JASC 5311
Service difficulty reports · 61,549
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 CALA2019062100990Frame · crackedFRAME AT BS 500A BETWEEN S-8R AND S-9R CRACKED AT I /B FASTENER HOLE AC OUTLET EXTRUSION SUPPORT BRACKET. REPAIRED THE FRAME IAW ECRA 5 311-02138 AND EA 5310-04716 REV I OP1 FIG 3.SDR CALA2019062210989Frame · crackedFRAME AT STA 480 BETWEEN S-8R AND S-9R CRACK AT I/B FASTENER HOLE AC OUTLET EXTRUSION SUPPORT BRACKET. REPAIRED FUSELAGE FRAME IAW ECR A 5311-02138 AND EA5310-04716 REV I OP1 FIG 3 .SDR CALA2019062210986Frame · crackedCABIN FRAME AT STA 500C RH FRAME CRACKED BETWEEN STR 8 AND STR 9 IN REF EA 5310-04716 REV I OP 2. R/H FRAME AT STA 500C BETWEEN STR8R AND STR9R REPAIRED IAW EA 53 10-04716 REV I OP 02 SEE FLEET CYCLE NON-ROUTINE 9676872 FOR ALL WORK ACCOMPLISHED.SDR CALA2019062210985Frame · crackedBS 380 CRACKED AT I/B RIVET BETWEEN STRINGERS 8 & 9R AT THE ACFT OUTLET EXTRUSION SUPPORT ATTACHMENT RIGHT SIDE OF CABIN. ACCOMPLISHED PERMANENT REPAIR AT FUSELAGE FRAME IAW EC/RA 5311-02172, EA5310-04716 REV. I .SDR CALA2019062210984Frame · crackedBS 380 CRACKED AT I/B RIVET BETWEEN STRINGERS 8 & 9R AT THE ACFT OUTLET EXTRUSION SUPPORT ATTACHMENT RIGHT SIDE OF CABIN. ACCOMPLISHED PERMANENT REPAIR ON THE FUSELAGE FRAME IAW EC/RA 5311-02170, EA#5310-04716 REV."I".SDR CALA2019062210983Frame · crackedAT BS 907 R CRACK NOTED AT I/B RIVET BETWEEN STR 8 & 9R AT THE ACFT OUTLET EXTRUSION SUPPORT ATTACHMENT RIGHT SIDE OF CABIN. ACCOMPLISHED PERMANENT REPAIR AT FUSELAGE FRAME STA 907 R, STR 8 TO 9R, PER UNITED EC/RA#5311-02175, REF. EA5310-04716 REV."I" .SDR CALA2019062100982Frame · crackedCABIN FRAME AT STA 500A R/H FRAME HAS A CRACK BETWEEN STR 8R AND 9R. REF FLEET CYCLE NON-ROUTINE 9676870. REPAIRED FRAME PER EA 5310-04716 REV I OP 2 FIG 3 VERIFIED BY INSPECTION.SDR CALA2019062210981Frame · crackedCABIN FRAME AT STA 440 L/H FRAME CRACKED BETWEEN STRINGER 8L AN D 9L REF FLEET CYCLE NON-ROUTINE 9676615. REPAIRED CRACKED FRAME PER EA 5310-04716 REV I OP2 FIG 3.SDR CALA2019062100980Frame · crackedCABIN FRAME AT STA 500A L/H FRAME CRACKED BETWEEN STRINGER 8L AN D 9L REF FLEET CYCLE NON-ROUTINE 9676622. REPAIRED CRACKED FRAME PER EA 5310-04716 REV I OP2 FIG 3 ADD EMP:U189708 VERIFIED REPAIR COMPLETED REF.EA 5310-04716 REV I OP2 FIG 3.SDR DALA2019061803623Frame Angle · corrodedEXFOLATION ON FRAME CLIP STA Y=908 BTW LONGERON 26LH TO LONGERON 28RH BOTH FACES AT AFT CARGO COMPARTMENT. NRC 0174: CORROSION LEVEL 2, FRAME CLIP STA Y=908 BTW LONG 26LH TO LONG 28RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B-717-200 SRM 51-41-02-0G. (LP #11SDR DALA2019061803621Frame · crackedCRACK ON RH WINDOW RING PAN STA Y=889 AT PAX CABIN. NRC 00197: CRACK ON RH WINDOW RING PAN STA Y=889 WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.SDR WVER201906170025Frame · corrodedLOWER FRAME SECTOR, @ FS 847.00 & 16, STGR 26L - 26R CORRODED BEYOND ALLOWABLE LIMITS.SDR CALA2019061700971Frame · crackedCABIN FRAME AT STA 500D R/H FRAME CRACKED BETWEEN STRINGER 8R AN D 9R REF FLEET CYCLE NON-ROUTINE 9676873. REPAIRED CRACKED FRAME PER EA 5310-04716 REV I OP2 FIG 3 ADD EMP:U243889 VERIFIED REPAIR COMPLETED REF.EA 5310-04716 REV I OP2 FIG.3SDR DALA2019061703618Frame Angle · crackedCRACK ON CLIP FRAME LONG 14RH STA 1022 AT FWD FACE OF BULKHEAD (CPAX). NRC 00401: FRAME CLIP WAS REPLACED PER B717-200 SRM 51-41-05-0G.SDR DALA2019061763613Frame · crackedCRACK ON FRAME, LONG 17RH STA 1037 (CPAX). NRC 00404: FRAME, LONG 17RH STA 1037 WAS REPAIRED PER B717-200 SRM 53-20-07-2R-4. (LP #1124857)SDR CA190617011Frame · corroded(CAN) FS 364, FRAME CORROSION. (TC# 20190617011)SDR CALA2019061700959Frame · crackedMAIN CABIN UPPER LOBE FUSELAGE FRAME AT STA 380 BETWEEN S-8L AND S-9L HAS CRACK AT I/B FASTENER HOLE FOR AC OUTLET EXTRUSION SUPP ORT BRACKET (REPAIR PER W/C SEQ #1655 FIG 3 STEP 9) REF FLEETCYCLE N/R 9666842 REPAIRED FRAME STA 380 S-7L AND S-8L PER EC/RA # 53SDR CALA2019061700968Frame · crackedAT BODY STA 867 R CRACK NOTED AT I/B RIVET BETWEEN STR 8 & 9 AT THE ACFT OUTLET EXTRUSION SUPPORT ATTACHMENT RIGHT SIDE CABIN MARKED (REF NR 99836083) ACCOMPLISHED PERMANENT REPAIR AT FUSELAGE FRAME STA 867 R BETWEEN STRINGER 8 & 9 PER EC/RA NUMBER 5311-02171 SDR CALA2019061700967Frame · crackedAT BODY STA 827 R CRACK NOTED AT I/B RIVET BETWEEN STR 8 & 9 AT THE ACFT OUTLET EXTRUSION SUPPORT ATTACHMENT RIGHT SIDE OF CABIN MARKED. (REF NR 99836082) ACCOMPLISHED PERMANENT REPAIR AT FUSELAGE FRAME STA 827 R STRINGER 8 TO 9 R PER EC/RA 5311-02173. REF EA SDR DALA2019061763584Frame · crackedCRACK INDICATION ON FRAME 36 AT HOLE A, REPAIR IN ACCORDANCE WITH WORK CARD 5311-01171-04A, AA 5311-01171. SB A320- 53-1264. AD-2018-06-04 IN FWD CARGO COMPARTMENTSDR CA190614021Frame · cracked(CAN) DURING CLOSE UP, A CRACK WAS FOUND ON FRAME 26, PART NUMBER S53572700200. W/O 33426718 NR 00386 ORIGINATING TASK GEN-05-00-400-0002..ATR TO SUPPLY REPAIR (TC# 20190614021)SDR REXA2019062740948Frame · corrodedFS 574.00 FRAME CORRODED ON FWD SIDE BETWEEN STRINGER 25L AND 25R. REPLACED FS 574 LOWER FRAME SECTION P/N 601R36024-61 IAW CRJ 200 SRM 51-42-06, 51-42-21, AND 51-40-11 TR#51-42SDR REXA2019062740947Frame · corrodedFS 589 FRAME CORRODED ON FWD AND AFT SIDES BETWEEN STRINGERS 22L AND 23R. REPLACED FS 589 FRAME IAW SRM 51-42-21, 51-42-06,51-40-11 TR 51-42 51-23-00, 51-21-16, 51-25-00, AND 51-21-11SDR SIMA201906184005Frame · corrodedFR80 HAS CORROSION IN THE SHUNT CONNECTION BAR CONTACT AREA-C/A-REPAIRED FR 80 SHUNT CONNECTION BAR CONTACT AREA IAW ERS-EM-53MR-3802.SDR DALA2019061753588Frame · crackedCRACK INDICATION OF THE UPPER RADIUS OF THE FRAME TAB. CRACK LENGTH APPROXIMATELY 1/8 IN. NRC 066-0002:5310-01436-01B/001 00042: REPLACED LT OVER-WING FRAME AT STA 696 PER AMDS WORK CARD 5310- 01436-03A.SDR CALA2019061400952Frame · damagedAFT CARGO FRAME STA 727D RBL 15 BETWEEN STR 25R AND 26R ELONGATED HOLE WHERE SIDE PANEL ATTACHES. FRAME