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 IXXA2022070001Door · corrodedRT WHEEL WELL PRESSURE DECK CORRDED STA 1094 RBL 47May 16, 2022 · N752CX · Boeing 757200SDR IXXA2022062302Pressure Deck · corrodedLT WHEEL WELL PRESSURE DECK CORRODEDMay 16, 2022 · N752CX · Boeing 757200SDR FDEA202205161395Seat Track · crackedMAIN DECK CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE - SEAT TRACK CRACKED, BETWEEN FR20 AND FR21, Y1959 COMPLIED WITH FEDEX EA: 6-5310-T0368594 PT1, EA TITLE: FUSELAGE - MAINFRAME - MCD Y1959 SEAT TRACK BENT AND CRACKED BETWEEN FR20 AND FR21 - REPAIR. REPAMay 16, 2022 · N671FE · Airbus A300*SDR SIMA20220516003None · noneFUSELAGE SKIN PUNCTURED BETWEEN FR 10/11 AND STR 20R/21R.( MAJOR REPAIR)-C/A-INSTALLED REPAIR DOUBLER, TRIPLER, AND FILLER IAW ERS-EM-53MR-4533May 16, 2022 · N918AE · Emb EMB145LRSDR SIMA20220516004None · noneFRAME 10 BENT BETWEEN STR 20R/21R. (MAJOR REPAIR)-C/A-PERFORMED DENT REPAIR IAW ERS-EM-53MR-4533May 16, 2022 · N918AE · Emb EMB145LRSDR CALA2022051601247None · cracked(AD2016-14-03) DURING ROTO PROBE OF FR35 STRINGER 28-31 FOUND LH S HOLE #2 CRACKED AND HOLE #4 WITH REJECTABLE DAMAGE. CONTACT EN GNEERING FOR REPAIR INSTRUCTIONS BEFORE FURTHER FLIGHT (REPAIR I AW R DWG & ECRA)May 15, 2022 · N478UA · Airbus A320232SDR IPXA2022052582522Bracket · crackedINSPECTION TYPE:SEGMDC AT FR21 RH SIDEALL UPPER PANEL SUPPORT STRUCTURE BRACKET DEFORMED/CRACKED.FABRICATED AND REPLACED BRACKET IAW SRM 53-13-18, SRM 51-70-12 AND SRM 51-40-21May 14, 2022 · N131UP · Airbus A300F4622RSDR ASAA2022051438376Intercostal · crackedCRACKED INTERCOSTAL BETWEEN FS328-FS344 LBL 48. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL BETWEEN FS328-FS344 LBL 48 IAW B737-800 SRM 51-40-02-0G-0.May 14, 2022 · N564AS · Boeing 737890SDR IPXA2022051482089Frame · dentedINSPECTION TYPE:SEG4FWD.PIT FRAME DENTED TWO PLACES IN UPPER J ANGLE STA 680 BETWEEN S-23L AND S-26LREPAIRED IAW SRM 53-00-07-2R-5 DETAIL III PER SRM 53-30-07-2RMay 14, 2022 · N412UP · Boeing 75724APFSDR SWAA2022061607782Channel · corrodedCORROSION ON MOP SILL AT FWD PASSENGER CABIN BS298 - BS328 RBL55. / [01] VERIFIED APPLICABILITY TO SRM 53-10-15-1A=2<BR>REMOVED CORROSION ON MOP SILL L=5.0 ; W=2.0 ; D=.025 MATERIAL ORIGINAL THICKNESS .080 MATERIAL REMAINING .055' AT FWD SERVICE DOOR RBL 55 BSMay 13, 2022 · N7876A · Boeing 7377Q8SDR SWAA2022061607785Support Angle · corrodedCORROSION ON THRESHOLD SUPPORT AT FWD PASSENGER CABIN BS294+11; BS314 RBL57 WL208. / [01] REMOVED CORROSION ON THRESHOLD SUPPORT ANGLE L=2.0 ; W=1.0 ; D=.020 MATERIAL ORIGINAL THICKNESS .090 MATERIAL REMAINING .070 FWD SERVICE