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 FDEA2019101762672Frame · corrodedFORWARD CARGO COMPARTMENT - CORROSION ON UPPER FLANGE OF FRAME AT BS 700 RBL1 COMPLIED WITH FEDEX EA # F-5310-T0349986 P1. FUSELAGE - MAINFRAME - STA 700 FRAME REPAIR BETWEEN STRINGERS S-28R AND S-28LSDR FDEA2019101762662Frame · damagedMAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 24 LEFT , EXISTING REPAIR OUTER ANGLE FOUND DAMAGED . MAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 24 LEFT , EXISTING DAMAGED OUTER REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PERSDR DALA2019101705967Frame · crackedA CRACK INDICATION ON FRAME 20 LH SIDE, LOWER INBOARD HOLE, DOOR STOP FITTING 1 AREA AT FWD GALLEY AREA (1 EA) (CRACK DIRECTION IS 6 O' CLOCK LOOKING AFT). REPAIRED HOLES LOC. FRAME 20 LH AT LEVEL DOOR STOP 1 FWD GALLEY AREA AS PER ER/A 581713-14AD REV.ORIGINASDR DALA2019101765959Frame · crackedDURING INSPECTION, FOUND CRACKED FRAME ON STATION 400 BTW S-8R AND S-9R AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. FRAME WAS REPAIRED PER. ERA 582022-14AD REV. ORIGINAL.SDR DALA2019101765958Frame · crackedDURING INSPECTION FOUND CRACKED FRAME ON STA 727B BTW S-8R AND S-9R AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. FRAME WAS REPAIRED PER. ERA 582022-14AD REV. ORIGINAL.SDR SWAA2022040605565Frame · crackedREF LOG PAGE 1102696 LEFT HAND PICKLEFORK CRACKED AT STA 663 / THE LH PICKLE FORK FRAME P/N 144A2410-7 WAS REMOVED AND REPLACED BY BOEING AOG UNDER AGREEMENT SWA-RE-1906934 IN VCV. REF. SWA EA 1-753-35957 REV IR FOR DETAILS OF THE BOEING AOG VISIT AND FOR DOCUSDR SWAA2022040605564Frame · crackedLEFT HAND PICKLE IS CRACKED AT STA 663. / THE LH PICKLE FORK FRAME P/N 144A2410-7 WAS REMOVED AND REPLACED BY BOEING AOG UNDER AGREEMENT SWA-RE-1906934 IN VCV. REF. SWA EA 1-753-35957 REV IR FOR DETAILS OF THE BOEING AOG VISIT AND FOR DOCUMENTATION OF ASSOCIATSDR SWAA2022040650882Frame · corroded***CORROSION*** ON ACB FRAME STA 887 WL 162 LBL10 TO RBL 22 / REMOVED CORROSION ON AFT CARGO BAY FRAME B.S.887 LBL10-RBL22 WL162. REPAIRED PER ER# 19-05335 REV IR AND SWA EA 1-753-35877 REV IRSDR REXA2019111851593Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 319 BETWEEN STRG 25 LH TO 27 AT MAIN AVIONIC COMPARTMENT. (E/E)(TCI:53-20-304.
SUMMARY:CORROSION ON FRAME IN STA. FS= 319 BETWEEN STRG 25 LH TO 27 AT MAIN AVIONIC COMPARTMENT. FRAME WAS MEASURED AND FOUND WITSDR REXA2019111851592Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 295 BETWEEN STRG 25 LH TO 26RH AT MAIN AVIONIC COMPARTMENT. (E/E)(TCI:53-20-304).
SUMMARY: CORROSION ON FRAME IN STA. FS= 295 BETWEEN STRG 25LH TO 26RH WAS REMOVED PER CRJ900 SRM 51-21-06.FRAME WAS MEASURED ASDR SWAA2019111138734Frame · crackedFRAME WEB CRACKED AT BS. 259, STR. 9L AT STRINGER CUTOUT. / REPAIRED FRAME WEB PER ER AND EA.SDR SWAA2019110138461Frame · corrodedAFT CARGO BAY FRAME AROUND POTABLE WATER TANK MOUNT CORRODED AT BS. 947, LBL 11. / REPAIRED FRAME IAW ATS ER AND EA.SDR REXA2019102451494Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME FS295 BTW. STGR.26L AND 26R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09).
