JASC 5342
Service difficulty reports · 578
Reports filed under 5342 · Fuselage, Stabilizer Attach Fittings, 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 = '5342' 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 = '5342' 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 SWIA202162954None · corrodedTHE R/H WINDSCREEN HAS A CORRODED DOUBLER BEHIND THE INBD FLOOR MOUNT FITTING. (C-CHECK RO 11-27-21) REPLACED R/H WINDSCREENS INBD FLOOR MOUNT FITTING DOUBLER WITH A SERVICEABLE DOUBLER (P/N=9395015-1) REFERENCING CRJ 700 SRM 51-41-02-001-001-A01. / TORQSDR CALA2021110102008Stringer · corrodedAFT CARGO FLOOR SLANT CORROSION (A3NB-53-4-6179) SEQ#549 DURING CLEANING OF AFT CARGO COMPARTMENT, SUSPECTED CORROSION WAS FOUND ON R/H STRINGER 38 FLOOR SLANT PANEL FROM FRAME 58 TO FRAME 59. FURTHER EVALUATION REQUIRED AS NOTED ON LTPR NR# 5001103184-0020. SSDR SWAA2021110833068Drag Brace · corrodedCORROSION FITTING ON DRAG BRACE FWD LOCATED AFT REAR SPAR LH POSITION AT VERTICAL STABILIZER. REPLACED FITTING REAR SPAR DRAG BRACE LH FWD POSITION O/B SIDE AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING # 148A8200 SHEET 4SDR SWAA2021110833067Drag Brace · corrodedCORROSION FITTING ON DRAG BRACE AFT POSITION LOCATED AFT REAR SPAR LH SIDE AT VERTICAL STABILIZER (1 EA). REPLACED FITTING DRAG BRACE LH AFT POSITION O/B SIDE AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DRAWING # 148A8200 SHEET SDR UATA2021100735214Attach Fitting · crackedL/H ELEVATOR LOWER AFT ATTACH FITTING ON FUSELAGE FOUND CRACKED AFTER ROUTINE NDI INSPECTION COMPLIED WITH. FITTING R&R PER SB212-53-52.SDR R61A2021071000561Angle · crackedRH ENGINE FIXED FAIRING, PYLON HEAT SHIELD ANGLE RIB #3 CRACKED. R/H ENGINE AFT FIXED FAIRING, PYLON HEAT SHIELD RIB #3 ANGLE HAS BEEN REPLACED WITH NEW AND INSTALLED IAW EMBRAER 170/175 SRM 51-42-01 AND 51-43-04, 51-43-03SDR SWAA2021062185543Skate Angle · chafedFIN TO BODY SKATE ANGLE IS CHAFED AT B.S. 1007-1016; R.B.L. 14; W.L. 306.5. FIN TO BODY SKATE ANGLE IS CHAFED. FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE FOUND IN SRM. LOCATED AND DRILLED NEW SKATE ANGLE IAW SRM 51-40-05-0G-0. INSTALLED NEW SKATSDR SWIA2021081060198Drag Angle · cracked*LH SIDE VERTICAL/FUSELAGE FWD DRAG ANGLE IS CRACKED (C-CHECK RO 8/6/2021) REPAIRED *LH SIDE VERTICAL/FUSELAGE FWD DRAG ANGLE REF CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY AND FORM M-337. SEE CONTINUE CARD FOR MORE DETAILSDR SWIA2021081860368Drag Angle · cracked* RH VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE HAS SUSPECTED CRACK (C-CHECK RO 8/16/2021) INSTALLED NEW RH AFT DRAG ANGLE ON VERTICAL STAB TO FUSELAGE IAW DWG BA670-35002, REV D, REF CRJ700 SRM 51-42-10-001-01-A01, CRJ700 SRM 