JASC 5412

Service difficulty reports · 1,087

Reports filed under 5412 · Nacelle/Pylon, Bulkhead/Firewall, 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 = '5412'
  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 QXEA200600715Firewall · crackedYYC - C4 LEFT HAND NACELLE FIREWALL AT XN121 IS CRACKED AT ZN-1.0 AND OUTBOARD YX 12.0. REPAIRED IAW RD 8-54-806 ISSUE 8.Mar 6, 2006 · N350PH · Dhav DHC8202SDR UPS06547182Bulkhead · chafedINSPECTION TYPE:CK NR 1 PYLON AFT BULKHEAD LOWER CORNERS LT & RT SIDE HAVE DEEP CHAFED MARKS ON FOUR LOCATIONS. COMPLIED WITH EA NR 757-5453-27-A1346 HAND UPS EO NR B757-5450-23996-AFeb 28, 2006 · N408UP · Boeing 75724APFSDR UPS06547181Bulkhead · chafedINSPECTION TYPE:CK NR 2 PYLON AFT BULKHEAD LOWER CORNER AREA LT & RT SIDE HAVE DEEP CHAFFED MARKS. COMPLIED WITH EA NR 757-5453-27 A1346 DATED 3/24/06 AND EO B757-5450-23 23996-A.Feb 28, 2006 · N408UP · Boeing 75724APFSDR QXEA200600617Bulkhead · chafedPDX C4 CHECK, RIGHT HAND NACELLE WHEEL WELL AFT BULKHEAD HAS CHAFED BETWEEN GRAVEL GUARD AND RECEPTACLES. REPAIRED IAW SRM 51-20-11, RD 8-54-2139 AND EA 2-54-253.Feb 24, 2006 · N349PH · Dhav DHC8202SDR QXEA200600615Firewall · crackedPDX-C4 CHECK, LEFT HAND NACELLE FIREWALL IS CRACKED AT STATION XN125, ZN0.0 AND YW166, VIEWED THROUGH PANEL 415AL. REPAIRED IAW RD 8-54-806.Feb 19, 2006 · N349PH · Dhav DHC8202SDR QXEA200600616Bulkhead · chafedPDX-C4 CHECK, LEFT HAND NACELLE AFT BULKHEAD HAS CHAFE MARKS FROM GRAVEL GAURD LOCATED 6" UP FROM BOTTOM OF NACELLE. REPAIRED IAW SRM 51-20-11, SRM 51-20-16, SRM 51-20-36 AND SRM 51-20-41.Feb 18, 2006 · N349PH · Dhav DHC8202SDR 06013Bulkhead · chafedREAR ENGINE MOUNT BULKHEAD WEB CHAFED AROUND HYDRAULIC UNION, NAC STA 221.90. REMOVED REPAIR AREA FASTENERS AND DAMAGED MATERIAL IAW B747 SRM 54-14-03. FABRICATED 4 X 9 INCH DOUBLER IAW B747 SRM 54-14-13 FIG 16.Feb 16, 2006 · N706CK · Boeing 747249FSDR QXEA200600401Angle · crackedPDX - LEFT HAND NACELLE: FIREWALL, CLOSING ANGLE, RIGHT HAND TOP IS CRACKED. REPAIRED IAW DASH-200 RD 8-54-1565 AND AMM 20-14-01.Jan 20, 2006 · N375PH · Dhav DHC8202SDR KCSA061557Bulkhead · chafedNR 2 PYLON HYD PRESSURE SUPPLY LINE JAM NUT CHAFING INTO AFT SIDE OF NAC STA 221 BULKHEAD WEB.Jan 2, 2006 · N712CK · Boeing 747122SDR 2005UALA01414Fitting · damagedNR 1 ENGINE AFT SAILTAIL COMPT LWR BKHD FITTING FAIL CONDUCTIVE TEST. NR 1 ENGINE AFT SAILTAIL COMPT LWR BKHD FITTING FAILED CONDUCTIVE TEST BECAUSE OF HEAT DAMAGE. MAJOR REPAIR WAS