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.
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 UPS802562J Angle · crackedMAINTENANCE REPORTED 'J' ANGLE CRACKED ON AFT PRESS BULKHEAD. REPAIRED PER UPS EO DC8-5310-6746.SDR USAA950256Angle · crackedPIT - DURING SCHEDULED SIP INSPECTION, FOUND CRACK IN THE FORWARD PRESSURE BULKHEAD LOWER CONNECTION ANGLE AT FRAME 1550 BETWEEN STATION 72 AND 3. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 53-11-00. (W)SDR ASAA9510007Bulkhead · crackedSEA - DURING D-CHECK, LOWER OUTBOARD CHORD OF BS 727 BULKHEAD, RBL 38 AND 27 WAS FOUND CRACKED. REPAIRED PER EA 5310-01326 AND BOEING TELEX ASA-SEA-95-0111RR. (Z)SDR ASAA9510006Bulkhead · crackedSEA - DURING D-CHECK, THE LOWER OUTBOARD CHORD OF BS 727 BULKHEAD, LBL 27 AND 38 WAS FOUND CRACKED. REPAIRED PER EA 5310-01325 AND BOEING TELEX ASA-SEA-95-0111RR. (Z)SDR UPS802519Beam · cracked(SUPPLEMENTAL MRR) DURING 'B' CHECK, MAINTENANCE FOUND AFT BULKHEAD BOTTOM SIDE OF J4 BEAM CRACKED. STOP DRILLED CRACK, FABRICATED DOUBLER AND CLIPS AND INSTALLED PER UPS EO DC8-5310-6735-A.SDR UPS802518Beam · cracked(SUPPLEMENTAL MRR) DURING 'B' CHECK, MAINTENANCE FOUND AFT BULKHEAD TOP SIDE OF J4 BEAM CRACKED. STOP DRILLED CRACK, FABRICATED DOUBLER AND CLIPS AND INSTALLED PER UPS EO DC8-5310-6735-A.SDR ABXA9500126Blkhd T-Cap · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION ON STA 110 BULKHEAD IN NOSE WHEEL WELL RIGHT TUNNEL. REPAIRED STA 110 BULKHEAD IAW ABX REA D953-10960-MR.SDR UPS802517Beam · crackedDURING B-CHECK, MAINTENANCE FOUND NR 3 AND 4 'J' BEAM CRACKED AT AFT BULKHEAD. REPAIRED PER UPS EO DC8-5310-6715A.SDR MWEA95135Latch Fitting · crackedDURING SERVICE CHECK, FOUND AFT PRESSURE BULKHEAD PLUG DOOR LOWER LATCH FITTING BROKEN. REMOVED DAMAGED FITTING, INSTALLED NEW FITTING. A/C RETURNED TO SERVICE.SDR AWXA9500100Chord · corrodedPHX - FLT 1530 - DURING C7 INSPECTION, FOUND CORROSION ON INNER CHORD AT RT AFT LAV FORWARD BULKHEAD R2 DOOR AREA. REMOVED AND REPLACED CHORD PER SRM 51-10-02 AND 51-40-02. (Z)SDR UPS802410J-Beam · crackedDURING B CHECK, MAINTENANCE REPORTED NR 3 AND NR 4 J-BEAM AT AFT PRESSURE BULKHEAD CRACKED. INSTALLED REPAIR PER UPS EO DC8-5310-6715A.SDR 9502969992Bulkhead · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN UPPER HORIZONTAL PRESSURE PANEL IN THE NOSE LANDING GEAR WHEEL WELL FS 83, LBL 36. REPAIRED PER EA 99-093492.SDR USAA950227Beam · crackedPIT - DURING SCHEDULED STRUCTURES VISIT (SIP), FOUND 2 INCH CRACK IN AFT PRESSURE BULKHEAD HORIZONTAL BEAM III LOWER RADIUS AT CENTER OF BEAM. EDDY CURRENT REF SIP 53-10-03. STOP DRILLED CRACK ENDS AND INSTALLED REPAIR PATCH, REPAIR ANGLES (2EACH) AND REAR FSDR ABXA9500123Blkhd Web · corrodedDURING C-CHECK INSPECTION, FOUND BULKHEAD WEB AT STA 110 HAD LEVEL I CORROSION AT LONGERON 27R AT THE LOWER T-CAP. REPAIRED WEB IAW ABX REA D953-10960-MR.SDR 9502939992Bulkhead · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN BULKHEAD FS 1038 JUST ABOVE INTERCOSTAL AT LONGERON 13R. REPAIRED PER EA 99-093501.SDR UPS802411J Beam · crackedDURING 'B' CHECK, MAINTENANCE REPORTED AFT PRESSURE BULKHEAD 'J' BEAM CRACKED 4TH BEAM UP FROM BOTTOM. FABRICATED AND INSTALLED REPAIR PER UPS EO DC8-5310-6694.SDR DLL16951030Blkhd Frame · corrodedAT HMV, FOUND FRAME CORRODED ON P-DOME LOWER INBOARD SIDE JUST AFT OF WHERE STRINGER 25 ENDS. REPAIRED PER SRM 53-11-00 FIG 809.SDR DLL16951029Blkhd Frame · corrodedAT HMV, FOUND P-DOME FRAME CORRODED AT LOWER END OVER A 2FT SECTION. AT THE FORWARD SIDE OF P-DOME LEFT SIDE JUST AFT OF AFT CARGO AREA STRINGER 41. REPAIRED PER SRM 53-11-00 FIG 809.SDR UPS802356Beam · crackDURING 'B' CHECK MAINTENANCE FOUND AFT BULKHEAD CRACKED AT HORIZONTAL "J" BEAM SUPPORT, 3RD SUPPORT FROM BOTTOM. INSTALLED REPAIR IAW EO DC8-5310-6669A.SDR 95UAL747008Blkhd Cap · corrodedLEVEL 2 CORROSION FOUND IN BS 1350 BULKHEAD LOWER CAP PLATE ASSY AND FITTINGS AT BOTH LBL AND RBL 127, WL 160. REPAIRED CAP PLATE ASSEMBLY AND REPLACED FITTINGS.SDR 9502342284Blkhd Beam · crackedDURING PERIODIC CHECK, MAINTENANCE FOUND FS 1183 BULKHEAD VERTICAL BEAM AT RBL 36.83 CRACKED IN RADIUS. REPAIRED PER NWA EA 22-096683.SDR 9502529928Web · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND .5 INCH CRACK IN THE AFT PRESSURE BULKHEAD WEB, LEFT SIDE. REPAIRED PER EA 99-093485 AND EO 5310-01130.SDR UPS802358Web · crackedDURING 'B' CHECK, MAINTENANCE FOUND 3.5 INCH CRACK IN LOWER LEG OF J3 WEB OF AIRPLANE AFT PRESSURE BULKHEAD COMPARTMENT 60. STOP DRILLED CRACK, FABRICATED DOUBLER AND INSTALLED REPAIR.SDR TAOA029507Angle · corrodedDURING C-CHECK, BLKHD ANGLE AT BS 1183, LBRL 26.9 AND WL 207 WAS FOUND CORRODED ON THE I/B SIDE. FABRICATED NEW TENSION ANGLE PER BAC DRAWING 69-60242 AND INSTALLED PER BAC DRAWING 65-19606. (W)SDR 95FDEA00123Blkhd Web · crackPOSSIBLE CRACK AT BS 950 BULKHEAD LBL 40 WL 185. REPAIRED CRACK IS 950 BULKHEAD AT LBL 40 WL 185 PER FEDEX SRM 53-10-9 FIG 2.SDR UP202240Bulkhead · corrosionWHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FORWARD SIDE OF 870 BULKHEAD WEB AT TEARSTRAP ON MAIN LANDING GEAR BULKHEAD FROM, LBL 20 RBL 30 WL 160. INSTALLED REPAIR IAW SRM 53-10-9, 51-30-2 AND UPS EO 727-53-1462.SDR 9502259756Fitting · crackedDURING PERIODIC CHECK, FOUND CRACKS IN THE AFT PRESSURE BULKHEAD VAULT DOOR UPPER RIGHT STOP FITTING AND