# Service difficulty reports: N32725, cancelled Jan 17, 2018 A list on [N32725, cancelled Jan 17, 2018](https://openairdocs.org/deregistered/N32725-2018-01-17.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 100 reports - [SDR CALA9901311](https://openairdocs.org/sdr/CALA9901311.md): Wire · broken · Oct 4, 1999 · N32725 · Boeing 727224 · Light System Wiring > INSPECTION FOUND THE EMERGENCY EXIT LIGHT AT R-1 DOOR INOPERATIVE. REPAIRED GROUND WIRE AND POWER WIRE AND OPERATION CHECKED GOOD IAW MM 33-50-1. - [SDR CALA9901312](https://openairdocs.org/sdr/CALA9901312.md): Connector · loose · Oct 2, 1999 · N32725 · Boeing 727224 · Emergency Lighting > INSPECTION FOUND EMERGENCY EXIT LIGHT AT L-1 DOOR INOPERATIVE. RESEATED CONNECTOR PLUG TO LIGHT AND OPERATION CHECKED GOOD IAW MM 33-51-02, PAGE 501. - [SDR CALA9901310](https://openairdocs.org/sdr/CALA9901310.md): Battery · discharged · Sep 30, 1999 · N32725 · Boeing 727224 · Emergency Lighting > INSPECTION FOUND RT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RECHARGED THE BATTERY AND OPERATION CHECKED GOOD IAW MM 33-60-01, PAGE 201. - [SDR CALA9901309](https://openairdocs.org/sdr/CALA9901309.md): Terminal · broken · Sep 30, 1999 · N32725 · Boeing 727224 · Emergency Lighting > INSPECTION FOUND THE R-2 DOOR EXIT SIGN INOPERATIVE. REPAIRED TERMINAL AT SOCKET AND OPERATION CHECKED GOOD IAW MM 33-53-01, PAGE 201. - [SDR CALA9900877](https://openairdocs.org/sdr/CALA9900877.md): Light · inop · Jul 27, 1999 · N32725 · Boeing 727224 · Emergency Lighting > INSPECTION FOUND THE SEAT MOUNTED EMERGENCY EXIT PATH LIGHT AT ROW 30 INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED. - [SDR CALA9900851](https://openairdocs.org/sdr/CALA9900851.md): Power Supply · inop · Jul 22, 1999 · N32725 · Boeing 727224 · Emergency Lighting > INSPECTION FOUND THE FORWARD ENTRY AND FORWARD GALLEY ESCAPE SLIDE EMERGENCY LIGHTS INOPERATIVE. THE BATTERY AND POWER SUPPLY IN E&E COMPARTMENT WAS REMOVED AND REPLACED. - [SDR CALA9802116](https://openairdocs.org/sdr/CALA9802116.md): Batteries · discharged · Nov 25, 1998 · N32725 · Boeing 727224 · Emergency Lighting > THE R-1 DOOR INTERIOR OVERHEAD LIGHT WOULD NOT TEST. THE BATTERIES WERE REPLACED IAW MM 33-50-101 AND OPERATION CHECKED GOOD. - [SDR CALA9801989](https://openairdocs.org/sdr/CALA9801989.md): Cables · out of adjust · Oct 23, 1998 · N32725 · Boeing 727224 · Landing Gear Door Retract Section > A LOUD EXTERNAL RUMBLE WAS HEARD ACCOMPANIED BY FLASHING GEAR WARNING LIGHTS WHILE CRUISING AT FL 290. THE AIRCRAFT WAS DIVERTED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DOORS OUT OF RIG. THE NOSE GEAR DOORS WERE ADJUSTED IAW MM - [SDR CALA9801578](https://openairdocs.org/sdr/CALA9801578.md): Bracket · cracked · Aug 27, 1998 · N32725 · Boeing 727224 · Leading Edge Slat Actuator > INSPECTION FOUND A.5 INCH CRACK IN SUPPORT BRACKET FOR LT WING NR 2 LEADING EDGE FLAP ACTUATOR. A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA9801577](https://openairdocs.org/sdr/CALA9801577.md): Rib · cracked · Aug 27, 1998 · N32725 · Boeing 727224 · Leading Edge Devices > INSPECTION FOUND A 1 INCH CRACK IN NR 5 SLAT ACTUATOR INBOARD ATTACH RIB. THE CRACK WAS STOP DRILLED, A REPAIR WAS INSTALLED IAW SRM 51-30-2 AND 51-10-1. - [SDR