JASC 5400
Service difficulty reports · 1,907
Reports filed under 5400 · Nacelle/Pylon Structure, 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 = '5400' 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.
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 = '5400' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWIA202162952None · corrodedTHE GALLEY #1 HAS A CORRODED DOUBLER LOCATED BEHIND THE FLOOR MOUNT FITTING AT THE INBD EDGE/AFT LOCATION. (C-CHECK RO 11-27-21) REPLACED THE CORRODED DOUBLER LOCATED BEHIND THE FLOOR MOUNT FITTING AT THE INBD EDGE/AFT LOCATION WITH A SERVICEABLE DOUBLER SDR FDEA202110142539None · cracked#1 PYLON AFT I/B SIDE [HYDRAULIC BAY AREA] INTERNAL LOWER FWD CLIP IS CRACKED REMOVED AND REPLACED CLIP PER BAC DWG # 313N3052SDR MASA20211013484None · noneLH INLET COWL LIPSKIN WAS FOUND TO HAVE ABRASION DAMAGE. PERFORMED PERMANENT REPIAR IAW CRJ 700/900 SRM 54-11-05, FIGURE 54-11-05-991-801, ITEM 1, EA 72-2021-180.SDR CALA2021101101843Spar · crackedB767-54-3-7013 - NO.2 PYLON STA185 UPPER SPAR WEB FOUND CRACKED AT LH ELECT BUNDLE CUTOUT POSITION TRANSFER REF NR 9130920 AND ORIGINATED BY EMP V896810 NO.1 PYLON NAC STA185 UPPER SPAR WEB LH ELECT BUNDLE CUTOUT PERMANENT REPAIRED (CAT A) AS PER SRM54-53-02-2SDR FDEA202110082521Web · crackedNO.2 ENG EXTERAL PYLON BOX (R/H) HAVE CRACK ON THE RIB8 REPLACED THE DAMAGED WEB WITH NEW ONE BY FASTENERS I.A.W. A300-600F SRM 51-72-10- 001, P. 2 AND 51-40-21-001, PARA. 6, P. 7B-23.SDR FDEA202110082520Web · crackedNO.1 PYLON BOX OUTSIDE SKIN HAS CRACKS ON THE RIB 8 BOTH SIDE. CRACKED RIB 8 WEB REPLACED NEW PART . INSTALLED WITH RIVETS AND FASTENERS I.A.W A300-600F SRM 51-72-10-001, PAGE 2 AND SRM 51-40-21-001 ,PARA 6 PAGE 7B -PAGE 23SDR DALA2021101106189None · noneSHIP 6807 CORROSION ON BUSHINGS (2EAS) OF UPPER LINK, LOWER ATTACH FITTING AT RH PYLON (MOT 2). CORRECTIVE ACTION: SUMMARY OF NRC 00524: BUSHINGS (2EAS) OF UPPER LINK, LOWER ATTACH FITTING AT RH PYLON (MOT 2) WERE REPLACED PER B757-200 SRM. (1975334)SDR FDEA202110052719Skin · unknownREPAIR ASSESSMENT: REPAIR DOUBLER FOUND ON RH SIDE UPPER SKIN PANEL OF #2 ENGINE NACELLE. DOT 151 REPAIR WAS PREVIOUSLY INSTALLED PER E.A. 1-5480-T0300648 C "NACELLE /PYLON- FILLET/FAIRINGS-LOWER VERTICAL STAB PANEL" REF. E.A. 1-5100-T0363904 'STRUCTURES-SDR FDEA202110052592Web · cracked#2 PYLON I/B SIDE WAS FOUND A WEB UPPER CORNER CRACK AT RIB 8A. REPLACED THE DAMAGE PART WITH NEW I.A.W A300-600F SRM 51-72-10-001,PAGE2SDR FDEA202110052590Web · cracked#2 PYLON O/B SIDE WAS FOUND A WEB UPPER CORNER CRACK AT RIB 8A. REPLACED THE