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 SWIA202164826None · crackedL/H SIDE FWD AVI BAY FLOOR AT F.S. 193.0 IS CRACKED. (C CHECK RO 3/11/2022) REPAIRED LH SIDE FWD AVI BAY FLOOR CRACK AT F.S. 193 IAW BOMBARDIER REO 601R-53-11-081 REV NC DATED 03-07-97. REF ATTACHED CONTINUATION FOR WORK PERFORMED. COMPLETED TASK CARD 51SDR SWIA202164401None · corrodedMAIN AVIONICS BAY STR 26L ATTACH ANGLE BETWEEN FS349.00 AND FS364.00 CORRODED. (C-CHECK RO 2/16/2022) REMOVED AND REPLACED STR 26L ATTACH ANGLE FROM FS349.00 TO FS364.00 REF. DRWG SH670-32050 REV. J, CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-4SDR SWIA202164400None · corroded*MAIN AVIONICS BAY STR 26R ATTACH ANGLE BETWEEN FS349.00 AND FS364.00 CORRODED. (C-CHECK RO 2/16/2022) REMOVED AND REPLACED STR 26R ATTACH ANGLE FROM FS349.00 TO FS364.00 REF. DRWG SH670-32050 REV. J, CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-SDR SWIA202164392None · corroded*MAIN AVIONICS BAY STR 21L BACK-UP SILL BETWEEN FS333.00 AND FS349.00 CORRODED. (C-CHECK RO 2/16/2022) REPLACED STGR 21L BACK-UP SILL BETWEEN FS333.00 AND FS349.00. REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH670-31810 REV AE. COMPLIED WITH TASK CARDSDR SWIA202164391None · corroded*MAIN AVIONICS BAY STR 21L BACK-UP SILL BETWEEN FS310.00 AND FS333.00 CORRODED. (C-CHECK RO 2/16/2022) REPLACED STGR 21L BACK-UP SILL BETWEEN FS310.00 AND FS333.00. REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH670-31810 REV AE. COMPLIED WITH TASK CARDSDR SWIA202164387None · corroded*MAIN AVIONICS BAY TCAS ANTENNA DOUBBLER BETWEEN FS295.00 AND FS310.00 CORRODED. (C-CHECK RO 2/16/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED DOUBLER. REF. CRJ 900 SRM 51-42-06-001-001-A01ANDSDR SWIA202164382None · none*MAIN AVIONICS BAY CRAWLWAY FLOORBOARD SUPPORT ANGLE AT FS280.00 CORRODED. (C-CHECK RO 2/16/2022) REPLACED MAIN AVIONICS BAY CRAWLAWAY FLOORBOARD SUPPORT ANGLE AT FS280.00 REF CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01 AND DWG CSDR SWIA202164379None · corroded*MAIN AVIONICS BAY FWD WATER-WASTE SURROUND STRUCTURE LOWER IMPACT ANGLE CORRODED. (C-CHECK RO 2/16/2022) REMOVED AND REPLACED FWD WATER-WASTE SURROUND STRUCTURE IMPACT ANGLE REF. DRWG SH670-32280 REV. H AND CRJ 900 SRM 51-42-06-001-001-A01. COMPLIED WSDR SWIA202164378None · corroded*MAIN AVIONICS BAY FWD WATER-WASTE SURROUND STRUCTURE LOWER DIAPHRAGM CORRODED (C-CHECK RO 2/16/2022) REMOVED AND REPLACED DAMAGED FWD WASTE WATER SURROUND STRUCTURE LOWER DIAPHRAGM. REF. CRJ 900 SRM 51-42-06-000-001-A01 AND DWG SH670-32280 REV. H. PRESSDR SWIA202164287None · damagedPILOTS WINDSHEILD, SIDE EXTERNAL POST HAS NUMEROUS SCRATHES (MARKED WITHIN RED GREASE