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 DALA2018072304621Frame · crackedDURING INSPECTION FOUND CRACK ON FRAME STA 440 BTW S-8R TO S-9R AT PAX CABIN. FRAME STA 440 BTW S-8R TO S-9R WAS REPAIRED PER ERA 570034-14AD REV ORIG.SDR DALA2018072304620Frame · crackedDURING INSPECTION FOUND CRACK ON FRAME STA 480 BTW S-8L TO S-9L AT PAX CABIN. FRAME STA 480 BTW S-8L TO S-9L AT PAX CABIN WAS REPAIRED PER ERA 570034-14AD REV ORIGINAL.SDR DALA2018072304619Frame · crackedDURING INSPECTION FOUND CRACK ON FRAME STA 440 BTW S-8L TO S-9L AT PAX CABIN. FRAME STATION 440 BTW S-8L TO S-9L WAS REPAIRED PER ERA 570034-14 AD REV ORIGINAL.SDR DALA2018072304618Frame · crackedDURING INSPECTION FOUND CRACK ON FRAME STA 400 BTW S-8L TO S-9L AT PAX CABIN. FRAME STA 400 BTW S-8L TO S-9L WAS REPAIRED PER ER/A 570034-14 AD REV ORIGINAL.SDR DALA2018072304616Frame · crackedDURING INSPECTION FOUND CRACK ON FRAME STA 500A BTW S-8R TO S-9R AT PAX CABIN. CRACKED ON FRAME STA 500A BTW S-8R TO S-9R AT PAX WAS REPAIRED PER ERA 570034-14AD REV ORIGINAL.SDR DALA2018072204614Frame · crackedDURING INSPECTION FOUND CRACK ON FRAME STA 400 BTW S-8R TO S-9R AT PAX CABIN. FRAME STA 400 BTW S-8R TO S-9R WAS REPAIRED PER ERA 570034-14AD REV ORIG.SDR DALA2018072404663Frame · crackedRT BS 1681 FRAME, CRACK INDICATION IN I/B HOLE OF ABOVE FLOOR INSPECTION AREA PER NDT MANUAL PART 6, 51-00-16 (OPEN HOLE). 5311-01207. REPAIRED REF PRI 570041-14AD REV 0, 1 AND ER/A 570041-14AD REV ORIGINAL.SDR DALA2018072404662Frame · crackedHFEC SHOWS CRACKS AT TWO RIVETS JUST BELOW STRINGER S-14L, STA 1640, FIRST INDICATION ON INSIDE EMANATING FROM UNDER STRAP PROGRESSING FWD TO RADIUS AND THE SECOND INDICATION EXTERNALLY VISIBLE AND END MARKED PROGRESSING AFT FROM RIVET. TOP CRACK APPROX. .375 SDR CALA2018072301666Frame · corrodedCORROSION ON THE RT FRAME 66 AT NUT PLATE HOLE (FLOOR LEVEL). BLENDED CORROSION AT RT FRAME 66 AROUND NUTPLATE HOLE, AT FLOOR LEVEL, FOUND OUT OF LIMITS, FABRICATED A NEW FITTING AND INSTALLED ON DAMAGED AREA IAW SRM 53-41-12-283-001. THICKNESS IS .157" REMOVESDR CALA2018072301665Frame · corrodedCORROSION ON RT FRAME 68 BELOW NUTPLATE AT FLOOR LEVEL. REMOVED CORROSION ON FR 68 RT BELOW NUT PLATE HOLE AT FLOOR LEVEL IAW SRM 53-41-12-283-001. PERFORMED REPAIR AT FR 68 ABOVE STR 23 IAW SRM 53-41-12-300-001 FIG 20101.SDR NACA2018071800060Frame · crackedCRACK ON FRAME 787 BETWEEN S-8L AND S-9L INBOARD FASTENER HOLE. CRACKED FRAME AT STA 787 BETWEEN STR 8L AND 9L REPAIRED IAW SB 53-1216 REV 1 FIG 8.SDR NACA2018071800059Frame · crackedCRACK ON FRAME 727E BETWEEN S-8L AND S-9L INBOARD FASTENER HOLE. CRACKED FRAME STA 727E BETWEEN STR 8 AND STR 9 LT REPAIRED IAW SB737-53-1216-FIG 8 REV 