JASC 5340
Service difficulty reports · 22,407
Reports filed under 5340 · Fuselage Main, 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 = '5340' 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 = '5340' 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 SWIA2021072159616Bracket · cracked* R/H MLG WHEEL WELL HAS BRAKE PRESSURE TRANSDUCER MOUNTING BRACKET CRACKED. (C-CHECK RO 7/18/2021) REMOVED AND REPLACED RH MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER BRACKET REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-41-00 AND DWG 601R75261, REV-N. NO LEAKS.SDR SWIA202159615Bracket · cracked* L/H MLG WHEEL WELL HAS BRAKE PRESSURE TRANSDUCER MOUNTING BRACKET CRACKED. (C-CHECK RO 7/18/2021) REMOVED AND REPLACED LH MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER BRACKET REF CRJ200 SRM 51-42-06, CRJ 200 SRM 51-41-00 AND DWG 601R75261, REV-N. NO LEAKSSDR SWAA2021061771014Attach Angle · crackedLEFT AC BAY HAS CRACK AT UPPER VAPOR BARRIER ATTACH ANGLE STA 663 LBL 8 SEEN THRU AC BAY. 8-19 ; / APPLYED BMS 3-23 OR EQUIVALENT CORROSION INHIBITIN COMPOUND TO REPAIR AREA [COR- BAN 35 ] IAW B-737-700 SRM 51-20-01;ACCOMPLISHED FUEL LEAK CHECK ON REPAIR AREA SDR MASA2021050900106Balance Weight · bird ingestionOVERWEIGHT LANDING (EMERGENCY DECLARED) + BIRD STRIKE INTO NO. 1 ENGINE (EMRGENCY DECLARED)SDR SWIA2021062358954Stringer Clip · corrodedCLEAT CORRODED AT FS 333.00, STGR 20R INTERCOSTAL, FWD SIDE UPPER OF FRAME. (C-CHECK RO: 6/20/21) / INSTALLED NEW CLEAT AT FS349 STGR 20R INTERCOSTAL REF DRAWING SH670-31950 REV. V AND CRJ-700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY. SEE COSDR SWIA202158953Cleat · corrodedCLEAT CORRODED AT FS 349.00, STGR 20R INTERCOSTAL, FWD SIDE UPPER OF FRAME. (C-CHECK RO: 6/20/21) / INSTALLED NEW CLEAT AT FS349 STGR 20R INTERCOSTAL REF DRAWING SH670-31950 REV. V AND CRJ-700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY.SDR SWIA2021062358952Cleat · corrodedCLEAT CORRODED AT FS 319.70, STGR 20R INTERCOSTAL, AFT SIDE UPPER OF FRAME. (C-CHECK RO: 6/20/21) / REMOVED AND INSTALLED CLEAT AT FS319.70, STGR 20R INTERCOSTAL REF DRAWING SH670-31950 REV. V AN CRJ-700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SSDR SWAA2021081370121Strap · corrodedDOT# A45-014; AFT CARGO PIT DOOR CUTOUT; INTERCOSTAL LOWER ATTACH STRAP HAS CORROSION; WL: 156; RBL: 19; STA: 787+12. ; / [01] REMOVED STRAP FROM STATION 787+12 TO REMOVE CORROSION IAW B737 SRM 51-40-02; [02] REMOVED CORROSION ON STRAP AT STATION 787+12 ORIGINSDR SWAA2021081370126Attach Angle · corrodedDOT# A45-027; AFT CARGO PIT; RH INTERCOSTAL UNDER Z-ANGLE HAS CORROSION; WL:156; RBL:22; STA: 747-767. ; / [01] REMOVED CORROSION ON R/H INTERCOSTAL AT STATION 747-767 ORIGINAL THICKNESS .032 REMOVED .007 REMAINING .025 INTERCOSTAL WAS FOUND TO BE OUT OF LIMITSDR SWAA2021060470125Attach Angle · corrodedAFT CARGO PIT; RH ATTACH ANGLE ON LOWER SURFACE OF FLOOR SHIELD HAS CORROSION; WL:156; RBL:22; STA: 767+4. ; / REMOVED CORROSION ON ATTACH ANGLE AT STATION 767+4 ORIGINAL THICKNESS .050 VERIFIED BY TOOL 36649 DUE 8-4-21MATERIAL REMOVED .012 REMAINING .038 ANGLSDR SWAA2021060470122Attach Angle · crackedDOT# A45-015; AFT CARGO PIT; RH