JASC 5330
Service difficulty reports · 79,329
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 SWAA2023050824363Skin · crackedEXTERNAL POWER RECEPTACLE CUTOUT CRACKED AT LOWER CENTER AREA<[01] ACCOMPLISHED REPAIR OF EXTERNAL POWER RECEPTACLE CUTOUT DAMAGE AT LOWER CENTER AREA IN REF WITH SRM 53-10-15-2R-4.;[02] CORRECTION TO STEP 1: ACCOMPLISHED REPAIR OF EXTERNAL POWER RECEPTACLE CUSDR IPXA2023050393101Skin · dentedINSPECTION TYPE:3C2 DENT ON FUSELAGE SKIN FWD AND UP FROM FWD L/H A/C BAY DOOR BETWEEN STA Y=475 - Y=495.REPAIRED DENTS AT THE FUSELAGE SKIN FWD AND UP FROM FWD L/H A/C BAY DOOR BETWEEN STA Y=475 - Y=495 IAW VTSAA EA 011-5310-01-A9933 I/R AND UPS EO MD11-5330-SDR DALA2023041002785Unknown · unknownSHIP 3354 DURING H CHECK, A DENT WAS FOUND AFFECTING THE FUSELAGE SKIN PANEL 10 P/N: F5347945521400 AT FR79 AND BETWEEN STR32LH & STR34LH. THE DENT WAS EVALUATED AND WAS FOUND OUT OF ADL DUE TO THE DAMAGE IS LOCATED WITHIN A RIVETED AREA AND AN EXCLUDED AREA. SDR HNAA2023042800130Unknown · unknownE968006 POSSIBLE SKIN CRACK AT 2 RIVETS AT FR79 BETWEEN STR3R AND 4R. REPAIRED IAW EMB145 SRM 53-20-01RE9 C,2 D-F FIG213 SHEET 2-3 AND PIEDMONT EO1-53-23-0101SDR DALA2023041002770Unknown · unknownSHIP 665 CORROSION ON INTERNAL DOUBLER THE FWD LAVATORY SERVICE BTW STA 700 TO 720 AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00144 INTERNAL DOUBLER ON FWD LAVATORY SERVICE BTW STA 700 TO 720 AT FWD CARGO COMPARTMENT WAS REPLACED PER B757-200 SDR DALA2023041002762Unknown · unknown(LOG 2705484) WHILE PERFORMING A GVI OF EXISTING REPAIR L/L 2447021 ER/A 602811 A DENT WAS FOUND MEASUREMENTS ( W=.900"X D=.010"). REMOVED AND REPLACED REPAIR ON FUSE SKIN STA 727K TO 727L STRINGER 23 RIGHT IAW ERA 602811-14 REV A.SDR DALA2023041002761Unknown · unknown(LOG 2705481) DURING INSPECTION FOUND DOUBLER REPAIR BETWEEN STA 727K AND 727L ON RH SIDE OF SKIN FWD OF AFT CARGO DOOR HAS MULTIPLE STEPPED, OVERSHOT AND UNDERSHOT RIVETS. REMOVED AND REPLACED OVER AND UNDER SHOT FASTENERS ON FUSE SKIN DOUBLER @ STA 727K AND SDR DALA2023041002760Unknown · unknown(LOG 2705257) DURING INSPECTION FOUND RH EXTERIOR FUSELAGE SKIN, FOUND A DENT AT STA 400 + 8", S-20R. REPAIR EXTERIOR SKIN DAMAGE STA 400+8" STR 20R, USING 2024-T3 .063 LOT# 5086648-1 IAW B737 SRM 51-00-01-2R REPAIR 3.SDR GTIA2023040637102Skin · dented"3 EACH DENTS LOCATED BETWEEN FRAMES 23 TO 24 AND FRAMES 24 TO 25 LH SIDE OF FUSELAGE. RAF-01 3069145-02 HAS BEEN GENERATED.