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 DALA2016110608288Rub Strip · corrodedCORROSION ON RT FUSELAGE SKIN SETTLEMENT AREA OF RUBSTRIPS OF STA Y:1080 BTW LONGS 30 TO 29R. CORROSION WAS REMOVED ON RT FUSELAGE SKIN SETTLEMENT AREA OF RUBSTRIPS OF STA Y:1080 BTW LONGS 30 TO 29R PER SRM 51-10-3 PAR 26. ORIGINAL THICKNESS IS 0.160 AND REMSDR ASOA20161105103Skin Panel · crackedLT SKIN CRACKED AT FWD HYD COMPT CUTOUT AT FS 187.00 STR 15L. REMOVED AND REPLACED SKIN PANEL AT FS 187.00 STR 15L PER SRM 51-42-06, 51-40-11-00,51-42-13 P/N 600-33052-145, DRAWING 600-33052. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR CALA2016110700860Skin · crackedFUSELAGE SKIN CRACKED STA 540, BETWEEN S-22R AND S-23R. SECOND FASTENER FROM TOP, AFT FASTENER. REFERENCE EA5310-05878 REV D CUTOUT CRACK FROM SKIN, FABRICATED REPAIR PARTS AND INSTALLED REF EA5310-05878 REV D OP5.SDR DALA2016110710245Skin · puncturedPUNCTURE AT FS 1773 BTWN S36 & S32 LT 53-00-01 REPAIR.SDR R61A20161114063Doubler · corrodedCORROSION INTERNAL DOUBLER ON BELLY PANEL 192CR. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-41-02.SDR SWAA2016111009562Skin · crackedSKIN CRACKED AT BS 440+2, STRINGER 3R. REPAIRED THE SKIN IAW EA.SDR DALA2016110408245Skin · corrodedCORROSION FOUND ON RT FUSELAGE SKIN SETTLEMENT AREA OF RUBSTRIPS BS 1080 BETWEEN LONGERONS 29 - 30R. THE CORROSION WAS REMOVED IAW SRM 51-10-3 PAR 26.SDR A8ZR20170504001Doubler · corrodedREPAIR DOUBLER FROM BS 887-927 & S21R-S23R HAS CORROSION.SDR IXXA20161130151Skin · corrodedFORWARD LOWER CARGO INTERNAL SKIN AT BS 632-654 STRINGER 34 - 35L HAS CORROSION. FOUND CORROSION TO BE OUT OF LIMITS, CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-00-01 REPAIR 12 FIGURE 201.SDR DALA2016110308372Skin · damagedDURING INSPECTION, FOUND FORWARD CARGO DOOR AFT SURROUND, SURROUND OUTER SKIN BENT OUTBD AND INBD EDGE WORN 21" ABOVE AFT BOTTOM CORNER. MAINTENANCE CUT AND REMOVED DAMAGED AREA ON FORWARD CARGO DOOR AFT SURROUND OUTER SKIN. FABRICATED REPAIR PARTS. ALODINED SDR CALA2016110400851Skin · corrodedLAVATORY FLUSH EXHAUST PORT HAS VISIBLE CORROSION SWELLING. INSTALLED REPAIR DOUBLERS REF ECRA 5331-02141.SDR DALA2016110308188Skin · crackedCRACK ON FUSELAGE SKIN (LENGTH 0.187") ON STA Y=1418 BTW LONG 2L AND 3L AND CRACK ON FUSELAGE SKIN (LENGTH 0.187") ON STA Y=1418 BTW LONG 2R AND 3R. CRACKS OF .187" ON SKIN WERE REPAIRED PER ETI 88-16-364 REV 6 AND ER/A 550324-14AD REV ORIGINAL.SDR DALA2016110308185Doubler · corrodedCORROSION ON EXTERNAL RADIO ALTIMETER ANTENNA CUTOUT BTW STA Y=712 AND Y=731. DOUBLER WAS REPLACED PER DGW 5911412 REV DV AND SRM 51-30-2 AND 51-30-5.SDR DALA2016110308184Doubler · corrodedCORROSION ON PRODUCTION DOUBLER BTW STA 598-617 AND LONG 29L-29R AT MID CARGO COMPT. DOUBLERS WERE REPLACED PER SRM 51-30-2, 51-30-5, 51-10-3, DWG 5911412 REV DU.SDR SIMA20161101003Skin · crackedRT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 AND ABOVE STRINGER 2R, APPROX 3/8' LONG. INSTALLED REPAIR DOUBLER, FILLER, SHIM DRAG ANGLE ON RT UPPER FUSELAGE AFT OF FRAME 75 AND ABOVE STRINGER 2R IAW SRM 53-31-01. SEE WIPS AND TASKS FOR DETAILS.SDR IXXA20161214213Skin · corrodedSKIN FOUND TO BE CORRODED. REMOVED