JASC 5420
Service difficulty reports · 3,948
Reports filed under 5420 · Nacelle/Pylon Miscellaneous 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 = '5420' 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 = '5420' 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 SWAA2021082095196Web · crackedRT ENGINE PYLON HAS CRACK ON AFT FAIRING WEB CRACK MEASURES 1' PERFORMED INTERIM REPAIR PER EA REPAIR -54EA-07899 PERMANENT ACTION REQUIRED: ACCOMPLISH OPTION 100 OPTION 2. OPTION 1: PERFORM 737-800 SRM 54-50-70-2R-6.REPAIR 6 TO REPAIR THE CRACKED FLANGE IF ALSDR SWAA2021081817778Fairing · cracked#1 ENG PYLON AFT FITTING IS CRACKED ON THE LOWER O/B SIDE. CRACK GOES INTO THE RADIUS / REMOVED AND REPLACED PYLON FAIRING IAW SRM 51-40-02 REMOVED AND INSTALLED #1 ENG AFT STRUT FAIRING TO FOM IAW AMM 54-52-04SDR C77A2020031000021Angle · crackedLH PYLON #3 HEAT SHIELD AFT OB ANGLE CRACKED. REPLACE #3 HEAT SHIELD AFT OB ANGLE P/N 170-39573-023, REF. EMB SRM 51-40-08, 51-40-02, 51-23-04. WO # 2819309025.SDR SWAA2021082303814Mount · broken#2 ENGINE AFT STRUT FAIRING AFT FAIRING SECTION HAS BROKEN MOUNT CASTING. / REMOVED AND REPLACED AFT FAIRING CAST ASSEMBLY PER SRM 51-40-02.SDR SWAA2021082315197Web · crackedRT ENGINE PYLON HAS CRACKON AFT FAIRING WEB CRACK MEASURES 1' /SDR SWAA2021082097560Stiffener · damagedLEFT ENGINE AFT STRUT FAIRING STIFFENER I/B BOLTS LOOSE WITH ELONGATED HOLES IN STIFFENER. STIFFENER LOCATED UNDER FWD END OF PANEL 434BL. / COMPLIED WITH EA 1-754-2497SDR SWAA2021081831742Stop · brokenBROKEN STRUT FAIRING RING STOP ON AFT COMPRESSION ROD AT RT PYLON (2 EA) / REPLACED RING STOP ON AFT COMPRESSION ROD AT RT PYLON IAW B737-700 SRM 51-10-02-0G-0 DWG 315A2080-6SDR SWAA2021081307952Angle · crackedAFT OF LEFT ENGINE PYLON; UPPER T/E SHELF PANEL MID SEAL BRACKET; ANGLE CRACKED ON FWD SIDE. / REMOVED AND REPLACED PER SRM 51-40-02.SDR RAIA2020031930001Fitting · cracked#1 ENGINE PYLON FWD YOKE LOWER FWD LINKAGE FITTING IS CRACKED - REMOVED AND REPLACED #1 ENGINE PYLON FWD YOKE LOWER FWD LINKAGE FITTING.SDR SWAA2021082302580Panel · cracked#1 ENG STRUT FAIRING AFT O/B PANEL CRACKED. / INSTALLED NEW PANEL PER SRM 51-10-02SDR DALA2020030201512Structure · crackedAD/MTC TASK-FOUND ONE CRACK AT AFT HOLE OF HORIZONTAL FLANGE AT NSTA221.250 AT NO.1 NACELLE,THE CRACK IS IN THE 5 O'CLOCK AT INBOARD OF LH.(ALI SSI 54-50-L16F,54-594-28) HORIZONTAL FLANGE AT NSTA221.250 AT NO.1 NACELLE CRACKED AREA REPAIRED AND ACCOMPLISHED ASSDR DALA2020030201511Structure · crackedAD/MTC TASK-FOUND ONE CRACK AT AFT HOLE OF HORIZONTAL FLANGE AT NSTA221.250 AT NO.2 NACELLE,THE CRACK IS IN THE 4 O'CLOCK AT OUTBOARD OF RH.