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 SWIA2020021848517Skin · corroded* THE SKIN BETWEEN FS295.00 AND FS310.00 BETWEEN STRG 26R AND 25R HAS CORROSION. (C-CHECK) RO 2/14/2020 REMOVED CORROSION ON INNER SKIN BETWEEN FS.295.00 & FS.310.00 AND BETWEEN STGR 25R & STGR 26R IAW CRJ900 SRM.FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGESDR CALA2019121702220Skin · dentedFOUND DENT IN FUSELAGE SKIN APPROXIMATELY 6" AFT AND 3" ABOVE THE FORWARD CARGO DOOR FORWARD UPPER CUTOUT.NO DMG DOT IN THE AREA. ON OR BEFORE THE AIRCRAFT REACHES 34000 TOTAL AIRCRAFT FLIGHT CY CLES PERFORM AN INSPECTION PER PART 2 OF ECRA 5331-02497. PLANNI SDR CALA2019120762148Skin · corrodedWATER SVC PAL CUTOUT INNER SKIN FWD EDGE FND CORR AT S39L-40L REFER TO NON-ROUTINE NO.9491027 - ORIGINATED BY EMP V906548 - SPEC NO.A3NB-53-3-6185. WATER SVC PNL CUTOUT INNER SKIN DOUBLER (REINFORCEMENT) REPLACED AS PER ECRA 5331-02536 FOR CORROSION DAMAGE WITSDR DALA2019120507059Skin · corrodedAFT CARGO COMP INTERNAL SKIN IS CORRODED BETWEEN STA 1197+22- STA 1197+44 S36R AFT OF REPAIR DOUBLER BLENDED AREA OF CORROSION REMOVED .045 MATERIAL, REMAINING THICKNESS .075 OUT OF POSSINBLE .120. FOUND TO BE OUT OF LIMITS. C/W SRM 53-00-01.SDR DALA2019120507058Skin · corrodedAFT CARGO COMP INTERNAL SKIN IS CORRODED BETWEEN BS 1197+22 - 1197+44, S36R AFT OF REPAIR DOUBLER. C/W SRM 53-00-01.SDR R61A2019120541351Skin · dentedDURING MAINTENANCE INSPECTION 2 DENTS WERE DISCOVERED ON RH FORWARD FUSLAGE BETWEEN FRAMES 8 & 9 AND BETWEEN STR 17R & 18R. DAMAGE WAS REPAIRED IAW EMBRAER ETD 2019-170-159946 B. AC RETURNED TO SERVICE.SDR SWIA2020020348105Skin · dentedD: COMPLIED WITH TEMPORARY REPAIR FOR DENT TO THE FUSELAGE LOWER SKIN AT FS409.00+16.00, STR 21R - STR 22R PER REO. PERMANENT REPAIR DUE BY 4400 FLT HRS. / **DO NOT CLOSE UNTIL PERMANENT REPAIR* (C-CHECK) RO:1/29/2020REPAIRED REF. CRJ200 SRM. REFERENSDR SWAA2019120939484Doubler · crackedELECENTERICAL GROUND POWER RECEPTACLE SURROUND DOUBLER (EGPR) CRACKED AT AFT EDGE BS. 234, ZONE 1. / REPAIRED DOUBLER IAW SRM.SDR SWIA2020021848512Skin · gouged* THE AFT CARGO DOOR SURROUND EXTERNAL SKIN UNDER THE PROTECTOR PLATE HAS SEVERAL GOUGES ON THE AFT SIDE. (C-CHECK) RO 2/14/2020 COMPLIED WITH REPAIR TO THE AFT CARGO DOOR SURROUND SKIN BENEATH THE PROTECTOR PLATE, BLENDS FOUND TO BE WITHIN LIMITS WITH NOSDR SWIA201902048208Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: DENT