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 DALA2019050202781Frame · crackedCRACK INDICATION IN OPEN HOLE LOWER INBOARD FRAME 16 RT SIDE AT LEVEL DOOR STOP FITTING 7 (INTERCOSTAL AREA). PERFORMED PERMANENT REPAIR LOC OPEN HOLE LOWER INBOARD FRAME 16 RT SIDE AT LEVEL DOOR STOP FITTING NR 7 (INTERCOSTAL AREA) AS PER PRI 577190-14 REV 0 SDR DALA2019050202780Frame · crackedCRACK INDICATION IN OPEN HOLE LOWER INBOARD FRAME 16 LT SIDE AT LEVEL DOOR STOP FITTING 7 (INTERCOSTAL AREA). PERFORMED PERMANENT REPAIR LOC OPEN HOLE LOWER I/B FRAME 16 LT SIDE AT LEVEL DOOR STOP FITTING 7 AS PER PRI 577188-14 REV O AND ER/A 577188-14AD.SDR NACA2019070800064Frame · dentedDISCREPANCY: STA 460 RT STR 17-16R DENT ON FRAME. CORRECTIVE ACTION: STA 460 RT STR 17-16R DENT ON FRAME REPAIRED BY REPLACING FRAME WITH MADE REPAIR PART IAW DWG #65-46532 REV 13 SRM REV 119 51-30-01 AND 51-40-02 PARA 4,7.SDR NACA2019070800068Beltframe · damagedDISCREPANCY: BS986 BELTFRAME RIGHT HAND SIDE @ S17R FLOORBEAM TO BELTFRAME ATTACH FASTENER HOLES DAMAGED. CORRECTIVE ACTION: STA 986 BELTFRAME RT SIDE @ STR 17R WITH DAMAGED FLOORBEAM TO BELTFRAME ATTACH FASTENER HOLES, REPLACED IAW DWG #65-46564 REV B. NEW BESDR SWAA2019052833080Frame · crackedFRAME CRACKED AT BS. 312, STR. 5L, ABOVE UPPER SILL WEB. REPAIRED FRAME PER EA & ER.SDR SWIA2019052445922Frame · crackedRT FS220 FRAME HAS A CRACK INDICATION AT FASTENER HOLE I/B OF LIGHTING HOLE JUST BELOW STG 13A (RT) 0.500" LONG. (202-MOD) RO: 05/23/2019 REMOVED DAMAGED UPPER FRAME SECTOR AND INSTALLED A NEW SERVICABLE RT FS 220 UPPER FRAME SECTOR P/N CC670-34146-6 IAW SRM.SDR REXA2019042900582Frame · corroded[IN REFERENCE NRC 88] INITIAL INSPECTION: CORROSION ON FRAME , FS333 BETWEEN STR 27 TO STR 26R. (E/E) (TCI: 100-09, 09E4, 09E5)
SUMMARY: LEVEL CORROSION 2; FRAME AT FS333 BETWEEN STR 27 TO STR 26R WAS REPAIRED PER SRM 53-00-06-201-004-A01, FIG. 53-00-06-995-8SDR REXA2019042900580Frame · corroded[IN REFERENCE NRC 88] INITIAL INSPECTION: CORROSION ON FRAME FS 349 BETWEEN STR 26L TO STR 26R. (E/E) (TCI: 100-09, 09E4, 09E5)
SUMMARY: LEVEL CORROSION 2; FRAME FS 349 BETWEEN STR 26L TO STR 26R WAS REPAIRED PER SRM 53-00-06-201-004-A01, FIG. 53-00-06-995-80SDR DALA2019043002801Frame · damagedSHIP 6801 BS 700, STR22L, FWD CARGO PIT, LBL 45.73, FRAME IS DAMAGED BEHIND NUT PLATE. STREAMER ATTACHED, DOT#2, I-104. CORRECTIVE ACTION: REPAIRED FWD CARGO BS 700 DAMAGE FRAME AT STR 22L BY CUTTING DAMAGE AREA AND INSTALL REPAIR DOUBLER IAW SRM. (1051824)SDR LR7A2019042901520Frame · corrodedDURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5312, FOUND THE RT FS450 RING SEGMENT LOWER END CORRODED AT WL143, RBL63. REPAIRED IAW SRM, FIG. XX-YYY-ZZ. NR# 2140. / PSE# 53-40-08, AD 2012-06-09.SDR LR7A2019042901509Frame · damagedDURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5312, FOUND THE LT FS241 RING SEGMENT LOWER WEB WITH DAMAGED SCREW HOLES AT WL150, LBL66. REPAIRED IAW SRM, FIG. 51-140-19. NR# 