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 DL73K000893Bulkhead · crackedTHE WEB OF THE FS 178 BULKHEAD WAS FOUND CRACKED AT RBL 1 AND WL 190. THE CRACK WAS REMOVED BY A 1.0 X 2.0 CUTOUT AND A DOUBLER WAS INSTALLED PER ERA 334328-14.SDR DL733000882Bulkhead · crackedTHE STATION 178 BULKHEAD WEB WAS FOUND TO BE CRACKED AT WL 213 NEAR LBL 5.7. THE RESULTING CUTOUT MEASURED APPROX 1 INCH UP/DOWN BY 1 INCH I/B - O/B. CORRECTIVE ACTION: ER/A 334374-14AD REV C.SDR DL72K000872Bulkhead · crackedTHE FS 1183 BULKHEAD WAS FOUND WITH A 1.5 INCH LONG TYPICAL CRACK IN THE WEB JUST BELOW THE LBL & RBL 8 STIFFENERS AT WL 182. THE CRACKS ARE TYPICAL OF BAC S/B 727-53-0175. THE CRACKS WERE CUT OUT OF THE WEB AND REPAIRED WITH TITANIUM DOUBLERS PER ER/A 37720SDR USAA000659Bulkhead · crackedCLT - FOUND WEB CRACKED 1 INCH, 178 BULKHEAD, LBL 5.7 AND WL 202 AND 199. INSTALLED DOUBLER PER TR 53-10-07 REV A. (M)SDR MWEA00396Angle · damagedTOOL MARKS ON LOWER PART OF AFT PRESSURE BULKHEAD DOOR SILL IN SEAL AREA. FABRICATED AND INSTALLED ZEE.SDR SWAA000817Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, HFEC INSPECTION INDICATED BS 178 BULKHEAD CRACKED RBL 5.5. REPAIRED BULKHEAD PER SRM.SDR RAAAOOB1005Bulkhead · crackedDURING SCHEDULED C2 CHECK, FOUND CRACKS IN NOSE WHEEL WELL LT SIDE BULKHEAD. REPAIRED CRACKS IN LT SIDE NOSE WHEEL WELL PRESSURE BULKHEAD FS 277 IAW SRM 53-10-9 FIG 4 AND COMPLIED WITH SERVICE BULLETIN 727-53-0145.M54 #98SDR RAAA00B1005Bulkhead · crackedDURING SCHEDULED C2 CHECK, FOUND CRACKS IN NOSE WHEEL WELL LT SIDE BULKHEAD FS 277. REPAIRED CRACKS IN LT SIDE NOSE WHEEL WELL PRESSURE BULKHEAD FS 277 IAW SRM 53-10-9 FIG 4 AND COMPLIED WITH SERVICE BULLETIN 727-53-0145.M54 #98SDR RAAA00B1004Bulkhead · crackedDURING SCHEDULED C2 CHECK, FOUND CRACKS IN NOSE WHEEL WELL LT SIDE BULKHEAD SKIN. REPAIRED CRACKS IN LT SIDE NOSE WHEEL WELL PRESSURE BULKHEAD FS 286 IAW SRM 53-10-9 FIG 4 AND COMPLIED WITH SERVICE BULLETIN 727-53-0145.SDR CA000519013Bulkhead · cracked(CAN) THE LEFT AND RIGHT MOUNTED FWD WING SUPPORT BULKHEADS WERE INSPECTED AND FOUND TO BE CRACKED ON THEIR LOWER MOUNTING FLANGES. (P/NS 44758-00 L/H & 44758-01 R/H)SDR CA000519012Bulkhead · cracked(CAN) THE LEFT AND RIGHT FUSELAGE MOUNTED FORWARD WING SUPPORT BULKHEADS WERE INSPECTED AND FOUND TO BE CRACKED ON THEIR LOWER MOUNTING FLANGES. (P/NS 44758-00 AND 44758-01).SDR SWAA000811Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, HFEC INSP INDICATED BS 178 BULKHEAD CRACKED, LBL 5.5. REPAIRED BULKHEAD PER SRM.SDR RRXA000989Bulkhead · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON AFT FRAME AFT PRESSURE BULKHEAD FRAME Z + 18 X + 2 TO -2 TOP ANGLE OF FRAME, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRISDR RRXA000988Bulkhead · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON AFT FRAME AFT PRESSURE BULKHEAD FRAME BOTTOM ANGLE ON FRAME & TOP ANGLE AT Z + 30 X -2 TO +4, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILSDR RRXA000987Bulkhead · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON AFT PRESSURE BULKHEAD FRAME TOP ANGLE ON FR & BOTTOM OF FRAME Z + 43 X + 2 TO -2, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FASDR RRXA000434Pressure Panel · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CABIN SHEAR WEB AND PRESSURE PANEL AT STA 848 AND LONGERON LEFT BL 44, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, REPLACED DOUBLER AND ANGLES IAW DC8 SRMSDR 