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 CALA2022090502269Skin · crackedFR35, STR. 30LH HOLE DAMAGE AND HOLE #2 CRACK INDICATIONS DURING NDT INSPECTION. INSPECTION REQUIREMENTS PER PART 2B OF THE LATEST REVISION OF EC FLIGHT CYCLES OR 121735 TOTAL FLIGHT HOURS (WHICHEVER COMES FIRS 9600 FLIGHT CYCLES OR 19200 FLIGHT HOURS (WHICHEVSDR CALA2022090502268None · crackedL/H SIDE PRESSURE PANEL BETWEEN FR 35-36 HOLES 13, 16, 22, 23, A ND 24 HAVE CRACK INDICATIONS. OF EC/RA 5331-02956. ON OR BEFORE FEBRUARY 28, 2023 PERFORM AN INSPECTIONOF THE LH FR 36 PRESSURE PANEL HOLES AREA PER PART 2 OF THE LATEST REVISION DIP 53-DIP NO INSDR CALA2022090502267Door Sill · corrodedCORROSION ON R2 DOORSILL FR68. AS NOTED ON LTPR NR#5001169410- 0020. PERFORMED REPAIR ON R2 DOOR SILL BEAM AT FR68 IAW SRM 53-41-14-300-001 REPAIR PRINCILE 7, CAT "A" MAJOR REPAIR WITH NO ADDITIONAL REQUIREMENTS REFER TO PREVIOUS SIGN OFF FOR WORK PERFORMED. WSDR SWIA202266417None · damagedTRANSFER FROM EAML 983376 : REF EAML 983241 FOR RAMP DAMAGE TO FWD FUSELAGE SKIN BETWEEN FRAMES 21-22 AND STRINGERS 16L-17L, FOUND SKIN PUNCTURE / DENT TO BE DETERMINE OUT OF LIMITS PER ERJ 175 SRM 53-10-01 MEASURING DEPTH .1614" (4.10MM), LENGTH 1.403", WIDSDR CALA2022090502258Seat Track · corrodedFWD CABIN, FR16, Y1292, SEAT TRACK CORRODED. REMOVED CORROSION ON TRACK ASSY Y1292, FOUND OUT LIMITS IAW SRM 53-11-14-283-007. REMOVED AND REPLACED TRACK ASSY ON MAIN CABIN FR12 TO FR24 Y1292 IAW SRM 51-42-11/001. EMP#: V935975 W/C: 3729 2 STA: ST ENG BFMSDR CALA2022090502257Panel · damagedRH FR 35-36 I/B PRESSURE PANEL HOLE HAS REJECTABLE DAMAGE INDICATION AT 6 O-CLOCK FACING UPWARD. REVISION OF EC/RA 5331-02954. ON OR BEFORE FEBRUARY 28, 2023 PERFORM AN INSPECTION OF THE FR 36 RH PRESSURE PANEL HOLE #9 AREA PER PART 2 OF THE LATEST DIP 53-DIP SDR VNAA202209029949Stringer · corrodedCORROSION ON STRG 26LH BTW FS. 280/265 AT FWD AVIONICS COMPARTMENT.SDR VNAA202209029948Splice · corrodedCORROSION ON SPLICE AT FS333 & STGR 25RH, FWD EQUIPMENT BAY.SDR VNAA202209029947Stringer Splice · corrodedCORROSION ON SPLICE AT FS333 & STGR 26RH, FWD E/E EQUIPMENT BAY.SDR VNAA202209029946Stringer · corrodedCORROSION ON STGR 24RH BTW FS477.4-FS501, FWD CARGO COMPARTMENTSDR VNAA202209029945Splice · corrodedCORROSION ON SPLICE AT FS477.4 & STGR 24RH, FWD CARGO COMPARTMENTSDR VNAA202209029944None · noneSCRATCHES ON LH SIDE SEAT RAIL STRUCTURE BETWEEN FS669 TO FS785, SCRATCHES AND CORROSION BETWEEN FS785 TO FS861 AND SCRATCHES BETWEEN FS861SDR VNAA202209029943None · noneSCRATCHES ON RH SIDE SEAT RAIL STRUCTURE BETWEEN FS669 TO FS785, SCRATCHES AND CORROSION BETWEEN FS785 TO FS861 AND SCRATCHES BETWEEN FS861SDR VNAA202209029942Plate · corrodedCORROSION ON NET ATTACHMENT PLATES (3 EAS) ON AFT BAGGAGE BAY DOOR CUTOUT STRUCTURE BETWEEN FS=1000.00 AND FS=1047.00.SDR VNAA202209029941None · noneCRACK ON CLIP AT AFT BAGGAGE BAY DOOR CUTOUT STRUCTURE BETWEEN FS=1047.00/FS=1051.30 AND STGR 7LH.SDR VNAA202209029950Web · noneCORROSION ON FLOOR PROTECTOR WEBS AT FUSELAGE LOWER FRAME SERVICE DOOR
