JASC 5310
Service difficulty reports · 38,548
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 SWAA2022032342909Web · corroded***CORROSION*** FWD CARGO DOOR LOWER SILL WEB STA 460-490 RBL29 WL156 / REMOVED DAMAGED WEB FROM FWD CARGO DOOR LOWER SILL DAMAGE TO FOUND OUT LIMITS PER S.R.M 53-30-15-1A-1 PARA H(1)(B) FIG 103 DETAIL 'D'. LOCATED AND DRILLED NEW WEB P/N 143A8122-10 PO # 7466SDR SWAA2022032342907Angle · corroded***CORROSION*** FWD L/H PASSENGER ENTRY DOOR THRESHOLD SUPPORT ANGEL HAS CORROSION STA. 294.5-STA. 328; WL 209; LBL57 / REMOVED AND REPLACED FWD; ENTRY DOOR THRESHOLD SUPPORT ANGLE AT STA. 294-5 - STA 328 WL 209 LBL 57 WITH NEW PART# 141A8112-20 P.O. 744368. ISDR SWAA2022032342902None · corroded***CORROSION*** R2 SERVICE DOOR INNER CORD HAS CORROSION STA. 962-987 RBL 52 WL 209 / R2 SERVICE DOOR INNER CORD CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1 REMOVED DAMAGED INNER CHORD FROM STA 897-1015 AT RBL 52 WL 209. LOCATED AND DRILLED NEW ISDR SWAA2022032342900Angle · corroded***CORROSION*** FWD R/H SERVICE DOOR THRESHOLD SUPPORT ANGEL HAS CORROSION STA. 294.5-STA. 328; WL 209; RBL57 / REMOVED AND REPLACED FWD R/H SERVICE DOOR THRESHOLD SUPPORT ANGLE; STA 294.5 TO STA 328 WL 209; RBL 57; PER DWG# 141A8310 SHEET 33 AND SRM 51-40-05-SDR SWAA2022032233920Angle · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE Z ANGLE CORRODED AT STA 727G TO 787+12' LBL 22 WL 156 / REMOVED CORROSION ON AFT CARGO Z ANGLE FROM STAITON 727G+12 TO 787+12 LBL 22 SL 156; STA 727G TO 747+1- FOUND WITHIN ALLOWABLE LIMITS WITH .038' MAT REMAINING; .040' SDR SWAA2022032233910Web · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE DOOR CUTOUT WEB AT STA 787+7' TO 847 RBL 26 WL156 CORRODED / REMOVED CORROSION ON AFT CARGO COMPARTMENT FLOOR STRUCTURE DOOR CUT OUT WEB STA 787+7' TO 847 RBL 26 WL156 IAW SRM 51-10-02-0G-0. VERIFIED LIMITS IAW SRM 53-60-1SDR SCNA20191025207Structure · corrodedSTA 328, RBL 48, HAS CORROSION AT SCREW HOLE. DOT008. REMOVED CORROSION AND FABRICATED REPAIR STRAP ON STA. 328 RBL 48. ALL WORK DONE IAW B737-800 SRM 51-10-02, 53-10-51, 51-40-05 AND AMM 51-21-41, 51-21-72SDR DALA201910216025Door Frame · cracked(LOG 1323054) DURING INSPECTION FOUND CRACKED FWD/LOWER AREA OF R1 DOOR JAMB. CRACK ON FRAME ON R1 DOOR JAMB WAS REPAIRED PER B737-800 STRUCTURAL REPAIR MANUAL TEMPORARY REVISION 53-141, 53-10-15 REPAIR 7.SDR SWAA2022032275598Strap · corrodedAFT CARGO STA 794+9 TO 807+14; RBL 23; WL 154; LOWER SILL STRAP HAS CORROSION ON UPPER SURFACE. / REMOVED CORROSION AT AFT CARGO LOWE SILL STRAP IAW 737-700 SRM 51-10-02-06-0 VEIFIED LIMTS AS ORG 'T' .100';LOSS