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 RRXA003787Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO ATTACH ANGLE AT STA. 1600 AND L12L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 & 51Jan 20, 2000 · N792FT · Doug DC873FSDR USAA000097Bulkhead · crackedPIT - RIGHT SIDE STA 965 BULKHEAD WEB LOWER END, WEB HAD 2 INCH CRACK. BULKHEAD FOUND CRACKED AT BS 965. CUT OUT DAMAGED WEB SECTION AND INSTALLED NEW PER SRM 53-03 FIG 19. (X)Jan 20, 2000 · N927VJ · Doug DC931SDR 0000641229Bulkhead · crackedDURING M-CHECK, FOUND CRACK AT BS 2122 LOWER BULKHEAD WEB. REPAIRED PER EA 12-172785.Jan 19, 2000 · N229NW · Doug DC1030SDR CA000128029Bulkhead · cracked(CAN) DURING A ROUTINE INSPECTION THE BULKHEAD AT STA. 317.75 WAS FOUND CRACKED IN THE UPPER LT FLANGE AREA. ALSO FOUND PIPER REINFORCEMENT PLATE CRACKED. THIS AREA HAD PREVIOUSLY BEEN ADDRESSED BY S/B 636A & KIT 763-917. INSTALLED SEPT 28/81 AT 3498.7 AIRFRJan 18, 2000 · Piper PA31350SDR ASAA0080023Bulkhead · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON FORWARD LOWER SURFACE OF AFT PRESSURE BULKHEAD CENTER BOTTOM DOUBLER AT FS 1338, LBL 3.5 TO RBL 3.5. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-02. (M)Jan 18, 2000 · N951AS · Doug DC982SDR ASAA0080021Bulkhead · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON FORWARD LOWER SURFACE OF AFT PRESSURE BULKHEAD AT FS 1338, LBL 10 TO 13. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-03 FIG 9. (M)Jan 18, 2000 · N951AS · Doug DC982SDR USAA000048Bulkhead · crackedBULKHEAD CRACKED AT BS 663, LT BUTTLINE 23, WATERLINE 201.5. INSTALLED SPLICE ANGLE PER TR 57-10-03. (M)Jan 18, 2000 · N243US · Boeing 737201SDR AU000128029Bulkhead · cracked(AU) DURING A ROUTINE INSPECTION THE BULKHEAD AT STA 317.75 WAS FOUND CRACKED IN THE UPPER LEFT FLANGE AREA. ALSO FOUND PIPER REINFORCEMENT PLATE (P/N 40682-10) CRACKED. THIS AREA HAD PREVIOUSLY BEEN ADDRESSED BY S/B 636A AND KIT 763-917. INSTALLED SEPT 2Jan 18, 2000 · Piper PA31350SDR SWAA000108Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 12. REPAIRED BULKHEAD PER SRM.Jan 17, 2000 · N105SW · Boeing 7372H4SDR SWAA000100Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND THROUGH ULTRASONIC INSPECTION BS 178 BULKHEAD CRACKED IN 3 PLACES, LBL 6.7, RBL 6.7 AND RBL 4.7. REPAIRED BULKHEAD PER SRM.Jan 17, 2000 · N506SW · Boeing 7375H4SDR USAA000182Bulkhead · crackedPIT - FOUND TWO CRACKS .75 INCH LOWER MOUNT BRACKET AREA, STATION 178 BULKHEAD AT RIGHT. INSTALLED DOUBLER PER TYP REPAIR 53-10-07 REV 1. (M)Jan 14, 2000 · N430US · Boeing 7374B7SDR USAA000181Bulkhead · crackedPIT - FOUND BL 0 BULKHEAD 178 CRACKED .75 INCH. INSTALLED DOUBLER AND FILLER PER TYP REPAIR 53-10-07 REV A. (M)Jan 14, 2000 · N430US · Boeing 7374B7SDR AWXA0000010Bulkhead · corrodedC-CK CORROSION LEVEL 1 NR 5279330. CORROSION OUT OF LIMITS AT AFT PRESSURE BULKHEAD STA 1016, STR 27R. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PLATE AND FILLER IAW SRM 53-80-08 FIG 201 MAT 2024-T3 .032 QQA2505 R698474 AND 2024-T3 .025, QQA2545 Jan 14, 2000 · N306AW · Boeing 7373G7SDR USAA000022Bulkhead · crackedFOUND BULKHEAD CRACKED. INSTALLED REPAIR KIT PER DWG 65C37732. (M)Jan 13, 2000 · N243US · Boeing 737201SDR USAA991447Bulkhead · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT STATION 178, RBL 4.75, WL 201 BULKHEAD. INSTALLED DOUBLER PER SRM 53-10-8 AND EA 66276. (M)Jan 12, 2000 · N346US · Boeing 737301SDR MWEA00027Bulkhead · corrodedUPPER WEB OF VENTRAL STAIRWAY BULKHEAD AT STATION 996 HAS AN AREA OF MODERATE CORROSION. MTC FABRICATED AND INSTALLED DOUBLER.Jan 12, 2000 · N207ME · Doug DC932SDR TWAA0101013Stop · corrodedDURING CHECK-C MAINT AT THE AFT CABIN BULKHEAD, THE DOOR EXTRUSION STOP HAD HEAVY CORROSION, BOTTOM LT SIDE OF DOOR AS VIEWED LOOKING FROM AFT. REPLACED DOOR STOP PER SPM 6-70-01 WITH NEW PART.Jan 9, 2000 · N9420D · Doug DC983SDR ABXA000050Web · corrodedDURING C-CHECK, FOUND THE AFT LOWER CARGO COMPARTMENT AFT BULKHEAD WEB EXFOLIATED AND RIVET HEADS POPPED JUST ABOVE LONGERON 30 ON BOTH SIDES OF BULKHEAD CENTER SUPPORT. REPLACED WEB IAW DC9 SRM 51-30-2 AND 51-30-5.Jan 6, 2000 · N934AX · Doug DC933FSDR UPS00831359Bulkhead · crackedINSPECTION TYPE:C123 ATTACH ANGLE CRACKED AT LOWER LT CORNER AT BULKHEAD AT FWD OF NLG C OMPARTMENT PANEL 601. REPAIRED AS PER SRM 53-2-0.Jan 4, 2000 · N752UP · Doug DC871FSDR SWAA000027Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD 3 EACH CRACKS, RBL1- LBL 6. REPAIRED BULKHEAD PER SRM.Jan 4, 2000 · N504SW · Boeing 7375H4SDR ABXA000061Bulkhead · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED ON RIGHT SIDE. REPAIRED AFT PRESSURE BULKHEAD IAW DC9 SRM 53-05.Jan 3, 2000 · N902AX · Doug DC932SDR TWAA0000804Bulkhead · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD AT BOTTOM CENTER END TIE AND BULKHEAD. REMOVED CORROSION IN ACCORDANCE WITH SRM 51-10-3, PAGE 21-22 AND SPM 6-80-01, PAGE 1 AND 2.Dec 30, 1999 · N110HM · Doug DC983SDR QXEA0000064Bulkhead · damagedPDX - DAMAGED LIGHTNING HOLE IN FORWARD PRESSURE BULKHEAD, HORIZONTAL BEAM VI AT CENTERLINE. METAL IS TORN APPROXIMATELY .070. REPAIRED IAW FOKKER SRM 53-02-01.Dec 30, 1999 · N476US · Fokker F28MK4000SDR MWEA99975Bulkhead · damagedAFT PRESSURE BULKHEAD HAS DRILLED START MARK ON AFT SLIDE AT THE LEFT THRUST REVERSER SECTOR BEARING AREA. MAINTENANCE FABRICATED AND INSTALLED DOUBLER.Dec 28, 1999 · N207ME · Doug DC932SDR AWXA9900482Bulkhead · crackedVERTICAL INTERCOSTAL WEB HAD NINE 4 INCH CRACKS ON AFT SIDE OF STA 178 PRESSURE BULKHEAD LBL 18, WL 172. REMOVED DAMAGED WEB PER SRM B737 51-40-02, HFEC INSP FOR CRACKS, FABRICATED WEB FROM 7075 T6 .020 R699797, DOUBLER FROM 7075 T6 .032 R700673 PER SRM B737 Dec 20, 1999 · N180AW · Boeing 737277SDR QXEA0000056Bulkhead · damagedPDX - AFT PRESSURE BULKHEAD SKIN, FORWARD