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 VGCA20230814001Skin Panel · crackedCRACKED SKIN RESULTING FROM TOOLING DAMAGE AT L1 DOOR UPPER HINGE CUTOUT NEAR S-10LSDR DALA2023081506648Unknown · unknown(LOG 2918077) CORROSION FOUND ON EXTERNAL SIDE OF FUSELAGE SKIN BS 727 TO 727B BETWEEN S-1 AND S-2R. ACCOMPLISHED ER 611033-14 FOR CORROSION ON EXTERNAL FUSELAGE SKIN BS 727-727B STR1 AND STR2.SDR FDEA202308141405Unknown · unknownCABIN , L3 DOOR CUTOUT AFT LOWER JAMB WEB SKIN FOUND CRACK AT STATION 1305.25 TO 1315.42 BETWEEN LONGERON 26 LEFT TO LONGERON 27 LEFT.SDR FDEA202308141404Unknown · unknownCABIN, R3 DOOR CUTOUT AFT LOWER JAMB WEB SKIN FOUND CRACK AT STATION 1305.25 TO 1315.42 BETWEEN LONGERON 26 RIGHT TO LONGERON 27 RGHT.SDR DALA2023081406584Unknown · unknownPUNCTURE IN FUSELAGE RT SIDE AFT OF FORWARD CARGO DOOR. THIS WAS ORIGINALLY DOCUMENTED IN LP #4849328 AND TRANSFERRED TO THIS LOG PAGE. MAINTENANCE REMOVED THE DAMAGE, DRILLED DOUBLER REF B717 53-03-01-2R PROCEDURE 1 REPAIR 1 CLASS 2 FIG 202 SHT 3, FABRICATED SDR CALA2023081402500Skin · gougedREF LP 4909862 . FUSELAGE SKIN GOUGE (BUTT JOINT AFT SKIN) STA. 360 BELOW S-24R ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF ECRA 5331-03034 ON OR BEFORE 200 FLIGHT CYCLES INITIATE A DIP TO ?ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF TOMC-APPROVAL FROM SC1ELBYSDR ASAA2023081145417Skin · dentedEVALUATE DENT ON AFT FUSELAGE APPROX. BETWEEN FR81 AND FR83 AND BETWEEN STR4L AND STR5L GROUNDED - YES. DENT FOUND TO BE OUT OF LIMITS, REMOVED DAMAGE, LOCATED, DRILLED, INSTALLED REPAIR DOUBLER AND RESTORED COATINGS REF A320 SRM 53-51-11-300-002. THIS IS A CASDR NACA2023081100003Unknown · unknownCORROSION ON FUSELAGE EXTERNAL SKIN AT BS727D S21R+4" REMOVED CORROSION LEVEL 2 AT FUSELAGE EXTERNAL SKIN AT BS727DS21R+4'' FROM P/N 65C38588 ORIGINAL THICKNESS 0.063'' REMOVED 0.063'' AND REMAINING THICKNESS IS 0'' AND IS OVER LIMITS PERFORM REPAIR PER SRM 53SDR SWAA2023082488272Skin · corrodedCORROSION ON FUSELAGE CROWN SKIN COMMON TO FASTENER ROWS LOCATED AT: BL 0; STA 1016+7 TO 1016+13; RBL & LBL 9; STA 1016+1 TO 1016+17; AND AT RBL & LBL 12 STA 1016+1 TO 1016+21.<[01] UPDATED STEPS 1-10;[02] UPDATED STEPS 1-10;[03] UPDATED STEP 2 AND 6;[04] ADDESDR LR7A2023081103299Skin · dentedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5301, FOUND RH FUSELAGE SKIN DENTED AT FS374, WL231, RBL75. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000992825. / PSE# 53-40-08, AD 2012-06-09SDR FDEA202308111396Skin · crackedWHILE PERFORMING LFEC INSPECTION IAW PT6 NTM 53-00-06 MULTIPLE CRACK INDICATIONS WERE NOTED AT THE UPPER L1 DOOR BEAR STRAP REPAIR AT THE UPPER FORWARD CORNER. FUSELAGE - PLATES AND SKIN - L1 DOOR CUTOUT, UPPER FWD CORNER, REPAIR REPLACEMENT. ACCOMPLISHED SDR I5EA2023081100019Unknown · unknownFUSELAGE SKIN CRACK AT STA. 727E, STR 24R, REPAIRED FUSELAGE RH SKIN AT STA.727E, STR. 