JASC 5330
Service difficulty reports · 79,329
Reports filed under 5330 · Fuselage Main, Plate/Skin, 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 = '5330' 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 = '5330' 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 DALA2019072204334Skin · dented(LOG 1179965) DURING INSPECTION FOUND FUSELAGE SKIN DENT WAS NOTED BETWEEN BS360-365, BETWEEN STR 28R-28L. ER/A 579622-14 SECTION I REPAIR WAS INSTALLED.SDR JGVR20190719002Skin · corrodedFOUND BUBBLING PAINT ON SKIN JUST OTBD OF RT NOSE CHIN FAIRING DURING TASK 53-10-00-2102. REPAIRED CORROSION ON RT FUSELAGE NOSE SKIN UNDERNEATH THE RT FWD FUSELAGE FAIRING(AFT OF FS 125 AND FS 136.20) IN ACCORDANCE WITH QRD ERO-959629 REV. IR, "LT/RT FORWARD SDR JGVR20190719001Skin · corrodedFOUND SUSPECTED LEVEL 1 CORROSION ON SKIN SURFACE JUST OTBD OF LT NOSE CHIN FAIRING DURING NLG AND NLG ACTUATOR HOUSING INSPECTION 53-10-00-2102. SUSPECT CORROSION FOUND TO EXTEND BENEATH FAIRING. REPAIRED CORROSION ON LH FUSELAGE NOSE SKIN UNDERNEATH THE LT FSDR SWAA2022031148512Skin · buckledSTA.887 BUTTSPLICE JOINT; FWD SKIN BUCKLED/BOWED APPROX. .100 AT REPAIR AREA. / REPAIRED PER EA 1-753-35242 (SEE ALL WIPS AND TASKS FOR INDIVIDUAL SIGN OFFS).SDR SWAA2019080835729Doubler · corrodedFUSELAGE CROWN DOUBLER PLATE CORRODED BETWEEN BS. 1036 TO BS. 1043, BETWEEN STR. 2L TO STR. 2R. / R&R DOUBLER PLATE IAW SRM AND DWG.SDR CALA2019072401252Skin · dentedFUSELAGE EXTERIOR SKIN LOWER LOBE FR25-26 STR 41-43 RT SKIN DENTED A3NB-53-3-6105 PER NON ROUTINE 9293391 DISCREPANT LOCATION SHOULD READ FR25-26, STR 42R-43R. ACCOMPLISHED INTERIM REPAIR PER ECRA 5331-02415 PART 1. ACCOMPLISH THE INITIAL INSPECTION REQUIREMENSDR K11A2019091172404Skin · corroded@ STA 1161, LAP SEAM STR 20L, EXTERNAL SKIN HAS AREA OF PULLING FASTENERS & PILLOWING SKIN.SDR AALA2019082629052Splice Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON INNER FUSELAGE SKIN BUTT SPLICE PLATE AT BS 887 AND S26L. REPAIRED BUTT SPLICE PLATE PER EA 296850.SDR ASAA2019071730145Skin · crackedDURING DAILY INSP FOUND 1 INCH LONG CRACK IN THE SKIN AT THE LAV WASTE VENT. UPON ACCESSING AREA FOR REPAIR FOUND INTERNAL DOUBLER CORRODED BEYOND LIMITS. GROUNDED - YES. REPAIRED IAW SRM 53-41-11-300-004. THIS IS A CATEGORY A REPAIR.SDR YENA201907170409Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION DAMAGE ON THE FWD FUSELAGE LOWER SKIN AT FRAME 34 AND BETWEEN STRINGERS 43L & 43R IN THE BELLY FAIRING AREA (SEE FIGURES 1 -6 OF THE REF /1/ REO). THE CORROSION DAMAGE WAS REMOVED AND AFTER BLEND OUT THE MATERIAL REMAINING SDR YENA201907170408Skin · corrodedDURING HEAVY MAINTENANCE, BELLY SKIN FR34 STR 43L 43R HAD CORROSION; (REF N/R# 44346 S/O 440594) REMOVED CORROSION ON BELLY SKIN FR 34 STR 43L AS PER SRM 51-74-00 MATERIAL LOSS FOUND TO BE BEYOND LIMITS IAW AMM SRM 53-21-11. REPAIRED FR 34 STR 43L 43R PER RESDR DALA2019071804290Skin · damagedSHIP 3870 A/C DAMAGE TO FUSELAGE AT FWD CARGO DOOR CUT OUT AFT SKIN . CORRECTIVE ACTION: REMOVED AND