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 R61A2022011400032Shear Angle · corrodedSHEAR CLIP CORRODED AT FRAME 90 AND STRINGS 27R-28R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08SDR R61A2022011400031Shear Angle · corrodedSHEAR CLIP CORRODED AT FRAME 82 AND STRINGS 26R-27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.SDR JJBA20211221034None · noneCORROSION AT FR61 BETWEEN STRG 14R AND STR 15R ON PARTITION PANEL. REMOVED AND REPLACED PARTITION SECTION AT FRAME 61 STRINGER 15R-14RSDR JJBA20211221032None · noneFWD WET AREA FLOOR SUPPORT AT FR 23+2 STR 15R CORROSION. REMOVED AND REPLACED 2EA ANGLES.SDR CALA2021122202425Spar · crackedSUPPORT TASK- EA5310-06900 (AD2019-11-02) STEP 22.7 3EA HOLES FOUND CRACK ON FRONT SPAR CHORD DETAIL REFER FINDING REPORT. TRANSFER REF NR LP 9130731 AND ORIGINATED BY EMP V924735. EA 5310-06900 REV D OP 011 STEP 22.7 (3EA) HOLE CRACK ON FRONT SPAR CHORD REPAISDR CALA2021122202420Panel · crackedAD 2005-11-02 - SUPPORT TASK EA 5300-01600 REV.A OP 01, LH 1809 BHD 1EA HOLE FOUND CRACK ON FWD OUTER CHORD LAYER TRANSFER REF. HX NON-ROUTINE LP 9130608 & ORIGINATED BY EMP V913 608 LH STA1809 BHD FWD OUTER CHORD REPAIRED AS PER EA5300-01600 REV A OP2(SEQ 161SDR MASA20211220069None · corroded"CORROSION ON SPLICE OF STGR25RH, FS333.00 AT MAIN AVIONICS COMPARTMENT.
SPLICE OF STGR25RH, FS333.00 AT MAIN AVIONICS COMPARTEMENT WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01"SDR MASA20211220067Frame · corroded"CORROSION ON FRAME 319.70 BTW STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT.
FRAME 319.70 BTW STGR26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ/900 SRM 53-00-06-201-001-A03."SDR SWIA202163553None · crackedLATE FIND-FR52 LH SIDE OF LOWER FUSELAGE FWD SIDE OF FRAME ATTACH ANGLE CRACKED AS MARKED (C-CHECK RO 1/3/2022) REMOVED AND REPLACED -FR52 LH SIDE OF LOWER FUSELAGE FWD SIDE OF FRAME ATTACH ANGLE REF EMB SRM 51-40-08SDR SWIA202163233None · damagedTRANSFER FROM EAML 805581 : GROUND VEHICLE DROVE INTO RIGHT SIDE OF AIRCRAFT FUSELAGE. LONG INDENTATIONS AND SCRATCHES IN THE AIRCRAFT SKIN ARE PRESENT. (FILED - CLOSED) COMPLIED WITH REO 690-53-31-619 REV "--" DATED 12/26/2021. REPAIRED DAMAGED SKIN ON RSDR 2021FA0000425None · noneIN SPECIAL DETAILED INSPECTION IAW AD 2012-26-02 WAS FOUND CRACK ON STR10R BETWEEN BS510 AND BS520 WITH 1,2" OF LENGHTSDR JJBA20211220031None · noneUNDER PASSENGER DOOR SIL AIRCRAFT SKIN CORROSION. REMOVED AND REPLACED PAX DOOR SILL.SDR MASA20211221634None · noneTHE FUSELAGE SKIN LOWER PANEL WAS FOUND TO HAVE A PREVIOUS BLENDOUT. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-61-01-001-003-A02, FIG. 53-61-01-991-806, ITEM 1 AND ITEM F (REV.38 DATED 9 JUL 2021 ). DEFECT LOCATION: FS 1000- FS 10L5 AND STRG 25R AND STRG 26SDR CALA2021122002417Repair · noneREF DTA LP 7628364 AS PER ECRA 5331-02818 PART 1 STEP 3;PLANNING TO CONTACT ENGINEERING AFTER 09 OCTOBER 2022 BUT BEFORE 09 NOVEMBER 2022 FOR ECRA 5331-02818 PART 3 PERMAMANT REPAIR. REFERENCE ECRA 5331-02818 PART 1 STEP 3. BEFORE 09 NOVEMBER 2022 FOR ECRA 533SDR CALA2021122002415Repair · noneACCOMPLISH A PERMANENT REPAIR PER PART 3 OF LATEST REVION OF ECRA 5331-02818 ON OR BEFORE 09 DECEMBER 2022. REF DTA LP 7037108 ACCOMPLISH PERMANENT REPAIR PER PART 3 OF LATEST REVISION OF ECRA 5331-02818 ON OR BEFORE 09 DECEMBER 2022. REF DTA LP7037108 ACCOMPLSDR CALA2021122002410Stringer · crackedSUPPORT TASK -EA 5310-06900 REV D OP 001 , AD 2019-11-02 LH BS 1035 BUILT-UP UNDERWING LONGERON FOUND 1EA CRACK PRINT AND ACCOMPLISH OP11 - REFER TRANSFER NON-ROUTINE LP 9130199 - AND ORIGINATED BY EMP V924733 FUSE LAGE LH UNDERWING LONGERON REPLACED AND INSTSDR CALA2021122002409Ring Assembly · crackedSUPPORT TASK - EA5310-06900 - (AD2019-11-02) STEP 22.7 2EA HOLES FOUND CRACK ON RING CHORD DETAIL REFER FINDING REPORT TRANSFER REFER NON-ROUTINE LP 9130728 - AND ORIGINATED BY EMP V924733SDR MASA20220125084Angle · cracked"CRACK ON LOWER ANGLE (ACCESS 212AR, REAR LATCH HOUSING), FWD EQUIPMENT COMPARTMENT.
LOWER ANGLE (ACCESS 212AR, REAR LATCH HOUSING), FWD EQUIPMENT COMPARTEMENT WAS REPLACED PER CRJ/900 SRM 51-42-13-001-001-A01 "SDR CALA2021122002408Skin · crackedSUPPORT TASK- EA5310-06900 (AD2019-11-02) STEP 20.2 3EA HOLES FOUND CRACK ON SKIN LAYER, DETAIL REFER FINDING REPORT. TRANSFER REF NR LP 9130730 AND ORIGINATED BY EMP V924733. DTA/DIP IS REQUIRED FOR INITIAL INSP AT 26,233 TOTAL FC WITH REPEAT INSP INTERVALS NSDR SWIA202164965None · corrodedJ ANGLE FLOOR BOARD ATTACHING PLATE ON FRAM AT FS. 409.00 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED AVIONICS BAY FLOOR BOARD SUPPORT J-ANGLE AT F.S. 409.00 IAW CRJ-200 SRM 51-42-21 AND 51-42-06. REF ATTACHED CONTINUATION FOR WORK PERFORMED.SDR SWIA202164242None · crackedCENTER WINDSHIELD POST (LWR. LEFT ANGLE BRACKET) CRACKED THROUGH AT RADIUS (AS MARKED) (C CHECK RO 2-11-2022) REMOVED AND REPLACED CENTER WINDSHIELD POST LWR LEFT ANGLE BRACKET IAW CRJ 200 SRM 51-40-11 AND 51-42-21 AND SKY CARD 51-900-1003-SKY NO WEIGHT CSDR 2022FA0000074Brake · leakingLANDED IN KJAC AT 0224 Z AND TAXIED TO JACKSON HOLE AVIATION RAMP. SET PARKING BRAKE AND SUTDOWN ENGINES 1 AND 3. BRIEFED COPILOT TO LEAVE THE PARKING BRAKE ON AS IT WAS NONSTANDARD PROCEDURE AFTER BEING CHICKED. THE RAMP AGENT POINTED TO THE LEFT MAIN GEAR ANSDR MASA20220125088None · corroded"CORROSION ON LOWER STRIKE SEAL AT GALLEY SERVICE DOOR SURROUND STRUCTURE
LOWER STRIKE SEAL WAS REPLACE PER CRJ900 SRM 51-42-06-001-001-A01 "SDR MASA20220125085Angle · none"CRACK ON ANGLE AT FRAME FS394 TO LONGERON {STGR25L), MAIN AVIONIC COMPARTMENT DOOR CUT OUT STRUCTURE.
