JASC 5312

Service difficulty reports · 20,045

Reports filed under 5312 · Fuselage Main, Bulkhead, 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 = '5312'
  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.

SDR UIEA2013012300020Bulkhead · crackedBS 1241 LT MLG WW PRESSURE BULKHEAD FOUND CRACKED AT LBL 75 AREA. REPAIRED IAW RS R1-53-48-10119)Jan 20, 2013 · N412MC · Boeing 74747UFSDR VNAA2013012300009Bulkhead · crackedDURING SCHEDULED MAINTENANCE FOUND FS 202 PRESSURE BULKHEAD WEB CRACKED AROUND THE PARKING BRAKE CABLE CUTOUT. FS 202 PRESSURE BULKHEAD WEB AT THE PARKING BRAKE CUTOUT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SJan 20, 2013 · N221PS · Cndair CL6002B19SDR ASOA2013020702983Bulkhead · crackedREAR PRESSURE BULKHEAD IS CRACKED AT TOP OF CARGO DOOR AFT TRACK AREA IS MARKED. REPAIRED IAW REO 601R-53-61-1541, REV D.Jan 19, 2013 · N932EV · Cndair CL6002B19SDR ASOA2013020702982Bulkhead · crackedREAR PRESSURE BULKHEAD IS CRACKED AT LINTEL ATTACH POINT AREA IS MARKED. REPAIRED IAW REO 601R-53-61-1230 AND GREO 601R-53-61-1230, REV R.Jan 19, 2013 · N932EV · Cndair CL6002B19SDR A6WA2013020500664Bulkhead · gougedAFT SIDE OF BULKHEAD FS 280 GOUGED. REPAIRED AFT SIDE FS 280 BULKHEAD IAW REO 601R-53-11-1727 REV F.Jan 17, 2013 · N412AW · Cndair CL6002B19SDR ASAA2013011793725Support · corrodedFWD CARGO COMPARTMENT AFT BULKHEAD LOWER SUPPORT CORRODED. REMOVED LOWER SUPPORT 2 ANGLE FROM FWD PIT AFT BULKHEAD IAW SRM 51-50-02. LOCATED, DRILLED, AND DEBURRED NEW ANGLE IAW SRM 51-40-05. INSTALLED NEW Z ANGLE IAW SRM 51-40-02, CICD AREA IAW AMM 51-21-91.Jan 17, 2013 · N593AS · Boeing 737890SDR REXA2013011800068Bulkhead · crackedFS 559 SEMI-PRESSURE BULKHEAD CRACKED. REPAIRED IAW PA 53-025 AND BOMBARDIER REOS 601R-53-41-260 AND 601R-53-41-609.Jan 17, 2013 · N8938A · Cndair CL6002B19SDR SWAA2013022613114Angle · crackedBS 540 BULKHEAD HAS CRACK IN THE SPLICE ANGLE BETWEEN STR 21R AND STR 22R. REPAIRED ANGLE IAW ER & EA 1-357-7919Jan 16, 2013 · N687SW · Boeing 7373Q8SDR DALA13002786307Fitting · crackedDURING HFEC OPEN HOLE ON BS 1000 BULKHEAD LOWER DRAG SPLICE FITTING ANGLES. REMOVED FASTENER HOLE AND FOUND CRACK 01EA AS MARK. BS 1000 BULKHEAD LOWER DRAG SPLICE FITTING REMOVED IAW SRM 51-40-02. NEW DRAG SPLICE FITTING HOLES PICKED UP IAW SRM 51-40-05. NJan 16, 2013 · N667US · Boeing 747451SDR SWAA2013021912826Bulkhead · puncturedPUNCTURE ON BULKHEAD BS 227.8 BL 0 WL 186 LOWER NOSE COMPARTMENT. REPAIRED BULKHEAD LOWER WEB BS 227.8 BETWEEN WL 180/ WL 190 AND BL 0 IAW EO N. AEM-HC53-012/13 R0 AND EA N. 1-353-21731 R0 FOR INSPECTION REQUIRED SEE TLD #T027942.Jan 15, 2013 · N665WN · Boeing 7373Y0SDR ASOA2013020102951Bracket · crackedREAR PRESSURE BULKHEAD AT FS 621.00 HAS 4 ISOLATOR BRACKET ASSY CRACKED AT RBL 45, 1 BRACKET AT RBL 9, 1 BRACKET AT LBL 9, 1 BRACKET AT LBL 27 AND 1 BRACKET AT LBL 36. REMOVED 8 EA DAMAGED ISOLATORS FROM FS 621 PRESSURE BULKHEAD AND INSTALLED NEW ISOLATORS, Jan 15, 2013 · N841AS · Cndair CL6002B19SDR SWAA2013013012138Stiffener · crackedBULKHEAD CRACKED HORIZ STIFFENER BETWEEN RBL10 AND 19 ON 727 BULKHEAD. R & R STIFFENER IAW SRM.Jan 15, 2013 · N687SW · Boeing 7373Q8SDR A6WA20134633Bulkhead · chafedAFT RIGHT SIDE OF FS 280 BULKHEAD AND VERTICAL POST AT RBL 9 CHAFED. REPAIRED AFT RIGHT SIDE OF 280 BULKHEAD AND VERTICAL POST AT RBL 9 IAW REO 601R-53-11-1727.Jan 14, 2013 · N416AW · Cndair CL6002B19SDR SWAA2013012811969Panel · crackedCRACK ON BULKHEAD PANEL 1542 IN CARGO COMPARTMENT. REPAIRED PANEL IAW AMM.Jan 14, 2013 · N665WN · Boeing 7373Y0SDR 2013FA0000049Bulkhead · brokenDURING 100 HR INSPECTION, LT ANCHOR WAS WORN AT MASTER CYLINDER ATTACH, OBLONGED HOLE. BULKHEAD WAS BROKEN AT RUDDER BAR ATTACH RESULTING IN POOR BRAKING AND LIMITED LT RUDDER TRAVEL. REPAIR WITH NEW PARTS.Jan 14, 2013 · N630RR · Cessna 172SSDR SWAA2013012311704Attach Bracket · crackedAFT CARGO BAY FWD BULKHEAD ATTACH BRACKET CRACKED BS 727, WL 163, RBL 5. REMOVED AND REPLACED ACB FWD BULKHEAD ATTACH BRACKET AT BS 727, WL 163 RBL 5 WITH NEW BRACKET PART NUMBER 7531203 IAW SRM 51-40-02. 56105U 17JAN13.Jan 14, 2013 · N554WN · Boeing 7377BXSDR SIMA20130113010Bulkhead · corrodedDURING 3C CHECK INSPECTION FOUND LEFT AFT FACE OF BULKHEAD ASSY AT FS 280.00 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED BULKHEAD IAW EO CR-53MR-174. THE AIRCRAFT WAS RETURNED TO SERVICE.Jan 13, 2013 · N511AE · Cndair CL6002C10SDR REXA2013011500061Bulkhead · gougedCARGO AREA FS 621 BULKHEAD FWD FACE HAS 14 GOUGES. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Jan 13, 2013 · N821AY · Cndair CL6002B19SDR REXA2013011500062Bulkhead · crackedSEVERAL HOLES FOUND TO BE ELONGATED AND 3 HOLES HAVE CRACKS ON FS 621 BULKHEAD BEHIND FIRESHIELD AT WL 90.93 TO WL 121.83. REPAIRED IAW BOMBARDIER REO 601R-53-61-4761.Jan 12, 2013 · N821AY · Cndair CL6002B19SDR ASOA2013012902922Bulkhead · crackedINDICATION NOTED AT FS 621 REAR PRESSURE BULKHEAD AT LBL 36, WL 78 APPROX .300 IN LENGTH AT 100/5 FULL SCREEN HEIGHT. REPAIRED FS 631 BULKHEAD AT LBL 36 & WL 78 IAW REO 601R-53-61-4765.Jan 11, 2013 · N847AS · Cndair CL6002B19SDR ASOA2013012902921Bulkhead · crackedINDICATION NOTED AT FS 621 REAR PRESSURE BULKHEAD AT LBL 27.50, WL 141 APRROX .150 IN LENGTH AND 55 PERCENT FULL SCREEN HEIGHT. COMPLIED REO 601R-53-61-1546 AND REO 601R-53-61-1541 REV D DATED 10/31/2011.Jan 11, 2013 · N847AS · Cndair CL6002B19SDR SWAA2013011611477Pressure Panel · crackedMAIN W/W FORWARD VERTICAL PRESSURE WEB CRACKED AT BS 663.75, RBL 43.80. REPAIRED WEB PER SRM.Jan 11, 2013 · N268WN · Boeing 7377H4SDR SWAA2013012812041Bulkhead · crackedAFT PIT - FWD BULKHEAD - LINER SUPPORT STRIP CRACKED AT STA 813 LEFT AND RIGHT SIDES. REMOVED AND REPLACED AFT PIT FWD BULKHEAD 5956040-43, 596040013 5956040-41 AND 5956040-11 INTERCOSTALS IAW B717 SRM 51-41-08 AND 51-41-02Jan 10, 2013 · N958AT · Boeing 717200SDR BGJA2013F00009Bulkhead · crackedFOUND BULKHEAD AT BS 295.17 CRACKED FROM UPPER LT AND RT LIGHTNING HOLE THROUGH INBD FLANGE. IN ADDITION A .2500" CRACK WAS FOUND PROTRUDING INBD FROM STRINGER RELIEF