JASC 5310

Service difficulty reports · 38,528

Reports filed under 5310 · Fuselage Main, 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 = '5310'
  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.

SDR SWIA2021072159619Lintel · cracked*FS280 LINTEL STGR 3L IS CRACKED (C-CHECK RO 7/18/2021) REPAIRED FS280 STR3L LINTEL AREA PER REO 601R-53-21-3463 (REV --) DATED 2021-07-05 (ALL STEPS COMPLIED WITH). / COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.May 11, 2021 · N878AS · Cndair CL6002B19SDR SWIA2021072159617Window Post · cracked* R/H WIINDSHIELD SIDE POST SUPPORT CRACKED. REPLACED RH WINDSHIELD SIDE POST SUPPORT BRACKET PER DWG 601R34032 (REV V) AND CRJ200SRM 51-42-06. / COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.May 11, 2021 · N878AS · Cndair CL6002B19SDR SWAA2021061771382Door Frame · crackedFOUND R1 DOOR FWD UPPER DOOR FRAME / PAN CRACK AT UPPER SECTION. ; / COMPLETED INSTALLATION NEW FRAME (PAN) AT R1 DOOR FWD UPPER CUT OUT REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A8370.;INSTALLED 50% OF FASTENERS AT NEW FRAME (PAN) ON R1 DOOR FWD UPPER CUT OUMay 11, 2021 · N416WN · Boeing 7377H4SDR AALA202105189021Pressure Web · crackedAIRCRAFT IN BASE MAINTENANE: FOUND CRACK IN WING CENTER SECTION VERTICAL PRESSURE WEB AT STA 663.75 AND RBL 25 TO 45. REMOVED AND REPLACED WEB AND INSTALLED DOUBLER AND SHIM REPAIR REF SRM 57-10-10-2R-3 ALT 2.May 11, 2021 · N838NN · Boeing 737823SDR AALA202105133605Door Frame · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON AFT CARGO DOOR FRAME LOCATED AT STA FR 52.5, STR S38R. REMOVED CORROSION AND INSTALLED FILLER PER EA 327642May 11, 2021 · N653AW · Airbus A320232SDR DALA2021051202670Crossbeam · crackedCRACK INDICATION FOUND ON FWD FUSELAGE CROSSBEAM SPLICING HOLE H2 ON FRAME 16 RH SIDE. PERFORMED REPAIR PER ER/A 591347-14AD PRI REV 0,1,2,3 AND ERA 591347-14AD REVISION ORIGINAL. (1806456)May 11, 2021 · N362NW · Airbus A320212SDR DALA2021051202669Crossbeam · crackedCRACK INDICATION FOUND ON FWD FUSELAGE CROSSBEAM SPLICING HOLE H4 ON FRAME 16 RH SIDE. PERFORMED REPAIR PER ER/A 591347-14AD PRI REV 0,1,2,3 AND ERA 591347-14AD REVISION ORIGINAL.May 11, 2021 · N362NW · Airbus A320212SDR DALA2021051202668Crossbeam · crackedSHIP 3262 CRACK INDICATION FOUND ON FWD FUSELAGE CROSSBEAM SPLICING HOLE H3 ON FRAME 16 RH SIDE. CORRECTIVE ACTION: PERFORMED REPAIR PER ERA 591347 14AD PRI REV 0,1,2,3 AND ERA 591347 14AD REVISION ORIGINAL. (1806447)May 11, 2021 · N362NW · Airbus A320212SDR DALA2021051202667Crossbeam · crackedSHIP 3262 CRACK INDICATION FOUND ON FWD FUSELAGE CROSSBEAM SPLICING HOLE H7 ON FRAME 16 RH SIDE. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A 591347-14AD PRI REV 0,1,2,3 AND ERA 591347-14AD REVISION ORIGINAL. (1806445)May 11, 2021 · N362NW · Airbus A320212SDR CALA2021051200640Fitting · corrodedA3NB-53-3-6033: R/H FWD PASSENGER/CREW DOOR LOWER CUTOUT HAS CORROSION AROUND THE SCUFF PLATE ATTACHING ANGLE FASTENER. FURTHER DETAILS AWAITEDMay 11, 2021 · N851UA · Airbus A319131SDR CALA2021051200638Fitting · corrodedMAIN CABIN FLOOR, AFT WET AREA, FR68, R-2 DOOR CUT OUT, LOWER CO RNER FITTING, HAS CORROSION - A3NB-53-3-6222 - NR 9296327 (42327 ) GENERATED BY V917055 AT HAECO LCQ. REMOVED & REPLACED MAIN CABIN AT FR 68 R/H, AFT CORNER FITTING I AW A319 SRM 51-72-11-911-001May 11, 2021 · N852UA · Airbus A319131SDR DALA2021051102639Crossbeam · crackedSHIP 3262 CRACK INDICATION FOUND ON FWD FUSELAGE CROSSBEAM SPLICING HOLE H26 ON FRAME 20 RH SIDE. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 591346-14 AD PRI REV 0, 1, 2 AND ER/A 591346- 14AD REV. ORIGINAL. (1805799)May 11, 2021 · N362NW · Airbus A320212SDR SWAA2021060271207Pressure Deck · dentedMULTIPLE DENTS ON FLIGHT DECK FLOOR WEB DROM STA 250 TO STA 260 AND FROM RBL 2' TO LBL 12'. AREA MARKED. / REPAIRED IAW EA 1-A53-33179. (SA-M 326 A1302995)May 10, 2021 · N8667D · Boeing 7378H4SDR DALA2021051002615Splice · corrodedSHIP 3262 CORROSION INTERNAL STRUCTURE SPLICE AT LEVEL OF FR68 AND BTW STGR 38L TO STGR 38R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SPLICE PER A320 SRM 51-72-11. (1804918)May 10, 2021 · N362NW · Airbus A320212SDR 2A6R2021051060504Pressure Deck · corrodedDURING 1000 HOUR INSPECTION FOUND THE PILOT'S SIDE COCKPIT FLOOR GROUND BRACKET AND UPPER AND LOWER SKIN CORRODED AT F.S. 1700May 10, 2021 · N530LN · Urocop EC135P2SDR 2A6R2021051060503Pressure Deck · damagedDURING A 1000 HOUR INSPECTION FOUND THE LEFT SIDE OF COCKPIT FLOOR BEHIND THE PILOT'S SEAT JUST FORWARD OF F.S. 3150 AND INBOARD OF L.B.L 500 SEVERAL MEDIUM SIZED DENTS AND DELAMINATE UPPER SKIN.May 10, 2021 · N530LN · Urocop EC135P2SDR SWIA2021081060291Stop Fitting · corroded* PASSENGER DOOR LOWER STOP BOLT FITTING CORRODED (C-CHECK RO 8/9/2021) REMOVED AND REPLACED PAX DOOR LOWER STOP FITTING IAW CRJ-700 AMM 52-11-02-000-806-A01 AND 52-11-02-400-806-A01May 9, 2021 · N614QX · Cndair CL6002C10SDR SWIA2021081060282Fitting · chafed* FWD CARGO DOOR SURROUND, UPPER FWD GUIDE FITTING CHAFED/GOUGED (C-CHECK RO 8/9/2021) REPLACED FWD CARGO DOOR SURROUNG UPPER FWD GUIDE FITTITNG IAW CRJ 700 AMM 53-31-23-400-801-A01 / OPS TEST GOODMay 9, 2021 · N614QX · Cndair CL6002C10SDR SWIA202158591Diaphragm · damagedLH DIAPHRAGM AT FS801.25 LOWER IB HOLE IS OVERSIZE (FILED CLOSED) REMOVED AND REPLACED LH DIAPHRAGM AT FS 801 IAW CRJ 700 SRM 51-42-21-001-001-AO1. NO WEIGHT CHANGE PART FOR PART REPLACEMENTMay 9, 2021 · N726SK · Cndair CL6002C10SDR SWIA202158590Diaphragm · damagedLH DIAPHGRAM AT FS768.00 TOP HOLE IS OVERSIZE (FILED CLOSED) REMOVED AND REPLACED LH DIAPHRAGM AT FS 768 IAW CRJ 700 SRM 51-42-21-001-001-AO1.NO WEIGHT CHANGE PART FOR PART REPLACEMENT.May 9, 2021 · N726SK · Cndair CL6002C10SDR CALA2021051000631Service Panel · corrodedB757-06-3-2222 EVIDENCE OF CORROSION FOUND AFT OF LAV SERVICE PA NEL (AREA MARKED) REF