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.
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
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 SWAA2022101146084None · crackedCRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500D TO BS520 AND STR28R FWD CARGO COMPARTMENT 2022-510733 / [01] REPLACED NEW WEB-INTERCOSTAL LOCATED BTW BS500D TO BS520 AND STR28R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 143ASDR SWAA2022100683004None · warpedOIL CANNING FOUND ON BS AFT PRESSURE BULKHEAD 5 IN. BELOW STRINGER 11R - 60 IN. FROM APEX. / [01] TRANSFERRED TO N/R FAULT TTG8Q00EXJBYSDR FDEA202209192452Snubber · gougedTAILCONE, EXTENDED SNUBBER ASSY STRUCTURE AKC7591-20 & 21 HAS GOUGE MARKS. AKC7591-21 IS INCORRECT PART PART NUMBER, CORRECT PART NUMBER IS AKC7591-24. FABERCATED AND INSTALLED NEW AKC7591-20 IAW DWG AKC7591SDR FDEA202209192384Beam · wornTAILCONE, AKC7539-13 BEAM HAS ELONGATED FASTENER ATTACHING L/H HOLES. FABRICATED NEW BEAM ACK7539-13 PER DWG AKC7539.SDR 2022FA0000541Failsafe · crackedDURING MAINTENENCE INSPECTION FOUND CRACKED HOLE ON FAIL SAFE CHORD, STA 1540, BETWEEN STR 35L AND STR 36L.SDR AALA202210057209Beam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION AROUND SEVERAL FASTENER HOLES IN THE LEFT WING TRAILING EDGE LOWER ACCESS PANELS SUPPORT STRUCTURE BEAM ASSEMBLY LOCATED BETWEEN LEFT WING STA 335 AND STA 440. REPLACED BEAM ASSEMBLY PER SRM 57-51-02-1A PROCEDURE 1 AND SSDR IPXA2022091786335Crossbeam · crackedINSPECTION TYPE:1C/2RH FR 17 BOTTOM HOLE AT MAIN DECK FLOOR BEAM ATTACHMENT JUNCTIONS HAS 2 REJECTABLE CRACK INDICATIONS AT 12 AND 6'O CLOCK POSITION IN FWD 2 LAYERS.ACCOMPLISHED PERMANENT REPAIR PER FINAL UPS EO A300-5310-84764-4 AND EA300-5710-A3023SDR SWAA2022101378716Stub Frame · crackedCRACK STUD FRAME LOCATED BS294 LEVEL STR8R AND WL266 AT FWD GALLEY AREA 2022-518243 / REPLACED STUB FRAME LOCATED BS294 LEVEL STR8R AND WL266 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8370 SHEET : 11 REV D: , DWG 141A8370 SHEET : 9 REV D: AND B7SDR AALA202210133742Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON AFT BULKHEAD LOWER L SUPPORT RIGHT SIDE. LOCATED BETWEEN STA 360 AND 540 AND RIGHT BUTT LINE 43SDR CALA2022091902403None · corrodedAFT CARGO FR 63-64 STR 41L HAS CORROSION PER HAECO LCQ NR 929068 2/30682 GENERATED BY N078570 (SUPPORT TASK) REMOVED AND REPLACED STRINGER 41L FR 63-64 IAW A320 SRM 51-72-11 -911-001. PERFORMED BY V052030 INSP BY V061771SDR CALA2022091902401None · corrodedAFT CARGO FR 63-64 STR 42L HAS CORROSION