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 CALA2020052200981Fitting · crackedDURING NDT HFEC ROTO INSPECTION OF #1 PYLON UPPER DRAG FITTING IAW NDTM PART 6, 51-00-16 CRACK INDICATIONS WERE FOUND AT HOLE #1 - CRACK POSITION :- 3:0''CLOCK; CRACK DEPTH :-0.591"; CRACK SIZE :- 0.050" REF AAR NR 9606668 REPAIRED HOLE #1 PER ECRA 5720-03193SDR CALA2020052200976Fitting · crackedDURING NDT HFEC ROTO INSPECTION OF #1 PYLON UPPER DRAG FITTING IAW NDTM PART 6, 51-00-16 CRACK INDICATIONS WERE FOUND AT HOLE #4 - CRACK POSITION :- 11:0''CLOCK; CRACK DEPTH :-0.500"; CRACK SIZE :- 0.060" REF AAR NR 9606671 REPAIRED HOLE #4 PER ECRA 5720-03193SDR CALA2020052200980Spar · crackedDURING NDT HFEC ROTO INSPECTION OF #1 PYLON UPPER DRAG FITTING IAW NDTM PART 6, 51-00-16 CRACK INDICATIONS WERE FOUND AT HOLE #3 - CRACK POSITION :- 3:0''CLOCK; CRACK DEPTH :-0.480"; CRACK SIZE :- 0.050" REF AAR NR 9606670 REPAIRED HOLE #3 PER ECRA 5720-031930SDR SIMA2020041325006Fitting · crackedLH ENGINE FWD YOKE LWR FWD FITTING CRACKED-C/A-REMOVED AND INSTALLED SERVICABLE LH FWD YOKE LWR FWD FITTING IAW EO ERS-EM-54MR-698SDR FDEA2020032090594Frame · cracked#2 PYLON, NACELLE STA 329, I/B UPPER CORNER CRACKED REMOVED #2 PYLON, I/B LATCH BEAM IAW B767SRM 51-40-02. REPAIRED #2 PYLON CENTER FRAME @ NACELLE STA 329, UPPER I/B CORNER IAW B767 SRM 54-52-71-2RM, REPAIR 4. RE- INSTALLED LATCH BEAM IAW B767 SRM 51-40-02SDR DALA2021091005364Structure · crackedDURING INSPECTION STAG FOR MAINTENANCE H CHECK FOUND CRACK COMMON TO THE #2 PYLON UPPER SPAR WEB AT NAC STA 221.25-237 AT POWER FEEDER CABLE CUTOUT TO THE INBOARD FORWARD NUTPLATE. C/W ERA 585804-14. (LP 1531838)SDR SWAA2021082385307Intercostal · cracked#1 FAN COWL INBD INTERCOSTAL CRACKED AT AFT SIDE OF OIL ACCESS. / REMOVED + REPLACED 1EA CRACKED INTERCOSTAL @ #1 ENGINE INBD FAN COWL IAW B737-800 SRM 51-40-02-0G-0; PARA 4&5. PART VERIFIED AS P/N: 314-2259-4 FOR NEW INTERCOSTAL IAZW B737-700 SRM 71-13-30; ITSDR HYIA2020031300001Beam · crackedDURING ULTRASONIC INSPECTION PERFORMED IN ACCORDANCE WITH AVENGER AEROSPACE SOLUTIONS AAS-ALS-15-002 REV C PER CAPE AIR REFERENCE 1 AMOC TO SATISFY AD2015-07-03, A CRACK WAS IDENTIFIED ON THE TOP FACE OF THE RIGHT HAND INBOARD ENGINE BEAM. THIS CRACK MEASURES SDR IPXA2020022655473Tee Fitting · damagedINSPECTION TYPE:SEGPYLON PANEL 485AL, R/H UPPER MID T-CHORD HAS ELONGATED HOLESREMOVED AND INSTALLED NEW PART #221-0081-328 IAW SRM 51-40-20SDR