REPAIRED EXSITING RIVETS & HI LOKS FOR REPAIR DOUBLER'S CUT OUT DAMAGE PER SRM 53-00-01 REPAIR 24 . (1175945)SDR SWAA2019082036106Skin · damagedEXTERNAL 540 SKIN SPLICE DAMAGED FASTENERS AND SKIN DAMAGED FORWARD OF STA 500D, ABOVE AND BELOW STR. 21L. / REPAIRED SKIN IAW ER AND EA.SDR IPXA2019080535280Skin · damagedINSPECTION TYPE:4C, EXTERIOR FUSELAGE SKIN TRIPLER REPAIR IS DAMAGED AT AFT SIDE OF FWD LOWER CARGO DOOR CUT OUT.REPAIRED DAMAGED EXTERIOR FUSE LAGE SKIN AT STA. Y=1002 BETWEEN LONGERON 40R AND LONGERON 42R IAW VT-SAA EA 011-5330-01-A7845 REV. IR AND UPS EO MDSDR CALA2019071801210Plate · corrodedAFT CARGO PIT SKIN PLATE BETWEEN STRG 38R-39R IS CORRDED APPRX. 2" AFT FRAME 65 A3NB-53-3-6185 PER NON ROUTINE 9293158 ACCOMPLISHED REPAIR IAW ECRA 5331-02416 PART 1. ACCOMPLISH THE IN ITIAL INSPECTION REQUIREMENTS PER PART 2 OF ECRA 5331-02416 ON OR BEFORE THSDR CALA2019071801212Skin · dentedREF LOG PAGE 3639919 DENT FOUND CREASE OUT OF LIMITS RE-EVALUATE DENT AND POSSIBLE CREASE BELOW LH PAX WINDOW 2 STA897+ FR23-24 STR21-22L PER NON ROUTINE 9293275 DENT FOUND TO BE OUT OF LIMITS PER SRM 53-11-11-283-001 AND SRM 53-11-11-283-012 DIA 02. ACCOMPLISSDR DALA2019071704283Skin · corrodedCORROSION EXTERNAL SKIN LOCATED FR69 TO FR70 BTW STR31R TO STR32R AT L OWER FUSELAGE (1 EA). PERFORMED PERMANENT REAPIR ON EXTERNAL SKIN LOCATED FR 69 TO FR 70 BTW STR 31R TO STR 32R AT LOWER FUSELAGE AS PER SRM 53- 41-11-300-004.SDR SWAA2022031232244Skin · corroded***CORROSION*** ON EXTERIOR FUSELAGE FILLER SKIN JUST BELOW TOILET SERVICE DOOR AT L/H STA. 867 LBL 24; WL 160 / REPAIRED EXTERNAL SKIN JUST BELOW TOILET WASTE SERVICE DOOR BS 867 LBL 24 WL 160 IAW ATS ER 19-04146 REV IR DATED 6AUG2019 AND SWA EA 1-752-2594 RESDR SWAA2022031283801Skin · corroded***CORROSION*** UNDER VERTICAL STABILIZER; ALONG PERIMETER OF LH AND RH REAR SPAR STRUCTURAL SUPPORT ANGLES; APPROX. STA 1035-1076; LBL 11-RBL 9 (UPPER CROWN) - MARKED / CORROSION ALONG PERIMETER OF LH & RH REAR SPAR STRUCTURAL SUPPORT ANGLES AT BS 1035-1076; SDR DALA2019082805025Skin · dentedFUSELAGE SKIN, AT THE FWD CARGO DOOR CUTOUT, BS 440, STRINGER 23R DENTED. SET UP REPETITIVE INSPECTIONS IAW SRM 53-00-01, REPAIR 24, PARAGRAPH 5 A&B.SDR ASAA2019071530172Skin · corrodedFOR TRACKING PURPOSES ONLY: REF L/P 12004554, FOUND CORROSION ON FUSELAGE SKIN AT TOILET OUTFLOW VENT. GROUNDED - YES. REPAIRED DAMAGED TO FUSELAGE SKIN IAW SRM 53-70-01-2R-3 REP 3, FOR ALL PARTIAL WORK ACCOMPLISHED SEE N/R-00001 S/N 7069107 W/O 1017101 2000/0SDR SWAA2022031232222Scuff Plate · crackedAFT CARGO AFT SCUFF PLATE IS CRACKED / LOCATED AND DRILLED NEW SCUFF PLATE PO# 756860/2 AFT CARGO AFT SCUFF PLATE PER SRM 51-40-05 AND DWG 146A8340 PART WILL BE INSTALLED ON CUSTOMER CARD 753-140-00-02YSDR SWAA2022031232223Scuff Plate · crackedAFT CARGO FWD SCUFF PLATE CRACKED / AFT CARGO FWD SCUFF PLATE PN # 7530659 IS LOCATED AND DRILLED IAW SRM 51-40-02-0G-0 AND SRM 51-40-08-0G-0 SCUFF PLATE WILL BE INSTALLED ON CARD # 763-140-00-02YSDR ASMF20190816003Skin · dentedDURING