1.SDR NACA2018071800058Frame · crackedCRACK ON FRAME 480 BETWEEN S-8R AND S-9R INBOARD FASTENER HOLE. CRACKED FRAME STA 480 BETWEEN STR 8R AND 9R REPAIRED IAW SB737-53-1216 REV 1 FIGURE 8.SDR NACA2018071800053Frame · corrodedCORROSION FOUND ON FRAME STA 1156 CORRODED AT LB 7 AND APPROX WL 224. CORRODED FRAME AT STA 1156 LBL 7 AND APPROX WL 224 REPAIRED IAW STA 1156 BULKHEAD FRAME CHORD REPAIR DWG R23260 1-053-015-001 REV NC.SDR NACA2018071800051Frame · crackedCRACK FOUND ON THE RT INBOARD CHORD BS 616, BOTTOM FASTENER. CRACKED IB RT CHORD AT BSTA 616 REPAIRED IAW SB 737-53A1254 REV 3 AND REPAIR INSTRUCTION DOC NR CS-26230- 015 DATED 10 JUNE 2013.SDR NACA2018071800050Frame · crackedCRACK FOUND ON THE LT INBOARD CHORD BS 616, BOTTOM FASTENER. REPAIRED LT I/B CHORD BS 616 IAW SB 737- 53A1254 FIG 19 REVISION 3 DTD 13 NOV 2017 WITH NO DEVIATIONS.SDR NACA2018071800030Beltframe · gougedGOUGE/TOOLING DAMAGE ON THE BELT FRAME 887 RIGHT HAND AT UPPER FLANGE AT BS21R. GOUGE/TOOLING DAMAGE ON THE BELT FRAME 887 & 907 RT AT UPPER FLANGE AT STR 21R BOTH FRAMES REPLACED WITH NEW FRAMES IAW REPAIR INSTRUCTIONS DOC NR CS 23260-O/O DATED 9 MAY 2018.SDR NACA2018071800005Frame · cracked2 CRACKS FOUND ON BS 727 CORD AT S18A [LEFT HAND]. REPLACED LT CHORD AT STA 727 FROM STR 18A – L TO STR 27L WITH NEW PART (P/N 65C38494-1) IAW SB 737-53A1166 REV 2 AND DWG 65C37277 REV -.SDR DALA2018071704526Frame · crackedLT 1681 FUSELAGE FRAME ABOVE FLOOR (FASTENER REMOVED) INBD HOLE HAS CRACK INDICATIONS. ACCOMPLISHED ERA 570157-14AD REV ORIGINAL.SDR DALA2019070504083Frame · not reportedSHIP 652 PER ERA 570156-14 SECTION II PERMANENT REPAIR IS REQUIRED ON THE BS 1681 RT FRAME AT THE MAIN DECK FLOOR LEVEL. CORRECTIVE ACTION: COMPLIED WITH PERMANENT REPAIR PER PRI 570156-14 REV 0,PRI 570156-14 REV 1, AND ER/A 570156-14AD REV ORIGINAL. (0650812)SDR SWAA2018073123922Splice Strap · corrodedLOWER INTERNAL FUSELAGE E&E COMPARTMENT BILGE FRAME BUTT SPLICE STRAP CORRODED AT BS 360, BETWEEN BL 0 TO RBL 6. REPAIRED BUTT SPLICE STRAP IAW EA.SDR SWAA2018073123920Frame · corrodedE&E COMPARTMENT STUB FRAME WEB CORRODED AT BS 328+6, BETWEEN STR 19L TO 19R. REPAIRED FRAME IAW EA.SDR AALA20180716009Frame · corrodedTHE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON FRAME CHORD AT STATION 335 STRINGER 23L. REPLACED FRAME CHORD PER EA 281917.SDR AALA20180716011Frame · corrodedTHE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON FRAME CHORD AT STATION 319 STRINGER 23L. REPLACED FRAME CHORD PER EA 281917 DRAFT 2.SDR SWAA2018073123969Frame · corrodedFORWARD OF L1 DOOR CABIN FLOOR AFT SIDE OF FRAME CORRODED AT BS 303.9. REPAIRED FRAME PER EA.SDR DALA2018071404524Frame · crackedDURING HFEC