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.

SDR DALA2015062804014Skin · crackedCRACKED FUSELAGE SKIN UNDER REMOVED DOUBLER AT AFT ACCESSORY COMPARTMENT, BS 1406 BETWEEN LONGERONS 1-2R. DAMAGE WAS REPAIRED WITH ER/A 534412-14AD, REV ORIG.Jun 27, 2015 · N981DL · Doug MD88SDR SWAA2015070841508Skin · crackedSKIN CRACKED BETWEEN BS 375.75 - 376.50, STRINGER 8L. REPAIRED SKIN IAW EA.Jun 26, 2015 · N355SW · Boeing 7373H4SDR UHLA201506260543Skin · crackedDURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 AND STRINGER 2L. THE SKIN WAS REPAIRED IAW ETD 2015-145-059490.Jun 26, 2015 · N567RP · Emb EMB145LRSDR SWAA2015070841477Skin · crackedSKIN CRACKED AT BS 362, STRINGER 1L. REPAIRED SKIN IAW SRM.Jun 26, 2015 · N355SW · Boeing 7373H4SDR AALA20150626024Skin · crackedVISUAL INDICATION OF CRACK IN FUSELAGE SKIN AT FASTENER HOLE LOCATION STATION 1418, JUST OTBD OF LONGERON 2R. INSTALLED REPAIR DOUBLER IAW SRM 53-04-00 FIGURE 40 & EA 252259.Jun 26, 2015 · N969TW · Doug DC983SDR SIMA20150626006Skin · crackedDURING INSPECTION, QA FOUND 2 CRACKS ON RT REAR FUSELAGE I SKIN AT FRAME 75 BELOW STRINGER 2R. ACFT WAS REMOVED FROM SERVICE FOR INSPECTION & WILL BE RETURNED TO SERVICE AFTER INSPECTION. PERFORMED PERMANENT REPAIR ON CRACKS ON RT REAR FUSELAGE I SKIN AT FRAJun 26, 2015 · N623AE · Emb EMB145LRSDR SIMA20150626005Skin · crackedDURING INSPECTION, QA FOUND 2 CRACKS ON LT REAR FUSELAGE I SKIN AT FRAME 75 ABOVE AND BELOW STRINGER 2L. ACFT WAS REMOVED FROM SERVICE FOR INSPECTION & WILL BE RETURNED TO SERVICE AFTER INSPECTION. PERFORMED PERMANENT REPAIR ON CRACKS ON LT REAR FUSELAGE I SKJun 26, 2015 · N623AE · Emb EMB145LRSDR DALA2015062704012Doubler · corrodedCORROSION ON PRODUCTION DOUBLER BS 579 BETWEEN LONGERON 28 - 29L. AREA WAS REPAIRED IAW ER/A 536442-14, REV ORIGINAL.Jun 26, 2015 · N981DL · Doug MD88SDR FDEA201506262061Repair · gougedFUSELAGE EXISTING REPAIR FINDING. THE REPAIR AT BS 540 - 640 FROM STRINGER 24 RT TO 28 LT. THE DOUBLER HAS NUMEROUS SCRATCHES TOOL MARKS & GOUGES. EXISTING QUADRUPLER REPAIR AT NR 1 FWD CARGO DOOR CUT-OUT-REPAIR. REPAIR CLASSIFIED AS MAJORJun 26, 2015 · N772FD · Boeing 757222SDR FDEA201506262059Repair · damagedFUSELAGE EXISTING REPAIR FINDING. THE REPAIR AT BS 540 - 640 FROM STRINGER 24 RT TO 28 LT. THE STRUCTURE FILLER HAS NUMEROUS SCRATCHES TOOL MARKS & GOUGES. EXISTING QUADRUPLER REPAIR AT NR 1 FWD CARGO DOOR CUT-OUT-REPAIR. REPAIR CLASSIFIED AS MAJORJun 26, 2015 · N772FD · Boeing 757222SDR FDEA201506262058Repair · gougedFUSELAGE EXISTING REPAIR FINDING. THE REPAIR AT BS 540 - 640 FROM STRINGER 24 RT TO 28 LT. THE TRIPLER HAS NUMEROUS SCRATCHES TOOL MARKS & GOUGES. QUADRUPLER REPAIR AT NR 1 FWD CARGO FOOR CUT-OUT - REPAIR. REPAIR CLASSIFIED AS MAJORJun 26, 2015 · N772FD · Boeing 757222SDR FDEA201506262057Repair · damagedFUSELAGE EXISTING REPAIR FINDING, THE REPAIR AT BS 540 - 640 FROM STRINGER 24 RT TO 28 LT. THE QUADRUPLER HAS NUMEROUS SCRATCHES, TOOL MARKS & GOUGES. QUADRUPLER REPAIR AT NR 1 FWD CARGO DOOR CUT-OUT-REPAIR. REPAIR CLASSIFIED AS MAJORJun 26, 2015 · N772FD · Boeing 757222SDR REXA2015062900124Skin · dentedMAINTENANCE WAS TASKED WITH PERMANENT REPAIR OF MULTIPLE DENTS IN THE AFT FUSELAGE SKIN BETWEEN FS 755.00 & 67.50% & BETWEEN STRINGERS S23L & 24R. THE DAMAGES MEASURE A MAXIMUM OF 4.00” DIA X .050” DEEP. REPAIRED IAW EA CRJ253-03514.Jun 26, 2015 · N835AY · Cndair CL6002B19SDR AALA20150626011Skin · crackedCRACKS AT FS 1474 RT CANT. INSTALLED DOUBLER REPAIR IAW SRM 53-01-00-001 FIG 2 SHEET 3.Jun 26, 2015 · N969TW · Doug DC983SDR FOTR20150725057Skin · scratchedFUSELAGE HAS SCRATCHED AREA BS 670-680, STRINGERS 23R AND 24R. REPAIRED ON FAS NR40673 W/O N293DH-01-02.Jun 25, 2015 · N293DH · Boeing 7572Q8SDR SWAA2015072342163Skin · crackedSKIN CRACKED AT BS 540, BETWEEN STRINGER 22L - 23L AT 3 & 9 O'CLOCK. REPAIRED SKIN IAW EO & EA.Jun 25, 2015 · N443WN · Boeing 7377H4SDR COEA2015062502900Skin · dentedHEAVY CHECK COE & MAJOR REPAIR. REAR FUSELAGE LT LOWER LATERAL SKIN DENTED AFT OF REAR ENTRY DOOR FROM CONTACT WITH SHOOT BOLT AT LEVEL OF STRINGER 12L. REPAIRED BY SRAS CE-3803 15 9427 DATED 7 15 15.Jun 25, 2015 · N900FX · Aerosp ATR42320SDR ASAA2015062512279Skin · damagedLOWER FUSELAGE AFT OF AFT CARGO DOOR INBD, LIGHTNING STRIKE DAMAGE MARK DOTTED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AND BEAR STRAP AT BS 847 BETWEEN S26R AND S27R OVERSIZED HOLE IAW EA 900ER-53EA-15350, REV NEW DATED 07/01/2015.Jun 25, 2015 · N462AS · Boeing 737990ERSDR FDEA201506252021Skin · damagedEXTERIOR SKIN, HAS AN OVERSIZE HOLE BETWEEN BS 1600 - 1620, STRINGERS 26 - 27R. REPAIRED IAW EA F-5310-T0316044. MAJOR REPAIR.Jun 25, 2015 · N772FD · Boeing 757222SDR FDEA201506252042Skin · corrodedAFT PIT BULKHEAD LOWER CHORD SKIN CORRODED AT STATION 1720, STRINGER 28L. AREA AT FUSELAGE WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-80-08-1A FIG 101 DETAIL IX. COMPLIED WITH EA F5300-T0317468 PART 1. CAT A REPAIR, MAJOR REPAIR.Jun 25, 2015 · N776FD · Boeing 757222SDR SIMA20150625003Skin · crackedRIGHT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2R, CRACK IS APPROX 3/8" IN LENGTH. FREQ=400KHZ, V-GAIN=76.0, H-GAIN=64.0, LPF=100, 50-500KHZ PROBE. ACCOMPLISHED REPAIR TO RT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE Jun 25, 2015 · N633AE · Emb EMB145LRSDR SIMA20150625004Skin · crackedRIGHT UPPER FUSELAGE SKIN CRACKED JUST ON FRAME 75 AT FIRST FASTENER BELOW STRINGER 2R, CRACK IS APPROX 3/8" IN LENGTH. USED FREQ=400KHZ, V-GAIN=76.0, H-GAIN=64.0, LPF=100, 50-500KHZ PROBE. ACCOMPLISHED REPAIR TO RT UPPER FUSELAGE SKIN CRACKED JUST ON FRAME Jun 25, 2015 · N633AE · Emb EMB145LRSDR FXGA201506251527Skin · tornTORN SKIN AT CARGO DOOR FWD FRAME FS 501.5, BETWEEN STRINGER 17L & 18L. TO REPAIR A TORN SKIN AT FWD EDGE OF A MAIN CARGO DOOR. REPAIR DAMAGED SKIN IAW C46 SRM AN 01-25LA-3 FIGURE 24.Jun 25, 2015 · N1822M · Curtis C46*SDR DALA2015062603968Skin · dentedTWO DENTS BETWEEN STRINGERS 17 & 18L BS 229. CUT OUT THE DAMAGE IAW SRM 53-04-3, FIG 2, SHT 5. DRILLED A REPAIR DOUBLER IAW SRM 53-04-3, FIG 2, SHT 5. INSTALLED REPAIR DOUBLER IAW SRM 53-04-3, FIG 2Jun 25, 2015 · N959DL · Doug MD88SDR AALA20150625009Skin · crackedCRACK IN FUSELAGE SKIN AT NOSE GEAR RT STRUT DOOR HINGE CUT OUT. STOP DRILLED CRACK IAW SRM 53-05-00-001. INSTALLED DOUBLER IAW SRM 53-05-00-001.Jun 25, 2015 · N969TW · Doug DC983SDR DALA2015062503976Skin · crackedFOUND CRACK ON FUSELAGE SKIN, LT SIDE, BS 1531. REPAIRED IAW SRM 53-00-01.Jun 24, 2015 · N908DA · Doug MD9030SDR DALA2015062503957Skin · crackedCRACKED INNER FUSELAGE SKIN JUST FWD OF CANTED FRAME, STA 1463 AND PROYECTION LONG 2R AT AFT ACCESSORY COMPARTMENT, RII: N ENTR 797732 W, SKIN DAMAGE WAS REPAIRED IAW ER/A 536423-14, REV ORIGINAL PERFORM A GENERAL VISUAL INSPECTION OF THE REPAIR WITHIN EVERY Jun 24, 2015 · N981DL · Doug MD88SDR DALA2015062503956Skin · damagedLIGHTNING STRIKES ON RT WINDOW BELT BETWEEN BS 636-655 FWD EDGE AND AFT UPPER CORNER. THE WINDOW BELT WAS REPAIRED IAW ER/A 536435-14, REV ORIGINAL.Jun 24, 2015 · N981DL · Doug MD88SDR DALA2015062403945Skin · damagedWEAR ON FUSELAGE SKIN REPAIR DOUBLER BETWEEN STA Y=1300-1309 AND LONGERON 18 RT TO 20 RT. PREVIOUS REPAIR DOUBLER WAS REMOVED AND NEW EXTERNAL DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04-2, FIG 2, SHEET 9 AND 51-30-2 SET UP A DECAL CONDITION MONITOR A1Jun 24, 2015 · N984DL · Doug MD88SDR SWAA2015071041778Skin · crackedLEFT BULKHEAD CHORD SKIN CRACKED AT BS 540, STRINGER 22L, AFT