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 SWAA2016040650643Skin · crackedBULKHEAD CHORD SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.SDR SWAA2016040650642Skin · crackedSKIN CRACKED AT BS 540, BETWEEN STRINGER 22L - 23L. REPAIRED SKIN IAW EA.SDR DALA2016032702358Skin · damagedLIGHTNING STRIKE ON WINDOW FRAME BETWEEN BS 750 TO 769 AND LONGERONS 12RT TO 13RT. REWORKED AREAS WERE MEASURED, UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1 AND 2. BLEND OUTS ON ZONE CRITICAL, THE ORIGINAL THICKNESS ON BLEND OUT 1 IS .086"SDR CALA2016032800191Skin · corrodedCORROSION AT STATION 500+10, ON BELLY OF ACFT, REFER TO LOG PAGE 9090297 & 9090298. ACCOMPLISHED INTERIM REPAIR IAW ECRA 5331-02088 PART 1. DIP ISSUED TO ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE MARCH 23 2017. PLANNING TO CONTACT ENGINEERING AFTER JANUARYSDR DALA2016032802350Skin · corrodedCORROSION ON SKIN UNDER LOWER AFT VHF ANTENNA BS 1470 S30. WORK IN PROGRESS.SDR DALA2016032702329Skin · crackedBS 1087 ABOVE STRINGER 14R, SKIN HAS A 2 DIRECTIONAL CRACK, VERTICAL LEG .5" & HORIZONAL LEG .1250". HFEC VERIFIED IAW NDT SPM 06-10-01.001 REQUEST ENGINEERING DISPOSITION. REPAIRED CRACK AT BS 1087, 514R IAW ER/A 543584-14 ASSOCIATED ER/A 00-543584 ADDED SDR WVER2016032600009Skin · chafedFS 977 LOWER FUSELAGE SKIN CHAFED AT STR 27.SDR DALA2018032601934Skin · dentedFUSELAGE SKIN WAS FOUND WITH MULTIPLE DENTS NEAR AN EXISTING REPAIR. THE DENTS WERE LOCATED BETWEEN BS 600 - 660, BETWEEN STRINGERS 15L - 18L. COMPLIED WITH A SPLICE REPAIR IAW ERA 542509-14, REV A.SDR COEA2016032539805Skin · corrodedHEAVY CHECK COE & MAJOR REPAIR. TAIL SECTION LOWER SKIN DOOR. REINFORCEMENT HAS LEVEL 2 CORROSION AT FRAME 45, FWD EDGE OF AVIONICS ACCESS DOOR CUT OUT. REPAIR IAW CE 1616 16 10190 DATED 5 10 2016.SDR SWAA2016051651854Post · crackedLEFT NR 3 WINDOW FRAME, E - F POST CRACKED IN 2ND LOWER FASTENER HOLE. REPAIRED POST IAW ACO.SDR COEA2016032503805Cover Plate · corrodedHEAVY CHECK COE & MINOR REPAIR. RT AOA PROBE COVER PANEL HAS LEVEL 2 CORROSION. REPLACED COVER PLATE WITH OEM PART.SDR COEA2016032502805Cover Plate · corrodedHEAVY CHECK COE & MINOR REPAIR. LT AOA PROBE COVER PANEL HAS LEVEL 2 CORROSION. REPLACED COVER PLATE WITH OEM PART.SDR ASAA2016032516214Skin · dentedSKIN DENTED FWD OF BS 259.5 BETWEEN STR 15-16 LT. ACFT GROUNDED. SKIN DENT FWD OF BS 259.5 BETWEEN STR 15-16 LT WAS REPAIRED IAW ATS ER 16-02100, DATED 02--APR-2016 AND EA 900ER-53EA-16877, DATED 02-APR-2016.SDR DALA2016032602449Skin · corrodedDURING SVC CHECK FOUND CORROSION AROUND LAV EXHAUST VENT RT SIDE OF AFT FUSELAGE. COMPARED WITH PRI 545291-14, REV 1 ALL STEPS C/W. C/W ERA 545291-14, REV ORIGINAL ALL REQUIRED