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 GAIA00635Pressure Panel · crackedDISCREPANCY: DURING ROUTINE MAINTENANCE CHECK, A CRACK WAS DISCOVERED IN THE VERTICAL WEB OF THE NOSE WHEEL WEB AT DOUBLER AT BS 246, LBL 23.5, WL 170. CORRECTIVE ACTION: ACCOMPLISHED NOSE WHEEL WELL VERTICAL WEB REPAIR BS 246, RBL 23.5, WL 170 IAW B727 SRM SDR GAIA00634Pressure Panel · crackedDISCREPANCY: DURING A ROUTINE MAINTENANCE CHECK AT, A CRACK WAS DISCOVERED IN THE VERTICAL WEB OF THE NOSE WHEEL WELL AT BS253, RBL 23.5, WL185. CORRECTIVE ACTION: ACCOMPLISHED NOSE WHEEL VERTICAL WEB REPAIR BS253, RBL 23.5, WL 185 IAW B727 SRM 53-10-9. THE ASDR GAIA00633Bulkhead · crackedDISCREPANCY: DURING A ROUTINE MAINTENANCE CHECK, A CRACK WAS DISCOVERED AROUND A RIVET ONE FOOT BELOW RADAR DISH MOUNT, BS178. CORRECTIVE ACTION: ACCOMPLISHED BS 178 WEB REPAIR IAW B727 S/B 727-53-098. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR GAIA00630Bulkhead · crackedDISCREPANCY: DURING A ROUTINE MAINTENANCE CHECK, A CRACK WAS DISCOVERED AT THE PRESSURE BULKHEAD AFT OF 940 BEAM AT RBL 50. CORRECTIVE ACTION: ACCOMPLISHED BS940 PRESSURE BULKHEAD REPAIR IAW BOEING DRAWING 65-89360. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR DHL2000715009Pressure Panel · crackedNOSE WHEEL WELL RIGHT SIDE PANEL LOWER BS 240.7 WL 150 CRACKED. INSTALL DOUBLER REPAIR PER B727 SRM 51-10-1. SIZE OF REPAIR 7.5 X 3.5 INCHES.SDR DHL2000715016Pressure Panel · crackedNOSE WHEEL WELL RIGHT SIDE LATERAL WEB PANEL AT BS 285.5 SHOW CRACK RUNNING BETWEEN RIVETS. FABRICATED AND INSTALLED DOUBLER REPAIR PER B727 SRM 51-40-2, AND 51-10-2. SIZE OF MATERIAL USED 15 X 15.5 INCHES.SDR USAA001724Bulkhead · crackedPIT - SKIN CRACKED 1.5 INCHES, WL 207, RBL 28 AFT STA 178 LIGHTENING HOLE. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER; REMOVED, FABRICATED NEW WEB FROM .071 INCH 2024-T3 AND INSTALLED. (X)SDR TWAA0015712Bulkhead · crackedDURING CHECK-C MAINT AN EDDY CURRENT CHECK OF THE BULKHEAD T-CAP SHOWED A CRACK APPROXIMATELY 1 INCH LONG IN RADIUS AT LONGERON 28L. INSTALLED NEW T-CAP PER SRM 53-03 FIG 37A AND BOEING DRAWING SERIES 5911425.SDR TWAA0015711Bulkhead · corrodedDURING CHECK-C MAINT, THE AFT PRESSURE BULKHEAD SKIN WAS CORRODED ALONG THE BOTTOM EDGE AT ''T'' CAP, STA 996 FROM LONGERON 27L TO 28R, 23 INCHES LONG BY 2.25 IN HIGH. REPAIRED PRESSURE BULKHEAD SKIN PER SRM 53-05 FIG 9.SDR AWXA0000705Pressure Panel · crackedC-CHECK, CABIN SUB-FLOOR AT FS 664, RBL 50, PRESSURE WEB CRACKED, O/B OF WIRE FEED THROUGH. CUT OUT DAMAGED WEB, FABRICATED AND INSTALLED REPAIR PARTS IAW ER 03-5310-00243DL1.SDR AWXA0000695Intercostal · corrodedC-CHECK CORROSION, INTERCOSTAL AT FS 1006 - 1016, LBL 18 REQUIRES REPLACEMENT DUE TO T-CAP REPAIR. REMOVED INTERCOSTAL, FABBED REPAIR PART, AND INSTALLED REPAIR IAW 737 SRM 51-10-2 AND 51-30-01.SDR AWXA0000693Intercostal · crackedC-CHECK, INTERCOSTAL CRACKED AT FS 178, LBL 24, WL 195. REMOVED, REPAIRED, AND REINSTALLED INTERCOSTAL IAW 737 SRM 53-10-08.SDR SWAA001918Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD HORIZONTAL WEB CRACKED, AFT SIDE, WL 207, LBL 20 & RBL 20. REPAIRED BULKHEAD PER SRM.SDR SWAA001917Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND 19 CRACKS AT BS 178 BULKHEAD, LBL 26 - RBL 15. REPAIRED