(ALI SSI 54-50-I16F,54-594-28) HORIZONTAL FLANGE AT NSTA221.250 AT NO.2 NACELLE CRACKED AREA REPAIRED AND ACCOMPLISHED ASDR DALA2020030201510Doubler · crackedMTC TASK-NO.1 PYLON IB UPR DOUBLERS FOUND CRACK AT NSTA230 REPAIRED THE CRACK ON NO.1 PYLON IB UPR DOUBLERS AT NSTA230 AS PER PRI 585398-14 REV.0 THE PRI 585398-14 REV.0 COMPARED AND COMPLIED WITH ERA585398-14 REV.ORIGINAL PLS ACCOMPLISH SEC:II OF ERA 585398-1SDR RAIA2020040160005Channel · crackedR/H PYLON INSIDE ACCESS PANEL 424DB UPPER "U" CHANNEL SUPPORT STIFFNER, P06 X22901.50 IS CRACKED AT O/B END....R&R UPPER "U" CHANNEL IN R/H PYLON ACCESS PANEL 424DB.SDR RAIA2020040160004Channel · crackedR/H PYLON INSIDE ACCESS PANEL 424DB UPPER "U" CHANNEL SUPPORT STIFFNER, P07 X23061.50 IS CRACKED AT O/B END....R&R UPPER "U" CHANNEL IN R/H PYLON ACCESS PANEL 424DB.SDR SWAA2021081908151Support · damagedRIGHT ENGINE AFT STRUT #1 FRAME SUPPORT OUTBOARD 2 HOLES COMMON TO STIFFENER SUPPORT ARE ELONGATED TO .387 / RIGHT ENGINE AFT STRUT #1 FRAME SUPPORT OUTBOARD 2 HOLES COMMON TO STIFFENER SUPPORT ARE ELONGATED TO .387. COMPLIED WITH TIME LIMITED REPAIR PER EA 1-SDR SWAA2021081908149Stiffener · elongatedRIGHT ENGINE AFT STRUT FAIRING STIFFENER COMMON TO THE #1 FRAME SUPPORT OUTBOARD 2 HOLES ARE ELONGATED DUE TO LOOSE FASTENERS / REMOVED AND REPLACED RIGHT STRUT FAIRING STIFFENER COMMON TO #1 FRAME SUPPORT PER SRM 51-40-02.SDR IPXA2020022655481Bracket · gougedINSPECTION TYPE:SEG#1 ENG NOSE COWL T/E, BRACKET FOR FAN COWL GUIDE PIN GOUGEDREMOVED & REPLACEDSDR SWAA2021081315218Angle · crackedLEFT AFT STRUT FAIRING AFT O/B ANGLE CRACKED REF. EA OTHER-54EA-07834 /SDR T17A2020030521004Closeout Panel · crackedR/H UPPER INBOARD PYLON PANEL IS CRACKING AT REAR ATTACH POINTSDR T17A2020031821004Closeout Panel · crackedDURING SCHEDULED INSPECTION MX FOUND A CRACK ON THE RH INBOARD UPPER PYLON PANEL AT THE REAR ATTACH POINT. MX PERFORMED A REPAIR TO THE PANEL IAW BEECHJET 400XP SRM 51-10-00 AND 51-50-10SDR REXA2020030200219Coaming · worn"INITIAL INSPECTION: WEAR ON LATCH DOOR COAMING EXTERNAL FACE AT LH ENGINE. (SM)(MOT 1)
"
"COAMING LATCH DOOR AND DOUBLER WERE REPLACED PER CRJ900 SRM 54-21-00-101-001-A01 AND SRM 51-42-10-001-001-A01 ANDSDR IPXA2020030252639Intercostal · crackedINSPECTION TYPE:2C#2 PYLON CARRY THRU REAR SPAR INTERCOSTAL IS CRACKED AT STA. YID= 375, XID= -7.1 AND ZID= 65.REPAIRED CRACKED #2 PYLON CARRY THRU REAR SPAR INTERCOSTAL AT STA. YID= 375, XID= -7.1 AND ZID= 65 IAW SRM 55-30-02 REPAIR 7 FIG. 204. (MAJOR)SDR SWIA2020033049699Plate · corrodedL/H PYLON UPPER SIDE AFT TRAILING EDGE BOTH BOND PLATES CORRODED (C-CHECK) RO:3/26/2020REPLACED L/H UPPER BONDING PLATES IAW RIL.SDR SWIA2020033049698Plate · corrodedL/H PYLON LOWER SIDE AFT TRAILING EDGE BOTH BOND PLATES CORRODED (C-CHECK) RO:3/26/2020REPLACED L/H LOWER BOND PLATES IAW CRJ200 RIL.SDR SWAA2021082324448Fairing · cracked#1 ENG. AFT PYLON; AFT FAIRING IS CRACKED / R&R'D AFT FAIRING ON #1 ENG. PER SRM 