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 DLL14981060Bulkhead Web · damagedGOUGE FOUND ON THE FS 1363 BLKHD WEB AT LBL 56.5 AND WL 168. REPAIRED PER ERA 331685-14AD.SDR DLL14981059Bulkhead Cap · damagedFOUR HOLES AT LBL 25.5 AND THREE HOLES AT 42.5 WERE MISDRILLED DURING FABRICATION OF THE REPLACEMENT LWR CAP OF THE FS 1363 BLKHD. REPAIRED PER ERA 331683-14AD.SDR DL72W981065Bulkhead Web · crackedCRACKS WERE DISCOVERED IN THE FS 178 BLKHD WEB AT WL 200 ANDLBL 5.8. REPAIRED PER ERA 331668-14.SDR F3LA98057Bulkhead Web · crackedPAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BULKHEAD WEB AT BS 178, LBL 6.7, WL 212-213. MAINTENANCE STOP DRILLED CRACK, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-11, PATE 2, DETAIL III AND PAGE 6, FIG 1. (M)SDR F3LA98056Bulkhead Web · crackedPAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BULKHEAD WEB AT BS 178, RBL 4.7, WL 190-191.5. MAINTENANCE REMOVED DAMAGED AREA (1 INCH BY 1 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-11, FIG 1, DETAIL IV AND SRM 51-30-2. (M)SDR C2XA98IA176Blkhd Stiffener · corrodedIAH - DURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD LOWER STIFFENER CORRODED. MAINTENANCE REMOVED AND REPLACED THE STIFFENER IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR QXEA9800851Bulkhead Beam · crackedREAR PRESSURE BULKHEAD BEAM II RADIUS IS CRACKED BL 125R AND BL 225R. REPAIRED IAW FOKKER SRM 53-02-18, PAGES 30 TO 35.SDR ABXA9800594Rib · crackedLEFT WING LEADING EDGE STUB UPPER RIB CRACKED AT APPROXIMATELY XFS.550. REPAIRED IAW DC8 SRM 51-1-8, 51-1-20D AND ABX DWG K05056.SDR USAA980210Bulkhead Web · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH CRACKS BS 178 LBL 4.75 WL 201 AND WL 198 BULKHEAD WEB. INSTALLED DOUBLER AND REPAIRED PER TR 53-10-11. (M)SDR QXEA9800844Bulkhead Beam · crackedREPAIR ON BEAM VI FOR FORWARD PRESSURE BULKHEAD LOWER FLANGE IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-18.SDR RRXA98130Rib · crackedDURING A MAINTENANCE VISIT, FOUND WING, CENTER L/E RIB AT XRS=360.250 HAS 0.5 INCH CRACK.SDR RAAA98B1077Blkhd Stiffener · crackedDURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1183 BULKHEAD VERTICAL STIFFENER CRACKED APPROX .15 INCH AT LBL 46.93, WL 189. REPAIRED PER S/B 727-53-0181. M-54 NR 519.SDR RAAA98B1069Bulkhead Chord · crackedDURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 950 BULKHEAD LOWER CHORD CORRODED AT STR 29R. ALSO, CHORD CRACKED APPROX 1.5 INCH AT SAME LOCATION BY TOOL DAMAGE FROM ADJACENT REPAIR IN PROGRESS. REPAIRED PER SRM 51-40-3. M-54 NR 500.SDR RAAA98B1043Blkhd Stiffener · crackedDURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1183 BULKHEAD VERTICAL STIFFENER CRACKED APPROX .2 INCH AT RBL 46.93, WL 189. REPAIRED PER S/B 727-53-0181. M-54 NR 262.SDR DHL9870642CBulkhead Fitting · corrodedAT C-CHECK, CORROSION ON FITTING LOCATED ON AFT SIDE OF BULKHEAD AND KEEL BEAM FWD END LBL 15, WL 166. REMOVED AND REPLACED FITTING PER SRM 51-10-1. N/R 3580.SDR 98FDEA00424Bulkhead Fitting · crackedSTA-VCE: DURING REMOVAL AND REPLACEMENT OF P/N AYB 7000-2 (Y=1156 BLKHD CORNER FITTING) A GAP WAS FOUND BETWEEN AYB 7000-2 WEB AND P/N NYB6054-25, NOT COVERED BY SRM STANDARDS. REF NRC NR N1341. MAJOR REPAIR PERFORMED IAW EA 8-5314-34489B. (29 JUNE 1998).SDR SWAA980845Bulkhead Web · crackedDURING SERVICE CHECK, FOUND CRACKED BULKHEAD WEB AT BS 178, WL 198.25 TO 199.25, WL 200.25 - 201.25, RBL 4.7; BS 178, WL 208.5- 209, LBL 6.7 AND WL 211.375 -211.75, LBL 6.7; AND BS 178, WL 201.5-202, LBL 6.7. REPAIRED PER BOEING SRM.SDR SWAA980842Bulkhead Angle · corrodedDURING SCHEDULED D-CHECK, FOUND CORRODED SIDEWALL TO BULKHEAD SUPPORT ANGLE AT BS 500D, RBL 25, WL 158. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA980840Bulkhead Angle · corrodedDURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR TO BULKHEAD SUPPORT ANGLE AT BS 500D, RBL 23, LBL 23, WL 156. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA980832Bulkhead Web · crackedDURING SCHEDULED D CHECK, FOUND CRACKED BULKHEAD WEB AT BS 178, WL 199-200 AND WL 201.5-202.25, LBL 47; WL 198.50-199.25, RBL 6.7 AND WL 212-213, RBL 47. REPAIRED PER BOEING SRM.SDR DL733981006Bulkhead Web · crackedFOUR CRACKS FOUND IN THE BLKHD WEB AT FS 178. THE CRACKS ARE LOCATED AT WL 200 AND WL 188, BETWEEN LBL 5.7 AND RBL 5.7. REPAIRED PER ERA 331672-14.SDR DL733981005Bulkhead Web · corrodedAFT PRESSURE BLKHD AT FS 1016 WAS FOUND CORRODED AND CRACKED AT BL 0. REPAIRED PER ERA 331673-14.SDR ABXA9800460Blkhd Fitting · crackedDURING C-CHECK, AFT PRESSURE BULKHEAD DOOR RIGHT VERTICAL SUPPORT FITTING WAS FOUND CRACKED. REPLACED FITTING IAW DC9 SRM 51-10-04.SDR CALA9800823Bulkhead Angle · crackedAFT UPPER FUSELAGE AFT BULKHEAD LOWER LEFT ANGLE CRACKED. INSTALLED NEW ANGLE PER SRM 53-40-00 FIG 6 VOL 1.SDR UPS98226738Bulkhead Frame · corrodedINSPECTION TYPE:D, FRAME ON FWD SIDE OF B/H 351 LT SIDE IS CORRODED BETWEEN STR 22 AND 23. FRAME REPAIRED IAW SRM 53-10-4 FIG 13.SDR SWAA980802Bulkhead Angle · crackedDURING SCHEDULED 1/2 D CHECK, FOUND CRACKED SUPPORT ANGLE FOR FWD BULKHEAD PANEL AT 727 + 2, RBL 4. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA980793Bulkhead Web · crackedDURING SCHEDULED 1/4D CHECK, FOUND ULTRA SONIC INSP REVEALS 100 PERCENT CRACK INDICATION RBL 5.4, WL 199 UNDER STRAP. REPAIRED CRACKED WEB PER BOEING SRM.SDR DL72S981007Bulkhead · crackedTHE RT SIDE WALL OF THE NOSE LANDING GEAR WHEEL WELL WAS FOUND WITH A .75 VERTICAL CRACK AT FS 277. THE CRACK IS TYPICAL OF BAC S/B 727-53-0145. THE CRACK WAS CUTOUT AND A DOUBLER INSTALLED PER SRM 51-40-2. A PORTION OF THE S/B MODIFICATION WAS ALSO INSTALSDR 98ZZZX2085Bulkhead · crackedDURING AIRFRAME MAINTENANCE, FOUND BULKHEAD ASSEMBLY (TAILBOOM RING) CRACKED IN UPPER RIGHT HAND CORNER NEAR FITTING. RECOMMEND USING A MORE HEAVY DUTY PART.SDR AU980668Press Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD WEB FORWARD FACE CONTAINED A TOTAL OF FIVE CRACKS. A CRACK WAS ALSO FOUND IN THE RADIUS OF THE VERTICAL CHORD OF THE BULKHEAD AT LBL 5.7 LEVEL WITH THE HORIZONTAL STIFFENER AT WL 184. FOUND DURING EDDY CURRENT INSPECTION IAW ESDR MWEA98564Strap · misinstalledTHE AFT VENTRAL DOOR JAMB UPPER LEFT AND RIGHT CORNER STRAPS HAVE BEEN TRIMMED INCORRECTLY. MTC FABRICATED AND INSTALLED STRAPS.SDR MWEA98562Bulkhead Door · crackedFOUND CRACK ON VENTRAL DOOR JAMB UPPER RIGHT CORNER. MTC REPAIRED WITH 5 DOUBLERS.SDR MWEA98571Bulkhead Tee · crackedFOUND CRACK ON FORWARD ACCESSORY COMPARTMENT T-ANGLE AT FS 69 BULKHEAD LEFT SIDE STATION X=10. MTC FABRICATED AND INSTALLED NEW T-ANGLE.SDR TWAA9807703Bulkhead Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT FS 996 LBBL 57, SIDE WALL BELOW FLOOR, WEB SUPPORT ANGLE FOR BULKHEAD WITH CRACK APPROX 3 INCHES LONG. REPAIRED PER SRM 53-05 FIG 93. (M)SDR AALA980874Bulkhead · corrodedTUL - FOUND CORROSION ON FORWARD FACE OF BULKHEAD