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 SIMA2020051109004Skin · dentedFUSELAGE SKIN HAS 1 DENT BETWEEN FRAME 11 AND 12 JUST BELOW STR 18L MAJOR REPAIR,FOUND ON RETUEN TO SERVICE-C/A-INSTALLED REPAIR DOUBLER AND FILLER BETWEEN FR 11 AND FR 12 STR 18L I/A/W EMB 175 SRM 53-10-01SDR CALA2020051100953Skin · dentedDENT REPORTED TO SM FRONT OF L2 DOOR. LOCATION IS STA 612 STR 16 L. DENT MEASURES 2.2"X2.8"X.120" A/Y IS 18.3 AND IS OUT OF LIMITS AND MUST BE REPAIRED, THE REPAIR MAY BE DELAYED SINCE ALL OTHER CRITERIA IS WITHIN LIMITS PER 757-3 SRM 53-00-01 NOTE I. INITIATESDR DALA2020051902409Skin · damagedWHILE PERFORMING SERVICE CHECK FOUND DAMAGE NEAR LOWER TCAS ANTENNA. REPAIRED PER ERA 7025422. (LP 7025422)SDR UIEA2020051200881Skin Panel · corrodedFX - KEEL BEAM #193P PANEL SKIN FOUND CORROSION.(<P>FX - KEEL BEAM #193P PANEL SKIN REPLACED AS PER SRM 51-10-02.</P>)SDR UIEA2020051200994Skin · chafedAPU COMPT AFT LOWER SKIN SURFACE AT STA 2742 FOUND CHAFING(<P>APU COMPT AFT LOWER SKIN SURFACE AT STA 2742 SKIN REPAIRED AS PER SRM 53-80-01-2R-1 FIG 201</P>)SDR SWIA2020061251094Skin Panel · dentedDENT DAMAGE ON FUSELAGE SKIN PANEL BETWEEN FS517.0-FS533.3 AND STR 15L-16L (FWD AND ABOVE THE R FWD CARGO DOOR). PLEASE EVALUATE AND REPAIR IF NECESSARY OR FILL DENT TO ELIMINATE VISUAL EVIDENCE IAW AMM. (C-CHECK) RO 6/8/2020 DENT BETWEEN FS517.0-FS533.3 AND SSDR SWAA2021042775717Skin · dentedDENT AT FUSELAE SKIN STA 360+14' ON STR 17L; L=3.25'; W=2.5'; Y=0.039'; WY=64.FOUND OUT OF LIMITS. DENT GOES ACROSS STR 17L. REPAIR ACCOMPLISHED AS PER AAR W.I 20159406 AND SWA EA 2015300513 REV IR.SDR SWIA2020061051037Doubler · corrodedDOUBLER FOR TCAS OMNIDIRECTIONAL ANTENNA HAD CORROSION. REMOVED AND REPLACED THE ANTENNA DOUBLER IAW DWG & SRM. COMPLIED WITH TASK CARD. LEAK CHECKED GOOD. OPS CHECKED GOOD.SDR NACA202005150004Skin · crackedWHILE PERFORMING AD 2012-26-02 (M), FOUND MFEC CRACK INDICATION ON CHEM MILL LINE STR10R, BS500B+4 TO BS500B+5 ONE INCH LONG. REPAIR IAW EA PD37-53-3157, BOEING REPAIR SKETCH NAC-NAC-20-0008-09C REF BOEING ID 202002140020-0004. IAW SB 737-53A1234 R2 FIG 34. SDR KCSA202005061060Bear Strap · corrodedL3 DOOR BEAR STRAP HAS CORROSION ON FWD SIDE OF DOOR CUTOUT JUST ABOVE THE UPPER DOOR HINGE FITTINGSDR IPXA2020050655016Skin · damagedINSPECTION TYPE:N/ADAMAGE AT FUSELAGE SKIN AT STA 500 TO STA 520 AND STRINGER 36L TO 38LREPAIRED DAMAGED SKIN AT STA 500, S36L TO 38L IAW EO B747-5330-76297-ASDR IPXA2020050655015Skin · damagedINSPECTION TYPE:N/ADAMAGE AT FUSELAGE SKIN STA 480 TO STA 500 AND STRINGER 35L TO 37LREPAIRED DAMAGED SKIN AT STA 480 TO 500 $35 L TO 37 L IAW EO B747-5330-76296-ASDR HALA2020050600105Skin · corrodedFUSELAGE SKIN FOUND SUSPECTED CORROSION AT FRAME 76 - FRAME 77, STRINGER 41 LH - STRINGER 42 LH. (AFT CUTOUT HOLE OF WASTE
