JASC 5312

Service difficulty reports · 20,047

Reports filed under 5312 · Fuselage Main, Bulkhead, newest first.

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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"

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SDR UPS97824832Bulkhead · crackedINSPECTION TYPE-D, FOUND AFT PRESSURE BULKHEAD CRACKED FS 1766, BL 24 TO 28 LT, WL +66. REMOVED DAMAGED AREA, FABRICATED DOUBLER, FILLER, FINGER DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-5 FIG 14A, 51-1-8, 51-1-21, 51-1-20D.Oct 11, 1997 · N805UP · Doug DC873FSDR 9720339946Bulkhead · corrodedDURING LINE CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD AT RADIAL NR 9 APPROXIMATELY 12 INCHES FROM OUTBOARD END. REPAIRED PER EA 99-152220.Oct 11, 1997 · N8926E · Doug DC931SDR USAA970291Bulkhead · corrosionCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT ALL SCREW HOLES .50 INCH BY .50 INCH AT STA 294 ENTIRE LENGTH UPPER CHORD SECTION 41, BULKHEAD. CORROSION TASK NR C53-107-01. INSTALLED SPLICE PER REPAIR DOCUMENT SRM 51-10-51. (X)Oct 10, 1997 · N385US · Boeing 7373B7SDR AALA972155Bulkhead Casting · corrodedTUL - CASTING CORRODED STRIGNER 30 AT 1183 BULKHEAD. REPLACED CORRODED CASTING STRINGER 30 AT STATION 1183. (M)Oct 10, 1997 · N873AA · Boeing 727223SDR 97FDEA00727Bulkhead Chord · corrodedNR 0415 011 - CORROSION (C53-132-02-1/2) ON BS 870 LOWER CHORD LBL 65 TO LBL 40.Oct 10, 1997 · N146FE · Boeing 72727CSDR 97FDEA00726Bulkhead Web · corrodedNR 0414 010 - CORROSION (C53-132-02-1/2) ON BS 870 BULKHEAD WEB, LBL 45 TO RBL 45.Oct 10, 1997 · N146FE · Boeing 72727CSDR ABXA9701672Blkhd Stiffener · crackedDURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD LT RADIAL STIFFENER, NR 2 CRACKED. REPAIRED RADIAL STIFFENER IAW ABX SUPP SRM DWG NR K05159.Oct 9, 1997 · N954AX · Doug DC941SDR ABXA9701671Blkhd Stiffener · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD RT RADIAL STIFFENER 3RD UP FROM FRP CRACKED. REPAIRED RADIAL STIFFENER IAW ABX SUPP SRM DWG NR K05159.Oct 9, 1997 · N954AX · Doug DC941SDR ABXA9701670Bulkhead Fitting · crackedDURING C-CHECK, FOUND FITTING CRACKED AT AFT PRESSURE BULKHEAD DOOR JAMB RT SIDE BETWEEN 3RD AND 4TH RADIAL STIFFENER, UP FROM FRP. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.Oct 9, 1997 · N954AX · Doug DC941SDR ABXA9701669Bulkhead Former · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD FORMER CRACKED (1ST UP FROM FRP LT SIDE). REMOVED AND REPLACED FORMER IAW DC9 SRM 51-30-2 AND 51-30-5.Oct 9, 1997 · N954AX · Doug DC941SDR SWAA970899Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT LT CHORD WL 193. REPAIRED PER BOEING SRM.Oct 8, 1997 · N52SW · Boeing 7372H4SDR DLL10972037Bulkhead Web · crackedTHE BULKHEAD STIFFENER PANEL AT FS 328, RBL 22 WAS FOUND CRACKED AT THE END OF THE FOURTH MILLED STIFFENER FROM THE BOTTOM. CRACK TRIMMED OUT WITH A 1 BY 0.5 TRIM OUT. REPAIRED PER ERA 330780-14.Oct 8, 1997 · N730DA · Lkheed 10113851SDR DLL10972028Bulkhead Web · corrodedFS 328 BULKHEAD WEB AT LBL 90 WAS FOUND TO HAVE CORROSION. CORROSION WAS CUTOUT. WEB WAS REPAIRED PER ERA 330749-14.Oct 8, 