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 2020F00290Frame · corrodedNON-ROUTINE 2794N743 DISCREPANCY. CORROSION AT FRAME 360 STR 28L-28R BL0.SDR SWIA2020060950995Frame · damagedREMOVE AND INSTALL LOWER FRAME SECTOR AT FS349 STR 23L - STR 23R FOR RT LONGERON REPLACEMENT. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW FS 349 LOWER FRAME COMMON TO SKIN FROM STR 23L TO STR 24R REF SRM AND DRAWING, DUE TO CORROSION FOUND WHEN ORIGINAL SDR UIEA2020050700956Frame · crackedCRACK DAMAGE WAS FOUND ON THE RING FRAME (P/N: 65B01700-527) AT STA 134.75, LBL 5.5.(<P>ACCOMPLISHED EI NO T2020A53M-1114 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2020050700964Frame · crackedCRACK DAMAGE ON FRAME 65B04172-7 AT STA 860 BETWEEN S-38L AND S-39L.(<P>REPAIRED THE FRAME DAMAGED AREA IAW EI NO T2020A53M-1122 REV. 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR SWIA2020060950992Frame · corrodedAFT CARGO AREA INTERNAL FUSELAGE BELOW FLOOR LEVEL AT FS 1015.0 IN BETWEEN STR 26L AND STR 26R THERE IS CORROSION ON FWD FRAME FLANGE. (C-CHECK) RO 4/23/2020 REPAIRED FRAME AT FS 1015.0 IN BETWEEN STR 26L AND STR 26R REF REO AND SRM. PRESSURE CHECKS GOOD. SDR FDEA202005021130Frame · gougedFORWARD AVIONICS’ COMPARTMENT, APPROX STA 449, UNDER RAM AIR DUCTING FOR ACM NR 1 (REF BOOT), 1 SCREW NOT SEATED AND 1 SCREW HAS WORN INTO FRAME RADIUS AT FWD INBD POSITION. DAMAGE TRIMMED OUT AND FRAME REPAIRED. REF SRM53-00-07-2R REPAIR NR 2 FIG 201 SHEETSDR SWIA2020052950896Frame · chafedFRAME 718 BETWEEN STR16L AND STR17L, FREE FLANGE CHAFED THROUGH AND INTO FRAME WEB BY HYDRAULIC SUCTION HOSE (MARKED), (48 MONTH) RO 5/28/2020. PERFORMED SPLICE REPAIR TO FS718 FRAME BETWEEN STR20L AND STR13L REF REO. COMPLETED TASK CARD.SDR YENA2020050510326Frame · crackedDURING HEAVY MAINTENANCE, CRACK ON FRAME 68RH UPPER CORNER WEB JOINT; REF W/O 2020 81/1 N/R 2020-117556. SDR FOR MAJOR REPAIR. PERMANENT REPARED IAW AEROMON EA 53-0354-20 & EC A20-431-01SDR SWIA202005210855Frame · crackedFOUND CRACK ON FRAME AT FS605 NEAR STRINGER 20R WHILE INVESTIGATING AREAS OF CORROSION. (C-CHECK) RO 5/16/2020 PERFORMED REPAIR TO FRAME 605 NEAR STRINGER 20R IAW BOMBARDIER REO NO. SKYCARD AND FORM 337 ATTACHED.SDR DALA2020050402344Frame · cracked(AIRCRAFT 3163, L/P 1554156) CRACK INDICATION ON FRAME 16 RH SIDE DOUBLE JOGGLE AREA OPEN FASTENER HOLE 5, CRACK DIRECTION IS 6 OCLOCK, AT FWD GALLEY AREA (1 EA). CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER ERA 585867-14AD REV. ORIGINAL AND PRI 585SDR EE4Y2020043011334Frame · corrodedLOWER