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 HNAA2022022300107Not Reported · not reportedE901417 - CORROSION ON DIAMOND GUSSET AT FRAME 22 .... REMOVED CORRODED DIAMOND GUSSET AT FRAME 22, POSITIONED DRILLED AND INSTALLED SERVICEABLE DIAMOND GUSSET IAW EMB 145 SRM 51-20-03, 51-40-02.SDR HNAA2022022300106Not Reported · not reportedE900666 - RH UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R. CRACK IS 3/8' LONG, MARKED. EASI #8071 USED. 50-500 KHZ PROBE, FREQ= 400 KHZ, V-GAIN= 78.0, H-GAIN= 65.0, LPF= 100 .... REPAIRED RH UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRASDR HNAA2022022300105Not Reported · not reportedE900517 - FUSELAGE SKIN HAS 2 POSSIBLE CRACKS AT FRAME 77 BETWEEN STRINGERS 05R AND 07R .... REPAIRED FUSELAGE SKIN CRACK AT FRAME 77 BETWEEN STRINGERS 06R AND 07R IAW PIEDMONT EO1-53-22-0025. ONE AREA NOT FOUND TO BE CRACKED, SEE TASK #1.SDR CALA2022022100467Stringer · damagedRII INSPECTION REQUIRED 2EA SKIN REPAIRS AT STA. 95.5 STRINGER 25L DUE TO LIGHTING STRIKES REF. LP 7695225. REGUIRED AS MAJOR REPAIR. AN ESFR MUST BE ACCOMPLISHED AND RECORDED. COMPLETED/FILED ESFR, SFR #1027780. COMPLETED/FILED ESFR, SFR #1027780.SDR SWAA2022032876148None · crackedCRACK ANGLE - CLIP LOCATED BS400 AND STR26L AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT 2022-98518 / [01] REPLACED ANGLE - CLIP LOCATED BS400 AND STR26L AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 REV. -<BR>P/N:SDR SWAA2022032876149None · crackedCRACK ANGLE - CLIP LOCATED BS440 AND STR26L AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT 2022-98519 / [01] REPLACED ANGLE - CLIP LOCATED BS440 AND STR26L AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 REV. -<BR>P/N:SDR SWAA2022032876146None · crackedCRACK ANGLE - CLIP LOCATED BS500B AND STR26L AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT 2022-98520 / [01] REPLACED ANGLE - CLIP LOCATED BS500B AND STR26L AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 REV. -.<BR>PSDR SWAA2022032876147None · crackedCRACK ANGLE - CLIP LOCATED BS500C AND STR26L AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT 2022-98522 / [01] REPLACED ANGLE - CLIP LOCATED BS500C AND STR26L AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 REV. -<BR>P/SDR DALA2022022401208None · noneSHIP 697 DENT ON FUSELAGE SKIN BTW STA 440 TO 460 AND BTW STG 22 AND 23 AT LH SIDE (FUS). CORRECTIVE ACTION: SUMMARY OF NRC 00026: DENT ON FUSELAGE SKIN BTW STA 440 TO 460 AND BTW STG 22 AND 23 AT LH SIDE WAS REPAIRED PER ETI-57-22-036 REV. 2 AND ERA 597434-14SDR DALA2022022201168None · noneSHIP 175 BULK CARGO INNER SKIN FOUND CORROSION AT STA1543 BETWEEN S39R AND S39L, CORRECTIVE ACTION: DAMAGE AREA REPAIR AS PER PRI:596985. (2128498)SDR DALA2022022201143None · noneSHIP 3268 NEED TO REPAIR EXTERNAL SKIN LOC. FR 60 TO FR 61 BTW STR 43R TO STR 44 AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR PER A320 SRM 53-00-11. (2128523)SDR DALA2022022201142None · noneSHIP 3268 NEED TO REPAIR EXTERNAL SKIN LOC. FR 60 TO FR 61 BTW STR 43R TO STR 44 AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-00-11. (2128488)SDR IPXA2022022079198Doubler · noneINSPECTION