JASC 5720

Service difficulty reports · 13,638

Reports filed under 5720 · Wing Miscellaneous Structure, 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 = '5720'
  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 C2XA95IA041Support · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT. ACFT APPROVED FOR RETURN TO SERVICE. (Z)Mar 30, 1995 · N27707 · Emb EMB120RTSDR 95ZZZX1749Fitting · rivet missingDURING AIRCRAFT INSPECTION FOR 10,000-HOUR X-RAY OF WING, FOUND 4 HUCK RIVETS ON LEFT WING JACK PAD WS 96 ON PN 5520130 JACK PAD FITTING WERE IMPROPERLY SWAGED AND COLLARS WERE MISSING. NO RECORD OF ANY WORK DONE IN THIS AREA. AREA NOT INSPECTED ON PHASE INSMar 30, 1995 · N360DA · Cessna 500CESSNASDR 9505289990Bracket · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND TWO INCH CRACK IN A PANEL ATTACH ANGLE RIGHT WING LEADING EDGE LOWER SURFACE WS 118. REPAIRED PER XEA X9-57-18.Mar 30, 1995 · N8950E · Doug DC931SDR COM11841Skin Support · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I AT WING RIBS NR 15, 16, 18 AND 21. THE SKIN SUPPORTS WERE REPLACED IAW AERODESIGN REPORT NR 1327-2. P/N: 120-17062-005, 2 EA; 120-17056-015, Mar 29, 1995 · N200CD · Emb EMB120RTSDR DLL17951392Cap Doublers · cutAT HMV, CUT EXISTING CAP AT IWS 293.58 AND 319.83 TO FACILITATE FASTENER REMOVAL. UPPER RIB CAPS, APPROX 10 INCHES FROM REAR SPAR. REF VA31744 AND EO 7-59089-3. CUT CAP AT 293.58 AND 319.83 TO FACILITATE FASTENER REMOVAL. FABRICATED DOUBLERS AS PER SRM 57-Mar 27, 1995 · N764DA · Lkheed 10113853SDR COM11839Supports · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION ASK NR 5720-551/651-01I AT WING RIBS NR 15 AND 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT NR 1327-2 AND EMB SRM P/N: 120-17056-019, 1 EA; 120-17056-017, 2 EA; 120-17056-0Mar 27, 1995 · N265CA · Emb EMB120RTSDR 9505186615Stiffener · corrodedDURING PERIODIC CHECK, THE WING CENTER SECTION REAR SPAR VERTICAL STIFFENER AT LBL 86 WAS FOUND CORRODED. DISCREPANT STIFFENER P/N 65B10671-1 IS MADE FROM BAC 1517-1672 EXTRUSION AND MATERIAL IS 7178-T6511 ALUMINUM. MADE REPAIR PER EA 66-97876.Mar 27, 1995 · N632US · Boeing 747251BSDR 9504636305Support · damagedDURING LINE CHECK (KIX), DAMAGE WAS FOUND ON THE LEFT WING LEADING EDGE LOWER PANEL SUPPORT AT WS 838 AND THE OUTBOARD FUELING DOOR. REPLACED DOOR AND SUPPORT.Mar 23, 1995 · N665US · Boeing 747451SDR COM11835Supports · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AT WING RIBS NR 15 AND NR 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT 1327-2. P/N 120-17056-019, 2 EA; 120-17056-017, 2 EA; 120-17056-015, 3 EA; 120-1Mar 21, 1995 · N266CA · Emb EMB120RTSDR ABXA9500295T Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING LOWER T-CAP AT FORWARD AND AFT FLANGES ON STRINGER NR 20. BLENDED IAW DC-9 SB 57-98.Mar 21, 1995 · N980AX · Doug DC932SDR ABXA9500294T Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING T-CAP BETWEEN STRINGERS 21 TO 22. BLENDED IAW DC-9 SB 57-98.Mar 21, 1995 · N980AX · Doug DC932SDR ABXA9500293T Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LOWER T-CAP ON LEFT WING BETWEEN