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 USAA960718Bulkhead Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 178 BULKHEAD SKIN RBBL 5 INCH WL 199. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-10-11. (M)SDR USAA960717Bulkhead Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION FOUND 1.5 INCH CRACK 178 BULKHEAD SKIN RBBL 5 INCH WL 202. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-10-11. (M)SDR USAA960715Bulkhead Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 178 BULKHEAD SKIN LBBL 5 INCH WL 199. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-10-11. (M)SDR EIAA9673Bulkhead Chord · corrodedSAT - BULKHEAD 756 UPPER T-CHORD CORRODED LBL 22 TO LBL 31. FABRICATED AND INSTALLED BULKHEAD T-CHORD SECTION BS 756 LBL 22 TO LBL 31 PER SRM 53-01 FIG 2, 51-10-3 AND 53-14-3. (M)SDR EIAA9654Bulkhead · gougeSAT - FOUND FUSELAGE STATION 37 BULKHEAD WEB GOUGED AT STRINGER 18L. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 4 ITEM 4. (M)SDR EIAA9653Bulkhead Web · gougeSAT - FOUND FUSELAGE STATION 37 BULKHEAD WEB GOUGED AT STRINGER 18R. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 1 AND FIG 2. (M)SDR 96ZZZX5829Tee Cap · crackedDURING INSPECTION OF AFT PRESSURE BULKHEAD AT STA Y=1766 IAW PSI 53.08.009/010C AND NDI 53-10-18, FOUND TWO CRACKS AT CORNER RADIUS OF THE TEE CAP AT LONGERON 10 RT AND LONGERON 10 LEFT. REPAIRED CRACKS BY INSTALLING A REPAIR ANGLE IAW SRM 53-2-5, PAGES 15 ANSDR 96ZZZM1539Bulkhead Tee · crackedDURING INSPECTION OF AFT PRESSURE BULKHEAD AT STATION Y=1766 IAW PSI 53.08.009/010C AND NDI 53-10-18, FOUND TWO CRACKS AT CORNER RADIUS OF THE TEE CAP AT LONGERON 10 RIGHT AND LONGERON 10 LEFT. REPAIRED CRACKS BY INSTALLING A REPAIR ANGLE IAW SRM 53-2-5 PAGE SDR SWAA961204Bulkhead Angle · corrodedDURING SCHEDULED D-CHECK, FOUND FLOOR TO AFT BULKHEAD SUPPORT ANGLE CORRODED AT BS 520, LBL 24 TO RBL 24. REPLACED PER BOEING SRM.SDR ABXA9700696Bulkhead Clip · crackedDURING ACCEPTANCE INSPECTION FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER CRACKED AT LONGERON 16L. REMOVED AND REPLACED END CLIPS AT LONGERON 16L IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.SDR MWEA435Pin Receptacle · crackedDURING C-CHECK, FOUND AFT PLUG DOOR JAMB ALIGNMENT PIN RECEPTACLE CRACKED AT 9 O'CLOCK POSITION. MTC REMOVED AND REPLACED RECEPTACLE IAW DOUGLAS DRAWING 5910163.SDR 96FDEA01615Bulkhead · crackedNR 0509 024, CRACK ON THE AFT SIDE OF THE 870 BULKHEAD AT RBL 9.5 AND WL 157.SDR ARWA9610011Bulkhead Dr Sill · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION AT AFT LWR CARGO COMPARTMENT BULKHEAD DOOR SILL, STA 1540, LONG 53L. CUT CORRODED AREA, REPAIRED IAW DC-8 SRM 53-2-0, FIG 2 SHT 4, 6 AND 