Boeing 757-222
Service difficulty reports · 15,539
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 = '757222' 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 = '757222' 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 FDEA201608022739Skin · chafedRIGHT WING-OTBD T/E MAIN FLAP NOSE SKIN LE FOUND CHAULK MARK AT 3" FROM OTBD EDGE. COMPLIED WITH PART 1 OF EA F-5750-T0327084. RT WING OTBD MAIN FLAP ASSY, CHAFE DAMAGE FOUND ON L/E OTBD SKIN WBL 557. REPAIR CLASSIFIED AS MAJORSDR FDEA201608012698Fitting · corrodedBS 1080 LT CREASE BEAM INNER SPICE FITTING FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02-0G, REV 118.0 AND FOUND EXCEED LIMIT IAW SRM 53-40-12-1A, REV 118.0 FITTING. REMOVED IAW SRM 51-40-02-0G, REV 118.0 AND REPLACED IAW DWG 144N5200, SHT 1, REV B WITHSDR FDEA201607312684Skin · damagedEXTERIOR SKIN, NUMEROUS SMALL NICKS AND SCRATCHES ALONG THE BELLY OF THE ACFT BETWEEN STR 26 LT AND 26 RT AT BODY STA 620-STA 640. STA 620-STA 640, STR 26L-26R EXTERIOR SKIN NUMEROUS NICKS AND SCRATCHES REMOVED IAW SRM 51-10-02, REV 118. FOUND WITHIN LIMIT IASDR FDEA201607302661Web · corrodedBS 960 - 984 LT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02-0G REV 118.0 & FOUND OUT OF LIMITS IAW SRM 53-40-13-1A REV 118.0. CREASE BEAM WEB REMOVED AND REPLACED IAW SRM 51-40-02-0G REV 118.0 AND DWG 144N5140 SHT 3 REV D. REPAIR CLASSDR FDEA201607302663Web · corrodedBS 1400 - 1420 RIGHT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 118. FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A REV 118. CREASE BEAM WEB REMOVED IAW SRM 51-40-02 REV 118. A NEW CREASE BEAM WEB INSTALLED IAW DWG 146N5590 SHTSDR FDEA201607302662Shear Web · corrodedBS 960 - 984, RIGHT SHEAR WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 118. FOUND OUT OF LIMITS IAW SRM 53-40-12-1A REV 118. THE SHEAR WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 118, AND DWG 144N5140 SHT 3 REV D. MAJOR REPAIR.SDR FDEA201607282644Seat Track · chafedBS 1460 - 1480 LBL 24.75 SEAT TRACK CROWN CHAFED. SEAT TRACK REPAIR CARRIED OUT BETWEEN STA 1410-1540 LBL 24.75 IAW SRM 53-00-52-2R OPTION 1, REPAIR 1, REV 118.0. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201607282643Seat Track · chafedBS 1430-1450 LBL 24.75 SEAT TRACK CROWN CHAFED. CHAFE REMOVED IAW SRM 51-10-02-0G REV 118.0. REWORKED AREA MAXIMUM DISTANCE BETWEEN LIPS 0.510" EXCEEDED MAXIMUM LIMT 0.480" IAW SRM 53-00-52-1A, REV 118.0. SEAT TRACK REPAIR CARRIED OUT BETWEEN STA 1410-STA 1SDR FDEA201607282642Crease Beam · corrodedBS 982 - 983 LEFT CREASE BEAM INNER ANGLE VERTICAL FLANGE FOUND CORRODED. REMOVED IAW SRM 51-10-02-0G, REV 118.0. REWORKED AREA EVALUATED AND FOUND CORROSION MORE THAN 50 PERCENT THRU EXCEEDED 10 PERCENT LIMIT IAW SRM 53-40-13-1A, REV 118.0 INNER CHORD REMOVSDR FDEA201607282641Crease Beam · corrodedBS 1360 - 1380 RT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW
SRM 51-10-02-0G, REV 118.0. REWORKED AREA EVALUATED ORIGINAL THK 0.040", REMAINING THICKNESS 0.026" AND MATERIAL THICKNESS REMOVED 0.014". FOUND EXCEED 10 PERCENT LIMIT IAW SRM 53-60-SDR FDEA201607282640Crease Beam · corrodedBS 1100 - 1120 LEFT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02-06, REV 118.0. ORIGINAL MATERIAL THICKNESS 0.063", REMAINING THICKNESS 0.044" AND MATERIAL THICKNESS REMOVED 0.019". FOUND EXCEEDED 10 PERCENT, LIMIT IAW SRM 53-40-13-1A,SDR FDEA201607282639Deck Plate · corrodedBS 1681 LBL 18 AFT DECK PLATE UPPER SURFACE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02-0G, REV 118.0. REWORK AREA ORIGINAL THICKNESS 0.071", REMAINING THICKNESS 0.044" AND MATERIAL THICKNESS REMOVED IS 0.027", FOUND EXCEEDED LIMIT IAW SRM 53-60-51-1SDR CALA2016072900467Light · inoperative2R SLIDE LIGHT INOPERATIVE. RELAMPED LIGHT, OPS CKS GOOD.SDR FDEA201607272633Stringer · corrodedAFT CARGO BAY STRINGER 30L CORRODED ON INBD SIDE BS 1420 - 1440. REMOVED CORROSION IAW SRM 51-10-02-0G, AREA WAS FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-03-1A, FIG 101 DET. II, REPAIRED STRINGER IAW SRM 53-00-03-2R FIG 201. MAJOR REPAIR.SDR CALA2016072995598Frame · corrodedCORROSION ON FRAME BS 1680, BL 0 JUST FWD OF AFT WASTE PAN. R & R THE FRAME IAW DWG 146N1032 AND SRM 51-40-05,PAR.4 FIG.2 AND 51-10-02,PAR.4 & 7, FIG.3,8,12 AND DWG 146N1025SDR CALA2016072595586Skin · gougedRIGHT FUSELAGE BS 660 AFT OF FWD CARGO DOOR HAS SMALL GOUGE IN SKIN. REPAIRED IAW ECRA 5330-05753.SDR FDEA201607252611Frame · corrodedAFT CARGO BAY, BS 1380 STRINGER 28L TO 29R FRAME WEB CORRODED. FRAME OUT OF LIMITS. R & R WITH NEW FABRICATED FRAME WEB STR 28R-STR 24L IAW DWG 146N1010, SHT 3, REV C. NEW FRAME WEB FABRICATED IAW DWG NR 146N1028, SHT 09, REV C. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201607222598Tee Fitting · corrodedAFT CARGO ENTRANCE DOOR SURROUND SUPPORT TEE FITTING UNDERNEATH SURFACE FROM BS 1380 - 1440 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02-0G. FOUND TO BE OUT OF LIMITS, NO ALLOW DAMAGE LIMITS IN SRM. REMOVED AND REPLACED WITH NEW IAW DWG 146N8522 & SRM SDR FDEA201607202550Skin Panel · delaminatedRIGHT WING INBD TE MAIN FLAP INTERIOR UPPER INTERSPAR PANEL LOWER SURFACE FOUND DELAMINATED AT WFS 180. COMPLIED WITH PART 1 EA F-5750-T0327826, TITLE: WING FLIGHT SURFACES SRM REPAIRS ON RT WING INBD MAIN FLAP UPPER BONDED SKIN OUTER & INNER FACESHEETS, STA SDR FDEA201607202548Skin · dentedLEFT WING INBD MAIN FLAP UPPER OTBD PANEL UPPER SURFACE FOUND DENTED AND DELAMINATED AT 15" FROM OTBD EDGE, 10" FROM T/E. REPAIR CARRIED OUT IAW SRM 51-70-10-2R, REV 118.0, SEE PART 1 OF EA F-5750-T0327752. REPAIR TO UPPER SKIN