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 IXXA20170320188Skin · corrodedSKIN BETWEEN STRINGERS 36 - 37R CORRODED AT BS 1170-1175. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-01-2R-12.SDR IXXA20170320185Skin · corrodedAFT LOWER CARGO BS 1175-1197 STRINGER 36R TO 37R SKIN CORRODED. REMOVED DAMAGE AREA AND REPAIRED IAW SRM 53-00-01-2R-12.SDR COEA2017020224913Skin Panel · corrodedHEAVY CHECK COE/MAJOR REPAIR: LT LOWER SKIN PANEL HAS LEVEL 2 CORROSION AT STRINGER 17, SKIN LAP BETWEEN FRAMES 24-25. REPAIRED PER SRAS CETS-588/17...11141 DATED 2/16/2017.SDR SIMA20170202002Skin · crackedRT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 AND ABOVE STRINGER 2R, CRACK IS APPROX 3/8" LONG ENDS MARKED. PERFORMED REPAIR TO RT UPPER FUSELAGE SKIN AFT OF FR 75 AND ABOVE STRINGER 2R IAW SRM 53-31-01 AND ETN-EM-51-40-02.SDR SIMA20170202001Skin · dentedLT RFII SKIN DENT BTW FR 78-79 AND STR 5L-6L. ACCOMPLISHED PERMANENT REPAIR DOUBLER FOR LT RFII SKIN DENT BTW FR 78-79 AND STR 5L-6L IAW ERS-EM-53MR-2572.SDR CALA2017020300230Skin · corrodedCORROSION ON SKIN AT DRAIN HOLE AT BS 727J BETWEEN STRINGERS 26 - 27L. REPAIRED IAW ECRA 5330-05932 REV ORIGAL STEP 18.SDR DALA2017020300899Skin · nickedNICK ON FWD LWR EDGE LT WINDOW BELT. THE NICKS BS 658 - 714 WERE BLENDED AND FOUND WITHIN LIMITS IAW SRM 53-05, FIGURE 111, 51-10-3 PARAGRAPH 21 AND ERA 554135-14 REV. ORIGINAL.SDR DALA2017020300898Skin · nickedNICK ON FWD LOWER EDGE LT WINDOW BELT IAW ER/A 554127-14 REV,ORIG. THE NICKS WERE BLENDED AND FOUND WITHIN LIMITS IAW SRM 53-05, FIGURE 111, 51-10-3 PARAGRAPH 21, AND ER/A. 554136-14 REV. ORIGINAL,SDR DALA2017020300881Skin · crackedTAIL SKIN HAS A CRACK BETWEEN TWO RIVETS AT BS 1437, LONGERON 4 & 5L. REPAIRED IAW PRI 554872-14 REV 0RIGINAL AND COMPLIED WITH ERA 554872-14 REV ORIGINAL.SDR ASOA201702020046Skin · crackedDURING C-CK. FUSELAGE SKIN CRACK AT FR 75 BTW STR 2L-3L. REPAIRED FUSELAGE SKIN IAW SRM 53-31-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201702026003Skin · crackedDURING C-CK. FUSELAGE SKIN CRACK AT FR 75 STR 1R. REPAIRED FUSELAGE SKIN IAW SRM 53-31-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SWIA201743083Skin · dentedMULTIPLE DENTS ON THE LT FUSELAGE 12 TO 14 INCHES AFT OF ICE DETECTOR. PERFORMED REPAIR TO FUSELAGE SKIN BETWEEN BS 235 AND 265, STRINGER 16L IAW REO.SDR SCNA20170201047Panel · damagedLEFT WING PANEL 551BT HAS EXPOSED COMPOSITE. REPAIRED THE WING PANEL.SDR SCNA20170201045Skin · damagedPANEL 192HR HAS EXPOSED COMPOSITE. REPAIRED PANEL 192HR.SDR SCNA20170201044Skin · damagedPANEL 192AR HAS EXPOSED COMPOSITE. REPAIRED PANEL 192AR.SDR SCNA20170201043Skin · damagedPANEL 192HL HAS EXPOSED COMPOSITE. REPAIRED PANEL 192HL.SDR DALA2017020200913Skin · corrodedCORROSION INTERNAL SKIN ON BILGE AREA IN THE AFT CARGO BAY, BS 1500 - 1520 BETWEEN STRINGERS 27 TO 28L. REPAIRED IAW SRM 53-00-01 REPAIR 2.SDR DALA2017020200870Skin · nickedFUSELAGE, NICKS ON AFT LWR EDGE LT WINDOW BELT STA Y=748. REF ERA 554116-14 REV ORIG SEC II.SDR DALA2017020200859Doubler · crackedAFT ACCESSORY