JASC 5530
Service difficulty reports · 2,534
Reports filed under 5530 · Vertical Stabilizer, 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 = '5530' 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 = '5530' 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 SWAA2022040683832Rib · crackedCRACK ON RIB #8 ON PANEL 321A DORSAL FIN 2022-129776 / [01] REPLACED RIB #8 AND FASTENERS LOCATED ON PANEL 321A DORSAL FIN IAW B737-700 SRM 51-40-02 AND DWG 174A1008 SHEET 2 REV. C. PART NUMBER USED: 174A1108-2 P.O:2022-128747.<BR>SEE INDIVIDUAL SIGN OFFS BELOSDR SWAA2022040583839Rib · crackedCRACK ON RIB #8 ON PANEL 321A DORSAL FIN 2022-144799 / [01] REPLACED RIB #8 ON PANEL 321A DORSAL FIN I.A.W. B737-700 DWG 147A0103 REV - AND SRM 51-10-02 Ï¿½TEM 9. <BR>SEE INDIVIDUAL SING-OFF BELOW;[02] CORRECTED STEP 1. REPLACED RIB #8 ON PANEL 321A DORSAL FINSDR IXXA2022032101Access Panel · delaminatedVERTICAL STAB, RIGHT HAND VERTICAL PNL @ FSS 14.128 DELAMINATEDSDR FDEA202203050421Spar · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NUMBER SN10550000 ON RIGHT HAND SIDE LOWER VERTICAL STABILIZER FORWORD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FROM SECONDSDR FDEA202203050420Spar · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NUMBER SN10550000 ON LEFT HAND SIDE LOWER VERTICAL STABILIZER FORWORD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FROM SECOND SDR REXA2022040100500Angle · crackedLH VERTICAL AFT DRAG ANGLE CRACKED REMOVED AND REPLACED LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-13-001-001-A01,51-42-21-001-001-A01 AND 51-42-22-001-001-A01.SDR REXA2022031000436Skin · noneWHILE ACCOMPLISHING RAPAIR ON L/H V.STAB FWD DRAG ANGLE, TECH DRILLED INTO SKIN. - REMOVED & REINSTALLED PANEL 325AL IAW CRJ 900 AMM 55-32-32-000/400-806(A01) REPAIRED L/H VERTICLE DRAG ANGLE (FWD) IAW REO 690-55-31-064. RESTORED SURFACE & SEALED IAW SRM 51-23SDR SWAA2022032878876None · corrodedCORROSION ON RUDDER COUNTER BALANCE FWD WEIGHT AROUND MOUNT BOLT HOLES. (MARKED) / [01] UPDATED MEASUREMENT AND PART FIELDS;[02] REMOVED RUDDER COUNTER BALANCE WEIGHT P/N 173A5103-1MIT AND INSTALLED NEW RUDDER COUNTER BALANCE WEIGHT P/N 173A5103-1MIT IAW CMM 5SDR REXA2022032200438Angle · crackedLH VERTICAL STAB DRAG ANGLE HAS SUSPECTED CRACK. - REMOVED AND REPLACED DRAG ANGLE IAW CRJ 900 SRM 51-42-22-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01SDR SWAA2022032176988Angle · crackedCRACK LEADING EDGE SUPPORT ANGLE LOC. STR2R TO STR2L AND BS 1021.27 AT VERTICAL STABILIZER 2022-85583 / [01] REPLACED SUPPORT ANGLE LOC. STR2R TO STR2L AND BS 1021.27 AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 176A3101 SHEET 4 REV: -;[02] REPLACESDR REXA2022031000427Drag Angle · crackedL/H AFT DRAG ANGLE IS CRACKED - REMOVED AND REPLACED LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-13-001-001-A01SDR 2022F00053Fairing · chippedLIGHTNING STRIKE DAMAGE OF THE VERTICAL FIN TIP FAIRING AND UPPER AFT RUDDER CAP. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ33675 DATED FEB. 20, 2022; 680A-0087, N537QS REPAIR RECOMMENDATION OF THE VERTICAL FIN TIP FAIRING AND UPPER AFT RUDDER CAP.SDR SWAA2022031476788Rib · crackedCRACK DORSAL FIN BRACKET RIB #8 AT VERTICAL STABILIZER 2022-104235 / [01] TOOL USED: CALIPER 0-6? P/N: 700-113-10 S/N: 0016656 DUE DATE: 11-MAY-22;[02] REPLACED BRACKET LOC. DORSAL FIN RIB #8 AT VERTICAL STABILIZER IAW B737-700 SRM-51-10-02 ITEM 9 AND DWG-174ASDR SWAA2022031473695Angle · crackedCRACK BRACKET ANGLE LOCATED AT BS 1016 UPPER FUSELAGE AT LEVEL S-2R AND S-2L AT VERTICAL STABILIZER 2022-95043 / [01] REPLACED BRACKET ANGLE AND FASTENERS LOCATED AT BS 1016 UPPER FUSELAGE AT LEVEL S-2R AND S-2L AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-40-SDR REXA2022030200299Angle · crackedRH AFT VERT DRAG ANGLE CRACKED. - REPAIRED IAW CRJ900 SRM 55-31-00-201-001-A01. SEALED AND PAINTED IAW CRJ 900 SRM'S 51-23-00-001-001-A01 AND 51-25-01-001-001-A01.SDR REXA2022030200300Angle · crackedLH AFT VERT. DRAG ANGLE CRACKED - REMOVED & REPLACED L/H AFT DRAG ANGLE, LOCATED/DRILLED/COUNTERSUNK NEW DRAG ANGLE, & PAINTED IAW CRJ-900 SRM'S 51-42-21-001-001-A01, 51-42-13-001-001-A01, 51-42-22-001-001-A01, 51-40-11-001-001-A01, & 51-25-01-001-001-A01.SDR IPXA2022020978814None · noneINSPECTION TYPE:CKLT VERT STAB SKIN PANEL DELAMINTEDINSTALLED TEMPORARY PANEL IAW EO B747-5530-82778-ASDR SWAA2022031470254Bracket · crackedCRACK BRACKET ANGLE LOCATED TERMINAL FITTING ASSEMBLY INTERNAL AREA ACCESS PANEL 323BR AT VERTICAL STABILIZER 2022-68031 / [01] REPLACED NEW BRACKET ANGLE(SPRING) LOCATED TERMINAL FITTING ASSEMBLY INTERNAL AREA ACCESS PANEL 323BR AT VERTICAL STABILIZER IAW B73SDR V0XD20220205001Drag Angle · crackedLEFT VERT STAB AFT DRAG ANGLE CRACKED .090" - CORRECTIVE ACTION: CUT OUT 2.2" DAMAGED SECTION AND REPAIRED LEFT VERTICAL STAB DRAG ANGLE IAW BOMBARDIER REO 670-55-31-018 REV-A 2016-11-10, EA 22-C7-55-122 REV IR 01/26/2022SDR SWAA2022031065941Angle · crackedCRACK ACCESS DOOR 323AL ANGLE VERTICAL STABILIZER 2022-55473 / [01] REPLACED ACCESS DOOR 323AL VERTICAL STABILIZER IAW B737-700 AMM 55-30-00-400-801 PARAGRAPH I (3).;[02] JOB COMPLETESDR SWAA2022031065942Plate · crackedCRACK ACCESS DOOR 323AR PLATE VERTICAL STABILIZER 2022-55472 / [01] REPLACED PLATE LOCATED AT ACCESS PANEL DOOR 323AR ON VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DRAWING # 172A6122 REV B;[02] REPLACED PLATE LOCATED AT ACCESS PANEL DOOR 323AR SDR SWAA2022031066153Rib · crackedCRACK ACCESS PANEL 321A LOCATED STRUCTURE RIB 8 AT VERTICAL STABILIZER 2022-55490 / [01] REPLACED RIB LOCATED STRUCTURE AT VERTICAL STABILIZER (DORSAL FIN RIB 8 ACCESS PANEL 321A ) IAW B737-700 SRM 51-10-02 PARAGRAPH 9;SRM 51-40-02 AND DWG 174A0103 SHEET 3 REVSDR SWAA2022031065355Panel · crackedCRACK ACCESS PANEL 324BL AT VERTICAL STABILIZER (2 EA) 2022-55333 / [01] TOOL USED HOTBONDER P/N: HCS9200B S/N: 16122983 DUE DATE: 16-JAN-23.;[02] TOOL USED: CALIPER P/N 500-464 S/N 15331926 DUE DATE: 28-SEP-22.;[03] TOOL USED: HOT BONDER P/N:HCS8800 S/N:01154SDR SWAA2022021872408Support Bracket · crackedCRACK LEADING EDGE SUPPORT BRACKET LOCATED AT BS 1016 BETWEEN S-2R AND S-2L AT VERTICAL STABILIZER 2022-58053 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23.;[02] REPLACED SUPPORT BRACKET (SPRING) AND FASTENERSDR SWAA2022021763323Support Bracket · crackedCRACK LEADING