OVERNIGHT CHECK, MAINTENANCE PERSONNEL DETECTED A DENT ON FUSELAGE LOWER SKIN SECTION 46 STA 806, BETWEEN STRINGERS 27L, 27R AND BL-0 OF 9” L, 2.5” W, 0.0455” Y; INSPECTION PERSONNEL EVALUATED THE DAMAGE AND FOUND OUT OF LIMITS IAW SRM 53-00-01 ALLOWABLSDR HNAA2019080800222Skin · crackedFUSELAGE UPPER SKIN CRACKED 2 PLACES,SKIN CRACK 1:ON FRAME 75 AT PREVIOUS REPAIR ON FIRST FASTENER BELOW STR 2L. SKIN CRACK 2: ON STR 2L JUST AFT OF FRAME 75....FIX: COMPLETED REPAIRS ON CRACKS AT LH FR75 AT STR 2L IAW EMB SRM 53-31-01 AND EO1-53-19-0322. NOSDR HNAA2019080800219Skin · crackedFUSELAGE SKIN CRACKED AROUND RIVET AT FRAME 77 BETWEEN STR3R-4R....FIX:ACCOMPLISHED REPAIR OF SKIN CRACK AT FR77 BETWEEN STR 3R-4R IAW SRM 53-22-01 AND E01-53-19-0323.SDR HNAA2019080800218Skin · crackedFUSELAGE SKIN IS CRACKED AROUND RIVET AT FRAME 77 BETWEEN STRINGERS 5R-6R. ACCOMPLISHED REPAIR OF SKIN CRACK ON FR77 BETWEEN STR 5R AND 6R IAW SRM 53-22-01 ITEM 9. AND EO1-53-19-0323.SDR HNAA2019080800217Skin · crackedFUSELAGE UPPER AFT SKIN CRACKED ON FRAME 75 AT FIRST FASTENER HOLE BELOW STRINGER 2R. COMPLETED REPAIR OF CRACKS AT RH FR 75 AT SYR 2 IAW SRM 53-31-01 AND EO1-53-19-0321SDR DALA2019071304240Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN BTW STA 1087 STRINGERS 13 AND 15R SIDE (SM). NRC 00158: SKIN BTW STA 1087 STRINGERS 13 AND 15R SIDE WAS REPAIRED PER ER/A :579571-14 REV ORIGINAL. ASSOCIATED ER/A 14-579571 ADDED FOR AC 9504. (LP #1168668)SDR CALA2019071501196Skin · dentedB757-06-3-0380 EXTERNAL FUSELAGE REPAIR HAS DENT AT APPROX. STA 612,ON STGR 17L,16-6 REF. ST. ENGINEERING N/R 0065099 INITIATE A DTA DIP/LP TO ACCOMPLISH INSPECTION REQUIREMENTS ON O R BEFORE THE A/C REACHES 67600 TOTAL A/C FLIGHT CYCLES. PLANNING TO CONTACT ESDR ASOA201907137071Skin · corrodedTYS A/C IS IN C-CHECK WHEN INSPECTION FOUND CORROSION DAMAGE TO THE FUSELAGE SKIN AT FRAME 81 AND STRINGER 21L TO 21R. MAINTENANCE REMOVED THE CORRODED AREA AND APPLIED A FILLER AND DOUBLER IAW ETD 2019-145-086179. ALL WORK ACCOMPLISHED AND WILL BE RELEASED ATSDR SWIA2019091246278Skin Panel · dentedDENT TO THE FUSELAGE SKIN PANEL .408" LENGTH X .398" WIDE X .031" DEEP AT FUSELAGE FRAME FS 589.00 BETWEEN STGR 19L - 20L. (C-CHECK) RO: 09/12/2019 REPAIRED DENT TO FUSELAGE SKIN PANEL @ FS 589.00 BETWEEN STRINGER 19L - 20L IAW REO.SDR IPXA201908145584Skin · chafedMAIN CABIN CREW ENTRY DOOR CUTOUT FAIL SAFE RING EXTERNAL SKIN CHAFE AT UPPER AFT CORNER. REPAIRED MAIN CABIN CREW ENTRY DOOR CUTOUT FAIL SAFE RING EXTERNAL SKIN IAW EO A300-5330-73446-A AND EA 300-5330-01-A7849 IR. (MINOR)SDR DALA2019071304236Skin · corrodedSEVERAL CORROSION POINTS ON FUSELAGE SKIN BTW STA Y=794 TO Y=851 BTW LONG 26L TO 26R AT FILLET PANELS AREA IN REF 5315-2001. (FUS). NRC 00420: CORROSION LEVEL 2, AREA WAS REPAIRED PER ER/A 579396-14 REV ORIGINAL SECTION I AND SECTION II. ASSOCIATED ER/A 00-579SDR SIMA20190711004Skin · crackedDURING HMBV INSPECTION, QC FOUND 2 CRACKS AROUND RIVETS ON RT REAR FUSELAGE I SKIN AT FR 75 BELOW STR 