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 DLM88091076Strap · damagedP-DOME: EXTERNAL STRAP REPAIR IAW 09-086680-12. C/W 09-086680-12 ME13Feb 18, 2009 · N966DL · Doug MD88SDR DLM88091074Strap · damagedP-DOME: EXTERNAL STRAP & DRAIN HOLE BUSHING REPAIR IAW 09-093855-03. C/W 09-093855-03 ME01Feb 18, 2009 · N966DL · Doug MD88SDR A6WA200940074Bulkhead · crackedCRACK FOUND ON FWD PRESSURE BLKHD AT FS 202.75, LBL 23.71 AROUND THE PARKING BRAKE CABLE FWD PRESSURE BLKHD REPAIRED IAW REO 601R-53-11-563. (K)Feb 18, 2009 · N421ZW · Cndair CL6002B19SDR USAA2009050491080Bulkhead · corrodedMCN - C24 - MAJOR REPAIR - INTERGRANULAR CORROSION ON AFT PRESSURE BULKHEAD SKIN AT BS 1016 BETWEEN S27L TO S27R. REPAIRED AFT PRESSURE BULKHEAD CENTER STIFFENERS AT BS 1016 BETWEEN S27L TO S27R IAW US AIRWAYS EA 130234.Feb 17, 2009 · N175AW · Boeing 73733ASDR SWAA091172Bulkhead · crackedDURING SCHEDULED SPV CHECK FOUND, VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER SRM.Feb 17, 2009 · N606SW · Boeing 7373H4SDR SWIA200921330Pressure Blkhd · crackedDURING C-CHECK, FS 559 PRESSURE BULKHEAD CRACKED. REPAIRED PER REO.Feb 15, 2009 · N864AS · Cndair CL6002B19SDR SWIA200921328Pressure Blkhd · crackedDURING C-CHECK, AFT PRESSURE BULKHEAD CRACKED AT LINTEL FITTING. REPAIRED PER REO.Feb 15, 2009 · N864AS · Cndair CL6002B19SDR AALA20090707TUL18Pressure Panel · corrodedPRESSURE DECK CORRODED. REPAIRED IAW EA B757-53-005461.Feb 13, 2009 · N614AA · Boeing 757223SDR ASOA200900199Bulkhead · corrodedRIGHT FS 280 BULKHEAD LOWER WEB HAS SURFACE CORROSION. BLENDED RT WEB TO WITHIN LIMITS CONDITION IAW SRM 53-11-10.Feb 11, 2009 · N751EV · Cndair CL6002C10SDR ASOA200900193Pressure Panel · crackedFS 460 PRESSURE FLOOR BETWEEN BL 0.0 TO RBL 9.0 HAS INDICATION NOTED 2.8" IN LENGTH FAILED NDT INSP. COMPLIED WITH FS 460 PRESSURE WEB REPAIR IAW REO 601R-53-41-884.Feb 10, 2009 · N848AS · Cndair CL6002B19SDR SWAA091062Bulkhead · crackedDURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER SWA EA.Feb 10, 2009 · N642WN · Boeing 7373H4SDR SWAA091047Stiffener · crackedDURING SCHEDULED 16Y CHECK, FOUND MLG BULKHEAD VERTICAL STIFFENER CRACKED AT BS 727, LBL 6. REMOVED AND REPLACED STIFFENER PER SRM.Feb 10, 2009 · N520SW · Boeing 7375H4SDR SWAA091046Stiffener · crackedDURING SCHEDULED 16Y CHECK, FOUND MLG BULKHEAD VERTICAL STIFFENER CRACKED AT BS 727, RBL 6. REMOVED AND REPLACED STIFFENER PER SRM.Feb 10, 2009 · N520SW · Boeing 7375H4SDR ABXA200903130014Bulkhead · crackedDURING C-CHECK INSPECTION, FOUND LWW BULKHEAD STA 1065 HAD BULGE AT LOWER HYDRAULIC FITTING LBL 70. FOUND CRACK ON STRUCTURE UNDER FITTING. BULKHEAD REPAIRED IAW B767 SRM 51-70-13 FIG 1. CRACK REQUIRED CUTOUT AND DOUBLER. CUT OUT CRACK AND FABRICATED DOUBLFeb 9, 2009 · N797AX · Boeing 767281SDR SWAA091007Pressure Panel · damagedDURING SCHEDULED 16Y CHECK, FOUND NOSE WHEEL WELL CEILING