# Service difficulty reports: N5WM, cancelled Aug 1, 2005 A list on [N5WM, cancelled Aug 1, 2005](https://openairdocs.org/deregistered/N5WM-2005-08-01.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 3 · 119 reports - [SDR P2EA01089](https://openairdocs.org/sdr/P2EA01089.md): Hydraulic Line · inoperative · Jun 7, 2001 · N5WM · Boeing 737297 · Hydraulic Power System > FLT 408 - MCI - WHILE ON APPROACH INTO MCI, AIRCRAFT A SYSTEM HYDRAULIC FAILED. DECLARED AN EMERGENCY. INSPECTED HYDRAULIC SYSTEM A AND FOUND LEAK IN FORWARD LEFT MAIN WHEEL WELL. REMOVED AND REPLACED HYDRAULIC LINE LEAK CHECKED GOOD PER BOEING MM 29-00 PAR - [SDR P2EA01025](https://openairdocs.org/sdr/P2EA01025.md): Skin · punctured · Apr 8, 2001 · N5WM · Boeing 737297 · Fuselage Main, Plate/Skin > FLT 350 - MDW - PUNCTURE THROUGH SKIN AT BS 933 WL 203 BETWEEN STRINGER 20L AND 21L. (M) - [SDR P2EA01028](https://openairdocs.org/sdr/P2EA01028.md): Skin · punctured · Apr 8, 2001 · N5WM · Boeing 737297 · Fuselage Main, Plate/Skin > MDW - FLT 350 - PUNCTURE THROUGH SKIN AT BS 933, WL 203 BETWEEN STRINGER 20L AND 21L. REPAIRED IAW SRM 53-30-3. (M) - [SDR P2EA00460](https://openairdocs.org/sdr/P2EA00460.md): Skin · cracked · Dec 8, 2000 · N5WM · Boeing 737297 · Service Doors > SJO - DURING Q-CHECK, FOUND THE L-2 DOOR SKIN BS 956.5 TO BS 962.5 BETWEEN BEAMS NR 6 AND NR 7 WITH CRACK. L = 1.1250 INCHES. W = 0.001 INCH. REPAIRED THE L-2 DOOR SKIN BS 956.5 TO BS 962.5 BETWEEN BEAMS NR 6 AND NR 7 IAW BOEING SRM 52-00-3 FIG 3. (X) - [SDR P2EA00451](https://openairdocs.org/sdr/P2EA00451.md): Fitting · cracked · Dec 2, 2000 · N5WM · Boeing 737297 · Horizontal Stabilizer, Tab Structure > SJO - DURING Q-CHECK, FOUND LEFT ELEVATOR HINGE SUPPORT AT BS 1156 ELEVATOR STA ZERO WITH CRACK L = 2.00 INCHES. W = 0.002 INCH. REPLACED THE LEFT ELEVATOR HINGE SUPPORT AT BS 1156 ELEVATOR STA ZERO IAW BOEING SRM 51-10-1 PAGE 8 AND SRM 51-30-2. (X) - [SDR P2EA00407](https://openairdocs.org/sdr/P2EA00407.md): Bulkhead · cracked · Nov 22, 2000 · N5WM · Boeing 737297 · Fuselage Main, Bulkhead > SJO - DURING Q-CHECK, FOUND THE BS 178 BULKHEAD AT WL 196 FROM LBL 25 TO RBL 25 WITH CRACK. L = 1.00 INCH. W = 0.001 INCH. REPLACED THE BS 178 BULKHEAD INTERCOSTAL AT WL 196 FROM LBL 25 TO RBL 25 IAW BOEING SB 737-53A1173 REV 3 DATED MAY 6, 1999, SECTION II - [SDR P2EA00396](https://openairdocs.org/sdr/P2EA00396.md): Channel · corroded · Nov 19, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, THE CABIN FLOOR CHANNEL AT BS 296.5 BETWEEN LBL 11.5 AND LBL 41 WL 208.5 WITH CORROSION OUT OF LIMITS, LENGTH 2.5 INCH, WIDTH 2 