DAMAGE PART WITH NEW I.A.W A300-600F SRM 51-72-10-001,PAGE2SDR CALA2021100601793None · noneB767-54-3-7024 - NO.1 PYLON STA185 UPPER SPAR WEB FOUND CRACKED AT LH ELECT BUNDLE CUTOUT POSITION TRANSFER REF NR LP9130922 AND ORIGINATED BY EMP V896810 RII INSPECTED BY HX126723 ADD EMP:V896826 NO.1 PYLON NAC STA185 UPPER SPAR WEB LH ELECT BUNDLE NO.1 PYLONSDR FDEA202110042505Stiffener · crackedRH PYLON FORWARD FAIRING STIFFENER CRACKED AT THE RIB JO0 FWD AREA REINFORCED REPAIR DOUBLER & ANGLE WORK INSTRUCTION I.A.W. A300-600F SRM 54-54-11- 201- 2, PARA. 5A, PAGE 201-207, FIG. 201.SDR SWAA2021111725744Panel · delaminatedNO-2 PYLON ACCESS PANEL 441EL EDGE AREA DELAMINATED MKD DOT ; / [01] PREPARED FOR REPAIR AT PANEL 441 EL AS PER B737-700 SRM. 51-70-06-2R-7; [02] VERIFIED STEP 1; OK TO INSTALL REPAIR PLIES; [03] REPAIRED AT PANEL 441 EL AS PER B737-700 SRM 51-70-06-2R-7 MATERSDR CALA2021100401775Panel · missingPDA 2 UPON ARRIVAL AT THE GATE, FOUND PANEL 436AL MISSING FROM THE #1 ENGINE O/B PYLON. DUE TO NOT HAVING THE CORRECT PANEL IN STOCK IN EWR. NEED TO CDL DDP COMPLIED WITH. PLACARD APPLIED. PANEL 436AL. DISPATCH DESK: 64 NAME: MANN DATE: 01-OCT-21- #1 PYLON NSDR UIEA2021092702124Skin Panel · corrodedNO.2 ENG AFT MOUNT LH MOUNT LH PNL FWD SIDE PNL FOUND CORROSION. NO.2 CORE COWL UPPER SKIRT FAIRING SKIN REPLACED IAW RI-54-00-15001 REV ASDR UIEA2021092702126Strut · misinstalledDURING ACCOMPLISHING INSPECTION TO SSID ITEM S-1, NACELLE STRUTS I/B AND O/B EDGE OF THRUST TANG NOT FULLY EXPOSE AND FASTENER SUBSTITUTION. NO.1 NACELLE STRUT THRUST TANG NOT FULLY EXPOSE AND FASTENER SUBSTITUTION IAW RI-54-00-14906 REV ASDR UIEA2021092702127Strut · misinstalledDURING ACCOMPLISHING INSPECTION TO SSID ITEM S-1, NACELLE STRUTS I/B AND O/B EDGE OF THRUST TANG NOT FULLY EXPOSE AND FASTENER SUBSTITUTION. NO.2 NACELLE STRUT THRUST TANG NOT FULLY EXPOSE AND FASTENER SUBSTITUTION IAW RI-54-00-14906 REV ASDR UIEA2021092702128Strut · misinstalledDURING ACCOMPLISHING INSPECTION TO SSID ITEM S-1, NACELLE STRUTS I/B AND O/B EDGE OF THRUST TANG NOT FULLY EXPOSE AND FASTENER SUBSTITUTION. NO.3 NACELLE STRUT THRUST TANG NOT FULLY EXPOSE AND FASTENER SUBSTITUTION IAW RI-54-00-14906 REV ASDR UIEA2021092702129Strut · misinstalledDURING ACCOMPLISHING INSPECTION TO SSID ITEM S-1, NACELLE STRUTS I/B AND O/B EDGE OF THRUST TANG NOT FULLY EXPOSE AND FASTENER SUBSTITUTION. NO.4 NACELLE STRUT THRUST TANG NOT FULLY EXPOSE AND FASTENER SUBSTITUTION IAW RI-54-00-14906 REV ASDR IXXA20211007052Bulkhead · crackedAIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE C CHECK VISIT.
