JASC 5534
Service difficulty reports · 820
Reports filed under 5534 · Vertical Stabilizer Miscellaneous Structure, 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 = '5534' 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 = '5534' 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 SWAA2022053108530Bracket · crackedCRACK DORSAL FIN FRONT SPAR CROSSBEAM BRACKET AT STA 1016 INTERNAL CAVITY AT VERTICAL STAB 2022-239726 / [01] REPLACED DORSAL FIN FRONT SPAR CROSSBEAM BRACKET AT STA 1016 INTERNAL CAVITY AT VERTICAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DWG 17SDR SWAA2022050295170Panel · erodedEROSION ACCESS PANEL 321A AT VERTICAL STABILIZER 2022-192704 / [01] TOOL USED: CALIPER P/N 500-464 S/N 15331932 DUE DATE 26-OCT-22.;[02] TOOL USED: HOTBONDER P/N HCS9200B-AV S/N 18196119 DUE DATE 24-FEB-2023.;[03] TOOL USED: MULTIMETER P/N: FLUKE87 S/N: 421801SDR YENA2022040500333Hinge Arm · elongatedDURING HEAVY MAINTENANCE, REMOVE AND REPLACE HINGE ARM 3 DUE TO ELONGATED HOLES AFTER THAT AIRBUS REJECT TEMPORARY REPAIR ON VERTICAL STABILIZER; AEROMAN WO# 2022-12/4 WCC# 2022-57697 RII INSPECTOR 8610212 AE REMOVED AND REPLACED HINGE ARM #2 LOCATED ON VERTSDR SWAA2022042088650Web · crackedCRACK ON WEB FWD POSITION ON ACCESS PANEL 321A AT VERTICAL STABILIZER 2022-148363 / [01] TOOL USED CALIPER P/N 500-197-30 S/N A18135101 DUE DATE 06-AUG-22 <BR>GAGE RADIUS P/N 06457055 S/N AE-28115 DUE DATE 05-JUL-22;[02] TOOL USED: TEMPERATURE CONTROLLER P/N: SDR SWAA2022042086155Angle · crackedCRACK DORSAL FIN FWD CLOSURE ANGLE RH SIDE AT VERTICAL STABILIZER 2022-148134 / [01] REPLACED CLOSURE ANGLE AND FASTENERS LOCATED RH SIDE AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02. AND DWG 147A0030. REV. ?B?. SEE INDIVIDUAL SIGN OFFS BELOW;[02] JOB COMPSDR SWAA2022041986089Access Panel · crackedCRACK ACCESS PANEL 321A DORSAL FIN RIB FWD POSITION VERTICAL STABILIZER 2022-122565 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23;[02] REPLACED ACCESS PANEL 321A DORSAL FIN RIB FWD POSITION ON VERTICAL STABISDR SWAA2022041885522Angle · crackedLT VERTICALSTAB ACCESS PANEL 323BL;SHOWS AFT CLOSURE ANGLE CRACKED AT FWD LWR AREA / [01] REMOVED AND REPLACED LT VERTICAL STAB. ACCESS PANEL 323BL AFT CLOSURE ANGLE PER REF B737-700 SRM 51-40-02-0G-0 AND DWG 172A6121.;[02] VERIFIED STEP 1.SDR SWAA2022040583842Angle · crackedCRACK SUPPORT ANGLE INTERNAL ARE ACCESS PANEL 323BL AT VERTICAL STABILIZER 2022-144814 / [01] REPLACED SUPPORT ANGLE INTERNAL ARE ACCESS PANEL 323BL AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DRAWING 176A3001 SHEET 22 REV D SEE SDR IXXA202201160001Spar Web · gougedVERT STAB INTERNAL (ACCESS 311AZ ) ABOVE RIB 4 HYD LINE CLAMP GOUGED RIB WEBSDR 2022F00091Spar Cap · crackedDURING COMPLIANCE WITH SIKORSKY SERVICE BULLETIN 76-015, A CRACK WAS DISCOVERED RADIATING AROUND THE UPPER LEFT HORIZONTAL STABILIZER ATTACHMENT FITTING BOLT HOLE. THE CRACK WAS INITIALLY DISCOVERED VISUALLY AND CONFIRMED WITH DYE-PENETRANT INSPECTION. THE CRASDR SWAA2021111833062Fitting · corrodedCORROSION FITTING AFT REAR SPAR DRAG BRACE FWD POSITION O/B SIDE AT VERTICAL STABILIZER ; 2021-486753 / [01] REPLACED FITTING DRAG BRACE R/H FWD POSITION O/B SIDE AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02; SRM B737-700 51-40-02; AND DWG 148A8200 SHEET 6SDR SWAA2021110924748None · corrodedCORROSION.