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 MWEA98245Blkhd Stiffener · corrodedTHE 1121 CANTED BULKHEAD LONGERON 14L STIFFENER WAS FOUND CORRODED. REMOVED AND REPLACED STIFFENER.Feb 27, 1998 · N212ME · Doug DC932SDR MWEA98244Blkhd Stiffener · corrodedTHE 1121 CANTED BULKHEAD STIFFENER AT LONGERON 12L WAS FOUND EXFOLIATED. REMOVED AND REPLACED STIFFENER.Feb 27, 1998 · N212ME · Doug DC932SDR MWEA98243Bulkhead Doubler · corrodedDOUBLER ON CANTED BULKHEAD 1089 LONGERON 11R WAS FOUND CORRODED. REMOVED AND REPLACED DOUBLER.Feb 27, 1998 · N212ME · Doug DC932SDR CALA9800336Bulkhead T · crackedINSPECTION FOUND A 2.5 CRACK THROUGH FASTENER HOLE ON VERTICAL LEG OF BULKHEAD T AT STA 1156 BETWEEN LONGERON 40L AND 39L. A NEW TEE CAP WAS INSTALLED IAW EA SA003-5310-03391.Feb 26, 1998 · N68044 · Doug DC1010SDR AU980271Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED AT BS 178. LT VERTICAL CHORD CRACKED IN TWO PLACES AND WEB CRACKED IN FIVE PLACES.Feb 26, 1998 · Boeing 737376SDR ABXA9800127Bulkhead Angle · corrodedDURING C-CHECK, FOUND THE SLANT PANEL ANGLE STATION 690 AND LBL 8 CORRODED. REPAIRED ANGLE IAW ABX REA D953-22465-MR.Feb 25, 1998 · N938AX · Doug DC931SDR USAA980095Bulkhead · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 178 BULKHEAD UNDER RADAR DISH MOUNT, INBOARD SIDE OF RT LOWER HAT SECTION LEG. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-11-1, SRM 53-10-11. (M)Feb 23, 1998 · N254AU · Boeing 737201SDR USAA980084Blkhd Stiffener · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 178 LBL 5.75 AT WL 183.5 STIFFENER, BULKHEAD. DOUBLER AND STIFFENERS INSTALLED, REPAIRED PER TR 53-10-17. (M)Feb 23, 1998 · N254AU · Boeing 737201SDR USAA980083Bulkhead · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 178 BULKHEAD LBL 5, WL 199. INSTALLED DOUBLER REPAIRED PER SRM 53-10-11. (M)Feb 23, 1998 · N254AU · Boeing 737201SDR MWEA98195Bulkhead Web · crackedRIGHT HAND LOWER WEB OF THE BULKHEAD AT FS 965 WAS FOUND CRACKED IN SEVERAL PLACES. REMOVED DAMAGED SEC OF WEB, FAB REPAIR PARTS IAW SRM 53-03 FIG 19, INSTALLED REPAIR PARTS IAW SRM 51-30.Feb 23, 1998 · N212ME · Doug DC932SDR MWEA98193Bulkhead Web · crackedWEB ATTACHED TO RADIAL STIFFENER APB FOUND CRACKED AT THE O/B END LONG14R. STOP DRILLED CRACK, FABED REPAIR ANGLES IAW DRAW J060110, INSTALLED REPAIR ANGLES IAW SRM 51-30.Feb 23, 1998 · N212ME · Doug DC932SDR DL72S980613Bulkhead Skin · crackedAT HMV, FOUND APU BLEED AIR CUTOUT FWD BLKHD RT W/W SKIN CRACKED. REPAIRED PER SRM 53-10-9 FIG 5.Feb 23, 1998 · N522DA · Boeing 727232SDR MWEA98184Bulkhead Clips · crackedWEB ATTACHED TO THE RADIAL STIFFENER ON THE APB WAS FOUND CRACKED ON THE OUTBOARD