-PERFORMED REPAIR INSTRUCTION ON DENT EXTERNAL SKIN LOC ON FR 23 PLUS 19 INCH AND BTW STRG 24-25 LH UPPER FUSELAGE IAW EA # 53-0722-23 RSDR DALA2023040602697Unknown · unknownSHIP 3352 AN EXISTING REWORK WAS FOUND AT SKIN PANEL F53486009208, M/F ABS5043B040, T42, BETWEEN FR 67-68 AND STR 51-52 RH. THE DAMAGE IS LOCATED AT AN EXCLUDED AREA AS PER ALLOWABLE DAMAGE A330 SRM TASK 53-41-11-283-004 FIGURE 6 SHEET 5. CORRECTIVE ACTION: FISDR SWIA20230519038Unknown · crackedAIRCRAFT SKIN JUST BELOW LH TRU DOOR AFT LOWER LATCH HAS POTENTIAL CRACK. (C-CHECK RO 5/15/2023) REMOVED CRACKED SKIN PANEL AND INSTALLED NEW SKIN PANEL (P/N 600-33052-79) AT L/H TRU DOOR REF CRJ200 SRM 51-42-06, CRJ-200 SRM 51-42-13 AND DWG 600-33052 RSDR HNAA202304280147Unknown · unknownE967856 POSSIBLE CRACKS AROUNF FASTENER (1EA) AT FR77 BTWEEN STR08R AND 09R. REPAIRED IAW EMB145 SRM 53-32-01 RE 9 C,2 D-F FIG 213 SHEET2-3 AND PIEDMONT EO1-53-23-0101SDR HNAA2023042800146Unknown · unknownE967855 POSSIBLE CRACKS AROUNDFASTENER (4EA) AT FR77 BETWEEN STR 05R-07R. REPAIRED IAW ETD2023-145-008966 AND PIEDMONT EO1-53-23-0107.SDR HNAA2023042800145Unknown · unknownE967854 POSSIBLE SKIN CRACKS AROUND FASTENER (3EA) AT FR77 BETWEEN STR03R AND 05R. REPAIRED IAW EMB145 SRM 53-32-01 RE 9 C,2 D-F FIG 213 SHEET 2-3 AND PIEDMONT EO1-53-23-0101SDR HNAA2023042800144Unknown · unknownE967852 POSSIBLE SKIN CRACKS AROUND FASTENER (1EA) AT FRAME 77 BETWEEN STR 08L AND 09L. REPAIRED IAW EMB145 SRM 53-32-01 RE9 C,2 D-F FIG 213 SHEET 2-3 AND PIEDMONT EO1-53-23-0102SDR AALA202304254812Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN, AROUND VACUUM WASTE VENT, LOCATED FROM BS 907 TO BS 927 AT LBL 22. REPAIRED SKIN PER SRM 53-70-01-2R-3.SDR DALA2023041302914Unknown · unknown(LOG 2703283) DURING INSPECTION FOUND B737-900ER FUSELAGE SKIN AT STA807-827 & STR-23L WITH DENT, GOUGE. ACCOMPLISH ER/A 594662-14 REV B.SDR GTIA2023040637091Skin · dentedREF MWI 3003068-1. DENT ON FUSELAGE FR 70 STR 39-41. RAF 01 GENERATED.-ACCOMPLISHED REPAIR OF FUSE SKIN FR70 STR 39-42 RH AS PER REPAIR INSTRUCTIONS REF REO L24358 AND RDAF 81177563/093/2023#A. THIS IS LIFE LIMITED TO 6MO PER RDAF 81177563/093/2023#A.SDR DALA2023040502663Unknown · unknownSHIP 663 FUSELAGE/ RHS / STA 199.9 AND WL 186.09 / BIRD STRIKE. CORRECTIVE ACTION: C/W SECTION I OF ERA 607614-14 REV ORIGINAL ON NRC 004. SEE LOG 2702845 FOR REPETITIVE INSP AND LOG 2702845 FOR PREMIANT REPAIR. (2703293)SDR DALA2023040502662Unknown · unknownSHIP 663 FUSELAGE / STA 199.9 AND WL 186.09 / BIRD STRIKE. CORRECTIVE ACTION: REF ERA 607614-14. (2702845)SDR