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 SWAA010590Splice Plate · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD SKIN SPLICE PLATE CRACKED AT LBL 4, WL 242. REPAIRED SKIN SPLICE PER BFG ER.Feb 27, 2001 · N301SW · Boeing 7373H4SDR ARWA0010204Bulkhead · crackedDURING ROUTINE MAINTENANCE, A CRACK IN THE BULKHEAD CAP AT STATION 449.0 BETWEEN STRINGERS 40 & 41 WAS DISCOVERED. PERMANENT REPAIR COMPLETED IAW SRM 53-11-00.Feb 27, 2001 · N260FA · Lkheed 1011385114SDR LR7A01004Bulkhead · crackedDURING SCHEDULED B3 CHECK PER JOB CARD HB0506, FOUND FS 608 LT WW BULKHEAD CRACKED AT RBL 62, WL 192 INSULATION MOUNT STUD. REPAIRED IAW SRM SMP 583-53-40-10.Feb 27, 2001 · N404LC · Lkheed 382GSDR LR7A01002Bulkhead · crackedDURING SCHEDULED B3 CHECK PER JOB CARD HB0505, FOUND FS 902 RT WEB CRACKED AT RBL 62, WL 220. REPAIRED IAW SRM SMP 583-51-140-17.Feb 27, 2001 · N404LC · Lkheed 382GSDR ASAA0110111Bulkhead · crackedPHX - DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178, LBL 7 CRACKED. REPAIRED PER SRM. (M)Feb 26, 2001 · N730AS · Boeing 737290CSDR ASAA0110112Bulkhead · crackedPHX - DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178, WL 200, LBL 7 CRACKED. REPAIRED PER SRM. (M)Feb 26, 2001 · N730AS · Boeing 737290CSDR 20010403CW019Bulkhead · damagedCORROSION FOUND EXFOLIATING (1) SPAR CAP ON RIGHT WING HEAVY CORROSION ON (2) UPPER CABIN CARRY THRU STRUCTURE. (3) VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON (4)CANTED BULKHEAD AT FUSELAGE STATION 20.5 BOTFeb 26, 2001 · N3232X · Cessna 150GSDR USAA010183Pressure Panel · crackedCLT - FOUND PRESSURE DECK CRACKED .25 INCH, BS 727B BETWEEN STRINGER 8 AND 9L. REPAIRED DOUBLER PER TR 53-10-14. (M)Feb 26, 2001 · N435US · Boeing 7374B7SDR USAA010182Pressure Panel · crackedCLT - FOUND PRESSURE DECK CRACKED 1 INCH, BS 664, LBL 32. INSTALLED DOUBLER AND STIFFENER PER TR 53-60-04 FIG 1. (M)Feb 26, 2001 · N435US · Boeing 7374B7SDR AWXA0001418Bulkhead · crackedCENTER WEB CRACKED FS 178 WL 187 RBL 0.7 (1.0L). REMOVED DAMAGE, NDT VERIFIED CRACK TERMINATED. FABED FILLERS AND DOUBLER; TREATED AND PRIMED AND INSTALLED REPAIR PARTS IAW SRM 53-10-03, NTM PT 6 51-00-00, SRM 53-10-08 AND SRM 51-40-02 AND SRM 51-20-01.Feb 26, 2001 · N306AW · Boeing 7373G7SDR AWXA0001417Bulkhead · crackedCENTER WEB CRACKED FS 178 RBL 5.0 WL 198 AND WL 202. CUT OUT DAMAGED AREA, NDT - NO CRACKS NOTED. FABED DOUBLER AND 3 FILLERS IAW SRM 53-10-08; INSTALLED IAW 51-40-02; TREAT AND PRIMED IAW SRM 51-20-01.Feb 26, 2001 · N306AW · Boeing 7373G7SDR UPS01235253Bulkhead · chafedINSPECTION TYPE:C+SI, OPERATING HANDLE FOR AIRSTAIRS PUMP HAS CHAFED AFT PRESSURE BULKHEAD. REPAIRED IAW SMRO EO 2001-006-019.Feb 23, 2001 · N941UP · Boeing 72722CSDR SWAA010537Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND 2 BS 178 BULKHEAD WEB CRACK, BEHIND DOUBLER, AT RBL 5.9, WL 201. REPAIRED BULKHEAD WEB PER SRM.Feb 22, 2001 · N307SW · Boeing 7373H4SDR AALA20010348Stiffener · crackedTUL - FOUND VERTICAL STIFFENER ON BULKHEAD 1183 HAS CRACK FROM LOWER END BL 8. INSTALLED REPAIR PER DRAWING NR 65C29080. INSTALLED BL 8 PREVENTATIVE MOD AND REPAIR KIT. (M)Feb 21, 2001 · N861AA · Boeing 727223SDR USAA010227Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .5 INCH, BS 178, RBL 5.7, WL 180 AFT SIDE. INSTALLED DOUBLER PER SRM 51-40-02. (M)Feb 21, 2001 · N432US · Boeing 7374B7SDR SWAA010526Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKS AT RBL 17.1, WL 163 & LBL 17.1, WL 229. REPAIRED BULKHEAD WEB PER BFG ER.Feb 21, 2001 · N672SW · Boeing 7373Q8SDR AWXA0001402Bulkhead · crackedCENTER WEB CRACKED AT FS 178 LBL 6 WL 212. STOP DRILLED CRACK; NDT CRACK TERMINATED. FABED AND INSTALLED DOUBLER AND 2 FILLERS IAW SRM 53-10-08.Feb 21, 2001 · N312AW · Boeing 7373S3SDR AWXA0001401Bulkhead · crackedCENTER WEB CRACKED AT FS 178 RBL 6 WL 210. STOP DRILLED CRACK IAW SRM 53-10-08; NDT NO CRACKS NOTED. FABED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-10-08.Feb 21, 2001 · N312AW · Boeing 7373S3SDR AWXA0001400Bulkhead · crackedCENTER WEB CRACKED FS 178 WL 187 LBL 0.7 AND RBL 0.7. REMOVED DAMAGE; NDT - NO CRACKS NOTED. FABED DOUBLER AND FILLER; INSTALLED DOUBLER AND FILLER IAW SRM 53-10-08.Feb 21, 2001 · N312AW · Boeing 7373S3SDR TWAA00103403Doubler · crackedDURING OP 15 MAINT CHECK FOUND PRESSURE DECK BULKHEAD DOUBLER WAS CRACKED AT 718 CASTING, LT MLG WHEEL WELL. REPLACED DOUBLER AND SEALED PER SRM 51-20-0 AND 51-60-0. FASTENER SUBSTITUTION PER SRM 51-30-5 FASTENER INSTALLATION.Feb 21, 2001 · N992Z · Doug DC931SDR AWXA0001371Bulkhead · crackedCENTER WEB CRACKED FS 178 WL 202 LBL 6.0. STOP DRILLED CRACK IAW SRM 53-10-08 FIG 209; NDT IAW NTM PT 6 51-00-00; STOP DRILL TERMINATED CRACK.Feb 16, 2001 · N312AW · Boeing 7373S3SDR AWXA0001370Bulkhead · crackedCENTER WEB CRACKED FS 178 WL 202 RBL 6.0. STOP DRILLED CRACK IAW SRM 53-10-08 FIG 209; NDT IAW NTMP 51-00-00 CRACK TERMINATED.Feb 16, 2001 · N312AW · Boeing 7373S3SDR AWXA0001365Bulkhead · crackedCENTER WEB CRACKED FROM STA 178 LBL 5.0 WL 198 AND 202. CUT OUT 2 CRACKS IAW SRM 53-10-08, NDT NO CRACKS NOTED; FABED AND INSTALLED 1 DOUBLER AND 3 FILLERS IAW SRM 53-10-08.Feb 16, 2001 · N312AW · Boeing 7373S3SDR AWXA0001364Bulkhead · crackedCENTER WEB CRACKED AT FS 178 RBL 5.0 WL 198, WL 202. CUT OUT 2 CRACKS IAW SRM 53-10-08, NDT NO CRACKS; FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08, TOP COAT APPLIED.Feb 16, 2001 · N312AW · Boeing 7373S3SDR AWXA0001361Bulkhead · crackedULTRASONIC INSP DETECTED ONE CRACK AT RBL 5.7 BEHIND STIFFENER AT WL 195-207 FS 178. CUT OUT DAMAGED AREA, FABED FILLERS AND DOUBLER; INSTALLED FILLERS AND DOUBLER IAW SRM 53-10-08 AND 51-40-02.Feb 16, 2001 · N306AW · Boeing 7373G7SDR AWXA0001360Bulkhead · crackedCENTER WEB CRACKED FS 178 LBL 5.0 WL 198 & 202. CUT OUT DAMAGED AREA, FABED FILLERS AND DOUBLER; INSTALLED FILLERS AND DOUBLER IAW SRM 53-10-08, 51-40-02.Feb 16, 2001 · N306AW · Boeing 