51-42-21-001-001-A01 AND CRJSDR SWIA202160313Drag Angle · cracked* LH VERTICAL STAB TO FUSELAGE FWD DRAG ANGLE HAS SUSPECTED CRACK (C-CHECK RO 8/16/2021) REPAIRED LEFT-HAND VERTICAL STAB. TO FUSELAGE FWD DRAG ANGLE. REF. REO 670-55-31-018 REV -A DATED 2016-11-10. / SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TSDR SWAA2021061776915Angle · chafedCONTINUE REPAIR** R/T AFT BS 1016 TO BS 1132 FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFED (TTG8Q0051PJS). ; / REMOVED AND REPLACED CLOSURE ANGLE AT RT AFT BS 1016 - 1132 FUSELAGE FIN TO BODY INTERFACE PER B737-700 SRM 51-40-02-0G-0 AND DWG 148A8300;SDR SWAA2021062876858Skate Angle · chafedR/H FWD SKATE ANGLE BS 1006 TO BS 1016 IS CHAFED. ; / [01] DAMAGE FOUND ON R/H FWD SKATE ANGLE BS 1006 TO BS 1016 P/N 147A3200-12 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR-9C; [02] REMOVED R/H FWSDR VNAA202105229994Drag Angle · crackedCRACK ON VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLESDR SWAA2021061772823Angle · chafedRT AFT BS 1016-1132 FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFED AREAS. 8-31 ; / (AMENDING STEP 10) PARTIALLY INSTALLED CLOSURE ANGLE AT RT AFT BS 1016 - 1132 FUSELAGE FIN TO BODY INTERFACE (PENDING TO INSTALL 2 HI-LOKS) PER B737-700 SRM 51-40-02-0GSDR SWIA2021062358945Drag Angle · corrodedRH VERT STAB TO FUSELAGE AFT DRAG ANGLE HAS CRACK. (C-CHECK RO: 6/20/21) / INSTALLED NEW DRAG ANGLE REF DWG BA670-35002 REV -F , CRJ 700 SRM 51-42-21-001-001-A01,CRJ 700 SRM 51-42-22-001-001-A01,CRJ 700 SRM 51-42-13-001-001-A01. COMPLIED WITH 51-900-1002-SKSDR SWIA2021062358944Drag Angle · corrodedRH VERT STAB TO FUSELAGE FWD DRAG ANGLE HAS CRACK. (C-CHECK RO: 6/20/21) / FABRICATED AND INSTALLED NEW PARTS OF THE REPAIR AT RH VERT STAB TO FUSELAGE FWD DRAG ANGLE REF CRJ 700 SRM 55-31-00-201-001-A01 , CRJ 700 SRM 51-42-21-001-001-A01 AND COMPLIED WITSDR SWIA202158891Drag Angle · crackedLH VERT STAB TO FUSELAGE AFT DRAG ANGLE HAS CRACK. (C-CHECK RO: 6/20/21) / INSTALLED NEW DRAG ANGLE REF DWG BA670-35002 REV -F , CRJ 700 SRM 51-42-21-001-001-A01,CRJ 700 SRM 51-42-22-001-001-A01,CRJ 700 SRM 51-42-13-001-001-A01. COMPLIED WITH 51-900-1002-SKYSDR SWIA2021062859068Drag Angle · crackedRH VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE CRACKED (C-CHECK RO 6/22/2021) PERFORMED PERMANENT REPAIR TO THE R/H VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE. REF. CRJ 900 SRM 55-31-00-201-001-A01. / SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. / COSDR SWIA2021062859067Drag Angle · crackedLH VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE CRACKED (C-CHECK RO 6/22/2021) PERFORMED PERMANENT REPAIR TO THE L/H VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE. REF. CRJ 900 SRM 