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 SWAA960104Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND 3 CRACKS ON BS 178 BULKHEAD ADJACENT TO 2 FASTENERS AT WL 234 RBL 10. REPAIRED PER BOEING SRM.Feb 18, 1996 · N318SW · Boeing 7373H4SDR 9605435505Blkhd Chord · corrodedDURING T-CHECK, FOUND CORROSION ON THE BS 324 BULKHEAD CHORD AT RBL 34, WATER LINE 208. REPAIRED CHORD (P/N 141N2932-1) PER EA 55-99494.Feb 17, 1996 · N505US · Boeing 757251SDR EISA96003Bulkhead · crackedFOUND 2.5 INCH VERTICAL CRACK IN FACE OF BS 1183 BULKHEAD LBL 36, WL 224. FABRICATED AND INSTALLED FILLER SHIM AND DOUBLER PER SRM 53-10-9. (M)Feb 16, 1996 · N315NE · Boeing 727223SDR DLL17960374Blkhd Beam · crackedTHE NLG W/W SIDEWALL BULKHEAD UPPER BEAM IS CRACKED IN ITS UPPER BEND RADIUS AT ITS AFT MOST END, STA 449. THE CRACK RUNS FWD APPROX 1.5 INCH AND HAS BEEN STOP DRILLED WITH A .25 INCH HOLE. THE BEAM WILL BE REPAIRED WITH TWO REPAIR ANGLES, PER DL ERA 273196 Feb 16, 1996 · N769DL · Lkheed 10113853SDR C2XA96IA051Bulkhead · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT REAR SPAR BULKHEAD CRACKED AT STRINGER 10 FRAME 25 TOP AFT HI-LOK COLLER SIDE. MAINTENANCE REMOVED HI-LOK, DRILLED HOLE TO NEXT OVER SIZE. PERFORMED EDDY CURRENT AND FOUND NO CRACK INDICATION AND REINSTALLED HI-LOFeb 16, 1996 · N16824 · Aerosp ATR42300SDR 96ZZZX952Bulkhead · crackedANNUAL INSPECTION REVEALED BOTH LEFT AND RIGHT SIDES OF LOWER FORWARD DOORPOST BULKHEAD (PN 1213407-2) CRACKED AS SHOWN IN CESSNA SEB 93-5R1. ALTHOUGH ACFT IS BELOW THE 4,000-HOUR TOTAL TIME SHOWN IN SERVICE BULLETIN, EXTENSIVE FLOAT OPERATION AND PRIOR DAMAGFeb 15, 1996 · N3870G · Cessna U206BSDR 9605426601Blkhd Web · crackedDURING P-CHECK, FOUND A CRACK IN THE BS 400 BULKHEAD WEB LBL 41 AT THE UPPER INBOARD CORNER OF THE LEFT CUTOUT. REPAIRED THE WEB (P/N 65B07936) PER EA 66-99395.Feb 15, 1996 · N601US · Boeing 747151SDR 9604539152Blkhd Door Jamb · crackedDURING H-CHECK, FOUND TWO CRACKS IN THE AFT CABIN DOOR JAMB SEAL RETAINER RING LEFT AND RIGHT SIDES AT APPROXIMATELY THE 3 AND 9 O'CLOCK POSITIONS. REPAIRED JAMB PER EA 91-109376.Feb 15, 1996 · N8911E · Doug DC914SDR SWAA960083Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178 CRACKED 2 PLACES WL 210 TO 213, RBL 5.7. REPAIRED PER BOEING SRM.Feb 13, 1996 · N318SW · Boeing 7373H4SDR SWAA960082Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178 CRACKED 2 PLACES WL 219, LBL 5 TO 12. REPAIRED PER BOEING SRM.Feb 13, 1996 · N318SW · Boeing 7373H4SDR SWAA960078Blkhd Angle · damagedDURING SCHEDULED D-CHECK, FOUND FUSELAGE BULKHEAD SUPPORT ANGLE CRUSHED AND DENTED AT BS 727, BBL 0. REPAIRED