WEB DAMAGED AT BS 277, RBL 16. REPAIRED WEB PER EA.Feb 9, 2009 · N520SW · Boeing 7375H4SDR ASOA200900176Bulkhead · cracked2 INDICATIONS NOTED ON FWD SIDE OF FS 621.0 PRESSURE BULKHEAD WEB, ABOVE AND BELOW LINTEL FITTING. INDICATION ABOVE FITTING IS APPROX .2" IN LENGTH AT 80% F.S.H. INDICATION BELOW FITTING IS APPROX .2" IN LENGTH AT 100% F.S.H. FAILED NDT INSPECTION. REPAIR PFeb 7, 2009 · N848AS · Cndair CL6002B19SDR A6WA200940057Bulkhead · crackedAFT PRESSURE BULKHEAD AT FS 621.00 AT THE LINTEL LOCATION CRACKED. REPAIRED IAW REO 601R-53-61-1230, REV D. (K)Feb 6, 2009 · N454AW · Cndair CL6002B19SDR COMA2009021050079Floor Skin · crackedPRESSURE FLOOR SKIN IS CRACKED IN THREE PLACES BETWEEN LBL 9 AND RBL 9 AT FS 460.00. REMOVED DAMAGE AND APPLIED A TEMPORARY REPAIR PER CRJ REO 601R-53-41-103 REV (D).Feb 6, 2009 · N590SW · Cndair CL6002B19SDR ASOA200900174Bulkhead · crackedSEMI PRESSURE BULKHEAD WEB FS 559.00 HAS HFEC INDICATION NOTED AT RBL 18 WL 59.10 INDICATION IS APPROX 1.5" LONG AND 100% FULL SCREEN HEIGHT. FAILS NDT INSPECTION. SEMI PRESSURE BULKHEAD WEB FS 559.00 HAS HFEC INDICATION NOTED AT RBL 18 WL 59.10 INDICATION IFeb 6, 2009 · N848AS · Cndair CL6002B19SDR QXEA2009021000099Pressure Panel · gougedPDX - C5- LT MLG WHEEL WELL HAS GOUGE ON AFT SKIN EDGE AT APPROX 5 INCH FROM FUSELAGE OUTBOARD. REMOVED SHARP EDGES AND BLENDED IAW CRJ SRM 51-12-06-101-001-A01. MATERIAL REMOVAL NEGLIGIBLE (<.002 INCH) WITHIN LIMITS PER SRM TASK 57-51-01-101-001-A01 TABFeb 6, 2009 · N603QX · Cndair CL6002C10SDR C8GA20090027Bulkhead · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RIGHT WHEEL WELL BS 870 BULKHEAD WEB CRACKED AT LOCK FASTENER LOAD CONTROL VALVE CUTOUT RBL 10. REMOVED DAMAGE, FABRICATED FILLERS FROM 2024 T3 .063 INCH AT AFT UPPER DIM 1.425 INCH BY .5Feb 5, 2009 · N357KP · Boeing 727230SDR ASOA200900170Bulkhead · corrodedLT 280 WEB CORRODED ON AFT SURFACE. LT 280 WEB REMOVED AND REPLACED PER SRM 51-42-06 AND 51-42-21. REMOVED LT LOWER WEB STRUCTURE AND STRAP IAW SRM 53-11-10 AND 51-42-06. LOCATED HOLES IN AFT FACE OF LOWER WEBS IAW SRM 51-42-06. FINISHED LOCATING HOLES IN Feb 5, 2009 · N753EV · Cndair CL6002C10SDR ASOA200900169Bulkhead · corrodedRT FS280 BULKHEAD LOWER WEB HAS SURFACE CORROSION. REMOVED AND REPLACED RT FS 280 WEB PER SRM 51-42-06 AND 51-42-21. REMOVED RT FS 280 LOWER WEB. DRILLED RT FS 280 LOWER WEB PER SRM 51-42-06. FINAL SIZED ALL HOLES IN RT 280 WEB PER SRM 51-42-06 AND 51-40-1Feb 5, 2009 · N753EV · Cndair CL6002C10SDR ASOA200900168Bulkhead · corrodedLT FS280 BULKHEAD LOWER WEB HAS SURFACE CORROSION.Feb 5, 2009 · N753EV · Cndair CL6002C10SDR SWIA200921268Bulkhead · crackedFS 559 PRESSURE BULKHEAD CRACKED AT RBL 9 WS 54.1 (C CHECK). REPAIRED PER REO.Feb 3, 2009 · N930SW · Cndair CL6002B19SDR SWIA200921265Isolator · crackedCRACKED ISOLATOR ON AFT BULKHEAD FS 621 (C CHECK). REPAIRED PER SRM.Feb 