55-31-00-201-001-A01. / SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. / COSDR SWIA2021062859005Drag Angle · cracked*RH VERTICAL STAB TO FUSELAGE DRAG ANGLE CRACKED. AREA MARKED. (C-CHECK RO 6/22/2021) PERFORMED PERMANENT REPAIR TO R/H VERTICAL STABILIZER TO RH FUSELAGE DRAG ANGLES. REF. CRJ 900 SRM 55-31-00-201-001-A01 / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SSDR SWIA202159004Drag Angle · cracked*LH VERTICAL STAB TO FUSELAGE DRAG ANGLE CRACKED. AREA MARKED. (C-CHECK RO 6/22/2021) PERFORMED PERMANENT REPAIR TO L/H VERTICAL STABILIZER TO FUSELAGE DRAG ANGLES. REF. CRJ 900 SRM 55-31-00-201-001-A01 / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY SDR SWAA2021050358495Attach Fitting · corrodedVERTICAL STAB FWD LEFT FRONT SPAR FUSELAGE ATTACH FITTING HAS CORROSION ON ON FWD AND AFT SIDES /SDR SWAA2021040557660Skate Angle · damagedLEFT FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFFING DAMAGE / REMOVED & REPLACED L/H FWD SKATE ANGLE BS 1005 - 1016 IAW SRM 51-40-02-0G-0 & DWGS 147A0030 REV- & 147A0070 REV. B 59191U 03-19-21 DISPLACED INSULATION AT STR 3-L BS 1000 - 1016 TO FOM IAW AMM 25-8SDR SWAA2021040557661Skate Angle · damagedRIGHT FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFFING DAMAGE / REMOVED & REPLACED R/H FWD SKATE ANGLE BS 1005 - 1016 IAW SRM 51-40-02-0G-0 & DWGS 147A0030 REV- & 147A0070 REV. B 59191U 03-19-21 DISPLACED INSULATION AT STR. 3-R BS 1000 - 1016 TO FOM IAW AMM 25SDR SWIA202157651Attach Angle · crackedCRACK FOUND AT V-STAB TO FUSE ATTACHMENT LH FWD DRAG ANGLE (C-CHECK RO 4/21/2021) PERFORMED REPAIR TO VERTICAL STAB LH FWD DRAG ANGLE REF CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY AND FORM 337. SEE CONTINUE CARD FOR MORE DSDR SWIA202157332Drag Angle · crackedLH V/STAB TO FUSELAGE ATTACHMENT AFT DRAG ANGLE POSSIBLE CRACK. MARKED (C-CHECK RO 4/3/2021) REMOVED UNSERVICEABLE PARTS AND INSTALLED NEW AFT DRAG ANGLE ON LH V/STAB TO FUSELAGE IAW CRJ SRM 51-42-13-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, CRJ700 SDR SWIA202159500Drag Angle · crackedVERTICAL STAB TO FUSELAGE RH FWD DRAG ANGLE IS CRACKED AT REAR SPAR DATUM 67.5%. (C-CHECK RO 7/10/2021) REPAIRED RH VERTICAL STAB TO FUSELAGE FWD DRAG ANGLE IAW REO 670-55-31-018 REV A, DATED 2016-11-10. COMPLETED FORM 337 AND MARJOR REPAIR TASK CARD 51SDR SWIA2021071459465Drag Angle · crackedVERTICAL STAB TO FUSELAGE LH FWD DRAG ANGLE IS CRACKED AT REAR SPAR DATUM 67.5%. (C-CHECK RO 7/10/2021) REPAIRED VERTICAL STAB TO FUSELAGE LH FWD DRAG ANGLE IAW REO 670-55-31-018 REV A, DATED 2013-11-10. COMPLETED MAJOR REPAIR FORM 337 AND TASK CARD 51-SDR SWAA2021031653819Skate Angle · chafedFUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE IS CHAFFED; RT SIDE BS 1016 