JASC 5350
Service difficulty reports · 6,118
Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350' 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 = '5350' 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 JR2R20241102845Doubler · corrodedLOWER BEACON LIGHT BASE PLATE ON WING TO BODY FAIRING CORRODED. REPLACEDSDR MAS2024F00017Doubler · corrodedLOWER BEACON LIGHT BASE PLATE ON WING TO BODY FAIRING CORRODED. REPLACEDSDR SWAA2024112555555Radome · delaminatedPER CUSTOMER REQUEST; FOUND NOSE RADOME DELAMINATED AT THE VERY TIP MARKED<[01] REMOVED DAMAGED RADOME BOOT AND FOUND A DELAMINATION IN THE COMPOSITE AT THE DISCREPANT LOCATION IAW AMM 53-52-00-000-802 PARAGRAPH 4.C(1-2).;[02] VERIFIED CORRECTIVE ACTION 1;[03]SDR HNAA2024120901175Attach Bracket · cracked53-2089 RH WING, WING TO BODY FAIRING ATTACH BRACKET #2 CRACKED JUST AFT OF SPAR 2. RAR ATTACH BRACKET IAW SRM 51-40-02SDR R61A2024111700539Strap · corrodedAFT WING TO FUSELAGE FAIRING ATTACHMENT STRAP BETWEENFR73-FR75, BETWEEN STR29L-STR23L FOUND CORRODED. CORRODED AFT WING TO FUSELAGE FAIRING ATTACHMENT STRAP BETWEEN FR73-FR75, STR29L-23L REMOVED AND REPLACED IAW SRM51-41-02 AND 51-43-04.SDR R61A2024111700538Strap · corrodedAFT WING TO FUSELAGE FAIRING ATTACHMENT STRAP BETWEEN FR73-FR75, BETWEEN STR29R-STR23R FOUND CORRODED. CORRODED AFT WING TO FUSELAGE FAIRING ATTACHMENT STRAP BETWEEN FR31-FR75, BETWEEN STR29R-23R REMOVED & REPLACED IAW SRM 51-41-02 & 51-43-04SDR VNAA202411290027Strap · corrodedDESCRIPTION
SECONDARY NRC: AFTER REMOTION OF CHANNEL///CORROSION ALONG OF ALL STRAP
CORRECTIVE ACTION
CORROSION ON STRAP WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED,THEREFORE IT IS OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND
MANUSDR CALA2024102900955Fairing · damagedUPON WALKAROUND FOUND PANEL 193DL MISSING ABOVE LH WING PART NIS IAD. PARTS UPDATED IN MATERIALS. MORE ITEMS ADDED TO MATERIALS AS PRECAUTIONARY. ALSO REQUIRES 12 EA BACB30LH3-5 (BOLTS), CANNOT ADD MORE ITEMS INTO MATERIALS. GVI OF THE PANEL ATTACH BRACKETS, FSDR DALA2024102410382Support · crackedSHIP 3133 CRACK SUPPORT WEB BELLY FAIRING LOC. FR 52 LH SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 621595-14. (0624225)SDR VNAA202411290030Fitting · corrodedDESCRIPTION: CORROSION ON FITTINGS AND HINGES OF SERVICE DOOR 196ER.
CORRCTIVE ACTION:
SUMMARY: FITTINGS AND HINGES WERE REMOVED PER CRJ-900 AMM 52-45-01-000-801 (CONFIG A01) AND SRM 51-41-02-001-001-A01, HINGES AND FITTINGS WERE MANUFACTURED PER NRC 00SDR VNAA2024101630015Angle · corrodedCORROSION ON MLG FAIRING SUPPORT STRUCTURE FS 821.76 SUPPORT ANGLE P/N BA670-30000-7955 (QTY. 2) AND P/N BA670-30000-7959 (QTY. 2)SDR SWAA2024102350789Panel · delaminatedPANEL 192BL IS DELAMINATED<[01] R&R PANEL 192BL PER AMM 53-51-21. REFERENCE TTG8Q00W949JSDR YENA2024102201388Tail Cone · damagedDURING HEAVY MAINTENANCE: FUSELAGE/ REAR FUSELAGE/ TAIL CONE/ FR 78-81 STGR 2L-2R/ MULTIPLE DAMAGE- PERMANENT REPAIR; REFERENCES /1/ AEROMAN EA 53-9042-24 COVER R0 AND PARTS 1-3 /2/ RDAF 81457190/005/2024 ISSUE A /3/ TD/81457190/058/2024#A. DURING CURRENT (10/SDR DALA2024101810197Access Panel · damagedSHIP 3142 HOLE ACCESS PANEL 192KB BELLY FAIRING ON EXISTING REPEIR LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED ACCESS PANEL 192KB BELLY FAIRING AT LOWER FUSELAGE AS PER ER/A 529512-14MA. (0614169)SDR 2024F00254Fairing · damagedDURING INSPECTION 80 HOLES WERE OVERSIZED DURING HI-LOCK REMOVAL ON THE BELLY FAIRING. 