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 AALA202203243292Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN BETWEEN FR 63 AND FR 64 BETWEEN S41L AND S42L. REPAIRED SKIN PER EA 334940.SDR AALA202203246297Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN BETWEEN FR 63 AND FR 64 AND BETWEEN S41R AND S42R. REPAIRED SKIN PER EA 334940.SDR SWAA2022041887197Baffle · damagedFORWARD CARGO BAY BAFFLE BETWEEN BS 500B AND 500C LBL 20 WL 154 IS DAMAGED / [01] CORRECTION TO TASK DETAIL SHOULD STATE ' FORWARD CARGO BAY BAFFLE BETWEEN BS 500B AND 500C LBL 25 WL 154 IS DAMAGED ';[02] REMOVED DAMAGED BAY BAFFLE; LOCATED AND DRILLED NEW BAYSDR SWAA2022041887201Attach Bracket · damagedFORWARD CARGO BAY ATTACH CLIP BS 500G FWD SIDE OF FRAME WL 154 RBL 25 IS DAMAGED / [01] REMOVED DAMAGED CLIP; LOCATED AND DRILLED NEW CLIP BS 500G FWD SIDE OF FRAME WL 154 RBL 25 IAW SRM 51-40-02-0G-0; 51-40-05-0G AND DWG 143A7505.;[02] OK TO INSTALL;[03] VERISDR SWAA2022041887202Attach Bracket · damagedFORWARD CARGO BAY ATTACH CLIP BS 500G AFT SIDE OF FRAME WL 154 RBL 25 IS DAMAGED / [01] REMOVED DAMAGED CLIP; LOCATED AND DRILLED NEW CLIP BS 500G AFT SIDE OF FRAME WL 154 RBL 25 IAW SRM 51-40-02-0G-0; 51-40-05-0G AND DWG 143A7505.;[02] OK TO INSTALL;[03] VERISDR SWAA2022041887203Attach Bracket · damagedFORWARD CARGO BAY ATTACH CLIP BS 500H FWD SIDE OF FRAME WL 154 RBL 25 IS DAMAGED / [01] REMOVED DAMAGED CLIP; LOCATED AND DRILLED NEW CLIP BS 500H FWD SIDE OF FRAME WL 154 RBL 25 IAW SRM 51-40-02-0G-0; 51-40-05-0G AND DWG 143A7505.;[02] OK TO INSTALL;[03] VERISDR SWAA2022041887204Attach Bracket · damagedFORWARD CARGO BAY ATTACH CLIP BS 500H AFT SIDE OF FRAME WL 154 RBL 25 IS DAMAGED / [01] REMOVED DAMAGED CLIP; LOCATED AND DRILLED NEW CLIP BS 500H AFT SIDE OF FRAME WL 154 RBL 25 IAW SRM 51-40-02-0G-0; 51-40-05-0G AND DWG 143A7505.;[02] OK TO INSTALL;[03] VERISDR FDEA202203220646Skin · dentedL/H LOWER LOBE FUSE SKIN AT STA. 247 AT STR23L HAS A CREASE BULGE ON FWD SIDE OF FRAME, NEEDS EVAL. EVALUATED DENT AT STA 247 S-23L, DAMAGE LOCATION IS LESS THAN 0.5" AWAY FROM FRAME AT STA 247, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-1A FIG 101, DET. ISDR IPXA2022032980632Skin · crackedINSPECTION TYPE:C5CRACK ON FUSELAGE SKIN (P/N:148T3121-2) ON STA 1725.5 , NEAR S-7R.REPAIR I.A.W 767-300F SRM 53-80-01-2R REPAIR 5, REV 82.01.SDR FDEA202203220638None · noneEXTERIOR FUSELAGE SKIN HAS AN OUTWARDLY PROTUDING DENT AT STA 1602 BETWEEN S16R AND S17R ACCOMPLISHED B757-2 SRM 53-00-51-2R REPAIR 29 - FIG 201 - SHEET 129 - CATEGORY B REPAIRSDR FDEA202203220630None · noneAGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND ON WEB AT CENTER CARGO COMPARTMENT AFT BULKHEAD STATION 1841 X = 17 . EXISTING REPAIR DOUBLER ON WEB AT CENTER CARGO COMPARTMENT AFT BULKHEAD STATION 1841 X = 17 EVALUATED AND FOUND WEB WITH DAMAGE AND EXCEESDR UIEA2022032400236Skid Shoe · corrodedCORROSION - MD CGO FUSELAGE SKIN AREA AT STA 1000 FWD S-16R TO S-17R(<P>ACCOMPLISHED <SPAN>EI # T2022A53M-636 REV 2. ATTACHED TO W/O 6828148. JOB COMPLETED.