N72825, cancelled Jul 14, 2005

Service difficulty reports · 82

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 = 'N72825' AND deregistration_id = 'N72825-2005-07-14'
  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 CALA0400482Fitting · corrodedINSPECTION FOUND FITTING AT AFT LOWER CORNER OF AFT BAGGAGE BIN DOOR CUTOUT CORRODED. A NEW FITTING WAS INSTALLED IAW SRM 51-30-5.May 8, 2004 · N72825 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0400165Wire · shortedMACH TRIM INOP LIGHT ILLUMINATED AND AIRCRAFT BEGAN TO DUTCH ROLL AT 31,000 FEET EN ROUTE. QRH PROCEDURE COMPLETED, BUT NO CHANGE RESULTED. THERE WAS MINIMUM CONTROL WITH THE RUDDER. THE AIRCRAFT WAS DIVERTED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTEFeb 24, 2004 · N72825 · Doug DC982 · Flight Control System WiringSDR CALA0300021Longeron · crackedINSPECTION FOUND A 1/2" CRACK IN LONGERON 2R AT STA 1418. A SPLICE REPAIR WAS INSTALLED IAW ECRA 5311-01132.Jan 30, 2003 · N72825 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0200485Fire Detector · malfunctionedTHE MID CARGO DET "B" CARGO DETECTION AND SUPRESSION LIGHT ILLUMINATED WHILE AT CRUISE ENROUTE FROM IAH TO ORD. SHORTLY AFTERWARDS THE MASTER WARNING AND CARGO FIRE INDICATION AND FIRE HORN ACTIVATED. BOTH FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS DIVEOct 3, 2002 · N72825 · Doug DC982 · Fire DetectionSDR CALA0200015Bracket · crackedINSPECTION FOUND A 1/2" CRACK IN VERTICAL STABILIZER R/H SIDE SUPPORT BRACKET FOR UPPER FAIRING ABOVE JACKSCREW. A DOUBLER WAS INSTALLED ON THE SUPPORT BRACKET IAW SRM 51-30-2.Jan 11, 2002 · N72825 · Doug DC982 · Vertical StabilizerSDR CALA0200007Hinge · corrodedINSPECTION FOUND LEFT I/B AND O/B VERTICAL STABILIZER HINGE PLATES CORRODED ON MATING SURFACES. NEW HINGE PLATES WERE INSTALLED IAW EA 5530-01238.Jan 9, 2002 · N72825 · Doug DC982 · Vertical StabilizerSDR CALA0200006Hinge · corrodedINSPECTION FOUND RIGHT I/B AND O/B VERTICAL STABILIZER HINGE PLATES CORRODED ON MATING SURFACES. NEW HINGE PLATES WERE INSTALLED IAW EA 5530-01238.Jan 9, 2002 · N72825 · Doug DC982 · Vertical StabilizerSDR CALA0100495Attach Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RT VERTICAL STABILIZER LOWER ATTACH ANGLE, 6 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 53-05.May 23, 2001 · N72825 · Doug DC982 · Fuselage, Stabilizer Attach FittingsSDR CALA0100494Attach Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN LT VERTICAL STABILIZER LOWER ATTACH ANGLE, 7 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 53-05.May 23, 2001 · N72825 · Doug DC982 · Fuselage, Stabilizer Attach FittingsSDR CALA0001243Doubler · corrodedINSPECTION FOUND AFT CARGO THRESHOLD EXTERNAL DOUBLER CORRODED AT FS 1160 - 1205, LONGERON 28R. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-1, 51-30-5, AND ECRA 5310-03027.Aug 7, 2000 · N72825 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001242Cargo Track · corrodedINSPECTION FOUND CARGO TIE DOWN TRACK CORRODED AT FS 1212 - 1220, LONGERON 28R. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-2, AND 51-10-3.Aug 7, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001241Strap · corrodedINSPECTION FOUND AFT LOWER CORNER STRAP OF AFT CARGO DOOR FRAME CORRODED AT STA 1212, L28R. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-30-4.Aug 7, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001240Web · corrodedINSPECTION FOUND AFT PIT TORQUE BOX UPPER WEB CORRODED UNDER CARGO TIE DOWN TRACK AT FS 1212 - 1218 ABOVE LONGERON 28R. THE WEB WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW ECRA 5310-04030, SRM 51-10-4, AND EA 9-5310-2-A0727.Aug 7, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001239Web · crackedINSPECTION FOUND A .5 INCH CRACK ON AFT SIDE OF UPPER WEB IN AFT PIT AT STA 1212, RT SIDE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 53-24-0, FIGURE 11, 51-30-2, AND 51-10-3.Aug 7, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001238Longeron · corrodedINSPECTION FOUND LONGERON 30 CORRODED AT STA 590 - 779. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-30-4, 51-30-2. THE EXISTING DOUBLER, WATER DRAIN, LONGERON SPLICES, FILLET, AND SKIN WERE REMOVED AND REINSTALLED IAW SRM 51-30-2, 51-30-1 AND 5Aug 7, 2000 · N72825 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0001237Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN LT THREAD SUPPORT ANGLE AT FIFTH STEP FROM BOTTOM OF VENTRAL STAIRS. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-30-2. THE VENTRAL STAIRS RETRACTABLE STEPS WERE REMOVED FOR REPAIR AND REINSTALLED IAW MM 52-63-Aug 7, 2000 · N72825 · Doug DC982 · Entrance StairsSDR CALA0001228Web · crackedINSPECTION FOUND LT CUSP WEB CRACKED O/B OF SEAT TRACK AT STA 1174 - 1304, LBL 54. THE CUSP WEB WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5, AND 53-05, FIGURE 16.Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001227Seat Track · corrodedINSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 1174 - 1309. THE SEAT TRACK AND FITTING WERE REMOVED AND A NEW TRACK AND FITTING WERE INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-3, AND 51-10-4.Aug 6, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001226Pan · corrodedINSPECTION FOUND CORROSION AROUND FASTENERS OF FORWARD CARGO DOOR LOWER JAMB PAN. THE CORRODED AREA WAS CUT OUT AND A NEW PAN AND SPLICES WERE INSTALLED IAW SRM 53-05, FIGURE 44.Aug 6, 2000 · N72825 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001225Pan · crackedINSPECTION FOUND THREE RIVET NUTS CRACKED AT FORWARD CARGO DOOR PAN FORWARD LOWER CORNER. THE CRACKS WERE 0.05 INCH LONG. THE CARGO DOOR PAN SECTION WAS REMOVED AND A NEW CARGO DOOR PAN SECTION WAS INSTALLED IAW SRM 51-30-2 AND 52-05, FIGURE 44.Aug 6, 2000 · N72825 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001224Cargo Track · corrodedINSPECTION FOUND RT CARGO TIE DOWN TRACK CORRODED AT STA 522 - 636, L28R. THE TIE DOWN TRACK WAS REMOVED AND A NEW TIE DOWN TRACK WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 51-10-4.Aug 6, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001223Angle · corrodedINSPECTION FOUND RT FLOOR PANEL TRANSITION ANGLE CORRODED AT FS 598 - 636. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-1.Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001222Cargo Track · corrodedINSPECTION FOUND RT CARGO TRACK CORRODED ON UPPER AND LOWER SURFACES IN FORWARD CARGO PIT AT FS 427 - 522. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-2 AND 53-05-4.Aug 6, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001221Skin · dentedINSPECTION FOUND FORWARD SKIN OF AFT CARGO DOOR DENTED. THE DENTED AREA WAS CUT OUT IAW SRM 52-05, FIGURE 3. A DOUBLER, FILLER, AND SHIMS WERE INSTALLED IAW SRM 52-05, FIGURE 3 AND 51-10-3.Aug 6, 2000 · N72825 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001220Stop · gougedINSPECTION FOUND AFT CARGO DOOR STOPS GOUGED. REPAIRED IAW ECRA 5330-02819.Aug 6, 2000 · N72825 