2000UALA00738Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR DL767000812Bulkhead · corrodedCORROSION DAMAGE FOUND ON THE AFT FACE AND FLANGES OF THE REAR SPAR BULKHEAD FITTINGS. THE CORROSION IS LOCATED JUST FWD OF THE FWD EDGE OF THE MLH W/W UPPER PRESSURE WEB, AND PROCEEDS INTO THE VERTICAL RAD II OF THE MACHINED FITTINGS ON BOTH THE LT AND RT SISDR DL733000811Bulkhead · crackedSTA 178 BULKHEAD WEB FOUND CRACKED AT WL 213 NEAR LBL 5.7. RESULTING CUTOUT MEASURED APPROXIMATELY 1 UP/DOWN BY 1 INBOARD/OUTBOARD. ER/A 334374-14AD.SDR SWAA000771Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND THRU HFEC INSP BS 178 BULKHEAD CRACKED, LBL 9, LBL 10 AND LBL 12. REPAIRED BULKHEAD PER SRM.SDR EIA2000153Splice · damagedHAECO-HKG - FOUND BS BH LEFT OUTER CHORD SPLICE FITTING NR 7 AND NR 8 BOLT HOLE TO CLOSE TO FLANGE WEB AFTER INSURANCE CUT PER EO 53-747-1513-98 REV C. BS 1480 BULKHEAD LEFT OUTER CHORD SPLICE FITTING REPLACED PER EO 53-747-1513-98 REV C ANS SB 747-53A-2380. SDR EIA2000145Bulkhead · crackedDURING ACCOMPLISHMENT OF BS 1480 BULKHEAD AND SPLICE COMPONENTS REPAIR AND MOD EO 53-747-1513-98C, LEFT BULKHEAD FASTENER HOLES NR 3, 5 AND 24, FOUND CRACKED. CARRIED OUT CRACK REMOVAL AND INSURANCE CUT PER EO 53-747-1513-98C PAR II AND BSB 53A2390. (M)SDR EIA2000144Bulkhead · crackedDURING ACCOMPLISHMENT OF BS 1480 BULKHEAD AND SPLICE COMPONENTS REPAIR AND MOD EO 53-747-1513-98C, BS 1480 RIGHT BULKHEAD FASTENER HOLES NR 1, 3, 5, 6 AND 22, FOUND CRACKED. CARRIED OUT CRACK REMOVAL AND INSURANCE CUT AS PER EO 53-747-1513-98C PART II AND BSBSDR AWXA0000258Pressure Panel · crackedC-CHECK, LT WHEEL WELL PRESSURE WEB HAS 2 CRACKS STA 663 LBL 33. FAB''D DOUBLER, ANGLE, AND FILLERS FROM 2024T3 .050 AND 7075 T6 .063. TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW ER 03-5310-0090-DL1.SDR TWAA0006407Stiffener · crackedDURING OP 16 MAINT CHECK, FOUND IN CABIN, TOP OF VERTICAL STIFFENER WAS CRACKED ON REAR PRESSURE BULKHEAD, ABOVE THE AFT ENTRY DOOR STRINGER NUMBER 1, FWD SIDE OF BULKHEAD. REPAIRED STIFFENER PER SRM 53-01, PAGE 10 FIG 2.SDR AU000546Bulkhead · cracked(AUS) FUSELAGE FORWARD PRESSURE BULKHEAD WEB CRACKED AT RIGHT BUTTOCK LINE 5.7 AND WATERLINE 8.3. FOUND DURING EDDY CURRENT INSPECTION.SDR AT0000269Bulkhead · crackedFOUND BULKHEAD WEB AT BS 965 CRACKED. FABRICATED REPAIR WEB AND INSTALLED IAW EO 9-5310-29-E1466, REV A.SDR 20000615SH033Bulkhead · misdrilledDURING C-CHECK, FOUND NUMEROUS HOLES MISLOCATED IN THE WEB AT RT BS 965 BETWEEN L7 AND L15. CAUSE UNKNOWN. (X)SDR USAA000564Bulkhead · crackedCLT - FOUND SKIN CRACKED 1.5 INCHES, FORWARD BULKHEAD AT STATION 178.6, RBL 5. INSTALLED DOUBLER PER TR 53-10-07. (M)SDR USAA000566Bulkhead · crackedCLT - FOUND SKIN CRACKED 1 INCH, BL 0, WL 187, BULKHEAD 178. INSTALLED FILLER AND DOUBLER PER SRM 53-10-08. (M)SDR USAA000567Bulkhead · crackedCLT - FOUND WEB FOR BULKHEAD CRACKED 1 INCH, STATION 178 LBL 5, 9 INCHES BELOW FLOOR LEVEL. INSTALLED DOUBLER PER TR 53-10-07. (M)SDR DL72K000740Bulkhead · crackedTHE LT AFT ENTRY DOOR FRAME ON THE FS 1183 BULKHEAD WAS FOUND WITH A TYPICAL CRACK AT WL 276. THE CRACK IS TYPICAL OF AD 99-18-05 AND BAC S/B 727-53-0210. THE CRACK WAS ROUTED OUT OF THE FRAME AND REPAIRED WITH THE S/B 727-530- 0210 REPAIR/MOD KIT ON ASDR P2EA00139Bulkhead · crackedSHO - DURING C-CHECK, NOSE WHEELWELL AFT BULKHEAD WEB CRACKED AT BS 294.5, RBL 7.5 AND WL 165. REPAIRED WEB AT BS 294.5 FROM RBL 7.5 TO LBL 6.12, BETWEEN WL 173 AND WL 150 IAW SB 