JUST ABOVE TOP LT LIGHTNING HOLE.Jan 10, 2013 · N9746C · Cessna T303SDR CALA2013011100025Angle · corrodedFORWARD CARGO BAY BULKHEAD BS 500D SUPPORT ANGLE HAS CORROSION JUST ABOVE S25R. INSTALLED SUPPORT ANGLE IAW SRM 51-40-02.Jan 9, 2013 · N29717 · Boeing 737724SDR CALA2013011100024Angle · corrodedFORWARD CARGO BAY BULKHEAD BS 500D SUPPORT ANGLE HAS CORROSION JUST ABOVE S25L. INSTALLED LT SUPPORT ANGLE IAW SRM 51-40-02.Jan 9, 2013 · N29717 · Boeing 737724SDR WVER2013010950103Bulkhead · corrodedFS 280.00 BULKHEAD WEBS CORRODED AND FS 280 CROSSBEAM CORRODED AND CRACKED AT LBL 9 AND RBL 9.Jan 9, 2013 · N501MJ · Cndair CL6002C10SDR WX0A071474Bulkhead · crackedRIGHT CANTED BULKHEAD 1463 AS 2 EACH CRACKS AT LONGERON 17R AND 18R. STOP DRILLED CRACKS, FABRICATED REPAIR DOUBLERS AND SHIMS.Jan 9, 2013 · N424NV · Doug MD83SDR SWAA2013030813484Splice Plate · crackedBULKHEAD CRACKED AT BS 540 IN THE SPLICE PLATE BETWEEN STR 21L AND 22L. REPAIRED BULKHEAD SPLICE PLATE BETWEEN PER ER & EA.Jan 8, 2013 · N687SW · Boeing 7373Q8SDR LR7A2013010800431Bulkhead · crackedDURING SCHEDULED B-2 CHECK, FOUND AFT FUSELGAE INTERIOR FS 968, UPPER BULKHEAD CRACKED AT RBL 18, WL 285 VERTICAL FIN ATTACHMENT. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-50-06.Jan 8, 2013 · N404LC · Lkheed 382GSDR FDEA201301080045Frame · crackedAFT FUSELAGE COMPARTMENT FORWARD BULKHEAD RT CHORD FOUND CRACKED AT STA 2007.Jan 8, 2013 · N614FE · Doug MD11FSDR SWAA2013012812022Bulkhead · corrodedRIGHT W/W BULKHEAD AT FLOOR LEVEL CORRODED FROM I/B SIDE THRU O/B SIDE. REPAIRED SKIN IAW NDT SPM.Jan 7, 2013 · N958AT · Boeing 717200SDR VNAA2013010500002Bulkhead · crackedDURING SCHEDULED MAINTENANCE FOUND FS 202 PRESSURE BULKHEAD AT BRAKE CABLE CUTOUT CRACKED. FS 202 PRESSURE BULKHEAD AT BRAKE CABLE CUTOUT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Jan 5, 2013 · N213PS · Cndair CL6002B19SDR VNAA2013010500001Bulkhead · crackedDURING SCHEDULED MAINTENANCE THE FS 621.00 REAR PRESSURE BULKHEAD WAS FOUND CRACKED. THE FS 621.00 REAR PRESSURE BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Jan 5, 2013 · N213PS · Cndair CL6002B19SDR IPXA3M76933Bulkhead Web · dentedINSPECTION TYPE: 4C, BS 2007 AFT PRESSURE BULKHEAD DENTED JUST OTBD OF RBL 60 STIFFENER. REPAIRED APB DENT IAW STASA EA 011-5310-01-A4426 REV IR AND EO MD11-5310-49726-A.Jan 4, 2013 · N272UP · Doug MD11FSDR CALA2013010700013Bulkhead · crackedCRACK IN LEFT MAIN WHEEL WELL FWD BULKHEAD APPROX 42" FROM CENTERLINE, 6" FROM CEILING. REPAIRED IAW SRM 57-10-10, REPAIR 3, ALT 2 CATEGORY B.Jan 4, 2013 · N17244 · Boeing 737824SDR FDEA201212314406Tee Fitting · crackedRT FWD PRESSURE BULKHEAD AT BS 595, RT LONGERON 43, FOUND CRACKED AT THE WEB AND TEE FITTING. SERVICABLE TEE FITTING INSTALLED IAW EA 8-5310-163797.Dec 31, 2012 · N397FE · Doug MD1010FSDR SWIA201232655Bulkhead · crackedCRACK NOTED AND MARKED ON FS 621 BULKHEAD WEB, FWD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING. (C-CHECK) REPAIRED FS 621 BULKHEAD WEB, FWD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING IAW REO.Dec 28, 2012 · N821AS · Cndair CL6002B19SDR SWIA201232567Bulkhead · crackedCRACK NOTED AND MARKED ON FS 621 AFT PRESSURE BULKHEAD WEB FWD FACE AT LBL 27.50 WL 131.0 ABOVE AFT CARGO DOOR AFT TRACK. (C-CHECK) INSTALLED FABRICATED REPAIR PARTS ON FS 621 BULKHEAD IAW REO.Dec 28, 2012 · N427SW · Cndair CL6002B19SDR SWIA201232566Bulkhead · crackedCRACK NOTED AND MARKED ON FS 621 AFT PRESSURE BULKHEAD WEB FWD FACE AT LBL 46.99 WL 108.64 AT LINTEL FITTING. (C-CHECK) INSTALLED FABRICATED REPAIR PARTS IAW REO.Dec 28, 2012 · N427SW · Cndair CL6002B19SDR SWAA2013010311061Panel · crackedBS 663 BULKHEAD FIBERGLASS PANEL CRACKED, LBL 34, WL 153. REPAIRED CRACK ON BS 663 BULKHEAD FIBERGLASS PANEL LBL 34, WL 153, PER EA1-A53-3376.Dec 28, 2012 · N555LV · Boeing 7377BDSDR ASOA2013012102867Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICAITON NOTED AT LBL 27.50, WL 130 APPROX .3" IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTION. REMOVED CARGO DOOR AFT TRACK FORM REAR PRESSURE BULKHEAD (FS 621) IAW SRM 51-42-06 & 51-42-21. REINSTALLED CARGO DOOR AFT TRDec 27, 2012 · N908EV · Cndair CL6002B19SDR REXA2012122401632Bulkhead · corrodedWHILE WORKING LEFT FS 280 BEAM LOWER BULKHEAD WEB FOUND TO BE CORRODED. REMOVED AND REPLACED LEFT FS 280 BEAM LOWER BULKHEAD WEB IAW EO #R53283.Dec 24, 2012 · N927XJ · Cndair CL6002D24SDR SWAA2013010711238Stiffener · crackedLEFT MAIN W/W FWD BULKHEAD STA-663, LBL-27, LOWER CORD VERT STIFFENER CRACKED AT LOWER RADIUS. REMOVED AND REPLACED DAMAGE VERTICAL STIFFENER AT BS 663 LBL 27 IAW SRM 51-40-02 & BOEING DOCUMENT 111A100.Dec 20, 2012 · N793SA · Boeing 7377H4SDR ASOA2013011802831Bulkhead · corrodedLT BS 280 BULKHEAD CORRODED. INSTALLED LT LOWER BULKHEAD WEB AT FS 280 IAW REO 670-53-11-594.Dec 19, 2012 · N716EV · Cndair CL6002C10SDR SWAA2012122810955Bulkhead · crackedRIGHT MLG W/W BULKHEAD VERTICAL PRESSURE WEB CRACKED AT BS 540, RBL 32.83. REPAIRED WEB IAW SRM.Dec 19, 2012 · N724SW · Boeing 7377H4SDR SWAA2012122710909Bulkhead · crackedLEFT MLG W/W BULKHEAD VERTICAL PRESSURE WEB CRACKED AT BS 540, LBL 42.83, 2.5". REPAIRED WEB IAW SRM.Dec 19, 2012 · N724SW · Boeing 7377H4SDR QMLA2012121912193Bulkhead · crackedDURING 300HR AF INSPECTION, DISCOVERED A CRACK RUNNING FORE AND AFT ALMOST CENTERLINE BETWEEN THE HYD FILTER BRACKETS. AFTER A THOROUGH CLEANING, ADDITIONALLY FOUND THE CRACK EXTENDING TO STA 233 TO THE DRIP PAN AND ALSO INTERNAL BEHIND THE RADIO RACK.Dec 19, 2012 · N431MA · Bell 222USDR SWIA201232506Bulkhead · crackedFS 621 AFT PRESSURE BULKHEAD CRACK INDICATION NOTED ON WEB AT AFT CARGO DOOR TRACK (UPPER). (C-CHECK) REPAIRED CRACK AT FS 621 AFT BULKHEAD WEB AT AFT CARGO DOOR TRACK IAW REO.Dec 18, 2012 · N910SW · Cndair CL6002B19SDR REXA2012122101781Bulkhead · dentedFS 621 BULKHEAD FWD FACE RBL18 JUST ABOVE FLOOR HAS A DENT MEASURING 1.5" X 1.5" X 0.025" DEEP. FOUND TO BE WITHIN LIMITS OF SRM 53-61-00 TR53-28.Dec 18, 2012 · N8751D · Cndair CL6002B19
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