JASC 5330
Service difficulty reports · 79,347
Reports filed under 5330 · Fuselage Main, Plate/Skin, 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 = '5330' 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 = '5330' 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 R61A201712090930Doubler · corroded*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** MAINTENANCE FOUND LEVEL 2 CORROSION ON FWD CARGO DOOR CUT OUT STRUCTURE ( FWD AND AFT DOUBLERS)THEY REMOVED AND REPLACED DOUBLERS IAW EMB 170 SRM 51-41-02, 51-43-02. AIRCRAFT REMAINS OUT OF SERVICE FORSDR REXA2017112101203Skin · dentedTHREE DENTS BELOW GALLEY SEVICE DOOR BS 338, STRINGER 19R. COMPLIED WITH EA 953-06233.SDR DALA2017112208273Skin · damagedFUSELAGE FWD CARGO BELLY SKIN IS CREASED AT BS 408 BETWEEN LONGERONS 29 AND 30R AT THE FRAME SHEAR TIE. REPAIRED IAW ERA 563268-14, REV C.SDR IPXA2017112223804Skin · damagedFUSELAGE SKIN DAMAGE AT STA 1770 BETWEEN STR 35R & 36R. REPAIRED PER EO B747-5330-66492A AND SRM 53-00-01-2R REPAIR 1.SDR DALA2017112008362Skin · damaged6 DISCREPANT HOLES GROUP B 2 HOLES ELONGATED IN SKIN 2 HOLES ARE OVER SIZE IN SKIN. REPAIR 2 HOLES OVER SIZE IN STRINGER REF EDA DV1927-MSN2095 REV G FIG 7-10 PER PRI 563575-14 REV (0), (1), (3).SDR DALA2017112008361Skin · damaged4 DISCREPANT HOLES GROUP B 2 HOLES ELONGATED ON SKIN AND 2 ARE OVER SIZE ON STRINGER REF EDA DV1927-MSN2095 REV G FIG 7-10. REPAIR PER PRE PRI 563575-14.SDR DALA2017112008360Skin · damaged4 DISCREPANT HOLES GROUP B 2 HOLES ELONGATED ON SKIN AND 2 ARE OVER SIZE ON STRINGER REF EDA DV1927-MSN2095 REV G FIG 7-10. REPAIR PER PRE PRI 563575-14.SDR DALA2017112008359Skin · damaged6 DISCREPANT HOLES GROUP B TWO HOLES ARE ELONGATED ON SKIN AND TWO HOLES ARE OVER SIZE ON SKIN PLUS TWO HOLES ARE COLD WORKED AND OVER SIZE ON STRINGER. REF EDA DV1927-MSN2095 REV G FIG 7-10, REPAIR PER PRI 563575-14.SDR DALA2017112108240Skin · corrodedCORROSION ON UPPER SURFACE OF THE SKIN BETWEEN BS 737 & 756, RBL 44 - 60. CORROSION OUT OF LIMITS AND WAS REPAIRED IAW ER/A 562387-14 REV. ORIGINAL. AND ETI-17-17-228 REV 1.SDR JGVR20171120001Skin · corrodedFOUND CORROSION ON EXTERIOR OF FUSELAGE SKIN AT APPROXIMATELY FS400 AT STRINGERS 3L, 3R, AND 4R. MECHANICALLY BLENDED, MEASURED, TREATED, AND REPLACED FASTENERS AS REQUIRED PER REPAIR DEFINITION S-750-0190/16RD.SDR 7C7A2017112000340Skin Panel · dentedMULTIPLE DENTS ON UPPER FUSELAGE AND FRONT PRESSURE BULKHEAD. REPAIRED IAW ECO 008.53-13.31.SDR 7C7A2017112000341Skin Panel · dentedCENTER FUSELAGE SKIN DENTS AT X424 AND X434 REPAIRED WITH RIVET PLUG AND RD8-53-7310.SDR SIMA20171119002Skin · crackedSKIN CRACKED AT FR 77 STR 3R. REPAIRED FR 77 STR 3R IAW SRM 53-32-01 ITEM 3FIGURE 204 SHEET 3.SDR DALA2017112208290Skin · not reportedUPPER SKIN, FWD SIDE OF BS 1040 LEFT SIDE. ACCOMPLISHED A REPAIR IAW PRI 563330-14 REV0,1,2 AND ERA 563330-14, REV ORIG.SDR DALA2017112008229Skin · puncturedDURING INSPECTION FOUND ZONE 5 LT AFT FUSELAGE UNDER THE 10TH AND 11TH WINDOWS FORWARD OF LT AFT PAX DOOR, APPROX MIDWAY DOWN ON FUSELAGE THERE IS A PUNCTURE APPROXIMATELY 8" LONG AND 4 1/2" WIDE. MAINTENANCE CUT OUT DAMAGE, FABRICATED REPAIR PARTS & TREATED PSDR SWAA2017121818495Bear Strap · corrodedFORWARD CARGO DOOR CUTOUT INNER SIDE CORRODED AT BS 492. REPAIRED THE BEAR STRAP IAW EA AND SRM.SDR VNAA2017112199903Skin · tornRIGHT AFT CORNER OF NLG CUT OUT IS CRACKED APPROX .250. REPAIRED THE SKIN AT BS 235 BETWEEN STRINGERS 26L AND 26R IAW REO 601R-53-11-048, REV D, AND REO 601R-53-11-3143, REV -.SDR FDEA201711173254Skin · corrodedSKIN ON THE RT FUSELAGE, AT BS 1139, STRINGER 44R IS BULGING AND RIVETS DISHING. INSTALLED A REPAIR IAW SRM 53-20-00, FIG 6.SDR CALA2017111704096Skin · gougedSKIN FRAMES 13 - 14, STRINGERS 22 - 23L GOUGED OUT OF LIMITS, FABRICATED AND INSTALLED A DOUBLER IAW SRM 53-00-11-300-042, FIG 20148.SDR SWAA2022020422138Skin · dentedSUPPLEMENTAL INFORMATION: PREVIOUS OPERATOR RECORDS INDICATE PRESENCE OF 3 DENTS AND 2 BLENDS ON THE CROWN OF THE AIRCRAFT AT STA 259.5 TO STA 268.5 BETWEEN S-2L AND S-3L. BOEING MESSAGE ARG-ARG-17-0153 AND ARG-ARG-16-0147 INDICATE PERMANENT REPAIR IS STILL RESDR SWAA2018010318827Doubler · crackedEXTERNAL POWER DOOR INTERNAL DOUBLER CRACKED AT CENTER LATCH POSITION. REPAIRED DOUBLER IAW SRM.SDR GTIA2017111602245Skin · dentedDENTS FOUND DURING A WALK AROUND. PERFORMED A REPAIR IAW EO 5311-1784, REV 00, AND RDAS 80383039/003/2017.SDR SWAA2018011819155Post · crackedRT NR 3 WINDOW FRAME E-F POST CRACKED IN THE 2ND AND 4TH LOWER FASTENER HOLES. REPAIRED POST IAW ACO.SDR ASAA2017111522875Skin · dentedFOUND A DENT BELOW THE R1 DOOR BS 295, STRINGER 22R. ACFT GROUNDED. REPAIRED DAMAGE TO SKIN IAW B737 800 SRM 53 00 01 2R 1 THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 50,000 FLT. CYCLES, INTERVAL OF 3,440 FLT. CYCLES. REFER TO 737 800 APB SRM SDR SIMA20171113003Skin · crackedLT UPPER AFT FUSELAGE CRACKED ABOVE STRINGER 2L JUST AFT OF FR75. REPAIRED LT UPPER AFT FUSELAGE SKIN ABOVE STRINGER 2L AND JUST AFT OF FRAME 75 IAW SRM 53-31-01 ITEM 11 FIG 219.SDR SWAA2017120418188Skin · crackedFUSELAGE SKIN CRACKED AT BS 540, STR 22L. REPAIRED SKIN PER ER & EA.SDR SWAA2017120418187Skin · crackedFUSELAGE SKIN CRACKED AT BS 540, STR 22R. REPAIRED SKIN PER EA.SDR N6WA2017111301Skin · brokenGPU RECEPTACLE OUT OF POSITION AND BROKEN. SKIN REPAIR PER REO. COMPLETED REPAIR OF GPU RECEPTACLE SKIN IAW SRM 51-25-01 AND REO 670-53-11-1344.SDR JR2R20171113003Skin · corrodedSUSPECTED CORROSION UNDER SKIN AROUND AFT LAVATORY SERVICE PANEL. AREA IS JUST FORWARD OF LOWER FORWARD CORNER OF DOOR. SKIN IS BULGED WITH APPARENT COUNTERSUNK RIVET THAT IS PULLED. REPAIRED SKIN AND INTERNAL DOUBLER FWD OF AFT LAV SERVICE DOOR IAW EA 30-201SDR FDEA201711123236Skin · puncturedPRIOR TO LOADING, RAMP DISCOVERED PUNCTURE IN FUSELAGE FWD OF MAIN CARGO DOOR. REPAIRED IAW EA F-5330-T0336569 PT 1 AND 2.SDR DALA2017111308060Doubler · crackedPANEL 6301A, INTERNAL DOUBLER IS CRACKED. REPAIRED PER ERA 563169-14 REV ORIGINAL.SDR RAIA201711110002Skin · crackedRIGHT FUSELAGE EXTERIOR SKIN AT FR 75 HAS 3 POSSIBLE CRACKS - MARKED. PERFORMED REPAIR ON RH FUSELAGE EXTERIOR SKIN AT FR 75.SDR DALA2017111208059Skin · corrodedCORROSION AT AFT LAV SERVICE PANEL, LOWER AFT CORNER. REPAIR COMPLETED AS PER ERA 563040-14 REV ORIG. TIME CONTROL ITEMS TO BE ACCOMPLISHED ON LOG 0293411.SDR SWAA2022020352451Scuff Plate · crackedSUPPLEMENTAL INFORMATION: AFT.CARGO ;AFT. SCUF FPLATE HAS CRACK LINE SHOWING. / REMOVED AND REPLACED PER SRM 51-40-02 .SDR SWAA2022020352446Scuff Plate · crackedSUPPLEMENTAL INFORMATION: FWD CARGO DOORWAY CENTER THRESHOLD IS CRACKED AT AFT STOP PIN CONTACT AREA. MRKD / REPLACED SCUFF PLATE PER TASK 53-11-02. LEAK CHECK GOOD PER AMM 05-51-91SDR DALA2017111008063Skin · crackedCRACK ON FUSELAGE SKIN AT BS 1022 AND LONGERON 14R. REPAIRED IAW ETI-17-17-210, REV 3, AND ER/A 562364-14, REV ORG.SDR CALA2017111003974Skin · corrodedAFT CARGO SKIN BETWEEN FRAMES 54 - 55, STRINGERS 43R - 43L AROUND DOMENUTS HAS SPOTS OF CORROSION. ACCOMPLISHED A REPAIR IAW SRM 53-00-300-013.SDR DALA2017111008035Skin · crackedCRACKED SKIN BS 1022, LONGERON 14L. PERMANENT REPAIR WAS ACCOMPLISHED IAW ETI-17-17-209 REV. 2 AND ER/A 521459-14 REV. A.SDR SWAA2018010918900Skin · crackedSKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED THE SKIN IAW ER & EA.SDR DALA2017110908042Doubler · crackedDURING INSPECTION, FOUND A CRACK ON A PRODUCTION DOUBLER CUTOUT OF EXTERNAL POWER RECEPTABLE. REPAIRED IAW SRM 53-10-15 REP.4SDR SWAA2022020322107None · crackedSUPPLEMENTAL INFORMATION: ***CORROSION*** ON AFT SERVICE DOOR MOP SILL FROM B.S. 867-986. / CORROSION EVALUATION WAS FOUND TO BE OUT OF LIMITS; LOCATED AND DRILLED NEW MOPSILL AT AFT SERVICE DOOR AREA. MOP SILL TO BE INSTALLED ON CARD #T707244. 86750U 15NOV17SDR SIMA20171107009Skin Panel · gougedCENTER FUSELAGE UPPER SKIN PANEL BETWEEN FR 35-36 STRG 1R-3R GOUGES, PERMANENT REPAIR. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-2836.SDR DALA2017110707996Skin · corrodedSEVERAL CORROSION POINTS ON THE SKIN BETWEEN BS 655 AND 696, LBL 44 AND LBL 60. REPAIRED IAW ER/A 562374-14 REV. ORIGINAL, AND ETI-17-17-210 REV 1.SDR DALA2017110707994Skin · corrodedCORROSION ON THE SKIN BETWEEN FRAMES 69 TO 70, STRINGERS 31 - 32R. REPAIRED IAW SRM 53-41-11-300-004.SDR R61A201711060815Skin · dentedDENT IN THE LT FWD FUSELAGE SKIN AT FRAMES 10L TO 11L, BETWEEN STRINGERS 18L TO 19L. INSTALLED TEMPORARY REPAIR IAW ETD2017-170-094874. MAJOR REPAIR.SDR AALA201712069002Annular Shell · crackedAIRCRAFT IN BASE MAINTENANCE. CRACKED SIDE SHELL ON FR 35 AT LEVEL OF STRINGER 30 LEFT HAND IN FORWARD CARGO COMPARTMENT. REPAIRED SIDE SHELL ON FR 35 AT LEVEL OF STRINGER 30 LEFT HAND IN FORWARD CARGO COMPARTMENT PER EA 275042.SDR AALA201712069001Annular Shell · crackedAIRCRAFT IN BASE MAINTENANCE. CRACKED SIDE SHELL AT FR 35 AND 1 INCH ABOVE LEFT HAND STRINGER 30 AT FORWARD CARGO COMPARTMENT. REPAIRED SIDE SHELL AT FR 35 AND 1 INCH ABOVE LEFT HAND STRINGER 30 AT FORWARD CARGO COMPARTMENT PER EA 275042.SDR IPXA2017111823681Skin Panel · dentedFUSELAGE SKIN DENT AFT OF FR 85 BETWEEN S44L AND 45. REPAIRED DENTS IAW SRM 53-10-12 FIG 210 SHT 1 AND 2.SDR DALA2017110407965Skin · corrodedFOUND ON A WALK AROUND AFT OF THE LAVATORY SERVICE DOOR HAS A 1.5 INCH CRACK AND CORROSION IN SKIN AT CAP POINT. REPAIRED THE SKIN IAW ERA 563023-14.SDR CALA2017110603936Skin · crackedFOUND TWO CRACKS IN THE SKIN AT BS 2195.75 BETWEEN STR 6 TO 8L. TRIMMED THE AREA IAW DRAWING 624W0013, SHT 1, REV B. HFEC INSPECTION CARRIED OUT IAW NTM PART 6 51-00-01, PROC 2. NO CRACK FOUND.
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