Z-ANGLE; LOWER SIDE ATTACH CLIP IS CRACKED IN RADIUS; WL: 155; RBL: 21; STA: 727+5. ; / CLIP REMOVAL & INSTALLATION ACCOMPLISHED ON FAULT TTG8Q004YWGX; FABRICATED NEW CLIP P/N 146A7505-4; ON SHOP W/O 42136-1600-0004. LOCATED ANDSDR AALA202106022880Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON CENTER FITTING LOCATED BETWEEN FR66 AND FR68 AT S23R. REPLACED FITTING PER SRM 51-72-11-911-001 AND DWG D53480505.SDR AALA202106029195Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORRODED AREA ON CENTER FITTING, MEASURING L=3.104 INCH, W= 0.310 INCH, D=0.069 INCH, AT FR66 TO FR68 AND STR 23L. REPLACED CENTER FITTING IAW SRM A321 51-42-11-801 AND DRAWING D53480505.SDR ASAA2021050334904Fitting · corrodedIN AFT WET AREA, CORROSION FOUND AROUND 2 EA. TOTAL LAVATORY FLOORSTRUCTURE FITTINGS, 1 EA. AT STA. 947, LBL 25, AND 1 EA. AT STA. 916, LBL 52. AREAS MARKED IN RED. GROUNDED - YES. CORROSION FOUND TO BE OUT OF LIMITS REF B737-800 SRM 53-70-51. ORIGINAL MAT'L TSDR SCNA20210514055Mount · crackedPSU MOUNT CRACKED AT ATTACH POINTS TO FRAME BRACKET STA 727D S8L. REMOVED AND REPLACED PSU MOUNT AT ATTACH POINTS TO FRAME BRACKET STA 727D S8L PO # 822467 IAW SRM 51-40-02-0G-0.SDR ASAA2021050334786Transition Panel · corrodedAFT CARGO COMPARTMENT RIGHT SIDE TRANSITION PANEL SHOWS EVIDENCE OF CORROSION FROM STA:727 TO STA:767. GROUNDED - YES. REMOVED DAMGE ON R/H TRANSITION PNL FROM STA 727 - 767 ORIG. THICKNESS 0.040 PER BAC 1496-377, REMOVED 0.009, MATL REMAINING 0.031 AND FOUND SDR FDEA202105031082Fitting · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO 6-5710-E0342809 B P2 STEP 5.D-5.E, TITLE: WINGS - CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM SDR DU4R2021050300068Attach Fitting · corrodedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND R/H MLG SUPPORT BEAM STABILIZER ATTACH FITTING HAS FRETTING ON BOTH LUG FACES. S/O 660006 N/R 39463SDR SWIA202158133Bracket · damagedCARGO DOOR SURROUND STRUCTURE, FWD TRACK "CLIP" TO BEAM DAMAGED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR SURROUND STRUCTURE FWD TRACK TO BEAM "CLIP"/BRACKET WITH REFERENCE TO SRM 51-42-21. COMPLETED 51-900-1003-SKY AND M-337.SDR FDEA202104291067Fitting · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "C" HOLE FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0361325 P1, TITLE: WINGS - BASIC WING STRUCTURE- CRACK HOLE C AT FR47 LHS DURING SB57-6121 EMSDR CALA2021043000579Fitting · crackedSHEAR FITTING AT STA540 RBL40.87 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 40.87. IAW B73 7-700 SRM 51-60-02 ECRA 5714-01208. REV ORIGINAL.SDR CALA2021043000578Fitting · crackedSHEAR FITTING AT STA540 RBL54.60 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 54.60. IAW SRM 51-40-02 AND ECRA 5716-01219 REV ORIGINAL.SDR CALA2021043000577Fitting · crackedSHEAR FITTING AT STA540 RBL54.60 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 54.60. IAW SRM 51-40-02 AND ECRA 5716-01219 REV ORIGINAL.SDR CALA2021043000582Fitting · crackedSHEAR FITTING AT STA540 RBL6.14 IS CRACKED-N/R6 227155 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 6.14 IAW B737- 700 SRM 51-40-02 AND ECRA 5714-01208. REV ORIGINAL.SDR CALA2021043000581Fitting · crackedSHEAR FITTING AT STA540 RBL15.04 IS CRACKED-N/R 6227154 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15.04 IAW B737 -700 SRM 51-40-02 AND ECRA 5714-01209 REV ORIGINAL.SDR CALA2021043000580Fitting · crackedSHEAR FITTING AT STA540 RBL32.40 IS CRACKED-N/R 6227153 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 32.40 IAW B737 -700 SRM 51-40-02 ECRA 5714-01209 REV ORIGINAL.SDR CALA2021043000576Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STA540 LBL6.14 IS CRACKED-N/R 6227150 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 6.14 IAW B737- 700 SRM 51-40-02 AND ECRA 5714-01209 REV ORIGINAL.SDR CALA2021043000575Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STA540 LBL15.04 IS CRACKED-N/R 6227149 REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 LBL 15.04. IAW B737-700 SRM 51-40-02 AND ECRA 5714-01208. REV ORIGINAL. SS FR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651 4SDR CALA2021043000574Fitting · crackedSHEAR FITTING AT BS 540, LBL 32.4 WAS CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02 AND ECRA 5714-01208. REV ORIGINAL.SDR CALA2021043000573Fitting · crackedSHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02 AND ECRA 5714-01209.SDR CALA2021043000572Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STA 540 LBL 54.60 IS CRACKED-622 7146 REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02 AND ECRA 5716-01208.SDR AALA202104299007Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: FOUND 1 INCH CRACK IN VAPOR BARRIER TO CENTER FUEL TANK ATTACH ANGLE. INSTALLED SPLICE REPAIR IAW SRM 57-10-10-2R-5.SDR AALA202104299006Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: FOUND 1 INCH CRACK IN VAPOR BARRIER TO CENTER FUEL TANK ATTACH ANGLE. INSTALLED SPLICE REPAIR REF SRM 57-10-10-2R-5.SDR DALA2021042902467Tee Fitting · crackedSHIP 665 RH STA 1640 STR.14 LWR T CLIP I/B HOLE CRACK INDICATIONS. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:5311-01218-01B/002 00005 WP: 2273186 COMPLY WITH ERA 590841-14AD REV A. (1794416)SDR SWAA2021060367729Attach Angle · corroded***CORROSION*** ON ATTACH ANGLE AT AFT CARGO BAY BS767 LBL5 WL151. / REMOVED AND REPLACED ATTACH ANGLE AT AFT CARGO BAY BS767 LBL5 WL151. IAW B-737-700; SRM 51-40-02; DWG# 146A7810 WITH P/N 146A1320-13. 59202U 06MAY21SDR SWAA2021060367730Attach Angle · corroded***CORROSION*** ON ATTACH ANGLE AT AFT CARGO BAY BS727E RBL5 WL151. / REMOVED AND REPLACED ATTACH ANGLE ITEM BAC1490-2815 LOT # 1455934-1 AT AFT CARGO BAY 727E RBL5 WL151 IAW SRM 51-40-02 AND DRAWING 146A7810 59861U 07MAY21SDR SWAA2021060367731Attach Angle · corroded***CORROSION*** ON ATTACH ANGLE AT AFT CARGO BAY BS727D+4 LBL5 WL151. / REMOVED & REPLACED ATTACH ANGLE ACB BS 727D+4; LBL 5; WL 151 WITH BAC 1493-672 LOT 1458580; P/N 146A7734-U PER DWG 146A7734; SRM 51-40-02-0G-0.