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 ASAA2025042257699Skin · corrodedSIGNS OF CORROSION FOUND AT STR 10 R/H BETWEEN STA 727A AND STA 887. SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" REPAIR ON FUSELAGE SKIN PN# 146A3131-10, 146A3151-94 BETWEEN STA 727A AND STA 887 AT STR 10 R/H IAW EA# 800-53EA-28658 REV00.SDR CALA2025042804270Skin · damagedPOSSIBLE LIGHTNING STRIKE DAMAGE FOUND AT APROX. BTW STA 632, APROX. BTW S-32R & S-31R. ACCOMPLISHED DVI PER STEP 6. A) PER A.V.O. 14441, REV A. FOUND BOTH FASTENER HOLES AT STA 632 BY S-32-R TO HAVE FRAYED COMPOSITE MATERIAL AT THE COUNTERSINK AREA OF REMOVESDR JIKA2025042501Lap Joint · corrodedDURING A 4YR HEAVY SCHEDULED INSPECTION AT WORLDWIDE AIRCRAFT SERVICES CORROSION BEYOND ALLOWABLE LIMITS WAS DISCOVERED ALONG THE UPPER RH FUSELAGE LAP SEAM BETWEEN FS 450 - FS 570. REPAIRS TO THE DAMAGED AREA WILL BE MADE IN REFERENCE TO SAAB STATEMENT TO OPESDR DALA2025042403189Skin · wornWEAR ON SKIN BTW STA Y=994 L24R TO L26R (AFT EDGE CUT OUT) AT AFT CARGO DOOR. WORN SKIN BTW STA Y=994 L24R TO L26R (AFT EDGE CUT OUT) AT AFT CARGO DOOR WAS REPAIRED PER PRI 625059-14 REV 7 AND ER/A 625059-14 REV ORIGINAL SECTION I: PERMANENT REPAIR.SDR DALA2025042303169Doubler · corrodedCORROSION ON INTERNAL DOUBLER AND ON INNER SIDE OF WASTE SERVICE PANEL BTW STA Y=1022 AND STA Y=1037 BTW LONG 23L AND LONG 25L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00232: CORROSION LEVEL 2. INTERNAL DOUBLER AT INNER SIDE OF WASTE SERVICE PANEL BTW STA Y=10SDR UIEA2025041400458Skin · dentedLOWER EXTERNAL FUSELAGE AT STA 893 BETWEEN STR 24R AND 25R SKIN WITH DENT.(<P>REPAIRED FUSELAGE SKIN SECTION FROM STA 887.75 TO STA 900 BETWEEN STR 23R AND 26R I/A/W COOPESA COO-EO-2025-22084-R00 REV: 00 DATED: MAR 27-25 AND BOEING MESSAGE COO-TLS-0049-03B DATSDR UIEA2025041600483Skin · damagedUPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 328.5 AND STR2R + 3.750", SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) I/A/W B737-800 SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP(1) THRU (5)(6) (PROTRUDING HESDR UIEA2025041600484Skin · damagedUPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 283 AND 5" BELOW STR 2R SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) I/A/W B737-800 BCF SRM 53-00-01-2R-38, REPAIR 38 PARG 4E STEP (1) THRU STEP(5) (6)(PROTRSDR UIEA2025041600485Skin · damagedUPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 284 AND 4.5" BELOW STR 2L SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) I/A/W B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP(1) THRU STEP (5)(6)( PROTSDR UIEA2025041600486Skin · damagedUPPER FUSELAGE EXTENAL SKIN SECTION AT STA 500E + 10.250" AND 2.5" BELOW STR-2L SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) I/A/W B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP(1) THRU STEP (5)SDR UIEA2025041600487Skin · damagedUPPER FUSELAGE EXTENAL SKIN SECTION AT STA 590 AND 1.5" ABOVE STR-3R SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) I/A/W B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP(1) THRU STEP (5)(6)( PROTRUSDR UIEA2025041600488Skin · damagedUPPER FUSELAGE EXTENAL SKIN SECTION AT STA 649" AND 2.250" ABOVE STR-1R SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) I/A/W B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP(1) THRU