EXHAUST SYSTEM). // FUSELAGE SKIN CORROSION AT FRAME 76 - FRAME 77, STRINGER 41 LH - 42 LH REPAIRED AS PER REPAIR DESIGN APPROVAL SSDR FDEA2020070641057Skin · corrodedAFT CARGO WASTE TANK AT APPROX STA 2000 & LBL 46 LWR INTERIOR SURFACE SKIN AREA EXFOLIATED. REPAIRED PER EA 1-5330-T0354479 TITLED: FUSELAGE - PLATES AND SKINS - AFT BODY KEEL PLANK P/N AJC 7164-503 - CORROSION BETWEEN BS 1997 AND BS 2005 AND BETWEEN L-44L ANSDR IPXA2020050655018Skin · damagedINSPECTION TYPE:N/ADAMAGE AT FUSELAGE SKIN AT STA 520 TO 580 AND STRINGER 37L TO 41LREPAIRED DAMAGED FUSELAGE SKIN AT STA 520 TO 580 AND STRINGER 37 L TO 41 L IAW EO B747-5330-76292-ASDR UATA2020050400001Skin · puncturedFOUND HOLE IN BELLY SKIN BETWEEN FRAME 2/F AND 3F. CLEANED HOLE TO 1/2 INCH ROUND AND INSTALLED A FLUSH PLUG PATCH PER CASA 212 SRM.SDR FDEA2020062300884Skin · dentedON WALK AROUND FOUND DENT ON R/H SIDE OF AIRCRAFT JUST AFT RADOME. FABRICATED DOUBLER, TRIPLER AND FILLER. DRILLED AND COUNTERSINK. ALODINED AND PRIMED IAW SRM 53-20-00 CLASS 2 REPAIR FIG 6. INSTALLED REPAIR PARTS IAW SRSDR FDEA2020052230881Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHT HAN HAND UNDERWING LONGERON AND FUSELAGE SKIN, FOUND 03 EACH CRACKS WHICH APPROXIMATELY 1.1" AND 0.9' AT STASDR FDEA2020050430884Skin · damagedON WALK AROUND FOUND DENT ON R/H SIDE OF AIRCRAFT JUST AFT RADOME. FABRICATED DOUBLER, TRIPLER AND FILLER. DRILLED AND COUNTERSINK. ALODINED AND PRIMED IN RSDR FDEA2020050430881Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHR HAND UNDERWING LONGERON AND FUSELAGE SKIN FOUND 03 EACH CRACKS WHICH APPROXIMATELY 1.1" AND 0.9' AT STATION 1033 STRINGSDR FDEA2020050430880Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE LEFT HAND UNDERWING LONGERON AND FUSELAGE SKIN FOUND 03 EACH CRACKS WHICH APPROXIMATELY 1.0" AT STATION 1028 SRINGSDR UIEA2020050700955Skin Panel · dentedDENT DAMAGE ON FUSELAGE SKIN PANEL AT STA 2716 NEAR RBL 11.(<P>REPAIRED DAMAGE AREA IAW EI NO T2020A53M-1136 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR DALA2020071002566Skin · damaged(LOG 1554527) WHILE ON THE LINE IN JFK THE AIRCRAFT SUSTAINED GROUND DAMAGE WHICH RESULTED IN PUNCTURE AND DENT. THE DAMAGE IS LOCATED BETWEEN THE NLG DOOR AND THE E&E BAY ACCESS DOOR AT STA 294.5-312 AND STR 28RH. MAINTENANCE REPAIRED DAMAGE PER ERA 583828-14SDR SWAA2020052678925Skin · dentedFOUND 3EA DENTS ON FUSELAGE EXTERNAL SKIN REPAIR FROM STA 440+3' TO 480+6' STR 27R DOT 107-004. REMOVED AND REPLACED FUSELAGE EXTERNAL SKIN REPAIR BETWEEN BS 440 +490; S-26R/S-28L BELOW FWD CARGO DOOR CUTOUT 'STAGE 3 REQUIREMENT FOR TCO-SWA-10-0499 IS PROPERLSDR SWIA202005190788Doubler · corrodedREMOVE AND REPLACE RADIO ALTIMITER #2 FWD AND AFT DOUBLERS (SPACERS) DUE TO CORROSION. (C-CHECK) RO 5/16/2020 REMOVED AND REPLACED RADIO ALTIMETER #2 FWD AND AFT DOUBLERS (SPACERS) REF CRJ900 SRM. CHECKS OKAY, COMPLETED TASK CARDSDR SWAA2020052674302Skin · dentedTWO DENTS OUT OF LIMITS BETWEEN STA 1036 AND STA 1037 AND STRINGER 15L; DENTS FOUND WITHIN 1' OF STRINGER 15L / INSTALLED EXTERNAL FUSELAGE REPAIR BETWEEN STA 1037 AND STA 1036; AND STRINGER 15L; PER REF 737 SRM 53-80-01-2R-3 REP 3; THIS REPAIR IS CATEGORY A RSDR CALA2020050200914Skin · crackedEXTERNAL POWER RECEPTACLE LOWER EDGE CUOUT IS CRACKED REF AAR N/R 99880377 