>>>>>VERTICAL FIN FWD R/H ATTACHMENT FITTING LUGS STA 1016 INNER BORE EVIDENCE OF PITTI CORROSION. ; / [01] REMOVED CORROSION ON VERTICAL FIN FWD R/H ATTACHMENT FITTING LUGS STA. 1016 PER REF. 737 SRM 51-10-02-0G-0; BY REAMING HOLE TO FINAL SIZE; 1.0SDR SWAA2021110924747None · corrodedCORROSION >>>>>>>VERTICAL FIN FRONT SPAR R/H FITTING LUG HAVE SIGN OF PITTI CORROSION AT INNER BORE. ; / [01] REMOVED CORROSION ON VERTICAL FIN FRONT SPAR R/H FITTING LUG; PER REF. 737 SRM 51-10-02-0G-0; BY REAMING HOLE TO FINAL SIZE ; 1.040 (0N VERTICAL); [02SDR SWAA2021110924746None · corrodedCORROSION >>>>>>>VERTICAL FIN FRONT SPAR L/H FITTING LUG HAVE SIGN OF PITTI CORROSION AT INNER BORE. ; / [01] REMOVED CORROSION ON VERTICAL FIN FRONT SPAR L/H FITTING LUG ; PER REF. 737 SRM 51-10-02-0G-0; BY REAMING HOLE TO FINAL SIZE ; 1.040;( ON VERTICAL); [SDR SWAA2021110919701Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT I/B REAR SPAR FITTINGS CORROSION ; /SDR SWAA2021110919700Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER; RIGHT FRON SPAR FITTING PITTING CORROSION ; /SDR SWAA2021110919699Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER ; LEFT FRON SPAR FITTING CORROSION ; /SDR SWAA2021110919698Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT FRON SPAR FITTINGS CORROSION ; /SDR SWAA2021110920602Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER ; RIGHT I/B REAR SPAR FITTINGS PITTING CORROSION ; / [01] REMOVED BUSHINGS AT RIGHT VERTICAL STABILIZER I/B REAR SPAR AS P[ER B737-700 SOPM 20-50-03; [02] AFTER BUSHING REMOVAL ; INSPECTED AREA AT VERTICAL STABILIZER; RIGHTSDR SWAA2021110920607Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; RIGHT I/B REAR SPAR FITTINGS PITTING CORROSION ; / [01] EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT); [02] EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT); [03] ISSUED SUMMARY EA 21-153-02759; [04] C/WSDR SWAA2021110920606Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; RIGHT O/B REAR SPAR FITTINGS PITTING CORROSION ; / [01] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q006KMKF; [02] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q0SDR SWAA2021110918242Angle · crackedVERTICAL FIN; FWD TERMINAL FITTING ASSY AFT FACE HORIZONTAL T ANGLE CRACKED 2 EA PLACES ; / [01] PERFORMED HFEC INSP ON VERTICAL FIN FWD TERMINAL FITTING ASSY AFT FACE HORIZ T ANGLE IAW B737 NDT P6 51-00-00 PROC.23; CRACKS NOTED MARKED.