JASC 5310
Service difficulty reports · 38,548
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.
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
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 SWAA2019121239576Crease Beam · corrodedCREASE BEAM INNER CHORD CORRODED AT BS. 706, RBL 64. / R&R CREASE BEAM INNER CORD IAW SRM & DWGSDR CALA2019112702099Flange · corrodedAFT WET AREA STA 947.5 IB LAV FITTING AND AREA WITH CORROSION (REF NR 99858430) REMOVED UPPER FLANGE AT STA 947.5 RBL 33 TO LBL 58 AND PERFORMED A REPAIR IAW EC/RA 5321-01330 AND SRM 53-70-51SDR CALA2019112702098Frame · dentedB757-06-0242 DENT ON AFT CARGO FRAME UPPER FLANGE AT STA 1340 AB OVE STR 26R. REF ST ENG N/R 0080810 CHECKED LIMITS TO DENT ON FRAME AT AFT CARGO STA 1340 ABOVE 5-26 R; L=.80", W=.60, D=.070". OUT OF LIMITS IAW B757-200 SRM 53-00- 07 AD1, FIG 101, PG 101. REPASDR CALA2019112702094Window Frame · crackedCRACK FOUND AFTER HFEC INSPECTION OF WINDOW L1 PER AVO # 284-19- 10-26-02 (CRACK CONDITION 1). CRACK FOUND AFTER HFEC INSPECTION OF WINDOW L1 HAS BEEN REPAIRED PER EC/RA # 5311-02301. INITIATE A DTA DIP FOR THE L1 WINDOW FRAME REPAIR TO " ACCOMPLISH AN INITIASDR CALA2019112702101Door Frame · corrodedAFT PASSENGER COMPARTMENT WET AREA L2 DOOR LOWER CHROD HAS CORROSION(REF NR 99859350) REMOVED DAMAGED AFT PASSENGER COMPARTMENT WET AREA L2 DOOR LOWER CHORD. LOCATED AND DRILLED NEW CHORD. INSTALLED NEW CHORD IAW B737-800 SRM 51-40-02, SRM 51-40-05, SRM 53-70-SDR CALA2019112702095Window Frame · crackedCRACK FOUND ON R1 WINDOW FRAME DURING HFEC INSPECTION IAW AVO # 284-19-10-26-02 STEP "B". CRACK FOUND ON R1 WINDOW FRAME DURING HFEC INSPECTION HAS BEEN REPAIRED PER EC/RA 5311-02302. INITIATE A DTA DIP FOR THE R1 WINDOW FRAME REPAIR TO " ACCOMPLISH AN INITIALSDR FDEA2019112653086Door Frame · crackedLOWER CENTER CARGO UPPER CENTER DOOR JAMB SUSPECT WITH CRACK AT DOOR DRIVE MOTOR FITTING ATTACHMENT AT STATION 1746. CRACK AT LOWER CENTER CARGO UPPER CENTER DOOR JAMB AT DOOR DRIVE MOTOR FITTING ATTACHMENT STATION 1746 CARRIED OUT REPAIR AS PER SRM 53-50-SDR FDEA2019112653090Door Frame · crackedCABIN - L3 DOOR AFT LOWER FUSELAGE JAMB WEB CRACKED AT STATION 1310 BETWEEN LONGERON 26 LEFT & 27 LEFT. CABIN - L3 DOOR AFT LOWER FUESELAGE JAMB, CRACKED WEB SKIN AT STATION 1310 BETWEEN LONGERON 26 LEFT AND 27 LEFT, REPAIRED AS PER SRM 53-40-5-2R FIGURE 201 SDR SWAA2019120939478Pressure Deck · crackedHORIZONTAL PRESSURE DECK WEB CRACKED AT BS. 664, RBL 42. / REPAIRED WEB PER SRM.SDR SIMA201912095004Floorbeam · crackedRH CENTER COCKPIT FLOOR BEAM AT BL 12.00 IS CRACKED, LOCATED JUST FWD OS FS280.00. -C/A-REPAIRED RH CENTER COCKPIT