02] VERIFIED STEP 1SDR SWAA2022010549813Rib · crackedCRACK DORSAL FIN RIB 8 AT VERTICAL STABILIZER ; 2021-549833 / [01] REPLACED RIB 8 AND FASTENERS LOC. DORSAL FIN AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 174A1008 SHEET 2 REV.C. REPLACED RIB 8 AND FASTENERS LOC. DORSAL FIN AT VERTICAL STABILIZESDR DALA2021111707084None · noneERA 590337-14AD SECTION I ISSUED FOR CRACK FINDINGS DURING EM5530-01048. ERA REVISED TO REV 'A' FOLLOWING DTE STAGE III. ACCOMPLISH SECTION III WITHIN 3000 FC OF SECTION I (28FEB21) AND REPEAT EVERY 2400 FC THEREAFTER. ASSOCIATED ER/A 95-590337 ADDED FOR AC 95SDR DALA2021111707085None · noneERA 590337-14AD SECTION I ISSUED FOR CRACK FINDINGS DURING EM5530-01048. ERA REVISED TO REV 'A' FOLLOWING DTE STAGE III. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION II WITHIN 3000 FC OF SECTION I (28FEB21) AND REPEAT EVERY 3000 FC THEREAFTER. ACCOMPLISH SECTSDR SWAA2022011042168Fitting · crackedVERTICAL FIN FRONT SPAR FITTING; FIX LEADING EDGE SPRING ANGLE CRACK NOTED. ; / [01] REMOVED FIX LEADING EDGE SPRING ANGLE AT VERTICAL FIN FRONT SPAR FITTING IAW SRM 51-40-02-0G-0.; [02] VERIFIED STEP #1; [03] LOCATED AND DRILLED NEW FITTING FIX LEADING EDGE VSDR SWAA2022010641156Rib · crackedDORSAL FIN INTERNAL FWD (#1) RIB; CRACK NOTED. ; / [01] REMOVED RIB #1 AT INTERNAL FWD DORSAL FIN REF B737-700 SRM-51-40-02-0G-0.; [02] FABRICATED RIB #1 P/N 174A1108-1 MAT USED 2024-O 0.040 CLAD P/O# 1679582 REF DWG#174A1108.; [03] VERIFIED STEP #1 AND #2.; [SDR LR7A2021091102974Web · crackedDURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, CRACK IN THE VERT STAB REAR BEAM WEB AT VSS10, FS1095, LBL15 / REPAIRED IAW LAC MEA 382-55-21-077. NR# 1000565839.SDR LR7A2021091102972Web · noneDURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5511, FOUND VERTICAL AUX BEAM WEB CHAFFED AT VSS, FS1016 BL0. / REPAIRED IAW LAC MEA 382-55-21-076. NR# 1000565771.SDR P5CA2021101600393None · noneTWO LIGHTNING STRIKES ON THE DIVERTER STRIP OF VERTICAL STABILIZER TIP(<P><SPAN><SPAN> </SPAN><SPAN>DIVERTER STRIP OF VERTICAL STABILIZER TIP WAS REPAIRED BY BLEND-OUT IAW BOEING SR# 4-5219944422</SPAN></SPAN></P>)SDR SWAA2021102030753Rib · crackedCRACK DORSAL FIN RIB 8 AT STA 867 (ACCESS PANEL 321A) AT VERTICAL STABILIZER. REPLACED RIB STA 867 IAW B737-700 SRM 51-40-02 AND FASTENERS DWG 174A0103 REV A. SEE INDIVIDUAL STEP SIGN OFFS BELOW REPLACED RIB STA 867 IAW B737-700 SRM 51-40-02 AND FASTENERS DWGSDR SWAA2021111826992Rib · crackedVERTICAL DORSAL FIN 321A FORWARDMOST RIB CRACKED ; / [01] REMOVED DORSAL FIN FWD RIB AS PER B737-700 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED HOLES ON NEW RIB AS PER B737-7 SRM 51-40-05-0G-0.; [03] VERIFIED STEP 1-2 . OK TO INSTALL NEW RIB; [04] INSTALLED FSDR SWAA2021111726866Rib · crackedDORSAL FIN FWD RIB CRACKED ; / [01] REMOVED DORSAL FIN FWD RIB AS PER B737-700 SRM 5-40-02-0G-0; [02] LOCATED AND DRILLED NEW RIB ASSEMBLY AS PER B737-700 SRM 51-40-05-0G-0; [03] VERIFIED STEP 2. OK TO INSTALL ON DORSAL