PER BOEING SRM.Feb 13, 1996 · N318SW · Boeing 7373H4SDR SWAA960077Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE BULKHEAD CRACKED AT BS 727 BBL 0. REPAIRED PER BOEING SRM.Feb 13, 1996 · N318SW · Boeing 7373H4SDR DL72K960334Blkhd Stiffener · crackedFOUND ON MV1 1183 BULKHEAD VERTICAL STIFFENER CRACKED 1 INCH AT LOWER END, BL 8L WL 185. REPAIR: REPAIRED PER M/M 55-11-0, PAR 9.Feb 11, 1996 · N472DA · Boeing 727232SDR CAL960181Bulkhead · crackedGSO - INSPECTION FOUND AN 8 INCH CRACK IN PRESSURE BULKHEAD AT PRESSURE FEED THROUGH FOR RADAR WIRING AT STATION 178. THE CRACKED SECTION WAS REMOVED. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-11. (M)Feb 11, 1996 · N14246 · Boeing 737247SDR CAL960180Bulkhead · crackedGSO - INSPECTION FOUND A 7 INCH CRACK IN PRESSURE BULKHEAD ON RIGHT SIDE JUST ABOVE HORIZONTAL STIFFENER AT STATION 178. THE CRACKED AREA WAS REMOVED AND A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-11. (M)Feb 11, 1996 · N14246 · Boeing 737247SDR UPS205599Bulkhead · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED SUSPECTED CRACK AT FASTENER HOLE ON BS 178 BULKHEAD LBL 9, WL 236. REMOVED 2 FASTENERS, CLEANED AREA, NDT INSPECTED FOUND CRACK. TRIMMED OUT AREA THAT WAS CRACKED. NDT VERIFIED CRACK CONTAINMENT FABRICATED REPAIR FFeb 10, 1996 · N931UP · Boeing 72725CSDR USAA960217Blkhd Fitting · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 727 BULKHEAD STIFFENER FITTING AT BL 0 WL 202.5. REMOVED CRACKED FITTING, INSTALLED NEW ONE, REPAIRED PER EO 5394G176. (M)Feb 7, 1996 · N274US · Boeing 7372B7SDR DLL10960276Blkhd Web · crackedWHILE PERFORMING INSPECTIONS PER SI 7-70645-12, THE FS 1212 CANTED BULKHEAD WAS FOUND WITH CRACKS IN THE TYPICAL LOCATION AT LBL 30, LBL 10, RBL 22.5 AND RBL 42.5. THE SUBJECT WEB IS M/F FROM .050 7075-T6 SHEET AND WILL BE REPAIRED PER DL ERA 273246 REV A.Feb 6, 1996 · N730DA · Lkheed 10113851SDR 96ZZZM378Blkhd Stringers · crackedINSPECTED AFT PRESSURE BULKHEAD STRINGER ATTACH FITTINGS (VISUAL INSPECTION ONLY) PER EO L10-53AD-1573C. FOUND TWO STRINGERS CRACKED A/C MAINTENANCE FERRIED TO KIND FOR REPAIRS.Feb 4, 1996 · N191AT · Lkheed 10113851SDR DL72S960300Blkhd Channel · wornAT MID VISIT 2, FOUND VERT SUPPORT CHANNEL WORN AT TOP STA 720D ABOVE STR 26 LT. REMOVED DAMAGED SECTION PER SRM 53-10-9 FIG 9. DRILLED NEW DOUBLER AND INSTALLED PER SRM 53-10-9 FIG 9.Feb 3, 1996 · N518DA · Boeing 727232SDR USAA960198Blkhd Angle · crackedPIT - DURING SIP INSPECTION, FOUND 2 CRACKS, 3 INCHES AND 1.5 INCHES A REPAIR DOUBLER AT THE FORWARD PRESSURE BULKHEAD FS 1550 AFT SIDE OF LOWER CONNECTION ANGLE SIP REF 53-10-06 VISUAL/EDDY CURRENT. REMOVED