JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), 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 = '5300' 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 = '5300' 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 CALA2022011400142Frame · crackedLH FRAME 20 DOUBLE JOGGLE HOLE "A" CRACKED 5311-02726. WORK ACCOMPLISHED BY VTMAE EMP V935774. ON OR CYCLES, AND AT INTERVALS NOT TO EXCEED 5,900 FLIGHT CYCLES, REVISION OF ECRA 5311-02726. BEFORE THE ACCUMULATION OF 35,451 TOTAL AIRCRAFT FLIGHT THEREAFTER, PSDR CALA2022011400140Frame · corrodedFWD CARGO BLIGE AREA 42R REPAIR CORRODED FR 22-27 REMOVED EXISTING REPAIR BUT & TRIMMED SECTION OF REPAIR AND INST ALLED IN FWD CARGO PIT BETWEEN FR 26-27RT ON STRINGER 42RT IAW A 320 SRM 51-72-11 AND SRM 53-21-13-300-003SDR 2022FA0000021None · none2L EMERGENCY DOOR DAMPNER PRESSURE LOW,SDR IXXA2022011303Stringer · corrodedSTRINGER CORRODED BEYOND LIMITSSDR IXXA20220113101Stringer Splice · corrodedSTRINGER SPLICE CORRODED BEYOND LIMITS.SDR ABXA2022011222Skin · corrodedDURING AIRCRAFT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE DISCOVERED CORROSION ON THE INTERNAL SURFACE OF THE FUSELAGE SKIN(146T3261-1) AT BS 1085 BETWEEN S37L-S38L AND BETWEEN S37R-S38R. CORROSION WAS FOUND TO BE OUT OF LIMITS PER 767-300 SRM 53-60-01 ALLOWABLSDR MASA20220112071Intercostal · corroded"CORROSION ON INTERCOSTAL (2 EA'S) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT.
INTERCOSTAL (2 EA'S) BTW FS349.00 TO FS364.00 NEAR 27 WERE REPLACED PER CRJ/900 SRM 51-42-06-001-001-A0I & CRJ/900 SRM 51-42-21-001-001-A01 "SDR MASA20220112060None · damaged"FS 235 LH UPPER FRAME SECTOR CRACKED AT UPPER HOLE COMMON TO FUSELAGE SKIN. (PN 670-34133-3)
INSTALLED A NEW SERVICEABLE FS 235 LH UPPER FRAME SECTOR PN CC670-34133-9 IAW CRJ-900 SRM
51-42-06-001-001-A01, 51-40-001-001-A01 AND 51-42-21-001-001-A01. THIS ISDR MASA20220112059None · damaged"MULTIPLE FASTENER HOLES ARE DAMAGED ON BLO AFT STIFFNER AT FS. 202 BULKHEAD. (PN 670-34114-7SB)
INSTALLED A NEW SERVICEABLE FS 202 BULKHEAD AFT STIFFNER PN CC670-34114-7SB IAW CRJ-900 SRM
51-42-06-001-001-A01 AND 51-42-21-001-001-A01. THIS IS A PERM REPAISDR CALA2022011400127Plate · corrodedUPPER FLOOR BEAM WEB STA 1680-1686 LBL19-LBL29 HAS CORROSION. REMOVED AND REPLACED REPAIR DOUBLER AT STA 1680-1686 LBL19-LBL29 PER B757 SRM 53-60-51 REPAIR 2. WORK PERFORMED BY V921314,V9212 24. RII ACCOMPLISHED ON AIMS NR 0144 IS ACCEPTED.SDR IXXA2022011201Shear Tie · corrodedSHEAR TIE CORRODED OUT OF LIMITS.SDR A6WA202202168103Angle · corrodedCORROSION ON CABIN FLOOR SILL RHS AT FS349.00 AND RBL41, WL73.5. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGED FLOOR SILL SECTION AND REPLACED WITH REPAIR ANGLE P/N 601R31148-1355 TO MATCH ORIGINAL FLOOR SILL CUTOUT AT FS349.00 Ï¿½ FS375.00 AND RBL 41.SDR FDEA202201110229Doubler · unknownAT THE TIME OF RECORDS REVIEW THE FOLLOWING WAS IDENTIFIED ON MAJIOR REPAIR W/O 45404 SNRM N00072,DOCUMENTATION PROVIDED IS INCOMPLETE UNABLE TO VERIFY ALL PARTIAL WORK ACCOMPLISHED FOR THE REPAIR,JPF PAGE 1 NOT PROVIDED,PAGE 2 STARTS AT JPF ITEM13,WITH SDR SWIA202264182None · corrodedANGLE SUPPORT, CRAWLWAY FLOOR FS280.00 P/N CC670-34256-3 