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 AWXA0001323Bulkhead · chafedNR 2 PYLON O/B STRUCTURE CHAFED AT FWD END ABOVE ENGINE. REMOVED BLKHEAD; LOCATED, DRILLED AND INSTALLED NEW BLKHEAD (P/N 65-79415-92) IAW SRM 51-30-02.Feb 9, 2001 · N180AW · Boeing 737277SDR QXEA0100064Angle · cutPDX- RIGHT HAND ENGINE FIREWALL AFT SIDE OUTBOARD ANGLE IS CUT INTO BY TGT HARNESS. REPAIRED IAW DHC-8 RD8-54-991.Jan 18, 2001 · N824PH · Dhav DHC8102SDR MWEA010079Bulkhead · damagedRIGHT HAND PYLON BULKHEAD LOWER WEB AT STATION 786 HAS SEVERAL ELONGATED HOLES. FABRICATED AND INSTALLED NEW WEB.Jan 18, 2001 · N500ME · Doug DC914SDR QXEA0100063Firewall · crackedPDX- NR 2 FIREWALL CRACKED AT INBOARD SIDE AT CORNER OF CUTOUT ON CLOSING MEMBER. REPAIRED IAW DHC-8 RD8-54-109, PAGE 3.Jan 16, 2001 · N824PH · Dhav DHC8102SDR QXEA0100062Angle · chafedPDX- LEFT HAND ENGINE FIREWALL APERTURE ANGLE IS CHAFED ON FRONT FLANGE RADIUS AND EDGE OF ANGLE NEAR TGT HARNESS AREA. REPAIRED IAW DHC-8 RD8-54-991.Jan 16, 2001 · N824PH · Dhav DHC8102SDR MWEA010060Bulkhead · misdrilledRT PYLON BULKHEAD AT STATION 786 HAS IMPROPERLY INSTALLED AND INPROPERLY SPACED HI-LOKS BETWEEN LONGERONS 9 RIGHT AND 10 RIGHT. FABRICATED AND INSTALLED REPLACEMENT WEB.Jan 16, 2001 · N500ME · Doug DC914SDR COMA0110012Firewall · crackedTHE AIRCRAFT HAS A CRACK IN THE APU FIREWALL WEB. INSTALLED A DOUBLER IN ACCORDANCE WITH AERODESIGN REPORT NR 2677-3.Jan 12, 2001 · N267CA · Emb EMB120RTSDR 20010209CW007Firewall · crackedFOUND 1.8 IN LONG CRACK IN FIREWALL. CRACK IS LOCATED BEHIND COWL SHOCKMOUNT BRACKET AT RIGHT FIREWALL STEP. REPAIRED CRACK IN ACCORDANCE WITH SB.Jan 11, 2001 · N9421Z · Cessna 172RSDR MWEA010018Bulkhead · damagedUPPER WEB ON LEFT HAND PYLON BULKHEAD AT STATION 786 HAS SEVERAL IMPROPERLY SPACED HOLES ON OUTBOARD EDGE. FABRICATED AND INSTALLED NEW WEB.Jan 8, 2001 · N500ME · Doug DC914SDR 0004556622Chord · crackedDuring "L" check found crack on the upper chord at the rear engine mount bulkhead NAC station 222 number one pylon. Repaired per EA 66-180413.Nov 20, 2000 · N622US · Boeing 747251BSDR AALA20004075Bulkhead · crackedAFW - RIGHT PYLON MID BULKHEAD HAS GOUGE BLENDED ON EDGE. BLEND OUT DAMAGE, DYE CHECK FOR CRACKS, ROTO-PEEN, ALODINED AND PRIMED THE BLENDED AREA. IT IS ACCEPTABLE FOR RETURN SERVICE WITH NOTED CONDITION. MRB 757-1624. (M)Nov 1, 2000 · N670AA · Boeing 757223SDR DL767002097Bulkhead · wornHOLE