FASTENER ROW 2ND FASTENER HOLE. REPAIRED SKIN IAW EA.Jun 23, 2015 · N221WN · Boeing 7377H4SDR SIMA20150623006Skin · crackedRIGHT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 1R & 3R. PERFORMED PERMANENT REPAIR OF RT REAR FUSELAGE I SKIN IAW ERS-EM-53MR-1406.Jun 23, 2015 · N612AE · Emb EMB145LRSDR DALA2015062403939Skin · scratchedSCRATCHES ON RT WINDOW BELT, BS 750-769, LWR EDGE. REPAIRED.Jun 23, 2015 · N981DL · Doug MD88SDR WVER0623201500014Skin · not reportedPERFORMED MAJOR REPAIR TO FUSELAGE SKIN BETWEEN BS 453 - 469 AND BETWEEN STR 9L AND 10L IAW REO 690-53-21-754.Jun 23, 2015 · N931LR · Cndair CL6002D24SDR SWAA2015080342413Bear Strap · crackedFORWARD CARGO BAY DOOR CUT OUT, BEAR STRAP INBOARD EDGE CRACKED AT LOWER FORWARD CORNER, 4" UP FROM LOWER DOOR CUT OUT EDGE. REPAIRED BEAR STRAP IAW ER & EA.Jun 22, 2015 · N380SW · Boeing 7373H4SDR SWAA2015072442190Skin · crackedFUSELAGE SKIN CRACKED AT LT CORNER OF AIR CONDITIONING GND SERVICE DOOR CUT OUT. REPAIRED SKIN IAW SRM.Jun 22, 2015 · N380SW · Boeing 7373H4SDR DALA2015062403944Skin · damagedLIGHTNING STRIKES ON RT WINDOW BELT STA Y=731-750, AFT UPPER CORNER. RT WINDOW BELT STA Y= 731-750 WAS REPAIRED IAW ETI-88-15-192, REV 1 AND ER/A 536436-14AD, REV ORIGINAL PERFORM HFEC INSPECTION EVERY 24 MONTHS IAW ERA 536436-14AD. RII COMPLETED.Jun 22, 2015 · N981DL · Doug MD88SDR XE4R2015FA0000331Skin · crackedDURING A DAILY CHECK, TWO CRACKS WERE DISCOVERED ON THE SKIN PANEL AROUND THE AFT LAVATORY VENT OUTLET BOTTOM EDGE, DIRECTLY ABOVE STR 32 RT BETWEEN FRAME 69-FRAME 70. THE CRACKS EXTENDED .40" AND .60" FROM THE LOWER OPENING OF THE AFT LAV VENT. DURING EVALUJun 21, 2015 · N624VA · Airbus A320214SDR SCNA20150626116Skin · dentedFUSELAGE DENT AFT OF L1 DOOR AT THE BEGINNING OF THE RVSM AREA AT BS 374 BETWEEN STR15 - 16L. PERMANENT REPAIR ACCOMPLISHED.Jun 21, 2015 · N821SY · Boeing 7378FHSDR FDEA201506211951Skin · dentedLEFT SIDE EXTERNAL FUSELAGE SKIN HAS DENT OUT ON FRAME 79, STRINGER 29L - 30L. EVALUATED DENT IAW SRM 53-18-12 & SRM 53-10-12 FIG 102 DIAGRAM 103 D, 0.020" A:0.00 DENT IS OUT OF LIMITS. REPAIRED SKIN SECTION IAW SRM 53-10-12 FIG 208. CLASSIFIED AS MAJOR CATJun 21, 2015 · N651FE · Airbus A300F4605RSDR V0XD20150621144Skin · damagedDAMAGE UNDER AFT BAGGAGE BAY DOOR AT FS 1015 BETWEEN STRINGER 20L & 21L. CUT OUT DAMAGED AREA OF SKIN, CUT OUT DAMAGED STRINGER 19L FROM FS 985.00 TO 1038.00. CUT OUT DAMAGED FRAME AT FS 1015.00 FROM STRINGER 19L TO 22L. REPLACED STRINGER 19L, PN