1997 · N730DA · Lkheed 10113851SDR DL72K972036Bulkhead Web · crackedSEVERAL CRACKS FOUND IN THE FS 178 BLKHD RBL 6, LBL 5 AND BL 0. REPAIRED PER ERA 330815-14.Oct 8, 1997 · N466DA · Boeing 727232SDR TWAA9809601Bulkhead Support · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND SUPPORT BRACKET ON AFT PRESSURE BULKHEAD AFT OF 24 RL CRACKED AT STA 579. REPLACED CRACKED ANGLE PER SRM 51-00. TOTAL TIME: 72,580 HOURS. TOTAL CYCLES: 77,573. (X)Oct 7, 1997 · N993Z · Doug DC931SDR 97FDEA00706Bulkhead Web · crackedEVIDENCE OF A CRACK AT FASTENER FWD SIDE OF BS 178 PRESSURE BULKHEAD WL 236, RBL 10. *S/D* REPAIRED DAMAGED PRESSURE BULKHEAD BS 178, WL 236, RBL 10 PER FED-EX SRM 53-10-9.Oct 6, 1997 · N134FE · Boeing 72725CSDR IXXA9800009Bulkhead Doubler · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE PRESSURE BULKHEAD FINGER DOUBLER BETWEEN FUSELAGE STATION 188 AN 208. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER, ONE EXTERNAL REPAIR DOUBLER, AOct 3, 1997 · N728PL · Doug DC862SDR DL72W971990Bulkhead · crackedA 2 INCH CRACK WAS FOUND IN THE 1183 BULKHEAD AT RBL 8.0 AND WL 180. THIS ER/A WILL GIVE INSTRUCTIONS TO ACCOMPLISH A REPAIR UNTIL THE FULL MODIFICATION REQUIRED BY AIRWORTHINESS DIRECTIVE 90-06-09 IS ACCOMPLISHED. THE REPAIR WILL BE INSTALLED ON THE FWD SIDOct 3, 1997 · N2816W · Boeing 727247SDR CA971010003Bulkhead · misinstalled(CAN) ON INSPECTION, FOUND THAT THE FIRST 12 INCHES AFT OF THE REAR PRESSURE BULKHEAD (STN 345.0) TO THE RIGHT OF CENTERLINE AT THE UPPER CENTER STRINGER, RIVETS WERE INSTALLED WITH INSUFFICIENT EDGE DISTANCE. AIRCRAFT TT: 2,277 HOURS.Oct 3, 1997 · Cessna 550SDR 97FDEA00702Bulkhead Web · corrodedNR 0414 002 CORROSION (C53-132-02 1/2) ON BS 870 BULKHEAD WEB LBL 45 TO RBL 45.Oct 3, 1997 · N146FE · Boeing 72727CSDR AU971603Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THE FOLLOWING LOCATIONS:-1. THREE CRACKS IN THE BULKHEAD WEB BETWEEN LBL 5.7 AND RBL 5.7 LOCATED UNDER THE RADAR SCANNER MOUNTING BRACKETS - CRACK LENGTHS 24MM (0.944IN) - 14MM (0.551IN) - 13MM (0.511IN) 2. CRACK IN Oct 1, 1997 · Boeing 737377SDR EIAA97222Bulkhead · corrodedDURING C-CHECK INSPECTION, DISCOVERED CORROSION, GOUGES, AND MISDRILLED HOLES ON THE FUSELAGE AFT REAR SPAR BULKHEAD DOUBLER AND CAP AT STA 942 BETWEEN LONGERONS14L TO 16L AND 12R TO 16R. REPAIRED BY TRIMMING AWAY DAMAGE, INSTALLING REPAIR DOUBLERS, ANGLES, ASep 29, 1997 · N915F · Doug DC915FSDR USAA970286Bulkhead Skin · crackINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK BS 178 BULKHEAD SKIN RIGHT UPPER ANTENNA (RADAR) MOUNT. INSTALLED REPAIR, REPAIRED PER SRM 53-10-11, FIGURE 1. (X)Sep 26, 1997 · N232US · Boeing 737201SDR UPS97224693Blkhd Stiffener · damagedINSPECTION TYPE-C, HYD LINE RUBBING STIFFENER. STIFFNER FOUND TO BE DAMAGED NECESSITATING A REPAIR. REPAIR CARRIED OUT IAW SRS EO 97-24-008 UPS ENG FILE NUMBER 727-53-1 967.Sep 26, 1997 · N938UP · Boeing 727173CSDR 9718419857Bulkhead Skin · crackedDURING ROUTINE MAINTENANCE, FOUND A CRACK IN THE AFT PRESSURE BULKHEAD SKIN AT THE LOWER LEFT CORNER AT THE DOOR JAMB. REPAIRED PER EA 98-152271.Sep 25, 1997 · N766NC · Doug