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 R61A2021102000820Crossbeam · noneFRAME 17 CROSSBEAM BETWEEN TRACK LEFT AND TRACK RIGHT HAS TOOLING MARKS. PERFORMED PERMANENT REPAIR BY CUTOUT AND L-ANGLE REPAIR ON RH FR 17 CROSSBEAM BETWEEN TRACK LEFT AND TRACK RIGHT REF SRM 53-00-10 R03.SDR UIEA2021091802048None · noneAFT CARGO DOOR STA 1810 1EA CRACK FOUND AT 7 O/C OF FASTENER HOLE AT SKIN LAYER APPROX 3/16" IN LENGTH(<P>AFT CARGO DOOR CUTOUT FORWARD UPPER CORNER SKIN PANEL CRACK AREA REPAIRED IAW SRM 53-60-01-2R-3 REPAIR 3. REPEAT INSPECTION IAW SRM 53-60-01-2R-3 REPAIR 3SDR UIEA2021091902049None · noneREFER EO 4453A749 PART 1, STA 2598 B/H SUPPORT FRAME MOD L/H FOUND EXISTING REPAIR PARTS WERE FOUND ON THE SB 747-53A2837 MOD AREAS.(<P>STA 2598 L/H MOD, LEFT UPPER CORNER STRUCTURE MOD DISCREPANCLES REPAIR AREAS REPAIRED IAW RI-53-00-14941 REV A.</P>)SDR UIEA2021091902050None · noneREFER TAR 36 - STA 2598 L/H LOWER CORNER DISCREPANCIES REPAIR(<P>LH STA 2598 LOWER AREA WEB CRACK REPAIRED IAW SB 747-53A2837 REV 0. FIG 35</P> / <P>MOD DOUBLER S.E.M AREAS REPAIRED IAW RI-53-00-14939 REV A.</P>)SDR UIEA2021091902051None · noneBS 2598 LH BULKHEAD 1EA FASTENER HOLE FOUND CRACK AT 1ST LAYER WITH APPROX 1/4" DEPTH RUNNING ONE O/C POSITION(<P>STA 2598 BULKHEAD LH OUTER CHORD 1EA FASTENER CRACK AREA FREEZE PLUG REPAIRED IAW RI-53-00-14940 REV A</P>)SDR UIEA2021091902052None · noneBS 2598 L/H BULKHEAD LOWER CORNER CUTOUT 3EA FASTENER HOLES FOUND CRACK AT WEB LAYER(<P>EMP - STA 2598 LH BULKHEAD LOWER CORNER CUTOUT 3EA FASTENER HOLE CRACK AREAS MODIFICATED IAW SB 747-53A2837 FIG 35 REV 0</P>)SDR UIEA2021091902053Web · damagedREFER EO 4453A749 PART 1, WHERE WEB INTERIM MOD AND A CHORD REPAIR FOUND AT UPPER LH CORNER CUTOUT. EMP - STA 2598 LH BULKHEAD UPPER CORNER CUTOUT AREAS MODIFICATED IAW SB 747-53A2837 FIG 31 REV 0SDR UIEA2021092202074Channel · crackedM/D STA 1080 TENSION TIE R/H AFT CHANNEL FOUND CRACKED. M/D STA 1080 TENSION TIE R/H AFT CHANNEL CRACK AREA REPAIRED IAW CS DOC NO : CS 27062-014 AND RI-53-40-14956 REV A.SDR UIEA2021092202075Channel · crackedM/D STA 1100 TENSION TIE R/H AFT CHANNEL FOUND CRACKED. M/D STA 1100 TENSION TIE R/H AFT CHANNEL CRACK AREA REPAIRED IAW CS DOC NO: CS 27062-014 AND RI-53-40-14956 REV ASDR UIEA2021092202076Channel · crackedM/D STA 900 TENSION TIE R/H AFT