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 UHLA201603150114Skin · damagedAPPROXIMATELY 43 LIGHTNING STRIKES BETWEEN FRAME 24 AND FRAME 27, STR 26L AND 27L. R & R DAMAGED AREA BETWEEN FRAME 24 AND FRAME 27, STR 26 AND 27 IAW ETD2016-170-025965.Mar 13, 2016 · N810MD · Emb ERJ170100SUSDR DALA2016031401910Skin · out of limitsSKIN OUT OF LIMITS BETWEEN LONGERONS 3 & 4L AT BS 610 - 695. REPAIRED IAW SRM 51-30-2, 51-10-4, 51-10-3. PAR 14 AND 21 AND 53-04-2, FIG 2, SHEET 6 AND 17.Mar 13, 2016 · N904DE · Doug MD88SDR ASOA2016031214589Skin · burnedBURN MARK ON RIVET ON STR 23L AND BS 409. REMOVED FASTENER. FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E. REPAIR TYPE 3 TEMPORARY. VALID TILL NEXT C-CHECK IN 4153 FLIGHMar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214588Skin · burnedDEFECT DESCRIPTION: BURN MARK ON RIVET ON BS 364 BTWN STR 21-22. REMOVED FASTENER.FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENER ,ALODINE,PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115 REV.E.Mar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214587Skin · burned2 BURN MARKS ON RIVETS ON STR 23L BETWEEN FS 310 - 333. REMOVED 2 FASTENERS. FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENERS, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E. REPAIR TYPE 3 TEMPORARY. VALID TILL NEXT C-CHMar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214586Skin · burnedBURNS ON STR 23L BETWEEN FS 295 - 310. REMOVED DAMAGE FROM BURNS ON STR 23L BETWEEN FS 295/310 IAW SRM 51-12-00. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-31. MATERIAL REMOVED WAS .600"L X .600"W X .009" DEEP. NR 2: .600"L X .600"W X .009" DEEP, Mar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214585Skin · burnedBURN MARK ON RIVET ON STR 23L, BETWEEN FS 280 - 295. REMOVED DAMAGE RIVET ON STR 23L BETWEEN FS 280/295 IAW SRM 51-42-06, DAMAGE CONTAINED TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE,PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E. REPAIR TYPMar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214584Skin · burnedBURN MARK ON RIVET ON STR 22L AND FS 280, MARKED P. REMOVED DAMAGED RIVET ON STR 22L AND FS 280 IAW SRM 51-42-06. FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E. REPAIR TYPEMar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214583Skin · burnedBURN MARK ON RIVET ON STR 23L BTWN F.S. 265 - 280. REMOVED DAMAGED RIVET ON STR 23L BETWEEN FS 265/280 IAW SRM 51-42-06, DAMAGE CONTAINED TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE,PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E, REPAIR TYPMar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214582Skin · burned3 RIVETS WITH BURN MARKS ON STR 23L BETWEEN FS 250 - 265. REMOVED 3 DAMAGE RIVETS ON STR 23L BETWEEN FS 250/265 IAW SRM 51-42-06, DAMAGE CONTAINED TO RIVET ONLY. INSTALLED 3 TEMP FASTENERS, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV EMar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214581Skin · burned8 RIVETS WITH BURN MARKS ON THEM AT FS 265 AND STR 24L, MARKED L. 5 BURN MARKS CONTAINED TO SURFACE FINISH DAMAGE ONLY. RESTORED SURFACE FINISH TO BURN MARKS IAW