JASC 5310

Service difficulty reports · 38,528

Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310'
  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.

SDR FDEA202201080114Seat Track · unknownN00373 AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR55 TO FR57.3,-Y1959 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A3Jan 8, 2022 · N731FD · Airbus A300*SDR FDEA202201080113Seat Track · unknownN00371 AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR59 TO FR60,Y1959 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-Jan 8, 2022 · N731FD · Airbus A300*SDR FDEA202201080112Seat Track · unknownN00370 AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR61 TO FR62,Y1456 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-Jan 8, 2022 · N731FD · Airbus A300*SDR SWAA2022021559161Tie Clip · crackedCRACK ON TIE CLIP LOCATED BS 520 STRINGER 25R AT FWD CARGO COMPARTMENT ; 2022-12145 / [01] REPLACED TIE CLIP LOCATED BS 520 STRINGER 25R AT FWD CARGO COMPARTMENT IAW EA#22-153-00257-WIP1 (TTG8Q00AHLRM) AND EA # 22-153-00257 (TTG8Q00AQBQ3) SEE INDIVIDUAL SIGN OJan 7, 2022 · N423WN · Boeing 737*SDR ASAA2022010737149Support · wornMOST INBD SUPPORT FOR FAIRING PANEL 193AR REQUIRES FABRICATION. GROUNDED - YES. FABRICATED MOST I/B SUPPORT FOR FAIRING PANEL 193AR IAW B737-800 SRM 51-40-05-0G-0.Jan 7, 2022 · N549AS · Boeing 7378FHSDR ASAA2022010737148Support · wornMOST INBD SUPPORT FOR FAIRING PANEL 193AL REQUIRES FABRICATION. GROUNDED - YES. FABRICATED MOST I/B SUPPORT FOR FAIRING PANEL 193AL IAW B737-800 SRM 51-40-05-0G-0.Jan 7, 2022 · N549AS · Boeing 7378FHSDR FDEA202201070022Bulkhead · damagedMDIS 652 53-10 4930 05JAN22 FNT OPEN U AFT PRESSURE BULKHEAD PUNCTURED AT LEFT SIDE, MAIN DECK FLOOR LEVEL, BY GUIDE BAR LEFT ABOARD FROM ONLOADING COMMANDER. SHGN 05JAN22 18:14 FNT U REMOVED MDC AFT LEFT BULKHEAD PARTITION TO ACCESS AND Jan 7, 2022 · N652FE · Airbus A300*SDR SWAA2022013158960Web · corrodedSUPPLEMENTAL INFORMATION: AFT CARGO THRESHOLD WEB HAS SURFACE CORROSION AROUND FASTENER HOLES. MARKED ; / [01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [02] INSPECTION C/W ON CA #1.; [03] PARTS DATA UPDATE ONLY;Jan 6, 2022 · N917WN · Boeing 737SDR REXA2022042000657None · corroded280 FLOOR BEAM IS CORRODED BETWEEN RBL 9 AND BL 0 - REMOVED AND REPLACED 280 FLOOR BEAM R/H SIDE IAW CRJ900 SRM 51-42-06, 51-42-13, 51-42-21, 51-42-22Jan 6, 2022 · N197PQ · Cndair CL6002D24SDR SWAA2022013159073Angle · corrodedR/H CABIN R1 DOOR CREASE BEAM O/B ATTACH ANGLE CORRODED ; / [01] REMOVED CORROSION FROM ATTACH ANGLE AND VERIFIED MATERIAL LOSS ( FOUND OUT LIMITS THICKNESS REMOVED MORE THAN 50% ) IAW SRM 53-10-15-1A-2.; [02] REMOVED ATTACH ANGLE IAW SRM 53-10-15-1A-2: SRM 51Jan 6, 2022 · N8623F · Boeing 7378H4SDR AALA202201215537Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF L CHANNEL SUPPORT OF THRESHOLD PLATE AT FWD SERVICE DOOR BETWEEN STA 300 AND STA 328 AT STR 19R, MEASURING L=1.0 IN, W=1.0 IN, D=0.015 IN. REPLACED SUPPORT WITH NEW IAW AARD 51-00-05-1.Jan 6, 2022 · N826NN · Boeing 737*SDR FDEA202201060021None · delaminatedREWORK N00508; CORRECTIVE ACTION REQUIRES REPORTABLE DISCREPANCY REPORT (RDR) PER ITEMS 3,5,6 (RDR REVISED 8-23-21) AND SERVICE DIFFICULTY REPORT ITEM 13,14 (GMM REVISION 177) REMOVED AND REPLACED LOWER AFT RUDDER REF AMM 27-20-20-4.Jan 6, 2022 · N586FE · Doug MD11FSDR FDEA202201060020None · delaminatedREWORK N00507; CORRECTIVE ACTION REQUIRES REPORTABLE DISCREPANCY REPORT (RDR) PER ITEMS 3,5,6 (RDR REVISED 8-23-21) AND SERVICE DIFFICULTY REPORT ITEM 13,14 (GMM REVISION 177) REMOVED AND REPLACED LOWER AFT RUDDER REF AMM 27-20-20-4.Jan 6, 2022 · N586FE · Doug MD11FSDR CALA2022010700066Stop Fitting · crackedRH-FR66, DOOR STOP #1, LOWER INBOARD HOLE HAS CRACK INDICTION.() SUPPORT TASK AD 2018-03-12. R/H FR66 #1 LOWER I/B HOLE. REPAIED AND REAMED IAW SRM 53-41-12- ATTACHED EMP# V934344 WORK ACCOMPLISHED AT ST ENGINEERING AEROSP 300-10. ORG REAMED .394 FINAL DIA. .4Jan 6, 2022 · N466UA · Airbus A320232SDR CALA2022010700065Stop Fitting · crackedRH-FR66, DOOR STOP #4, UPPER INBOARD HOLE HAS CRACK INDICATION.( ) SUPPORT TASK AD 2018-03-12 R/H FR66 #4 DOOR STOP UPPER I/B HOLE. REPAIRED AND REAMED IAW SR FORM 44-0008 ATTACHED. EMP# V934344 WORK ACCOMPLISHED AT ST ENGI M 53-41-12-300-10. ORG. REAMED .394 Jan 6, 2022 · N466UA · Airbus A320232SDR CALA2022010700063Stop Fitting · crackedRH-FR66, DOOR STOP #5, LOWER INBOARD HOLE HAS CRACK INDICATION.( ) SUPPORT TASK AD 2018-03-12 R/H FR66 #5 DOOR STOP LOWER HOLE. REPAIRED AND REAMED IAW SRM 53 44-0008 ATTACHED EMP# V934344 WORK ACCOMPLISHED AT ST ENGINEERIN -41-12-300-10. ORG. REAMED .394 FIN Jan 6, 2022 · N466UA · Airbus A320232SDR CALA2022010700062Stop Fitting · crackedRH-FR68, DOOR STOP #6, LOWER INBOARD HOLE HAS CRACK INDICATION.( ) SUPPORT TASK AD 2018-03-12. R/H FR68 #6 DOOR STOP LOWER I/B HOLE REPAIRED AND REAMED IAW SRM FORM 44-0008 ATTACHED EMP# V934344 WORK ACCOMPLISHED AT ST ENGIN 53-41-12-300-10 ORG. REAMED .394 FIJan 6, 2022 · N466UA · Airbus A320232SDR CALA2022010700061Stop Fitting · crackedRH- FR66, DOOR STOP #6, LOWER INBOARD HOLE HAS CRACK INDICATION. () SUPPORT TASK AD 2018-03-12 R/H FR66 #6DOOR STOP LOWER I/B HOLE. REPAIRED AND REAMED IAW SRM FORM 44-0008 ATTACHED. EMP# V934344 WORK ACCOMPLISHED AT ST ENGI 53-14-12-300-10. ORG. REAMED .394 FJan 6, 2022 · N466UA · Airbus A320232SDR CALA2022010700055Door Frame · crackedL2 DOOR FRAME 68 DOOR STOP FITTING #1 LOWER INBOARD HOLE IS CRAC KED IN THE FRAME WEB AT 5:00 AND 10:00 POSITION. REO-L23516 REV IR IS INCLUDED AS APPENDIX A FOR REFERENCE.