40 OVERSIZED HOLES AT LWS 37 AND 40 OVERSIZED HOLES AT RWS 37. REPAIR WAS ACCOMPLISHED IAW AQRD ENGINEERING REPAIR ORDER ERO-981793 AND CESSNA 680 SRM 51-40-03.SDR UIEA2024101100983Bracket · corrodedCORROSION - BRACKET, WING TO BODY FAIRING INTERNAL PNL SUPPORT STUCTURE STA 921. LBL 1.(<P>1. REMOTE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV=101. 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV=101 AND BOEING DWG #65B06704, SH2 REV=F AND NO: 65B04118 SH6 REV=A. SDR UIEA2024101100984Support Angle · corrodedCORROSION-ANGLE WING TO BODY FAIRING INTERNAL PNL SUPPORT STRUCTURE STA 894 LBL 5.(<P>1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G-0 REV.101. 2. INSTALL NEW PART I.AW SRM 51-40-02-0G-0 REV.101 AND DWG #65B06714 SH3 REV.F, 65B06714 SH5 REV.A. 3. JOB COMPLETED ASDR UIEA2024101100985Support Angle · corrodedCORROSION-ANGLE WING TO BODY FAIRING INTERNAL PNL SUPPORT STRUCTURE STA 930 LBL 4.(<P>1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G-0 REV.101. 2. FABRICATED PART I.A.W W/S #40804. 3. INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV=101 AND DWG #65B06712 SH3 REV=G & SSDR DALA2024101410086Access Panel · delaminatedSHIP 3144 DELAMINATED ACCESS PANEL 191BB BELLY FAIRING AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED ACCESS PANEL 191BB AT LOWER FUSELAGE AS PER ER/A 542077-14. (0604590)SDR DALA2024101510104Flange · brokenDURING REMOVAL OF WTBF PANEL 195HB FOUND WTBF LONGERON ASSEMBLY NUT PLATE ATTACHMENT FLANGES BROKEN 2 EA P/N: C02383111-001. INSTALLED WTBF LONGERON ASSEMBLY P/N: C02383111-001 IAW A220 ASRP 51- 42-21 AND AMDS WC 5352-01038-01A ASSOCIATED AA 5352-01038 ADDED FSDR DALA2024101410068Radome · delaminatedSHIP 3160 DELAMINATION EXTERNAL SKIN NOSE RADOME. CORRECTIVE ACTION: REPLACED NOSE RADOME AS PER A320 FAM AMM 53-15-11-000-001-A. (0602710)SDR DALA2024101009961Radome · damagedSHIP 3152 FOUND RADOME DAMAGE ON BIRD STRIKE INSPECTION. CORRECTIVE ACTION: REMOVED DAMAGED RADOME AND INSTALLED SERICEABLE ONE PER A319 AMM 53-15. (9997973)SDR SWIA202510210007Fairing · corrodedMLG SUPPORT ASSY FAIRING RH HAS CORROSION. (C-CHECK RO 10/20/2025)COMPLIED WITH REO 670-53-83-163 FOR THE REPAIR OF R/H MLG SUPPORT ASSY FAIRING. TASK CARD 51-900-1002-SKY COMPLETED, M-337 ATTACHEDSDR CALA2024100802603Door · damagedRIGHT LOWER WING TO BODY PANEL DOOR 192DR GOUGE AT AFT EDGE INNER SURFACE STRUCTURE REF AAR N/R 9902980 ACCOMPLISHED REPAIR AT WING CENTER SECTION LOWER SUPPORT BEAM LOWER CHORD RBL 40.875 IAW SRM B737-900ER 57-10-13-2R-3.SDR QXEA2024100700231Fairing · crackedCRACK IN LEFT HAND WHEEL WELL FORWARD PANEL JUST BELOW THE PARKING BRAKE VALVE. REMOVED FROM SERVICE. C/W T/C ETD2024-170-026814/1. TAPE