CALA9801576](https://openairdocs.org/sdr/CALA9801576.md): Channel · cracked · Aug 27, 1998 · N32725 · Boeing 727224 · Wing Miscellaneous Structure > INSPECTION FOUND A 1.25 INCH CRACK IN CHANNEL INSIDE TRAILING EDGE AT UPPER SKIN OUTBOARD END OF AFT FALSE SPAR ABOVE NR 3 FLAP TRANSMISSION. A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA9801575](https://openairdocs.org/sdr/CALA9801575.md): Bracket · cracked · Aug 27, 1998 · N32725 · Boeing 727224 · Trailing Edge Flap Actuator > INSPECTION FOUND A.375 INCH CRACK IN SUPPORT BRACKET FOR LT WING NR 1 LEADING EDGE FLAP ACTUATOR. A NEW BRACKET WAS INSTALLED IAW SRM 51-10-1 AND 51-30-2. - [SDR CALA9801574](https://openairdocs.org/sdr/CALA9801574.md): Stiffener · cracked · Aug 27, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.5 INCH CRACK IN AFT CARGO STIFFENER AT STA 950A, LONGERON 29R. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2, 51-10-1, 51-10-2. - [SDR CALA9801573](https://openairdocs.org/sdr/CALA9801573.md): Skin · corroded · Aug 27, 1998 · N32725 · Boeing 727224 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN CORRODED AT LT SIDE, STA 1166, TWO INCHES ABOVE TOP OF FLOORBEAM. THE CORRODED AREA WAS CUT OUT, A DOUBLER WAS INSTALLED IAW ECRA 5330-02699. - [SDR CALA9801558](https://openairdocs.org/sdr/CALA9801558.md): Bottle Pin · corroded · Aug 27, 1998 · N32725 · Boeing 727224 · Wing, Fuselage Attach Fittings > INSPECTION FOUND RT AFT BOTTLE PIN CORRODED. THE BOTTLE PIN AND FORWARD AND AFT BUSHINGS WERE REMOVED AND REPLACED, THEN SAFETIED AND SEALED IAW MM 57-41-1. - [SDR CALA9801557](https://openairdocs.org/sdr/CALA9801557.md): Fitting · corroded · Aug 27, 1998 · N32725 · Boeing 727224 · Horizontal Stabilizer, Attach Fittings > INSPECTION FOUND LT AND RT HORIZONTAL STABILIZER ATTACH FITTING CORRODED. THE CORROSION WAS REMOVED BY BORING HOLES. NEW BUSHINGS AND BEARINGS WERE INSTALLED. THE BEARINGS WERE TORQUED AND SAFETIED IAW ECRA 5550-01033. - [SDR CALA9801556](https://openairdocs.org/sdr/CALA9801556.md): Bolt · corroded · Aug 27, 1998 · N32725 · Boeing 727224 · Trailing Edge Flaps > INSPECTION FOUND RT WING FLAP TRACK NR 5 CORRODED AT FORWARD ATTACH BOLT. THE NR 5 FLAP TRACK AND ATTACH BOLT WERE REMOVED AND REPLACED IAW MM 57-50-0. - [SDR CALA9801555](https://openairdocs.org/sdr/CALA9801555.md): Rib · cracked · Aug 27, 1998 · N32725 · Boeing 727224 · Ailerons > INSPECTION FOUND A.5 INCH CRACK IN RT OUTBOARD AILERON LEADING EDGE RIB JUST OUTBOARD OF NR 3 HINGE. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4. - [SDR CALA9801554](https://openairdocs.org/sdr/CALA9801554.md): Skin · cracked · Aug 27, 1998 · N32725 · Boeing 727224 · Fuselage Main, Plate/Skin > INSPECTION FOUND A.25 INCH CRACK IN FUSELAGE SKIN JUST FORWARD OF CAPTAIN'S WINDSHIELD WIPER AREA. THE CRACKED AREA WAS CUT OUT IAW SRM 51-10-1. A DOUBLER, TRIPLER, AND FILLER WERE INSTALLED IAW SRM 51-30-2, 51-20-4, AND ECRA 5330-02698. - [SDR CALA9801553](https://openairdocs.org/sdr/CALA9801553.md): Beam · cracked · Aug 27, 1998 · N32725 · Boeing 727224 · Wing Miscellaneous Structure > INSPECTION FOUND A.5 INCH CRACK IN J BEAM AT CUTOUT AREA ABOVE NR 7 SPOILER. THE J BEAM WAS REPAIRED IAW ECRA 5780-02914. - [SDR CALA9801552](https://openairdocs.org/sdr/CALA9801552.md): Skin · delaminated · Aug 27, 1998 · N32725 · Boeing 727224 · Elevator, Tab Structure > INSPECTION FOUND RT ELEVATOR CONTROL TAB INBOARD TRAILING EDGE DELAMINATED. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27-30-11. - [SDR CALA9801551](https://openairdocs.org/sdr/CALA9801551.md): Skin · delaminated · Aug 27, 1998 · N32725 · Boeing 727224 · Trailing Edge Flaps > INSPECTION FOUND RT WING INBOARD AFT FLAP LOWER SURFACE DELAMINATED AT MID OUTBOARD AREA. THE AFT FLAP WAS REMOVED AND REPLACED IAW MM 27-51-10. - [SDR CALA9801550](https://openairdocs.org/sdr/CALA9801550.md): Skin · debonded · Aug 27, 1998 · N32725 · Boeing 727224 · Trailing Edge Flaps > INSPECTION FOUND LT INBOARD FOREFLAP DEBONDED ON LOWER SURFACE ABOVE NR 4 CARRIAGE. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-2. - [SDR CALA9801549](https://openairdocs.org/sdr/CALA9801549.md): Skin · debonded · Aug 27, 1998 · N32725 · Boeing 727224 · Aileron Tabs > INSPECTION FOUND LT OUTBOARD AILERON TAB TRAILING EDGE DEBONDED 41.5 INCHES FROM INBOARD END. THE OUTBOARD AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41. - [SDR CALA9801546](https://openairdocs.org/sdr/CALA9801546.md): Angle · cracked · Aug 27, 1998 · N32725 · Boeing 727224 · Wing Miscellaneous Structure > INSPECTION FOUND LT WING INBOARD NR 7 SPOILER ACTUATOR SUPPORT FITTING LOWER ANGLES (TWO EACH) RIB PANEL SUPPORTS CRACKED. THE CRACKS WERE.5 INCH LONG. THE INBOARD AND OUTBOARD ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-10-1 AND 51-30-2. - [SDR CALA9801545](https://openairdocs.org/sdr/CALA9801545.md): Skin · torn · Aug 27, 1998 · N32725 · Boeing 727224 · Wing, Plate/Skin > INSPECTION FOUND LEFT WING UPPER TRAILING EDGE SKIN TORN AT ALL THREE HINGES OF NR 6 SPOILER. THE TORN AREAS WERE CUT OUT IAW SRM 57-30-4. A DOUBLER WAS INSTALLED AT EACH OF THE THREE HINGES IAW SRM 57-30-4, FIGURE 10, SHEET 3. - [SDR CALA9801544](https://openairdocs.org/sdr/CALA9801544.md): Bulkhead Beam · cracked · Aug 27, 1998 · N32725 · Boeing 727224 · Fuselage Main, Bulkhead > INSPECTION FOUND TWO 1.5 CRACKS IN AFT BULKHEAD VERTICAL SUPPORT BEAM AT AFT CARGO COMPARTMENT, BS 1183, RBL 46.93. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW ECRA 5310-03758. - [SDR CALA9801548](https://openairdocs.org/sdr/CALA9801548.md): Skin · debonded · Aug 26, 1998 · N32725 · Boeing 727224 · Spoilers > INSPECTION FOUND LT WING NR 4 SPOILER DEBONDED AT LOWER SKIN. THE NR 4 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1. - [SDR CALA9801547](https://openairdocs.org/sdr/CALA9801547.md): Skin · debonded · Aug 26, 1998 · N32725 · Boeing 727224 · Spoilers > INSPECTION FOUND THE LT WING NR 6 SPOILER LOWER SKIN DEBONDED AT FORWARD END. THE NR 6 SPOILER WAS REMOVED AND REPLACED IAW MM 57-00 AND 27-60-1. - [SDR CALA9801543](https://openairdocs.org/sdr/CALA9801543.md): Bolts · corroded · Aug 26, 1998 · N32725 · Boeing 727224 · Vertical Stabilizer > INSPECTION FOUND FOUR VERTICAL STABILIZER TENSION TIE BOLTS CORRODED AT TOP OF STABILIZER. THE FOUR BOLTS WERE REMOVED AND REPLACED IAW SRM 55-20-00. - [SDR CALA9801542](https://openairdocs.org/sdr/CALA9801542.md): Sidewall · cracked · Aug 26, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.125 INCH CRACK IN LEFT SIDEWALL OF NLG WHEEL WELL. THE CRACKED AREA WAS CUT OUT IAW SRM 51-20-1. DOUBLER AND FITTINGS WERE INSTALLED