FUN.; [04] INSTALLED NEW RIB AT DORSAL FSDR DALA2021100406039None · noneSHIP 194 RIGHT VERTICAL STAB HONEYCOMB PANEL DELAMINATED BETWEEN AUX SPAR AND FROUNT SPAR AND FSS 195.39 TO FSS 220.521. REPAIRED PER SRM 55-30-01 AND 51-70-10. (LP 1967733)SDR DALA2021100206000None · noneSHIP 194 LEFT VERTICAL STAB HONEYCOMB PANEL DELAMINATION BETWEEN AUX SPAR AND FRONT SPAR AND FSS118.75 TO FSS145.128. REPAIRED PER SRM 55-30-01 AND 51-70-10. (LP 1967795)SDR SWAA2021101924464None · crackedCRACKED REAR SPAR LT FWD DRAG BRACE FITTING INBOARD POSITION AT VERTICAL STABILIZER. REMOVED REAR SPAR DRAG BRACE FITTING IAW SRM 51-40-02, DUE TO NO FOUND ALLOWABLE DAMAGE ON SRM AND MUST BE REPLACED AND PERFORMED VISUAL INSPECTION ON AREA AND NO FOUND DAMAGSDR SWAA2021101922253None · corrodedCORROSION REAR SPAR LH DRAG BRACE FITTING AT FWD O/B POSITION AT VERTICAL STABILIZER ; 2021-437292 / [07] INSTALLED NEW REAR SPAR LH DRAG BRACE FITTING AT FWD O/B POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DRAWING # 148A8200 SHEET 4 REV -; [SDR SWAA2021101922254None · corrodedCORROSION REAR SPAR LT DRAG BRACE FITTING AT AFT INBD POSITION OF VERTICAL STABILIZER, REMOVED REAR SPAR LH DRAG BRACE FITTING IAW SRM 51-40-02. PERFORMED A VISUAL INSPECTION OF AREA AND NO FOUND DAMAGE. DRILLED A NEW REAR SPAR LT DRAG BRACE FITTING IAW SRM SDR SWAA2021110122342None · crackedCRACK VERTICAL STAB RIB 8. REMOVED AND REPLACED THE RIB IAW SRM 51-40-02 AND DWG 174A0103 SHEET 3 REV A.SDR FDEA202109222353Spar Cap · crackedDURING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION ON THE LEFT HAND FORWARD FLANGE OF UPPER SECTION REAR SPAR CAP AT LOWER VERTICAL STABILIZER , NUMBER 4 BANJO FITTING STATION Y = 2164 , FOUND 01 EACH CRACK INDICATION BETWEEN THE LOWEST TWO FASTENERS.SDR SWAA2021110920599None · corroded>>> CORROSION >> VERTICAL STABILIZER; RIGHT FRON SPAR FITTING PITTING CORROSION ; / [01] REMOVED BUSHING AT VERTICAL STABILIZER RIGHT FRONT SPAT FITTING AS PER B737-700 SOPM 20-50-03; [02] REMOVED CORROSION AT VERTICAL STABILIZER RIGHT FROM SPAR FITTING REF B7SDR SWAA2021110920598None · corroded>>> CORROSION >> VERTICAL STABILIZER ; LEFT FRON SPAR FITTING CORROSION ; / [01] REMOVED BUSHING AT VERTICAL STABILIZER LEFT FRONT SPAR FITTING AS PER B737-700 SOPM 20-50-03; [02] REMOVED CORROSION AT VERTICAL STABILIZER LEFT FROM SPAR FITTING REF B737-7 SRM 5SDR SWAA2021093016029Spar · corrodedPITTING ON DORSAL FIN FRONT SPAR FITTING RH BOLT (STA 1016) AT VERTICAL STABILIZER (1EA) ; 2021-403818 / [01] REMOVED RH BOLT ON DORSAL FIN FRONT SPAR FITTING AT VERTICAL STABILIZER (STA 1016) IAW B737-700 AMM 55-30-00-000-801 STEP 2F(7)(B) AND PERFORMED GENERSDR DALA2021090205178Spar Cap · damagedERA 585576-14AD SECTION I ISSUED FOR DEVIATION TO WC5530-01048 / SB B717-55A0012 INSPECTION TO VERT STAB LEADING EDGE AND SPAR CAP ERA REVISED TO REV 'A' FOLLOWING DTE. REFER TO LP #1505142. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION II INSPECTION EVERY 300
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