Boeing 757-232
Service difficulty reports · 15,843
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '757232' 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 aircraft_model_key = '757232' 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 DALA2016032302256Strap · brokenMAIN CABIN FLOORBEAM STABILIZER STRAP BROKEN APPROXIMATELY BS 370-377, LBL 24.5. REMOVED EXISTING REPAIR STRAP, 1 EA AND FILLERS, 2 EA IAW SRM 51-40-01, FABRICATED NEW REPAIR STRAP FROM 7075-T6 .040", PO ST00006369 DIM 12.3750" X 2.3750" AND FILLERS FROM 7075SDR DALA2016032102218Doubler · corrodedPOSSIBLE CORROSION AROUND AFT LAV DUMP CHUTE, FLANGE AREA, VISIBLE FROM AFT CARGO BIN INSIDE SURFACE. REPLACED PAN DOUBLER REF DWG 146N3650. PERFORMED LEAK CHECK ON ALL AFFECTED LINES IAW AMM 12-17-01-301, NO LEAKS NOTED.SDR DALA2016032102217Ball Screw · corrodedLT WING NR 4 FLAP BALLSCREW CORRODED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 080-0001:2751-2538/001 00239 BALL SCREW INSTALLED ON AMDS CARD 2751-2538. UNSUCCESSFUL PARTS CHANGE SENT TO RECORDS 64723.SDR DALA2016032102219Slide · out of toleranceL4 DOOR ESCAPE SLIDE OBSTRUCTING INSTALLATION OF ESCAPE SLIDECOVER. REPLACED SLIDE ON RC 2566-9001-4L.SDR DALA2016032302257Seat Track · not reportedMAIN CABIN SEAT TRACK FROM BS 1075-1180, LBL 45 IS OUT OF LIMITS IAW J/C 2021-2076. R & R OUT OF LIMITS SEAT TRACK AT LBL 45 FROM BS 1075-1180 IAW SRM 51-40-02, 53-40-52, 51-40-05, 51-20-01, AMM 20-60-07-842-001, 51-21-00, AND ENGINEERING DWG DOCUMENT 144N50SDR DALA2016032002215Support · corrodedMAIN CABIN BS 365, RBL 62 SUPPORT BEAM TEE CAP CORRODED. REMOVED CORROSION AT MAIN CABIN BS 365, RBL 67 SUPPORT BEAM TEE CAP IAW SRM 51-10-02 AREA WITH ORIGINAL THICKNESS OF .125 MATT LOSS .017 MATERIAL REMAINING .108 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51SDR DALA2016032202266Connector · unsecureLT EMERGENCY ESCAPE SQUIB LIGHT REMAINS ON. SWAPPED SQUIB TEST PANEL. NO HELP. ORIGINAL REINSTALLED. FOUND CONNECTOR D5530, LT SLIDE BOTTLE PRESSURE LOOSE. RESECURED CONNECTOR SQUIB TEST OK. VERIFIED BOTTLE PRESS OK, REF WDM 25-65-11.SDR DALA2016032302262Lanyard · loose1R SLIDE ARMED LIGHT INTERMITTENT ON WHEN ARMED. DOOR ARMS AND DISARMS OK BUT ARMING HANDLE IS STIFF. FOUND LANYARD AND BUCKLE LOSSE ON SLIDE PACK REPLACED R-1 DOOR SLIDE IAW WC 2566-9001.SDR DALA2016032002214Seat Track · corrodedMAIN CABIN SEAT TRACK FROM BS 1070- 1180, RBL 45 IS OUT OF LIMITS. REMOVED THE SEAT TRACK IAW SRM 51-40-02. LOCATED & DRILLED A NEW SEAT TRACK SECTION IAW SRM 51-40-05 & 53-40-52. TREATED, PRIMED & TOP COATED NEW SECTION OF SEAT TRACK IAW SRM 51-20-01 AND AMSDR DALA2016031802175Battery Pack · inoperativeEMERGENCY LIGHTS ROWS 19-26, INOPERATIVE. R & R THE BATTERY PACK CHARGER IAW AMM 33-51.SDR DALA2016031802174Wire · disconnectedEMERGENCY EXIT SEAT LIGHT ROW 5 RT INOPERATIVE. WIRE ON BACK SIDE OF LIGHT SOCKET HANGING LOOSE. REPLACED LIGHT AND HARNESS, EMERGENCY LIGHT AT 