7373G7SDR AWXA0001359Bulkhead · crackedULTRASONIC INSPEC DETECTED 2 CRACKS AT LBL 5.7 BEHIND STIFFENER BETWEEN WL 195 & WL 207 STA 178. CUT OUT DAMAGED AREA, FABED FILLERS & DOUBLER, INSTALLED FILLERS AND DOUBLER IAW SRM 53-10-08 & 51-40-02.Feb 16, 2001 · N306AW · Boeing 7373G7SDR AWXA0001358Bulkhead · crackedULTRASONIC INSPECTION DETECTED 2 CRACKS BEHIND STRAP AT LBL 5.7 APPROX 3 INCHES ABOVE WL 207 AT FS 178. STOP DRILLED CRACK IAW SRM 53-10-08 FIG 209; NDT FOUND OUT CRACK TERMINATED; FABED DOUBLER AND 2 FILLERS AND DOUBLER; TREAT AND PRIMED IAW SRM 53-10-08 FIGFeb 16, 2001 · N306AW · Boeing 7373G7SDR AWXA0001352Bulkhead · crackedBS 178 BKLHD WEB CRACKED AT WL 201 LBL 6. REPAIRED IAW BSB 737-53A1173 AND SRM 53-10-08 FIG 209.Feb 16, 2001 · N302AW · Boeing 7373G7SDR AWXA0001351Bulkhead · crackedBS 178 BKLHD WEB CRACKED AT WL 202 LBL 5.5. REPAIRED IAW BSB 737-53A1173 AND SRM 53-10-08 FIG 209.Feb 16, 2001 · N302AW · Boeing 7373G7SDR AWXA0001350Bulkhead · crackedBS 178 BLKHD WEB CRACKED AT WL 202 RBL 5.5. REPAIRED IAW BSB 737-53A1173 AND SRM 53-10-08 FIG 209.Feb 16, 2001 · N302AW · Boeing 7373G7SDR AWXA0001348Bulkhead · crackedBS 178 BLKHD WEB CRACKED AT LBL 5.5 WL 199. REPAIRED WEB IAW BSB 737-53A1173 AND SRM 53-10-08 FIG 209.Feb 16, 2001 · N302AW · Boeing 7373G7SDR AWXA0001347Bulkhead · crackedSTA 178 BULKHEAD RT SIDE INTERCOSTAL CRACKED AT WL 207 AS MARKED (VIEW FROM ABOVE FLOOR). REPAIRED CRACK IN INTERCOSTAL, CLIP AND WEB IAW BSB 737-53A, PART 1 WORK PLAN D, 2, A, 2&3, AND FIG 68 (PAGE 73). CLIP - P/N 65-45833-468.Feb 16, 2001 · N302AW · Boeing 7373G7SDR AWXA0001345Intercostal · crackedBS 178 BULKHEAD LT INTERCOSTAL AT LT SIDE CHORD WL 207 IS CRACKED (IDENTIFIED DURING INITIAL INSP ON C-12 CHECK). REPAIRED CRACKS IN WEB, CLIP AND INTERCOSTAL AT STA 178 LT IAW BSB 737-53A1173 PARTS I, D, 2, A, 2 & 3, FIG 68, PAGE 73 AND SRM 51-70-12. PARTS Feb 16, 2001 · N302AW · Boeing 7373G7SDR AWXA0001343Bulkhead · crackedBS 178 WEB CRACKED AT WL 199 RBL 5.5 (CRACK IDENTIFIED DURING C-12 INITIAL INSPECTION). REPAIRED WEB IAW BSB 737-53A1173 AND SRM 53-10-08 FIG 209.Feb 16, 2001 · N302AW · Boeing 7373G7SDR RRXA10839Attach Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO AFT LWR CARGO COMPARTMENT BULKHEAD DIVIDERS ATTACH ANLGE AT STA Y+14, Z-7, X-24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATEFeb 15, 2001 · N801GP · Doug DC871FSDR SWAA010476Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 4.7, WL 212-213. REPAIRED BULKHEAD PER SRM.Feb 15, 2001 · N672SW · Boeing 7373Q8SDR CALA0100121Bulkhead · crackedINSPECTION FOUND TWO CRACKS ON FLOOR STRUCTURE WEB AT LT AND RT W/L 195, ONE CRACK ON CENTER WEB AT W/L 200, LBL 5.7 AND ONE CRACK ON CENTER WEB AT W/L 201, RBL 5.7 DURING 737 FUS-BS 178 BULKHEAD INSPECTION. THE CRACKS WERE .5 INCH IN LENGTH. REPAIRS WERE Feb 15, 2001 · N70330 · Boeing 7373T0SDR 0103369992Bulkhead · corrodedDuring H-check found corrosion on the horizontal flange of the floor