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.

SDR AWXA200301641Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .125 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB, AFT SIDE AT RBL 75, WL 187. MAINTENANCE CUT OUT CRACKED SECTION OF BS 178 BULKHEAD WEB AT RBL 75, WL 187; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST;Dec 3, 2003 · N174AW · Boeing 73733ASDR AWXA200301581Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .125 INCH CRACK WAS FOUND ON BULKHEAD VERTICAL BEAM WEB BETWEEN BS 178 AND BS 179.5, LBL 5.7, WL 178. MAINTENANCE CUT OUT CRACKED AREA OF BULKHEAD WEB BETWEEN BS 178 AND BS 179.5, LBL 5.7, WL 178; FABRICATED A NEW REPLDec 3, 2003 · N174AW · Boeing 73733ASDR AWXA200301527Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD FORWARD FACE WEB AT BUTTON HEAD HI-LOK HOLES AT 6 O'CLOCK POSITION WL 234 LBL 9 AND LBL 11. MAINTENANCE CUT OUT DAMAGE ON BS 178 BULKHEAD FORWARD FACE WEB AT WL 234 LBL 9 AND LDec 3, 2003 · N174AW · Boeing 73733ASDR COMA0360529Post · crackedTHE RIGHT BULKHEAD POST AT FS 559, RBL 9, WL 50 HAS A CRACKED FLANGE. REMOVED PORTION OF CRACKED FLANGE, FABRICATED AND INSTALLED A REPAIR ANGLE IAW REO 601R-53-41-057.Dec 2, 2003 · N927CA · Cndair CL6002B19SDR SWAA032641Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 202, RBL 5 AND LBL 5. REPAIRED WEB PER SRM.Nov 30, 2003 · N383SW · Boeing 7373H4SDR SWAA032624Bulkhead · crackedDURING SCHEDULED C3 CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 6L. REPAIRED WEB PER SRM.Nov 29, 2003 · N326SW · Boeing 7373H4SDR CA031127011Bulkhead · cracked(CAN) DURING THE 100 HOUR INSPECTION PLAY WAS NOTICED IN THE NOSE GEAR AREA. UPON INSPECTION THE LT NOSE SECTION BULKHEAD WAS FOUND TO BE CRACKED VERTICALLY THROUGH THE CENTER OF THE LIGHTENING HOLE. DOUBLER PATCHES WERE INSTALLED AND RIVETED INTO PLACE AND Nov 25, 2003 · Cessna 310LSDR AWXA200301555Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-04 CHECK A .625 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT LBL 13.5, WL 183. MAINTENANCE CUT OUT CRACK ON BS 178 BULKHEAD WEB AT LBL 13.5, WL 183; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLNov 25, 2003 · N336AW · Boeing 737375SDR AWXA200301554Bulkhead · crackedDURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB, AFT SIDE, AT RBL 5, WL 200.25 TO WL 201.25. MAINTENANCE PERFORMED HFEC INSPECTION TO VERIFY CRACK END, STOP DRILLED CRACK, RE-ACCOMPLISHED HFEC INSPECTION TO VERIFY CRACK CONTAINED; FABRICATEDNov 25, 2003 · N336AW · Boeing 737375SDR SWAA032574Pressure Panel · corrodedDURING SCHEDULED 1/4D CHECK, FOUND A .75 LONG CRACK AT BS 665 BEADED WEB, LBL 32. REPAIRED WEB PER SRM.Nov 21, 2003 · N354SW · Boeing 7373H4SDR CALA0300697Beam · corrodedINSPECTION FOUND STA 110 BULKHEAD BEAM WEB CORRODED AT MAIN BATTERY GROUND STUD HOLE. THE BEAM WEB WAS REPAIRED IAW ECRA 5310-04387.Nov 20, 2003 · N72821 · Doug DC982SDR SWAA032573Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD CRACKED AT STR 7L. REPAIRED BULKHEAD WEB PER SRM AND ERO.Nov 20, 2003 · N343SW · Boeing 7373H4SDR SWAA032558Pressure Panel · crackedDURING SCHEDULED PM CHECK, FOUND A 3.5 LONG CRACK AT NLG W/W SIDE WEB, BS 258. REPAIRED WEB PER SWA EA.Nov 18, 2003 · N501SW · Boeing 7375H4SDR GTIA031042Pressure Panel · corrodedFOUND RIGHT MLG W/W CEILING PRESSURE WEB HAS CORROSION RUNNING UNDER STIFFENERS IN NUMEROUS AREAS. FABRICATED PRESSURE FLOOR DOUBLER AND INTERNAL FINGER DOUBLER. INSTALLED REPAIR PARTS. (M)Nov 17, 2003 · N818NK · Doug DC981SDR UPS03841581Bulkhead · crackedINSPECTION TYPE: C1, AFT PRESSURE BULKHEAD IS CRACKED AT STATION 1766 AT LBL 36, 65 INCHES ABOVE FLOOR LEVEL. REMOVED EXISTING REPAIR DOUBLER,CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT AREA, FABRICATED AND INSTALLED FILLER AND REPLACEMENT DOUBLER I.Nov 14, 2003 · N718UP · Doug DC871FSDR COMA0370052Bulkhead · crackedPRESSURE BULKHEAD WEB AT FS 1098 STR 8R, 9R IS CRACKED AT NR 4 HYD LINE CONNECTION. PERFORMED MAJOR REPAIR IN ACCORDANCE WITH CANADAIR REO 670-53-61-034 REV B.Nov 14, 2003 · N340CA · Cndair CL6002C10SDR COMA0370051Bulkhead · crackedPRESSURE BULKHEAD WEB AT FS 1098 STR 8L - 9L IS CRACKED AT NR 4 HYD LINE CONNECTION. PERFORMED MAJOR REPAIR IN ACCORDANCE WITH CANADAIR REO 670-53-61-034 REV B AND DEVIATION ENG ORDER (WVAC) 601R-53-4406.Nov 14, 2003 · N340CA · Cndair CL6002C10SDR CALA0300710Bulkhead · damagedAN IMPROPER REPAIR WAS DISCOVERED ON THE AFT PRESSURE BULKHEAD DOME WEB JUST AFT OF THE Y-CHORD BETWEEN S9R AND S11R DURING A 4C CHECK AT HOBBY. THE AREA WAS REPAIRED IAW ECRA 5311-01174.Nov 12, 2003 · N12318 · Boeing 7373T0SDR SWAA032493Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED ABOVE STR 7L. REPAIRED WEB PER SRM.Nov 10, 2003 · N661SW · Boeing 737317SDR C2XA03SH442Firewall · crackedSHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT UPPER APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Nov 10, 2003 · N16541 · Emb EMB145LRSDR SWAA032483Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND 2 EA CRACKS AT BS 178 BULKHEAD WEB LBL 7, WL 213 AND LBL 5, WL 213. REPAIRED BULKHEAD WEB PER SRM.Nov 9, 2003 · N525SW · Boeing 7375H4SDR COMA0370049Bulkhead · crackedFS 1098.20 BULKHEAD RIGHT WEB BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B.Nov 9, 2003 · N371CA · Cndair CL6002C10SDR DL73S031001Bulkhead · crackedA SMALL CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE FS 1016 AFT P-DOME WEB AT BL 0, WL 244. THE CRACK EMANATED IN 2 DIRECTIONS FROM THE HOLE AND WAS TOTAL OF .625 INCH LONG (INCLUDING HOLE DIA). THE CRACK WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLENov 8, 2003 · N312DL · Boeing 737232SDR SWAA032478Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED (3 EA) AT LBL 1, WL 187, RBL 1, WL 187, AND RBL 