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 96ZZZX3204Bulkhead · crackedDURING ANNUAL INSPECTION, HORIZONTAL STABILIZER WAS FOUND TO HAVE LOOSE MOTION. A DOUBLER KIT FROM CESSNA WAS INSTALLED TO CORRECT THIS PROBLEM. HOWEVER, DURING REPAIR, IT WAS NOTED THE RUDDER BELLCRANK HAD ELONGATED HOLES WHERE THE CABLES ATTACHED AND THE TSDR SWAA960382Bulkhead Web · crackedDURING SCHEDULED SV CHECK, FOUND BULKHEAD AT BS 178 PRESSURE WEB CRACKED 3 PLACES AT WL 213, LBL 4.7 AND LBL 6.7, WL 209.5. REPAIRED PER BOEING SRM.SDR SWAA960381Bulkhead Web · crackedDURING SCHEDULED SV CHECK, FOUND BULKHEAD AT BS 178 PRESSURE WEB CRACKED 3 PLACES AT WL 201, WL 199 AND WL 198, RBL 4.7. REPAIRED PER BOEING SRM.SDR SWAA960380Bulkhead Web · crackedDURING SCHEDULED SV CHECK, FOUND BULKHEAD AT BS 178 PRESSURE WEB CRACKED AT WL 213, RBL 6.7. REPAIRED PER BOEING SRM.SDR RAAAE896011Blkhd Stiffener · corrodedDURING SCHEDULED NR 2 CHECK, FOUND FS 200, LBL 7, BULKHEAD VERTICAL STIFFENER CORRODED AT STRINGER 38. REPAIRED PER SRM 51-3-7, FIG 1, SHT 2. (M)SDR DL73E961288Bulkhead Web · crackedDURING ACOMPLISHMENT OF SI 3-69482-12, TWO CRACKS WERE DISCOVERED ON THE FWD FACE OF THE STA 178 BULKHEAD WEB. THE FIRST CRACK IS LOCATED UNDER THE RBL 5.7 VERTICAL STRAP AT APPROX WL 200 AND THE SECOND IS LOCATED UNDER THE LBL 5.7 VERTICAL STRAP AT APPROX WLSDR DL72P961627Bulkhead Web · crackedTHE FS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 27. THERE IS A .125 VERTICAL CRACK AND A .5 HORIZONTAL CRACK AT WL 170. THE WEB IS A BONDED ASSEMBLY OF CLAD 2024-T3 WITH A LOCAL THICKNESS OF 0.050. THE CRACK LOCATION IS OUTSIDE OF THE INSPECTION AREA SPECSDR DL72P961225Bulkhead Web · crackedTHE BS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 27. THERE IS A .125 VERTICAL CRACK AND A .5 HORIZONTAL CRACK AT WL 170. THE WEB IS A BONDED ASSEMBLY OF 2024-T3 CLAD WITH A LOCAL THICKNESS OF 0.050. THE CRACK LOCATION IS OUTSIDE OF THE INSPECTION AREA SPECSDR ABXA9600559Bulkhead Tee Cap · crackedDURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD T-CAP CRACKED AT APPROXIMATELY LONGERON 27L. REPLACED T-CAP IAW DC-9 SRM 53-03, FIGURE 37A.SDR ABXA9600551Bulkhead Tee · trimmedDURING C-CHECK INSPECTION AND AFT PRESSURE BULKHEAD T-CAP CHANGE, LONGERON 25 LEFT TEE WAS TRIMMED FOR ACCESS. REPAIRED IAW ABX REA D953-15276-MR.SDR AU960575Bulkhead · cracked(AUS) FUSELAGE BULKHEAD LOCATED AT FS 155.76 CRACKED AT LOWER RH CORNER- CRACK EXTENDED FOR THE FULL WIDTH OF THE ANGLESDR RRXA96105Bulkhead · corrodedBULKHEAD CAP AT Y=70 BETWEEN LONGERONS 28L TO 28R CORROSION DAMAGE. BULKHEAD CAP REPAIRED BY DOUBLER AND FILLER REPAIR IAW REO-01930 AND TREATED AREA IAW DC-8 SRM 51-1-8.SDR AALA960752Bulkhead · corrodedTUL - FOUND CORROSION ON FWD SIDE OF BULKHEAD STATION 1309 LEFT AT BOTTOM OF BULKHEAD BETWEEN NR 1 AND NR 2 SEAT TRACKS. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01. (M)SDR SWAA960341Blkhd Web · crackedDURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 178 WL 277 AND AT RBL 11.7 WL 219. REPAIRED PER BOEING SRM.SDR SWAA960325Blkhd Web · chafingDURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD WEB CHAFING DAMAGE AT BS 727 RBL 6 WL 164 UNDER FLAP DRIVE GEARBOX. INSTALLED REPAIR PER TRAMCO EWO 96-0115.SDR SWAA960321Blkhd Web · damagedDURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD WEB AND BULKHEAD STIFFENER DAMAGED AT BS 1016 TO 1020. REPAIRED PER BOEING SRM.SDR DL73E961068Blkhd Stiffener · crackedDURING ACCOMPLISHMENT OF S.I. 3-69482-12, CRACKS WERE DISCOVERED IN THE BS 178 BULKHEAD WEB AND THE RBL 5.7 VERTICAL STIFFENER. THE VERTICAL STIFFENER AT RBL 5.7 ADJACENT TO WL 15 HAS A 1 INCH CRACK ALONG THE RADIUS. THE CHORD IS MANUFACTURED FROM BAC1505-10SDR 96FDEA00886Bulkhead Fitting · crackedNR0089 AND 027, CRACK IN FLANGE OF 740 FORGING RT SIDE FROM STR 19R TO INTERCOSTAL. *S/D* REPLACED 740 FORGING RT SIDE PER FEDEX EA 7-5310-29171.SDR UPS96420101Blkhd Web · corrodedINSPECTION TYPE 'C', FOUND ON WEB EDGE FASTENER SEM AT LT AT STR 38L WL 225 AT BS 2360 REAR PRESS BULK. REPAIRED DAMAGE IAW SRM 51-10-04 FIG 86 BOEING TELEX UPS-AMS-96-012 3RE APP DOC DFX 96-104, EFN 747-0761.SDR CA960517103Bulkhead · cracked(CAN) BULKHEAD ASSEMBLY BUCKLED AND CRACKED FROM LIGHTENING HOLE THROUGH TO INBOARD FLANGE.SDR CALA9600799Blkhd Stiffener · crackedINSPECTION FOUND A .5 INCH CRACK IN RADIUS OF VERTICAL STIFFENER AT STA 727 BULKHEAD. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2 AND 51-21.SDR AWXA960311Blkhd Doubler · crackedPAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND BULKHEAD DOUBLER AT BS 1156 CRACKED BETWEEN TWO FASTENERS. STOP DRILLED CRACK, NDI VERIFIED CRACK CONTAINMENT. REPAIRED WIT MOD PER SB 53-1086 R3. (M)SDR 9610939968Press Dome T Cap · corrodedDURING H-CHECK, FOUND CORROSION ON THE PRESSURE DOME T-CAP AT FS 604, LONGERON 30. REPAIRED T-CAP (P/N 5914865-29) PER EA 99-109435.SDR SWAA960268Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AROUND 3 FASTENERS, AT WL 234, RBL 7-10. REPAIRED PER TI T1-A53-015.SDR SWAA960267Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 6.7, WL 197.5-198.6, AT LBL 4.7, WL 197-198.6, AT LBL 4.7, WL 202.5-203.5, AND RBL 4.7, WL 197.5 -198.5. REPAIRED PER SWA EWO 97-0189.SDR DLL13961024Bulkhead Web · crackedCRACKS WERE FOUND IN THE F.S. 1212 CANTED BULKHEAD WEB. THE DAMAGE WAS TRIMMED OUT, FILLED AND REINFORCED. ACCOMPLISHED REPAIRS PER DL ERS 273699-14.SDR CALA9600722Bulkhead Web · crackedINSPECTION FOUND A 7 INCH CRACK IN BULKHEAD PRESSURE WEB AT STA 664, RBL 30. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR 96ZZZX2637Bulkhead · corrodedDURING C-CHECK, FOUND SKIN HAS CORROSION LEVEL 2 AT AFT BULKHEAD WALL FORWARD SIDE FLOOR LEVEL, RBL 7 INCHES AND RBL 15 INCHES. REPAIRED IAW DACO ACTION NR 291159.SDR SWAA960245Blkhd Channel · crackedDURING SCHEDULED 1/2 D-CHECK, FOUND U-CHANNEL CRACKED AT BS 727 BULKHEAD AT RBL 3. REPLACED PER BOEING SRM.SDR SWAA960241Blkhd Strap · crackedDURING SCHEDULED 1/2 D-CHECK, FOUND RT HORIZ STRAP CRACKED AT FWD END AT BS 727 BULKHEAD, AT S22R. REPLACED PER BOEING SRM.SDR SWAA960239Bulkhead · crackedDURING SCHEDULED 1/2 D-CHECK, FOUND SEVERAL CRACKS AT BLOW OUT PANEL CUTOUT IN CENTER OF BULKHEAD AT BS 948. REPAIRED PER BOEING SRM.SDR AWXA960305Bulkhead Fitting · corrodedPAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND BULKHEAD SUPPORT FITTING CORRODED BEYOND LIMITS. REPLACED FITTING PER IAW SCM 51-10-1. (M)SDR SCNA96110Blkhd Stiffener · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STIFFENER, BS 1183 LBL 59 WL 220. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 51-40-4.SDR SCNA96109Blkhd Stiffener · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STIFFENER, BS 1183 RBL 61, WL 220. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 51-40-4.SDR AU960604Bulkhead · cracked(AUS) FUSELAGE BULKHEAD CRACKED IN AREA OF LOWER CURVED SECTION - CRACKLENGTH 6.35MM (0.25IN)SDR 96ZZZX2471Bulkhead · crackedWHILE PERFORMING 900 HOUR/36 MONTH PRESSURE BULKHEAD INSPECTIONS, FOUND SMALL CRACK AT RIVET HOLE ON FORWARD PRESSURE BULKHEAD. CRACK WAS ON AIR BOX. AIRCRAFT HAD ABOUT 7,500 CYCLES. REPAIR DATA OBTAINED FROM DER TO INSTALL PATCH. SUBMITTER STATED THIS IS SDR SCNA96124Bulkhead Strap · crackedDURING HEAVY MAINTENANCE VISIT, CRACKS WERE FOUND IN THE FORWARD BULKHEAD STRAP/SKIN BETWEEN THE 2ND, 3RD, 4TH, AND 5TH FASTENERS AT BS 178, BL ZERO, WL 183. FABRICATED A REPAIR DOUBLER AND STRAP IN ACCORDANCE WITH B727 SRM 51-30-2, AND SB 727-23-0065.SDR DL72W961019Bulkhead Fitting · misdrilledWHILE ACCOMPLISHING A PRELIMINARY ATTEMPT TO FIT THE 65-18722-8 FORWARD MOUNT FITTING INTO POSITION, NOTED THAT SEVEN OF THE HOLES COMMON TO THE B.S. 1183 FRAME DO NOT LINE UP. THESE HOLES AND THE AMOUNT OF OFFSET ARE INDICATED ON FIGURE 1. DL ERA 3033483-14SDR 96ZZZX2269Blkhd Bracket · corrodedLEVEL 2 CORROSION, CENTER CARGO COMPARTMENT BELOW FLOOR PANEL AT FORWARD BULKHEAD, STA 1363, BL 6 ON LT SIDE SUPPORT BRACKET, HAS CORROSION. REMOVED AND REPLACED