TYPE:N/AD771626 FUSELAGE SKIN DOUBLER FR 84 - 86 S44L - S44R DMG'EDREPAIRED PER EO A300-5330-82774-BSDR SWAA2022032175520Gusset · crackedFWD CARGO BAY GUSSET CRACKED BS 500D STR 19L/H / [01] REMOVED FWD CARGO BAY GUSSET AT BS 500D; STR 19 L/H IAW SRM 51-40-02-0G-0;[02] RECEIVED NEW GUSSET PART# 143A9481-5; LOCATED AND DRILLED IAW SRM 51-40-05-0G-0 AND DWG 143A7902; ID: 174; REV:-; OK TO INSTALLSDR SWAA2022032175521Gusset · crackedFWD CARGO BAY GUSSET CRACKED BS 500D STR 19R/H / [01] REMOVED FWD CARGO BAY GUSSET AT BS 500D; STR 19 R/H IAW SRM 51-40-02-0G-0;[02] RECEIVED NEW GUSSET PART#143A9481-6; LOCATED AND DRILL IAW SRM 51-40-05-0G-0 AND DWG 143A7902; ID: 174; REV:-; OK TO INSTALL;[0SDR YENA2022031500217Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION STRINGER 41R BETWEEN FR32/FR34 IN FWD CARGO COMPARTMENT; REF: ARM W/O 2022 2/1 N/R 2022-19284 REPLACED SECTION STRINGER 41R AND FASTENERS LOC ON FR32 TO FR34 IAW SRM A320 51-72-11, 51-42-11 AND DRAWINGS # E533231472, D532314SDR EE4Y2022031015231Pressure Deck · crackedDURING MAINTENANCE ACCOMPLISHMENT WERE FOUND TWO ATTACHING FASTENER HOLES WITH CRACKS LOCATED AT LH PRESSURE DECK MEMBRANE ONLY AT FR36 STR30-31LH, THE DAMAGES WERE FOUND OUT OF ALLOWABLE DAMAGE LIMITS AS PER SB A320-1263 AND SB A320-1264, DUE TO THIS FACT DETSDR DALA2022022201134None · noneSHIP 3268 NEED TO COMPLY WITH REPAIR EXTERNAL SKIN LOC. FR 61 TO FR 62 BTW STR 43R TO 44 AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR PER A320 53-00-11. (2127820)SDR CALA2022022100462Skin · crackedFR 35 STR 30 LH CRACK INDICATIONS NOTED IN FASTENER HOLE #2 FRAM E,AFT SKIN FWD SKIN LAYERS AND HOLE #3 FRAME LAYER ONLY. 5331-02848 PART 1.1. ACCOMPLISH PERMANENT REPAIR AT LH FR 35 STR BEFORE 16AUG2022. ALL WORK ACCOMPLISHED ON HAECO NR 9298178 AND 30 HOLES SDR SWAA2022032875306Gusset · crackedCRACK GUSSET LOCATED ON BS 500D AT LEVEL STRINGER 19L FWD CARGO COMPARTMENT 2022-98449 / [01] REPLACED GUSSET LOCATED ON BS 500D AT LEVEL STRINGER 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 143A7902; SHEET 259; REV. -. PART USED 143A9481-6; POSDR SWAA2022031175299Baffle · crackedFWD CARGO COMP L/H BETWEEN STA 500 AND STA 500A LBL 24' BAFFLE CRACKED / [01] REMOVED FWD CARGO COMP L/H BETWEEN STA-500 AND STA 500A LBL 24 BAFFLE. AS PER B-737-700-SRM-51-40-02-0G-0;[02] VERIFIED STEP 1 OK TO INSTALL NEW BAFFLE;[03] INSTALLED NEW BAFFLE AT FSDR R61A2022031000194Door · corrodedCF III, WASTE DOOR FOUND CORRODED. R&R WASTE DOOR IAW AMM 20-10-01.SDR AALA202202289947Skin · corrodedAIRCRAFT WAS GROUNDED: 3 BY 1 INCH AREA OF CORROSION WITH A 0.5 INCH LONG CRACK LOCATED AT STA 919 AND BETWEEN STR 21 TO 22 LEFT. REINFORCED WITH DOUBLER/TRIPLER REPAIR PER SRM 53-70-01-2R-3 AND EA 334273.SDR DALA2022021801111None · noneSHIP 175 LOWER FUSELAGE SKIN AT AFT VACUUM BLOWER OUTLET PORT FOUND WITH CORROSION, CORRECTIVE ACTION: REPAIR AS PER B767-300 SRM53-60- 01-2R, TO C/O INSPECTION 37500 FLIGHT CYCLES AFTER AIRPLANE DELIVERY OR 6000 FLIGHT CYCLES. (2125940)SDR SWAA2022032873967Stringer · crackedCRACK STRINGER 26R LOC BS540 AT FWD CARGO COMPARTMENT 2022-109242 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N:130064101 