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 HEER201908143161Skin · corrodedFORWARD ROOF SKIN WAS FOUND TO BE CORRODED - ONE PLACE, STATION 61.88, LBL 5.27. THE REPAIR DOCUMENTATION WILL BE SUBMITTED TO A STRUCTURAL FAA-DER FOR APPROVAL. THE FORWARD ROOF SKIN WILL THEN BE REPAIREDSDR EE4Y2019081309387Doubler · crackedEXTERNAL LOWER FUSELAGE, POWER RECEPTACLE, INTERNAL CUTOUT DOUBLER WITH CRACK. NOTE: THE DOUBLER WAS REPLACED AS PER SRM GUIDELINES (REF. JOB: A1H153 ITEM 1-18).SDR SWAA2022031457572Scuff Plate · crackedFWD CARGO BAY FWD SCUFF PLATE IS CRACKED / ACCOMPLISHED FCB FWD SCUFF PLATE REPAIR AND RE-INSTALLED IAW EA #1-A53-2076 REV 11SDR SWAA2022031457573Scuff Plate · crackedFWD CARGO BAY AFT SCUFF PLATE IS CRACKED / REMOVED AND REPLACED NEW FCB AFT SCUFF PLATE PN# 654A0004-338; PO# 758415 IAW SRM 51-40-02: IAW AMM 53-11-02-020-801 AND IAW AMM 53-11-02-420-801SDR UIEA2019081435044Skin · corrodedFOUND AFT CARGO UNDER FLOOR AREA CORROSION AT BS 1197+22 - 1197+44, S-36R TO S-37R. REMOVED THE CORROSION IAW SRM 51-10-02-0G-0 REV. 110. REPAIRED IAW EI T2019A53M-3220 REV. 1. CONDITION CHECK NORMAL.SDR DALA2019081304747Doubler · cracked(LOG 1219555) DURING INSPECTION FOUND CRACKED INNER PRODUCTION DOUBLER ON EXTERNAL POWER RECEPTACLE FWD LWR CORNER AREA. REPAIR WAS PERFORMED AT INNER PRODUCTION DOUBLER (2 EAS) ON EXTERNAL POWER RECEPTACLE FWD LWR CORNER AREA. PER B737-800 SRM 53-10-15 REPAIRSDR SWAA2019082736328Doubler · crackedEXTERNAL POWER DOOR CUTOUT CRACKED IN 2 PLACES ON AFT EDGE. REPAIRED DOUBLER IAW SRM.SDR SWAA2022031432566Scuff Plate · crackedAFT CARGO DOOR FWD SCUFF PLATE HAS CRACKED; DOT 56-01. / LOCATED AND DRILLED NEW FT CARGO DOOR; FWD CORNER SCUFF PLATE IAW B737-700 SRM 51-40-05-OG-OSDR SWAA2022031433597Skin · corroded***CORROSION*** ON THE FUSELAGE SKIN FWD SIDE OF STA 1016 SPLICE STR 28R TO 26L WL APPROXIMATELY 186 / REPAIRED FUSELAGE SKIN FWD SIDE OF BS 1016 SPLICE STR 28R-26L APPROX WL 186. DAMAGE 23'L X 1.95'W X .003'D FOUND OUT OF LIMITS DUE TO BEING AT/AROUND FASTENESDR SWIA2019092746358Skin Panel · damagedDAMAGED SKIN PANEL P/N 601R-33010-107 BETWEEN FS.193.00 - FS.210.00 LHS (C-CHECK) RO: 09/26/2019 REPLACED SKIN PN 601R-33010-107 BETWEEN FS193.00-FS210 LHS IAW SRM. LEAK CHECK GOOD.SDR IPXA2019081205509Skin · dentedRH EXT FUSELAGE DENT AT FR 18, 4 O'CLOCK POSITION.REPAIRED DENT RH FUSELAGE SKIN BETWEEN FR17 AND FR18, STR 33R IAW EO A300-5330-73589-A AND VT-SAA EA 300-5310-01-A7877 RE I/R. (MINOR)SDR SWAA2022031483843Scuff Plate · crackedACB AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED ACB AFT CORNER SCUFF PLATE PER REF EA 1-A53-2076 REV 11SDR SWAA2022031409182Skin · corroded***CORROSION*** AROUND FASTENERS