PANEL, MULTIPLE REPAIRS TO BONSDR FDEA201607202546Skin · dentedLEFT WING INBD MAIN FLAP UPPER OTBD PANEL UPPER SURFACE FOUND DENTED AND DELAMINATED AT 59.5-62.5" FROM OTBD EDGE, 6-11" FROM T/E. REPAIR CARRIED OUT IAW SRM 51-70-10-2R, REV 118.0, SEE PART 1 OF EA F-5750-T0327752. REPAIR TO UPPER SKIN PANEL, MULTIPLE REPAISDR FDEA201607202542Door Sill · corrodedBS 690 - 730 L2 DOOR CUTOUT LOWER SILL INNER FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02-0G, REV 118.0. REWORKED AREA EVALUATED AND FOUND CORROSION MORE THAN 50 PERCENT THRU, EXCEEDED LIMIT IAW SRM 53-30-15-1A, REV 118.0. INNER CHORD REMOVED BETWEEN SSDR CALA2016072195570Control Module · malfunctionedABORTED TAKEOFF APPROACHING 125 KTS DUE TO SPOILER ALERT MESSAGE. REQUESTED FIRE/RESCUE FOR HOT BRAKES, TOWED TO GATE REPLACED SPOILER CONTROL MODULE 1R IAW MM 27-09-00, ACCOMPLISHED TAKEOFF CONFIG WARNING CARD MODULE TEST, AND LANDING CONFIG WARNING CARD MODSDR FDEA201607182506Frame · corrodedAFT CARGO BAY BS 1701 BETWEEN S29L - 29R, FRAME HAS CORROSION. REMOVED CORROSION ON THE FRAME IAW SRM 51-10-02-0G. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101 DET V. REMOVED & REPLACED THE FRAME IAW SRM 51-40-02-0G & DWG 146N1020. MAJOR REPAIR.SDR FDEA201607152463Frame · corrodedAFT CARGO BS 1661 S27 - 29L FRAME HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02-0G ORIGINAL MATERIAL 0.063 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A, FIG 101 .01" LOSS DET II R & R FRAME AT STA 1661 IAW SRM 51-40-02-0G AND DWG 146N1024, FROM S24L-S24RSDR FDEA201607152459Strap · corrodedEMPENNAGE AFTER REMOVAL OF APU INLET DOOR FOUND STRAP AT BS 1825 BETWEEN S3 - 6R CORRODED. REMOVED FOUND OUT OF LIMIT IAW SRM 53-80-15-1A, FIG 101, TABLE 101, REV 118.0 AND REPAIR CARRIED OUT IAW SRM 53-80-15-2R, FIG 202, DETAIL 1, REV 118.0. REPAIR CLASSIFISDR FDEA201607152458Strap · corrodedEMPENNAGE, AFTER REMOVAL OF APU INLET DOOR FOUND STRAP AT BS 1787 BETWEEN S3 - 6R WITH CORROSION. CORROSION OUT OF LIMITS IAW SRM 51-10-02-0G, REV 118.0. THOUGH STRAP REMOVED AND NEW STRAP FABRICATED IAW DWG NR 148N3138, SHT 1, REV C AND INSTALLED IAW DWG NRSDR FDEA201607152457Angle · corrodedAFTER REMOVAL OF APU INLET DOOR FOUND STRAP BETWEEN BS 1787 - 1825 AT STRINGER 6R WITH CORROSION. CORROSION OUT OF LIMITS IAW SRM 51-10-02-0G, REV 118.0. THRU ANGLE R & R WITH NEW ANGLE, PN 148N3152-1 IAW DWG NR 148N3105, SHT 1, REV C. REPAIR CLASSIFIED AS SDR FDEA201607152456Angle · corrodedAPU INLET DOOR CUTOUT INLET DOOR INBOARD STRAP FOUND CORRODED. APU INLET DOOR CUT-OUT STA 1787-1825, STR 3R INBD STRAP ANGLE, FOUND CORROSION OUT OF LIMIT IAW SRM 51-10-02-0G, REV 118.0, CORROSION THRU ANGLE. R & R WITH NEW ANGLE, PN: 654N0244-620 IAW DWG NRSDR FDEA201607152454Frame Splice · gougedAFT CARGO, BS 1520 STRINGER 24R FRAME SPLICE GOUGED. R & R WITH NEW FABRICATED FRAME SPLICE IAW DWG NR 146N1017, SHT 4, REV B. NEW FRAME SPLICE FABRICATED IAW DWG NR 146N1042, SHT 04, REV B. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201607142448Motor · failedAT CRUISE ALT OF 35,000 FEET LOST TEMPERATURE CONTROL OF COCKPIT SHORTLY AFTER WE EXPERIENCED A LOSS OF PRESURIZATION. CABIN ALTITUDE WARNING LIGHT ILLUMINATED. EMERGENCY DESCENT INITIATED AT 10,000 FT. PRESSURIZATION RETURNED AND IT WAS ABLE TO CONTROL CABINSDR FDEA201607142445Skin Panel · dentedDENT ON EXTERNAL FUSELAGE BS 422 AND ABOVE STR 24R FURTHER DENT EVALUATION, IT WAS FOUND OUT OF LIMITS IAW SRM 53-00-01-1A, FIG 101, DETAIL III, A/Y=7.8. THE SKIN WAS REPAIRED IAW SRM 53-00-01-2R, FIG 201, REPAIR NR 7 AND SRM 51-40-02. MAJOR REPAIR, CAT-B.SDR FDEA201607142443Floorbeam · corrodedCABIN - FLOORBEAM WB AT STA 1681, RBL 52 FOUND CORRODED AFTER SHEET METAL PTF CLIP REMOVAL. CORROSION EVALUATED AND FOUND MORE THAN 50 PERFORMED THROUGHOUT OF LIMIT IAW SRM 53-00-51-1A, REV 118.0. FLOORBEAM REMOVED AT STA 1681, RBL 70-LBL 70 IAW SRM 51-40-02SDR FDEA201607132439Pump · failedON CLIMBOUT AT 11,500 FT AND OIL TEMP WENT INTO YELLOW BAND FOR APPROX 2 MINUTES COMPLIED WITH RED TABS, BROUGHT POWER BACK AND TEMP DECREASED BELOW YELLOW. WHILE CLIMBING: LT OIL PRESSURE 170, LT OIL TEMP 137, RT OIL PRESSURE 130, RT OIL TEMP 161 AT FLIGHT ISDR FDEA201607072300Frame · corrodedAFT CARGO BAY, BS 1400 STRINGERS 29R - 29L FRAME WEB CORRODED, BOTH FRONT AND AFT SURFACE. FRAME REMOVED AND REPLACED IAW DWG 146N1011 SHT 3 REV E. FRAME FABRICATED IAW DWG 146N1028 SHT 8 REV D. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201607012208Web · corrodedAFT CARGO BAY, BS 1460-1480 CARGO DOOR LOWER SILL WEB CORROSION. SILL WEB R&R WITH NEW FABRICATED STA 1460-1480 CARGO DOOR SILL LOWER SILL WEB IAW DWG 146N8522, SHT 7, REV C. NEW LOWER SILL WEB FABRICATED IAW DWG 146N8522-42, SHT 7, REV C. REPAIR CLASSIFIEDSDR FDEA201606292191Frame · dentedLOWER FUSELAGE STA 231, BL0 FRAME HAS A DENT. TRIMMED OUT DAMAGED AREA ON FRAME BS 231.25 BL0. FABRICATED REPAIR ANGLE. INSTALLED REPAIR CW EA F-5310-T0326376 P1. THIS IS A MAJOR REPAIR. PERFORMED SATISFACTORY FUNCTIONAL OPS CHECK OF FWD ACCESS DOOR IAW SDR FDEA201606292196Frame Splice · gougedAFT PIT STA 1520, S25R FRAME SPLICE GOUGED. REMOVED DAMAGE IAW SRM-51-10-02-0G, FOUND TO BE OUT OF LIMITS IAW, SRM-53-00-07-1A FIG 101, DET V. R & R SPLICE IAW-SRM-51-40-02-0G AND DWG 146N1017. REPAIR CAT-A, MAJOR REPAIR AT STA 1520, S-25R.SDR FDEA201606292194Stringer · corrodedFWD CARGO PIT, STR 22L CORRODED BETWEEN FRAME BS 700-720. REMOVED CORROSION IAW SRM-51-10-02-0G, NO ALLOWABLE DAMAGE IAW SRM. FABRICATED AND INSTALLED STRINGER FILLER AND HAT SECTION REPAIR, STA 660-STA 752, S22L