INSPECTION ITEMS HAVE BEEN C/W. ASSOCIATED ER/A 14-545291, ADDED FOR AC 3223.SDR SWAA2016032850252Skin · corrodedCENTER WING BOX, LOWER OVERWING EMER SKIN CORRODED, AT THE FWD 2 FASTENER HOLES. REPAIRED SKIN IAW EA.SDR DALA2016032702357Skin · damagedLIGHTING STRINKE ON LOWER WINDOW FRAME, BS 1100 RT SIDE. REWORKED AREAS WERE MEASURED, UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1 AND 2. BLEND OUT ON ZONE CRITICAL, 1 THE ORIGINAL THICKNESS IS .084" AND REMAINING THICKNESS .080", THE ORISDR DALA2016032702353Skin · damagedLIGHTNING STRIKES ON WINDOW FRAME BETWEEN BS 731 TO BS 750 AND LONGERONS 12 RT TO 13 RT. REWORKED AREAS WERE MEASURED (UT) WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PARAGRAPH 5, FIG 3, SHEET 1 AND 2. BLEND OUT ON ZONE CRITICAL, 1 IS .090" AND REMAINING THICKNESSDR DALA2016032702352Skin · damagedLIGHTNING STRIKES, FOUR ON WINDOW FRAME BETWEEN BS 674 TO 693 AND LONGERONS 14TO 15R. MEASURE REWORKED AREAS, UT) WAS ACCOMPLISHED IAW DC/MD NDT SPM 04-00-07 PAR 5, FIG 3, SHEET 1 AND 2. BLEND OUT ON ZONE CRITICAL BLEND OUT, 2 THE ORIGINAL THICKNESS ES .120 SDR CALA2016032800187Skin · dentedDENT IN RT FWD FUSELAGE, 14" FWD OF GND POWER RECEPTACLE CUT OUT, AT STATION 215. REPAIRED DENT IAW SRM 53-00-01 REPAIR 3.SDR DALA2016032802351Skin · corrodedCORROSION ON INTERNAL SKIN SURFACE AT BS 1443 BETWEEN STR 27R AND 26 RT. COMPLIED WITH ER/A 545293-14, REV ORIGINAL.SDR A6WA201643728Skin · damagedLEFT FWD AVIONICS ACCESS PANEL 131AL, FASTENER HOLES IN SKIN HAVE 6 FREEZE PLUGS PULLING THROUGH. REPAIRED LT FWD AVIONICS PANEL HOLES IN FUSELAGE OUTER SKIN IAE REO 601R-53-11-2879, REV A DATED 2016 03 23 & REO 601R-53-11-162 REV C.SDR FDEA201603251051Skin · dentedFUSELAGE SKIN STATION 655, BETWEEN STRINGER 24R - 23R, HAS A DENT, AFTER EVALUATION OF REPORTED DENT, WAS FOUND OUT OF LIMITS IAW SRM 53-00-01-2R FIG 101 DETAIL 3. REPAIRED SKIN IAW SRM 53-00-01-2R FIG 201 REPAIR 7. THIS REPAIR IS CLASSIFIED AS CATEGORY B MASDR FDEA201603251050Skin · dentedFUSELAGE SKIN STATION 677, BETWEEN STRINGER 23R - 24R, HAS A DENT. AFTER EVALUATION OF REPORTED DENT, WAS FOUND OUT OF LIMITS IAW SRM 53-00-01-2R FIG 101 DETAIL 3. REPAIRED DAMAGED SKIN IAW SRM 53-00-01-2R FIG 201 REPAIR 7. THIS REPAIR IS CLASSIFIED AS CATESDR DALA2016111608866Skin · corrodedCORROSION BTW FUSELAGE SKIN AND DOUBLER ON LOWER CORNER AT AFT LAVATORIES SERVICE PANEL CUT OUT. REMOVED CORROSION AREAS, MEASURE: ORIG, MATERIAL THICKNESS IS 0.063" REMAINING THICKNESS IS 0.055". REPAIRED PER ER/A.SDR FDEA201603241020Skin · damagedAGEING ACFT, EXISTING REPAIR AT FWD CARGO FUSELAGE DOOR CUT OUT, AFT JAMB SKIN STATION 1002.3, LONGERON -40R TO -41R. EXISTING REPAIR AT FWD CARGO FUSELAGE DOOR CUT