HAECO GSO NR LP 9282246 PERFORM AN INSPECTION PER PART 2 OF ECRA 5361--01083 ON OR BEFORE 62,200 TOTAL AIRCRAFT FLIGHT CYCLES. EC/RA 5361-0183, PERFORM AN INSPECTION PER PARMay 9, 2021 · N57868 · Boeing 75733NSDR SWIA2021070959355Door Frame · corroded* CORROSION DETECTED ON SERV DOOR SURROUND STRUCTURE, FIRST (3) VIEWED FWD-T-AFT, WEB FLOOR PROTECTOR, ATTACHMENT "CLEATS". (C-CHECK RO 7/7/2021) REMOVED AND REPLACED NEW CLEATS ON SERVICE DOOR SURROUND STRUCTURE REF CRJ900 SRM 51-42-06-001-001-A01 ANDMay 8, 2021 · N899SK · Cndair CL6002D24SDR SWIA2021070959353Door Frame · corroded* CORROSION DETECTED SERVICE DOOR SURROUND STRUCTURE (INBD) LWR SILL "ANGLE" SEVERAL PLACES BETWEEN F.S. 319.70 AND 349.00 (MARKED). (C-CHECK RO 7/7/2021) REMOVED AND REPLACED NEW LOWER SILL ANGLE ON SERVICE DOOR REF CRJ900 SRM 51-42-06-001-001-A01 AND May 8, 2021 · N899SK · Cndair CL6002D24SDR SWIA2021070959347Buttstrap · corroded* CORROSION ON FS280 BUTT STRAP BETWEEN STGR24L & STGR24R (C-CHECK RO 7/7/2021) REPAIRED CORROSION ON FS 280 BUTT STRAP BETWEEN STR. 24L AND 24R AS PER MHIRJ REO 690-53-21-1376 REV -- DATED 2021-05-22. SEE CONTINUE CARD FOR DETAILS.M-337 AND TASK CARD 5May 8, 2021 · N899SK · Cndair CL6002D24SDR SWIA202158595Rail · brokenMODULE RAIL LOCATED RBL27 FWD OF FS797.00 BROKEN (FILED CLOSED) RECEIVED NEW SERVICEABLE MODULE RAIL FROM STORES. REMOVED AND INSTALLED ON CAMP# 22603115May 8, 2021 · N726SK · Cndair CL6002C10SDR DALA2021051002631Door Frame · damagedSHIP 3356 ERA #572134-14 HAS BEEN ISSUED FOR ELONGATED HOLE IN THE L1 DOOR CUT OUT LOWER AFT CORNER ANGLE FITTING. SECTION 1 IS A TIME LIMITED REPAIR. CORRECTIVE ACTION: INSTALLED SCUFF PLATE LOC IN THE L1 DOOR CUT OUT LOWER AFT CORNER ANGLE FITTING AS PER AMMMay 8, 2021 · N856NW · Airbus A330223SDR AALA202107235100Window Frame · damagedAIRCRAFT IN BASE MAINTENANCE: D= 0.296 INCH HOLE SIZE DIAMETER IN WINDSHIELD FRAMING AT WL 433. REPLACED WINDSHIELD FRAMING COUPLING FITTING LOCATED AT FR4 LEFT STA433 IAW EA 328175.May 7, 2021 · N701UW · Airbus A319112SDR SWAA2021061770322Pressure Deck · corrodedCORROSION FLIGHT DECK FLOOR STRUCTURE AT STA 221 AND ABOUT LBL 40 WITH CORROSION ; / THIS FAULT WILL BE RESOLVED ON ANOTHER FAULT. TTG8Q004YNXH; VERIFIED. FABRICATED WEB (SHEAR TIE) AT COCKPIT LH SIDE BETWEEN STA 219 AND STA 225 LBL 40, WL 208 MATERIAL USED 20May 7, 2021 · N416WN · Boeing 7377H4SDR SWAA2021061770299Pressure Deck · corrodedCORROSION****COCKPIT WEB LHS: STA 219 STA 225; LBL 40; WL 208 ; / FABRICATED WEB (SHEAR TIE) AT COCKPIT LH SIDE BETWEEN STA 219 AND STA 225 LBL 40; WL 208 MATERIAL USED 2024 0 0.040 DIMENSION 5'X 8' IN IAW DWG# 141A5137;HEAT TREATED FABRICATED SHEAR TIE FROM 2May 7, 2021 · N416WN · Boeing 7377H4SDR SWAA2021052770644Panel · crackedAT RAM AIR INLET LIP ASSEMBLY FOUND CRACK AT O/B SIDE AFT CORNER / RECEIVED SERVICEABLE PANEL LT RAM AIR INLET LIP ASSY 191HL APPLIED TOP COAT PER B737-700 AMM 