FOUND ELONGATED IN THE AFT BULKHEAD OF THE NR 1 PYLON ON THE LOWER FWD GSE HOLE (6TH FROM THE TOP). THE RIVET HOLES INSTALLED PER BOEING S/B 767-54-0010 WERE DOUBLE DRILLED. ADDITIONAL WEAR DAMAGE FOUND JUST BENEATH THE GSE HOLE. ER/A 396279-14.Oct 18, 2000 · N110DL · Boeing 767232SDR 20001121SH004Firewall · crackedFIREWALL HAD CRACK APPROXIMATELY .75 INCH STARTING AT LOWER LEFT COWL MOUNT TOWARDS BATTERY BOX MOUNT. CESSNA SB 98-53-02. PERTAINS TO THIS SITUATION, BUT IS ONLY ON 172R MODEL. (X)Oct 17, 2000 · N74GW · Cessna 172SSDR QXEA0002862Firewall · crackedPDX- RIGHT HAND SIDE OF FIREWALL IS CRACKED APPROXIMATLY 24.5 INCHES ABOVE OIL COOLER DECK AT FIRE DETECTOR STAND OFF BRACKET. REPAIRED IAW DHC-8 RD 8-54-109.Sep 30, 2000 · N366PH · Dhav DHC8202SDR DL767001798Bulkhead · damagedFOUR HOLES FOUND ELONGATED IN THE AFT BULKHEAD OF BOTH PYLONS. ON THE NR 1 PYLON I/B FLANGE, THE UPPER HOLE, THE SECOND FROM THE TOP, AND THE 5TH GSE FASTENER HOLE FROM THE TOP WERE DAMAGED. ON THE NR 2 PYLON, THE UPPER GSE HOLE ON THE I/B FLANGE WAS FOUND WSep 13, 2000 · N105DA · Boeing 767232SDR 0003189881Bulkhead · crackedTAIL INTERIOR- CRACKED LIGHTENING HOLE IN WEB OF LEFT PYLON BULKHEAD AT STA 1209 BETWEEN L11 AND L14. CUT OUT DAMAGED WEB, DRILLED REPLACEMENT WEB FABRICATED DOUBLER PER EA 98-177275 AND SRM 51-30-2.Sep 10, 2000 · N676MC · Doug DC951SDR DL767001647Bulkhead · damagedWEAR DAMAGE FOUND ON THE I/B FLANGES OF BOTH THE NR 1 AND NR 2 PYLON AFT ENGINE MOUNT BULKHEADS. THIS DAMAGE IN CONJUNCTION WITH MULTIPLE NUT PLATE ATTACH RIVETS ON THE NR 1 PYLON GSE ATTACH HOLE REQURED THE HOLE TO BE ENLARGED TO INCORPORATE NEAREST ATTACH RAug 24, 2000 · N115DA · Boeing 767232SDR QXEA0002357Firewall · damagedYXX- LEFT HAND NACELLE FORWARD FIREWALL INBOARD LOWER AREA HAS TWO RIVETS WITH HEADS CHAFED OFF AND AREA OF CHAFING JUST ABOVE XM107-80 AND ZM1.5-00. REPAIRED IAW RD 8-54-1333.Aug 20, 2000 · N822PH · Dhav DHC8102SDR QXEA0002356Firewall · chafedYXX- CHAFE DAMAGE ON NR 2 FORWARD OUTBOARD FIREWALL WEB AT STATION YN107.18 AND ZN-10.50. REPAIRED IAW DHC-8 RD 8-54-1330, 8-54-081, AND SRM 51-00-06.Aug 18, 2000 · N822PH · Dhav DHC8102SDR DL767001645Bulkhead · wornTHE UPPER GSE FASTENER HOLE IN THE AFT ENGINE BULKHEAD OF THE NR 2 PYLON WAS WORN AND ELONGATED. ER/A 334822-14.Aug 18, 2000 · N112DL · Boeing 767232SDR QXEA0002352Firewall · crackedYXX- LEFT HAND NACELLE FIREWALL EXTENSION TUBE IS CRACKED