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001219Cargo Track · corrodedINSPECTION FOUND FORWARD CARGO PIT LT CARGO TRACK CORRODED ON UPPER AND LOWER SURFACES OF CLIP NUT FLANGES AT FS 370 - 522. THE CARGO TRACK WAS REMOVED AND A NEW CARGO TRACK WAS INSTALLED IAW SRM 51-10-4 AND 53-05, FIGURE 4G.Aug 6, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001218Floor Panel · corrodedINSPECTION FOUND AFT PIT FLOOR PANEL CORRODED AT FS 1212 - 1230. THE FLOOR PANEL WAS REMOVED AND A NEW FLOOR PANEL WAS INSTALLED IAW SRM 53-20, FIGURE 11, 51-10-3, 51-10-4, AND ECRA 5320-01265.Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Floor PanelSDR CALA0001217Intercostal · corrodedINSPECTION FOUND RT INTERCOSTAL CORRODED AT FS 1292 - 1309. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-50-2, 51-10-4, 51-30-2, AND 51-30-5.Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001216Fairing · chafedINSPECTION FOUND UPPER RT HORIZONTAL STABILIZER FAIRING CRACKED AT FORWARD UPPER END AND CHAFING IN THREE AREAS AT FORWARD UPPER END AND DELAMINATION NEAR CENTER OF UPPER EDGE OF FAIRING. THE ANGLE WAS REMOVED AND A REPAIR ANGLE, DOUBLER, AND FILLER WERE INSTAug 6, 2000 · N72825 · Doug DC982 · Horizontal Stabilizer StructureSDR CALA0001215Web · crackedINSPECTION FOUND A .75 INCH CRACK IN TAIL COMPARTMENT FORWARD SIDE OF STA 1485 WEB LT SIDE SKIN. REMOVED WEB IAW SRM 51-30-2 AND STOP DRILLED CRACK IAW SRM 55-01, FIGURE 2. A NEW DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 4, 51-10-4, 51-10-3, AND 51-30.Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001213Skin · dentedINSPECTION FOUND LT AFT FUSELAGE SKIN DENTED AT FS 1497. A NEW SKIN PATCH WAS INSTALLED IAW SRM 53-01, FIGURE 2, 53-34, FIGURE 5, AND 51-60-0.Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001212Structure · gougedINSPECTION FOUND LT HORIZONTAL STABILIZER FORWARD UPPER AND LOWER BARREL NUT HOLES GOUGED. REAMED BARREL NUT HOLES AND INSTALLED BUSHINGS IAW EA 9-5511-2-A0738 AND ECRA 5511-01029.Aug 6, 2000 · N72825 · Doug DC982 · Horizontal Stabilizer StructureSDR CALA0001211Door Frame · bentINSPECTION FOUND LOOSE AND PULLED RIVETS IN FUSELAGE SKIN AND AFT NLG DOOR JAMB WAS BENT AND GOUGED AT STA 110. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51-30-2. THE AFT DOOR JAMB WAS REMOVED AND A NEW DOOR JAMB WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Main, StructureSDR CALA0001210Flange · crackedINSPECTION FOUND A 1 INCH CRACK IN AFT FUSELAGE AC SERVICING PANEL CUTOUT FLANGE. REMOVED AND REPLACED DOUBLER IAW SRM 53-34-0, FIGURE 4, SHEET 1.Aug 6, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001198Web · crackedINSPECTION FOUND A .25 INCH CRACK IN WEB SKIN AT RT SIDE OF TAIL COMPARTMENT STA 1485, JUST FORWARD OF RUDDER TRIM. THE WEB AND ANGLE WERE REMOVED AND THE CRACKED AREA WAS REMOVED IAW SRM 51-30-2 AND 55-01, FIGURE 4. DOUBLERS AND AN ANGLE WERE INSTALLED IAW Aug 2, 2000 · N72825 · Doug DC982 · Vertical StabilizerSDR CALA0001183Pan · crackedINSPECTION FOUND AFT CARGO DOOR PAN CRACKED AT FORWARD UPPER CORNER AND AT APPROXIMATELY 12 INCHES FROM FORWARD UPPER CORNER. THE CRACKS WERE .25 INCH LONG. THE CRACKS WERE STOP DRILLED IAW SRM 52-03, FIGURE 8. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SJul 28, 2000 · N72825 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001168Strap · corrodedINSPECTION FOUND AFT PIT, AFT BULKHEAD, RIGHT SIDE RETAINER STRAP CORRODED AT FS 1338. A NEW RETAINER STRAP WAS INSTALLED IAW SRM 51-10-2, 53-24-0, FIGURE 11, AND 51-10-3.Jul 26, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001167Seat Track · corrodedINSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 807 - 1022, RBL 54. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4F, 51-30-1, 51-30-5, AND 51-60-0.Jul 26, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001166Attach Angle · crackedINSPECTION FOUND A 1.6 INCH CRACK IN L-1 DOOR LOWER FORWARD CORNER SEAL ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND A NEW ATTACH ANGLE WAS INSTALLED IAW SRM 51-30-7, 51-10-4, AND 51-10-3.Jul 26, 2000 · N72825 · Doug DC982 · Passenger/Crew DoorsSDR CALA0001165Strap · corrodedINSPECTION FOUND AFT CARGO BAY FRAME STRAP CORRODED AT STA 1231, LONGERON 28R-30. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-5.Jul 26, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001164Doubler · chafedINSPECTION FOUND AFT CARGO DOOR OUTER LOWER AFT DOUBLER CHAFED. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2.Jul 26, 2000 · N72825 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001162Skin · gougedINSPECTION FOUND THE AFT FUSELAGE SKIN DENTED AND GOUGED AT STA 1320 BELOW NR 2 ENGINE PYLON, LONGERON 19R. THE GOUGE WAS BLENDED IAW SRM 53-01, FIGURE 1, SHEET 3. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 20.Jul 25, 2000 · N72825 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001160Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1212, LONGERON 28L-29R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4.Jul 25, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001159Channel · corrodedINSPECTION FOUND RIGHT O/B FLOOR PANEL HAT CHANNEL CORRODED AT STA 826 - 907, RBL 54. THE HAT CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 53-21-00.Jul 25, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001158Seat Track · corrodedINSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 796 - 946, LBL 54. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-4, 53-05, FIGURE 4F, 51-30-2, 51-30-1, AND 51-10-3.Jul 25, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001157Seat Track · corrodedINSPECTION FOUND LT SIDE CENTER SEAT TRACK CORRODED AT FS 1031 - 1241, LBL 24. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, 51-10-3, AND 53-05, FIGURE 4F.Jul 25, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001156Pan · crackedINSPECTION FOUND A 1.2 INCH CRACK IN MID CARGO DOOR AFT PAN FLANGE ADJACENT TO TORQUE TUBE CAM. THE CRACK WAS STOP DRILLED IAW SRM 52-03, FIGURE 1. THE EXISTING REPAIR DOUBLER WAS REMOVED FOR ACCESS. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A Jul 25, 2000 · N72825 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001155Angle · gougedINSPECTION FOUND L-1 DOOR UPPER AFT LINER ATTACH ANGLE GOUGED. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5.Jul 25, 2000 · N72825 · Doug DC982 · Passenger/Crew DoorsSDR CALA0001154Cargo Track · corrodedINSPECTION FOUND LT CARGO TIE DOWN TRACK CORRODED AT STA 522 - 788, LONGERON 27L. THE CORROSION WAS REMOVED AND FOUND WITHIN LIMITS AT STA 522 - 655 AND STA 684 - 788. THESE SECTIONS WERE ALODINED AND PRIMED IAW SRM 51-10-3 AND 53-01. THE SECTION FROM STA 6Jul 25, 2000 · N72825 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001151Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1155 - 1221, LONGERON 29R. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.Jul 24, 2000 · N72825 · Doug DC982 · Fuselage Miscellaneous Structure
Back to N72825, cancelled Jul 14, 2005