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 AWXA200300658Bulkhead · crackedDURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 5.7, WL 212.5-213.5. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK IS CONTAINED; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PART IAW B737-3May 16, 2003 · N166AW · Boeing 73733ASDR AWXA200300650Bulkhead · crackedDURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT LBL 4.7, WL 201-202. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW SRM 5May 16, 2003 · N166AW · Boeing 73733ASDR UPS03240749Washer · missingINSPECTION TYPE: C, AIR LEAK AT NWW PRESSURE PANEL, RT FWD PANEL. PANEL REMOVED IAW MM 20-80-01. FIBRE WASHERS FOUND TO BE MISSING & REPLACED IAW IPC 25-53-00. ON FURTHER INVESTIGATION CRACK FOUND ON NWW SIDE WALL. AREA CUT OUT IAW SRM 51-40-2. REPAIRED May 15, 2003 · N954UP · Boeing 727185CSDR SWAA031089Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, LBL 5.7, WL 183 & WL 213. REPAIRED BULKHEAD WEB PER SRM.May 14, 2003 · N661SW · Boeing 737317SDR GTIA030422Pressure Panel · crackedNOSE WHEEL WELL STATION 38 RBL 11, BULKHEAD SUPPORT WEB IS CRACKED. REMOVED CRACKED WEB. LOCATED AND DRILLED ON NEW WEB. INSTALLED WEB. (M)May 13, 2003 · N810NK · Doug DC981SDR DHL2003747514Beam · crackedDURING C-CHECK, AFT PRESS BULKHEAD BS 1183 LBL 36.4 VERTICAL BEAM CRACK INDICATION WL 149 APPROX IS ABOUT 1 INCH LONG NDT, CONFIRMED. STOP DRILLED CRACK IAW B-727 SRM 51-10-1. AREA HFEC INSPECTED AND VERIFIED CRACKS END IN STOP DRILL HOLES. INSTALLED S/B REMay 12, 2003 · N747DH · Boeing 727224SDR DHL2003747507Bulkhead · crackedDURING "C" CHECK DISCREPANCY AS FOLLOWS, "AFT. PRESS. BULKHEAD BS 1183 RBBL 36.4 VERTICAL BEAM IS CRACKED FROM INB/OUT AFT. FLANGES. STOP DRILLED CRACKS AND INSTALLED REPAIR PARTS PER S/B 727-53-0192 REV. 1, FIG. 2.May 12, 2003 · N747DH · Boeing 727224SDR CALA0300246Pressure Panel · crackedINSPECTION FOUND A CRACK IN RT PRESSURE DECK AT STA 665-675, RBL 35-45. THE PRESSURE DECK WAS REPAIRED IAW ECRA 5312-01021.May 12, 2003 · N16339 · Boeing 7373T0SDR CALA0300241Bulkhead · corrodedINSPECTION FOUND FORWARD FACE OF AFT PRESSURE BULKHEAD CORRODED JUST AFT OF FS 1016 AT LBL 6 TO RBL 6. REPAIRED APB IAW DRAWING 65C28106-1.May 12, 2003 · N10323 · Boeing 7373T0SDR UPS03440768Bulkhead · crackedINSPECTION TYPE:C, FX - STA 1480 PRESSURE BULKHEAD LEFT O/B LOWER WEB FOUND CRACKED AT LBL 90 TO LBL 92 HI-LOK AREA. FX STA 1480 PRESSURE BULKHEAD LEFT O/B LOWER WEB REPAIRED AS PER SRM 51-40-02 FIG 1 JUST AT LBL 90 TO LBL 92.May 10, 2003 · N521UP · Boeing 747200SDR 03FDEA00695Doubler · corrodedIN CENTER ACCESSORY COMPT STA 1156, BULKHEAD BETWEEN LONGERONS L50-49, LT LOWER CORNER OF BATTERY HAS CORROSION AT DOUBLER. REMOVED DOUBLER IAW SRM 51-31-01. FAB NEW DOUBLER ON TRAVELER 2/330509. INSTALLED NEW DOUBLER IAW SRM 51-33-01. PAINTED AREA IAW SMay 8, 2003 · N375FE · Doug DC1010SDR AMTA200300659Bulkhead · corrodedCOMPARTMENT AFT BULKHEAD CORRODED FS 1685 LBL 24 TO LBL 28 JUST ABOVE CARGO FLOOR. REPAIRED BULKHEAD IAW SRM 51-50-07. (M)May 7, 2003 · N162AT · Lkheed 10113853SDR MWEA030204Bulkhead · gougedAFT PRESSURE BULKHEAD HAS A GOUGE ON THE RIGHT SIDE LOCATED AT ABOUT 11:00 POSITION (LOOKING FROM THE AFT SIDE) FROM THE CENTER OF THE THRUST REVERSE SECTOR, THE GOUGE IS ABOUT 3.5 FROM THE CENTER OF THE SECTOR. BLENDED OUT GOUGE, PERFORMED THICKNESS TEST FOUMay 7, 2003 · N807ME · Doug DC981SDR MWEA030203Bulkhead · gougedAFT PRESSURE BULKHEAD SKIN HAS A GOUGE ON THE RIGHT SIDE LOCATED AT ABOUT THE 7:00 POSITION (LOOKING FROM THE AFT SIDE) FROM THE CENTER SECTOR. BLENDED GOUGE, PERFORMED THICKNESS CHECK. THICKNESS WITHIN LIMITS.May 7, 2003 · N807ME · Doug DC981SDR LR7A03044Splice · crackedDURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND LT MLG WW FS 617 AFT BULKHEAD LOWER PANEL SPLICE CRACKED AT OUTBD END, LBL 80, WL 150. REPLACED LOWER SPLICE IAW LOCKHEED DWG 339149. NR 0031.May 4, 2003 · N404LC · Lkheed 382GSDR AUS20030692Bulkhead · cracked(AUS) FUSELAGE BULKHEAD CRACKED AT TOP RT TAIL BOOM FITTING BRACKET.FOUND DURING INSPECTION IAW AD/HU389/108.May 2, 2003 · Doug 600NSDR SWAA030995Pressure Panel · crackedDURING SCHEDULED SPECIAL VISIT, FOUND UPPER NLG W/W SKIN CRACKED AT AFT OUTBOARD LT CORNER OF NOSE TIRE BRAKE PAD. REPAIRED SKIN PER SWA EA.May 2, 2003 · N334SW · Boeing 7373H4SDR 2003FA0000565Bulkhead · crackedTIME SINCE LAST AD REQUIRED INSPECTION 901.8. ORIGINALLY INSPECTED ON 9/19/74 WITH 1246 TT, FOUND OK. REINSPECTED AT 1502 AND 2334.58 TT AND FOUND, OK. ALSO INSPECTED AT 3345.1 AND FOUND AIRWORTHY. CURRENT INSPECTION REVEALED TWO SMALL CRACKS .1250 AND .25May 1, 2003 · N9VP · Cessna 182NSDR AWXA200300486Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD FLOOR WEB AT WL 207, LBL 24. MAINTENANCE REMOVED CRACKED FLOOR WEB BS 178 BULKHEAD, WL 207, LBL 24, AND DISCOVERED A CRACKED ATTACH ANGLE. REMOVED CRACKED ATTACH ANGLE; FABRICApr 29, 2003 · N164AW · Boeing 73733ASDR AWXA200300484Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT WL 213, LBL 11. MAINTENANCE STOP DRILLED CRACK AND CUT OUT CRACKED AREA OF BS 178 BULKHEAD WEB AT WL 213, LBL 11; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FAApr 