JASC 5312

Service difficulty reports · 20,045

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 DLM88070459Tee Fitting · damagedTOOLING MARKS ON LOWER T-CAP CHORD OF AFT PRESSURE BULKHEAD AT STA 1338 BETWEEN LONGERONS 28L-28R. SKIN P/N 5911429-151 TRIMMED FOR ACCESS. CHORD P/N SR09530001-33 SPLICED PER EA 09-086680-12 REV E, OPN 0603. SKIN REPAIRED PER SRM 53-03 FIG 37.Apr 16, 2007 · N945DL · Doug MD88SDR COMA0760331Floor Skin · crackedDURING A HMV7 INSPECTION, THE PRESSURE FLOOR SKIN AT FS 460 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CRACKED IN 3 PLACES. PERFORMED REPAIR PER REO 601R-53-41-10.Apr 16, 2007 · N931CA · Cndair CL6002B19SDR C2XA07SH021Firewall · chafedSHV - DURING C-CHECK MAINTENANCE APU FIREWALL LOWER SECTION HAS RIVET INDENTATION. MAINTENANCE REPAIRED APU FIREWALL AT FRAME 81 LOWER SECTION IAW EC5310-01359. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.Apr 15, 2007 · N13990 · Emb EMB145LRSDR DHL2007782502Pressure Panel · crackedCABIN PRESSURE WEB AT BS 740 TO 760, LT, IS CRACKED AT AFT HOLE. FABRICATED NEW PRESSURE WEB FROM 7075-T6, .040" BY 13.5" BY 9.5", PO NR 9004539, PER B727 SRM 53-10-3 FIG 7 AND 51-20-1. TREATED, PRIMED, AND INSTALLED PRESS WEB PER B727 SRM 51-10-2 AND 51-30-Apr 14, 2007 · N782DH · Boeing 727227SDR DHL2007782501Pressure Panel · crackedCABIN PRESSURE WEB AT BS 740 TO 760, RT, IS CRACKED AT AFT HOLE. FABRICATED NEW PRESSURE WEB FROM 7075-T6, .040" BY 13.5" BY 9.5", PO NR 9003110, PER B727 SRM 53-10-2 FIG 3. TREATED, PRIMED, AND INSTALLED PRESS WEB PER B727 SRM 51-10-2 AND 51-30-2.Apr 14, 2007 · N782DH · Boeing 727227SDR 07FDEA01495Bulkhead · damagedSCRATCH IN PRESSURE BULKHEAD AT C54, TR 4 LT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-101318 AND RAS/045121/010/2006 ISSUE "A".Apr 13, 2007 · N810FD · Airbus A310324SDR DJFA2007048BDoubler · crackedDURING A SHCEDULED INSPECTION, MAINTENANCE DISCOVERED MULTIPLE CRACKS IN THE NOSE WHEEL WELL AREA. THE LT TOP DOUBLER WAS FOUND CRACKED. THE CRACK ON THE DOUBLER WAS .8 INCHES LONG. MX REMOVED AND REPLACED THE DOUBLER IAW DRAWING NR 671800, REPLACED 67177Apr 12, 2007 · N704LX · Cessna 750SDR ABXA070124Bulkhead · crackedCRACK OF UNKNOWN LENGTH AND DIRECTION IN DOUBLER UPPER LEFT AFT PRESSURE BULKHEAD DOOR CUTOUT CORNER. STOP DRILLED CRACK IN -13 DOUBLER, INSTALLED REPAIR IAW DC9 SRM J060088-543 AND DC9 SB 53-137.Apr 12, 2007 · N785TW · Doug DC915FSDR CA070502005Bulkhead · cracked(CAN) PARTS WERE CRACKED AT ATTACH POINTS OF WHEEL WELL COVER SKIN 2412011-1 AND BULKHEADS STATION 108 AND 124 AND CRACK ON WHEEL WELL COVER AT RT FRONT CORNER WHERE IT ATTACHES TO BULKHEAD STATION 108. TIEDOWN RINGS ALSO ATTACH IN THIS AREA. (TC NR 20070502Apr 10, 2007 · Cessna 172RGSDR ABXA070125Bulkhead · crackedAFT PRESSURE BULKHEAD SKIN