N500MH, cancelled May 16, 2006

Service difficulty reports · 200

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 = 'N500MH' AND deregistration_id = 'N500MH-2006-05-16'
  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 RRXA011037Altimeter · defectiveF/O''S ALTIMETER STICKS AT 700 TO THOUSANDS OF FEET PER CLIMBOUT AND LEVEL FLIGHT. ON LANDING ALTIMETER STUCK AT 43,000 FT. VSI STUCK AT 1000 FPM DESCENT. RII ISOLATED STATIC LEAK TO F/O''S STATIC MANIFOLD. TIGHTENED ALL STATIC LINES AND FITTINGS AT F/O''Apr 18, 2001 · N500MH · Doug DC871F · Altimeter, Barometric/EncoderSDR RRXA010016Fire Detector · activatedNR 2 ENG FIRE WARN SYS ACTIVATED INFLIGHT. ENG SHUTDOWN. OUTBOARD FIRE AGENT DISCHARGED. REMOVED AND REPLACED 3 FIRE DETECTOR ELEMENTS AND FIRE DETECTOR CNT''L UNIT. OP''S CHECKS GOOD IAW UAL MM 26-11-07.Mar 8, 2001 · N500MH · Doug DC871F · Fire DetectionSDR RRXA001089Computer · faultyDURING CRUISE FLIGHT AIRCRAFT REQUIRED 3 UNITS RIGHT RUDDER TRIM FOR COORDINATED FLIGHT DEPOWERED RUDDER TO MAINTAIN A/C CONTROL ACCOMPLISED QRH. REMOVED AND REPLACED YAW COMPUTER, OP'S CK'D GOOD IAW DC-8 M/M 22-11-1 AND 22-10-0. RT SPOILER SWIVEL LEAKING. Dec 13, 2000 · N500MH · Doug DC871F · Autopilot ComputerSDR RRXA003616Indicator · malfunctionedNO NOSE GEAR DOWN GREEN LIGHT WHEN GEAR WAS EXTENDED FOR LANDING, RAN EMERGENCY CHECK LIST AND LANDED WITHOUT INCIDENT.Nov 21, 2000 · N500MH · Doug DC871F · Landing Gear Position and WarningSDR RRXA003615Landing Gear · failedGEAR WOULD NOT RAISE AFTER T/O MECHANICAL GROUND SHIFT PROBLEM. JACKED AIRCRAFT. ACCOMPLISHED GEAR SWING IAW DC-8 MM 32-30-0. GEAR SWINGS NORMALLY IAW DC-8 MM 32-30-0. INSPECTED NOSE GEAR GROUND SHIFT AND OPS CHECKS GOOD IAW 32-23-1. LUBED NOSE GEAR & GROUND Nov 20, 2000 · N500MH · Doug DC871F · Landing Gear Retraction/Extension SystemSDR RRXA003614Switch · out of adjWHEN LANDING GEAR WAS HYD LOWERED, NO NOSE GEAR DOWN GREEN & GEAR UNSAFE LIGHT STAYED ON. ADJUSTED DOOR SWITCH AND FOUND TO BE OK IAW DC-8 MM32-30-0.Nov 20, 2000 · N500MH · Doug DC871F · Landing Gear Position and WarningSDR RRXA003613Check Valve · misinstalledAFTER T/O UNABLE TO RAISE LANDING GEAR, NO MECHANICAL OR ELECT. GROUND SHIFT. SEPARATED INNER & OUTER NOSE STRUT. FOUND PISTON HEAD & RETURN CHECK VALVE INSTALLED UPSIDE DOWN. INSTALLED PISTON HEAD & CHECK VALVE CORRECTLY IAW DC-8 OHM 32-2-1. GROUND SHIFT CHENov 20, 2000 · N500MH · Doug DC871F · Landing Gear Retraction/Extension SystemSDR RRXA003331Nose Cowl · dentedDURING A MAINTENANCE VISIT FOUND A DENT TO THE NR 2 ENGINE NOSE COWL AT 9 O'CLOCK POSITION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 71-5-1 AND EO#00-262 WITH APPROct 30, 2000 · N500MH · Doug DC871F · Engine Cowl FlapsSDR RRXA003330Panel · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE WING PANEL O/B OF MLG AT STA XRS 76, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0.Oct 30, 2000 · N500MH · Doug DC871F · Wing, Plate/SkinSDR RRXA003842Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO CANTER BULKHEAD BRACKET AT STA. 1766 AND L3R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51Oct 27, 2000 · N500MH · Doug DC871F · Fuselage Main, BulkheadSDR RRXA003837Vane · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO #1 FLAP VANE ABOVE I/B END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 27-51-14.Oct 24, 2000 · N500MH · Doug DC871F · Aileron TabsSDR RRXA003225Plate · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLE IN PLATE VERT STAB AT STA 1680 LEFT L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 20, 2000 · N500MH · Doug DC871F · Vertical Stabilizer, Plate/SkinSDR RRXA003224Stiffener · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE STIFFENERS ON THE WEB BELOW HORIZ STAB. CONSTANT SECTION AT STA 1810 INSIDE ACC 60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 20, 2000 · N500MH · Doug DC871F · Elevator StructureSDR RRXA003223Sill · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AND DOUBLE DRILLED HOLES TO THE R-1 DOOR SILL PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 