support tee on RHS of the aft pressure bulkhead. Repaired per EA. 99-180937.Feb 14, 2001 · N8960E · Doug DC931SDR EISA20010042Bulkhead · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT AFT CARGO BULKHEAD BS 1060, WL 208. FABRICATED AND INSTALLED REPAIR FRAME DOUBLER, FILLER, AND REPAIR ANGLE, AT BS 1060 WL 208. ALODINED AND PRIMED IAW SRM 53-10-8 FIG 3, 51-10-2, 51-30-2.Feb 14, 2001 · N312NE · Boeing 727223SDR CA010302006Bulkhead · cracked(CAN) CRACK ABOVE LT RUDDER STOP BOLT LOCATION ON (BULKHEAD) FLANGE BEND RADIUS DIRECTLY ABOVE BOLT. A/C HANGARED FOR LAST 15 YRS & NOT SUBJECTED TO WIND. REMOVAL & INSP SHOWS POOR STANDARD PRACTISE OF DRIVING 90 DEGS STIFFENER INTO BEND RADIUS OF FLANGE (ASSYFeb 14, 2001 · Cessna 182HSDR DL72S010270Bulkhead · crackedTHE FS 1183 BULKHEAD WEB WAS FOUND WITH A .5 INCH CRACK AT RBL 8 AND WL 182. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED WITH A TITANIUM DOUBLER PER ER/A 380049-14.Feb 14, 2001 · N525DA · Boeing 727232SDR SWAA010453Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKS AT LBL 12 TO LBL 13, WL 218 & RBL 6.7, WL 200 TO WL 201. REPAIRED BULKHEAD WEB PER SRM.Feb 13, 2001 · N672SW · Boeing 7373Q8SDR RRXA10809Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO L/H KEEL BEAM STRESS PANEL AT STA. 690-779 AND L35L-L33L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLEFeb 12, 2001 · N801GP · Doug DC871FSDR USAA010137Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .125 INCH, TWO PLACES, BS 1016 AT APPROX STRINGER 3L. INSTALLED DOUBLER PER EA 69021. (M)Feb 12, 2001 · N251AU · Boeing 737201SDR RRXA10789Stringer · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LOWER STRINGER #55 AT STA. 495 CAN'T AND 508 CAN'T, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIRAND INSTALLED IAW DC-Feb 10, 2001 · N801GP · Doug DC871FSDR RRXA10810Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO R/H KEEL BEAM ACCESS COVER AT STA. 742-749 AND L33R-L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLEFeb 9, 2001 · N801GP · Doug DC871FSDR RRXA10752Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FUSELAGE FRAME AT STA. 1170 AND LONGERON 36 TO 35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAFeb 9, 2001 · N8091U · Doug DC871FSDR DHL2001712520Pressure Panel · crackedC-CHECK, MLG WHEEL WELL TOP SURFACE SHOWS 6 CRACKS OF .75 INCH BETWEEN LBL 25 AND LBL 40, STA 900.000 AND STA 910.000. REMOVED FLOOR PANELS, BRACKETS, CLIPS, STRAPS IAW DWG 65-89360-3. PERFORMED STOP DRILL IAW DWG 65-89360. FABRICATED DOUBLER (ALCLAD 2024, Feb 9, 2001 · N712DH · Boeing 72729SDR DL73K010244Bulkhead · crackedTHE FS 178 BULKHEAD WEB WAS FOUND WITH TWO 1 INCH CRACKS AT RBL 5.7 AND WL 213. THE WEB HAD A PREVIOUS REPAIR DOUBLER FOR CRACKS AT RBL 5.7, WL 200 & BL 0, WL 190. THE EXISTING REPAIR WAS REMOVED AND A NEW ALUMINUM DOUBLER FABRICATED AND INSTALLED TO ENCOMPFeb 9, 2001 · N238WA · Boeing 737247
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