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 DALA2023033102499Unknown · unknownSHIP 658 DTE, ERA 606827-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE FRAME INNER FLANGE AT STA 820 & S-28L/R. CORRECTIVE ACTION: REF ERA 606827-14AD. (2696529)SDR DALA2023033102498Unknown · unknownSHIP 658 DTE, ERA 606884-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE FRAME INNER FLANGE AT STA 760 & S-28L/R. CORRECTIVE ACTION: REF ERA 606884-14AD. (2696522)SDR DU4R2023033100003Frame · crackedDURING SCHEDULED MAINTENANCE AT HAECO, LAKE CITY, FLORIDA FOUND RIGHT FR 16 DOUBLE JOGGLE HOLE #6 HAS A CRACK INDICATION IN FRAME LAYER STARTING AT 4 MM I/B FACE AND EXTENDING O/B 4 MM AT 1:0'CLOCK POSITION AS VIEWED FROM EXTERIOR. S/O 339001 N/R 28054SDR DU4R2023033100002Frame · crackedDURING SCHEDULED MAINTENANCE AT HAECO, LAKE CITY, FLORIDA FOUND RIGHT FR 16 DOUBLE JOGGLE HOLE #8 HAS A CRACK INDICATION IN FRAME LAYER STARTING AT I/B FACE AND EXTENDING O/B 4 MM AT 1:0'CLOCK POSITION AS VIEWED FROM EXTERIOR. S/O 339001 N/R 28053SDR SWAA2023050522488Frame · crackedCRACK FRAME ON BS 907 AND BETWEEN STR25R TO STR26R AFT CARGO COMPARTMENT 2023-212796<[01] REPLACED FRAME ON BS 907 AND BETWEEN STR24R TO STR24L AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DWG# 147A1007; SHEET 42; REV.D. SEE INDIVIDUAL SIGN OFF BSDR DALA2023040302522Plate · corroded(LOG 2695677) DURING INSPECTION FOUND FWD CARGO PIT RH TRANSITION PLATE STA 420-440 UPPER SIDE IS CORRODED. REMOVED AND REPLACE TRANSITION PLATE RH STA 420-440 IAW BOEING 737-800 SRM 51-40-02.SDR DALA2023040302520Unknown · unknown(LOG 2695742) DURING INSPECTION FOUND L2 DOOR SILL SCUFF PLATE SUPPORT Z ANGLE TOP SURFACE CORRODED BS 950 -966. LBL50. REPAIRED SUPPORT Z ANGLE IAW ERA 606528-14 REV ORIGINAL.SDR DALA2023033102497Unknown · unknownSHIP 665 DTA MONITOR INSPECTION LOG REF ERA 606981-14. CORRECTIV ACTION: REF ERA 606981-14. (2695510)SDR DALA2023033102496Unknown · unknownSHIP 5648 REPETITIVE LFEC INSPECTION ER/A 607267-14. CORRECTIVE ACTION: REF ERA 607267-14AD. (2695726)SDR DALA2023033102491Unknown · unknownSHIP 665 CRACK ON FRAME STA. 1420, AND S-26L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00423. FRAME STA. 1420, AND S-26L AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (2695927)SDR DALA2023033102490Unknown · unknownSHIP 665 CRACK ON FRAME STA. 1600, BTW S-26R TO S-27R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00431. FRAME STA. 1600, BTW S-26R TO S-27R AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (2695775)SDR DALA2023033102472Unknown · unknownSHIP 3221 CRACK INDICATION FOUND ON WEB HORIZONTAL FLANGE IN THE RADIUS OF FR 68 AT STRGR 22LH. CORRECTIVE ACTION: COMPLIED WITH ERA 607098-32. (2696195)SDR DALA2023033102471Unknown · unknownSHIP 3230 NEED TO ACCOMPLISH