#3 HOL REPAIR ON THE FR68 DOOR STOP #1 AND STR 22 FLANGE PER PART 3 OF E START DIA .269"Jan 6, 2022 · N484UA · Airbus A320232SDR CALA2022010700052Window Frame · crackedAFTER REMOVAL OF WINDOW IN 1 LH POSITION, DURING POST REMOVAL INSPECTION, CAN SEE WHAT ARREARS TO BE CRACKED. REQUESTING HFEC INSPECTION TO VERIFY STATUS OF WINDOW FRAME. PHOTO ATTACHED LOCKED FOR FERRY FLIGHT TO ADD DEMENSIONS PERFORMED HFEC IAW NTM PART 6Jan 6, 2022 · N33209 · Boeing 737824SDR SWAA2022010658850Panel · elongatedCENTER WHEEL WELL PANEL 193D HAS MULTIPLE ELONGATED FASTENER HOLES. ; / [01] REMOVED AND REPLACED CENTER WHEEL WELL PANEL 193D<BR>I/A/W AMM 53-51-21Jan 6, 2022 · N475WN · Boeing 7377H4SDR REXA2022042000685Channel · corrodedR/H SIDE SEAT RAIL MOUNTING CHANNEL @FS780 TO FS820 HAS AREAS OF CORROSION J/C:900-53-900-514 - COMPLIED WITH EA# CRJ953-12557, REV IR DATED 1/18/2022 - REPAIRED CHANNEL PER EA CRJ953-12557.Jan 5, 2022 · N197PQ · Cndair CL6002D24SDR REXA2022042000655Support Angle · corrodedFWD FLOOR SUPPORT @ FS280 IS CORRODED BETWEEN RBL9 AND LBL9 JC:900-53-140-509 - REMOVED AND REPLACED FWD FLOOR SUPPORT @F.S.280 BETWEEN RBL9 AND LBL9 IAW CRJ900 SRM 51-42-06Jan 5, 2022 · N197PQ · Cndair CL6002D24SDR YENA2022031400190Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.250 INCH APPROX IN COCKPIT (1 EA); ACCOMPLISHED THE REPAIR OF THE (1) CRACK IN THE LH WINDSHIELD FRAMING NEAR THE CENTERJan 5, 2022 · N506JB · Airbus A320232SDR V0XD20220206001Joint · corrodedCORRODED ON THE CIRCUMFERENTIAL JOINT AT FS 280.00 FROM STR. 25L TO STR. 24 R. CORRECTIVE ACTION: REMOVED, BLENDED AND SMOOTH DEPTH BLEND RATIO OF 20:1 CORROSION ON THE CIRCUMFERENTIAL JOINT AT FS 280.00 FROM STR. 25L TO STR. 24 R IAW OLIVER WYMAN CAVOK ENGINEJan 5, 2022 · N525AE · Cndair CL6002C10SDR AALA202201266246Channel · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOOR SUPPORT CHANNEL BETWEEN STA 2129 AND 2150 AT RH SIDE. REPLACED FLOOR SUPPORT CHANNEL WITH NEW IAW B777-200 SRM 51-40-02-0G AND 51-40-05-0G.Jan 5, 2022 · N798AN · Boeing 777223SDR EE4Y2022010514844Skin · damagedDURING THE STRUCTURE INSPECTION, IT IS FOUND A PUNCTURE DAMAGE INTO AN EXISTING REPAIR DOUBLER. WAS REPAIRED FOLLOWING REPAIR INSTRUCTIONS PER E.O # COO-EO-2021-14379-R00 AND ETD2021-190-039139 DTD NOV 22,2021Jan 5, 2022 · N955UW · Emb ERJ190100IGWSDR SWAA2022021058043Web · corrodedSUPPLEMENTAL INFORMATION: **CORROSION** AFT CARGO COMPARTMENT BILGE AREA; FLOOR SUPPORT STRUCTURE AT RBL-14 BETWEEN STA-727A AND STA-727B; SPOTS OF CORROSION AND RIVETS (2 EACH) MISSING. DOT#208-171 ; / [01] REMOVED FASTENERS ON AFT CARGO COMP. BILGE AREA; FLOJan 4, 2022 · N791SW · Boeing 737SDR SWAA2022010657909None · corrodedCORROSION SPOTS ON CABIN FLOOR WEB AFT WET AREA B.S. 1006+9 L.BL. 40'. (51-002). REMOVED CORROSION AT AFT CABIN FLOOR WEB AT STA 1006+9 AND LBL 40' IAW SRM 