APPLIED AS TEMP REPAIR. RETURNED TO SERVICE. NO PARTS REPLACED.SDR SWAA2024103145317Radome · crackedNOSE RADOME EXTERNAL AREA FWD CENTER SECTION HAS CRACK<[01] INSTALLED NEW PROTECTIVE BOOT AT NOSE RADOME PER B737AMM53-52-00-400-802 PART USED BOOT PO#2090506;[02] VERIFIED WORK PERFORMEDSDR SWAA2024111144743Support Angle · crackedR/H FUS FWD BODY FAIRING SUPPORT ANGLE CRACKED AT FASTENER'S TAIL I/B KRUEGER FLAP # 3 MKD DOT<[01] REMOVED AND REPLACED R/H FUS FWD BODY FAIRING SUPPORT ANGLE IAW<BR>SRM 51-40-02-0G-0 AND DWG 116A3118;[02] VERIFIED STEP 1SDR HNAA2024110101052Support Angle · cracked53-2243 BODY FAIRING 195EL UPPER SUPPORT ANGLECRACKED AT X14216.5. RAR ANGLE IAW SRM 53-23-12SDR HNAA2024110101051Support Angle · cracked53-2245 BODY FAIRING 195EL LWR SUPPRT ANGLE CRACKED AT X13801.5. REPAIRED IAW SRM 57-20-07SDR DALA2024092609449Fairing · brokenSHIP 3147 BROKEN WING TO FUSELAGE FAIRING (192KB PANEL). CORRECTIVE ACTION: REMOVED BROKEN WING TO FUSELAGE FAIRING (192KB PANEL) PER A319 AMM 53-35 AND INSTALLED REPLACEMENT WING TO FUSELAGE FAIRING PER A319 AMM 53-35. (5883882)SDR UIEA2024092300928Bracket · corrodedCORROSION - BRACKET FWD FUSELAGE LOWER SURFACE WING TO BODY AREA STA 920.(<P>1. REMOVED CORROSION BRACKETS IAW SRM 51-40-02-0G-0 REV=60. 2. INSTALLED NEW BRACKETS IAW DWG 65B06704 SH2 REV. H, 65B04118 SH2 REV. P AND SRM 51-40-02-0G-0 REV. 60. 3. CONDITION CHECSDR SWAA2024092540305Panel · debondedWING TO BODY FAIRING PANEL 192CL DISBANDED AT EDGE. REF.TTG8QVJS7H<[01] ACCOMPLISHED PERMANENT REPAIR TO PANEL 192CL; PER SRM 53-40-70-1A-1. AND RESTORED FINISH PER AMM;51-21-99.;[02] EDITED: ADDED DAMAGE REPAIR TYPESDR SWAA2024091637450Radome · crackedDURING ETOPS PDSC WALK AROUND; FOUND SEVERAL CRACKS AND DELAMINATED DIVETS ON RADOME SURFACE.<[01] REMOVED AND REPLACED RADOME IAW AMM 53-52-00SDR SWAA2024101535766Radome · deterioratedDETERIORATED EXTERNAL RADOME DIVERTER STRIP RT SIDE AT AFT POSITION AT UPPER FUSELAGE 2024-559019<[01] REPLACE RADOME AT UPPER FUSELAGE IAW ROW 44 BROADBAND ANTENNA B737-800 AMMS 23-36-12 SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK CARD COMPLETED<BR>REPLACE RADOMESDR A6WA202409108807Sealant · failedDURING CLIMB ABOVE 10K AND SPEED 268KTS A/C BUFFETS. WAS NOT FELT IN YOKE, AP WAS DISENGAGED. BUFFETING NOT PRESENT ABOVE 270KTS AND BELOW 265KTS. FLIGHT CONTROLS OPERATE NORMALLY WHEN BUFFETING OCCURS. BUFFETING OCCURS AT APPROX 2* NOSE UP AND 2* NOSE DOWN. SDR SWAA2024091135054Tail Cone · delaminatedFUSELAGE SECTION 48 DELAMINATION COMMON TO TAIL CONE<[01] PERFORMED PERMANENT REPAIR OF THE TAIL CONE IAW SRM 51-70-04SDR SWAA2024091135091Panel · crackedCRACK ON PANEL 194 FL; EDGE OF APU DRAIN MAST HOLE. CRACK ON PANEL 194 FL EDGE OF APU DRAIN MAST HOLE.<[01] ACCOMPLISHED PERMANENT REPAIR PER.SRM.53-60-70-2R-1 REPAIR1; AND SRM.51-70-05-2R-1 REPAIR 1.;[02] C/WSDR SWAA2024091135180Panel · delaminatedPANEL 194GL HAS DELAM 10IN. L X 1.25W EXTENDING 4IN.12IN. AFT OF PANEL L/E AND 13IN. UP FROM PANEL LOWER EDGE. PANEL 194GL HAS DELAM 10IN. L X 1.25W EXTENDING 4IN.12IN. AFT OF PANEL L/E AND 13IN. UP FROM PANEL LOWER EDGE.