JASC 5410
Service difficulty reports · 4,119
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 HALA2022122700315Acoustic Panel · damagedETOPS - #1 ENGINE ACOUSTIC PANELS / ICE IMPACT 4 EACH DAMAGED AT P[OSITIONS 5 TO 12 O'CLOCK. REMOVED AND REPLACED PANELS 4 EACH #1 ENGINE ICE IMPACT ACOUSTIC PANEL PER AMM 72-21-41 AT 5 TO 12 O'CLOCK POSITIONS.SDR AALA202212280953Nut · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT PYLON SPIGOT FITTING NUT. MAINTENANCE REPLACED THE NUT IAW TASK CARD 26C411554031.SDR FDEA202212172944Beam · damagedAFTER OPENING PYLON PANEL 437BL (#1 ENGINE OTBD) FOUND BOTH AFT DOOR HINGE FITTINGS WITH EXCESSIVE PLAY AND HINGE BOLTS WEARING INTO PYLON FITTINGS. ITEM REPAIRED PER E.A. H-5451-T0372182 P1.SDR AALA202301273488Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT PYLON LOWER SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. MAINTENANCE REPLACED LOWER SPIGOT FITTING PER SRM 54-51-12.SDR SWAA2022121682320Panel · delaminatedPANEL 193AL HAS LEADING EDGE DELAMINATION APPROX. 16 INCHES FROM TOP EDGE. DAMAGED AREA IS APPROXIMATELY 8 INCHES LONG BY 1.75 INCHES WIDE. PERMANENT REPAIR IN 730 DAYS. SPEED TAPE APPLIED TO DAMAGE AREA IAW SRM 53-40-70-1A-1-A00094.SDR SWAA2023013080796Web · crackedCRACK WEB OUTBOARD FAN COWL INTERNAL AREA ON ENGINE 2 2022-691652<[01] REPLACED NEW WEB OUTBOARD FAN COWL INTERNAL AREA ON ENGINE 2 IAW B737-700 SRM 51-40-02 AND CMM 314-2200;[02] REPLACED NEW WEB OUTBOARD FAN COWL INTERNAL AREA ON ENGINE 2 IAW B737-700 SRM 51SDR AALA202301194442Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT FITTING LOWER RETAINING PLATE. MAINTENANCE REPLACED RETAINING PLATE PER SRM 51-72-11.SDR AALA202301197374Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT FITTING LOWER RETAINING PLATE. MAINTENANCE REPLACED RETAINING PLATE PER SRM 51-72-11.SDR DALA2022120607845Rub Strip · corrodedCORROSION ON RUB STRIP OF OUTBOARD COWLING FWD EDGE AT LH ENGINE. OUTBOARD FAN COWL ENGINE 1 WAS REPLACED FOR SERVICEABLE IAW AMM 71-11.SDR AALA202212142579Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT PYLON LOWER SPIGOT FITTING BASE PLATE. MAINTENANCE REPAIRED SPIGOT FITTING BASE PLATE PER SRM 54-51-12-283-001.SDR AALA202212148249Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT PYLON LOWER SPIGOT FITTING BASE PLATE. MAINTENANCE REPAIRED SPIGOT FITTING BASE PLATE PER SRM 54-51-12-283-001.SDR YENA2022112901177Fitting · crackedDURING HEAVY MAINTENANCE: INDICATION OF CRACK ON BUSHING HOUSING AT LH PYLON AFT INBOARD FITTING. INBOARD SPAR OF LH PYLON WAS REPLACED PER EMB 190 SRM 51-43-03 PAR 4&5 AND SRM 51-43-04 PAR.4 