CORROSION ON FLOOR PROTECTOR WEBS WAS REMOVED PER CRJ/700 SRM 51-21-06-001-001-A01 AND MEASUREMENT WAS PERFORMED ON FLOOR PROTECTOR WEBS
(4EA'S) WITH ORIGINAL THICKNESS IS 0.063 AND MINIMSDR VNAA202209029951None · noneAFTER REMOVAL OF RH/LH MLG´S PISTON AXLE, CORROSION ON THREADS OF CYLINDER ASSY RH/ LH MLG´S}. (AYP)
THREADS OF CYLINDER ASSY AT LH MLG WAS CLEANED PER CRJ700 SRM 51-26-00-001-001-A01 AND AFTER CLEANLINESS, AREA WAS INSPECTED PER CRJ-700 SRM
51-11-00-001-001SDR VNAA202209029952Skin · corrodedHIDDEN DAMAGE AFTER SEALANT REMOVAL ON UPPER BEACOM, SCRIBE LINES WAS FOUND ON FUSELAGE SKIN. (REF. SURROUND BEACOM SEATTLEMENT AREA).
DAMAGED FUSELAGE SKIN. (REF. SURROUND BEACOM SEATTLEMENT AREA) WAS REPAIRED PER EA 22-C7-53-1002 REV. IRSDR VNAA202209029953None · corrodedHIDDEN DAMAGE IN REF NRC:00192: AFTER REMOVAL TO SEAL OF FWD BAGGAGE BAY DOOR{ CORROSION WAS FOUND ON FWD/AFT LOWER PLATE OF FWD BAGGAGE
BAY DOOR.}
FWD/AFT LOWER PLATE OF FWD BAGGAGE BAY DOOR WERE REPLACED PER CRJ 700 SRM 51-42-06-001-001-A01SDR VNAA202209029954None · corrodedCORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA FS= 349 AT MAIN AVIONICS COMPARTMENT. (E/E)
NEW INTERCOSTAL (2EAS) STA.310 AT 319.70 AND 319.70 AT STA.349 WERE INSTALLED PER CRJ-700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.SDR VNAA202209029955None · corrodedCORROSION ON INTERCOSTALS (3EAS) BETWEEN FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT.
INTERCOSTALS (3EAS) BETWEEN FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT
WERE REPACED PER CRJ 700 SRM 51-42-20-001-001-A01 AND SRM 51-42-06SDR VNAA202209029957Skin · gougedNICK & GOUGE ON FUSELAGE SKIN BTW FS1031-FS1051 & BTW STGR 24R-26R. (2 LOCATIONS).
CORRECTIVE ACTION:
NICK & GOUGE ON FUSELAGE SKIN BTW FS1031-FS1051 & BTW STGR 24R-26R,REPAIR PER EA 22-C7-53-0951 REV. IRSDR VNAA202209029956Access Panel · corrodedCORROSION AT HINGE OF ACCESS PANNEL 196ER
CORRECTIVE ACTION:
HINGE OF ACCESS PANNEL 196ER WAS REPLACE PER CRJ-700 SRM 51-41-02-001-001-A01SDR VNAA202209029924None · corrodedCORROSION ON FLOOR BEAM 9RBL IN STA. FS= 977 TO FS= 1098 AT AFT BAGGAGE BAY
FLOOR BEAM 9RBL IN STA. FS= 977 TO FS= 1098 AT AFT BAGGAGE BAY WAS REPAIRED PER CRJ 700 SRM 53-00-41-201-001-A01SDR VNAA202209029923None · corrodedCORROSION ON FLOOR BEAM 27LBL IN STA. FS= 977 TO FS= 1098 AT AFT BAGGAGE BAY
FLOOR BEAM 27LBL IN STA. FS= 977 TO FS= 1098 AT AFT BAGGAGE BAY WAS REPAIRED PER CRJ 700 SRM 53-00-41-201-001-A01SDR VNAA202209029922None · corrodedCORROSION ON FLOOR BEAM 9LBL IN STA. FS= 977 TO FS= 1098 AT AFT BAGGAGE BAY.
