N782FD
Service difficulty reports · 48
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N782FD' AND registry_match = 'registration' 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 n_number = 'N782FD' AND registry_match = 'registration' 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 FDEA202204190992Floorboard · damagedMDIS 782 53-21 5101 23MAR22 ORF FACT U RAMP REPORTED A HOLE IN AFT CARGO COMP FLOOR @STA 1500. HOLE @ 1" OIL 23MAR22 16:19 ORF U NO RESTRICTION REF : SR57-53-001 ONE HOLE IN AFT CARGO FLOOR AT STA 1500 1" IN DIA. TEMP REPAIR INSTALLED SDR FDEA202107291889Slide · detachedWITH THE R2 DOOR IN THE DISARMED POSITION, THE SLIDE/ RAFT FELL OUT OF THE DOOR BUT DID NOT INFLATE. THE GIRD BAR REMAINED ATTACHED TO THE AIRCRAFT EVEN THOUGHT THE DOOR WAS DISARMED. R&R R1 DOOR SLIDE IAW B757 AMM 25-66-01-4.SDR FDEA202107271871Slide · detachedWITH THE R2 (UPDATED TO REFLECT R1) DOOR IN THE DISARMED POSITION, THE SLIDE/ RAFT FELL OUT OF THE DOOR BUT DID NOT INFLATE. THE GIRT BAR REMAINED ATTACHED TO THE AIRCRAFT EVEN THOUGHT THE DOOR WAS DISARMED. R & R DOOR ESCAPE SLIDE IAW AMM 25-66-01-4, ASSISDR FDEA202102230436Adc · failedPDIS 782 34-11 4300 23FEB21 MDT FACT U LOG PAGES: 2980148 FO AIR DATA INSTRUMENTS WENT BLANK DURING TO ROLL. R/I 23FEB21 05:38 MDT U REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: 4040800-912 POS: 2 SRL: 90032121 TAG NBR: 6852G2 ON MPN: 4040800-912 CSDR FDEA202101140097Spring · brokenLT GEAR SPRING RETAINER ASSEMBLY BROKEN AT THE START OF LT GEAR OPERATION CHECK. SDR ENTERED IN ERROR AGAINST WRONG TAIL NUMBER.SDR FDEA2020080711743Intercostal · damagedFUSELAGE SKIN BULGED FROM BS 1420 TO 1440, AT INTERCOSTAL BETWEEN STRINGERS 28R AND 29R. REMOVED, FABRICATED, AND INSTALLED THE NEW INTERCOSTAL IAW DWG 146N5398, REV P, A , DWG 146N5425 REV -, AND SRM 51-40-02-0G. EVALUATED AREA OF DAMAGE AND FOUND HOLES IN SDR FDEA2020080511743Intercostal · unknownFUSELAGE SKIN BULGE FROM BS1420 TO BS1440 AT INTERCOSTAL BETWEEN S-29R AND S-28R. REMOVED FABRICATED AND INSTALLED INTERCOSTAL BETWEEN BS1420-1440 STR28R-29R IAW DWG 149N5398 REV P , A , SRM 51-40-02-0G. EVALUATED AREA OF DAMAGE AND FOUND HOLES IN THE INTERCOSDR FDEA2020080311743Intercostal · damagedFUSELAGE SKIN BULGE FROM BS 1420 TO BS 1440 AT INTERCOSTAL BETWEEN S-29R AND S-28R. REMOVED FABRICATED AND INSTALLED INTERCOSTAL BETWEEN BS1420-1440 STR28R-29R IAW DWG 149N5398 REV P , A , B757 SRM 51-40-02-0G. EVALUATED AREA OF DAMAGE AND FOUND HOLES IN THE SDR FDEA201909052122Floor Panel · puncturedRAMP REPORTED SMALL PUNCTURE IN FLOOR OF AFT CARGO COMPARTMENT. HOLE IS LOCATED AT APPROX STA 1372 RT SIDE APPROX 8 INCHES FWD OF LOWER AFT CARGO DOOR OPENING. COMPLIED WITH EA F-5321-T0349330 PT1. PATCH III INSTALLED OVER PUNCTURE.SDR FDEA2019061321274Circuit Card · failedINTERMITTENT GEAR NOT DOWN WARNING FOR DURATION OF FLIGHT UNTIL GEAR EXTENDED SHGN 11JUN19 