TO BS 1132 / REMOVED AND REPLACED SKATE ANGLE AT BS 1016 TO BS 1132 IAW SRM 51-40-02; DWG 148A8300 REV. A AND DWG 148A3590 57049U 25FEB21SDR SWAA2021022448930Angle · wornR/H UPPER FUSELAGE AFT FIN TO BODY INTERFACE CLOSURE ANGLE FWD SECTION HAS WEAR MARK. / REPAIRED FUSELAGE FIN TO BODY INTERFACE- CLOUSURE ANGLE R/H FWD SECTION PER REF B737-700 SRM 53-80-71-2R-6 REPAIR 6. STA 1026 RBL 12; WATER LINE 305.5SDR SWAA2021021543824Angle · wornLH FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE IS WORN TO STA 1016.00 THRU STA 1006.00 / REMOVED AND REPLACED L/H FUSELAGE FIN BODY INTERFACE CLOSURE ANGLE STA 1006 TO STA 1016 PER REF DWG 147A0030 AND B737-700 SRM 51-40-02-0G-0SDR SWAA2021021543825Angle · wornRH FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE IS WORN TO STA 1016.00 THRU STA 1006.00. / REMOVED ANDREPLACED R/H FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE STA 1006 TO STA 1016 PER REF DWG 147A0030 AND B737-700 SRM 51-40-02-0G-0SDR SWAA2021021547732Angle · wornLH FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE IS WORN TO STA 1030.00 THRU STA 1132.02. / REMOVED AND REPLACED L/H FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE STA 1030.00 THRU STA 1132.02 PER REF B737-700 SRM 51-40-02-0G-0 AND DWG #148A8300SDR IPXA2021012865006Stiffener · crackedINSPECTION TYPE: 2C 2164 BULKHEAD LOWER HORIZ STIFFENER IS CRACKED AT THE RT OUTBOARD END. REMOVED, FABRICATED AND REPLACED STIFFNER, IAW DWG AJC7001 AND SRM 51-31-01 & 51-35-01. (MINOR)SDR SWIA202156263Drag Angle · crackedLH VERTICAL STAB TO FUSELAGE AFT DRAG ANGEL HAS A POSSIBLE CRACK (C-CHECK) RO 2/13/2021 INSTALLED NEW LH VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE REF CRJ 700 SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01, SRM 51-42-13-001-001-A01 AND BOMBARDIER DWG BSDR VNAA2021010499911Drag Angle · crackedRT LOWER VERTICAL STAB TO FUSELAGE ATTACHMENT ANGLE BRACKET. HAS EVIDENCE OF A CRACK 1 1/2" LONG ON THE REPAIR DOUBLER.SDR REXA2021011200863Drag Angle · crackedVERTICAL STAB TO REAR FUSELAGE LT AFT DRAG ANGLE APPEARS TO BE CRACKED ON FWD SIDE. REPLACED VERTICAL STAB TO REAR FUSELAGE LT AFT DRAG ANGLE, IAW CRJ 900 SRM 54-40-11-001-001-A01, 51-42-22-001-001-A01, 51-42-13-001-001-A01
AND 51-42-21-001-001-A01.SDR SWIA202054897Angle · crackedRT FUSELAGE V-STAB CLOSING ANGLE ON FWD SIDE OF V-STAB REAR SPAR AT APPROXIMATELY FS 2541.5 HAS EVIDENCE OF CRACK. C-CHECK RO 12/28/2020. VERIFIED RT FUSELAGE V-STAB CLOSING ANGLE ON FWD SIDE OF V-STAB REAR SPAR AT APPROXIMATELY FS 2541.5 IS CRACKED, REF CRJSDR SWIA202054213Nut Plate · brokenBROKEN NUTPLATE ON LOWER LT DORSAL FIN MOUNTING FLANGE. C-CHECK RO 11/20/2020. REMOVED AND REPLACED BROKEN NUTPLATE ON LOWER LT DORSAL FIN MOUNTING