- 60214U 12MAY21SDR SWAA2021060367740Attach Fitting · corroded***CORROSION*** ON STINGER ATTACH FITTING AT AREA AFT OF ACB BS1011 RBL25 WL193.MARKED / REMOVED AND INSTALLED NEW FITTING ITEM HFAB53-FT5-002 FROM BAC1303-101649 LOT # 1411422-1 PER JOB NUMBER 539321 AND CUSTOMER RO NO 823013 SWA LOCATED AND DRILLED IAW SRM 5SDR SWAA2021060367742Attach Angle · corroded***CORROSION*** ON INTERCOSTAL ATTACH ANGLE AT AREA AFT OF ACB BS947 S-20R WL187. MARKED / REMOVED AND REPLACED T-CLIP AT STA. 947 S-20R WL187 PER SRM 51-40-02; 51-40-05; SRM 51-20-01; SOPM 20-41-02 AND DWG; 147A8801 91195U 5-8-21SDR AALA202105149633Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON BORE OF FORWARD LUG OF AFT DOOR LOCK FITTING, MEASURING DIAMETER= 1.289 INCH AND W= 0.641 INCH, BETWEEN FR26 AND FR27 AT STR 39R AT FORWARD CARGO COMPARTMENT DOOR. REPLACED LOCK FITTING REF A320 SRM 51-41-11-801SDR AALA202105141934Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON BORES OF FORWARD LUG OF AFT DOOR LOCK FITTING, MEASURING DIAMETER = 1.251 INCH AND W = 0.646 INCH, AT FR27 AND STR 39. REPLACED LOCK FITTING LOCATED FR27 FORWARD CARGO COMPARTMENT DOOR REF A320 SRM 51-41-11-801 SDR AALA202105139904Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON BORE OF FORWARD LUG (DIAMETER: 1.269 INCHES, WIDTH: 0.650). REPLACED LOCK FITTING BETWEEN FR 27 AND FR 28 FORWARD CARGO COMPARTMENT PER SRM 51-42-11-801.SDR CALA2021042800553Fitting · crackedPER NR 9294160/40160 AD 2018-03-12: R2 DOOR FRAME 68 STOP FITTIN G NO. 1 INBOARD LOWER HOLE IS CRACKED IN THE WEB AT 6:OO. "REPAI R BEFORE NEXT FLIGHT". GENERATED BY V061633 ACCOMPLISHED THE FINAL REAM OF THE R-2 DOOR FRAME 68 DOOR STOP FITTING #1 INBOARD LOWESDR AALA202105069020Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK RIGHT CENTER WINDOW POST CONTINUITY FITTING CRACKED AT FR2 AND -Y20. REPLACED CONTINUITY FITTING PER EO 5319Y017 AND REPAIR DRAWINGS R53112919 AND R53112958.SDR AALA202105069019Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK LEFT CENTER WINDOW POST CONTINUITY FITTING CRACKED AT FR2 AND Y20. REPLACED CONTINUITY FITTING PER EO 5319Y017 AND REPAIR DRAWINGS R53112919 AND R53112958.SDR ASAA2021042334842Attach Angle · corrodedAFT CABIN AREA SHEAR PLATE ATTACH ANGLE HAS CORROSION AT FR69 RBL48. GROUNDED - YES. REMOVED SHEAR PLATE ATTACH ANGLE AND REPLACEC WITH NEW ANGLE P/N D5347112520100 IAW A320 SRM 51-44-11 AND 51-72-11.SDR REXA2021051900361Attach Angle · corrodedRH ELECTRICAL CONNECTOR PLATE ATTACHMENT ANGLE HAS NUMEROUS OVERSIZED HOLES & CORROSION AND REQUIRES REPLACEMENT. P/N: CC670-51876-3. LOCATED @ FS 280 CROSSBEAM - LOCATED, DRILLED, INSTALLED AND TOPCOATED SERVICEABLE RH ATTACH ANGLE IAW CRJ 700 SRM 51-40-11-00SDR SWIA202158655Attach Angle · corrodedCORROSION FOUND AT PAX DOOR ON FLOOR BOARDS' FWD ANGLE ATTACTMENT APPROX FS310.00 & STGR18L. (C-CHECK RO 6/04/2021) REPLACED WITH NEW PAX DOOR SILL FWD CAP ANGLE REF. CRJ700 SRM 51-42-06-001-001-A01 AND DRAWING SH670-31810 REV AE / . COMPLIED WITH SKYWESDR 2A6R2021042060106Attach Angle · corrodedDURING 1000 HOUR INSPECTION, FOUND 3 ANGLES THAT ATTACH CONTROL POST TO FLOOR CORRODED. AFTER REMOVING THE ANGLES, FOUND THAT THE FLOOR UNDER THE ANGLES WAS ALSO CORRODED.SDR SWIA2021062859160Attach Angle · corrodedATTACH ANGLE ON FRAME ON LH SIDE FS1047, AFT SIDE OF AFT BAG BAY DOOR LOWER SIDE ABOVE SILL CORRODED. (C-CHECK RO 6/22/2021) REMOVED ATTACH ANGLE ON LOWER FS1047 ABOVE CARGO BAY LOWER SILL. ATTACH ANGLE HAS 100% EXFOLIATION REPLACE ANGLE. REF: CRJ900 SR
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