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 JGVR20190522002Skin · corrodedREPAIRED NUMEROUS AREAS ON LOWER FUSELAGE SKIN, DOUBLERS, AND STRINGERS OF THE DROP AISLE AREA BETWEEN FS 157 AND FS 426 BY BLENDING OUT CORROSION, PERFORMING NDT AND INSTALLING DOUBLERS AND FILLERS AS REQUIRED PER RESEARCH AND DEVELOPMENT MRO ENGINEERING REPASDR SWAA2022030806523Skin · corrodedEXTERNAL FUSELAGE SKIN UNDER ADF ANTENNA STA 663+10 - 706 BETWEEN STR 1-2R HAS CORROSION AROUND FASTENER HOLES / REMOVED CORROSION ON EXTERNAL FUSELAGE SKIN UNDER ADF ANTENNA STA 663 + 10' TO STA 706 BETWEEN STR 1 AND STR 2R IAW SRM 51-10-02-0G-0. VERIFIED ALLSDR CA190527003Skin · corroded(CAN) CORROSION IN FUSELAGE SKIN BTW FS605-621 AND STR25R-26R. (TC# 20190527003)SDR DALA2019111436666Skin · damagedLIGHTNING STRIKE ON SKIN @ STA 522, O/B STR 39R. REPAIRED PER SRM 53-00-01. (LP 085148)SDR DALA2019111436665Skin · damagedLIGHTNING STRIKE ON SKIN @ STA 654A+30, O/B STR 39R. REPAIRED PER SRM 53-00-01. (LP 1085131)SDR SIMA20190521003Skin · damagedTRANSFERRED FROM AML PAGE 4391436 ITEM 2" SEE ITEM 1 LOGPAGE 4391435FOUND DAMAGE BETWEEN FRAME 61-64 AND STRINGER 19L AND 20L. MULTIPLE DENTS AND SCRATCHES NOTED. INSPECTED AND FOUND INTERNAL STRUCTURE TO BE A SERVICEABLE CONDITION . MAJOR REPAIR-C/A-REPAIRED SDR DALA2019052203261Skin · damagedSHIP 667 PER ERA 573682-14 SECTION II PERMANENT REPAIR IS REQUIRED. CORRECTIVE ACTION: REPLACED DAMAGE SKIN AREA FROM STA 610 TO STA 660, FROM S-14L TO S-19L IAW SRM AND ERA 573990- 14 REV C. REPLACED STRINGER FROM STA 530 TO STA 630 IAW SRM. INSTALLING ILLUMISDR IPXA2019052542466Skin · corrodedINSPECTION TYPE:C12 CORROSION ON FUSELAGE SKIN NEAR STA 655, S-34L - S-35L. REPAIR IAW SRM 53-00-01 ALLOWABLE DAMAGE 1, REV 74.00.SDR IPXA2019052542465Skin · corrodedINSPECTION TYPE:C12 CORROSION ON FUSELAGE SKIN NEAR STA 654 PLUS 128, S-34L - S-35L. REPAIR IAW SRM 53-00-01 ALLOWABLE DAMAGE 1, REV 74.00.SDR CALA2019052400817Skin · crackedA3NB-533-6315: FR 35 STR 30L, FOUND HOLE #2 TO HAVE CRACK INDICATION IN SKIN LAYER, IN THE 12 O'CLOCK DIRECTION AS VIEWED FROM OUTSIDE AND 2 CRACK INDICATIONS IN THE SIDE SHELL LAYER AT 12 O''CLOCK AND 5 O'CLOCK DIRECTION - ON N/R 9298541 REPAIRED LT FR35 HOLESDR DALA2019052203131Skin · cracked(LOG 1084852) DURING INSPECTION FOUND CRACK ANGLE BS500H AND STR 26R AT FWD CARGO COMPARTMENT. PERFORMED REPAIR ON EXTERNAL SKIN BS 196.5 AND LBL 4 AT LOWER FUSELAGE AS PER ER/A NO 577610-14 REVISION ORIGINAL AND PRI NO 577610-14 REVISION 0,1,2 AND 3.SDR IPXA2019052142335Skin · dentedINSPECTION TYPE:M1 AGING INSPECTION - EXTERNAL SKIN AT STA 700, APPROX. STR 7L( JUST ABOVE THE LETTER S) AREA ON SIN HAS A SHARP PROTRUDING DENT, NO DOC. ON ADMREPAIRED PER EA #757-5330-27-A2345.SDR IPXA2019052142332Skin · dentedINSPECTION TYPE:SEG AGING INSPECTION - RT FUSELAGE AT STA 740, STR 24 AND 25R HAS A SHARP PROTRUDING DENT, NO DOC ON ADMREPAIRED PER SRM 53-00-01-2R-29.SDR SWIA2019070346033Skin · dentedFUSELAGE EXTERIOR SKIN DENT BETWEEN FS235 €“ FS250 STR14L AND STR15L QTY 2. (C-CHECK) RO: 07/02/2019 THE 2EA DENTS LOCATED ON THE EXTERIOR FUSELAGE SKIN BETWEEN F/S 235 AND F/S 250 AND STR. 14L AND STR. 15L WERE REPAIRED IAW REO. ALL REQUIRED STEPS HAVE BEENSDR IPXA2019062874809Skin · chafedINSPECTION TYPE: 3C, EXTERIOR FUSELAGE SKIN IS CHAFED AT BS 1153, LONGERON 44R. REPAIRED THE SKIN IAW EA 011-5330-A7781, REV I/R, AND EO MD11-5330-72888-A. MAJOR.SDR IPXA2019062443666Panel · crackedINSPECTION TYPE:3C, LEFT UNDER WING CANTED PANEL CAP IS CRACKED AT STA. 1236.8 AND Z=-100.REPAIRED CRACKED LEFT UNDER WING CANTED PANEL CAP AT STA. 1236.8 AND Z=-100 IAW UPS EO MD11-5310-72700-A. (MAJOR)SDR DALA2019052103172Structure · damagedSHIP 683 SUMMARY OF NRC 00530 THE EDGE OF THE DOOR L1 CUTOUT BETWEEN THE SKIN AND THE BEARSTRAP WAS REPAIRED PER ER/A NO. 578089-14 AD. CORRECTIVE ACTION: REF ERA 578089-14AD. (1083408)SDR HEER20190520958Skin · corrodedFORWARD SHELL OUTER SKIN WAS FOUND TO BE CORRODED NEAR TWO EXISTING INSERTS AND AN OEM DOUBLER INSTALLATION.SDR FXGA201905201944Skin · not reportedFUSELAGE SKIN REPAIR AT F/STA 235 LONGERON 19L. SRM 53-04-3 FIGURE 11. PERFORM REPAIR PER SRM 53-04-3 FIGURE 11. THIS IS A CLASS 1 REPAIR AND REQUIRES RE-INSPECTION.SDR SWAA2019061133524Skin · damagedPRESSURIZED SKIN DAMAGED AT BS. 207, R/H SIDE 9 IN ABOVE FORWARD ELECTRONIC AND EQUIPMENT BAY CUTOUT. / REPAIRED SKIN PER EA.SDR REXA2019051900727Skin · crackedFUSELAGE SKIN CRACKED 2 PLACES AT NOSE MLG CUTOUT RADIUS @ FS 235. REPAIRED PER CREO 601R-53-11-048 REV "D".SDR GTIA2019051903361Skin Panel · damagedSKIN PNL @ BTW FR 35-35.1 STR 39R SIDE HAS ABRASION DAMAGE L 43MM W X49MM W X 0.48MM (15% REMOVED) D X 3.2 MM T RAF 01 235325901 OPENED-REVIEWED LTPRNRI 5000887457-0010 AND HAS BEEN ACCOMPLISHED. THIS REPAIR IS CAT B AND MUST BE INSPECTED AT INTERVALS PER SRM SDR DALA2019052003104Skin · scratched(LOG 5726277) DURING INSPECTION FOUND CORROSION UNDER FWD CARGO SCUFF PLATE. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-13.SDR A6WA2019052046622Skin · crackedFUSELAGE SKIN IS CRACKED AT THE NLG SPADE DOOR CUT OUT, RT AFT CORNER REPAIRED FUSELAGE SKIN AT THE NLG SPADE DOOR CUT OUT RH AFT CORNER IAW REO 601R-53-11-048.SDR WVER2019051814Skin · chafedFUSELAGE EXTERNAL SKIN @ FS 977.00, STGR 27 IS CHAFED, FROM CONTACT WITH WING TO BODY FAIRING. THIS IS OVER A PREVIOUS REPAIR.SDR FXGA201909051942Skin · corrodedCORRODED FUSELAGE SKIN REPAIRS AROUND MULTIPLE CABIN