STRINGERS 20 TO 21. BLENDED IAW DC-9 SB 57-98.Mar 21, 1995 · N980AX · Doug DC932SDR ABXA9500292T Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING LOWER T-CAP BETWEEN STRINGERS 19 TO 20. BLENDED IAW DC-9 SB 57-98.Mar 21, 1995 · N980AX · Doug DC932SDR ABXA9500268Cap · corrodedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP BETWEEN STRINGERS 22-23. BLENDED IAW DC-9 SB 57-98.Mar 20, 1995 · N980AX · Doug DC932SDR COM11827Support · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I, AT WING RIBS NR 15 AND 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERO DESIGN REPORT NR 1327-2. P/N 120-17056-013, 120-17056-015 (4 EA), 120-17056-017 (2 EA), 12Mar 18, 1995 · N257CA · Emb EMB120RTSDR ABXA9500286Cap · crackedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND RIGHT WING LOWER T-CAP CRACKED IN THE RADIUS JUST AFT OF STRINGER NR 16. BLENDED IAW DC-9 SRM 51-10-3.Mar 17, 1995 · N980AX · Doug DC932SDR ABXA9500287Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP, AFT OF STRINGER NR 11. BLENDED IAW DC-9 SRM 51-10-3.Mar 16, 1995 · N980AX · Doug DC932SDR ABXA9500285Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP, BETWEEN STRINGERS 11-12. BLENDED IAW DC-9 SB 57-98.Mar 16, 1995 · N980AX · Doug DC932SDR 95FDEA00287Stiffener · corrosionCORROSION ON 870 LOWER CENTER WING CHORD, LBL 6 ON VERTICAL FLANGE. ACCOMPLISHED REPAIR AT BS 870 LWR CHORD PER FEDEX EA 7-5710-23931 AND FEDEX EA 7-5710-23944.Mar 16, 1995 · N185FE · Boeing 72722SDR UPS202660Clip · corrodedWHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON T-CLIP BS 760, LBL 70.5, WL 204. INSTALLED REPAIR PER UPS EO B727-5710-121F.Mar 15, 1995 · N911UP · Boeing 72727CSDR ABXA9500283Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING LOWER T-CAP HORIZONTAL FLANGE INSIDE BARREL NUT HOLES IN STRINGERS 11, 14, 16, 18, 20 AND 21. BLENDED IAW DC-9 SB 57-98.Mar 15, 1995 · N980AX · Doug DC932SDR ABXA9500267Cap · corrodedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP, INSIDE BARREL NUT HOLES IN STRINGERS NR 12, 13, 14, 15, 16, 17, 18, 19 AND 21. BLENDED IAW DC-9 SRM 51-10-3 AND SB 57-98.Mar 15, 1995 · N980AX · Doug DC932SDR UPS802658Doubler · corrodedWHILE IN 'C' CHECK MAINTENANCE FOUND CORROSION ON RT WING L/E LWR SURFACE DOOR DOUBLER AT STA XFS 360-366. REPAIRED PER UPS EO FILE NR DC8-57-0539.Mar 14, 1995 · N813UP · Doug DC873FSDR COM11832Skin Support · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I AT WING RIBS NR 15 AND 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT NR 1327-2. P/N: 120-17056-007, 2 EA; 120-17056-019, 2 EA; 120-17056-017, 2 EA;Mar 10, 1995 · N463CA · Emb EMB120RTSDR DLL10950993Angle · crackedLEFT T/E BAT STRUCTURE LWR CAP AT ITES 275.00 APPROX 13 INCHES OUTBD OF OUTBD HINGE FITTING NBR 2 SPOILER LWR CAP HAS A 2 INCH CRACK GOING THROUGH FASTENER HOLE.Mar 9, 1995 · N730DA · Lkheed 10113851SDR 96ZZZX1310Vertical Support · crackedDURING D-CHECK, LT WING LEADING EDGE FS 106.8 VERTICAL SUPPORT LOWER END IS CRACKED AT FASTENER ATTACH POINT. FAB NEW ANGLE MATERIAL .050 INCH 2024-T3 LENGTH = 17 INCH BY 2 INCH. INSTALLED PER SRM 