INCHES, DEPTH.025 INCH. REPLACED THE CABIN FLOOR CHANNEL AT BS 286.5 BETWEEN LBL 11.5 AND LBL 41 WL 208.5 IA - [SDR P2EA00413](https://openairdocs.org/sdr/P2EA00413.md): Floor Support · corroded · Nov 19, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN FLOOR ANGLE AT BS 286.5 BETWEEN LBL 11.5 AND LBL 41 WL 208.5 WITH CORROSION OUT OF LIMITS. L = 4.00 INCHES. W = 0.50 INCH. D = 0.040 INCH. REPLACED THE PASSENGER CABIN FLOOR ANGLE AT BS 286.5 BETWEEN LBL 11.5 - [SDR P2EA00412](https://openairdocs.org/sdr/P2EA00412.md): Floor Support · corroded · Nov 19, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN FLOOR SUPPORT STIFFENER AT BS 294.5 TO BS 312 LBL 11 WL 208.5 WITH CORROSION OUT OF LIMITS. L = 4.00 INCHES. W = 1.00 INCH. D = 0.040 INCH. REPLACED THE PASSENGER CABIN FLOOR SUPPORT STIFFENER AT BS 294.5 TO - [SDR P2EA00389](https://openairdocs.org/sdr/P2EA00389.md): Channel · cracked · Nov 17, 2000 · N5WM · Boeing 737297 · Wing Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE RIGHT WING TRAILING EDGE CAVITY LOWER CHORD CHANNEL AT RSS 180 WITH CRACK. (M) - [SDR P2EA00387](https://openairdocs.org/sdr/P2EA00387.md): Crossbeam · cracked · Nov 16, 2000 · N5WM · Boeing 737297 · Passenger/Crew Doors > SJO - DURING Q-CHECK, FOUND THE FORWARD CARGO DOOR NR 5 CROSSBEAM WEB AFT END WITH CRACK. (M) - [SDR P2EA00455](https://openairdocs.org/sdr/P2EA00455.md): Flap Track · cracked · Nov 14, 2000 · N5WM · Boeing 737297 · Trailing Edge Flaps > SJO - DURING Q-CHECK, FOUND THE RIGHT WING OUTBOARD FLAP TRACK LOWER INBOARD FLANGE BETWEEN NR'S 30 AND 35 HORIZONTAL ATTACHMENT SCREWS WITH TWO CRACKS.313 LENGTH,.001 INCH WIDE, AND.250 INCH LENGTH,.001 INCH WIDE. REPLACED THE RIGHT WING OUTBOARD FLAP TR - [SDR P2EA00384](https://openairdocs.org/sdr/P2EA00384.md): Flap Track · cracked · Nov 14, 2000 · N5WM · Boeing 737297 · Trailing Edge Flaps > SJO - DURING Q-CHECK, FOUND THE RIGHT WING OUTBOARD FLAP TRACK LOWER INBOARD FLANGE BETWEEN NRS 30 AND 35 HORIZONTAL ATTACHMENT SCREWS WITH TWO CRACKS. (M) - [SDR P2EA00386](https://openairdocs.org/sdr/P2EA00386.md): Angle · corroded · Nov 14, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE APU TORQUE BOX RIGHT ANGLE FROM BS 1118 TO 1138 WITH CORROSION OUT OF LIMITS. (M) - [SDR P2EA00379](https://openairdocs.org/sdr/P2EA00379.md): Web · cracked · Nov 14, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE CABIN FLOOR WEB FROM BS 1016 TO BS 1028 RBL 5 TO LBL 5 WL 208 WITH CRACK. L = 0.500 INCH. W = 0.005 INCH. REPAIRED THE CABIN FLOOR WEB FROM BS 1016 TO BS 1028 RBL 5 TO LBL 5 WL 208 IAW BOEING SRM 51-40-2 FIG 1. (X) - [SDR