AT WELD AND BOLT HOLES. REPAIRED IAW DHC-8 RD 8-54-16, AND 8-54-8.Aug 16, 2000 · N822PH · Dhav DHC8102SDR UPS00233656Firewall · crackedINSPECTION TYPE:C, SUSPECT CRACK ON WEB OVER ENGINE NR 2 HORIZONTAL FIRE WALL BS 1376 RT. HFEC C/O, CRACK CONFIRMED. FABRICATED AND INSTALLED WEB IAW DRAWING 657555.Aug 15, 2000 · N925UP · Boeing 72731CSDR QXEA0002354Firewall · crackedYXX- RIGHT HAND NACELLE FIREWALL FOUND CRACKED ABOVE INBOARD END OF OIL COOLER. REPAIRED IAW DHC-8 SRM 51-40-11, 54-00-00 PAGE 1 AND 20-21-18.Aug 11, 2000 · N822PH · Dhav DHC8102SDR MWEA00431Stiffener · crackedMKE - FOUND LEFT PYLON BULKHEAD HAS A CRACKED STIFFENER 3RD FROM TOP. FABRICATED AND INSTALLED NEW STIFFENER. (M)Aug 4, 2000 · N805ME · Doug DC981SDR COMA0010313Bulkhead · crackedUPON COMPLIANCE OF 1C-CHECK TASK 433-01Z, THE LEFT NACELLE FRAME 14 EXHAUST PAN SUPPORT BULKHEAD WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACCORDANCE WITH EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 33712-1, IR-7-2Aug 3, 2000 · N247CA · Emb EMB120RTSDR 00FDEA00367Firewall · crackedDURING ROUTINE INSP NR 2 ENG FIREWALL FOUND CRACKED AT APPROX 8 O''CLOCK POS AT FIRELOOP BRACKET. STOP DRILLED THE CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 54-10-1.Jun 5, 2000 · N101FE · Boeing 72722CSDR CA000801022Firewall · loose(CAN) FIRE WALL NEEDS TO BE STIFFENED.May 31, 2000 · Rhnflu EA300LSDR EIA2000138Fitting · crackedDURING ACCOMPLISHMENT OF EO54-747-1042-90, NR 3 PYLON REAR ENGINE MOUNT BULKHEAD FITTING FOUND CRACKED. NR 3 PYLON REAR ENG MOUNT BULKHEAD FITTING REPLACED PER SRM 51-10-01 PAGE 18 AND REWORKED PER EO54-747-1042-90. (M)Apr 21, 2000 · N482EV · Boeing 747212BSDR EIA2000137Fitting · crackedDURING ACCOMPLISHMENT OF EO54-747-1042-90, NR 1 PYLON REAR ENGINE MOUNT BULKHEAD FITTING FOUND CRACKED. NR 1 PYLON REAR ENGINE MOUNT BULKHEAD FITTING REPLACED PER SRM 51-10-01 PAGE 18 AND REWORKED PER EO54-747-1042-90. (M)Apr 21, 2000 · N482EV · Boeing 747212BSDR EIA2000136Fitting · crackedDURING ACCOMPLISHMENT OF EO54-747-1042-90, NR 4 PYLON REAR ENGINE MOUNT BULKHEAD FITTING FOUND CRACKED. NR 4 PYLON REAR ENGINE MOUNT BULKHEAD FITTING REPLACED PER SRM 51-10-01 PAGE 18 AND REWORKED PER EO 54-747-1042-90. (M)Apr 21, 2000 · N482EV · Boeing 747212BSDR EIA2000135Web · crackedFOUND NR 3 PYLON MID SPAR BULKHEAD WEB NAC STATION 205 CRACKED WITH PREVIOUS STANDARD REPAIR. REF SRM 54-10-03 PAGE 30. MID SPAR WEB