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.
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
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 SWIA201127964Bulkhead · crackedC-CHECK, CRACK NOTED AND MARKED ON FS 621 BULKHEAD WEB, FORWARD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING. REPAIRED PER REO.SDR RU3A1119Bulkhead · buckledBULKHEAD AND AIRCRAFT SKIN AT FORWARD FUSELAGE STATION 235 IS CRACKED AND BUCKLED.SDR ASOA201101747Bulkhead · crackedREAR PRESSURE BULKHEAD FWD FACE IS CRACKED ABOVE LINTEL ATTACH POINT AREA. REPAIRED IAW 601R-53-61-1230.SDR COMA2011091550069Bulkhead · crackedREAR PRESSURE BULKHEAD CRACKED AT LINTEL ATTACHMEMT AREA. REMOVED DAMAGE AREA OF REAR BULKHEAD AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1230 AND REO 601R -53-61-4190.SDR COMA2011091550068Bulkhead · dentedREAR PRESSURE BULKHEAD DENTED AND GOUGED JUST INBOARD OF CONNECTOR J257. REMOVED DAMAGE AREA OF REAR BULKHEAD JUST ABOVE LINTEL FITTING AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-4190.SDR 29GA94653091411ABulkhead · crackedDURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED BULKHEAD CRACKED FS 163 STRINGER 9R STARTING AT STRINGER CLEARANCE RADIUS 1.5 INCHES. STOPPPED DRILLED CRACKED AND INSTALLED DOUBLER REPAIR.SDR ASOA201101737Isolator · crackedCARGO COMPARTMENT AFT PRESSURE BULKHEAD MOUNTING ISOLATOR CRACKED. R & R CRACKED ISOLATOR IAW SRM 51-40-11. MINOR REPAIR.SDR ASOA201101735Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .3" IN LENGTH 90 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD WEB IAW REO 601R-53-61-1541.SDR SWIA201127708Bulkhead · crackedC-CHECK, FS 621 AFT PRESSURE BULKHEAD AFT WEB CRACKED NEAR CARGO DOOR TRACK UPPER ATTACH POINT. REPAIR PER REO.SDR REXA201100552Bulkhead · crackedFS 621.0 PRESSURE BULKHEAD HAS A SCREW MARK AT RBL 27 APPROX .002D. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.SDR REXA201100551Bulkhead · crackedFS 621.0 PRESSURE BULKHEAD HAS A SCREW MARK AT RBL 36 APPROX .002D. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.SDR AALA20110916TUL01Bulkhead · corrodedCORROSION ON STATION 1088 BULKHEAD LOWER SIDE OF AUXILIARY POWER UNIT INLET BOX. INSTALLED FILLER TO LOWER SECTION OF APU INLET AT STATION 1088 PER AARD 51-00-05.SDR ASOA201101721Isolator · brokenBROKEN ISOLATOR ON REAR PRESSURE BULKHEAD FWD FACE AT RBL 42.9 APPROX 26" ABOVE FLOOR. R & R ISOLATOR IAW SRM 51-42-13. REPAIR IS CLASSIFIED AS A MINOR REPAIR.SDR REXA201100550Bulkhead · crackedFS 559 SEMI-PRESSURE BULKHEAD FOUND CRACKED. REPAIR IAW BOMBARDIER REO 601R-53-41-260 REV E AND 601R-53-41-609 REV B.SDR SWIA201127722Bulkhead · crackedC-CHECK, FS 202 PRESSURE BULKHEAD CRACKED AT BRAKE CUTOUT. REPAIR PER REO.SDR SWAA2012071605816Bulkhead · crackedLEFT MLG WHEEL WELL FWD BULKHEAD BELOW "A" SYSTEM PRESSURE MODULE CRACKED. REPAIRED BULKHEAD IAW EA.SDR SWAA116563Bulkhead · crackedDURING SCHEDULED 24Y CHECK FOUND, AFT PRESSURE BULKHEAD DOME WEB CRACKED AT BS 1016, STR 7R. REPAIRED WEB IAW EO.SDR SWIA201127606Bulkhead · crackedFS 621 PRESSURE BULKHEAD FORWARD WEB FACE ABOVE UPPER CARGO DOOR TRACK FITTING IS CRACKED. (C-CHECK) REPAIR PER REO.SDR SWIA201127605Bulkhead · crackedFS 559 PRESSURE BULKHEAD CRACKED AT LEFT SIDE. (C-CHECK) REPAIR PER REO.SDR ASOA201101676Isolator · brokenISOLATOR AT 18LBL 21.5 " FROM FLOOR IS BROKEN ON CABIN SIDE OF PRESSURE BULKHEAD. R & R ISOLATOR IAW SRM CH 51-42-13. R & R ISOLATOR IAW SRM 51-42-13. THIS IS A MINOR REPAIR.SDR REXA201100548Bulkhead · damagedFS 559.0 BULKHEAD RT WEB FAILS NDT WITH AN INDICATION NOTED AT RBL 9 WL 54.10 AND RBL 18 WL 59.10 APPROX .10 INCH IN LENGTH AND 78 PERCENT FSH. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 REV E, REO 601R-53-41-609 REV B, DEVIATION "E" BSC STANDARD REPAIRS 601RSDR USAA2011091100012Pressure Panel · crackedC1 CHECK - CRACKED PRESSURE WEB OVER THE LEFT MAIN LANDING GEAR WHEEL WELL AT BS 664 AND LBL 40. REPAIRED PRESSURE WEB OVER THE LEFT MAIN LANDING GEAR WHEEL WELL AT BS 664 AND LBL 40 IAW EA 103335.SDR ASOA201101664Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD WEB DAMAGE IAW EC/TC 601R-53-61-1230.SDR NOCA08311Bulkhead · damagedDURING FLIGHT, AIRCRAFT JACK THAT WAS IN THE FWD CARGO PIT SLID BACK AND IMPACTED THE AFT BULKHEAD THERE WAS DAMAGE ON THE ANGLE ASSEMBLY, SUPPORT BRACKET, SUPPORT TEE, STUB FRAME, BLOWOUT PANEL, STANCHION - REMOVED DAMAGED PARTS ACCOMPLISHED DETAILED VISUAL ISDR REXA201100547Fitting · crackedAFT PRESSURE BULKHEAD LINTEL FITTING FOUND CRACKED AT FS 621. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.SDR SWIA201127608Bulkhead · crackedFS 621 BULKHEAD CRACKED AT FORWARD FACE UPPER LINTEL FITTING INTERFACE. (C-CHECK) REPAIRED PER REO.SDR IPXA11669256Failsafe · crackedINSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FTG WAS FOUND 1EA FASTENER HOLE CRACKED AT FAIL SAFE STRAP ON 4 & 10 O/C POSITION THROUGH THICKNESS. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FTG FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-ISDR IPXA11669252Failsafe · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG WAS FOUND 1EA FASTENER HOLE CRACKED AT FAIL STRAP ON 2 O/C POSITION THROUGH THICKNESS FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG FAIL SAFE STRAP REPLACED IAW EO NR B767-5350-17922-I, APPSDR DALA1152229018Pressure Panel · crackedDURING PSV IN MSP, MAINTENANCE NOTED 2.4 INCH LONG CRACK COMMON TO THE CANTED PRESSURE PANEL JAMB PAN LOCATED AT STA 69. THE CRACK IS LOCATED IN THE LOWER RADIUS OF THE VERTICAL LEG OF THE PAN. PERMANENT REPAIR INSTALLED PER ER/A 494540-14.SDR SWIA201127483Bulkhead · crackedDURING C-CHECK, FS 559 BULKHEAD CRACKED ON LEFT AND RIGHT SIDES. REPAIRED PER REO.SDR IPXA11669255Failsafe · crackedINSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FTG FAIL SAFE STRAP AREA SUSPECT CRACK FOUND, REMOVE FASTENER FOR NDT CONFIRMATION. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP AT MOST LOWER FASTENER REMOVED AND REINSTALLED IAWSDR IPXA11669251Failsafe · crackedINSPECTION TYPE: C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP AREA SUSPECT CRACK FOUND, REMOVE FASTENER FOR NDT CONFIRMATION. FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP AT MOST LOWER FASTENER. R & R IAW EO NR B767-5SDR SWIA201127542Bulkhead · crackedFS 202 PRESSURE BULKHEAD IS CRACKED AT PARKING BRAKE CABLE FITTING. (SERVICE) REPAIRED PER REO.SDR SWIA201130345Bulkhead · crackedC-CHECK, CRACK ON FS 621 BULKHEAD WEB, FORWARD