SIDE HAS A .015 DEEP MARK FROM SCREW LOCATED 7 BELOW STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 3 (1,3).Dec 19, 1999 · N476US · Fokker F28MK4000SDR SWAA992096Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 7. REPAIRED BULKHEAD PER SRM.Dec 18, 1999 · N129SW · Boeing 7372T4SDR SWAA992086Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED LBL 7 AND RBL 5. REPAIRED BULKHEAD PER SRM AND SWA RA NR 1-353-2187.Dec 17, 1999 · N361SW · Boeing 7373H4SDR CA000110037Bulkhead · cracked(CAN) THE BULKHEAD AT STN 228 WAS INSPECTED AS PER CF-98-38 AND SB 2/52. THE BULKHEAD WAS FOUND CRACKED IN SEVERAL LOCATIONS AND REPLACEDDec 16, 1999 · Dhav DHC2MK1SDR TWAA0000112Bulkhead · chafedDURING CHECK-C MAINT, THE AFT ACCESSORY COMPARTMENT AT STA 1380 BULKHEAD, HAD WORN AREA THROUGH WEB BELOW LONGERON 4L. REPAIRED BULKHEAD PER SRM 53-01, FIG 2 SHEET 3 PAGE 9. DOUBLER TREATED AND PRIMED PER SRM 51-10-03, PAGE 16 AND 18.Dec 15, 1999 · N913TW · Doug DC982SDR DL72S992762Bulkhead · crackedTHE WEB OF THE FS 1183 BULKHEAD WAS FOUND WITH A .75 INCH LONG TYPICAL CRACK AT RBL 26 AND WL 169. THE CRACK IS TYPICAL OF BOEING S/B 727-53-0215. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED PER THE S/B AS DOCUMENTED IN ER/A 368897-14.Dec 15, 1999 · N540DA · Boeing 727232SDR SWAA992044Frame · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD LEFT AND RIGHT OUTBOARD CHORDS CRACKED AT WL 207. REMOVED AND REPLACED BOTH CHORD SECTIONS PER SRM.Dec 10, 1999 · N328SW · Boeing 7373H4SDR DL73K992701Bulkhead · crackedTWO CRACKS WERE FOUND IN THE FS 178 BULKHEAD WEB. THE DAMAGE WAS FOUND AT MV IN ATL AND REPAIRED PER ERA 333854-14.Dec 10, 1999 · N242WA · Boeing 737247SDR AALA991891Bulkhead · corrodedTUL - FOUND CORROSION AROUND SEVERAL FASTENERS ON FORWARD SIDE OF STATION 1338 PRESSURE BULKHEAD RIGHT SIDE ABOVE VAULT DOOR JAMB, JUST BELOW RIGHT A/C DUCT. REMOVED DAMAGE BY BLENDING. INSTALLED DOUBLER PER ESO 80559, DATED 12-10-99. (M)Dec 9, 1999 · N279AA · Doug DC982SDR SWAA992022Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 12. REPAIRED BULKHEAD PER SRM.Dec 6, 1999 · N328SW · Boeing 7373H4SDR SWAA992012Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACKED AT 5 EACH PLACES, BETWEEN LBL 7 AND RBL 7. REPAIRED BULKHEAD PER SRM.Dec 4, 1999 · N505SW · Boeing 7375H4SDR ABXA000037Bulkhead · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD NR 2 TEE CAP CRACKED. REPLACED TEE CAP IAW EA 53120033.Dec 3, 1999 · N944AX · Doug DC931SDR ABXA000036Bulkhead · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD NR 6 TEE CAP CRACKED. REPLACED NR 6 TEE CAP IAW EA 53120037.Dec 3, 1999 · N944AX · Doug DC931SDR AALA991862Bulkhead · crackedTUL - FOUND CRACK IN BULKHEAD 1183 RBL 25 WL 169. REPAIRED PER CARD 5478 SB 727-53-0215. FASTENERS IN REPAIR ARE INSTALLED WITH HEADS AFT SB CALLS FOR HEADS FORWARD. (M)Dec 3, 1999 · N863AA · Boeing 727223SDR P2EA99335Bulkhead · crackedSJO - C-CHECK, WEB CRACKED AT BS 178, LBL 10 INCHES, WL 235. DEFECT SIZE, LENGTH .375 INCH. REPAIRED BULKHEAD WEB AT BS 178 FROM LBL 7 TO LBL 17.5, BETWEEN WL 240 AND WL 230.5 PER SRM 53-10-11 FIG 1. (M)Dec 2, 1999 · N219US · Boeing 737281SDR 2000ZZZX261Bulkhead · corrodedIN C/W CESSNA SI MEB 99-10, ULTRASONIC NDT INSPECTION, FOUND ENGINE BEAMS AND CANTED BULKHEAD CORRODED BEYOND THE MATERIALS ACCEPTABLE THICKNESS. CAUSE OF CORROSION WAS FROM LEAKING EXHAUST AND HIGH TURBO TEMPERATURE. TO COVER ENGINE BEAMS AFTER NDT INSPECTIDec 2, 1999 · N330MR · Cessna 340ASDR GAIA99227Bulkhead · crackedFOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. TAIL SKID CAVITY BULKHEAD WEB AT STATION 1183 HAS CRACK ON LEFT SIDE 5 INCHES BELOW FLOOR. REMOVED EXISTING REPAIR AND INSPECTEDec 1, 1999 · N77780 · Boeing 727232SDR USAA991281Bulkhead · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..750 INCH CRACK AT STATION 178, LBL 4.75, WL 198 BULKHEAD. INSTALLED REPAIR DOUBLER PER TR 53-10-07 REV A. (M)Nov 30, 1999 · N421US · Boeing 737401SDR USAA119914Bulkhead · crackedFOUND DURING C-CHECK, RIGHT MAIN WHEEL WELL STATION 870, PRESSUER WEB HAS 3 INCH CRACK JUST OUTBOARD OF KEEL BEAM. INSTALLED WEB REPAIR AT RIGHT MAIN WHEEL WELL RIGHT OF STATION 870, LOWER WEB INBOARD. MATERIAL USED, 2024-T3, .040 INCH, 14 INCH BY 6 INCH. RNov 29, 1999 · N924TS · Boeing 727227SDR QXEA9902514Bulkhead · chafedPDX - ANGLE AND BULKHEAD CHAFFED IN RIGHT WHEELWELL WHERE AFT OUTBOARD EDGE OF GEAR DOOR CONTACTS. REPAIRED IAW HORIZON AIR EA 4-57-328.Nov 29, 1999 · N482US · Fokker F28MK4000SDR RRXA000312Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND AFT PRESSURE BULKHEAD CRACKED AT STA 1766 AND LONGERON 3 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED ENGINEERING SKENov 23, 1999 · N605AL · Doug DC873FSDR T64R442EWABulkhead · crackedREAR PRESSURE BULKHEAD CIRCUMFERENTIAL FRAME TOP RIGHT SIDE HAS CRACK STATION 1766-L3R. NDT CONFIMRED END OF CRACK. CUT OUT CRACK SECTION. FABRICATED REPAIR ANGLES. TREATED AND PRIMED. INSTALLED REPAIR PER EO NR 99-186 WITH APPROVED 8110-3 DATED 9/24/99. Nov 23, 1999 · N605AL · Doug DC873FSDR EIA990306Splice · crackedMZJ - AFT PRESS BULKHEAD, FORWARD SIDE AT THE 9:30 AND 11:00 O''CLOCK POSITIONS THE -15 SPLICES ARE CRACKED. REPAIRED ELONGATED FASTENER HOLES, GOUGE, AND CRACK DAMAGE ASSOCIATED WITH AFT PRESS BULKHEAD TEE-CHORD SPLICE AT L6L-L8L. REPAIRED SEAL PLATE AT TEENov 20, 1999 · N941F · Doug DC933FSDR SWAA991949Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED AT 9 EACH PLACES. REPAIRED BULKHEAD PER DALFORT XEA X2-53-267.Nov 20, 1999 · N359SW · Boeing 7373H4SDR USAA991257Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 665, LBL 31 PRESSURE DECK BELOW CABIN FLOOR BULKHEAD. INSTALLED DOUBLER PER TR 53-60-04. (M)Nov 18, 1999 · N417US · Boeing 737401
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