P2EA00380](https://openairdocs.org/sdr/P2EA00380.md): Channel · cracked · Nov 14, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN AT BS 257 TO BS 267 BL ZERO WL 208 CHANNEL WITH CRACK. L = 0.50 INCH. W = 0.005 INCH. REPLACED THE PASSENGER CABIN AT BS 257 TO BS 267 BL ZERO WL 208 CHANNEL IAW BOEING SRM 51-10-1 PAGE 8 AND SRM 51-30-2. (X) - [SDR P2EA00393](https://openairdocs.org/sdr/P2EA00393.md): Slat Track · cracked · Nov 13, 2000 · N5WM · Boeing 737297 · Leading Edge Devices > SJO - DURING Q-CHECK, FOUND THE LT WING NR 1 SLAT AUXILIARY TRACK UPPER INBOARD CORNER WITH CRACK LENGTH.50 INCH, WIDTH.50 INCH. REWORKED THE LEFT WING NR 1 SLAT AUXILIARY TRACK UPPER INBOARD CORNER AND WAS FOUND TO BE WITHIN LIMITS IAW BOEING SRM 57-20-1 F - [SDR P2EA00378](https://openairdocs.org/sdr/P2EA00378.md): Slat Track · cracked · Nov 13, 2000 · N5WM · Boeing 737297 · Leading Edge Devices > SJO - DURING Q-CHECK, FOUND THE LEFT WING NR 1 SLAT AUXILIARY TRACK UPPER INBOARD CORNER WITH CRACK. (X) - [SDR P2EA00405](https://openairdocs.org/sdr/P2EA00405.md): Floorbeam · corroded · Nov 12, 2000 · N5WM · Boeing 737297 · Fuselage Main, Floor Beam > SJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN FLOORBEAM UPPER FLANGE BS 312 RBL 8 TO LBL 14 WITH CORROSION OUT OF LIMITS, LENGTH 22 INCHES, WIDTH 2 INCHES, DEPTH.030 INCH. REPAIRED THE PASSENGER CABIN FLOORBEAM UPPER FLANGE BS 312 RBL 8 TO LBL 14 IAW BOEIN - [SDR P2EA00404](https://openairdocs.org/sdr/P2EA00404.md): Stringer · cracked · Nov 12, 2000 · N5WM · Boeing 737297 · Wing, Longeron/Stringer > SJO - DURING Q-CHECK, FOUND THE RIGHT WING NR 2 FUEL TANK UPPER SURFACE STR 13 WBL 135.5 WITH CRACK INDICATION. CONFIRMED CRACK AT THE RIGHT WING NR 2 FUEL TANK UPPER SURFACE STR 13 WBL 135.5 BY HFEC INSPECTION ON 11-18-00. L = 1.250 INCHES. W = 0.001 INCH. - [SDR P2EA00381](https://openairdocs.org/sdr/P2EA00381.md): Floorbeam · corroded · Nov 12, 2000 · N5WM · Boeing 737297 · Fuselage Main, Floor Beam > SJO - DUIRNG Q-CHECK, FOUND THE PASSENGER CABIN FLOORBEAM UPPER FLANGE BS 312 RBL 8 TO LBL 14 WITH CORROSION OUT OF LIMITS. (M) - [SDR P2EA00399](https://openairdocs.org/sdr/P2EA00399.md): Bulkhead · cracked · Nov 11, 2000 · N5WM · Boeing 737297 · Fuselage Main, Bulkhead > SJO - DURING Q-CHECK, FOUND THE BULKHEAD UPPER FUSELAGE WEB AT BS 178 RBL 14 WL 218 WITH CRACK INDICATION. CONFIRMED CRACK AT THE BULKHEAD UPPER FUSELAGE WEB AT BS 178 RBL 14 WL 218 ON 11/19/00. (M) - [SDR P2EA00400](https://openairdocs.org/sdr/P2EA00400.md): Frame · cracked · Nov 11, 2000 · N5WM · Boeing 737297 · Fuselage Main, Frame > SJO - DURING