DALA2020022401352Structure · crackedMTC TASK-NO.1 STRUT MID SPAR CUTOUT AREA AT NAC STA221.25 FOUND CRACK. NO.1 STRUT MID SPAR WEB CUTOUT AT NAC STA221.25 CRACKED AREA REPAIRED AS PER PRI585200-14 REV.0. PRI585200-14 REV.0 COMPARED AND COMPLIED WITH ER/A585200-14 REV.ORIGINAL. ASSOCIATED ER/A 14SDR SIMA202003029007Yoke · crackedRH FWD PYLON LWR YOKE CRACKED-C/A-REMOVED AND INSTALLED SERVICABLE YOKE IAW ERS-EM-54MR-698SDR HSRR2020022520Crossbeam · crackedAFT NACELLE CROSS BEAM CRACKED AT OUTBOARD MOUNT FLANGE.SDR 9WGA4112020021801Rivet · looseREF BOEING TASK CARD 71-101-05-02, WHILE PERFORMING AFT ENG GVI, FOUND SEVERAL LOOSE AND POPPED RIVETS INSIDE ENG INLET (6 O CLOCK POSITION), CORROSION ISSUES.SDR 9WGA202002180192Rivet · looseDURING SERVICE CHECK, INSPECTION OF BOEING TASK CARD 71-101-05-02, PERFORMING AFT ENG., GVI FOUND SEVERAL LOOSE AND POPPED RIVETS INSIDE ENG INLET (6 O CLOCK POSITION), CORROSION ISSUES BEING WORKED.SDR P5CA202002198047Rub Strip · corrodedCORROSION - WEAR STRIP, NO. 1 ENG R/H CORE COWL L/E OUTER SIDE, NEAR 2:00.(<P>REMOVE DAMAGED PARTS IAW SRM 51-40-02 REV. 76. INSTALL NEW PARTS IAW SRM 51-40-02 REV. 76 AND GOODRICH CMM 71-13-24 FIG 1 SH 1 OF 22 REV. 44. JOB COMPLETED AND CONDITION CHECK SATISFSDR P5CA202002198049Rub Strip · corrodedCORROSION - SURFACE, NO. 2 ENG R/H CORE COWL EXTERIOR FWD L/E WEAR STRIP. TOTAL 4EA.(<P>REMOVE DAMAGED PARTS IAW SRM 51-40-02 REV. 76 (OFF PARTS: PN 224-2301-71 & 224-2301-146). INSTALL NEW PARTS IAW SRM 51-40-02 REV. 76 AND GOODRICH CMM 71-13-24 REV. 44. JOB SDR IPXA2020021752210Fairing · dentedINSPECTION TYPE:SEG#2 PYLON R/H SIDEWALL LOWER ANGULAR FAIRING HAS DENTS, ADJACENT TO T/R AFT FAIRING.EVALUATED DENT ON R/H PYLON FILLET FAIRING AT RIB 7. DENT MEASURES 0.700 LENGHT, 0.500 WIDE, 0.020 DEEP - FOUND IN LIMITS IAW SRM 54-50-00 FIG 103. HFEC WITH SDR SWAA2021082181302Stiffener · cracked#1 ENGINE I/B FAN COWL FRAME STIFFENER IS CRACKED / REMOVED #1 ENGINE I/B FAN COWL. IAW B737 AMM 71-11-2-000-802-F00 STEPS 4.D.(1) THRU 4.E.(2)(D) REMOVED CRACKED FRAME STIFFENER IAW SRM 51-40-02-0G-0; STEP FIGURE 8 AND FIGURE 10. INSTALLED SERVICEABLE STIFFENSDR IPXA2020021252062Bearing · corrodedINSPECTION TYPE:C#2 PYLON SPIGOT BEARING IS CORRODED AND FROZEN.RECEIVED NEW BEARLY VERIFIED P/N A5461087000200 IS EFFECTIVE FOR A/C N131UP. NEW BEARING INSTALLED ON TC NO 545017-01-3-481SDR DALA2020021181092Fitting · damagedSHIP 697 #1 PYLON DRAG FITTING HOLE #5 COUNTERSINK HAS PITTING. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 033-0001:5720-01100-0101A/013 00418 COMPLIED WITH ERA 584933-14AD REV. O. (1480538)SDR DALA2020021181089Fitting · damagedSHIP 697 #2 PYLON DRAG FITTING ALL 10 FASTENERS REMOVED IN STEP 24 A REQUIRE REPLACEMENT DUE TO DAMAGE. CORRECTIVE ACTION:SUMMARY SEE NR FOR 032-0001:5720-01100-0101B/003 00355 COMPLIED WITH ERA 584956-14AD REV. O. (1480527)SDR DALA2020021181088Brace · crackedSHIP 697 #2 PYLON DRAG BRACE - HOLE #2 HAS CRACK INDICATION IN SKIN. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 032-0001:5720-01100-0101B/005 00359 COMPLIED WITH ERA 584956-14AD REV. O. (1480523)SDR DALA2020021181086Fitting · corroded(AIRCRAFT 697, L/P 1480537) #1 PYLON DRAG FITTING HOLE #4 COUNTERSINK HAS PITTING. CORRECTIVE ACTION: COMPLIED WITH ERA 584933-14AD REV. O. VERIFIED PRI 584933-14AD REV. 0-2 AND ERA 584933-14AD REV. O MATCH.SDR FDEA2020020650275Plate · corroded#2 ENGINE PYLON FAIRING O/B SKIN SPLICE PLATE CORRODED REMOVED WORN SPLICE PLATE, REFERENCE A300-600 SRM 54-55-51, ALODINED & PRIMED NEW SPLICE PLATE, REFERENCE A300-600 SRM 51-21-10, INSTALLED NEW SPLICE PLATE, REFERENCE A300-600 SRM 51-40-21SDR FDEA2020020650272Longeron · cracked#2 PYLONAFT FAIRING, FWD I/B "U" CHANNEL CRACKED AT LOWER HOLE REMOVED WORN CHANNEL REFERENCE A300-600 SRM 51-40-21, FABRICATED NEW CHANNEL, REFERENCE A300-600 SRM 54-55-51, 51-40-44 & FED-X GMM 07-0-1001, ALODINED & PRIMED NEW CHANNEL, REFERENCE A300-600 SDR SWIA2020022748866Frame · damagedLH PYLON AFT FAIRING FWD FRAME OB MOUNT EAR FWD HOLE ELONGATED. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED ON L/H PYLON AFT FAIRING FWD FRAME O/B AND RESTORED SURFACE PROTECTION RIVETS HEAD , REF. SRM.SDR CALA2020020300326Panel · missingPANEL 436BR (#1 ENGINE INBOARD SIDE) MISSING ON ARRIVAL. PANEL INSTALLED AMM 54-53-01-410-005. EXT ITEM RAISED FOR PAINT (4413461) AND PDA LOG PAGE RAISED, INCLUDING SDR (4413304)SDR IPXA2020020351653Longeron · damagedINSPECTION TYPE:SEG#1 PYLON FAIRING 475AL O/B LONGERON HAS ELONGATED HOLESR&R LONGERON IAW SRM 51-40-21SDR FDEA202001310251Bracket · crackedLEFT NACELLE RIB AFT OF PANEL 437BL LH BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02, AND DWG 313T3380, REV N.SDR SWIA2020021848702Bracket · crackedRH UPPER TANSCOWL HAS 2EA CRACKED A-BRACKETS INBOARD AND OUTBOARD SIDE (C-CHECK) RO 2/14/2020 REMOVED AND REPLACED 2EA CRACKED A BRACKETS ON