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 AWXA0001972Web · crackedD: HFEC confirms 2ea cracks in Sta 178 bulkhead skin 1 at RBL 1 and 1 at LBL 1 WL 187. Cracks are apprx .750 in length vertical 12 oclock to 6 oclock positionC:Cut dammaged area, HFEC no cracks noted Cal #0714. Frabricated repair doubler 2024 T#. 040 PO # x950May 10, 2001 · N327AW · Boeing 7373Q8SDR 20010529CW005Bulkhead · crackedCRACKED AT 2:00 POSITION IN RADIUS OF BEND. CRACK LENGTH 2 INCHES.May 9, 2001 · N193TW · Bell 206L4SDR AWXA0001720Bulkhead · crackedBS 178 BLKHD WEB AT LBL 10.3-10.6 WL 218 CRACKED BENEATH ANGLE. CUT OUT DAMAGE TO WEB AND INSTALLED A REPAIR DOUBLER AND FILLER IAW SRM 53-10-08 PG 287-298.May 9, 2001 · N158AW · Boeing 7373G7SDR AWXA0001974Stiffener · corrodedD: Lower aft pressure bulkhead 6 oclock position radial stiffener corroded @ BL 0C: Removed damaged section of radial stiffener. Frabricated -7-8-10 +-11 repair parts and installed repair parts per DWG 65C 28106 + SRM 51-40-02May 8, 2001 · N327AW · Boeing 7373Q8SDR AWXA0001973Bulkhead · corrodedAFT PRESSURE BULKHEAD LOWER 6 O`CLOCK POSITION CORROSION ON BULKHEAD WEB RBL 3 TO LBL 3. REPAIRED PER ER 03-5383-01141-DD2 & ER 03-5383-01141-DD4.May 8, 2001 · N327AW · Boeing 7373Q8SDR UPS01435834Pressure Panel · corrodedINSPECTION TYPE:N/A 2 INCH HOLE CORRODED IN APU PRESS PAN CUTOUT. *S/D* TRANSFERRED TO UPS NRC 352493.May 8, 2001 · N524UP · Boeing 747*SDR USAA010520Pressure Panel · damagedCLT - FOUND UNBEADED PRESSURE WEB APPROX 3 SQUARE FEET, BS 666 WL 55. REINFORCING ANGLES INSTALLED PER SB 737-57-1234 AND EA 69561. (M)May 8, 2001 · N247US · Boeing 737201SDR UPS01435940Pressure Panel · crackedINSPECTION TYPE:C-2 NOSE W/W TUNNEL RT BS 300 VERTICAL BEAM WEB BETWEEN 1ST & 2ND CLIP (COUNT FROM TOP) FOUND LOWER STANDOFF HOLE CRACKED APPROX .25 INCH & .375 INCH LONG. CRACKED WEB REPLACED PER SRM 51-10-01.May 8, 2001 · N671UP · Boeing 747123SDR UPS01435937Pressure Panel · crackedINSPECTION TYPE:C-2 NOSE W/W TUNNEL - LT BS 320 VERTICAL BEAM WEB BTN 4TH & 5TH CLIP (COUNT FROM TOP) FOUND CRACK AT STAND OFF HOLE APPROX .125 INCH LONG. BS 320 LT WEB REPLACED PER SRM 51-10-01 & 51-30-02.May 8, 2001 · N671UP · Boeing 747123SDR UPS01435936Pressure Panel · crackedINSPECTION TYPE:C-2 NOSE W/W TUNNEL - RT BS 320 VERTICAL BEAM WEB BTN 4TH & 5TH CLIP FOUND CRACK AT STANDOFF HOLW APPROX .125 & .0625 INCH LONG. CRACKED WEB REPLACED PER SRM 51-10-01 & 51-30-02.May 8, 2001 · N671UP · Boeing 747123SDR UPS01435935Pressure Panel · crackedINSPECTION TYPE:C-2 NOSE W/W TUNNEL - LT BS 300 VERTICAL BEAM WEB BETWEEN 1ST & 2ND CLIP (COUNT FROM TOP) FOUND CRACK AT LOWER STAND OFF HLE APPROX .375 & .25 INCH LONG. LT BS 300 VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 & 51-30-02.May 8, 2001 · N671UP · Boeing 747123SDR CA010508014Former · cracked(CAN) THE INSPECTION REQUIRED BY CF-98-38 BULKHEAD CRACKS STA. 288 WAS CARRIED OUT ON THE AIRCRAFT. THE BULKHEAD AND THE CHANNEL ASSEMBLY WERE FOUND TO BE CRACKED. P/N C2FS533 FORMER WAS REPLACED WITH A NEW PART. P/N C2FS4045A CHANNEL ASSEMBLY WAS REPLACED WITMay 8, 2001 · Dhav DHC2*SDR