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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DL72S981607Bulkhead Web · crackedSTA 1303 INSIDE OF VERT RT SIDE CTR OF BULKHEAD WEB CRACKED AT CUTOUT FOR STR. REMOVED SECTION OF ANTI-ICE DUCT FOR ACCESS, REMOVED HORT SUPPORT BRACE FOR ACCESS, REMOVED EXISTING FASTENER AND DOUBLER. STOP DRILLED CRACK, FAB AND DRILLED REPAIR DOUBLER PER SSDR DL72S981577Bulkhead Angle · corrodedFWD B/B STA 740 BLKH LWR ANGLE/CORRODED LOC BETWEEN STA 27R AND 28R. NOTE, FOUND DURING OK TO INST STG 27R REPAIR N/R 1349. BEGAN REMOVING ANGLE, CONT REMOVING ANGLE. REMOVED ANGLE BEGAN INSTALLATION OF NEW ANGLE. DRILLED UP NEW ANGLE. DRILLED UP ANGLE DOSDR TWAA9812120Bulkhead · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION AT BOTTOM OF AFT PRESSURE BULKHEAD, 6 IN LBL TO 6 IN RBL. REMOVED CORROSION BY CUTTING OUT CORRODED SECTION PER SRM 53-03, FIG 9 PAGE 12B. INSTALLED DOUBLER PER SRM 53-03, FIG 9.SDR SWAA981454Bulkhead Panel · crackedDURING SCHEDULED 1/2 D-CHECK, FOUND BULKHEAD PANEL AT BS 380 RT SIDE GOUGED AND CRACKED. REPAIRED PER BOEING SRM.SDR SWAA981424Bulkhead · damagedDURING SCHEDULED 1/2D CHECK, FOUND FWD LAV FWD BULKHEAD COMPOSITE DAMAGED SEVERAL AREAS. REPAIRED PER BOEING SRM.SDR TWAA9812005Bulkhead Web · crackedDURING OP 16 MAINT CHECK, FOUND BULKHEAD 965 RBL 58, APPROX 28 IN ABOVE FLOOR LINE WITH CRACK IN WEB. STOP DRILLED AND INSTALLED DOUBLER. INSTALLED NEW WEB PER MO 72J15, PHASE K, PER DRAWING 4709532 REV A, AND 5936993 REV D.SDR TWAA9812004Bulkhead Doubler · corrodedDURING OP 16 MAINT CHECK, FOUND SPAR WEB DOUBLER ON AFT SIDE OF BULKHEAR WEB, STA 965 RT SIDE, CRACKED. REPAIRED WITH .090 DOUBLER 2024-T3 AND INSTALLED PER MO 72J15, PHASE K AND DAC DRAWING 4709532 AND 5936993.SDR ABXA9800642Bulkhead Bracket · crackedWHILE COMPLYING WITH 'C' INSPECTION, FOUND THE AFT FACE OF THE AFT PRESSURE BULKHEAD HAD A CRACKED BRACKET AT LOWER LEFT CORNER OF DOOR JAMB. REPLACED BRACKET IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.SDR 98ZZZX3409Bulkhead · crackedBULKHEAD WAS CRACKED AT THE LT UPPER CORNER AT THE T/R GEARBOX ATTACHMENT POINT THROUGH THE UPPER ADJACENT RIVET HOLE AND BACK THROUGH THE BULKHEAD RADIUS RE-CONNECTING WITH ANOTHER CRACK PROGRESSING FROM THE ATTACHMENT POINT HOLE FORWARD TOWARD THE TOP RADIUSSDR IXXA9800100Bulkhead Doubler · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED IN THE LOWER RADOME COMPARTMENT BULKHEAD INNER DOUBLER AT FUSELAGE STATION 44. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW DOUBLER AND TWO REPAIR SPLICE DOUBLERS INSDR ARWA9807124Bulkhead Bracket · crackedBOTH ATTACH BRACKETS HOLDING PRESS. SEALS TRUMPETS ARE CRACKED AT AFT PRESSURE BULKHEAD AREA. FABRICATED REPAIR AND INSTALLED IN ACCORDANCE WITH JOSSAIR, CO EO NR18R539001. WORK ACCOMPLISHED UNDER ARROW AR FORM JW3B, WORK ORDER 980802, CONTROL NR 5009.SDR TWAA9811506Bulkhead · crackedDURING OP 16 MAINTENANCE CHECK AT STA 965, THE BULKHEAD WEB HAD 2 EACH CRACKS APPROX 2 INCHES LONG AT WL 200, JUST INBD OF LONGERON 18R. REPLACED FULL BULKHEAD WEB WITH SAME AS ORIGINAL .032 INCH 7075T6 ALUMINUM MATERIAL. ATTACHED WITH MS L0470AD RIVETS AND SDR SWAA981405Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND CRACKED BS 178 LT BULKHEAD CHORD ANGLE WL 207. REMOVED AND REPLACED PER BOEING SRM.SDR BIER9804052Rib · crackedFOUND RIB CRACKED AS REFERENCED IN CESSNA SL ME76-2. INSTALLED KIT SK414-8E.SDR TWAA9812104Bulkhead Fitting · damagedDURING CHECK-C MAINT, FOUND THE AFT BULKHEAD T-FITTING DAMAGED. CRACK WAS 2.5 BY 1.7 AT AREA OF AFT JACK POINT. REMOVED AND REPLACED T AS PER SRM 53-03, FIG 37A.SDR SWAA981373Bulkhead · damagedDURING SCHEDULED C4 CHECK, FOUND RT BULKHEAD (CENTER) TORN UNDER MAGAZINE POUCH. REPAIRED PER BOEING MM.SDR P2EA98136Bulkhead · crackedSJO - FUSELAGE BULKHEAD WEB CRACKED AT BS 294.5, LBL 16 INCHES, WL 165 (E/E COMPT). REPAIRED WEB AT BS 294.5, LBL 13 TO LBL 18, BETWEEN WL 170 AND WL 160 PER BOEING FAX COO-SJO-98-0491RR DATED JULY 21, 1998. DOCUMENTED ON FAA FORM 8110-3. (M)SDR ABXA9800641Bulkhead Web · corrodedWHILE COMPLYING WITH C INSPECTION, FOUND THE AFT PRESSURE BULKHEAD WEB CORRODED BETWEEN LONGERON 26L TO 30L. REPAIRED IAW ABX REA D953-24142MR.SDR TWAA9811908Bulkhead Clip · crackedDURING OP 16 MAINTENANCE CHECK, FOUND 2 INCH CRACK ON STA 1143 CANTED BULKHEAD WEB CLIP, RT SIDE A RUDDER TRIM CABLE CUT-OUT. REPLACED CRACKED ANGLE PER SRM 51-01, PG 1 ITEM C. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X)SDR ABXA9800624Bulkhead Former · crackedDURING C-CHECK, FOUND CRACK AFT PRESSURE DOME END FORMER AT LONGERON 12 LT. REPAIRED IAW DC9 SERVICE DRAWING J060110 AND 51-30-5.SDR P2EA98133Bulkhead · crackedC-CHECK ITEM. BS 727 BULKHEAD SKIN CRACKED RBL 32, WL 200.5. DEFECT SIZE - 1.375 INCH. REPAIRED FUSELAGE BULKHEAD WEB AT BS 727, WL 194.25 AND WL 202 BETWEEN RBL 26.5 AND RBL 39.25 PER BOEING FAX COO-SJO-98-0486RR DATED 7-16-98. DOCUMENTED ON FAA FORM 8110SDR COMA9860180Bulkhead Angle · crackedDURING C-CHECK, FOUND PRESSURE BULKHEAD ANGLE BRACKET CRACKED. REPLACED ANGLE BRACKET.SDR AU981095Bulkhead · cracked(AUS) FORWARD FUSELAGE BULKHEAD FORWARD FACE CONTAINED SIX WEB CRACKS. FOUND DURING ULTRASONIC INSPECTION.SDR IXXA9800095Bulkhead Fitting · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON AFT PRESSURE BULKHEAD LOWER SUPPORT FITTING AT FUSELAGE STATION 1744, LONGERON 36. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION A NEW FITTING IN ACCORDANCE WITH DOUGLASSDR AU981094Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THE FOLLOWING AREAS: SIDE CHORDS AT WL 207 LT AND WL 207 RT (2 CRACKS). VERTICAL CHORD AT LBL 5.7 AFT FACE 3. INTERCOSTALS AT WL 197 LT AND WL 195 RT (2 CRACKS). FOUND DURING EDDY CURRENT INSPECTION.SDR ABXA9800646Bulkhead Jamb · crackedWHILE COMPLYING WITH C INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB UPPER RIGHT CORNER CRACKED. REPAIRED IAW ABX REA D953-24119.SDR SWAA981327Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND CRACKED BS 178 BULKHEAD LBL 5.7, WL 200 TO 201. REPAIRED PER BOEING SRM.SDR SWAA981317Bulkhead Angle · corrodedDURING SCHEDULED D-CHECK, FOUND FLOOR TO BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, LBL 21, RBL 21 WL 180. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA981312Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND CRACKED BS 178 BULKHEAD, LBL 10 TO 11, WL 215 AND RBL 8.75 TO 9.5 WL 215. REPAIRED PER BOEING SRM.SDR SWAA981311Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND CRAKCED AT BS 178 BULKHEAD, LBL 5.7, WL 198 TO 202, RBL 5.7, WL 198 TO 202 AND LBL 5.7, WL 212 TO 213. REPAIRED PER BOEING SRM.SDR SWAA981305Bulkhead · crackedDURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED FWD SIDE OF BULKHD, RBL 5 WL 201 AND WL 201 LBL 5. REPAIRED PER BOEING SRM.SDR UPS98227240Bulkhead Fitting · crackedINSPECTION TYPE-C, (CHORD ANGLE) BULKHEAD FITTING BS 740 LT HAS CRACKS. LT BULKHEAD FITTING REPLACED IAW EO B727-5310-7477.SDR UPS98227239Bulkhead Fitting · crackedINSPECTION TYPE-C, BULKHEAD FITTING BS 740 RT HAS CRACKS. RT BULKHEAD FITTING REPLACED IAW EO B727-5310-7477.SDR RAAA98B2030Bulkhead Chord · damagedDURING SCHEDULED B3 CHECK PER CARD B146001, FOUND BS 950 BULKHEAD UPPER CHORD TOOL DAMAGED AT RBL 42. REPAIRED PER SRM 51-40-3, M-54 NR 208.SDR DL73S981396Bulkhead Web · cracked8 CRACKS FOUND IN THE BS 178 BULKHEAD WEB. REPAIRED PER ERA 331867-14.SDR 98ZZZX3410Bulkhead · mismanufacturedBULKHEAD WOULD NOT FIT, OUTSIDE DIMENSION ON THE TWO UPPER OUTSIDE EDGES IS LARGER THAN THE ORIGINAL PART CAUSING MISALIGNMENT OF THE UPPER PLATE. INSTALLED NEW PART.SDR ABXA9800606Bulkhead Tee Cap · crackedAFT PRESS BULKHEAD TEE CAP CRACKED AT LONGERON 10R. REPAIRED IAW DC8 SRM 53-2-5, 51-1-20D AND 51-3-0.SDR ABXA9800604Bulkhead Web · crackedRADOME BULKHEAD, RIGHT