DOOR BS 312 = 1 RBL 57 WL 208 PERMay 13, 2022 · N7876A · Boeing 7377Q8SDR SWAA2022061607788Intercostal · crackedCRACKED INTERCOSTAL AT FWD PASSENGER CABIN BS277+7 BL0 WL208. / [01] REMOVED CRACKED INTERCOSTAL FROM FWD PASSENGER CABIN BS 277+7 BL 0 WL 208 . LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-05 AND DWG # 141A5410 ; 0K TO INSTALL;[02] INSPECTED & VERIFIED CMay 13, 2022 · N7876A · Boeing 7377Q8SDR SWAA2022061407783Intercostal · crackedCRACKED INTERCOSTAL AT FWD PASSENGER CABIN BS317 RBL31 WL208. / [01] VERIFIED APPLICABILITY AS PER SRM 53-10-51-1A-1.<BR><BR>CRACK WAS FOUND OUT OF LIMIT DUE DISTANCE FROM HOLE; NO PERMITTED; IAW SRM 53-10-51-1A-1 STEP 4.B(1)(A); FIG.105.<BR><BR>LOCATED AND DRMay 13, 2022 · N7876A · Boeing 7377Q8SDR SWAA2022061407784Support Angle · crackedCRACKED SUPPORT ANGLE AT FWD SERVICE DOOR BS294 RBL53 WL208. / [01] CRACKED SUPPORT ANGLE AT FSD FOUND TO BE OUT OF LIMITS I.A.W SRM 53-10-51-1A-1; PART WILL BE REPAIRED BY REPLACEMENT I.A.W SRM 51-10-02-0G-0;[02] REMOVED CRACKED SUPPORT ANGLE AT FSD BS294 RBLMay 13, 2022 · N7876A · Boeing 7377Q8SDR SWAA2022061407789Intercostal · crackedCRACKED INTERCOSTAL AT FWD PASSENGER CABIN BS312+9 LBL46 WL208. / [01] VERIFIED APPLICABILITY AS PER SRM 53-10-51-1A-1. CRACK WAS FOUND OUT OF LIMIT DUE DISTANCE FROM HOLE; NO PERMITTED; IAW SRM 53-10-51-1A-1 STEP 4.B(1)(A); FIG.105.<BR><BR>LOCATED AND DRILLEDMay 13, 2022 · N7876A · Boeing 7377Q8SDR SWAA2022061307690Threshold · corrodedFWD SERVICE DOOR CUTOUT STRUCTURE UNDER THRESHOLD CORRODED. / [01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO OUT OF LIMITS PER SRM 53-10-15.;[02] REMOVED AND REPLACED FWD SERVICE DOOR THRESHOLD ANGLE IAW SRM 51-40-02.;[03] COMPLETED CORROSIONMay 13, 2022 · N8631A · Boeing 7378H4SDR SWAA2022053107717Skin · brokenBROKEN EXTERNAL SKIN NUT PLATES BS 663 TO BS 706 BTW STR 1 TO STR 2R AT UPPER FUSELAGE ( (REFERENCE SRM 53-40-01-2R-1) 2022-239678 REPAIR SKIN LOC ON AREA ADF N.1 ANTENNA BS 663 TO BS 706 BTW STR 1 TO STR 2R AT UPPER FUSELAGE IAW B737-700 SRM SRM 53-40-01-2R-May 13, 2022 · N7841A · Boeing 7377L9SDR IPXA2022052382371Floor Panel · corrodedINSPECTION TYPE:3CMAIN CABIN FLOOR PANEL IS CORRODED BETWEEN STA. X=75.260 TO X=47.500.REMOVED AND REPLACED FLOOR PANEL IAW AMM 53-21-10-400-801. (MINOR)May 13, 2022 · N257UP · Doug MD11FSDR QXEA2022051600195Floor Mat · looseNON SLIP FLOORING ON THE TOP OF THE AIRSTAIRS IS PULLED UP AND IS A TRIPPING HAZARD. REMOVED FROM SERVICE. REMOVED PEELED UP NON-SKID TAPE AND REPLACED WITH A NEW PIECE. NO TRIPPING HAZARD EXISTS. AIRCRAFT RETURNED TO SERVICE.May 13, 2022 · N445QX · Bombdr