ABOVE RADOME CENTERED BETWEEN THE WINDSHIELD 9' ABOVE RADOME DENT MEASURES 6"X 4.9" AND IS 0.1 INCHES IN DEPTH. COMPLIED WITH TEMPORARY REPAIR PER EMBRAER ETD PERMANENT REPAIR FOR 7500 CYCLES DUE BY TAC 9658, PART NSDR 7C7A2019120320523Skin · dentedLARGE DENT UNDER R/H FUSELAGE ICE SHIELDSDR DALA2019120206996Doubler · cracked(LOG 1382485) DURING INSPECTION FOUND CRACKED INTERNAL PRODUCTION DOUBLER ON EXTERNAL POWER RECEPTACLE CUT OUT. CRACK ON INTERNAL PRODUCTION DOUBLER ON EXTERNAL POWER RECEPTACLE CUT OUT WAS REPAIRED PER B737-800 SRM 53-10-15 REPAIR 5.SDR C77A2020020530041Skin · dentedDURING BASIC CHECK AT EAMS, INSPECTION DISCOVERED A DENT ON THE FORWARD FUSELAGE SKIN BETWEEN FR13 & FR14 AND STGR-19L & THE SKIN SEAM. REFER ETD2019-170-156012 FOR THE DENT LOCATION AND MEASUREMENTS. EAMS REQUESTED AND RECEIVED RELIEF IN THE FORM OF ETD2019-1SDR SWIA2020012147832Skin · damagedADM# 2935 FWD FUSELAGE BETWEEN FS 265.00-280.00, 1.5" RIGHT OF STR 26R . PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO:1/17/2020REPAIRED FWD FUSELAGE DAMAGE BETWSDR 29GA2019120600001Skin · damagedFLIGHT# N/A REPORT: DURING REPO OF AC TO THE LINE , DAMAGE OCCURED TO THE RH SIDE ABOVE FIN. CORRECTIVE ACTION: PERFORMED REPAIR TO FRAME STATION 827 AND SKIN IAW EO 340B-5390-2019-001 ALL CHECKS GOODSDR ASAA2019120471504Skin · dentedAFT FUSELAGE SKIN DENT BTW FR 64/65 AND STR 40/41 LH. REF EA A320-53EA-00124. REQUIRES PERMANENT REPAIR. GROUNDED - YES. INSTALLED PERMANENT CATEGORY 'A' REPAIR REF A320 SRM 53-41-11-30-093.SDR SWIA2020010947596Doubler · corrodedTCAS ANTENNA DOUBLER PLATE BETWEEN FS295.00 - FS310.00 AND BETWEEN STGR27 - STGR26R CORRODED, MARKED, (INSIDE FUSELAGE) (C-CHECK) RO 01/07/2020 EVALUATED ANTENNA DOUBLER PLATE BETWEEN FS 295.00 TO FS 310.00 AND STR 27 TO STR 26 RH FOUND TO BE OUT OF LIMITS MASDR SWAA2019121639631Skin · corrodedFUSELAGE EXTERNAL SKIN HAD AREAS OF CORRODED BETWEEN BS. 927 TO BS. 1006, BETWEEN STR. 2L TO STR. 2R. / REPAIRED SKIN PER ER AND EA.SDR C77A2019112600003Doubler · corrodedDURING THE B6 BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED INSIDE THE P/N 170-2365-01-404-109 AFT WI-FI (ATG) ANTENNA FITTING/SKIN DOUBLER. REFERENCE FIGURE 1 FOR DETAILS AFTER DAMAGE REMOVAL. THE AFT WI-FI (ATG) ANTENNA FITTING WAS INSTALLED BY STC STSDR DALA2019112606939Skin · chafedCHAFING EXTERNAL SKIN BETWEEN STRINGER 43L AND STRINGER 43R AT LEVEL FRAME 34 AT LOWER FUSELAGE, PERFORMED REPAIR SECTION I AS PER PRI 583239-14 REV.0 AND ER/A NO.583239-14AD REV. ORIGINAL ,SDR SWIA2019021848508Skin · dentedADM #2757. 