INSPECTION OF FUSELAGE FRAME 1640 LEFT HAD A CRACK INDICATION AT THE INNER CHORD FORWARD BEND RADIUS BETWEEN THE TWO FASTENERS BELOW THE EDGE OF THE INTERCOSTAL STRAP AT STRINGER 14L.SDR DALA2019082004877Frame · not reportedPER ERA 570091-14AD, SECTION II REPAIR IS REQUIRED ON THE BS 1640 RHS FRAME AT L-14F. ACCOMPLISHED REPAIR I.A.W. ERA 570091-14AD REV A SECTION II. (0646068)SDR IPXA2018071331627Frame · crackedINSPECTION TYPE:C, CRACK FOUND APPROX 0.2" LENGTH DURING HFEC INSPECTION ON RT STA 903.5 BL 89 BELOW WL 200 AT FRAME INNER CHORD TRANSITION RADIUS. FRAME INNER CHORD TRANSITION RADIUS AT STA 903 RBL 89 CARRIED OUT REPAIR AS PER EO B767-5310-68072-A APPENDIX B.SDR IPXA2018081322696Frame · crackedFRAME TRANSITION RADIUS FOUND CRACKED FOUND APPROXIMATELY 5/16 INCH IN LENGTH, FOUND DURING HFEC INSPECTION AT BS 883.5, LBL 89, BELOW WL 200. THE FRAME WAS REPAIRED IAW EO B767-5310-69149, APPENDIX B.SDR IPXA2018081232695Frame · crackedA CRACK WAS FOUND APPROXIMATELY 3/8 INCH IN LENGTH IN THE FRAME TRANSITION RADIUS., FOUND DURING HFEC INSPECTION AT BS 903.5, RBL 89, BELOW WL 200. THE FRAME WAS REPAIRED IAW EO B767-5310-69148, APPENDIX B.SDR HYIA20180717002Frame · corrodedWHILE CONDUCTION OTHER MAINTENANCE, AN AREA OF CORROSION WAS NOTED ON THE FUSELAGE FRAME ASSEMBLY AT FS 214.00, JUST ABOVE THE 501110-12 STRIKER PLATE FOR THE LOWER PASSENGER DOOR PIN. THE 501110-12 STRIKER PLATE WAS REMOVED FOR FURTHER INSPECTION. UPON REMOSDR FDEA201807121666Frame · damagedHEAVY GOUGE MARK FOUND ON THE FRAME AT STA 231.25 BL0 DUE TO CONTACT WITH THE FORWARD ACCESS DOOR LATCH PIN. CARRIED OUT FRAME REPAIR IAW SRM 53-00-07-2R REPAIR 7 FIGURE 202 REV124.SDR JGVR20180711002Frame · corrodedBLENDED CORRODED AREAS ON UPPER FRAME IN THE NOSE WHEEL WELL AT FS 77 LOCATED UNDER AND AROUND HYDRAULIC FEED THROUGH FITTINGS, PERFORMED EDDY CURRENT AND ULTRASONIC INSPECTIONS AND REPORTED TO ENGINEERING FOR DISPOSITION. CLEANED, TREATED AND PRIMED BARE METASDR A6WA2018071845931Frame · crackedFRAME 605 ON THE FWD SIDE ABOVE AND BELOW STRINGER 9L CRACKED. REPAIRED FRAME 605 IAW REO 601R-53-61-5214.SDR A6WA2018071345931Frame · crackedFRAME 605 ON THE FWD SIDE ABOVE AND BELOW STRINGER 9L CRACKED. REPAIRED FRAME 605 IAW REO 601R-53-61-5214.SDR SWIA2018073144931Frame · corrodedCORROSION FOUND ON LOWER FRAME SECTOR AT FS310.00 BETWEEN STGR 26L TO STGR 26R. (C-CHECK) RO: 07/29/2018 REMOVED AND REPLACED FRAME SECTOR AT FS310.00 BETWEEN STGR 26L TO STGR 26R IAW REO. PRESSURIZATION LEAK CHECK PASSED.SDR SWIA2018073144915Frame · crackedFRAME FS333 CRACKED LOCATED BETWEEN STR 0 AND STR 1L. (C-CHECK) RO: 07/29/2018. REMOVED AND INSTALLED NEW REPLACEMENT FRAME, P/N: 601R32004-41 AT LT FS 333.00 