DAMAGED BRACKET PER SRM 51-10-5.SDR 96ZZZM924Bulkhead Bracket · corrodedFOUND LEVEL 2 CORROSION, CENTER CARGO COMPARTENT BELOW FLOOR PANEL AT FORWARD BULKHEAD, STATION 1363, BL 6 ON LEFT SIDE SUPPORT BRACKET HAS CORROSION. REMOVED AND REPLACED DAMAGED BRACKET PER SRM 51-10-5. (M)SDR AU960633Bulkhead · cracked(AUS) FORWARD DOORPOST BULKHEAD CRACKED AT RELIEF NOTCHES ON BOTH LH AND RH SIDES - CRACK LENGTH 7MM (0.275IN)SDR 9610919862Bulkhead Former · crackedDURING H-CHECK, FOUND A .50 INCH CRACK IN THE AFT PRESSURE BULKHEAD HORIZONTAL FORMER AT Z=14. REPAIRED FORMER (P/N 9915558-27) PER EA 98-108866.SDR 96ZZZX3101Bulkhead · gougedATW - LT MLG BAY, FRAME 29 BULKHEAD, HAS A GOUGE APPROXIMATELY 7 INCHES LONG WITH 3 DAMAGED RIVET HEADS AND IS APPROXIMATELY .012 INCH DEEP. MEASURED DEPTH AGAIN WITH PAINT STRIPPED. REPAIRED LT MLG AT FRAME 29. REFER TO WC NR 1063 FOR NDT. EPOXY PRIMED ANSDR 96ZZZX3100Bulkhead · gougedATW - RT MLG BAY FRAME 29 BULKHEAD HAS A GOUGE APPROXIMATELY 8.50 INCHES LONG WITH 4 DAMAGED RIVET HEADS AND IS APPROXIMATEY .009 INCH DEEP. AFTER REMOVAL OF PAINT, RE-MEASURED DEPTH FOUND TO BE .007 INCH DEEP AND REPORTED TO BAE. NDT WAS ACCOMPLISHED ON WC SDR 96ZZZX2991Bulkhead · crackedDURING ANNUAL INSPECTION, RT BULKHEAD AT FS 27.25 WAS FOUND CRACKED. THIS AND THE OPPOSITE PART ON THE LT SIDE ARE WHERE THE NLG STEERING CABLES ATTACH VIA STEEL PULLEY BRACKETS. SUBMITTER SUGGESTS MFG EITHER PRODUCE REINFORCEMENT KIT OR STRENGTHEN NEW COMPOSDR DL72P961144Bulkhead Web · crackedTHE BS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 26. THERE IS A .25 INCH CRACK AT WL 170. THE WEB IS A BONDED ASSEMBLY OF 2024-T3 CLAD WITH A LOCAL THICKNESS OF .050 INCH. THE CRACK LOCATION IS OUTSIDE OF THE INSPECTION AREA SPECIFIED BY BOEING SERVICE BULSDR DL72W961020Blkhd Web · crackedTHE STA 1183 BULKHEAD WEB WAS FOUND CRACKED IN TWO LOCATIONS. THE DAMAGE WAS TRIMMED OUT WITH DIMENSIONS OF 2.6250 INCH AT LBL 8, WL 190 AND 8 INCH BY 3.1250 INCH AT LBL 14, WL 173. THE BULKHEAD WEB IS MANUFACTURED FROM 0.050 INCH CLAD 2024-T3. THIS ER/A AUSDR W8PA960017Bulkhead Bracket · brokenDURING C-CHECK, FOUND AFT BAY BULKHEAD ATTACH BRACKET BROKEN. INSTALLED NEW BRACKET AND DOUBLER. (M)SDR SWAA960213Bulkhead · crackedDURING SCHEDULED C3 CHECK, FOUND BULKHEAD SKIN CRACKED AT CONTROL CABIN LEFT SIDE, 6 INCHES UP FROM FLOOR AND 6 INCHES FROM O/B EDGE. REPAIRED PER BOEING SRM.SDR USAA960394Bulkhead · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK 1156 BULKHEAD. STOP DRILLED BOTH ENDS OF CRACK, MANUFACTURED, HEAT TREATED, AND INSTALLED REPAIR. REPAIRED PER EO 5391G3569. (X)
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