STEP (5)(6)( PROSDR UIEA2025042100553Skin · damagedUPPER FUSELAGE EXTENAL SKIN SECTION AT STA 819.5 AND STR-14R SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) IAW B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP (1) THRU STEP (5)(6) (PROTRUDING HEADSDR UIEA2025042100554Skin · damagedUPPER FUSELAGE EXTENAL SKIN SECTION AT STA 778.5 AND STR-1 + 2.750 INCH R, SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) IAW B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP (1) THRU STEP (5)(6) (PSDR UIEA2025042100555Skin · damagedUPPER FUSELAGE EXTENAL SKIN SECTION AT STA 620 AND 1 INCH BELOW STR-3L SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) IAW B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP (1) THRU STEP (5)(6)( PROTRSDR REXA2026072801219Skin · wornWEAR ON EXTERNAL FUSELAGE SKIN BTW BS 881 TO 913, BTW STGR 27 TO STGR 26LH WEAR ON EXTERNAL FUSELAGE SKIN BTW FS 881.00 TO FS 913.00, BTW STGR 27 TO STGR 26LH WAS REPAIRED PER EA CRJ953-19152 REV. IRSDR SWIA202507170421Doubler · chafedTHE FWD ATG ANTENNA ETERNAL DOUBLER WHERE ANTENNA ATTACHES IS CHAFED. (C-CHECK RO 07/16/2025)PERFORMED FWD ATG ANETNNA DOUBLER. REF CRJ900 SRM 51-40-06-001-001-A01 , REF CRJ900 SRM 51-42-20-001-001-A01 AND PER GOGO D12938-20210 REV D. COMPLIED WITH TASK CARDSDR IPXA2025052564732Skin · crackedTWO CRACKS FOUND INSIDE HOLE T ON FR47 RH HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII SDR SIMA20250421003Skin · dentedREAR FUSELAGE HAS DENT AT FR99/100 STR 2R/3R (MAJOR REPAIR) CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW ERS-EJ-53MR-5185 R1SDR DALA2025042403229Skin · corrodedWHILE ACCOMPLISHING DVI OF DOUBLER EDGE AROUND WASTE BOX CUT-OUT , FOUND CORROSION ON AFT INBOARD CORNER. (REF CC# 171-0784323) . REMOVED AND REPLACED WASTE BOX CUT-OUT DOUBLER. IAW BOMBARDIER DWG C01342100 REV-T AND A220 ASRP BD500-A-J51-42-21-00AAA-078A-A. (SDR DALA2025042403227Skin · corrodedFUSELAGE SKIN HAS CORROSION AROUND THE FORWARD PASSENGER DOOR SCUFF PLATE ATTACH FASTENER HOLES 6OL, 8OL . SUMMARY SEE NR FOR ADDITIONAL INFORMATION 038-0001:5331-01297- 01A/001 00181 REPAIRED PER PRI 625637-14 REV 0, PRI 625637-14 REV 1, PRI 625637-14 REV 2, SDR DALA2025042403226Skin · corrodedFUSELAGE SKIN HAS CORROSION AROUND THE AFT CARGO DOOR LOWER SCUFF PLATE ATTACH FASTENER HOLE 6OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 016-0001:5331-01297- 02C/001 00180 REPAIRED PER PRI 625644-14 REV 0, PRI 625644-14 REV 1, PRI 625644 REV 2, AND FINAL ERSDR CALA2025042304161Skin · chafedREF. N/R 39049 (REWORK PER E/A 5300-02120 OP1 STEP 4.1) AREA REW ORKED ON N/R 39049 RQUIRES EVALUATION OF LIMITS AND REPAIR. REPAIRED CHAFE MARK ON FUSELAGE EXT SKIN FR 34 STGR 43L-43R. REC EIVED ECRA 5321-02162 THAT PROVIDES PERMANENT REPAIR INSTRUCTION S FOSDR R61A2025042100198Doubler · corrodedDURING HEAVY CHECK CF III FOUND CORROSION ON INNER DOUBLER AT WASTE DOOR CUT-OUT FR88 BETWEEN STR 27-28 R/H. REMOVED AND REPLACED INNER DOUBLER WASTEWATER DOOR CUT OUT IAW SRM51-43-03SDR VNAA20250528006Skin · corrodedWEAR ON SKIN PANEL LOWER SECTION OF FUSELAGE BTW FS 910.00/919.00 STGR 27/26RH. BLENDED OUT ON SKIN PANEL LOWER SECTION OF FUSELAGE BTW FS 910.00/919.00 STGR 27/26RH WAS PERFORMED PER CRJ-900 SRM 51-12-00-001-001-A01 AND EVALUATED, THEREFORE IS WITHIN LIMITS ISDR ASAA2025042057698Skin · corrodedWATER SERVICE PANEL HAS CORROSION ON THE SKIN ON FWD SIDE BETWEEN STR-25R AND STR-26R. SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY "B" REPAIR ON FUSELAGE SKIN PN: 147A3400-4 AT WATER SERVICE PANEL CUT-OUT AT STA STA 907-927 BETWEEN STR 25R AND STR 27 R IAWSDR ASAA2025042057646Skin Panel · corrodedRIGHT SIDE OF AIRPLANE AT STR-23R BETWEEN STA-727H AND STA727F HAS CORROSION IN SEVERAL PLACES. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" REPAIR ON FUSELAGE SKIN P/N # 146A3251-32 AT STR23R BETWEEN STA727F AND STA 727H IAW EA # 800-53EA-28608 REV 00.SDR ASAA2025042057602Skin Panel · corrodedCORROSION ON THE SKIN AT STR-23L FROM STA-787 TO STA-887 SEVERAL PLACES. SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR TO FUSELAGE SKIN PANEL 146A3201-32 BETWEEN STA 807-827 STGR 23L IAW EA 800-53EA-28614 REV00. NO CORROSION NOTED BETWEEN STA SDR ASAA2025042057601Skin Panel · corrodedCORROSION ON SKIN AT STA-927 BETWEEN STR-24L AND STR-25L. SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEFORY A MINOR REPAIR TO FUSELAGE SKIN PANEL 147A3400-4 AT STA 927 BETWEEN STGR 23L-25L IAW EA 800-53EA-28595 REV00. SRXR430X.SDR ASAA2025042057600Skin Panel · corrodedHOT WATER DRAIN BETWEEN STR-24L AND STR 25L HAS CORROSION AT THE BASE ON INBOARD SIDE. SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR TO FUSELAGE SKIN PANEL 147A3400-4 AT I/B SIDE OF HOTWATER DRAIN BETWEEN STA 986.5-1016 STGR 24L-25L IAW EA 800SDR DALA2025042403224Skin · corrodedFUSELAGE SKIN HAS CORROSION AROUND THE FORWARD CARGO DOOR LOWER SCUFF PLATE ATTACH FASTENER HOLES 18OL. COMPLIED WITH ER/A 625638-14 REV. A PRI REV. 0 AND FINAL ER/A 625638-14 REV. A SECTION I. (LP# 0923463)SDR CALA2025042104054Skin · scratchedFOUND SCRACH LINE ON EXTERIOR FUSELAGE R/H BTW STA.400 AND STA. 420 AND S-14R. PERFORMED REPAIR PER EO 250100 REV P1, P2, P3, P4, P5, AND P6 IAW EO 250100 REV IR AND EC/RA 5330-07509. REF ELB LOGS 4571389 AND 4571342 FOR DIP REQUIREMENTS PER ECRA5330-07509.SDR SWIA20250613419Skin · corrodedUPON REMOVAL OF THE APU AFT SHIELD ASSEMBLY, 8 SPOTS OF PITTING CORROSION/CHAFFING DAMAGE WERE FOUND ON THE EXTERNAL FUSELAGE SKIN AT THE MOUNTING POINTS AT VARIOUS LOCATIONS FROM FS 682.00 +10 €“ FS 700.00 IN BETWEEN STR12R-STR15R. (C-CHECK RO 06/12/2025)UPOSDR CALA2025042104053Skin · corrodedAFT R/LWR FUSELAGE LAV SERVICE ACCESS PNL 166AR SKIN AROUND IT BOWED OUT. ESFR REPORTING FOR MAJOR REPAIR REF ECRA 5360-01946 TO LAV SERVICE PANEL ACCOMPLISHED REPAIR ON FUSELAGE SKIN AROUND LAV SERVICE ACCESS PANEL 166AR PER ECRA 5360-01946. REF ST NR 122227.SDR SWIA2025082500418Skin · dentedEXTERNAL FUSELAGE FS394 @ APPROXIMATLY STG17L DENTED, HN235814 (C-CHECK RO 8/21/2025) INSTALLED REPAIR PARTS ON EXTERNAL FUSELAGE FS394 @ APPROXIMATLY STG17L REF CRJ 900 SRM 51-42-21-001-001-A01 AND REO 690-53-21-1979, REV --, DATED ON 2025-07-07,PRSDR SWIA20250603.418Skin · gougedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA86155-ETD2023-170-020925-PR1 - TEMPORARY REPAIR OF GOUGE AND 2 DENTS ON PERFORMED ON LH FWD FUSELAGE BETWEEN STGR17L-18L AND FR10-11. PERFORM PERMANENT REPAIR FROM SECTION C. OF ETD2023-170-020925 REV /: DATED AUGUST 2SDR IPXA2025052534907Skin · crackedCRACK FOUND IN FASTENER HOLE ON BULK CARGO DOOR SCUFF PLATE. AREA MARKED IN RED. ACCOMPLISHED E.A.