JASC 5311
Service difficulty reports · 61,540
Reports filed under 5311 · Fuselage Main, Frame, 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 = '5311' 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 = '5311' 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 DALA2022101806745Frame · crackedSHIP 5805 DURING INSPECTION PER REMOVED PARTS: CRACK ON FRAME STA 1540 RBL 12 BTW S- 28R/29R AT AFT CARGO. IN REF NRC 179. C2. CORRECTIVE ACTION: SUMMARY OF NRC 00286: FRAME STA 1540 RBL 12 BTW S- 28R/29R WAS REPAIRED PER ER/A 602910-14 REV ORIGINAL SECTION I:SDR DALA2022101906762Frame · corrodedSHIP 655 CORROSION ON FRAME STA 620 BTW S-27L AND S- 26L AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00311- DOUBLER ON FRAME STA 620 BTW S-27L AND S-26L AT FWD CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (2454589)SDR P5CA2022092700180Support Frame · crackedEMP - APU COMPT LH STA 2685 SUPPORT FRAME FOUND CRACK (EMP APU COMPT LH STA 2685 FRAME REPAIRED AS PER SRM 53-80-07-2R-1 AND 51-70-11-2R-0)SDR FDEA202210152567Frame · dentedMAIN DECK CARGO COMPARTMENT. RIGHT HAND SIDE STATION 1661 LONGERON 12 RIGHT FRAME FLANGE FOUND DENTED. REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR DALA2022101706695None · noneSHIP 5646 DTE, 602699-14 FUSELAGE / ATTACH FITTINGS / LH LANDING GEAR / PRESSURE DECK ASSY WEB / STA 1080 - 1180, LBL 8.20 - LBL 70 / CORROSION. CORRECTIVE ACTION: REF ERA 602699-14. (2453104)SDR IPXA2022101587153Frame · dentedINSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1360 STRINGER 26L NEEDS AN ALTERNATIVE METHOD TO INSPECT EXISTNG REPAIR PER EO# B757-5310-73926-A APPENDIX A STEP #4FOLLOWED INSPECTION METHOD PER VT MAE EA# 757-5360-27-A3047 REV- UPS EO NO: B757-5310-28011-BSDR JJBA20221125024Frame · crackedCF 4, FRAME 59 CRACKED BTWEN STR 15L-16L FRAME IS REPAIRED WITH AN EXTENDED SPLICE ON L/H CENTER FUSE 4 FRAME 59, BTW STR 15L-16L.SDR CALA2022101802830Frame · crackedL/H FR20 DOOR STOP #7 TOP I/B HOLE HAS A CRACK INDICATION IN FRA ME AND INTERCOSTAL LAYERS. REPAIR BEFORE NEXT FLIGHT. REMOVED CRACK ON LH FR20, DOOR STOP 7, IN HOLE #1, ON FRAME AND INTERCOSTAL, IAW AIRBUS DRAWING R53113118, FLOWCHART 4, REPAIR C ODE A AND ECSDR CALA2022101802827Frame · crackedL/H FR16 DOOR STOP #7 TOP I/B AND BOTTOM I/B HOLES HAVE CRACK IN DICATIONS IN FRAME AND INTERCOSTAL LAYERS. REPAIR BEFORE NEXT FL IGHT. REMOVED CRACK ON LH FR16 DOOR STOP 7, IN HOLES #1 AND #3 ON FRAM E AND INTERCOSTAL, IAW AURBUS DRAWING R531B118, FLOWCHART 4SDR CALA2022101802823Frame · crackedRH FRAME 16 DOOR STOP FITTING #7 TOP INBOARD HOLE CRACKED AT 7:0 0 POSITION IN THE FRAME LAYER AND DOOR STOP FITTING #7 BOTTOM IN BOARD HOLE CRACKED AT 8:00 POSITION IN THE FRAME LAYER. REPAIR B EFORE NEXT FLIGHT. REMOVED AND INSTALLED INTERCOSTAL AND DOOR STOSDR DALA2022101706694None · noneSHIP 5805 DTE, 602910-14 FUSELAGE / MAIN FRAME / STA 1540 FRAME S-28R & S- 29R / CORROSION AND CRACK. CORRECTIVE ACTION: REF ERA 602910-14. (2451989)SDR DALA2022101706688None · noneSHIP 655 IN REF NRC 0262: DENT ON FRAME STA 1520 BTW S-24L - S-27L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00611: DENT ON FRAME STA 1520 BTW S-24L - S-27L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM HFEC INSPECTION WAS ACCOMPLISHSDR DALA2022101706687None · noneSHIP 655 IN REF NRC 0262: DENT ON FRAME STA 1520 BTW S-24L - S-27L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00611: DENT ON FRAME STA 1520 BTW S-24L - S-27L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM, HFEC INSPECTION WAS ACCOMPLISSDR DALA2022101406662Longeron Splice · corrodedAIRCRAFT 9526, INITIAL INSPECTION:CORROSION ON LONG SPLICE 30 BTW STA Y=889-908 AT AFT CARGO COMPARTMENT (C2). CORRECTIVE ACTION: LONG SPLICE 30 BTW STA Y=889-908 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-01-0G PAR. 6 & 51-41-05-0G PAR. 8. LSDR CALA2022101402800Intercostal · crackedL/H FR16 DOOR STOP #7 HOLES 1&3 HAVE CRACK INDICATIONS IN INTERC OSTAL AND FRAME AT 3 O CLOCK "REPAIR BEFORE NEXT FLIGHT" SUPPORT TASK AD RELATED (AD 2022-02-11) GENERATED AT HAECO LCQ PER NR 9 292408 (42408) BY V061632 REMOVED AND REPLACED INTERCOSTAL AND REASDR CALA2022101402798None · gouged(SUPPORT TASK) MAIN CABIN FRAME AT STA 1640 HAS 1EA SUBSTRUCTURA L TEE CLIP IS GOUGED AND KNIFE EDGED ON THE UPPER LOWER LEGS AT S14L. TRANSCRIBED FROM HAECO GSO NRC# 9282170 REMOVED AND REPLACED TEE-CLIP AT STA 1640 PN: 146N8749UP IAW B757-200 SRM 51-40-02-0SDR SWIA202266730None · corrodedCF III LOWER FUSELAGE HAS CORRODED SHEAR CLIP ALONG FR 88 BETWEEN STGR 28R AND STGR 27R FWD OF WASTE SERVICE BOX. (C-CHECK RO 11/3/2022) REMOVED AND REPLACED SHEAR CLIP ALONG FR 88 BETWEEN STGR 28R AND STGR 27R FWD OF WASTE SERVICE BOX. REF SRM 51-40SDR CALA2022101402796Angle · gouged(SUPPORT TASK) MAIN CABIN FRAME AT STA 1640 SUBSTRUCTURAL TEE CL IP UPPER AND LOWER LEG IS GOUGED AND KNIFE EDGED AT S14R. TRANS CRIBED FROM HAECO GSO NRC# 9282166SDR DALA2022101306598None · noneSHIP 3223 NEED TO COMPLY WITH ER/A 547942-14AD. CORRECTIVE ACTION: COMPLIED WITH ERA 547942-14AD. (2448749)SDR DALA2022101306597None · noneSHIP 3223 NEED TO COMPLY WITH ERA 547942-14AD. CORRECTIVE ACTION: COMPLIED WITH ERA 547942-14AD. (2448747)SDR DALA2022101306596None · noneSHIP 3223 NEED TO COMPLY WITH ER/A 547942-14AD. CORRECTIVE ACTION: COMPLIED WITH ERA 547942-14AD. (2448745)SDR DALA2022101306595None · noneSHIP 3223 NEED TO COMPLY WITH ERA 547942-14AD. CORRECTIVE ACTION: COMPLIED WITH ERA 547942-14AD. (2448741)SDR AALA202210137443Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FRAME AT LEFT HAND DOOR STOP FITTING #1 LOWER INBOARD FASTENER HOLE. AT FR 68 AND S22L. REPARED FRAME PER SRM 53-41-12-300-010 AND EA 339017.SDR JJBA20221125025Frame · crackedRF 1 FRAME 72, SHARE CLIP BTWN STR 7L-10L CRACKED SHARE CAP FR 72 BTR STR 7L-10L FORMED FOR REPLACEMENT. NEW SHEAR CLIP FABRICATED. SHEAR CLIP FR 72 BTW STR 7L-10L SEPARATED . NEW SHEAR CLIP INSTALLED.SDR SWIA202266729None · gougedSHEARCLIP GOUGED IN MAIN CABIN AT FR60 BETWEEN STRINGER 12L AND 13L. (C-CHECK RO 11/3/2022) REMOVED SHEAR CLIP AND REPLACED WITH FABRICATED SHEAR CLIP PN: EAMSFAB170-21153-002 AT FR 60 BETWEEN STRINGERS 12L AND 13L REF