DOUBLERS, STOP DRILLED CRACKS AND INSTALLED NEW DOUFeb 1, 1996 · N482US · Fokker F28MK4000SDR UPS405460Bulkhead · crackedWHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED BULK CARGO COMP. T-CHORD ON BULKHEAD FOR CARGO FLOOR STRUCTURE IS CORRODED AND CRACKED ON HORIZ. FLANGE AT STA 2160, RBL 2, 23, AND 29. REPLACED UPPER CHORD PER SRM 51-30-02.Feb 1, 1996 · N691UP · Boeing 747121SDR UPS405435Blkhd Web · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK IN BULKHEAD WEB AT BS 2160 RBL 30. REPAIRED AS PER SRM 51-40-02.Feb 1, 1996 · N691UP · Boeing 747121SDR UPS405429Blkhd Web · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK IN BULKHEAD WEB AT BSTA 2160 LBL 35. REPLACED WEB BETWEEN RBL 8 TO LBL 58, ALL TO SRM 51-40-02.Feb 1, 1996 · N691UP · Boeing 747121SDR UPS405418Frame Web · dentedWHILE IN FOR C-CHECK, MAINTENANCE FOUND DENT IN FRAME WEB UNDER UPPER CHORD AT BS 1760 LBL 52, DAMAGE OUT OF LIMITS PER SRM 53-10-01. REMOVED DAMAGED SECTION OF FRAME WEB AND REPAIRED IAW SRM 51-40-02.Feb 1, 1996 · N691UP · Boeing 747121SDR 9603276730Blkhd Fitting · crackedDURING PERIODIC CHECK, FOUND A .5 INCH CRACK IN THE FS 1480 BULKHEAD HORIZONTAL BEAM TIE FITTING LEFT OUTBOARD END, ABOVE STRINGER 36L. REPLACED TIE FITTING PER SRM 51-10-01, PAR 9.Feb 1, 1996 · N630US · Boeing 7472J9FSDR 96ZZZX881Bulkhead · crackedDURING ANNUAL INSPECTION, CRACKS WERE FOUND ON BULKHEAD AT FS 2.5 WHERE JACK STRUT ATTACHES. JACK STRUT FITTINGS WERE ALSO FOUND CORRODED AND WORN. SUSPECT ROUGH OPERATION ON SKIS CAUSED CRACKS.Jan 31, 1996 · N28916 · Luscom 8ASDR DL73S960252Blkhd Web · crackedREF. E.O. 03-069482-12 ME-04 OPN. 0445.1, 2 INCH CRACK AND 1 INCH CRACK IN BS 178 BULKHEAD WEB AT RT BL 5.7 INBOARD OF VERTICAL STIFFENER. .50 INCH CRACK IN 178 BULKHEAD WEB AT RT BL 5.7 OUTBOARD OF VERTICAL STIFFENER. TWO .25 INCH CRACKS AND 1 INCH CRACK INJan 30, 1996 · N304DL · Boeing 737232SDR DL73S960254Blkhd Web · crackedREF. E.O. 03-069482-12 OPN. 445. WEB IS CRACKED AT TWO LOCATIONS JUST INBOARD AND ONE LOCATION JUST OUTBOARD OF THE VERTICAL STIFFENER AT LBL 5.7 BETWEEN WL 207 AND WL 184. WEB IS CRACKED AT TWO LOCATIONS JUST INBOARD OF VERTICAL STIFFENER AT RBL 5.7 BETWEENJan 29, 1996 · N312DL · Boeing 737232SDR DLL10960395Blkhd Angle · crackedTHE 1641601-102 ANGLE INSTALLED AS PART OF THE FS 1363 BULKHEAD MODIFICATION PER DAL EO 7-47702-3AD WAS FOUND CRACKED AT A FASTENER HOLE DURING ROUTINE LAYOVER INSPECTIONS AND OPERATIONS. THE CRACK APPEARS TO HAVE BEEN THE RESULT OF PRELOAD, CAUSED BY A GAP BJan 27, 1996 · N719DA · Lkheed 10113851SDR ABXA9600397Web · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A