IAW ECRA 5310-03759. - [SDR CALA9801541](https://openairdocs.org/sdr/CALA9801541.md): Skin · delaminated · Aug 26, 1998 · N32725 · Boeing 727224 · Ailerons > INSPECTION FOUND AREAS OF DELAMINATED SKIN ON TOP AND BOTTOM OF LT WING OUTBOARD AILERON OUTBOARD TRAILING EDGE WEDGE PANEL. THE WEDGE PANEL WAS REMOVED AND REPAIRED IAW SRM 57-50-5. THE PANEL WAS REINSTALLED IAW SRM 51-10-1. - [SDR CALA9801540](https://openairdocs.org/sdr/CALA9801540.md): Skin · cracked · Aug 26, 1998 · N32725 · Boeing 727224 · Trailing Edge Flaps > INSPECTION FOUND A.875 INCH AND.25 INCH CRACK IN LT OUTBOARD FOREFLAP LEADING EDGE CUTOUT ABOVE NR 1 FLAP TRACK. THE FLAP WAS REPAIRED IAW SRM 57-50-4, FIGURE 1. - [SDR CALA9801539](https://openairdocs.org/sdr/CALA9801539.md): Skin · cracked · Aug 26, 1998 · N32725 · Boeing 727224 · Leading Edge Devices > INSPECTION FOUND A.5 INCH CRACK IN RT WING NR 6 SLAT AT OUTBOARD HOOK. A REPAIR WAS ACCOMPLISHED IAW SRM 57-50-3, FIGURE 10. - [SDR CALA9801538](https://openairdocs.org/sdr/CALA9801538.md): Beam · cracked · Aug 26, 1998 · N32725 · Boeing 727224 · Wing Miscellaneous Structure > INSPECTION FOUND A.75 INCH CRACK IN RT WING TRAILING EDGE J BEAM JUST ABOVE NR 8 SPOILER MOUNT. REPAIR PARTS WERE INSTALLED IAW ECRA 5720-01676. - [SDR CALA9801509](https://openairdocs.org/sdr/CALA9801509.md): Skin · cracked · Aug 25, 1998 · N32725 · Boeing 727224 · Fuselage Main, Plate/Skin > INSPECTION FOUND A 2 INCH CRACK IN LT FUSELAGE SKIN BETWEEN WINDOWS NR 16 AND NR 17 AT STA 680. THE CRACKED AREA WAS REPAIRED IAW SRM 51-40-00, 51-10-6, AND 51-10-2. - [SDR CALA9801508](https://openairdocs.org/sdr/CALA9801508.md): Web · corroded · Aug 25, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND CORROSION ON TOP OF AFT CABIN FLOOR SUPPORT WEB AT BS 1148 TO 1183, RBL 25 TO LBL 25. THE CORRODED AREA WAS CUT OUT IAW SRM 51-40-2. A DOUBLER WAS INSTALLED IAW SRM 51-40-2, FIGURE 1. - [SDR CALA9801507](https://openairdocs.org/sdr/CALA9801507.md): Web · corroded · Aug 25, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND LT LAV FLOOR WEB CORRODED AT STA 1130, LBL 27. THE CORRODED AREA WAS CUT OUT IAW SRM 51-40-2. A DOUBLER WAS INSTALLED IAW SRM 51-40-2, FIGURE 1, SHEET 6. - [SDR CALA9801506](https://openairdocs.org/sdr/CALA9801506.md): Bracket · cracked · Aug 25, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.0781 INCH CRACK AT UPPER FORWARD LEG OF LT GEAR UPLOCK SUPPORT BRACKET WHERE IT MOUNTS TO FUSELAGE BS 910 BETWEEN STRINGER 18A LEFT AND 18L. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4. - [SDR CALA9801505](https://openairdocs.org/sdr/CALA9801505.md): Skin · corroded · Aug 25, 1998 · N32725 · Boeing 727224 · Fuselage Main, Plate/Skin > INSPECTION FOUND FORWARD LOWER C-3 DOOR CUTOUT CORRODED IN AFT CARGO COMPARTMENT BETWEEN LONGERON 25R AND 26R. THE CORRODED AREA WAS REMOVED IAW SRM 51-30-2. A DOUBLER WAS INSTALLED IAW SRM 53-10-1, PAGE 5, FIGURE 1. - [SDR CALA9801504](https://openairdocs.org/sdr/CALA9801504.md): Stringer · cracked · Aug 25, 1998 · N32725 · Boeing 727224 · Vertical Stabilizer > INSPECTION FOUND A.5 INCH CRACK AT ATTACH BOLT IN STRINGER 9R AT VERTICAL STABILIZER INNER COMPARTMENT NR 9 RIB. THE CRACKED AREA WAS REMOVED IAW SRM 55-30-4. A REPAIR WAS INSTALLED IAW SRM 55-20-4, FIGURE 1, SHEET 5, AND SRM 