737-53-1079 REV 3, SECTION III FIG 3. SEE COOPESA W/O N10316-1-194, VAM100 NR 5SDR 2000UALA00753Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-11.SDR P2EA00128Bulkhead · dentedSJO- DURING C-CHECK, DENT ON BULKHEAD WEB AT BS 294, WL 184 AND RBL 3.5. REPAIRED DENT AT BS 924 BETWEEN RBL 2 AND RBL 5 AND FROM WL 187.1 TO WL 182.1 IAW SRM 51-40-2, FIG 1. SEE COOPESA W/O N10316-1-22, VAM100 NR 109 AND 912SDA132. (X)SDR SWAA000708Bulkhead · crackedDURING SCHEDULED 1/2 D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 10. WL 234. REPAIRED BULKHEAD PER SRM.SDR 00FDEA00357Bulkhead · damagedFWD FUSELAGE BULKHEAD AT BS 595 OF SUBJECT A/C WAS DAMAGED IN LANDING INCIDENT AND HAS BEEN OPERATING UNDER REPETITIVE INSP PER EA 1-5330-46611 REV D. *S/D* REPAIRED BULKHEAD AT BS 595 LT & RT SIDES. REF SNRM N00019 INCLUDES EA 1-5310-46693.SDR CA000427021Bulkhead · cracked(CAN) UPON INSPECTION, A SMALL BULGE AND CRACK WAS FOUND ON THE FUSELAGE EXTERIOR AT THE WING FRONT SPAR ATTACH AREA ON BOTH LEFT AND RIGHT SIDES. FUSELAGE INTERIOR WAS REMOVED AND THE SIDE FLANGES ON THE BULKHEAD ASSYS WERE FOUND TO BE CRACKED. NO ABNORMAL SDR RRXA001918Pressure Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER ON COCKPIT PRESSURE DECK APPROX 14 INCHES LEFT OF CENTER AT STA 45 TO STA 52, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRISDR DLM90000689Bulkhead · crackedTHE STATION 1520.225 CANTED BULKHEAD WEB WAS FOUND CRACKED AT THE JOGGLED SPLICE FOR THE UPPER AND LOWER WEBS AT STR 8L & 8R (11 O''CLOCK AND 1 O''CLOCK POSITIONS). ONE CRACK WAS 10 INCHES AND THE OTHER WAS 18 INCHES. THE CRACKED SECTIONS OF WEB WERE CUT OFSDR SWAA000679Bulkhead · corrodedDURING SCHEDULED 1/2D CHECK, FOUND BS 1016 PRESSURE BULKHEAD CORRODED JUST BELOW CABIN FLOOR LINE, BL 0. REPAIRED BULKHEAD PER SRM.SDR USAA000531Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178, BULKHEAD WEB RBL 4.75, WL 201. INSTALLED DOUBLER PER SRM 53-10-08. (M)SDR USAA000532Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB LBL 4.75, WL 201. INSTALLED DOUBLER. (M)SDR USAA000533Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB LBL 4.75, WL 198. INSTALLED DOUBLER PER SRM 53-10-08. (M)SDR USAA000534Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB RBL 4.75, WL 198. INSTALLED DOUBLER PER SRM 53-10-08. (M)SDR USAA000536Bulkhead · crackedCLT - FOUND WEB CRACKED .25 INCH LONG, STATION 178 BULKHEAD WEB RBL 1, WL 206. INSTALLED DOUBLER PER SRM 53-10-08. (M)SDR RRXA002028Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT PRESSURE BULKHEAD AT STA 1766 RT AND RBL 25.5 INCHES TO 27 INCHES 34.5 INCHES TO 34.75 INCHES & 35.5 INCHES TO 35.75 INCHES Z AXIS + 65.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED ANSDR RRXA002027Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT PRESSURE BULKHEAD AT STA 1766 LT AND LBL 24.25 INCHES TO 27.25 INCHES & 33.5 INCHES TO 36.25 INCHES LBL Z AXIS + 65.5 INCHES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREASDR RRXA001894Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT PRESSURE BULKHEAD AT STA 1766 RT AND RBL 25.5 TO 27, 34.5 TO 34.75 AND 35.5 TO 35.75 Z AXIS + 65.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABSDR RRXA001893Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT PRESSURE BULKHEAD AT STA 1766 LT AND LBL 24.25 TO 27.25 & 33.5 TO 36.25 LBL Z AXIS + 65.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED A
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