DALA2023040502652Unknown · unknownSHIP 3311 LWR FUSELAGE FWD CARGO DOOR CUTOUT EXTERIOR SKIN HAS AREA OF DAMAGE FRAME 20A LWR FWD CORNER. CORRECTIVE ACTION: COMPLIED WITH PRI 607389-14. (2703840)SDR IPXA2023050293089Skin · dentedINSPECTION TYPE:3C*MAJOR REPAIR* R/H FUSELAGE SKIN DENT REPAIR AT STA Y=1035 ABOVE LONGERON 41.REPAIRED DENTED SKIN AT THE R/H FUSELAGE AT STA Y=1035 AND LONGERON 41R IAW VTSAA EA 011-5330-01-A9898 I/R AND UPS EO MD11-5330-86734-A DATED 04/28/2023 FAA FORM 810SDR ASAA2023040342993Skin · dentedFUSELAGE STA.294.5 LH LOWER BELLY SKIN TO MID SKIN LAP SEEM DENTED-5.0"L X 5.50"W X0.028"D - DEPTH OF LOWER SKIN.DENT WIDTH IS LONGITUDINAL IN LENGTH & RUNS ALONG THE FRAME.STREAMER (HIDDED DAMAGE INSPECTION ON INTERIOR STRUCTURE IS REQUIRED. GROUNDED - YES. DSDR SWAA2023041423038Flange · crackedEXTERNAL POWER DOOR CUTOUT LOWER FLANGE IS CRACKED<[01] NDT IAW B737-700 SRM 53-10-15-2R-4; PAGE 2; STEP 4.C (7) AND D; TOOL # 44291; DUE 03NOV23; NO DEFECTS NOTED.;[02] OK TO TREAT AND PRIME;[03] LOCATED AND DRILLED EXTERNAL POWER DOOR CUTOUT DOUBLER AND FILLSDR DALA2023040502643Unknown · unknown(LOG 2699667) DURING INSPECTION FOUND LIGHTING STRIKE "HOLE IN SKIN "BETWEEN FRM 500F AND 500G AND STR 20R &21R. CUT OUT DAMAGED AREA PER B737 SRM 53-00. INSTALLED DOUBLER PER B737 SRM 53-00-01-2R PROCEDURE 3.SDR IPXA2023040392564Unknown · unknownINSPECTION TYPE:CK1C*MAJOR REPAIR* FRAME 12 LAVATORY VENTURI EXTERNAL DOUBLER INSTALLATION FOR RCD PURPOSES ONLYCOMPLIED WITH UPS EO A300-5330-72601-B AND RCD 269970SDR DALA2023040302549Unknown · unknownSHIP 3221 CRACK EXTERNAL SKIN LOCATED FR28 PLUS 6 INCHES AND STR43LH AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ERA 607113-14AD REV.ORIGINAL. (2700327)SDR DALA2023111709498Unknown · unknownSHIP 6808 B757-200 / FUSELAGE / STA1240 / STR22R-23R / SKIN DENT / REPAIR. CORRECTIVE ACTION: REF ERA 607399-14. (2698175)SDR SWIA202305190036Unknown · corrodedCORROSIION AROUND FASTENERS HOLES ON THE FUSELAGE FOR LEFT FORWARD FUSELAGE ACCESS PANEL 131AL, (C-CHECK RO 5/15/2023) BLENDED OUT CORROSION AROUND FASTNER HOLES FOR ACCESS PANEL 131AL REF CRJ 200 SRM 51-21-06 AND FOUND IN LIMITS REF CRJ 200 SRM 53-00-3SDR DALA2023040502630Unknown · unknownSHIP 6808 WORKING NRC 16 ERA/PRI 607399-14 REV ORIG. CORRECTIVE ACTION: C/W ERA 607399-14 REV ORIG ON NRC 16. MONITOR LOG IS LOG PAGE 2698175. (2699168)SDR DALA2023040502623Unknown · unknownSHIP 5648 COMPLY WITH ERA 607267-14 REV ORIGINAL. CORRECTIVE ACTION: COMPLIED WITH ERA 607267-14 REV ORIGINAL (2699227)SDR DALA2023040302558Unknown · unknownSHIP 3221 A CRACK WAS FOUND IN EXTERNAL SKIN BETWEEN FR28 TO FR29 AND STRG 43LH TO STRG 44. CORRECTIVE ACTION: COMPLIED WITH ERA 607113-32. (2699179)SDR DALA2023110909255Unknown · unknownSHIP 6714 FUSELAGE / STA 620 - 640 / LIGHTNING DAMAGE. CORRECTIVE ACTION: REF ERA 607354-14. (2697128)SDR FDEA202303310566Skin · corrodedR/H LOWER HORIZONTAL ON SIDE WALL SKIN AT LONGERON 35R IN BETWEEN STA 2136-2151, LIGHT SURFACE CORROSION UNDER EXISTING REPAIR DOUBLER AREA. REPAIRED CORRODED AREA PER E.A.1-5330-T0373990SDR DALA2023040602721Unknown · unknownSHIP 5646 ER/A 483952-14 / SECTION V ONE TIME INSPECTION. CORRECTIVE ACTION: REF ERA 483952-14. (2697767)SDR DALA2023040402606Unknown · unknownSHIP 3354 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN FROM FR13 BTW STR2L TO STR3L ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOC. FR13 BTW STR2L AND STR3L AS PER A330 SRM 53-11-11-300-003. (2697839)SDR DALA2023040302567Unknown · unknownSHIP 6714 LIGHTNING STRIKES BETWEEN STA 600 AND 690 AT LAP JOINT ON LEFT HAND SIDE. NR CARD 23,24,25,26,27, AND 28. CORRECTIVE ACTION: COMPLIED WITH PRI 607354-14 REV 0- REV 4 AND ERA 607354-14 REV ORIGINAL. PRI MATCHES ERA. (2697611)SDR FDEA202303310536Skin · chafedAGING AIRCRAFT - EXISTING REPAIR AT FUSELAGE SKIN CENTER LOWER CARGO AFT DOOR JAMB CUTOUT STATION 1781 RIGHT HAND SIDE BETWEEN LONGERON 39 RIGHT TO LONGERON 41 RIGHT. EXISTING REPAIR AT FUSELAGE SKIN CENTER LOWER CARGO AFT DOOR JAMB CUTOUT STATION 1781 RSDR AALA202305108409Skin · damagedAIRCRAFT WAS GROUNDED: EXTERNAL POWER ACCESS RECEPTACLE AREA HAS EDGE DAMAGE TO LOWER EDGE OF SURROUND OPENING. SMALL CRACK 3/4 INCH LONG ON FORWARD SIDE. **SUPPLEMENTAL REPORT FOR AALA202304038409: REPAIRED DAMAGED AREA IAW SRM 53-10-15-1A-4** (CLOSED)SDR SWIA2023050100018Unknown · dentedCREASED/DENT DAMAGE FOUND ON UPPER FUSELAGE SKIN 3.5" AFT OF 31.875% BETWEEN STR 4R-5R (C-CHECK RO 4/26/2023) COMPLIED WITH REPAIR ON UPPER FUSELAGE SKIN 3.5" AFT OF 31.875% BET. STR 4R-5R REF REO 601R-53-71-222 REV A DATED 2023-04-08, COMPLIED WITH SSDR SWAA2023050122238Gusset · crackedCRACK GUSSET LOCATED BS500D AT LEVEL STR19L FWD CARGO COMPARTMENT 2023-219727<[01] REPLACED GUSSET LOCATED BS500D AT LEVEL STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7902; SHEET 209; REV: -<BR>SEE INDIVIDUAL SIGN OFF BELOWSDR SWAA2023050122240Gusset · crackedCRACK GUSSET LOCATED BS500D AT LEVEL STR19R FWD CARGO COMPARTMENT 2023-219728<[01] REPLACED GUSSET AND FASTENERS