7. TREATED AND INSTALLED REPAIRED PARTS IAW DC-8 SRM 51-1-8, 51-1-17, 51-1-21.SDR 96FDEA01614Bulkhead · crackedNR 0507 023, POSSIBLE CRACK ON AFT SIDE OF BS 950 BULKHEAD AT LBL 4 WL 176 AND AT LBL 11, WL 181 TO 184.SDR 97ZZZM458Blkhd Doubler · crackedIN HYD BAY AT FRAME 29 BULKHEAD, THE TWO MOST OUTBOARD STIFFENERS LEFT AND RIGHT WERE FOUND TO HAVE CRACKED DOUBLERS AT BOTTOM BOLT HOLE. THESE STIFFENERS ARE NOT COVERED IN EO E95/003/653, STATION 47.20 LT/RT, END OF CRACKS MARKED WITH GREASE PENCIL. REPLACSDR 97ZZZM457Blkhd Stiffeners · crackedPERFORMED ET AT FRAME 29 BULKHEAD TO C/W EO E95/003/653 ITEM NR 3. FOUND CRACKS AT STIFFENER STATION 36.62, 31.13, 25.94 LEFT AND 36.62, 31.13, 25.94 RT. REPAIR STIFFENERS IAW EO E95/005/654. END OF CRACKS MARKED WITH GREASE PENCIL. REPAIRED FRAME 29 STIFFSDR USAA960690Bulkhead Angle · crackedPIT - DURING SIP AND B-CHECK, FOUND 4 INCH CRACK IN FRONT PRESSURE BULKHEAD LOWER CONNECTION ANGLE AFT SIDE FRAME 1550 BETWEEN STRINGER 3 AND 72. DETECTED BY VISUAL/EDDY CURRENT. STOP DRILLED CRACK ENDS AND INSTALLED TWO EXTERNAL DOUBLERS PER SRM 53-02-18 FISDR DL73E962457Bulkhead · crackedDURING INSPECTION PER SI 3-69482-12, STATION 178 BULKHEAD WAS FOUND CRACKED IN SEVERAL LOCATIONS. REPAIR ACCOMPLISHED PER ERA 304293-14 REV B. THE BULKHEAD WEB IS FABRICATED FROM 0.032 CLAD 2024-T3.SDR CALA9601516Bulkhead · crackedINSPECTION FOUND A 6 INCH CRACK IN BULKHEAD BEHIND STIFFENER ON RT SIDE AT STA 178, WL 218. ALSO, A 1 INCH CRACK WAS FOUND AT WL 230.5, RT SIDE. THE CRACKED AREA AT WL 218 WAS REMOVED AND THE CRACK AT WL 230.5 WAS STOP DRILLED IAW SRM 53-10-11. REPAIR DOUBLSDR 9624519760Bulkhead Panel · crackedDURING LINE CHECK, FOUND A 3 INCH CRACK IN THE SLANTED PRESSURE PANEL TO FUSELAGE ATTACH ANGLE APPROXIMATELY LBL 24 ABOVE THE REAR SPAR. REPAIRED ANGLE (P/N 9923419-9) PER EA 97-111746.SDR 9623489957Bulkhead T Cap · corrodedDURING H-CHECK, FOUND CORROSION ON THE FS 756 BULKHEAD T-CAP BETWEEN LONGERONS 29L TO 29R. REPAIRED T-CAP (P/N 9958212-3) PER EA 99-111734.SDR 8512489957Bulkhead T Cap · corrodedDURING H-CHECK, FOUND CORROSION ON THE FS 756 BULKHEAD T-CAP BETWEEN LONGERONS 29L - 29R. REPAIRED T-CAP (P/N 9958212-3) PER EA 99-111734.SDR F3LA96050Bulkhead Web · crackedPAE - FOUND NUMEROUS PREVIOUS REPAIRS AND MORE CRACKS DURING INSPECTION ON BS 178 CENTER WEB BULKHEAD. CENTER WEB WS REPLACED IAW BOEING SRM AND BOEING DRAWING NR 65-16300. REPLACEMENT ACCOMPLISHED ON TRAMCO MWO FUSELAGE 212. (M)SDR F3LA96049Bulkhead Web · crackedPAE - FOUND 1 INCH LONG CRACK IN BS 663.75 BULKHEAD WEB, RBL 48, 8.5 INCHES BELOW THE PRESSURE DECK. REPAIRED CRACK IN BULKHEAD WEB BS 663.75, RBL 48 8.5 INCHES BELOW PRESSURE DECK IAW EWO 