5CD, OPS CHECK GOOD.SDR DALA2016031702171Interphone · inoperativeSERVICE INTERPHONE INOPERATIVE AT NUMEROUS LOCATIONS. TROUBLESHOT AND REPAIRED IAW REF WDM 23-41-12. R & R AUDIO ACCESSORY UNIT IAW 23-42-01.SDR DALA2016031402183Jackscrew · corrodedNR 5 FLAP DRIVE BALL SCREW. JACKSCREW HAS PITTING IN GROOVES OF SCREW AFT END AREA. REPLACED JACKSCREW REF: AMM 27-51-11.SDR DALA2016031402182Jackscrew · corrodedNR 6 FLAP DRIVE JACKSCREW. RUST, BROWN RESIDUE VISIBLE ON BALL SCREW. REPLACED JACKSCREW REF: AMM 27-51-11.SDR DALA2016031402181Universal · corrodedNR 3 FLAP DRIVE AFT UNIVERSAL IS CORRODED. REPLACED U-JOINT AS NECESSARY REF AMM 27-51-17.SDR DALA2016031202056Floor Support · crackedMAIN CABIN INTERCOASTAL CRACKED BETWEEN BS 760-780, BL 0. REMOVED CRACKED ANGLE A BL0 BS 768-780 IAW SRM 51-40-02. FABRICATED NEW ANGLE FROM EXTRUSION, PN: BAC 1430-2721, 7075-T6 PO 651DL-00269 IAW DWG 143N5140, REV: A & BJ. TREATED AND PRIMED THE NEW ANGLESDR DALA2016031502167Shear Web · damagedMAIN CABIN SHEAR WEB HAS SEVERAL ELONGATED HOLES AT BS 760-780, BL 0. REMOVED SHEAR WEB AND FABRICATED REPAIR, INSTALLED REPAIR REF SRM, PRIMED AND TREATED.SDR DALA2016031402061Floor Support · crackedMAIN CABIN INTERCOASTAL CRACKED ON FWD END AT BS 660, RBL 44. REMOVED CRACKED ANGLE AT MAIN CABIN INTERCOASTAL BS RBL 44IAW SRM 51-40-02. FABRICATED AND INSTALLED NEW ANGLE FROM PN BAC1490-2721 7075T6, PO 651DL-00262 IAW DWG 143N5140, REV: D. ALODINED AND PSDR 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.SDR FDEA201603090911Collar · damagedAIRCRAFT L1 DOOR WILL NOT CLOSE. GUST LOCK DOESN’T OPEN, SO DOOR WON’T OPEN. R & R L1 DOOR GUST LOCK COLLAR IAW AMM 52-11-08-8. OPERATIONAL CHECK OF L1 ENTRY DOOR NORMAL, RII PROCEDURES COMPLIED WITH.SDR DALA2016031001830Firewall · wornNR 2 PYLON UPPER FWD OTBD FIRE WALL , OTBD T/R FWD VERTICAL SPRING STEEL STRIKER WEAR PLATE IS EXCESSIVELY WORN. REF N/R 327, ACCOMPLISH SRM 54-51-02, FIG 201, REPAIR OF DAMAGE. ACCOMPLISHED REPAIR IAW SRM 54-51-02, FIG 201, REPAIR 1, ON NR 327.SDR DALA2016031202055Skate Angle · corrodedMAIN CABIN SKATE ANGLE CORRODED BS 1140, RT SIDE CP53-252-01I. REMOVED CORROSION AT BS 1140 RT SIDE SKATE ANGLE EVALUATED AREA WITH ORIGINAL THICKNESS .200 MATERIAL REM .149 MATERIAL LOSS .051 FOUND OUT OF LIMITS IAW SRM 53-40-13, REMOVED ANGLE AT BS 1140 RTSDR DALA2016030801805Bearing · corrodedBEARING RUSTED, NR 2 SLAT OTBD, INBD SUPPORT BEARING HAS RUST COMING OUT OF IT. SUMMARY NR FOR ADDITIONAL INFORMATION 001-0258:2020-2339/008. CLEANED AND LUBED BEARING IAW PS 900-2-1001-0258:2020-2339/008.SDR DALA2016030501796Cusp Web · corrodedUPON REMOVAL OF CORROSION ON CUSP WEB FOUND OTBD CHORD CORRODED AT BS 1602, RBL 65. INSTALLED CUSP WEB BS 1600-1620, CUSP WEB BS 1620-1640, NEW CORD SECTION 2 EA REPAIR ANGLES AND INNER CREASE BEAM SPLICE IAW SRM 51-40-02 AND DWG 146N8722 REV: F.SDR DALA2016030401792Flap Track · corrodedNR 2 FLAP TRACK HAS RUST COMING OUT