PENCIL) (C CHECK RO 02-12-2022) REMOVED DAMAGED PILOT WINDSHIELD STRAP REF CRJ 200 AMM 56-11-01-000-801 INSTALLED NEW PILOT WINDSHIELD STRAP REF CRJ 200 AMM 56-11-01-400-SDR SWIA202164286None · damagedCO-PILOTS WINDSHEILD, SIDE EXTERNAL POST HAS NUMEROUS SCRATHES (MARKED WITHIN RED GREASE PENCIL) (C CHECK RO 02-12-2022) REMOVED AND REPLACED WITH NEW CO-PILOT WINDSHIELD STRAP REF CRJ-200-AMM 56-11-01-000-801 AND CRJ 200 AMM 56-11-01-400-801 . LEAK CHECSDR R61A2022010500022Support · corrodedCFIII FLOOR STRUCTURE CORROSION FOUND ON RH FLOOR SUPPORT BETWEEN FR88 & FR90 REPLACED IAW SRM 51-41-01SDR QMLA2021121020064Doubler · crackedDURING A 2060 1000 HOUR/36 MONTH INSPECTION, THE REAR DOUBLER PN: L533M1321262 WAS FOUND TO HAVE
ABOUT A 6 INCH CRACK RUNNING FROM LEFT REAR TO RIGHT FORWARD. THE A-PROFILE LEFT PN:
L533M1017375 AND A-PROFILE RIGHT PN: L533M1017376 WERE FOUND TO HAVE 1 INCH SDR JJBA20211210011None · noneFUSELAGE EXTERIOR TAIL - CRACK .100" LONG IN FUSELAGE SKIN STARTING AT FASTENER HOLE AT FR 75 STRG 2R. REPAIRED TRIMMED OUT IN FUSELAGE SKIN STARTING AT FASTENER HOLE AT FR 75 STRG 2R WITH REPAIR DOUBLER, REPAIR FILLER, AND FORMED REPAIR ANGLE.SDR CALA2021121202342Fitting · corrodedMAIN CABIN R2 DOOR SILL HAS (2EA) AREAS OF CORROSION ON UPPER SU RFACE CENTER SHAPE SILL ONLY. GENERATED BY N078592 PER HAECO LCQ NR 9294286/22286 REMOVED AND REPLACED R-2 DOOR SILL SHAPE SILL IAW A320 SRM 51-42 -11/001 PARA 6 DOT REMOVED KC50 BY MECH V061630 SDR CALA2021121202341Fitting · corrodedR2 DOOR SILL FWD CORNER FITTING HAS CORROSION. GENERATED BY N078 592 PER HAECO LCQ NR 9294287. REMOVED AND REPLACED CORNER FITTING AT R2 DOOR SILL IAW A320 SRM 51-42-11/001 PARA 6 B,F DOT REMOVED KC51 BY MECH V061630 INSP BY V919150SDR MASA20211210602None · noneWHILE PERFORMING SB670BA-53-045, LH FS220 FRAME (UPPER) FAILED NDT (CRACKED).
REMOVED AND INSTALLED NEW SERVICEABLE LH FS220 UPPER FRAME SECTOR PN: CC670-34146-5 IAW CRJ900-SRM 51-42-21-001-001-A01, PLUS 51-40-11-001-001-A01. THIS IS A PERM REPAIR.SDR MASA20211210601Web · nonePOSSIBLE CRACK ON FS202 BULHEAD AT UPPER RBL7.0. DAMAGE ALSO HAS A GOUGE
REMOVED GOUGE DAMAGE IAW CRJ900-SRM 51-12-00-001-001-A01. REMAINING THICKNESS ACCEPTABLE. REPAIRED AREA OF CRACK IAW REO-670-53-11-1381. NO DAMAGE NOTED AFTER NDT FOR BOTH AREAS. THIS ISDR MASA20211210600None · noneWHILE PERFORMING SB670-53-045, FOUND LH FRAME SECTOR AT FS235 TO BE CRACKED.
REMOVED AND INSTALLED NEW SEVICEABLE LH FS235 FRAME, UPPER FRAME SECTOR PN: CC670-34133-9S (MHIRJ PCN-CC670-34133-7-8-091720151029) IAW CRJ900-SRM 51-42-06-001-001-A01 AND 51-42-21-0SDR MASA20211130599None · noneWHILE PERFORMING SB670-53-045, FOUND LH FRAME SECTOR AT FS235 TO BE CRACKED.