CRACKED AT UPPER LEFT DOOR CUTOUT. REMOVED AND REPLACED SKIN IAW DC9 SRM 51-30-2 AND 51-30-5.Apr 10, 2007 · N785TW · Doug DC915FSDR ABXA070127Pressure Panel · corrodedPRESSURE PANEL AT FS 1350, RIGHT BUTT LINE 40 WAS CORRODED. REMOVED, REPLACED AND REINSTALLED PRESSURE PANEL AT FS 1350, RIGHT BUTT LINE 40.Apr 10, 2007 · N794AX · Boeing 767281SDR MASA200700232Bulkhead · crackedFWD PRESSURE BULKHEAD CRACKED. REPAIRED FWD PRESSURE BULKHEAD.Apr 8, 2007 · N27173 · Cndair CL6002B19SDR COMA0760305Bulkhead · crackedCRACK PROPAGATING FROM PARKING BRAKE CABLE HOLE IN FWD HYD COMPARTMENT FS 202.75, BL 23.71. COMPLIED WITH REO-53-11-563.Apr 8, 2007 · N915CA · Cndair CL6002B19SDR TRAX200700493Floor Skin · corrodedCORROSION ON RIGHT PRESSURE FLOOR FROM FS 460 TO FS 513. [SUP 4-23-07] COMPLIED WITH ALL FAA APPROVED DATA.Apr 8, 2007 · N856AS · Cndair CL6002B19SDR TRAX200700492Floor Skin · corrodedCORROSION ON LEFT SIDE PRESSURE FLOOR SKIN FROM FS 460 TO FS 513. [SUP 4-23-07] REPAIRED IAW ALL FAA APPROVED DATA.Apr 8, 2007 · N856AS · Cndair CL6002B19SDR TRAX200700484Bulkhead · crackedSTA 280 BULKHEAD WEB CRACKED AT RBL 9. BEGAN REMOVING FASTENERS THROUGH LT AND RT STA 280 WEB AND RELATED STRUCTURE AS PER CRJ 200 SRM 51-42-00 AND REO 601R-53-11-926. EWB 702040900. CONTINUED REMOVAL OF ASSOCIATED PARTS. MADE CUT AND REMOVED CRACKED / CApr 7, 2007 · N856AS · Cndair CL6002B19SDR TRAX200700483Bulkhead · crackedSTA 280 BULKHEAD WEB CRACKED AT LBL 9.Apr 7, 2007 · N856AS · Cndair CL6002B19SDR ABXA070123Bulkhead · crackedAFT PRESSURE BULKHEAD DOOR CUTOUT UPPER RIGHT CORNER DOUBLER HAD APPROXIMATELY 1.5" RADIUS CRACK. REPAIRED UPPER RIGHT CORNER OF AFT PRESSURE BULKHEAD IAW DC9 SRM J060088-543 REPAIR AND DC9 SB 53-137.Apr 6, 2007 · N785TW · Doug DC915FSDR MASA200700231Bulkhead · crackedFS 621.00 PRESSURE BULKHEAD WEB HAS A .50 CRACK A LBL 18.0 WL 113. REPAIRED PRESSURE BULKHEAD WEB.Apr 4, 2007 · N7264V · Cndair CL6002B19SDR 07FDEA01342Bulkhead · crackedLT AIR COND COMPT CRACK 1" LONG ON VERTICAL BULKHEAD. REPAIRED WEB IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1.Apr 4, 2007 · N387FE · Doug DC1010SDR 07FDEA01341Bulkhead · crackedRT AIR COND COMPT CRACK 1" LONG ON VERTICAL BULKHEAD. REPAIRED CRACK IAW SRM 53-30-00 FIG 6 SHT 8 VOL 1.Apr 4, 2007 · N387FE · Doug DC1010SDR 07FDEA01335Bulkhead · crackedRT AIR COND COMPT CRACK 1" LONG ON VERTICAL BULKHEAD. REPAIRED WEB IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1.Apr 4, 2007 · N387FE · Doug DC1010SDR 07FDEA01334Bulkhead · crackedRT MLG W/W FOUND 1 CRACK 2" LONG ON VERTICAL BLKHD. REPAIRED BLKHD IAW SRM 53-00-01 FIGURE 4 SHT 2 VOL.1.Apr 4, 2007 · N389FE · Doug DC1010SDR 07FDEA01325Bulkhead · brokenFOUND A STRUT OF BULKHEAD BROKEN. REPAIRED STRUT IAW SRM 53-00-01 FIGURE 2 SHT 2 VOL 1.Apr 4, 2007 · N389FE · Doug DC1010SDR KCSA071114Bulkhead · corrodedBS 2360 BULKHEAD FORWARD LOWER CHORD CORRODED AT STRINGER END FITTING HOLES FROM STR 26L TO STR 26R.Apr 4, 2007 · N701CK · Boeing 747236BSDR 07FDEA01294Bulkhead · crackedRT AIR COND. COMP. CRACK 2" LONG ON EXTERNAL REPAIR ON VERTICAL BLKHD. REPAIRED IAW FEDEX E.A 8-5320-94639 PART 2.Apr 3, 2007 · N389FE · Doug DC1010SDR 07FDEA01292Bulkhead · crackedLT MLG W/W FOUND 1 CRACK 2" LONG ON VERTICAL BLKHD. REPAIRED IAW SRM 53-00-01 FIGURE 4 SHT 2 VOL 1.Apr 3, 2007 · N389FE · Doug DC1010SDR 07FDEA01271Pressure Panel · corrodedRT MLG W/W FOUND CORROSION ON PRESSURE PANEL STA 1381 UNDER SLANT PANEL. REPAIRED IAW FEDEX EA 8-5730-103734.Apr 3, 2007 · N554FE · Doug DC1010SDR SWAA071718Bulkhead · crackedDURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 3R. REPAIRED WEB PER SRM.Apr 3, 2007 · N326SW · Boeing 7373H4SDR 07FDEA01302Bulkhead · corrodedFOUND CORROSION AT FRAME 39 BULKHEAD LOWER T-PROFILE AND ON PARTS OF BULKHEAD PANEL IN AREA OF THE T-PROFILE. REPAIRS OF ALL AFFECTED AREAS MENTIONED AND PERFORMED IAW EA 6-5314-99221AND RAS 014851/020/2001 ISSUE "A".Apr 3, 2007 · N814FD · Airbus A310324SDR 2007FA0000334Bulkhead · crackedSMALL CRACK AT RUDDER CABLE CUTOUT IB, APPROX .2500 INCH, NO CAUSE.Apr 2, 2007 · N42053 · Cessna 182LSDR F3LA200700053Beam · bentDURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FWD BULKHEAD BEAM RT OF CENTER BENT. REPLACED BULKHEAD BEAM IAW A319 SRM 51-42-11, PARA. 5, PG 6-7 AND PARA 6, PG 22-23, AND SRM 51-44-21.Mar 31, 2007 · N906FR · Airbus A319111SDR SWAA071643Bulkhead · crackedDURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, LBL 23, WL 193. REPAIRED WEB PER BOEING SB AND SRM.Mar 31, 2007 · N685SW · Boeing 7373Q8SDR 2007UALA00957Bulkhead · corrodedAFT EQUIPMENT BAY, AFT SIDE OF FRAME AND ON PRESSURE BULKHEAD STA 1016 TO 1021 RBL 0 TO RBL 8 WL 90 TO 92 STR 24R TO 25R SEALANT LIFTED WITH LARGE AMOUNT OF POWDER. ALSO FRAME AFT SIDE WEB HAS CORROSION, SAME LOCATION. MAJOR REPAIR ACCOMPLISHED: REMOVED CORMar 30, 2007 · N364UA · Boeing 737322SDR DLM88070452Tee Fitting · wornAFT PRESSURE BULKHEAD TEE LOWER PORTION REPAIR AT STA 1338, LONGERON 28L-28R - WEAR. A PORTION OF THE LOWER PART OF BULKHEAD TEE WAS SECTIONED AND NEW SECTION INSTALLED PER EA 09-086680-12 REV E.Mar 29, 2007 · N943DL · Doug MD88SDR UPS07849619Bulkhead · corrodedINSPECTION TYPE:C2 A/C COMPT FWD BULKHEAD CORRODED AT STA 8 BL 0. REMOVED CORRODED WEB AND CHANNEL AT STA 8 BL 0 IAW SRM 51-1-20D, FABRICATED AND INSTALLED REPAIR WEB, AND CHANNEL AT STA 8 BL 0 IAW SRM 51-09-00 FIG 068A, AND EO DC8-5350-7876.Mar 29, 2007 · N805UP · Doug DC873FSDR TRAX200700440Angle · crackedRIGHT OBLIQUE ANGLE AFT OF 621 BULKHEAD IS CRACKED (AS MARKED). REMOVED RT OBLIQUE ANGLE AFT OF621 BULKHEAD. OK