PER HAECO LCQ NR 929068 4/30684 GENERATED BY N078570 (SUPPORT TASK) REMOVED & REPLACED AFT CARGO STRINGER 42L IAW A320 SRM 51-72-11- 911-002. PERFORMED BY V052030 INSP BY V061771SDR FDEA202209152325None · wornFR54/FR54.2 LH NO.5 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) BUT LESS THAN 0.0846 INCHES(2.15MM) SLOT GAP ACTUAL VALUE 1.21MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A FIG.201 PAGE 201-210 PERFORM RAIL HOLE REPAIR ACCOMPLISHED.SDR SWAA2022092756907Floor Panel · out of position2EA FLOOR PANEL INSERTS REQUIRE REPOSITIONING TO ACCOMMODATE FLOOR BEAM REPAIR FLOOR PANEL 221EF / [01] GENERAL NOTE: REFERENCE EA 22-153-02676-WIP5 STEP2 ON FAULT TTG8Q00E9MAJ FOR ALLOWANCE TO REPOSITION (MOVE) INSERT LOCATIONS AS REQUIRED.;[02] IDENTIFIED MASDR ASAA2022091539965Trans Panel · corrodedAFT CARGO LH TRANSITION PANEL CORRODED ON UPPER AND LOWER SURFACES. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND TRANSITION PNL TO BE OUT OF LIMITS IAW B737-900 SRM 53-00-1A-2 REPAIRED TRANSITION PANEL IAW B737-900 SRM 53-00-53-2R-5W=1.00 O=.040 SDR CALA2022091602378Beam · corrodedAFT PASSENGER COMPARTMENT WWET AREA:POSSIBLE CORROSION POINTS ON FLOOR BEAM STA. 986.5IN LBL 27,LBL35 AND LBL43 (REF AAR NR 99944 132) PERFORMED REPAIR AT STA 986.5 IAW B737-800 SRM 53-70-51-2R-4, SR M 51-10-02, SRM 51-40-02, SOPM 20-10-03, AMM 51-21-41-370-80SDR SWAA2022100571977Floor Support · crackedFLOOR SUPPORT CRACKED BS 344+9 LBL 12 WL 208 / [01] REMOVED FLOOR SUPPORT AT BS 344-360 BL0 WL 208 FOR ACCESS AND REMOVED CRACKED FLOOR SUPPORT AT BS 344+9 LBL12 WL 208 PER SRM 51-40-02.;[02] CERTIFIED ACTION 1.;[03] LOCATED AND DRILLED NEW FLOOR SUPPORT AT BSSDR SWAA2022100571978Floor Support · crackedFLOOR SUPPORT CRACKED BS 380+7 LBL 14 WL 208 / [01] REMOVED CRACKED FLOOR SUPPORT AT BS 380+7 LBL 14 WL 208 PER SRM 51-40-02.;[02] LOCATED AND DRILLED NEW FLOOR SUPPORT AT BS 380+7 LBL 14 WL 208 PER SRM 51-40-05; DWG#143A5400. REQUEST OK TO INSTALL.;[03] VERIFSDR SWAA2022100571981Floor Support · crackedFLOOR SUPPORT CRACKED BS 277+7 BL0 WL 208 / [01] REMOVED CRACKED FLOOR SUPPORT AT BS 277+7 BL0 WL208 PER SRM 51-40-02.;[02] LOCATED AND DRILLED NEW FLOOR SUPPORT AT BS 277+7 BL0 WL 208 PER SRM 51-40-05; DWG#141A5400. REQUEST OK TO INSTALL.;[03] VERIFIED CORRECSDR SWAA2022100571979Floor Support · crackedFLOOR SUPPORT CRACKED BS 312+5 RBL 31 WL 208 / [01] REMOVED CRACKED FLOOR SUPPORT AT BS 312+5 RBL 31 WL 208 PER SRM 51-40-02.;[02] REMOVED CRACKED FLOOR SUPPORT AT BS 312+5 RBL 31 WL 208 PER SRM 51-40-02. UPDATED