ACCOMPLISHED PER EVA UA-EVA-50816B.Dec 7, 2005 · N793UA · Boeing 777222SDR UPS05145852Bulkhead · crackedNR 2 ENG LT INLET COWL AFT BULKHEAD WEB CRACKED AT STATIC LPORT LINE UNION TO EEC. REPAIRED BULKHEAD WEB AS PER EO A300-7110-20525.Dec 4, 2005 · N140UP · Airbus A300F4622RSDR CA051128010Fitting · cracked(CAN) DURING CRUISE, IT WAS OBSERVED THAT THE DIRECT READING OIL PRESS GAUGE WAS AT ZERO ON RT ENGINE. AUTO SYN PRESSURE GAUGE, TEMPS, OIL WARNING LIGHT ALL INDICATED ENG WAS FINE. IT WAS THEN FOUND A LEAK ON RT ENG DURING VISUAL CONFIRMATION. ENG WAS SHUTDOWNNov 24, 2005 · Doug DC3CS1C3GSDR LR7A05145Bulkhead · crackedDURING C-6 CHECK PER HC5711, FOUND NR 3 NACELLE OUTBOARD BULKHEAD CRACKED. REPAIRED IAW DRAWING R05-025-06 PER LAC MEA382-54-05-078, NR 0387.Oct 17, 2005 · N403LC · Lkheed 382GSDR 2005FA0001461Firewall · crackedFIREWALL, CRACK IN BASE METAL DUE TO ENGINE VIBRATION. (K)Oct 5, 2005 · Urocop EC135P1SDR DL76S050727Bulkhead · damagedTOOLING DAMAGE WAS INCURRED ON THE MID SPAR BULKHEAD, HOLE COMMON TO UPPER SPAR FITTING AND UPPER SPAR WEB. HOLE WAS OVERSIZED TO REMOVE DAMAGE PER ER/A 099683-14. REF AD 2004-16-12, EO 01-074906-03AD.Aug 11, 2005 · N116DL · Boeing 767332SDR USAA050742Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, NR 2 PYLON LEADING EDGE SKIN. TRIMMED OUT DAMAGE FABRICATED AND INSTALLED FILLER AND DOUBLER. (M)Jun 8, 2005 · N526AU · Boeing 7373B7SDR AMTA200500422Shim · migratedBULKHEAD/ FIREWALL, NR 1 ENGINE STRUT UPPER LINK FITTING HAS MIGRATING SHIM AT OB HORIZONTAL FLANGE PP, STA 174.3. COMPLIED WITH PART 1 OF ERA 757-54R-5870. (K)May 5, 2005 · N519AT · Boeing 75723NSDR UIEA200500064Pylon · crackedNR 4 PYLON OB SKIN FOUND (2) CRACKS ON ACCESS DOOR 482AR CUTOUT CRACK 1INCH TO 1.5 INCH ON BOTH SKIN AND DOUBLER. (K)Apr 26, 2005 · N536MC · Boeing 747228FSDR HE66100341Firewall · crackedFIREWALL IS CRACKED BY FASTNERS AND HAS BEEN REPAIRED SEVERAL TIMES BEFORE. INTEGRITY IS COMPROMISED AND DO NOT WANT ENGINE TO INGEST FOD.Apr 17, 2005 · N202LF · Bolkms BO105LSA1SDR USAA050505Shim · migratedBFM - FOUND PYLON MID BULKHEAD SHIM MIGRATION, NR 1 PYLON MID BULKHEAD SHIMS, UPPER, REPLACEMENT AND REAMNG AFT UPPER HOLE. ACCOMPLISHED PER EO 5402R022A PARTS 2/6. (M)Apr 14, 2005 · N611AU · Boeing 7572B7SDR USAA050504Bulkhead · damagedFOUND PYLON MID BULKHEAD DAMAGED 1.25 INCH DIAMETER BY .030 INCH DEEP, NR 1 PYLON, MID BULKHEAD, UPPER AFT SLEEVER BOLT ATTACH AREA. ACCOMPLISHED SPOTFACING TO REMOVE DAMAGE PER EA 