DUE DATE: 11-MAR-22;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATSDR SWAA2022032273898Angle · crackedCRACK ANGLE - CLIP LOCATED ON BS 440 AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2022-80383 / [01] REPLACED ANGLE - CLIP LOCATED ON BS 440 AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND B737-700 SRM 51-40-02 AND SDR SWAA2022032273899Angle · crackedCRACK ANGLE - CLIP LOCATED ON BS 500C FWD FACE AT LEVEL STR 26R AT FWD CARGO COMPARTMENT 2022-80384 / [01] REPLACED ANGLE - CLIP LOCATED ON BS 500C FWD FACE AT LEVEL STR 26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ; B737-700 SRM 51-40-02 AND SDR SWAA2022031673880Splice Plate · corrodedDOT#44-186 FWD CARGO COMPARTMENT FWD SPLICE PLATE CORRODED / [01] NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. FWD CARGO BAY FLOOR SPLICE PLATE IS OUT OF LIMITS.;[02] VERIFIED AND REPLACED ON SHELF: NEW FWD CARGO FLOOR SPLICE PLATE MPN: 453A1611-25 ATAG: A115564 ISDR SWAA2022031673883Angle · corrodedDOT#40-186 FWD CARGO COMPARTMENT Z ANGLE CORRODED STA 500C+6' TO 500I LBL24 WL 156 / [01] REMOVED CORROSION FROM STA 500C+6 -500G IAW SRM 51-10-02 10X MAGNIFY ORIGINAL THICKNESS .040 .008 MATERIAL REMOVED OUT OF LIMITS IAW SRM 53-00-53-1A-2 AAR TOOL NO. 36647 SDR SWAA2022031673875Angle · corrodedDOT#35-186 FWD CARGO COMPARTMENT Z ANGLE CORRODED STA 460+6' TO 500C LBL 24 WL 156 / [01] REMOVED CORROSION FROM STA 460+ 6 - STA 500 B IAW SRM 51-10-02 10X MAGNIFY ORIGINAL THICKNESS .040 .003 MATERIAL REMOVED .037 MATERIAL REMAINS FOUND TO BE IN LIMITS IAW SSDR SWAA2022030373988Skin · corrodedSKIN PITTING AND ANOMALIES FROM STA 887 TO 1016 STR 4L TO 4R / [01] CORROSION REMOVAL STEPS 1- 20;[24] RESQUEST OK TO RE-INSTALL FASTENERS IN PANEL SKIN L/H BS 927+10' TO 947+10' STR 3 ; L/H BS 947 TO 967 STR 4 ; L/H BS 967 BTW STR 3 -STR4 ; L/H BS 987+14' TO SDR SWAA2022030373990Skin · corrodedSKIN PITTING AND ANOMALIES FROM STA 887 TO 1016 STR 4R TO 14R / [01] CORROSION REMOVAL STEPS 1-3.;[30] STATUS COMPLETE STEPS 1-38. SKIN DAMAGE REPAIRED ON REF: FAULT TTG8Q00B2878; TTG8Q00B2WUH ; EA 22-153-00606 REV: A.;[31] ALL WORK COMPLETE;[32] UPDATE STEP 1SDR AALA202202275080Skin · corrodedAIRCRAFT WAS GROUNDED: CORROSION OF SKIN AROUND WASTE TANK EXHAUST VENT BETWEEN STA 907 AND STA 927 BETWEEN STR 21L AND STR 22L. **SUPPLEMENTAL REPORT: ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 53-70-01-2R AND EA334273.** (CLOSED)SDR AALA202202249365Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON FUSELAGE SKIN LOCATED AT STA 972 BETWEEN LBL 26 AND LBL 27. REPAIRED SKIN PER EA 333893.SDR IPXA2022022479366Stiffener · noneINSPECTION TYPE:1CLH MLG 3RD VERTICAL STIFFENER CRACK AT LWR END WHEEL WELL.REMOVED AND REPLACED CRACKED STIFFENER IAW MD-11 SRM 51-35-01 AND 51-33-01 (MINOR).SDR DALA2022021801113None · noneSHIP 175 CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STA 1543, S39L-39R. CORRECTIVE ACTION: ER/A REVISION IS REQUIRED PRIOR TO 37,500 TOTAL FLIGHT CYCLES IN ORDER TO ENSURE THIRD STAGE APPROVAL IS RECEIVED. (2125145)SDR CALA2022021800421Plate · corrodedAFT CARGO PIT R/H DOOR SILL SUPPORT BOX BETWEEN FR52A-56, HAS CO RROOSION