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 COMA2009102650197Bulkhead · crackedFWD PRESSURE BULKHEAD AT FS 202.75 IS CRACKED AROUND PARKING BRAKE CABLE. REPAIRED CRACK AT FS 202.75 IAW REO 601R-53-11-1773.Oct 23, 2009 · N967CA · Cndair CL6002B19SDR SWAA096801Pressure Panel · crackedDURING SCHEDULED 2HC1 CHECK, FOUND LT WHEEL WELL PRESSURE DECK WEB CRACKED AT BS 664, LBL 33. REPAIRED WEB PER SRM.Oct 22, 2009 · N630WN · Boeing 7373H4SDR A6WA200940708Pressure Blkhd · crackedLT LOWER NOSE HYD COMPARTMENT AT FS 202.75, BL 23.71, WL 69.984, PRESSURE BULKHEAD CRACKED AT PARKING BRAKE LOCATION. LT LOWER NOSE HYD COMPARTMENT AT FS 202.75, BL 23.71, AND WL 69.984 CRACK REPAIRED IAW REO 601R-53-11-1789. (K)Oct 21, 2009 · N469AW · Cndair CL6002B19SDR A6WA200940747Bulkhead · crackedAFT PRESSURE BULKHEAD WEB ABOVE CARGO DOOR TRACK IS CRACKED AT FS 621, LBL 27.5, WL 130. CUT OUT ON DAMAGE PORTION OF WEB ABOVE CARGO DOOR TRACK AT FS 621, LBL 27.5, WL 130. NDT PERFORMED ON CUT OUT WET INSTALLATION OF PIECES IAW REO 601R-53-61-1541, REV B. Oct 20, 2009 · N411ZW · Cndair CL6002B19SDR SWIA200922984Fitting · gougedTHE 9G BULKHEAD FITTINGS GOUGED. (C CHECK) REPAIRED PER REO.Oct 20, 2009 · N986CA · Cndair CL6002B19SDR A6WA200940721Bulkhead · crackedFS 621.00 AFT PRESSURE BULKHEAD LT CRACKED AT LINTEL/LOCATION W/L 106.117 (.100 LONG). FS 621.00 AFT PRESSURE BULKHEAD LT CRACK AT LINTEL FITTING LOCATION W/L 106.117. REPAIRED IAW REO 601R-53-61-1230, REV D. (K)Oct 19, 2009 · N469AW · Cndair CL6002B19SDR ASOA200901173Bulkhead · crackedLEFT FS 280 WEB HAS CRACK AND CORRODED. REMOVED LT FS 280 LOWER BULKHEAD WEB IAW SRM 51-42-06-001-001-A01. DRILLED UP NEW FS 280 LOWER LT WEB IAW SRM 51-40-11-001-001-A01. OK TO INSTALL NEW WEB AS PER SRM 51-42-06 PG 1 - PG 17Oct 19, 2009 · N758EV · Cndair CL6002C10SDR ASOA200901168Bulkhead · crackedSUSPECT FS 202.00 BULKHEAD TO BE CRACKEDOct 19, 2009 · N825AS · Cndair CL6002B19SDR A6WA200940746Pressure Blkhd · crackedREAR PRESSURE BULKHEAD WEB IS CRACKED AT THE LINTEL LOCATION FS 621, LBL 46, WL 110. CUT OUT ON WEB AT FS 621, LBL 46, WL 110 NDT PERMORMED ON CUTO OUT, WET INSTALLATION OF ALL PIECES FABRICATED IAW REO 601R-53-61-1230, REV D. (K)Oct 16, 2009 · N411ZW · Cndair CL6002B19SDR SWIA200922990Fitting · crackedFS 621 BULKHEAD LINTEL FITTING CRACKED. (C CHECK) REPAIRED PER REO.Oct 16, 2009 · N431SW · Cndair CL6002B19SDR ASOA200901149Bulkhead Web · cracked5 INDICATIONS NOTED ON FS 559.0 BULKHEAD WEB AND CAP ANGLE AS LISTED: (1) 100 PERCENT FSH, 1 INCH LONG IN WEB AT RBL 18.0 WL 59.10 (2) 75 PERCENT FSH 0.25 INCH LONG IN WEB APPROX 1 INCH OTBD OF RBL 9.0 WL 59.70 (3) 50 PERCENT FSH, 0.5 INCH LONG IN WEB AT RBL 9Oct 16, 2009 · N830AS · Cndair CL6002B19SDR 2009F00094Bulkhead · damagedCUSTOMER SERVICE AGENT STEPPED ON BOTTOM STEP OF PASSENGER DOOR, WITHOUT THE A/C TAIL-STAND IN PLACE. A/C TAIL CONTACTED GROUND, DAMAGING AFT BULKHEAD AND TAIL TIE-DOWN ASSY.Oct 15, 2009 · N861MA · Cessna 208BSDR LR7A2009101900137Bulkhead Web · crackedDURING SCHEDULED B-2 CHECK IAW JOB CARD HB5302, FOUND AFT FUSELAGE INTERIOR UPPER BHD WEB CRACKED AT FS946, WL265, LBL50. REPAIRED IAW SRM SMP583 FIG 51-140-12. NR 2039Oct 15, 2009 · N402LC · Lkheed 382GSDR LR7A2009101900135Bulkhead Web · crackedDURING SCHEDULED B-2 CHECK IAW JOB CARD HB3200, FOUND LT MAIN WHEEL WELL BULKHEAD WEB CRACKED AT FS577, WL200, LBL76. REPAIRED IAW LAC MEA 382-53-09-031.Oct 15, 2009 · N402LC · Lkheed 382GSDR LR7A2009101900132Tee Fitting · crackedDURING SCHEDULED B-2 CHECK IAW JOB CARD HB5302, FOUND AFT FUSELAGE INTERIOR BHD INNER CAP CRACKED AT FS792, WL175, RBL85. REPAIRED IAW SRM SMP583 FIG 53-50-14. NR 2020Oct 15, 2009 · N402LC · Lkheed 382GSDR LR7A2009101900131Tee Fitting · crackedDURING SCHEDULED B-2 CHECK IAW JOB CARD HB5302, FOUND AFT FUSELAGE INTERIOR LT SIDE BULKHEAD INBD TEE CAP CRACKED AT FS946, WL260, LBL64. REPAIRED BY FABRICATING AND REPLACING TEE CAP IAW SRM SMP583 FIG 53-50-04 AND CHAP 51-60 AND 51-70.Oct 15, 2009 · N402LC · Lkheed 382GSDR ASOA200901142Isolator · crackedJOB 8723611 OPERATION 223/621 PRESSURE BULKHEAD FWD SIDE HAS TWO CRACKED ISOLATORS, ONE AT LBL 36 BELOW WL 97.50 AND ONE AT RBL 36 ABOVE WL 97.50.Oct 15, 2009 · N830AS · Cndair CL6002B19SDR SWIA200923725Bulkhead · crackedFS 621 BULKHEAD CRACKED AT LINTEL FITTING INTERFACE. (C CHECK) REPAIRED PER REO.Oct 14, 2009 · N431SW · Cndair CL6002B19SDR SWIA200923724Bulkhead · crackedBULKHEAD WEB AT FS 559 CRACKED. (C CHECK) REPAIRED PER REO.Oct 14, 2009 · N431SW · Cndair CL6002B19SDR SWIA200923528Bulkhead · gougedFS 280 RIGHT SIDE BULKHEAD GOUGED. (C CHECK) REPAIRED PER REO.Oct 14, 2009 · N988CA · Cndair CL6002B19SDR SWIA200923527Isolator · crackedFIVE CRACKED ISOLATORS ON AFT PRESSURE BULKHEAD FS 621. (C CHECK) REPLACED PER SRM.Oct 14, 2009 · N988CA · Cndair CL6002B19SDR