INBD AND OUTBD SIDES OF RH UPPER TRANSCOWL WITH NEW BRACKETS (P/N CN624-2082-201) AND NEW FASTENERS PER BOMBARDIERSDR DALA2020012420573Fitting · cracked(AIRCRAFT 673, L/P 1455956) ENG PYLON #2 DRAG FITTING OPEN HOLE HAS AN INDICATION OF CRACK LIKE DEFECT IN THE UPPER SKIN PORTION OF THE HOLE CLOCKED AT THE 3 OCLOCK POSITION (INBOARD SIDE) LOOKING AFT. CORRECTIVE ACTION: REPAIRED #2 ENGINE PYLON #2 DRAG FITTINSDR DALA2020012420572Fitting · cracked(AIRCRAFT 673, L/P 1455949) THE #2 ENG PYLON #4 DRAG FITTING OPEN HOLE HAS (2) INDICATIONS OF CRACK LIKE DEFECTS (1) IN THE UPPER SKIN PORTION OF THE HOLE CLOCKED AT THE 12 OCLOCK POSITION LOOKING AFT AND (1) INDICATION IN THE BOTTOM(FITTING) ALSO AT THE 12 OCSDR IPXA2020012215185Panel · crackedINSPECTION TYPE:SEG#1 PYLON PANEL 413BL HAS CRACKFABRICATED DOUBLER, INSTALLED DOUBLER, REPAIRED #1 PYLON PNL 413BL IAW SRM 54-52-51 FIG 205SDR IPXA2020012251206Panel · discoloredINSPECTION TYPE:C1DISCOLORATION AND CORROSION ON THE INBD LWR PANEL (P/N:313U8740-1) OF PYLON#3.REPAIR I.A.W. BOEING SRID:3-4615236673 AND UPS EO B747-5430-75247-A.SDR IPXA2020012215157Panel · discoloredINSPECTION TYPE:C1DISCOLORATION AND CORROSION ON THE INBD LWR PANEL (P/N:323U8740-2) OF PYLON#1. REPAIR I.A.W BOEING SRID:3-4615341970 AND UPS EO B747-5430-75246-A.SDR IPXA2020012151156Panel · discoloredINSPECTION TYPE:C1DISCOLORATION AND CORROSION ON THE INBD LWR PANEL (P/N:323U8740-1) OF PYLON#4.REPAIR I.A.W BOEING SRID:3-4615341318 AND UPS EO B747-5430-75249-A.SDR REXA2020012840055Coaming · worn"INITIAL INSPECTION: WEAR ON CUT OUT (COAMING) OF LATCH DOOR AT LH ENGINE UPPER TRANSCOWL. (MOT1).
""COAMING WAS REPLACED FOR NEW ONE (P/N: CN624-2060-209) PER CRJ900 SRM51-42-10-001-001-A01 AND SRM 51-42-06-001-00SDR REXA2020012800056Spigot · worn"INITIAL INSPECTION: WEAR ON SPIGOT AT TRANSCOWL LATCH DOOR LH ENGINE.(MOT1)
""SPIGOT AT TRANSCOWL LATCH DOOR LH ENGINE WAS REPLACED FOR NEW ONE (P/N: CN624-2067-205) PER CRJ-900 SRM 51-42-06-001-SDR REXA2020012870058Latch · worn"INITIAL INSPECTION: WEAR ON SETTLEMENT AREA OF DOORS 444CT AND 444CB (ON STRUCTURE OF FWD CORE-COWL) RH ENGINE RH-MOT-2