20, 2000 · N500MH · Doug DC871F · Fuselage Main, StructureSDR RRXA003222Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FRAME IN BEND RADIUS UNDER NUT PLATE A PIT AT STA 140 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 20, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003221Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE MID ACC COMPT INTERCOSTAL BETWEEN STA 660 - 680 AT L25L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 20, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003220Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE WING T/E PANEL BETWEEN STA XRS 98 & 139, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 20, 2000 · N500MH · Doug DC871F · Trailing Edge FlapsSDR RRXA003219Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE T/E LWR PANEL AT STA XRS 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 20, 2000 · N500MH · Doug DC871F · Trailing Edge FlapsSDR RRXA003218Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LWR WING T/E PANEL AT STA XRS 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 20, 2000 · N500MH · Doug DC871F · Trailing Edge FlapsSDR RRXA003839Gusset · tool damageDURING A MAINTENANCE VISIT FOUND DRILL DAMAGE TO FRAME 120 TOP FWD CORNER OF CARGO DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4, 53-2-0, 51-1-20D.Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003239Access Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LT UPPER AILERON ACCESS PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 19, 2000 · N500MH · Doug DC871F · AileronsSDR RRXA003238Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LWR WING T/E PANEL FWD END BETWEEN STA XRS 340 & 419, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 19, 2000 · N500MH · Doug DC871F · Trailing Edge FlapsSDR RRXA003237Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LWR WING T/E PANEL O/B OF FLAP ACTUATOR AT STA 419, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 19, 2000 · N500MH · Doug DC871F · Trailing Edge FlapsSDR RRXA003236Intercostal · crackedDURING A MAINTENANCE VISIT FOUND AN INTERCOSTAL STRAP BROKEN LT SIDE OF CENTER TRACK AT STA 400, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003235Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A BROKEN INTERCOSTAL STRAP RT SIDE OF CENTER TRACK AT STA 400, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003234Web · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AND A LARGE HOLE TO THE LT SIDE OF CABIN FLOOR WEB AT STA 120, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Floor PanelSDR RRXA003233Floorbeam · damagedDURING A MAINTENANCE VISIT FOUND A TEAR IN THE CABIN FLOORBOARD FRAME AT STA 1680, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Main, Floor BeamSDR RRXA003232Skin · dentedDURING A MAINTENANCE VISIT FOUND A DENT TO THE RT FWD O/W EXIT DOOR IN EDGE OF OUTER SKIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003231Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO LIGHTENING HOLE ON THE FRAME WEB AT FS 1372, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003230Frame · tool damageDURING A MAINTENANCE VISIT FOUND DRILL MARKS ON FRAME TOP FWD CORNER OF CARGO DOOR AT STA 120, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003229Frame · damagedDURING A MAINTENANCE VISIT FOUND A HOLE IN THE FUSELAGE FRAME FOR ACCESS DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003228Bracket · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE BRACKET ON THE VERT STIFFENERS AT STA 680 RBL -24 Z AXIS -2, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003227Strap · brokenDURING A MAINTENANCE VISIT FOUND A BROKEN T/E STRAP ON FRAME AT STA 360 AND L13R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003226Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FRAME AT STA 360 ABOVE LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003247Stringer Clip · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CLIP AT THE LT CENTER WING THRU ACCESS HOLE 516 THRU MID SPAR ACCESS HOLE 560E AT