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 95ZZZX886Bulkhead · crackedJFK - DURING CHECK C-9B, FOUND A 28 INCH VERTICAL CRACK IN AFT BULKHEAD, STA 1363, THROUGH 8 STIFFENERS, WITH 7 STIFFENERS SHEARED. STOP DRILLED CRACKS AND REPAIR PER SRM 53-11-00, FIGURE 851. AIRCRAFT TOTAL TIME 60,716 HOURS; 22,699 CYCLES.SDR 95ZZZX885Intercostal · brokenJFK - DURING CHECK C-9B, FOUND FORWARD END OF INTERCOSTAL, AFT BULKHEAD STA 1363, BROKEN AWAY FROM BULKHEAD BETWEEN STRINGERS 41L AND 42L, WHEELWELL. INSTALLED CLIP ANGLE PER SRM 53-12-00. AIRCRAFT TOTAL TIME: 60,716 HOURS; 22,699 CYCLES.SDR 95ZZZX884Blkhd Skin · crackedDURING CHECK C-9B, FOUND .25 INCH CRACK IN AFT BULKHEAD SKIN, STA 1363, ON OUTBOARD RIVET HOLE BETWEEN STIFFENER 15 AND 16; FOUND 4 INCH CRACK AT OUTBOARD FRAME, LT WHEELWELL, AT NR 16 STIFFENER. STOP DRILLED CRACKS AND REPAIRED WITH DOUBLERS PER SRM 53-11-00SDR 95ZZZX1094Bulkhead · crackedFOUND UPPER BULKHEADS CRACKED AT TOP OF RUDDER PEDAL TORQUE TUBE OPENING JUST AFT OF MOUNTING BOLT FOR PN 2460004-1 BELLCRANK ASSY. LT SIDE CRACKED COMPLETELY THROUGH. RT SIDE ALSO DAMAGED DUE TO BOLT HEAD ON THE BELLCRANK HITTING IT. FOUND UPPER BULKHEADS,SDR 95ZZZX1093Bulkhead · crackedFOUND UPPER BULKHEADS CRACKED AT TOP OF RUDDER PEDAL TORQUE TUBE OPENING JUST AFT OF MOUNTING BOLT FOR PN 2460004-1 BELLCRANK ASSY. LT SIDE CRACKED COMPLETELY THROUGH. RT SIDE ALSO DAMAGED DUE TO BOLT HEAD ON THE BELLCRANK HITTING IT. FOUND UPPER BULKHEADS,SDR 95ZZZX1092Bulkhead · crackedFOUND UPPER BULKHEADS CRACKED AT TOP OF RUDDER PEDAL TORQUE TUBE OPENING JUST AFT OF MOUNTING BOLT FOR PN 2460004-1 BELLCRANK ASSY. LT SIDE CRACKED COMPLETELY THROUGH. RT SIDE ALSO DAMAGED DUE TO BOLT HEAD ON THE BELLCRANK HITTING IT. FOUND UPPER BULKHEADS,SDR 95ZZZX1091Bulkhead · crackedFOUND UPPER BULKHEADS CRACKED AT TOP OF RUDDER PEDAL TORQUE TUBE OPENING JUST AFT OF MOUNTING BOLT FOR PN 2460004-1 BELLCRANK ASSY. LT SIDE CRACKED COMPLETELY THROUGH. RT SIDE ALSO DAMAGED DUE TO BOLT HEAD ON THE BELLCRANK HITTING IT. FOUND UPPER BULKHEADS,SDR 9502089981Blkhd Web · oil cannedDURING PERIODIC CHECK, FOUND OIL CANNING IN THE LEFT LAVATORY BULKHEAD WEB AT THE INBOARD LIGHTENING HOLE. REPAIRED PER EA 99-096894.SDR ABXA9500151Bulkhead Skin · dentedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A DENT AND PUNCTURE IN AFT PRESSURE BULKHEAD SKIN, FORWARD FACE, BETWEEN LONGERON 29R AND 30R APPROXIMATELY EIGHT INCHES UP FROM TEE CAP. REPAIRED IAW DC-9 SRM CHAPTER 53-01, FIGURE 1, SHEET 2.SDR USAA950133Hat Channel · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 30 INCH CORRODED AREA LT LAVATORY AFT FWD BULKHEAD. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)SDR 95ZZZX846Bulkhead · corrodedJFK - DURING CHECK C-3B, FOUND CORROSION AT SIX O'CLOCK POSITION OF DRAIN HOLES FORWARD OF PRESSURE BULKHEAD STA 1809. REMOVED DOUBLER, REPAIRED FRAME PER SRM 51-50-03, AND REINSTALLED ORIGINAL DOUBLER. AIRCRAFT TOTAL TIME: 63,846 HOURS; 31,029 CYCLES.SDR 95ZZZX844Former Ring · corrodedJFK - DURING CHECK C-3B, FOUND CORROSION ON FORMER RING AT SIX O'CLOCK POSITION IN AREA OF DRAIN HOLES, FORWARD SIDE OF PRESSURE BULKHEAD AFT OF LAVATORY TANK. REMOVED CORROSION SECTION OF FORMER RING AND SPLICED IN NEW SECTION PER SRM 53-11-00, PAGE 815. ASDR 95ZZZX842Rivets · missingJFK - DURING CHECK C-3B, FOUND TWO RIVETS MISSING FROM AFTER PRESSURE BULKHEAD AND AREA BULGE AT SIX O'CLOCK POSITION. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-11-00, PAGE 808. AIRCRAFT TOTAL TIME: 63,846 HOURS; 17,917 CYCLES.SDR 95ZZZX841Web · crackedJFK - DURING CHECK C-3B, FOUND A ONE INCH CRACK IN AFT PRESSURE BULKHEAD WEB. INSTALLED REPAIR PER SRM 53-11-00, PAGE 808, FIGURE 805. AIRCRAFT TOTAL TIME: 63,846 HOURS; 17,917 CYCLES.SDR USAA950225Bulkhead · crackedPIT - DURING SCHEDULED STRUCTURES VISIT, FOUND 7.5 INCH CRACK IN AFT SIDE OF FORWARD PRESSURE BULKHEAD BETWEEN STA 72 AND STA 73. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PLATE PER SRM 53-11-00, PAGE 2. (X)SDR USAA950063Blkhd · crackedPIT - DURING SCHEDULED SIP VISIT FOUND A 2.5 INCH CRACK IN THE REAR PRESSURE BULKHEAD BEAM NR 3 AT BODY LINE 750 RT. REF - INSPECTION SIP 53-10-03 LFEC PROCEDURE. INSTALLED WEB REPAIR PATCH AND NEW REAR FACE DOUBLER AND TWO 92. REPAIR ANGLES PER USAIR EA 29SDR UPS802104Supports · crackedWHILE IN 'B' CHECK MAINTENANCE, FOUND 3RD AND 4TH HORIZONTAL SUPPORTS ABOVE NR 60, DOOR CRACKED ON AFT PRESSURE BULKHEAD. REPAIRED PER UPS EO DC8-5310-6570 AND DC8-5310-6605A.SDR SWAA950085Bulkhead · crackedDURING SCHEDULED C3 CHECK, FOUND PRESSURE BULKHEAD CRACKED IN RADIUS OF FWD VERTICAL FLANGE OF T-SUPPORT AT BS 178 LBL 5.5 WL 183.0. REPAIRED PER SWA RA 1-253-1239.SDR AWXA9500049Intercostal · crackedPHX - FLT 31 - DURING C-8 INSPECTION, FOUND INTERCOSTAL ON BULKHEAD 727 CRACKED BETWEEN LT VERTICAL FRAMES 4 AND 5. REPAIRED PER SRM 51-30-2 AND 53-10-02. (W)SDR AWXA9500048Blkhd Angle · crackedPHX - FLT 31 - DURING C-8 INSPECTION, FOUND 7 CRACKS IN NOSE WHEEL WELL AFT VERTICAL BULKHEAD, STA 294.5 RBL 75, LOCATION 5TH FROM TOP TO 12TH. CRACKS WERE VERIFIED BY EDDY CURRENT. REPAIRED PER AWA EO 53-11-08 PART II. (W)SDR DL72W950564Support · corrodedDURING HMV, CORROSION ON TOP HORIZ SUPPORT STA 1166 BULKHEAD AT CENTER CEILING SUPPORT STRAP. REPAIRED PER SRM 51-40-4 FIG 3.SDR 9501281146Bulkhead Angle · corrodedDURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SUPPORT ANGLE OF THE FORWARD BULKHEAD IN THE CENTER WHEEL WELL, AT RBL 10-29. INSTALLED REPAIR ANGLE PER EA 11-93766.SDR USAA950134Hat Channel · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 30 INCH CORRODED AREA RT AFT LAVATORY FWD BULKHEAD. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)SDR 95ZZZX5352Angle · crackedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE MAIN CABIN COMPARTMENT AFT PRESSURE BULKHEAD ATTACH ANGLE IS CRACKED AT APPROXIMATELY 10 O'CLOCK POSITION, RT SIDE. FABRICATED AND INSTALLED PRESSURE BULKHEAD REPAIRS IAW DC9 SRM 53-05-SDR 9501141146Bulkhead Support · corrodedDURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SUPPORT ANGLE OF THE FORWARD BULKHEAD IN THE CENTER WHEEL WELL AT LBL 19-29. INSTALLED REPAIR ANGLE PER EA 11-93766.SDR CAL950069Blkhd Support · corrodedGSO - INSPECTION FOUND THE RT AFT LAVATORY FWD BULKHEAD SUPPORT CORRODED. THE CORRODED SUPPORT ANGLE WAS REMOVED, AND A NEW ONE WAS INSTALLED IAW SRM 53-10-2, 51-30-2, AND 51-10-1. (W)SDR ABXA9500048Blkhd Tee · gougedDURING C-CHECK INSPECTION, FOUND BULKHEAD STA 965 INBOARD T-CAP HAD GOUGES AND DRILL STARTS FROM LONGERON 18L TO 18R, FORWARD AND AFT EDGES. REPAIRED IAW DC-9 SRM 53-01 FIGURE 1 SHEET 3 AND ABX REA D953-10788-MR.SDR SWAA950051Bulkhead · crackedDURING SCHEDULED QUARTER D CHECK, FOUND MANY CRACKS EXTENDING FROM THE INBOARD VERTICAL ROW OF BULKHEAD FASTENER HOLES, LBL 5.25 AND WL 185.5. REPAIRED PER SWA RA 1-253-1236.SDR SWAA950050Bulkhead · crackedDURING SCHEDULED 1/4 D CHECK, FOUND SEVERALS CRACKS EXTENDING FROM UNDER RIVET HEADS AT FWD SIDE OF PRESSURE BULKHEAD AT BS 178, LBL 6 AND WL 183.0. REPAIRED PER SWA RA 1-253-1236.SDR ABXA9500039Blkhd Tee · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION ON BULKHEAD TEE AT STA 1039 BETWEEN LONGERON 30 AND 26L. REPAIRED TEE IAW ABX REA D953-10761-MR.SDR 95ZZZX1303Bulkhead · crackedDURING REPLACEMENT OF THE FIREWALL, THE FORWARD BULKHEAD OF THE FRONT DOOR POST BULKHEAD ASSEMBLY WAS FOUND CRACKED. THERE WAS A CRACK APPROXIMATELY 3 INCHES IN LENGTH WHERE THE ELEVATOR CONTROL BRACKET ATTACHES TO THE BULKHEAD. THE CRACK APPEARS TO HAVE ORISDR 95ZZZW52Horiz Beam · crackedDURING C-CEHCK, AFT PRESSURE BULKHEAD THIRD HORIZONTAL BEAM FROM BOTTOM CRACKED AT BL '0' 3 INCHES. REPAIRED PER DOUGLAS SRM CHAPTER 53. TOTAL CYCLES 24057.SDR 9500939945Bulkhead · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN FS 110 BULKHEAD TUNNEL AT LONGERON 27R, 6 INCHES UP FROM BOTTOM CORNER. REPAIRED PER XEA X9-53-50.SDR ABXA9500010Web · damagedDURING C-CHECK, INSPECTION FOUND DRILL STARTS IN LEFT P-DOME SKIN WEB. REPAIRED IAW ABX REA D953-10713-MR.SDR ABXA9500006Web · dentedDURING C-CHECK INSPECTION, FOUND DENT IN LEFT P-DOME SKIN AT APPROXIMATELY THE 10:00 O'CLOCK