16:26 MEM U PERFORMED BITE PROCEDURE FOR PSEU PER 757 FIM 32_09 F/T_802 NO FAULTS STORED. PERFORMED PSEU GROUND TEST FOR SYS #1 AND SYS #2 LDG GEAR SYSTEMS ; BOTSDR FDEA201807101658Skin · dentedDENT ON OUTER FUSELAGE SKIN BETWEEN STA 420 & STA 440 BETWEEN S-17L & S-18L. MEASURED, CUT OUT AND REPAIRED DENTED AREA ON FUSELAGE SKIN IAW SRM 5-40-02-0G, SRM 51-40-05-0G AND SRM 53-00-00-01-2R REPAIR 16.SDR 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 FDEA201606282158Dome Nut · corrodedCABIN L1 DOOR INTERNAL UPPER WEB, 03 EA DOME NUTS FOUND CORRODED.SDR 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 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 FDEA201606141997Frame · gougedAFT CARGO COMPARTMENT, BS 1520, STR 22R-STR 23R. FRAME WEB HAS GOUGE MARKS.SDR FDEA201606131972Stringer · corrodedAFT CARGO COMPARTMENT, STA 1618, STR 21L, STRINGER HAS CORROSION. STRINGER REMOVED AND REPAIR IAW SRM 51-40-02 AND SRM 53-00-03, REPAIR 2, REV 118. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201606091905Frame · corrodedAFT CARGO COMPARTMENT, BS 1460, STR 26R-28L, FRAME WEB CORROSION. R & R WITH NEW FABRICATED FRAME WEB IAW DWG 146N1014, SHT 6 REV D. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201606091896Skin · damagedFUSELAGE RT SIDE, THERE IS A LIGHTNING STRIKE AT BS 680 - BS 700 BETWEEN STR 24- STR 25. LIGHTNING STRIKE REMOVED,
FOUND OUT OF LIMIT IAW SRM 53-00-01, FIG 101, DETAIL II, REV 118. REPAIR CARRIED OUT IAW SRM 53-00-01, FIG 201, REPAIR 15, REV 118. THIS IS ASDR FDEA201606071858Stringer · corrodedAFT CARGO COMPARTMENT STATION 1510 - 1530, STRINGER 29R, STRINGER CORROSION. CORROSION OUT OF LIMITS, R & R WITH NEW STR STA 1460-STA 1620, STR 29R IAW SRM 51-40-02, REV 118 AND DWG 146N3400, SHT 03, REV F IN REF TO JOB CARD N02233 IAW WORK DETAIL ATTACHED. SDR FDEA201606071857Stringer · corrodedAFT CARGO COMPARTMENT STATION 1460 - 1480, STRINGER 29R, STRINGER CORROSION. AFT CARGO COMPARTMENT OUT OF LIMIT, STR STA 1460-STA 1620, STR 29R.
R & R WITH NEW STR STA 1460-STA 1620 IAW SRM 51-40-02, REV 118 AND DWG 146N3400, SHT 03, REV F. REPAIR CLASSIFISDR FDEA201606061855Skin · damagedFUSELAGE RIGHT SIDE THERE IS A LIGHTNING STRIKE AT BS 500 - 520 BETWEEN STRINGER 25 - 26 WITH STICKER 633. LIGHTNING STRIKE MARK REMOVED AREA FOUND OUT OF LIMIT IAW SRM 53-00-01, FIG 201, DET II, REV 118, DEPTH OF CLEAN UP 15 PERCENT MAX, AD REPAIR CARRIED OUSDR FDEA201606061854Skin · damagedFUSELAGE RT SIDE THERE IS A LIGHTNING STRIKE AT BS 480 - 500, BETWEEN STRINGER 25 - 26 WITH STICKER 630. FUSELAGE EXTERIOR SKIN AT BS 480-500, STR 25R-26R LIGHTING STRIKE MARK. REMOVED AREA, FOUND OUT OF LIMIT IAW SRM 53-00-01, FIG 201, DET II, REV 118, DEPTSDR FDEA201606061853Skin · damagedFUSELAGE RT SIDE THERE IS A LIGHTNING STRIKE AT BS 460 - 480, BETWEEN STRINGER 25 - 26 WITH STICKER 613. REMOVED AREA, FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 