CHANNEL FOUND CRACKED. M/D STA 900 TENSION TIE R/H AFT CHANNEL CRACK AREA REPAIRED IAW CS DOC NO: CS 27062-014 AND RI-53-40-14956 REV A.SDR UIEA2021092202077Channel · crackedM/D STA 1060 TENSION TIE R/H AFT CHANNEL FOUND CRACKED. M/D STA 1060 TENSION TIE R/H AFT CHANNEL CRACK AREA REPAIRED IAW CS DOC NO: CS 27062-014 AND RI-53-40-14956 REV A.SDR UIEA2021092302078Channel · crackedM/D STA 1040 TENSION TIE R/H AFT CHANNEL FOUND CRACKED(<P>M/D STA 1040 TENSION TIE R/H AFT CHANNEL CRACK AREA REPAIRED IAW CS DOC NO: CS 27062-014 AND RI-53-40-14956 REV A</P>)SDR UIEA2021092302079Channel · crackedM/D STA 1020 TENSION TIE R/H AFT CHANNEL FOUND CRACKED. M/D STA 1020 TENSION TIE R/H AFT CHANNEL CRACK AREA REPAIRED IAW CS DOC NO: CS 27062-014 AND RI-53-40-14956 REV ASDR UIEA2021092302080Channel · crackedM/D STA 900 TENSION TIE L/H AFT CHANNEL FOUND CRACKED.(<P>M/D STA 900 TENSION TIE L/H AFT CHANNEL CRACK AREA REPAIRED IAW CS DOC NO: CS 27062-014 AND RI-53-40-14956 REV A</P>)SDR UIEA2021092302083Channel · crackedM/D STA 1080 TENSION TIE L/H AFT CHANNEL FOUND CRACKED(<P>M/D STA 1080 TENSION TIE L/H AFT CHANNEL CRACK AREA REPAIRED IAW CS DOC NO: CS 27062-014 AND RI-53-40-14956 REV A</P>)SDR UIEA2021092302084Channel · crackedM/D STA 1100 TENSION TIE L/H AFT CHANNEL FOUND CRACKED. M/D STA 1100 TENSION TIE L/H AFT CHANNEL CRACK AREA REPAIRED IAW CS DOC NO: CS 27062-014 AND RI-53-40-14956 REV ASDR UIEA2021092302085Channel · crackedM/D STA 1020 TENSION TIE L/H AFT CHANNEL FOUND CRACKED. M/D STA 1020 TENSION TIE L/H AFT CHANNEL CRACK AREA REPAIRED IAW CUSTOMER SERVICE REPAIR INSTRUCTION DOC NO: CS 27062-014 AND RI-53-40-14956 REV ASDR UIEA2021092302086Web · inadequateREFER TO EO: 4453A749-2, STA 2598 R/H B/H MOD WERE WEB INTERIM MOD AT UPPER RIGHT CORNER CUTOUT(<P>STA 2598 R/H B/H STRUCTURE MOD RIGHT UPPER CORNER CUTOUT EXISTING INTERIM MOD AREA REPAIRED IAW SB 747-53A2837 REV A FIG 30 AND EO 4453A749-2</P>)SDR UIEA2021092302097Tension Tie · crackedM/D STA 1100 TENSION TIE R/H 1EA CRACK WAS FOUND ON THE FIRST LAYER COUNTED FROM FWD APPROX 0.030" IN DEPTH FOUND CRACKED. M/D STA 1100 TENSION TIE R/H FWD DOUBLER P/N : A0911-313 FABRICATED AND REPLACED IAW IAI CUSTOMER SERVICE REPAIR INSTRUCTION DOC NO: CS 2SDR UIEA2021092402101Reveal · crackedM/D - L2 DR FWD CUTOUT FDW REVEAL LWR AREA FOUND CRACKED. M/D ENTER DOOR 