ANGLE AT FRAME FS 394 TO LONGERON (STGR25L), MAIN AVIONIC COMPARTMENT DOOR CUT OUT STRUCTURE
WAS REPLACED PER EA 72-2022-008 REV. IR "SDR FDEA202112183104Fairing · looseON POST FLIGHT WALK AROUND FOUND FOLDING AFT SECTION OF TAILCONE DETACHED AND ROTATED 180 DEG, IS HELD BY THE HOLD OPEN SNUBBER. REMOVED AND INSTALLED SERVICEABLE TAILCONE PER MM 53-52-01-4,AND REINSTALLED REMOVED PANELS PESDR IXXA2021121801Shear Tie · corrodedSHEAR TIE CORRODEDSDR QMLA2022031020015Frame · crackedLOWER LH DAMAGE OF SHORT PITCH DISTANCE AND EDGE DISTANCE IN U-PROFILE (FRAME CAP) AND AFT L- ANGLE. LOWER RH DAMAGE OF SHORT PITCH DISTANCE IN U-PROFILE (FRAME CAP) AND AFT L-ANGLE. LOWER LH DAMAGE OF 1.5 LONG CRACK. UPPER LH, CENTER AND RH DAMAGE OF SHORTSDR SWIA202164506None · gougedEXTERNAL FUSELAGE SKIN AT APPROX. FS969-FS985 STGR27 HAS 1EA CHAFE AND 1 EA GOUGE. (C CHECK RO 2/17/2022) COMPLIED WITH FUSELAGE SKIN REPAIR AT FS977-FS985 STGR27 REF BOMBARDIER REO 670-53-00-290 REV -F DATED 2019/04/26. COMPLIED WITH TASK CARD 51-900-1002SDR SWIA202164298None · corroded* THE FRAME DOUBLER AT FS473.15 AT THE LH PRESSURE FLOOR SILL BEWEEN STR 17L AND 16L HAS CORROSION. (MARKED) (C CHECK RO 02-12-2022) REPAIRED FRAME DOUBLER AT FS473.15 AT THE LH PRESSURE FLOOR SILL BETWEEN STR 17L AND 16L REF REO 601R-53-41-2999 REV -- DASDR MASA20220125091None · corroded"CORROSION ON FLOOR SEAT RAIL FS=581-485 LBL9 AND RBL9
FLOOR SEAT RAIL WERE REPPLACED PER CRJ/900 AMM 53-00-49"SDR MASA20220125079None · corroded"CORROSION ON SIDE SEAT RAILS IN SECTIONS FS485.00 -FS573.00 STGR 15RH AT PAX CABIN. (CPAX)
SIDE SEAT RAILS WAS REPLACED PER CRJ900 AMM 53-00-49 "SDR MASA20211217078None · corroded"CORROSION ON SIDE SEAT RAILS IN SECTIONS FS661+16.00 -FS669.00 STGR 15LH AT PAX CABIN. (CPAX)
SIDE SEAT RAILS WAS REPLACED PER CRJ900 AMM 53-00-49 IN SECTIONS FS661+16.00 -FS669.00 STGR 15LH AT PAX CABIN"SDR MASA20211217076Skin · cracked"CRACK ON EXTERNAL FUSELAGE SKIN BTW FS=193.00 AND STGR 16LH-17LH
FUSELAGE SKIN BTW FS=193.00 AND STGR 16LH-17LH WAS REPAIRED PER EA 81-2021-100 REV. IR"SDR SWIA202163550None · corrodedR/H O/B PANEL SUPPORT AT FR 84 HAS CORROSION AS MARKED. (C-CHECK RO 1/3/2022) REMOVED AND REPLACED R/H O/B PANEL SUPPORT AT FR 84 REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK ACCOMPLISHEDSDR R61A2022010300013Shear Panel · corrodedCORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE, RH SHEAR WEB BETWEEN FR87 AND FR88. REPLACED IAW SRM 51-43-01 AND 51-42-01SDR R61A2022010200011Gusset · corrodedCORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE GUSSET ON RH OUTBOARD SIDE AT FR90, REPLACED IAW SRM 51-41-02SDR R61A2022010200010Splice · corrodedCORROSION FOUND ON AFT WET AREA FLOOD