OF .015'; REMAINING .085' IS OUT OF LIMITS IAW 73SDR SWAA2022032275595Angle · corrodedAFT CARGO STA 947; RBL 18 TO LBL 11; WL 166; BULKHEAD TO FLOOR SUPPORT ANGLE HAS CORROSION ON UPPER SURFACE / AFT CARGO STA 947 RBL 18 TO LBL 11 WL 166 BULKHEAD TO FLOOR SUPPORT ANGLE HAS CORROSIEN FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED DATA SRM 53-00-5SDR SWAA2022032275594Angle · corrodedAFT CARGO. STA 947; RBL 23; WL166; CURVED BULKHEAD TO SIDEWALL SUPPORT ANGLE HAS CORROSION ON UPPER SURFACE. / REMOVED CORROSION FORM CURVED SIDEWALL SUPPORT IAW SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED DATA. REMOVED DAMAGED BULKHEAD SISDR SWAA2022032275590Intercostal · corrodedAFT CARGO STA 747+10 TO 767; RBL 23; WL 154; BAFFLE ANGLE HAS CORROSION ON LOWER SURFACE AROUND NUTPLATE HOLES / REMOVED AND EVALUATED CORROSION ON -8 INTERCOSTAL. ORIGINAL THICKNESS .030' LOSS OF .013' WITH .027' REMAINING BLEND FOUND TO BE OUT OF LIMITS PER SDR SWAA2022032275585Intercostal · corrodedFWD CARGO COMPARTMENT R/H Z ANGLE BETWEEN STA 500A AND 500D ABOVE STR 25 R AREA; WL 156.4 TOP SKIN SURFACE HAS 5 EA AREAS OF CORROSION AS MARKED. REMOVED CORROSION ON RIGHT HAND Z-ANGLE STA 500A TO 500D UPPER SURFACE 5 EACH AREAS; USEING 10X MAG NO FURTHER CORSDR AALA201910259031Door Frame · crackedAIRCRAFT IN BASE VISIT: OVERWING EMERGENCY EXIT DOOR FRAME SEGMENT OUTER FLANGE INDICATES A CRACK AT FR41. INSTALLED A DOUBLER REPAIR IAW EA# A9-52R-34702.SDR AALA201910259032Door Frame · crackedAIRCRAFT IN BASE VISIT: LH OVERWING EMERGENCY EXIT AFT INBOARD FRAME HAS INDICATION OF A CRACK. INSTALLED DOUBLER REPAIR ON OVERWING EMERGENCY EXIT DOOR FLANGE SEGMENT OUTER FLANGE IAW EA# A9-52R-34702.SDR C77A2019101700001Crossbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING THE B6 BASIC CHECK AT EAMS ON THE UPPER FLANGE OF THE P/N 170-21769-405 FR17 CROSSBEAM IN THE CABIN FLOOR STRUCTURE OF THE FORWARD FUSELAGESDR CALA2019101801774Pressure Panel · crackedLH PRESSURE PANEL BETWEEN FRAME 35-36 HOLE 2,4,13,14,15,16,21,23 ,24,25,26,27 AND 28 ARE CRACKED IN THE PRESSURE PANEL CONTACT EN GINEERING FOR INSTRUCTIONS AND REPAIR BEFORE NEXT FLIGHT AD 2018 -06-04 PER LCQ NON ROUTINE 9292324. LH PRESSURE PANEL AT FR35-36SDR DALA2019101705943Door Frame · crackedHIDDEN DAMAGED: IN REF NRC= 00103: CRACK ON LOWER DOOR JAMB BTW STA 994 STRINGERS 26 AND 27LH OF AFT CARGO COMPARTMENT. SUMMARY OF NRC 00639: LOWER DOOR JAMB BTW STA 994 STRINGERS 26 AND 27LH OF AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 582240- 14 REV.ORIGINSDR SWAA2019102838273Pressure Deck · crackedHORIZONTAL PRESSURE DECK TO BE CRACKED BETWEEN BS. 663 