3, 2009 · N930SW · Cndair CL6002B19SDR AALA2009020900031Bulkhead · damagedFASTENER MISDRILLED AT AFT PRESSURE BULKHEAD THIRD FASTENER INBOARD AT THREE O’CLOCK POSITION. REPAIRED DAMAGED AREA OF BULKHEAD IN ACCORDANCE WITH ESO 61000 DATED 29 JAN 2009.Feb 3, 2009 · N907AN · Boeing 737823SDR A6WA200940064Pressure Blkhd · crackedCRACK FOUND ON PRESSURE BULKHEAD FS 202.75 AT BL 36.71 AROUND PARKING BRAKE CABLE. CRACK ON PRESSURE BULKHEAD FS 202.75 AT LBL 36.71 REPAIRED IAW REO 601R-53-11-563. (K)Feb 3, 2009 · N447AW · Cndair CL6002B19SDR A6WA200940055Bulkhead · crackedCRACK FOUND ON PILOT BULKHEAD FS 280, RBL 9. REPAIR TO PILOT BULKHEAD CARRIED OUT IAW REO 601R-53-11-171, REV D. (K)Feb 3, 2009 · N447AW · Cndair CL6002B19SDR AALA2009020900022Bulkhead · canningAFT PRESSURE BULKHEAD OIL CANNING JUST AFT OF STA 1016 APPROX 3 O`CLOCK, 6 INCH BY 6 INCH AREA. REPAIRED DAMAGED AREA OF BULKHEAD PER ESO 61000 DATED 29 JAN 09.Feb 3, 2009 · N907AN · Boeing 737823SDR SWAA090795Pressure Panel · crackedDURING SCHEDULED 12Y CHECK, FOUND LT WHEEL WELL UPPER PRESSURE WEB CRACKED AT BS 665, BETWEEN LBL 13 TO LBL 33. REPAIRED WEB PER SRM.Feb 3, 2009 · N643SW · Boeing 7373H4SDR DLM88090270Bulkhead · dentedHIDDEN DAMAGE, DENT, ON AFT P DOME. REMOVED DAMAGE IAW SRM 53-05 FIG 115. REPAIR PARTS INSTALLED IAW EA 09-086680-12 ME 06.Feb 2, 2009 · N976DL · Doug MD88SDR SWIA200921320Pressure Blkhd · crackedC-CHECK, AFT SIDE OF PRESSURE BULKHEAD HAS NUMEROUS CRACKS. REPAIRED PER REO.Jan 30, 2009 · N405SW · Cndair CL6002B19SDR SWIA200921319Bulkhead · crackedC-CHECK, FS 621 AFT PRESSURE BULKHEAD CRACKED. REPAIRED PER REO.Jan 30, 2009 · N405SW · Cndair CL6002B19SDR QXEA2009020200059Bulkhead · corrodedPDX - C2 - SEVERAL AREAS OF CORROSION ON LT LOWER BULKHEAD AFT SIDE AT FS 280. REMOVED THE CORROSION IN THE REQUIRED AREAS IAW CRJ REO 670-53-11-052. UT THICKNESS CHECKED BLENDED AREAS IAW CRJ 700 NDTM 51-00-04, MIN REMAINING THICKNESS .037 INCH. ALODINED AJan 30, 2009 · N619QX · Cndair CL6002C10SDR ASOA200900145Bulkhead · crackedFWD PRESSURE BULKHEAD FS 202.75 HAS A CRACK AT PARKING BRAKE CABLE. REPAIRED CRACK NEAR PARKING BRAKE CABLE AT FWD PRESSURE BULKHEAD IAW REO 601R-53-11-563. COMPLIED WITH ECTC EO 600-53-217 C/W.Jan 29, 2009 · N850AS · Cndair CL6002B19SDR FDEA200901290379Pressure Panel · crackedLT MLG WHEEL WELL INBD WALL UPPER AFT CORNER HAS CRACK FROM STIFFENER GOING FWD TOWARD PREVIOUS REPAIR, VERIFIED AND MARKED USING ET, LOCATED ABOVE NR 1 HYD SYSTEM RESERVOIR COMPLIED WITH EA 8-5310-123830 TITLE, FUSELAGE-MAIN FRAME- KEEL STRUCTURE/UNDERWING BAJan 29, 2009 · N392FE · Doug MD1010FSDR ASOA200900184Bulkhead Web · crackedFS 559 WEB AND CAP ANGLE HAS INDICATIONS NOTED, LT CAP ANGLE AT LBL 18.0, APPROX .3" (100% FSH), AND RT WEB AT WL 59.10, APPROX 1.0" (90% FSH) AND RT WEB AT WL 54.10, APPROX .5" (70% FSH). ALL FAILED NDT INSPECTION. REPAIRED