FLOOR BEAM AT BL12.00 IAW SRM CH. 53-11-43-200-003.SDR CALA2019112862083Pressure Panel · crackedREF AAR DLH N/R 9031510, LH SIDE PRESSURE PANEL BETWEEN FR35-36 HOLES 4 AND 13 HAVE CRACK INDICATIONS. CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5331-02510. DIP L OGPAGE TO READ AS FOLLOWS, ASDR CALA2019112862082Window Frame · crackedREF AAR DLH N/R 9031350, ROTO PROBE INSPECTION SHOWS CRACK INDIC ATION AT WINDSHIELD SIDE POST UPPER ATTACHMENT, LH SIDE. HOLE ID ENTIFIED AS #3 LHS. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5331-02523. DIP L OGPAGE TO BE CREATED TO READ AS FOLLOWS, ACCOSDR CALA2019112702090Channel · dentedAFT CARGO COMPARTMENT STA.747 L/H JUST ABOVE THE SIDE PLATE BETW EEN STR24L TO 24L THERE IS A DENT ON THE HAT SECTION. INITIATE A DTA DIP TO -ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE AIRCRAFT REACHING 75,000 TOTAL FLIGHT CYCLES. PLANNIN G TO CONTACTSDR SWAA2022032461353Intercostal · crackedFWD CABIN FLOOR SUPPORT INTERCOSTAL CRACKS BETWEEN STA 380 & 400 AT RBL 10 MKD / REMOVED AND INSTALLED NEW FLOOR SUPPORT INTERCOSTAL BETWEEN STA 380 TO 400 RBL 10' AT FWD CABIN IAW B737 SRM 51-40-02-0G-0SDR FDEA2019112643084Beam · corrodedTRANSVERSE BEAM B/S 1040-1075, RBL 25 IS CORRODED BEYOND LIMITS IAW SRM 53-00-51-1A ,ALLOWABLE DAMAGE 1, DETAIL III. REPLACED TRANSVERSE BEAM IAW SRM 51-40-02 AND BOEING DRAWING #114N8250.SDR FDEA2019112643083Beam · corrodedTRANSVERSE BEAM B/S 1040-1075 RBL 46 IS CORRODED BEYOND LIMITS IAW SRM 53-00-51-1A, ALLOWABLE DAMAGE 1, DETAIL III. INSTALLED NEW TRANSVERSE BEAM IAW SRM 51-40-02 AND BOEING DRAWING # 144N8250SDR FDEA201911243082Beam · corrodedTRANSVERSE BEAM B/S 1040-1075, LBL 25 IS CORRODED BEYOND LIMITS IAW SRM 53-00-51-1A, ALLOWABLE DAMAGE 1, FIG 101, DETAIL III REPLACED BEAM IAW SRM 51-40-02 AND BOEING DRAWING#144N8250SDR CALA2019120322104Angle · crackedB757-52-3-0001 FORWARD CARGO DOOR FWD AND AFT UPPER CORNER ANGLE S CRACKED REMOVED AND REPLACED THE FWD AND AFT UPPER CORNER ANGLES OF THE FWD CARGO DOOR; P/N: 69-53919U5, BATCH NO. 0003562701, PO NO. SA G1951849 AND 69-53919U6, BATCH NO. 0003573491, PO NO. SASDR FDEA2019112633066Beam · corrodedCORROSION ON NUT PLATES FOR FLOOR ATTACHMENTS, AFT CARGO COMPARTMENT AT STA 1902. REMOVED CORROSION IAW SRM 53-00-01 VOL II. ORIG THICKNESS 0.063". AFTER REWORK 0.045". OUT OF LIMITS. FABRICATED ANGLE ON T19/1450803. INSTALLED ANGLE IAW SRM 51-31-01 VOL SDR SWAA2022032421920Baffle · crackedFWD CARGO BAY BAFFLE LBL 21 BS 500-500A UPPER FLANGE HAS A CRACK / REMOVED AND REPLACED FCB BAFFLE AT STA; 500 - 500A LBL 21 PER SRM 51-40-02 AND DWG. 143A7505. 