SUMMARY:ON NRC. 00163 CORROSION LEVEL 1 ON FRAME FS295 BTW. STGR.26L AND 26R AT MAIN AVIONICS COSDR DALA2019101505900Frame · corrodedFRAME CORRODED OUT OF LIMITS, BS 1022, LONGERON 27L TO 27R . THE FRAME 2 WAS REPAIRED PER SRM 53-20-07-2R-3.SDR SWAA2022040663860Frame · crackedL/H PICKLE FORK FITTING AND FAIL - SAFE STRAP ARE CRACKED AT THE LOWER AFT FASTENER AND CRACK EXTENDS PAST THE FASTENER; LOCATED AT BS 663 / THE LH PICKLE FORK FRAME P/N 144A2410-7 & FAIL SAFE STRAP P/N 144A2412-1 WAS REMOVED AND REPLACED BY BOEING AOG UNDER ASDR SWAA2022040663859Frame · crackedR/H PICKLE FORK IS CRACKED AT THE LOWER AFT FASTENER CRACK DOES NOT EXTEND PAST THE FASTENER; LOCATED AT BS 663 / THE RH PICKLE FORK FRAME P/N 144A2410-8 & FAIL SAFE STRAP P/N 144A2412-2 WAS REMOVED AND REPLACED BY BOEING AOG UNDER AGREEMENT SWA-RE-1906934 IN SDR REXA2019102341537Frame · corroded"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON FRAME FS= 333 BETWEEN STRG 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 SDR DALA2019101505899Frame · crackedFRAME CRACKED. STA 674 RH. CONDITION 3. (REF STEP 7). REPLACED FRAME ON AMDS WORK CARD 5310-01436-03B.SDR R61A201911071206Frame · corrodedMAJOR: CORROSION-FWD WET AREA FR17 RH SIDE AS MARKED. CUTOUT CORRODED AREA REF EMB SRM 53-00-10 REPAIR 03, AND INSTALLED FABRICATED FILLER AND INNER DOUBLER REF EMB SRM 51-40-08 FR PN: 170-21769-403. SEE EAMS W/O H6997 SN 178 FOR WORK DETAILS. AIRCRAFT REMASDR SWAA2019110138459Strap · corrodedFORWARD CARGO DOORWAY, FORWARD FRAME STRAP CORRODED ON INBOARD FLANGE AT BS. 440, BETWEEN RBL 28 TO RBL 30. / REPAIRED STRAP IAW EA AND ER.SDR REXA2019102431499Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME FS319.70 BTW STGR 26L AND 26R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09).
SUMMARY OF NRC 00172: CORROSION LEVEL-1 ON FRAME FS319.70 BTW STGR 26L AND 26R AT MAIN AVIONISDR REXA2019101301498Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME FS333 BTW. STGR 26L AND 25R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIXA]. (E/E)(TCI 100-09).
SUMMARY: CORROSION LEVEL 1 ON FRAME FS333 BTW. STGR 26L AND 25R AT MAIN AVIONICS COMPARTMENT WAS RSDR REXA2019102431496Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME FS310 BTW. STGR.26L AND 25R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIXA].(E/E)(TCI 100-09).
CORROSION LEVEL 1 ON FRAME FS310 BTW. STGR.26L AND 25R AT MAIN AVIONICS COMPARTMENT WAS REMOVED PERSDR CALA2019101401753Frame · dentedDENT ON FWD CARGO RH FRAME UPPER FLANGE AT STA 660 BETWEEN STR 23R-24R REF ST ENG N/R 0074716 CHECKED LIMITS TO DENT ON FWD CARGO RH FRAME UPPER FLANGE AT STA 660 BETWEEN S-23R AND S-24R; L=1.2", W=.80", D=.050", OUT OF LIMITS IAW B757-200 SRM 53-00-07 FIG 101SDR CALA2019101401752Frame · dentedDENT ON FWD CARGO LH FRAME UPPER FLANGE AT STA 660 ABOVE STR 23L . RF ST ENG 0074714 CHECKED LIMITS TO DENT ON FWD CARGO LH FRAME UPPER FLANGE AT STA 660, S-23L; L=1.0", W=.80", D=.017". OUT OF LIMITS IAW 757-200 SRM 53-00-07 REPAIR, FIG 201, PG 201. REPAIR ISSDR CALA2019101401751Frame · dentedB757-06-3-0230 DENT ON FWD CARGO RH FRAME UPPER FLANGE AT STA 780 ABOVE STR 24R. REF ST ENG N/R 0074715 CHECKED LIMITS TO DENT ON FWD CARGO RH FRAME UPPER FLANGE AT STA 780 ABOVE 5-24R; L=1.0", W=.90", D=.055". OUT OF LIMITS IAW SRM 53-00-07 FIG 101. REPAIRED SDR REXA2019102411502Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME FS349 BTW. STGR. 26L AND 25R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09).