201, DET II, REV 118, DEPTH OF CLEAN UP 15 PERCENT MAX AND REPAIR CARRIED OUT IAW SRM 53-00-01, FISDR FDEA201606051849Frame · corrodedAFT CARGO COMPARTMENT STATION 1560, STRINGER 30 - 29L, FRAME WEB CORROSION.SDR FDEA201606051848Skin · chafedRIGHT WING OTBD TE MAIN FLAP, NOSE SKIN FOUND CHAFE MARK AT 2.5" FROM OTBD EDGE.SDR FDEA201605311764Channel · damagedCABIN STATION 1720, LBL 65 - RBL 65, DECK PLATE ATTACHED CHORD CHANNEL, FOUND HOLE ELONGATED AFTER DECK PLATE REMOVAL. CHANNEL REMOVED IAW SRM 51-40-02, REV 117. NEW CHORD CHANNEL FABRICATED IAW DWG 146N5317, SHT 1, REV AND INSTALLED IAW DWG 146N5300, SHT 23SDR FDEA201605311763Angle · damagedCABIN STATION 1720, LBL 65 - RBL 65, DECK PLATE ATTACHED CHORD ANGLE, FOUND HOLE ELONGATED AFTER DECK PLATE REMOVAL. CABIN, STA 1720, LBL 65-RBL 65 DECK PLATE ATTACHED CHORD ANGLE WITH ELONGATED HOLE REMOVED IAW SRM 51-40-02, REV 117. NEW CHORD ANGLE INSTALLSDR FDEA201605261739Stringer Splice · corrodedAFT CARGO COMPARTMENT, STATION 1460, STRINGER 28L, STRINGER SPLICE HAS CORROSION. R & R WITH NEW FABRICATED STA 1460, STR 28L, STRINGER SPLICE IAW DWG 146N3400, SHT 02, REV C. NEW STRINGER FABRICATED IAW DWG 146N3820, SHT 01, REV C.SDR FDEA201605261738Frame Splice · gougedAFT CARGO COMPARTMENT, STATION 1520, STRINGER 24R, FRAME SPLICE HAS GOUGE MARKS. FRAME SPLICE REMOVED AND REWORKED AREA TREATED IAW SRM 51-10-02 AND SRM 51-20-01, REV 118. MATERIAL REMOVED 0.027" OUT OF LIMIT. FRAME SPLICE R & R WITH NEW FABRICATED FRAME SPSDR FDEA201605141582Floorbeam · corrodedCABIN STATION 1681, RBL 10 - 47, FLOORBEAM UPPER FLANGE FOUND CORROSION AFTER DECK PLATE REMOVAL. CABIN, STA 1681, RBL 10-47 FLOORBEAM UPPER FLANGE CORROSION REMOVED IAW SRM 51-10-02, REV 117. REWORKED AREA ORIGINAL THICKNESS 0.158" MATERIAL THICKNESS. REMASDR FDEA201605091517Strap · corrodedRIGHT SIDE EMPENNAGE LOWER OUTER HORIZONTAL STAB PIVOT STRAP FOUND CORRODED. PIVOT STRAP REMOVED AND NEW FABRCIATED IAW DWG 182N1608 SHT 1 REV A AND INSTALLED IAW DWG 182N1601 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201605091515Strap · corrodedLEFT SIDE EMPENNAGE LOWER OUTER HORIZONTAL STAB PIVOT STRAP FOUND CORRODED. PIVOT STRAP REMOVED AND NEW FABRICATED IAW DWG 182N1608 SHT 1 REV A AND INSTALLED IAW DWG 182N1601 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201605091516Strap · corrodedEMPENNAGE, RT SIDE, LOWER INNER HORIZONTAL STABILIZER PIVOT STRAP. FOUND CORROSION RT LOWER INNER HORIZONTAL STABILIZER CORRODED PIVOT STRAP REMOVED AND NEW PIVOT FABRICATED IAW DWG NR: 182N1608, SHT 1, REV A AND INSTALLED IAW DWG NR