91195U 11.22.19SDR AALA2019120969022Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR ACTUATOR ATTACHMENT FITTING ON KEEL BEAM AFT LUG WORN AT FR 42 AND S42R. REPLACED FITTING PER EA 300673.SDR SWAA2022032461311Angle · crackedCABIN AREA FLOOR SUPPORT ANGLE 312 TO 328 LBL 45 CRACKED AT UPPER SURFACE / REMOVED & REPLACED FLOOR SUPPROT ANGLE BETWEEN STA ; 312 THRU STA 328 AND LBL 45 AS PER BOEING DRAW . # 141A5400 AND B737-7 SRM 51-40-02-0G-0 .SDR SWAA2022032443860Intercostal · corrodedPASSENGER CABIN; STA 947 LBL 25 WL 208; UPPER SURFACE OF INTERCOSTAL HAS CORROSION UNDER LAV MOUNT / REMOVED CORROSION ON INTERCOSTAL UPPER SURFACE STA 947 LBL 25 FOUND ORIG T .210' WITH .053' LOSS AND .155' REMAINING TO BE OUT OF LIMITS IAW B737 SRM 53-70-51-SDR SWAA2022032443859Intercostal · corrodedPASSENGER CABIN; STA 947 LBL 50 WL 208; UPPER SURFACE OF INTERCOSTAL HAS CORROSION UNDER LAV MOUNT / REMOVED CORROSION ON INTERCOSTAL STA 947 LBL 50 ORIG T .230' LOSS .075' REMAINING .155' OUT OF LIMITS IAW B737 SRM 53-70-51-1A-1. REMOVED AND REPLACED INTERCOSSDR R61A201911261337Crossbeam · gougedMAJOR: INCOMING PREVIOUS GOUGE DAMAGE L= 0.4 W= 0.1 H= 0.080 FOUND AT CROSSBEAM 57 WEB AREA. FABRICATED, DRILLED AND INSTALLED REPAIR '' L'' ANGLE FOR CROSSBEAM 57 PER ETD2019-170-158123 AND SRM 51-40-08. RESTORED SURFACE TREATMENT PER SRM 51-23-06, CPM 51-25SDR YENA201911251672Structure · corrodedDURING HEAVY MAINTENANCE, (NR 2019-313370) CORROSION LOWER SILL BTW FR66 - FR68 AT LEVEL STR23L AT AFT GALLEY AREA; REMOVED AND REPLACED LOWER SILL LOCATED BTW FR66 - FR68 AT LEVEL STR 23L AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DRAWING D53480505. TOOL USDR YENA201911251671Structure · corrodedDURING HEAVY MAINTENANCE, (REF NR 2019-313369) CORROSION LOWER SILL LOC BTW FR66 TO 68 AT LEVEL STR23 AT AFT GALLEY AREA; REMOVED AND REPLACED LOWER SILL BTW FR66 TO FR68 AT LEVEL STR 23R AT AFT GALLEY AREA IAW SRM A 320-51-72-11 AND A320 51-72-11 AND DRAWING SDR SWAA2022032443803Web · corrodedAFT CARGO DOOR CUTOUT LOWER THRESHOLD WEB HAS CORROSION STA 794 TO 847 RBL 21 TO 27 WL 163 / REMOVED CORROSION FROM AFT CARGO DOOR CUTOUT LOWER THRESHOLD WEB STA 794 TO 847 RBL 21 TO 27WL 163 AND CHECKED LIMIT FOUND TO BE OUT OF LIMIT ORIG 'T' OUR LOSS .020' RSDR SWAA2022032443830Angle · corrodedFWD CARGO COMPARTMENT FLOOR STRUCTURE R\H Z-ANGLE STA 500B TO 500I; RBL 23; WL 153 HAS CORROSION AT NUTPLATE HOLES. / REMOVED CORROSION ON FWD CARGO COMPARTMENT FLOOR STRUCTURE RH Z ANGLE STA 500B TO 500I RBL23 WL153 IAW SRM 51-10-02-0G-0. VERTICAL WITH 10X MASDR SWAA2022032443820Beam · corrodedPASSENGER CABIN STA 947+10 TO 986; RBL 57; WL 208. INNER CREASE BEAM CORD IS CORRODED ON UPPER SURFACE / REMOVED CORROSION ON R2 CREASE BEAM AT STA 947+10 TO 986.0 ORIG 'T' .080' REMAINING .050' LOSS OF .030' OUT OF LIMITS REMOVED & REPLACED R2 CREASE BEAM IAWSDR SWAA2022032443843Web · corrodedAFT PIT WEB CORRODED AT BS 927 TO 931; RBL 2; WL 147 / AFT PIT WEB CORRODED AT BS 927 TO 931 RBL 2 WL 147 REPLACED WEB WITH P/N: 147A7500-6 IAW BOEING DWG# 147A7500 REV- ID: 0044 AND SRM 51-40-02-0G-0 CORROSION FOUND TO BE 'OUT OF LIMITS' OF ORIGINAL: .045' RESDR SWAA2022032443840Intercostal · corrodedAFT PIT WEB CORROSION AT BS 747 TO 767; RBL 22; WL 153 / AFT CARGO WEB CORROSION AT B.S. 747 TO B.S. 767 RBL 22; WL 153. BLENDED AND REMOVED CORROSION I/A/W SRM 51-10-02-0G-0 AND CHECKED WITH 10X MAG. MATERIAL THICKNESS IS .040. MAT LOSS IS .016 REMAINING THICSDR SWAA2022032443833Angle · corrodedFWD CARGO COMPARTMENT FLOOR STRUCTURE STA 500I; RBL 24 TO LBL 24; WL 153 BULKHEAD LOWER SUPPORT ANGLE HAS CORROSION. / REMOVED CORROSION FWD CARGO COMPARTMENT FLOOR STRUCTURES STA 500I; RBL 24 TO LBL 24; WL BULKHEAD LOWER SUPPORT ANGLE; NO PUBLISHED LIMITS OUTSDR SWIA2019123147502Door Frame · cracked* FORWARD CABIN - APPROX. FS.330.00 BETWEEN STGR 1 AND 2 LEFT HAND ABOVE PAX DOOR CUT OUT- FRAME HAS SIGNS OF A CRACK AT A TOOLING HOLE (C-CHECK) RO 12/27/2019 REMOVED AND INSTALLED NEW FRAME SECTION AT FS333, BETWEEN STR1L AND STR2L REF CRJ200 SRM AND SDR SWAA2019112639150Door Frame · corrodedFORWARD CARGO DOOR UPPER DOOR FRAME WEB CORRODED AT BS. 460, STR. 19R. / REPAIRED WEB PER EA & ER.SDR SWAA2019112539086Crease Beam · corrodedPASSENGER CABIN INNER CREASE BEAM CHORD CORRODED ON UPPER SURFACE BETWEEN BS. 947+10 TO BS. 986, RBL 57. / R&R R2 CREASE BEAM IAW SRM & DWG.SDR R61A201911201299Crossbeam · corrodedWHILE IN HEAVY CHECK FOUND FR 84 CROSSBEAM IS CORRODED OUTBOARD OF LH INBOARD SEAT TRACK. REPAIRD CROSS BEAM REF. ETD2019-170-155492 RESTORED FINISH REF EMB SRM 51-23-04, 51-23-05. 51-23-06.SDR R61A201911201292Shear Angle · corrodedWHILE IN HEAVY CHECK - CORROSION_FR.87 ST26R TO 27R HAS HAS CORRODED SHEAR CLIP. REMOVED AND INSTALLED NEW SHEAR CLIP FR 86 STGR 26R-27R REF SRM 51-40-08SDR R61A201911201291Shear Angle · corrodedWHILE IN HEAVY CHECK - CORROSION_CORROSION AT FR.89 STR.26-27 R.HAND SHEAR CLIP. REMOVED AND REPLACE SHEAR CLIP REF SRM 51-40-02SDR R61A201911201290Shear Angle · corrodedWHILE IN HEAVY CHECK - CORROSION_CORROSION AT FR.88 STR.26-27 R.HAND SHEAR CLIP. REMOVED DAMAGED SHEAR CLIP REF SRM 51-40-08. LOCATED AND DRILLED NEW SHEAR CLIP REF SRM 51-40-02, SRM 51-23-04.INSTALLED SHEAR CLIP AND APPLIED TOP COAT AT FR. 88 STR.26 - 27 REFSDR HNAA2019112700368Window Frame · crackedCAPTS WINDOW PILLAR CRACKED, BTWEEN W/S