IAW-SRM-53-00-03-2R, REPAIR 2, CAT-A, REPAIR.SDR FDEA201606292193Skin · chafedRT WING, OTBD FLAP, BOTTOM SKIN CHAFED AT INBD CORNER. CHECK LIMITS, FOUND OUT OF LIMITS IAW SRM-57-53-01-1A, PG 7, FIG 101, DET VI. R & R SKIN PANEL 113N3500Y24 AT RT WING, OTBD FLAP INBD IAW SRM-51-40-02-0G AND DWG 113N3500, CAT-A , MAJOR REPAIR.SDR FDEA201606282160Frame Splice · gougedAFT PIT STA 1520, FRAME SPLICE S24R GOUGED. R & R SPLICE FRAME AT STA 1520, STR 24R, IAW-SRM-51-40-02-0G AND DWG 146N1017, THIS IS A CAT A REPAIR. REMOVED GOUGES IAW-SRM-51-10-02, ORIGINAL MATERIAL .071, REMAINING .041, OUT OF LIMITS IAW SRM-53-00-07-1A, FIGSDR FDEA201606272154Skin · chafedRT WING, UPPER INTERSPAR SKIN, UPPER SURFACE FOUND CHAFE MARK AT WBL 76-78, 20" LONG FROM SKIN T/E, WING TO BODY FAIRING MATING AREA. MINOR CHAFE MARK BLEND OUT ON 112N3101-12, AFT MACHINED SKIN AT APPROX WBL 76.00 TO 78.00. TRACE FROM REAR SPAR TO STRINGER SDR FDEA201606242135Skin · damagedSCRIBE LINE DAMAGE FOUND AT LAP SEAM S-14R, BS 777 TO BS 779. COMPLIED WITH EA F-5330-T0325500, PT 1: FUSELAGE, PLATES AND SKINS, SECTION 43- SCRIBE LINE INSPECTIONS, STR S-14R, BS 777.032 TO BS 778.99, 1.65" LG. CLASSIFIED AS A CAT B MAJOR REPAIR.SDR FDEA201606242134Frame · corrodedAFT CARGO COMPARTMENT, STA 1480, STR 27R-26R, FRAME WEB CORROSION FOUND AFTER ATTACHED ANGLE REMOVED.SDR FDEA201606212075Stringer Splice · corrodedAFT CARGO BAY BS 1460 STRINGER 30 STRINGER SPLICE HAS CORROSION. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW DWG 146N3400 SHT 2 REV C. STRINGER SPLICE FABRICATED IAW DWG 146N3820 SHT 01 REV C. REPAIR CLASSIFIED AS MAJOR.SDR CALA2016062295473Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER CHORD CORRODED AT BS 1640 BETWEEN BL0 AND RBL 24.75. REMOVED CORROSION AND FOUND BLEND OUT EXCEED SRM LIMITS. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED NEW UPPER CHORD SPLICE. REPAIR CHORD FROM RBL63-LBL 24.75 REF ECRA 531SDR CALA2016062295472Stringer · corrodedLOWER LOBE AT BS 1642, STR S-22R WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED STR SECTION FROM BS1620-1652. ACP HFEC INSPECTION OF OPEN FASTENER HOLES. NO CRACKS FOUND. FABRICATED AND INSTALLED STR SPLICE REPAIR REF SRM 53-00-03, REPAIR 1.SDR FDEA201606192068Collar · failedGUST LOCK CRACKED ON L1 FWD ENTRY DOOR. REMOVED L1 DOOR HOLD OPEN LOCK COLLAR AND INSTALLED NEW SPLIT COLLAR IAW AMM 52-11-08-8. OPS CHECK NORMAL ON GROUND.SDR CALA2016062295465Skin · puncturedR-4 DOOR INNER SKIN WAS FOUND PUNCTURED NEAR UPPER HINGE. FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR REF ECRA 5210-02732.SDR CALA2016061795461Slide · unwanted deployDURING OPERATION OF DOOR, 1R SLIDE INADVERTENTLY DEPLOYED. R & R DOOR 1R ESCAPE SLIDE UP TO STEP 3, E 13, REF AMM 25-66-01.
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