DHC8402SDR CALA2022051301231Stiffener · crackedSUPPORT TASK : EA 5310-07143 REV D OP 002 (AD 2017-17-16) RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BETWEEN WL 159 TO 185 FOUND 1EA CRACK AS MARKED TRANSFER REF HXWO 779691 AND ORIGINATED BY EMP V914372 RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BMay 13, 2022 · N686UA · Boeing 767300SDR SWAA2022061607300Angle · crackedCRACK IN VERTICAL L ANGLE BS 692 RBL 0.5 WL 206.5 / [01] REMOVED ANGLE AT VERTICAL ANGLE BS 692 RBL .5 WL 206.5 PER SRM 51-40-02;[02] VERIFIED THE APPLICABILITY OF SRM 51-40-02-0G-0;[03] FORMED NEW VERTICAL 'L' ANGLE BS 692 RBL 0.5 WL206.5 MATERIAL USED 7075T0May 12, 2022 · N7876A · Boeing 7377Q8SDR AALA202206011552None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23L. REPLACED LOWER SILL PER SRM 51-72-11.May 12, 2022 · N709UW · Airbus A319112SDR SROM051220223Shear Web · corrodedBAGGAGE COMPARTMENT AFT SHEAR WEB PN: 85339527-107SP CORRODED AT FS STA. X707 AND LBL 35. THIS CORROSION FALLS OUTSIDE THE ALLOWABLE BLEND AREA OF SRM 53-40-43. REPLACEMENT IS REQUIRED.May 12, 2022 · N792CP · Bombdr DHC8402SDR SROM051220222Shear Web · corrodedBAGGAGE COMPARTMENT AFT SHEAR WEB PN: 85339627-111 CORRODED AT MULTIPLE SPOTS BETWEEN FS STA. X712 - X788. SRM 53-40-43 ALLOWS SOME BLENDING BUT DOES NOT ALLOW BLENDING AROUND THE RADIUS OF A LIGHTNING HOLE. CORROSION AT STA. X771 IS IN THE STAY-OUT AREA OFMay 12, 2022 · N792CP · Bombdr DHC8402SDR SCNA20220523051Floor Support · crackedDEFECT: FOUND DAMAGE TO FRAME, AFT CARGO @STA. 807, STR. 24L TO 22L. RESOULTION: REPAIRED FRAME @ STA 807 STR 24L - 22L IN ACCORDANCE WITH SCA ENG-53SCA-10965 REV00 AND ATS ER 22-01698 REV IR.May 11, 2022 · N819SY · Boeing 73786NSDR EE4Y2022051115564Skin Panel · dentedUPPER FORWARD FUSELAGE EXTERNAL SKIN WITH DENT AND CREASE LOCATED BETWEEN FR04 AND FR05, BETWEEN STRINGER 10LH AND STRINGER 12LH. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2022-190-014169 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EMay 11, 2022 · N140BZ · Emb ERJ190200LRSDR EE4Y202051115562Skin Panel · dentedUPPER FORWARD FUSELAGE EXTERNAL SKIN WITH DENT, LOCATED AT FR04+265MM, STRINGER 10RH+20MM. NOTE: THE FUSELAGE SKIN PANEL WAS REPAIRED AS PER EMBRAER ETD2022-190-013658 REV:A GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2022-15381 INSTRUCTIONS (May 11, 2022 · N140BZ · Emb ERJ190200LRSDR HYIA20220511002Rib · crackedWHILE PERFORMING OTHER MAINTENANCE, A CRACK WAS DISCOVERED IN THE LEFT CLOSE OUT RIB. THIS CRACK EXTENDS VERTICALLY THROUGH TWO FASTENERS HOLES IN THE FIRST ROW OF ATTACH HI-LOKS BETWEEN THE AFT TRUNNION SUPPORT AND THE CLOSE