""SUMMARY: REINFORCING LATCH ON ACCES DOORS 444CT AND 444CB WERE REPLACED FOR NEW ONE (2E/A, P/N:CN624-3084-201) PER CRSDR SWIA2020021848747Insert · missingLH UPPER TRANS COWL INBD NYLON SLIDER INSERT MISSING (C-CHECK) RO:2/14/2020REPLACED LH UPPER COWL I/B NYLON SLIDER INSERT AS REQ. REF CRJ 700 AMM.SDR SWIA2020021848737Coaming · chafedLH LOWER TRANS COWL INNER SKIN DOUBLER CHAFED NEXT LATCH ASSY (C-CHECK) RO:2/14/2020INSTALLED NEW L/H LWR TRANS COWL DOUBLER NEXT TO LATCH ASSY. REF REO.SDR SWIA2020021848735Doubler · chafedLH UPPER TRANS COWL INNER SKIN DOUBLER CHAFED NEXT LATCH ASSY. (C-CHECK) RO:2/14/2020REMOVED & REPLACED L/H UPPER TRANS COWL DOUBLER NEXT TO LATCH ASSEMBLY REF REO.SDR SWIA2020021848734Coaming · chafedRH UPPER TRANS COWL INNER SKIN DOUBLER CHAFED NEXT LATCH ASSY. (C-CHECK) RO:2/14/2020 NEW INNER SKIN DOUBLER RH TRANS COWL WAS INSTALLED PER CRJ 700 SRM & BOMBARDIER REO.SDR A6WA2020012247125Bonding Plate · corrodedNR 2 PYLON UPPER TRAILING EDGE, TWO BONDING PLATES HAD CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACE BOTH BONDING PLATES IAW SRM TEMP REV 51-42, SRM 51-42-10, & 51-25-00 REV 37.SDR REXA2020020500139Hinge Arm · looseINITIAL INSPECTION : FREE PLAY ON LATCHES DOOR AT UPPER HALF TRANSCOWL RH ENGINE ( MOT 2 )
SUMMARY OF NRC:00021; HINGE HOUSING WAS REPLCED PER CRJ-900 SRM 51-42-21-001-001-A01. AND SRM 51-42-10-001-001-A01, BUSDR REXA2020020500138Spigot · wornINITIAL INSPECTION : WORN SPIGOT ON DOOR OF LATCHES AT UPPER HALF TRANSCOWL RH ENGINE ( MOT 2 )
SUMMARY OF NRC:00020; SPIGOT WAS REPLACED PER CRJ-900 SRM-51-42-06-001-001-A01.SDR REXA2020020500137Bearing · crackedINITIAL INSPECTION : ELONGATED HOLE, CRACKED AND WORN SETTLEMENT LATCHS SHIMS ON COAMING AT LOWER HALF TRANSCOWL RH ENGINE ( MOT 2 )
SUMMARY OF NRC:00018; COAMING LATCH DOOR AND PAD BEARINGS 2 EA'S (SHIMS) WERE REPLACED PER CRJ-900 SRM 51-42-06-001-00SDR REXA2020020500136Hinge · looseINITIAL INSPECTION : FREE PLAY ON LATCHES DOOR AT LOWER HALF TRANSCOWL LH ENGINE ( MOT 1 )
COMPLETE: SUMMARY OF NRC 00016: FREE PLAY ON LATCHES DOOR AT LOWER HALF TRANSCOWL LH ENGINE (MOT 1 ) WAS ATTENDED PER CRJ-900 SSDR REXA2020020500135Spigot · wornINITIAL INSPECTION : WORN SPIGOT ON DOOR OF LATCHES AT LOWER HALF TRANSCOWL LH ENGINE ( MOT 1 )
SUMMARY: ON NRC. 00013, SPIGOT ON DOOR OF LATCHES AT LOWER HALF TRANSCOWL LH ENGINE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01SDR REXA2020020500134Latch · crackedINITIAL INSPECTION: ELONGATED HOLE, CRACKED AND WORN SETTLEMENT LATCHS SHIMS ON COAMING AT UPPER HALF TRANSCOWL LH ENGINE ( MOT 1 ).SUMMARY OF NRC:00011; PAD BEARINGS (2EAS), COAMING AND DOUBLER WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-13
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