STATION 1841, STRINGER 43R. REMOVED SECTION OF FRAME AND SPLICED IN A NEW SECTION OF FRAME AND WEB PER SRM 53-20-00. (M)SDR 98ZZZX1877Bulkhead · crackedBULKHEAD FOUND CRACKED 1.6 INCHES RUNNING CIRCUMFERENTIALLY OUTBOARD OF LOWER LEFT HAND TAILBOOM ATTACH HOLE. 7 INCHES LONG.SDR SWAA980717Bulkhd Support · wrinkledDURING SERVICE CHECK, FOUND WRINKLED SIDE BULKHEAD SUPPORT AT BS 380, STR 25L TO 19L, LBL 29 TO 55, WL 194 TO 160. REMOVED AND REPLACED PER BOEING SRM.SDR F3LA98039Bulkhead Support · corrodedPAE - DURING C-CHECK INSPECTION REPORTED, CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT AT BS 947 FROM RBL 22 - LBL 22. MAINTENANCE FABRICATED BULKHEAD TO FLOOR SUPPORT AND INSTALLED PER SRM 51-30-2, 51-30-5 AND 51-30-8. (M)SDR DHL9870717CBulkhead · crackedAT C-CHECK, AFT BAGGAGE 950 BULKHEAD CRACKED AT APPROX RBL 22 WL 185. STOP DRILLED ENDS OF CRACK, HFEC, INSTALLED DOUBLER REPAIR 12 X 5. N/R 3713SDR DHL9870716CBulkhead · crackedAT C-CHECK, AFT BAGGAGE 950 BULKHEAD CRACKED AT APPROX RBL 12 WL 185. STOP DRILLED END OF CRACK, HFEC, INSTALLED DOUBLER REPAIR PER SRM 53-10-9, 12 X 5. N/R 3711SDR ABXA9800493Bulkhead Fitting · corrodedSTATION 70 BULKHEAD FORWARD SIDE LONGERON 31R INBOARD FITTING HAS HEAVY CORROSION ON LOWER FLANGE BELOW BOLT HEAD. REPLACED FITTING IAW SRM 51-1-21 AND DWG 4614397.SDR P5CA9800967Bulkhead · crackedLEFT AND RIGHT NLG WHEEL WELL FORWARD CORNERS CANTED BULKHEAD AND SIDEWALL LOWER CHORD FOUND CRACKED. REPAIRED AS PER SB 747-53-2112.SDR GLBA98068Fire Loop · chafedLT WHEEL WELL FIRE DETECTION ILLUMINATED. AIRCRAFT RETURNED TO GATE. REPLACED FIRE LOOP. (M)SDR ARWA980439Bulkhead Web · damagedDURING D-CHECK, FOUND FUSELAGE AT FS 35.0 BULKHEAD HAS TWO BIG HOLES AT CENTER SECTION. REMOVED BULKHEAD WEB. INSTALLED NEW SECTION OF WEB IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.980010-0031. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 980010,SDR ARWA980437Bulkhead Skin · crackedDURING D-CHECK, FOUND AFT LOWER CARGO COMPARTMENT FS 1400 BULKHEAD ACCESS PANEL IS CRACKED. REMOVED SKIN, FABRICATED NEW SKIN AND INSTALLED IN ACCORDANDE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS AND PARTS, EO 98022303. WORK ACCOMPLISHED UNDER ARROW SDR DHL9870742CBulkhead · crackedAT C-CHECK, AFT BAGGAGE 950 BULKHEAD HAS 3 INCH CRACK AT RBL 57 WL 191. STOP DRILLED CRACK, HFEC. INSTALLED DOUBLER REPAIR PER SRM 53-10-9, 5.75 BY 2.75, N/R 3695.SDR DHL9870741CBulkhead · crackedAT C CHECK, AFT BAGGAGE 950 BULKHEAD HAS 8 INCH CRACK AT LBL 22 WL 185. STOP DRILLED CRACK, HFEC. INSTALLED DOUBLER REPAIR PER SRM 53-10-9, 5 BY 12, N/R 3696.SDR DL733980852Bulkhead Web · corroededAFT PRESSURE BLKHD AT FS 1016 WAS FOUND CORRODED AND CRACKED AT APPROX BL 0.0. THE CORROSION INCLUDED SURFACES 0 THE DOME WEB (GORE) AND BOTH THE LT AND RT 'C' CHANNEL STIFFENERS. AN ACCESS HOLE WAS CUT INTO THE FUSESLAGE SKIN TO FACILITATE THE GORE REPAIR. SDR 98ZZZX1633Seal · failedAIRCRAFT WOULD NOT HOLD CABIN PRESSURE. MAINTENANCE FOUND AFT PRESSURE BULKHEAD SEAL THAT SEALS APU BLEED AIR LINE AND THE AFT PRESSURE BULKHEAD HAD FAILED. CAUSE OF FAILURE IS UNKNOWN. DATE OF SEAL MANUFACTURE, 12-29-87. SUBMITTER RECOMMENDED A MANDATORY SDR 9808819928Bulkhead Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON KEEL TO BULKHEAD FITTING AT FS 748 TO 754, BL 0 THRU RBL 3. REPLACED FITTING (P/N 3915134-517N) PER SRM 51-10-8.
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