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"

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SDR CAL960530Bulkhead Angle · corrosionDURING INSPECTION, FOUND CORROSION AT LOWER L-ANGLE. REMOVED ATTACH ANGLE FROM AFT BLKHD FABRICATED SHIM FOR ANGLE, ALODINED, PRIMED AND INSTALLED PER IAW 727 SRM 51-30-2, 51-10-1 AND 53-10-2. (M)Mar 16, 1996 · N15774 · Boeing 727227SDR DL73S960651Blkhd Web · crackedTHE BS 178 BULKHEAD WEB WAS FOUND CRACKED BENEATH THE VERTICAL STIFFENERS AT LBL 5.7 AND RBL 5.7. DAMAGE REMOVAL RESULTED IN A 1.45 INCH LEFT AND RIGHT BY 1.2 INCH UP AND DOWN CUTOUT ON THE LT SIDE AND A 1.5 INCH LEFT AND RIGHT BY 5.1 INCH UP AND DOWN CUTOUT Mar 14, 1996 · N330DL · Boeing 737232SDR AALA960399Blkhd Skin · crackedTUL - CRACK IN FORWARD SKIN OF TAIL SKID, LT SIDE, AT ANGLE BRACKET, STA 1183. INSTALLED DOUBLER PER SRM 53-10-2, PAGE 28. TST: 64,360. CYCLES: 46,865. (X)Mar 14, 1996 · N719AA · Boeing 727227SDR AU960274Doubler · cracked(AUS) REAR BULKHEAD RH TAILPLANE ATTACHMENT BRACKET DOUBLER CRACKED THROUGH - FURTHER INSPECTION FOUND REAR BULKHEAD CRACKED IN THESAME AREAMar 13, 1996 · Cessna U206GSDR AU960326Bulkhead · cracked(AUS) FORWARD DOOR POST BULKHEAD CRACKED IN BEND RELIEF NOTCHES ON LH AND RH SIDESMar 12, 1996 · Cessna 182QSDR 96ZZZX1800Bulkhead · crackedDURING 100-HOUR INSPECTION, FOUND RUDDER PEDAL TUBE MOUNTING BLOCKS FLEXING UP AND DOWN WHEN PRESSURE WAS APPLIED TO PEDALS. FURTHER INSPECTION OF THE PROBLEM REVEALED CRACKS IN THE LOWER BULKHEADS (172RG PART CATALOG, FIGURE 19, INDEX 16 AND INDEX 20) BELOW Mar 10, 1996 · N9561B · Cessna 172RGSDR 96ZZZX1799Bulkhead · crackedDURING 100-HOUR INSPECTION, FOUND RUDDER PEDAL TUBE MOUNTING BLOCKS FLEXING UP AND DOWN WHEN PRESSURE WAS APPLIED TO PEDALS. FURTHER INSPECTION OF THE PROBLEM REVEALED CRACKS IN THE LOWER BULKHEADS (172RG PART CATALOG, FIGURE 19, INDEX 16 AND INDEX 20) BELOW Mar 10, 1996 · N9561B · Cessna 172RGSDR 96ZZZX1798Bulkhead · crackedDURING 100-HOUR INSPECTION, FOUND RUDDER PEDAL TUBE MOUNTING BLOCKS FLEXING UP AND DOWN WHEN PRESSURE WAS APPLIED TO PEDALS. FURTHER INSPECTION OF THE PROBLEM REVEALED CRACKS IN THE LOWER BULKHEADS (172RG PART CATALOG, FIGURE 19, INDEX 16 AND INDEX 20) BELOW Mar 10, 1996 · N9303D · Cessna 172RGSDR 96ZZZX1797Bulkhead · crackedDURING 100-HOUR INSPECTION, FOUND RUDDER PEDAL TUBE MOUNTING BLOCKS FLEXING UP AND DOWN WHEN PRESSURE WAS APPLIED TO PEDALS. FURTHER INSPECTION OF THE PROBLEM REVEALED CRACKS IN THE LOWER BULKHEADS (172RG PART CATALOG, FIGURE 19, INDEX 16 AND