ER/A 605354-14 REVISION ORIGINAL SECTION II BIRD STRIKE MAJOR REPAIR. CORRECTIVE ACTION: COMPLIED WITH ERA. (2695915)SDR AALA202307050437Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT UPPER DOUBLE JOGGLE AREA AT FASTENER HOLES 6, A, B , C AND LOWER INBOARD FASTNER HOLE AT DOOR STOP #7 AT FR 16 RIGHT. REPLACED FRAME SECTION PER EA 343711.SDR DALA2023040502655Channel · corroded(LOG 2694208) DURING INSPECTION FOUND L-1 DOOR LOWER JAMB MOP SEAL CHORD EXFOILATED. REMOVED AND REPLACED L-1 MOP SEAL CHORD IAW BOEING 737-800 SRM 54-40-02.SDR DALA202304050001Channel · corroded(LOG 2694208) DURING INSPECTION FOUND L-1 DOOR LOWER JAMB MOP SEAL CHORD EXFOILATED. REMOVED AND REPLACED L-1 MOP SEAL CHORD IAW BOEING 737-800 SRM 54-40-02.SDR DALA2023033102474Unknown · unknownAIRCRAFT 9571, INITIAL INSPECTION: CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SECTION OF DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-04-0G, B717-200 SRM 51-41-02-0G, B717-200 SRM 51-41-05-0G. AND B717-2SDR DALA2023033102473Unknown · unknownAIRCRAFT 9551, INITIAL INSPECTION: CRACK ON INNER FITTING OF BEAM # 2 IN FWD EDGE AND BEAM # 3 ON FWD EDGE APPROX BTW STA Y=954 AND STA Y=964 AT AFT CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: INNER FITTING OF BEAM # 2 IN FWD EDGE AFT CARGO COMPARTMENT DOOR WASSDR DALA2023033002455Unknown · unknownSHIP 658 DTA MONITOR INSPECTION LOG REF ERA 606750-14AD. CORRECTIVE ACTION: REF ERA 606750-14AD. (2693885)SDR DALA2023033002449Unknown · unknownSHIP 658 DENT ON UPPER CHORD OF FRAMES STA. 760 AND 780, BTW LBL 2 TO RBL 2 AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00292: DENT ON UPPER CHORD OF FRAME 780, BTW LBL 2 TO RBL 2 AT FWD CARGO COMPARTMENT. WAS REPAIRED PER ER/A N 606750-14AD RESDR 2A6R2023032966804Frame · crackedCRACK DAMAGE WAS DISCOVERED ON FRAME # 5A AT FUSELAGE STATION 5,023MM. ONE CRACK WAS LOCATED AT THE FLANGE RADIUS WHERE THE FRAME MEETS THE OUTER STRUCTURE AT THE RH SIDE. THE CRACK WAS STOP DRILLED THEN RE-ENFORCED VIA AN AIRBUS REPAIR DOUBLER (PN: L533M102SDR 2A6R2023032966803Frame · corrodedDURING 1000 HOUR INSPECTION, CORROSION DAMAGE WAS NOTED TO THE T-CAP (PN: L533M1028203) OF FRAME 3 AT APPROXIMATELY FUSELAGE STATION 3,150MM. THE DAMAGE REQUIRES PART REPLACEMENT AND DUE TO PART AVAILABILITY, THE PART WAS FABRICATED PER AIR METHODS ENGINEERINSDR 2023FA0000172Unknown · unknownDURING MAINTENENCE INSPECTION FOUND CORROSION ON FRAME INNER CHORD, STA 1417, STR 19R TO STR 20R.SDR 2023FA0000171Unknown · unknownDURING MAINTENENCE INSPECTION FOUND CORROSION ON FRAME INNER CHORD, STA 1197+88, STR 20L.SDR AALA202304043202Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FASTENER HOLE IN FRAME LOCATED AT BS 500I AND S26R. ACCOMPLISHED SPLICE REPAIR OF FRAME PER SRM 53-30-07-2R.SDR DALA2023032802389Unknown · unknownAIRCRAFT 9513, CRACK ON OVERWING FRAME STA Y=674 LH SIDE AT WING BOX AREA. CORRECTIVE ACTION: OVERWING FRAME STA Y=674 LH WAS REPLACED PER CARD 5310-01436-03A. (LP 2691308)SDR DALA2023032902422Unknown · unknownSHIP 5649 COMPLY WITH ERA 607185-14AD REV. ORIGINAL SECTION 1. CORRECTIVE ACITON: COMPLIED WITH ERA 607185-14AD REV. ORIGINAL SECTION 1. (2690943)SDR DALA2023032702356Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CORROSION AT CUSP ANGLE LOWER SURFACE ON STA=560 TO STA =579 ON FWD CARGO COMPARTMENT RH SIDE. CORRECTIVE ACTION: CUSP ANGLE LOWER SURFACE ON STA =560 TO STA=579 ON FWD CARGO COMPARTMENT RH SIDE WAS REPAIRED PER B717 200 SRM SDR DALA2023032702355Unknown · unknownAIRCRAFT 9513, AFTER REMOVAL WEB BTW STA Y=200 TO 208 AND STRINGERS L13 TO L18 CORROSION WAS FOUND AT CUSP ANGLE AT STA Y-200 ON STRINGER L18. CORRECTIVE ACTION: CUSP ANGLE AT STA Y-200 ON STRINGER L18 WAS REPAIRED PER B717-200 SRM 53-00-55-2 REPAIR 3 PAR. 5. SDR VNAA202327030004Door · unknownIS67052110200 IMPROVED CORROSION RESISTANCE OF PHASE IV PAX DOOR, REQUIRES COMPLETION.SDR VNAA202327030003Door · unknownSB 670BA-52-042 PAX DOOR MODIFICATION TO THE INSTALLATION OF ACCESS PANELS AND COVERS, REQUIRES COMPLETION.SDR VNAA202327030002Stringer · corrodedSTRINGER 25R IS CORRODED IN MULTIPLE LOCATIONS BETWEEN FS 280.00 AND 333.00.SDR VNAA202327030001Frame · corrodedFRAME AT FS 310.00 IS CORRODED BETWEEN STGR 24L AND 26R.SDR AALA202306239424Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD CENTER POST RIGHT HAND SIDE FRAME UPPER BOLT HOLES CRACKED AT FR 2 AND Y0. REPLACED FRAME PER EA 343543.SDR AALA202306234699Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD CENTER POST LEFT HAND SIDE FRAME UPPER BOLT HOLES CRACKED AT FR 2 AND Y0. REPLACED FRAME PER EA 343543.SDR AALA202304260109Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FOOT COUPLING FASTENER HOLE AT FR 43 BETWEEN S21L AND S23L. REPLACED FRAME PER EA 343587.SDR SWIA2023040326Unknown · crackedCRACKED SHEAR CLIP AT FR 83 STRG 27R - 28R. REMOVED AND REPLACED SHEAR CLIP AT FR 83 STRG 27R - 28R. REF SRM 51-40-08. SHEAR CLIP REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTEDSDR DALA2023032802382Unknown · unknownSHIP 658 DTE, ERA 606749-14. CORRECTIVE ACTION: REF ERA 606749-14. (2689159)SDR DALA2023032802379Unknown · unknownSHIP 658 DENT ON FRAME STA. 820 FROM LBL 2 TO RBL 2 AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00719: FRAME STA. 820 FROM LBL 2 TO RBL 2 AT FWD CARGO COMPARTMENT WAS REPAIRED PER ER/A 606749-14AD ORIG. (2689390)SDR SWAA2023042720875Frame · crackedCRACK FRAME ON BS 947.5 AND RLB3.0 WL154 AFT CARGO COMPARTMENT 2023-200341<[01] REPLACED FRAME SECTION LOC BTW STR 23R TO STR 23L BS 947.5 AND WL154 AFT CARGO COMPARTMENT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 