2L FWD SURROUND STRUCTURE REPAIRED IAW RI NO: RI-53-00-14958 REV BSDR UIEA2021092602121Support Frame · damagedREFER TO EO 4453A749 PART 2, STA 2598 R/H SUPPORT FRAME MOD R/H FOUND EXISTING REPAIR PARTS WERE FOUND ON THE SB 747-53A2837 REV 0. MOD AREA(<P>EMP - STA 2598 R/H UPPER CORNER SUPPORT FRAME P/N : 65B02508-4 REPAIRED IAW RI-53-00-14986 REV A.</P>)SDR UIEA2021092602123Support · deformedAFT CARGO STA 1900-1920 R/H UPPER CEILING SUPPORT FOUND DEFORMED. AFT CARGO STA 1800-1920 RBL 96 CEILING CHANNEL P/N : 65B60847-25 ASSY REPAIRED IAW RI-53-00-15000 REV ASDR FDEA202110022446Web · damagedL1 DOOR CUTOUT, INNER WEB AT SNUBBER LOCATION IS DAMAGED DAMAGE BLENDED ON L1 DOOR CUTOUT WEB IAW B757-200 SRM 51-10-02 . ORIGINAL THICKNESS OF WEB IS .050 , REMAINING THICKNESS IS .025 , LOSS OF MATERIAL IS .025 FOUND TO BE OUT OF LIMITS IAW BAC DWG 141NSDR SWIA202163114None · cracked* R/H TRU BAY DOOR LANDING IS CRACKED AT THE AFT LATCH CUTOUT, MARKED. (C CHECK RO 12-19-21) REPLACED RH TRU BAY DOOR LANDING REF. CRJ700 SRM'S 51-42-06-001-001-A01 AND 51-42-13-001-001-A01, REO 670-53-11-1742 REV --, DATED: 2021-10-13 AND DWG CC670-33040SDR SWIA202163111None · cracked* TRU BAY FLOOR, R/H SIDE, HAS A CRACK AT THE AFT SIDE OF THE ACCESS DOOR OPENING, MARKED. (C CHECK RO 12-19-21) REPAIRED CRACKED R/H TRU BAY AREA IAW REO 670-53-11-1749 REV.-- DATED 2021-11-06. COMPLIED WITH TASK CARD 51-900-1002-SKYSDR SWIA202163110None · cracked* TRU BAY FLOOR, L/H SIDE, HAS A CRACK AT THE AFT SIDE OF THE ACCESS DOOR OPENING, MARKED. (C CHECK RO 12-19-21) REPAIRED CRACKED L/H TRU BAY AREA IAW REO 670-53-11-1744 REV.-- DATED 2021-11-05. COMPLIED WITH TASK CARD 51-900-1002-SKYSDR R61A2021102600829Stringer · corrodedWHILE IN HEAVY CHECK FOUND MAIN CABIN STRINGER 19R IS CORRODED BETWEEN FR 88 AND FR 89. REPLACED DAMAGED SECTION OF STRINGER19R AT FR 88-89 BY SPLICING REF ETD2021-170-33667 & E170 SRM 53-23-03SDR R61A2021102000818Doubler · gougedGOUGE IN EXTERIOR FUSELAGE SKIN FWD OF AND BELOW AFT.PASSENGER
DOOR @ FRAME 82 AND STRINGER 21L.PERFORMED PERMANENT REPAIR ON EXTERIOR FUSELAGE SKIN FWD OF AND BELOW AFT
PAX DOOR @ FRAME 82 AND STRINGER 21L
REPAIR DOUBLER AND FILLER REF: SRM 53--
23-01 REPSDR R61A2021102000103Doubler · gougedGOUGE IN EXTERIOR FUSELAGE SKIN FWD OF AND BELOW AFT PASSENGER
DOOR @ FRAME 82 AND STRINGER 21L.
