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 VGCA2019112619005Skin · corrodedCORROSION ON CENTER WING BOX UPPER SKIN PANEL AT BODY STATION 870, LEFT BODY LINE 67SDR CALA2019112532036Skin · stainedB757-06-3-0230 BLUE WATER STAINS ON FWD CARGO LH SIDE WALL FROM STA 600 TO STA 900 STR 21L TO STR 26L. RG56 REF ST ENG N/R 00810 00SDR DALA201911216795Skin · dented(AIRCRAFT 6812, L/P 1367012) DENTS ON EXTERNAL FUSELAGE REPAIR DOUBLER BTW STA: 1600-1620 AND STGR: 18L-19L. CORRECTIVE ACTION: EXTERNAL FUSELAGE REPAIR DOUBLER BTW STA: 1600-1620 AND STGR: 18L-19L WAS REPLACED PER ERA 583144-14 REV. ORIGINAL AND ETI-57-19-163SDR DALA2019112006792Skin · not reportedREPAIR AT FR23 AT STR22L WAS ACCOMPLISHED PER A319 SRM 53-00-11 FIGURE 204 (SUPERSEDED BY TASK 53-00-11-300-042 FOR THIS FRAME SECTION). REQUIRES FOLLOW ON INSPECTIONS PER A319 SRI TASK 53-00- 11-205-017 IIR-53-00-11-2-017-00. THIS INSPECTION REQUIREMENT HAS BSDR SWIA2020031049104Skin · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA EA - REMOVED DAMAGE FROM SKIN AROUND THE GROUND AIRCONNECTION DOOR, WIFI DOUBLER AND FOUND REMAINING SKIN THICKNESS TO BE WITIN LIMITS REF STS EA --, ACCOMPLISH A DETAILED VISUAL INSPECTION PER NDTM OF THE REPAIR AREASDR DALA2020022501408Fastener · damagedSHIP 3893 DURING LIGHTNING STRIKE INSPECTION, FOUND DAMAGED FASTENER AT STATION 488 STRINGER 18L . CORRECTIVE ACTION: DAMAGE FOUND TO BE OUT OF LIMITS PER B737-900 SRM 53-00-01-1A-5 FIG 102 SHEET 1. PERFORMED CATEGORY C REPAIR PER B737-900 SRM 53 -00-01-2R-38 SDR SWIA2020010947604Skin · dentedFUSELAGE DENT LOCATED NEAR UPPER FLANGE OF STGR24L AT 3.50" AFT OF FS 202.75 CANNOT BE DRESSED-BACK TO ORIGINAL COUNTOUR REFERENCING REO AS IT GOES INTO NON-MILLED SKIN UNDER, OR COMMON TO, STGR24L. (C-CHECK) RO 01/07/2020 PERFORMED PATCH REPAIR TO FUSELAGE DSDR U2RA2019121980001Skin · dentedDENT IN SKIN BELOW FORWARD CARGO DOOR CUTOUT, AT BODY STATION 578, BETWEEN STRINGERS 26R AND 27R - ACCOMPLISHED MAJOR REPAIR OF FUSELAGE SKIN IN ACCORDANCE WITH BOEING SERVICE REQUEST ID # 3-4540838648.SDR SWIA2019121847025Skin · chafedWHILE ACCESSING FOR PRESSURE FLOOR MOD SB 670-53-036 FOUND SKIN CHAFFED UNDER PANEL 196DL AT STR27 BETWEEN FS.977 - 985.00. (C-CHECK) RO 12/14/2019 REPAIRED SKIN CHAFE BY BLENDING OUT DAMAGED AREA FOR NDT THICKNESS CHECK,FOUND DAMAGED ARES OUT OF LIMITS PER RSDR NACA2019111800140Skin · crackedDISCREPANCY: TEMPORARY REPAIR INSTALLED @ BS325-BS347, S35L-S36L, PERMANENT REPAIR OR DTA ANALYSIS REQUIRED. CORRECTIVE ACTION: REMOVED AND REPLACED TEMPORARY REPAIR @ BS325-BS347, S35L-S36L IAW AMES DOC. 47390REA01 AND B767-300 SRM 51-40-02 P7, AND AMM 51-21-SDR SIMA20191118001Skin · dentedDENT AND SCRATCH LH REAR FUSELAGE II BETWEEN FR 78 AND FR 79 AND STR 5L AND 7L-C/A-PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-3952SDR 2020F00048Skin · damagedRIGHT WING ROOT SKIN DAMAGE (MIS-DRILLED HOLE). ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ23664M1 DATED NOV. 11, 2019; 680-0149 (N389QS) RIGHT WING ROOT SKIN DAMAGE (MIS-DRILLED HOLE).SDR DALA2019112086779Skin · dented(AIRCRAFT 6812, L/P 1364514) 2 DENT WERE DONE ON NEW SECTION SKIN STA 600 BTW STRINGER 18LH-19LH, PROTUBERANCE WAS DONE ON NEW SECTION SKIN STA 620 ABOVE STRINGER 18LH AND TOOL MARKS WERE DONE ON SPLICE REPAIR DOUBLER STA 589-596 STRINGER 17LH. CORRECTIVE ACTISDR SIMA2019121216005Skin · crackedRH AFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R.-C/A-INSTALLED REPAIR DOUBLER, FILLER, "L" ANGLE AND SHIM FOR REPAIR OF RH AFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R IAW EMB 145 SRM 53-31-01, ITEM 1SDR SIMA2019112516004Skin · crackedFUSELAGE CRACK BETWEEN FO WINDSHIELD AND DV WINDOW-C/A-REPAIRED UPPER SKIN PANEL I/A/W ENVOY ERS-EM-56MR-162SDR A6WA2019112047016Skin · crackedNOSE LANDING GEAR SPADE DOOR CUT OUT RH AND LH AFT CORNERS CRACKED AIRCRAFT REMOVED FROM SERVICE REPAIRED NOSE LANDING GEAR SPADE DOOR CUTOUT SKIN RH AND LH CORNERS IAW BOMBARDIER REO 601R-53-11-010SDR YENA2019111950657Skin · dentedDURING HEAVY MAINTENANCE, WHILE PERFORMING EVALUATION TO CONVERT TO PERMANENT A TEMPORARY REPAIR IAW REF/2/ RDAS ADDITIONAL DAMAGES WERE FOUND IN THE SURROUNDING AREA TO THE DENT. DENTS AND GOUGES WERE FOUND BETWEEN FR 14-16 & STGR 36RH OF THE FWD AVIONICS BAYSDR DALA2019111966764Plate · damaged(LOG 1361049) DURING INSPECTION FOUND SEVERAL NICKS ON ALTERNATE STATIC PORT PLATE. ALTERNATE STATIC PORT PLATE (FUS) WAS REPAIRED PER ETI-37-19-339 REV 5 AND ERA 583069-14 REV ORIGINAL.SDR YENA2019111850650Skin · dented(HEAVY MAINTENANCE)DURING NORMAL OPERATIONS AT DCA ON 9/22/2019, N348JB (MSN 511) WAS REPORTED WITH A DENT AT THE CENTER FUSELAGE III FR 89 STGR 20-21R. THE DENT WAS MEASURED TO BE 129MM L X 73MM W AND AT DEEPEST POINT 2.44MM (SEE REF /1/ ETD FOR DETAILS). THSDR SWAA2022040759807Intercostal · crackedMAIN CABIN FLOOR STRUCTURE INTERCOSTAL AT BL0 BETWEEN STA 500D AND STA 520 HAS UPPER ANGLE CRACKED AT FASTENER HOLE. / REMOVED AND REPLACED UPPPER ANGLE AT MAIN CABIN FLOOR STRUCTURE INTERCOSTAL AT BL0 BETWEEN STA 500D AND STA 520 AS PER REF B737-700 SRM 51-40SDR SWIA2019123147527Skin · corrodedEXTERNAL SKIN UNDER FARING 191BB AND 192BB HAS CORROSION