</SPAN></P>)SDR UIEA2022032300221Skin · corrodedCORROSION DAMAGES ON INNER SURFACE OF FUSELAGE SKIN DURING PERFORMING INSP PER SB 747-53A2878(<P>REPAIR DAMAGE AREA IAW EI NO. T2022A53M-636 REV 2. JOB COMPLETED</P>)SDR UIEA2022032300226Skin · corrodedCORROSION - SKIN SURFACE LWR FUESLAGE INSIDE OF WING TO BODY FAIRING AT STA 840, S-44L & S-45L(<P>REM0VE DAMAGE AREA FASTENERS IAW SRM 51-40-02 REV 94. ACCOMPLISH <SPAN>EI # T2022A53M-746 REV 1 & DWG #142A3544 SHEET 7 REV B AND DWG #142A3784 SHEET 12 REV F. JOSDR CALA2022032100735Bolt · missingPDA 3 PDA INSPECTION FOUND, WING TO BODY FAIRING 191DL ONE BOLT MISSING ON LEFT AFT CORNER INSTALLED NEW BOLT. CHECKED THIS AREA. NO DAMAGE FOUND. REF GMM 02-30-95 ADD EMP:U175071SDR UIEA2022032300220Skin · gougedDURING AIRCRAFT TOUCH UP PAINT MX FOUND GOUGE IN LOWER AFT SECTION OF FUSELAGE AT APPROX FS 1632 IN THE NON PRESSURIZED AREA(<P ><SPAN>REPAIRED FUSELAGE IAW B767 SRM 53-00-01-2R-12 REPAIR 12. EO 6753A992</SPAN></P> / <P> </P>)SDR SWAA2022042086113Bracket · brokenBROKEN SUPPORT BRACKET INSULATOR LOCATED BS578 TO BS663.75 AND BETWEEN STR10R TO STR16R AT PASSENGER CABIN (4 EA) 2022-147999 / [01] REPLACED INSOLATER BRAKET (1E/A) AND INSOLATOR BRACKET (3E/A) LOCATED ON BS578 AND BETWEEN STR10R TO STR16R AT PASSENGER CABIN SDR DALA2022032201863Not Reported · not reported(LOG 8292898) DURING INSPECTION FOUND L/H AUX STATIC PORT HAS 4 LIGHTNING STRIKES. DAMAGE REPAIRED PER SRM 53-00-01 REPAIR 13.SDR CALA2022032100714Frame · crackedF/O''S UPPER OUTBOURD CORNER WINDOW FRAME IS CRACKED. LOCK FOR MX FERRY PHOTO ADDED RAMS REQUITED LOGPAGE UNLOCKED FOR UPDATE COMPLETED STEPS B1&2 OF AVO9568 REF NDT PART 6 51-00-01. CORRECTION: COMPLETED STEPS B3 & B4 OF AVO9568 REF NDT PART 6 INSPECTION EVALSDR DALA2022032101829Not Reported · not reportedCRACK ON EXTERNAL FUSELAGE SKIN STA Y=1040 LONG 14RH. SUMMARY OF NRC 00049: FUSELAGE SKIN STA Y=1040 LONG 14RH WAS REPAIRED PER ERA 597705-14 REV. ORIGINAL SECTION 1. PERMANENT REPAIR AND PRI REV. 0,1,2,3 AND 4. REPETITIVE INSPECTIONS WILL BE MONITORING UNDER SDR DALA2022032502002Skin · crackedREFERENCE ER/A 597705-14 FUSELAGE / SKIN / Y=1037, L-13R TO L- 14R / CRACKS, RESULTING IN A BOEING APPROVED RE-ENFORCING REPAIR . ACCOMPLISH SECTION II: REPETITIVE GENERAL VISUAL INSPECTION EVERY 24 MONTHS AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT ASSOCIATESDR 7C7A2022031700012Skin · corrodedCORROSION DAMAGE ON CENTER FUSELAGE RH TOP SKIN PANEL ASSEMBLY PN 85320282 BETWEEN X291.40 -X312.35 AND STR. 1-2S. REF. 008.53-22.07SDR LR7A2022031603094Skin · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND LH FUSELAGE SKIN CRACKED AT FS942, LBL62, WL225. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR#0155. / PSE# 53-50-06, AD 2012-06-09SDR LR7A2022031603093Skin · crackedDURING SCHEDULED B-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH FUSELAGE SKIN CRACKED AT FS737, LBL62, WL175. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0152.SDR LR7A2022031603092Doubler · crackedDURING SCHEDULED B-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH FS823-872 SKIN DOUBLER CRACKED AT LBL62, WL175. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR#0133.SDR LR7A2022031603091Skin · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND LH FUSELAGE SKIN CRACKED AT FS872, LBL62, WL192. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 0131. / PSE# 53-50-06, AD 2012-06-09SDR LR7A2022031603089Skin · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND LH FUSELAGE SKIN CRACKED AT FS139, LBL47, WL155. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 0077. / PSE# 53-50-08, AD 2012-06-09SDR DALA2022031701794None · none(LOG 2158621) DURING INSPECTION FOUND FWD FUSELAGE SKIN AT STA 380-400 AND STR 16L-18L DENTS. REPAIRED PER ERA 14-598006.SDR YENA2022031700269Shear Tie · corrodedDURING HEAVY MAINTENANCE, INITIAL INSPECTION: [CPCP FINDING] CORROSION IN SHEAR CLIP AT FR 72 & STGR 26L-27L AT AFT CARGO COMPARTMENT; REF TOMX WO 1846 NR -00160 SHEAR CLIP WAS REPLACED PER EMB-190 SRM 51-12-01 PAR 6 AND SRM 51-10-03 PAR 4 A AND PER EMB-190 SRSDR YENA2022031700268Shear Tie · corrodedDURING HEAVY MAINTENANCE, INITIAL INSPECTION: [CPCP FINDING] CORROSION IN SHEAR CLIP OVER FR-- 80 BTW STGR-28L / STGR-27L AT AFT CARGO COMPARTMENT; REF TOMX WO 1846 NR -00134 SHEAR CLIP WAS REPLACED PER EMB-190 SRM 51-12-01 PAR 6 AND SRM 51-10-- 03 PAR 4 A ANDSDR YENA2022031700267Shear Tie · corrodedDURING HEAVY MAINTENANCE, INITIAL INSPECTION: [CPCP FINDING] CORROSION IN SHEAR CLIP OVER FR-75 BTW STGR-26L / STGR-27L AT AFT CARGO COMPARTMENT; (RESOLVED ON W/O: 1153864 TASK CARD: NR-00044 ) REF TOMX WO 1846 NR -00107 SHEAR CLIP WAS REPLACED PER EMB-190 SDR YENA2022031700266Shear Tie · corrodedDURING HEAVY MAINTENANCE, INITIAL INSPECTION: [CPCP FINDING] CORROSION IN SHEAR CLIP OVER FR-- 77 BTW STGR-27L / STGR-28L AT AFT CARGO COMPARTMENT; REF TOMX WO 1846 NR -00123 SHEAR CLIP WAS REPLACED PER EMB-190 SRM 51-12-01 