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 MWEA98245Blkhd Stiffener · corrodedTHE 1121 CANTED BULKHEAD LONGERON 14L STIFFENER WAS FOUND CORRODED. REMOVED AND REPLACED STIFFENER.SDR MWEA98244Blkhd Stiffener · corrodedTHE 1121 CANTED BULKHEAD STIFFENER AT LONGERON 12L WAS FOUND EXFOLIATED. REMOVED AND REPLACED STIFFENER.SDR MWEA98243Bulkhead Doubler · corrodedDOUBLER ON CANTED BULKHEAD 1089 LONGERON 11R WAS FOUND CORRODED. REMOVED AND REPLACED DOUBLER.SDR CALA9800336Bulkhead T · crackedINSPECTION FOUND A 2.5 CRACK THROUGH FASTENER HOLE ON VERTICAL LEG OF BULKHEAD T AT STA 1156 BETWEEN LONGERON 40L AND 39L. A NEW TEE CAP WAS INSTALLED IAW EA SA003-5310-03391.SDR AU980271Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED AT BS 178. LT VERTICAL CHORD CRACKED IN TWO PLACES AND WEB CRACKED IN FIVE PLACES.SDR ABXA9800127Bulkhead Angle · corrodedDURING C-CHECK, FOUND THE SLANT PANEL ANGLE STATION 690 AND LBL 8 CORRODED. REPAIRED ANGLE IAW ABX REA D953-22465-MR.SDR USAA980095Bulkhead · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 178 BULKHEAD UNDER RADAR DISH MOUNT, INBOARD SIDE OF RT LOWER HAT SECTION LEG. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-11-1, SRM 53-10-11. (M)SDR USAA980084Blkhd Stiffener · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 178 LBL 5.75 AT WL 183.5 STIFFENER, BULKHEAD. DOUBLER AND STIFFENERS INSTALLED, REPAIRED PER TR 53-10-17. (M)SDR USAA980083Bulkhead · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 178 BULKHEAD LBL 5, WL 199. INSTALLED DOUBLER REPAIRED PER SRM 53-10-11. (M)SDR MWEA98195Bulkhead Web · crackedRIGHT HAND LOWER WEB OF THE BULKHEAD AT FS 965 WAS FOUND CRACKED IN SEVERAL PLACES. REMOVED DAMAGED SEC OF WEB, FAB REPAIR PARTS IAW SRM 53-03 FIG 19, INSTALLED REPAIR PARTS IAW SRM 51-30.SDR MWEA98193Bulkhead Web · crackedWEB ATTACHED TO RADIAL STIFFENER APB FOUND CRACKED AT THE O/B END LONG14R. STOP DRILLED CRACK, FABED REPAIR ANGLES IAW DRAW J060110, INSTALLED REPAIR ANGLES IAW SRM 51-30.SDR DL72S980613Bulkhead Skin · crackedAT HMV, FOUND APU BLEED AIR CUTOUT FWD BLKHD RT W/W SKIN CRACKED. REPAIRED PER SRM 53-10-9 FIG 5.SDR MWEA98184Bulkhead Clips · crackedWEB ATTACHED TO THE RADIAL STIFFENER ON THE APB WAS FOUND CRACKED ON THE OUTBOARD END. INSTALLED REPAIR CLIPS IAW SRM 51-30 AND DRAWING J060110.SDR DLL10980449Bulkhead Web · crackedTHE FS 1212 BULKHEAD WEB WAS FOUND WITH A .25 LONG CRACK AT RBL 42.5. THE CRACK WAS ROUTED OUT AND A LOCAL DOUBLER REPAIR INSTALLED PER ER/A 364062-14AD, REV A. THE REPAIR WAS GRANTED AMOC APPROVAL FOR AD 96-20-10.SDR AU980408Bulkhead · cracked(AUS) LT AND RT LOWER AFT DOOR POST BULKHEADS (PN 0512187-1 LT AND PN 0512187-2 RT) CRACKED. FOUND DURING INSPECTION IAW SB SEB 97-1. PART TC: 5,920.SDR 99FDEA00320Bulkhead Web · crackedN0222 - DURING A/C P-F CONVERSION AT OAN, FOUND A 0.50 IN CRACK IN THE CANTED BULKHEAD AT BS 2163.685. TRIMMED WEB TO REMOVE CRACK AND INSTALLED A TITANIUM FILLER AND DOUBLER IAW EA NR 8-5310-35908.SDR