DC951SDR 9718359962Bulkhead · crackedDURING M CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 110, RIGHT INBOARD VERTICAL BEAM ATTACH POINT. REPAIRED PER EA 99-151652.Sep 24, 1997 · N914RW · Doug DC931SDR 9718449102Bulkhead · crackedDURING L CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT THE RIGHT OUTBOARD AND INBOARD FITTINGS FS 110. REPAIRED PER EA 91-151699.Sep 23, 1997 · N92S · Doug DC915SDR SWAA970868Bulkhead · crackedDURING SCHEDULED C4 CHECK, FOUND AFT PRESSURE BULKHEAD AT BS 1016 OIL CANNING. REPAIRED PER BOEING SRM.Sep 22, 1997 · N51SW · Boeing 7372H4SDR DLL10971923Web · corrosionTHE LBL 22 WEB JUST AFT OF THE FWD NLG DOOR HINGE CUTOUT WAS FOUND CORRODED. A SECTION OF THE WEB MEASURING 8 BY 12 WAS CUT OUT. THE WEB IS MADE FROM TWO BONDED SHEETS OF 7075-T6 CLAD MATERIAL, ONE MEASURING .071 THK AND THE OTHER .025 THK. INSTALLED DOUBLESep 22, 1997 · N730DA · Lkheed 10113851SDR CKSA97539Bulkhead Frame · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD FWD SIDE FROM L24RH TO L12L HAS AREAS OF SPOT CORROSION LOWER SIDE. REMOVED CORRODED FRAME SECTION IAW L1011 SRM 51-21-01. REPAIRED IAW LOCKHEED L1011 SRM 53-11-0 FIG 848. FRAME REPAIR AT S25 ANSep 21, 1997 · N102CK · Lkheed 1011385115SDR ABXA9701692Bulkhead · crackedFUSELAGE STA 680 LBL 5 TO LBL 22 JUST BELOW THE CENTER WING LOWER FORWARD SPAR, THE PRESSURE BULKHEAD IS CRACKED IN TWO PLACES. REMOVED CRACKED SECTION OF DOME, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 53-25, FIGURE 13.Sep 21, 1997 · N822AX · Doug DC863SDR 9718439102Bulkhead · crackedDURING L CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL LIGHT OUTBOARD FITTING FS 110. REPAIRED PER EA 91-151699.Sep 21, 1997 · N92S · Doug DC915SDR W8PA971487Blkhd Support · corrodedPAE - CORROOSION ON FLORR TO BULKHEAD SUPPORT ANGLE ALONG LOWER FLANGE AT BS 947.5, RBL 21, WL 165. REMOVED ANGLE, FABRICATED NEW AND INSTALLED.Sep 19, 1997 · N953WP · Boeing 7373B7SDR ABXA9701512Blkhd Fitting · crackedDURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB FITTING AT THE LOWER RT STOP PAD ATTACH FASTENER HOLE CRACKED. REPLACED THE FITTING IAW DC9 SRM 51-30-5 AND 51-30-5.Sep 19, 1997 · N967AX · Doug DC941SDR CA971003010Doubler · broken(CAN) DURING ANNUAL INSPECTION, A CRACK AT A RIVET HOLE WAS FOUND IN THE ABOVE DOUBLER. AFTER REMOVING THE DOUBLER IT WAS FOUND TO BE CRACKED INTO TWO PIECES. THE BULKHEAD ASSEMBLY WAS FOUND TO HAVE A .50 INCH CRACK RUNNING FROM EACH SIDE OF THE RIVET HOLE. Sep 18, 1997 · Cessna 210JSDR AU971539Web · cracked(AUS) FORWARD PRESSURE BULKHEAD WEB CRACKED IN SEVEN PLACES:- A. AREA UNDER THE RADAR SCANNING MOUNTING BRACKETS CONTAINED FOUR CRACKS BETWEEN LBL 5.5 AND RBL 5.7 - CRACK LENGTHS 27MM (1.06IN), 13MM (0.5IN) AND TWO CRACKS OF 16MM (0.630IN)B. TWO CRACKS EITHERSep 18, 1997 · Boeing 737377SDR DHL9774211CBulkhead · corrodedAT C-CHECK, FWD CARGO COMPT BS 740 BULKHEAD BEAM CORRODED AT LOWER CHORD BETWEEN STGRS 27 AND 28 RT. REMOVED CORROSION, WITHIN LIMITS, EXCEPT O/B AREA OF CHORD FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW CHORD AT FWD CARGO COMPT PER SRM 51-30Sep 17, 1997 · N742DH · Boeing 727225SDR CKSA97530Bulkhead · corrodedDURING ROUTINE B-CHECK INSPECTION, FOUND EVIDENCE OF CORROSION ON AFT SIDE OF STA 870 BULKHEAD APPROX RBL50. REMOVED CORROSION IAW B727 SRM 51-10-6. FOUND OUT OF LIMITS IAW B727 SRM 51-10-1. INSTALLED DOUBLER REPAIR IAW SKETCH AIA/E/2635 DTD 9/9/97. NON-ROSep 17, 1997 · N727CK · Boeing 72722CSDR 97FDEA00675Bulkhead · crackedCRACK IN 1183 BULKHEAD LBL 10, WL 172. CUT OUT CRACK FINAL APPROX 1 BY 1.5 AND INSTALLED A .063202473 DOUBLER PER EA 7-5310-29205. DATED 9/3/97.Sep 17, 1997 · N496FE · Boeing 727227SDR TWAA9711311Bulkhead Skin · crackedSTL - REPLACED PORTION OF PRESSURE BULKHEAD AT NR 3 HOLE DUE TO CRACK. (M)Sep 16, 1997 · N996Z · Doug DC932SDR TWAA9711310Bulkhead Skin · crackedSTL - REPLACED A PORTION OF PRESSURE BULKHEAD SKIN AT NR 2 HOLE DUE TO CRACK. (M)Sep 16, 1997 · N996Z · Doug DC932SDR TWAA9711309Bulkhead Skin · corrodedSTL - REPLACED LOWER AFT BULKHEAD SKIN AT LONGERON 25 RIGHT DUE TO CORROSION. (M)Sep 16, 1997 · N996Z · Doug DC932SDR TWAA9711303Bulkhead Skin · crackedSTL - REPLACED SECTION OF AFT PRESSURE BULKHEAD SKIN AT UPPER RIGHT CORNER OF DOOR OPENING DUE TO CRACK. (X)Sep 16, 1997 · N996Z · Doug DC932SDR ASAA9740059Bulkhead Seal · tornSEA - DURING STRUCTURAL INSPECTION THE PRESSURE BULKHEAD AT STA 1016, LOWER WEATHER SEAL WAS FOUND TORN. REPAIRED PER EA 5320-01318. TT: 16,604 HOURS. TC: 8,816. (X)Sep 15, 1997 · N786AS · Boeing 7374S3SDR ARWA970918Bulkhead · corrodedDURING CPCP INITIAL INSPECTION, FOUND 'C' BELLY, AFT BULKHEAD WALL FRAME REPAIR BETWEEN LONGERON 35L AND LONGERON 35R IS CORRODED (REPAIR AT FRAME) FS 1320. REMOVED CORROSION ON 'C' BELLY AFT BULKHEAD WALL ON STR 35L TO 35R, FABRICATED DOUBLER AND SHIM FROM SSep 15, 1997 · N345JW · Doug DC863SDR AWXA9700576Blkhd Stiffener · damagedDURING SCHEDULED C-11 INSPECTION, FOUND NR 4 RT ZEE STIFFENER DAMAGED ON BS 1016 AFT PRESSURE BULKHEAD FWD FACE RBL 40, WL 274. REPLACED ZEE STIFFENER PER SRM 51-40-02 AND 51-10-02.Sep 14, 1997 · N314AW · Boeing 7373S3SDR DL72S971880Blkhd Stiffener · crackedTWO CRACKS WERE FOUND IN THE VERTICAL STIFFENER AT RBL 36.83 ON THE FORWARD SIDE OF THE BS 1183 BULKHEAD. THE CRACKS ARE APPROX 1.75 AND 1 LONG AND ARE LOCATED AT APPROX WL 237 IN THE IB AND OB RADIUS, RESPECTIVELY, OF THE AFT CHORD. THIS AREA IS ADDRESSED ISep 12, 1997 · N528DA · Boeing 727232SDR CALA9701465Bulkhead Web · cracked.5 INCH CRACK AT APU OAD CONTROL VALVE CUT OUT IN RIGHT WHEEL WELL AT FWD BULKHEAD. FABRICATED AND INSTALLED DOUBLER REPAIR PER EC/RA 5310-01544.Sep 12, 1997 · N32725 · Boeing 727224SDR 9717449962Bulkhead Fitting · crackedDURING M-CHECK, FOUND CRACK IN KEEL BEAM TO BULKHEAD FITTING FS 756. REPLACED FITTING PER SRM 51-01.Sep 12, 1997 · N914RW · Doug DC931SDR 97ZZZX4261Bonding · crackedDURING A PRE-PURCHASE INSPECTION, A CRACK WAS NOTICED IN THE BONDING PASTE (THICKENED RESIN) ATTACHING THE AFT BULKHEAD TO THE TAIL CONE AT THE LOWER LEFT CORNER. THE CRACK IS 2.25 INCHES LONG. THE MANUFACTURER STATED THIS TYPE OF CRACK OCCURS FROM STRIKING Sep 11, 1997 · N332CH · Diamon DA20A1
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