PAR 6 AND SRM 51-10-- 03 PAR 4 A ANSDR YENA2022031700265Shear Tie · corrodedDURING HEAVY MAINTENANCE, INITIAL INSPECTION: [CPCP FINDING] CORROSION IN SHEAR CLIP OVER FR-83 AND STGR-22L AT AFT CARGO COMPARTMENT; REF TOMX WO 1846 NR -00151 SHEAR CLIP WAS REPLACED PER EMB-190 SRM 51-12-01 PAR 6 AND SRM 51-10-03 PAR 4 A AND SRM 51-75-16 SDR YENA2022031700264Shear Tie · corrodedDURING HEAVY MAINTENANCE, INITIAL INSPECTION: [CPCP FINDING] CORROSION IN SHEAR CLIP AT FR 72 & STGR 27L-28L AT AFT CARGO COMPARTMENT; REF TOMX WO 1846 NR -00161 SHEAR CLIP WAS REPLACED PER EMB-190 SRM 51-12-01 PAR 6 AND SRM 51-10-03 PAR 4 D AND SRM 51-75-16 SDR YENA2022031700263Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION FOUND ON SHEARCLIP AT FRAME 76 STR 22L & 23L AFT CARGO COMPARTMENT; REF TOMX WO 1846 NR -00270 CORROSION WAS REMOVED ON SHEARCLIP AT FRAME 76 STR 22L & 23L AFT CARGO COMPARTMENT AND EVALUATE, ORIGINAL THICKNESS IS .040" AND SDR YENA2022031700262Shear Tie · corrodedDURING HEAVY MAINTENANCE, INITIAL INSPECTION: [CPCP FINDING] CORROSION IN SHEARCLIP AT FR 90 & STGR 29L-29R AT AFT CARGO COMPARTMENT; SUMMARY OF NRC 00166: CORROSION WAS REMOVED ON SHEARCLIP AT FR 90 STGR29L-29R AT AFT CARGO COMPARTMENT AND MEASURE, OT= 0.40" SDR YENA2022031700261Shear Tie · corrodedDURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING CORROSION IN SHEAR CLIP AT FR 89 AND STGR 29 L-29R AT AFT CARGO COMPARTMENT; SHEAR CLIP WAS REPLACED PER EMB-190 SRM 51-12-01 PAR 6 AND SRM 51-10-03 PAR 4 A, SRM 51-41-01 PAR 4 AND SRM 51-41-02 PAR-.4 SDR SWAA2022041284129Angle · corrodedC-1 CARGO PIT; FLOOR PANEL L/H ZEE ANGLE; AREAS OF CORROSION ON UPPER SIDE AT LOWER SIDE WALL PANEL ATTACH FASTENER HOLES; BS 500+15 TO BS 500E+1; LBL 25; WL 156; AREAS MARKED IN BLACK; DOT: 148-002 / [01] REMOVED CORROSION ON Z ANGLE IAW SRM 51-10-02-0G-0 ITESDR SWAA2022041284132Angle · corrodedC-1 CARGO PIT; BS 500I; LBL 25 TO RBL 25; WL 156; AREAS OF CORROSION ON UPPER SIDE OF AFT B/H TO FLOOR BEAM ATTACH ANGLE; AREAS MARKED IN BLACK; DOT: 148-004 / [01] REMOVED DAMAGE FLOOR BEAM ATTACH ANGLE IAW SRM 51-40-02-0G-0;[02] REMOVED CORROSION IAW SRM 51-SDR SWAA2022040684288Gusset · crackedCRACK GUSSET LOCATED BS 500D; STRINGER 19R FWD CARGO COMPARTMENT 2022-129813 / [01] REPLACED GUSSET LOCATED BS 500D STRINGER 19R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-0-02 ITEM 9 AND DRAWING 143A7902 REV -; SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED GUSSDR SWAA2022040684291Gusset · crackedCRACK GUSSET LOCATED BS 500D; STRINGER 19L FWD CARGO COMPARTMENT 2022-129817 / [01] REPLACED GUSSET LOCATED BS 500D STRINGER 19L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7902 