2099.SDR LR7A2019042901508Frame · crackedDURING SCHEDULED C-13 CHECK UNDER JOB CARD HC3215, FOUND THE NOSE WHEEL WELL LT FS140 FRAME FLANGE CRACKED AT RIVET HOLES AT LBL44, WL152. REPAIRED IAW SRM, FIG. 51-140-19. NR# 2073.SDR LR7A2019042901502Frame · crackedDURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS781 RING SEGMENT CRACKED IN THE BEND RADIUS AT WL270, LBL61. REPAIRED IAW SRM, FIG. 53-50-07. NR 2040. / PSE# 53-50-05, AD 2012-06-09.SDR DALA2019043002733Frame · crackedCRACK INDICATION ON FRAME 16 RH SIDE AT DOOR STOP 1 LOWER INBD HOLE AT FWD GALLEY AREA (1 EA) (AT 9 OCLOCK ). PERFORMED REPAIR INSTRUCTIONS ON FRAME 16RH SIDE AT DOOR STOP 1 LOWER INBD HOLE AT FWD GALLEY AREA AS PER PRI 577136-14 REV.0 PRI 577136-14. REV.1 PRISDR DALA2019043002732Frame · crackedCRACK INDICATION ON FRAME 16 RH SIDE AT DOOR STOP 7 LOWER INBD HOLE AT FWD GALLEY AREA (1 EA) (AT 6 OCLOCK ). PERFORMED REPAIR INSTRUCTIONS ON FRAME 16RH SIDE DOOR STOP 7 UPPER AT FWD GALLEY AREA AS PER PRI 577136-14 REV. 0 PRI 577136- 14 REV 9. PRI 577136-14 SDR DALA2019043002731Frame · crackedCRACK INDICATION ON FRAME 16 RH SIDE DOOR STOP 7 UPPER INBD HOLE AT FWD GALLEY AREA (1 EA) (AT 6 OCLOCK ). PERFORMED REPAIR INSTRUCTIONS ON FRAME 16RH SIDE DOOR STOP 7 UPPER AT FWD GALLEY AREA AS PER PRI 577136-14 REV.0 PRI 577136- 14 REV 1. PRI 577136-14 REV.SDR CA190430004Frame · corroded(CAN) CUSTOMER REPORTS 3 AREAS OF BLENDED CORROSION DAMAGE TO LOWER FRAME SECTORS AT FS 942.00 AND FS 969.00 (TC# 20190430004)SDR SWIA2019052445920Frame · crackedFS 235 RT UPPER FRAME SECTOR HAS A VISUAL CRACK. (202-MOD) RO: 05/23/2019) NEW SERVICABLE RT UPPER FRAME SECTOR WAS INSTALLED IAW SRM.SDR DALA2019042902697Frame · crackedCRACK INDICATION ON FRAME 20 RH SIDE, HOLE A, AT LEVEL DOOR STOP 7, CR ACK DIRECTION 4 O'CLOCK AT FWD GALLEY AREA (1 EA). PERFORMED PERMANENT REPAIR INSTRCTION ON FR 20 R/H SIDE HOLE"A" AT LEVEL OF DOOR STOP 7 AS PER ER/A #577036-14AD.SDR CA190429007Frame · corroded(CAN) FS581 FRAME CORROSION BLENDS BTW STR17L - STR18L ORIGINAL MAT. THK. OF THIS FRAME IS .063 LOWEST REM. MAT. THK.AT ATTACH FLANGE IS .051 LOWEST REM. MAT. THK.AT WEB FLANGE IS .061 (TC# 20190429007)SDR DALA2019042972708Frame · crackedCRACK FRAME 36 FOUND AT HOLE B, PERFORMED TIME LIMITED REPAIR LOC AT LEVEL FR 36 IN FWD CARGO COMPARTMENT AS PER ER/A 577359-14AD REV ORIGINAL AA5311-01171 SB A320 53, AD-2018-06-04SDR DALA2019042702672Frame · crackedCRACK INDICATION ON FRAME 16 RH SIDE, HOLE 6, AT LEVEL DOOR STOP 7, CR ACK DIRECTION 2 O'CLOCK. AT FWD GALLEY AREA (1 EA). PERFORMED SECTION I AS PERMANENT REPAIR LOCATED ON FR 16R/H SIDE HOLE 6 AT LEVEL DOOR STOP 7 AS PER PRI 577038-14 AND ER/A 577038-14AD .SDR C77A202002260028Frame Splice · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTURE: P/N 170-86101-001 LH UPPER SHEET, P/N 170-86101-001 RH UPPER SHEET, P/N 170-86181-005 RH PANEL SUSDR DALA2019042802771Repair · gougedSHIP 6801 MAIN CABIN @ BS1280 EXISTING REPAIR HAS A