INDEX 20) BELOW Mar 10, 1996 · N9303D · Cessna 172RGSDR 96ZZZX1796Bulkhead · crackedDURING 100-HOUR INSPECTION, FOUND RUDDER PEDAL TUBE MOUNTING BLOCKS FLEXING UP AND DOWN WHEN PRESSURE WAS APPLIED TO PEDALS. FURTHER INSPECTION OF THE PROBLEM REVEALED CRACKS IN THE LOWER BULKHEADS, 172RG PART CATALOG, FIGURE 19, INDEX 16 AND INDEX 20), BELOWMar 10, 1996 · N115HM · Cessna 172RGSDR 96ZZZX1795Bulkhead · crackedDURING 100-HOUR INSPECTION, FOUND RUDDER PEDAL TUBE MOUNTING BLOCKS FLEXING UP AND DOWN WHEN PRESSURE WAS APPLIED TO PEDALS. FURTHER INSPECTION OF THE PROBLEM REVEALED CRACKS IN THE LOWER BULKHEADS (172RG PART CATALOG, FIGURE 19, INDEX 16 AND INDEX 20) BELOW Mar 10, 1996 · N115HM · Cessna 172RGSDR DL72K961463Bulkhead Web · crackedTHE BS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 26. THERE IS A 1 INCH CRACK AT WL 166.5. REPAIRED PER ER/A 303276-14.Mar 9, 1996 · N491DA · Boeing 727232SDR DL72K960743Bulkhead · crackedA .5 INCH CRACK WAS FOUND IN THE 1183 BULKHEAD AT LBL 8 AND WL 168 AS A RESULT OF INSPECTIONS PER SI 4-59275-12. ACCOMPLISHED REPAIRS PER DL ERA 303278-14AD.Mar 9, 1996 · N491DA · Boeing 727232SDR RAAAB196007Bulkhead · crackedDURING SCHEDULED C-CHECK INSPECTION OF NLG WHEEL WELL, FOUND LEFT PRESSURE BULKHEAD CRACKED AT BS 259. REPAIRED PER SRM 51-4-2. (M)Mar 8, 1996 · N831RV · Boeing 72722CSDR DL72K960531Blkhd Beam · crackedFOUND DURING A-2 LETTER CHECK - 1.50 INCH CRACK VERTICAL BEAM BS 1183 BLKHD AT RBL 8. REPAIRED PER MM 53-11-0, PG 811.Mar 8, 1996 · N491DA · Boeing 727232SDR 96ZZZX2392Bulkhead · crackedDURING ANNUAL INSPECTION, FOUND AFT BULKHEAD AT FS 230.18 CRACKED AT LEFT RUDDER CABLE CUT OUT. THIS BULKHEAD HAD PREVIOUSLY CRACKED AT THE RIGHT RUDDER CABLE CUT OUT AND WAS REPAIRED. AD 72-07-09 AND CESSNA SB SE72-3 BOTH PERTAIN TO THIS AREA AND DO NOT ALLMar 8, 1996 · N70802 · Cessna 182MSDR USAA970095Bulkhead · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO .5 INCH CRACKS BS 178 RBL 4.75 WL 198 WL 201 BULKHEAD. STOP DRILLED AND INSTALLED DOUBLER, REPAIRED PER TR 53-10-07 REV A. (M)Mar 7, 1996 · N519AU · Boeing 7373B7SDR DLL13960514Blkhd Web · crackedTHE FS 1212 BLKHD WAS FOUND WITH A 7 INCH VERTICAL CRACK AT RBL 22.5. THE CRACK WAS CUT OUT AND A REPAIR FILLER AND DOUBLER WERE INSTALLED PER DL ERA 273431-14A.Mar 7, 1996 · N786DL · Lkheed 10113851SDR CA970311031Bulkhead · cracked(CAN) CRACKS AND PULLED RIVETS ON LOWER SUPPORT. LEFT HEAD BULKHEAD P/N 206-031-107-117H CRACKED. INNER SKIN CRACKED AT FS98 AND BL9.Mar 7, 1996 · Bell 206BSDR AU960990Web · cracked(AUS) REAR PRESSURE BULKHEAD WEB LOCATED BETWEEN HORIZONTAL BEAMS II AND III AND VERTICAL BEAMS 425L AND 1050L CRACKED VERTICALLY - CRACK LENGTH 52MM (2IN) - FOUND DURING EDDY CURRENT INSPECTION IAW ER F28-53-10-15K PART 4Mar 5, 1996 · Fokker F28MK4000SDR DLM88960915Blkhd Web · damagedTHE P-DOME LOWER WEB AT STA 1338 WAS DAMAGED DURING A TAIL STRIKE INCIDENT. THE DAMAGE IN THE LOWER WEB WAS SPLICED PER DL ERA 273378-14.Mar 3, 1996 · N957DL · Doug MD88SDR DL73S960510Blkhd Web · crackedDURING ACCOMPLISHMENT OF S.I. 3-69482-12, A 1 INCH CRACK WAS FOUND IN THE RADIUS OF THE VERTICAL CHORD OF THE LBL 5.7 VERTICAL STIFFENER AT BS 178. THE BULKHEAD WEB WAS ALSO FOUND CRACKED AT SEVERAL LOCATIONS BETWEEN WL 184.5 AND 207 AND LBL 5.7 TO RBL 5.7. Mar 3, 1996 · N326DL · Boeing 737232SDR CAL960332Blkhd T-Cap · corrodedHOU - INSPECTION FOUND T-CAP CORRODED AT AFT BULKHEAD STATION 110 IN NLG WHEEL WELL RIGHT TUNNEL. THE CORROSION WAS REMOVED AND THE AREA WAS TREATED IAW SRM 51-10-3. (M)Mar 3, 1996 · N19504 · Doug DC932SDR UPS96805825Blkhd Doubler · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FWD PRESS BULKHEAD.Mar 2, 1996 · N811UP · Doug DC873FSDR MWEA96053Blkhd Stiffener · crackedDURING INSPECTION, FOUND RADIAL STIFFENER CRACKED AT 9 O'CLOCK POSITION ON AFT PRESSSURE BULKHEAD. INSTALLED DOUBLE ANGLE REPAIR IAW SRM 53-01 FIG 2 SHT 4.Mar 2, 1996 · N80ME · Doug DC914SDR 96FDEA00381Blkhd Support · corrodedREMOVED VERTICAL CHORD TO ACCESS TERMINAL FITTING AND DISCOVERED CORROSION ON BULKHEAD SUPPORT CHANNEL, BS 1342 WL 238 TO 246 RBL 24. REMOVED AND REPLACED BS 1342 BULKHEAD SUPPORT CHANNEL OF BS 1342 RBL 24 WL 193 TO 258.Mar 1, 1996 · N194FE · Boeing 72722SDR N3VR96010Blkhd Fitting · corrosionREF N/R 3592, FS 1183 BULKHEAD TO FLOOR ATTACH FITTING IS BLOWN IN CORNER LEFT SIDE STRINGER 17 LEFT. REMOVED AND REPLACED FITTING IAW SRM 51-30-2. (M)Feb 28, 1996 · N590CA · Boeing 727231SDR 96FDEA00351Blkhd Web · corrosionON REMOVAL OF THE REAR, UPPER AND LOWER SPAR CHORDS, FOUND 870 BULKHEAD WEB HAS CORROSION, LBL TO RBL 70 WL 174 TO 140. REMOVED AND REPLACED 870 BULKHEAD WEB.Feb 28, 1996 · N194FE · Boeing 72722SDR AU960382Bulkhead · cracked(AUS) RH FORWARD DOOR POST BULKHEAD CRACKED IN AREA OF BEND RELIEF NOTCH - AD/CESSNA206/48 AMDT1 CARRIED OUT APPROXIMATELY 200 HOURSPREVIOUSFeb 27, 1996 · Cessna U206GSDR 96ZZZM633Blkhd Web · crackedMCI - DURING SPECIAL CHECK, FOUND AFT BULKHEAD WEB CRACKED AT INBOARD SIDE OF WHEEL WELL STATION 1363, WL 102. REPAIRED PER SRM 53-11-00 AND 51-10-02. (M)Feb 27, 1996 · N11003 · Lkheed 10113851SDR 96ZZZM632Blkhd Web · crackedMCI - DURING SPECIAL CHECK, FOUND MULTIPLE CRACKS IN BULKHEAD AND STIFFENER WEBS, FS 1363, RBL 42.5, WL 102 TO WL 143. REPAIRED PER SRM 51-10-02 AND 53-11-00. (M)Feb 27, 1996 · N11003 · Lkheed 10113851SDR USAA960284Blkhd Fishplate · crackedPIT - DURING SIP VISIT INSPECTION, ACCOMPLISHED SIP 53-10-06 AND FOUND 4 INCH AND 3.5 INCH CRACK IN FRONT PRESSURE BULKHEAD FISHPLATE BETWEEN STRINGER 72 AND 73. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-02-18 PG 28. (M)Feb 26, 1996 · N478US · Fokker F28MK4000SDR USAA960063Bulkhead Angle · crackedPIT - DURING Q- CHECK, FOUND 1 INCH CRACK IN ANGLE AT CTR PRESSURE BULKHEAD ANGLE CRACK, STRINGER 64 RHS, STATION 14911. VISUALLY DETECTED AND VERIFIED BY NDT. INSTALLED REPAIR ANGLES PER USAIR EA NR 46216. (M)Feb 26, 1996 · N865US · Fokker F28MK0100SDR SWAA960131Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD BS 178 CRACK ON LEFT SIDE AT WL 194 IN RADIUS OF SIDE CHORD. REPAIRED PER SWA ACO 96-0017.Feb 26, 1996 · N54SW · Boeing 7372H4SDR SWAA960126Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD SKIN CRACKED AT BS 178 WL 235 APPROX LBL 13. REPAIRED PER BOEING SRM.Feb 26, 1996 · N54SW · Boeing 7372H4SDR SWAA960125Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND APU COMPARTMENT UPPER BULKHEAD CRACKED AT LIGHTENING HOLE BETWEEN BS 1136 AND 1121 RIGHT SIDE AND BETWEEN BS 1121 AND 1104 LEFT SIDE. REPAIRED PER BOEING SRM.Feb 26, 1996 · N54SW · Boeing 7372H4SDR SWAA960124Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE BULKHEAD CRACKED 2 PLACES, ONE AT LBL 10 AND AT LBL 11, WL 219. REPAIRED PER BOEING SRM.Feb 26, 1996 · N54SW · Boeing 7372H4SDR QXEA9600080Blkhd Web · crackedPDX - FRONT PRESSURE BULKHEAD CRACK IN AFT SIDE OF WEB AT HORIZONTAL BEAM NR VI. CRACK FOUND DURING C-CHECK. CRACK REPAIRED I/A/W SRM. AIRCRAFT RETURNED TO SERVICE.Feb 26, 1996 · N802PH · Fokker F28MK1000SDR IXXA9632Blkhd Cover · crackedDURING THE D-CHECK INSPECTION, FOUND CRACKS ON THE BULKHEAD COVER AT FS 857.125. REPAIR WAS PERFORMED PER DACO SRM 51-1-4, 51-1-8, 51-1-21, AND 53-2-0. (X)Feb 26, 1996 · N820BX · Doug DC871SDR 96FDEA00341Blkhd Web · cutWHILE WORKING NR0788, FOUND A CUT IN 950 BULKHEAD VERTICAL WEB BL 0 WL 208 AFT SIDE. REPAIRED CUT IN 950 BULKHEAD VERTICAL WEB AT BL 0 WL 208 AFT SIDE PER FEDEX SRM 53-10-9 FIG 2.Feb 26, 1996 · N194FE · Boeing 72722SDR USAA960280Bulkhead · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH LONG CRACK FUSELAGE BULKHEAD STATION 178, WL 200, RBL 6 INCHES. INSTALLED REPAIRED DOUBLER, REPAIRED PER TR 53-10-11. (M)Feb 24, 1996 · N243US · Boeing 737201SDR CAL960292Blkhd Skin · corrodedHOU - INSPECTION FOUND CORROSION IN SKIN AT AFT PRESSURE BULKHEAD FORWARD FACE LOWER CENTER AREA. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-5. (X)Feb 24, 1996 · N17812 · Doug DC982SDR 96ZZZX1260Fitting · corrodedTHESE FITTINGS ARE MADE OF STEEL, DISSIMILAR METAL CORROSION HAD STARTED BETWEEN SKIN AND FITTINGS WHERE THEY ATTACH. ON TWO OF FITTINGS, SEVERAL RIVETS HAD POPPED THE HEADS OFF WHERE ATTACHED TO SKIN. THESE FITTINGS ATTACH FORWARD OF THE AFT BULKHEAD WHERE Feb 22, 1996 · N3927W · Piper PA32260SDR 96ZZZX1259Fitting · corrodedTHESE FITTINGS ARE MADE OF STEEL, DISSIMILAR METAL CORROSION HAD STARTED BETWEEN SKIN AND FITTINGS WHERE THEY ATTACH. ON TWO OF FITTINGS, SEVERAL RIVETS HAD POPPED THE HEADS OFF WHERE ATTACHED TO SKIN. THESE FITTINGS ATTACH FORWARD OF THE AFT BULKHEAD WHERE Feb 22, 1996 · N3927W · Piper PA32260SDR 96ZZZX1258Fitting · corrodedTHESE FITTINGS ARE MADE OF STEEL, DISSIMILAR METAL CORROSION HAD STARTED BETWEEN SKIN AND FITTINGS WHERE THEY ATTACH. ON TWO OF FITTINGS, SEVERAL RIVETS HAD POPPED THE HEADS OFF WHERE ATTACHED TO SKIN. THESE FITTINGS ATTACH FORWARD OF THE AFT BULKHEAD WHERE Feb 22, 1996 · N3927W · Piper PA32260SDR 96ZZZX1257Fitting · corrodedTHESE FITTINGS ARE MADE OF STEEL, DISSIMILAR METAL CORROSION HAD STARTED BETWEEN SKIN AND FITTINGS WHERE THEY ATTACH. ON TWO OF FITTINGS, SEVERAL RIVETS HAD POPPED THE HEADS OFF WHERE ATTACHED TO SKIN. THESE FITTINGS ATTACH FORWARD OF THE AFT BULKHEAD WHERE Feb 22, 1996 · N3927W · Piper PA32260SDR 9606549605Bulkhead · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 1046 CANTED BULKHEAD UPPER CAP BETWEEN LONGERONS 3L TO 6L. REPAIRED CAP PER EA 99-108995.Feb 22, 1996 · N605NW · Doug DC932SDR 9605491149Blkhd Web · corrodedDURING T-CHECK, FOUND CORROSION ON THE FS 2007 AFT PRESSURE BULKHEAD WEB AND STIFFENER AT LBL 32, Z = -40. REPAIRED WEB (P/N NJC6040-501) AND STIFFENER (P/N NJC6040-109) PER EA 11-99304.Feb 22, 1996 · N149US · Doug DC1040SDR AU960202Bulkhead · cracked(AUS) LH AND RH SIDE FORWARD DOORPOST BULKHEAD CRACKED - FOUND DURING INSPECTION IAW AD/C180/75 AMDT1Feb 21, 1996 · Cessna 182MSDR AU960203Bulkhead · cracked(AUS) STRUT ATTACHMENT BULKHEAD CRACKED ON LH SIDE - CRACK STARTS AT BEND RELIEF NOTCH AND GOES UNDER THE STRUT ATTACHMENT FITTING -CRACK LENGTH APPROXIMATELY 9.525MM (0.375IN)Feb 19, 1996 · Cessna R182
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