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 FDEA201604091179Bulkhead · crackedCENTER WW RT BULKHEAD CRACKED. R & R FACTORY DOUBLER.Apr 9, 2016 · N303FE · Doug MD1030FSDR FDEA201604091178Bulkhead · crackedCENTER WW LT FWD BULKHEAD CRACKED. R & R FACTORY DOUBLER.Apr 9, 2016 · N303FE · Doug MD1030FSDR ASOA2016040814750Bulkhead Web · corrodedRT WEB AT FS 280 CORRODED. REMOVED CORROSION DAMAGE IAW SRM 51-21-06-001-001 A01 CORROSION FOUND UNDER FASTENER HEADS. COMPLIED WITH EC/TC REO 670-53-11-1142 AND REO 670-53-11-1142.Apr 8, 2016 · N600QX · Cndair CL6002C10SDR SWIA201642102Bulkhead · gougedFS 621 BULKHEAD HAS 15 AREAS WITH SMALL CIRCULAR GOUGES. REPAIRED IAW REO. LEAK CHECKED GOOD, NO LEAKS NOTED.Apr 8, 2016 · N8982A · Cndair CL6002B19SDR DXTA2016040806229Firewall · crackedAPU FIREWALL CRACKED UNDER LT UPPER TRUSS MOUNT ATA 51. REPAIRED IAW REPAIR DEFINITION S-750-0156 23PRD & SRM 51-40-03. DOUBLER & 6712625-15-2 FILLER WAS FABRICATED. MATCH DRILL 1 DOUBLER & 2 FILLER IAW DWG 6712625 & PRELIMINARY REPORT S-750-0156 23PRD. INApr 8, 2016 · N956QS · Cessna 750SDR SWAA2016042051114Stiffener · crackedFORWARD BULKHEAD STIFFENER CRACKED AT BS 663.75, BETWEEN RBL 5 - RBL 34. R & R STIFFENER IAW SRM & DWG.Apr 8, 2016 · N715SW · Boeing 7377H4SDR REXA2016040800600Bulkhead · damagedFOUND REAR PRESS BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED AT INBD LOWER CORNER, APPROX .200" IN LENGTH 90% FSH. FAILED NDT INSPECTION. CONTINUATION CARD 8783615 OP 76. REPAIRED REAR PRESS BULKHEAD AT THE LINTEL ATTACHMEApr 8, 2016 · N8836A · Cndair CL6002B19SDR SWAA2016042151198Bulkhead · crackedLEFT MAIN WW BULKHEAD CRACKED AT BS 663, LBL 35. REPAIRED WEB IAW SRM.Apr 6, 2016 · N470WN · Boeing 7377H4SDR REXA2016040600601Bulkhead · damagedFOUND FS 202.75 PRESS BULKHEAD WEB AT BL 23.71 HAS INDICATION NOTED, APPROX .500 IN LENGTH 50% FSH, FAILED NDT. CONTINUATION CARD 8783615 OP 66 & 82. REPAIRED FS 202.75 PRESS BULKHEAD IAW REO 601R-53-11-563 REV C. THIS IS A MAJOR REPAIR.Apr 6, 2016 · N8836A · Cndair CL6002B19SDR ASOA2016040514743Bulkhead Web · corrodedLT WEB AT FS 280 CORRODED AT LB12. REMOVED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01 CORROSION FOUND UNDER FASTENER HEADS. COMPLIED WITH EC/TC REO 670-53-11-1142 AND REO 670-53-11-1142.Apr 5, 2016 · N600QX · Cndair CL6002C10SDR SWAA2016042151206Pressure Panel · crackedCENTER WING BOX VERTICAL PRESS WEB CRACKED AT BS 663, RBL 42. REPAIRED WEB IAW SRM.Apr 