FUSELAGE, AFT CARGO COMPARTMENT INTERNAL STRUCTURE, AT FR 80, BETWEEN STR 27RH AND STR 28RH LOWER FLANGE WITH CORROSION. NOTE: THE FRAME WAS REPLACED AS PER NOM ROUTINE ITEM JOB A1H251 ITEM 1-39.SDR FDEA2020051190834Doubler · damagedAGING AIRCRAFT, EXISTING REPAIR AT MAIN DECK CARGO FRAME STATION 1681 LONGERON 12 RIGHT HAND SIDE. EXISTING REPAIR AT MAIN DECK CARGO FRAME STATION 1681 LONGERON 12R RIGHT HAND SIDE EVALUATED AND FOUND REPAIR DOUBLER DAMAGED / DENTED. MAIN DECK CARGO FRAME STASDR FDEA2020051190833Doubler · damagedAGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO FRAME STATION 1641 LONGERON 11 RIGHT HAND SIDE . EXISTING REPAIR AT MAIN DECK CARGO FRAME STATION 1641 LONGERON 11 RIGHT HAND SIDE EVALUATED AND FOUND REPAIR DOUBLER DAMAGED / DENTED. MAIN DECK CARGO FRAMSDR DALA2020043002333Frame · damaged(AIRCRAFT 3144, L/P 1553789) DURING FRAME INSPECTION FOUND HOLE 2 @ FITTING 1 TO BE MEASURING 0.285 OUT OF LIMITS. REF. AMDS 5311-01216-08 STEP 17. AD RELATED ACTION REQUIRED PRIOR TO FURTHER FLIGHT. FR 68 RH SIDE. CORRECTIVE ACTION: REPAIRED PER ERA 586637-14SDR DALA2020043002332Frame · damaged(AIRCRAFT 3144, L/P 1553787) DURING FRAME INSPECTION FOUND HOLE 4 @ FITTING #1 TO BE MEASURING 0.285 OUT OF LIMITS REF. AMDS 5311-01216-08 STEP 17. AD RELATED ACTION REQUIRED PRIOR TO FURTHER FLIGHT. FR 68 RH SIDE. CORRECTIVE ACTION: REPAIRED PER ERA 586637-14SDR DALA2020043002330Frame · damaged(AIRCRAFT 3144, L/P 1553784) DURING FRAME INSPECTION FOUND HOLE 3 FITTING 1 TO BE MEASURING 0.285 OUT OF LIMITS REF. AMDS 5311-01216-08 STEP 17. AD RELATED ACTION REQUIRED PRIOR TO FURTHER FLIGHT FR68 RH SIDE. CORRECTIVE ACTION: REPAIRED PER ERA 586637-14AD RESDR SWIA2020060950986Frame · corrodedCORROSION ON FS349 LOWER FRAME SECTOR BETWEEN STR 26L - STGR 26R. (C-CHECK) RO 4/23/2020 BLENDED, AND EVALUATED FS 349 LOWER FRAME SECTOR CORROSION ON STR 26L TO STR 26R. UPON REMOVAL OF FS 349 FRAME FOR ACCESS ON JOB 710222104 MX TRANS 20918758. ADDITIONAL SDR FDEA2020043080816Frame · crackedFWD CARGO PIT-R/H SIDE,FRAME 846 AT STR 22 RT. CRACKED AT FASTENER HOLE. REMOVED,FABRICATED AND INSTALLED STANCHION STUB (FRAME) ON FWD CARGO PIT R/H SIDE AT STA 846 BETWEEN STR-21R TO STR-26R IAW B 757 SRM 51-40-02-OG AND B. DWG : 143N5811, REV : - , RESDR DALA2020043002323Frame · corrodedCORROSION ON FR 16 AT LEVEL OF STRINGER 23R/H SIDE, PERFORMED PERMANENT REPAIR ON FR 16 AT LEVEL OF STRINGER 23R/H SIDE AS PER PRI 522853-14 REV O, REV 1,REV 2,REV 3 AND ER/A 522853-14 REV "C"SDR 2A6D20200428001Frame · chafedTHERE IS DAMAGE ON THE