REMOVED AND INSTALLED NEW SEVICEABLE LH FS235 FRAME, UPPER FRAME SECTOR PN: CC670-34133-9S (MHIRJ PCN-CC670-34133-7-8-091720151029) IAW CRJ900-SRM 51-42-06-001-001-A01 AND 51-42-21-0SDR MASA20211130598None · noneWHILE PERFORMING SB670-53-045, FOUND RH FRAME SECTOR AT FS235 TO BE CRACKED.
REMOVED AND INSTALLED NEW SEVICEABLE LH FS235 FRAME, UPPER FRAME SECTOR PN: CC670-34133-8 /10S (MHIRJ PCN-CC670-34133-6-100120110818-REV1) IAW CRJ900-SRM 51-40-11-001-001-A01, 51-42-SDR MASA20211130597None · noneWHILE PERFORMING SB670-53-045, FOUND RH FRAME SECTOR AT FS220 FAILED NDT (CRACKED).
REMOVED AND INSTALLED NEW SEVICEABLE RH FS220 FRAME, UPPER FRAME SECTOR PN: CC670-34146-6 IAW CRJ900-SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01. THISSDR CALA2021121002338Antenna · corroded(A3NB-44-3-6004) GCS ANTENNA ADAPTER PLATE HAS EXFOLIATING CORRO SION CENTER AREA AFT ON ANTENNA. DOT 102-116.() GCS ANTENNA ADAPTER PLATE REPAIRED IAW EA 319-4420-13-A2749 REV'' _'' AND UAL EC/RA 5341-01290. NO DEVIATIONS EMP# V934344 WORK ACC OMPLISHED T ST SDR CALA2021121002337Fitting · cracked(REPAIR BEFORE NEXT FLT) ROTO PROBE OF RH FR16 #7 DOOR STOP FIT TING HOLES FOUND CRACKS IN THE I/B TOP AND I/B BOTTOM HOLES.() REPAIRED HOLES #1-3 FROM FRAME AND INTERCOASTAL DOOR STOP FITTIN G #7 FR16 LH IAW EA 319-5311-13-A2715, ECRA 5311-02680. EMP# V93 33SDR CALA2021121002332None · crackedRT MLG W/W VERTICAL PRESSURE DECK WEB CRACKED REF AAR N/R 9638163 REPAIRED RT MLG W/W VERTICAL PRESSURE WEB AS PER B737 SRM 57-10-10-2R-3 WORK ACCOMLPISHED BY V937767SDR SWIA202164374None · corroded* THE FS280 CROSSBEAM HAS CORROSION AT LBL9 WHERE IT ATTACHES TO THE ANGLE. (MARKED) (C-CHECK RO 2/16/2022) REMOVED DAMAGED L/H FS280.00 CROSSBEAM AND REPLACED WITH NEW. REF. REO#670-53-11-594 REV -A DATE 2015/06/26, DWG CC670-34010 REV -K, CRJ900 SRMSDR SWIA202164373None · corroded* THE FS280 FLOOR PANEL SUPPORT ANGLE HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK RO 2/16/2022) REMOVED AND REPLACED THE FS280 FLOOR SUPPORT ANGLE P/N:CC670-34095-1 WITH NEW REF. CRJ900 SRM 51-42-06-001-001-A01, AND CRJ900 SRM 51-42-21-001-0SDR SWIA202164372None · corroded*MAIN AVIONICS BAY FWD WATER-WASTE SURROUND STRUCTURE UPPER DIAPHRAM CORRODED. (C-CHECK RO 2/16/2022) REMOVED AND REPLACED DAMAGED FWD WASTE WATER SURROUND STRUCTURE DIAPHRAGM. REF. DRWG SH670-32280 REV. H AND CRJ 900 SRM 51-42-06-001-001-A01 REV. 38 DASDR SWIA202164371None · gouged*AFT BAGGAGE BAY DOOR, FWD FLOOR SUPPORT SPLICE/JOINT IS GOUGED. FLAGGED (C-CHECK RO 2/16/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE WITHIN LIMITS. REF. MHIRJ REO 690-53-61-1054 REV --, 2022-01-08. CRJ 900 SRM 51-42-21-001-001-A01 DSDR SWIA202164059None · damagedWHILE PERFORMING SB670SH-53-042 FOUND F.S.847 RBL 18 POST WITH PREVIOUS CUTOUT WITH FILLER DOUBLER REPAIR. (FILED CLOSED) COMPLIED WITH MHIRJ REO 670-53-41-586 AND REO 670-53-51-584, SKYCARD 51-900-1002-SKY(CL600-2C10), FORMS M337, AND SDR. TOTTAL WIEGHTSDR SWIA202163850None · distortedBRACKET AT F.S. 1000.0 STGR 23L (P/N MM670-43600-003) IS DISTORTED. (C CHECK RO 1/16/2022) REPLACED BRACKET AT FS1000 STGR 23L WITH NEW BRACKET REF CRJ-700 SRM 51-42-06-001-001-A01, DWG MM670-43600 REV NC. COMPLIED WITH TASK CARD 51-900-1002-SKY.SDR A6WA202101178075None · corrodedFS 574.00+10 TO FS 589.00+8 & LBL 46 FRETTING CORROSION COMMON TO ANGLE AT LWR SIDE OF CARGO DOOR OPENING AT FLOOR LEVEL ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED 5 OFF AREAS P1 THROUGH P5 OF BLENDED CORROSION DAMAGE AS: P1 1.60"L X 0.80"W X .068" MIN RESDR MASA20211213610Beam · corrodedTHE CENTER FLOOR BEAM WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 53-31-43, FIG. 53-31-43-991-801, ITEM 6 (REV. 38 DATED JUL. 25, 2020). DEFECT LOCATION: FS 621.00-661.00+22.50, LBL 9.00SDR MASA20211213607None · corrodedTHE CENTER FLOOR BEAM AT PAX CABIN WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-00-41-201-001-A03 (FLOORBEAMS FS 280.00 -FS 1098.20 REPAIRS), FIG. 53-00-41-995-829 (REV. 38 DATED JUL. 25, 2020).SDR MASA20211213606None · corrodedHE RBL9.00 CENTER FLOOR BEAM AT PAX CABIN WAS FOUND WITH CORROSION DAMAGE.
PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53 -31-43-101-A03 AND 53-00-41-201-001-A03
(FLOORBEAMS FS 280.00 -FS 1098.20 REPAIRS), FIG 53-00-41-995-829 (REV. 38 DATED JUL. 25, 2020). SDR DALA2021121007611Access Panel · unsecureSHIP 3161 - LIGHT GAS SMELL REPORTED BY FA'S LOCATED IN MIDDLE OF THE CABIN. FOUND LEFT BELLY FUEL SUMP POINT INSIDE LANDING GEAR DOOR LEVER ACCESS PANEL NOT FULLY SEATED AND LEAKING. RESEATED SUMP PLUNGER VALVE AND CLEANED COMPARTMENT.SDR 2021FA0000371None · noneCOIL CORD INSULATION FAILED AFTER BEING INSTALLED 2 YEARS.SDR IXXA2021120901Floor Support · corrodedFLOOR SUPPORT PAN IS CORRODEDSDR 2022FA0000609None · noneDURING ROUTINE INSPECTION FOR A HYD. LEAK IT WAS NECESSARY TO GAIN ACCESS UNDER FIREWALL AND R/H LOWER SIDE PENAL FABRIC AND INSULATION. DISCOVERED SEVERE INTERGRANULAR CORROSION ON IHA LOWER FIREWALL FRAME BEGRIMING 16" ABOVE IHA LOWER R/H ENGINE MOUNT ATTACHSDR 2022FA0000608None · noneDURING ROUTINE INSPECTION FOR A HYD. LEAK IT WAS NECESSARY TO GAIN ACCESS UNDER FIREWALL AND R/H LOWER SIDE PENAL FABRIC AND INSULATION. DISCOVERED SEVERE INTERGRANULAR CORROSION