29, 2003 · N164AW · Boeing 73733ASDR AWXA200300483Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT WL 210, RBL 6. MAINTENANCE STOP DRILLED CRACK AND CUT OUT CRACKED AREA OF BS 178 BULKHEAD WEB AT WL 210, RBL 6; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRApr 29, 2003 · N164AW · Boeing 73733ASDR AWXA200300482Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT WL 207, LBL 11. MAINTENANCE STOP DRILLED CRACK AND CUT OUT CRACKED AREA OF BS 178 BULKHEAD WEB AT WL 207, LBL 11; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATEApr 29, 2003 · N164AW · Boeing 73733ASDR CA030514004Flange · cracked(CAN) CRACK ON BULKHEAD FLANGE APPROX. .7500 LONG CRACK. NOSE COMPARTMENT AREA, NOSE WHEEL STEERING IDLER SHAFT SUPPORT INTERCOSTAL BULKHEAD.Apr 28, 2003 · Beech 100BEECHSDR 03FDEA00631Bulkhead · crackedLEFT MLG WHEEL WELL STATION 870 BULKHEAD IS CRACKED AT LBL 42 APPROXIMATELY W/L 185.5 AND BELOW HORIZONTAL CHORD REPAIRED IN ACCORDANCE WITH FEDEX EA 7-5310- 69465.Apr 28, 2003 · N218FE · Boeing 727200SDR 03FDEA00632Bulkhead · crackedRIGHT MLG WHEEL WELL STATION 870 BULKHEAD IS CRACKED AT RBL 56 W/L 185.5. REPAIRED IN ACCORDANCE WITH FEDEX EA 7-5310-69465.Apr 28, 2003 · N218FE · Boeing 727200SDR DLM88030397Bulkhead · damagedTOOL DAMAGE (DRILL MARKS) WERE FOUND ON AFT PRESSURE BULKHEAD LOWER CAP NEAR SKIN DRAIN HOLES. REPAIRED BY BLENDING 0.007 INCH DEPTH LHS AND 0.009 INCH DEPTH RHS PER FAA DER APPROVED REPAIR INSTRUCTIONS.Apr 27, 2003 · N918DL · Doug MD88SDR DL73G030394Bulkhead · crackedTHE FS 178 BULKHEAD WEB WAS FOUND WITH 3 TYPICAL CRACKS, 1 AT LBL 5.7 & WL 200, 1 AT RBL 5.7 & WL 200, AND 1 AT RBL 5.7 & WL 211. THE CRACKS ARE TYPICAL OF AD 2000-05-29 AND BAC S/B 737-53A1173. THE CRACKS WERE REPAIRED WITH ALUMINUM REPAIR DOUBLERS PER THEApr 25, 2003 · N223DZ · Boeing 73735BSDR SWAA030937Bulkhead · crackedDURING SCHEDULED C1 CHECK, FOUND SECONDARY HEAT EXCHANGER OUTBOARD SUPPORT BULKHEAD WEB CRACKED, BS 585 & LBL 40.875. REPAIRED BULKHEAD WEB PER SWA EA.Apr 25, 2003 · N396SW · Boeing 7373H4SDR CA030528010Pressure Panel · cracked(CAN) DURING A 'C' CHECK INSPECTION A 13 INCH CRACK DISCOVERED IN THE WHEEL WELL UPPER PRESSURE SKIN ALONG AIRCRAFT CENTER LINE AT EDGE OF STRINGER BETWEEN FRAMES 29 TO FRAME 32. MANUFACTURER CONTACTED. DAMAGE REPAIRED IAW MFG REPAIR INSTRUCTION HC532H9018.Apr 23, 2003 · Bac 146200ASDR ASAA0380410Bulkhead · gougedOKC - DURING 30K CHECK, FOUND RIGHT MLG WHEEL WELL AFT PRESSURE BULKHEAD IS GOUGED AT FS 1003. REPLACED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 51-70-4. (M)Apr 