TRANSMISSION DECK FRAME JUST INBOARD OF THE SPLICE. DAMAGE MEASURES AT 0.017” IS 13MM WIDE AND 5MM LONG LOCATED AT APPROX. STA 3640, BL 210R, AND WL 1839.SDR JR2R202004281346Frame · crackedL/H WHEEL WELL FRAME 52 IS CRACKED. REPAIRED IAW EMB 175 SRM 53-22-04.SDR 2A6D2020042701301Frame · chafedTHERE IS CHAFFING ON THE R/H UPPER FORWARD SECTION OF THE X FRAME MEASURED AT .012” DEEP APPROX. 4MM WIDE AND 3 MM LONG.SDR CALA2020050200890Frame · dentedFWD CARGO STATION 500B FRAME DENTED 2 INCHES ABOVE SPLICE BETWEEN STRINGER 26&27 REPAIRED FRAME PER SRM53-30-07 REPAIR 2. PLACED ON DIP TO REINSP ECT AFTER 50,000 FLT CYCLES AFTER AIRPLANE DELIVERY. REPEAT INSP CDTIONS EVERY 10,000 FLIGHT CYCLES AS SHOWN IN FISDR CALA2020050200889Frame · dentedFWD CARGO F.S.500A STR 25R FRAME DENTED REPAIRED FRAME PER SRM 53-30-07 REPAIR 2. PLACED ON DIP TO REINSPECT 50,000 FLT CYCLES AFTER AIRPLANE DELIVERY WITH REPEAT INSPECTIONS EVERY 10,000 FLT CYCLES AS SHOWN IN FIGURE 208/REPAIR 2. LFEC INSPECTION OF THE FRAMESDR IPXA2020052635668Frame · crackedINSPECTION TYPE:C3AFT AVI COMP BILGE AREA L/H CANTED FRAME IS CRACKED AT STA 469.173.ACCOMPLISHED PERMANENT REPAIR ON CRACKED CANTED FRAME IN AFT AVIONICS COMPARTMENT AT STA 469.173 IAW MD11 SRM 53-10-07 REPAIR 1 FIGURE 201 REV. 66. (MAJOR)SDR IPXA2020051855411Frame · crackedINSPECTION TYPE:3CFUSELAGE FRAME AT STA. 469.173 CANT AND X=60 IS CRACKED.REPAIRED CRACKED FUSELAGE FRAME AT STA. 469.173 CANT AND X=60 IAW SRM 53-10-07 REPAIR 1 FIG. 201. (MAJOR)SDR UIEA2020042800853Frame · crackedAPU COMP - LH STA 2664.19 FRAME FOUND CRACK.(<P>APU COMP - LH STA 2664.19 LH WL 310 FRAME CRACK AREA REPAIRED IAW RI-53-82-14008 REV. A. </P>)SDR UIEA2020042800893Frame · crackedLH STA 2231 FRAME STR 16L 1 EA HOLE FOUND 2 EA CRACKS AT FRAME STRAP AT 3 O/C POSITION THROUGH THICKNESS AND 6 O/C POSITION APPROX 0.030" DEPTH.(<P>STA 2231 STA 16L-17L FRAME STRAP FASTENER HOLE CRACK AREA REPAIRED IAW RI-53-60-14005 REV. A.</P>)SDR UIEA2020042800894Frame · crackedLH STA 2231 FRAME STR 25 1 EA HOLE CRACKS AT FRAME INNER CHORD AT 8 O/C POSITION THROUGH THICKNESS.(<P>STA 2231 STA 25L FRAME INNER CHORD FASTENER HOLE CRACK AREA REPAIRED IAW SRM 53-60-15-2R-2 REPAIR 2. </P>)SDR SWAA2020051945080Frame · crackedBS 294 STUB FRAME INBOARD FLANGE IS CRACKED COMMON TO MOPSILL ATTACH FASTENER HOLES; RBL 55; WL 207.5. / TRIMED OUT CRACK IN STUB FRAME INBOARD FLANGE AND INSTALLED REPAIRED PART AT BS294 RBL55 WL207.5 PER SRM 53-10-15-2R-7. 