DAMAGED PORTION OF SKIN AND INSTALLED REPAIR IAW SRM 53-00-01 FIGURE 201 REPAIR 3.SDR SCNA20161101284Skin · puncturedWING TO BODY PANEL 193AR HAS THREE PUNCTURES TO EXTERIOR SKIN. REPAIRED THE PUNCTURES TO EXTERIOR SKIN ON PANEL 193AR.SDR HALA2016110100379Skin · corrodedCORROSION FOUND ON INTERNAL SKIN BS 1131-1153 BETWEEN STRINGER 37 & 38R. CUT OUT DAMAGESDR DALA2016110208128Skin · corrodedCORROSION AROUND CUTOUT OF AFT LAVATORY SERVICE ACCESS PANEL. CORROSION WAS FOUND OUT OF LIMITS AND WAS REPAIRED PER ER/A 550350-14 REV ORIGINAL.SDR JRAA2017081100445Skin · corrodedDURING INSPECTION IAW CARD 53-30-00-101, FOUND FUSELAGE SKIN AT BS 1016 BETWEEN STRINGERS 24R - 25R WAS CORRODED. A REPAIR WAS CARRIED OUT IAW DOCUMENT 2016R002.SDR BJNA20161031001Skin · corrodedCORROSION ON AFT CARGO DOOR CUT OUT FORWARD LOWER CORNER.SDR IPXA2016110110110Skin · puncturedPUNCTURE IN SKIN BS 1862.70 STRINGER 25L. ACCOMPLISHED DOUBLER REPAIR IAW EO B757-5330-62332A.SDR DALA2016110108103Skin · crackedDURING INSPECTION FOUND BS 540, BETWEEN STR 22L AND STRINGER 23L, 8 EACH OPENED FASTENER HOLES FOR NDT INSP, 2ND HOLE DOWN ON AFT ROW, HOLE HAS CRACK INDICATION IN FUSELAGE SKIN. MAINTENANCE REPAIRED STATION 540 SKIN CRACK STRINGER 22L-23L ON CUSTOMER CARD 5SDR FDEA201610313761Skin · crackedTWO CRACK INDICATIONS APPROXIMATELY ONE INCH, EACH IN LENGTH. FOUND DURING X-RAY INSPECTION AT BS 5-123 AT LONGERON 6R SPLICE AFT CTR SECTION. REPAIRED IAW DWG A5A7112 REV 'D' AND SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR DXTR2016103102Skin · gougedLT FUSELAGE SKIN AT WING FAIRING SCRATCHED (GOUGED) APPROXIMATE LOCATION FS 254.00 WL.100. SKIN THICKNESS IN THIS AREA IS 0.040". REPAIRED IAW ENGINEERING ORDER ERO-868481.SDR SWAA2016120810299Skin · crackedLOWER BULKHEAD SKIN CRACKED AT BS 540, STR 22R. REPAIRED SKIN PER EA & ER.SDR CALA2016110295889Skin · crackedLT FUSE SKIN AT FR35 STR 30L HAS A CRACK INDICATION ON HOLE MARKED 2. INTERIM REPAIR ACP IAW EC RA5330-05813 PART 1.SDR CALA2016110295888Skin · crackedRT FUSE SKIN AT FR35 STR 30R HAS A CRACK INDICATION ON HOLE MARKED 2. INTERIM RPR ACP IAW ECRA 5330-05813 PART 1.SDR DALA2016103107949Doubler · corrodedCORROSION ON PRODUCTION DOUBLER BETWEEN BS 579 - 598 X -60. THE DOUBLER WAS REPLACED IAW SRM 53-20-51 FIG. 1 ITEM 25 AND 51-41-05.SDR 2017FA0000444Skin · corrodedDURING A C1 CHECK, IAW TASK CARD 53-30-00-101, FOUND A CRACK ON FUSELAGE SKIN AT BS 937, STRINGER 24L. REPAIRED IAW REPAIR PLAN DOCUMENT 2016R001.SDR SWAA2016112809951Skin · crackedR1 DOOR FORWARD FRAME CUTOUT CRACKED AT BS 294, RBL 54. REPAIRED IAW SRM.SDR CALA2016103100834Skin · damagedCREASE ON FUSELAGE SKIN AT BS 1040 AT STRINGER 20L FORWARD OF TAIL COMPARTMENT OPENING. COMPLIED WITH ECRA 5330-05818.SDR SIMA20161029003Skin · corrodedSKIN CORRODED BETWEEN BS 295 & 310 AND STRINGERS 26-27L. REPAIRED PER ERS-CR-53MR-2372.SDR SIMA20161029005Skin · gougedFUSELAGE SKIN IS GOUGED BETWEEN BS 969 AND FS985.00 AT STRINGER 27. REPAIRED FUSELAGE SKIN IAW ERS-CR-53MR-2377.SDR AALA201611309003Skin · crackedCRACK ON FORWARD CARGO BAY SKIN PANEL AT FRAME 35 AND STRINGER 30L. REPAIRED SKIN IAW EA 264947.SDR IXXA20161130154Skin · corrodedSKIN CORRODED AROUND