<[01] REPAIRED PANEL PER SRM 53-60-70-2SDR SWAA2024101634869Angle · crackedCRACK SUPPORT STRUCTURE WING TO BODY FAIRING ANGLE BS 500D AT LEVEL STRINGER 19R AT LOWER FUSELAGE 2024-565327<[01] REPLACED SUPPORT STRUCTURE WING TO BODY FAIRING ANGLE BS 500D AT LEVEL STRINGER 19R AT LOWER FUSELAGE I.A.W. B737-700 SRM 51-40-02 AND DRAWING #SDR SWAA2024101634870Angle · crackedCRACK SUPPORT STRUCTURE WING TO BODY FAIRING ANGLE BS 500D AT LEVEL STRINGER 19L AT LOWER FUSELAGE 2024-565328<[01] REPLACED SUPPORT STRUCTURE WING TO BODY FAIRING ANGLE BS 500D AT LEVEL STRINGER 19L AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02-0G-0 AND DRAWINGSDR HNAA2024092500863Angle · crackedLH WING TO FUSE FAIRING LWR ANGLE CRACED AT FR47. RAR ANGLE IAW SRM 51-40-02.SDR HNAA2024092500864Angle · cracked53-2036 RH WING TO FUSE FAIRING LWR ANGLE CRACKED AT BTW FR47-48. RAR ANGLE IAW SRM 51-40-02SDR IPXA2024091744748Fairing · damagedLH BODY FAIRING PANELS DAMAGED OPEN SEPARATE ITEM FOR PANEL 193BL UNDER TASK [T3F18E0054ZFR], PANEL 193CL UNDER TASK [T3F18E0054ZFZ], PANEL 193DL UNDER TASK [T3F18E0054ZG1], PANEL 193FL UNDER TASK [T3F18E0054ZG2] AND PANEL 193GL UNDER TASK [T3F18E0054ZG3] NO FSDR DALA2024090608755Cable · brokenMAINTENANCE FOUND A BROKEN KEVLAR CABLE AT THE TAIL CONE SLIDE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00917: THE KEVLAR CABLE AT TAIL CONE SLIDE WAS REPLACED PER B717 AMMSDR IPXA2024090644748Fairing · damagedLH BODY FAIRING PANELS DAMAGED FOLLOWING PANELS FOUND DAMAGED. 193GL WITH A DELAMINATION AT 3" TO 13" FROM FWD EDGE AND 26" TO 28" FROM INBD CORNER<BR><BR>193FL WITH A DELAMINATION AT 22,5" TO 29" FROM OUTBD EDGE AND 8" TO 19" FROM AFT EDGE AND A SECOND DELAMISDR SWI2024F01224Support Angle · corrodedSUPPORT ANGLE OF WING FAIRING 196 AR ON RH AND LH HAS CORROSION. (C-CHECK RO 11/9/2024) SUPPORT ANGLE FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED IAW CRJ700 SRM 51-40-06SDR SWIA202411250903Fairing · crackedAFT WING TO BODY L/H DIAPHRAGM HAS A CRACK AT FS909. (C-CHECK RO 11/23/2024) REPAIRED AREA ON AFT WTB LH DIAPHRAGM AT 909.00 IAW REO 670-53-82-478 REV-A DATE: 2014-11-12NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S102524-4 PO# 174025 DATE SDR IPXA2024092390936Strap · corrodedINSIDE AFT TAIL COMPARTMENT EXFOILATION CORROSION AT STA 1787.4 R/H INTERNAL UPPER AT APU AIR INLET DUCT. DOT 140-007 INSTALLED 5EA REPAIR PARTS, 1EA AFT STRAP, NEW STRAP P/N 148N3138-20, 2 UPPER ANGLES STRAP, 2 LOWER ANGLES STRAP AND REPAIR WASHER IAW B757 SRSDR CALA2024090300532Panel · missingPDA 1 MISSING PANEL AFT OF L MLG ON LEFT BOTTOM OF FUSELAGE. FOUND PANEL 194CL MISSING FROM AIRPLANE. SEE PIC FOUND PANNEL 194CL MISSING. PERFORMED WALK AROUND INSPECTION PER AMM 03-00-00-200-802. NO DAMEGE FOUND ON AIRCRAFT. RAN FLAPS UP AND DOWN PER AMM 27-5SDR SWAA2024082930485Radome · crackedNOSE RADOME PROTECTIVE BOOT CRACKING<[01] C/W;[02] REMOVED AND REPLACED NOSE RADOME IAW B737 AMM 53-52-00. ADJUSTMENT AND BOND CHECK IS GOOD
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