REPAIRED PER SRM 54-10-03 FIG 12. (M)Apr 21, 2000 · N482EV · Boeing 747212BSDR GAIA00208Firewall · crackedDURING ZERO B-CHECK AT STAMBAUGH/BQK, FOUND NR 1 ENGINE PYLON FIREWALL CRACKED OUT AT NAC STATION 146. REPAIRED IAW SRM 54-10-0 AND BOEING REPAIR SKETCH STS-BQK-99-00003H/00005H. REPAIR CARRIED OUT ON STS WORK ORDER SROO522, NR0018. AIRCRAFT RETURNED TO SERApr 12, 2000 · N1269Y · Boeing 727243SDR UPS00232256Web · crackedINSPECTION TYPE:C, LEFT AND RIGHT WEBS AT BS 1387 OVER THE ENGINE 2 HORIZONTAL FIREWALL ARE CRACKED. LT WEB AND BODY SKIN ATTACH TEE REPLACED IAW DRAWING 65-17555.Apr 5, 2000 · N912UP · Boeing 72762CSDR P2EA00192Firewall · crackedSJO - DURING C-CHECK, FOUND THE NR 2 ENGINE FIREWALL RIGHT SECTION NAC STATION 120 WEB WITH CRACK 3 INCHES LENGTH, WIDTH .006 INCHES. REPLACED THE NR 2 ENGINE FIREWALL RIGHT SECTION NAC STATION 120 WEB P/N 65-53558-8 IAW BOEING SRM 51-10-1 PAGE 5. (M)Apr 3, 2000 · N209US · Boeing 737222SDR QXEA0000473Firewall · crackedPDX - LEFT-HAND ENGINE NACELLE FIREWALL WAS CRACKED DIRECTLY BELOW FUEL PRESSURE LINE FIREWALL FITTING. REPAIRED IAW HORIZON AIR EA 4-54-89, FOKKER SRM 51-31-01, SRM 51-31-05 AND SRM 51-30-2.Feb 13, 2000 · N488US · Fokker F28MK4000SDR 20000405SH024Firewall · chafedAFTER REMOVING THE ENGINE FOR FOD, NOTICED THERE WERE TWO RUBBED INDENTATIONS TO THE UPPER LEFT PORTION OF THE FIREWALL. UPON FURTHER INVESTIGATION, NOTED THE BLEED VALVE BOLT HEADS WERE WORN CONSIDERABLY. THIS WAS THE ORIGINAL FACTORY INSTALLATION. (X)Feb 1, 2000 · N611BP · Doug 600NSDR ASOA00011Frame · crackedDURING C-CHECK, FOUND LT AND RT NACELLE FRAME NR 1 CRACKED. MAINTENANCE REPLACED CRACK FRAMES PER EO 120-54-0034. AIRCRAFT RETURNED TO SERVICE. (X)Jan 22, 2000 · N273AS · Emb EMB120RTSDR QXEA9902250Firewall · crackedPDX - THERE IS A CRACK IN THE AFT FIREWALL OF THE NR 2 ENGINE, OUTBOARD SIDE, AT BEND IN MATERIAL JUST ABOVE FIRE DETECTION LOOP BRACKET. REPAIRED IAW HORIZON AIR EA 9-54-219 AND RD 8-54-430.Oct 29, 1999 · N827PH · Dhav DHC8102SDR QXEA9902256Firewall · crackedPDX - THERE IS A CRACK IN THE AFT FIREWALL OF THE NR 1 ENGINE, ON THE INBOARD SIDE, AT THE BEND IN MATERIAL JUST ABOVE THE FIRE DETECTION LOOP BRACKET. REPAIRED IAW RD 8-54-806.Oct 20, 1999 · N827PH · Dhav DHC8102SDR MWEA99540Bulkhead · damagedFABRICATED AND INSTALLED DOUBLERS PER SRO 5936993 DRAWING FOR STATION 786 LEFT AND RIGHT PYLON BULKHEAD.Aug 26, 1999 · N600ME · Doug DC914SDR 99FDEA00463Firewall · crackedLT FWD INTERNAL COMP OVERTOP CF NR 2 ENG HORZ FIREWALL/PYLON, 1 1/2 CRACK IN HORIZONTAL ANGLE RADIUS UPPER SECTION OF COMP. REPLACED CRACKED CHORD ANGLE PER SRM 51-16-1.Aug 9, 1999 · N185FE · Boeing 72722SDR MWEA99458Firewall · gougedLEFT PYLON FIREWALL UPPER CAP IS GOUGED. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR.Jul 28, 1999 · N209ME · Doug DC932SDR F3LA99106Firewall · crackedDEN - DURING C-CHECK, INSPECTION REPORTED FIREWALL FROM CLAMP 12 O'CLOCK POSITION AT NACELLE STA 204.5 (6 INCHES AFT OF FORWARD ENGINE MOUNT ON NACELLE). MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 51-70-13. TC: 27,402. (X)Jul 16, 1999 · N578US · Boeing 737301SDR UPS99230121Firewall Web · crackedINSPECTION TYPE:C, STRUCTURE OVER NR 2 ENGINE HORIZ FIREWALL LEFT AND RIGHT WEBS AT BS 1376 ARE CRACKED. FABRICATED AND INSTALLED WEBS IAW DRG NR 65-17555.Jul 6, 1999 · N928UP · Boeing 72722CSDR EIA990229Firewall · crackedHKG - DURING C/D CHECK, NR 1 ENGINE TURBINE SECTION FIREWALL HAS A CRACK AT THE 3 O'CLOCK POSITION. FIREWALL CRACK REPAIRED PER RS-R-72-53-34080, 8110-3. (M)Jul 6, 1999 · N481EV · Boeing 747132SDR AT9900391Blkhd Frame · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND ON THE CABIN LEFT FORWARD PYLON BULKHEAD AFT SIDE LOWER FRAME/FLOOR AT BS 965 CORRODED. CUT, DRILLED, AND DEBURRED NEW ANGLE (SUPPORT). LOCATED, CUT, DRILLED, TRIMMED NEW ANGLE REPAIR, ALODINED, PRIMED, AND May 15, 1999 · N817AT · Doug DC932SDR ABXA9900320Rib · crackedDURING C-CHECK, FOUND RIB UNDER PANEL AT TOP OF NR 2 PYLON, STATION 1038-1048 CRACKED. REPAIRED RIB IAW DC9 SRM 54-01.Apr 19, 1999 · N943AX · Doug DC931SDR QXEA9900556Firewall · crackedYXX - CRACK IN NR 1 FIREWALL, INBOARD SIDE JUST ABOVE CUT OUT FOR ATTACHMENT HARDWARE OF MAIN LANDING GEAR RETRACT ACTUATOR ATTACH FITTING. REPAIRED IAW DASH 8 RD 8-54-10147, CONAIR EO 2254 AND HORIZON AIR EA 9-54-193.Mar 31, 1999 · N816PH · Dhav DHC8102SDR ABXA9900253Bulkhead · crackedDURING C-CHECK, FOUND LEFT PYLON SUPPORT BULKHEAD CRACKED AT STATION 965 LOWER ATTACH ANGLE. REPLACED LEFT PYLON SUPPORT BULKHEAD LOWER ATTACH ANGLE IAW DC9 SRM 51-30-1 AND 51-30-5.Mar 5, 1999 · N931AX · Doug DC933FSDR CA990303019Firewall · cracked(CAN) A CRACK FOUND ON THE FIRWALL RADIATING FROM THE RIVETS UNDERNEATH THE RIGHT HAND COWL MOUNT BRACKET.Feb 26, 1999 · Cessna 172R
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