GOUGE BEWTEEN S9L AND S14L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON FRAME STA 1280 STR 10L TO STR 15L IAW ER/A# 513680-14AD REV B SECTION II PERMANENT REPAIR. (1048926)SDR DALA201904302757Frame · corrodedSHIP 5806 AFT CARGO CORROSION - LOCATED AT FRAME 1360 BELOW FAIL SAFE CHORD FROM 28L - 28R. CORRECTIVE ACTION: AREAS BETWEEN STR. 28L AND 29L, 29R AND 28R, 29R AND 30, ARE WITHIN LIMITS PER B757 SRM. PRI 577528-14 ADDRESSING FRAM WEB 1360/S-29R-S-30R. 28L TO 2SDR DALA2019042762669Frame · crackedCRACK INDICATION ON FRAME 16 LH SIDE LOCATED AT DOOR STOP 7 UPPER INBD HOLE AT FWD GALLEY AREA (1 EA) (AT 4 OCLOCK). PERFORMED SECTION I AS REPAIR INSTRUCTION LOCATED ON FRAME 16L/H SIDE AT DOOR STOP 7 UPPER INBOARD HOLE AT FWD GALLEY AREA AS PER PRI 577135-14SDR DALA2019042762668Frame · crackedCRACK INDICATION ON FRAME 16 LH SIDE LOCATED DOOR STOP 7 LOWER INBD HO LE AT FWD GALLEY AREA (1 EA) (AT 3 OCLOK ). PERFORMED SECTION I AS PER REPAIR INSTRUCTION LOCATED ON FRAME 16L/H SIDE AT DOOR STEP 7 UPPER INBOARD HOLE AT FWD GALLEY AREA AS PER PRI 577135-SDR REXA2019042500691Frame · crackedFRAME 605 IS CRACKED JUST BELOW STGR 9L, IN THE CARGO BAY. REPAIRED FRAME 605 IAW REO 601R-53-61-5214 REV A.SDR DALA2019042602656Frame · crackedUPPER CANTED FRAME CRACKED AT 12 OCLOCK POSITION. REMOVED UPPER CTR FRAME ASSY. DRILLED UP REPLACEMENT FRAME PER MD88 DRAWING 5966768Y1. 301936. REINSTALLED UPPER CTR FRAME ASSY PER MD88 DRAWING 5966768Y1.SDR CA190424002Frame Angle · corroded(CAN) DURING MAINTENANCE INSPECTION LEVEL 2 CORROSION WAS OBSERVED ON THE AFT FACE OF FRAME FS295, BETWEEN STRINGERS 26L AND 25R. FRAME SECTION REPLACED IAW THE MANUFACTURER`S SRM. (PN SH670-31353-1) (TC# 20190424002)SDR SWIA2019050645826Frame · crackedONE CRACK INDICATION NOTED ON RT FS220 FRAME AT I/B SIDE OF FASTENER HOLE I/B OF LIGHTING HOLE BELOW STGR13R 0.200" LONG. (C-CHECK) RO: 05/04/2019 REMOVED AND INSTALLED SERVICABLE RT FS 220 UPPER FRAME SECTOR IAW SRM.SDR SIMA2019043022005Frame · crackedFO'S SIDE UPPER FRAME #10 HAS APPROX. A 2" CRACK.-C/A-RE-EVALUATED AND FOUND UPPER FRAME 10 SEGMENT P/N 145-02409-002 TO FIT TH U-CHANNEL SPLICE PROPERLY. INSTALLED THE NEW FRAME 10 UPPER SEGMENT IAW SRM 51-40-02.SDR SIMA201904292003Frame · crackedPILOTS SIDE UPPER FRAME #10 HAS APPROX. A 2" CRACK. -C/A-INSTALLED NEW LH FRAME 10 SECTION IAW SRM 51-40-02.SDR REXA201904260505Frame · corrodedCORROSION ON FRAME FS:310 BTW STGR 24LH AND 24RH AT MAIN AVIONICS COMPARTMENT. CORROSION LEVEL 2: FRAME STA. FS=310 BTW STGR 24LH AND 24RH AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ-900 EA NO. CRJ953-08650 REV. IRSDR SWIA2019050645825Frame · crackedLT FS 235 UPPER FRAME SECTOR HAS VISUAL CRACK. (C-CHECK) RO: 05/04/2019 REMOVED AND INSTALLED SERVICABLE LT FS 235 UPPER FRAME SECTOR IAW SRM.SDR DALA2019042622658Frame · corrodedCORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND FRAME WEB SURFACE CORROSIONAT STA1197+66. S-38L TO S-37R. AND S-33R TO S-34R. REPLACED WEB. (LP 1039818)SDR SIMA201904221001Frame · crackedFRAME 10 CRACKED RH SIDE BELOW COPILOT?S DV WINDOW-C/A-REMOVED AND REPLACED RH FRAME 10 IAW EMB 145 SRM 51-40-02SDR CA190425026Frame · corroded(CAN) FRAME AT FS319 BLENDED TO REMOVE CORROSION BETWEEN STGR 25L AND 26L. (TC# 20190425026)SDR REXA201904260506Frame · corrodedCORROSION ON FRAME STA FS:295 BTW STGR 24LH AND 24RH AT MAIN AVIONICS COMPARTMENT (E/E) (TCI 100-09)