SWAA096595Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND BULKHEAD UPPER CHORD CRACKED AT BS 178, LBL 24. REMOVED AND REPLACED CHORD PER BAC DWG.Oct 14, 2009 · N367SW · Boeing 7373H4SDR FDEA200910143563Doubler · corrodedSTA 1860 UPPER BULKHEAD LWR SURFACE DRAIN HOLE RBL 13" DOUBLER CORRODED. STA 1860 UPPER BULKHEAD LWR SURFACE DRAIN HOLE CORRODED DOUBLER. REMOVED AND REPLACED IAW SRM 51-40-02. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Oct 14, 2009 · N934FD · Boeing 75721BSDR A6WA200940709Bulkhead · crackedPILOT BULKHEAD AT FS 280.00, RBL 11.00 FOUND (2) GOUGES BTWN STR 13A AND 14A (SIZE 2.75" L X .230" W X .020 DEEP) EACH. REPAIR PERFORMED ON PILOT BULKHEAD AT FS 280.00, RBL 11.00 IAW REO 601R-53-11-1727, REV C. (K)Oct 13, 2009 · N469AW · Cndair CL6002B19SDR SWAA096568Bulkhead · corrodedDURING SCHEDULED 24Y CHECK, FOUND BULKHEAD CHORD CORRODED AT BS 1016, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED CHORD PER SRM.Oct 13, 2009 · N689SW · Boeing 7373Q8SDR SWAA096506Pressure Panel · crackedDURING SCHEDULED OTS CHECK, FOUND PRESSURE DECK WEB CRACKED AT BS 664, LBL 26.97. REPAIRED WEB PER EA.Oct 13, 2009 · N347SW · Boeing 7373H4SDR SWIA200923480Bulkhead · gougedC-CHECK, FS 280 BULKHEAD GOUGED. REPAIRED PER REO.Oct 10, 2009 · N983CA · Cndair CL6002B19SDR USAA2009110292998Pressure Panel · crackedSAL - MAJOR REPAIR - BC7 CHECK - CRACKED PRESSURE PANEL AT FR 35 - FR 36, +Y1292. REPAIRED PRESSURE PANEL AT FR 35 - FR 36, +Y1292 IAW EO 5310-01008 AND TASK CARD M2C53306.Oct 9, 2009 · N621AW · Airbus A320231SDR USAA2009110292997Pressure Panel · crackedSAL - MAJOR REPAIR - BC7 CHECK - CRACKED PRESSURE PANEL AT FR 35 - FR 36, -Y1292. REPAIRED PRESSURE PANEL AT FR 35 - FR 36, -Y1292 IAW EO 5310-01008 AND TASK CARD M2C53307.Oct 9, 2009 · N621AW · Airbus A320231SDR QXEA2009101200773Bulkhead · corrodedLT AND RT FS 280.00 BULKHEAD WEBBING SHOWS SIGNS OF CORROSION. RT 280 BEAM PREVIOUSLY REMOVED. REMOVED AFFECTED FASTENERS AT CORRODED SECTION AND BLENDED LIGHT SURFACE CORROSION. BLEND DEPTH AT .005 DEEP, WITHIN LIMITS IAW SRM 53-11-10 PG 201 REPAIR "A". OROct 9, 2009 · N609QX · Cndair CL6002C10SDR ASOA200901113Bulkhead · crackedFOUND CRACK AT PARKING BRAKE CABLE AT FS 202.75 AT BL 23.71 PRESSURE BULKHEAD. WORK COMPLETED IAW EC/TC REO 601R 53-11-1785.Oct 8, 2009 · N927EV · Cndair CL6002B19SDR COMA2009100950195Bulkhead · crackedFWD PRESSURE BULKHEAD AT FS 202.75 IS CRACKED