FACE, AT LINTEL FITTING TO WEB INTERFACE. REPAIRED IN REFERENCE TO REO.SDR DALA1152536309Bulkhead · brokenA BROKEN WEB WAS FOUND ON BULKHEAD OF FORWARD CARGO COMPARTMENT STA 720 LBL 7. S: 0.5"X0.7. REPAIRED THE WEB PER ER/A 495575-14 REV 0.SDR SWIA201127478Bulkhead · crackedFS 621 AFT PRESSURE BULKHEAD WEB AT UPPER AFT CARGO TRACK WEB. (C-CHECK) REPAIR PER REO.SDR ASOA201101626Isolator · brokenAFT BULKHEAD, LT SIDE HAS A BROKEN ISOLATOR. R & R BROKEN ISOLATOR IAW SRM 51-42-13.SDR LR7A2011082900225Bulkhead · crackedDURING SCHEDULED B-1 CHECK IAW JOB CARD HB5302, FOUND T-ANGLE AND BULKHEAD WEB CRACKED AT FS 990, RBL 63, WL 266. REPAIR ACCOMPLISHED BY REPLACEMENT IAW DWG 353042 AND SMP583 53-50-04.SDR 2011FA0000551Bulkhead · crackedDURING POST FLIGHT VISUAL CHECK, THE MECHANIC NOTICED EVIDENCE OF A CRACK IN THE TAILCONE LT BULKHEAD FRAME AFT OF ENGINE CARRY-THROUGH BEAM AT FS 367.48. THE CRACK WAS VERY SMALL IN THE RADIUS. R & R BY DIRECT REPLACEMENT WITH NEW PART FROM MFG.SDR FDEA201108283532Bulkhead · crackedCENTER LANDING GEAR WHEEL WELL RT BULKHEAD FWD SIDE, FOUND DOUBLER CRACKED AT BS 1391. NEW DOUBLER INSTALLED PER SRM 51-31-01, REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.SDR SWIA201127406Bulkhead · crackedFS 559 BULKHEAD CRACKED AT LEFT SIDE. (C-CHECK) REPAIR PER REO.SDR ASOA201101610Bulkhead · crackedCRACK INDICATION NOTED AT LBL 36.20, WL 79.0, FS 621. REAR PRESSURE BULKHEAD WEB APPROX .50 IN LENGTH. VERTICALLY AT HEEL LINE 100 PERCENT FULL SCREEN HEIGHT. FAILED NDT. REPAIRED IAW REO 601R-53-1285.SDR REXA201100540Bulkhead · crackedFS 559.00 BULKHEAD FAILS NDT WITH AN INDICATION ON RIGHT WEB RBL 18 AND RT CAP ANGLE RBL 9 GREATER THAN 50 PERCENT FSH. REPAIRED FS 559.00 BY CUTTING OUT DAMAGE, FABRICATING PARTS, & INSTALLING FABRCATED PARTS IAW BOMBARDIER REO 601R-53-41-260 REV E. DATED 0SDR SWIA201127405Bulkhead · crackedFS 559 BULKHEAD CRACKED AT LEFT AND RIGHT SIDES. (C-CHECK) REPAIR PER REO.SDR ASOA201101602Bulkhead · crackedCRACK ON BS 202 BULKHEAD. FABRICATED REPAIR DOUBLER IAW REO 601R-53-11-563, REPAIR 2 AND INSTALLED REPAIR IAW REO 601R-53-11-2177 P1 AND REO 601R-53-11-563.SDR SWAA116031Pressure Panel · crackedDURING SCHEDULED 22Y CHECK, FOUND PRESSURE DECK WEB CRACKED BETWEEN BS 665 TO BS 675, BETWEEN RBL 35 TO RBL 45. REMOVED AND REPLACED WEB PER SRM.SDR SWIA201129062Bulkhead · crackedFS 202 BULKHEAD CRACKED AT EMERGENCY BRAKE CABLE. (C-CHECK) REPAIRED PER REO.SDR UALA2011082404528Pressure Deck · corrodedCORROSION ON PRESSURE DECK FROM 1681 TO 1685 RBL 10 - RBL 55. MAJOR REPAIR ACCOMPLISHED: PRESSURE DECK AT STATION 1681-1685 RBL 10 - RBL 55 PER THE INSTRUCTIONS ON PEMCO PD57-53-173 WITHOUT DEVIATION. A FAA FORM 8100-9 DATED AUG 18TH 2011 WAS RECEIVED AND THISDR VNAA2011082400020Bulkhead · damagedDURING SCHEDULED MAINTENANCE DAMAGE WAS FOUND ON PRESSURE BULKHEAD AT FS 621.0. THE PRESSURE BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.SDR SIMA201123503Bulkhead · corrodedDURING MAINTENACE BASE VISIT FOUND CORROSION ON RIGHT WEB. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT WEB IAW AE EO-53MR-174 AND CRJ SRM 51-42-06 AND 51-42-13. THE AIRCRAFT WAS RETURNED TO SERVICE.
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