96386. (M)Apr 14, 2005 · N611AU · Boeing 7572B7SDR AMTA200500335Shim · migratedNR 1 ENGINE STRUT MID BULKHEAD HAS MIGRATING SHIMS AT PP STATION 174 LOWER INBOARD AND LOWER OUTBOARD ATTACH POINTS. REPAIRED PER PART 1 OF ERA 757-54R-5835. (M)Mar 31, 2005 · N526AT · Boeing 75723NSDR UIEA200500037Mount · crackedDURING SCHEDULED INSPECTION, NR 4 PYLON, BULKHEAD UPPER CHORD CRACKED AT STATION 270. STOP DRILLED THE CRACK PER 747 SRM 51-10-01. NDT INSPECTED THE REPAIR AREA, INCLUDING HFEC INSPECTION OF ALL TRIMMED FLANGE EDGES AND STOP DRILLED HOLES TO ENSURE CRACK REMMar 23, 2005 · N527MC · Boeing 7472D7BSDR UIEA200500035Bulkhead · crackedDURING SCHEDULED INSPECTION, NR 1 PYLON, THE BULKHEAD UPPER LEFT SIDE FORWARD AND AFT CHORD ANGLES WERE FOUND CRACKED. TRIMMED AND STOP DRILLED THE CRACK PER 747 SRM 51-10-01 NDT INSPECTED THE REPAIRED AREA, INCLUDING HFEC INSPECTION OF ALL TRIMMED FLANGE EDGMar 23, 2005 · N527MC · Boeing 7472D7BSDR UIEA200500036Bulkhead · crackedDURING SCHEDULED INSPECTION, NR 3 PYLON, THE BULKHEAD UPPER LEFT AND RIGHT SIDE FORWARD CHORD ANGLES WERE FOUND CRACKED. STOP DRILLED THE CRACK PER 747 SRM 51-10-01. NDT INSPECTED THE REPAIR AREA, INCLUDING HFEC INSPECTION OF ALL TRIMMED FLANGE EDGES AND STOMar 23, 2005 · N527MC · Boeing 7472D7BSDR UIEA200500029Bulkhead · crackedDURING SCHEDULE MAINTENANCE, THE BULKHEAD UPPER LEFT AND RIGHT SIDE FORWARD CHORD ANGLES WERE FOUND CRACKED, NR 2 PYLON. STOPPED DRILLED THE CRACK END AND NDT INSPECTED TO ENSURE CRACK CONTAINMENT. INSTALLED ALUMINUM REPAIR ANGLES COMMON TO THE UPPER FORWARDMar 21, 2005 · N527MC · Boeing 7472D7BSDR ABXA050081Bulkhead · crackedWEB ON LEFT PYLON BULKHEAD WAS OIL CANNED AND CRACKED AT LOWER INBOARD LIGHTNING HOLE. REPAIRED AREA IAW DC-9 SRM 53-01.Mar 21, 2005 · N975AX · Doug DC941SDR QXEA200500490Firewall · crackedPDX - NR 1 ENGINE NACELLE, AFT FIREWALL INBOARD SIDE POSSIBLE CRACK AT STATION XN125/YW142/ZN9.5. REPAIRED IAW HORIZON AIR EA 2-54-223.Mar 11, 2005 · N366PH · Dhav DHC8202SDR 2004UALA01141Firewall · gougedNR 2 PYLON I/B FIREWALL BULKHEAD IS GOUGED.Nov 19, 2004 · N575UA · Boeing 757222SDR USAA040772Pressure Panel · chafedPIT, C-4, WEB, .5 INCH BY .4 INCH BY .025 INCH DEEP, CHAFED PRESSURE PANEL STATION 145 TOP OF PYLON WEB. INSTALLED DOUBLER IAW EA 95897.Oct 26, 2004 · N613AU · Boeing 7572B7SDR MALA040680Bulkhead · chafedDURING 4K INSPECTION IN LAN, RT NACELLE INNER WALL CHAFED AT NS 205 O/B SIDE OF NACELLE REPAIRED IAW SAAB SRM 54-10-10. AIRCRAFT