IN COMPLIANCE OF TASK CARD ATI-54-812-00-02, MAINTENANCE IDENTIFIED 3 INCH CRACK TO THE #2 PYLON BULKHEAD
LOCATED AT NAC STA 163.50 DAMAGE FOUND TO BE OUT OF LIMITS IAW BOEING 767-200 SRM 54-50-07.
SDR IPXA2021100774728Longeron · noneINSPECTION TYPE:A300ENG 1 ACCESS PANEL 475AL I/B MID ATTACHMENT PLATE WITH ENLONGATED HOLES MARKED WITH RED.REMOVE AND REPLACE P/N 221-0081-327 IAW SRM 51-42-21.SDR IPXA2021100474583None · crackedINSPECTION TYPE:CCRACKED PLATE AT NO.2 PYLON PANEL SUPPORT STRUCTURE BETWEEN PANEL 422DR AND 424CR UPPER CRNER. DOT NO 17-07REMOVE AND REPLACE PLATE PER SRM 51-40-21SDR IPXA2021092574274Skin · corrodedINSPECTION TYPE:SEG4#2 ENGINE PYLON, INBD SKIN, INTERIOR, AT APPROX. NAC STA 169.8 INBD SIDE HAS CORROSIONAFTER REMOVED CORROSION IN THE AREA FOUND TO BE IN LIMITS PER SRM 54-50-01 FIG 01 SHEET 4 DETAIL VSDR HYIA20210924001Beam · crackedDURING MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE RIGHT HAND OUTBOARD ENGINE BEAM (P/N: 5654109-8) IN THE AREA UNDERNEATH THE FORWARD ENGINE MOUNT DOUBLER. THIS CRACK TRAVELS LEFT TO RIGHT ACROSS THE TOP FACE OF THE BEAM AND PARTIALLY DOWN THE OUTBOARDSDR DALA2021121707854None · noneSHIP 3308 PYLON 1 AFT INBD T/E. SEVEN SCREWS PULLED THROUGH SKIN AFT LOWER EDGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOC LOWER AFT PYLON FAIRING #1 AS PER ER/A #595848-14. (8092309)SDR JJBA20210923005None · noneAFTER NDT INSPECTION, CRACK FOUND IN LH PYLON YOKE BLIND FASTENER HOLE. HOLE REPAIRED WITH BUSHING AND ALTERNATE MATERIALSDR IPXA2021100674645None · crackedINSPECTION TYPE:C#1 PYLON FAIRING 413BL HAS CRACK LOC AT LOWER CUTOUT CORNERFABRICATED DOUBLER IAW SRM 54-21-51 FIG 205SDR SWIA202162750None · chafed*RIGHT ENGINE €“ T/R COWLING DISHING FORWARD CHANNEL AND DOUBLER ARE CHAFED. (MARKED) (C-CHECK RO 11-20-2021) REMOVED AND INSTALLED NEW DOUBLER ON THE RH ENGINE UPPER T/R COWLING REF: CRJ700 SRM 51-42-06-001-001-A01. RESTORED FINISH. UPON REMOVAL AND INSTSDR SWIA202162749None · chafed*RIGHT ENGINE - T/R COWLING DISHING AFT CHANNEL AND DOUBLER ARE CHAFED. (MARKED) (C-CHECK RO 11-20-2021) REMOVED AND INSTALLED NEW DOUBLER ON THE RH ENGINE UPPER T/R COWLING REF: CRJ700 SRM 51-42-06-001-001-A01. RESTORED FINISH.UPON REMOVAL AND INSTALLATIOSDR SWIA202162535None · damagedCOMPLY WITH REO 670-52-11-104 REV-H DATED: 2016-08-14 / TRANSFER REPAIR DOUBLER ON NEW PAX DOOR AFT WEB (C-CHECK RO 11/10/2021) COMPLIED REO 