ON UPPER FUSELAGE SKIN UNDER DORSAL FIN BS905 - BS1007 S-2L TO S-2R. MARKED / REMOVED DAMAGE ON FUSELAGE SKIN AROUND FASTENERS BS 905-1007 STR 2L- STR 2R. AND REPAIRED PER ATS ER# 19-04527 REV IR AND SWA EA 1-753-35537 REV IRSDR SWIA2019100246381Skin · scratchedAFT EQUIP BAY DOOR CUT OUT AT STRG 25L HAS DEEP SCRATCHES AND A DENT. REMOVED AND REPLACED LH WEB ON AFT EQUP BAY CUTOUT IAW SRM.SDR DALA2019082005180Skin · corrodedFUSELAGE / SKIN / DOUBLER / STA Y=1022.091 AND L29R / ARE CORRODED. ASSOCIATED ER/A 00-580391 ADDED FOR AC 9505. (LP #1214643)SDR CALA2019081201352Skin · crackedRH BS1035 UNDERW ING LONGERON FITTING AREA, 1EA HOLE FOUND CRACK AT FX SKIN, DETA ILS REFER ATTACHED FIG, REFER NR LP 9131053. FX SKIN STA 993 TO STA 1035 BETWEEN STR 35R TO STR 38R SKIN REPAIRED AS PER EC/RA NR. 5331-02418 REV.SDR R61A201908090828Skin · dentedWHILE IN HEAVY CHECK - INBOUND DMI FOR DENT FOUND FWD LH FUSELAGE SKIN BETWEEN FR9 AND FR11, STGR 17L AND 18L WITH FR10 DEFORMATION. RECONTOURED AND INSTALLED NEW SHEAR CLIP ON DENT FUSELAGE SKIN BETWEEN FRAMES 9 AND 11 STGR 17L AND 18L REFER SRM 51-40-08 ANSDR SWAA2022031435700Scuff Plate · crackedAFT CARGO FWD AND AFT SCUFF PLATES ARE CRACKED / REMOVED AND REPLACED AFT CARGO FWD AND AFT SCUFF PLATES PER AMM 53-11-02AMT 122078SDR SIMA20190808010Skin · gougedFUSELAGE SKIN SCRATCHED/GOUGED BETWEEN F77/80 AND STR 9L/10L. C/A-REPAIRED FUSELAGE SKIN BETWEEN FR 77/80 AND STR 9L/10L IAW ERS-EM-53MR-3869.SDR SIMA20190808012Skin · scratchedCFI FUSELAGE SKIN HAS 2 SMALL SCRATCHES BTW FR21-22 AND STR 19R-20R. C/A-REPAIRED CFI FUSELAGE SKIN 2 SMALL SCRATCHES BTW FR21-22 AND STR 19R-20R IAW SRM 53-21-01.SDR SIMA20190808011Skin · crackedFFLL TOP SKIN CRACKED AT RIVET BTW LT DV WINDOW AND PILOT WINDSHIELD. C/A-REPAIRED FFLL TOP SKIN CRACKED AT RIVET BTW LT DV WINDOW AND PILOT WINDSHIELD IAW EO EM-5300-2232.SDR SWAA2022031449333Panel · crackedCLOSE OUT PANEL IS CRACKED O/B OF PNL 194DR(STANDBY PUMP) AND JUST IB OF #5 FLAP TRACK. / REPAIRED DAMAGED AREA TO CLOSE OUT PANEL PER SRM 51-70-05-2R-2 SEE WIPS AND SUB TASK FOR INDIVIDUAL SIGN OFFSSDR SWAA2022031483833Scuff Plate · crackedFORWARD CARGO BAY; FORWARD CORNER SCUFF PLATE IS CRACKED. / RECIEVED FCB FORWARD CORNER SCUFF PLATE (P/N 7530406). TO BE INSTALLED ON CUSTOMER CARD # 753-646-63-01. 59577U 09AUG19SDR SWAA2022031483834Scuff Plate · crackedFORWARD CARGO BAY; AFT CORNER SCUFF PLATE IS CRACKED. / RECIEVED ACB AFT CORNER SCUFF PLATE (P/N 7530065). TO BE INSTALLED ON CUSTOMER CARD # 753-646-63-01. 