RETURNED TO SERVICE 9/29/04.Sep 29, 2004 · N368PX · Saab 340BSDR UIEA200400166Bulkhead · crackedDURING SCHEDULED MAINTENANCE INSPECTION, THE BULKHEAD UPPER ASSEMBLY FORWARD ANGLE FRAMES OF THE NR 3 PYLON LHS AND RHS WERE FOUND CRACKED. STOP DRILLED THE CRACK ENDS PER 747 SRM 51-10-01. HFEC INSPECTED TO ENSURE CRACK CONTAINMENT. FABRICATED AND INSTALLESep 21, 2004 · N512MC · Boeing 747230BSDR 2004FA0000816Stiffener · cracked2 INCH LONG CRACK IN LT AREA OF FIREWALL STIFFENER IN AREA OF THE PARKING BRAKE BRACKET MOUNTING. BELIEVED TO BE CAUSED BY FLEXING OF FIREWALL BY APPLICATION OF PARKING BRAKE. THIS IS THE SECOND AC IN FLEET WITH THIS PROBLEM. THIS AREA NEEDS ADDITIONAL REINSep 2, 2004 · N7267H · Cessna 182SSDR 0401286638Bulkhead · crackedDURING H-CHECK FOUND CRACK IN NR 2 PYLON ENGINE MOUNT BULKHEAD FRAME WEB. REPAIRED PER EA 66-165162.Jul 20, 2004 · N638US · Boeing 747251BSDR QXEA200400496Firewall · crackedPDX - NR 2 NACELLE FIREWALL HAS A CRACK .300 INCH LONG AT STATION XN125.00 AND ZN-7.00, LEFT HAND SIDE BY EXHAUST OPENING. REPAIRED IAW RD 8-54-104.Jul 2, 2004 · N359PH · Dhav DHC8202SDR 121JWFirewall · crackedTHE LT AND RT ENGINE ALUMINUM FIREWALLS (P/N 660001-11 / -12 CHANNEL) HAVE DEVELOPED VERTICAL CRACK INDICATIONS AT THE LOWER SHEAR CLIP ATTACHMENT TAB. BOTH THE LT AND RT ENGINE IB LOWER TABS ARE COMPLETELY SHEARED AT THE FLANGE RADIUS.Jun 22, 2004 · N121JW · Gulstm 690ASDR C2XA04SH375Firewall · crackedSHV-DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, STEP 4 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 18, 2004 · N13969 · Emb EMB145SDR SWIA200413455Bulkhead · crackedRIGHT NACELLE OUTBOARD BULKHEAD CRACKED OUT AT OUTBOARD TAILPIPE SUPPORT IN NUT PLATE AREA. FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 51-70-05.Jun 17, 2004 · N196SW · Emb EMB120ERSDR UIEA200400103Bulkhead · crackedD-CHECK, DURING MAINTENANCE INSPECTION. NR 4 PYLON LT SIDE, BULKHEAD STRAPS WERE FOUND CRACKED AT NAC STA 286.0 AND WL 146.5. THE AFT END OF THE STRAP CRACK WAS STOPPED DRILLED AND HFEC INSPECTED TO ENSURE CRACK CONTAINMENT. THE SKIN ACCESS CUT OUT EDGE CHAJun 4, 2004 · N808MC · Boeing 747212BSDR UIEA200400102Bulkhead · crackedD-CHECK, DURING MAINTENANCE INSPECTION. NR 1 PYLON LT SIDE, BULKHEAD STRAPS WERE FOUND CRACKED AT NAC STA 286.0 AND W.L. 146.5, ALSO THE STRUT SKIN ASSEMBLY AT THE AFT LOWER ACCESS CUT OUT EDGE ADJACENT TO THE STRAP CRACK LOCATION WAS FOUND WITH CHAFING DAMAGJun 4, 2004 · N808MC · Boeing 