EMB SRM 51-40-08. WEIGHT OF FABRISDR DALA2022101406671None · noneSHIP 197 AMOC REQUIRED TO AD 14-14-04: ERA 602721-14AD ISSUED FOR REPAIR TO STA 859.5, RBL 89 BULKHEAD. CORRECTIVE ACTION: AMOC TO AD 14-14-04 REQUIRED AT OR BEFORE 50,000 TOTAL FLIGHT CY CLES. (2447508)SDR DALA2022101406653None · noneSHIP 5646 DTE, 602588-14 FUSELAGE / MAIN FRAME / RH LANDING GEAR / PRESSURE DECK WEB, STA 1080 TO 1153.78 & BL 0 TO RBL 70 / CORROSION. CORRECTIVE ACTION: REF ERA 602588-14. (2447743)SDR 2A6R2022101165202Frame · crackedDURING A SCHEDULED INSPECTION ASB21-01, DAMAGE WAS DISCOVERED AT FRAME 5 AT APPROXIMATELY FS 4,709MM RELATING TO THE STC SR00566DE, DRAWING 739-1600, WALL. THE DAMAGE IS ADJACENT TO THE MEDICAL WALL ATTACH FITTING LOCATIONS. PERFORMED THE ALERT SERVICE BULSDR AALA202210174239Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED OPEN HOLE ON FRAME AT LEFT HAND AFT PASSENGER / CREW DOOR CUT OUT UPPER AFT CORNER AT FR 68 AND S8L. REPAIRED FRAME PER EA 338987.SDR DALA2022101406636None · none(LOG 2445892) DURING INSPECTION FOUND COCKPIT NUMBER 1 WINDOW RH WAS FOUND CRACK ON COCKPIT NUMBER 1 WINDOW FRAME ASSEMBLY RH ON OUTBOARD UPPER CORNER INNER STRUCTURE FACE. NUMBER 1 WINDOW FRAME ASSEMBLY RH WAS REPAIRED PER ER/A 602485-14AD REV ORIGINAL.SDR DALA2022101406635None · none(LOG 2445830) DURING INSPECTION FOUND COCKPIT WINDOW FRAME ASSEMBLY", WAS FOUND CRACK 1.250" LONG ON COCKPIT NUMBER 1 WINDOW FRAME ASSEMBLY ON OUTBOAR UPPER CORNER EXTERIOR FACE. COCKPIT NUMBER 1 WINDOW FRAME ASSEMBLY ON OUTBOARD UPPER CORNER EXTERIOR FACE WASSDR SROM2022101002Frame · corrodedCORROSION DAMAGE ON FUSELAGE FRAME UPPER WEB AND CAP. DAMAGE IS BEYOND MANUFACTURES PUBLISHED LIMITS. DAMAGE AT STA. X32.400 STRINGERS 30P AND 30S. PART NUMBERS ARE 85329152-103 (LH) / 85329256-101 (RH)SDR 2022FA0000590Frame · corrodedCORROSION FOUND ON AUX FRAME AT BS 887 BTWN S24L AND S25L IN AFT CARGO PITSDR SWIA202266919Frame · corrodedFRAME SECTOR F.S.310 IS CORRODED AT STRINGER 27L. REMOVED THE FRAME SECTION, REINFORCMENT STRAP, AND SPLICES IAW SRM 51-42-21 AND 51-42-06. INSTALLED A FRAME NEW SECTION IAW SRM 51-42-21 AND 51-42-06. MAJOR REPAIR.SDR SWIA202266666None · corrodedCORROSION IN L/H FLOOR BEAM FR.87. (C-CHECK RO 10/25/2022) REMOVED AND REPLACED L/H FLOOR BEAM FR.87. REF EMB SRM 51-40-08. L/H FLOOR BEAM REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED.SDR SWIA202266665None · corrodedCORROSION IN R/H FLOOR BEAM AT FR.87. (C-CHECK RO 10/25/2022) REMOVED AND REPLACED R/H FLOOR BEAM FR.87. REF EMB SRM 51-40-08. L/H FLOOR BEAM REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTEDSDR DALA2022101206572None · none(LOG 2443108) DURING INSPECTION FOUND CRACK WAS NOTED IN LH WINDOW FRAME NO 1 AT TOP OF INSPECTION AREA JUST BELOW UPPER RADIUS. CRACK EXTENDS FROM AFT EDGE OF FRAME APPROX. 