MM 670-351Jun 21, 2015 · N169GJ · Cndair CL6002C10SDR SWAA2015082443151Skin · crackedFUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA & ER.Jun 20, 2015 · N7834A · Boeing 737752SDR SIMA20150620007Skin · crackedLEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L, CRACK IS APPROX 3/4" IN LENGTH. EASI 8071 USED. FREQ=400KHZ, V-GAIN=76.0, H-GAIN=64.0, LPF=100, 50-500KHZ PROBE. ACCOMPLISHED REPAIR TO LT UPPER FUSELAGE SKIN JUST AFT OF FRAME 75 & Jun 20, 2015 · N633AE · Emb EMB145LRSDR DALA2015062203931Skin · damagedLIGHTNING STRIKE ON LT FUSELAGE WINDOW BELT AFT EDGE BETWEEN BS Y=408 TO Y=427. LIGHTNING STRIKE ON LT FUSELAGE WINDOW BELT AFT EDGE BETWEEN BS Y=408 TO Y=427 WERE REPAIRED IAW ERA 536438-14, REV. ORIGINAL. ORIGINAL THICKNESS 0.086". REMAINING THICKNESS 0.0Jun 20, 2015 · N981DL · Doug MD88SDR FDEA201506201930Skin · dentedPROTRUDING DENT STATION 523 AT STRINGER 26L. COMPLIED WITH EA F-5330-TO318148 PART 1 FUSELAGE PLATES & SKIN. REPAIR AT STATION 523 BETWEEN STRINGERS 26L - 27L.Jun 20, 2015 · N970FD · Boeing 75728ASDR FDEA201506201929Skin · dentedTWO EACH DENTS STATION 490 BELOW 27L. COMPLIED WITH EA F-5330-TO318149 PART 1 FUSELAGE PLATES & SKINS. REPAIR AT STATION 490 BETWEEN STRINGERS 27L - 28L.Jun 20, 2015 · N970FD · Boeing 75728ASDR DALA2015062203892Skin · damagedLIGHTNING STRIKES ON RT WINDOW BELT BETWEEN STA Y= 655-674 FWD WAS REPAIRED ON UPPER CORNER: WITH DIMENTIONS AS FOLLOWS (UT) WAS ACCOMPLISHED IAW NDT-SPM PART 4, 04-00-078 PAR 5 FIG 3, STA Y=655-674 RT, PLACE FWD UPPER CORNER, ORIGINAL THICKNESS 0.120, REMAINIJun 20, 2015 · N981DL · Doug MD88SDR SWAA2015071041720Skin · corrodedKEEL BEAM SKIN ASSEMBLY CORRODED BETWEEN BS 607 TO 630, BETWEEN LBL 6.30 - RBL 6.30. REPAIRED SKIN IAW EO & EA.Jun 19, 2015 · N615SW · Boeing 7373H4SDR SIMA20150619005Skin · chafedFUSELAGE SKIN INSIDE 424DB IS CHAFED. REPAIRED FUSELAGE SKIN CHAFE INSIDE 424DB IAW ERS-EM-53MR-1398.Jun 19, 2015 · N612AE · Emb EMB145LRSDR DALA2015062203932Skin · damagedLIGHTNING STRIKE ON FUSELAGE WINDOW BELT AFT UPPER CORNER BETWEEN BS Y=560 TO Y=579 AND STA Y=579 TO Y=598. LIGHTNING STIKE ON FUSELAGE WINDOW BELT AFT UPPER CORNER BS Y= 579 TO Y=598 IN REF. CARD 19, ZONE 100 WERE REPAIRED IAW ER/A 536451-14, REV ORIGINAL, WJun 19, 2015 · N981DL · Doug MD88SDR WVER0619201593112Skin · gougedBL 0, BS 910, GOUGE IN SKIN. REPAIRED IAW REO'S 670-53-00-290 AND 690-53-00-294.Jun 19, 2015 · N931LR · Cndair CL6002D24
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