AROUND NUT PLATES (C-CHECK) RO 12/27/2019 REMOVED CORROSION UNDER FAIRINGS PANELS 191BB AND 192BB REF CRJ200 SRM, MATERIAL THICKNESS IS OUT LIMITS REF CRJ200 SRM, COMPLIED WITH ALL STEPS 1-6 REF BOMBSDR A6WA2019112047015Doubler · damagedFWD LHS FUSELAGE ACCESS PANEL 131AL SURROUND DOUBLER HAS TWO SCREW HOLES WITH DEEP COUNTERSINKS AT 1 O"CLOCK & 3 O"CLOCK. AIRCRAFT REMOVED FROM SERVICE REPAIRED IAW BOMBARDIER REO 601R-11-162 REV.C, DATED 2015/11/16.SDR FDEA2019111542959Stop · wornLATCH STOPS WORN ACCESS PANEL 311AB RH SIDE. TITLE: FUSELAGE - PLATES AND SKINS - 311AB ACCESS DOOR CUTOUT LANDING SKIN RH FWD DAMAGE REPAIR WAS ACCOMPLISHED ON EA 8-5310-T0350318. MAJOR REPAIRSDR DALA2019111406668Skin · crackedLEFT AFT FUSELAGE STA 1702 JUST BELOW STRINGER 6L EXTERIOR SKIN IS CRACKED EXTENDING AFT FROM RIVET HEAD. REPAIRED PER SRM 53-80-01. (LP 1359045)SDR SWAA2022040663873Skin · corrodedFOLLOWING REMOVAL OF THE LH PICKLE FORK FRAME ASSY BY BOEING AOG; CORROSION WAS FOUND AT TWO FASTENER HOLE LOCATIONS IN THE P/N 144A3311-51 SKIN. THE CORROSION AND HOLE LOCATIONS ARE DOCUMENTED IN BOEING FRR-5. LOCATION: STA 665-667; WL 197; LBL 70. NRC WRITTESDR FDEA201901130109Skin · corrodedR/H AFT FUSELAGE BELOW HORZ. STAB CUT-OUT, NUMEROUS SURFACE CORROSIONS AROUND FASTENER HOLES FOR PNL 348BF AND 347DF REPAIRED AFT FUSELAGE SURFACE AT HORIZONTAL TAB CUTOUT IAW SRM 53-70-01-00 REPAIR #3 FIG 201 PG 202 AND JPF ITEMS.SDR C77A2020011540014Finger Doubler · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS FOUND TO THE CENTER FUSELAGE III
CARGO DOOR SURROUND LOWER FINGER PLATE. REFERENCE ETD2019-170-152677 FIGURE 1 FOR
DETAILS, FOR THE DAMAGE LOCATIONS AND DIMENSION. THE DAMAGE IS IN A NO DAMAGE ALLOWED
AREA OFSDR FDEA2019122633297Skin · corrodedRT AFT FUSELAGE BELOW APU COMP COOLING AIR OUTLET, EXFOLIATION CORROSION AROUND FASTENER HOLE FOR PNL 347DF. REPAIRED AREA BELOW APU COMP COOLING AIR OUTLET REF SRM 53-70-01 FIG 201 SH 1 MAJOR REPAIR.SDR FDEA2019111532941Skin · crackedFR40 CTR WING JOINT AT UPPER SKIN LEVEL LH MIDDLE HOLE NDT HFEC INSPECTION FOUND CRACK SIGNAL. FR40 CTR WING JOINT AT UPPER SKIN LEVEL LH MIDDLE HOLE CRACK. COMPLIED WITH FEDEX EA:6-5710-T0350731 P1. TITLE: WINGS - BASIC WING STRUCTURE - CRACK IN THE MISDR DALA2019111846746Skin · dented(AIRCRAFT 5643, L/P 1358130) LOCATED DENT AT FUSELAGE SKIN STA 500, STR 23R-24R. CORRECTIVE ACTION: FABRICATED REPAIR DOUBLER AND FILLER IAW B757 SRM 53-00-01, REPAIR 29 & NDTM PT 6 51-00-16, INSTALLED ID TAG IAW DPS 900-5-1 NO:04, PERFORM A DECAL CONDITION INSDR DALA2019111846745Skin · dented(AIRCRAFT 