REMOVED AND REPLACED EXTERNAL POWER INNER DOUBLER P/N 141A3722-1 2 PER B737 SRM 52-40-02 AND DWG 141A3702 AND ECRA 5331-02671SDR IPXA2020050154815Skin · damagedINSPECTION TYPE:N/AAC MX REPORTED DAMAGE TO THE LEFT SIDE OF FUSELAGE SKINS AT STA 520 TO STA 580 STRINGER 37L TO 41L P/N: 142U3260-12 AND P/N: 142U3262-11 (REF SRM 53-20-01-0I-1 FIG 1 ITEM 5 AND 21)ACCOMPLISHED EO# B747-5330-76292-A REV 04/XX/2020SDR IPXA2020050154813Skin · damagedINSPECTION TYPE:N/AAC MX REPORTED DAMAGE TO THE LEFT SIDE FUSELAGE SKIN AT STA 500 TO STA 520 AND S36L TO 38L, P/N: 65B07659-305 (REF SRM 53-10-01-OI-1 FIG 1 DETAIL III ITEM 1).ACCOMPLISHED EO# B747-5330-76297-A REV 04/29/2020.SDR IPXA2020050154812Skin · damagedINSPECTION TYPE:N/AAC MX REPORTED DAMAGE TO THE LEFT SIDE FUSELAGE SKIN AT STA 480 TO STA 500 AND S35L TO 37L, P/N: 65B07659-305 ( REF SRM 53-10-01-0I-1 FIG 1 DETAIL III ITEM 1)ACCOMPLISHED EO# B747-5330-76296-A REV 04/XX/2020.SDR 6CBA2020043020192Skin · corrodedTHE FOLLOWING PROBLEM/RESOLUTION WAS FOUND ON THIS AIRCRAFT DURING THE 1200HR/12MONTH INSPECTION.
CORROSION SPOTS WERE FOUND ON THE FUSELAGE BELLY SKIN AT THE RH LONGITUDINAL LAP JOINT AT STRINGER 20 BETWEEN FRAMES 18 AND 19.
THE CORROSION HAS BEEN REMOVED SDR DU4R2020043000014Skin · gougedDURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND FR 25 - 26, STR. 25L TO BE GOUGED. S/O 418149 N/R 28001SDR SWIA2020060950933Skin · dentedRT FUSELAGE SKIN HAS DENT OUTBOARD OF NLG AFT GEAR DOOR HINGE POINT APPROX FS 232 / BL 8 RT. (C-CHECK) RO 4/27/2020 REPAIRED THE DENT AT THE RT FUSELAGE SKIN, OUTBOARD OF NLG AFT GEAR DOOR HINGE POINT. REF REO. REFERENCE THE CONTINUE CARD FOR DETAILS.SDR IPXA2020052255629Skin · damagedINSPECTION TYPE:2CCUT OUT FUSELAGE SKIN BETWEEN STA 1801 - 1821 AND BETWEEN LONGERONS 45R & 47R TO ACCESS LONGERON 46R REPLACEMENT.REPAIRED FUSELAGE SKIN CUT OUT BETWEEN STA 1801 - 1821 AND BETWEEN LONGERONS 45R & 47R IAW MD-11 SRM 53-00-01, REPAIR 1, FIGURE 2SDR SWIA2020060950980Doubler · corrodedCORROSION FOUND ON TCAS OMNIDIRECTIONAL ANTENA CHANNEL BETWEEN FS295.0 - FS310 COMMON TO STR 27. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW TCAS ANTENNA CHANNEL DOUBLER BETWEEN FS 295.0 TO FS 310 REF DRAWING AND SRM. PRESSURE CHECK GOOD. SEE CONTINUATIOSDR QXEA2020051900166Skin Panel · dentedREF RD 84-55-1521/1 TEMP REPAIR FOR DENT DAMAGE TO AFT FUSE SKIN PANEL PN 85537506 FWD OF FRAME #3 STR 28P. APPLIED YELLOW DOT FOR IDENTIFICATION PURPOSES ONLY.SDR UIEA2020050100926Skin · corrodedSTA 1065 LOWER INTERNAL SKI AND STRINGERS HAVE SURFACE CORROSION.(<P>REMOVED CORROSION. DID SCAN INSPECTION, FOUND SKIN TO BE OUT OF LIMITS. INSTALLED DOUBLER AND TRIPLER IAW REA 47401 REV A.