SUMMARY OF NRC 00135: CORROSION LEVEL 2 ON FRAME STA FS:295 BTW STGR 24LH AND 24RH AT MAIN AVIONICS COMPARTMENT (E/E) WAS REPAIRED PER EA NO: CRJ953-08649 REVSDR DALA2019042312582Frame · crackedINITIAL INSPECTION:CRACK ON FRAME WEB AT STA 1542 CANT AND 10:00 -11:00 O'CLOCK POSITION, AFT ACCESORY COMPT. FRAME WEB WAS REPAIRED PER ETI-90-19-023 REV.4 AND ER/A 577494-14 REV. ORIGINAL ASSOCIATED ER/A 14-577494 ADDED FOR AC 9234. (LP# 1039346)SDR CA190425025Frame · corroded(CAN) FS589 FRAME BLENDED TO REMOVE SURFACE CORROSION IN A SMALL AREA ABOVE STGR 19L. (TC# 20190425025)SDR SWAA2019050832434Frame · crackedFRAME CRACKED AT BS. 727A, STR. 8R. REPAIRED FRAME PER EA.SDR SWAA2019050832433Frame · crackedFRAME CRACKED AT BS. 787, STR. 8R. REPAIRED FRAME PER EA.SDR FDEA2019042290856Frame · dentedMAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR DENTED AT RIGHT HAND STATION 1661, LONGERON 12 RIGHT CABIN - MAIN DECK CARGO COMPARTMENT AT RIGHT HAND FRAME STATION 1661 LONGERON 12 RIGHT , EXISTING DENTED REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G SDR R61A201905010459Frame · damaged***WHILE AIRCRAFT WAS IN FOR BRIDGING*** MAINTENANCE FOUND DURING FASTENER REMOVAL, DAMAGES ON LOWER FR 17, STR 27L TO 27R, IN THE RADIUS AND BY THE LOWEST FASTENER. REMOVED AND REPLACED DAMAGED LOWER FR 17, STR 27L-27R IAW SRM 51-40-08. SEE APPROVED ETD2019-SDR DALA201904222553Frame · crackedFUSELAGE FRAME AT STA Y 696 RT SIDE HAS A CRACK. REF AA 5310-01436 CRACK IS CONDITION 3. NRC 026-0004:5310-01436-01D/001 00060: REPLACED FRAME AT STA 696 RH PER WORK CARD 5310-01436-03B. (LP #1037420)SDR FDEA2023012348850Frame · crackedWINGS - BASIC WING STRUCTURE - INSPECT FR40 LOWER OUTBOARD RADIUS FOR COMPLY WITH E.O. 6-5710-E0333574 REV NO. F POS. P35WINGS - BASIC WING STRUCTURE - INSPECT FR40 LOWER OUTBOARD RADIUS FOR INFO. COMPLIED WITH E6-5710-E0333574P35F. THIS ITEM WAS FACTESDR CA190425023Frame · cracked(CAN) FS 333 FRAME CRACKED BETWEEN STR 0 TO STR 1L (TC# 20190425023)SDR CALA2019041900613Frame · crackedCRACK INDICATION IN FRAME LAYER AT FR16 L/H SIDE HOLE "D" REPAIR L/H FR16 CROSSBEAM BEFORE NEXT FLIGHT PER STEP 6 ACCOMPLISHED INTERIM REPAIR ON FRAME LAYER AT FR16 L/H HOLE D PER ECRA 5311-02131 PART 1, ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF ECRA 53SDR SIMA20190418001Frame · corrodedSSI 53-30-48; FRAME 65 IS CORRODED AT STAINLESS GUIDE PLATE BETWEEN STRINGERS 16L-17L-C/A-REPAIRED FRAME 65 AT STAINLESS GUIDE PLATE BTW STRINGERS 16L-17L IAW ERS-EM-53MR-3741
Back to JASC 5311