<BR>TOOL USED : NORTEC 6SDR DU4R2020070900050Bracket · corrodedBONDING BRACKET LT SIDE OF VERT STAB JUST BELOW UPPER RUDDER HINGE HAS EXFOLIATED CORROSION REQUIRING REPLACEMENT.SDR FDEA2020070211408Fitting · damaged01 EACH FASTENER HOLE FOUND ELONGATED DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT NUMBER 4 BANJO FITTING RIGHT HAND SIDE AFT 4TH HOLE COUNTING FROM BELOW 01 EACH FASTENER. HOLE ELONGATED DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ATSDR FDEA2020070211407Fitting · crackedCRACK INDICATION FOUND ON 01 EACH HOLE DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON SKIN PANEL LAYER AT NUMBER 4 BANJO FITTING. RIGHT HAND SIDE FORWARD EXISTING REPAIR 5TH HOLE COUNTING FROM BELOW CRACK ON 01 EACH HOLE DURING HIGH FREQUENCY EDDYSDR IPXA2020070157186Angle · crackedINSPECTION TYPE:SV LOWER VERTICAL STABILIZER REAR SPAR FIRE SEAL ANGLE CRACKS. REMOVED AND REPLACED CRACKED LOWER VERTICAL STABILIZER REAR SPAR FIRE SEAL IAW EA 011-5530-01-A8380 REV IR AND EO MD11-5530-77008-A. (MAJOR)SDR VNAA202006239996Drag Angle · crackedVERTICAL STABILIZER RT AFT DRAG ANGLE HAS EVIDENCE OF A CRACK APPROX 1/2" LONG. CUT AWAY DAMAGED AREA OF RT AFT VERTICAL STAB DRAG ANGLE PER SRM 55-31-00-201-001-A01, STEPS 5B1 AND 5B2. C/W STEP 5/B/3 OF SRM 55-31-00-201-001-A01 (NDT).SDR FDEA2020061981269Fitting · 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 STABSDR SWAA2020063093953Angle · gougedGOUGE CLOSURE ANGLE LOC BTW STA 1100 TO 1132.02 RT SIDE AT VERTICAL STABILIZER. REPAIRED CLOSURE ANGLE LOC BTW STA 1100 TO 1132.02 RT SIDE AT VERTICAL STABILIZER SRM 53-80-71-2R-6 REPAIR 6 AND DWG 148A3590.SDR IPXA2020062656961Intercostal · crackedINSPECTION TYPE:2C LOWER VERTICAL STABILIZER REAR CENTER SPAR TO LOWER PANEL INTERCOSTAL RT SIDE IS CRACKED AT STA YID= 375 AND XID= -7.1. REPAIRED CRACKED LOWER VERTICAL STABILIZER REAR CENTER SPAR TO LOWER PANEL INTERCOSTAL RT SIDE AT STA YID= 375 AND XID= SDR SWAA2020062288150Nut Plate · brokenBROKEN NUT PLATE AT VERTICAL STABILIZER REAR SPAR LT SIDE LOWER SUPPORT ANGLE. REMOVED AND REPLACED NUT PLATE AT VERTICAL STABILIZER REAR SPAR LT LOWER SUPPORT ANGLE AS PER SRM 51-40-02-0G-0.SDR FDEA202005130924Fitting · damagedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT AS PER EARN NR - 0015 REQUEST ON ALL FASTENER HOLES AT LEFT HAND BANJO FITTING FORWARD AND AFT REPAIR AREA STATION Y = 2164 AND FOUND NUMBER 4 HOLE FROM BOTTOM UP AT AFT ROW WITH DAMAGE INDICASDR FDEA2020050430879Fitting · 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 APPROXIMATELY STATION Y = 2164SDR SWAA2020051176066Skate Angle · chafedL/H VERTICAL STAB. SKATE ANGLE HAS EVIDENCE OF CHAFFING .(MARKED) / REMOVED AND REPLACED LH FWD SKATE ANGLE PER SRM 51-40-02.SDR SWAA2020051176067Skate Angle · chafedR/H VERTICAL STAB. SKATE ANGLE HAS EVIDENCE OF CHAFFING .(MARKED) / REMOVED AND REPLACED RH FWD VERTICAL STABILIZER SKATE ANGLE PER SRM 51-40-02.SDR REXA2020042800543Drag Angle · crackedVERTICAL STAB, LH, AFT DRAG ANGLE, POSSIBLE CRACK.