51-10-2. - [SDR CALA9801503](https://openairdocs.org/sdr/CALA9801503.md): Plate · cracked · Aug 25, 1998 · N32725 · Boeing 727224 · Vertical Stabilizer, Plate/Skin > INSPECTION FOUND A 4 INCH CRACK IN VERTICAL STABILIZER INNER COMPARTMENT NR 1 RIB LOWER LT CORNER PLATE JUST AFT OF S-DUCT. THE RIVETS WERE REMOVED IAW SRM 51-30-2. A DOUBLER WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA9801502](https://openairdocs.org/sdr/CALA9801502.md): Support · corroded · Aug 25, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND LT AFT LAV AISLE SIDEWALL FLOOR SUPPORT CORRODED. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-10-1. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-1, PAGE 4. - [SDR CALA9801439](https://openairdocs.org/sdr/CALA9801439.md): Stiffener · cracked · Aug 11, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 0.3 INCH CRACK IN AFT CARGO COMPARTMENT STIFFENER AT STA 950A, LONGERON 30R. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-40-4. - [SDR CALA9801438](https://openairdocs.org/sdr/CALA9801438.md): Fitting · cracked · Aug 11, 1998 · N32725 · Boeing 727224 · Trailing Edge Flaps > INSPECTION FOUND A 0.6 CRACK IN FITTING AT RT INBOARD MIDFLAP RIB LEADING EDGE JUST OUTBOARD OF NR 5 CARRIAGE. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4. FASTENERS WERE INSTALLED IAW SRM 51-30-2. - [SDR CALA9801437](https://openairdocs.org/sdr/CALA9801437.md): Circumferential · corroded · Aug 10, 1998 · N32725 · Boeing 727224 · Fuselage Main, Frame > INSPECTION FOUND CORROSION ON FORWARD AND AFT FACE OF CIRCUMFERENTIAL AT LOWER FORWARD NOSE COMPARTMENT, BS 219 BETWEEN STRINGER 24R AND 26R. THE CORRODED AREA WAS CUT OUT IAW SRM 51-40-2. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10- - [SDR CALA9801436](https://openairdocs.org/sdr/CALA9801436.md): Web · cracked · Aug 10, 1998 · N32725 · Boeing 727224 · Wing Miscellaneous Structure > INSPECTION FOUND A.5 INCH CRACK IN WEB PANEL NEXT TO BOOST PUMP INSIDE NR 2 FUEL TANK AT LT WS 171.50. THE WEB PANEL WAS REPAIRED IAW SRM 51-40-2, FIGURE 1. - [SDR CALA9801435](https://openairdocs.org/sdr/CALA9801435.md): Seat Track · corroded · Aug 10, 1998 · N32725 · Boeing 727224 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND SEAT TRACK CORRODED AT BS 380-420, RBL 24. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5 AND 51-10-5. - [SDR CALA9801434](https://openairdocs.org/sdr/CALA9801434.md): Bracket · cracked · Aug 10, 1998 · N32725 · Boeing 727224 · Cargo/Baggage Doors > INSPECTION FOUND A 1 INCH CRACK AT LOWER AFT END OF AFT CARGO C-2 DOOR FRAME SIDE BRACKET. THE DOOR FRAME BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA9801433](https://openairdocs.org/sdr/CALA9801433.md): Stringer · cracked · Aug 10, 1998 · N32725 · Boeing 727224 · Vertical Stabilizer > INSPECTION FOUND A.5 INCH CRACK AT ATTACH BOLT IN NR 7 STRINGER OF RT VERTICAL STABILIZER INNER COMPARTMENT AT NR 4 RIB. THE CRACKED SECTION WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-4. Next page: https://openairdocs.org/deregistered/N32725-2018-01-17/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N32725' AND deregistration_id = 'N32725-2018-01-17' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N32725-2018-01-17/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.