5, WL 213. REPAIRED WEB PER SRM.Nov 7, 2003 · N358SW · Boeing 7373H4SDR SWAA032467Pressure Panel · crackedDURING SCHEDULED 5Y CHECK, FOUND LT AND RT WHEEL WELL CUTOUT AFT WEB DOUBLERS CRACKED. REMOVED AND REPLACED WEBS PER SRM.Nov 6, 2003 · N739GB · Boeing 7377H4SDR C2XA03TY191Firewall · crackedTYS, DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND CRACKED. MAINTENANCE REPAIRED THE CRACKS I/A/W EMB-145-SRM-53-32-13 AND EC5330-01287.Nov 6, 2003 · N16999 · Emb EMB145LRSDR TIM2003F00001Bulkhead · crackedBULKHEAD FOUND TO BE CRACKED AT INSPECTION. (CNTRL NR 81)Nov 5, 2003 · N195GA · Beech 1900CSDR S03853091Bulkhead · canningB-18612 THE DATUM A/C HAD AN OIL CAN CONDITION ON BS 1016 PRESSURE BULKHEAD. THE OIL CAN CONDITION WAS REPAIRED USING THE 738 SRM 53-80-08 REPAIR ON 4 NOV 10/02. THE ABOVE REPAIR BOEING CONSIDER IT WAS STRUCTURALLY ACCEPTABLE AS A TEMPORARY REPAIR, FOR A PERNov 5, 2003 · Boeing 737800*SDR COMA0370047Bulkhead · crackedFS 1098.20 BULKHEAD RIGHT WEB BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPAIRED BY REMOVING AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B.Nov 4, 2003 · N369CA · Cndair CL6002C10SDR SWAA032430Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 187, RBL 1. REPAIRED WEB PER SRM.Nov 3, 2003 · N525SW · Boeing 7375H4SDR COMA0370046Bulkhead · crackedFS 1098.20 BULKHEAD WEB BETWEEN STRINGERS 8L AND 9L IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B.Nov 2, 2003 · N368CA · Cndair CL6002C10SDR SWAA032416Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND 0.5 INCH CRACK IN PRESSURE WEB AT BS 665, LBL 32.5. REPAIRED PER SRM.Oct 31, 2003 · N661SW · Boeing 737317SDR QXEA200301406Bulkhead · crackedCKB- DURING INSPECTION OF THE PRESSURE BULKHEAD LEFT HAND SIDE, NDT SHOWED INDICATIONS OF CRACK. REPAIRED IAW BOMBARDIER EO 670-53-61-034 AND HORIZON AIR EO 53-44B.Oct 29, 2003 · N612QX · Cndair CL6002C10SDR QXEA200301405Bulkhead · crackedCKB- DURING DNT INSPECTION OF THE PRESSURE BULKHEAD AT FS 1098.20 RIGHT HAND SIDE SHOWS INDICATIONS OF CRACK. REPAIRED IAW BOMBARDIER EO 670-53-61-034, AND HORIZON AIR EO 53-44B.Oct 29, 2003 · N612QX · Cndair CL6002C10SDR COMA0370044Bulkhead · crackedFS 1098.20 BULKHEAD RIGHT WEB BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B.Oct 29, 2003 · N367CA · Cndair CL6002C10SDR SWAA032355Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 201, RBL 5.5. REPAIRED WEB PER SRM.Oct 25, 2003 · N692SW · Boeing 7373T5SDR COMA0370043Bulkhead · crackedFS 1098.20 BULKHEAD RT WEB BETWEEN STRINGERS 8R AND 9R ARE CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B AND REO 670-53-61-089.Oct 24, 2003 · N354CA · Cndair CL6002C10SDR 03297625Bulkhead · damagedDURING INSPECTION A DENT WITH A HOLE WAS DISCOVERED AT FS 621.00 RBL 9.00.Oct 24, 2003 · N625BR · Cndair CL6002B19SDR UPS03841551Bulkhead · crackedINSPECTION TYPE:C2 MAIN CABIN AFT PRESSURE BULKHEAD IS CRACKED AT STATION 1766 AT RBL 26 65.5 INCHES ABOVE FLOOR LEVEL CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRO8530007 AND SRM 53-2-5 FIG 14A.Oct 23, 2003 · N867UP · Doug DC873FSDR UPS03841516Bulkhead · crackedINSPECTION TYPE:C2 MAIN CABIN AFT PRESSURE BULKHEAD IS CRACKED 2 PLACES AT STA 1766 AT LBL 26 AND LBL 35, 65 .5 INCH ABOVE FLOOR LEVEL. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW SRM 53-2-5 FIG 14A ANDOct 23, 2003 · N867UP · Doug DC873FSDR 03FDEA01796Structure · corrodedCOMPLY WITH EA 7-5310-73206 FUSELAGE - MAIN FRAME - BS 950 BULKHEAD LOWER STRUCTURE CORROSION REPAIR, P/N 65-16338-7. COMPLIED WITH EA 7-5310-73206 FUSELAGE - MAIN FRAME - BS 950 BULKHEAD LOWER STRUCTURE CORROSION REPAIR P/N 65-16338-7, AT MAE.Oct 23, 2003 · N269FE · Boeing 727200SDR 03295670Bulkhead · damagedDURING INSPECTION DAMAGE TO THE PRESSURE BULKHEAD AT FS 621.Oct 22, 2003 · N670BR · Cndair CL6002B19SDR COMA0370041Bulkhead · crackedFS 1098.20 BULKHEAD RIGHT WEB BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B.Oct 22, 2003 · N354CA · Cndair CL6002C10SDR COMA0370042Bulkhead · crackedFS 1098.20 BULKHEAD RIGHT WEB BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPLACED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B.Oct 22, 2003 · N354CA · Cndair CL6002C10SDR DL757030946Bulkhead · corrodedTHE BREAK RING SECTION OF THE FS 1720 BULKHEAD WAS FOUND WITH AREAS OF CORROSION AND CRACK INDICATIONS NEAR STRINGER 18R. THE SECTION WAS CUT OUTBOARD OF THE DAMAGE AND THE SECTION FROM STRINGER 18R TO 12R WAS REMOVED. A NEW SECTION WAS FABRICATED AND SPLICEOct 21, 2003 · N659DL · Boeing 757232SDR EIA2003153Bulkhead · corrodedLT WING WW BAY 1241 CANTED PRESSURE BULKHEAD WEB CORRODED FROM LBL 50-97 LBL. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 479-53-176.Oct 19, 2003 · N479EV · Boeing 747132SDR UPS03241534Pressure Panel · crackedINSPECTION TYPE:C NLG W/W BS 290 LBL 0 SUSPECT CRACKS IN ROW OF RIVETS AT NLG CEILING. AREA CUTOUT IAW SRM 51-40-2 FIG 1, HFEC NDF. REPAIRED CUTOUT IAW SRM 51-10-2 FIG 1.Oct 19, 2003 · N927UP · Boeing 72731CSDR SWAA032298Bulkhead · crackedDURING SCHEDULED C1 CHECK, FOUND PRESS BULKHEAD CRACKED AT BS 1016, STR 6L AT THE Y-CHORD ATTACH AREA. REPAIRED BULKHEAD PER SRM.Oct 18, 2003 · N311SW · Boeing 7373H4SDR ASOA03517Stringer · crackedDURING A C-CHECK IN MCN, THE FS 718 BETWEEN STRINGERS 10-12 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 718 BETWEEN STRINGERS 10-12 ON THE RIGHT SIDE IAW ASA EO 600-53-0067A. (M)Oct 17, 2003 · N868AS · Cndair CL6002B19SDR USAA030214Stiffener · corrodedFOUND RADIAL STIFFENER CORRODED 2 INCH BY 1 INCH AREA, AFT PRESS BULKHEAD STATION 1016 AT BL 0. INSTALLED SPLICE SECTION AND REPAIR DOUBLERS PER EO 5302V112 AND BOEING DWG 65C28106 AND EA 77188. (M)Oct 17, 2003 · N592US · Boeing 737301
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