BULKHEAD PER SRM & XEA X2-53-283.SDR 2000UALA00745Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR SWAA001885Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKS AT LBL 1, WL 213 - WL 216 AND RBL 12 TO RBL 14, WL 226. REPAIRED BULKEAD PER ACO 7154-53.SDR LR7A00186Cap · crackedDURING SCHEDULED B-CHECK, THE RT FS 1012 BULKHEAD CAP WAS DISCOVERED CRACKED 6.0 INCHES IN LENGTH. REPAIRED PER MEA 382-53-00-121 R1 AND LYNDEN DRAWING R00-0024-4 REV A.SDR AU000947Bulkhead · cracked(AUS) FORWARD TAIL BULKHEAD CRACKED IN THE AREA OF THE HORIZONTAL STABILIZER ATTACHMENT POINT. (X)SDR 20010424CW009Bulkhead · crackedWHILE PERFORMING 100 HOUR INSPECTION, FOUND A CRACK IN THE UPPER RADIUS ABOVE THE RIGHT RUDDER STOP BOLT. PROBABLE CAUSE WOULD BE FROM THE RUDDER CONTACTING TOO HARD, POSSIBLE WIND DAMAGE. RECOMMED A SOFT HEADED STOP BOLT.SDR P2EA00273Bulkhead · damagedSJO - DURING C-CHECK, TEMPORARY REPAIR AT BS 178 FROM LBL 8 TO LBL 15 AND FROM WL 233 AND WL 238. INSTALLED PERMANENT REPAIR AT BS 178 FROM LBL 8 TO LBL 15 AND FROM WL 233 TO WL 238 IAW SRM 53-10-1 FIG 1. (M)SDR P2EA00263Bulkhead · crackedSJO - DURING C-CHECK, TEMPORARY REPAIR AT BS 178 FROM RBL 8 TO RBL 15 AND BETWEEN WL 233 TO WL 238. INSTALLED PERMANENT REPAIR AT BS 178 FROM RBL TO RBL 15 AND FROM WL 233 TO WL 238 IAW SRM 53-10-11 FIG 1. (M)SDR 2000UALA00751Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR USAA001613Bulkhead · crackedCLT - FOUND THE BULKHEAD WEB CRACKED .5 INCH, STATION 178 RBL 6.75, WL 198. ENLARGED CUTOUT OF DAMAGE (3 INCHES BY 5 INCHES) AND INSTALLED DOUBLERS PER SRM 53-10-11 FIG 1. (M)SDR USAA001609Bulkhead · crackedCLT - FOUND AFT NOSE W/W BULKHEAD CRACKED 1.5 INCHES, ACT SUPPORT BEAM WEB STATION 228, WL 185.5, BL 0. INSTALLED FILLER AND DOUBLER PER SRM 51-40-2. (M)SDR AU000995Post · cracked(AUS) FUSELAGE RIGHT FORWARD LOWER DOOR POST BULKHEAD CRACKED AT RELIEF HOLE PER AD/CESSNA206/48 AMDT1. CRACK LENGTH 8.2 MM (0.325 INCH). AD/CESSNA206/48 AMDT1 WAS NOT DUE FOR ANOTHER 120 HOURS. (X)SDR SWAA001873Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 188.5, LBL 75 & RBL 75, WL 205, RBL 26. REPAIRED BULKHEAD WEB PER SRM.SDR USAA001598Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB LBL 6.75 WL 201. ENLARGED CUT OUT OF DAMAGE (3 INCHES BY 5 INCHES) AND INSTALLED DOUBLERS. (M)SDR 20000927SH001Bulkhead · crackedSTA 49.5 BULKHEAD CRACKED AT UPPER NOSE GEAR ATTACH AREA - ALSO WINDSHIELD BRACE BUCKLED AT LOWER ATTACH AREA - NOTE: BRACE INSTALLED AS PART OF STC SA 1434AT. (X)SDR USAA001551Bulkhead · crackedBULKHEAD CRACKED. FABRICATED NEW WEB PER SRM 51-10-02SDR P2EA00284Bulkhead · crackedSJO - DURING C-CHECK, VERTICAL CHORD CRACKED AT BS 178. LBL 5.7 AND WL 184. FABRICATED AND REPLACED VERTICAL CHORD AT BS 178, LBL 5.7 AND FROM WL 177 AND WL 197 IAW SRM 53-10-11 FIG 8 AND SRM 51-10-1. (X)SDR USAA001549Bulkhead · crackedCLT - FOUND WEB CRACKED 1 INCH, BS 178 PLUS 1.5, RBL 29, WL 207. INSTALLED FABRICATED WEB PER SRM 51-30-01. (M)SDR USAA001548Bulkhead · crackedCLT - FOUND WEB CRACKED 1 INCH, BS 178 PLUS 1.5, LBL 29, WL 207. INSTALLED FABRICATED WEB PER SRM 51-10-01. (M)SDR USAA001539Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED 3 INCHES, STATION 178, LBL 5.7, WL 211-214. INSTALLED DOUBLER PER SRM 