AND 5 AND SRM 51-41-02 PAR.4 AND 6 & AMM 20-10-01-910-801-A.'SDR SWAA2022112374390Fairing · crackedENG #1 AFT STRUT FAIRING: EVIDENCE OF A CRACK ON TRAILING EDGE FAIRING FWD OB SIDE. COMPLETED PER EA 22-154-03457.SDR UIEA2022111901197Fuse Pin · crackedRH NACELLE PYLON ATTACH FUSE PIN UPPER LINK WITH CRACK INDICATION(<P>FUSE PIN OF UPPER LINK WAS REPLACED IAW AMM 54-51-03-404-030-002</P>)SDR SWAA2023010588365Cowl Latch · crackedENG 1 OUTBD FAN COWL CRACKED AT FWD OF FWD LATCH.<[01] REPLACED ENG 1 OUTBD FAN COWL. REF AMM 71-11-02.SDR SWAA2022120771230Panel · pulledNR 2 ENGINE HAS CRACKED LOUVERED PANEL AT 1 O'CLOCK BLEED AIR VALVE. SCREW IS PULLED THROUGH PANEL. REPLACED THE PANEL IAW AMM 72-23-07.SDR DALA2022111507370Structure · handler errorLEFT ENGINE CONTACTED JET BRIDGE UPON PARKING. GUIDENCE WAS FOLLOWED WITH 3 MARSHALLERS. R/R #1 ENG INLET COWL PER B737 AMM 71-11. OPS CK GOOD.SDR HYIA20221114002Crossbeam · crackedDURING MAINTENANCE ON N223PB, A MULTIPLE CRACKS WERE VISUALLY IDENTIFIED ON THE RH NACELLE CROSSOVER BEAM (P/N: 5654104-2). ONE CRACK ON THE FRONT FACE OF THE BEAM AT APPROXIMATE RWS 87.44 WITH AN APPROXIMATE LENGTH OF 3.780 INCHES. A SECOND CRACK WAS IDENTIFISDR CALA2022110403050Fairing · missingDURING THE CHECK FOUND PANEL MISSING ON LH ENG 5ÓCLOCK (RHS). INSTALLED PANEL ON L/H 5 OCLOCK ENGINE START POSITON. NO FURTHER ACTION REQUIRED. WORK ACCOMPLISHED.SDR IPXA2022102487436Web · crackedINSPECTION TYPE:C#1 PYLON AT RIB 19 LOWER CHORD WEB CRACKED.REMOVED AND INSTALLED CHORD WEB IAW-SRM 51-40-21.SDR CALA2022102402931None · noneRH WING, T/E LWR SKIN SUPPORT PLATE FOR HYD LINE CONNECTIONS FROM PYLON IS WORN-OUT REMOVED AND REPLACED SUPPORT PLATE IAW SRM 57-21-11-300-005. EMP : V933863 WC: 36421 STA: ST ENG BFM ESFR# 1030227SDR IPXA2022102387404Frame Angle · crackedINSPECTION TYPE:SEG#1 ENG AFT FAIRING PNL 475AL HAS A CRACKED ANGLE RH FWDREMOVED AND REPLACED FRAME/ANGLE IAW A300 SRM 51-40-21SDR IPXA2022102387403Frame Angle · crackedINSPECTION TYPE:SEG#2 ENG AFT FAIRING PNL 485AL HAS A CRACKED ANGLE RH FWDREMOVED AND REPLACED FRAME/ANGLE IAW A300 SRM 51-40-21SDR IXXA2022101204Access Door · cracked#2 PYLON OB HYDRAULIC BAY DOORSDR HNAA2022102500275Reinforcement · corrodedE937355 - CORROSION ON 3 TRIANGLE REINFORCEMENTS ON LH ENGINE INTERNAL UPPER COWLING .... RAR 3 TRIANGLE REINFORCEMENTS ON LH ENGINE UPPER COWLING INTERNAL STRUCTURE IAW EMB 145 SRM 51-20-01 AND 51-40-02.SDR AALA202209276152Frame · crackedAIRCRAFT IN BASE MAINTENANCE: AFTER REMOVAL UPPERFITTING AT INBBOARD FRAME AT PANEL 444EL AT NACELLE STRUT RIGHT FOUND UPPERCHORD FRAME FITTING