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 RJEY2019052800003Skin Panel · wornWEAR IB EXTERNAL SKIN PANEL LOC. ON FR34 BTW STR 43L TO STR 43R.SDR 29GA2019042600002Skin · damagedNO FLIGHT# DISCOVERED DURING INSPECTION REPORT: LEFT SIDE FUSELAGE STA 583-608 AND ABOVE SL1517 HAS 2 GOUGES/DENTS 1, .20" DEEP 1 1/2" BY 1/2".2, .015 DEEP X 1/2" X 1/4". CORRECTIVE ACTION: PERFORMED SHEET METAL REPAIR I.A.W. SAAB REPAIR STATEMENT 340 SDS 047SDR C77A2019042400001Skin · dentedDURING MAINTENANCE, 3 DENTS WERE DISCOVERED BETWEEN FR10/FR11 AND S-15L/S-17L ON THE FORWARD FUSELAGE LH LATERAL SKIN PANEL. THE DENTS EXCEEDED LIMITS OF SRM PART II 53-10-01/AD02 BECAUSE THAT NUMBER OF DENTS ARE NOT ALLOWED TO BE LOCATED IN THE SAME BAY. TSDR SWAA2022030746775Skin · corroded***CORROSION*** SIGNS OF CORROSION UNDER DORSAL FIN AREA BETWEEN STA 927 TO STA 1006. STR2L TO STR2R / REPAIRED CORROSION DAMAGE UNDER DORSAL FIN BS 927-1006 BETWEEN STR 2L-2R. AREA #1 4.8' X 4.0' REMAINING .040' DMG .040'. AREA #2; 1.5' X 1' REMAINING .040' OSDR 2019FA0000269Skin · chafedCHAFE DAMAGE ON LOWER COWLINGSDR SWIA2019060545951Skin · scratchedR/H FUSELAGE 4" FWD OF REAR SPAR(VS67.50%) BETWEEN STGR 10 AND STGR12, HASVERTICAL SCRATCH 7" IN LENGTH. (C-CHECK) RO: 06/02/2019 REPAIRED R/H FUSELAGE 4" FWD OF REAR SPAR(VS67.50%) BETWEEN STGR 10 AND STGR12 IAW REO.SDR SWIA2019060545950Skin · dentedFUSELAGE SKIN DENT FS236 JUST ABOVE STR15 LEFT. (C-CHECK) RO: 06/02/2019 REPAIRED DENT IAW REO AND SRM.SDR FDEA2019042530882Skin · chafedFORWARD CARGO COMPARTMENT DOOR FORWARD FUSELAGE CUTOUT SKIN AT STATION 899 BETWEEN LONGERON 40 AND LONGERON 42 FOUND WITH CHAFFED CHAFFED MARK AT FORWARD CARGO COMPARTMENT DOOR FORWARD FUSELAGE CUTOUT SKIN STATION 899 BETWEEN LONGERON 40 AND LONGERON 42 TRSDR CALA2019042600645Skin · crackedACCOMPLISH INTERIM REPAIR AT FUSELAGE SKIN BETWEEN STA 375 AND S TA 420 AND STR 19R & STR 21R PER UNITED EC/RA 5331-02363. ON OR BEFORE THE AIRCRAFT REACHES 50,000 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSPECTION PER PART 2 OF EC/RA 5331-02363. PLANNING TO SDR CALA2019042600644Skin · crackedACCOMPLISH INTERIM REPAIR AT FUSELAGE SKIN BETWEEN STA 177 & STA 196 AND STR 24L PER UNITED EC/RA 5331-02361. ON OR BEFORE THE A IRCRAFT REACHES 50,000 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSPECTION PER PART 2 OF EC/RA 5331-02361. PLANNING TO CONTACT E NGSDR CALA2019042600643Skin · damagedACCOMPLISHED INTERIM REPAIR AT FUSELAGE SKIN BETWEEN STA 360 & S TA 380 AND BETWEEN STR 16L & 19L PER UNITED EC/RA 5331-02362. ON OR BEFORE THE AIRCRAFT REACHES 50,000 TOTAL AIRCRAFT FLIGHT CYC LES, PERFORM AN INSPECTION PER PART 2 OF EC/RA 5331-02362. PLANN ISDR ASOA201904237038Skin · chafedA/C IS IN C-CHECK WHEN INSPECTION FOUND A CHAFE AT FRAME 70 BETWEEN STRINGER12R AND 13R. MAINTENANCE PERFORMED REPAIR PROCEDURES IAW ECTC ETD2019-145-048747.ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA201904237037Skin · crackedA/C IS IN C-CHECK WHEN INSPECTION FOUND THE EXTERIOR SKIN CRACKED AT FRAME 75,STRINGER 2R. MAINTENANCE REPAIRED THE SKIN AT FRAME 75 IAW EMB SRM 53-31-01 REF. FIGURE #219-FUR 53-00-016-72. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR SWAA2022030754326Skin · chafedLOG BOOK PG# 1131206 - WHILE REMOVING DORSAL FIN - FOUND CHAFFED AREA UNDER TIP OF DORSAL FIN AT STA 852-853 - JUST LEFT OF STR.1 - THAT MEASURES .300LX30'W X.014 DEEP / REMOVED DAMAGE AT STR 1 ON STA 850 - 855 ORIGINAL T .040' REMOVED .013' REMAINING T = .027SDR SWAA2019043032076Skin · gougedCROWN SKIN GOUGED AT BS. 276, BETWEEN STR. 5L TO STR. 6L. / REPAIRED SKIN PER SRM.SDR UIEA2019042603970Skin · corrodedM/D STA 1475 RH STR 8-9 SKIN FOUND CORROSION.(<P>CABIN STA 1475 RH STR 8-9 INNER SKIN SURFACE CORROSION REMOVED AND RE-PROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN ALLOWABLE DAMAGE LIMIT IAW 53-00-01 1 FIG 101.</P>)SDR UIEA2019042603971Skin · corrodedM/D STA 1475 RH STR 1-2 SKIN FOUND CORROSION.(<P>CABIN STA 1475 RH STR 1-2 INNER SKIN SURFACE CORROSION REMOVED AND RE-PROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN ALLOWABLE DAMAGE LIMIT IAW SRM 53-00-01 1 FIG 101. </P>)SDR UIEA2019042603974Skin · corrodedM/D STA 1240 LH STR 17-18 SKIN FOUND CORROSION.(<P>CABIN STA 1240 LH STR 17-18 INNER SKIN SURFACE CORROSION REMOVED AND RE-PROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN ALLOWABLE DAMAGE LIMIT IAW 53-00-01 1 FIG 101. </P>)SDR UIEA2019042603975Skin · corrodedM/D STA 1240 LH STR 16-17 SKIN FOUND CORROSION.(<P>CABIN STA 1240 LH STR 16-17 INNER SKIN SURFACE CORROSION REMOVED AND RE-PROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN ALLOWABLE DAMAGE IAW SRM 53-00-01 1 FIG 101. </P>)SDR UIEA2019042603977Skin · corrodedM/D STA 1240 LH STR 15-16 SKIN FOUND CORROSION.(<P>CABIN STA 1240 LH STR 15-16 INNER SKIN SURFACE CORROSION REMOVED AND RE-PROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN ALLOWABLE DAMAGE LIMIT IAW SRM 53-00-01 1 FIG 101.</P>)SDR UIEA2019042603981Skin · corrodedM/D STA 1240 LH STR 14-15 SKIN FOUND CORROSION.(<P>CABIN STA 1240 LH STR 14-15 INNER SKIN SURFACE CORROSION REMOVED AND RE-PROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN ALLOWABLE DAMAGE LIMIT IAW SRM 53-00-01 1 FIG 101.</P>)SDR UIEA2019042603983Skin · corrodedM/D STA 1240 LH STR 13-14 SKIN FOUND CORROSION.(<P>CABIN STA 1240 LH STR 13-14 INNER SKIN SURFACE CORROSION REMOVED AND RE-PROTECTED IAW 51-10-02 AND SRM 51-20-01. CHECKED WITHIN ALLOWABLE DAMAGE IAW SRM 53-00-01 1 FIG 101. </P>)SDR UIEA2019042603986Skin · corrodedM/D STA 1240 LH STR 12-13 SKIN FOUND CORROSION.(<P>CABIN STA 1240 LH STR 12-13 INNER SKIN SURFACE CORROSION REMOVED AND RE-PROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN ALLOWABLE DAMAGE LIMIT IAW 53-00-01 1 FIG 101.</P>)SDR UIEA2019042603988Skin · corrodedM/D STA 1355 RH STR 15-16 SKIN FOUND CORROSION.(<P>CABIN STA 1355 RH STR 15-16 INNER SKIN SURFACE CORROSION REMOVED AND RE-PROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN ALLOWABLE DAMAGE LIMIT IAW SRM 53-00-01 1 FIG 101. </P>)SDR UIEA2019042604000Skin · cracked2 EA FASTENER HOLE FOUND CRACK IN SKIN AT STA 38L FROM 980 TO 990 DRAG SPLICE FTG AREAS(<P>FUS-STA 939-991.5 STR 37R-39L FUS SKIN REPAIRED AS PER RI-53-21-13484 REV.A. THIS REPAIR IS A CAT B REPAIR. SUPLEMENTAL INSPECTION IS REQUIRE AS PER SRM 53-20-01-2R-2 FISDR UIEA2019042604006Skin · cracked1 EA FASTENER HOLE FOUND CRACK IN SKIN AT STA 38R FROM 980 TO 990 DRAG SPLICE FTG AREAS.