POSITION. REPAIRED DENT IAW ABX REA D953-10728-MR.SDR IXXA9526Bulkhead Web · crackedDURING ROUTINE C-CHECK, A 1 INCH CRACK WAS LOCATED IN THE AFT PRESSURE BULKHEAD, FS 1766, AT LONGERON 11 LEFT. REPAIR WAS ACCOMPLISHED IAW AIRCRAFT SRM AND SB 53-73. (X)SDR ABXA9500009Web · dentedDURING C-CHECK INSPECTION, FOUND P-DOME DENTED AT APPROXIMATELY THE 12:30 O'CLOCK POSITION. REPAIRED DENT IAW ABX REA D953-10735-MR.SDR ABXA9500008Web · dentedDURING C-CHECK INSPECTION, FOUND TWO DENTS IN RIGHT P-DOME SKIN BETWEEN THE 2:00 AND 3:00 O'CLOCK POSITIONS. REPAIRED DENTS IAW ABX REA D95310735-MR.SDR ABXA9500007Web · dentedDURING C-CHECK INSPECTION, FOUND P-DOME DENTED AT APPROXIMATELY THE 2:00 O'CLOCK POSITION. REPAIRED DENT IAW ABX REA D953-10735-MR.SDR ABXA9500073Frame · gougedDURING COMPLIANCE OF A.D. 79-24-01; S.B. 53-127, FOUND GOUGE AT 10 O'CLOCK POSITION ON PLUG DOOR STOP. BLENDED OUT GOUGE AT 10 O'CLOCK POSITION IAW DC-9 SRM 51-01.SDR TSAA9553020Bulkhead Chord · crackedDURING HEAVY MAINTENANCE VISIT, FOUND BS 727 BULKHEAD OUTER CHORD CRACKED BETWEEN S22L AND 23L, 5.25 INCHES LONG. STOP DRILLED PER SRM 51-10-01 IAW BOEING MESSAGE ALO-HNL 94-0388RR DATED 29 DECEMBER 94 AND REPAIRED PER ECO 1325. AIRCRAFT RETURNED TO SERVICE.SDR DL72S950066Bulkhead · crackedDURING LETTER CHECK, FOUND A .75 INCH CRACK IN FS 1183 BULKHEAD WEB AT UPPER EDGE OF HORIZONTAL STIFFENER AT WL 168 AT RBL 25. REPAIRED PER SRM 53-10-9 FIG 6.SDR UP801915Beam · crackMAINTENANCE REPORTED APPROX 1.75 INCH CRACK AT BOTTOM RADIUS OF NR 3 ANGLE (BEAM) ON PRESSURE BULKHEAD AT CENTER. INSTALLED REPAIR IAW EO DC8-6310-6306A, TEMP REV 53-81, 53-7-0.SDR DLL16950259Stiffener · corrodedDURING OVERHAUL AT AFT P-DOME, STIFFENER IS CORRODED ON LWR END WHERE IT TIES TO STR 25. REMOVED CORROSION AND INSTALLED STIFFENER AND SPLICE PER SRM 53-11-00 FIG 809.SDR DLL16950250Stiffener · corrodedDURING OVERHAUL AFT P DOME STIFFENER IS CORRODED FROM WHERE IT TIES TO STR 41 TO HALF WAY UP STIFFENER. REMOVED CORRODED SECTION, INSTALLED STIFFENER SECTION AND SPLICE PER SRM 53-11-00 FIG 809.SDR TSAA9553001Bulkhead · crackedDURING SCHEDULED INSPECTION OF AFT PRESSURE BULKHEAD AT BS 1016, (AD 84-20-03), FOUND .75 INCH EXPOSED CRACK AT RIVET, LOCATED AT AFT CENTER PRESSURE BULKHEAD WEB AT 7 O'CLOCK POSITION. REPAIRED PER ECO 2544. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TIME: 26SDR 95ZZZX546Bulkhead · crackedDURING CHECK C-2D, FOUND CRACK APPROXIMATELY TWO INCHES IN BULKHEAD BELOW APU FLOW CONTROL VALVE, IN RT MLG WHEELWELL. STOP DRILLED CRACK AND INSTALLED DOUBLER PER TWA DWG C03242 AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 61,014 HOURS; 40,930 CYCLES.
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