147A0002 REV: -; DWG 147A1047 REVSDR DALA2023032602317Unknown · unknownAIRCRAFT 9571, CORROSION AT SLIDE SUPPORTS LOCATED AT RBL 53 BETWEEN STA-163 AND STA-186. CORRECTIVE ACTION: NEW SUPPORTS (2EAS) WERE REPLACED PER B717-200 SRM 51-41-01-0G PAR 6. (LP 2686865)SDR SWAA2023050320563Frame · crackedCRACK FRAME LOCATED BS380 AND BETWEEN STR8L TO STR9L AT PASSENGER CABIN 2023-208650<[01] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 200053402; DUE DATE: 13-MAY-23;[02] PERFORMED DETAIL VISUAL INSPECTION IAW B737-700 SRM 51-10-02 AND NDT INSPECTISDR SWAA2023042720669Frame · crackedCRACK FRAME ON BS 907 AND BETWEEN STR25R TO STR26R AFT CARGO COMPARTMENT 2023-200308<[01] REPLACED FRAME ON BS 907 AND BTW STR 24R TO STR 24L IAW B737-700 DWG 147A7500 REV D AND SRM 51-40-02 SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED FRAME ON BS 907 AND BTW SDR DALA2023032602315Unknown · unknownAIRCRAFT 9571, DURING OK TO TREAT RH WING BOX AREA WITH CIC, CRACKED CUSP MEMBRANE WEB WAS FOUND ON STA Y= 715-720 X=-44 AT PASSENGER CABIN FLOOR STRUCTURE. CORRECTIVE ACTION: CUSP MEMBRANE WEB ON STA Y= 715-720 X=-44 AT PASSENGER CABIN FLOOR STRUCTURE WAS REPSDR DALA2023032602314Unknown · unknownAIRCRAFT 9577, TAIL COMPT FRAME CRACKED STA 1133 AT STR 2R-MARKED. CORRECTIVE ACTION: COMPLIED WITH ER/A 607133-14 REV. ORIG. PRI REV. "0" ALL INSTRUCTIONAL STEPS. I ALL INSTRUCTIONAL STEPS ON ER/A 607133-14 REV. ORIG. PRI REV. "0" MATCH FINALE ER/A 607133-14 SDR DALA2023032602313Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON RH CUSP WEB STA. Y= 198 TO Y=202 (R1) RBL50 AT PASSENGER CABIN. CORRECTIVE ACTION: RH CUSP WEB STA. Y=200 TO Y=218 (R1) RBL50 AT PASSENGER CABIN WAS FABRICATED AND REPLACED PER DWG 9936535 REV. CS ITEM: -95 AND BSDR LR7A2023032403283Doubler · crackedDURING SCHEDULED B-3 CHECK UNDER WHILE PERFORMING OTHER MAINTENANCE, FOUND #2 RH WINDOW POST CRACKED AT FS107, WL235, RBL34. / REPAIRED IAW LAC MEA 382-53-23-019. NR# 1000920698.SDR DALA2023032402307Unknown · unknownAIRCRAFT 9513, CUSP ANGLE ON R1 DOOR JAMB WAS FOUND CORROSION ON CUSP WEB TO BTW STA 218 TO STA 237 RH. CORRECTIVE ACTION: CUSP WEB TO BTW STA 218 TO STA 237 RH WAS FABRCATED AND REPAIRED PER B 717-200 SRM 53-00-55-2R-4 FIG 226, DWG 9930538-109 REV. CC AND WASSDR DALA2023032402306Unknown · unknownAIRCRAFT 9513, CUSP ANGLE ON R1 DOOR JAMB WAS FOUND CORROSION ON ANGLE SUPPORT BTW STA 137 TO STA 160. CORRECTIVE ACTION: ANGLE WAS FABRICATED PER DWG 5910085 REV DE. (LP 2685491)SDR DALA2023032402305Unknown · unknownAIRCRAFT 9513, CUSP ANGLE ON R1 DOOR JAMB WAS FOUND CORROSION ON ANGLE SUPPORT BTW STA 200 TO STA 210. CORRECTIVE ACTION: ANGLE SUPPORT WAS REPLACED PER DRAWING 5910085 ITEM 15 REV. DJ. (LP 2685489)
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