JASC 5312

Service difficulty reports · 20,047

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 04FDEA00569Bulkhead · corrodedFWD NOSE WHEEL WELL BULKHEAD FWD SIDE HAS A CORRODED STRAP. REMOVED CORRODED STRAP. STRAP FOUND TO BE AN EXISTING REPAIR. FABRICATED REPAIR IAW DC10 SRM 53-00-01 VOL 1. INSTALLED IAW DC10 SRM 51-33-01 VOL 2, CORROSION FOUND TO BE LEVEL 2.Mar 4, 2004 · N302FE · Doug DC1030FSDR C2XA04SH138Firewall · crackedSHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT HAND UPPER SUPPORT ARM MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 3, 2004 · N26549 · Emb EMB145LRSDR C2XA04SH135Firewall · crackedSHV-DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT HAND UPPER APU SUPPORT ARM MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 2, 2004 · N26549 · Emb EMB145LRSDR USAA040031Stiffener · corrodedPIT - FOUND STIFFENER CORRODED, BS 1016 APBH CHANNEL STIFFENER RIGHT SIDE BOTTOM. CORRODED SECTIONS REPLACED PER EO 5302V112. (M)Feb 28, 2004 · N356US · Boeing 737301SDR AWXA200400335Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-12 CHECK A .5 INCH CRACK WAS FOUND AT LIGHTNING HOLE IN BS 178 BULKHEAD VERTICAL WEB BEAM RBL 5, WL 195. MAINTENANCE REMOVED CRACKED SECTION OF BS 178 BULKHEAD VERTICAL WEB BEAM AT RBL 5, WL 195; FABRICATED A NEW REPLACEMENT SECTFeb 28, 2004 · N328AW · Boeing 7373B7SDR AWXA200400257Vertical Beam · crackedLCQ - MAJOR REPAIR - DURING C-12 CHECK .5 INCH CRACK WAS FOUND AT LIGHTNING HOLE ON VERTICAL BEAM WEB AFT SIDE OF BS 178 BULKHEAD LBL 5.7, WL 195. MAINTENANCE REMOVED VERTICAL BEAM WEB AFT SIDE OF BS 178 BULKHEAD LBL 5.7, WL 195; FABRICATED A NEW REPLACEMENT Feb 28, 2004 · N328AW · Boeing 7373B7SDR USAA040030Bulkhead · corrodedPIT - FOUND REAR PRESS BULKHEAD CORRODED 2 INCHES BY 4 INCHES, STATION 1016 BL 0 REAR PRESSURE BULKHEAD. CORRODED SECTIONS REPLACED PER EO 5302V112. (M)Feb 27, 2004 · N356US · Boeing 737301SDR C2XA04SH121Firewall · crackedSHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT AND RIGHT UPPER APU MOUNTS. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 27, 2004 · N12552 · Emb EMB145LRSDR HALA0400278Bulkhead · crackedDURING 2A CHECK, TWO CRACKS MEASURING 2.0 INCHES AND 1.5 INCHES WERE FOUND ON THE CANTED FRAME REAR SPAR BULKHEAD AT STA 1178.225 AT LONGERON 17L, IN THE CAPS FORWARD FLANGE. REPAIR IN WORK.Feb 26, 2004 · N484HA · Boeing 717200SDR SWAA040620Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND PRESSURE BULKHEAD CRACKED AT BS 1016, LAP SPLICE 3 AND LAP SPLICE 4. REPAIRED BULKHEAD PER ER.Feb 26, 2004 · N302SW · Boeing 7373H4SDR SWAA040607Bulkhead · crackedDURING SCHEDULED PM CHECK, FOUND BULKHEAD WEB CRACKED AT BS 727, LBL 13.5 AND LBL 14.5, 25 BELOW CEILING IN MAIN WHEEL WELL. REPAIRED WEB PER EA.Feb 26, 2004 · Boeing 7372H4SDR 2004UALA00166Bulkhead · damagedNEED REPAIR TO BS 178 FWD BULKHEAD. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB ON FWD BULKHEAD AT BS 178, LBL 5.7, WL 212.Feb 24, 2004 · N904UA · Boeing 737522SDR SWAA040564Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 5.7. REPAIRED WEB PER SRM.Feb 23, 2004 · N319SW · Boeing 7373H4SDR SWAA040545Bulkhead · crackedDURING SCHEDULED SPV, FOUND WEB CRACKED AT BS 178, WL 235 AND LBL 8, LBL 9, LBL 10 AND LBL 12.5. REPAIRED WEB PER SRM.Feb 21, 2004 · Boeing 7372H4SDR SWAA040531Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND WING CENTER SECTION BEADED WEB CRACKED AT RBL 38. REPAIRED WEB PER SRM.Feb 20, 2004 · N319SW · Boeing 7373H4SDR 04FDEA00495Bulkhead · puncturedWHILE WORKING FED EX WORK CARD, PUNCTURED BULKHEAD BS 227 LBL 21 WL 187. REPAIRED PUNCTURED BULKHEAD BS 227, LBL 21, WL 187 IAW SRM 51-40-2, 51-30-2 AND 51-10-2.Feb 20, 2004 · N234FE · Boeing 727200SDR DL73S040177Bulkhead · canningTHE GORE WEB OF THE AFT PRESSURE DOME AT FS 1016 WAS FOUND WITH AN OIL CAN CONDITION BETWEEN STRINGER 2R & 3R NEAR THE OUTER -Y- CHORD OF THE DOME. THE OIL CAN WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 088605-14.Feb 19, 2004 · N380DL · Boeing 737247SDR SWAA040512Bulkhead · crackedDURING SCHEDULED SPV, FOUND WEB CRACKED AT BS 178, LBL 9 TO LBL 11, WL 234. REPAIRED WEB PER SRM.Feb 18, 2004 · N363SW · Boeing 7373H4SDR UJJ2004F00000Adapter · crackedWHILE INVESTIGATING CABIN PRESSURE LEAKS, IT WAS FOUND THAT BOTH AFT PRESSURE BULKHEAD RUDDER CARRY THROUGH SEAL ADAPTERS WERE CRACKED IN SEVERAL PLACES. THESE ADAPTERS ARE MADE OF THERMOFORMED (ABS) PLASTIC, RIVETED INTO PLACE USING A METAL DOUBLER, AND HAVEFeb 17, 2004 · N160SF · Beech 200BEECHSDR AMWA121Bulkhead · crackedTHREE CRACKS WERE FOUND IN FWD BULKHEAD FROM A SINGLE RIVET. CRACKS WERE APPROXIMATELY 1/2" OR SHORTER. PERFORMED EDDY CURRENT INSPECTION AND REPAIRED CRAKCS BY INSTALLING DOUBLER AND SHIME IN ACCORDANCE WITH RAYTHEON AIRCRAFT FR- CO-01004Feb 13, 2004 · N26YV · Beech 1900DSDR USAA040003Bulkhead · crackedPIT - FOUND FORWARD BULKHEAD WEB CRACKED .5 INCH, 178 BULKHEAD WEB AT UPPER LEFT RADAR ANTENNA MOUNT. REPAIRED PER DRAFT EA 77664, PATCH, PER SRM 53-10-08 FIG 211. (M)Feb 12, 2004 · N519AU · Boeing 7373B7SDR USAA04000CBulkhead · crackedFOUND FORWARD BULKHEAD CRACKED .5 INCH, 178 BULKHEAD WEB AT UPPER RIGHT RADAR ANTENNA MOUNT. REPAIRED PER DRAFT EA 77664, PATCH PER SRM 53-10-08 FIG 211. (M)Feb 12, 2004 · N519AU · Boeing 7373B7SDR LR7A04029Pressure Panel · corrodedDURING SCHEDULED B2 INSPECTION PER JOB CARD HB3202 RIGHT MLG BAY SIDE WALL (PRESSURE PANEL) SKIN CORRODED AT FS 537. REPAIRED IAW SMP583 FIG 53-40-10, FS 537 WL 156 RBL 62.Feb 12, 2004 · N401LC · Lkheed 382GSDR SWAA040450Bulkhead · corrodedDURING SCHEDULED D CHECK, FOUND CORROSION ON WEB AT BS 1016, FWD SIDE OF BULKHEAD. REPAIRED WEB ER.Feb 12, 2004 · N309SW · Boeing 7373H4SDR SWAA040447Pressure Panel · crackedDURING SCHEDULED SERVICE CHECK, FOUND