USAA980077Bulkhead Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2.5 INCH CRACK BS 178 BULKHEAD AT UPPER LEFT RADAR MOUNT BULKHEAD SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-11, FIG 1. (M)SDR UPS98225858Bulkhead Skin · crackedINSPECTION TYPE-SI, BS 178 BULKHEAD IS CRACKED AROUND FASTENERS AT BS 10, WL 235. REMOVED DAMAGED AREA .5 X 3 ENCOMPASSING 3 CRACKS. REPAIRED BS 178 AT LBL 10, WL 235, PER 727 SRM 53-10-9 AND SRM 51-30-2.SDR EIA990015Bulkhead Gussett · corrodedDURING C-CHECK, MAIN CABIN AFT PRESSURE BULKHEAD, BS 840 LEFT SIDE OF DOOR JAMB LOWER PLATE HAS HEAVY CORROSION, NRC 0589. REPLACED GUSSET IAW SRM 51-30-05. (M)SDR P5CA9800374Bulkhead · crackedFUSELAGE BS140 B/H FWD FACE FOUND CRACKED AT RBL 38 2 PLACES. WEB REPAIRED AS PER SRM 53-10-04 FIG 89.SDR AU980224Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD WEB CRACKED IN SIX PLACES.SDR 9808396612Bulkhead · crackedDURING M-CHECK, FOUND CRACK ON TOP OUTBOARD (RHS) CORNER AT BULKHEAD 400, ZONE 110. REPAIRED PER EO 6-53-41184.SDR ABXA9800081Blkhd Doubler · crackedDURING C-CHECK COMPLIANCE WITH S/B 53-137, FOUND DOUBLER CRACKED RADIALLY IN UPPER RIGHT AND UPPER LEFT CORNERS. REPAIRED DOUBLER IAW ABX REA D953-22492-MR AND DC9 S/B 53-137.SDR P5CA9800296Bulkhead · crackedCRACKED ON BODY STATION 140 BULKHEAD AT LBL 38. REPAIRED AREA WEB PER BAC SRM 53-10-06.SDR P5CA9800295Bulkhead · deformedDEFORMATION AT 6 O'CLOCK POSITION ON APU FIRE BULKHEAD AT STATION 2658. DRESSED OUT DEFORMED AREA PER BAC SRM 51-10-01.SDR P5CA9800286Bulkhead · corrodedLEVEL 1 CORROSION, ON THE FORWARD SIDE OF THE APU BULKHEAD AT STATION 2658, RIGHT BODY LINE 512. CORROSION REMOVED AND AREA TREATED PER BAC SRM 51-10-01 AND 51-10-02.SDR 9803899931Bulkhead Doubler · crackedDURING AFT PRESSURE BULKHEAD INSPECTION, FOUND CRACKS IN THE -71 DOUBLER AT THE AFT PRESSURE BULKHEAD UPPER DOOR CUTOUT. REPAIRED PER EA 99-154161.SDR 9803889931Bulkhead Skin · crackedDURING AFT PRESSURE BULKHEAD INSPECTION, FOUND CRACK IN THE AFT PRESSURE BULKHEAD SKIN AT THE UPPER DOOR CUTOUT 11.5 RIGHT OF CENTER LINE. REPAIRED PER EA 99-154161.SDR AU980268Chord · cracked(AUS) FORWARD PRESSURE BULKHEAD LT SIDE CHORD LOCATED AT WL 207 CRACKED. CRACK LENGTH 38.1MM (1.5 INCH). FOUND DURING VISUAL INSPECTION IAW ER B73-53-10-39C.SDR C2XA98IA019Bulkhead · crackedIAH - DURING C-CHECK INSPECTION, THE MAIN LANDING GEAR WHEEL WELL AFT BULKHEAD WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER REPAIR OVER THE AFFECTED AREA IAW ATR42-500 SRM 51-70-00, AND THE AIRCRAFT WAS APPROVED FOR RETUSDR AU980266Web · cracked(AUS) FORWARD PRESSURE BULKHEAD WEB SKIN CRACKED IN EIGHT PLACES. FOUND DURING ULTRASONIC INSPECTION.SDR UPS98825892Bulkhead Angle · corrodedINSPECTION TYPE:C AFT SIDE OF F/S 70 O/B OF 33R LOWER BULKHEAD L ANGLE HAS HEAVY CORROSION AROUND BOLT AND BETWEEN IT AND LONGERON FITTING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHORD IAW SRM 53-2-5 51-1-20D, AND DWG 5613064.SDR DL72W980354Blkhd Stiffener · crackedCRACKS WERE FOUND IN THE L/RBL 36083 VERT STIFFENER ON THE FWD SIDE OF THE BS 1183 BLKHD. CRACKS WERE LOCATED AT APPROX WL 238 AND WERE NO MORE THAN 2 IN LENGTH. REPAIR PER ERA 331332-14.SDR MWEA98148Bulkhead · corrodedDURING INSPECTION, FOUND LIGHT CORROSION ON FWD SIDE OF APB LEFT SIDE FROM APPROXIMATELY LONG 26L TO 28L. MTC REPAIRED IAW SRM 53-03 FIG 9 SHEET 1 AND 51-30-5.SDR DL73S980339Bulkhead Web · crackedDURING INSPECTION, SERVERAL CRACKS WERE FOUND IN THE BLKHD WEB AT FS 178. THE CRACKS WERE LOCATED AT WL 192 TO 202 AND LBL 5 AND RBL 5. REPAIRED PER ERA 331313-14.SDR DL72W980341Bulkhead Beam · crackedMTC FOUND A .1875 INCH CRACK IN THE OUTBD AFT FLANGE OF THE RBL 8 VERT BEAM IN THE FS 1183 BLKHD, WHICH BEGINS AT WL 182. REPAIRED PER ERA 362891-14, REV A.SDR AU980301Bulkhead · cracked(AUS) FUSELAGE AFT DOOR POSTS P/N 0512187-1 (LT) AND P/N 0512187-2 (RT) CRACKED. FOUND DURING INSPECTION IAW CESSNA SB SEB 97-1.SDR 9807886612Bulkhd Fastener · crackedDURING M-CHECK, FOUND CRACK ON FASTENER HOLE AT FS 140 BULKHEAD, STR 14R, INNER RING DOUBLER AREA. REPAIRED PER EA 66-156319.SDR 9803919931Bulkhead Doubler · crackedDURING AFT PRESSURE BULKHEAD INSPECTION, FOUND CRACKS IN THE AFT PRESSURE BULKHEAD UPPER DOOR CUTOUT -13 DOUBLER. REPAIRED PER EA 99-154161.SDR 9803909931Bulkhead Doubler · crackedDURING AFT PRESSURE BULKHEAD INSPECTION, FOUND CRACK IN THE -9 DOUBLER AT THE AFT PRESSURE BULKHEAD UPPER DOOR CUTOUT. REPAIRED PER EA 99-154161.SDR AU980302Bulkhead · cracked(AUS) FUSELAGE LOWER AFT DOOR POST BULKHEADS P/N 0512187-1 AND P/N 0512187-2 CRACKED. FOUND DURING INSPECTION IAW CESSNA SB SEB97-1.SDR SWAA980151Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 6.7, WL 202 TO 203. REPAIRED PER BOEING SRM.SDR SWAA980150Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 4.7, WL 199 TO 199.75 AND WL 201.5 TO 202.25. REPAIRED PER BOEING SRM.SDR SWAA980149Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 4.7, WL 201.75 TO 202.75. REPAIRED PER BOEING SRM.SDR SWAA980146Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 6.7, WL 209.75. REPAIRED PER BOEING SRM.SDR QXEA9800331Bulkhead Beam · crackedPDX - PREVIOUS DOUBLER REPAIR AT TOP SURFACE OF HORIZONTAL BEAM VI APPEARS TO BE CRACKED ON FORWARD SIDE OF FORWARD PRESSURE BULKHEAD. REPAIRED IAW HORIZON EA 4-53-370.SDR DHL9872446CBulkhead · crackedAT C-CHECK, 1183 BULKHEAD RT FWD SIDE WL 237.1 I/B AND O/B SIDES OF VERTICAL STIFFENER CRACKED 37 RIGHT OF CENTER. STOP DRILL, HFEC, INSTALLED REPAIR PER S/B 53-0192, AND SRM 51-30-2. N/R 3499.SDR AU980156Bulkhead · cracked(AUS) FUSELAGE FORWARD PRESSURE BULKHEAD CONTAINED FIVE WEB CRACKS ANDTWO CRACKS IN THE LH VERTICAL STIFFENER.SDR SWAA980139Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND CRACKS ON BS 178 BULKHEAD AT WL 188, LBL 0.5 AND RBL 0.5. REPAIRED PER BOEING SRM.SDR SWAA980112Bulkhead Skin · damagedDURING SCHEDULED A1 CHECK, FOUND BS 178 BLKHD AND SKIN DAMAGED. REPAIRED PER BOEING SRM.
Back to JASC 5312