LOCATED BS500D AT LEVEL STR19R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02 AND DRAWING #143A7902; SHEET 209; RESDR SWAA2023050122249Angle · crackedCRACK ANGLE LOCATED BS400 AT LEVEL STR26L FWD CARGO COMPARTMENT 2023-219732<[01] REPLACED ANGLE LOCATED BS400 AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7505 SHEET 81 REV - <BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] RSDR SWAA2023050122250Angle · crackedCRACK ANGLE LOCATED BS500C AT LEVEL STR26L FWD CARGO COMPARTMENT 2023-219733<[01] REPLACED ANGLE LOCATED BS500C AT LEVEL STR26L FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 .DWG 143A7505 SHEET 82 REV- SRM 51-10-02 ITEM 9. MEASURES OF CRACK IS: L =0.470? .TSDR SWAA2023050122470Stringer · crackedCRACK STRINGER 23L LOCATED BS540 AT FWD CARGO COMPARTMENT 2023-219755<[01] TOOL USED ULTRASONIC THICKNESS INSTRUMENT P/N 45MG S/N 221859911 DUE DATE 07-NOV-23.;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X1693P030456; DUE DATE: 12 MAR 24SDR SWAA2023050122471Stringer · crackedCRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT 2023-219758<[01] UT EQUIPMENT P/N: 45MG; S/N: 221859911; DUE DATE: 07-NOV-23;[02] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022237; DUE DATE: 26-JAN-24.;[03] TOOLS USED: TEMPERATURE CONTROSDR IPXA2023041692893Skin · dentedATB, AFTER RAISING GEAR HANDLE GEAR DISAGREE AND GEAR DOORS EICAS MESSAGE. NOSE GEAR LIGHT REMAINED GREEN MAIN GEAR INDICATORS BLANK. OBVIOUS VIBRATION WHILE AIRBORNE. AFTER CHECKLIST AND LANDING GEAR HANDLE ALL INDICATIONS NORMAL.T/S PER FIM 32-30-00-815-816SDR DALA2023033102493Unknown · unknownSHIP 665 IN REFERENCE NRC 00050: NICKS (3 EAS) ON FUSELAGE SKIN STA. 1708, BTW S-19R TO S-20R. CORRECTIVE ACTION: SUMMARY OF NRC 00653. AREA WAS REPAIRED PER ER/A 607089-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 607089-14 REV 0. (2695925)SDR CALA2023033100936Unknown · damagedDURING ACCOMPLISHMENT OF EA 5310-07772 REV. ORIG OP 001 (SB 53-1383 R00), HOLES 2 &4 ON THE LH FRAME 35 AND HOLES 1, 2 & 3 ON THE RH FRAME 35 WERE FOUND DAMAGED. DURING REPAIR EMBODIMENT, HOLES #10 ON BOTH THE LH / RH SIDE WERE FOUND TO BE OUTSIDE OF EA 5310-0SDR HALA2023033000136Unknown · unknownSUPPLEMENTAL SUBMISSION TO HALA2023032700010. RESOLUTION UPDATED. AIRCRAFT CAME IN WITH DENT ON AIRCRAFT LEFT SIDE UNDER WING SCAN LIGHTS. DAMAGE OUT OF LIMITS FOR REVENUE FLIGHT. PERFORMED HFEC ON DAMAGE AREA SKIN & SURROUNDING & FRAME 30 NO CRACKS NOTED. PER
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