5643, L/P 1358095) DENT ON EXTERNAL FUSELAGE SKIN BTWN STA 1320-1340, BTWN STR 29L-30. CORRECTIVE ACTION: FABRICATED REPAIR PARTS. LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR PARTS AS REQ IAW B757 SRM 53-00-01 R.29, SRM 51-40-02, 51-40-05, 51-40-0SDR CALA2019111601976Panel · damagedRH FR35 STRINGER 30 HAS REJECTABLE DAMAGE ON HOLE NUMBER 3 ON NR 9290222 PER HAECO LCQ REPAIRED #3 HOLE RH FR35 AT STR 30 IAW ECRA 5331-02503. CREATE A DTA DIP TO READ ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF ECR A 5331-02503 ON OR BEFORE 09MAY2020. PLANNISDR DALA2019111546724Skin · damaged(LOG 1358494) DURING HCK AT QRO, MULTIPLE NICKS WERE FOUND AFFECTING AN EXISTING REPAIR INSTALLED PER REF /2/ ON SKIN PANEL P/N 143A3252-30 BETWEEN STATION 380-440 AND STRINGERS 20R-26R. MAINTENANCE REPAIRED DAMAGE PER ERA 583069-14.SDR SWAA2019111438819Skin · corrodedFOLLOWING REMOVAL OF THE R/H PICKLE FORK FRAME ASSEMBLY CORROSION WAS FOUND AT TWO FASTENER HOLE LOCATIONS IN THE SKIN, BETWEEN BS. 665 TO BS. 667, RBL 70. / REPAIRED SKIN PER EA.SDR FDEA201911122926Skin · damagedEXTERNAL SKIN DOUBLER REPAIR IS GOUGED IN 2 PLACES AND DENTED AT FASTENER HOLE BS 418-BS 419,STR 17 LEFT SIDE AFT OF L1 DOOR REMOVED AND REPLACED DOUBLER PER B757 SRM 53-00-01-2RSDR C77A2020012700024Doubler · corrodedCORROSION FORWARD CARGO ON TRANSPONDER 1 ANTENNA DOUBLER BETWEEN FRAMES 19 AND 20 AND STRINGERS 26L AND 27L, X= 230", Y= -11", Z= -65";REMOVED AND REPLACED TRANSPONDER 1 ANTENNA DOUBLER BETWEEN FRAMES 19 AND 20 AND STRINGERS 26L AND 27L. REF EMB175 SRM 51-40-0SDR AALA201911229031Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON GOGO ANTENNA INTERNAL MOUTING BRACKET DOUBLER BETWEEN FR 56 AND FR 57, BETWEEN S42L AND S43L. REPAIRED GOGO ANTENNA INTERNAL MOUTING BRACKET DOUBLER PER EA 299502.SDR FDEA2019111522926Skin · gougedEXTERNAL SKIN DOUBLER REPAIR IS GOUGED IN 2 PLACES AND DENTED AT FASTENER HOLE BS 418-BS 419,STR 17 LEFT SIDE AFT OF L1 DOOR REMOVED AND REPLACED DOUBLER PER B757 SRM 53-00-01-2RSDR DALA2019111306630Skin · delaminatedDELAMINATED UPPER SKIN PANEL 147EB. REPAIRED UPPER SKIN PANEL 147EB ON LOWER FUSELAGE AS PER ER/A 582728-14 PRI REV.0; ER/A 582728-14 REV.ORIGINAL AND FAM A320 SRM 51-77-13-911-007.SDR DALA2019111306629Access Panel · delaminatedDELAMINATED ACCESS PANEL 191BB AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 191BB AT LOWER FUSELAGE AS PER ER/A N .542077-14MA REV C A319 SRM 51-77-13-911-001 AND SRM 51-77-13-911-006.SDR SWIA2019122747439Doubler · corrodedNTERNAL FUSELAGE AT BS 559+80 TO 559+96 FOUND CORROSION ON THE BELLY DRAIN