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 DALA2016082606312Skin · crackedON WAKE UP CHECK, FOUND A THREE INCH CRACK WITH CORROSION BUBBLE TWO FEET AFT OF NR 3 VHF ANT CENTER LINE OF BELLEY SKIN. REPAIRED IAW 550141-14.SDR DALA2016082506276Doubler · corrodedCORROSION ON INNER FUSELAGE SKIN DOUBLER, LONGERONS 28 - 29R, BS 205 - 218. DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-02.SDR MTNA20160829002Doubler · corrodedANTENNA DOUBLER AT FRAMES 32 - 33, STRINGER 21, IS CORRODED. DOUBLER REMOVED AND REPLACED IAW SRM 51-25-01SDR C77A20160823003Skin · corrodedCORROSION DAMAGE TO THE CENTER FUSELAGE III LOWER SKIN BETWEEN FRAMES 77-78 AND STRINGER 29L-29R. REPAIRED IAW ETD2016-170-075217.SDR JR2R20160825373Skin · damagedRIGHT FUSELAGE SKIN CREASED BETWEEN FS 605 AND 626, LONGERON 21R. LENGTH IS 21" AND EXTENDS 2.5" OVER THE MID CARGO DOOR CUTOUT UPPER EXTERNAL DOUBLER. ACCOMPLISHED A TEMPORARY REPAIR TO THE RIGHT FUSELAGE SKIN BETWEEN FS 598 TO 630 LONGERONS 20R TO 22R IAW ALSDR ASOA20160824056Skin · crackedDURING C-CHECK, THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND A FASTENER AT FRAME 77 STRINGER 7 - 8R. MAINTENANCE REMOVED THE CRACK AND PERFORMED A BUSHING REPAIR IAW SRM 53-32-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20160824055Skin · crackedDURING C-CHECK, THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS FROM FRAME 77 - 78 AND STRINGERS 4 - 8L. MAINTENANCE REMOVED THE CRACKS AND PERFORMED BUSHING REPAIRS IAW SRM 53-32-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR DALA2016110208149Skin · corrodedSKIN CORRODED AFT OF BS 1002 ABOVE STRINGER 26. BLENDED AREA IAW SRM 53-00-00 FIG 103. FOUND TO BE OUT OF LIMITS. REPAIRED IAW ER/A 54713-14 REV O.SDR SWAA2016091407793Skin Panel · delaminatedLEFT SIDE MAIN WHEEL WELL DELAMINATED AT LOWER FUSELAGE. REPAIRED SKIN PANEL IAW SRM.SDR SWAA2016091407792Skin Panel · delaminatedMAIN WHEEL WELL AT LOWER FUSELAGE FORWARD INBD SKIN PANEL DELAMINATED. REPAIRED SKIN PANEL IAW SRM.SDR SWAA2016091255661Skin · crackedL2 DOOR FUSELAGE SKIN CRACKED AT UPPER HINGE CUTOUT FORWARD EDGE. REPAIRED CUTOUT IAW SRM.SDR ABXA20160823136Skin · corrodedCORROSION FOUND ON INTERNAL LEFT BS 955 FUSELAGE SKIN. REPAIRED THE SKIN. AIRCRAFT WAS GROUNDED.SDR DALA2016082706313Skin · corrodedCORROSION DAMAGE TO FUSELAGE SKIN AT BS 1197+132 BETWEEN STRINGER 39L AND 39R. REPAIRED IAW ERA 550141-14.SDR DALA2016082406184Skin · damagedLIGHTNING STRIKE AT FUSELAGE 200, LONGERON 7L, RT SIDE ON REF LP 0532712. PERMANENT REPAIR WAS PERFORMED IAW SRM 53-04-2, FIG 2. PERFORMED VISUAL INSPECTION ON PERMANENT REPAIR AT INITIAL 8000 FC AND REPETITIVE ENTRY 8000 FC IAW SRM 53-04-2, FIG 2, PAR D.SDR DALA2016082406181Skin · damagedINITIAL: LIGHTING STRIKE ON RT WINDOW BELT AFT LOWER CORNER STA Y=613. ALSO, FWD LOWER CORNER STA Y= 796. LIGHTNING STRIKE ON RT WINDOW BELT STAY=598-617 WAS REPAIRED ER/A 549267-14, REV ORIGINAL SECTION 1 AND MUST BE MONITORED WITH MONITOR 2638502.SDR AALA20160822005Skin · damagedA DENT AND GOUGE ON FUSELAGE SKIN AT BS 870, STRINGER 22R. INSTALLED A REPAIR DOUBLER IAW SRM 53-00-01-2R-3.SDR DALA2016082306153Skin · crackedFUSELAGE SKIN CRACKED BS 1076 STRINGER 14R. REPAIRED THE