747212BSDR 2004FA0000424Doubler · corrodedDURING ANNUAL INSPECTION FOUND POPPED RIVET HEADS IN FIREWALL DOUBLERS, REMOVED DOUBLERS FOUND EXFOLIATION EXCEEDING 40 PERCENT THICKNESS ON BACK SIDE OF DOUBLERS, REPLACED DOUBLER, RECOMMEND CLOSE INSPECTION OF RIVET HEADS IN THIS AREA.May 29, 2004 · N734BZ · Cessna 172NSDR MALA040282Fireshield · crackedNR 4 ENGINE FIRE LIGHT ILLUMINATED. BLEW 1ST BOTTLE, LIGHT STILL ON, BLEW 2ND BOTTLE, LIGHT DID NOT EXTINGUISH FOR APPROXIMATELY 1 MINUTE. ABORTED TAKEOFF AT 95 KTS. NO VISIBLE INDICATION OF FIRE. INSPECTED BY FIRE DEPARTMENT. CREW DID NOT SWITCH LOOPS TOMar 22, 2004 · N520XJ · Bac AVRO146RJ85ASDR ABXA040075Bulkhead · crackedLT FORWARD PYLON BULKHEAD WAS CRACKED AT BOTTOM AT LT BUTT LINE 44.0. REPAIRED LT FORWARD PYLON BULKHEAD IAW DC-9 SRM 53-03.Feb 9, 2004 · N967AX · Doug DC941SDR CA040130009Cap · cracked(CAN) NOT UNUSUAL FOR THE OLDER STYLE BEAM CAP TO CRACK. THIS IS A REGION THAT IS PART OF OUR INSPECTION PROGRAM. THERE IS A MORE EXTENSIVE INSPECTION AFTER 10,000 HOURS.Jan 30, 2004 · Bell 212SDR AMWA111Firewall · crackedDURING INSPECTION RT ENGINE FIRE WALL WAS FOUND CRACKED AROUND THE O/B SECTION OF WEB APPROX AT 5 INCHES LONG IN VERT POSITION. BEHIND ATTACH ANGLE FOR COWLING. THEN CRACK TURNS HORIZONTAL GOING I/B APPROX 2.5. REPAIRED DAMAGE AREA BY STOP DRILLING CRACK ENJan 2, 2004 · N138ZV · Beech 1900DSDR AWXA200400038Fitting · crackedLCQ - MAJOR REPAIR - DURING C-12 CHECK A .0625 INCH CRACK WAS FOUND IN FORWARD SLEEVE BOLT HOLE OF NR 1 ENGINE PYLON RT MID BULKHEAD FITTING PPS 174.30. MAINTENANCE REAMED OUT HOLE; FABRICATED A BUSHING; INSTALLED REPAIR PART IAW AWA ER 19-5453-04006-SS1.Dec 24, 2003 · N909AW · Boeing 7572G7SDR QXEA200301604Firewall · crackedPDX- CRACK IN FIREWALL JUST OUTBOARD OF CLOSING ANGLE AND ABOVE FIRE LOOP BRACKET. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-54-806.Dec 18, 2003 · N353PH · Dhav DHC8202SDR QXEA200301566Firewall · crackedPDX - LEFT HAND NACELLE INNER FIREWALL IS CRACKED AT THE BEND. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51-40-00.Dec 17, 2003 · N353PH · Dhav DHC8202SDR ENHA20032002BBulkhead · crackedRT NACELLE WAS WEARING AND CRACKING WITH RT AFT LOWER COWL. REPLACED BULKHEADDec 17, 2003 · N90PB · Beech 200BEECHSDR ENHA20032002ABulkhead · crackedRT NACELLE WAS WEARING AND CRACKING AT CONTACT WITH RT AFT LOWER COWL. REPLACED BULKHEADDec 17, 2003 · N90PB · Beech 200BEECH
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