59577U 09AUG19SDR CALA2019080901327Skin · corrodedFUSELAGE SKIN PREVIOUS REPAIR DOUBLER SKIN FOUND SURFACE CORROSION AT STA 1197+120 BETWEEN STR 37L-38L CORROSION REMOVED PER SRM 51-10-02, ORG 0.065'' BLEND OUT AREA REMAIN 0.045'' WIDTH 2'' LENGTH 2'', CHECKED NOT WITHIN SRM53-00-01 ALLOWABLE DAMAGE 1 FIG 101SDR ASAA2019082631463Skin · dentedRH FUSELAGE SKIN HAS A DENT AT FR19R AND STR30R GROUNDED - YES. DENT FOUND TO BE OUT OF LIMITS PER A320 SRM 53-11-11; CUT OUT DAMAGED AREA PER A320 SRM 53-11-11-300-041; FABRICATED DOUBLER PER SRM 53-11-11-300-041; PERFORMED HFEC (NO CRACKS NOTED) PER NTM SDR SWAA2022031449296Skin · bentAS PER MAINTENANCE REQUEST: GROUND POWER DOOR CUT-OUT ON FUSELAGE SKIN BENT ON FWD EDGE / REPAIRED PER EA # 1-753-35386. LEAK CHECK GOOD PER AMM 05-51-91.SDR CA191022036Skin · corroded(CAN) CORROSION DAMAGE TO THE INTERNAL SURFACE OF THE LOWER SKIN BETWEEN FS349.00 FS364.00 AND STR 26R STR27 (TC# 20191022036)SDR CA191022032Skin · corroded(CAN) FUSELAGE SKIN CORROSION BETWEEN FS295.00 - FS310.00 AND STR24R - STR26R. THERE ARE MULTIPLE AREAS WITH 100% MATERIAL LOSS (TC# 20191022032)SDR JJBA2019081605009Skin · canningOIL CANNING PREVIOUS REPAIR ON SKIN AT FR 19 - FR 20, STR 10L-12L, JUST AFT OF PAX DOOR. REPAIRED OIL CANNING PREVIOUS REPAIR ON SKIN AT FR19-FR20, STR 10L-12LSDR IPXA2019080545318Skin · puncturedFUSELAGE PUNCTURE LEFT SIDE OF FUSELAGE JUST FORWARD OF STA 2000, 3RD STRINGER DOWN FROM LAP SEAM, 2 FRAMES AFT OF BUTT SPLICE. REPAIRED DAMAGE IAW EO B747-5330-73527-A.SDR DALA2019080504579Skin · corrodedCORROSION INTERNAL STRUCTURE UPPER EXTERNAL SKIN CENTER TANK FR 41 TO FR 42 AND +Y1732 TO +Y1292 IN PASSENGER CABIN (1 EA), PERFORMED REPAIR INSTRUCTION ON OINTERNAL SKIN STRUCTURE UPPER EXTERNAL SKIN CENTER TANK FR41 TO FR42 AND + Y1732 TO +Y1292 IN PASSENGERSDR CA191022017Doubler · corroded(CAN) 44EA AREAS OF CORROSION ON AND AROUND THE LAV SERVICE SKIN DOUBLER BETWEEN FS559.00+80 & FS559.00+112 AND STRINGERS 20R & 24R (TC# 20191022017)SDR DALA2019111196530Skin · damagedLIGHTNING STRIKE DAMAGE AT ONE RIVET FWD OF FRAME 13, 1.5 INCHES ABOVE UPPER LEFT LAP JOINT REF LOG 5463683. PER A319 SRM 53-11-11-300-033. REMOVED FASTENER, PERFORMED A DETAILED VISUAL INSPECTION WITH A 10X PER A319 NTM 51-90-00. NO ADDITIONAL DAMAGE. INSTALLSDR DALA2019111196529Skin · damagedLIGHTNING STRIKE DAMAGE AT FRAME 20, 18 INCHES ABOVE LEFT UPPER LAP JOINT, REF LOG 5463687. PER A319 SRM 53-11-11-300-033, REMOVED FASTENER, PERFORMED A DETAILED VISUAL INSPECTION WITH 10X PER A319 NTM 51-90-00. NO ADDITIONAL DAMAGE. INSTALLED TEMPORARY BLIND SDR DALA2019110806484Skin · damagedLIGHTNING STRIKE DAMAGE AT 3.5 INCHES BELOW FRAME 2 AND 3.75 INCHES OUTB OF Y330. REMOVED FASTENER, PERFORMED A DETAILED VISUAL INSPECTION WITH A 10X PER A319 NTM 51-90-00. NO ADDITIONAL DAMAGE. INSTALLED TEMPORARY BLIND FASTENER, RESTORED FINISH. THIS IS A CASDR ABXA201908063135Skin · corrodedCORROSION ON THE UPPER CENTER WING SKIN AT FUSELAGE STATION 960. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR A6WA2019080546781Skin · crackedLEFT TRU SKIN LANDING CRACKED NEAR LATCH. REPAIRED SKIN IAW SUPP. 19-016B.SDR SWAA2022031433474Scuff Plate · crackedFWD CARGO COMPARTMENT AFT CORNER SCUFFPLATE IS CRACK / LOCATED AND DRILLED FWD CARGO COMPARTMENT AFT CORNER SCUFF PALTE PN #7530065 IAW SRM 51-40-05-0G-0SDR FDEA201908021792Doubler · wornEXISTING REPAIR AT FUSELAGE SKIN FORWARD CARGO FORWARD JAMB CUTOUT STA 895.700 BETWEEN LONGERON 39 RIGHT TO LONGERON 42 RIGHT. EXISTING REPAIR AT FUSELAGE SKIN FWD CARGO FWD JAMB CUTOUT STA 895.700 BETWEEN L39R TO L42R EVALUATED AND FOUND EXISTING REPAIR DSDR QMLA2019081429066Plate · crackedRT TORQUE PLATE HAS A 1 IN. CRACK. AIRCRAFT REMAINS OUT OF SERVICE AT THIS TIME.SDR YENA2019080920438Skin · corrodedPBI WAS FOUND WITH CORROSION DAMAGE ON SKIN PANEL AT FR70 BETWEEN STGR 30RH-32RH AT THE REAR FUSELAGE. ACCOMPLISHED A PERMANENT REPAIR PER THE REF /1/ EA AND COMPLIES WITH REF /2/ RDAS.SDR DALA2019080624627Skin · recessedUPPER FUSELAGE, SEVERAL LOCATIONS, AFT OF BS 650, FWD AND AFT OF TWO GPS ANTENNAS. ACFT SKIN RECESSED AT SKIN TO STRINGER ATTACHEMENT, SMALL RECTANGULAR. REPAIRED IAW PRI 579977-14, REV 0, 1, 2, AND ER/A 579977-14, REV ORIGINAL, SECTION I.SDR SWAA2019080635688Doubler · damagedGROUND POWER RECEPTACLE DOOR DOUBLER AND SKIN ALONG THE LOWER FORWARD EDGE DAMAGED. / REPAIRED DOUBLER PER SRM.SDR SWAA2022031401719Scuff Plate · crackedAFT CARGO BAY AFT SCUFF PLATE IS CRACKED / REPAIRED PER: EA 1-A53-2076 REV 11SDR SWAA2022031401720Scuff Plate · crackedAFT CARGO BAY FWD SCUFF PLATE IS CRACKED / REPAIRED PER:EA 1-A53-2076 REV 11SDR DALA2021062303402Skin · damagedSHIP 663 ERA 579977-14 REV 0 SECTION I TIME LIMITED REPAIR ACCOMPLISHED. CORRECTIVE ACTION: ER/A 579977-14 HAS BEEN REVISED, CURRENT REVISION IS 'A'. AREA ON FUSELAGE SKIN WAS REPAIRED PER ERA 579977-14 REV. B SECTION LL REPAIR PERMANENT. (1201453)SDR SWAA2019082836373Skin · damagedL2 DOOR CREASE FUSELAGE SKIN DAMAGED AT BS. 962, BETWEEN STR. 19L TO STR. 21L. REPAIRED DOUBLER PER EA.SDR ASAA2019080193401Skin · gougedMAIN CABIN AFT GALLEY SERVICE DOOR CUTOUT FWD FRAME EXTERNAL SKIN EDGE GOUGED JUST ABOVE UPPER TORQUE TUBE MOUNT. GROUNDED - YES. REMOVED AND REPLACED SKIN CORNER 147A3110-6 REF B737-800 SRM 51-40-02 AND BAC DWG 147A0020 REV -.SDR CALA2019081651359Skin · damagedFOUND DAMAGE AT STA 418 STR 14R TO 15R. DENT MEASURE .040 DEPTH BY 1.2 BY .7 A/Y=17.5 PER SRM 53-0 0-01. REPAIRED IAW SRM 53-00- 01 REPAIR 29. THIS IS A CATAGORY B REPAIR.
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