2R. AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. C/A-PERFORMED PERMANENT REPAIR TO CRACKS ON RSDR SWAA2022031167239Scuff Plate · crackedFWD CARGO FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED FORWARD CORNER SCUFF PLATE IAW E.A. 1-A53-2076 REV 11SDR SWAA2022031167240Scuff Plate · crackedFWD CARGO AFT CORNER SCUFF PLATE CRACKED / REPAIRED AFT CORNER SCUFF PLATE IAW E.A. 1-A53-2076 REV 11SDR CALA2019071401191Skin · crackedSUPPORT TASK EA5380-01178 REV A RT BETWEEN STA1640 AND 1654 STR FUSELAGE SKIN FOUND 2EA CRACKS AS MARKED. REF NR LP 9130486 REPAIRED PER SRM 53-80-01 REPAIR 7. REPAIR ACCOMPLISHED HKG NR# UNJ504874. PER SRM 53-80-01 REPAIR 7 PARA 5A. INITIAL INSPECTION THRESHOSDR DALA2019071104150Finger Doubler · corrodedINITIAL INSPECTION. CORROSION ON FINGER DOUBLER BTW STA Y: 585 TO Y: 570, S26L AT FWD CARGO COMPARMENT. FINGER DOUBLER WAS REPLACED PER SRM 51-00-07-0G, PAR. 5. CORROSION LEVEL 2. (LP1164589)SDR SIMA20190710001Skin · dentedDURING HMBV INSPECTION, QC FOUND A DENT ON UPPER FUSELAGE SKIN BETWEEN FR 68-69, STR 2R-3R. DENT OIL CANNED AFTER RECONTOUR. AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER HMBV INSPECTION. C/A-PERFORMED PERMANENT RSDR FDEA201907091513Skin · dentedLT FUSELAGE OUTER SKIN AT FS 215 AROUND S-21L HAS A DENT. EVALUATED DENT ON SKIN STA. 215 AROUND S-21L A\Y FOUND TO BE IN LIMITS IAW SRM 53-00-01-1A. HFEC IAW NDTM PT6 51-00-19 CRACK NOTED. CUT OUT DAMAGED AREA, FABRICATED DOUBLER, AND INTALLED DOUBLER IAW SRMSDR ABXA20190709123Skin · corrodedCORROSION ON THE FUSELAGE SKIN AT FUSELAGE STATION 955, STRINGER 23R. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA20190709120Skin · damagedDAMAGE IN THE FUSELAGE SKIN AT FUSELAGE STATION 266, STRINGER 34L. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA20190709119Skin · corrodedCORROSION ON THE FUSELAGE SKIN AT FUSELAGE STATION 786, STRINGER 38R. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR A6WA2019071046694Skin · dentedAIRCRAFT SKIN HAS TWO PROTRUDING DENTS BETWEEN FS 621-640 AND IN BETWEEN STRINGERS 25L AND 26L. REPAIRED SKIN BETWEEN FS 621-640 BETWEEN STRINGER 25L AND 26L IAW EA# AWAC-CRJ253-01271.SDR FXGA201907091953Skin · corrodedFUSELAGE SKIN CORRODED ABOVE FORWARD BAG PIT DOOR. TO REPAIR CORRODED FUSELAGE SKIN ABOVE FORWARD BAG PIT DOOR, AT F/STA 162 BETWEEN STRINGER 23R & 24R. CUT-OUT DAMAGE AND REPAIR SKIN PER EAC EO 0502.SDR SWAA2022031103769Skin · crackedLOWER AFT CORNER OF EXTERNAL POWER CUTOUT HAS A CRACK ABOUT .190' IN LENGTH. / REMOVED DAMAGE PER SRM 53-10-15-1A-4SDR SWAA2022031160555Plate · corroded***CORROSION*** ON HINGE CLOSEOUT PLATE AT CUTOUT FOR TOILET SERVICE DOOR (145AL) - MARKED / ACCOMPLISHED REPAIR EA 1-752-2595 REV IR AND ER 19-04268 REV IR.SDR MK1Y20190902022Skin · corrodedFOUND CORROSION DAMAGE ON THE FUSELAGE INNER SKIN, STA 1141, STR 37L TO STR 37R, CCOMMON TO EXISTING REPAIR.SDR MK1Y20190902021Skin · damagedFOUND NICKS SCRATCHES AND BLEND OUTS ON FUSELAGE EXTERNAL SKIN STA 196 TO STA 246 STR 13L TO STR 21R.
Back to JASC 5330