Q-CHECK, FOUND THE BULKHEAD LOWER FUSELAGE CHORD AT BS 178 LBL 24 WL 195 WITH CRACK INDICATION. CONFIRMED CRACK AT THE BULKHEAD LOWER FUSELAGE CHORD AT BS 178 LBL 24 WL 195 ON 11/19/2000. (M) - [SDR P2EA00444](https://openairdocs.org/sdr/P2EA00444.md): Frame · cracked · Nov 11, 2000 · N5WM · Boeing 737297 · Fuselage Main, Frame > SJO - DURING Q-CHECK, FOUND THE BULKHEAD LOWER FUSELAGE CHORD AT BS 178 LBL 24 WL 195 WITH CRACK INDICATION. CONFIRMED CRACK AT THE BULKHEAD LOWER FUSELAGE CHORD AT BS 178 LBL 24 WL 195 ON 11/19/00, LENGTH.50 INCH, WIDTH.005. REPLACED THE BULKHEAD LOWER FU - [SDR P2EA00356](https://openairdocs.org/sdr/P2EA00356.md): Bulkhead · cracked · Nov 11, 2000 · N5WM · Boeing 737297 · Fuselage Main, Bulkhead > DURNIG Q-CHECK, FUOND THE BULKHEAD WEB AT FS 178 WL 195 BETWEEN LBL 11-14 WITH CRACK. AFTER NDT INSPECTION, CONFIRMED NO CRACK. (M) - [SDR P2EA00357](https://openairdocs.org/sdr/P2EA00357.md): Bulkhead · cracked · Nov 11, 2000 · N5WM · Boeing 737297 · Fuselage Main, Bulkhead > SJO - DURING Q-CHECK, FOUND THE BULKHEAD WEB AT BS 178 WL 226 RBL 5.7 WITH CRACK. AFTER NDT INSPECTION, CONFIRMED NO CRACK. (M) - [SDR P2EA00365](https://openairdocs.org/sdr/P2EA00365.md): Skin · cracked · Nov 11, 2000 · N5WM · Boeing 737297 · Fuselage Main, Plate/Skin > SJO - DURING Q-CHECK, FOUND THE L-1 DOOR UPPER HINGE CUT OUT WITH CRACK. (M) - [SDR P2EA00377](https://openairdocs.org/sdr/P2EA00377.md): Support Bracket · cracked · Nov 11, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE L-1 DOOR LOWER AFT SUPPORT WITH CRACK. L = 0.50 INCH. W = 0.005 INCH. REPLACED THE L-1 DOOR LOWER AFT SUPPORT IAW BOEING SRM 51-10-1 PAGE 8. (X) - [SDR P2EA00406](https://openairdocs.org/sdr/P2EA00406.md): Spar · cracked · Nov 10, 2000 · N5WM · Boeing 737297 · Wing Spar > SJO - DURING Q-CHECK, FOUND THE LEFT WING REAR SPAR SECTION AT RSS 205 TRAILING EDGE ANGLE CRACKED LENGTH.250 INCH WIDTH.005 INCH. REPLACED THE LEFT WING REAR SPAR SECTION AT RSS 205 TRAILING EDGE ANGLE IAW BOEING SRM 51-10-1 PAGE 8. (M) - [SDR P2EA00403](https://openairdocs.org/sdr/P2EA00403.md): Stiffener · cracked · Nov 10, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE BULKHEAD LOWER FUSELAGE STIFFENER AT BS 178 RBL 5.5 WL 185 WITH CRACK INDICATION. CONFIRMED CRACK AT THE BULKHEAD LOWER FUSELAGE STIFFENER AT BS 178 RBL 5.5 WL 185 ON 11/20/00. (M) - [SDR P2EA00340](https://openairdocs.org/sdr/P2EA00340.md): Window · cracked · Nov 10, 2000 · N5WM · Boeing 737297 · Flight Compartment Windows > SJO - DURING Q-CHECK, FOUND THE NR 1 WINDOW RIGHT UPPER SIDE CORNER WITH CRACK. (M) - [SDR