5, 2016 · N715SW · Boeing 7377H4SDR SWAA2016041851070Pressure Panel · crackedMAIN WW VERTICAL SPAR WEB CRACKED AT BS 663, LBL 34. REPAIRED WEB IAW SRM.Mar 31, 2016 · N463WN · Boeing 7377H4SDR DALA2016033102544Bulkhead · crackedRT W/W AFT PRESSURE BULKHEAD BS 1180, RBL 10 ANGLE CRACKED. R & R RT W/W AFT PRESSURE BULKHEAD ANGLE BS 1180, RBL 10 IAW SRM 57-40-02 AND DWG 149N7528 REV: AA AND SRM 51-20-05 AND 51-40-02.Mar 30, 2016 · N651DL · Boeing 757232SDR DALA2016033002635Bulkhead · crackedTAIL INTERIOR CANTED BULKHEAD STA 1520, FORWARD AND AFT WEB IS CRACKED RT SIDE. REPAIRED IAW SRM 53-10-03, PARA 10A.Mar 29, 2016 · N957DN · Doug MD9030SDR DALA2016033002437Stiffener · crackedLEFT WW AFT PRESSURE BULKHEAD INBD SIDE LOWER STIFFENER CRACKED. REMOVED CRACKED STIFFENER LT WW AFT PRESSURE BULKHEAD INBD IAW SRM 51-40-02. FORMED NEW PART IAW ORIGINAL PART FROM .063" 7075-O IAW DWG 144N2503, REV H. HEAT TREATED FROM HEAT TREATED FROM 7075Mar 29, 2016 · N651DL · Boeing 757232SDR DALA2016033002420Structure · not reportedPRESSURE DOME LOWER CHARD SPLICE FOUND BETWEEN LONGERON 26, 27 RT/LT IN DISCREPANCY TO INSPECTION CARD 5310-01414-1701 AT AFT CARGO COMPARTMENT. AREA WAS REPAIRED IAW ER/A 593209-14, REV ORIGINAL AND ETI 88-16-114, REV 1.Mar 29, 2016 · N994DL · Doug MD88SDR SIMA20160327003Stiffener · crackedFS 202.75, BULKHEAD STIFFENER POST AT RBL 30 FAILED NDT INSPECTION. FOUND A CRACK APPROX .125" LONG. PERFORMED MAJOR REPAIR TO FS 202.75, BULKHEAD STIFFENER POST AT RBL 30 IAW REO 670-53-11-1139, DATED 2016-03-20.Mar 27, 2016 · N506AE · Cndair CL6002C10SDR REXA2016032600560Bulkhead · chafedFOUND REAR PRESS BULKHEAD WEB HAS 4 CHAFED AREAS, AT WL 105, LBL 27.50, LBL 18.00, RBL 27.50 & RBL 36.20, APPROX .200" LONG BY .200" WIDE & .002 DEEP. REPAIRED 4 CHAFED AREAS IAW REO 601R-53-61-2155 REV A DATED 2013 08 13. THIS IS A MAJOR REPAIR.Mar 26, 2016 · N8836A · Cndair CL6002B19SDR SWAA2016040850720Pressure Panel · crackedMAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB IAW SRM.Mar 26, 2016 · N7840A · Boeing 73773VSDR REXA2016032600483Bulkhead · gougedAFT PRESS BULKHEAD FWD FACE HAS 9 SCREW GOUGES, APPROX 29" ABOVE THE FLOOR. AFT PRESS BULKHEAD GOUGES REMOVED & FOUND TO BE WITHIN LIMITS IAW REO 601R-53-61-2155 REV A. ONE EACH AREA FOUND OUT OF LIMITS. DAMAGE CUT OUT & REPAIRED IAW REO 601R-53-61-1285 REVMar 26, 2016 · N8976E · Cndair CL6002B19SDR ASAA2016032616125Bulkhead Web · crackedPOSSIBLE CRACK ON RT WHEEL