670-52-11-104 REV-H DATED: 2016-08-14 / REMOVED AND INSTALLED REPAIR DOUBLER ON NEW PAX DOOR AFT WEBSDR IPXA2021100874737Fairing · elongatedINSPECTION TYPE:3CFASTENER HOLES WERE FOUND ELONGATED ON THE THE R/H WING #3 PYLON TO WING AFT FAIRING.REPAIRED ELONGATED FASTENER HOLES IAW VT-SAA EA 011-5481-01-A9365 REV I/R AND UPS EO MD11-5450-81821-A . (MINOR)SDR IPXA2021092174138Bracket · crackedINSPECTION TYPE:SEG#1 ENGINE AFT FAIRING FRAME STA 272 RH SIDE BRACKET IS CRACKED.REMOVED CRACKED BRACKET AND INSTALLED REPLACEMENT PER SRM 51-40-02 AND 51-10-02 PR 9.SDR IPXA2021093074436Rib · noneINSPECTION TYPE:C3#1 PYLON FAIRING 439AL FWD VEE RIB IS GOUGED.REMOVE AND REPLACE #1 PYLON FAIRING 439AL FWD VEE RIB IAW SRM 54-01-42. (MINOR)SDR IPXA2021093074430Support · crackedINSPECTION TYPE:SEG#2 PYLON OB SIDE AFT FAIRING FWD SUPPORT AFTER REMOVING CORROSION FOUND A .422" CRACK AT BOTTOM HOLE OF SUPPORTREPAIRED SUPPORT PER EO# B757-5450-27-A2700SDR IPXA2021092474216Rib · chafedINSPECTION TYPE:3C#3 PYLON FAIRING 489AL VEE RIB IS CHAFED.REMOVED AND REPLACED CHAFED #3 PYLON FAIRING 489AL VEE RIB IAW SRM 54-01-42. (MINOR)SDR IXXA20211007050Skate Angle · chafedAIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE C CHECK VISIT#2 PYLON FORWARD EDGE OF SKATE ANGLE IS CHAFFED AT 447AR PANEL.CHAFE BEYOND LIMITS IAW BOEING STRUCTURE REPAIR MANUAL 54-51-71.
PREVIOUS BLEND NOTED. REMOVED AND REPLACED FORWARD END SKATE ANGLE.SDR HNAA2021100600489None · noneE879830 - LH ENGINE PYLON FWD YOKE UPPER AFT JO-BOLT HOLE DAMAGED. (LOCATED AT OUTBD EDGE OF PYLON UPPER SKIN). .... LH ENGINE PYLON FWD YOKE UPPER AFT JO-BOLT HOLE DAMAGED. (LOCATED AT OUTBD EDGE OF PYLON UPPER SKIN)SDR IPXA2021101574985Pylon · corrodedINSPECTION TYPE:SEG4#2 ENGINE PYLON OB INTERIOR STRUCTURE HAS EXFOLIATION CORROSION AT APPROX NEC 120.0REPAIR IAW EO B757-5450-81451-ASDR IPXA2021092274160Skin · noneINSPECTION TYPE:SEG4#2 ENGINE PYLON OUTBD FWD SKIN AT LOWER ANGLE, HAS INTERGRANGUAR CORROSIONREPAIR #2 ENGINE PYLON OUTBD FWD SKIN PER EA#757-5450-27-A2665SDR CALA2021071901137Strut · corrodedREF AMES NR 0966. NUMBER 2 ENGINE STRUT COMMON TO NOZZLE FAIRING AFT PAN SKIN HAS CORROSION AROUND BEARING HOLE BLENDED AFT PAN SKIN. FOUND TO BE OUT OF LIMITS. REMOVED AND REP LACED IAW B757-200 SRM 51-40-02 PARAGRAPH 9 AND B757-200 SRM 51- 40-04. SEE BACK ANSDR SWIA202161432None · crackedHOLE #3 ON UPPER R/H PYLON CRACKED (C-CHECK RO 