96-0606. LEAK CHECKED ALL ITEMS. REMOVED FOR ACCESS, NO LEAKS FOUND.SDR 96ZZZX5714Bulkhead · corrodedAT FUSELAGE STA 17.00 RT SIDE WHERE BULKHEAD AND SUPPORT CONNECT TOGETHER BENEATH FLOORBOARD, IT WAS FOUND TO BE BADLY CORRODED IN AN AREA OF ABOUT 4 INCHES IN DIA AND LIGHTER CORROSION FOR ABOUT A 12 INCH DIAMETER. SUBMITTER STATED THAT SOMETHING WAS SPILLEDSDR P5CA9600807Bulkhead Web · crackedCRACK AT APU DUCT CUTOUT AT LEFT WHEEL WELL BULKHEAD. REPAIRED WITH KIT 015M0425-1 PER BAC SERVICE BULLETIN 747-53-2309.SDR CALA9601802Bulkhead · crackedINSPECTION FOUND A .4375 INCH CRACK AT RT CORNER OF BULKHEAD BS 400. A CRACK OF UNIDENTIFIED LENGTH WAS FOUND AT LT CORNER OF BULKHEAD BS 400. THE AREAS WERE REPAIRED IAW ECRA 5310-03369.SDR DL73K962459Bulkhead · crackedSTATION 178 BULKHEAD WAS FOUND CRACKED IN SEVERAL LOCATIONS. DAMAGE CUTOUTS ARE 1 INCH X 2 INCH AT RBL 4, WL 200 AND WL 203, AND LBL 4, WL 200, AND A 1 INCH BY 1 INCH AT RBL 7 WL 200. IN ADDITION TO THE WEB CRACKS, THE VERTICAL CHORD HAS A .50 INCH CRACK AT SDR ABXA9700695Bulkhead Clip · crackedDURING ACCEPTANCE INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER CRACKED AT LONGERON 15L. REPLACED END CLIP AT LONGERON 15L IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.SDR ABXA9700325Bulkhead Ftg · crackedDURING C-CHECK, THE AFT PRESSURE BULKHEAD AFT RADICAL 16 WAS FOUND CRACKED ON THE INBOARD END. REPLACED IAW DC9 SRM.SDR 9622561227Bulkhead · corrodedDURING T-CHECK, FOUND CORROSION ON THE FORWARD SIDE OF THE FS 1521 CENTER LANDING GEAR WHEEL WELL BULKHEAD FROM LBL 12 TO RBL 12, 18 INCHES ABOVE THE SHELF. REPAIRED THE BULKHEAD PER EA 12-110282.SDR USAA960685Bulkhead Angle · crackedPIT - DURING SIP VISIT, SIP REF NR 53-10-06, FOUND 2 CRACKS, ONE 6 INCH AND ONE 3.5 INCH AT CONNECTION ANGLE AT FORWARD PRESSURE BULKHEAD, FRAME 1550 AFT BETWEEN STRINGER NR 72 AND STRINGER NR 3. DETECTED BY VISUAL, DYE PENETRANT AND EDDY CURRENT. STOP DRILLSDR TWAA9613007Bulkhead Panel · corrodedMCI - DURING OP-16, FOUND CORROSION ON ALL SUPPORTS ON VERTICAL BULKHEAD PANEL, FS 1322. REMOVED CORROSION PER SRM 91-01-3, AND REPLACED PARTS PER SRM 51-10. (M)SDR 9622559854Bulkhead Panel · crackedDURING H-CHECK, FOUND A CRACK IN THE HORIZONTAL PRESSURE PANEL AT FS 83, LEFT SIDE. REPAIRED PANEL (P/N 9910073-3) PER EA 98-11708.SDR SWAA961097Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACK AT WL 191 AND 201, LBL 5. REPAIRED PER BOEING SRM.SDR CALA9601872Blkhd Stiffener · corrodedINSPECTION FOUND CORROSION AROUND LOWER BOLT HOLE OF T-SHAPED VERTICAL STIFFENER AT CENTER WHEELWELL AFT FACE OF FORWARD BULKHEAD, XCW -15.0. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM'S 51-10-00, 51-21-01, AND 51-31-01.SDR RRXA96118Bulkhead · holeWHILE PREFORMING CONSTANT SECTION INSPECTION FOUND A 3 INCH HOLE IN AFT PRESSURE BULKHEAD WEB AT Y=1606 RT. REPAIRED BY DOUBLER REPAIR IAW DALFORT AVIATION EXPEDITE ENGINEERING AUTHORIZATION XEA: X8-53-866.SDR MWEA96609Bulkhead Door · dentedDURING D-CHECK, FOUND AFT PRESSURE BULKHEAD PLUG DOOR HAS DENT IN LOWER PAN NEAR BAYONET. MAINTENANCE INSTALLED REPAIR IAW SRM 52-01 FIG 2.SDR MWEA96581Bulkhead Doubler · missingDURING D-CHECK, FOUND PART OF FINGER DOUBLER MISSING ON FWD SIDE OF AFT PRESSURE BULKHEAD AT 10 O'CLOCK POSITION NEAR DOOR JAMB. FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 53-01.SDR MWEA96580Bulkhead · scratchDURING D-CHECK, FOUND SMALL SCRATCH ON FWD SIDE OF AFT PRESSURE BULKHEAD FIVE INCHES ABOVE FLOOR LEVEL BLENDED BEYOND LIMITS. INSTALLED REPAIR IAW DAC TELEX SVC-ORD-0246/DMF.SDR MWEA96566Blkhd Stiffener · crackedDURING D-CK, FOUND CRACKED STIFFENER ON AFT SIDE OF AFT PRESSURE BULKHEAD JUST BELOW DOOR JAMB. INSTALLED STIFFENER IAW SRM 53-01.SDR MWEA96565Blkhd Stiffener · crackedDURING D-CK, FOUND CRACK IN STIFFENER, AFT SIDE OF AFT PRESSURE BULKHEAD AT FOUR O'CLOCK POSITION JUST OUTBD OF DOOR JAMB APPROX .25 INCH IN LENGTH. INSTALLED DOUBLE ANGLE REPAIR IAW SRM 53-01, SHEET 4.SDR MWEA96554Bulkhead Fitting · corrodedDURING D-CK, FOUND END FITTING AT PRESSURE BULKHEAD T-CAP HAS HEAVY CORROSION LONG 26L. REPLACED END FITTING IAW SRM 51-10-4 AND 51-30.SDR 96ZZZM1523Bulkhead Support · corrodedMCI - DURING OP-16, FOUND CORROSION ON BULKHEAD FLOOR SUPPORT, FS 1322. INSTALLED NEW SUPPORT PER SRM 51-01 AND TWA STANDARD PRACTICES.SDR UPS96421325Bulkhead Web · crackedINSPECTION TYPE-C, CRACK IN BULKHEAD WEB AT BS 1480. INSTALLED REPAIR DOUBLER IAW UPS EO B747-5310-3100C.SDR CALA9601536Blkhd Fasteners · brokenINSPECTION FOUND THREE EACH RIVET HEADS BROKEN OFF AT BULKHEAD STA 1183 UPPER AFT WEB, LT SIDE. THE FASTENERS WERE REMOVED AND REPLACED IAW SRM 51-30-2.SDR AALA961505Bulkhead · crackedTUL - FOUND CRACK IN PRESSURE BULKHEAD STATION 110 AFT OF LEFT TRUNNION. INSTALLED FIGURE DOUBLER PER SRM 53-04 FIG 38 SHEET 21. (M)SDR 97ZZZX1499Bulkhead · corrodedDURING C-CHECK INSPECTION, INTERGRANULAR CORROSION WAS NOTED ON LOWER CHORD OF BULKHEAD STA 351 BETWEEN S21L EXTENDING TO S26L.SDR 97ZZZX1434Bulkhead · corrodedDURING C-2 INSPECTION, CORROSION WAS NOTED ON THE BACKSIDE BULKHEAD STA 294.5 EXTENDING FROM RBL 25 TO RBL 45.SDR 97ZZZM390Bulkhead Rivets · mis installedFORWARD SIDE OF REAR PRESSURE DOME , 2 RIVETS NEED SHIMS AT HORIZONTAL STIFFENERS TO CENTER RING AS MARKED. DRILLED OUT 2 RIVETS MADE SHIM FROM SHEET METAL, INSTALLED SHIM AND 2 RIVETS. (M)
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