53-70-51-1A-1-A00108. REMOVED SHEAR WEB CORROSION WAS EXFOLIATING WEB IS OUT OF LIMITS IAW 51-40-02-0GJan 4, 2022 · N452WN · Boeing 7377H4SDR V0XD20220202002Stringer · corrodedCORRODED ON STR 26R FROM FS 280.00 TO FS 319.00. CORRECTIVE ACTION: REMOVED AND REPLACED STR 26 R (P/N: SH670-31634-2) FROM FS 280.00 TO FS 319.00 IAW CRJ 700 SRM 51-42-06-001-001.Jan 3, 2022 · N525AE · Cndair CL6002C10SDR AALA202201251470Intercostal · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN INTERCOSTAL AT STA 312 AND RBL 31, MEASURING L=0.5 IN, W=0.25 IN, D=0.007 IN. REPLACED INTERCOSTAL WITH NEW IAW SRM 51-10-02.Jan 3, 2022 · N823NN · Boeing 737*SDR AALA202201047990Fitting · noneAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD RIGHT HAND CONTINUITY FITTING AT FR 2 AND Y0 REQUIRES REPLACEMENT PER EO 5319Y017-002 REQUIREMENTS. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.Jan 3, 2022 · N702UW · Airbus A319112SDR REXA2022021000220Floorboard · crackedFWD EQUIPMENT COMPARTMENT LH SIDE AT FS 193 THE FLOOR IS CRACKED. " REPAIRED FWD EQUIPMENT LH SIDE FS 193 FLOOR CRACK IAW CRJ 900 SRM 53-11-43-201-001-A01. REMOVED AND REINSTALLED BRAKE ACCUMULATOR LINES AND GAUGE BRKT AND PERFORMED OPS/LEAKS/BLEEDJan 2, 2022 · N905XJ · Cndair CL6002D24SDR SWAA2022010557434Dome · delaminatedSUPPLEMENTAL INFORMATION: 4 HOLE AND DELAMINATION ON RADAR DOME ; NOTED 4 HOLES AND DELAMINATION ON RADAR DOME / [01] TEMP REPAIRED PER SRM53-10-72; [02] CONFIRMED SRM REFERENCE 53-10-72-1A-1 IS THE CORRECT REFERENCE FOR THIS INTERIM REPAIR.Jan 1, 2022 · N412WN · Boeing 737SDR V0XD20220328001None · noneDENT IN FUSELAGE BELLY SKIN AT FS 270 BETWEEN STR 23L AND STR 24 L. CORRECTIVE ACTION: DRESS BACK TO ORIGINAL CONTOUR AT FS 270 BETWEEN STR 23L AND STR 24 L AND RESTOR TO FINISH IAW OLIVER WYMAN CAVOK EA 22-C9-53-0355 REV A DATE 03/27/2022.Jan 1, 2022 · N550NN · Cndair CL6002D24SDR VNAA202201019991Skin · damagedDAMAGE TO THE LH FUSELAGE SKIN AT PASSENGER DOOR CUT OUT FS349.Jan 1, 2022 · N501BG · Cndair CL6002C10SDR 2022F00034None · damagedDAMAGE TO THE LH FUSELAGE SKIN AT PASSENGER DOOR CUT OUT FS349.Jan 1, 2022 · N501BG · Cndair CL2151A10SDR NZAF20220112EA21Skin · damagedDURING ROUTINE MAINTENANCE MX DISCOVERED DAMAGE TO THE LH FUSELAGE SKIN AT PASSENGER DOOR CUT OUT FS349. THE DAMAGE WAS MAPPED AND SUBMITTED TO MHIRJ AND REPAIRED AS PER REPAIR ENGINEERING ORDER REO670-53-21-02212.Jan 1, 2022 · N501BG · Cndair CL6002C10SDR SIMA20211231001None · noneSSI 53-23-005 CORROSION ON RH INBD SEAT TRACK AT FRAME 82 AND 84.