9/27/2021) PERFORMED REPAIR FOR CRACKED FASTENER HOLE # 3 TO RH UPPER PYLON SKIN IAW REO 670-54-51-059 REV - - DATE 2021-08-02. REAMED HOLE TO INTERFERENCE FIT .307 / .310 DIAMETER INSTALLED HST11AG10 + HSSDR CALA2021071601115Strut · corrodedREF AMES NR 0966. NUMBER 2 ENGINE STRUT COMMON TO NOZZLE FAIRING AFT PAN SKIN HAS CORROSION AROUND BEARING HOLE BLENDED AFT PAN SKIN. FOUND TO BE OUT OF LIMITS. REMOVED AND REP LACED IAW B757-200 SRM 51-40-02 PARAGRAPH 9 AND B757-200 SRM 51- 40-04. SEE BACK ANSDR HNAA2021072700335Bracket · bentE867564 - RH PYLON RIB 5 INTERNAL BRACKET BENT (RIVET INCORRECTLY INSTALLED MISSED BRACKET). REMOVED AND INSTALLED R/H PYLON RIB 5 INTERNAL BRACKET AND R/H PYLON UPPER AFT SKIN IAW EMB 145 SRM 51-40-02.SDR JJBA20210708015Flange · crackedRH PYLON YOKE UPPER FLANGE HOLE (X1) FOUND WITH CRACK. RH PYLON YOKE UPPER FLANGE HOLE REAMED. AFTER NDT INSPECTION, DAMAGE IS STILL PRESENT AT RH PYLON YOKE UPPER FLANGE. HOLE OVERSIZED AT SECOND PERMISSIBLE DIMENSION (0.421). 2 BUSHINGS LOCALLY FABRICATED. RSDR V0XD20210516001Spigot · gougedL/H NACELLE LOWER COWL PANEL 433AL ALLIGNMENT OIN IS GOUGED. CORRECTIVE ACTION: REMOVED AND REPLACED THE ALLIGNMENT PIN (SPIGOT) P/N: CN624-2067-204 IAW SRM 51-42-06.SDR UIEA2021050101048Indicator · leaking#1 PYLON DIFFERENTIAL PRESSURE INDICATOR LEAKING(<P>REMOVED AND REPLACED #1 PYLON DIFF PRESS IND PER AMM -29-11-17. NO LEAKS NOTED.</P>)SDR P5CA2021042800156None · noneDURING WALK AROUND FOUND EVIDENCE OF BIRD STRIKE ON RH ENGINE INLET. PERFORMED HPC BOROSCOPE THROUGH PLUGS B1-0, B1-1, B1-6 AND B1-12 IAW AMM 72-00-00-706-146-110. NO DAMAGE NOTED.SDR SWAA2021031152468Access Panel · delaminatedDELAMINATED ACCESS PANEL 193AR BODY FAIRING AREA AT LOWER FUSELAGE / REPAIRED ACCESS PANEL 193AR BODY FAIRING AREA AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-3 REP 3 TOOL USED CALIPER PN 500-197-30 SN A18229508 DUE DATE 09-AUG-21 HOT BONDER PN HCS9200B SDR SWAA2021040151256Access Panel · elongatedELONGATED HOLE ACCESS PANEL 444CR AT RT PYLON / REPLACED ACCESS PANEL #444CR AT RT PYLON IAW DRAWING # 313A2730 MATERIAL USED 2024-T351 0.250' PO 2014-521219SDR SWAA2021040151252Plate · crackedCRACK PLATE INTERNAL AREA I/B FAN COWL ON ENGINE 1 / REPLACED PLATE INTERNAL AREA I/B FAN COWL ON ENGINE 1 IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND CMM GOODRICH 71-13-30
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