END. INSTALLED REPAIR CLIPS IAW SRM 51-30 AND DRAWING J060110.Feb 20, 1998 · N212ME · Doug DC932SDR DLL10980449Bulkhead Web · crackedTHE FS 1212 BULKHEAD WEB WAS FOUND WITH A .25 LONG CRACK AT RBL 42.5. THE CRACK WAS ROUTED OUT AND A LOCAL DOUBLER REPAIR INSTALLED PER ER/A 364062-14AD, REV A. THE REPAIR WAS GRANTED AMOC APPROVAL FOR AD 96-20-10.Feb 20, 1998 · N714DA · Lkheed 10113851SDR AU980408Bulkhead · cracked(AUS) LT AND RT LOWER AFT DOOR POST BULKHEADS (PN 0512187-1 LT AND PN 0512187-2 RT) CRACKED. FOUND DURING INSPECTION IAW SB SEB 97-1. PART TC: 5,920.Feb 20, 1998 · Cessna 172PSDR 99FDEA00320Bulkhead Web · crackedN0222 - DURING A/C P-F CONVERSION AT OAN, FOUND A 0.50 IN CRACK IN THE CANTED BULKHEAD AT BS 2163.685. TRIMMED WEB TO REMOVE CRACK AND INSTALLED A TITANIUM FILLER AND DOUBLER IAW EA NR 8-5310-35908.Feb 20, 1998 · N387FE · Doug DC1010SDR USAA980077Bulkhead Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2.5 INCH CRACK BS 178 BULKHEAD AT UPPER LEFT RADAR MOUNT BULKHEAD SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-11, FIG 1. (M)Feb 19, 1998 · N223US · Boeing 737201SDR UPS98225858Bulkhead Skin · crackedINSPECTION TYPE-SI, BS 178 BULKHEAD IS CRACKED AROUND FASTENERS AT BS 10, WL 235. REMOVED DAMAGED AREA .5 X 3 ENCOMPASSING 3 CRACKS. REPAIRED BS 178 AT LBL 10, WL 235, PER 727 SRM 53-10-9 AND SRM 51-30-2.Feb 19, 1998 · N904UP · Boeing 72751CSDR EIA990015Bulkhead Gussett · corrodedDURING C-CHECK, MAIN CABIN AFT PRESSURE BULKHEAD, BS 840 LEFT SIDE OF DOOR JAMB LOWER PLATE HAS HEAVY CORROSION, NRC 0589. REPLACED GUSSET IAW SRM 51-30-05. (M)Feb 19, 1998 · N915F · Doug DC915FSDR P5CA9800374Bulkhead · crackedFUSELAGE BS140 B/H FWD FACE FOUND CRACKED AT RBL 38 2 PLACES. WEB REPAIRED AS PER SRM 53-10-04 FIG 89.Feb 18, 1998 · N3203Y · Boeing 747128SDR AU980224Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD WEB CRACKED IN SIX PLACES.Feb 18, 1998 · Boeing 737376SDR 9808396612Bulkhead · crackedDURING M-CHECK, FOUND CRACK ON TOP OUTBOARD (RHS) CORNER AT BULKHEAD 400, ZONE 110. REPAIRED PER EO 6-53-41184.Feb 18, 1998 · N612US · Boeing 747251BSDR ABXA9800081Blkhd Doubler · crackedDURING C-CHECK COMPLIANCE WITH S/B 53-137, FOUND DOUBLER CRACKED RADIALLY IN UPPER RIGHT AND UPPER LEFT CORNERS. REPAIRED DOUBLER IAW ABX REA D953-22492-MR AND DC9 S/B 53-137.Feb 16, 1998 · N938AX · Doug DC931SDR P5CA9800296Bulkhead · crackedCRACKED ON BODY STATION 140 BULKHEAD AT LBL 38. REPAIRED AREA WEB PER BAC SRM 53-10-06.Feb 14, 1998 · N3203Y · Boeing 747128SDR P5CA9800295Bulkhead · deformedDEFORMATION AT 6 O'CLOCK POSITION ON APU FIRE BULKHEAD AT STATION 2658. DRESSED OUT DEFORMED AREA PER BAC SRM 51-10-01.Feb 14, 1998 · N3203Y · Boeing 747128SDR P5CA9800286Bulkhead · corrodedLEVEL 1 CORROSION, ON THE FORWARD SIDE OF THE APU BULKHEAD AT STATION 2658, RIGHT BODY LINE 512. CORROSION REMOVED AND AREA TREATED PER BAC SRM 51-10-01 AND 51-10-02.Feb 14, 1998 · N3203Y · Boeing 747128SDR 9803899931Bulkhead Doubler · crackedDURING AFT PRESSURE BULKHEAD INSPECTION, FOUND CRACKS IN THE -71 DOUBLER AT THE AFT PRESSURE BULKHEAD UPPER DOOR CUTOUT. REPAIRED PER EA 99-154161.Feb 14, 1998 · N90S · Doug DC931SDR 9803889931Bulkhead Skin · crackedDURING AFT PRESSURE BULKHEAD INSPECTION, FOUND CRACK IN THE AFT PRESSURE BULKHEAD SKIN AT THE UPPER DOOR CUTOUT 11.5 RIGHT OF CENTER LINE. REPAIRED PER EA 99-154161.Feb 14, 1998 · N90S · Doug DC931SDR AU980268Chord · cracked(AUS) FORWARD PRESSURE BULKHEAD LT SIDE CHORD LOCATED AT WL 207 CRACKED. CRACK LENGTH 38.1MM (1.5 INCH). FOUND DURING VISUAL INSPECTION IAW ER B73-53-10-39C.Feb 12, 1998 · Boeing 73733ASDR C2XA98IA019Bulkhead · crackedIAH - DURING C-CHECK INSPECTION, THE MAIN LANDING GEAR WHEEL WELL AFT BULKHEAD WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER REPAIR OVER THE AFFECTED AREA IAW ATR42-500 SRM 51-70-00, AND THE AIRCRAFT WAS APPROVED FOR RETUFeb 11, 1998 · N19446 · Aerosp ATR42500SDR AU980266Web · cracked(AUS) FORWARD PRESSURE BULKHEAD WEB SKIN CRACKED IN EIGHT PLACES. FOUND DURING ULTRASONIC INSPECTION.Feb 11, 1998 · Boeing 73733ASDR UPS98825892Bulkhead Angle · corrodedINSPECTION TYPE:C AFT SIDE OF F/S 70 O/B OF 33R LOWER BULKHEAD L ANGLE HAS HEAVY CORROSION AROUND BOLT AND BETWEEN IT AND LONGERON FITTING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHORD IAW SRM 53-2-5 51-1-20D, AND DWG 5613064.Feb 10, 1998 · N752UP · Doug DC871FSDR DL72W980354Blkhd Stiffener · crackedCRACKS WERE FOUND IN THE L/RBL 36083 VERT STIFFENER ON THE FWD SIDE OF THE BS 1183 BLKHD. CRACKS WERE LOCATED AT APPROX WL 238 AND WERE NO MORE THAN 2 IN LENGTH. REPAIR PER ERA 331332-14.Feb 10, 1998 · N296WA · Boeing 727247SDR MWEA98148Bulkhead · corrodedDURING INSPECTION, FOUND LIGHT CORROSION ON FWD SIDE OF APB LEFT SIDE FROM APPROXIMATELY LONG 26L TO 28L. MTC REPAIRED IAW SRM 53-03 FIG 9 SHEET 1 AND 51-30-5.Feb 9, 1998 · N203ME · Doug DC932SDR DL73S980339Bulkhead Web · crackedDURING INSPECTION, SERVERAL CRACKS WERE FOUND IN THE BLKHD WEB AT FS 178. THE CRACKS WERE LOCATED AT WL 192 TO 202 AND LBL 5 AND RBL 5. REPAIRED PER ERA 331313-14.Feb 9, 1998 · N328DL · Boeing 737232SDR DL72W980341Bulkhead Beam · crackedMTC FOUND A .1875 INCH CRACK IN THE OUTBD AFT FLANGE OF THE RBL 8 VERT BEAM IN THE FS 1183 BLKHD, WHICH BEGINS AT WL 182. REPAIRED PER ERA 362891-14, REV A.Feb 9, 1998 · N296WA · Boeing 727247SDR AU980301Bulkhead · cracked(AUS) FUSELAGE AFT DOOR POSTS P/N 0512187-1 (LT) AND P/N 0512187-2 (RT) CRACKED. FOUND DURING INSPECTION IAW CESSNA SB SEB 97-1.Feb 9, 1998 · Cessna 172PSDR 9807886612Bulkhd Fastener · crackedDURING M-CHECK, FOUND CRACK ON FASTENER HOLE AT FS 140 BULKHEAD, STR 14R, INNER RING DOUBLER AREA. REPAIRED PER EA 66-156319.Feb 9, 1998 · N612US · Boeing 747251BSDR 9803919931Bulkhead Doubler · crackedDURING AFT PRESSURE BULKHEAD INSPECTION, FOUND CRACKS IN THE AFT PRESSURE BULKHEAD UPPER DOOR CUTOUT -13 DOUBLER. REPAIRED PER EA 99-154161.Feb 9, 1998 · N90S · Doug DC931SDR 9803909931Bulkhead Doubler · crackedDURING AFT PRESSURE BULKHEAD INSPECTION, FOUND CRACK IN THE -9 DOUBLER AT THE AFT PRESSURE BULKHEAD UPPER DOOR CUTOUT. REPAIRED PER EA 99-154161.Feb 9, 1998 · N90S · Doug DC931SDR AU980302Bulkhead · cracked(AUS) FUSELAGE LOWER AFT DOOR POST BULKHEADS P/N 0512187-1 AND P/N 0512187-2 CRACKED. FOUND DURING INSPECTION IAW CESSNA SB SEB97-1.Feb 6, 1998 · Cessna 172PSDR SWAA980151Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 6.7, WL 202 TO 203. REPAIRED PER BOEING SRM.Feb 5, 1998 · N669SW · Boeing 7373A4SDR SWAA980150Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 4.7, WL 199 TO 199.75 AND WL 201.5 TO 202.25. REPAIRED PER BOEING SRM.Feb 5, 1998 · N669SW · Boeing 7373A4SDR SWAA980149Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 4.7, WL 201.75 TO 202.75. REPAIRED PER BOEING SRM.Feb 5, 1998 · N669SW · Boeing 7373A4SDR SWAA980146Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 6.7, WL 209.75. REPAIRED PER BOEING SRM.Feb 5, 1998 · N669SW · Boeing 7373A4SDR QXEA9800331Bulkhead Beam · crackedPDX - PREVIOUS DOUBLER REPAIR AT TOP SURFACE OF HORIZONTAL BEAM VI APPEARS TO BE CRACKED ON FORWARD SIDE OF FORWARD PRESSURE BULKHEAD. REPAIRED IAW HORIZON EA 4-53-370.Feb 5, 1998 · N476US · Fokker F28MK4000SDR DHL9872446CBulkhead · crackedAT C-CHECK, 1183 BULKHEAD RT FWD SIDE WL 237.1 I/B AND O/B SIDES OF VERTICAL STIFFENER CRACKED 37 RIGHT OF CENTER. STOP DRILL, HFEC, INSTALLED REPAIR PER S/B 53-0192, AND SRM 51-30-2. N/R 3499.Feb 5, 1998 · N724DH · Boeing 727228SDR AU980156Bulkhead · cracked(AUS) FUSELAGE FORWARD PRESSURE BULKHEAD CONTAINED FIVE WEB CRACKS ANDTWO CRACKS IN THE LH VERTICAL STIFFENER.Feb 5, 1998 · Boeing 737376SDR SWAA980139Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND CRACKS ON BS 178 BULKHEAD AT WL 188, LBL 0.5 AND RBL 0.5. REPAIRED PER BOEING SRM.Feb 4, 1998 · N669SW · Boeing 7373A4SDR SWAA980112Bulkhead Skin · damagedDURING SCHEDULED A1 CHECK, FOUND BS 178 BLKHD AND SKIN DAMAGED. REPAIRED PER BOEING SRM.Feb 4, 1998 · N323SW · Boeing 7373H4
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