24R, IAW B737-400 SRM 53-00-01, REPAIR 31SDR R61A2023090700481Skin · corrodedFRAME 89-90 STRINGERS 29L-29R HAS CORROSION ON SKIN AS MARKED. PERFORMED TEMPORARY REPAIR BY CUTOUT AND DOUBLER REPAIR AT FRAME 89-90 STRINGERS 29L--29R ON SKIN IN ACCORDANCE WITH, REF ETD2023--170-020249.SDR SWIA2023081601Unknown · gougedTWO GOUGES ON LH FUSELAGE SKIN BETWEEN FR10-FR11 AND STGR 16L- STGR 17L (FILED CLOSED)REPAIRED LH FUSELAGE SKIN BETWEEN FR10-FR11 AND STGR 17L- STGR 18L, IN REF. TO ETD2023-170-019944, REV. A. COMPLETED 51-00-00-002-SKY-U AND M-337. **NOTE** STRINGER 16L WAS ISDR DALA2023081406611Unknown · unknownSHIP 0690 FUSELAGE / LHS SKIN / S-14 / DENT. CORRECTIVE ACTION: REF ERA 602039-14. (2911518)SDR DALA2023081406607Unknown · unknownSHIP 0685 FWD LAV SERVICE PANEL PAN HAS FASTENERS PULLING THROUGH SKIN. CORRECTIVE ACTION: REF ERA 611098-14. (2911172)SDR SWIA2023081101Unknown · gougedTWO GOUGES ON LH FUSELAGE SKIN BETWEEN FR10-FR11 AND STGR 16L- STGR 17L (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSSDR I5EA2023081100004Unknown · unknownAFT CARGO STA. 927 BETWEEN STR 26R AND 25R INTERNAL SURFACE OF SKIN HAS CORROSION. CUT OUT DAMAGED SECTION OF SKIN AND INSTALLED DOUBLER AND TRIPLER IAW B737-300 SRM 51-40-02 AND B737-300 SRM 53-00-01 REPAIR 35.SDR CALA2023081102481Skin · dentedDENT REPORTED BY RAMP ON LOWER FUSELAGE RIGHT SIDE , JUST FWD OF WING BODY FAIRING. DAMAGE WAS BLENDED, NEEDS HFEC AND REMEASUREMENT OF DEPTH. PERFORMED NDT ON FUSELAGE SKIN REF. NDT PART 4 51-00-00 PROC. 2 C/W AVO STEP 1H.MFEC PER NDT PART 6 53-30-09. NO CRASDR DALA2023081006527Unknown · unknownSHIP 0685 FUSELAGE / SKIN / FWD LAV. SVC. PANEL CUTOUT / CORRISION. CORRECTIVE ACTION: REF ERA 611098-14. (2910334)SDR SWAA2023090787509Access Panel · delaminatedDELAMINATED ACCESS PANEL 193AL AT LOWER FUSELAGE 2023-490660<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: B20189416 DUE DATE: 19-DEC-23.;[02] TOOL USED HOT BONDER PN: HCS9200B-AV; SN: 18196126; DUE DATE: 26/MAR/24;[03] TOOL USED SCALE PN: CR5200; SN: 834251454SDR DALA2023081406618Unknown · unknownSHIP 0693 A SCRATCH/DENT WAS INDUCED AT FUSELAGE SKIN, BETWEEN STA 1459-1480 AND BETWEEN S 6L & S 7L. CORRECTIVE ACTION: REF ERA 601684-14AD.SDR DALA2023081106560Unknown · unknown(LOG 2909164) SMALL DENT AFT AND BELOW 1R CABIN DOOR. DENT WAS REPAIRED IAW B737-900 SRM 53-00-01-2R-1.SDR COEA2023081016919Skin · damagedDISCREPANCY: FUSELAGE HAS HAIL DAMAGE LOCATED BETWEEN FRAMES 32-33 & STRINGERS 1LH-1RH, FWD OF FRAME 33. STRINGERS 1LH-1RH, FWD OF FRAME 33. CORRECTIVE ACTION: REPAIR PER SRAS ES_00221562_01...21227 ISSUE A, DATED 8/9/2023.SDR COEA2023081015919Skin · damagedDISCREPANCY: FUSELAGE HAS HAIL DAMAGE LOCATED BETWEEN FRAMES 31-32 & STRINGERS 3-4 LH, FWD OF FRAME 32. STRINGERS 3-4 L/H FWD OF FRAME 32. CORRECTIVE ACTION: REPAIR PER SRAS ES_00221562_01...21227 ISSUE A, DATED 8/9/2023.SDR NACA2023080800002Unknown · unknownCORROSION ON FUSELAGE EXTERNAL SKIN AT BS796 S20R~S21R. 1. REMOVED DAMAGE PARTS 2. PERFORMED AIR ASIA WPS CODE LM BACF3TOIE30G65 FOR REPAIR PARTS 3. IA,AW B737-300 SRM 51-40-2 PAGE 6~7 (REV 130) INSTALLED REPAIR PARTS.SDR SWAA2023082186976Skin · delaminatedPANEL 193AR HAS A DELAMINATION ON THE OUTER SURFACE SKIN<[01] REPAIR OF DELAMINATION ON THE OUTER SURFACE SKIN OF PANEL 193AR WAS REPAIRED IAW SRM 51-70-05-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023081486700Seal · crackedLH HORIZONTAL UPPER FRONT SPAR SLIDING SEAL IS CRACKED.<[01] REMOVED AND REPLACED UPPER FRONT SPAR SLIDING SEAL IAW AMM 53-31-31.SDR SWAA2023081486701Seal · crackedRH HORIZONTAL UPPER FRONT SPAR SLIDING SEAL IS CRACKED.<[01] REMOVED AND REPLACED RH HORIZONTAL STABILIZER UPPER FRONT SPAR SLIDING SEAL PER AMM 53-31-31.SDR DALA2023081106552Skin · dented(LOG 2907793) DENT ON FUSELAGE EXTERIOR SKIN AT STA 727J+5 BETWEEN STR 22R AND 23R. C/W ER/A 610299-14.SDR FDEA202308081373Skin · corrodedFOUND THE LOWER FUSELAGE SKIN CORROSION INSIDE BODY FAIRING 192JR AT BS 930 TO BS 940 AND S-49L TO S-49R. THE LOWER FUSELGE SKIN CORRODED AREA AT BS 930 TO BS 940 AND S-49L TO S-49R REMOVED & THE REWORKED AREA MEASURED THE ORIGINAL THICKNESS IS T=0.100", SDR DALA2023080906492Unknown · unknownCRACK ON DOUBLER AND FILLER DOOR JAMB AT FWD CARGO DOOR. SUMMARY OF NRC 00084: REPAIR DOUBLER ON AFT INNER PAN SECTION DOOR JAMB AT FWD CARGO DOOR WAS REPLACED PER B717-200 SRM 52-30-02-2R PROCEDURE 4 REPAIR 4. AND REPAIR FILLER DOES NOT EXIST BECAUSE THE REPASDR CALA2023080902454Skin · unknownSTA. 400 FLUSH REPAIR JUST AFT OF THE R1 DOOR REQUIRES A NEW CURRENT REPAIR TO BE INSTALLED.THIS LOG PAGE IS FOR ESFR REPORTING PURPOSES ONLY. SEE NON ROUTINE 1516324 FOR WORK PERFORMED. LOG CREATED FOR REPORTING PURPOSES ONLY-SEE L/P 5390282 FOR INSP REQUIREMSDR IPXA2024081211321Skin · dentedFUESLAGE DENT @ STA 654 +88 BETWEEN 35-36R PERFORMED PERMANENT REPAIR IAW EO-87841-REQ3.SDR IPXA2023081493906Floor Panel · damagedINSPECTION TYPE:C*** MAJOR REPAIR *** PNL 132MG IS DAMAGED.FABBED PNL 132MG PER SREO A300-5320-16407.SDR DALA2023081106549Skin · dented(LOG 2906287) DURING INSPECTIONS, A CREASE IN DENT WAS FOUND COMMON TO THE FUSELAGE SKIN (PN 146A3251-41) AT APPROX. BS 727J+5, BETWEEN S-22R AND S-23R. MAINTENANCE REPAIRED DAMAGE PER ERA 610299-14.SDR DALA2023081006525Unknown · unknownSHIP 6714 FUSELAGE SKIN STA 440 AND S-23RH/24RH DENTED. CORRECTIVE ACTION: REF ERA 610870-14. (2905912)SDR IPXA2023080793830Floor Panel · corrodedINSPECTION TYPE:1C3CFLOOR PANEL HAS CORROSION UNDER RCB WALL Y= 475 TO -Y=500BLENDED AREA FOUND TO BE OUT OF LIMIT IAW SRM 51-21-01 , REPLACED FLOOR PANEL IAW SRM 51-31-01. MINORSDR IPXA2023080793828Floor Panel · corrodedINSPECTION TYPE:1C3CFLOOR PANEL HAS CORROSION UNDER RCB WALL AT STA X=25BLENDED AREA FOUND TO BE OUT OF LIMITS IAW DM-11 SRM 51-21-01,REPLACED FLOOR PANEL IAW