PERFORMED PERMANENT REPAIR ON EXTERIOR FUSELAGE SKIN FWD OF AND BELOW AFT
PAX DOOR @ FRAME 82 AND STRINGER 21L
REPAIR DOUBLER AND FILLER REF: EMB175 SRM 53--
SDR JJBA20211001004None · noneCOCKPIT ENTRY FLOOR BEAM HAS SIGNS OF CORROSION, TOOLING MARKS AND INCORRECT NUT PLATE INSTALLED. REMOVED AND REPLACED DAMAGE PROFILE REINFORCEMENT AT COCKPIT ENTRY FLOOR BEAM. CORROSION LEVEL 2SDR JJBA20211001003None · noneCOPILOT SIDE SEAT TRACKS (INBD/OUTBD) FLOOR BEAMS SHOW SIGNS OF CORROSION. REMOVED CORROSION AND EVALUATED AREA FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER IND/OUT ISDE AT COPILOT SIDE SEAT TRACKS FLOOR BEAMS. INSTALL REPAIR DOUBLER. CORROSION LEVEL 2SDR SWAA2021100525608Seat Track · corrodedCABIN SEAT TRACK STA 847 LBL 45 WL 208 HAS CORROSION AT BASE DOT A-21-16 ; / [01] REMOVED DAMAGE AT BASE IAW 51-10-02-0G-0. USING 10X MAG; [02] VERIFIED STEP 1.; [03] VERIFIED LIMITS; LOSS 0.009' ON BASE MAX ALLOWED 0.040' I/A/W SRM 53-00-52-1A-1.<BR><BR>AAR TSDR CALA2021100101758None · corrodedAFT CARGO FR 61 ART STR 40 STRINGER CORRODED. (A3NB-53-4-6199). GENERATED BY N078592 AT HAECO LCQ PER NR 9294540 (28540). OCCURS FIRST. SUBSEQUENT INSPECTION INTERVALS AND INSPECTION MET HOD TBD. CURRENT PTT:77217 PTC:30071. MECH:V063868 INSP:LC119 REPAIRED STSDR SWIA202163310None · crackedANGLE BRACKET CRACKED FS 621 TO FS 625 AT RBL 14. (C CHECK RO 12/28/2021) REMOVED AND REPLACED R/H OBLIQUE ANGE BETWEEN FS 621 AND FS 625 AT STR 14R IAW CRJ 200 SRM 51-42-21SDR SWIA202163290None · corrodedAFT POTABLE WATER DRAIN DOUBLER CORRODED BETWEEN FS 605 AND FS 621, STGR 26R AND 25R. (C CHECK RO 12/28/2021) REPAIRED AFT POTABLE WATER DRAIN DOUBLER BETWEEN FS 605 AND FS 621, STGR 26R AND 25R BY REMOVING AND INSTALLING NEW SERVICABLE DRAIN MAST DOUBLER SDR SWIA202162782None · corrodedMAIN AVIONICS BAY FS310.00 CORRODED BETWEEN STR 27 AND STR 26R (C-CHECK RO 11-24-21) REPLACED MAIN AVIONICS BAY FS310 FRAME FROM STR 23L TO 25R, FRAME SPLICE AND STR 25R CLEAT REF CRJ700 SRM 53-00-06-201-006-A01. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GSDR SWIA202162780None · corrodedMAIN AVIONICS BAY FS295.00 FRAME CORRODED BETWEEN STR 26L AND STR 26R (C-CHECK RO 11-24-21) REPLACED MAIN AVIONICS BAY FS295 FRAME FROM STR 26L TO 26R AND 2EA FRAME SPLICES AND CLEATS REF CRJ700 SRM 53-00-06-201-006-A01. COMPLIED WITH 51-900-1002-SKY. LEAKSDR R61A2021102600828Beam · corrodedWHILE IN HEAVY CHECK FOUND MAIN CABIN CORROSION ON PASSENGER FLOOR STRUCTURE FR 17 CROSSBEAM INBOARD AND OUTBOARD OF RH SEAT TRACK BEAM, FABRICATED, LOCATED AND DRILLED L ANGLE REINFORCEMENT FOR PASSENGER FLOOR STRUCTURE FR 17 CROSSBEAM I/B AND O/B OF R/H SEATSDR R61A2021102600827None · corrodedWHILE IN HEAVY CHECK FOUND AFT CARGO CORRODED RH SHEAR CLIP, FR 75, STGR 29L-29R. REMOVED AND REPLACED RH SHEAR CLIP AT FR 75 STR 29L-29R. REF EMB SRM 51-40-08.SDR