</P>)SDR FDEA2020043080812Skin · dentedDENT ON FUSELAGE SKIN AT BSTA 1691 BETWEEN STR 14-15 L/H EVALUATED DENT OF FUSELAGE SKIN BS1691 BETWEEN STR 14-15 L/H IAW SRM 53-00-01-1A AND FOUND TO BE OUTSIDE SRM LIMITS DUE TO PROXIMITY TO ADJACENT LAP JOINT. REFER TO FEDEX EA F-5330-T0353565 TITLE FUSELSDR JR2R202004281556Skin · dentedL/H FUSELAGE DEANTED BETWEEN FR21-FR22 AND STR 22L AND STR 23L. REPAIRED IAW EMB ETD2020-170-012861SDR SWIA2020070650921Skin · dentedTWO DENTS FOUND OUT-OF-LIMITS ON THE LEFT SIDE FORWARD FUSELAGE SKIN PANEL LOCATED AT FRAME 11 AND BETWEEN STRINGERS 17L AND 18L. DENT FORWARD OF FRAME 11 MEASURES 3.84"L X 3.18"W X .060"D WITH A CREASE. DENT AFT OF FRAME 11 MEASURES 2.16"L X 1.45"W X .033"D.SDR SWIA2020060950925Skin · dentedRIGHT SIDE FUSELAGE APPROXIMATELY AT 7 O'CLOCK POSITION. BETWEEN FS364.00 & FS379.00. DENT LOCATED BELOW AND SLIGHTLY AFT OF FWD POTABLE WATER SERVICE PANEL. DENT MEASURES 2.5" W X 2.5" L WITH A MAXIMUM DEPTH OF 0.078" AT THE DEEPEST POINT. W/D = 32.05. REQUISDR SWIA2020060550921Skin Panel · dentedTWO DENTS FOUND OUT-OF-LIMITS ON THE LEFT SIDE FORWARD FUSELAGE SKIN PANEL LOCATED AT FRAME 11 AND BETWEEN STRINGERS 17L AND 18L. DENT FORWARD OF FRAME 11 MEASURES 3.84"L X 3.18"W X .060"D WITH A CREASE. DENT AFT OF FRAME 11 MEASURES 2.16"L X 1.45"W X .033"D. SDR FDEA202004270930Skin · crackedPACK #1 EXHAUST EXTERNAL FUSELAGE SKIN - UPPER AFT CORNER - CRACK EMANATING FROM FASTENER HOLE TO CUTOUT. CONFIRMED WITH NDT HFEC. REPAIRED / REMOVED CRACKED SKIN CONDITION. REF: MD-11 SRM 53-20-15-2R REPAIR #3 SHEET 1SDR YENA2020050470320Skin · crackedDURING HEAVY MAINTENANCE, CRACK STR 9L FR73 UPPER FUSELAGE; REF AEROMAN NR 2020-125482: R & R STR 9L FR73 UPPER FUSELAGE IAW SRM 51-40-08 AND DWG #190-67977-803.SDR SWIA2020060950977Skin · gougedEVALUATE GOUGE ON FUSELAGE SKIN UNDER PAX DOOR AFT OF FS 333. (C-CHECK) RO 4/23/2020 REPAIRED FUSELAGE SKIN UNDER PAX DOOR AFT OF FS 333. WITHIN LIMITS REF REO. SEE CONTINUATION CARD FOR DETAILS.SDR FDEA2020042961056Skin · damagedWHILE ACCOMPLISHING TASK CARD 53309364, RE- INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN DAMAGE, FOUND DAMAGE STILL EXISTS BETWEEN FRAMES 32 AND 33 AND STRINGER 45R AND 46R, PREVIOUS BLENDED OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10-12,SDR FDEA2020042961054Skin · damagedWHILE ACCOMPLISHING TASK CARD 53309364, RE-INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN DAMAGE, FOUND DAMAGE STILL EXISTS APPROX 7" FWD OF FRAME 35 AND BETWEEN STRINGER 45R AND 46R, PREVIOUS BLENDED OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-SDR FDEA2020042961053Skin · damagedWHILE ACCOMPLISHING TASK CARD 53309364, RE-INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN DAMAGE, FOUND DAMAGE STILL EXISTS BETWEEN FRAMES 33 AND 34 AND BETWEEN S45R AND S46R, PREVIOUS BLEND OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10-12, FIGSDR FDEA202004261052Skin · damagedWHILE ACCOMPLISHING TASK CARD 53309364, RE-INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN, FOUND DAMAGE STILL EXISTS BETWEEN FRAMES 30 AND 31 AND BETWEEN S45R AND S46R, PREVIOUS BLEND OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10-12 FIG 208. ASDR SWAA2020051877323Skin · damagedPREVIOUS BLEND ON FUSELAGE SKIN BS460+19; 5' BELOW STR25L / REPAIRED PER ATS ER 20-02510 REV IR AND SWA EA #20-153-00526 REV IR
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