OUT, AFT JAMB SKIN EVALUATED & FOUND DAMAGED REPAIR CARRIED OUT AT FWD CARGO IAW EA -5330-T032SDR AALA20160324013Skin · crackedAIRCRAFT WAS GNDED. FUSELAGE SKIN CRACKED AT STATION 1485, ALONG CANT RIVET LINE JUST AFT OF RT T/R ACCUMULATOR ACCESS DOOR. ACCOMPLISHED SKIN REPAIR IAW SRM 53-01-00-001.SDR AALA20160324002Skin · crackedAIRCRAFT WAS IN BASE MX. FUSELAGE SKIN IS CRACKED AT STATION 1380 & LONGERON 14R. REPAIRED SKIN IAW SRM 53-01-00-001 & AARD 53-30-00-02;.SDR YENA20160324261Finger Doubler · corrodedAFT CARGO DOOR FUSELAGE CUTOUT LOWER BEAM FWD FINGER DOUBLER CORRODED AT FRAME 77 +1. REPLACED FINGER DOUBLER IAW SRM REF 51-43-03, REF EAMS NR H4870-00370.SDR SWAA2016032850300Doubler · crackedRIGHT DOUBLER CRACKED AT BS 235.8. REPAIRED DOUBLER IAW SRM.SDR DALA2016032402332Skin · dentedDENT LOCATED LOWER EXTERIOR FUSELAGE SKIN, BS 584, S27-28L. FOUND DENT OUT OF LIMITS, CUT OUT DAMAGE, FABRICATED REPAIR AND INSTALLED REPAIR IAW SRM.SDR DXTA2016032306214Skin · corrodedCORROSION WAS FOUND UP TO 0.003 INCHES DEEP ON THE SKIN, PN 6711032-9, OF THE LOWER SKIN BOND ASSEMBLY, PN 6711030-4, ALONG THE FWD PRESS BULKHEAD PLANE AT LBL 17.5. ALL CORROSION DAMAGE WAS REMOVED BY BLENDING. THE REMAINING THICKNESS WAS MAPPED USING ULTRASDR DXTA2016032306213Skin · corrodedCORROSION WAS FOUND ON THE 6711070-2 RT AFT CABIN SKIN UNDER THE TCAS ANTENNA AT FS 205.00, RBL 4.17. ALL CORROSION DAMAGE WAS REMOVED BY BLENDING. THE REMAINING THICKNESS WERE MAPPED USING ULTRASOUND. THE MINIMUM REMAINING THICKNESS WAS 0.025 INCHES. THE SDR DXTA2016032306212Skin · corrodedCORROSION WAS FOUND UP TO 0.012 INCH DEEP ON THE LT SKIN, PN 6711032-21, OF THE LT SKIN BOND ASSEMBLY, PN 6711033-3, AT FS 187 ABOVE STRINGER 12L. ALL CORROSION DAMAGE WAS REMOVED BY BLENDING. THE REMAINING THICKNESS WAS MAPPED USING ULTRASOUND.SDR DALA2016032402283Skin · deformedDEFORMED FUSELAGE SKIN AND DOUBLERS ON LOWER AND FWD, AFT CORNERS AT AFT LAVATORY SERVICE PANEL CUTOUT. REPAIRED LOWER FWD CORNER IAW ERA 397822-14 MA, REV B.SDR DXTA2016032306209Skin · corrodedSEVERAL CORROSION SITES WERE FOUND ON THE FUSELAGE SKINS. PRESS VESSEL SKIN IS CORRODED AT THE FOLLOWING ATA 53 LOCATIONS ALONG THE UPPER SURFACE, FS 527 3 SPOTS, FS 413 1 SPOT, FS 388 3 SPOTS, FS 362 1 SPOT, FS 370 1 SPOT, FS 327, FS 316, FS313, FS 298, FS 2SDR FDEA201603231010Skin Panel · damagedINCOMING LIGHTNING STRIKE REPAIR, FUSELAGE SKIN STATION 1216, BELOW STRINGER 7L IS OUT OF LIMITS IAW SRM, REQUIRES REPAIR. REPAIRED LIGHTNING STRIKE IAW SRM 53-00-01-2R FIG 201 REPAIR NR 7. MAJOR REPAIR.SDR SIMA20160322006Skin · crackedRIGHT UPPER FUSELAGE SKIN CRACKED AT FRAME 75, ABOVE STRINGER 2R. REPAIRED RT UPPER FUSELAGE SKIN CRACK IAW ERS-EM-53MR-1984.SDR