(<P>FUS-STA 939-991.5 STR 37R-39R FUS SKIN REPARIED AS PER SRM 53-20-01-2R-2 REPAIR 2, THIS REPAIR IS A CAT B REPAIR. SUPLEMENTAL INSPECTION IS REQUIRE AS PER SRM 53-20-01-SDR UIEA2019042604030Skin · corrodedM/D STA 1355 LH STR 17-18 SKIN FOUND CORROSION.(<P>CABIN-STA 1355 LH STR 17-18 INNER SKIN SURFACE CORROSION REMOVED AND RE-PROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT. <BR /></P>)SDR UIEA2019042604032Skin · corrodedM/D STA 1355 LH STR 16-17 SKIN FOUND CORROSION.(<P>CABIN-STA 1355 LH STR 16-17 INNER SKIN SURFACE CORROSION REMOVED AND RE-PROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.<BR /></P>)SDR SIMA201904232002Skin · corrodedFUSELAGE INTERNAL SKIN CORRODED BETWEEN FR 3-4 AND BELOW STR 17R-C/A-RAR SKIN PANEL AT FR 3-4 STR 17R IAW EMB 145 SRM 51-40-02SDR SWAA2022030761924Skin · scratchedREF DEFECT # 0578948 (MX NOTE); TWO LARGE VERTICAL SCRATCHES ANTERIOR OF AFT (CAPTAINS SIDE) ENTRY DOOR / REPAIRED FUSELAGE SKIN PER SRM 53-70-01-2R-1 REPAIR 1. PERFORM A LFEC AND DETAILED VISUAL INSPECTION OF REPAIRED AREA AT 50;000 FLT CYCLES SINCE NEW OR 18SDR SWIA2019050345823Skin · damagedFUSELAGE SKIN DAMAGE AT FS 640-654 AND STR'S 23L-24L. (C-CHECK) RO: 05/02/2019 REPAIRED FUSELAGE SKIN DAMAGE AT FS 640-654 AND STR'S 23L-24L. BY EXTERNAL DOUBLER IAW REO.SDR DALA2019042622657Skin · crackedTAIL EXTERNAL SKIN FOUND CRACKED AT BS 1725 BUTT SPLICE S-7R CRACKED CHORD STRAP AND SKIN REPAIRED PER SRM 53-80-01. (LP 1039937)SDR CALA2019042200626Skin · crackedROTO PROBE INSEPCTION SHOWS CRACK INDICATION AT FUSELAGE SKIN, FR35, STR30, LH SIDE, LOWER AFT HOLE INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-02126. DTA DIP INITIATED TO ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE 10 OCT 1 9. PLANNING TO CONTACT ENGINEERSDR DALA2019042202548Skin · corrodedON WALK AROUND FOUND CORROSION LWR FWD CORNER OF AFT LAV SERVICE DOOR AREA. C/W REPAIR PER ERA 577463-14 REV ORIG - ALL RII ITEMS C/W. (LP5673084)SDR CA190422008Access Panel · corroded(CAN) CORROSION WASTE ACCESS PANEL SURROUND DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON THE WASTE ACCESS PANEL SURROUND OF MSN: 50017 (HB-JBH). THE CORROSION WAS BLENDED. HFEC INSPECTION CONFIRMED THAT ALL CORROSION IS REMOVED. THE MINIMUM REMAINING TSDR SWAA2019050332189Skin · corrodedAFT CARGO COMPARTMENT SKIN IN BILGE CORRODED AT BS. 747-4, BL 0. REPAIRED SKIN IAW SRM.SDR HALA2019042320200Skin · cracked2.25 IN CRACK FOUND UNDER FUSELAGE TAIL SECTION APPROX 1197 RIGHT LONGERON L25-L30. // CUT OUT AND REPAIRED CRACK PER 717 SRM 53-00-00-2R-2. TREATED, PRIMED AND PAINTED SURFACES PER 717 SRM 51-22-01. OK FOR SERVICE.SDR DALA2019042202549Doubler · wornINITIAL INSPECTION: WEAR ON LOWER FWD DOUBLER AT FWD CARGO COMPARTMENT DOOR. LOWER FWD DOUBLER AT FWD CARGO COMPARTMENT DOOR WAS REPLACED PER DC-9/MD-80 SRM 51-30-2 AND ER/A 486624-14MA REV. ORIGINAL. (LP1039055)SDR SWAA2019051632745Skin · corrodedFUSELAGE SKIN CORRODED BETWEEN BS. 890 TO BS. 