STA XCW +46 BETWEEN STRINGER 72 - 73, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 18, 2000 · N500MH · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003246Stringer Clip · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CLIP AT THE LT CENTER WING THRU ACCESS HOLE 516 THRU MID SPAR ACCESS HOLE 560E AT STA XCW +46 BETWEEN STRINGER 73 - 74, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 18, 2000 · N500MH · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003245Stringer Clip · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT LWR CLIP LT CENTER WING THRU ACCESS HOLE 516 THRU MID SPAR ACCESS HOLE 560E AT STA XCW +23 & SCW +46 BETWEEN STR 73 - 74, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 18, 2000 · N500MH · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003244Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED INTERCOSTAL STRAP BETWEEN CENTER SEAT TRACK AND 2ND FROM O/B TRACK AT STA 360, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 18, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003243Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED INTERCOSTAL STRAP BELOW 3RD FROM O/B TRACK AT STA 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 18, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003242Seat Track · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE 3RD TRACK FROM RIGHT O/B SIDE BETWEEN STA''S 859 & 879, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 18, 2000 · N500MH · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003241Seat Track · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE CENTER SEAT TRACK FRAME AT STA 70, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 18, 2000 · N500MH · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003240Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE PRESSURE BULKHEAD TIE IN FITTING IN THE RT MAIN WHEEL WELL FWD UPPER I/B CORNER AT STA 8576.125 X-3 Z-10, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 18, 2000 · N500MH · Doug DC871F · Fuselage Main, BulkheadSDR RRXA003838Plate · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R1 SERVICE DOOR SCUFF PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW EO 00-257 WITH APPROVED 8110-3 DATED 09/26/00.Oct 17, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003836Clip · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO STRINGER CLIP AT STA. XW485 AND BETWEEN STRINGER 62-63, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW Oct 17, 2000 · N500MH · Doug DC871F · Wing, Plate/SkinSDR RRXA003255Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A BROKEN INTERCOSTAL STRAP LT SIDE OF CENTER SEAT TRACK AT STA 660 AT X=+5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1Oct 17, 2000 · N500MH · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003254Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A BROKEN INTERCOSTAL STRAP LT SIDE OF CENTER SEAT TRACK AT STA 620 AT X=+3, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-Oct 17, 2000 · N500MH · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003253Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A BROKEN INTERCOSTAL STRAP LT SIDE OF CENTER SEAT TRACK AT STA 560 AND X=+3, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-Oct 17, 2000 · N500MH · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003257Panel · tornDURING A MAINTENANCE VISIT FOUND A TEAR TO THE RT CUSP LINE AT STA 182 - 202, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 17, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003256Panel · crackedDURING A MAINTENANCE VISIT FOUND A BROKEN CUST LINE PANEL AT STA 1340 - 1400, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 17, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003252Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A BROKEN INTERCOSTAL STRAP LT SIDE OF CENTER SEAT TRACK AT STA 500 X=+3, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 17, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous Structure
Back to N500MH, cancelled May 16, 2006