AROUND PARKING BRAKE CABLE. REPAIRED CRACK AT FS 202.75 IAW REO 601R-53-11-1773.Oct 8, 2009 · N924CA · Cndair CL6002B19SDR IPXA09M57847Doubler · damagedINSPECTION TYPE:2/C REPAIR SURVEY SEQ NR 287-F2-01 AT APPROX STA 1401, X=75 AND X=85 ON LT MLG HORIZONTAL PRESSURE BULKHEAD IS NOT IN MD11 SRM. REPAIRED AS PER IPXA EO NR MD11 5320-35408-A AND SAA EA NR 011-5330-01-A2083 ISSUE A, REF IPXA RCD NR 366112.Oct 7, 2009 · N287UP · Doug MD11FSDR IPXA09M57839Pressure Panel · damagedINSPECTION TYPE:2C REPAIR SURVEY SEQUENCE NR 287-F2-02 AT APPROX STA 1501 X=35 AND X=45 ON LT MLG HORIZONTAL PRESSURE WEB IS NOT IN MD-11 SRM. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR IAW SAA EA 011- 5330-01-A2074-A AND IPXA EO MD11-5330-35362-A.Oct 7, 2009 · N287UP · Doug MD11FSDR A6WA200940687Bulkhead · crackedFWD PRESSURE BULKHEAD FS 202.75, LBL 23.71, WL 69.7, CRACKED AT PARKING BRAKE LINE LOCATION (CRACK LENGTH 1.500") FWD PRESSURE BULKHEAD FS 202.75, LBL 23.71, WL 69.7. REPAIRED AT PARKING BRAKE IAW REO 601R-53-11-563. (K)Oct 6, 2009 · N408AW · Cndair CL6002B19SDR SWAA096370Bulkhead · crackedDURING SCHEDULED MV3 CHECK, FOUND MLG FWD UPPER BULKHEAD WEB CRACKED AT BS 663.75, RBL 42. REPAIRED WEB PER SWA EA.Oct 5, 2009 · N769SW · Boeing 7377H4SDR SWAA096344ABulkhead · crackedDURING SCHEDULED MV3 CHECK, FOUND MLG FWD UPPER BULKHEAD WEB CRACKED AT BS 663.75, RBL 42. REPAIRED WEB PER EA.Oct 5, 2009 · N769SW · Boeing 7377H4SDR TIPR20090025Pressure Blkhd · dentedDURING A MX INSP (C-CHECK), A DENT WAS FOUND ON THE AFT PRESSURE BULKHEAD (DOME WEB) AT BS 1269 RBL 20, DENTED. REPAIRED IAW SRM 53-80-08 FIG.201 REPAIR 2.Oct 5, 2009 · N769VA · Boeing 767222SDR ASOA200901095Bulkhead · crackedFOUND FS 559 BULKHEAD WEB HAS 2 INDICATIONS NOTED: 1) RT WEB I/B OF RBL 18, WL 59.10 INDICATION NOTED APPROX. .5" IN LENGTH, 100% FSH, 2) RT WEB O/B OF RBL 9, WL 54.10 APPROX. .2" IN LENGTH, 50% FSH, AND FOUND FS 559 LT CAP ANGLE HAS INDICATION NOTED APPROX. .Oct 3, 2009 · N838AS · Cndair CL6002B19SDR USAA2009100592699Doubler · crackedPIT - FPBH - MAJOR REPAIR - CRACKS AROUND EXISTING TOOLING HOLES ON VERTICAL BEAM DOUBLER AT BS 180, WL 190, RBL 5.7. REPAIRED VERTICAL BEAM DOUBLER AT BS 180, WL 190, RBL 5.7 IAW US AIRWAY EA 113646.Oct 3, 2009 · N430US · Boeing 7374B7SDR A6WA200940639Bulkhead · crackedFWD PRESSURE BULKHEAD IS CRACKED AT THE PARKING BRAKE LOCATION. FWD PRESSURE BULKHEAD AT THE PARKING BRAKE