3 " FORWARD OF FS613.0 AND 6" BELOW WL72.5 (ABOVE AND IN BETWEEN FORWARD AND CENTER BAGGAG BAY DOORS). DENT APPROXIMATELY 1" WIDE AND 0.025" DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDSDR CALA2019120322105Housing · corrodedB757-06-3-0270 APU AIR INLET HOUSING FWD EDGE BULGED AROUND FAST ENERS. RL029 REF. ST. ENGINEERING N/R 0080779 REMOVED CORROSION AND CHECKED LIMIT TO APU AIR INLET HOUSING FWD L THICKNESS IS .250". OUT OF LIMITS IAW B757-200 SRM 53-80-15 FI G 101, DETAIL I ANDSDR Y2PA201911265046Skin · crackedDISCREPANCY: DURING C-CHECK AT KBVO, CRACK WAS FOUND ON NLG SKIN AND DOUBLER AT AFT LH CORNER OF WHEEL WELL. CRACK
DIMENSIONS HAVE BEEN SENT TO DFJ
CORRECTIVE ACTION: PHOENIX RISING REPAIRED CRACK AT NOSE WHEEL WELL LF AFT CORNER FRAME 7 AT STRINGER 22 IAW SDR Y2PA201911265045Skin · corrodedDISCREPANCY:DURING C-CHECK AT KBVO, EXCESSIVE CORROSION FOUND AT SPOT WELDS AT FRAME 18, FROM STRINGER 19-22 ON
BOTH LH AND RH SIDES OF THE FUSELAGE
CORRECTIVE ACTION: PHOENIX RISING REPAIRED CORROSION AT LH FRAMES 16-18 AT STRINGERS 19-21 IAW DRAWING 19-SDR Y2PA2019112600025Skin · corrodedDISCREPANCY:DURING C-CHECK AT KBVO, EXCESSIVE CORROSION FOUND AT SPOT WELDS AT FRAME 18, FROM STRINGER 19-22 ON
BOTH LH AND RH SIDES OF THE FUSELAGE
CORRECTIVE ACTION: PHOENIX RISING REPAIRED CORROSION AT LH FRAMES 16-18 AT STRINGERS 19-21 IAW DRAWING 19-SDR Y2PA201911265044Skin · corrodedDISCREPANCY: DURING C-CHECK AT KBVO MULTIPLE SPOTS OF CORROSION FOUND ON LH SIDE OF FUSELAGE DURING SPOT WELD NDT
INSPECTION.2 SPOTS ARE OUT OF LIMITS, AREAS ARE LOCATED FROM FRAME 18 TO FRAME 19, BETWEEN STRINGER 10 TO STRINGER 13
CORRECTIVE ACTION: PHSDR Y2PA201911265043Skin · corrodedDISCREPANCY: DURING C-CHECK AT KBVO MULTIPLE SPOTS OF CORROSION FOUND ON RH SIDE OF FUSELAGE DURING SPOT WELD NDT
INSPECTION.12 SPOTS ARE OUT OF LIMITS, AREAS ARE LOCATED FROM FRAME 5 TO FRAME 19, BETWEEN STRINGER 15 TO STRINGER 20
CORRECTIVE ACTION: PHOENSDR IPXA2019112549386Skin · crackedINSPECTION TYPE:N/AFUSELAGE SKIN CRACK AT THE UPPER AFT CORNER OF THE RH AC DOOR STA535 .REPAIRED IAW EO MD11-5330-7424-A.SDR SWAA2019122639904Skin · corrodedEXTERNAL CROWN SKIN CORRODED BETWEEN BS. 905 TO BS. 986.5, BETWEEN STR. 2L TO STR. 2R. REPAIRED SKIN PER ER AND EA.SDR ABXA201912104186Skin · damagedDAMAGE IN THE FUSELAGE SKIN AT THE RIGHT FORWARD DOOR CUTOUT, AFT LOWER CORNER, STRINGER 20R, BETWEEN FUSELAGE STATIONS 325 AND 347. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201912104185Skin · damagedDAMAGE IN THE FUSELAGE SKIN AT THE LEFT FORWARD DOOR CUTOUT, AFT LOWER CORNER, STRINGER 20L, BETWEEN FUSELAGE STATIONS 325 AND 347. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR CALA2019112702089Skin · chafedV/STAB R/H ROOT PNL 321AR 322AR TO FUSELAGE INTERFACE CROWN SKIN FOUND CHAFING FROM BSTA 2129 TO BSTA 2150 REF NON-ROUTINE NO. 9 488996 - ORIGINATED BY EMP V916782 SPEC NO. B777-55-3-7032. PERFORMED BY EMP V916782, V/STAB R/H ROOT PNL 321AR 322AR TO FUS ELAGE SDR FDEA201911243085Skin · dentedINCOMING ITEM : LOWER LH FUSELAGE AT STA 1225, BETWEENSTRINGERS 32L-33L HAS A DENT COMPLIED WITH EA H-5310-T0350997 A. TITLED "FUSELAGE-MAINFRAME-FUSELAGE SKIN, STA 1225 BETWEEN S32L-33L, DENT". REMOVED AND REINSTALLED PIT SIDEWALL PANEL IAW B767 AMM 25-SDR MK1Y20191124005Skin · dentedDURING MAINTENENCE CHECK FOUND DENTS COMMON TO THE UPPER AND LOWER FUSELAGE SKIN PANEL (P/N 146T3231-1, 146T3241-12)SDR MK1Y20191124004Skin · corrodedDURING MAINTENENCE DEEP CORROSION FOUND ALONG THE DRAIN MAST CUTOUT.SDR U2RA2019121930001Skin · dentedSKIN DENT WITH CREASE, AT BODY STATION 580, BETWEEN STRINGERS 26R AND 27R, JUST BELOW THE FORWARD CARGO DOOR THRESHOLD - ACCOMPLISHED MAJOR REPAIR OF FUSELAGE SKIN IN ACCORDANCE WITH BOEING SERVICE REQUEST ID # 3-4540838648.SDR U2RA2019121920001Skin · dentedDENT IN SKIN BELOW FORWARD CARGO DOOR CUTOUT AT BODY STATION 580, BETWEEN STRINGERS 28R AND 29R - ACCOMPLISHED MAJOR REPAIR OF FUSELAGE SKIN IN ACCORDANCE WITH BOEING SERVICE REQUEST ID # 3-4540838648.SDR DALA2019112836950Skin · corrodedCORROSION AFT CARGO THRESHOLD DOOR PAN AND LOWER SKIN DOOR CUT OUT. NRC 001-0371:5231-2002/002 00002: COMPLIED WITH ER/A 582992-14 REV O. (LP #1371567)SDR DALA2019112506914Skin · gougedSHIP 3832 ON INITIAL WALK AROUND FOUND DENT AND GOUGE ON FUSELAGE APPROX. 36" AFT OF L-1 DOOR OPENING AT FLOOR LEVEL .CORRECTIVE ACTION: C/W ERA 583316-14 REV ORIG SECTION . (6362042)SDR DALA2019112536901Skin · damaged(AIRCRAFT 6715, L/P 1371474) NICKS AND SCRATCHES ON FUSELAGE SKIN STA 1455 TO 1475 BTW STGR 26R TO 29R. CORRECTIVE ACTION: NICK ON BS:1459.750, BTW:27RH-28RH WAS REPAIRED PER ER/A 583236-14 REV. ORIGINAL, SECTION I: PERMANENT REPAIR AND ETI-57-19-173 R1. FOR BSDR DALA2019112536900Skin · not reported(AIRCRAFT 5643, L/P 1371379) FUSELAGE SKIN STA 395 STR 18R TO 17R PERMANENT REPAIR. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR AT FUSELAGE SKIN STA 395 STR CUT OUT IAW DELTA ERA 582140-14 REV ORIGINAL SECTION 1.SDR DALA2019112536899Skin · damaged(AIRCRAFT 5643, L/P 1371258) 2 DEEP BLEND OUTS AROUND FASTENERS ON EXTERNAL FUSELAGE SKIN BTWN STA 1520-1540 ON STR 27R. CORRECTIVE ACTION: REPAIRED AREA IAW B757 SRM 53-00-01 REPAIR 28 INSPECTION THRESHOLD 25,000 FLIGHT CYCLES. REPEAT INTERVALS 6,000 FLIGHT CSDR DALA2019112206841Skin · dented(AIRCRAFT 5643, L/P 1369948) LOCATED DENT AT FUSELAGE SKIN STA 460, STR 22R - 23R. CORRECTIVE ACTION: DENT OUT OF LIMITS PER B757 SRM 53-00-01. REMOVED DAMAGE, FABRICATED FILLER , DOUBLER, TRIPLER, ALODINED AND REPAIR PARTS. INSTALLED REPAIR PARTS. SEALED AFFESDR C77A2020020530040Skin · dentedDURING BASIC CHECK AT EAMS, DENT WAS FOUND ON THE FORWARD FUSELAGE SIDE SKIN PANEL P/N 170-03385-003 TO BE OUT OF LIMITS AND CLOSE TO THE RIVET LINE PER SRM 53-10-01/AD02. REFERENCE ETD2019-170-155785, FIGURE 1 FOR DETAILS OF THE DENT LOCATION AND DIMENSION. ESDR DALA2019112516898Skin · dented(AIRCRAFT 5643, L/P 1368823) LOCATED DENT AT FUSELAGE SKIN STA 690 STR 23L-24L. CORRECTIVE ACTION: CUT OUT DAMAGED AREA AND REPAIRED AREA IAW B757 SRM 53-00-01 REPAIR 28 FIGURE 201 THIS IS A CATEGORY B REPAIR AND REQUIRES SUPPLEMENTAL INSPECTIONS AS GIVEN IN BSDR V0XD201911240001Skin · gougedGOUGE AT BOTTOM FO FUSELAGE SKIN ALONG STRINGER 27 BEWTEEN FS 953.00 AND 969.00; CORRECTIVE ACTION: REPAIRED SKIN IAW BOMBARDIER REO 670-53-51-157, DATED: 2019-11-15.SDR DALA2019112216847Skin · damaged(LOG 1368966) DURING INSPECTION FOUND 737-800 FUSELAGE SKIN AT STA 727J-767 & STR 20L-22L HAS GROUND DAMAGE. DAMAGE REPAIRED PER ERA 573865-14.SDR SIMA201911210001Skin · corrodedINNER FUSELAGE SKIN CORRODED BETWEEN FS280 & FS295 BETWEEN STGR 25R & 24R -C/A-C/W ERS-CR-53MR-3954 SKIN REPAIR(DOUBLER) AT F.S 295 STR 24R-25RSDR DALA2019112106800Skin · dented(AIRCRAFT 5643, L/P 1368752) LOCATED 3 DENTS ON EXTERNAL SKIN REPAIR BTWN STA 1600-1620 APPROX STR 17L. CORRECTIVE ACTION: REMOVED DAMAGED FUSELAGE SKIN REPAIR DOUBLER STA 1600 TO 1620 STR 17L IAW B757 SRM 51-40-02. FABRICATED AND INSTALLED NEW REPAIR DOUBLER SDR VGCA201911269007Skin · dentedDENT IN FUSELAGE SKIN AT STATION 348 BETWEEN STRINGER 4R AND 5R
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