EDGE SUPPORT BRACKET LOCATED AT BS 1016 BETWEEN S-2R AND S-2L AT VERTICAL STABILIZER ; 2022-58053 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23.; [02] REPLACED SUPPORT BRACKET (SPRING) AND FASTESDR CALA2022012000197Keelbeam · elongatedWHILE ACCOMPLISHING FCD 5330-05575 RH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE EXCEPT HOLES #R 13 AND #R19. REPAIRED RH KEEL BEAM FASTENER HOLE AND FITTING IAW EC/RA 5330-0 6891. EMP: V935774 WC: 0018386 STA: ST ENG BFM SFR# 1SDR CALA2022012000194Keelbeam · elongatedWHILE ACCOMPLISHING FCD 5330-05575 LH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE (NO DOT) REPAIRED LH KEEL BEAM FASTENER HOLES AND FITTINGS IAW EC/RA 5330 -06891 EMP: V935774 WC: 0018385 STA: ST ENT BFM SFR# 1027501SDR ASAA2022011237482Hinge Arm · crackedRUDDER ATTACH FITTINGS, #1 HINGE ARM , LOWER LUG, 3RD FASTENER HOLE FROM LEFT HAS CRACK INDICATION AT 7 O'CLOCK POSITION GROUNDED - YES. REMOVED & REPLACED #1 HINGE ARM IAW ASA AIRBUS DWG D55371321 REV. D, ASA AIRBUS A320 SRM 55-36-42 & EA # A32055EA-01311 REVSDR SWAA2022021461048Fitting · corrodedON VERTICAL FIN AFT SPAR FITTINGS;LH FITTING DRAG BRACE;FWD MAIN O/B HAS CORROSION INSIDE OF LUG BORE. ; / [01] LOCATED DRILLED AND PRIMED HOLES AT NEW FITTING ON VERTICAL FIN AFT SPAR DRUG BRACE FWD MAIN O/B IAW B737 ARM 51-40-05-0G-0 ; AND 51-21-41-370-802; SDR IPXA2022013078453Angle · noneINSPECTION TYPE:3C#2 PYLON BANJO FITTING LWR SUPPORT ANGLE IS CRACK.REMOVED AND REPLACED SUPPORT ANGLE IAW MD11 SRM 51-31-01 (MINOR)SDR IPXA2022013078450Intercostal · crackedINSPECTION TYPE:3C#2 PYLON CARRY THRU REAR SPAR INTERCOSTAL IS CRACKED AT STA. YID= 375, XID= 7.1 AND ZID= 65.REPAIRED CRACKED #2 PYLON CARRY THRU REAR SPAR INTERCOSTAL AT STA. YID= 375, XID= 7.1 AND ZID= 65 IAW SRM 55-30-02 REPAIR 7 FIG. 203. (MAJOR)SDR FDEA202201120048Spar · 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 FOUNDSDR IPXA2022012478194None · noneINSPECTION TYPE:CR/H VERT. STAB. LWR FWD TORQUE BOX PANEL HAS 1EA AREA OF DELAMINATION/DISBONDREPAIRED PANEL IAW B757 SRM 51-70-10-2R PER SRM 55-30-01-2R-5SDR IPXA2022012278134None · noneINSPECTION TYPE:C5DISBOND DAMAGE ON R/H VST TORQUE BOX PANEL (P/N:175T2001-4) AT UPR FWD SIDE.REPAIR I.A.W BOEING SRID:3-5253366378 AND UPS EO B767-5530-82629-ASDR IPXA2022012078048None · noneINSPECTION TYPE:C5DISBOND DAMAGE ON L/H VST TORQUE BOX PANEL(P/N:175T2001-1)REPAIR I.A.W 767-300F SRM 55-30-1, REPAIR 1 , 767-300F SRM 51-70-10, REPAIR GENERAL AND 767-300F SRM 51-70-10, REPAIR 2 REV.82.01.SDR SWAA2022021559546Bracket · crackedCRACK SUPPORT BRACKET BS1016 BTW STR 2R TO STR 2L AT VERTICAL STABILIZER ; 2022-12216 / [01] REPLACED SUPPORT BRACKET (SPRING) AND FASTENER LOCATED ON BS1016 BTW STR 2R TO STR 2L AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRSDR SWAA2022013158140Channel · crackedA22-005; VERT STAB STA1016; LBL11; 5' ABOVE VERT STAB L/H ATTACH FTG; LATERAL SUPPORT CHANNEL CRACKED AT STRAIN RELIEF CUTOUT. ; / [01] REMOVED VERTICAL STAB LATERAL SUPPORT CHANNEL STA 1016 IAW SRM 51-40-02; [02] VERIFIED NEW PART TO BE MPN: 176A3101U26 ATAG:SDR R61A2022021400144Structure · damagedRUDDER AND VERTICAL STABLIZER DAMAGED BETWEEN