LOCATION REPAIRED IAW REO 601R-53-11-1772. (K)Oct 1, 2009 · N422AW · Cndair CL6002B19SDR A6WA200940662Pressure Blkhd · crackedCRACK FOUND AT FS 202.75, LBL 23.71 ON PRESSURE BULKHEAD AT PARKING BRAKE LOCATION. AT FS 202.75, LBL 23.71 ON PRESSURE BULKHEAD AT PARKING BRAKE LOCATION. REPAIR CARRIED OUT IAW REO 601R-53-11-563. (K)Oct 1, 2009 · N468AW · Cndair CL6002B19SDR ASOA200901072Pressure Blkhd · crackedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS A INDICATION NOTED APPROX .1 INCH IN LENGTH, 60 PERCENT FSH. FAILED NDT INSP. REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETE AND THE REPAIR C/W THE REQUIREMENTS OF EC/Oct 1, 2009 · N876AS · Cndair CL6002B19SDR SWAA096241Pressure Panel · crackedDURING SCHEDULED 12Y CHECK, FOUND NOSE WHEEL WELL CEILING SNUBBER CUTOUT SKIN WEB CRACKED AT RBL 7.75. REPAIRED WEB PER ACO.Oct 1, 2009 · N656SW · Boeing 7373H4SDR SWAA096240Pressure Panel · crackedDURING SCHEDULED 12Y CHECK, FOUND NOSE WHEEL WELL CEILING SNUBBER CUTOUT SKIN WEB CRACKED AT LBL 7.75. REPAIRED WEB PER ACO.Oct 1, 2009 · N656SW · Boeing 7373H4SDR SWAA096235Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STR 15R. REPAIRED BULKHEAD PER SRM.Oct 1, 2009 · N511SW · Boeing 7375H4SDR CALA2009100100581Bulkhead · canningEA 5310-04639 REV A OIL CANNING AT AFB BS 1016 BETWEEN STR ONE AND TWO RBL 11 APPROX FROM BL 0 APB BS 1016. REPAIRED PER ECRA 5311-01466. ACCOMPLISH INITIAL HFEC INSP OF THE APBH REPAIR PER ECRA PART 2 TABLE 1 PRIOR TO 36000 FLT CYC FROM WHEN REPAIR WAS INSTOct 1, 2009 · N14250 · Boeing 737824SDR A6WA2009410677Bulkhead · crackedCRACK FOUND ON AFT PRESSURE BULKHEAD AT FS 621.00, LBL 27.50, W/L 130.0 (UPPER END OF CARGO TRACK). REPAIR PERFORMED ON AFT PRESSURE BULKHEAD AT FS 621.00, LBL 27.50, W/L 130.00. PERFORMED IAW REO 601R-53-61-1541.Sep 30, 2009 · N468AW · Cndair CL6002B19SDR A6WA200940669Bulkhead · gougedGOUGES FOUND ON PILOT BULKHEAD AT FS 230.00, WL 94.00, RBL 10, (700" X 2.00", .052 " DEEP AND .300, .200, .020 DEEP). REPAIR PERFORMED ON PILOT BULKHEAD AT FS 280 WL 94.00, RBL 10 IAW REO 601R-53-11-1727 REV C. (K)Sep 30, 2009 · N468AW · Cndair CL6002B19SDR A6WA200940675Bulkhead · crackedAFT PRESSURE BULKHEAD AT FS 621.00 FOUND CRACKED AT LINTEL FITTING LOCATION (.250 LONG). AFT PRESSURE BULKHEAD FS 621.00 AT LINTEL LOCATION REPAIR PERFORMED IAW REO 601R-53-61-1230. (K)Sep 29, 2009 · N468AW · Cndair CL6002B19
Back to JASC 5312