51-10-02 AND SRM 51-40-02SDR SWAA2021082310423Stiffener · cracked#2 NACELLE STRUT FAIRING HAS A CRACKED STIFFENER AT THE AFT END- INBD. SIDE ADJACENT TO THE STABILIZING LINK. / R&R NEW AFT SECTION OF #2 PYLON STRUT FAIRING PER SRM 51-10-02 AND SRM 51-40-02. REFER TO WIP AND SUBTASK SECTIONS FOR INDIVIDUAL SIGNOFFS.SDR RAIA2020021600001Support Angle · crackedL/H SUPPORT ANGLE BETWEEN #5 AND #6 PROFILE BRACKET IS CRACKED .........REMOVED AND REPLACED SUPPORT ANGLE BETWEEN #5 AND #6 PROFILE BRACKETSDR ABXA2020021409032Angle · corrodedCRACKED ANGLE #1 PYLON AFT NACELLE STRUT FAIRING OUTBD UPPER STRINGER ATTACH "L". THE AIRPLANE WAS GROUNDED.SDR A6WA2020021147157Angle · crackedRIB ON LH PYLON LOWER FLANGE CRACKED FS605. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED IAW AWAC SUPPLEMENT 14-252A.SDR RAIA2020020163001Bracket · crackedL/H PYLON #5 AND #6 PROFILE BRACKET IS CRACKED.....................REMOVED AND REPLACED L/H PYLON #5 AND #6 PROFILE BRACKETSSDR SROM2020013020Bracket · crackedREPLACE BROKEN AND CRACKED LT PYLON BRACKET FWD OF O/B LUG FITTING YW STA. 155.20. REPLACED WITH NEW IAW DRAWING NO. 85404001 REV. A AND SRM 51-42-05 REV. 19.SDR SWAA2021081314902Angle · crackedLEFT ENGINE NACELLE AFT OUTBOARD SUPPORT ANGLE CRACKED APPROX 1.5 INCHES LENGTH AND EMANATING INTO ANGLE RADIUS / R & R'D #1 ENG. AFT O/B SUPPORT ANGLE IAW SRM 51-40-02.SDR SWAA2021081924075Bracket · cracked#1 ENG PYLON HAS LEFT SIDE AFT FITTING CRACKED AT PYLON ATTACH POINT / REMOVED AND REPLACED PYLON FAIRING AFT BRACKET ASSY IAW SRM 51-40-02.SDR SWIA2020040649938Fastener · wornCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD FOR THE RH PYLON BY REPLACING AFFECTED FASTENERS AND COLLARS, INCLUDING DOING ALL APPLICABLE RELATED INVESTIGATIVE AND CORRECTIVE ACTIONS, IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUSDR FDEA2020012320197Bracket · crackedNR 1 ENGINE PYLON SUB-STRUCTURE IS CRACKED ON THE OTBD SIDE AT THE TOP OF THE PYLON JUST FWD OF THE WING FWD SPAR. REMOVED AND REPLACED CRACKED BRACKET IAW DWG 313N5004 REV D AND SRM 51-40-02.SDR IPXA2020012251233Support Strut · corrodedINSPECTION TYPE:SEG, RH PYLON AFT UPPER RH SIDE PNL 484BR SUPPORT STRUCTURE CORROSION AROUND SCREW HOLECLEANED SURFACE STRUCTURE OF SCREW HOLE @14B 14A REMOVED CORROSION. FOUND TO BE WITHIN LIMITS IAW SRM 51-73-11 @ RH PLON ONL 484BRSDR IPXA2020012251237Support · corrodedINSPECTION TYPE:SEGLH ENGINE PYLON LH SIDE AFT UPPER AREA PNL SUPPORT STRUCTURE @ RIB 16 HAS CORROSIONREMOVED LIGHT SURFACE CORROSION BY HANDSDR SWIA2020021848613Fairing · crackedLEFT ENGINE NACELLE FAN COWL DOOR HINGE LINE FAIRING 433BB CRACKED (C-CHECK) RO 2/14/2020 ORDERED AND RECEIVED NEW LEFT ENGINE NACELLE FAN COWL DOOR HINGE LINE FAIRING 433BB INSATALLED ON ZONE BOOK JOB 91513340 OP 7004 MX TRASN#19937298.SDR