MEASUREMENT TABLE.;[03] LOCATED AND DRILLED NEWSDR SWAA2022100571982None · crackedMOPSILL INNER CHORD CRACKED BS 303.9 LBL 55 WL 209 / [01] UPDATED MEASUREMENTS. REMOVED FWD ENTRY DOOR MOPSILL IAW SRM 51-40-02.;[02] LOCATED AND DRILLED NEW FED MOP SILL IAW SRM 51-40-05-0G-0 AND BOEING DWG 141A8110 APPLIED CHEMICAL CONVERSION COAT AND PRIMEDSDR SWAA2022100571983Floor Support · crackedFLOOR SUPPORT CRACKED BS 312+9 LBL 43 WL 208 / [01] REMOVED CRACKED FLOOR SUPPORT BS 312+9 LBL 43 WL 208 PER SRM 51-40-02.;[02] LOCATED AND DRILLED NEW FLOOR SUPPORT PER SRM 51-40-05; DRW # 141A5400. REQUEST OK TO INSTALL.;[03] VERIFIED CORRECTIVE ACTION #2<BRSDR AALA202209216192Doubler · deformedAIRCRAFT IN BASE MAINTENANCE: SEVERAL FASTENER HOLES AT 1016 BULKHEAD AFT SIDE ON UPPER STRAP (REMOVED FASTENERS) BETWEEN S-3R AND S-5R ARE DEFORMED. REMOVED EXISTING DOUBLER/TRIPLER REPAIR AFT SIDE OF BULKHEAD. INSTALLED DOUBLER REPAIR PER EA 338028.SDR CALA2022091602374Seat Track · corrodedCABIN SEAT TRACK -Y765 FR20-22 IS CORRODED ON TOP SURFACE. CABIN SEAT TRACK REMOVED AND INSTALLED NEW SEAT TRACK P/N 531127 822020A I.A.W SRM 51-72-11 AND 51-42-11. (T#87305) WORK ACCOMPLI SHED AT ST ENGINEERING OF MOBILE AT BFM ON N/R#: 36182SDR IPXA2022091486254Shear Plate · corrodedINSPECTION TYPE:SEG3, MAIN CABIN STA 1681 RBL 35 CORROSION LOCATED AT AFT SHEAR WEBWORKED PER UPS EO B757-5310-84662-A, UPS RCD 283456 AND VT MAE 757-5360-27-A3017 REV-SDR IPXA2022091486248Floorbeam · corrodedINSPECTION TYPE:SEG3, EXFOLIATION CORROSION ON 1680 FLOOR BEAM FROM RBL 38.0 TO RBL 41.37 LOCATED ON UPPER BEAM FLANGE LOWER SURFACEWORKED PER UPS EO B757-5310-84662-A, UPS RCD 283460 AND VT MAE 757-5360-27-A3017 REV-SDR F3LA2022111000145Stringer · corrodedDISCREPANCY: REFERENCE NRB000859 AT CARGO COMPARTMENT. RH SIDE BETWEEN FR64 TO FR65 S-37 TO S-39 RIVETS WERE FOUND WITH CORROSION
CORRECTIVE ACTION REMOVED AND REPLACED CORRODED STRINGER FR64-FR65 S-39R P/N D5348003022000 S/N 81130763/003/2022#A IAW EA A2-53RSDR SWAA2022100552828Flange · crackedAPU INLET DUCT WITH MULTIPLE CRACKS AT FWD FLANGE / [01] REMOVED THE DAMAGED PLIES AND PREPARED AREA TO APPLY THE FABRIC REPAIR PLIES; NO WATER NOTE; AT APU INLET DUCT. REF B737-700 SRM 51-70-04-2R-10 REPAIR 10 PARAGRAPH 4.;[02] VERIFIED 1. OK TO APPLY REPAIR;SDR SWAA2022100552846Floor Support · crackedFWD CABIN FLOOR SUPPORT BETWEEN STA 380 AND STA 400 BL0 INTERCOASTAL FRAME CRACK WL 208.1. / [01] REMOVED INTERCOSTAL AT FWD CABIN FLOOR SUPPORT BET. STA 380 TO STA 400 BL 0.PER B 737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILL NEW INTERCOASTAL.PER B 737-700SDR CALA2022091402356None · corrodedAFT CARGO FR 63-64 STR 42R HAS CORROSION. GENERATED BY N078570 A T HAECO LCQ PER NR. 9290683 (30683).