REPAIRED AS REF ECRA 5310-07631 SEE FLEETCYCLE L/P 9672871 FOR WORK PERFORMED. VERIFIED ACCOMPLISHMENT OF FRAME REPAIR REF ECRA 5310-07631SDR CALA2019061400951Frame · damagedAFT CARGO FRAME STA 727A RBL 15 BETWEEN STR 25 R AND 26 R ELONGATED HOLE WHERE SIDE PANEL ATTACHES. FRAME REPAIRED AS REF ECRA 5310-07631 SEE FLEETCYCLE L/P 9672868 FOR WORK PERFORMED. VERFIED ACCOMPLISHMENT OF FRAME REPAIR REF. EC/RA 5310-07631SDR CALA2019061400950Frame · damagedAFT CARGO FRAME STA 767 RBL 15 BETWEEN STR 25R AND 26R ELONGATED HOLE WHERE SIDE PANEL ATTACHES. FRAME REPAIRED AS REF ECRA 5310-07631 SEE FLEETCYCLE L/P 9672873 FOR ALL WORK PERFORMED. VERIFIED ACOMPLISHMENT OF FRAME REPAIR REF. EC/RA 5310-07631SDR CALA2019061400949Frame · damagedAFT CARGO FRAME STA 727E RBL 15 BETWEEN STR 25R AND 26R ELONGATED HOLE WHERE SIDE PANEL ATTACHES. FRAME REPAIRED AS REF ECRA 5310-07631 SEE FLEETCYCLE L/P 9672872 FOR ALL WORK PERFORMED. VERIFIED ACCOMPLISHMENT OF FRAME REPAIR REF. EC/RA 5310-07631SDR CALA2019061400953Frame · wornAFT CARGO FRAME STA 727B RBL 15 BETWEEN STR 25R AND 26R ELONGATE D HOLE WHERE SIDE PANEL ATTACHES. FRAME REPAIRED AS REF ECRA 5310-07631 REF FLEETCYCLE L/P 9672869 FOR ALL WORK PERFORMED. VERIFIED ACCOMPLISHMENT OF FRAME REPAIR REF ECRA 5310-07631SDR SWAA2022031033343Strap · crackedAFT CARGO DOOR LOWER SILL STRAP CRACKED AT APPROX. BS 840 RBL 22WL 156 / REMOVED AFT CARGO DOOR LOWER SILL STRAP AT APPROX. BS 840 RLB 22 WL 156 IAW SRM 51-40-02-0G-0. LOCATED; DRILLED AND INSTALLED NEW STRAP ITEM 7530562 P.O. #750517 IAW SRM 51-40-05-0G-0. SRSDR R61A2019062830613Frame Splice · crackedJUNCTION OF CENTER FUSELAGE 2 AND 3 PASSENGER CABIN CRACKED AT SPLICE STRINGER 9L AND 10L FR59. STRINGER REPLACED IAW ETD 2019-170-083637.SDR CALA2019061400942Frame · crackedMAIN CABIN UPPER LOBE FUSELAGE FRAME AT STA.400 BETWEEN S-8R AND S-9R HAS CRACK AT I/B FASTENER HOLE FOR AC OUTLET EXTRUSION SUP PORT BRACKET (REPAIR PER W/C SEQ#1655 FIG 3 STEP 9). REMOVED DAMAGED SECTION OF FRAME AND INSTALLED REPAIR CHANNELS P ER EC/RA#5310SDR DALA2019061303542Frame · crackedCRACK ON FRAME, LONG 17LH STA 1037 (CPAX). NRC 00402: FRAME STA 1037 AT LONG 17LH WAS REPAIRED B717-200 SRM 53-20-07-2R-4. (LP #1120245)SDR SIMA201906132003Frame · gougedLH FRAME 60 IS GOUGED NEAR STR 5 LH-C/A-CW WITH REPAIR TO LH FRAME 60 NEAR STR 5L IAW SRM 53-00-04 FIGURE 206.SDR DALA2019061303543Frame Angle · crackedCRACK ON CLIP FRAME LONG 16RH STA 1022 AT FWD FACE OF BULKHEAD (CPAX). NRC 00398: FRAME LONG 16RH STA 1022 AT FWD FACE OF BULKHEAD WAS REPLACED PER B717-200 SRM 51-41-05-0G AND DWG #9912243 REV. JS. (LP #1120252)SDR SIMA20190612001Frame Angle · corrodedFRAME CLIP ON FRAME 65 AT CARGO DOOR SILL CORRODED. -C/A-COMPLIED WITH REPAIR IAW SRM 53-31-04.SDR DALA2019061203520Frame · crackedCRACK ON RING PAN UPPER AFT CORNER STA Y:832 RH SIDE AT PASSENGER CABIN (CPAX). NRC 00242: CRACK ON RING PAN UPPER AFT CORNER STA Y:832 RH SIDE AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 56-20-02 REPAIR 1. (LP #1118572)SDR DALA2019061103517Frame Angle · crackedCRACK ON CLIP FRAME LONG 5LH STA 1022 AT FWD FACE OF BULKHEAD (CPAX). NRC 00393: FRAME CLIP LONG 5LH STA 1022 WAS REPAIRED PER B717-200 SRM 53-00-06-2R-2. (LP #1117079)SDR CA190612005Frame · corroded(CAN) FS310 FRAME BLENDED TO REMOVE SURFACE CORROSION FWD AND AFT SIDES. FWD SIDE BETWEEN STGR 27 AND 26L, AFT SIDE AT STGR 26R. (TC# 20190612005)SDR CA190611007Frame · corroded(CAN) FS319 FRAME BLENDED TO REMOVE SURFACE CORROSION FWD AND AFT SIDES. FWD SIDE BETWEEN STGR 26R AND 26L, AFT SIDE AT STGR 26R. (TC# 20190611007)SDR SWAA2019070334331Frame · dentedFRAME DENTED AT BS. 344, STR. 14R AT FASTENER. REPAIRED FRAME PER ER AND EA.SDR SWIA2019070246019Frame · corrodedFOUND FS349 LOWER FRAME TO BE CORRODED. (C-CHECK) RO: 06/30/2019 REPLACED FS349 LOWER FRAME IAW SRM. LEAK CHECK GOOD.SDR CALA2019061000912Frame · corrodedCORROSION ON AFT CARGO FRAME FWD SIDE AROUND SHEAR TIES, BRACKETS AND STR CLIPS AT STA 1440 BETWEEN STR 28L-29R. R EF ST-ENG N/R 0063844 LIMITS (L=7.0" W=4.0" D=.025) IAW B757-300 SRM 53-00-07 ALLOW. D MG 1 FIG 101 DET II. FABRICATED AND INSTALLED INTERIM REPASDR FDEA2019061361282Frame · dentedMAIN DECK - FUSELAGE MAIN FRAME DEFORMED, AT FR75, BETWEEN STGR10L AND STGR11L REPAIRED THE DEFORMED FRAME(MAIN DECK - FUSELAGE MAIN FRAME, AT FR75, BETWEEN STGR10L AND STGR11L) PER A300-600F SRM53-10-13 FIGURE 202. THIS REPAIR CATEGORY "B". FIRST INSPECTISDR FDEA2019061361284Frame · dentedMAIN DECK - FUSELAGE MAIN FRAME DEFORMED, AT FR59, BETWEEN STGR13L AND STGR14L REPAIRED THE DEFORMED FRAME(MAIN DECK - FUSELAGE MAIN FRAME, AT FR59, BETWEEN STGR13L AND STGR14L) PER A300-600F SRM53-10-13 FIGURE 202. THIS REPAIR CATEGORY "B". FIRST INSPECTISDR FDEA2019061361283Frame · dentedMAIN DECK - FUSELAGE MAIN FRAME DEFORMED, AT FR58, BETWEEN STGR13L AND STGR14L REPAIRED THE DEFORMED FRAME(MAIN DECK - FUSELAGE MAIN FRAME, AT FR58, BETWEEN STGR13L AND STGR14L) PER A300-600F SRM53-10-13 FIGURE 202. THIS REPAIR CATEGORY "B". FIRST INSPECTISDR YENA2019061060316Frame · crackedDURING HEAVY MAINTENANCE, R/H CENTER WING BOX FRAME 36 PRESSURE PANEL ATTACHMENT HOLE B IS CRACKED IN THE TITANIUM ANGLE AT 6:00; REF HAECO SO# 440573 NR# 38548 REPAIRED R/H CENTER WING BOF FRAME 36 PRESSURE PANEL HOLE B AS PER REO#L21985 REF EC A19-336-01 ATSDR IPXA2019061243111Support Bracket · crackedINSPECTION TYPE:124C, FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME STA 38.2 @ LBL 41 BRACKET CRACKED.REMOVED & REPLACED IAW AIRBUS DWG # A25576614000 & A300-600 SRM 51-40-21.SDR CALA2019060700890Frame · crackedAT BS 727D R CRACK NOTED AT I/B RIVET BETWEEN STR 8 AND 9 AT THE AFT OUTLET EXTRUSION SUPPORT ATTACHMENT RT SIDE OF CABIN REF AAR N/R 99836081 ACCOMPLISHED FRAME REPAIR AT STA 727D RT SIDE BETWEEN STR 8 AND 9 AS PER B737 EA 5310-04716 REV I OP001 FIG 3 ADD EMP
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