REPAIRED VERT STAB LH AFT DRAG ANGLE IAW EA CRJ953-0172 & SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 & 51-42-22-001-001-A01, 51-40-11-
00SDR SWAA2020050436722Channel · crackedVERTICAL STAB STAB STA 1016; 7.5' ABOVE FUSELAGE SKIN @ VERTICAL STAB MOUNT. LATERAL SUPORT CHANNEL CRACKED AT BOTH SIDES AT RADIUS / REMOVED AND REPLALCED VERTICAL STABIZER SPRING ASSEMBLY P/N 176A3101-26 I/A/W SRM 51-40-02-0G-0 AND BOEING DRAWINGS 176A3101 RSDR SIMA2020041431001Profile · crackedVERT.STAB., AFT SPAR3, L/H PROFILE CRACKED ABOVE RUDDER 1 TOP CENTER HINGE FITTING.-C/A-VERT.STAB., AFT SPAR 3, L/H PROFILE ABOVE RUDDER 1 TOP CENTER HINGE FITTING REPAIRED AS PER ETD 2020-145-013336.SDR SWAA2020033120972Skate Angle · wornL/H VERTICAL STABILIZER SKATE ANGLE WORN STA 1006 TO STA 1088 / REMOVED + REPLACED L/H VERTICAL STAB SKATE ANGLE STA 1016 TO 1088 IAW SRM 51-40-02-0G-0 + DWG 148A8300 SHT 2 REV A RX0388SDR SWIA2020040649953Drag Angle · crackedVERTICAL STAB'S RH AFT DRAG ANGLE HAS EVIDENCE OF A CRACK. (C-CHECK) RO 4/3/2020 REPAIRED VERTICAL STAB€™S RH AFT DRAG ANGLE PER BOMBARDIER REO. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD.SDR SWIA2020040649952Drag Angle · crackedVERTICAL STAB'S LH AFT DRAG ANGLE IS CRACKED. (C-CHECK) RO 4/3/2020 REPAIRED VERTICAL STAB€™S LH AFT DRAG ANGLE PER BOMBARDIER REO. SEE CONTINUE CARD FOR DETAILS.SDR SWIA2020040649951Drag Angle · crackedVERTICAL STAB'S LH FWD DRAG ANGLE IS CRACKED (MARKED). (C-CHECK) RO 4/3/2020 COMPLIED WITH REPAIR TO THE VERTICAL STABILIZER LH FWD DRAG ANGLE IAW REO AND COMPLIED WITH TASK CARD.SDR SWIA2020040149805Drag Angle · crackedL/H AFT DRAG ANGLE AT VERTICAL STABILIZER TO FUSELAGE IS CRACKED (C-CHECK) RO:3/29/2020PERFORMED CUTOUT REPAIR OF THE LH AFT DRAG ANGLE AT VERTICAL STABILIZER TO FUSELAGE REF CRJ 700 SRM. SKYCARD COMPLIED WITHSDR SWIA2020040149804Drag Angle · crackedL/H FWD DRAG ANGLE AT VERTICAL STABILIZER TO FUSELAGE IS CRACK (C-CHECK) RO:3/29/2020PERFORMED CUTOUT REPAIR OF THE LH FWD DRAG ANGLE AT VERTICAL STABILIZER TO FUSELAGE REF CRJ 700 SRM & REO. SKYCARD COMPLIED WITHSDR RAIA2020032660002Support Bracket · crackedVERTICAL STAB RH SIDE VERT TOP, RH MOVABLE FAIRING 'L' ANGLE SUPPORT BRACKET IS CRACKED - R&R VERTICAL STAB RH SIDE VERY TOP "L" ANGLE BRACKET.SDR SWAA2020040218837Bracket · crackedVERTICAL STAB PANEL 323BL FORWARD SKATE ANGLE BRACKET HAS HOLE IN IT. / REMOVED SKATE ANGLE BRACKET FROM VERTICAL STAB PANEL 323 BL IAW B737 SRM 51-40-02-0G-0 STEP 4.E. RECEIVE NEW SKATE ANGLE BRACKET PART NUMBER 172A6125U3. LOCATED & DRILLED NEW SKATE ANGLE BSDR SWAA2020040821836Skate Angle · chafedCHAFING ON THE LEFT SKATE ANGLE AT VERTICAL STAB BS1011 LBL14. / REMOVED; LOCATED; DRILLED AND INSTALLED SKATE ANGLE STA. 1011 LBL 14 PER SRM 51-40-05 FIG.4; SRM 51-40-02 PAR 4B; DWG. 147A0030 AND DWG. 147A3200. 91195U 3-4-20SDR SWAA2020040126802Skate Angle · wornVERTICAL STAB.RH FWD SKATE ANGLE AFT OF DORSAL FIN AREA WORN / REMOVED AND REPLACED FWD SKATE ANGLE RH SIDE PER SRM 51-40-02-0G-0 AND DWG 147A0030 REV BSDR SWAA2020040126803Skate Angle · wornVERTICAL STAB.RH AFT SKATE ANGLE WORN FWD AND AFT OF VERTICAL STAB; ATTACH POINTS / REMOVED AND REPLACED RH AFT SKATE ANGLE PART # 148A8310-4 PER SRM 51-40-02-0G-0 AND DWG 148A8300 REV CSDR SWAA2020040126804Skate Angle · wornVERTICAL STAB.LH AFT SKATE ANGLE WORN AFT OF VERTICAL STAB; ATTACH POINTS / REMOVED AND REPLACED RH AFT SKATE ANGLE PART # 148A8310-3 PER SRM 51-40-02-0G-0 AND DWG 148A8300 REV C
Back to JASC 5534