SWAA2021081710375Fairing · delaminatedSTRUT THRUST REVERSER FAIRING PANEL R/H (431ER) HAS DELAM ON FWD EDGE. DELAM IS L= 2 1/4'; W = 3/4'; DAMAGE IS INTO 2 PLYS. / CLOSING DMA #0263513 R&R #1 ENG T/R STRUT FAIRING PANEL 431ER PER M/M 54-53-02 CLEARING #22759SDR V0XD20200203003Stand Off · crackedR/H LOWER TRANS COWL INBD ANGLE WEDGE CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED R/H LOWER TRANSCOWL I/B STANDOFF (P/N: 624-2082-201) IAW CRJ700 SRM 51-42-13 AND 51-42-22.SDR AALA202001239015Stiffener · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON INTERIOR UPPER SPAR STIFFENER CRACKED AT PYLON STATION 153.90 AND NACELLE BL 0. REPAIRED SPAR STIFFENER PER EA 301259.SDR SWIA2020012347972Support Bracket · chafedLH ENGINE OUTBOARD CORE COWL SUPPORT ATTACH BRACKET IS CHAFFED. (C-CHECK) RO:1/22/2020REMOVED AND REPLACED LH ENGINE OUTBOARD CORE COWL SUPPORT ATTACH BRACKET GEMM.SDR SWIA2020012347971Support Bracket · chafedLH ENGINE INBOARD CORE COWL SUPPORT ATTACH BRACKET IS CHAFFED. (C-CHECK) RO:1/22/2020REMOVED AND REPLACED LH ENGINE INBOARD CORE COWL HOLD OPEN ROD BRACKET. REF. GE CF34-8E LMM.SDR SWIA2020012347968Attach Bracket · chafedRH ENGINE INBOARD CORE COWL HOLD UP ATTACH BRACKET IS CHAFFED. (C-CHECK) RO:1/22/2020REMOVED AND REPLACED CHAFFED HOLD UP ATTACH BRACKET ON RH ENGINE INBOARD CORE COWL. REF GE CF34-8E LMM.SDR SWIA2020012347967Attach Bracket · chafedRH ENGINE OUTBOARD CORE COWL HOLD UP ATTACH BRACKET IS CHAFFED. (C-CHECK) RO:1/22/2020REMOVED AND REPLACED RH ENGINE OUTBOARD CORE COWL HOLD UP ATTACH BRACKET. REF. GE CF34-8E LMM.SDR SWAA2020011585181Web · cracked#2 ENGINE OUTBOARD FAN COWL INTERNAL VERTICAL WEB AFT OF OIL SERVICE DOOR IS CRACKED AT UPPER RADIUS / REMOVED INTERNAL VERTICAL WEB AT #2 ENG O/B FAN COWL AFT OF OIL SERVICE DOOR IAW SRM 51-40-02-0G-0. DRILLED NEW WEB IAW SRM 51-40-02-0G-0 AND CMM 71-13-30. ISDR IPXA2020030452753Support Angle · crackedINSPECTION TYPE:CUPON INSPECTION OF #2 PYLON PYLON I/B LWR SIDE SKIRT SUPPORT ANGLE WELD REPAIR EO A300-5454-47743-A STEP 6.B. FOUND CRACK STARING AT RIVET HOLE TOWARD FWD EDGECOMPLIED W/ UPS EO NO A300-5450-75218-A TITLE N131UP NO2 ENGINE PYLON INBRD SIDE LOWSDR SWIA2020012147956Support Angle · damagedDURING RH PYLON DENT REPAIR ON REMOVAL DAMAGED UPPER PYLON SUPPORT ANGLE (C-CHECK) RO:1/17/2020REMOVED AND REPLACED WITH NEW SUPPORT ANGLE RH PYLON COMMON TO FUSELAGE SKIN REF CRJ-200 SRM BOMBARDIER REO AND BOMBARDIER DWG PRESSURE CHECK GOODSDR SWIA2020030348970Stiffener · cracked*RH ENG EXHAUST FAIRING SECOND STIFFENER CRACKED OUTBD LWR SIDE (MARKED) (C-CHECK) RO 2/28/2020 PERFORMED SRS042 DOUBLER REPAIR ON RH ENGINE EXHAUST FAIRING STIFFENER ON OUTBOARD LOWER SIDE REF BOMBARDIER PART#228-50181 CMM. CUT OUT NEW DOUBLER PIECE FROM
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