CORRODED (C CHECK RO 02-03-22) REMOVED AND INSTALLED NEW ANGLE SUPPORT, CRAWLWAY FLOOR FS280.00 P/N CC670-34256-3 REF CRJ 700 SRM 51-42-06-001-001-A01SDR CALA2022011200116Frame · crackedR1 WINDOW FRAM UPPER OUTBOARD CORNER HAS POSSIBLE CRACK.. REMOVED R1 WINDOW FOR MAINT REF AMM 56-11-11. ACCOMPLISHED STEPS 1.A THROUGH 6 OF AVO 9418. SEE ALSO LOG PAGE 7748414, C/W AVO 09418 STEPS B3 & B4 AS REQUIRED, R1 WINDOW OTBD POST UPPER CORNER HAS CRACKSDR CALA2022011200115Cleat · corrodedFWD CARGO BILGE HAS CORRODED CLEAT AT FR28 STR41R-42R. PER HAECO LCQ NR 9292476/30476 GENERATED BY V079881 REMOVED AND REPLACED CLEAT IN FWD CARGO PIT AT FR28 STR 41R-42RT IAW A320 SRM 51-72-11SDR SWIA202265314None · corrodedATENNA DOUBLER IS CORRODED BETWEEN F.S. 295 TO F.S. 310 STGR 26R TO 26L. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED ANTENNA DOUBLER BETWEEN F.S. 295 TO F.S. 310 STGR 26R TO 26L IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV. 38B DATESDR SWIA202265308None · corrodedH DOUBLER AT FS 533.00 STRINGER 26L IS CORRODED. (C-CHECK RO 4/9/2022) H DOUBLER AT FS 533.00 STRINGER 26L WAS REMOVED AND REPLACED AS REQUIRED IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-42-22-001-001-A01 REV.38B DATED 14 DEC 2020. MAJOR REPAIR TASK CASDR SWIA202265306None · corrodedDOUBLER CORRODED AT STGR 27 BETWEEN FS 485.00 AND FS 517.00. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED DOUBLER AT STGR 27 BETWEEN FS 485.00 AND FS 517.00 IAW CRJ 700 SRM 51-42-06-001-001-A01 REV. 38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-10SDR SWIA202265090None · corroded*AFT CARGO FLOOR SUPPORT ANGLE BETWEEN LBL 27 €“ 36, ATTACHED TO BULKHEAD 621.00 (C-CHECK RO 3/14/2022) REMOVED CORROSION AFT CARGO FLOOR SUPPORT ANGLE BETWEEN LBL27-36 ATTACHED TO BULKHEAD FS 621.00 REF CRJ200 SRM 51-21-06 / ORIGINAL MATERIAL .094 IAW SDR SWIA202265030None · corroded*CORROSION ON STOWAGE AFT OTBD FLOOR MOUNT DOUBLER LBL 36 (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM AFT OTBD FLOOR MOUNT DOUBLER LBL 36 REF: CRJ-200 SRM 51-21-06. FOUND TO BE IN LIMITS REF CRJ200 SRM 53-00-00, SEE CONTINUATION CARD FOR DETAILS OF WORSDR SWIA202264941None · crackedOBLIQUE ANGLES BETWEEN F.S. 621.00 AND F.S. 625.00, STRINGER 14L AND STRINGER 14R ARE CRACKED. (C CHECK RO 3/11/2022) REPLACE WITH NEW 2 EA OBLIQUE ANGLES BETWEEN F.S. 621.00 AND F.S. 625.00 ON STRINGER 14L AND 14R. ALL NEW HARDWARE INSTALLED. NEW OBLIQUE SDR SWIA202264837None · chafedEVALUATE 2 SKIN CHAFES AT STGR. 27 JUST FWD OF F.S. 977 (MARKED) (C-CHECK RO 3/11/2022) PERFORMED REPAIR TO EXTERNAL SKIN AT FWD AND AFT OF FS 977 AND STRINGER 27 REF REO 670-53-00-687 REV -- DATED 2022-02-07 (ALL STEPS COMPLIED WITH) AND REO 670-53-00-SDR YENA2022022500093Doubler · out of limitsDURING HEAVY MAINTENANCE, (E/A A21-1381-01) FUSELAGE/ XM ANTENNA STRUCTURAL DEMOD/ OVERSIZED DOUBLER HOLES FR 54-55 @ STGR 1L-1R - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR SWIA202264154None · damaged9 INCH CREASE FOUND ON FUSELAGE SKIN AT F.S 319-333 BETWEEN STRINGER 25L-26L (C CHECK RO 02-03-22) REPAIR TO FUSELAGE SKIN BETWEEN FS310.00 TO FS349.00 AND STR 24 & 27 LHS . COMPLIED WITH REO 670-53-21-2218 REV -- DATED 