182N1601, SHT 1, REV C. SDR FDEA201605091514Strap · corrodedEMPANNAGE, LEFT SIDE, LOWER INNER HORIZONTAL STABILIZER PIVOT STRAP FOUND CORROSION LT LOWER INNER HORIZONTAL STABILIZER CORRODED PIVOT STRAP. REMOVED AND NEW PIVOT STRAP FABRICATED IAW DWG NR:182N1608, SHT 1, REV A AND INSTALLED IAW DWG NR 182N1601 SHT, REV SDR FDEA201605071494Intercostal · corrodedCABIN STATION 1621, STRINGER 13L INTERCOSTAL WEB FOUND CORROSION. INTERCOSTAL WEB CORROSION REMOVED IAW SRM 51-12-02 REV 117. FOUND 50% MATERIAL LOSS. INTERCOSTAL WEB R & R WITH FABRICATED WEB IAW SRM 51-40-02 REV 117 & DWG 146N8734 SHT 1 REV C. INTERCOSTSDR FDEA201605041457Deck Plate · corrodedBS 1681 LBL 10 - 17 DECK PLATE UPPER SURFACE FOUND CORRODED. COMPLIED WITH EA F-5310-T0325421 PART 1 P1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201605041453Pan · chafedCABIN L1 DOOR EXTERNAL HANDLE PAN FOUND CHAFED. REMOVED IAW SRM 51-10-02 REV 117. FOUND EXCEEDS LIMIT IAW SRM 52-10-01-1A REV 117. HANDLE PAN REMOVED IAW SRM 51-40-02 REV 117 & REPLACED IAW DWG 141N6100 SHT 8 REV K & SHT 14 REV F. REPAIR CLASSIFIED MAJOR ISDR FDEA201605031445Seat Track · chafedCABIN STATION 1550 - 1570, LBL 24.75 SEAT TRACK CROWN CHAFED. CHAFE REMOVED IAW SRM 51-10-02, REV 117. REWORKED AREA CLEAN UP DEPTH ON THE LIP OF SEAT TRACK CROWN 0.040" AFTER REMOVAL THE MAXIMUM DIAMETER BETWEEN THE LIPS 0.504" EXCEED THE MAXIMUM LIMIT 0.48SDR FDEA201604281420Floorbeam · damagedCABIN STATION 1440, RBL 19, FLOORBEAM UPPER FLANGE FASTENER HOLE ELONGATED. REPAIR CARRIED OUT IAW SRM 53-00-51-2R FIG 201 REPAIR 5 REV 117. REPAIR CLASSIFIED MAJOR IAW GMM.SDR FDEA201604281419Seat Track · damagedCABIN STATION 1316, RBL 45.5, SEAT TRACK OTBD FLANGE HOLE ELONGATED. REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIG 201 OPTION 1 REV 117. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201604281418Seat Track · damagedCABIN STATION 1475, LBL 24.75, SEAT TRACK INBD FLANGE FASTENER HOLE ELONGATED. REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIG 201 REPAIR 1 REV 117. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201604281417Seat Track · chafedCABIN STATION 1590, RBL 45.5 SEAT TRACK INBD FLANGE CHAFED. CHAFE REMOVED IAW SRM 51-10-02, REV 117. REWORKED AREA CLEANED UP DEPTH OF 0.021" MATERIAL ORIGINAL, THICKNESS 0.080" AND REMAINING THICKNESS 0.059" FOUND EXCEED 10 PERCENT LIMIT IAW SRM 53-00-52-1ASDR FDEA201604221350Crease Beam · corrodedCABIN 1360 - 1380 RT CREASE BEAM WEB UPPER SURFACE FOUND CORROSION. CORROSION, REMOVED IAW SRM 51-10-02, REV 117. MATERIAL REMOVED 0.010" FOUND EXCEED LIMIT IAW SRM 53-60-13-1A, REV 117. CORRODED CREASEBEAM WEB. R & R IAW SRM 51-40-02, REV 117 & DWG 146N55SDR FDEA201604221338Crease Beam · corrodedCABIN STATION 940 - 960 RT CREASE BEAM WEB FOUND CORROSION. R & R IAW SRM 51-40-02 REV 117 & DWG 144N5140 SHT 3 REV D. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201604141213Support · crackedCABIN STATION 680 - 698, RBL 24.75, SEAT TRACK SUPPORT FOUND CRACK & CORROSION. COMPLIED WITH EA F-5310-T0325422A PART: 1, P1 TITLE: FUSELAGE, MAINFRAME SEAT TRACK SUPPORT INSTALLATION, BETWEEN STA 640 AND STA 700, RBL 24.75. REPAIR CLASSIFIED AS MAJOR.
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