CRACK IN NOSE WHEEL WELL UNDER RT FWD NOSE PANEL BS 243. REPAIRED WEB PER EA.Feb 12, 2004 · Boeing 7372H4SDR DL73S040152Bulkhead · corrodedCORROSION WAS NOTED AT BS 1016 PRESSURE BLKHD, AT BL 0 AND AFFECTED THE WEB/GORE AND CHANNEL STIFFENERS. REPAIRED PER ERA 386069-14AD.Feb 12, 2004 · N319DL · Boeing 737232SDR SWAA040443Bulkhead · crackedDURING SCHEDULED C1 CHECK, FOUND BULKHEAD WEB CRACKED AT BS 1016, BETWEEN STRINGER 3R AND STRINGER 5R. REPAIRED WEB PER EA.Feb 11, 2004 · N675AA · Boeing 7373A4SDR AKG2004F00003Bulkhead · damagedIN COMPLETING AD, NOT ONLY WAS SCORING FOUND ACROSS THE MID SPAN, BUT ALSO ALL THE WAY AROUND WHERE THE (U) FRAME LAYS ON TOP OF THE BULKHEAD WEB. THERE IS NOT A PATCH REPAIR FOR THIS. THE BULKHEAD WEB WILL HAVE TO BE REPLACED.Feb 10, 2004 · N447AC · Beech B200SDR AKG2004F00002Bulkhead · damagedIN COMPLETING AD, NOT ONLY WAS SCORING FOUND ACROSS THE MID SPAN, BUT ALSO ALL THE WAY AROUND WERE THE (U) FRAME LAYS ON TOP OF THE BULKHEAD WEB. THERE IS NOT A PATCH REPAIR FOR THIS. THE BULKHEAD WEB WILL AVE TO BE REPLACED.Feb 10, 2004 · N911CX · Beech C90SDR CALA0400094Bulkhead · corrodedINSPECTION FOUND FORWARD SIDE OF AFT PRESSURE BULKHEAD LEFT AND RIGHT OF CENTER STIFFENER (APB DOME WEB) CORRODED AT STA 1016, BL 0. A REPAIR DOUBLER WAS INSTALLED IAW BOEING DRAWING 65C28106.Feb 9, 2004 · N14347 · Boeing 7373T0SDR CALA0400093Stiffener · corrodedINSPECTION FOUND FORWARD SIDE LOWER AFT PRESSURE BULKHEAD CENTER CHANNEL STIFFENER CORRODED AT BS 1016-1025, BL 0. STIFFENERS AND SPLICES WERE INSTALLED IAW BOEING DRAWING 65C28106.Feb 9, 2004 · N14347 · Boeing 7373T0SDR 04FDEA00375Bulkhead · corrodedCORROSION, AFT CARGO BAY, CORROSION ON 1183 BULKHEAD BS 1183 LBL 2 WL 153. *S/D* REMOVED BS 1183 BL 0 (I) BEAM. FABRICATED AND INSTALLED NEW (I) BEAM IAW FED EX EA 7-5310-70618 & SRM 51-30-2.Feb 9, 2004 · N237FE · Boeing 727200SDR SWAA040406Bulkhead · corrodedDURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD WEB AT BS 1016, LBL 2 TO RBL 2. REPAIRED WEB PER ACO.Feb 8, 2004 · N604SW · Boeing 7373H4SDR SWAA040405Stiffener · corrodedDURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD CHANNEL STIFFNERS AT BS 1016, BL 0. REPAIRED PER ACO.Feb 8, 2004 · N604SW · Boeing 7373H4SDR SWAA040389Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, RBL 45. REPAIRED WEB PER SRM.Feb 7, 2004 · N695SW · Boeing 7373Q8SDR AUS20040103Bulkhead · corroded(AUS) FUSELAGE BULKHEAD CORRODED IN AREA BENEATH VERTICAL FIN FRONT ATTACHMENT PLATE AND STRINGER HAT ASSEMBLY ATTACHMENT AREA.Feb 5, 2004 · Piper PA28161SDR 0400306730Panel · crackedDURING L-CHECK FOUND CRACK IN CANTED PRESSURE DECK CLOSURE PANEL AT BS 1241. REPAIRED PER EA 67-165097.Feb 5, 2004 · N630US · Boeing 7472J9FSDR LR7A04026Bulkhead · crackedDURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND FS 617 BULKHEAD AT WL 210 EXISTING REPAIR CRACKED AT LBL 