SUMMARY: ON NRC. 00175, CORROSION LEVEL 1, FRAME FS349 BTW. STGR. 26L AND 25R AT MAIN AVIONICS COSDR DALA2019101525924Frame · crackedCRACK IN FRAME BS 1640 UNDER STRAP AT STRINGER 14L. UNABLE TO DETERMINE LENGTH. REPAIR MUST BE COMPLETED PRIOR TO FURTHER FLIGHT. COMPLIED WITH ER/A 581573-14AD REV ORIGINAL.SDR DALA2019101525923Frame · crackedDURING ACCOMPLISHMENT OF OPEN HOLE EDDY CURRENT PER AA5311-01207-01B STEP 13, FOUND INBOARD HOLE HAS CRACK INDICATION AT APPROXIMATELY 3 O'CLOCK POSITION AS VIEWED FROM REAR. INDICATION IS IN THE STA 1681 FRAME, NOT THE CLIP ON AFT SIDE OF FRAME. CANNOT DETERMSDR DALA2019101205868Frame Angle · corrodedCORROSION FRAME CLIP STA. Y=908 BTW L= 29R/28L, Y=927 BTW L= 29R/29L, Y=954 BTW L= 29L/28R, Y=974 BTW L= 29R/26L AND Y=1002 BTW L= 29L/29R AT AFT CARGO COMPARTMENT. (CORROSION LEVEL 2): FRAME CLIPS STA Y= 974 AND 1002 WERE REPLACED PER B717-200 SRM 51-41-02-0GSDR DALA2019101205866Frame · crackedCRACK ON FRAME STA Y= 1178.225 CANT BTW PROJECTION LONGERON 17 AND 16 RH AT AFT ACCESSORY COMPARTMENT. DOUBLER ON FRAME STA Y=1178.225 CANT BTW PROJECTION LONGERON 17 AND 16 RH AT AFT ACCESSORY COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G AND DWG SR95SDR EE4Y201910119892Frame · damagedUPPER CARGO CABIN AT BS 907 STR 17R LEVEL FRAME NOTCH WITH HOLE ENLONGATE.WAS REPAIRED PER AERONAUTICAL ENGINEERS EO9670 REV P2,REPAIR INSTRUCTIONS (REF:JOB:A1H217 ITEM 2-40)SDR DU4R20191011031Frame · crackedDURING SCHEDULED INSPECTION, FOUND R1 DOOR FR16 HOLE 5 HAS A CRACK INDICATION.SDR DU4R201910110032Frame · crackedDURING SCHEDULED INSPECTION, FOUND R-1 DOOR FR16 HOLE D HAS A CRACK INDICATION NR 193074 32246SDR DALA2021072104110Frame · crackedSHIP 3233 WHILE ACCOMPLISHING ALI 531153-02-1 (JIC 5311-2036), CRACKS WERE FOUND IN FR16 RHS IN HOLES #6,#C,#D,AND #F. CORRECTIVE ACTION: PERFORMED INSPECTION AS PER ER/A 580975-14AD REV.ORIGINAL. OK TO CONTINUE TO MONITOR. JOB COMPLETE. (1309622)SDR HNAA2019111400356Frame · crackedFRAME 81 LWR HALF HAS A CRACK....FIX: R&RD FRAME 81 LWR HALF IAW EMB 145 SRM 51-40-02. NOTE: A/C IN HVY CHK (ABI)SDR DALA2019101415879Frame · dentedDENT ON FRAME STA 560 BTW STRINGERS S24L AND S25L, AT FWD CARGO COMPARTMENT. FRAME AT STA 560 BTW STRINGERS S24L AND S25L, AT FWD CARGO COMPARTMENT WAS REPAIRED PER ETI-57-19-122 REV. 5 AND E/RA 582075-14AD. REV. ORIGINAL.SDR DALA2019101105830Frame · crackedCRACK ON FRAME STA 1037 AND LONGERON 17L (CPAX) (SM). NRC 00529: FRAME STA 1037 AND LONGERON 17L WAS REPAIRED PER ER/A 581846-14 REV. ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-581846 ADDED FOR AC 9506. (LP #1309535)SDR SWIA2019101046453Stringer Splice · corrodedFS477 STRINGER 19 RH SPLICE ANGLE CORRODED. (C-CHECK) N817SK RO: 10/9/2019INSTALLED NEW SPLICE ANGLE IAW SRM. LEAK CHECK GOOD.SDR SWIA2019101046435Frame Splice · corrodedFS319.70 FRAME SPLICE IS CORRODED AT STR21L. (C-CHECK) N817SK RO: 10/9/2019REMOVED AND INSTALLED NEW L/H FRAME/SPLICE SECTOR AT FS319.70 FROM STR17L TO STR21L IAW SRM.SDR AALA201910159028Frame · damagedAIRCRAFT IN BASE MAINTENANCE: BAFFLE CLIP ATTACHMENT POINT ON FRAME HAS ELONGATED HOLE AT BS 500H AND S25L. REPAIRED FRAME PER EA 299052.SDR IPXA2019101197724Frame · damagedINSPECTION TYPE:12YR, FRAME 47 FASTNER HOLE Q WAS OVERSIZED, LT SIDE. REPAIRED THE FRAME IAW EO A300-5710-74239-A & EA 300-5710-01-A7909. (MINOR REPAIR)SDR RAIA2019101090001Frame · crackedFRAME 75 IS CRACKED BETWEEN STR 1 AND STR 2 R/H SIDE. REPAIRED FR 75 CRACKED BETWEEN STR 1 & 2 RH.SDR IPXA2019100947709Frame · gougedFRAME 47 WAS GOUGED ON THE SPLICE AND ON THE FRAME BETWEEN STRINGERS 24 & 26L. ACCOMPLISHED A REPAIR ON THE FRAME IAW EO A300-5310-74222-A & EA 300-5310-01-A7910.SDR DALA2019100905793Frame · crackedFOUND ONE CRACK AT FWD OUTER CHORD AT S-7R STA1809, LENGTH IS 5MM,AS REMARKED. PERFORMED THE REPAIR CRACK FWD OUTER CHORD AT S-7R STA1809 IAW W/C 5310-01380-06 AND B767-400 SRM 53-80-08 REPAIR 9,REV.58 09/05/2019.PLS DO A SUPPLEMENTAL INSPECTION AS PER B767-40SDR SWAA2019110638644Frame · dentedDENT ON THE FRAME AT AFT CARGO BAY BS 727C 3" ABOVE S-22R WL173. / REPAIRED PER: EA 1-753-35959 REV IR AND ATS ER 19-05297 REV IR.SDR REXA2019102381536Frame · corroded"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON FRAME FS= 319 BETWEEN STRG 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 SDR DALA2019100905786Frame · crackedCRACK WITH 0.125 IN OF LENGTH WAS FOUND ON OVERWING FRAME AT STA Y=674.000 RH. OVERWING FRAME AT STA Y=674.000 RH WAS REPLACED PER B717-200 CARD 5310-01436-03B. (LP #1306202)SDR A6WA2019100846909Frame · corrodedFS 605 FRAME BETWEEN STR 25R AND STR 25L HAS HEAVY CORROSION WITH EXFOLIATION REMOVED AND REPLACED FRAME SECTION AND REINFOREMENT ANGLE IAW SRM 51-42-06 AND 51-42-21SDR A6WA2019100846908Frame · corrodedFS 605 FRAME BETWEEN STR 25R AND STR 25L HEAVY CORROSION WITH EXFOLIATION REMOVED AND REPLACED FRAME SECTION AND REINFORCEMENT ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21
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