ANTENNA AT STRINGER 37 - 38L AND BS 566 - 588. BLENDED AREAS FOUND TO BE OUT OF LIMITS REPAIRED IAW REA47224REA19 AND SRM 53-00-01 REPAIR 14 FIGURE 201.SDR SIMA20161028005Skin · crackedDURING IMBV INSPECTION, QA FOUND A CRACK AROUND ONE FASTENER AT FRAME 77 JUST ABOVE STRINGER 4R. AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW SRM 53-32-01 AND ETN EM-53-194.SDR SIMA20161028006Skin · crackedDURING IMBV INSPECTION, QA FOUND THE FUSELAGE EXTERNAL SKIN CRACKED AROUND ONE FASTENER AT FRAME 78, STRINGERS 3-4L . AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED PERMANENT REPAIR IAW SRM 53-32-01 AND ETN-EM-53-194 .SDR V0XD20161108191Skin · gougedFS 977 EXTERIOR SKIN AT STR 27 SHOWING SIGNS OF GOUGING. REPAIRED GOUGING IAW REO 670-53-51-108 REV DATE 2016-11-07. NDT PERFORMED. NO CRACK INDICATIONS NOTED.SDR DALA2016102908225Skin · dentedDENT ON FUSELAGE SKIN APPROXIMATELY AT STA 646, 2" ABOVE STRINGER 18L. ACCOMPLISHED PERMANENT REPAIR FOR A DENT ON FUSELAGE SKIN AT STA 646 2" ABOVE STRINGER 18L IAW ER/A 547309-14 REV ORIG.SDR DALA2016102908224Skin · dentedDENTS (3) ON FUSELAGE SKIN APPROXIMATELY AT STA 621, 2" BELOW STRINGER 17L, STA 630, " BELOW STRINGER 17L AND STA 636, 1" ABOVE STRINGER 18L. ACCOMPLISHED PERMANENT REPAIR FOR DENTS (3) ON FUSELAGE SKIN IAW ER/A 547309-14 REV ORIG.SDR SIMA20161028003Skin · dentedDENT WITH POSSIBLE LIGHTNING STRIKE JUST FWD FRAMNE 4 BETWTEEN STRINGER 14 AND 15L. REPAIRED IAW ERS-EM-53MR-2352.SDR DALA2016102907979Doubler · crackedCRACK ON PRODUCTION DOUBLER IN ELEVATOR ACCUMULATOR ACCESS DOOR FRAME AT BS 1474. DOUBLER WAS REPLACED IAW SRM 51-30-5, 51-30-2 AND DWG 5917686-7 REV AA.SDR R61A201610270673Skin · corrodedMAINTENANCE REPORTED CORROSION DAMAGE ON THE FUSELAGE SKIN AROUND WASTE SERVICE DOOR CUT OUT AREA. REPAIRED IAW ETD2016-170-098279 REV A. AND SRM 51-41-02, 51-10-02, 53-23-03, 51-00-04 & 51-21-01.SDR R61A201610270672Skin · corrodedMAINTENANCE REPORTED CORROSION DAMAGE ON FUSELAGE SKIN AROUND WASTE SERVICE DOOR CUT OUT AREA. REPAIRED IAW ETD2016-170-098279 REV A. AND SRM 51-41-02, 51-10-02, 53-23-03, 51-00-04 & 51-21-01.SDR R61A201610270671Skin · corrodedMAINTENANCE REPORTED CORROSION DAMAGE ON FUSELAGE SKIN AROUND WASTE SERVICE DOOR CUT OUT AREA. REPAIRED IAW ETD2016-170-098279 REV A. AND SRM 51-41-02, 51-10-02, 53-23-03, 51-00-04 & 51-21-01.SDR CALA2016110295883Skin · crackedSTA 2195.75 STR 7R TO 8R, FUSELAGE SKIN FOUND CRACK AROUND 2EA FASTENER. FUSELAGE SKIN STA 2195.75 STR 7R TO STR 8R REPAIRED AS PER EA 5300-01986 OP 010.SDR DALA2016110108100Skin · dentedDURING THE CURRENT MAINTENANCE CHECK OF THE DATUM AIRCRAFT , 5 (EA) DENTS WERE FOUND ON THE FUSELAGE SKIN, BETWEEN STA 620 TO 650 AND S-17L TO S-18L. REFERENCE ER/A 547309-14 REV ORIG.SDR DALA2016102807854Skin · crackedCRACKED SKIN AND PRODUCTION DOUBLER BS 1470, LONG 23 - 24R. REPAIRED IAW SRM 53-01 FIG 02 AND 53-34.SDR DALA2017010500110Skin · corrodedCORR SKIN AT STA 1002 STR 28R-25R. BLENDED CORROSION ON INTERNAL DOUBLER "SKIN" AT STA 1002 L25R-L28R FOUND TO BE WITHIN LIMITS IAW SRM 53-20-15 NOMINAL .071 .040. REMAINING REPAIRED OUT OF LIMITS AREA IAW ER/A 549633-14.
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