DALA2016032602327Skin · damagedREWORK OF EXTERNAL SKIN AT LOWER FUSELAGE FROM FRAMES 68 TO 70 BETWEEN STRINGERS 25 - 28R . FOUND OUT LIMITS IAW SRM 53-41-11. PARA 4F FIG 108, SHEET1,ON P2. PERFORMED A PERMANENT REPAIR IAW SRM 53-41-11, PARA 5M FIG 214.SDR TSAA20160322007Bear Strap · not reportedBEAR STRAP AT STATION 303.9, JUST ABOVE LOWER HINGE, AT WL 238 LT & REPAIRED IAW SRM 53-10-01 REPAIR 14 REV 108. BEAR STRAP REPAIR AREA AT STATION 303.9 RE-FINISHED AS REQUIRED IAW AMM 51-21-99 REV 82.SDR DALA2016032302250Skin · damagedELONGATED HOLE ON FUSELAGE SKIN, BS 370-375 OVER LONG 29 LT. ELONGATED HOLE WAS REPAIRED IAW ETI-88-16-102, REV 1 AND ERA 543192-14, REV ORIGINAL.SDR VNAA2016032200024Skin · crackedSKIN AT BS 235 HAS A CRACK AT STR 26L AND 26R. REPAIRED SKIN AT FS 235 FROM STR 26R TO STR 26L IAW REO.SDR WVER2016032200001Skin · damagedFUSELAGE SKIN DAMAGED BETWEEN STR 21-23R AT FS 265. REPAIRED IAW REO690-53-11-858 REV, DATED 2016-03-21.SDR COEA2016032106805Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. REAR CTR FUSELAGE RT LATERAL LOWER SKIN PANEL EXTERIOR SURFACE HAS LEVEL 2 CORROSION AT THE FWD & AFT EDGES OF THE SERVICE DOOR CUT OUT. REPAIRED IAW CE 1542 16 10208 5 9 2016.SDR COEA2016032105805Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. REAR CTR FUSELAGE RT LATERAL UPPER SKIN PANEL EXTERIOR SURFACE HAS LEVEL 2 CORROSION AT THE AFT EDGE OF THE SERVICE DOOR CUT OUT. REPAIRED IAW CE 1542 16 10208 DATED 5 9 2016.SDR COEA2016032104805Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. FWD CTR FUSELAGE RT LOWER SKIN PANEL HAS LEVEL 2 CORROSION, FRAMES 14 - 15 AT SKIN LAP, STRINGER 17R. REPAIRED IAW CE 1560 16 10201 DATED 5 6 2016.SDR FDEA201603210962Skin Panel · damagedTO COMPLY WITH EA 1-5330-T0313867 A PART 4 FWD INTERMEDIATE FUSELAGE SKIN PANEL ASSEMBLY. INTERIM REPAIR OF IMPACT DAMAGE AT LOWER FWD CARGO DOOR JAMB CUT OUT. ACCOMPLISHED REPAIR IAW SRM 53-00-15-2R FIG 202 REPAIR 8 & EA 1-5330-T0313867B PT 4. INITIAL INSPESDR SWIA201642063Skin · dentedDENT ON BS 624, STR 20R. COMPLIED WITH EA AND ALL STEPS COMPLETED OF PERMANENT REPAIR.SDR SIMA20160321002Skin · corrodedPERMANENT REPAIR TO FUSELAGE SKIN, BETWEEN FS 421.00 & 437.00 & STRINGER 21LT. COMPLETED WITH PERMANENT REPAIR TO FUSELAGE SKIN IAW ERS-CR-53MR-1912 REV 1.SDR SIMA20160321001Skin · dentedDURING MBV INSPECTION, A DENT WAS FOUND, BETWEEN FRAME 25 & 26, BETWEEN STRINGERS 20R & 21R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REPAIRED DENT IAW ERS-EM-53MR-1993. REPAIR MATERIALS, FILLER 20SDR SWAA2016032350137Skin · crackedFUSELAGE SKIN CRACKED AT STATION 312 - 330, STRINGER 4L. REPAIRED SKIN IAW SRM.
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