1 INCH FWD. REPAIR COMPLIED WITH PER ERA 602196-14AD REV A.SDR IPXA2022100886960Frame · dentedINSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1560 BETWEEN STRINGERS S25R AND S26R HAS TWO DENTS ON THE UPPER FLANGE OF FRAME 1560 NO DENTS ARE ALLOWED PER SRM 53-00-07-1A-1REPAIRED FRAME 1560 PER SRM 53-00-07-2R-5 DETAIL 1SDR IPXA2022100886958Frame · dentedINSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1480 AT STRINGERS 26R THERE ARE TWO DENTS ON THE UPPER FLANGE OF FRAME NO DENTS ARE PERMITTED PER SRM 53-00-07-1A-1REPAIRED FRAME 1460 PER SRM 53-00-07-2R-5 DETAIL 1SDR IPXA2022100886957Frame · dentedINSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1520 BETWEEN STRINGERS 23R AND 26R THERE ARE TWO DENTS ON THE UPPER FLANGE OF FRAME NO DENTS ARE PERMITTED PER SRM 53-00-07-1A-1REPAIRED FRAME 1460 PER SRM 53-00-07-2R-5 DETAIL 3SDR IPXA2022100886956Frame · dentedINSPECTION TYPE:SEG1INCOMING REPAIR ACCOMPLISHED ON FS 1300 BETWEEN STRINGERS S23L AND S26L WAS DONE PER SRM 51-70-11. CUSTOMER REQUEST TO REMOVE REPAIR AND INSTALL REPAIR PER SRM 53-00-07-2R-5 DETAIL 3REPAIRED FRAME 1300 LH PER SRM 53-00-07-2R-5 DETAIL 3 AND SDR IPXA2022100886955Frame · dentedINSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1460 BETWEEN STRINGERS S25L AND S26L THERE IS A .420" LONG BY .032" DEEP DENT ON THE UPPER FLANGE NO DENTS ARE ALLOWED PER SRM 53-00-07-1A-1REPAIRED FRAME 1460 PER SRM 53-00-07-2R-5 DETAIL 3SDR IPXA2022100886954Frame · dentedINSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1540 1.2" O/B OF STRINGER S26R HAS A .70" LONG BY .45" WIDE BY .50" DEEP GOUGE ON THE UPPER PART OF WEB INTO THE FRAME FLANGEREPAIRED FRAME 1460 PER SRM 53-00-07-2R-5 DETAIL 2SDR HNAA2022102500295Frame · crackedE939229 - FR 72 CRACKED BETWEEN STGR 17L AND STGR 16L .... REMOVED AND REPLACED FR 72 LH SECTION IAW EMB-145 SRM 51-40-02.SDR DALA2022101106557None · noneSHIP 3115 - EXISTING RE-WORK FLOOR STRUCTURE BEAM LOCATED AT FR16 AND Y1292 AT FWD GALLEY AREA. CORRECTIVE ACTION: EVALUATED RE-WORKED AREA FLOOR BEAM Y1292 AND FOUND WITHIN LIMITS AS PER A319 SRM 53-11-14-991-012. (2441792)SDR CALA2022101002749Frame · crackedFUSELAGE FRAME AT STA 800 BELOW STRINGER 8L IS CRACKED AT ATTACH BRACKET RIVET. REPORTED BY V921209 REPAIRED FASELAGE FRAME AT STA 800 BETWEEN STRING 8L-9LSDR CALA2022101002748Frame · crackedFUSELAGE FRAME AT STA 1540 BELOW STRINGER 8L IS CRACKED AT ATTAC H BRACKET RIVET. REPORTED BY V921209 REPAIRED FUSELAGE FRAME AT STA 1540 BETWEEN STRINGERS 8L-9L PER B757-200 SRM 53-00-07 REPAIR 8. SEE NR 151186-0200-0131 FOR DETA ILSSDR CALA2022101002747Frame · crackedFUSELAGE FRAME AT STA 1120 BELOW STRINGER 8R IS CRACKED AT ATTACH BRACKET RIVET. REPORTED BY V921209 REPAIRED FUSELAGE FRAME AT STA 1120 BETWEEN S8R & S9R.SDR CALA2022101002744Frame · crackedLEFT FR 35 STR 30 HOLE 1,2,3, HAS A OUT OF ROUND INDICATION IN THE FR LAYER INTERIOR FACE AT 3-7 O''CLOCK AND AFT SKIN LAYER FWD SKIN LAYER AS VIEWED FROM EXTERIOR ADDITIONALY HOLE FOUND AT L/H FR35 STR28 FOUND CRACKED PER HAECO LCQ N/R 9290148/30148/9290149 SDR SWAA2022111056930Frame · crackedCRACK FRAME ON BS 947.5 AND LBL8.1 AFT CARGO COMPARTMENT 2022-561846 / [01] REPLACED FRAME ON BS 947.5 AND LBL8.1 AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG?S 147A1047 REV. - AND 147A7410 REV A. <BR>SEE INDIVIDUAL SIGN-O
Back to JASC 5311