FRAME FROM STR 0 TO APPROXIMATELY STR 3 IAW SRM. COMPLIED WITH THE PRESSURIZATION OF THE AIRCRAFT IAWSDR SWAA2022022194323Frame · corroded***CORROSION*** ACB BILGE FRAME ON UPR CHORD - STA 947; LBL 8 / REMOVED CORROSION 6' X 1' X .002' FROM .063' FROM BS 947 FRAME UPPER CHORD AT LBL 8 AND REFINISHED AREA ALL IAW ER 18-03418 REV IR AND EA 1-753-33032 REV IRSDR FOTR2018080800001Frame · crackedFORWARD CARGO BAY, BS 500B FRAME WAS CRACKED AT THE INBD SIDE OF WIRE PENETRATION HOLE.SDR SWAA2018073123963Frame Splice · corrodedAFT CARGO BAY FLOOR STRUCTURE FRAME SPLICE CORRODED AT BS 787, BETWEEN STR 24R TO STR 25R. R&R SPLICE PER SRM AND DWG.SDR V0XD20180707001Frame · corrodedFRAME SECTION AT FS 319.00 SHOWS SIGNS OF CORROSION AT STR 21L. REMOVED AND REPLACED FRAME SECTION AT FS 319.00 AND STR 21L IAW SRM 51-42-06, 51-40-11, 53-21-23, 51-25-16, 51-21-11SDR DALA2018070604413Frame · dentedDURING INSPECTION FOUND DENT ON FRAME STA 747 AND S-23L AT AFT CARGO COMPARTMENT. FRAME WAS REPAIRED PER ETI 37-18-414 REV 1 AND ERA NO 569883-14 REV ORIGINAL.SDR DALA2018070604412Frame · dentedDURING INSPECTION FOUND DENT ON FRAME STA 727J AND S-24L AT AFT CARGO COMPARTMENT. FRAME WAS REPAIRED PER ETI-37-18-416 REV 1 AND ERA NO 569856-14 REV ORIGINAL.SDR DALA2018070604411Frame · dentedDURING INSPECTION FOUND DENT ON FRAME STA 727H BTW S-23L TO S-22L AT AFT CARGO COMPARTMENT. FRAME WAS REPAIRED PER ETI-37-18-415 REV 1 AND ERA NO 569899-14 REV ORIGINAL.SDR SWAA2022022100532Frame · corroded***CORROSION*** ACB STA 947 FRAME HAS CORROSION AT LBL 9 / REMOVED CORROSION ON ACB BS 947 FRAME LBL 9; 5' X 1.2'; .005' MAX DEPTH; ORIGINAL THICKNESS .063'. OUT OF LIMITS PER SRM 53-00-07; ALLOWABLE DAMAGE 1; FIG 102; DETAIL C. REWORKED AREA PER ER 18-03331 RSDR SWIA2018081044985Frame · corrodedBS 605 FRAME HAD CORROSION. REPAIRED THE FRAME IAW REO.SDR DALA2018070904434Frame · crackedRIGHT HAND AFT 1640 FRAME, 2 ADDITIONAL CRACK INDICATIONS BELOW S-14. FIRST HOLE INDICATION 2.250 INCHES BELOW S-14 AND 4.500 INCHES BELOW S-14. REPAIRED REF PRI 569586-14AD REV 0,1,2,3. AND FINAL ER/A 569586-14AD REV ORIGINAL.SDR DALA2018070904433Frame · crackedDURING OPEN UP OF 5311-01218-01B RT FRAME 1640, FOUND FRAME CRACKED AT S-14R. REPAIRED REF PRI 569586-14AD REV 0,1,2,3. AND FINAL ER/A 569586-14AD REV ORIGINAL.SDR DALA2018070904432Strap · crackedRT FRAME 1640, INNER CHORD STRAP CRACKED AT S-14R. REPAIRED REF PRI 569586-14AD REV 0,1,2,3. AND FINAL ER/A. 569586-14AD REV ORIGINAL.SDR DALA2018070404404Frame · crackedRT FRAME 1640, INNER CHORD CRACKED 2" BELOW S-14R. REPAIRED REF PRI 569586-14AD REV 0,1,2,3. AND FINAL ER/A 569586-14AD REV ORIGINAL.
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