#: 300-5317-27-A3915, PRELIMINARY 1, STEP# 2: "INCREMENTALLY REAM THE 1 EACH CRACKED HOLE IN STEPS OF 0.4 MM UNTIL DAMAGE FREE AND ROUND CONDITION ACHIEVED OR MAXSDR VNAA20250602020Skin · damagedPERMANENT REPAIR OF THE PAX DOOR CUTOUT LOWER FWD CORNER ACCOMPLISH PERMANENT REPAIR PER REO 690-53-21-1441. PAX DOOR CUT OUT LOWER FWD CORNER WAS REPAIRED PER CRJ-900 SRM 53-21-01-201-010-A01.SDR VNAA20250529009Skin · corrodedCORROSION DAMAGE TO FUSELAGE SKIN BETWEEN FS280.00-FS295.00 AND STR24R-STR25R. CORROSION DAMAGE TO FUSELAGE SKIN BETWEEN FS280.00-FS295.00 AND STR24R-STR25R WAS REPAIRED PER REO 690-53-21-1933 REV. - - .SDR VNAA20250528004Skin · dentedDENT ON EXTERNAL SKIN BTW FS295.00 TO FS 310.00 AND STGR 19RH TO STGR 20RH AT FWD FUSELAGE. DENT ON EXTERNAL SKIN BTW FS295.00 TO FS 310.00 AND STGR 19RH TO STGR 20RH AT FWD FUSELAGE WAS REPAIRED PER REO 670-51-00-085 REV.-A AND PER REO 690-53-21-1941 REVSDR SWIA202505200418Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA85288-ERJ 175 SRM TOPIC: 51-75-16 MXCODEID68878-PR - FOUND DENT ON FWD LH SIDE FUSELAGE AT STGR 15L AND FR11 UNDER THE SKYWEST LOGO. DENT IS FOUND TO BE WITHIN LIMITS PER ERJ 175 SRM 53-00-00/AD02 TABLE 102. THE DENT ISDR SWAA2025052058345Skin · debondedPANEL 194FR OUTER SKIN IS DISBONDED. (MARKED)<[01] PANEL 194FR OUTER SKIN DIS BOND WAS REPAIRED IAW SRM 51-70-05-2R-2;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR CALA2025042804268Skin · damagedPOSSIBLE LIGHTNING STRIKE DAMAGE FOUND AT APROX. BTW STA 609+216, APROX. BTW S-35R & S-34R.SEE PIC ACCOMPLISHED DVI PER STEP 6. A) PER A.V.O. 14441, REV A. FOUND THREE FASTENER HOLES AT STA 609+216 BY S-34-R TO HAVE FRAYED COMPOSITE MATERIAL AT THE COUNTERSINSDR R61A2025042100197Skin · dentedBIRD STRIKE FWD FUSELAGE BETWEEN FRA1 AND FRA 2 BETWEEN STR 12L TO 18L.PERFORMED REPAIR IAW ETD2025-170-906422, INSTALLED FILLER AND DOUBLER. ALSO REF VP-016675-2025 N/R #1 FOR WORK ACCOMPLISHED.SDR CALA2025041804031Skin · damagedLIGHTING STRIKE DMG'S NOTED ON LP 4523702 (REF ECRA 5310-08557) REQUIRE UAL QC RE-EVALUATION AT FIRST OPPORTUNITY WHERE GND TIME ALLOWS - NOT TO EXCEED 5 CYCLES. PER GMM 06-35-05 - LIGHTING STRIKE DMG'S NOTED ON LP 4523702 (REF ECRA 5310-08557) REQUIRE UAL QC SDR UIEA2025032700391Skin · damagedFUS SECTION 48 APPROX STA 2658 - STA 2701, WL 280-WL 340 AREA FOUND FUS SKIN SEVERAL RIVETS LOOSE(<P>SKIN REPLACED AS PER RI-53-80-17492 REV B. NO FURTHER DEFECTS NOTED</P>)SDR N6WA2025041803Skin · dentedDENT IN LH FUSELAGE SKIN AT FS549 BETWEEN STRINGER 16L AND STRINGER 17L. REPAIRED DENT ON LH FUSELAGE SKIN AT FS 545 BETWEEN STRINGERS 16L AND STRINGER 17L IAW EO-C550-53MR-067-O AND AWATS EO-25-CRJ5-53-074.SDR 2025FA0000493Stiffener · crackedFUSELAGE AFT LWR SKIN, STIFFENER CRACKED.SDR VNAA20250602001Skin · dentedSEVERAL DENTS ON EXTERNAL FUSELAGE SKIN BTW FS 1181.00 TO FS1211.00 OF THE AREA COVERED BY LH/RH VENTRAL FIN FAIRING DENTS ON EX•TER NAL FUSELAGE SKIN BTW FS 1181.00 TO FS1211.00 OF THE AREA COVERED BY LH/RH VENTRAL FIN FAIRING WERE REPAIRED PER REO 690-53-7SDR REXA2025052200593Skin · damaged"MR 25425 LOCATE THE REPAIR ON THE AFT LH FUSELAGE LOCATED BELOW THE HP DOOR, BETWEEN FS1108.00 - FS1126.00 AT S21L. REMOVED PREVIOUS REPAIR IAW CRJ700 SRM 51-42-21-001-001-A01. PERFORMED EDDY CURRENT ON FUSELAGE SKIN AND DOUBLER BETWEEN FS1116-FS1126 STRINGE
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