OUT RIB. THE CRACK EXTENDS BETWEMay 11, 2022 · N83PB · Cessna 402CSDR HYIA20220511001Spar Cap · corrodedWHILE PERFORMING OTHER MAINTENANCE, CORROSION WAS IDENTIFIED ON THE LEFT HAND AFT LOWER OUTBOARD SPAR CAP (P/N 5122041-23) AT WING STATION 222.0 TO 229.71. THE DEEPEST AREA OF CORROSION WAS MEASURED AT .033. THIS SPAR CAP WAS REPLACED WITH A FACTORY NEW PARMay 11, 2022 · N83PB · Cessna 402CSDR V0XD20220511003Fitting · scratchedLT AND RT NLG BEARING CAPS HAVE SCRATCHES- BLENDED AREAS WITHIN LIMITS IAW EMBRAER 145 SRM 53-11-08May 11, 2022 · N18556 · Emb EMB145LRSDR V0XD20220511002Fitting · corrodedPITTING CORROSION LH TRUNION FITTING- CORRECTIVE ACTION REMOVED CORROSION WITHIN LIMITS IAW EMBRAER 145 SRM 53-11-08May 11, 2022 · N18556 · Emb EMB145LRSDR V0XD20220511001Fitting · corrodedPITTING CORROSION ON NLG TRUNION FITTING RH, REMOVED CORROSION WITHIN LIMITS AND ANODIZED IWAS EMBRAER 145 SRM 53-11-08May 11, 2022 · N18556 · Emb EMB110*SDR IXXA2022072208Skin Panel · corrodedLEFT WING EXTERNAL LOWER SURFACE SKIN STR L6 AT WS 150.5 TO 177.5 CORRODEDMay 10, 2022 · N752CX · Boeing 757200SDR IXXA202262304Skin Panel · corrodedCORROSION ON EXTERNAL SIDE OF RIGHT WING REAR SPAR LOWER CHORD IN RIGHT WHEEL WELL WHERE SPAR ATTACHES TO CENTER WING BOXMay 10, 2022 · N752CX · Boeing 757200SDR SCNA20220523056Stringer · crackedDEFECT: DAMAGE FOUND ON STRINGER 23L AT STA 727A. RESOLUTION: REPAIRED STRINGER @ STA 727A 23L IAW B737 SRM 53-00-03-2R-1 REV 75 THIS IS A CATEGORTY "A". NO FURHTER INSPECTIONS.May 10, 2022 · N819SY · Boeing 73786NSDR IXXA2022061307Web · corrodedCORROSION ON WEB AT STA 530May 9, 2022 · N255CM · Boeing 767223SDR IPXA2022052882602Stringer · crackedINSPECTION TYPE:3CUPPER CTR AUXILIARY TANK STRINGER 46 IS CRACKED AT STA XCW=17.00REMOVED,FAB,REPAIRED THE CRACKED STRINGER 46 AT STA XCW=17.00 IAW VTSAA EA 011-5730-01-A9562 REV I/R AND UPS EO MD11-5710-83696-A. FAA FORM 8100-9 SIGNED BY S.KANG (AR-605677) (May 9, 2022 · N257UP · Doug MD11FSDR IPXA2022052782568Stringer · crackedINSPECTION TYPE:3CUPPER CTR AUXILIARY TANK STRINGER 45 AT STA X=-17 , X=-46 AND BETWEEN XCW=-6.00 AND XCW=-29.00 HAS A CRACKED.REMOVED, FAB, REPAIRED THE CRACKED STRINGER 45 AT STA X=-17,X=-46 AND BETWEEN XCW=-6.00 AND XCW=-29.00 IAW SRM 57-10-03 REPAIR 1 FIG May 9, 2022 · N257UP · Doug MD11FSDR CALA2022051101197None · corroded(SUPPORT TASK) AFT PIT AFT ACCESSORY AREA, WASTE SERVICE PAN COR RODED AT UPPER SURFACE BETWEEN BS 1680 AND 1700 AND BETWEEN STRI NGER S-26R AND STRINGER S-29R. TRANSCRIBED FROM HAECO NR 928591 0. REMOVED AND REPLACE DOUBLERON WASTE SERVICE PAN BS1680-1700 S2May 9, 2022 · N12125 · Boeing 737SDR IPXA2022052882603Longeron Splice · crackedINSPECTION TYPE:3CCAC COMPARTMENT HAS A LONGERON 38R SPLICE THAT IS CRACKED AT STA 6-90.REMOVED,FAB, REPAIRED THE CRACKED LONGERON 38R SPLICE AT STA 6-90 IAW VTSAA EO 011-5330-01-A9568 REV I/R AND UPS EO MD11-5310-83794-A . FAA FORM 8100-9 SIGNED BY P.LAU (AR-May 8, 2022 · N257UP · Doug MD11FSDR IPXA2022052582487Stiffener · crackedINSPECTION TYPE:3CR/H WING TO BODY CANTED PANEL CAP VERTICAL STIFFENER IS CRACKED AT STA. 1256.REMOVED, FABRICATED AND REPPLACED STIFFENER IAW DWG. AYB7104 AND SRM 51-33-01. (MINOR)May 8, 2022 · N257UP · Doug MD11FSDR IPXA2022052582504Support Angle · crackedINSPECTION TYPE:3CL/H WING TO BODY SUPPORT ANGLE IS CRACKED AT STA. 5-113.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. A5A7064 AND SRM 51-33-01. (MINOR)May 8, 2022 · N257UP · Doug MD11FSDR IPXA2022052582503Support Angle · crackedINSPECTION TYPE:3CR/H WING TO BODY SUPPORT ANGLE IS CRACKED AT STA. 1661.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. AFA7769 AND SRM 51-33-01. (MINOR)May 8, 2022 · N257UP · Doug MD11FSDR IPXA2022052582502Support Angle · crackedINSPECTION TYPE:3CR/H WING TO BODY SUPPORT ANGLE IS CRACKED AT STA. 5-113.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. A5A7064 AND SRM 51-33-01. (MINOR)May 8, 2022 · N257UP · Doug MD11FSDR IPXA2022052382388Doubler · chafedINSPECTION TYPE:3CTAIL CONE HORZ. BEAM REPAIR DOUBLER HAS CHAFE DAMAGE.REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 53-80-02 REPAIR 5. (MINOR)May 8, 2022 · N257UP · Doug MD11FSDR CALA2022050901185None · corrodedAFT CARGO TORSION BOX COVER SHEET HAS CORROSION. GENERATED BY V0 52030 ON HAECO LCQ NR 9292430/44430 REMOVED AND REPLACED AFT CARGO COVER SHEET IAW A319 SRM 51-72-11 ACMP BY MECH V052030 INSP BY V061334May 8, 2022 · N804UA · Airbus A319131SDR JR2R8471860Door · corrodedLAV SERVICE DOOR CORRODEDMay 8, 2022 · N80343 · Emb ERJ170200LRSDR SIMA20220507017Shear Tie · corrodedFR 75 IS CORRODED BETWEEN STR 28 RT AND STR 29 RT (MAJOR REPAIR)-C/A-COMPLETE:RAR'D FRAME SHEAR CLIP AT FR75 BETWEEN STR 28RH AND STR 29RH IAW SRM 51-40-08.May 7, 2022 · N232NN · Emb ERJ170200LRSDR SIMA20220507019Shear Tie · corrodedFR 74 IS CORRODED BETWEEN STR 28 RT AND STR 29 RT (MAJOR REPAIR)-C/A-COMPLETE:INSTALLED NEW SHEAR CLIP IAW SRM 51-40-08May 7, 2022 · N232NN · Emb ERJ170200LRSDR SIMA20220507018Floor Support · corrodedFR CLEAT/FLOORBOARD SUPPORT AT FR75 IS CORRODED BETWEEN STRS 29L AND 29R. (MAJOR REPAIR)-C/A-COMPLETE:REMOVED AND REPLACED FR CLEAT IAW SRM 51-40-08May 7, 2022 · N232NN · Emb ERJ170200LR
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