SKIN IAW ER/A 547505-14.SDR KCSA201608221058Skin · crackedR3 MAIN ENTRY DOOR CUTOUT UPPER AFT CORNER BS 1318 BETWEEN STRINGERS 16 R & 17R HAS A CRACK IN THE SKIN AND BEARSTRAPSDR FDEA201608222948Skin · damagedBIRD STRIKE DENTED THE LT FORWARD FUSELAGE AT STA 148.5, WL 215. DENT MEASURES 6.4" X 3.5" X 0.336". REPAIRED DAMAGE IAW SRM 53-00-01, FIG 201, TABLE 5 WHICH REQUIRES REPETITIVE INSPECTION. CONTACT MOCC AFTER 30K FLT CYCLE INSPECTION TO SET UP 12K FLT CYCLESDR CALA2016082395666Skin · dentedEXTERNAL FUSELAGE SKIN DENTED 2 FT AFT OF THE L2 DOOR. DENT FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE & INSTALLED EXTERNAL DOUBLER IAW SRM 53-41-11.SDR DALA2016082306171Doubler · corrodedCORROSION ON FUSELAGE SKIN DOUBLER BETWEEN LONGERONS 29 AND 30L. FOUND TO BE OUT OF LIMITS. REPLACED THE DOUBLER IAW SRM 51-30-02.SDR DALA2016082206137Skin · damagedLIGHTNING STRIKE ON LT WINDOW BELT BETWEEN STA Y655-674, UPPER AFT CORNER. LIGHTNING STRIKE ON LT WINDOW BELT STA 655-674, AFTER UPPER CORNER WAS REPAIRED IAW ER/A 549237-14, REV ORIGINAL, SRM 51-10-3, PARA 21 AND SRM 53-05, FIG 111.SDR DALA2016082206136Skin · damagedLIGHTNING STRIKE ON LT WINDOW BELT BETWEEN STA Y712-731, FWD AND AFT SECTION. LIGHTNING STRIKE LT WINDOW BELT BETWEEN STA 712-731, AFT/FWD MID SECTION WERE REPAIRED IAW ER/A 549237-14, REV ORIGINAL, SRM 53-05, FIG 111 AND SRM 51-10-3, PARA 21.SDR DALA2016082206135Skin · damagedLIGHTNING STRIKE ON LT WINDOW BELT BETWEEN STA Y=674-Y=693, LOWER AFT CORNER. LIGHTNING STRIKE ON LT WINDOW BELT BETWEEN STA 674-693. AFT LOWER CORNER, WAS REPAIRED IAW ER/A 549237-14, REV ORIGINAL, SRM 53-05, FIG 111 AND SRM 51-10-3 PARA 21.SDR ASMF201610009Skin · damagedCAPTAIN REPORTED A LIGHTNING STRIKE IN THE FUSELAGE SKIN DURING DESCENT. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19, DETECTING SEVERAL LIGHTNING STRIKES ON LEFT WINDOW FRAME NUMBERS 2 AND 3 AT D-F SILL AND E-F, G-H POSTS. INSSDR SWAA2016092308059Skin · crackedL1 DOOR LOWER HINGE CUTOUT CRACKED AT BS 304, STR 13L. REPAIRED CUTOUT IAW ER & EA.SDR FDEA201608203068Doubler · corrodedFOUND A DOUBLER IS CORRODED AT BS 1155, BETWEEN LONGERON 48 - 49R. REMOVED AND REAPLCED THE DOUBLER IAW SRM 51-21-01 AND DWG NAA6064.SDR DALA2016082106226Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN, BS 1494 BETWEEN LONGERON 3L AND 4L. REPAIRED IAW ERA 549236-14, REV O. (LP# 2643887)SDR DALA2016082206148Skin · corrodedAFT CARGO COMPARTMENT BILGE AREA RIGHT SIDE SKIN, BS 1193 - 1200 BETWEEN LONGERONS 29 - 30R CORRODED. REPAIRED IAW PRI/ERA 549063-14.SDR FDEA201608193201Skin · corrodedAFT FUSELAGE WASTE TANK AREA BS 2000 SKIN CORRODED INBD OF LONGERON 43L. IAW SRM 53-20-00 FIG 4 SHEET II VOL I. REMOVED CORROSION FROM SKIN IAW SRM 53-20-00 FIG.4SDR DALA2016082006235Skin · crackedFUSELAGE SKIN CRACKED, BS 1437 ABOVE RIGHT PYLON. REPAIRED IAW PRI/ERA 549946-14.SDR DALA2016082006164Skin · corrodedCORROSION ON INNER FUSELAGE SKIN AT BS 541 LONGERON 30, MID CARGO COMPARTMENT. REPAIRED IAW SRM 53-31-02.SDR A6WA201644246Skin · chafedRIGHT MLG APRON STRUCTURE SKIN OUTER SURFACE GOUGED JUST FWD OF FS 554.SDR IPXA2016082907556Skin · corrodedINSPECTION TYPE: 3C, AFT EXTENDED FUSELAGE SKIN PANEL BELOW LT HORIZONTAL