CRACKED. REMOVED, FABRICATED AND INSTALLED NEW UPPER CHORD AT NUMBER 2 NACELLE STRUT INBOARD FRAME AT PANEL LOCATIONSDR 2022FA0000544Panel · dentedDURING MAINTENENCE INSPECTION FOUND FILLING REPAIR ADJACENT TO A DENT ON ENGINE #2, CF6-80C2, INLET COWL LOWER ACOUSTIC PANEL BETWEEN 6 AND 7 O'CLOCK.SDR AALA202209272496Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON FORWARD OUT BOARD SHACKLE UPPER PIN AT PYLON STATION 6793 AND RIB 4. REPLACED PIN PER AMM 54-51-17.SDR CALA2022091602392Panel · missingPDA 3 #1 ENGINE PYLON DOOR 433CL MISSING. INSTALLED LEFT PYLON LEFT SIDE ACCESS PANEL 433CL. AERODYNAMIC SMOOTHNESS AND FIT AND FINISH FOUND SATISFACTORY.SDR CALA2022090902317Rivet · missingPDA 3 DURING WALKAROUND FOUND 3 MISSING RIVETS AND 3 LOOSE RIVETS AT #2 ENGINE PYLON AFT AREA BY ENGINE EXHAUST. PHOTOS ADDED. REMOVED AND REPLACE LOOSE RIVETS ON AFT ENGINE. PYLON PER SRM 51-50-02.SDR CALA2022090902316Rivet · missingPDA 3 DURING WALKAROUND FOUND 1 MISSING RIVET AT #1 ENGINE AFT PYLON INBOARD AREA BY EXHAUST. PHOTO ADDED. REPLACED MISSING RIVET WITH NEW ONE PER SRM 51-40-02.SDR DALA2022090605962None · noneSHIP 654 WEAR ON WEB AT INB/OUTB SIDES, LH PYLON BTW NAC STA 100 TO NAC STA 102.7 (LH ENG.) CORRECTIVE ACTION: SUMMARY OF NRC 00363: WEB AT INB/OUTB SIDES, LH PYLON BTW NAC STA 100 TO NAC STA 102.7 WAS REPAIRED PER PRI 601534-14 REV 1 AND ERA 601534-14 REV ORISDR SWAA2022092647824Web · cracked#2 ENGINE OB FAN COWL #424 HAS WEB CRACKED JUST AFT OF ENGINE OIL ACCESS DOOR (MARKED) / [01] REMOVED WEB AFT OF ENGINE ACCESS DOOR PER SRM 51-40-02.;[02] REMOVED AND REPLACED WEB IAW SRM 51-40-02SDR IPXA2022083085756Seal · crackedINSPECTION TYPE:A300PYLON PANEL 423BL HAS CRACK UNDER SEAL RETAINERINSTALLED DOUBLER REPAIR IAW SRM 54-52-51SDR FDEA202208222028Inlet · corroded#1 ENGINE INLET COWL MOUNT FLANGE ON THE ENGINE SIDE IS CORRODED SPORADICALLY AROUND THE ENTIRE CIRCUMFERENCE OF THE ENGINE REMOVED AND REPLACED ENGINE PER FEDEX CARD # 7180260-01-02SDR JJBA20221017009Yoke · damagedDAMAGED HOLE #1 PYLON YOKE UPPER FLANGE, AFT FASTENER. REPAIRED HOLE ON #1 PYLON YOKE UPPER FLANGE AT AFT FASTENER LOCATION.SDR IPXA2022083085763Seal · crackedINSPECTION TYPE:A300PYLON PANEL 423BL HAS A CRACK UNDER SEAL RETAINERINSTALLED DOUBLER REPAIR IAW SRM 54-52-51SDR IPXA2022083085759Seal · crackedINSPECTION TYPE:A300PYLON PANEL 413BL HAS CRACK UNDER SEAL RETAINERINSTALLED DOUBLER REPAIR IAW SRM 54-52-51SDR HKGA202208240001Clevis · shearedLEFT HAND ENGINE NACELLE, IB SIDE , UPPER FWD SUPPORT ROD FWD CLEVIS WAS FOUND TO BE SHEARED AT THE THREADED PORTION OF THE CLEVISSDR UIEA2022073000793Panel · delaminatedENGINE 1, ACOUSTIC SHROUD WITH SEVERAL DENTS BETWEEN 4 AND 7 HRS(<P>INLET COWL ACOUSTIC PANEL DENTS WERE REPAIR IAW EO 1971A286</P>)SDR CALA2022081002007Panel · missingPDA 2 DURING WALKAROUND FOUND PANEL MISSING FROM #2 ENGINE PYLON INBOARD SIDE. PHOTO ADDED. PERFORMED VISUAL INSPECTION OF A/C FOUND NO DAMAGE .INSTALLED PANEL P/N 311T3065-247 REF IPC. 54-53-01-01 SECURED FOR FLT.SDR SWAA2022081040106Panel · damaged#2 ENGINE FAN DUCT PANELS #2 AND #3 HAVE HARDWARE HOLES ELONGATED / [01] REMOVED AND REPLACED #2 ENGINE FAN DUCT PANELS #2 AND #3 POSITIONS PER AMM 72-23-07SDR FDEA202208031863Skin · corroded#1 PYLON UPPER SKIN AND OUTBD FITTING HOLE #9 HAS REJECTABLE INDICATIONS OF CORROSION AT 3 TO 5 O'CLOCK TITLE: WINGS - PLATES AND SKINS - LH WING, UPPER SKIN AT DRAG FITTING REJECTABLE CRACK / CORROSION INDICATIONS . ACCOMPLISHED STEPS 1-25 IAW EA F-5730-TSDR FDEA202208031858Fitting · corroded#1 PYLON INBD FITTING HOLE #2 HAS REJECTABLE INDICATIONS ON CORROSION 6 TO 10 O'CLOCK. TITLE WING - PLATES AND SKIN - LH WING, UPPER SKIN AT DRAG FITTING REJECTABLE CRACK / CORROSION INDICATIONS. ACCOMPLISHED STEPS 1-25 PER EA F-5730-T0369611 PT1. MAJOR RSDR GTIA2022080436570None · damaged"DURING HEAVY CHECK FOUND GOUGE ON #1 PYLON RAF # 2935790-01 OPENED
SDR ITEM -VERIFIED NR # 5001171797-0030 AND TC # 1003778439-0010. GOUGE WAS REPAIRED AS PER SPIRIT EO 5452-2204 RE.00 "SDR FDEA202207311834Beam · chafed#1 ENG INBD PANEL 436CR HAS A LOOSE NUTPLATE THAT HAS WORN INTO THE STRUT FAIRING BEAM. REPAIRED #1 ENGINE INBD SKIRT BEAM AT FOWARD END REF 767 SRM 54-52-71-2R FIG 203 REPAIR 3 PAGE 15 AND 767 SRM 51-40-03-0G.SDR FDEA202207301849Beam · chafed#1 ENGINE, PYLON PANEL 437BR HAS WORN HINGES. MWT 0000481208 : MEYER, LONNY W - 03-AUG-2022 10:53 SKIRT PANEL WAS REMOVED AND BUSHINGS REPLACED REF 767 SRM 51-40-02, SEE JPF FOR MAINTENANCE PERFORMEDSDR IXXA2022101302Frame · crackedNUMBER 1 ENGINE I/B CORE COWL NUMBER 4 FRAME IS CRACKEDSDR SWAA2022080835628Cowling · corroded#1 ENGINE INLET COWL HAS NUMEROUS AREAS OF CORROSION AROUND ATTACHING FASTENERS FOR UPPER AND LOWER BARREL SKINS PT# OF COWL 314-2100-3 SN# 4779001 / [01] REMOVED #1 ENGINE INLET COWL PER AMM 71-11-01 REMOVED T12 SENSOR PER AMM 73-21-05;[02] UPDATED MEASUREMENSDR IPXA2022080684960Skin · corrodedINSPECTION TYPE:CK14#1 PYLON AFT SKIN INNER DOUBLER HAD 2 LOCATIONS OF CORROSION DAMAGE. THE FWD CORROSION LOCATION IS LOCATED BETWEEN PP STA 153 AND PP STA 160. THE AFT CORROSION LOCATION IS LOCATED BETWEEN PP STA 182.2 AND PP STA 185.35. BOTH LOCATIONS ARE O
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