PREVIOUS REPAIR ON THE AFT PRESSURE BULKHEAD LOWER WEB THAT WAS CORRODED AND HAD DRILL STARTS. REPAIRED AFT PRESSURE BULKHEAD WEB IAW ABX REA D953-14176-MR.Jan 26, 1996 · N936AX · Doug DC931SDR DLL13960193Strap · crackedTHE BULKHEAD SPLICE STRAP AT FS 1363 LBL 42.5 WAS FOUND CRACKED. THE SUBJECT STRAP IS M/F 0.100 7075-T6 CLAD. ACCOMPLISHED REPAIRS PER DL ERA 272789-14AD.Jan 25, 1996 · N790DL · Lkheed 10113851SDR DLL10960195Waterline · elongatedWHILE ACCOMPLISHING THE CENTER WEB SPLICE ON THE FS 1363 BKHD PER SI 7-69959-14AD, OPN 0319, THE POTABLE WATER LINE CUTOUT WAS DAMAGED AND ELONGATED THROUGH THE WEB AND FWD MOD SPLICE STRAP. THE ORIGINAL CUTOUT WAS A 1.25 DIA HOLE. THE ELONGATED CUTOUT HAS AJan 25, 1996 · N714DA · Lkheed 10113851SDR 96ZZZX1837Blkhd Frame · crackedDURING C-CHECK, FORWARD CARGO COMPARTMENT, CRACK IN FRAME ON AFT BULKHEAD AT FLOOR LEVEL. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 22,205 HRS. AIRCRAFT TC: 42,206.Jan 25, 1996 · N818SJ · Doug DC981SDR 9604379155Bulkhead · corrodedDURING H-CHECK, FOUND CORROSION ON THE HORIZONTAL PRESSURE PANEL AT FS 110, RIGHT SIDE BETWEEN THE TWO VERTICAL FITTINGS. REPAIRED PANEL PER EA 91-106633.Jan 25, 1996 · N8914E · Doug DC914SDR AALA960180Bulkhead · corrodedAFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE MAIN CABIN PRESSURE DECK. BLEND-OUTS EXCEEDED SRM MAXIMUM LIMITS. REMOVED CORROSION, ROTO-PEENED. ALODINED, PRIMED, AND PAINTED. APPROVED BY ENGINEERING WITH NOTED CONDITION PER MRB 767-1115Jan 24, 1996 · N313AA · Boeing 767223SDR DLL10960240Web · crackedAT LAYOVER IN ATL WHILE PERFORMING SI 7-70645-12, THE FS 1212 CANTED BULKHEAD WAS FOUND WITH VERTICAL CRACKS AT RBL 22.5 LBL 10 AND LBL 30. THEY MEASURE 9, 8 AND 9 INCHES RESPECTIVELY. ALSO, WHILE ACCOMPLISHING REPAIR, ONE HOLE AT LBL 30 WAS DRILLED WITH SHOJan 23, 1996 · N720DA · Lkheed 10113851SDR DLL10960190Bulkhead · crackedWHILE PERFORMING INSPECTION SI 7-70645-12, THE FS 1212 CANTED BULKHEAD WAS FOUND WITH A 12 INCH LONG VERTICAL CRACK AT RBL 22.5. THE SUBJECT WEB IS M/F .050 7075 T6 CLAD SHEET. ACCOMPLISHED REPAIRS PER DL ERA 273152-14.Jan 23, 1996 · N712DA · Lkheed 10113851SDR DLL10960168Bulkhead · crackedWHILE PERFORMING THE SI 7-70645-12 FS 1212 CANTED BULKHEAD INSPECTION, CRACKS WERE FOUND AT FOUR LOCATIONS. REPAIRED PER DL ERA 273100 RA.Jan 22, 1996 · N713DA · Lkheed 10113851SDR DLL10960148Canted Blkhd · crackedWHILE PERFORMING INSPECTIONS PER SI 7-70645-12, THE FS 1212 CANTED BULKHEAD WAS FOUND WITH CRAL\CKS IN THE TYPICAL MANNER AT LBL 10, RBL 22.5, RBL 22.5 AND RBL 42.5. THE CRACKS WERE CUT OUT AND REPAIR DOUBLERS WERE INSTALLED PER DL ERA 