ON IHA LOWER FIREWALL FRAME BEGRIMING 16" ABOVE IHA LOWER R/H ENGINE MOUNT ATTACHSDR 2022FA0000607None · crackedAS OF THIS DATE THE ENGINE HAS 380 HOURS SINCE A MAJOR OVERHAUL. AIRCRAFT WAS IN A NORMAL CRUISE CONFIGURATION. ENGINE STARTED TO RUN ROUGH, PILOT RETURNED TO THE AIRPORT WITH NO FURTHER ISSUES. UPOND TEAR DOWN THE EXHAUST PUSH ROD HAD PUNCHED THROUGH THE ROCKSDR SWIA202163911None · crackedANGLE CRACKED ON FWD SIDE OF BULKHEAD FS280 LBL26 (C CHECK RO 1/18/2022) REMOVED AND REPLACED ANGLE ON FWD SIDE OF BULKHEAD FS280 LBL26 REF REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG CC670-34010 REV -JSDR MASA20211213620None · dentedTHE LH FUSELAGE SKIN PANEL WAS FOUND WITH A DENT. PERFORMED PERMANENT REPAIR IAW CRJ7/9 53-11-01, FIG. 53-11-01-991-806, ITEM 1 (REV. 38 DATED 9 JUL. 2021 ). DEFECT LOCATION: FS 278.00 BETWEEN STRG. 22L AND STRG. 23LSDR MASA20211213619None · dentedTHE FUSELAGE LOWER SKIN PANEL WAS FOUND WITH A DENT. PERFORMED PERMANENT REPAIR IAW CRJ?/9 53-61-01. DEFECT LOCATION : FS 1047-FS 1051, STGR. 22L - STGR. 23LSDR MASA20211213618None · corrodedTHE UPPER CAP AFT FLOOR BEAM FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 53-31-43-991-801, ITEM 7 (REV. 33 DATED JUN.25, 2017).SDR MASA20211213611None · corrodedTHE UPPER CAP OF THE LBL9.00 CENTER FUSELAGE FLOOR BEAM BETWEEN FS661+16-FS661+32 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-31-43-001-A03, FIG. 53-61-43-991-801, ITEM 2A (REV. 33 DATED JUN. 25, 2017). DEFECT LOCATION: FS SDR JJBA20211208015None · noneREMOVE, RE-FABRICATE AND INSTALL DOUBLER AT REAR FUSELAGE SKIN RAR 2 ANTENNA THAT WAS DAMAGED ON INSTALL. REMOVED, FABRICATED AND REINSTALLED REPAIR DOUBLER AT REAR FUSELAGE SKIN RAT 2 ANTENNASDR CALA2021121002313Pressure Blkhd · crackedLT MLG W/W VERTICAL PRESSURE DECK WEB CRACKED REF AAR N/R 9638162 REPAIRED LT MLG W/W VERTICAL PRESSURE WEB AS PER B737 SRM 57-10-10-2R-2 ALTERNITIVE 2 PREFORMED HFEC AND LFEC RE-INSPECT AT EVARY 36,000 FC WITH A THRESHOLD OF 56,000 FC I.A.W B737 SRM 57-10-10-SDR CALA2021121002312Pressure Blkhd · crackedRT MLG W/W VERTICAL PRESSURE DECK WEB CRACKED REF AAR N/R 9638163 REPAIRED RT MLG W/W VERTICAL PRESSURE DECK WEB AS PER B737 SRM 57-10-10-2R-3 ALTERNATIVE 2 PERFORM HFEC AND LFEC RE-INSP AT EVERY 36,000 FC WITH A THRESHOLD OF 56,000 FC AFTER REPAIR COMPLETION SDR CALA2021121002311None · corrodedAFT FLOOR STRUCTURE WEB LEFT AND RIGHT SIDES STA 987 TO 1006 HAV E CORROSION (REF. AAR NR 99917088). REMOVED AND REPLACED (2EA) FLOOR WEB R/2 L/2 ON BS 987 TO 1006 I AW B737-800 SRM 51-40-02 (WORK ACCOMPLISHED BY V916729 AND AAR Q C V895387).
Back to JASC 5300