2022-01-17. COMPLIED WITH TASK CARSDR SWIA202264086None · corrodedCORROSION ON LH FLOOR DOUBLER AROUND LH FORWARD WINDSCREEN FLOOR MOUNT FITTING AND ALONG THE FORWARD EDGE BETWEEN FRAMES 19 AND 20. (C CHECK RO 01/28/2022) / REMOVED AND REPLACED LH FLOOR DOUBLER AROUND LH FORWARD WINDSCREEN FLOOR MOUNT FITTING AND ALOSDR SWIA202264085None · corrodedCORROSION ON CENTER SHEAR PANEL AT FR 87-88 (C CHECK RO 01/28/2022) REMOVED AND REPLACED CENTER SHEAR PANEL AT FR 87-88 REF EMB SRM 51-40-08SDR SWIA202263827None · gougedEXTERNAL R/H FUSELAGE GOUGED DURING MAINTENANCE BETWEEN FRAMES 89-90 AND STRINGERS 11R-13AR AS MARKED. (C-CHECK RO 1/15/2022) EAMS WARRANTY. REPAIRED GOUGE ON EXTERNAL R/H FUSELAGE BETWEEN FRAMES 89-90 AND STRINGERS 11R-13AR BY MEANS OF BLENDING OUT DAMSDR FXGA202201102201None · noneCORRODED ZEE CHANNELS AROUND COCKPIT WINDSHIELD. TO REPLACE CORRODED ZEE CHANNELS AT THE BOTTOM CORNERS OF THE CENTER WINDSHIELD. REMOVE CORRODED ZEE ANGLES, AND INSTALL NEW ONES FOLLOWING STANDARD PRACTICES PER DC-9/MD-80 SRM. INSTALL NEW PARTS WITH SAME TYPESDR JJBA20220110014Not Reported · not reportedREAR FUSELAGE SKIN HAS CORROSION UNDER RAT #2 ANTENNA BASE. CUT OUT DAMAGE ON EXTERNAL SURFACE OF FUSELAGE SKIN AT RAT #2 ANTENNA LOCATION AND INSTALLED REPAIR DOUBLER, FILLER AND SHIMSDR CALA2022011200110Cleat · corrodedFWD CARGO BILGE HAS CORRODED CLEAT @ FR26 STR44-STR43L. PER HAEC O LCQ NR 9292464/30464 GENERATED BY V079881 REMOVED AND REPLACED CLEAT IN FWD CARGO FR 26 STR 44-43LT IAW A3 20 SRM 51-72-11SDR CALA2022011200109None · corrodedFWD CARGO TORSION BOX UPPER SKIN HAS CORROSION AT MULTIPLE FASTE NER HOLES. PER HAECO LCQ NR 9292518/30518 GENERATED BY V079881 REMOVED AND REPLACED FWD CARGO TORSION BOX SKIN IAW A320 ARM 51- 72-11 INSTALLED FWD CARGO PROFILE PANEL IAW A320 SRM 51-22-11SDR CALA2022011200108None · corrodedFWD CARGO BILGE FR28 STR43R-STR42R HAS CORRODED CLEAT. PER HAECO LCQ NR 9292470/30470 GENERATED BY V079881 REMOVED AND REPLACED CLEAT IN FWD CARGO FR28RT BETWEEN 43R-42R I AW A320 SRM 51-72-11SDR HALA2022011100010Skin · damagedDURING PDC FOUND BOTTOM TAIL AREA FUSELAGE SKIN DAMAGE AND AFT GALLEY DRAIN MAST DAMAGE. DAMAGE AREA: FRAME 61-70, STRINGER 42LH - 40 RH. 176" LONG 22" WIDE // REPAIRED DAMAGE TO BOTTOM TAIL AREA AT FRAME 61-70 STRINGER 42LH-40RH AS PER AIRBUS WOTD: M-308924-ESDR IXXA2022011100001Beam · corrodedSUPPORT BEAM CORROSION AT APPROX. STATION 588-595 LBL5 - LBL 14SDR EE4Y202215149Fitting · crackedDURING SPECIAL DETAILED INSPECTION ON WINDSHIELD CENTRAL LOWER NODE WERE FOUND CONTINUITY FITTINGS WITH CRACKS. THE CRACK WAS REPAIRED IAW YO CONTINUITY FITTINGS REPLACEMENT AND REPAIR INSTRUCTIONS R53112919 ISSUE D.SDR IXXA2022021112Web · corrodedFABRICATE NEW PRESSURE DECK AT STA610~632, LEFT SIDE. CORRODEDSDR IXXA2022021111Web · corrodedFABRICATE NEW PRESSURE DECK AT STA1263, LBL30 CORRODEDSDR IXXA2022021110Support Web · corrodedFABRICATE NEW PRESSURE DECK AT STA522~544, LBL24~40 IN FLC. CORRODEDSDR IXXA2022012608Support Plate · corrodedFABRICATE NEW PRESSURE DECK AT STA1411, LBL24~LBL44 IN ALCSDR MASA20220109066Stringer · corroded"CORROSION ON STGR 27 BTW FS310.00 TO FS319.70 AT MAIN AVIONICS COMPARTMENT.
