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 RRXA97005Bulkhead Web · damagedDURING MAINTENANCE VISIT, FOUND PRESSURE BULKHEAD WEB PUNCH HOLE AT Y=8. REPAIRED MINER DAMAGE IN PRESSURE BULKHEAD WEB BY DOUBLER REPAIR AT Y=8 IAW ENGINEERING SKETCH EAR 8-53-1509.SDR F3LA96075Dome · mis repairedPAE - REPAIR ON BS 1016 PRESSURE DOME DOES NOT CONFORM TO THE SRM. REMOVED OLD REPAIR AND INSTALLED NEW REPAIR ON PRESSURE DOME BS 1016, LBL 19, WL 244 PER SRM 53-10-4 FIGURE 3. (M)SDR DHL9774019CBulkhead Angle · crackedAT C-CHECK, AFT AIRSTAIRS RT TORQUE BOX FS 1263 RBL 23 AIRSTAIRS OPERATING MECHANISM SUPPORT STRUCTURE ATTACH ANGLES UNDER SHELF CRACKED FWD AND AFT SIDE OF BULKHEAD FS 1263. REPLACED DAMAGE ATTACH ANGLES PER SRM 51-10-1, 2.25 BY 7.5 BY 1.SDR SWAA961440Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE BULKHEAD WEB CRACKED AT WL 218, RBL 9.5 AND AT WL 202, RBL 5. REPAIRED PER BOEING SRM.SDR DL73E970018Bulkhead Web · crackedDURING INSPECTIONS PER SI 3-69482-12, THE STATION 178 BULKHEAD WAS FOUND CRACKED IN ONE LOCATION APPROXIMATELY AT RBL 4 AND WL 200. THE RESULTING DAMAGE CUTOUT IS 1 WIDE AND 4.75 LONG. THE BULKHEAD WEB IS FABRICATED FROM 0.032 CLAD 2024-T3.SDR ABXA9700686Bulkhead Door · crackedDURING C-CHECK, WHILE ACCOMPLISHING S/B 53-137 A CRACK WAS FOUND IN THE UPPER RT DOOR CORNER OF THE AFT PRESSURE BULKHEAD. THE BULKHEAD WAS REPAIRED IAW REA D953-17604-MR.SDR 96FDEA01709Bulkhead Fitting · crackedTHE CENTER LANDING GEAR WHEEL WELL AREA HAS A CRACK AT THE RT BULKHEAD AND DRAG LINK VERTICAL SUPPORT FITTING AT STA 1453 AT X = - 31.50 CRACK MEASURES 13 AT LOWER END OF FITTING. ADDITIONALLY, VERTICAL STIFFENERS AND DIAGONAL STIFFENER HAVE DEEP GOUGES AT STSDR 97ZZZX276Bulkhead · crackedDURING C/W OF AD 72 07-09, FOUND 4 CRACKS IN BULKHEAD P/N 1212859-1 AND 3 CRACKS IN BULKHEAD P/N 1212409-6. THE REST OF THE FIN STRUCTURE WAS DYE CHCKED AND INSPECTED AND NO FURTHER CRACKS WERE FOUND. ONE FORWARD VERTICAL FIN BOLT HAD SHOWN SIGNS OF LOOSENINSDR 97ZZZX275Bulkhead · crackedDURING C/W OF AD 72 07-09, FOUND 4 CRACKS IN BULKHEAD P/N 1212859-1 AND 3 CRACKS IN BULKHEAD P/N 1212409-6. THE REST OF THE FIN STRUCTURE WAS DYE CHCKED AND INSPECTED AND NO FURTHER CRACKS WERE FOUND. ONE FORWARD VERTICAL FIN BOLT HAD SHOWN SIGNS OF LOOSENINSDR USAA960791Bulkhead · crackedPIT - DURING Q-1 CHECK, FOUND TWO 3 INCH CRACKS AND 2 .75 INCH CRACKS (LT AND RT SIDES) CENTER PRESSURE BULKHEAD STATION 14911 AT STATION NR 11 (LHS) AND AT STATION NR 64 (RHS). ROUTED OUT CRACKS IN THE FRAME AND INSTALLED SHIMS AND NEW FABRICATED ANGLES PER SDR DLL10970169Bulkhead Web · crackedBS 1212 BULKHEAD WEB FOUND CRACKED AT RBL 6. CRACK IS 2 INCHES. THE RBL 6 LOCATION REQUIRES A CHANGE TO THE DOUBLER PROFILE TO ACCOMMODATE A CABLE PASS-THROUGH.SDR 97FDEA00002Bulkhead Forging · crackedLT FUSE 870 BULKHEAD FORGING. CRACKED BEYOND LIMITS OF SB 727-53-116, REF NR