TO TREAT AND PRIME RT OBLIQUE ANGLE AND PAINT. OK TO INSTALL.Mar 29, 2007 · N830AS · Cndair CL6002B19SDR KCSA071099Bulkhead · dentedAFT PRESSURE BULKHEAD HAS 2 DENTS STA 2382, WL 190, RBL 40.Mar 29, 2007 · N701CK · Boeing 747236BSDR COMA0760291Bulkhead · crackedDURING MID CHECK INSPECTION FOUND FS 202.75 BULKHEAD CRACKED, BL 23.71 AT CUTOUT FOR HYDRAULIC LINE. REMOVED DAMAGE AND INSTALLED DOUBLER PER BOMBARDIER REO 601R-53-11-563.Mar 28, 2007 · N403CA · Cndair CL6002B19SDR KCSA071092Bulkhead · dentedAFT PRESSURE BULKHEAD HAS (2) SMALL DENTS LBL 45, WL 210, STA 2400.Mar 28, 2007 · N701CK · Boeing 747236BSDR 2007UALA00901Pressure Panel · damagedAFT PRESSURE DECK BS 1681.80 AT RBL 40 IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED DOUBLER/FILLER REPAIR.Mar 26, 2007 · N506UA · Boeing 757222SDR 07FDEA01121Skin · crackedINSPECT/REPAIR/MOD LT AND RT TEE CAPS, CARD E8-5310-7-3327 PT.4. C/W FUSELAGE-AD96-18-11-LT AND RT 1156 BULKHEAD TEE AND SKIN CRACK-REPAIR. MAJOR REPAIR.Mar 23, 2007 · N40061 · Doug DC1010SDR 07FDEA01120Bulkhead · crackedINSPECT/REPAIR/MOD LT AND RT TEE CAPS. CARD E8-5310-7-3327 PT.3. C/W E8--5310-105179- FUSELAGE-AD 96-18-11-LT AND RT 1156 BULKHEAD TEE AND SKIN CRACK-REPAIR. MAJOR REPAIR.Mar 23, 2007 · N40061 · Doug DC1010SDR 07FDEA01110Bulkhead · gougedSOME GOUGES FOUND AT BULKHEAD 54, APPROX Y-953 AND Z-957, REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-106419 AND RAS 049380/2007 ISS. AMar 23, 2007 · N816FD · Airbus A310304SDR SWAA071534Stiffener · crackedDURING SCHEDULED 18Y CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT BS 1016, STR 3R. REPAIRED STIFFENER PER SRM.Mar 22, 2007 · N350SW · Boeing 7373H4SDR SWAA071511Bulkhead · crackedDURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 17R. REPAIRED WEB PER SRM.Mar 22, 2007 · N308SA · Boeing 7373Y0SDR SWAA071529Bulkhead · crackedDURING SCHEDULED 18Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 10 O`CLOCK POSITION. REPAIRED WEB PER ER.Mar 22, 2007 · N350SW · Boeing 7373H4SDR SWAA071544Stiffener · crackedDURING SCHEDULED 18Y CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT BS 1016, STR 9L. REPAIRED STIFFENER PER SRM.Mar 22, 2007 · N349SW · Boeing 7373H4SDR SWAA071535Stiffener · crackedDURING SCHEDULED 18Y CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT BS 1016, STR 4R. REPAIRED STIFFENER PER SRM.Mar 22, 2007 · N350SW · Boeing 7373H4SDR 2007UALA00844Bulkhead · buckledAFT PRESSURE BULKHEAD STA 1720 HAS A BUCKLE IN ITS WEB, ABOUT ONE QUARTER INCH DEFLECTION BY 18 INCHES LONG. FIVE INCHES FROM THE BOTTOM, BETWEEN THE TWO VERTICAL BEAMS AT LBL 9.20 AND RBL 9.20 DAMAGE TO FOLLOWING AREAS: GOUGES STA 1720 STR 29L TO OUTBOARD SMar 21, 2007 · N594UA · Boeing 757222
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