51-10-1, PAR 4 AND SRM 51-30-2. TAT: 53,881.4 HRS. TAC: 3Mar 9, 1995 · N705DH · Boeing 72722CSDR 96ZZZM99999Angle · crackedDURING D-CHECK, LEADING EDGE SUPPORT ANGLE CRACKED AT UPPER AFT CORNER ALONG RADIUS FSS 337. REMOVED AND REPLACED ANGLE PER SRM 51-10-1 15 INCHES BY 2 INCHES 2024-T3 .040.Mar 9, 1995 · N705DH · Boeing 72722CSDR 96ZZZM390Angle · crackedDURING D-CHECK, VERTICAL LEADING EDGE SUPPORT ANGLE, SECOND FROM AFT END IS CRACKED AT LOWER FASTENER FSS 106.8 SEEN THROUGH ACCESS PANEL 6402. REMOVED FASTENERS PER SRM 51-30-2. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED DOUBLER 2024-T3 .050 PER SRM 51Mar 9, 1995 · N705DH · Boeing 72722CSDR 96ZZZM389Angle · crackedDURING D-CHECK, FOUND LOWER SUPPORT ANGLE CRACKED IN TWO PLACES FORWARD OF LOWER SPAR LE SPAR LE STATION 130.7. REMOVED FASTENERS PER SRM 51-30-2. REMOVED DAMAGED AREA AT SUPPORT ANGLE PER SRM 51-40-2. FABRICATED NEW SECTION OF SUPPORT ANGLE 17 INCH BY 1 INMar 9, 1995 · N705DH · Boeing 72722CSDR RAAAB295004Angle · crackedDURING SCHEDULED 6C CHECK PER CARD 22004, FOUND RT WING UPPER SPAR ANGLE TO LEADING EDGE RIB BRACKET CRACKED. REPAIRED ANGLE PER SRM 51-40-3. (X)Mar 8, 1995 · N832RV · Boeing 72722CSDR 95ZZZX1446Channel · corrodedDURING HIDDEN DAMAGE INSPECTION OF WINGS, CHANNEL FOUND BAD. PART REPLACED AND WING RETURNED TO SERVICE. RECOMMEND BETTER HEAT TREATING AND CORROSION PROTECTION DURING MANUFACTURE.Mar 8, 1995 · N6444S · Cessna 150HSDR 95ZZZX1445Channel · corrodedDURING HIDDEN DAMAGE INSPECTION OF WINGS, CHANNEL FOUND BAD. PART REPLACED AND WING RETURNED TO SERVICE. RECOMMEND BETTER HEAT TREATING AND CORROSION PROTECTION DURING MANUFACTURE.Mar 8, 1995 · N6444S · Cessna 150HSDR 95ZZZX1444Cap Angle · corrodedDURING HIDDEN DAMAGE INSPECTION OF WINGS, CAP ANGLE FOUND BAD. PART REPLACED AND WING RETURNED TO SERVICE. RECOMMEND BETTER HEAT TREATING AND CORROSION PROTECTION DURING MANUFACTURE.Mar 8, 1995 · N6444S · Cessna 150HSDR 95ZZZX1443Cap Plate · corrodedDURING HIDDEN DAMAGE INSPECTION OF WINGS, CAP PLATE FOUND BAD. PART REPLACED AND WING RETURNED TO SERVICE. RECOMMEND BETTER HEAT TREATING AND CORROSION PROTECTION DURING MANUFACTURE.Mar 8, 1995 · N6444S · Cessna 150HSDR 95ZZZX1442Channel · corrodedDURING HIDDEN DAMAGE INSPECTION OF WINGS, RT CHANNEL FOUND BAD. PART REPLACED AND WING RETURNED TO SERVICE. RECOMMEND BETTER HEAT TREATING AND CORROSION PROTECTION DURING MANUFACTURE.Mar 8, 1995 · N6444S · Cessna 150HSDR 95ZZZX1441Channel · corrodedDURING HIDDEN DAMAGE INSPECTION OF WINGS, CHANNEL FOUND BAD. PART REPLACED AND WING RETURNED TO SERVICE. RECOMMEND BETTER HEAT TREATING AND CORROSION PROTECTION DURING MANUFACTURE.Mar 8, 1995 · N6444S · Cessna 150HSDR 95ZZZX1440Angle · corrodedDURING HIDDEN DAMAGE INSPECTION OF WINGS, RT ANGLE FOUND BAD. PART REPLACED AND WING RETURNED TO SERVICE. RECOMMEND BETTER HEAT TREATING AND CORROSION PROTECTION DURING MANUFACTURE.Mar 8, 1995 · N6444S · Cessna 150HSDR 95ZZZX1439Angle · corrodedDURING HIDDEN DAMAGE INSPECTION OF WINGS, ANGLE FOUND BAD. PART WAS REPLACED AND WING RETURNED TO SERVICE. SUBMITTER RECOMMENDS BETTER HEAT TREATING