57449U 27APR20SDR SWIA202005070549Frame · gouged*FS605.00 FRAME IS CORRODED, STGR20L €“ STGR24R. (48 MO INSP) RO 5/6/2020 REMOVE CORROSION ON THE AFFECTED AREA, GOUGE NOTED ON THE FS605.00 FRAME DURING REMOVAL OF CORROSION. GOUGE PUNCTURED THROUGH FRAME. REMOVED AND INSTALLED NEW FROM SLPICE ANGLES ATSDR SWIA202005070548Frame · cracked*FS574.00 FRAME IS CORRODED, STGR23L €“ STGR20L. (48 MO INSP) RO 5/6/2020 REMOVED CORROSION IN MULTIPLE AREA ON FRMAE AT FS574.00 BETWEEN STGR23L AND STGR20L. AFTER CORROSION REMOVAL, FOUND CRACK ON FLANGE NEAR RIVET HOLE OUTBOARD SIDE OF STGR23L REF CSDR DALA2020043002322Frame · crackedCRACK INDICATION ON FRAME 16 CROOSSBEAM SPLICING AT HOLE 2 AT FRAME 16LH SIDE IN PASSENGER CABIN (1 EA), PERFORMED REPAIR INSTRUCTIONS AT FRAME 16 CROOSBEAM SPLICING ON HOLE 2(B) L/H SIDE PASSENGER CABIN AS PER ERA 586039-14 REV ORIGINAL AND PRI 586039-14 REV SDR DALA2020043002321Frame · crackedCRACK INDICATION ON FRAME 16 LH SIDE ON CROSSBEAM SPLICING AT HOLE 3 IN PASSENGER CABIN (1 EA), PERFORMED REPAIR INSTRUCTION AT FRAME 16 CROSSBEAM SPLICING ON HOLE 3(C) L/H SIDE PASSENGER CABIN AS PER ERA 586039-14 REV ORIGINAL AND PRI 586039-14 REV 0, REV 1 ASDR DALA2020043002320Frame · crackedCRACK INDICATION ON FRAME 16 LH SIDE ON CROSSBEAM SPLICING AT HOLE 4 IN PASSENGER CABIN (1 EA), PERFORMED REPAIR INSTRUCTIONS AT FR 16 CROSS BEAM SPLICING ON HOLE 4(D) L/H SIDE PASSENGER CABIN AS PER ER/A 586039-14 REV ORIGINAL AND PRI 586039-14 REV O, REV 1 ASDR CALA2020042400869Frame · dentedB757-53-3-0523. AFT CARGO COMPARTMENT BS1400 S26L FRAME FOUND W ITH A DENT. MEASURED DENT AT AFT CARGO FRAME STA.1400 S26L FOUND TO BE WITH IN LIMITS IAW B757-300 SRM 53-00-07. INSTALLED DENT DOT ECRA 20 60-01042. LOG PAGE WAS CONVERTED TO ELB FORMAT ON MAY 03SDR MASA20200424106Frame · corrodedREMOVED AND REPLACED DISCREPANT FRAME AT FS379 IAW SRM 51-40-11 FS379 STGR 23RSDR MASA20200423015Frame · corrodedINSTALLED -001 DOUBLER AND NEW FRAME TO INTERCOASTAL CLIP IAW EA 70-2020-050SDR IPXA2020060856294Support · crackedINSPECTION TYPE:3C AFT CARGO BILGE AREA LOWER FRAME SUPPORT HAS A CRACK AT STA 1841 ABOVE LONGERON 43. REMOVED CRACKED FRAME SUPPORT, FABRICATED AND INSTALLED IN AFT CARGO AT STA 1841 ABOVE LONGERON 43 IAW SRM 51-35-01 AND DWG AGA7098. (MINOR)SDR SWAA2020052044309Frame · crackedCRACK IN RADIUS OF FRAME AT BS312 INBD FLANGE STRINGER 5LT / INSTALLED REPAIR ANGLE AT BS312 INBD FLANGE STRINGER 5LT PER SRM 53-10-07-2R-1 89232U 01MAY20 DAMAGE WAS REMOVED FROM RADIUS OF FRAME AT BS312 INBD FLANGE STRINGER 5LT AS PER SRM 51-10-02-09-0 IN ARESDR DALA2020043002334Frame · damaged(AIRCRAFT 3144, L/P 