JASC 5312

Service difficulty reports · 20,045

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 TSAA0653030Bulkhead · crackedTHREE CRACKS AROUND BS 1016 AFT PRESSURE BULKHEAD GORE WEBS NEAR DOME CAP. WEB SPLICE AND REPAIR DOUBLERS COMPLETED IAW ALOHA'S ECO 3567. HFEC COMPLIED IAW NDT MANUAL PART 5, 51-00-00 FIG 16. FAA FORM 8100-9 RECEIVED.Apr 6, 2006 · N807AL · Boeing 7372T4SDR 2006UALA00654Bulkhead · damagedFOUND LT AC BAY OB SIDE OF DOOR CUTOUT 22" FROM AFT END. BULKHEAD WEB DAMAGED FROM CONTACT WITH DOOR LATCH. DAMAGE AREA TRIMMED OUT REF MM51-20-01 & EA I060153.Apr 6, 2006 · N334UA · Boeing 737322SDR QXEA200601159Bulkhead · chafedPDX - FRONT SIDE OF FWD PRESSURE BULKHEAD AT 3 1/2 INCHES RIGHT OF CENTER CUTOUT (VIEWED LOOKING AFT) SKIN IS CHAFED AND STEP WORN. MAINTENANCE REPAIRED IAW Q400 SRM 51-14-08, NDTM PART 6, 51-00-02, HORIZON EA 6-53-669 AND RD 8/4-53-1471.Apr 4, 2006 · N405QX · Bombdr DHC8402SDR 06FDEA1304Bulkhead · crackedDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND CENTER WING, FRONT SPAR, PRESSURE BULKHEAD, STA 1159, X = -10, Z = -75: CRACK 7 INCH LONG. PERFORMED STRIP PAINT AREA, PERFORMED STOP DRILL 5/16'' DIA HOLE AT BOTH ENDS OF CRACK, NDI CHECK IAW CMM 20-20-03,Apr 4, 2006 · N568FE · Doug DC1010SDR TRAX200600030Bulkhead · crackedSUSPECT CRACK AT FWD PRESSURE BULKHEAD BRAKE CABLE CUTOUT. REPAIRED IAW REO-601R-53-11-563 (CLOSED).Apr 3, 2006 · N859AS · Cndair CL6002B19SDR P5CA0601466Bulkhead · corrodedTHE 1241 BULKHEAD CORRODED AT LBL 10 TO RBL 98 (BELOW UPPER CHORD). REPAIRED PER BOEING 8100-9. REMOVED CORROSION AT BS 1241 LBL 10 TO RBL 98. WORK ACCOMPLISHED ON ECRA 921FT-57-474-010 REV NEW.Mar 31, 2006 · N921FT · Boeing 747283BSDR UIEA200600063Bulkhead · crackedFOUND 01 OFF CRACK AT STA 400 WHEEL WELL BULKHEAD PAN ASSY LOWER RT CORNER CUT OUT RBL.15.0. CARRIED OUT EDDY CURRENT INSP, AS PER MTM PT-6 51-00-00 FIG 16 AND 23, NIL CRACK INDICATION AT THIS LINE AND FASTENER HOLES. PAN ASSY REMOVED, FOUND CRACK ON BULKHEAMar 30, 2006 · N540MC · Boeing 747243BSDR SWAA061128Pressure Panel · crackedDURING SCHEDULED SERVICE CHECK, FOUND NLG W/W CEILING PANEL CUTOUT CRACKED AT BS 251.625, LBL 7.75 & RBL 7.75. REPAIRED PANELS PER SWA EA.Mar 30, 2006 · N344SW · Boeing 7373H4SDR SWAA061121Pressure Panel · crackedDURING SCHEDULED C2 CHECK, FOUND NLG W/W CEILING PANEL CUTOUT CRACKED AT BS 251.625, LBL 7.75 & RBL 7.75. REPAIRED PANELS PER SWA EA.Mar 29, 2006 · N504SW · Boeing 7375H4SDR EIAA2006041Pressure Panel · crackedDURING B CHECK; FOUND 2 CRACKS IN NOSE WHEEL WELL TOP PANEL WEB. CRACKS REPAIRED PER SRM 53-10-04, FIG 119.Mar 27, 2006 · N471EV · Boeing 747273CSDR CALA0600111Frame · corrodedINSPECTION FOUND CORROSION ON LOWER FRAME OF STA 227.8 BULKHEAD, LBL 6 TO RBL 6. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR IAW ECRA 5311-01252 WITHIN 6,000 FLIGHT CYCLES OR 24 MONTHS WHICH EVER COMES FIRST.Mar 27, 2006 · N14346 · Boeing 7373T0SDR SWAA061080Panel · crackedDURING SCHEDULED SERVICE CHECK, FOUND NLG W/W CEILING PANEL CRACKED AFT OF LT BRAKE MOUNT, BS 251.62, LBL 7.75. MX FERRY TO DAL FOR REPAIRS. REPAIRED PANEL PER SWA EA.Mar 23, 2006 · N347SW · Boeing 7373H4SDR 2006FA0000353Bulkhead · crackedBULKHEAD, PN 071220510, CRACKED AT TIE DOWN HOLE. BULKHEAD, PN 0712206, CRACKED AT BOLTHOLES ATTACHMENT TO ELEVATOR BELLCRANK SUPPORT MOUNT. (K)Mar 22, 2006 · N2233G · Cessna 182ASDR 2006FA0000352Bulkhead · crackedBULKHEAD, PN 071220510, CRACKED AT TIE DOWN HOLE. BULKHEAD, PN 0712206 CRACKED AT BOLT HOLES ATTACHMENT TO ELEVATOR BELLCRANK SUPPORT MOUNT. (K)Mar 22, 2006 · N2233G · Cessna 182ASDR ABXA060156Bulkhead · crackedRADIAL CRACK IN AFT PRESSURE BULKHEAD UPPER LEFT CORNER LOCATED 11.25" LEFT OF CENTER. STOP DRILL 250 IAW DC9 SRM 51-10-4.Mar 22, 2006 · N990AX · Doug DC941SDR SIMA200608704Web · corrodedCOCKPIT RT BULKHEAD LWR WEB CORRODED AT STA 20. REMOVED DAMAGE. PREPARED LWR WEB, FABRICATED BUTTSTRAP. REPAIR DONE IAW REO. (K)Mar 21, 2006 · N505AE · Cndair CL6002C10SDR SIMA200608702Web · corrodedCOCKPIT LT BULKHEAD LWR WEB CORRODED. REMOVED CORROSION, PREPARED LWR WEB AND FABRICATED A BUTTSTRAP. REPAIR DONE IAW REO. (K)Mar 21, 2006 · N505AE · Cndair CL6002C10SDR SWAA060862Pressure Panel · crackedDURING SCHEDULED C4 CHECK, FOUND NLG W/W CEILING WEB CRACKED AT BS 294.5, RBL 8. REPAIRED WEB PER SWA EA.Mar 15, 2006 · N649SW · Boeing 7373H4SDR SWAA060861Stiffener · corrodedDURING SCHEDULED 1/4D CHECK, FOUND BS 1016 PRESS BULKHEAD RT SIDE RADIAL STIFFENER CORRODED. REPAIRED STIFFENER PER BAC DRAWING.Mar 15, 2006 · N664WN · Boeing 7373Y0SDR UIEA200600041Pressure Panel · crackedLT WLG WELL - FOUND A SMALL CRACK IN THE CANTED PRESSURE PANEL AT BS 1241. REPAIRED IAW SRM 53-10-07 FIG 6.Mar 13, 2006 · N512MC · Boeing 747230BSDR UPS06446639Bulkhead · corrodedL/G RT WLG W/W BS 1241 RBL 7-8 I/B OF AILERON PROGRAMMER LWR WEB FOUND CORRODED. CORROSION BLEND OUT 0.054" BY 1.5" BY 6" EXCEED SRM 57-10-01 FIG 1 LIMITS, RT WLG W/W BS 1241 RBL 7-8 AREA BHD WEB REPAIRED AS PER HX RS NR R57-12-35467 AND UPS EO# B747-5710-240Mar 10, 2006 · N681UP · Boeing 747121SDR SWAA060789Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 10, WL 234. REPAIRED WEB PER SRM.Mar 10, 2006 · N360SW · Boeing 7373H4SDR IXXA06SMN086SBulkhead · corrodedDURING ROUTINE C CHECK, FLT CMPT CORR BETWEEN FINGER DOUBLER AND BULKED, STA 67 RBL 53. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06130 DATE 03-09-06 EO SEMAN 2006174 DATE 03-15-06. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17, 18. FOUND OUT OF LIMITS IAW Mar 9, 2006 · N602AL · Doug DC873FSDR EIA2006056Pressure Panel · crackedDURING CHECK FOUND 2 CRACKS IN NWW ON SIDE PANEL BETWEEN BS280-300, WL 170. REPAIRED IAW SRM 53-10-04, FIG 116.Mar 8, 2006 · N479EV · Boeing 747132SDR ABXA060168Strap · crackedAFT CARGO COMPARTMENT FORWARD BULKHEAD REINFORCEMENT STRAP AT STATION 980 AND JUST ABOVE LONGERON 33 LEFT, CRACKED. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE AT REINFORCEMENT STRAP AT STA 980, JUST ABOVE LONGERON 33 LEFT IN AFT CARGO COMPARTMENT, FORWARD Mar 8, 2006 · N828AX · Doug DC863FSDR UPS06446638Bulkhead · corrodedRT WLG W/W CANTED BULKHEAD LOWER AREA SURFACE CORROSION REVEALED AT BS 1241 RBL 36-50. CORROSION BLEND OUT 0.039" BY 2" BY 12" EXCEED SRM 53-10-01 FIG 1 LIMITS, RT WLG W/W CANTED BULKHEAD BS 1238 TO BS 1241 RBL 35" TO RBL 55". REPAIRED AS PER HX RS NR R53-48Mar 8, 2006 · N681UP · Boeing 747121SDR 2006UALA00448Bulkhead · crackedBS 1809 BULKHEAD RT SIDE, FWD OUTER CHORD, INBD FLANGE HAS A CRACK COMING OUT OF THE FASTENER HOLE. DAMAGE FOUND AS A RESULT OF ROUTINE INSPECTION, MANDATED PER AD 2005-11-02. REPAIRED PER AD REQUIREMENTS.Mar 8, 2006 · N641UA · Boeing 767322SDR TAMF20060005SBulkhead · crackedDURING INSPECTION CHECK WAS FOUND A CRACK ON NOSE WHEEL BULKHEAD RT VERTICAL CHORD STA 287, BL 25. DAMAGE WILL BE REPAIRED IAW EWO 767 53-006, SRM 57-70-12 FIGURE 1.Mar 8, 2006 · N767QT · Boeing 767200SDR TAMF20060004SBulkhead · crackedDURING INSPECTION CHECK WAS FOUND A CRACK ON NOSE WHEEL BULKHEAD LT VERTICAL CHORD STA 287, BL 25. DAMAGE WILL BE REPAIRED IAW EWO 767 53-005, SRM 57-70-12 FIGURE 1.Mar 8, 2006 · N767QT · Boeing 767200SDR 200600293Bulkhead · corrodedBS 1480 FWD BULKHEAD WEB, LBL 36-42, LBL 51.5 AND RBL, 24.75, CORROSION - REPAIR. THIS ECRA PROVIDES INSTRUCTIONS TO REMOVE CORROSION, HFEC INSPECT TO VERIFY ALL DAMAGE IS REMOVED, SPOTFACE THE FASTENER LOCATIONS FOR PROPER SEATING OF THE FASTENERS, AND TO OVMar 7, 2006 · N923FT · Boeing 7472U3BSDR LR7A06008Bulkhead · crackedDURING 'B-1' CHECK PER HB5302, FOUND SIDE BULKHEAD WEB CRACKED AT FS902, WL200, RBL68. REPAIRED IAW SMP583 51-140-17, N/R 0070.Mar 7, 2006 · N403LC · Lkheed 382GSDR LR7A06006Bulkhead · crackedDURING 'B-1' CHECK PER HB5302, FOUND OVERHEAD BULKHEAD WEB CRACKED AT FS946, WL275, RBL50. REPAIRED IAW SMP583 51-140-17, N/R 0068.Mar 7, 2006 · N403LC · Lkheed 382GSDR ASOA06282Pressure Blkhd · crackedDURING A C-CHECK, THE PRESSURE BULKHEAD FORWARD FACE, AT FS 409+128, BOTTOM OB RADIUS OF THE VERTICAL BEAM AT RBL 18, WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE PRESSURE BULKHEAD FORWARD FACE, AT FS 409+128, BOTTOM OB RADIUS OF THE VERTICAL BEAM AT RBLMar 6, 2006 · N857AS · Cndair CL6002B19SDR AWXA200600573Bulkhead · crackedMSN - DURING C16 CHECK DISCOVERED CRACK, 2.0 INCES, IN BULKHEAD CENTER WEB AT LEFT UPPER ANENNA MOUNT AT BS 178, BL 5.7L, WL 209. MAINTENANCE CUT AND REMOVED DAMAGED PART OF CENTER WEB AT BS 178 UPPER ANTENNA MOUNT BL 5.7L, WL 209. FABRICATED DOUBLER AND FILMar 5, 2006 · N309AW · Boeing 7373G7SDR AWXA200600571Beam · crackedMCN - DURING C16 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, 0.75 INCHES, AT BS 178, WL 182, BL 17.1L. MAINTENANCE CUT OUT AND REMOVED CRACKED VERTICAL BEAM WEB AT BL 17.1L, BS 178 AFT SIDE OF BULKHEAD WL 182. FABRICATED DOUBLER AND REPAIR WEB IAW BOEING 737-Mar 5, 2006 · N309AW · Boeing 7373G7SDR AWXA200600617Bulkhead · crackedMCN - DURING C16 CHECK DISCOVERED CRACK, 0.30 INCHES AT BS 178 BL 5.7R VERTICAL BEAM ON AFT SIDE OF BULKHEAD AT WL 181. CRACK IS AT LANDING GEAR PULLY CUT OUT LOWER FWD CORNER. MAINTENANCE REPAIRED VERTICAL BEAM ON AFT SIDE OF BS 178 BULKHEAD AT BL 5.7R WL Mar 3, 2006 · N309AW · Boeing 7373G7SDR UPS06146478Bulkhead · crackedAFT CARGO COMP TOP OF PRESSURE BULKHEAD AT FS 54 CENTER LINE BRACKET HAS CRACK. REMOVED AND REPLACED BRACKET PER A300 SRM 15-40-00.Mar 2, 2006 · N129UP · Airbus A300F4622RSDR 06FDEA0898Bulkhead · crackedDISCREPANCY CLG SPACE FOUND 1EA CRACK 1 INCH LONG ON SKIN OF BLKHD AT STA 1501 X30 RT. PERFORMED REPAIR DOUBLER IAW SRM 53-00-00 FIG 10 VOL 1 AND REPLACED FIITING IAW SRM 51-33-01 PAR 6-10 VOL 2.Mar 2, 2006 · N68054 · Doug DC1010SDR 06FDEA0905Bulkhead · crackedCLG WHEEL WELL SPACE FOUND 4EA CRACKS FROM .5" INCH TO 2 INCHES LONG ON UPPER SIDE LEFT VERTICAL BULKHEAD FROM STA 1491 TO 1501 LEFT SIDE X 31. INSTALLED CABLE, PULLEY, ACCUMULATOR AND PIPES IAW MM 27-51-07-2 AND MM 27-51-09-2 AND MM 20-10-01-2 AND MM 29-12Mar 2, 2006 · N68056 · Doug DC1010SDR USAA060372Bulkhead · crackedFOUND WEB CRACKED, BS 178 RBL 10.5 WL 218. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 201, DEFECT SIZE: 1".Mar 1, 2006 · N334US · Boeing 737301SDR ASAA0610210Bulkhead · corrodedNWW COMPARTMENT AFT PRESSURE BULKHEAD LT ACCESS HOLE AT BSTA 267 LWR CORNER BEAM HAS CORROSION. REPLACED PWR SRM 51 30 02.Feb 27, 2006 · N742AS · Boeing 737290CSDR UPS06846439Bulkhead · corrodedINSPECTION TYPE:C1 IN 60 HOLE CORROSION ON WEB UNDER L-ANGLE OF BULKHEAD JUST AFT OF HOLE ENTRANCE. REMOVED CORRODED WEB AND ANGLE AT STA 1788 IAW SRM 53-02-00-0. FABRICATED AND INSTALLED REPAIR WEB AND ANGLE AT STA 1788 IAW SRM 53-02-00-0, 53-05-03-0, AND SFeb 22, 2006 · N703UP · Doug DC871FSDR SWAA060685Stiffener · bulgedDURING SCHEDULED C4 CHECK, FOUND BS 1016 AFT PRESS BULKHEAD RADIAL STIFFENER BULGED AT STR 9R. MX FERRY TO DHN FOR REPAIRS. REPAIRED RADIAL STIFFENER PER SRM.Feb 22, 2006 · N314SW · Boeing 7373H4SDR DL73S060147Bulkhead · puncturedPUNCTURE REPAIR FOR AFT BULKHEAD WEB. THE NLG DOWNLOCK ACTUATOR FAILED AND CAUSED A PUNCTURE IN THE AFT BULKHEAD WEB AT FS 294.5, BL 0, WL 165. THE PUNCTURE MEASURED 1.5 X .75 INCH. THE ACTUATOR WAS REPLACED AND THE AIRCRAFT FERRIED IN AN UNPRESSURIZED STATFeb 20, 2006 · N324DL · Boeing 737232SDR ABXA060094Door · crackedDOUBLER AT RIGHT UPPER AFT, AFT PRESSURE BULKHEAD DOOR CORNER HAD A .875 INCH RADIAL CRACK. REPAIRED AREA IAW REA D953-53267MR.Feb 14, 2006 · N941AX · Doug DC931SDR 06FDEA0682Bulkhead · crackedAFT BODY BLKHD EXT STRUCTURE FOUND 1 CRACK 0.50" LONG ON HORIZONTAL LONGERON AT STA 2163.685 X37 LT SIDE. REPAIRED CRACKED STIFFENER IAW SRM 53-40-00 FIG 7 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163376/N00376 AND IAW SRM 53-40-00 FIG 7 VOL 1.Feb 14, 2006 · N68056 · Doug DC1010SDR MASA200600710Bulkhead · crackedFOUND A CRACK IN 621 PRESSURE BULKHEAD WEB AT BRACKET WHILE CONDUCTING NDT INSPECTION. PERFORMING PERM REPAIR.Feb 13, 2006 · N653ML · Cndair CL6002B19SDR CA060210009Angle · corroded(CAN) DURING A C-CHECK HEAVY CORROSION WAS FOUND ON THE FRONT PRESSURE BLK STA 120.0 ON THE LOWER AFT CAP ANGLE P/N 85310109 AND ON THE FORWARD CAP ANGLE P/N 85310108. THE DAMAGE WAS SUBMITTED TO MFG WHO ISSUE A SPECIFIC REPAIR TO BE CARRIED OUT. (TC NR 200602Feb 10, 2006 · Dhav DHC8102SDR SWAA060491Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, RBL 5.7, WL 184. REPAIRED WEB PER BFG ER.Feb 9, 2006 · N351SW · Boeing 7373H4SDR CA060209006Bulkhead · cracked(CAN) DURING AN ANNUAL INSPECTION, AM AME NOTICED THE MLG STRUT BULKHEAD UNDER THE CABIN FLOOR HAD SMALL CRACKS. UPON FURTHER INSPECTION WITH THE FLOORS REMOVED IT WAS FOUND THE ENTIRE MLG ATTACHMENT BULKHEAD/BOX STRUCTURE WAS NEAR FAILURE. MANY COMPONENTS MAKFeb 8, 2006 · Cessna 150
Back to JASC 5312