(SUPPORT TASK) REMOVED AND REPLACED STR 42R AT FR 60-FR64 AFT CARGO IAW ;A320 S RM 51-72-11-911-002. INSTALLED 2EA CLENTS AT FR 60 IAW A320 SRM 51-22-11-911-00SDR FDEA202209122313Deck Plate · corrodedMAIN CABIN AFT PRESSURE DECK WEB IS CORRODED AT APPROX STA 1695 AT APPROX LBL 8 REPAIRED AFT DECK PRESSURE PLATE CORROSION, UPPER SURFACE @ STA 1695, LBL 8 IAW FEDEX EA F-5310-T0370248, RELEASED SEP 08, 2022, TITLED" FUSELAGE - MAINFRAME - AFT DECK PLATE, SDR FDEA202209122312Deck Plate · corrodedMAIN CABIN AFT PRESSURE DECK WEB IS CORRODED AT APPROX STA 1689 AT APPROX LBL 8 REPAIRED AFT DECK PRESSURE PLATE CORROSION UPPER SURFACE @ STA 1689, LBL 8 IAW FEDEX EA F-5310-T0370248-P1, RELEASED SEP 08, 2022, TITLED " FUSELAGE - MAINFRAME - AFT DECK PLATSDR FDEA202209122311Deck Plate · corrodedMAIN CABIN AFT PRESSURE DECK WEB IS CORRODED AT APPROX STA 1684 AT APPROX LBL 8 REPAIRED AFT DECK PRESSURE PLATE CORROSION UPPER SURFACE @ STA 1684, LBL 8 IAW FEDEX EA F-5310-T0370-P1, RELEASED SEP 08, 2022, TITLED "FUSELAGE - MAINFRAME - AFT DECK PLATE STSDR YENA2022091300896None · noneDURING HEAVY MAINTENANCE: FORWARD FUSELAGE/FLOOR STRUCTURE / RIGHT TRACK BETWEEN FRAMES 12 AND 14 / CORROSION / PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR FDEA202209102379Adapter · gougedAFT MAIN DECK CARGO COMPT FOUND CROSSBEAM FITTED WITH CLS ADAPTER GOT 2EA GOUGED MARKS AT FR63/BETWEEN -Y1456 AND -Y1959 DAMAGED CROSSBEAM REPALCED NEW PART, INSTALLED WITH FASTENERS I.A.W A300-600 SRM 51-72-10-001, PAGE.2 AND SRM 51-40-21-001, PARA.7,PAGESDR CALA2022091202335Skin · noneLIGHTNING STRIKE EXTERNAL SKIN BTW FRAME 43 TO FRAME 44 AND BTW STRIN GER 1R TO STRINGER 1L ON UPPER FUSELAGE. SEE AEROMAN NON ROUTINE 2022-343081. (SHEET 03). PERFORMED ROTOTEST INSPECTION ON OPEN FASTENERS DIAMETER HOLES ARE : 0.187 INCH . TOOL USED ELECTROSDR SWIA202266888Window Post · crackedLOWER CENTER RIGHT SIDE WINDSHEILD POST FITTING HAS A POSSIBLE CRACK AT FWD RADIUS. (C-CHECK RO 11/12/2022) REMOVED, REPLACED AND INSTALLED NEW WINDSHIELD CENTER POST LOWER RIGHT SIDE FITTING P/N 601R33237-2. PER BOMBARDIER DWG # 601R33237 REV-C AND RSDR SWAA2022101451698Doubler · crackedEXTERNAL POWER RECEPTACLE FUSELAGE SKIN INNER DOUBLER HAS CRACK AT FWD LOWER HINGE AREA. / LOCATED AND DRILLED NEW DOUBLER AS PER REF SRM 51-40-05-0G-0STARTING NEW INNER DOUBLER