S001. INSTALLED NEW LT 870 FORGING PER FED EX EA 7-5310-28935, SB 727-53-116, SRM 51-30-2.SDR MZZA96207Bulkhead Web · crackedTNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, 4.5 INCH LONG CRACK WAS FOUND ON BS 950 PLUS 5.13 PRESSURE BULKHEAD WEB TO RT BULKHEAD FITTING SPLICE ANGLE (69-16269-2) AT WL 174.80. THE DAMAGED SPLICE ANGLE, P/N 69-16269-2 WAS REMOVED AND REPLACED PER B7SDR USAA960793Bulkhead · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 178 BULKHEAD LBL 5.7 WL 184 BEAM CHORD. STOP DRILLED AND INSTALLED REPAIR ANGLE, REPAIRED PER TR 53-10-17. (M)SDR SWAA961403Bulkhead Skin · crackedDURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 BULKHEAD WEB SKIN CRACKED UNDERNEATH REINFORCEMENT CHANNEL. INSTALLED REPAIR DOULBER PER BOEING SRM.SDR TWAA9615820Bulkhead Fitting · corrodedMCI - DURING CHECK C, FOUND CORROSION ON AFT PRESSURE BULKHEAD FITTING, SEVERAL SPOTS. REMOVED AND REPLACED LONGERON FITTING PER SRM 51-00 AND INSTALLED FASTENERS PER SRM 51-30-2. AIRCRAFT TOTAL TIME: 19,271 HOURS; 15,596 CYCLES. (X)SDR DLL10970168Bulkhead Cap · crackedFS 449 BULKHEAD FOUND CRACKED IN HORIZONTAL FLANGE OF THE CAP. THE LOCATION IS FBL 19 AND EXTENDS FROM THE FORWARD EDGE, THROUGH AN EXISTING SEAL RETAINER HOLE, AND TOWARD THE CAP RADIUS. THE REPAIR WILL BE ACCOMPLISHED BY SB 093-53-233,2.A PAGES 7-9.SDR 97ZZZX191Bulkhead · crackedINSPECTION FOUND 3 CRACKS IN BULKHEAD AND 4 IN BULKHEAD DOUBLER. INSPECTION AND REPLACEMENT OF PARTS DONE IAW AD 72-07-09 AND CESSNA SE 72-3 AND SE 72-29.SDR GTIA9700131Bulkhead Frame · crackedMHV - AFT PRESS BULKHEAD LEFT SIDE, THE 1ST AND 2ND HORIZONTAL FRAMES UP FROM CABIN FLOOR LEVEL ARE CRACKED. STOP DRILLED CRACKS. FABRICATED DOUBLER AND CLIPS PER SRM 51-01. INSTALLED PER 53-01 FIG 2, 51-10-3. (M)SDR DL73K962709Bulkhead Web · fatigueTHE STATION 178 BULKHEAD WEB WAS FOUND CRACKED IN SEVERAL LOCATIONS. DAMAGE CUTOUT DIMENSIONS ARE: 1 BY 4 FOR RBL 5.7 AT WL 198 TO 201; 1 BY 4 FOR LBL 5.7 AT WL 198 TO 201; AND 2 BY 1 FOR RBL 1 AT WL 188. DIMENSIONS ARE I/B TO O/B VERTICALLY RESPECTIVELY. SDR CKSA96396Blkhd Stiffener · corrodedDURING C-1 CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD, WEB AND VERTICAL STIFFENER HAS INNER GRANULAR CORROSION AT RBL 22 AT FLOOR LINE. REPAIRED VERTICAL STIFENER IN ACCORDANCE WITH AIA DRAWING AIA/E/2443 AND REPORT NR 96 AIA 197 DATED 12-12-96 EA 96-348. SDR CKSA96388Bulkhead · corrodedDURING C-1 CHECK INSPECTION, FOUND FORWARD BULKHEAD STA 8 IS CORRODED BOTH SIDES OF STRINGER TIE AT STRINGER 35R AND STRINGER TIE FITTING ALSO CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER IAW AIA SKETCH AIA/E/2427 EA 96-348 REPORSDR DL72W970038Blkhd Stiffener · crackedA CRACK WAS FOUND IN THE VERTICAL STIFFENER AT LBL 36.83 ON THE FWD SIDE OF THE BS 1183 BULKHEAD. THE CRACK WAS APPROX 1.75 LONG AT WL 237. THE STIFFENER WAS REPAIRED PER BOEING S/B 727-53-0192.SDR