AREAS ON FLOOR BEAM BETWEEN FS=977 TO FS=1005.5 AND FS=1037.5 TO FS=1098 ON 9LBL WAS CLEANED PER CRJ-700 SRM 51-26-00-001-001-A01 AFTER CLEANLINESS,
AREA WAS INSPECTED PER CRJ-700 SSDR VNAA202209029921None · corrodedCORROSION ON LOWER ANGLE OF WING-TO-FUSELAGE-FAIRING AT FS STA 939
DAMAGED LOWER ANGLE OF WING-TO-FUSELAGE-FAIRING AT FS STA 939 WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01.SDR VNAA202209029920None · corrodedCORROSION ON SETTLEMENT AREA COVER BY 173BZ AND 174BZ ACCESS PANELS ON MLG WHEEL WELL.)
AREA ON SETTLEMENT AREA COVER BY 173BZ AND 174BZ ACCESS PANELS ON MLG WHEEL WELL (6 EA´S) WERE
MEASURED, #1 NOMINAL THICKNESS IS 0.060¨ AND MAXIMUN DEPTH REMOVED 0.004" ,SDR VNAA202209029919None · corrodedCORROSION ON EWIS (PX31, PX19 ARNESS) SUPPORTS (2 EA´S, 1 PER SIDE) BETWEEN FS=797.00 TO FS= 807.00 AND 35LBL/35RBL AT LH/RH MLG WHEEL WELL
SUPPORTS (2 EA´S, 1 PER SIDE) BETWEEN FS=797.00 TO FS= 807.00 AND 35LBL/35RBL AT LH/RH MLG WHEEL WELL WERE RELACED PER SDR VNAA202209029918None · corrodedCORROSION IN RH FAIRING SUPPORT DIAPHRAGMS (3 EA´S, 1 EA LH SIDE 2EA´S RH SIDE) IN STA. FS= 797.00 TO FS= 807.00 AND 35LBL/35RBL AT RH MLG WHEEL WELL.
FAIRING SUPPORT DIAPHRAGMS (3 EA´S, 1 EA LH SIDE 2EA´S RH SIDE) IN STA. FS= 797.00 TO FS= 807.00 AND 35LBL/3SDR VNAA202209029917Skin · corrodedCORROSION ON EXTERNAL SKIN AT FWD FUSELAGE FAIRING SEATLEMENT AREA BTW FS 597-693 (UNDER ACCESS 191AB, 191BB & 192BB).
EXTERNAL SKIN AT FWD FUSELAGE FAIRING SEATLEMENT AREA BTW FS 597-693 (UNDER ACCESS 191AB, 191BB & 192BB) WAS REPAIRED PER EA 22-C7-53-0986 RSDR VNAA202209029916Stringer · corrodedCORROSIÓN ON STGR 24RH BTW FS 453-FS478. (FWD BAGGAGE COMPARTMENT).
STGR 24RH BTW FS 453-FS478. (FWD BAGGAGE COMPARTMENT) WAS REPAIRED PER CRJ 700 SRM 53-00-03-201-001-A01SDR VNAA202209029915Doubler · corrodedCORROSION ON DOUBLER BETWEEN FS=295/FS=310 AND STGR 26LH/26RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT.
DOUBLER BETWEEN FS=295/FS=310 AND STGR 26LH/26RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ700 SRM
51-42-06-001-001SDR VNAA202209029914Frame · corrodedCORROSION ON FRAME BETWEEN FS=295.00 AND STGR 25RH/27RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT.
FRAME BETWEEN FS=295.00 AND STGR 25RH/27RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ 700 SRM 53-00-06-201-006-A01SDR VNAA202209029913Skin · corrodedCORROSION ON SKIN BETWEEN FS=295.00/FS=310.00 AND STGR 24RH/25RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT.
SKIN BETWEEN FS=295.00/FS=310.00 AND STGR 24RH/25RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPAIRED PER EA 22-C7-53-0990 REV. SDR VNAA202209029912Stringer · corrodedCORROSION ON STGR 26LH BETWEEN FS= 319.70 AND FS=310 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT.