STGR 27 BTW FS310.00 TO FS319.70 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01"SDR CALA2022011000083None · corrodedB767-53-3-7025 FWD CARGO COMPT - FLOOR BEAM UPPER SURFACE CORROSION CRACK AT STA632 BTN LBL30"-LBL32" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF516482 AND ORIGINATED BY EMP V896820 FWD CARGO COMPT STA 632 BETWEEN LBL 43 AND RBL 43 FLOOR BEAM UPPER CHORD REPLACSDR IXXA202201090001Intercostal · bentREMOVED AND REPLACED INTERCOASTAL AT STATION 592 BETWEEN RBL 4-13SDR A6WA202201088168None · crackedTWO EACH CRACKS FOUND AT PRESSURE FLOOR SUPPORT STRUCTURE AT FS 484.00 & RBL 36 AS FOLLOW: (P1) 1.00"L CRACK ON LOWER O/B CORNER OF INTERCOSTAL DWG #601R31171-15 AND (P2) .400"L CRACK ON UPPER SIDE OF BEND RADIUS ON CLIP DWG #601R31171-09. **************AIRCSDR SWIA202264697None · cracked*LEFT OVERWING EMERGENCY EXIT DOOR €“ TOP OF THE DOOR FRAME IS CRACKED AT THE AFT BAYONET. (MARKED) (C CHECK RO 02/25/2022) REPAIRED LEFT OVERWING EMERGENCY EXIT DOOR €“ TOP OF THE DOOR FRAME AT AFT BAYONET / REF REO 670-52-21-078 REV --, 2022-01-24 / CSDR SWIA202264078None · dentedDENT OIL CANNING ON RH FUSELAGE, FWD. OF FRAME 94 AND ABOVE STRINGER 23R, AT REAR FUSELAGE ACCESS DOOR. (C CHECK RO 01/28/2022) REPAIRED DENT ON RH FUSELAGE, FWD. OF FRAME 94 AND ABOVE STRINGER 23R, AT REAR FUSELAGE ACCESS DOOR. REF SRM 53-30-01/REPAIR12P.SDR MASA20220108070None · corroded"CORROSION ON SPLICE OF STGR25LH, FS333.00 AT MAIN AVIONICS COMPARTMENT.
SPLICE OF STGR25LH, FS333.00 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 & CRJ900 SRM 51-42-21-001-001-A01 "SDR FDEA202201080027Stiffener · crackedEMPENNAGE - TAILCONE RIGHT HAND SIDE LOWER GUIDE PIN RECEPTACLE BRACKET STIFFENER AT RIGHT HAND SIDE STATION 2163.685 Z = 20.000 X =-30.00 FOUND CRACK. EMPENNAGE - TAILCONE RIGHT HAND SIDE STATION 2163.685 Z = 20.000 , X = -30.00 CRACKED LOWER GUIDE PIN RESDR GTIA2022011036214None · nonePER WEEKLY CHECK FOUND L1 DOOR EMER ASSIST BOTTLE REQ SERVICING. -SERVICED L1 DOOR EMER ASSIST BOTTLE IAW AMM 52-10-00.SDR CALA2022011000082Intercostal · crackedR/H FR 16 DOORSTOP FITTING #7 HAS CRACK INDICATION NOTED IN HOLE #1 & #3 TO READ AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART AFT REACHES 39,510 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAAT INSPE R." REFF VT MAE NRC 0020970 FOR WORK PERFORMED. 2A OF LAT
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