TWAA9730002Bulkhead · crackedLAX - DURING C-CHECK, FOUND A FOUR INCH CRACK IN CANTED PRESSURE BULKHEAD HYDRAULIC COMPARTMENT, LBL 10.0. REPAIRED CANTED PRESSURE BULKHEAD PER LOCKHEED DRAWING NR 7622-385. (M)SDR GTIA9700053Bulkhead · crackedMHV - ON BULKHEAD BETWEEN FORWARD CARGO BAY AND FORWARD ACCESSORY COMPARTMENT AT STATION 218 EXISTS SEVERAL CRACK REPAIRS THAT ARE NOT PER SRM. REMOVED EXISTING REPAIRS, FABRICATED NEW PATCHES PER SRM 53-10-1 FIG 7B, 53-01 FIG 2, 51-10-3. INSTALLED IAW 53-01SDR 9626379981Bulkhead · crackedDURING PERIODIC CHECK, FOUND NOSE WHEEL WELL PRESSURE PANEL CRACKED AT FS 110 AT INBOARD VERTICAL BEAM ON RIGHT SIDE. FABRICATED DOUBLER AND REPAIRED PER EA 99-111924.SDR SWAA961345Bulkhead Support · crackedDURING SCHEDULED C2 CHECK, FOUND FWD BULKHEAD SUPPORT CRACKED 2.5 AT BS 727B. REPAIRED PER BOEING SRM.SDR DL73K962708Bulkhead Web · crackedSIX CRACKS WERE FOUND ON THE FWD FACE OF THE FS 178 BULKHEAD WEB. THREE INDEPENDENT CUTOUTS WERE REQUIRED TO REMOVE THE CRACKS. TWO CUTOUTS MEASURE 5.O VERTICALLY BY 1.0 INBOARD-OUTBOARD AT WL 197 TO WL 202 AND ARE AT THE LBL 5.7 AND RBL 5.7 VERTICAL STRAP PSDR SWAA961365Bulkhead Angle · corrodedDURING SCHEDULED D-CHECK, FOUND FLOOR TO BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, LBL 21 TO RBL 21, WL 179. REPAIRED PER BOEING SRM.SDR SWAA961360Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND PRESSURE WEB CRACKED AT BULKHEAD BS 178, RBL 4.7, WL 201. REPAIRED PER TRAMCO EWO 96-0691.SDR SWAA961359Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND PRESSURE WEB CRACKED AT BULKHEAD BS 178, LBL 4.7, WL 198. REPAIRED PER TRAMCO EWO 96-0691.SDR SWAA961358Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND PRESSURE WEB CRACKED AT BULKHEAD BS 178, LBL 6.7, WL 212.5. REPAIRED PER TRAMCO EWO 96-0691.SDR SWAA961357Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND WEB AT BULKHEAD BS 178, BL 0, WL 187, CRACKED 1 INCH LONG. REPAIRED PER TRAMCO EWO 96-0690.SDR GTIA9700128Bulkhead Frame · crackedMHV - AFT PRESSURE BULKHEAD RIGHT SIDE, 1ST 2ND, 3RD HORIZONTAL BULKHEAD FRAMES UP FROM CABIN FLOOR LEVEL ARE CRACKED. STOP DRILLED CRACKS, FABRICATED DOUBLERS AND INSTALL IAW 53-01 FIG 2. (M)SDR GTIA9700127Bulkhead Frame · crackedMHV - AFT PRESSURE BULKHEAD RT SIDE 4TH HORIZONTAL BULKHEAD FRAME UP FROM CABIN FLOOR PANEL IS CRACKED AT OUTBOARD END. STOP DRILLED CRACK, FABRICATED DOUBLERS AND INSTALLED IAW 51-10-2, 51-10-3, 53-01 FIG 2. (M)SDR COMA9610358Bulkhead · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: FWD PRESSURE BULKHEAD DAMGED. PERFORMED REPAIR IAW COMAIR ENGINEERING 53-012.SDR TWAA9730001Bulkhead Cap · crackedLAX - DURING C-CHECK, FOUND .4375 INCH CRACK IN BULKHEAD LOWER CAP THROUGH HORIZONTAL FLANGE AND UP VERTICAL FLANGE, FS 229, RBL 42. STOP DRILLED CRACK AND INSTALLED DOUBLER PER LOCKHEED DWG NR 1642621.SDR CALA9700388Bulkhead Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT L-ANGLE AT CENTER CARGO FORWARD BULKHEAD FS 1521, RBL 19. THE CRACK WAS STOP DRILLED, AN L-ANGLE AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-00-01, FIGURE 2 AND 51-31-01.SDR 97ZZZM62Bulkhead Frame · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND AFT PRESSURE BULKHEAD MAIN FRAME STATION 996, RBL 56 CORRODED AT FASTENER HOLE.SDR CALA9601890Bulkhead Cap · corrodedINSPECTION FOUND T-CAP CORRODED AFT OF AFT PRESSURE BULKHEAD AT STA 996, LONGERON 28R. A NEW T-CAP SECTION WAS INSTALLED IAW SRM 53-03, FIGURE 37.SDR USAA960772Bulkhead Web · corrosionINT - DURING Q-4 CHECK, VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION REAR PRESSURE BULKHEAD WEB LOWER EDGE BS 1016, S23R. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. (X)SDR GTIA9700035Bulkhead Frame · crackedMHV - AFT PRESSURE BULKHEAD DOOR CANTED FRAME ON RT SIDE OF DOOR FRAME IS CRACKED AT UPPER END WHERE THE BULKHEAD MEETS THE FUSELAGE SKIN. REMOVED FRAME, TRIM CRACK AREA PER SRM 51-01, DYE PEN, NO CRACKS FOUND. REINSTALLED FRAME IAW SRM 51-10-3, 53-11-3 PAGESDR CALA9601891Bulkhead Cap · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT PRESSURE BULKHEAD T-CAP AT RT LAV NEAR STRINGER 34 AND A .5 INCH CRACK IN T-CAP AT RT LAV NEAR STRINGER 14. A REPLACEMENT SECTION OF T-CAP WAS SPLICED IN AT EACH LOCATION IAW SRM 53-03, FIGURE 37 AND ECRA 5310-03392.SDR CA961205016Bulkhead · cracked(CAN) ON INSPECTION A 1.5 INCH CRACK WAS FOUND ON BOTH THE LEFT AND RIGHT SIDE WHERE THE FRONT FITTINGS ATTACH TO THE WING.SDR GTIA9700030Bulkhead Frame · crackedMHV - AFT PRESS BULKHEAD FORWARD SIDE LEFT CANTED FRAME ABOVE BULKHEAD DOOR HAS A CRACKED ATTACH CLIP AT UPPER END WHERE BULKHEAD MEETS THE FUSELAGE SKIN. REMOVED AND FABRICATED NEW CLIP, INSTALLED IAW 51-10-2, 51-10-3, 53-01. (M)SDR DLL10962664Bulkhead · crackedDURING INSPECTION OF THE FS 499 BULKHEAD, ADDITIONAL CRACKS WERE FOUND. ORIGINALLY THIS LOCATION HAD BEEN MODIFIED PER A LAX SB.SDR ABXA9700178Blkhd Stiffener · gougedDURING C-CHECK, FOUND VERTICAL STIFFENER GOUGED ON FORWARD BULKHEAD IN ALC COMPARTMENT. REPAIRED VERTICAL STIFFENER IAW ABX REA D953-17379-MR.SDR SWAA961315Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 11 TO 13.5 AND AT LBL 16 TO 17. REPLACED PER BOEING SRM.SDR USAA960768Bulkhead Skin · crackedINT - DURING Q-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND CRACK .25 INCH LONG AT STATION 178 BULKHEAD SKIN LBL 4 WL 199. STOP DRILLED CRACK AND FABRICATED DOUBLER AND INSTALLED. REPAIRED PER TR 53-10-07 STEP 2 AND 3. (M)SDR 97ZZZX555Bulkhead · crackedDURING 100 HR INSPECTION A CRACK WAS FOUND ON THE FWD BULKHEAD WHERE THE CYCLIC BEARING SUPPORT ATTACHES. MOVING CYCLIC FWD AND AFT YOU CAN SEE THIS LOWER LEFT CORNER FLEX, THE CRACK CAN ONLY BE SEEN FROM UNDER THE LEFT SEAT AREA. AIRCRAFT TIME 870 HRS. SUB
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