PRESSURE BULKHEAD STRUCTURE FS 559Jan 28, 2009 · N841AS · Cndair CL6002B19SDR USAA2009022390412Bulkhead · corrodedSAL - C21 - MAJOR REPAIR - GALVANIC CORROSION ON AFT PRESSURE BULKHEAD WEB SKIN AT BS 1016, LBL 6. REPAIRED AFT PRESSURE BULKHEAD WEB SKIN AT BS 1016, LBL 6 IAW US AIRWAYS EA 132273.Jan 26, 2009 · N332AW · Boeing 7373B7SDR AALA2009021100078Pressure Panel · crackedWHEEL WELL PRESSURE DECK CRACKED JUST AFT AND OUTBOARD UNDER CLIP ABOVE FUEL SHROUD LINE. INSTALLED DOUBLER ON PRESSURE DECK PER AARD 53-30-00-13.Jan 26, 2009 · N9420D · Doug DC983SDR A6WA200940040Bulkhead · crackedCRACK FOUND ON FWD PRESSURE BULKHEAD AT FS 202.75 LBL 23.71 AT THE PARKING BRAKE LOCATION. FWD PRESSURE BULKHEAD AT FS 202.75 LBL 23.71 REPAIRED IAW REO 53-11-1571.Jan 23, 2009 · N412AW · Cndair CL6002B19SDR A6WA200940039Bulkhead · crackedPILOTS BULKHEAD FS 280 LBL 9 RBL 9 AFT ANGLE CRACKED. PILOTS BULKHEAD AT FS 280 AFT ANGLE REPAIRED IAW REO 601R-53-11-136 REV A.Jan 23, 2009 · N412AW · Cndair CL6002B19SDR A6WA200940038Bulkhead · crackedPILOTS BULKHEAD CRACKED AT FS 280.00 RBL 9 AND LBL 9. PILOTS BULKHEAD AT FS 280.00 RBL 9 AND LBL 9 REPAIRED IAW REO 601R-53-11-171 REV D,Jan 23, 2009 · N412AW · Cndair CL6002B19SDR IPXA09855281Bulkhead · misrepairedINSPECTION TYPE:SV SS752-F3-12, PRESSURE BULKHEAD WEB REPAIR, FS 980 DOES NOT CORRELATE TO A SRM. REPAIRED PER TIMCO REO-G12528 REV C AND UPS EO DC8-5320-32803A.Jan 22, 2009 · N752UP · Doug DC871FSDR A6WA200940067Bulkhead · crackedCRACK FOUND ON PILOT BULKHEAD FS 280, RBL 9 JOB PERFORMED ON PILOT BULKHEAD FS 280, RBL 9 IAW REO 601R-53-11-171, REV "D" SCHEME "B". (K)Jan 21, 2009 · N451AW · Cndair CL6002B19SDR A6WA200940046Angle · crackedCRACK FOUND ON TOP ANGLE AFT FACE OF PILOT BULKHEAD FS 280 LBL 9. CRACK LENGTH IS 1.500. CUT OUT PERFORMED AND PART FABRICATED AND INSTALLED ON TOP ANGLE AFT FACE OF PILOT BULKHEAD FS 280 LBL P IAW REO 601R 53-11-138 REV NC.Jan 21, 2009 · N451AW · Cndair CL6002B19SDR UPS09554472Bulkhead · dentedINSPECTION TYPE:C3 DENT AT BS 1200 LBL 6 WL 146 BULKHEAD CLOSURE WEB. REMOVED, FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 53-00-53- 1A1, SRM 53-60-53-0I SRM 51-40-02.Jan 21, 2009 · N417UP · Boeing 75724APFSDR ASOA200900115Bulkhead · crackedLT AND RT FS 559 BULKHEAD WEB AND CAP ANGLE HAVE INDICATIONS AT CAP ANGLES LBL RBL 18 APPROX .3" IN LENGTH 90% FSH AND RT WEB AT WL 58.10 APPROX .2" IN LENGTH 60% FSH, WL 54.10 APPROX .5" IN LENGTH 80% FSH AND WL 59.10 APPROX 1.0" IN LENGTH 100% FSH. ALL THESJan 21, 2009 · N850AS · Cndair CL6002B19SDR SWAA090456Bulkhead · crackedDURING SCHEDULED 16Y CHECK, FOUND VERTICAL BEAM CRACKED AT BS 178, LBL 17. REPAIRED BEAM PER ACO.Jan 21, 2009 · N361SW · Boeing 7373H4SDR SWAA090454Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER ER.Jan 21, 2009 · N330SW · Boeing 7373H4
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