51-21-73-370-803, PANEL WILL BE INSTALLED ON CUSTOMER CARD 5331-1-14524-NG.May 7, 2021 · N747SA · Boeing 7377H4SDR FDEA202105071145Fitting · damagedDURING PERFORMING EO EG-5310-EO332629K P5 STEP 11.P,FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA 998 STGR35L NEAR THE EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y405,AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE OF COUNTERSUMay 7, 2021 · N883FD · Boeing 777FHTSDR FDEA202105071143Fitting · damagedDURING PERFORMING EO EG-5310-EO332629K P6 STEP 13.H, 11 EA YYT-10 FASTENER HOLES WERE 1ST OVERSIDED AT STA 993-1003 STGR35RH-36RH, 3EA YLK-16 FASTENER HOLES WERE OVERSIZED TO 0.562" AT STA1024 STGR36RH-37RH. REPAIR CARRIED OUT TO 11EA YYT-10 FASTENER HOLESMay 7, 2021 · N883FD · Boeing 777FHTSDR FDEA202105071146Fitting · damagedDURING PERFORMING EO EG-5310-EO332629K P6 STEP 11.M, FOUND 01 EA EXISTING HOLES OVERSIZED (DIAMETER:0.434") ON THE SKIN AT STA 993 - STA1035,STGR 35R - 37R. THE BOEING DRAWING 675W0002 SH 7 VIEW 1B6 CALL OUT THE DIAMETER 0.371". COMPLIED WITH EO: G-5310-E0May 7, 2021 · N883FD · Boeing 777FHTSDR FDEA202105071144Fitting · damagedDURING PERFORMING EO EG-5310-EO332629K P5 STEP 11.M,FOUND 01EA EXISTING HOLES OVERSIZED (DIAMETER:0.434") ON THE SKIN AT STA 993-STA 1035 STGR 35L-37L. THE BOEING DRAWING 675W0002 SH 7 VIEW 1B6 CALL OUT THE DIAMETER 0.371". COMPLIED WITH EO: G-5310-E033262May 7, 2021 · N883FD · Boeing 777FHTSDR SCNA20210514027Frame · crackedCRACK AT FASTENER HOLE STA 727B S8L. REPAIRED CRACK IN FRAME AT FASTENER HOLE @ STA. 727B, STR 8L PER ER # 21-01759 REV IR AND ENG-53SCA-10739 REV 00May 7, 2021 · N815SY · Boeing 7378BKSDR DALA2021051102646Pressure Deck · crackedSHIP 651 CRACK IN FLOOR WEB OUTBD OF RBL 26 AT FLOOR LINE. STATION 199. CORRECTIVE ACTION: REMOVE WEB, FABRICATED NEW WEB, INSTALLED, TREATED AND PRIMED REF DRAWING. (1802763)May 7, 2021 · N651DL · Boeing 757232SDR CALA2021051000624Door Frame · crackedL1 DOOR FRAME 16 STOP FITTING NO7 LWR INBRD HOLE IS CRACKED IN TH E INTERCOSTAL FITTING AND UPPER INBRD HOLE IS CRACKED IN THE WEB AND INTERCOSTAL. REPAIR B EFORE NEXT FLT CONTACT ENG APPROVED R ERPAIR INSTRCTIONS PER NR 9292142 / 22142 GEN BY V061633 ACCOMPLIMay 7, 2021 · N468UA · Airbus A320232SDR CALA2021051000627Fitting · crackedDURING ROTO-PROBE OF RH FR16 NO 1 DOOR STOP FITTING, A CRACK INDIC ATION WAS NOTED IN THE UPPER I/B HOLE AT 2 O''CLOCK. CRACK INDICA TION IS IN THE INTERCOSTAL. PER VT NRC 0001666. GENERATED BY V93 4208 REMOVED AND REPLACED INTERCOSTAL FITTING P/N D53114236201May 7, 2021 · N851UA · Airbus A319131SDR DU4R2021050700071Shear Web · crackedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND SHEAR WEB FRAME 592.4 OF FWD CARGO DOOR AFT FRAME IS CRACKED. S/O 660006 N/R 38630May 7, 2021 · N362NC · Boeing 737330SDR VNAA202105079993Structure · corrodedCIRCUMFERENTIAL JOINT INTERFACE CORRODED BETWEEN FS280 TO FS282 ABD BETWEEN STGR 25R