COMPARTMENT, CRACKED DOUBLER ON STA Y= 1463 CAT BTW LONG 17L TO 18L. DOUBLER ON STA Y= 1463 CAT BTW LONG 17L TO 18L WAS REPAIRED PER SRM 53-01 FIG 2 (SHEET 4).SDR DALA2019050602820Skin · damagedRT FRACTAL ANTENNE LOCATED 1 ROW FWD OF DWG LOCATION, REPAIR PER ER/A 554888-14 SECTION 1.SDR IXXA20170320190Bear Strap · corrodedAFTER REMOVING THE FORWARD LOWER CORNER SEAL DEPRESSOR ON THE FORWARD LOWER CARGO DOOR, FOUND CORROSION ON THE BEAR STRAP COMMON TO THE SEAL DEPRESSOR. BLENDED CORROSION IAW SRM 53-00-15. BLEND WAS OUT OF LIMITS. REPAIRED IAW ENGINEERING DOCUMENT 47224REA12 RSDR IPXA2017022514412Skin · damagedINSPECTION TYPE: 3C, CHAFE DAMAGE IN FUSELAGE EXTERIOR SKIN, BS 1170, LONGERON 44R. REPAIRED THE SKIN IAW EA 011-5330-01-A6626 REV. IR AND EO MD11-5330-63375-A.SDR IPXA2017022714453Skin · damagedINSPECTION TYPE: 3C, EXTERIOR FUSELAGE SKIN CHAFED NEAR BS 1150, LONGERON 44L. REPAIRED THE SKIN IAW EA 011-5330-01-A6625 REV. IR AND EO MD11-5330-63382-A.SDR CALA2017020300222Skin · dentedON WALK AROUND, CAPTAIN REPORTED TWO DENTS AFT OF THE L1 DOOR NEAR THE STATIC PORTS REF ECRA 5331-02150 PART 1. INSTALLED INTERIM REPAIR.SDR DALA2017020100912Skin · dentedDENTS ON FUSELAGE SKIN AT BS 642, 645, AND 648, BETWEEN STRINGERS 17 AND 18L AND BS 649 BETWEEN STRINGERS 18 AND 19L. REPAIRED IAW SRM 53-00-01 REPAIR 3 FIG 201.SDR DALA2017020200842Skin · nickedNICK ON EXTERIOR SKIN BS 480 - 500, S45R. CUT OUT THE DAMAGE AREA IAW SRM 53-00-01, REPAIR 1. INSTALL THE REPAIR IAW SRM 51-20-05.SDR AALA20170131036Doubler · crackedAIRCRAFT IN BASE MAINTENANCE. CRACK ON RIGHT HAND FORWARD DOUBLER BETWEEN STRINGER 1R AND 2R. INSTALLED SKIN DOUBLER PER SRM 53-05-00-001 AND EA 267054.SDR 7C7A2017013100276Skin · dentedDENT ON LT FUSELAGE SKIN AT BS 282 AND STRINGER 13P.SDR DALA2018092705775Skin · dented(AIRCRAFT 5646, L/P 2870917) WHILE IN C CHECK IN ATL, MTC WAS ASKED TO DISPOSITION A DENT THAT HAD BEEN PREVIOUSLY DISPOSITIONED PER THE SRM AND TRACKED BY LOG PAGE 8841850. UPON FINDING THE DAMAGE, MTC FOUND A SECOND DENT OUTSIDE OF PERMANENT ALLOWABLE LIMITSSDR IXXA20170320193Skin · corrodedCORROSION ON STRINGER 29R AND ON THE INTERIOR SKIN BS 1085. BLENDED THE CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-01, FIGURE 101. REMOVED AND REPLACED UPPER AND LOWER SHEAR TIE IAW SRM 51-40-02 SECTION 7.SDR WVER2017020592802Skin · chafedEXTERNAL FUSELAGE SKIN HAS DAMAGE ON EXISTING REPAIR LOCATED 6" FWD OF FS 927 ON STR 27.SDR DALA2017013100911Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN BS 377, STRINGER 21. ACCOMPLISHED PERMANENT REPAIR IAW ER/A 554303-14 REV ORIG.SDR DALA2017013100760Skin · damagedELONGATED HOLES IN FUSELAGE SKIN BS 947 LONGERON 26L. THE DAMAGE WAS REPAIRED IAW ERA 554117-14, REV ORIGINAL, SECTION II.SDR DALA2018122317356Skin · dentedFOUND DENT DURING WALK AROUND, PERMANENT REPAIR ON EXTERNAL SKIN FUSELAGE BTW FR.1 TO FR.2 AND 24" INCH BELOW WINDOW LH SIDE AS PER A319 SRM 53-00-11-300-029SDR SWIA201743062Skin · dentedTWO DENTS ON FUSELAGE SKIN BETWEEN BS 421 - 453, STRINGERS 16 - 21L. REPAIRED THE SKIN IAW REO.SDR