FLANGE, REF SRM.SDR R61A2020110800736Fitting · scratchedREAR FUSELAGE FR 100 LT HORIZ STAB TO FUSELAGE FITTING HAS TOOLING DAMAGE. BLENDED IAW SRM 51-10-03 & FOUND WITHIN LIMITS, IAW SRM 51-75-16. (MAJOR)SDR R61A2020110800735Fitting · corrodedREAR FUSELAGE FR 100 RT HORIZ STAB TO FUSELAGE FITTING HAS TOOLING DAMAGE. REPLACED IAW SRM 51-40-08. (MAJOR)SDR A6WA202010207336Floor Support · corrodedRT PRESSURE FLOOR SILL ANGLE AT FS 507 AND RBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL ANGLE AT FS 507 AND RBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURESSDR IPXA2020071457784Support Channel · corrodedINSPECTION TYPE:3C LT AFT FUSELAGE TO HORIZ STAB FAIRING SUPPORT CHANNEL IS CORRODED. REMOVED, FABRICATED AND REPLACED CHANNEL IAW DWG AJC7898 AND SRM 51-31-00. (MINOR)SDR SIMA20200512001Drag Angle · crackedDURING HMBV INSPECTION, QA FOUND THE RH VERTICAL DRAG ANGLE FWD SECTION CRACKED-C/A-REMOVED AND REPLACED THE RH VERTICAL DRAG ANGLE FWD SECTION IAW EMB 145 SRM 51-40-02SDR ASOA2020052783044Drag Angle · crackedDURING C CHECK INSPECTION FOUND VERTICAL STABILIZER DRAG ANGLE CRACKED AT FASTENER ON RT SIDE JUST AFT OF PRESSURE BULKHEAD. MAINTENANCE REPAIRED IAW SRM 53-31-02 AND SRM 51-40-02.SDR SWAA2020041434130Skate Angle · wornUPPER FUSELAGE L/H FWD SKATE ANGLE IS WORN AS MARKED / REMOVED DAMAGE AT L/H FWD SKATE ANGLE IAW SRM 53-80-13-1A-1. ORIGINAL THICKNESS .063' AFTER REWORK. .053'; .010' MATERIAL LOSS; OUT OF LIMITS IAW SRM 53-80-13-1A-1 FIG 104. TOOL: 18173 DUE: 11/27/20. REMOVSDR SWAA2020041434131Skate Angle · wornUPPER FUSELAGE R/H FWD SKATE ANGLE IS WORN AS MARKED / REMOVED DAMAGE AT RH FWD SKATE ANGLE IAW SRM 53-80-13-1A-1. ORIGINAL THICKNESS .063'; AFTER REWORK .050' .013' MATERIAL LOSS OUT OF LIMITS IAW SRM 53-80-13-1A-1 FIG 104. TOOL: 18173 DUE: 11/27/20 REMOVED OSDR SWAA2020041420336Skate Angle · chafedRIGHT SKATE ANGLE HAS CHAFING IN MULTIPLE AREAS AT VERTICAL STAB BS1012 RBL15. / REMOVED AND REPLACED RIGHT SKATE ANGLE AT VERTICAL STAB FROM BS1006 TO BS1016 RBL15; P/N 147A3200-12; IAW SRM 51-40-02 AND DWG 417A0030. APPLIED TOP COAT AND ABRASION RESISTANT TESDR SWAA2020041420337Skate Angle · chafedLEFT SKATE ANGLE HAS CHAFING IN MULTIPLE AREAS AT VERTICAL STAB BS1012 LBL15. / REMOVED; LOCATED; DRILLED AND INSTALLED NEW SKATE ANGLE STA;1012 LBL15 PER SRM 51-40-05; SRM 51-40-02 AND DWG; 147A0030. 91195U 3-9-20SDR SWIA2020031049195Drag Angle · crackedRH FWD VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED. (C-CHECK) RO 3/6/2020 REMOVED DAMAGED ANGLE AND FILLER REF CRJ-900 SRM FABRICATED NEW PICES REF CRJ-900 SRM INSTALLED NEW FABRICATED PARTS REF CRJ-900 SRM RESTORED FINISH TO INSTALLED PARTS CRJ-
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