P2EA00341](https://openairdocs.org/sdr/P2EA00341.md): Window · cracked · Nov 10, 2000 · N5WM · Boeing 737297 · Flight Compartment Windows > SJO - DURING Q-CHECK, FOUND THE NR 1 WINDOW LEFT UPPER SIDE CORNER WITH CRACK. (M) - [SDR P2EA00342](https://openairdocs.org/sdr/P2EA00342.md): Angle · cracked · Nov 10, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN AT BS 328 LBL 46 WL 202 WITH CRACKED ANGLE. (M) - [SDR P2EA00354](https://openairdocs.org/sdr/P2EA00354.md): Stiffener · cracked · Nov 10, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE BULKHEAD STIFFENER AT BS 178 LBL 5.5 WL 182 CRACKED. (M) - [SDR P2EA00355](https://openairdocs.org/sdr/P2EA00355.md): Spar · cracked · Nov 10, 2000 · N5WM · Boeing 737297 · Wing Spar > SJO - DURING Q-CHECK, FOUND THE LEFT WING REAR SPAR SECTION RSS 205 TRAILING EDGE ANGLE CRACKED. (M) - [SDR P2EA00358](https://openairdocs.org/sdr/P2EA00358.md): Clip · cracked · Nov 10, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE FRAME SUPPORT CHIP AT BS 663.75 STRINGER 10L WITH CRACK. (M) - [SDR P2EA00359](https://openairdocs.org/sdr/P2EA00359.md): Skin · cracked · Nov 10, 2000 · N5WM · Boeing 737297 · Leading Edge Devices > SJO - DURING Q-CHECK, FOUND THE LEFT WING LEADING EDGE SKIN AT FSS 282 WITH CRACK. (M) - [SDR P2EA00362](https://openairdocs.org/sdr/P2EA00362.md): Clip · cracked · Nov 10, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE CABIN FRAME SUPPORT CLIP AT BS 616 STRINGER 2L CRACKED. (M) - [SDR P2EA00363](https://openairdocs.org/sdr/P2EA00363.md): Door Frame · cracked · Nov 10, 2000 · N5WM · Boeing 737297 · Fuselage Main, Structure > SJO - DURING Q-CHECK, FOUND THE L-1 DOOR LOWER FORWARD CORNER OF FRAME CRACKED. (M) - [SDR P2EA00364](https://openairdocs.org/sdr/P2EA00364.md): Clip · cracked · Nov 10, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE CABIN FRAME SUPPORT CLIP AT BS 639 STRIGNER 2R CRACKED. (M) - [SDR P2EA00366](https://openairdocs.org/sdr/P2EA00366.md): Skin · delaminated · Nov 10, 2000 · N5WM · Boeing 737297 · Spoilers > SJO - DURING Q-CHECK, FOUND THE LEFT INBOARD GROUND SPOILER WITH DELAMINATION. (M) - [SDR P2EA00376](https://openairdocs.org/sdr/P2EA00376.md): Channel · corroded · Nov 10, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE CABIN FLOOR CHANNEL BETWEEN BS 1006 - BS 1030 BL ZERO HAD CORROSION OUT OF LIMITS. L = 7.00 INCHES. W = 2.00 INCHES. D = 0.040 INCH. REPLACED THE CABIN FLOOR CHANNEL BETWEEN BS 1006 - BS 1030 BL ZERO IAW BOEING SRM 51-10-1 P - [SDR P2EA00395](https://openairdocs.org/sdr/P2EA00395.md): Frame · cracked · Nov 9, 2000 · N5WM · Boeing 737297 · Fuselage Main, Frame > SJO - DURING Q-CHECK, FOUND PASSENGER CABIN FRAME INTERNAL FLANGE AT BS 460 BETWEEN STRINGER 13-14R CRACKED, LENGTH 1 INCH, WIDTH.002 INCH. REPAIRED PASSENGER CABIN FRAME INTERNAL FLANGE AT BS 460 BETWEEN STRINGER 13-14R IAW BOEING SRM 53-10-4 FIG 10. (M) - [SDR P2EA00401](https://openairdocs.org/sdr/P2EA00401.md): Floorbeam · corroded · Nov 9, 2000 · N5WM · Boeing 737297 · Fuselage Main, Floor Beam > SJO - DURING Q-CHECK, FOUND THE CABIN FLOORBEAM UPPER FLANGE AT BS 294.5 BETWEEN RBL 10-12 WL 208.5 WITH CORROSION. CONFIRMED CORROSION OUT OF LIMITS AT BS 294.5 BETWEEN RBL 10-12 WL 208.5 ON 11/20/00. (M) - [SDR P2EA00402](https://openairdocs.org/sdr/P2EA00402.md): Floorbeam · corroded · Nov 9, 2000 · N5WM · Boeing 737297 · Fuselage Main, Floor Beam > SJO - DURING Q-CHECK, FOUND THE CABIN FLOORBEAM UPPER FLANGE AT BS 328 BETWEEN RBL 10.75-49 WL 208.5 WITH CORROSION. CONFIRMED CORROSION OUT OF LIMITS AT BS 328 BETWEEN RBL 10.75-49 ON 11/20/00. (M) - [SDR P2EA00456](https://openairdocs.org/sdr/P2EA00456.md): Channel · cracked · Nov 9, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN AT BS 807 RBL 18 WL 203 WITH CRACKED CHANNEL, LENGTH.500 INCH, WIDTH.005 INCH. REPLACED THE PASSENGER CABIN CHANNEL AT BS 867 RBL 18 WL 203 IAW BOEING SRM 51-10-1 PAGE 8 AND 51-30-2. REF P2EA00344. (M) - [SDR P2EA00369](https://openairdocs.org/sdr/P2EA00369.md): Frame · dented · Nov 9, 2000 · N5WM · Boeing 737297 · Fuselage Main, Frame > SJO - DURING Q-CHECK, FOUND THE AFT CARGO COMPARTMENT FRAME BETWEEN STRINGER 24-25L BS 827 WITH DENT. (M) - [SDR P2EA00370](https://openairdocs.org/sdr/P2EA00370.md): Frame · dented · Nov 9, 2000 · N5WM · Boeing 737297 · Fuselage Main, Frame > SJO - DURING Q-CHECK, FOUND THE AFT CARGO COMPARTMENT FRAME BETWEEN STRINGER 24-25L BS 807 WITH DENT. (M) - [SDR P2EA00343](https://openairdocs.org/sdr/P2EA00343.md): Angle · cracked · Nov 9, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure > SJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN AT BS 727 RBL 65 WITH CRACKED ANGLE ON FLOOR SUPPORT. (M) - [SDR P2EA00375](https://openairdocs.org/sdr/P2EA00375.md): Floorbeam · cracked · Nov 9, 2000 · N5WM · Boeing 737297 · Fuselage Main, Floor Beam > SJO - DURING Q-CHECK, FOUND THE CABIN FLOORBEAM AT BS 312 RBL 1 WL 207 WITH CRACK. (M) Next page: https://openairdocs.org/deregistered/N5WM-2005-08-01/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 = 'N5WM' AND deregistration_id = 'N5WM-2005-08-01' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N5WM-2005-08-01/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.