WINDOWS. TO REPAIR CORRODED FUSELAGE SKIN AROUND CABIN WINDOWS AT THE FOLLOWING LOCATIONS: F/STA 285 LEFT SIDE, F/STA 770 LEFT SIDE, F/STA 790 RIGHT SIDE AND F/STA 930 RIGHT SIDE. THE FUSELAGE SKIN IS CORRSDR RJEY2019052200002Box Beam · crackedCRACK INDICATION ON FRAME 43 FROM THE FIRST HOLE TO FORWARD OF SIDE BOX BEAM AT -Y16.50.0 IN PAX CABIN.SDR DALA2019051803090Skin · crackedSHIP 3861 FUSELAGE SKIN SCRATCHED STA 500A TO 500B JUST BELOW STRINGER 18L MKD. CORRECTIVE ACTION: C/W ERA 578166-14 REV ORIG (1078688).SDR FXGA201905171941Skin · dentedFUSELAGE DENT AT F/STA 1228 STINGER 23L. TO REPAIR AN OUT OF LIMITS DENT AT F/STA 1228 STINGER 23L. REFORM DENT AND PERFORM REPAIR PER SRM 53-04-2 FIGURE 2 SHEET 2. THIS REQUIRES RE-INSPECTION PER 53-04-2 PARA D.SDR CALA2019051700785Pressure Panel · crackedAD 2018-06-04 EA 5330-05216 DOT NO.A3- NO DOT RT SIDE PRESSURE PANEL BETWEEN FRAME 35 AND 36 ADDITIONAL FASTENERS OUTSIDE THE CUT OUT AREA CRACKED AT 2,5,15,18,20,21,23,24,28,29. CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS AND REPAIR BEFORE NEXT FLIGHT N/R S/SDR DALA2023053104375Unknown · unknownSHIP 683 L-1 DOOR CUTOUT, CRACK FOUND IN UPPER FWD CORNER BEARSTRAP. REPAIR PER ER/A 578089-14AD. CORRECTIVE ACTION: REF ERA 578089-14AD. (1077613)SDR SWAA2022030846477Skin · corroded***CORROSION*** ON FUSELAGE EXTERNAL SKIN AT B.S. 887-1016; UNDER DORSAL FIN. / REPAIRED CORROSION ON THE FUSELAGE EXTERNAL SKIN B.S. 887 TO 1016 STR 3L TO STR 3R IAW EA 1-753-35008 REV IR AND ATS ER 19-03359 REV IR DATED 05-JUN-2019.SDR SWAA2019062133960Skin · dentedFUSELAGE SKIN DENTED BETWEEN BS. 1016+ 8.5 TO BS. 1024.5, 2" ABOVE STR. 16R. / REPAIRED SKIN PER SRM AND EA.SDR DALA2019051703077Skin · damagedDAMAGE AT STA 484 3" BELOW STR 24R. REF N/R 5. INSTALLED REPAIR DOUBLER REF. SRM 53-04-3.REF N/R 5. LOG ENTRY FOR LFEC REINSPECT. PLEASE SET UP. (LP1077538)SDR DALA2019051703076Skin · damagedDAMAGE AT STA 484 3" BELOW STR 24R. INSTALLED REPAIR DOUBLER REF. SRM 53-04-3. DAMAGED AREA PAINTED ON N/R 9. (LP1077364)SDR DALA2019051703075Skin · damagedDAMAGE AT STA 541 AT STR 25R. INSTALLED REPAIR DOUBLER REF. SRM 53-04-3. DAMAGED AREA PAINTED ON N/R 9. (LP1077363)SDR DALA2019051703070Doubler · damagedDAMAGE AT STA 541 AT STR 25R REF N/R 4. INSTALLED REPAIR DOUBLER REF SRM 53-04-3 FIG 8 SHEET 3. REF N/R 4. (LP1077522)SDR R61A2019060150565Skin · corrodedWHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND @ EXTERNAL FUSELAGE SKIN WASTE SERVICING CUTOUT. REPAIR WORK DONE IAW SRM 51-70-03 AND ETD 2019-170-067922. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.SDR I5EA2019052800031Skin · crackedDISCREPANCY: FOUND CRACK AT FUSELAGE STA 787 BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STA 787 BETWEEN STRINGERS 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA20190530Skin · crackedDISCREPANCY: FOUND CRACK AT RT FUSELAGE STA: 867 BETWEEN STRINGERS 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA 867 BETWEEN STRINGERS 8R AND 9R PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052800029Skin · crackedDISCREPANCY: FOUND CRACK AT LT FUSELAGE STA 500A BETWEEN 8L AND 9L. CORRECTIVE ACTIONS: ACCOMPLISHED REPAIR AT LT FUSELAGE STA 500A BETWEEN STRINGERS 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052800028Skin · crackedDISCREPANCY: FOUND CRACK AT LT FUSELAGE STA 727D BTWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STA 727D BETWEEN 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052500027Skin · crackedDISCREPANCY: FOUND DAMAGE AT RT FUSELAGE STA 727D BETWEEN STRINGERS 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA 727D BETWEEN STRINGERS 8R AND 9R PER AD 2001-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052500026Skin · crackedDISCREPANCY: FOUND CRACK AT RT FUSELAGE STA 460 BETWEEN STRINGERS 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA 460 BETWEEN STRINGERS 8R AND 9R PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052400025Skin · crackedDISCREPANCY: FOUND CRACK AT LT FUSELAGE STA 400 BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STA 400 BETWEEN STRINGERS 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052400024Skin · damagedDISCEPANCY: FOUND DAMAGE AT LT FUSELAGE STA 440 BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIRS AT LT FUSELAGE STA 440 BETWEEN STRINGERS 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052300022Skin · crackedCRACK FOUND AT STA 500 RT BETWEEN STRINGER 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA. 500 BETWEEN STRINGERS 8R AND 9R PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052300020Skin · crackedDISCREPANCY: FOUND CRACK AT FUSELAGE SECTION 47 LOWER PLATING AROUND FUSELAGE STA LT 1016 BETWEEN STRINGERS 20 AND 23L. CORRECTIVE ACTION: ACCOMPLISHED CRACK REPAIR AT FUSELAGE SECTION 47 LOWER PLATING AROUND FUSELAGE STATION LT 1016, BETWEEN STRINGERS 20L ANSDR CALA2019052000787Skin · dentedREF. L/P 3230818. PERFORMED CAT. B REPAIR ON FUS SKIN @ BS 620 S28L. REQUIRES DIP FOR REPEAT INSPECTIONS EVERY 6,000 FC. INITIATED DIP TO REINSPEXT EVERY 6000 FLT. CYCLES REF. SRM #53-00-01 REPAIR 29 TABLE 206 ZONE "A" OK TO PLACE ON DIP TO BE RE-INSPECTED EVESDR I5EA2019052100018Skin · crackedDISCREPANCY: FOUND CRACK AT FUSELAGE STA. 867 RT BETWEEN STRINGERS 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA. 867 BETWEEN STRINGERS 8R AND 9R PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.
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