60. REPAIRED IAW SMP583 FIG 53-40-10, FS 617 WL 200 - 210 LBL 63-73.Feb 5, 2004 · N403LC · Lkheed 382GSDR SWAA040356Bulkhead · corrodedDURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CORRODED AT BS 1016, RBL 1. REPAIRED WEB PER AD.Feb 4, 2004 · Boeing 7372H4SDR SWAA040343Bulkhead · crackedDURING SCHEDULED SPV, FOUND 2 EACH CRACKS ON WEB AT BS 178, WL 217, LBL 11 AND AT BS 178, WL 207, LBL 24. REPAIRED WEB PER SRM.Feb 3, 2004 · N361SW · Boeing 7373H4SDR AUS20040120Structure · cracked(AUS) REAR PRESSURE BULKHEAD CLEAT LOCATED AT STRINGER 7L AND BULKHEAD BEAM AT STRINGER 6L CRACKED. FOUND DURING INSPECTION IAW AD.Feb 2, 2004 · Beech 200BEECHSDR SWAA040335Bulkhead · crackedDURING SCHEDULED SPV, FOUND WEB CRACKED AT BS 178, WL 227, LBL 11. REPAIRED WEB PER SRM.Feb 2, 2004 · N361SW · Boeing 7373H4SDR DL73S040131Bulkhead · canningTHE WEB OF THE FS 1016 AFT P-DOME WAS FOUND WITH AN OIL-CAN CONDITION BETWEEN S-3L & S-5L. THE DAMAGED AREA OF WEB WAS CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 088351-14AD.Jan 31, 2004 · N309DL · Boeing 737232SDR SWAA040322Bulkhead · crackedDURING SCHEDULED SPV, FOUND WEB CRACKED AT BS 178, LBL 1, WL 186.5. REPAIRED WEB PER SRM.Jan 31, 2004 · N361SW · Boeing 7373H4SDR UPS04441925Strap · crackedINSPECTION TYPE:C BS 1241 RIGHT BULKHEAD SPLICE STRAP AFT HOLE CRACK FOUND RUNNING AFT APPROX .125 INCH. AFT BOLT HOLE REPAIRED AS PER RS R53-41-35107 BS 1241 RIGHT BULKHEAD SPLICE STRAP WILL BE REPLACED WITHIN 2 YEARS AFTER CRACK DISCOVERY AS PER EO B747-531Jan 29, 2004 · N672UP · Boeing 747123SDR ABXA040059Stiffener · crackedAFT PRESSURE BULKHEAD FORWARD RIGHT STIFFENER, 4TH FROM TOP, WAS CRACKED AT TEE. REPAIRED AREA IAW DC-9 SSRM K05159.Jan 28, 2004 · N962AX · Doug DC941SDR UPS04441923Strap · crackedINSPECTION TYPE:C BS 1241 LEFT BULKHEAD SPLICE STRAP AFT HOLE FOUND CRACKS AT FWD AND AFT SIDE. BS 1241 LEFT BULKHEAD SPLICE STRAP WILL BE REPLACED WITHIN 2 YEARS AFTER CRACK DISCOVERY AS PER EO B747-5310-0323 PARA D (3).Jan 25, 2004 · N672UP · Boeing 747123SDR LR7A04018Tee Fitting · crackedDURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND FS 477 CABIN OVERHEAD BULKHEAD TEE CRACK AT BL 0-8R. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-22, FS 477 WL 285 LBL 8 - LBL 10.Jan 24, 2004 · N402LC · Lkheed 382GSDR LR7A04007Cap · crackedDURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND HAIRLINE CRACK RT MWW INTERCOSTAL BEAM O/B CAP AT FS 479 WL 200. BEAM CAP REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 479 WL 200 RBL 62.Jan 24, 2004 · N402LC · Lkheed 382GSDR LR7A04004Cap · crackedDURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND FS 479 WL 200 LT INTERCOSTAL BEAM BROKEN/CRACKED THROUGH. BEAM CAP (TEE) REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 479 WL 200 LBL 62.Jan 24, 2004 · N402LC · Lkheed 382G
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