STAB., HSS 2122.881 IS CORRODED AT LONGERON 12L. REPAIRED THE SKIN PANEL IAW EA 011-5330-01-A6415 REV. I/R AND EO MD11-5330-61706-A.SDR SIMA20160818004Skin · crackedRIGHT FUSELAGE SKIN HAS TWO CRACKS AT FRAME 75 AND STRINGER 2R. PERFORMED A PERMANENT REPAIR IAW SRM 53-31-01 FIG 219.SDR 4AER20161017002Skin · corrodedSKIN PANEL FROM BS 727G TO 907 & STRINGER 25L TO 25R HAD CORROSION.SDR SWAA2016091255660Skin · corrodedFORWARD GALLEY DOOR BOTTOM SIDE OF FLOOR STRUCTURE CORRODED AT BS 294.5. R & R SKIN IAW SRM AND DWG.SDR FDEA201608172900Skin · damagedFUSELAGE EXTERIOR SKIN THERE ARE NUMEROUS LIGHTNING STRIKES AT BS 680 - 740 STRINGERS 27 - 28L. COMPLIED WITH EA F-5330-T0327528, PART 1. REPAIR RIVETS AND LIGHTNING DAMAGES ON FUSELAGE SKIN PANEL BETWEEN STA 680-STA 716 AND S-27L-S-28L. REPAIR CLASSIFIED ASDR JR2R08172016175Skin · dentedDENT DAMAGE TO FUSELAGE SKIN LOCATED AT BS 218, TWO INCHES ABOVE LONGERON 18R. REPAIRED SKIN IAW SRM 53-04 FIG. 12C.SDR DALA2017053104391Skin · corrodedCORROSION REPAIR AT STA 208 SKIN AT GALLEY DRAIN. REPAIRED PER ERA 549712-14 SECTION 1 ON 16AUGUST16.SDR ABXA20160816130Skin · corrodedCORROSION FOUND AROUND FASTENER HOLES ON INTERNAL SKIN BS 955. REPAIRED IAW REA B653-62159-MR. THE AIRCRAFT WAS GROUNDED.SDR DALA2016081706140Skin · damagedBLENDOUT AT FUSELAGE SKIN BS 580, STR 22L. REMOVED FASTENERS AT FUSELAGE SKIN BS 580 STR 22L PERFORMED UT INSP ORIGINAL MATERIAL 0.056, MATERIAL LOSS 0.019, MATERIAL REM 0.037, OUT OF LIMITS. CUTOUT DAMAGE, DIM 2.1 X 1.0, FABRICATED DOUBLER, FILLER, AND INSTASDR P5CA2016081700210Skin · damagedLIGHTNING STRIKE AT BS 287 - 340, STRINGERS 14 - 15R SKIN. REPAIRED IAW EI T2016A53M-1652 REV. 1.SDR P5CA2016081800213Skin · corrodedCORROSION ON SKIN BS 1736 STRINGER 44L. REPAIRED IAW EI T2016A53M-1637 REV. 2.SDR VNAA2016081600015Skin · crackedEXTERNAL FUSELAGE SKIN CRACKED AT RIGHT AFT CORNER OF THE NOSE LANDING GEAR WHEEL WELL DOOR CUTOUT AT BS 235, RBL 6.0. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE EXTERNAL FUSELAGE SKIN AT THE NOSE LANDING GEAR WHEEL WELL DOOR CUTOUT’S RIGHT HAND SIDE AFT RADSDR DALA1800573732Skin · crackedBS 540 SKIN SPLICE CRACKED. REPAIRED IAW 5331-01257, SECT 08.SDR DALA2017053104390Skin · corrodedREPAIR OF FUSELAGE SKIN, SURROUND DOUBLER, AFT LAVATORY SERVICE DOOR CUTOUT STATION 1307, L-22L DUE TO CORROSION. REPAIR WAS ACCOMPLISHED PER ERA 549411-14 SECTION 1 ON 15AUG16.SDR DALA2016081606037Skin · crackedCRACK ON EXTERNAL FUSELAGE STA 1133 BETWEEN LONGERON 2-3 RT, CARD 14, ZONE 200. REPAIR WAS ACCOMPLISHED IAW ER/A 547895-14 AD REV ORIGINAL. LENGTH CRACK 0.150". REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE ONLY. ADDITIONAL ER/A REV WITH AMOC IS REQUIRED SDR DALA2016081606036Skin · crackedCRACK ON EXTERNAL FUSELAGE STA 1133 BETWEEN LONGERON 2-3 LT, CARD 13, ZONE 200. REPAIR WAS ACCOMPLISHED IAW ER/A 547895-14, REV ORIGINAL. LENGTH CRACK 0.200". REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE ONLY. ADDITIONAL ER/A REVISION WITH AMOC IS REQUIRSDR FOTR20160815001Skin · damagedLOWER FUSELAGE SKIN BS 1180 - 1400 FROM STRINGER 26L TO 26R DAMAGED. REMOVED AND REPLACED SKIN IAW EA 16230 REV. IR.
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