AND DV WINDOWS....FIX: PERFORMED EDDY CURRENT INSPECION AT CAPT,S PILLAR INNER AND OUTER SURFACE SKIN. NO CRACKS FOUND AT HIS TIME. PILLAR FOUND TO BE SEPARATING AT SEAM. NOTE: A/C FERRIED TO SBY WHERE 7 RIVETS REPLACED SDR C77A2019111900002Doubler · corrodedDURING THE B6 BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED IN THE FORWARD FUSELAGE AT THE RH COCKPIT FLOOR DOUBLER (P/N 170-03238-005) DURING INSPECTION IN THE AREA. THE DAMAGE EXCEEDED THE LIMITS PROVIDED IN THE SRM BECAUSE OF ITS DEPTH. EAMS REQUESTESDR C77A2019111900001Doubler · corrodedDURING THE B6 BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED IN THE FORWARD FUSELAGE AT THE RH COCKPIT FLOOR DOUBLER (P/N 170-03238-005) DURING INSPECTION IN THE AREA. THE DAMAGE EXCEEDED THE LIMITS PROVIDED IN THE SRM BECAUSE OF ITS DEPTH. EAMS REQUESTESDR SWAA2022032359810Gusset · crackedSUSPECT CRACK AT BS 500D L/H STR 19L GUSSET / REMOVED AND REPLACED GUSSET AT BS 500D STR 19L IAW B737-700 SRM 51-40-02-0G-0 AND DWG #143A7902SDR SWAA2022032321860Intercostal · crackedCRACKED INTERCOSTAL AT B.S. 277-294.5; R.B.L. 1; W.L. 208.1. / REMOVED & REPLACED NEW INTERCOSTAL P/N 141A5410-3 IAW DRW 141A5400 & SRM 51-40-02-0G-0 AT BS 277 - 294.5 RBL 1 WL 208.1SDR SWIA2019123147501Vertical Beam · cracked* FS 409+128 VERTICAL POST OUTBOARD HALF HAS A SUSPECTED CRACK AT RBL 18, NEAR THE LOWER END'S FASTENER. (C-CHECK) RO 12/27/2019 REMOVED CRACK OUTBD POST AND INSTALLED NEW P/N 601R32208-30 VERTICAL OUTBD POST RBL18 AT FS409+128 REF BOMBARDIER REO AND BOMBARDISDR SWIA2019122747244Bracket · corrodedLOWER FRAME BRACKET AT BS 349 AND STRINGER 17R AT SERVICE DOOR WAS CORRODED. BLENDED CORROSION ON LOWER FRAME BRACKET FOUND CORROSION TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED BRACKET WITH NEW BRACKET IAW DWG.SDR ASAA2019121983633Beam · corrodedAFT WET AREA LONGITUDINAL BEAM AT Y160 FR68-FR70 HAS CORROSION ON TOP SIDE GROUNDED - YES. NO ALLOWABLE DAMAGE LIMITS GIVEN IN A319 SRM. REMOVED AND REPLACED FLOOR BEAM P/N D5347219620000 PO# 960133.1 IAW A319 SR, 51-42-11.SDR ASAA2019121983632Beam · corrodedAFT WET AREA LONGITUDINAL BEAM AT -Y160 FR68-FR70 HAS CORROSION ON TOP SIDE GROUNDED - YES. NO ALLOWABLE DAMAGE LIMITS GIVEN IN A319 SRM. REMOVED AND REPLACED FLOOR BEAM P/N D5347209700200 IAW A319 SRM 51-42-11.SDR SWAA2022032334283Angle · corrodedAFT CARGO COMPARTMENT L/H 'Z' ANGLE FROM STA 727F TO 807; LBL 25; W/L 157 HAS MULTIPLE AREAS OF CORROSION / REMOVED CORROSION FROM L/H ZEE ANGLE STA 727F TO STA 807 IAW SRM 51-10-02-0G-0 PAR 15. EVALUATED MATERIAL LOSS ORIGINAL=.040' REMAINING=.034' LOSS=.007'
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