SRM 51-25-16. REMOVED 3 DAMAGED RIVETS AT FS 265 AND STR 24L IAW SRM 51-42-06. FOUND DAMAGE CONMar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214580Skin · burnedBURN MARK ON RIVET ON STR 24L BETWEEN FS 250/265, MARKED K. REMOVED DAMAGED RIVET ON STR 24L BETWEEN FS 250/265 IAW SRM 51-42-06. FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115 REV E.Mar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214579Skin · burned2 RIVETS WITH BURN MARKS ON FS 250 AND STR 24L, MARKED J. REMOVED DAMAGED RIVETS ON F 250 AND STR 24L IAW SRM 51-42-06. FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E. REPAIRMar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214578Skin · burnedBURN MARK ON RIVET ON FS 235 BETWEEN STR 25L/26L, MARKED I. REMOVED DAMAGED RIVET ON FS 235 BETWEEN STR 25L/26L IAW SRM 51-42-06. FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115 REV EMar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214577Skin · burned2 BURN MARKS BETWEEN FS 220/235 AND STR 25L/26L, MARKED H. REMOVED DAMAGE FROM DAMAGED LOCATION 1 IAW SRM 51-12-00, DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-31. REMOVED DAMAGED RIVET FROM DAMAGE LOCATION 2 IAW SRM 51-42-06, FOUND DAMAGE TO BE CONTAINED Mar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214576Skin · burnedBURN MARK ON SKIN BETWEEN FS 202.75/220 AND STR 25L/26L, MARKED G. REMOVED DAMAGE BETWEEN FS 202.75/220 & STR 25L/26L IAW SRM 51-12-00. DAMAGE IS OUT OF LIMITS IAW SRM 53-00-31. BLEND 0.5" X 0.5" X 0.006. COMPLIED WITH EDDY CURRENT IAW NDTM 51-20-06. NO DEMar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214575Skin · burnedBURN MARK ON RIVET 4" AFT OF FS 202.75 AND 1" ABOVE STR 26L, MARKED F. REMOVED DAMAGED RIVET 4" AFT OF FS 202.75 AND 1" ABOVE STR 26L IAW SRM 51-42-06. FOUND DAMAGE TO BE CONTAINED TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORMar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214574Skin · burnedBURN MARK ON RIVET ON FS 202.75, 1" ABOVE STR 26L, MARKED E. REMOVED DAMAGED RIVET ON FS 202.75, 1" ABOVE STR 26L IAW SRM 51-42-06. FOUND DAMAGE TO BE CONTAINED TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-0Mar 12, 2016 · N914EV · Cndair CL6002B19SDR ASOA2016031214573Skin · burnedBURN MARK ON SKIN EDGE 4" AFT OF FS 169, JUST UNDER STR 25L, MARKED C. REMOVED DAMAGE ON SKIN EDGE 4" AFT OF FS 169 JUST UNDER 25L IAW SRM 51-12-00. DAMAGE IS OUT OF LIMITS IAW SRM 53-00-31. BLEND 0.65" X 0.15" X 0.015". COMPLIED WITH DISPOSITION IAW EA 2Mar 12, 2016 · N914EV · Cndair CL6002B19SDR DALA2016031401908Skin · crackedCRACKS OF 1.156" AND 0.093" ON FUSELAGE SKIN ON BS 374 AT THE UPPER FWD DOOR JAMB CORNER OF THE FWD CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW ER/A 543154-14AD, REV ORIG.Mar 12, 2016 · N993DL · Doug MD88SDR SWAA2016042551258Skin · crackedAFT GALLEY DOOR SKIN CUT OUT CRACKED AT FASTENER HOLE ON FWD LOWER CORNER. REPAIRED SKIN IAW EA.Mar 11, 2016 · N361SW · Boeing 7373H4SDR SWAA2016042551259Bear Strap · crackedAFT GALLEY DOOR LOWER HINGE CUT OUT BEAR STRAP CRACKED. REPAIRED DOUBLER IAW SRM & EA.Mar 11, 2016 · N361SW · Boeing 7373H4SDR SIMA20160311006Skin · crackedRIGHT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 2R & 3R. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-1979.Mar 11, 2016 · N651AE · Emb EMB145LRSDR SIMA20160311005Skin · crackedLEFT REAR FUSELAGE I SKIN CRACKS AT FRAME 75, BETWEEN STRINGERS 1L & 3L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN AT FRAME 75, BETWEEN STRINGERS 1L & 3L IAW ERS-EM-53MR-1978.Mar 11, 2016 · N651AE · Emb EMB145LRSDR F3LA2016031400010Floor Panel · corrodedDURING C CHECK INSPECTION NOTED AFT WET AREA FLOOR STRUCTURE AFT RT CORNER, BETWEEN FRAME 69 & 70, SHEAR PLATE CORRODED. R & R AFT WET AREA FLOOR STRUCTURE LT CORNER, FRAME 69 & 70, SHEAR PLATE IAW SRM 51-42-11.Mar 11, 2016 · N207FR · Airbus A320214SDR DALA2016031201891Skin · damagedLIGHTNING STRIKE ON LT FUSELAGE SKIN WINDOW BELT LOWER EDGE AND LOWER CORNER BETWEEN BS 389 TO BS 408. DAMAGE WAS BLENDED OUT, IAW SRM 53-05, FIG 111. AREA WAS MEASURED: BLENDED OUTS WERE FOUND IN ZONE 3 AND NO CRITICAL ZONE THEREFORE ALL ARE WITHIN LIMITS IMar 11, 2016 · N994DL · Doug MD88SDR DALA2016031301879Skin · corrodedSKIN CORRODED AT BS 1005 ABOVE LONGERON 27R AND ON LONGERON 25R AT BS 1003 AFT OF LOWER CARGO DOOR CUTOUT. BLENDED CORROSION, AND FOUND WITHIN LIMITS IAW SRM 53-00-00, FIG 103.Mar 11, 2016 · N954AT · Boeing 717200SDR ASOA20160312011Skin · dentedDENT AT FRAME 10 AFT OF NLG. CUTOUT DAMAGE AND INSTALLED FILLER AND DOUBLER IAW ETD2016-145-024575. ACFT RELEASED AND RETURNED TO SERVICE.Mar 11, 2016 · N15980 · Emb EMB145LRSDR FDEA201603110895Skin · crackedFUSELAGE, REFERENCE SNRM N00892, FOUND ONE EACH FASTENER HOLE CRACKED, AT STATION 1661, LONGERON 52 AREA. CARRIED OUT REPAIR IAW EA 1-5330-T0324043 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 11, 2016 · N575FE · Doug MD11FSDR FDEA201603101194Skin · crackedLEFT STATION 1156, FUSELAGE SKIN LAYER HAS ONE EACH FASTENER HOLE WITH A CRACK INDICATION AT LONGERON 39L. REPAIRED IAW EA 8-5310-T0324512.Mar 10, 2016 · N303FE · Doug MD1030FSDR DALA2016031301925Skin · dentedDENT ON EXTERNAL SKIN AT LOWER FUSELAGE ON FRAME 69 BETWEEN STR 28 RT TO STR 29 RT. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATION ON FRAME 69, STR 27 RT TO STR 32 RT IAW ERA 544182-14AD REV A AND PRI 524182-14.Mar 10, 2016 · N309US · Airbus A320211SDR CALA2016031195212Skin · corrodedFUSELAGE SKIN CORROSION AT BS 780 - 800 & STRINGER 46L - 47L, INNER SURFACE. INTERIM REPAIR ACP IAW PART 1.1 OF ECRA 5330-05593.Mar 10, 2016 · N117UA · Boeing 747422SDR CALA2016031100160Skin · not reportedECRA 5331-02078 REPAIR TO FUSELAGE SKIN, BS 907 - 927, BETWEEN STRINGER -20L & -23L.Mar 10, 2016 · N27246 · Boeing 737824SDR AALA20160310006Skin · dentedDENT AFT OF TAT PROBE AT STATION 272, BETWEEN STRINGER 19L & 20L. DENT IS 1.5 INCHES BY 1.5 INCHES & .080 DEEP. REPAIRED DENT WITH CUT OUT & DOUBLER IAW EA 258680. ACFT IN BASE MX.Mar 10, 2016 · N836NN · Boeing 737823SDR DALA2016031101858Skin · corrodedBULGE OUTER FUSELAGE SKIN AND DOUBLER BETWEEN LONG 30 TO LONG 28, RT BS 130 APPROXIMATELY AT E/E DOOR JAMB. BULGE WAS EVALUATED WITH NEXT DIMENTIONS: D=1.5", X=0.095", D/X=15.78. THEREFORE IT IS WITHIN LIMITS IAW SRM 53-04-1, PAR 7 E CONDITION 1B. HFEC