WELL FORWARD BULKHEAD, NEAR THE TOP, IT IS LOCATED JUST ABOVE THE SPOILER HYD CONTROL VALVE. ACFT GROUNDED. REMOVED DAMAGE AND ACCOMPLISHED REPAIR IAW SRM 57-10-10-2R-3, REPAIR 3. REPAIR IS A CATEGORY B REPAIR. THRESHOLD IS AT 56Mar 26, 2016 · N546AS · Boeing 737890SDR SWAA2016050251490Pressure Deck · crackedMAIN LANDING GEAR PRESS DECK, UPPER SURFACE CRACKED, AT BS 665, LBL 39. REPAIRED DECK IAW EA.Mar 25, 2016 · N636WN · Boeing 7373H4SDR SWAA2016040550621Stiffener · crackedPRESSURE BULKHEAD STIFFENER CRACKED AT BS 1016. R & R STIFFENER IAW SRM & DWG.Mar 25, 2016 · N767SW · Boeing 7377H4SDR DALA2016032602419Bulkhead · crackedCANTED BULKHEAD, BS 1520, AFT WEB IS CRACKED LT SIDE. ACCESS INSIDE LT VENT BOX. REPAIRED BULKHEAD IAW SRM 51-10-03, FIG 9C.Mar 25, 2016 · N957DN · Doug MD9030SDR AALA20160325005Pressure Panel · crackedAIRCRAFT WAS IN BASE MX. CTR WING SPAR VERTICAL PRESS WEB IN MLG WW AT FUSELAGE STATION 663.75, IS CRACKED BETWEEN LBL 24 & 40 & BETWEEN RBL 31 & 40. REMOVED EXISTING TEMPORARY REPAIRS & ACCOMPLISHED PERMANENT REPAIR IAW SRM 57-10-10-2R-3 & EA 258587.Mar 25, 2016 · N916AN · Boeing 737823SDR COEA2016032425805Bulkhead · corrodedHEAVY CHECK COE & MAJOR REPAIR. FWD PRESS BULKHEAD FWD SURFACE HAS AREAS OF LEVEL 2 CORROSION. REPAIR IAW CE 1586 16 0184 DATED 5 3 2016.Mar 24, 2016 · N805HC · Aerosp ATR42500SDR REXA2016032400517Bulkhead · corrodedCORROSION OF FS 280.00 BULKHEAD LOWER INBD CORNER AT LBL 12 & RBL 12. REPAIRED DAMAGE TO FS 280 BULKHEAD LOWER INBD CORNERS AT LBL 12 & RBL 12 IAW EA CR953-04133 REV 1R DATED 03 16 16 & REPLACED CLIPS IAW SRM 51-42-06-001-001-A01.Mar 24, 2016 · N924XJ · Cndair CL6002D24SDR SWAA2016032850213Pressure Panel · crackedRIGHT MAIN WW CRACKED AT BS 663, RBL 43. REPAIRED WW IAW EA.Mar 24, 2016 · N7737E · Boeing 7377BDSDR REXA2016032300489Bulkhead · crackedFS 202 BULKHEAD CRACKED AROUND PARKING BRAKE CABLE PASS THROUGH HOLE. REMOVED CRACK BY PERFORMING CUT OUT OF DAMAGE & FABRICATING & INSTALLING ALL REPAIR PARTS IAW REO 601R-53-11-563.Mar 23, 2016 · N8976E · Cndair CL6002B19SDR FQAR20160323013Bulkhead · crackedDURING INSPECTION, A BULKHEAD DOUBLER IN THE EMPENNAGE WAS FOUND CRACKED. THE DEFECT WAS VISIBLE BY REMOVING A FAIRING THAT JOINS THE EMPENNAGE AND VERTICAL FIN AND LOOKING UP AND AFT. THE DOUBLER HAD 4 CRACKS. THEY WERE LOCATED BESIDE THE TOP, OTBD RIVETSMar 23, 2016 · N302PA · Piper PA44180SDR SWAA2016032950382Pressure Panel · crackedRIGHT MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN RBL 40 - 45.64. REPAIRED WEB IAW SRM.Mar 22, 2016 · N920WN · Boeing 7377H4SDR WVER2016032000016Bulkhead Web · corrodedFS 280 LOWER AFT BULKHEAD WEB, RT SIDE CORRODED. REPAIRED IAW REO 670-53-11-594, REV A.Mar 21, 2016 · N911FJ · Cndair CL6002D24SDR REXA2016031800482Bulkhead · crackedREAR PRESS BULKHEAD HAS A CRACK AT THE UPPER INBD EDGE OF THE LINTEL FITTING. REPAIRED REAR PRESS BULKHEAD AT LISTED FITTING IAW REO 601R-53-61-1230 REV F.Mar 18, 2016 · N8976E · Cndair CL6002B19SDR WVER2016031800004Post · crackedDURING INCORPORATION OF SB 670BA-53-044, NDT FOUND INDICATION OF CRACKS APPROXIMATELY. .125" ON FWD SIDE OF FS 202.75 BULKHEAD, AT THE TOP OF STIFFENER POSTS, LBL 30 AND RBL 30. REPAIRED LT AND RT POST'S IAW REO 670-53-11-1138, REV, DATED 2016-03-11.Mar 18, 2016 · N506MJ · Cndair CL6002C10SDR DALA2016032502328Bulkhead · crackedBS 1022, RT PYLON SUPPORT BULKHEAD, STRINGER 6R CRACKED. BULKHEAD REPAIRED IAW SRM 53-00-05, REP 2.Mar 17, 2016 · N954AT · Boeing 717200SDR AALA201605039010Pressure Deck · crackedAIRCRAFT IN BASE MX. CRACK INDICATIONS ON FASTENER HOLE H10L OF CORNER BRACKET OF PRESS DECK MEMBRANE, UPPER SURFACE IN THE FWD CARGO COMPARTMENT AT FRAME 36, BETWEEN +Y1292 & +Y1523. REPAIRED IAW EA 258985.Mar 16, 2016 · N651AW · Airbus A320232SDR AALA201605039009Pressure Deck · crackedAIRCRAFT IN BASE MX. CRACK INDICATIONS ON FASTENER HOLE H1L OF CORNER BRACKET OF PRESS DECK MEMBRANE, UPPER SURFACE IN THE FWD CARGO COMPARTMENT AT FRAME 36, BETWEEN +Y1292 & +Y1523. REPAIRED IAW EA 258985.Mar 16, 2016 · N651AW · Airbus A320232SDR AALA201605039008Pressure Deck · crackedAIRCRAFT IN BASE MX. CRACK INDICATIONS ON FASTENER HOLE H5R OF CORNER BRACKET OF PRESS DECK MEMBRANE, UPPER SURFACE IN THE FWD CARGO COMPARTMENT AT FRAME 36 & BETWEEN -Y1292 & -Y1523. REPAIRED IAW EA 258977.Mar 16, 2016 · N651AW · Airbus A320232SDR SWAA2016041250801Bulkhead · crackedAFT PRESS BULKHEAD WEB CRACKED AT BS 1016, RBL 2.5. REPAIRED WEB IAW EA.Mar 16, 2016 · N767SW · Boeing 7377H4SDR SWAA2016040150740Bulkhead · crackedAFT PRESS BULKHEAD WEB CRACKED AT BS 1016, BETWEEN STRINGER 7R - 15R. REPAIRED WEB IAW EA.Mar 16, 2016 · N767SW · Boeing 7377H4SDR COEA2016031534911Bulkhead · chafedHEAVY CHECK COE/MAJOR REPAIR: FWD PRESSURE BULKHEAD UPPER LT FORWARD SURFACE HAS LEVEL 2 CORROSION. REPAIRED IAW SRAS CE-1460/16, 10247 DATED 5/23/2016.Mar 15, 2016 · N911FX · Aerosp ATR42300SDR