RIB 10 AND RIB 13 AT TRAILING EDGE. REMOVED AND REPLACED THE RUDDER AND REPAIRED VERTICAL STABLIZER IAW EMB 170/175 ETD170-001452 AND AERNNOVA T1-170-22-001. ALSO REF VP-001581-2022 N/R 1 C1 THRU C6.SDR IPXA2022010777620None · noneINSPECTION TYPE:C13DISBOND DAMAGE (APPROX 7.0'' X 6'') ON R/H VST TORQUE BOX PANEL (P/N:175T2001-4) AT LWR AFT SIDEREPAIR I.A.W 767-300F SRM 55-30-01-2R-1 REV.82.01 AND 767-300F SRM 51-70-10-2R REPAIR GENERAL REV.82.01SDR IPXA2022010577543None · noneINSPECTION TYPE:C13DISBOND DAMAGE ON R/H VST TORQUE BOX PANEL (P/N:175T2001-4) AT LWR AFT SIDE.REPAIR I.A.W 767-300F SRM 55-30-01-2R-1 REV.82.01 AND 767-300F SRM 51-70-10-2R REPAIR GENERAL REV.82.01.SDR FDEA202112263146Fitting · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NO. SN10550000 REVISION C ON RIGHT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FROMSDR FDEA202112263145Fitting · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550012 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 SDR SWAA2022011856030Seal Plate · delaminatedLEFT VERTICAL STAB TRAILING EDGE SEAL PANEL 324ABL IS DELAMINATED AND HAS SECTIONS OF THE SEAL MISSING ; / [01] RECEIVED NEW SEAL PANEL P/N 175A1601-86; [02] OK TO INSTALL PANEL.; [03] INSTALLED NEW PANEL P/N 175A1601-86 REF B 737 SRM 51-40-02. WORK WAS ACCOMPSDR ASAA2021122237483Hinge Arm · cracked#7 RUDDER HINGE FITTING, UPPER HINGE ARM, FWD R/H FASTENER HOLE HAS CRACK INDICATION GROUNDED - YES. REPLACED #7 HINGE ARM IAW ASA EA#A320-55EA-01269 REV.00, ASA AIRBUS DWG D55371052 SHEET 5, VEIW 5-5 & SRM 55-36-42SDR SWAA2022011953643Panel · crackedLT SIDE HORIZONTAL FUSELAGE BLADE GUIDE FOR PANEL 333AT CRACKED. ; / [01] REMOVED LT SIDE HORIZONTAL FUSELAGE BLAD GUIDE FOR PANEL 333AT IAW B737 SRM 51-40-02; [02] VERIFIED STEP M#1; [03] OK TO INSTALL NEW REPLACEMENT.; [04] INSTALLED LT SIDE HORIZONTAL FUSELSDR SWAA2022011953644Panel · crackedRT SIDE HORIZONTAL FUSELAGE BLADE GUIDE FOR PANEL 343AT CRACKED. ; / [01] REMOVED RT SIDE HORIZONTAL FUSELAGE BLADE GUIDE FOR PANEL 343AT IAW B737 SRM 51-40-02; [02] VERIFIED STEP #1; [03] OK TO INSTALL NEW REPLACEMENT; [04] INSTALLED RT SIDE HORIZONTAL FUSELASDR SWAA2022010451827Angle · crackedPANEL 323AL SKATE ANGLE CLIP IS CRACKED / [01] UPDATED MEASUREMENTS; [02] REMOVED AND REPLACED PANEL 323AL SKATE ANGLE CLIP IAW SRM 51-40-02-01-0G AND BAC DWG 172A6122; [03] VERIFIED CORRECTIVE ACTIONS STEP 2.SDR REXA2021120701114Angle · crackedL/H AFT VERTICAL STABILIZER DRAG ANGLE IS CRACKED. C/A: REMOVED AND REPLACE DRAG ANGLE IAW CRJ 900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 & 51-40-11-001-001-A01SDR VNAA2022010299915Angle · crackedVERTICAL STABILIZER L/H AFT DRAG ANGLE IS CRACKED. CORRECTIVE ACTION: REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS I/A/W BOMBARDIER REO 670-55-31-018 REV. A DATED 2016-11-10SDR SWAA2021120741057Panel · crackedCRACK ACCESS PANEL 321A RIB #8 AT VERTICAL STABILIZER ; 2021-512090 / [01] REPLACED RIB #8 AT ACCESS PANEL 321A IAW B737-700 DWG 174A0103 REV:A AND SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SEGN OFF BELOW.; [02] REPLACED RIB #8 AT ACCESS PANEL
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