1550849) DURING FRAM INSPECTION FOUND HOLE 4 @ FITTING 4 TO BE MEASURING 0.2835, OUT OF LIMITS REF AMDS 5311-01216-08 STEP 17. AD RELATED, ACTION REQUIRED PRIOR TO FURTHER FLIGHT FR68 RH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 586637-14ASDR DALA2020043002329Frame · damaged(AIRCRAFT 3144, L/P 1550847) DURING FRAME INSPECTION, FOUND HOLE 1 AT FITTING 7 TO BE MEASURING 0.285 AND OUT OF ROUND. OUT OF LIMITS REF AMDS 5311-01216-08 STEP 17. AD RELATED, ACTION REQUIRED PRIOR TO FURTHER FLIGHT. FR 68 RH SIDE. CORRECTIVE ACTION: REPAIRESDR DALA2020043002319Frame · crackedCRACK INDICATION ON FRAME 36 , CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 1 AT FR 36, PERFORMED REPAIR AT CWB FRONT SPAR VERTICAL STRINGER POSITION 1 AT FR 36 AT HOLE ZONE 1 (INB SIDE) Y1292 IN FWD CARGO COMPARTMENT AS PER PRI 585863-14AD REV 0,1SDR CALA2020042400864Frame · cracked(CUSTOMER REQUEST - SUPPORT TASK) FRAME CRACKED AT FASTENER HOLE STATION 1580 BETWEEN STRINGERS 8R AND 9R. REF ST-SAA NR 0092124. CUTOUT CRACK L=1.250 W=1.050 AND INSTALLED PERMANENT REPAIR ON FRAME STA 1580 BETWEEN STRINGER 8R AND 9R IAW B757-3 SRM 53-00-07 RSDR CALA2020042400865Frame · cracked(CUSTOMER REQUEST - SUPPORT TASK) FRAME CRACKED AT FASTENER HOLE STATION 1580 BETWEEN STRINGERS 8L AND 9L. REF ST-SAA NR 0092123. CUTOUT CRACK 1.180 X 1.040 AND INSTALLED PERMANENT REPAIR ON FRAME STA 1580 BETWEEN STRINGER 8L AND 9L IAW B757-3 SRM 53-00-07-R8 SDR VNAA202004219996Frame · corrodedFUSELAGE LOWER FRAME AT FS295, STGR27 IS CORRODED ON FWD SIDE. REPAIRED IAW CRJ 900 SRM 53-00-06-101-002-A04SDR MASA2020042121011Frame · corrodedCORROSSION FWD E&E FS319 FRAME 23R-21L. R&R'D FRAME SECTOR FS319SDR IPXA2020061056338Beltframe · dentedINSPECTION TYPE:3C MAIN CABIN BELT FRAME DENTED AT STA 715 LONGERON 13R. CUTOUT DAMAGE AND ACCOMPLISHED PERMANENT REPAIR ON BELT FRAME IN MAIN CABIN AT STA 715 LONGERON 13R IAW EA 011-5310-01-A8168 REV I/R AND EO MD11-5310-76728-A. (MAJOR)SDR IPXA2020060856248Beltframe · dentedINSPECTION TYPE:3C MAIN CABIN BELT FRAME DENTED AT STA 695 LONGERON 12R. CUT OUT DAMAGE AND ACCOMPLISHED PERMANENT REPAIR OF MAIN CABIN BELT FRAME AT STA 695 LONGERON 12R IAW EA 011-5310-01-A8171 REV I/R AND EO MD11-5310-76700-A. (MAJOR)SDR REXA2020042800562Frame · corrodedFS 364 FRAME CORRODED BETWEEN STRINGER 27 & 26R.
OK TO INSTALL. WVAC STAMP INSP INSTALLED THE NEW SERVICEABLE FS 364 FRAME P/N SH670-32090-9 IAW BOMBARDIER REO NO. 601-53-21-687 REV A DATED 2016/06/06 STEPS 8 THRU 9. WVAC STAMP
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