273149.Jan 22, 1996 · N715DA · Lkheed 10113851SDR AU960085Bulkhead · cracked(AUS) LH LOWER FORWARD DOORPOST BULKHEAD CRACKED FROM BEND RELIEF NOTCH- FOUND DURING INSPECTION IAW AD/C180/74 AMDT1 AND CESSNA SEB95-19Jan 22, 1996 · Cessna 182PSDR USAA970024Bulkhead · crackedPIT - DURING Q-1 CHECK, FOUND TWO .5 INCH CRACK (LT SIDE) OF CENTER FUEL TANK PRESSURE BULKHEAD AT FRAME 14911 AND STATION 11. STOP DRILLED AND CUT OUT CRACKED AREA. INSTALLED FILLER AND NEW ANGLES PER EA NR 34272. (M)Jan 20, 1996 · N863US · Fokker F28MK0100SDR USAA970023Bulkhead · crackedPIT - DURING Q-1 CHECK, FOUND 3 INCH CRACK (RT SIDE) OF CENTER FUEL TANK PRESSURE BULKHEAD AT FRAME 14911 AND STATION 64. STOP DRILLED AND CUT OUT CRACKED AREA. INSTALLED FILLER AND NEW ANGLES PER EA NR 34272. (M)Jan 20, 1996 · N863US · Fokker F28MK0100SDR MWEA96022Tee · corrodedDURING INSPECTION, FOUND AFT CARGO COMPARTMENT AFT BULKHEAD STA 996 LOWER CENTER SUPPORT TEE ANGLE CORRODED TO EXCESS AT CENTER NUTPLATE LOCATIONS. REMOVED CORROSION AND INSTALLED DOUBLER ANGLE REPAIR IAW SRM 53-01 FIG 2. ACFT RETURNED A/C TO SERVICE.Jan 20, 1996 · N502ME · Doug DC932SDR MWEA96021Web · corrodedDURING INSPECTION, FOUND WEB AT STA 996 AFT PRESSURE BULKHEAD HAD MODERATE CORROSION FROM LONGERON 28L TO 28R AT 6 O'CLOCK POSITION. INSTALLED REPAIR IAW SRM 53-01 FIG 2 AND RETURNED A/C TO SERVICE.Jan 20, 1996 · N502ME · Doug DC932SDR USAA960058Bulkhead · chaffedPIT - DURING Q-6 INSPECTION, FOUND TWO CHAFFED 4 INCH RADIUS AREAS FROM RIGHT ENGINE THRUST REVERSER CABLE DRUM SHAFT BOLT HEADS IN STATION 1338 AFT PRESSURE BULKHEAD AFT SIDE. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 78-30-14. (M)Jan 19, 1996 · N820US · Doug DC982SDR USAA960057Bulkhead · chaffedPIT - DURING Q-6 INSPECTION, FOUND TWO CHAFFED 4 INCH RADIUS AREAS FROM LEFT ENGINE THRUST REVERSER CABLE DRUM SHAFT BOLT HEADS IN STATION 1338 AFT PRESSURE BULKHEAD AFT SIDE. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 78-30-14. (M)Jan 19, 1996 · N820US · Doug DC982SDR USAA960092Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1875 INCH CRACK STATION 178 BULKHEAD SKIN RBL 4.75 WL 201. INSTALLED DOUBLER, REPAIRED PER EA 40743. (M)Jan 17, 1996 · N423US · Boeing 737401SDR USAA960090Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 178 BULKHEAD SKIN LBL 4.75, WL 201. INSTALLED DOUBLER, REPAIRED PER EA 40743. (M)Jan 17, 1996 · N423US · Boeing 737401SDR USAA960089Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 178 BULKHEAD SKIN LBL 4.75, WL 198. INSTALLED DOUBLER, REPAIRED PER EA 40743. (M)Jan 17, 1996 · N423US · Boeing 737401
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