TO BS. 675, LBL 31. / REPAIRED DECK IAW SRM.SDR A6WA2019102846960Beam · chafedFOUND CARGO DOOR HORIZONTAL BEAM TO BE CHAFED ON FED SIDE BELOW THE GROOVE PULLEY.SDR CALA2019101801763Window Frame · crackedWHILE PERFORMING HFEC INSPECTION OF R-1 WINDOW FRAME ,A CRACK WAS FOUND , REF FIG 12 PAGE 11 CRACK CONDITION #1 SHORT CRACK CRACK CONDITION # 1 SHORT CRACK OF R-1 WINDOW FRAME HAVE BEEN REPAIRED PER EC/RA 5311-02256. SEE FLEET CYCLE N/R # 9697716 ALL PAPERWORKSDR AALA201910169014Window Frame · crackedAIRCRAFT WAS GROUNDED: FLIGHT DECK RIGHT HAND SLIDING WINDOW LATERAL WINDSHIELD FRAME VERTICAL STIFFENER CRACKED AT FR 4. REPAIRED WINDOW FRAME PER EA 299400.SDR DALA2019101505909Door Frame · crackedR1 DOOR FRAME 16, STOP FITTING NR 7 STRINGER 10R. HOLE NR 1 NOTED A CRACK INDICATION. ACCOMPLISHED PR/I 581975-14AD REV 0,1,2,3,4 AND COMPLIED WITH ER/A 581975-14AD REV ORIGINAL.SDR DALA2019101505911Door Frame · crackedR1 DOOR FRAME 16, STOP FITTING NR 1, STRINGER 22R. NOTED A CRACK INDICATION FROM 3 HOLE. PRI 581975-14AD REVS 0,1,2,3, AND 4 ACCOMPLISHED AND COMPLIED WITH ER/A 581975-14AD REV. ORIGINAL.SDR DALA2019101505910Door Frame · crackedR1 DOOR FRAME 16, STOP FITTING NR 7 STGR 10R. HOLE 3 NOTED A CRACK INDICATION . ACCOMPLISHED PR/I 581975-14AD REV 0,1,2,3,4 AND COMPLIED WITH ER/A 581975-14AD REV ORIGINAL.SDR SWAA2022040685020Floor Support · crackedFLOOR SUPPORT CRACKED AT BS 277-294 BL 0 WL 208 / REMOVED CRACK DAMAGED FLOOR SUPPORT AT BS277-294 BL0 WL208 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-05-0G-0 LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-05-0G-0 OK TO INSSDR SWAA2022040863863Fitting · crackedDURING INSPECTION OF BS 663.7 FRAME FITTING CRACKS WERE FOUND ON LHS AND RHS FRAME FITTINGS AS WELL AS THE LHS FAIL SAFE STRAP STA 663.75. REF: EA 1-753-35798 REV 1 / THE LH PICKLE FORK FRAME P/N 144A2410-7 & FAIL SAFE STRAP P/N 144A2412-1. THE RH PICKLE FORK SDR R61A201911071207Crossbeam · corrodedMAJOR: CORROSION_CENTER FUSELAGE III DRY AREA 53-23 R.HAND SIDE OF FR.84 CROSSBEAM. BLENDED CORROSION CENTER FUSELAGE FR.84 CROSSBEAM, NOMINAL THICKNESS .080" MATERIAL LOSS.040", FOUND TO BE OUT OF LIMITS REF SRM 51-10-03, 51-75-16.REMOVED AND REPLACED. R.HANDSDR DALA2019101655937Stop Fitting · crackedA/C 3118 CLOSED LOG 1315432. 1L DOOR FR20, STOP FITTING #3 STGR 18. HOLE #2 NOTED CRACK INDICATION. VERIFIED BY QC 2018. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 091-0001:5311-2031/034 00280 REPAIRED PER PRI 581989-14AD REV 0, REV 1, REV 2 AND ERA 581989-14ADSDR DALA2019101505908Door Frame · crackedL1 DOOR FRAME 16, STOP FITTING NR 7 STRINGER 10L. HOLE NR 1 NOTED A CRACK INDICATION. ACCOMPLISHED PR/I 581976-14AD REV 0,1,2 AND 3 AND COMPLIED WITH ER/A 581976-14AD REV ORIGINAL.SDR DALA2019101505907Door Frame · crackedL1 DOOR FRAME 16, STOP FITTING NR 7, STRINGER 10L WAS FOUND TO HAVE A CRACK INDICATION ON THE NR 3 HOLE. ACCOMPLISHED PR/I 581976-14AD REV 0,1,2 AND 3 AND COMPLIED WITH ER/A 581976-14AD REV ORIGINAL.SDR DALA2019101505906Door Frame · crackedFRAME 16L, NR 1 FITTING, NR 3 HOLE HAD A CRACK INDICATION. ACCOMPLISHED PR/I 581976-14AD REV 0,1,2 AND 3 AND COMPLIED WITH ER/A 581976-14AD REV ORIGINAL.SDR SWAA2022040559442Angle · crackedFOUND CRACK ON UPPER SURFACE OF ANGLE BETWEEN STA 380 AND 400 AND ABOUT RBL 8.5 / REMOVED AND INSTALLED NEW ANGLE BETWEEN STA 380 TO STA 400 RBL 8.5' IAW B737 SRM 51-40-02-0G-0SDR DALA2020020400869Structure · damaged(AIRCRAFT 5643, L/P 5894078) HARD LANDING ON NOSE WHEEL AFTER MAINS TOUCHED DOWN. CORRECTIVE ACTION: WHILE PERFORMING HARD LANDING PHASE I INSPECTION FOUND EXTENSIVE DAMAGE. REQUIRES PHASE II INSP. PER B757 AMM 05-51. REF. L/P 1251252 FOR PHASE II INSPECTION CSDR R61A201910281162Doubler · corrodedCORROSION-FWD WET AREA LH AFT DOUBLER FR19-20 AS MARKED. REMOVED AND REPLACED LH AFT DOUBLER AT FR 19-20 REF SRM 51-40-08, 51-23-04. APPLIED TOP COAT AT FWD WET AREA LH AFT DOUBLER FR19-20 REF SRM51-23-06 PO#251151 SEE EAMS W/O H6997 SN 185 FOR WORK DETAILS.SDR R61A201910281161Support · corrodedCORROSION-FWD WET AREA LH MONUMENT SUPPORT FR19 AS MARKED. LOCATED, DRILLED, ALODINE, AND INSTALLED LH MONUMENT SUPPORT AT FR19 IN FORWARD WET AREA. REF SRM 51-40-02, 51-40-08, 51-23-04 APPLIED SURFACE PROTECTION REF SRN 51-23-04,51-23-05,51-23-06 PN 170-04074SDR R61A201910281160Support · corrodedCORROSION-FWD WET AREA LH MONUMENT SUPPORT FR16 AS MARKED. LOCATED, DRILLED AND ALODINE AND INSTALLED LH MONUMENT SUPPORT AT FR16 IN FORWARD WET AREA. REF SRM 51-40-02, 51-40-08, 51-23-04 APPLIED SURFACE PROTECTION REF SRM 51-23-04,51-23-05,51-23-06. SEE EAMSSDR R61A2019101931110Crossbeam · damagedDURING HEAVY CHECK MAINTENANCE FOUND CROSS BEAM TOP FLANGE SCORED AT FR 17; LBL 12.5' TO RBL 12.5" (BETWEEN RH/LH INBD SEAT TRACKS). REPAIRED FR 17; LBL 12.5' TO RBL 12.5"
CROSSBEAM TOP FLANGE BY MEANS OF CUTTING OUR DAMAGE,FABRICATING AND INSTALLING A DOUBLESDR A6WA2019101546927Post · crackedFS 409+128 RBL 18 POST OUTBOARD IS CRACKED IN THE RADIUS AT THE BOTTOM PASSED ONE RIVET. REPAIRED FS 409+128 RBL 18 OUTBOARD POST IAW REO 601R-53-41-056 REV FSDR DALA2019101405886Door Frame · corrodedCORROSION ON LOWER DOOR JAMB OF AFT COMPARTMENT CARGO. (CORROSION LEVEL 2) LOWER DOOR JAMB WAS REPLACED PER B717-200 SRM 53-20-15-2R-7 