SRM 51-31-01. MINORSDR DALA2023080806438Unknown · unknownCORROSION DAMAGE TO INTERNAL SKIN BETWEEN LONGERON 21-22L, FRAMES Y1037- Y1058 AT AFT CARGO COMPARTMENT, DAMAGE IS ESTIMATED TO EXCEED THE ALLOWABLE LIMITS. SUMMARY OF NRC 00656: CORROSION LEVEL 2. INTERNAL SKIN BETWEEN LONGERON 21-22L BTW FRAMES STA Y=1037 - SDR SWIA20231027806Unknown · corrodedMULTIPLE AREAS OF CORROSION ON THE EXTERNAL LOWER SKIN WHERE FORWARD WING FAIRINGS ( 191BB AND 192BB ) ATTACH AT FASTENER HOLES. (C-CHECK RO 10/29/2023) REMOVED MULTIPLES AREAS OF CORROSION ON THE EXTERNAL LOWER SKIN WHERE FORWARD WING FAIRINGS ( 191BB ANDSDR DALA2023080806463Unknown · unknown(LOG 2904770) A/C HIT BY RAMP BAGGAGE CART NEAR FWD CARGO DOOR. PUNCTURE DAMAGE NOTED. COMPLETED CAT 3 REPAIR PER B737 SRM 53-00-01-2R PROCEDURE 3 REPAIR 3.SDR SWI2023F00412Unknown · corrodedFWD BAGGAGE COMPARTMENT - FS533 BTWN STGRS 25L/26L/ - BUTTERFLY DBLR CORRODED (C-CHECK RO 10/4/2023) REMOVED CORROSION ON DOUBLER AT FS533, BETWEEN STGR 25L AND 26L AND FOUND OF OUT LIMITS REF. CRJ-700 SRM, 51-21-06-001-001-A01 AND CRJ-700 SRM, 53-31-23SDR SWIA20230928805Unknown · chafedL/H FUSELAGE APRON SKIN PANEL AT F/S 409+128 TO F/S 559.00 BELOW WL 73.50 HAS DEEP CHAFING (C-CHECK RO 9/26/2023) REPAIRED L/H FUSELAGE APRON SKIN PANEL AT F/S 409+128 TO F/S 559.00 BELOW WL 73.50 IAW REO 601R-53-41-115 REV. A DATED 2005-07-20 AND COMPLIEDSDR DU4R2023082800028Skin · dentedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND R/H FUSELAGE EXTERIOR SKIN HAS DENT BETWEEN FR 4 - 5, STR. 35R TO 36R. S/O 339001 N/R 28519SDR DU4R2023081400026Skin · dentedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND R/H FUSELAGE EXTERIOR HAS DENT AT FR32+5", STR. 37R - 38R. S/O 339001 N/R #28520SDR SWIA2023081105Unknown · damagedTRANSFER FROM EAML 1186655 : REFERENCE EAML #1186584. STATION VEHICLE BACKED INTO AIRCRAFT, DAMAGING AFT DRAIN MAST AND CAUSING TWO DENTS FORWARD OF DRAIN MAST. #1 DENT IS 1.905 MM DEEP, 63.5 MM LONG AND 9.52 MM WIDE. #2 DENT IS .762 MM DEEP, 12.7 MM LONG AND SDR YENA2023080800927Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION FRAME 32 SHEAR TIE BTW STR43R AND STR44 IN FWD CARGO COMPARTMENT REF AEROMSAN WO1222982-NR2023-403471; (RESOLVED ON W/O: 1222982 TASKCARD: NR-00014 ) REMOVED AND REPLACED SHEAR TIE LOC. FR 34 BTW STR 41R AND STR 42R IN FWD CSDR SWIA202308070005Unknown · damagedTRANSFER FROM EAML 1186655 : REFERENCE EAML #1186584. STATION VEHICLE BACKED INTO AIRCRAFT, DAMAGING AFT DRAIN MAST AND CAUSING TWO DENTS FORWARD OF DRAIN MAST. #1 DENT IS 1.905 MM DEEP, 63.5 MM LONG AND 9.52 MM WIDE. #2 DENT IS .762 MM DEEP, 12.7 MM LONG AND SDR DALA2023112909809Unknown · unknownSHIP 3062 DTI PER REV C OF ER/A 596427-14 FOR SKIN DOUBLER REPAIR INSTALLED BETWEEN FR30 AND FR33 AND BETWEEN STR 26L AND S7L. CORRECTIVE ACTION: INSPECTED. OK FOR SERVICE. (2901523)
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