ON UPPER SURFACE.A3NB-05-3-6023. GENERATED BY V919150 A T HAECO LCQ PER NR:9298328 (36328) REMOVED 7 REPLACED AFT CARGO PIT R/H DOOR SILL SUPPORT FR52A-56 IAW A320 SRM 51-72-11 PERFORMEDSDR DALA2022021701093None · noneSHIP 174 FOUND 2 DENTS COMMON TO FWD FUSELAGE RH SIDE BETWEEN STA148.75 AND STA164.75 AND 5.7" BELOW THE LAP SPLICE AT STR24, CORRECTIVE ACTION: REPAIRED AS PER PRI592090-14 REV.0. (2124700)SDR DALA2022021701057None · noneSHIP 3130 - L2 DOOR HAS DENT IN OUTER SKIN, LOWER AFT CORNER. CORRECTIVE ACTION: REPAIR PER A319 SRM 52-10-00. (2124761)SDR SWAA2022031573552Gusset · crackedGUSSET CRACKED BS 500D STR 21L FWD CARGO BAY / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-OG-0 STEP 9.;[02] REMOVED GUSSET CRACKED AT BS 500D STR.21 L FWD CARGO BAY;IAW SRM 51-40-02-OG-0.;[0SDR SWAA2022031573553Gusset · crackedGUSSET CRACKED BS 500D STR 19R FWD CARGO BAY / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-OG-0 STEP 9.;[02] REMOVED GUSSET CRACKED AT BS 500D STR. 19R FWD CARGO BAY;IAW SRM 51-40-02-OG-0.;[0SDR SWAA2022030373527None · crackedCRACK AND EDGE DAMAGE ON FSD CUTOUT FWD FRAME ON FITTING FOR FSD UPPER HINGE CUTOUT; LOCATED AT BS 295 STR 10R (MARKED) / [01] REQUEST NDI FOR END OF CRACK;[09] LOCATED AND DRILLED NEW FSD UPPER HINGE BOX I.A.W SRM 51-40-05-0G-0 AND BOEING DWGS 141A8353;141A83SDR REXA2022030300349Stringer · corrodedSTGR 26L BETWEEN FS 1000 AND FS 1015 CORRODED. - REPAIRED STR 26L BETWEEN FS 1000 TO FS 1015 IAW ENDEAVOR AIR EA CRJ 953-12832.SDR IPXA2022030279655Skin · damagedINSPECTION TYPE:A300AT APPROX STA 1860 LOWER SKIN BETWEEN STR 25L-25R HAS SEVEREDAMAGE THROUGH SKINREPAIRED PER EA 757-5381-27-A2839 AND UPS EO B757-5310-82987-ASDR IPXA2022022779462Intercostal · noneINSPECTION TYPE:C4R/H WHEEL WELL LWR FWD BRAKE ACCUMLATOR INTERCOSTAL IS CRACK.REPAIRED CRACK INTERCOSTAL IAW MD-11 SRM 53-40-12 REPAIR 3 AND SRM 51-33-01 PG8 (MINOR)SDR SWAA2022022172736Skin · corrodedAFTER PAINT STRIP FOUND SOME SKIN PITTING AND ANOMALIES FROM STA 887 TO 1016 AND STR 14R TO STR 4L / [01] TRANSFERED TO LOG PAGE 1934972 EA 22-151-00483;[02] OK TO FERRY TSR 2022001181SDR DALA2022021701095None · noneSHIP 174 ERA 592090-14 REV A ISSUED FOR REPAIR TO STA 157, S24R REPAIR DO UBLER. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: ACCOMPLISH ERA 592090-14 REV A SECTION IV AT OR BEFORE 37500 TOT AL FLIGHT CYCLES (2123353)SDR IPXA2022021579031Skin · noneINSPECTION TYPE:N/ASKIN DMG AT TAIL BALL STAND AFT SKIN PNL AT STA 2598 BETWEEN S-26R AND S-42RREPAIRED PER EO B747-5330-82748-ASDR SWAA2022031572355Skin · corrodedCORROSION AROUND FASTENERS ON FUSELAGE SKIN FROM B.S. 1016-1088; L.B.L. 15-R.B.L.15; W.L. 306.5. / [01] REMOVED CORROSION FROM AROUND FASTENERS AT FUSELAGE UPPER SKIN BS 1016 TO BS 1088; LBL15 -RBL15; WL 306.5 IN AREA OF 20' X 1.5' ORIGINAL MATERIAL THICKNESS SDR DALA2022022701239None · noneSHIP 174 ERA 596987-14AD ISSUED FOR REPAIR TO STA 1725.5, STR 7R. FOLLOW ON ACTION IS REQUIRED, CORRECTIVE ACTION: ACCOMPLISH ERA 596987-14AD SECTION II AT 37500 TOTAL FLIGHT CYCL ES, THEN EVERY 6000 FLIGHT CYCLES THEREAFTER (2121066)
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