R61A2021102600826None · corrodedWHILE IN HEAVY CHECK FOUND AFT CARGO CORRODED RH SHEAR CLIP, FR 74, STGR 29L-29R. REMOVED AND REPLACED RH SHEAR CLIP,FR 74, STGR 29L-29R. REF EMB SRM 51-40-08SDR JJBA20210930050None · noneFWD FUSELAGE II DENTS FOUND ON LH LOWER SKIN BTW FR 10-11 AND BTW STR 20L-21L. FWD FUSELAGE II DENT FOUND ON LH LOWER SKIN BTW FR 10-11 AND BTW STR 20L-21L REPAIRED WITH DOUBLERSDR JJBA20210930007None · nonePILOT SIDE INBD AND OUTBD SEAT TRACK FLOOR BEAMS SHOW SIGNS OF CORROSION (FS9-FS10 4WD LBL12 AND LBL24). BLENDED AREA FOUND TO BE OUT OF LIMITS IN RIGHT SIDE INBD AND OUTBD SIDE TRACK PLACE BEAM. FABRICATED 2 REPAIR DOUBLER IN INBD AND OTBD SIDE. APPLIED ALODISDR CALA2021100101743None · corrodedAFT CABIN, R/H SIDE BETWEEN FR69-70 FRAME SUPPORT HAS HEAVY CORR OSION ON UPPER AND LOWER SURFACES IN SEVERA AND IS RUNNING UNDER SHEAR PLATE PER 9296979 / 30979 GEN V913126 REMOVED AND REPLACED FR69-70 FRAME SUPPORT STR23R IAW A320 SRM 5 1-72-11-911-001 BY MESDR CALA2021100101742Fitting · corrodedFWD CARGO DOOR SILL FR28 CORNER FITTING HAS CORROSION PER NR 929 2413 / 26413 A3NB-53-36105 GEN BY N061680. REMOVED AND REPLACED FORWARD CARD DOOR SILL AT FR28 STR39R CORNE R FITTING . IAW DWG C2D53231725 AND A320 200 SRM 51-42-11/001. M ECH V061680 INSP BY V0SDR CALA2021100101739Plate · corrodedR/H SHEAR PLATE FR69-70 CORRODED WITH 100% MATERIAL LOSS AROUND FASTENER HOLE PER NR 9296982 / 30982 GEN BY V061619 REMOVED AND REPLACED R/H FR69-70 STR23R SHEAR PLATE IAW A320 SRM 51-72-11-911-001 BY MECH V915153 INSP BY V901665SDR V0XD20211129001None · corrodedCORRORED ON TCAS ANTENNA DOUBLE IN MAIN AVIONICS BAY. CORRECTIVE ACTION REMOVED AND REPLACED TCAS ANTENNA DOUBLER (P/N: SH670-32364-7S) IN MAIN AVIONICS BAY IAW CRJ 900 SRM 51-42-06 AND SRM 51-42-21.SDR SWIA202162779None · corrodedCORROSION ON LOWER IMPACT ANGLE INSIDE FORWARD LAV WATER WASTE SERVICE DOOR SURROUND STRUCTURE (C-CHECK RO 11-24-21) REMOVED AND INSTALLED NEW IMPACT ANGLE REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-32280 REV H. COMPLIED WITH TASK CARD 51-900-1002-SDR SWIA202162778None · corrodedCORROSION ON LOWER DIAPHRAGM INSIDE FORWARD LAV WATER WASTE SERVICE DOOR SURROUND STRUCTURE (C-CHECK RO 11-24-21) REMOVED AND INSTALLED NEW LOWER DIAPHRAGM INSIDE FORWARD LAV WATER WASTE SERVICE DOOR. REF: CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-3228SDR SWIA202162431None · wrong partTHE WRONG PART WAS INSTALLED ON THE RAD ALT COVER AT FS 1031 (C-CHECK RO 11-05-2021) REPLACED DOUBLER WITH NEW. REF DRAWING MM670-35007 REV. W, CRJ 700 SRM 51-42-06-001-001-A01 & 51-41-02-001-001-A01. LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SKYSDR R61A2021101700806Gusset · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CFIII, GUSSET PLATE AFT FR90 RBL 25 CORRODED. CFIII, GUSSET PLATE AFT FR90 RBL 25 REPLACED IAW 51-41-02.
Back to JASC 5300