STGR 26LH FS=333.00 AND FS=280.00 WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01SDR VNAA202209029911Stringer · corrodedCORROSION ON STGR 25LH BETWEEN FS=333.00 AND FS=310.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT.
DAMAGED STGR 25LH BETWEEN FS=333.00 AND FS=310.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED
PER CRJ700 SRM 51-42-06-001-001-A01 ASDR VNAA202209029910Stringer · corrodedCORROSION ON STGR 25RH BETWEEN FS=333.00 AND FS=319.70 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT.
STGR 25RH BETWEEN FS=333.00 AND FS=319.70 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01
AND CRJ-SDR VNAA202209029999Stringer · corrodedCORROSION ON STGR 26RH BETWEEN FS=333.00 AND FS=319.70 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT.
STRINGER 26RH FS 333 TO FS 280 WAS REPLACED PER CRJ/700 SRM 51-42-06-001-001-0A1. AND CRJ/700 SRM 51-42-21-001-001-A01.SDR VNAA202209029998Stringer · corrodedCORROSION ON STGR 26RH BETWEEN FS=364.00 AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT.
STGR 26RH BETWEEN FS=364.00 AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01SDR VNAA202209029997Stringer · corrodedCORROSION ON STGR 26RH BETWEEN FS=333.00 AND FS=319.70 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT.
STRINGER 26RH FS 333 TO FS 280 WAS REPLACED PER CRJ/700 SRM 51-42-06-001-001-0A1. AND CRJ/700 SRM 51-42-21-001-001-A01.SDR VNAA202209029996Stringer · corrodedCORROSION ON STGR 26RH BETWEEN FS=364.00 AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT.
STGR 26RH BETWEEN FS=364.00 AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01SDR VNAA202209029995Post · corrodedCORROSION ON POST AT LBL12 BETWEEM FS=280 AND STGR 25LH/24LH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (LOWER SECTION).
POST AT LBL12 BETWEEM FS=280 AND STGR 25LH/24LH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ 700 SRM
5SDR VNAA202209029994Skin · bulgedBULGE ON FUSELAGE SKIN BTW FS295-310 & STGR 17R-18R.
FUSELAGE SKIN BTW FS295-310 & STGR 17R-18R WAS REPAIRED PER EA 22-C7-53-0997 REV.IRSDR VNAA202209029993None · dentedNICKS ON FUSELAGE SKIN EXTERNAL SURFACE, BTW FS517-FS581 & BTW STGR19L-25L, (SURROUNDING FWD CARGO DOOR CUTOUT SEVERAL LOCATIONS).
FUSELAGE SKIN EXTERNAL SURFACE, BTW FS517-FS581 & BTW STGR19L-25L, (SURROUNDING FWD CARGO DOOR CUTOUT SEVERAL LOCATIONS) WAS REPSDR VNAA202209029992None · corrodedCORROSION ON METALLIC STRAPS AT FAIRING 193AB.
METALLIC STRAPS WERE REPLACED ON FAIRING 193AB PER CRJ-700 SRM 51-42-10-001-001-A01SDR VNAA202209029991Access Panel · corrodedCORROSION AT ACCESS PANEL 542BZ.
CORROSION AT ACCESS PANEL 542BZ WAS REPLACED PER CRJ700 SRM 57-22-55-001-001-A01 ITEM 1.SDR K11A2023033000198Seat Track · corrodedFUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 767 AND STA 807 LBL 60" (APPROX 30" IN LENGTH) HAS EVIDENCE OF CORROSION.SDR SWIA202266626None · cracked* FORWARD EQUIPMENT COMPARTMENT FLOOR WEB, SUSPECTED CRACK @ L/H SIDE APPROX FS193, MARKED. (C-CHECK RO 10/24/2022) REPAIRED FORWARD EQUIPMENT COMPARTMENT FLOOR WEB L/H SIDE REF. CRJ-700 SRM 53-11-43-201-001-A01 AND COMPLIED WITH CRJ-700 SRM 53-11-43-SDR COEA2022102105803Web · corrodedW/O 238881 NR 200018 HEAVY CHECK COE/MAJOR REPAIR: PAX DOOR THRESHOLD UPPER SURFACE BETWEEN FRAMES 36-39 HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIR PER ATR72 536770-200-802-A01.
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