ASOA201701291114Skin · chafedFUSELAGE EXTERNAL SKIN CHAFED AT STRINGER 27 BETWEEN FS 969 - 1000, (3) AREAS TOTAL. REPAIRED DAMAGED AREA REPAIRED IAW REO 670-53-00-290 REV D, DATED 09/10/2015 AND EC/TC REO 670-53-00-290.SDR 2017F00124Skin · gougedTHE LT SIDE OF THE FUSELAGE HAS SEVERAL GOUGES. DAMAGE IS LOCATED AT BS 253.4 ABOVE STRINGER WL 104.8. ACCOMPLISHED MAJOR REPAIR IAW AQRD ERO 880379.SDR DALA2017013000806Skin · corrodedDURING REMOVAL OF VHF3 ANTENNA, FOUND CORROSION ON FUSELAGE SKIN BS 1460 & 1480 AND STRINGERS 29 & 30R, UNDERNEATH OF VHF3 ANTENNA. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01 ALLOWABLE DAMAGE 1 DETAIL II FIG 101 AND DWG 146N3531. REPASDR CALA2017012900186Skin · dentedFOUND DENT IN CROWN ABOVE R3 WINDOW RIGHT OF CENTERLINE. REPAIRED DENT IN ACCORDANCE WITH ECRA 5330-5908 SEE HANGER N/R 5850867 FOR ALL WORKED PREFORMED, SEE LOG PAGE 3951924 FOR DIP CREATED FOR PERMANENT REPAIR. ALL WORK PERFORMED ON ECRA 5330-05908SDR DXTR2017012801Skin · gougedTHE LT SIDE OF THE FUSELAGE HAS SEVERAL GOUGES. DAMAGE IS LOCATED AT FS 253.4 JUST ABOVE STRINGER WL 104.8. ACCOMPLISHED MAJOR REPAIR IAW AQRD ERO-880379.SDR F3LA2017021500081Skin · corrodedAFT RIGHT FUSELAGE LAVATORY BACKING SYSTEM EXHAUST VENT SKIN CUT-OUT SEPERATING AND CORRODED JUST FORWARD OF FRAME 70. REPAIRED THE SKIN.SDR DALA2017012800727Skin · crackedDURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON THE FUSELAGE SKIN, DOUBLER AND TRIPLER REPAIR BTW BS 161.5 - 188.25 AND LONGERONS 11 TO 14R.SDR DALA2017012800704Skin Panel · damagedLIGHTNING STRIKE DAMAGE ON WINDOW PANEL 15R. REMOVED WINDOW PANEL PER SRM 51-40-02. PREPARED NEW PANEL FOR INSTALLATION PER SRM 51-40-02 AND 51-40-08. INSTALLED NEW PANEL PER SRM 51-40-02. RII COMPLIED WITH.SDR CALA2017012900185Skin · dentedDENT OF FUSELAGE SKIN AT STA 807 S-23L LOCATED UNDER EXISTING DOUBLER ON LAP SEAM. REPAIRED PER EC/RA 5330-05913, PART 1.SDR EE4Y201701272294Skin · crackedFUSELAGE SKIN BETWEEN 827 AND 887 AND BETWEEN STR 23R AND 27R, SKIN WITH CRACK.SDR UIEA2017020100132Skin · damagedBS 200 STRINGERS 24A TO 26R SKIN ONE FASTENER HOLE FOUND LIGHTNING STRIKE. INSTALLED A FREEZE PLUG REPAIR IAW R1-52-10-11688 REV A.SDR DALA2017012700670Finger Doubler · corrodedAFT CARGO COMPARTMENT, CORROSION WAS FOUND ON FINGER DOUBLER FROM BS 1193 TO 1250 AND LONGERON 26L. THE FINGER DOUBLER WAS FABRICATED IAW DWG 5911423 REV CD, THE FINGER DOUBLER WAS REMOVED AND INSTALLED IAW SRM 51-30-2 AND 51-30-5.SDR U2RA201702220001Skin Panel · dentedDURING "D' CHECK INSPECTION FOUND SCRAPE AND DENT IN FUSELAGE BELLY SKIN AT BODY STATION 820 LEFT OF BUT LINE 2 INCHES BETWEEN STRINGERS 46 LEFT AND 47 RIGHT. REPAIRED DAMAGED FUSELAGE SKIN BY INSTALLING EXTERNAL DOUBLER IN ACCORDANCE WITH SRM 53-00-01 REPAIRSDR COEA2017012540913Skin · corrodedINTERIOR SKIN, FRAMES 8 - 9 INSULATION STANDOFF CORRODED BELOW WINDOW SILL. REPAIRED IAW SRAS ES-576/17.SDR COEA2017012539913Skin · corrodedINTERIOR SKIN, FRAMES 9 - 10 INSULATION STANDOFF CORRODED BELOW WINDOW SILL. REPAIRED IAW SRAS ES-576/17.
Back to JASC 5330