PROCEDURE 7 AND B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP1313860)SDR CALA2019101401754Frame · dentedDENT ON AFT CARGO LH FRAME UPPER FLANGE AT STA 1520 STR 26L. REF ST ENG N/R 0074536 CHECKED LIMITS TO DENT ON AFT CARGO LH FRAME AT STA1520, S-26L;L =.70", W=.50", D= .038". OUT OF LIMITS IAW B757-200 SRM 53-00-07 FIG 101. REPAIRED FRAME IAW B757-200 SRM 53-00SDR AALA201911139035Crease Beam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN CREASE ANGLE BETWEEN BS 940 AND BS 986 AT RBL 46. REPLACED CREASE ANGLE PER AARD 51-00-05-1.SDR DALA2019101205869Door Frame · crackedCRACK ON FWD DOOR JAMB OF RH MLG. FWD DOOR JAMB OF RH MLG WAS REPAIRED PER ETI-17-19-186 REV. 2 AND ER/A 582048-14 REV. ORIGINAL. SECTION I : PERMANENT REPAIR.SDR AALA201910319008Window Frame · crackedAIRCRAFT IN BASE VISIT: CRACK INDICATION ON LATERAL POST WINDSHIELD UPPER BOLT RH SIDE ATTACHMENT AREA L=0.112 APPROX IN COCKPIT (1 EA). ACCOMPLISHED REPAIR ON LATERAL POST WINDSHIELD FRAME RH IAW EA #298334.SDR REXA2019102411506Door Frame · corrodedINITIAL INSPECTION: CORROSION ON MOUNTING ANGLE OF SERVICE DOOR SURROUND STRUCTURE LOWER SILL.(PTAS)(TCI 53-20-219).
SUMMARY: ON NRC: 00218 CORROSION LEVEL 2, MOUNTING ANGLE OF SERVICE DOOR SURROUND STRUCTURE LOWER SILL WAS REPLACED PER CRJ-900 SRM 51-42-06-0SDR FDEA201910112599Door Frame · crackedMAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX AT STATION 1305.25 TO STATION 1315.42 L-26 LEFT TO L-27 LEFT FOUND CRACKED. REPAIRED AS PER SRM 53-40-15- 2R FIGURE 201 REPAIR 3 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .SDR SWAA2022040507864Threshold · crackedFWD CARGO BAY FWD CORNER THRESHOLD CRACKED. / RECEIVED; LOCATED AND DRILLED FWD CARGO BAY FWD THRESHOLD AND WILL BE INSTALLED IAW CARD N. 753-140-00-01Y. 59847U; 01NOV19; SRM 51-40-05-0G-0 59847U; 01NOV19.SDR SWAA2022040450835Support · crackedCRACKED FLOOR BOARD SUPPORT; AT B.S. 540; B.L. 0 - R.B.L. 24.5; W.L. 208.1; AT INBOARD END / REMOVED AND REPLACED CRACKED FLOOR BOARD SUPPORT; AT B.S.540; B.L.0-R.B.L.24.5; W.L.208.1; AT INBOARD END I.A.W. DWG 143A5240-36 AND AIPC SWA D638A001-SWA-0102. 20OCT1SDR R61A2019102561132Doubler · corrodedFLOOR DOUBLER FOUND CORRODED AT FR17, LBL11-36. REMOVED AND REPLACED DOUBLER IAW SRM 51-41-02 AND 51-43-04SDR DALA2019101105835Window Frame · crackedCRACK INDICATION ON INTERNAL AREA LOWER ATTACHMENT OF THE WINDSHIELD CENTER POST RH SIDE IN COCKPIT (1 EA) L= (0.375 IN. APPROX.). PERFORMED REPAIR ON INTERNAL AREA LOWER ATTACHMENT OF THE WINDSHIELD CENTER POST RH SIDE IN COCKPIT AS PER ER/A 581650-14AD. REPA
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