COEA2016031508911Bulkhead · damagedHEAVY CHECK COE & MAJOR REPAIR. FWD PRESS BULKHEAD WEB FWD HAS FRETTING. UPPER LT INBD BONDING POINT LEVEL 2 DOUBLER REPAIR AT FRAME 1 IAW SRM 531110-300-803-A01.Mar 15, 2016 · N911FX · Aerosp ATR42300SDR COEA2016031507911Bulkhead · damagedHEAVY CHECK COE & MAJOR REPAIR. FWD PRESS BULKHEAD WEB, FWD SURFACE HAS FRETTING, UPPER RT INBD BONDING POINT LEVEL 2. DOUBLER REPAIR AT FRAME 1 IAW SRM 531110-300-803-A01.Mar 15, 2016 · N911FX · Aerosp ATR42300SDR COEA2016031503911Bulkhead · corrodedHEAVY CHECK COE & MAJOR REPAIR. FWD PRESS BULKHEAD FWD SURFACE, LOWER RT INBD BONDING POINT HAS FRETTING. LEVEL 2 CORROSION CORRECTIVE ACTION. DOUBLER REPAIR SRM 531110-300-808-A01.Mar 15, 2016 · N911FX · Aerosp ATR42300SDR COEA2016031502911Bulkhead · corrodedHEAVY CHECK COE & MAJOR REPAIR. FWD PRESS BULKHEAD, LOWER LT INBD BONDING POINT HAS FRETTING AT LOWER LT CORNER. LEVEL 2 CORROSION CORRECTIVE ACTION. DOUBLER REPAIR SRM 531110-300-808-A01.Mar 15, 2016 · N911FX · Aerosp ATR42300SDR WVER2016031500015Fitting · mislocatedWHILE PERFORMING SB 670BA-53-044, REV-C, REINFORCEMENT OF THE LT AND RT SIDES OF THE FS 202.75 BULKHEAD, 1-OFF EXISTING HOLE IN FUSELAGE SKIN WILL FALL ON EDGE OF MACHINED REBATE AND 2-OFF EXISTING HOLE IN BULKHEAD WILL FALL CLOSE TO MACHINED RADIUS IN FITTINGMar 15, 2016 · N911FJ · Cndair CL6002D24SDR 2016FA0000134Firewall · buckledDURING ANNUAL INSPECTION, FOUND LOWER FIREWALL BUCKLED ON RT SIDE NEAR NLG REINFORCEMENT PLATE.Mar 15, 2016 · N5110Q · Cessna 172SDR WVER2016031591112Bulkhead · damagedWHILE PERFORMING SB 670BA-53-044, REV-C, REINFORCEMENT OF THE LT AND RT SIDES OF THE FS 202.75 BULKHEAD, 1-OFF EXISTING HOLE IN FUSELAGE SKIN WILL FALL ON EDGE OF MACHINED REBATE AND 2-OFF EXISTING HOLE IN BULKHEAD WILL FALL ON MACHINED RADIUS IN FITTING. PN:Mar 15, 2016 · N911FJ · Cndair CL6002D24SDR FQAR20160314012Doubler · crackedDURING INSPECTION, A BULKHEAD DOUBLER IN THE EMPENNAGE WAS FOUND CRACKED. THE DEFECT WAS VISIBLE BY REMOVING A FAIRING THAT JOINS THE EMPENNAGE AND VERTICAL FIN AND LOOKING UP AND AFT. THE DOUBLER HAD 2 CRACKS; THEY WERE LOCATED BESIDE THE TOP, OTBD RIVETS, Mar 14, 2016 · N317PA · Piper PA44180SDR WVER2016031300011Stiffener · crackedFWD SIDE OF BULKHEAD AT FS 202.75, FOUND INDICATION ON TOP OF STIFFENER AT RBL30.00 APPROXIMATELY .1250" LONGERON STIFFENER FAILED NDT.Mar 13, 2016 · N911FJ · Cndair CL6002D24
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