BETWEEN FLAP TRACK AND WING LOWER SURFACE AT AFT INBD CORNER ATTACH AREA. REPAIRED FLAP TRACK CORROSION IAW CMM 27-51-82. CORROSION IS LEVEL 1. REPAIRED ON NR 85. REMOVED/INSTALLED ON NR 275.SDR DALA2016030501795Cusp Web · corrodedMAIN CABIN CUSP WEB CORRODED BETWEEN BS 1140-1160 LT SIDE. CP53-243-01I. R & R MAIN CABIN CUSP WEB AND DOUBLER BS 1140-1160 LT SIDE IAW SRM 51-40-02 AND DWG 144N5200, REV B.SDR DALA2016030501794Seat Track · damagedMAIN CABIN SEAT TRACK HAS GOUGES AND SCRATCHES BETWEEN BS 900- 1070, LBL 22. R & R MAIN CABIN SEAT TRACK CROWN BS 900-1070, LBL22 IAW SRM 51-40-02.SDR DALA2016030301790Nut · corrodedNR 6 WING FLAP NUT AND SCREW BALL HAS RUST, BROWN RESIDUE ON BALLSCREW. REPLACED NR 6 WING FLAP BALL SCREW REF AMM 27-51-21.SDR DALA2016030301787Floorbeam · corrodedMAIN CABIN FLOORBEAM T-CAP CORRODED BS 1640, LBL 60-RBL 60.SDR DALA2016030101657Skin · dentedRT WING NR 6 SLAT, PROTRUDED DENT 17" FROM INBD SIDE. EVALUATED RT WING NR 6 SLAT 17" FROM INBD SIDE IAW SRM 57-43-02, FIG 101, PGS 101-105 AND FOUND DENT TO BE OUT OF LIMITS. TAP TESTED TYPE A L/E T/E WEDGE AND FOUND NO DEFECTS IAW SB 757-57-0066. APPLIED PSDR DALA2016030101656Skin · dentedRT WING, NR 6 SLAT CENTER SECTION OF T/E WEDGE HAS A DENT 2 X 2 INCHES. EVALUATED RT WING NR 6 SLAT CENTER SECTION OF T/E WEDGE IAW SRM 57-43-02, FIG 101, PGS 101-105 AND FOUND DENT TO BE OUT OF LIMITS. TAP TESTED TYPE A L/E T/E WEDGE AND FOUND NO DEFECTS ISDR DALA2016022901655Skin · corrodedLT EXTERIOR FUSELAGE HAS BULGE ON FRAME BS 640 BETWEEN S17-S18L. EVALUATED BULGE ON FRAME 640 BETWEEN S17-18L, L=.040, W=1.10. ASSET 0018677. REMOVED PREVIOUS REPAIR AND CUT OUT DAMAGE AREA . FABRICATED REPAIR DOUBLER AND FILLER FROM 2024T3 .063. PO ST- 0SDR DALA2016031402060Light · misinstalledL4 DOOR SLIDE POWER PACK, PN 64062-1, NON-LED LIGHT, HAS 1 BLUE WIRE AND 1 WHITE WIRE INDICATING & LED POWER PACK. IAW ERA 523270-14, REV O. IF WIRE COLORS ON SLIDE SIDE, ARE WHITE AND BLUE THEN MAINTENANCE ACTIONS MUST BE TAKEN TO REPLACE PN 64062-1 BATTERY PSDR DALA2016031402059Light · misinstalledR4 DOOR SLIDE POWER PACK, PN 64062-1, NON-LED LIGHT HAS 1 BLUE WIRE AND 1 WHITE WIRE INDICATING A LED POWER PACK. IAW ERA 523270-14, REV O. IF WIRE COLORS, ON SLIDE SIDE, ARE WHITE AND BLUE THEN MAINTENANCE ACTIONS MUST BE TAKEN TO REPLACE, PN 64062-1 BATTERYSDR DALA2016022901569Light · inoperativeL2 DOOR SLIDE INDICATOR LIGHT INOPERATIVE OR DAMAGED. CLEANED & LUBED SWITCHES & TARGETS. OPS CHECKED GOOD.SDR DALA2016032402336Nut · corrodedNR 5, FLAP TRANSMISSION BALL SCREW NUT ASSY HAS PITTING IN GROOVE. REPLACED NR 5 FLAP TRANSMISSION BALL SCREW NUT ASSY IAW AMM 27-51, REFER TO NR00086.SDR DALA2016031402058Light · misinstalledR2 DOOR SLIDE POWER PACK, PN 64062-1, NON-LED LIGHT INSTALLED. WIRES ROUTED FROM LIGHT ARE BLUE AND WHITE INDICATING LED LIGHT INSTALLED IAW ERA523270-14, REV O. WIRE COLORS, ON SLIDE SIDE ARE WHITE AND BLUE THEN MAINTENANCE ACTIONS MUST