SWAA011374Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT FOUND WEB CRACKED AT BS 178, LBL 27, WL 207. REPAIRED WEB PER SRM.May 8, 2001 · N342SW · Boeing 7373H4SDR AWXA0001715Bulkhead · crackedULTRASONIC CRACK INDICATION BS 178 BLKHD WEB, 1.1 INCH LENGTH, RBL 9.3-10.4 BENEATH ANGLE. REMOVED STRAPS, BRACKETS, ANGLES AND CHANNEL; CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER AND FILLER; REINSTALLED STRAPS, BRACKETS, ANGLMay 8, 2001 · N158AW · Boeing 7373G7SDR AWXA0001713Bulkhead · crackedBLKHD 178 WEB HAS 2 CRACKS .5 INCH AT LBL .5 AND RBL .5 WL 189. REMOVED LOCALIZER ANTENNA MOUNT BOX; CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER AND FILLER; REINSTALLED LOCALIZER ANTENNA MOUNT BOX IAW SRM 53-10-08 PG 287-298.May 8, 2001 · N158AW · Boeing 7373G7SDR AWXA0001711Bulkhead · crackedTWO CRACKS AT HI-LOKS BS 178 WEB FWD SIDE WL 234.1 RBL 11-12. REMOVED FASTENERS; CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER AND FILLER; REINSTALLED BRACKETS AND STIFFENER AND L-ANGLE IAW SRM 53-10-08 PG 287-298.May 8, 2001 · N158AW · Boeing 7373G7SDR AWXA0001710Bulkhead · crackedTWO CRACKS AT HI-LOKS BS 178 WEB FWD SIDE WL 234.1 LBL 11-12. REMOVED FASTENERS; CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER AND FILLER; REINSTALLED BRACKETS AND STIFFENER AND L-ANGLE IAW SRM 53-10-08 PG 287-298.May 8, 2001 · N158AW · Boeing 7373G7SDR AWXA0001709Bulkhead · crackedA .5 INCH CRACK EMANATING FROM BENEATH STRAP BS 178 BLKHD FWD SIDE RBL 4.7 FROM WL 200.2-200.7. REMOVED BRACKETS, STIFFENER AND L-ANGLE; CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER AND FILLER; REINSTALLED BRACKETS AND STIFFENERMay 8, 2001 · N158AW · Boeing 7373G7SDR AWXA0001708Bulkhead · crackedULTRASONIC INSPECTION OF BS 178 BLKHD WEB FOUND CRACK .4 INCH LENGTH LBL 6.7 WL 212-212.4 BENEATH STRAP. REMOVED BRACKETS AND STIFFENER; CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER AND FILLER; REINSTALLED BRACKETS AND STIFFENERMay 8, 2001 · N158AW · Boeing 7373G7SDR AWXA0001707Bulkhead · crackedVISUAL INSPECTION OF BS 178 BLKHD WEB FWD SIDE REVEALED CRACK EMANATING FROM BENEATH STRAP AT WL 198.5-198.8 LBL 4.7. CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-08 PG 287-298.May 8, 2001 · N158AW · Boeing 7373G7SDR AWXA0001706Bulkhead · crackedHFEC INDICATES .7 INCH CRACK EMANATING FROM BENEATH STRAP BS 178 FWD SIDE WL 201.8-202.1 LBL 4.7. CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-08 PG 287-298.May 8, 2001 · N158AW · Boeing 7373G7SDR AWXA0001705Bulkhead · crackedHFEC INDICATES .25 INCH CRACK RUNNING HORIZ IN WEB BS 178 WL 207 RBL 11.6-11.75. CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-08 PG 287-298.May 8, 2001 · N158AW · Boeing 7373G7SDR AWXA0001704Bulkhead · crackedHFEC INDICATES .2 INCH CRACK EMANATING FROM BENEATH STRAP BS 178 BLKHD FORWARD SIDE WL 198.6-198.8 RBL 4.7. CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-08 PG 287-298.May 8, 2001 · N158AW · Boeing 7373G7SDR AWXA0001703Bulkhead · crackedBS 178 WEB CRACKED .4 INCH WL 198.2-198.6 RBL 6.7 BENEATH STRAP. CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-08 PG 287-298.May 8, 2001 · N158AW · Boeing 7373G7SDR AWXA0001702Bulkhead · crackedBS 178 WEB CRACKED .5 INCH WL 206 RBL 1-1.5. CUT OUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-10-08 PG 287-298.May 8, 2001 · N158AW · Boeing 7373G7SDR AWXA0001701Bulkhead · crackedUPON REMOVAL OF STRAP FOUND .2 INCH CRACK BS 178 WL 210 LBL 4.7. CUTOUT DAMAGED WEB; LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-10-08 PG 287-298.May 8, 2001 · N158AW · Boeing 7373G7SDR USAA010513Bulkhead · brokenCLT - FOUND PRESSURE BULKHEAD WEB WITH BROKEN AREA .5 INCH BY .5 INCH, BS 178 WL 183 AT RBL 17. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER. (M)May 7, 2001 · N423US · Boeing 737401SDR USAA010511Bulkhead · crackedCLT - FOUND PRESSURE BULKHEAD WEB WITH THREE CRACKS, .125 INCH, .250 INCH AND .85 INCH, BS 178 WL 188 AND WL 234 RBL .5 TO LBL 12. DAMAGE CUTOUT, INSTALLED FILLERS AND REPAIR DOUBLER PER SRM 53-10-08 FIG 209, EO 5300V153 AND EA 69580. (M)May 7, 2001 · N423US · Boeing 737401SDR USAA010508Bulkhead · crackedCLT - FOUND BS 178 PRESSURE BULKHEAD WEB WITH CRACKS .125 INCH, .5 INCH, .8 INCH, 1 INCH AND 1.1 INCH, BS 178, FROM WL 188 TO WL 212.5, RBL 6.6 TO LBL 5. DAMAGE REMOVED, FILLERS AND REPAIR DOUBLER INSTALLED PER SRM 53-10-01, 53-10-08 AND EO 5300V153. (M)May 7, 2001 · N426US · Boeing 7374B7SDR AWXA0001694Bulkhead · crackedULTRASONIC INSP REVEALS CRACK VERT POSITION AT I/B EDGE LBL 5.7 AT WL 234 BS 178 LOCATION .75 INCH LENGTH. REPAIRED IAW SRM 53-10-11 FIG 1 DETAIL III AND SRM 51-30-2 PG 5 AND REF DWG 65-16300.May 7, 2001 · N186AW · Boeing 737277SDR 2001UALA00690Bulkhead · crackedFWD PRESSURE BULKHEAD SKIN CRACKED. STA 178, WL 214.5, LBL 5.7 TO RBL 5.7. INSTALLED DOUBLER REPAIR.May 7, 2001 · N315UA · Boeing 737322SDR 2001UALA00689Bulkhead · crackedWEB CRACKED AT UPPER RT RADAR MOUNT OUTBOARD LWR SIDE STA 178. INSTALLED DOUBLER.May 7, 2001 · N314UA · Boeing 737322SDR SWAA011373Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234, LBL 7.0. REPAIRED WEB PER SRM.May 7, 2001 · N661SW · Boeing 737317SDR 2001UALA00691Bulkhead · crackedBULKHEAD WEB CRACKED AT LOWER RT RADAR MOUNT. STA 178, WL200, RBL 5. REPAIR DOUBLER INSTALLED.May 6, 2001 · N974UA · Boeing 737291SDR GAIA01177STTee Chord · crackedDURING A LTC INSPECTION IT WAS DISCOVERED THAT THE STATION 950 BULKHEAD UPPER ATTACH ANGLE IN LEFT WHEEL WELL (LBL 50) IS CRACKED. ACCOMPLISHED 950 BULKHEAD T-CHORD REPAIR LBL 50 IAW SRM 51-40-4 FIG 1. (M)May 5, 2001 · N6809 · Boeing 727223SDR GAIA01174STPressure Panel · crackedDURING A LTC INSPECTION, A CRACK WAS DISCOVERED IN THE NOSE WHEEL WELL UPPER PRESSURE WEB AT BL 0 AT BS 277. ACCOMPLISHED NOSE WHEEL WELL UPPER PRESSURE WEB REPAIR BS 277 BL 0 IAW SRM 51-40-2 FIG 1. (M)May 5, 2001 · N6809 · Boeing 727223SDR GAIA01170STPressure Panel · crackedDURING A LTC INSPECTION, A CRACK WAS DISCOVERED IN THE NOSE WHEEL WELL LEFT WEB JUST BELOW FORWARD PRESS PANEL STATION 277. ACCOMPLISHED NOSE WHEEL WELL PRESSURE WEB REPAIR BS 277 LEFT IAW B727 SRM 53-10-2 FIG 2 AND SRM 51-30-2. (M)May 5, 2001 · N6809 · Boeing 727223SDR GAIA01134STPressure Panel · crackedDURING A LTC INSPECTION, A CRACK WAS DISCOVERED