AND STGR 25L.May 7, 2021 · N718PS · Cndair CL6002C10SDR SWIA2021081060289Fitting · corrodedPASSENGER DOOR SURROUND STRUCTURE FITTING. LOCATED TOWARD FWD AT THE MID SECTION HAS CORRODED FASTENER AND NUTPLATE. IDENTIFIED WITH TAPE. (C-CHECK RO 8/9/2021) REPLACED HARDWARE AND NUTPLATES ON PAX DOOR SURROUND STRUCTURE FITTING IAW CRJ 700 SRM 51-May 6, 2021 · N614QX · Cndair CL6002C10SDR SWIA2021081060288Fitting · corrodedPASSENGER DOOR SURROUNDING STRUCTURE FITTING. LOCATED TOWARD AFT AT THE MID SECTION HAS CORRODED FASTENER (1) AND NUTPLATE. IDENTIFIED WITH TAPE. (C-CHECK RO 8/9/2021) REMOVED AND REPLACED NUTPLATE AT PAX DOOR SURROUND STRUCTURE MID LOCATION REF CRJ70May 6, 2021 · N614QX · Cndair CL6002C10SDR SWAA2021060469781Door Frame · crackedR1 DOOR SURROUND;FWD TOP CORNER INSIDE THE FRAME BEHIND THE T/T LATCH RECEIVER EVIDENCE OF A CRACK AT FASTNER (MARKED) ; / TASK COMPLETE; FINAL AUDIT C/W; FINAL AUDIT C/WMay 6, 2021 · N220WN · Boeing 7377H4SDR MASA20210528220Stringer · corrodedCORROSION ON STRINGER 24RH IN STA. FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT |STRINGER 24RH IN STA . FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-20-001-001-A01May 6, 2021 · N953LR · Cndair CL6002D24SDR IPXA2021052169654Window Frame · corrodedINSPECTION TYPE:2CCAPT'S WINDSHIELD LOWER FRAME HAS CORROSION.REPAIRED CAPT'S WINDSHIELD LOWER FRAME IAW VT-SAA EA 011-5310-01-A9112 REV. I/R AND UPS EO MD11-5310-80419-A. (MINOR)May 6, 2021 · N260UP · Doug MD11FSDR REXA2021051900338Angle · corrodedL/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED AND REPLACED R/H CROSSBEAM, UPPER DOUBLE ANGLE AND LOWER DOUBLER ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-22-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 53-11-4May 6, 2021 · N368CA · Cndair CL6002C10SDR REXA2021051900337Crossbeam · corrodedL/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED & REPLACED LH 280 CROSSBEAM IAW CRJ 700 AMM 53-11-41-201-003-A01. WVAC EMP #6027May 6, 2021 · N368CA · Cndair CL6002C10SDR REXA2021051900336Crossbeam · corrodedL/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED & REPLACED LH 280 CROSSBEAM IAW CRJ 700 AMM 53-11-41-201-003-A01.May 6, 2021 · N368CA · Cndair CL6002C10SDR REXA2021051800344Angle · corrodedR/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED AND REPLACED R/H CROSSBEAM, UPPER DOUBLE ANGLE, LOWER DOUBLER ANGLE, TEE FITTING AT RBL 9 AND J-ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-20-001-001-A01, 51-42-13-001-001-A01, 5May 6, 2021 · N368CA · Cndair CL6002C10SDR REXA2021051800343Angle · corrodedR/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED AND REPLACED R/H CROSSBEAM, UPPER DOUBLE ANGLE, LOWER DOUBLER ANGLE, TEE FITTING AT RBL 9 AND J-ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-20-001-001-A01, 51-42-13-001-001-A01, 5May 6, 2021 · N368CA · Cndair CL6002C10
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