21, 2003 · N931AS · Doug DC982SDR ASAA0380378Bulkhead · crackedOKC - DURING 30K CHECK, FOUND AFT PRESSURE BULKHEAD FORWARD FACE IS CRACKED AT OP MOST RIVETS. REPLACED WEB AT BL 0 PER SRM 51-30-5. (M)Apr 21, 2003 · N931AS · Doug DC982SDR 03FDEA00550Bulkhead · corrodedCORROSION FWD CARGO BAY 740 LWR CHORD RBL 12 WL 148.5 UPPER SURFACE AROUND FASTENERS.Apr 21, 2003 · N486FE · Boeing 727200SDR SWAA030893Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 227 & LBL 17.1. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM.Apr 20, 2003 · N690SW · Boeing 7373G7SDR SWAA030877Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 2 EA ) AT BS 178, WL201 AT LBL 5.5 & BS 178, WL 213 AT RBL 6.5. REPAIRED BULKHEAD WEB PER SRM.Apr 18, 2003 · N378SW · Boeing 7373H4SDR 03FDEA00504Bulkhead · corrodedFORWARD CARGO PIT AFT BULKHEAD LEFT LOWER ANGLE HAS NUMEROUS AREAS OF CORROSION. *S/D* REPAIRED LT BOTTOM FWD CARGO PIT AFT BULKHEAD ANGLE IAW BOEING 727-200 SRM 51-40-03.Apr 17, 2003 · N218FE · Boeing 727200SDR 03FDEA00503Bulkhead · corrodedFORWARD CARGO PIT RIGHT AFT BULKHEAD ANGLE HAS NUMEROUS AREAS OF CORROSION. *S/D* REPAIRED RT FWD CARGO PIT BULKHEAD ANGLE IAW B727-200 SRM 51-40-03.Apr 17, 2003 · N218FE · Boeing 727200SDR EIA2003063Bulkhead · corrodedSTA 1241, LT WHEEL WELL AFT PRESSURE BULKHEAD, PRESSURE ANGLE (65B10821-1) IS CORRODED BEYOND THE SRM ALLOWABLE LIMITS AND REQUIRES REMOVAL AND REPLACEMENT. STA 1241 LT WHEEL WELL AFT PRESSURE BULKHEAD REPAIRED PER ECRA 471-57-212-2 AND ECRA 471-57-214-2.Apr 16, 2003 · N471EV · Boeing 747273CSDR EIA2003059Bulkhead · corrodedLEFT WING MAIN LANDING GEAR WELL BS 1241 VERT BULKHEAD CORROSION AT LBL 94 UNDER HORIZ ANGLE AT VERT CANTED SPLICE. REMOVED CORROSION, NDT AREA, FABBED AND INSTALLED REPAIR PER ECRS 471-57-209-2.Apr 16, 2003 · N471EV · Boeing 747273CSDR 03FDEA00449Bulkhead · crackedCRACK IN LEFT WHEEL WELL STATION 870 BULKHEAD SKIN WEB. ** S/D ** REPAIRED CRACK IAW FEDEX EA 7-5310-69465Apr 15, 2003 · N218FE · Boeing 727200SDR 03FDEA00450Bulkhead · crackedCRACKS IN RIGHT WHEEL WELL, 870 BULKHEAD SKIN WEB. REPAIRED CRACK IAW FEDEX EA 7-5310-69465Apr 15, 2003 · N218FE · Boeing 727200SDR DL73G030364Bulkhead · crackedINSPECTION OF THE FS 178 BULKHEAD WEB PER AD 2000-05-29 REVEALED SEVERAL CRACKS IN THE CENTER WEB BETWEEN WL 219 & 226 AND BETWEEN LBL 12 & RBL 5.7. THE CENTER WEB WAS REMOVED AND A WEB INSTALLED TO CORRECT THE PROBLEM. THE REPLACEMENT WAS ACCOMPLISHEApr 15, 2003 · N224DA · Boeing 73735BSDR AWXA200300445Bulkhead · crackedYVR - MAJOR REPAIR - DURING C-15 CHECK 4 EACH 1/2 INCH CRACKS