DOUBLERS LT AND RT. REMOVED CORROSION FROM 2EA FUSELAGE BELLY DRAIN DOUBLERS IAW SRM.SDR RAIA2019111510003Skin · corrodedMAIN CABIN BELLY SKIN HAS CORROSION BETWEEN STR 21LH & 21RH BETWEEN FRAME 38 & 39- REMOVED CORROSION FROM BELLY OF FUSELAGE INTERNAL SKIN BETWEEN FR38-39, STR21L-21R, FABRICATED DOUBLER & BEGAN INSTALLATION. COMPLETED REPAIR ON MAIN BELLY SKIN AT FR 3SDR A6WA2019111346998Skin · dentedFOUND 1EA. PROTRUDING DENT LOCATED BETWEEN F.S.654.50 AND F.S.672.20 BETWEEN STGR27 AND STGR26R. AIRCRAFT REMOVED FROM SERVICE REPAIRED DENT DAMAGE TO FUSELAGE LOWER SKIN FROM F.S.654.50 TO F.S.672.20, STGR 27 TO STGR26R IAW ASAP EA# AWAC-CRJ253-01371.SDR LR7A20191112213Skin · dentedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5301, FOUND THE FWD FUSELAGE LH SKIN WITH MULTIPLE DENTS AND SCRATCHES AT FS192.5-197.5, WL164-170, LBL73. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 0170.SDR CALA2019111101960Skin · dentedCUSTOMER SERVICE REPORTS DENT NEAR L2 DOOR. DENT IS BETWEEN STRINGER 15 AND 16 AT STATION 392.25. MEASURED DENT LOCATED BETWEEN STR 15 AND 16 L AND B.S.392 DENT MEASURES 4.625L X3.25 W WITH A DEPTH OF .140 A/Y= 3.25/.140=23.2, AND IS NOT WITH IN THE ALLOWABLE SDR CALA2019111101959Skin · damagedSUPPORT TASK EA 5300-02572 REV A OP 002 DURING VIASAT AFT DOUBLE R INSTALLATION P/N AR230-2502-02,1EA HOLE MIS-DRILLED THROUGH DO UBLER AND CROWN SKIN AT STA 625.5 ABOVE I/B SIDE OF STR 2R.REF S T. ENGINEERING N/R ACCOMPLISHED EC/RA 5300-02664 ON CROWN STRUCTUSDR CALA2019111101958Skin · damagedSUPPORT TASK EA 5300-02572 REV A OP 002 DURING VIASTAT FWD DOUBL ER INSTALLATION P/N AR230-2502-01, 2EA HOLES WERE MIS-DRILLED TH ROUGH DOUBLER AND CROWN SKIN AT STA 575 JUST I/B OF STR 2R. REF ST ENG N/R 0076290 ACCOMPLISHED EC/RA 5300-02664 ON CROWN STRUCTURSDR SWIA2019122747433Skin · corrodedFUSELAGE AFT BOTTOM OUTER SKIN HAS SEVERAL CORRODED FASTENERS FROM BS 559+80 TO 559+112, STRINGER 27. REMOVED THE CORROSION FROM THE EXTERNAL SKIN IAW SRM 51-21-06. ORIGINAL MATERIAL THICKNESS .058", MINIMUM MATERIAL REMAINING .051", MAX MATERIAL REMOVED .SDR SWIA2019122747431Skin · dentedFUSELAGE SKIN DENTED AT APPROXIMATELY BS 256, STRINGERS 25 - 26R. REPAIRED THE SKIN IAW REO, FOUND TO BE WITHIN LIMITS.SDR SWIA2019121846955Skin · corrodedFOUND MULTIPLE AREAS OF CORROSION AROUND FASTNER HEADS ON THE OUTER SKIN OF THE AIRCRAFT FROM F.S 559.00 TO F.S 574.00 FROM STRINGER 25L TO 25R. (C-CHECK) RO 12/14/2019 REMOVED CORROSION FROM F.S 559.00 TO F.S 574.00 STRINGER 25L TO 25R IAW REO. WEIGHT CHAN
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