1006, BETWEEN STR. 2L TO STR. 2R. REPAIRED SKIN IAW ER AND EA.SDR R61A201904190463Skin · dented******MAJOR******WHILE AC WAS IN FOR HEAVY CHECK FOUND UNRECORDED DAMAGE (REFEER TO NRIC 4000427-1000-0043) FOUND OUT OF LIMITS PER SRM 53-10-01 AD01. MX REPAIRED DAMAGE CUT OUT AT FR 18+5" AND 1" ABOVE STR 28R IAW SRM 28R FWD FUSELAGE EXTERNAL SKIN PERM REPAISDR SIMA2019042919006Skin · crackedFUSELAGE SKIN HAS A CRACK INDICATION .250 INCHES IN LENGTH 1 RIVET ABOVE STRINGER 6L AT FRAME 77. -C/A-REPAIRED FUSELAGE SKIN AT FRAME 77 IAW SRM 53-32-01.SDR SIMA2019042319003Skin · crackedFUSELAGE SKIN HAS A CRACK INDICATION .125 INCHES IN LENGTH 1 RIVET BELOW STRINGER 6L AT FRAME 77 -C/A-EVALUATED WITH HFEC FOUND NO CRACK. RESTORED SURFACE PROTECTION IAW CPM 51-25-01.SDR DALA2019042002581Skin · crackedINITIAL INSPECTION: CRACKS ON FUSELAGE SKIN STA Y 1494 BTWN LONG 3R-5R. SUMMARY OF NRC 00086: CRACKS ON FUSELAGE SKIN STA Y 1494 BTWN LONG 3R-5R WERE REPAIRED PER ETI-90-19-017 REV. 2 AND ERA 577443 -14 REV. ORIG. SECTION I. ACCOMPLISH SECTION II REPETITIVE INSDR SWAA2022030737073Skin · dentedWHILE WORKING NOSE WHEEL STEERING RIG AND OP'S CHECK JACKED NOSE OF AIRCRAFT. THE AFT END OF THE AIRCRAFT SETTLED ON A LADDER CAUSING DAMAGE AT THE FOLLOWING LOCATION SKIN DENTED AT STA 1049 STR 27L-27R / DENT DAMAGE AT BS 1049 STR 27L TO 27R FOUND TO BE OUT OSDR DALA2019042392577Skin · crackedINITIAL INSPECTION: CRACK ON FUSELAGE SKIN ON AFT NLG DOOR AFT HINGE RH SIDE. FUSELAGE SKIN ON AFT RH NLG DOOR AFT HINGE, WAS REPAIRED (AS PERMANENT REPAIR) PER VOL I SRM 53- 30-01 FIG 17. (LP# 1036617)SDR DALA2019042392576Skin · crackedINITIAL INSPECTION: CRACK ON FUSELAGE SKIN STA. Y=1437 AND BTW LONGERONS 12RH AND 13RH. SUMMARY OF NRC 00058 FUSELAGE SKIN STA Y=1437 AND BTW LONGERONS 12RH AND 13RH WAS REPAIRED (AS PERMANENT REPAIR) PER ER/A 577191-14 REV ORIGINAL AND ETI-90-19-015 REV 2.SDR CALA2019041900614Skin · crackedROTO PROBE INSPECTION SHOWS CRACK INDICATIO N AT FUSELAGE SKIN FR35, STR 30, RH SIDE, LOWER AFT HOLE INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-02126. DTA DIP INITIATED TO ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE 10 OCT 1 9. PLANNING TO CONTACT ENGINEESDR CALA2019041900606Skin · corrodedL2 PAX DOOR SILL UPPER SKIN SURFACE IB AND OB SIDES FRAME 68 STR 23LH HAS CORROSION A3NB-53-3-6299 GENERATED BY V061595 ON HAECO LCQ NR 9298559 REMOVED AND REPLACED L2 DOOR SILL IAW A320 SRM 51-72-11-911-001 PERFORMED BY MECH V915153 RII INSP BY N078625SDR SWAA2022030727395Skin · corrodedAFT CARGO DOOR SURROUND STRUCTURE EXTERNAL SKIN BELOW CUTOUT HAS CORROSION AROUND FASTENER HOLES STA 797-842 RBL 27 / BLENDED AND REMOVED CORROSION AT AFT CARGO DOOR SURROUND EXTERNAL SKIN BELOW CUTOUT AROUND FASTENER HOLES ORG T .080' MAX MATERIAL LOSS OF .00SDR SWAA2022030742444Skin · dentedTRANSFERED FROM LOG BOOK #0901149. BAGGAGE CART DAMAGED LOWER LEFT AFT FUSELAGE. ONE DENT AT 727:PLUS 3' AND 5' ABOVE 26L TO CENTER OF DENT; MEASURES 9' VERTICAL AND 5'HORIZ; .130 DEEP 2ND DENT AT 727:PLUS 3.5' AND 4' ABOVE 27L TO CENTER OF DENT; MEASURES APPX
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