REV. -; SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED GSDR SWAA2022040684292Angle · crackedCRACK ANGLE - CLIP LOCATED BS 400; STRINGER 26L FWD CARGO COMPARTMENT 2022-129821 / [01] REPLACED ANGLE - CLIP AND FASTENERS LOCATED BS 400; STRINGER 26L FWD CARGO COMPARTMENT IAW SRM B737-700 51-40-02 AND DRAWING 143A7505 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[SDR SWAA2022040584293Angle · crackedCRACK ANGLE - CLIP FWD FACE OF BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENT 2022-144836 / [01] TOOL USED: CALIPER; P/N: 500-196-30; S/N: A20231804; DUE DATE: 26-AUG-22.;[02] REPLACED ANGLE - CLIP LOC. FWD FACE OF BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENSDR SWAA2022040584295Gusset · crackedCRACK GUSSET BS 500D AT LEVEL STR 19L FWD CARGO COMPARTMENT 2022-144840 / [01] TOOL USED: CALIPER; P/N: 700-113-10; S/N: 0023246; DUE DATE: 23-SEP-22;[02] REPLACED GUSSET BS 500D AT LEVEL STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02SDR SWAA2022040584294Gusset · crackedCRACK GUSSET BS 500D AT LEVEL STR 21L FWD CARGO COMPARTMENT 2022-144842 / [01] TOOL USED: CALIPER; P/N: 500-197-30; S/N: A21146280; DUE DATE: 17-OCT-22;[02] REPLACED GUSSET LOC. BS 500D AT LEVEL STR 21L FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02; SRM B737SDR SWAA2022040584296Gusset · crackedCRACK GUSSET BS 500D AT LEVEL STR 19R FWD CARGO COMPARTMENT 2022-144844 / [01] TOOL USED: CALIPER; P/N: 700-113-10; S/N: 0023246; DUE DATE: 23-SEP-22;[02] REPLACED GUSSET LOCATED BS 500D AT LEVEL STR 19R FWD CARGO COMPARTMENT IAW SRM 51-40-02 AND SRM 51-10-02 SDR IPXA2022031580147None · brokenINSPECTION TYPE:SEGE/E COMP FLOOR PANEL 121YF BROKENREPAIR IAW SREO A300-5320-42722FSDR DALA2023041302904Unknown · unknownER/A 597798-14, FUSELAGE / SKIN / LH WINDOW BELT PANEL / Y=522-541 / LIGHTNING STRIKE. SUBJECT REPAIR REQUIRES FOLLOW-ON REPETITIVE INSPECTION AND PERMANENT REPAIR. ACCOMPLISH ER/A 597798-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 24 MONTHS OF SECTION ISDR SWAA2022041283815Frame · crackedCRACK ACCESS PANEL COVER CUT OUT ENTRY DOOR LOCATED BS 303.9 AND BTW STRINGER 7L TO STR 9L AT PASSENGER CABIN 2022-131708 / [01] REPLACED ACCESS PANEL COVER CUT OUT ENTRY DOOR LOCATED BS 303.9 AND BTW STRINGER 7L TO STR 9L AT PASSENGER CABIN IAW B737-700 SRM 5SDR SWAA2022040883665Access Panel · elongatedLOWER FUSELAGE ACCESS PANEL 194E SEVERAL FASTENER HOLE ELONGATED / [01] ACCOMPLISHED VISUAL INSPECTION FOUND ALL HOLES DAMAGE AS PER B737 NTM 51-05-01 AND PREPARED AREA FOR DRY PROCCES AS PER B737 SRM 51-70-05-2R-0.;[02] VERIFIED STEP #1;[03] ACCOMPLISHED DRY
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