AT FASTENER ON THE NOSE WHEEL WELL LEFT SIDEWALL BS 240, BELOW PANEL CUTOUT. ACCOMPLISHED NOSE WHEEL WELL LEFT SIDE PRESSURE WEB REPAIR BS 240 IAW B727 SRM 51-40-2 FIG 1. (M)May 5, 2001 · N6809 · Boeing 727223SDR GAIA01133STPressure Panel · crackedDURING MAINTENANCE, A CRACK WAS DISCOVERED IN THE NOSE WHEEL WELL UPPER PRESSURE WEB AT BS 243. ACCOMPLISHED NOSE WHEEL WELL UPPER PRESSURE WEB REPAIR BS 243 RBL 15 IAW B727 SRM 51-40-2 FIG 1. (M)May 5, 2001 · N6809 · Boeing 727223SDR GAIA01132STPressure Panel · crackedDURING MAINTENANCE IT WAS DISCOVERED THAT THE INNER WEB IS CRACKED IN THE NOSE WHEEL WELL LEFT SIDE AT BS 277, WL 160 INSIDE THE LIGHTENING HOLE. ACCOMPLISHED INNER WEB REPAIR BS 277 LEFT WL 160 IAW B727 SRM 53-10-2 FIG 1 SRM 51-30-2. (M)May 5, 2001 · N6809 · Boeing 727223SDR GAIA01130STBulkhead · crackedDURING MAINTENANCE, A CRACK WAS DISCOVERED AT BS 178 WL 218 RBL 6-20 AT STIFFENER 1R. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR BS 178 WL 218 RBL 6-20 IAW KITTY HAWK WORK CARD 2210 FIG 2 REV DATED JUNE 15, 1994. (M)May 5, 2001 · N6809 · Boeing 727223SDR GAIA01129STBulkhead · crackedDURING MAINTENANCE A .375 INCH CRACK PROTRUDING OUT OF VERTICAL STIFFENER IN BULKHEAD WEB WAS DISCOVERED AT BS 178 WL 198 RBL 01. ACCOMPLISHED BS 178 BULKHEAD REPAIR, BS 178 WL 198 RBL 01 IAW B727 SRM 53-10-9 FIG 4. (M)May 5, 2001 · N6809 · Boeing 727223SDR GAIA010128STBulkhead · crackedDURING MAINTENANCE, 3 CRACKS WERE DISCOVERED PROTRUDING OUT OF FASTENER HOLES AT BULKHEAD BS 178 WL 238 RBL 08-16. ACCOMPLISHED BS 178 BULKHEAD REPAIR BS 178 WL 238 RBL 08-1 6 IAW B727 SRM 53-10-9 FIG 4. (M)May 5, 2001 · N6809 · Boeing 727223SDR GAIA01127STBulkhead · crackedDURING MAINTENANCE, TWO CRACKS WERE DISCOVERED PROTRUDING OUT OF FASTENERS HOLES AT BULKHEAD BS 178 WL 238 LBL 12-14. ACCOMPLISHED BS 178 BULKHEAD REPAIR BS 178 WL 238 LBL 12-14 IAW B727 SRM 53-10-9 FIG 4. (M)May 5, 2001 · N6809 · Boeing 727223SDR UPS01836003Pressure Panel · corrodedINSPECTION TYPE:C1,3 RIGHT NOSE TUNNEL UPPER PRESSURE WEB IS CORRODED BEYOND LIMITS AT STA -80 TO -99 AT RBL 36. REPAIRED WEB IAW SRM 53-2-0 FIG 1D.May 4, 2001 · N880UP · Doug DC873FSDR UPS01835990Pressure Panel · corrodedINSPECTION TYPE:C2,3 STA 4 RBL 58 PRESSURE WEB IS CORRODED BEYOND LIMITS. REPAIRED WEB IAW SRO 8530026.May 2, 2001 · N880UP · Doug DC873FSDR 2001UALA00626Bulkhead · crackedSTA 178 BULKHEAD LBL 5.7, WL 214, UPPER LT ANT MOUNT O/B SIDE IS CRACKED. ACCOMPLISHED DOUBLER REPAIR.May 2, 2001 · N313UA · Boeing 737322SDR AALA20011026Pressure Panel · crackedTUL - FOUND TWO CRACKS ON UPPER PRESS DECK AT STATION 290 IN NLG W/W. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 53-10-9. (M)May 1, 2001 · N718AA · Boeing 727227SDR TSAA0153061Pressure Panel · crackedFOUND CRACK NOTED AT LEFT UPPER CORNER NLG PRESSURE PANEL. CONFIRMED CRACK BY UTILIZING HFEC METHOD. (M)May 1, 2001 · N817AL · Boeing 7372X6CSDR 2001UALA00614Bulkhead · crackedBS 178 BULKHEAD 2 EA CRACKS ON INBD SIDE OF LWR WX RADAR ANTENNA MOUNT. ACCOMPLISHED DOUBLER REPAIRS.May 1, 2001 · N974UA · Boeing 737291
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