(LEVEL 2 CORROSION)-C/A-PERFORMED SPLICE DEVICE REPAIRS ON RH INBD SEAT TRACK AT FRAME 82 AND 84 IAW EMB 175 SRM 53-00-10 REPAIR 02P FIGURE 208.Dec 31, 2021 · N224NN · Emb ERJ170200LRSDR AALA202201252972Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF FWD SHIELD IN AFT CARGO COMPARTMENT AT STA 800 AND RBL 25, MEASURING L=2.0 IN, W=1.5 IN, D=0.022 IN. REPLACED SHIELD WITH NEW IAW SRM 51-20-01.Dec 30, 2021 · N823NN · Boeing 737*SDR AALA202201258778Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF TRANSITION PANEL BETWEEN STA 727I AND STA 800 AT LBL 26, MEASURING L=2.5 IN, W=2.5 IN, D=0.019 IN. ACCOMPLISHED PERMANENT REINFORCING SPLICE REPAIR IAW SRM 51-00-05.Dec 30, 2021 · N823NN · Boeing 737*SDR SIMA20211230004None · noneSSI 53-23-005 CORROSION IN AFT GALLEY AREA ON CENTER SHEAR PANEL.(LEVEL2 CORROSION)-C/A-REMOVED AND REPLACED AFT GALLEY CENTER SHEAR PANEL IAW EMB 175 SRM 51-40-08.Dec 30, 2021 · N224NN · Emb ERJ170200LRSDR SIMA20211230003None · noneSSI 53-10-027, RH FLOOR SILL UNDER FWD GALLEY AREA BETWEEN FRAME 12 AND FRAME 14 HAS CORROSION.(LEVEL2 CORROSION)-C/A-REMOVED AND REPLACED THE RH FLOOR SILL UNDER FWD GALLEY AREA BETWEEN FRAME 12 AND FRAME 14 IAW EMB 175 SRM 51-40-08.Dec 30, 2021 · N224NN · Emb ERJ170200LRSDR SIMA20211230005None · noneSSI 53-23-005 CORROSION IN AFT GALLEY AREA ON RH SHEAR PANEL.(LEVEL2 CORROSION)-C/A-REMOVED AND REPLACED AFT GALLEY RH SHEAR PANEL IAW EMB 175 SRM 51-40-08.Dec 30, 2021 · N224NN · Emb ERJ170200LRSDR CALA2021123002486Frame · crackedL/H FR35 STR30 HOLE #1 PRODUCED CRACK INDICATIONS AT THE 2:00 PO SITION. HO,LE #3, #4. LH FORWARD PIT AFT OF FRAME 35 HOLES COMMO N TO ANGLE FITTING REMOVAL UPPER ROW 7TH AFT OF FRAME 35 INTERIO R SURFACE IS GOUGED JUST ABOVE THE HOLE AT 12:00. PER HAECO LCQ NDec 30, 2021 · N803UA · Airbus A300*SDR SWAA2022021157099Web · crackedCRACK WEB LOCATED BETWEEN BS 294.5 TO BS 303.9 AND STR 16L AT PASSENGER CABIN ; 2021-576202 / [01] REPLACED WEB LOCATED BETWEEN BS 294.5 TO BS 303.9 AND STR 16L AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8180 SHEET 22 REV-. SEE INDIVIDUAL Dec 29, 2021 · N7866A · Boeing 737*SDR SIMA20211229006None · noneFRAME 67 IS CRACKED AROUND RIVET HOLES AT STR 18L-C/A-COMPLETE: C/W FRAME 67 SPLICE REPAIR AT STR,18L IAW SRM 53-00-04 ITEM #4 FIG.201.Dec 29, 2021 · N685AE · Emb EMB145LRSDR SIMA20211229004None · noneFRAME 66 IS CRACKED AROUND RIVET HOLES AT STR 18 L-C/A-COMPLETE: REPAIRED IAW SRM 53-00-04 ITEM #4 FIG 201.Dec 29, 2021 · N685AE · Emb EMB145LRSDR AALA202201255838Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF TRANSITION PANEL BETWEEN STA 500G AND STA 500I AT RBL 26, MEASURING L=12.0 IN, W=3.0 IN, D=0.011 IN. REPLACED TRANSITION PANEL WITH NEW IAW AARD 51-00-05-1.Dec 29, 2021 · N823NN · Boeing 737*SDR AALA202201259163Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF TRANSITION PANEL BETWEEN STA 500F AND STA 500G AT RBL 26, MEASURING L=12.0 IN, W=3.0 IN, D=0.011 IN. REPLACED TRANSITION PANEL WITH NEW IAW AARD 51-00-05-1.Dec 29, 2021 · N823NN · Boeing 737*
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