STRUCTURE GUSSET ON RH INBD SIDE AT FR89, REPLACED IAW SRM 51-43-01SDR R61A2022010200009Splice · corrodedCORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE GUSSET ON RH OUTBD SIDE AT FR89, REPLACED IAW SRM 51-43-03SDR R61A2022010200008Panel Support · corrodedCORROSION FOUND ON AFT WET AREA FLOOR PANEL SUPPORT ON RH OUTBD SIDE, BETWEEN FR88 AND FR90. REPLACED IAW SRM 51-43-03SDR R61A2022010200007Shear Panel · corrodedCORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE, CENTER SHEAR WEB BETWEEN FR87 AND FR88. REPLACED IAW SRM 51-42-01SDR R61A2022010200006Shear Panel · corrodedCORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE, LH SHEAR WEB BETWEEN FR87 AND FR88. REPLACED IAW SRM 51-41-01SDR MASA20211221622None · noneTHE LH FUSELAGE SKIN PANEL WAS FOUND WITH DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-12-00, SRM 51-40-11-001-001.SDR 2A6R2021121762704None · noneDURING 1000 HOUR AIRFRAME INSPECTION, FOUND SEVERAL CRACKS UNDER THE MAIN TRANSMISSION DECK. LEFT & RIGHT LONGERONS P/N L533M1017281 & P/N L533M1017282 WERE CRACKED IN THE UPPER FLANGES AT X4565 WITH L/H CRACK MEASURING 0.50 LONG AND R/H MEASURING 0.60 LONE. SDR IXXA2021121702Intercostal · bentINTERCOSTAL BENTSDR IXXA2021121701Shear Tie · corrodedCORROSION ON SHEAR TIE.SDR SWIA202163556None · failedR/H ELEVATOR INBD PCU FAILED BACKLASH FAILED BACKLASH FUNCTIONAL TEST (C-CHECK RO 1/3/2022) REMOVED AND REPLACED RH INBOARD PCU TO ELEVATOR HINGE HARDWARE. REF AMM 27-32-02. TW #TC2-61343 DUE 2-3-22. TW#TC2-8951 DUE 10-26-22.RE-CHECK OF BACKLASH ON RH ESDR SWIA202163555None · failedL/H ELEVATOR OTBD PCU FAILED BACKLASH FAILED BACKLASH FUNCTIONAL TEST (C-CHECK RO 1/3/2022) REMOVED AND REPLACED HARDWARE, BOLT AND BUSHING, FOR THE LH ELEVATOR OTBD PCU. REF E-175 AMM 27-32-02. TORQUE WRENCH ASSET 61343, CAL DUE 02-03-22. PERFORMED BACSDR SWIA202163554None · failedL/H ELEVATOR INBD PCU FAILED BACKLASH FAILED BACKLASH FUNCTIONAL TEST (C-CHECK RO 1/3/2022) / REMOVED AND REPLACED HARDWARE FOR THE LH INBD ELEVATOR PCU. REF E-175 AMM 27-32-02. TORQUE WRENCH: ASSET 61343, CAL DUE 02-03-22. PERFORMED BACKLASH CHECK OF SDR SWIA202163544None · corrodedR/H O/B CROSS BEAM DOUBLER PLATE FR87-FR88 HAS CORROSION AS MARKED. (C-CHECK RO 1/3/2022) REMOVED AND REPLACED R/H O/B CROSS BEAM DOUBLER PLATE FR87-FR88 REF EMB SRM 51-40-08 SEE CONTINUATION CARD FOR WORK ACCOMLPISHEDSDR SWIA202163105None · failedRIGHT ENGINE FAIL (N1 /N2 DROP) APPROXIMATELY 600 AGL, HIGH ITT, LOUD LOW FREQUENCY VIBRATION. FO SIDE PFD AND MFD MULTIPLE DROP OFFS STOPPED AFTER INFLIGHT SHUTDOWN. NORMAL SINGLE ENGINE LANDING. (FILED CLOSED - FLIGHT 5092) PLEASE REFERENCE AML 80687
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