BE TAKEN TO REPLACE PSDR DALA2016022801621Floor Support · corrodedMAIN CABIN AFT WET AREA FLOOR SUPPORT CORRODED BETWEEN BS 1640-1660, LBL 60.SDR DALA2016022801620Floor Support · corrodedMAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1600-1681, LBL 60. R & R THE FLOOR SUPPORT IAW SRM 51-40-02.SDR DALA2016022601467Skin · damagedDOUBLER REPAIR INSTALLED ON THE AFT CARGO DOOR AS ACCOMPLISHED ON JC NR 60, LOG 6528906, REF SRM 52-30-01, REPAIR 4, REF J/C NR 60 & LOGPAGE 6528906, PERMANENT MAJOR REPAIR INSTALLED ON LWR SKIN SECTION OF THE AFT CARGO DOOR REQUIRE A THRESHOLD INSPECTION ATSDR DALA2016022301465Skin · dentedERA383903-14AD, REV E FS 520 TO FS 550/S14L TO S16L, LT SKIN DENTS & FS 540 FRAME SHEAR TIE CRACKED AD2001-20-12 - RESTRICTION 2. ERA INI CYC ACTL/2110 CONVERTED TO SCEPTRE ON 09OCT13 03:51 UTC AD NR FROM ACTL 2001-20-12, ENG ACTL AD NR DOES NOT HAVE ASSOCIATSDR DALA2016022401373Lens · missingEMERGENCY WHITE LIGHT ARROW 4C LENS NOT INSTALLED. INSTALLED LIGHT LENS AMM 33-51.SDR DALA2016032102177Ballscrew · corrodedNR 4 FLAP DRIVE BALLSCREW. RUST/BROWN RESIDUE IS VISIBLE AT UPPER AND LOWER BUSHING AREAS. R & R BALLSCREW IAW AMM.SDR DALA2016022401433Frame · crackedWHILE REMOVING GROUND STUD AT FS 460 BETWEEN STR 4L & 5L. FOUND CRACKS COMING FROM HOLE IN FRAME. REPAIRED FRAME AT S.460 BETWEEN STR 4L & 5L IAW SRM 53- 00-07, FIG 202. REQUIRES DETAILED VISUAL INSP AT 37,5000 FLIGHT CYCLES FROM REPAIR INSTALLAION OR 50,000 SDR DALA2016022401374Lamp · inoperative36C EMERGENCY ROW LIGHT INOPERATIVE. SECURED AND RELAMPED LIGHT ASSY IAW MM 33-51.SDR DALA2016022401372Bulb · inoperativeSEAT ASSY 26DEF EMERGENCY LIGHT ON SEAT ASSY INOPERATIVE. R & R BULBS IAW AMM 33-51.SDR DALA2016022501432Skin · damagedFOUND FASTENER ON LT WINGLET IN ZONE 6, T/E WITH LIGHTNING STRIKE DAMAGE. REMOVED DAMAGED FASTENER IAW SRM BLENDED WINGLET SUPPLEMENT 57-31-01, REPAIR 1. WILL REQUIRE FASTENER REPLACEMENT WITHIN 10 FLIGHTS AND 20 HOURS. SEALED IAW FIG 102. C/W PERMANENT REPSDR DALA2016022301347Doubler · crackedCRACK INDICATION ON EXTERNAL DOUBLER AT BS 954 BETWEEN STR 14R-15R, POSSIBLE FRETTING/INTERGRANULAR CORROSION. ACCOMPLISHED BLEND OUT OF DEFECTS ON EXTERNAL DOUBLER AT BS 954 BETWEEN STR 14R-15R IAW ERA 472309-14, REV C, PERFORMED LFEC INSP OF AREA IAW NDTM SDR DALA2016022901834Skin · dentedDENT AT AFT CARGO DOOR REPORTED BY GROUND CREW IAW SRM 52-30-01 DENT IS WITHIN LIMITS. AN EXAMINATION OF THE DENT IS MADE EVERY 300 FLIGHT CYCLES. C/W INSPECTION OF CARGO DOOR DENT IAW SRM 52-30-01, NO FURTHER DAMAGE NOTED OK TO CONTINUE ON MON. TRIMMED-OUTSDR DALA2016022501431Control Rod · corrodedCORROSION ON RT ELEVATOR CONTROL ROD WHICH ATTACHES ELEVATOR CONTROL MECHANISM IN AFT EQUIPMENT ACCESS TO INBD CONNECTING LINK AT INBD END OF RT HORIZONTAL STABILIZER ACCESS NR 345AB. ROD END. R & R RT ELEVATOR CONTROL ROD IAW AMM-27-31-15/20-11-00, ASSET 00
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