INSPEMar 10, 2016 · N904DE · Doug MD88SDR DALA2016031101872Skin · wornWEAR ON OUTER SKIN FWD SIDE OF BS 192 AND BEAM NR 6 AT FWD ENTRY DOOR. DUE EXCESSIVE DAMAGE AREA WAS REPAIRED IAW ER/A 486216-14 MA, REV A.Mar 10, 2016 · N904DE · Doug MD88SDR DALA2016031101870Skin · corrodedCORROSION AT FUSELAGE, BS 1338, BETWEEN LONGERON 19L/20 LT. REPAIR WAS ACCOMPLISHED IAW ER/A 543198-14, REV ORIGINAL AND ETI-88-16-105 OF DATE: 04-MAR-16.Mar 10, 2016 · N904DE · Doug MD88SDR DALA2016031101847Skin · not reportedDISCREPANT AREA WAS FOUND ON FUSELAGE SKIN, EXTERNAL DOUBLER REPAIR AT BS 1418 AND BETWEEN LONGERON 1 AND 3 RT. THE ER/A 498486-14, REV. ORIGINAL WAS GENERATED AND FROM SECTION I: ER/A REVISION REQUIRED, AMOC IAW SID AD 2004-11-07.Mar 10, 2016 · N994DL · Doug MD88SDR DALA2016031101843Skin · scratchedLEFT AFT FUSELAGE EXTERNAL SKIN HAS DEEP SCRATCH AT BS 1686 BETWEEN S14L AND S15L. TOPCOATED AREA LT AFT FUSELAGE EXTERNAL SKIN AT BS 1686, S14L AND S15L IAW AMM-51-20-00.Mar 10, 2016 · N651DL · Boeing 757232SDR SRXR20160310003Skin · gougedL5 DOOR LOWER FWD JAMB STOP SUPPORT STRUCTURE IS GOUGED, ACCOMPLISHED REPAIR ON NRC A025042 IAW EA 747-5330-39-A6139.Mar 10, 2016 · N744VG · Boeing 74741RSDR COEA2016030904911Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. FWD CTR FUSELAGE RT UPPER SKIN PANEL HAS LEVEL 2 CORROSION AFT OF FRAME 17, BETWEEN STRINGER 7A RT & 8R. DOUBLER REPAIR IAW SRM 53-00-00-300-803.Mar 9, 2016 · N911FX · Aerosp ATR42300SDR SWAA2016042551298Skin · crackedLOWER AFT CORNER OF FWD ENTRY DOOR SKIN CRACKED AT BS 344, STRINGER 16L. REPAIRED SKIN IAW SRM.Mar 9, 2016 · N394SW · Boeing 7373H4SDR SWAA2016042551257Skin · crackedRIGHT LOWER AFT CORNER OF DOOR SKIN CUT OUT FASTENER HOLES CRACKED AT BS 322, STRINGER 17R. REPAIRED SKIN IAW EA.Mar 9, 2016 · N361SW · Boeing 7373H4SDR SWAA2016042551256Skin · crackedFORWARD LT DOOR FUSELAGE SKIN FASTENER HOLE CRACKED ON LOWER AFT CORNER. REPAIRED SKIN IAW EA.Mar 9, 2016 · N361SW · Boeing 7373H4SDR SWAA2016041250804Skin · crackedAFT LOWER SUPPORT FOR R1 DOOR CUT OUT CRACKED. R & R CUT OUT IAW SRM.Mar 9, 2016 · N361SW · Boeing 7373H4SDR SWAA2016040550617Skin · crackedAFT CARGO DOOR CUT OUT FWD LOWER CORNER SKIN CRACKED. REPAIRED SKIN IAW SRM.Mar 9, 2016 · N638SW · Boeing 7373H4SDR SWAA2016032850291Bear Strap · crackedL1 DOOR BEAR STRAP SKIN CUT OUT CRACKED AT BS 303.9, STRINGER 13L. REPAIRED CUT OUT IAW SRM.Mar 9, 2016 · N387SW · Boeing 7373H4SDR DALA2016031001917Skin · corrodedCORROSION ON EXTERNAL SKIN AT LOWER FUSELAGE FROM FRAME 69 TO FRAME 70 BETWEEN STR 29R TO STR 30R. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN AT LOWER FUSELAGE FROM FRAME 69 TO FRAME 70 BETWEEN STR 29R, STR 30R IAW SRM 53-41-11 PARA 5.D FIG 205 PAGES 256/262Mar 9, 2016 · N309US · Airbus A320211SDR SWAA2016031149833Skin · crackedSKIN CRACKED AT BS 540, CHORD FWD FASTENER ROW 2ND FASTENER HOLE BELOW STRINGER 22L. REPAIRED SKIN IAW SRM.Mar 9, 2016 · N407WN · Boeing 7377H4SDR SWAA2016031149832Skin · crackedSKIN CRACKED AT BS 540, CHORD FWD FASTENER ROW, 3RD FASTENER HOLE BELOW STRINGER 22L.Mar 9, 2016 · N407WN · Boeing 7377H4
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