53-10-11. (M)SDR AWXA0000678Bulkhead · crackedC-CHECK, STA 183, LBL 5.7, WL 178, WEB CRACKED. FABRICATED REPAIR DOUBLER IAW B737 SRM 51-40-2 FIG 1, TREATED AND PRIMED IAW MM 51-23-00, CRACK DRESSED OUT AND REPAIRED IAW SRM 51-40-2 FIG 1 AND 53-10-2.SDR AWXA0000676Bulkhead · crackedC-CHECK, STA 178, LBL 11.5, WL 218 BULKHEAD WEB CRACK EMANATING FROM HORIZONTAL U SECTION. REPLACED WEB IAW EO 53-12-07.SDR AWXA0000675Bulkhead · crackedC-CHECK, STA 178, RBL 1, WL 187, BULKHEAD AFT FACE WEB CRACKED. REPLACED WEB IAW EO 53-12-07.SDR 2000UALA00764Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00742Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR QXEA0002821Bulkhead · crackedPDX- RIGHT HAND AIR CYCLE MACHINE BULKHEAD WALL APPEARS TO BE CRACKED AT LOWER EDGE, SEEN THROUGH PANEL 24A. REPAIRED IAW FOKKER SRM 51-31-05, 51-31-01, 53-02-18 PAGE 29 AND 51-10-04.SDR AALA20001662Bulkhead · corrodedTUL - FOUND FORWARD SIDE OF AFT PRESS BULKHEAD CORRODED, 2 INCHES BY 1 INCH, AROUND NUTPLATES BELOW RIGHT CONTER DUCT ABOVE AFT ENTRY DOOR RBL 3 TO RBL 5. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 80559 DATED 9/22/00. (M)SDR MWEA00818Bulkhead · tool damageMKE - NUMEROUS TOOL MARKS ON FORWARD SIDE OF APB TEE, BETWEEN SHOVEL CLIPS 4 EACH LEFT TO 4 EACH RIGHT. (X)SDR QXEA0002753Bulkhead · crackedPDX- RIGH HAND AIR CYCLE MACHINE BULKHEAD APPEARS TO BE CRACKED AT LOWER EDGE BETWEEN NOSE BAY AND AIR CYCLE MACHINE COMPARTMENT. REPAIRED IAW FOKKER SRM 53-02-18 PAGE 29.SDR TWAA0015505Rib · crackedDURING OP 15 MAINT CHECK AT WS 111.5 RIB BOTH I/B AND O/B FORMER FOOT BETWEEN REAR SPAR AND STA 11, WERE CRACKED THRU LOWER CENTER VERTICAL FASTENERS, CONFIRMED BY NDT. INSTALLED CLIP ON EACH PER DRAWING 9911606 AND SPM 6-70-1 PARA 4, PAGE 2 AND 3. INSTALLEDSDR 0003609968Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED FROM DOOR OPENING TO FASTENER HOLE. FIRST FASTENER ROW ABOVE DOOR 10 INCHES LEFT OF INTERCOSTAL. REPAIRS ACCOMPLISHED PER EA 99-177766. L/P 1498846SDR AWXA0000665Frame · crackedC-CHECK, SIDE CHORD CRACKED AT FS 178, RBL 26, WL 207. CUT OUT DAMAGED AREA, INSTALLED REPLACEMENT SECTION OF CHORD AND SPLICE ANGLE IAW AWA ER 03-5312-000256-DL3.SDR AWXA0000663Bulkhead · crackedC-CHECK, CENTER WEB CRACKED AT FS 178 RBL 5.5 WL 200. CUT OUT DAMAGED AREA, FABRICATED DOUBLERS AND FILLER, INSTALLED REPAIR PARTS IAW 737 SRM 53-10-08 FIG 209.SDR AWXA0000661Bulkhead · crackedC-CHECK, CENTER WEB CRACKED AT FS 178 LBL 5.5 WL 200. CUT OUT DAMAGED AREA, FABRICATED DOUBLERS AND FILLER, INSTALLED REPAIR PARTS IAW 737 SRM 53-10-08 FIG 209.SDR AWXA0000660Bulkhead · crackedC-CHECK, BULKHEAD ACCESS HOLES REQUIRED AT FS 178, RBL 21, WL 198. CUT OUT ACCESS HOLES, FABRICATED AND INSTALLED REPAIR PARTS IAW 737 SRM 53-10-08 FIG 206 AND 204.SDR AWXA0000659Bulkhead · crackedC-CHECK, BULKHEAD ACCESS HOLES REQUIRED AT FS 178, LBL 26, WL 198. CUT 2 ACCESS HOLES IN WEB IAW 737 SRM 53-10-00 FIG 204 AND 206, INSTALLED REPAIR PARTS IAW 737 SRM 57-10-08 FIG 204 AND 206.SDR AWXA0000655Intercostal · crackedC-CHECK, INTERCOSTAL CRACKED AT FS 178 RBL 24 WL 195. REMOVED DAMAGED INTERCOSTAL IAW 737 SRM 51-40-02, FABRICATED REPAIR PARTS IAW SRM 53-10-08 FIG 207, INSTALLED PARTS IAW SRM 51-40-02.
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