SILL. ALSO, FOUND A CRACK IN THE SILL AT THE UPPER LEFT DOOR STOP FITTING. REPLACED THE STOP FITTING AND REPAIRED THE SILL CRACKS PER SRM 53-05, FIG.30 ASDR UPS802203Bulkhead Web · crackedWHILE IN 'C' CHECK MAINTENANCE FOUND 1 INCH LONG CRACK ON PRESSURE BULKHEAD WEB AT FS 980, RBL 2.65. INSTALLED REPAIR IAW UPS EO DC8-53-1308.SDR DL72W950643Bulkhead Web · crackedBS 1183 BULKHEAD WEB CRACKED IN 4 PLACES AT RBL18. 1.0 INCH CRACK AT WL173, 0.5 INCH CRACK AT WL175, 1.25 INCH CRACK AT WL177, AND 1.0 INCH CRACK AT WL 179. CRACKS STOP DRILLED AND REPAIR DOUBLER INSTALLED. DAMAGE FOUND DURING LETTER CHECK, REPAIRED PER EARSDR CAL950123Bulkhead · corrodedBFM - INSPECTION FOUND CENTER MLG WHEELWELL AFT BULKHEAD CORRODED FROM LBL 31 TO RBL 31. THE BULKHEAD WAS REPAIRED IAW SRM 51-00. (X)SDR ABXA9500207Stiffener · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON STIFFENER ON AFT FACE OF CANTED BULKHEAD 1089 AT LONGERON 6 LEFT. REPLACED STIFFENER IAW DC-9 SRM CHAPTER 51-30-2.SDR ABXA9500206Stiffener · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON STIFFENER ON AFT FACE OF CANTED BULKHEAD 1089 AT LONGERON 8 LEFT. REPLACED STIFFENER IAW DC-9 SRM CHAPTER 51-30-2.SDR ABXA9500205Stiffener · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON STIFFENER ON AFT FACE OF CANTED BULKHEAD 1089 AT LONGERON 11 LEFT. REPLACED STIFFENER IAW DC-9 SRM CHAPTER 51-30-2.SDR 95ZZZX1100Bulkhead · crushedDURING A ROUTINE INSPECTION, NOTICED TAIL TIE-DOWN HOOK BROKEN AND SKIN CRUSHED IN THE SAME AREA. THIS CONDITION WAS CAUSED DURING LOADING FREIGHT AND ACFT FALLING ON TAIL. THE CRUSHED REAR BULKHEAD CONTAINS A LIGHTENING HOLE FOR THE ELEVATOR BELLCRANK AND PSDR USAA950189Blkhd Angle · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 36 INCH CORRODED AREA, STATION 947 BULKHEAD LOWER ATTACH ANGLE S-26 R TO S-26L. REPAIRED PER BOEING DRAWING NR PL 65-49616 REV LTR AND SHT 13 OF 73 ID NR 12. CORROSION TASK NR C53-208-01, CORROSION LESDR TSAA9553034Bulkhead Web · crackedDURING HEAVY MAINTENANCE VISIT, FOUND CRACK IN BULKHEAD WEB, DT 178, WL 185.0, RT LOWER NOSE COMPARTMENT. REPAIRED PER ECO 2518R1. AIRCRAFT RETURNED TO SERVICE. (X)SDR TSAA9553033Bulkhead Web · crackedDURING HEAVY MAINTENANCE VISIT, FOUND CRACK IN BULKHEAD WEB AT BS 178, WL 1850, LT LOWER NOSE COMPARTMENT. REPAIRED PER ECO 2518R1. AIRCRAFT RETURNED TO SERVICE. (X)SDR TSAA9553031Bulkhead Fitting · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND BULKHEAD-TO-FLOOR BEAM FITTING AT BBL '0' AND BS 727 CRACKED HORIZONTALLY ACROSS RADIUS OF FORWARD FLANGE, .75 INCH LONG. REPAIRED PER ECO 2331 PART I AND IV. AIRCRAFT RETURNED TO SERVICE. (X)SDR SWAA950170Blkhd Tee · crackedDURING SCHEDULED C3 CHECK, FOUND TWO CRACKS IN THE I/B AND O/B FWD TEE CHORDS AT BS 178 PRESSURE BULKHEAD, LBL 5.7. REPAIRED PER SWA RA 1-253-1240.SDR SWAA950169Blkhd Web · crackedDURING SCHEDULED CHECK, FOUND CRACKS IN THE FWD PRESSURE BULKHEAD WEB BETWEEN WL 184 TO 207, BS 178. REPAIRED PER SWA RA 1-253-1240.SDR SWAA950149Bulkhead · crackedDURING SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 178, WL 184, LBL 5.7, PRESSURE BULKHEAD, AT FASTENER HOLES. REPAIRED PER TRAMCO EWO 95-0119.SDR 95ZZZW222Door Jamb · crackedSTL - DURING C-CHECK, FOND A .875 INCH CRACK IN UPPER LEFT CORNER OF AFT PRESSURE BULKHEAD PASSENGER DOOR JAMB. STOP DRILLED CRACK AND REPAIRED PER S/B 53-137. TOTAL CYCLES 29,619.SDR ABXA9500233Blkhd Tee · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE STA 110 BULKHEAD LOWER TEE CAP. TEE CAP WAS REPAIRED IAW ABX REA D953-10867-MR.SDR USAA950182Bulkhead Skin · crackedINT -DURING Q-4 CHECK VISUAL INSPECTION, FOUND .75 INCH VERTICAL CRACK IN FORWARD PRESSURE BULKHEAD SKIN BS 178, BS 178 RBL 5, WL 200. REPAIRED PER T/R 53-10-07. (Z)SDR USAA950181Bulkhead Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .375 INCH VERTICAL CRACK IN FORWARD PRESSURE BULKHEAD SKIN (BS 178) BS 178, LBL 5, WL 200. REPAIRED PER T/R 53-10-07. (Z)SDR DLL16950472Frame Segments · crackedDURING AIRCRAFT HMV IN ATL, THE FRAME SEGMENTS ON THE AFT PRESSURE DOME BETWEEN S23 AND S44 WERE FOUND WITH CRACK IN THE LOWER FLANGE RADII. THE DAMAGE WAS TRIMMED OUT, SPLICE STRAPS WERE ADDED, AND THE REPAIR AREA WAS TREATED FOR CORROSION.SDR DL72S950691Channels · wornCHANNELS WORN FWD B/B AFT BULKHEAD TWO VERTICAL SUPPORT CHANNELS ARE WORN (LOC OVER STG 26L AND 26R) AT FLEX JOINTS. ALSO, RIVETS SHEARED LEFT SUPPORT AT CEILING. FOUND AT HMV, REPAIRED PER SRM 53-10-9 FIG 8, REPLACED RIVETSSDR ABXA9500092Fitting · crackedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 80-02-16, THE AFT PRESSURE DOME PLUG DOOR LUG SHOWED A CRACK INDICATION ON THE X-RAY. FITTING WAS REPLACED IAW DC-9 SRM 51-30-5.SDR 95ZZZX891Blkhd Skin · crackedJFK - DURING CHECK C-9B, FOUND FUSELAGE SKIN, AFT BULKHEAD SKIN, CRACKED AT OUTBOARD NR 7 STIFFENER, STA 1363, AND FOUND A 1.50 INCH CRACK AT OUTBOARD END OF NR 9 STIFFENER. STOP DRILLED CRACKS AND REPAIRED WITH DOUBLER PER SRM 53-11-00, FIGURE 850. AIRCRAFTSDR 95ZZZX888Blkhd Angle · crackedJFK - DURING CHECK C-9B, FOUND A 3 INCH CRACK IN AFT BULKHEAD OUTBOARD CORD ANGLE, THROUGH BOTH LEGS AT WL 160, STA 1363, AND FOUND EXTERIOR CORD ANGLE CRACKED. REPAIRED PER SRM 53-11-00, FIGURE 842. AIRCRAFT TOTAL TIME: 60,716 HOURS; 22,699 CYCLES.
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