WEB HAS TWO 15 INCH CRACKS, 6 ABOVE AND BELOW FRP. REPAIRED IAW ABX REA D853-23417 MR.SDR AU980759Bulkhead · cracked(AUS) BULKHEAD LOCATED AT FS 257.6 CRACKED. PART TOTAL CYCLES: 4,996.SDR QXEA9800966Bulkhead Web · crackedPDX - AT FRONT PRESSURE BULKHEAD WEB AND UPPER AREA ALONG HORIZONTAL BEAM VIII BETWEEN OUTBOARD RIVETS 8-9 UPPER ROW AND 9-10 LOWER ROW. THERE IS A 10 MM CRACK. REPAIRED IAW FOKKER SRM 53-07-18, PAGE 35, FIGURE 13, 51-31-01 AND 51-31-05.SDR SWAA981170Bulkhead · crackedDURING SCHEDULED RON CHECK, FOUND CRACKED NLG WHEEL WELL CEILING PRESSURE BULKHEAD LOCATED AT FWD RT ACCESS PANEL AT AFT I/B CORNER. REPAIRED PER BOEING TI-A53-001.SDR GAIA9863Bulkhead Web · crackedDURING ROUTINE C-CHECK, A CRACK WAS FOUND ALONG THE AFT PRESSURE BULKHEAD WEB APPROXIMATELY 1.2 INCHES LONG JUST ABOVE WL 263 AND LBL 26.83, BS 1183. THE CRACK WAS STOP DRILLED USING A 0.187 INCH HOLE. THE CRACK WAS THEN NDT TO ENSURE CRACK LIMITATION. REPASDR SWAA981204Bulkhead · crackedDURING SCHEDULED TRAN CHECK, FOUND CRACKED INDICATION NOTED DURING UT, BS 178 BULKHEAD, WL 198.3 TO 202.5, RBL 4.7 AND BS 178, WL 198.0 TO WL 202.5, LBL 4.7. REPAIRED PER BOEING SRM.SDR ABXA9800553Beam · crackedAFT PRESSURE BULKHEAD AFT SIDE, HORIZONTAL BEAM HAS 3.5 CRACK ON LOWER FLANGE AND 1 CRACK ON UPPER FLANGE AT AIRCRAFT CENTERLINE, 24 ABOVE FRP. REPAIRED PER ABX REA D853-23406MR.SDR ABXA9800552Flange · crackedAFT PRESSURE BULKHEAD AFT SIDE HORIZONTAL BEAM HAS 3 CRACK ON LOWER FLANGE AT AIRCRAFT CENTERLINE. REPAIRED IAW ABX REA D853-23407MR.SDR P2EA98117Bulkhead Beam · crackedSJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD NR J2C-51-2525, A CRACK WAS NOTED ON THE FORWARD CARGO COMPT, AFT PRESSURE BULKHEAD, VERTICAL BEAM, RBL 15, WL 167.5 (FRONT SPAR, WING CENTER SECTION). REPLACED BEAM AS PER SRM 51-10-1, PAGE 5. (M)SDR COMA9860163Blkhd Brackets · crackedAT 48 MONTH INSPECTION TASK 002-53-310-501, ATTACH BRACKETS AT PRESSURE BULKHEAD 621 LEFT AND RIGHT ARE CRACKED. REPLACED BRACKETS.SDR TWAA9810315Bulkhd Fitting · crackedSTL - THE UPPER END FITTING ON AFT PRESSURE BULKHEAD LT Z24 RIB WAS CRACKED AT TEE FITTING. REMOVED AND REPLACED END FITTING PER ARA 15188. CHECK-C 3-12-98 STL. (X)SDR TWAA9810312Bulkhead Skin · crackedSTL - FOUND BULKHEAD SKIN CRACKED .25 INCH AT LT BULKHEAD AT Z24L, ON OTBD TOP SIDE, SECOND HOLE FORM END. REPAIRED SKIN PER ARA 15189. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X)SDR 98UAL900282Bulkhead · crackedBS 1156 PRESSURE BULKHEAD FORWARD LEFT HAND SIDE AT L40 LONGERON HAS A CRACK. MANUFACTURED AND INSTALLED NEW REPAIR ANGLE.
Back to JASC 5312