INSTALLATION AS PER REF SRM 51-40-02-0G-0 AND DWG 141A3702;[17] INSTALLED NEW INNESDR FDEA202209092553Seat Track · corrodedMDCC SEAT TRACK SURFACE CORRODED AT FR18 8"~FR18 14", -Y450. REMOVED EXISTING REPAIR (REF TO PREVIOUS REPAIR ASSESSMENT DATA N00562 FOR AGING AIRCRAFT ASSESSMENT INFORMATION), INSTALLED NEW FABRICATED SEAT TRACK WITH SPLICES, THIS IS CAT.B REPAIR I.A.W A30SDR FDEA202209092528Seat Track · noneMDCC SEAT TRACK SURFACE CORRODED AT FR18 10"~FR18 15",-Y953 REPLACED THE SEAT TRACK WITH FABRICATED PART I.A.W A300-600 SRM 53-12-16-001 , PAGE.9/10 , FIG.1(SHEET-4) & GMM 07-0-1001 & 51-40-21-001 , PARA.6&7 , PAGE.7B-50.SDR AALA202209120512Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: EVIDENCE OF CORROSION ON STRINGER AT STA 310 AND STR 23L. REPAIRED PER EA 337948.SDR AALA202210076528Intercostal · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN AFT ENTRY FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN BS 947 AND BS 962, AT LBL 25. REPLACED INTERCOSTAL PER SRM 53-70-51.**SUPPLEMENTAL REPORT FOR AALA202209296528: ENGINEERING REVIEWED THIS EVENT AND DSDR SWAA2022092951288Post · corrodedFWD LAV DOOR POST IS CORRODED AT THE BOTTOM / [01] REMOVED DAMAGED 6.5? SECTION OF LAV POST IAW SRM 51-10-02.;[02] INSTALLED REPAIR PART PER EA# TTG8Q00ETZ11.;[03] INSPECTION COMPLETE ON CORRECTIVE ACTION #2 FOR REPAIR PER EA 22-125-02765 ON TTG8Q00ETZ11.SDR SWAA2022092651400Web · crackedCRACK WEB LOCATED BTW STA 500D TO STA 520 AT STR 28R AT FWD CARGO COMPARTMENT 2022-493562 / [01] REPLACED WEB AND FASTENERS LOCATED BTW STA 500D TO STA 520 AT STR 28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9. AND DWG#143A7902 REVSDR HYIA20220909002Door Frame · corrodedDURING MAINTENANCE, CORROSION DAMAGE WAS NOTED UNDERNEATH THE STRIKER PLATE FOR THE UPPER CLAMSHELL DOOR PIN ENGAGEMENT HOLE LOCATED ON THE MAIN CABIN DOOR POST. (F.S. 213.6) THE DEPTH OF THIS CORROSION IN GREATER THAN 25% OF THE THICKNESS OF THE DOOR POST ANDSDR JR2R20220908823None · corrodedLH FLOOR SILL CORRODED AT FR84SDR JR2R20220908795Doubler · corrodedFLOOR WEBB PLATE BETWEEN FR12 THRU FR14 AND RBL36 THRU RBL48 CORRODEDSDR JR2R20220908813None · corrodedRH FLOOR SILL BETWEEN FR88 AND FR90 CORRODEDSDR JR2R20220908812Shear Panel · corrodedRH FLOOR SHEAR PANEL BETWEEN FR87 AND FR88 CORRODEDSDR JR2R20220908807Shear Panel · corrodedCENTER FLOOR SHEAR PANEL BETWEEN FR87 AND FR88 IS CORRODEDSDR JR2R20220908820Beam · corrodedFLOOR BEAM BETWEEN FR86 AND FR88 AT RBL 9 IS CORRODED
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