WERE FOUND AT RIVET HOLES ON REAR PRESSURE BULKHEAD AT BS 1016, AFT OF STR 7 L/H. MAINTENANCE CUTOUT DAMAGED PORTION OF WEB ON REAR PRESSURE BULKHEAD AT BS 1016, AFT OF STR 7 L/H; FABRICATED A FILLEApr 15, 2003 · N188AW · Boeing 737277SDR ABXA030167Pressure Panel · corrodedONE SHEARED FASTENER AND SKIN BULGED AT DOUBLER RIGHT WHEEL WELL UPPER PRESSURE PANEL, STA 716, RIGHT BUTT LINE 56. REPAIRED AREA IAW REA D953-47174.Apr 14, 2003 · N942AX · Doug DC931SDR UPS03840448Bulkhead · crackedINSPECTION TYPE: C1, MAIN CABIN AFT PRESSURE BULKHEAD IS CRACKED AT STA 1766 RBL 35 AT APPROX 66 INCHES ABOVE FLOOR LEVEL. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER IAW SRM 53-2-5 FIG 14A, FOUND TO BE WITHIN RANGApr 13, 2003 · N808UP · Doug DC873FSDR CA030414006Bulkhead · cracked(CAN) FUSELAGE SKIN PANEL UNDER REFUELING STEPS NOTED HAVING A BULGE AREA AROUND MOUNTING BOLT. SKIN MOVEMENT ALSO WAS EVIDENT WHEN WEIGHT WAS APPLIED TO THE STEP. DETAIL INSPECTION OF AREA FOUND BOTH THE FUSELAGE SKIN AND BULKHEAD WHERE THE STEP IS MOUNTED Apr 11, 2003 · Cessna 182SSDR GTIA030289Bulkhead · crackedAFT ACC AREA BULKHEAD CRACKED AT STA 1463 CANT APPROX LONGERON 3L. REMOVED 2 PART WEB ASSY. FABBED WEB AND DOUBLER ASSY. INSTALLED WEB AND DOUBLER ASSY.Apr 11, 2003 · N814NK · Doug DC983SDR AUS20030427Bulkhead · damaged(AUS) REAR PRESSURE BULKHEAD DAMAGED. A SMALL DENT APPROXIMATELY 10.1MM (0.4IN) LONG CONTAINING A SHARP INDENT WAS FOUND TO BE CRACKED. SUSPECT CAUSED DURING EQUIPMENT LOADING SOME TIME PREVIOUSLY.Apr 11, 2003 · Beech B200TSDR 2003FA0000424Bulkhead · crackedPART WAS FOUND CRACKED DURING INSPECTION REQUIRED BY AD 72-07-09. PART WAS CRACKED AT IT HAND RUDDER CONTROL CABLE HOLE, BETWEEN HOLE AND BULKHEAD FLANGE. PROBABLE CAUSE IS FATIGUE. RECOMMEND THAT CONTROL LOCK IS ALWAYS PUT IN WHEN AIRCRAFT IS STORED OUTSIDApr 11, 2003 · N2727Q · Cessna 182KSDR AWXA200300475Bulkhead · crackedYVR - MAJOR REPAIR - DURING C-15 CHECK A 1/2 INCH CRACK WAS FOUND AT HOLE ON VERTICAL WEB, AFT SECTION OF BS 178 BULKHEAD, AT RBL 17, WL 188. MAINTENANCE CUTOUT DAMAGED AREA OF WEB AT AFT SECTION OF BS 178 BULKHEAD, AT RBL 17, WL 188; FABRICATED A WEB SPLICE AApr 10, 2003 · N188AW · Boeing 737277SDR AWXA200300467Bulkhead · crackedDURING C-15 CHECK A .5 INCH CRACK WAS FOUND ON WEB DURING ULTRASONIC INSPECTION OF FORWARD PRESSURE BULKHEAD BS 178, 2 INCHES ABOVE WL 195 AT LBL 5.7. MAINTENANCE CUTOUT DAMAGED SECTION OF WEB; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FAApr 10, 2003 · N188AW · Boeing 737277
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