AND CORROSION PROTECTION DURING MANUFACTURE.Mar 8, 1995 · N6444S · Cessna 150HSDR 95ZZZX1438Channel · corrodedDURING HIDDEN DAMAGE INSPECTION OF WINGS, LT CHANNEL FOUND BAD. PART REPLACED AND WING RETURNED TO SERVICE. RECOMMEND BETTER HEAT TREATING AND CORROSION PROTECTION DURING MANUFACTURE.Mar 8, 1995 · N6444S · Cessna 150HSDR 95ZZZX1424Doubler · crackedFOUND A CRACK IN THE WALKWAY SKIN DOUBLER. AREA IS ALMOST IMPOSSIBLE TO VIEW BECAUSE THERE IS NO INSPECTION OPENINGS IN THIS AREA. CRACK WAS SEEN THROUGH A SMALL RIB CUT OUT AREA. SUBMITTER RECOMMENDS AN INSPECTION PLATE BE INSTALLED IN THIS AREA FOR INSPECMar 8, 1995 · N39954 · Piper PA28161SDR UPS202617Chord · crackedWHILE IN "D" CHECK MAINTENANCE FOUND CRACK ON UPPER CHORD LEFT WING STA 656.5, S-8 VENT BOX, FWD. INSTALLED REPAIR PER SB 727-57-0127.Mar 6, 1995 · N938UP · Boeing 727173CSDR UPS202593Chord · corrodedWHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON VERTICAL FLANGE OF THE 740 CHORD RBL 10-45. INSTALLED REPAIR PER UPS EO B727-5710-6628A AND B727-5710-6763.Mar 6, 1995 · N938UP · Boeing 727173CSDR DL72S950943Spar Stiffener · crackedFOUND DURING F-1 LETTER CHECK, NR 6 SLAT I/B TRACK I/B AND O/B SPAR STIFFENER ANGLES CRACKED 2 INCHES. REPLACED STIFFENERS PER MM 57-20-21 PG 813.Mar 6, 1995 · N489DA · Boeing 727232SDR DL72S950942Stiffener · crackFOUND DURING F-1 LETTER CHECK, NR 6 L/E SLAT O/B TRACK I/B AND O/B SPAR STIFFENER ANGLES CRACKED. REPLACED STIFFENERS PER MM 57-20-21 PG 813.Mar 6, 1995 · N489DA · Boeing 727232SDR COM11809Supports · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01i AND 5720-552/652-01I AT WING RIBS NR 15, 16, AND 18. P/N 120-17056-019, 2 EA; 120-17056-017, 2 EA; 120-17056-015, 4 EA; 120-17056-013, 2 EA; 120-17056-007, 2 EA; 12Mar 6, 1995 · N247CA · Emb EMB120RTSDR 96ZZZM1404Tee Cap · crackedRIGHT WING LOWER TEE CAP CRACKED IN THE RADIUS AFT OF STRINGER 16 EXTENDING UNDERNEATH STRINGER 15 (AD90-18-03 UPDATED TO 96-10-11). REMOVED AND REPLACED STA XCW 58.5 RIGHT AND LEFT TEE CAPS IAW MDC SERVICE BULLETING 57-98 REV 8 DATED 3-15-91 AND WORKORDER NRMar 3, 1995 · N908VJ · Doug DC932SDR 9503866614Chord · corrodedDURING PERIODIC CHECK, THE RIGHT WING LOWER SURFACE MID-SPAR CHORD (STRINGER 10) FORWARD ATTACH FLANGE WAS FOUND CORRODED AT WBL 837-840, JUST OUTBOARD OF THE NR 4 PYLON. STRINGER IS MACHINED FROM 2024-T3511 EXTRUSION PER BAC 1506-2562. MADE REPAIR PER EA 66Mar 3, 1995 · N614US · Boeing 747251BSDR 95ZZZW545Flange · corrodedLEVEL 2 CORROSION, LEFT AUXILLARY TANK UPPER ATTACH FLANGE HAS INTERGRANULAR CORROSION. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1.Mar 1, 1995 · N772CA · Doug DC862SDR UPS202592Doubler · corrodedWHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON WING DOUBLER WS 187 LT. INSTALLED REPAIR PER SRM 57-10-1, 57-10-2, 51-30-00, OHM 20-10-03.Feb 28, 1995 · N916UP · Boeing 72727CSDR UPS202585Chord · crackedWHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CRACK IN FASTENER HOLE IN CHORD RT WING (MRR FILED OPEN).Feb 28, 1995 · N916UP · Boeing 72727C
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