# Service difficulty reports: N500MH, cancelled May 16, 2006

A list on [N500MH, cancelled May 16, 2006](https://openairdocs.org/deregistered/N500MH-2006-05-16.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 4 · 200 reports

- [SDR RRXA011037](https://openairdocs.org/sdr/RRXA011037.md): Altimeter · defective · Apr 18, 2001 · N500MH · Doug DC871F · Altimeter, Barometric/Encoder
  > F/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''
- [SDR RRXA010016](https://openairdocs.org/sdr/RRXA010016.md): Fire Detector · activated · Mar 8, 2001 · N500MH · Doug DC871F · Fire Detection
  > NR 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.
- [SDR RRXA001089](https://openairdocs.org/sdr/RRXA001089.md): Computer · faulty · Dec 13, 2000 · N500MH · Doug DC871F · Autopilot Computer
  > DURING 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.
- [SDR RRXA003616](https://openairdocs.org/sdr/RRXA003616.md): Indicator · malfunctioned · Nov 21, 2000 · N500MH · Doug DC871F · Landing Gear Position and Warning
  > NO NOSE GEAR DOWN GREEN LIGHT WHEN GEAR WAS EXTENDED FOR LANDING, RAN EMERGENCY CHECK LIST AND LANDED WITHOUT INCIDENT.
- [SDR RRXA003615](https://openairdocs.org/sdr/RRXA003615.md): Landing Gear · failed · Nov 20, 2000 · N500MH · Doug DC871F · Landing Gear Retraction/Extension System
  > GEAR 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
- [SDR RRXA003614](https://openairdocs.org/sdr/RRXA003614.md): Switch · out of adj · Nov 20, 2000 · N500MH · Doug DC871F · Landing Gear Position and Warning
  > WHEN 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.
- [SDR RRXA003613](https://openairdocs.org/sdr/RRXA003613.md): Check Valve · misinstalled · Nov 20, 2000 · N500MH · Doug DC871F · Landing Gear Retraction/Extension System
  > AFTER 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 CHE
- [SDR RRXA003331](https://openairdocs.org/sdr/RRXA003331.md): Nose Cowl · dented · Oct 30, 2000 · N500MH · Doug DC871F · Engine Cowl Flaps
  > DURING 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 APPR
- [SDR RRXA003330](https://openairdocs.org/sdr/RRXA003330.md): Panel · delaminated · Oct 30, 2000 · N500MH · Doug DC871F · Wing, Plate/Skin
  > DURING 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.
- [SDR RRXA003842](https://openairdocs.org/sdr/RRXA003842.md): Fitting · cracked · Oct 27, 2000 · N500MH · Doug DC871F · Fuselage Main, Bulkhead
  > DURING 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 51
- [SDR RRXA003837](https://openairdocs.org/sdr/RRXA003837.md): Vane · cracked · Oct 24, 2000 · N500MH · Doug DC871F · Aileron Tabs
  > DURING 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.
- [SDR RRXA003225](https://openairdocs.org/sdr/RRXA003225.md): Plate · damaged · Oct 20, 2000 · N500MH · Doug DC871F · Vertical Stabilizer, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND ELONGATED HOLE IN PLATE VERT STAB AT STA 1680 LEFT L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003224](https://openairdocs.org/sdr/RRXA003224.md): Stiffener · cracked · Oct 20, 2000 · N500MH · Doug DC871F · Elevator Structure
  > DURING 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.
- [SDR RRXA003223](https://openairdocs.org/sdr/RRXA003223.md): Sill · cracked · Oct 20, 2000 · N500MH · Doug DC871F · Fuselage Main, Structure
  > DURING A MAINTENANCE VISIT FOUND A CRACK AND DOUBLE DRILLED HOLES TO THE R-1 DOOR SILL PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003222](https://openairdocs.org/sdr/RRXA003222.md): Frame · cracked · Oct 20, 2000 · N500MH · Doug DC871F · Fuselage Main, Frame
  > DURING 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.
- [SDR RRXA003221](https://openairdocs.org/sdr/RRXA003221.md): Intercostal · cracked · Oct 20, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR RRXA003220](https://openairdocs.org/sdr/RRXA003220.md): Panel · delaminated · Oct 20, 2000 · N500MH · Doug DC871F · Trailing Edge Flaps
  > DURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE WING T/E PANEL BETWEEN STA XRS 98 & 139, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003219](https://openairdocs.org/sdr/RRXA003219.md): Panel · delaminated · Oct 20, 2000 · N500MH · Doug DC871F · Trailing Edge Flaps
  > DURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE T/E LWR PANEL AT STA XRS 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003218](https://openairdocs.org/sdr/RRXA003218.md): Panel · delaminated · Oct 20, 2000 · N500MH · Doug DC871F · Trailing Edge Flaps
  > DURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LWR WING T/E PANEL AT STA XRS 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003839](https://openairdocs.org/sdr/RRXA003839.md): Gusset · tool damage · Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR RRXA003239](https://openairdocs.org/sdr/RRXA003239.md): Access Panel · delaminated · Oct 19, 2000 · N500MH · Doug DC871F · Ailerons
  > DURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LT UPPER AILERON ACCESS PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003238](https://openairdocs.org/sdr/RRXA003238.md): Panel · delaminated · Oct 19, 2000 · N500MH · Doug DC871F · Trailing Edge Flaps
  > DURING 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.
- [SDR RRXA003237](https://openairdocs.org/sdr/RRXA003237.md): Panel · delaminated · Oct 19, 2000 · N500MH · Doug DC871F · Trailing Edge Flaps
  > DURING 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.
- [SDR RRXA003236](https://openairdocs.org/sdr/RRXA003236.md): Intercostal · cracked · Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND AN INTERCOSTAL STRAP BROKEN LT SIDE OF CENTER TRACK AT STA 400, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003235](https://openairdocs.org/sdr/RRXA003235.md): Intercostal · cracked · Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A BROKEN INTERCOSTAL STRAP RT SIDE OF CENTER TRACK AT STA 400, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003234](https://openairdocs.org/sdr/RRXA003234.md): Web · cracked · Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Floor Panel
  > DURING 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.
- [SDR RRXA003233](https://openairdocs.org/sdr/RRXA003233.md): Floorbeam · damaged · Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Main, Floor Beam
  > DURING A MAINTENANCE VISIT FOUND A TEAR IN THE CABIN FLOORBOARD FRAME AT STA 1680, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003232](https://openairdocs.org/sdr/RRXA003232.md): Skin · dented · Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING 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.
- [SDR RRXA003231](https://openairdocs.org/sdr/RRXA003231.md): Frame · cracked · Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO LIGHTENING HOLE ON THE FRAME WEB AT FS 1372, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003230](https://openairdocs.org/sdr/RRXA003230.md): Frame · tool damage · Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND DRILL MARKS ON FRAME TOP FWD CORNER OF CARGO DOOR AT STA 120, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003229](https://openairdocs.org/sdr/RRXA003229.md): Frame · damaged · Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND A HOLE IN THE FUSELAGE FRAME FOR ACCESS DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003228](https://openairdocs.org/sdr/RRXA003228.md): Bracket · cracked · Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR RRXA003227](https://openairdocs.org/sdr/RRXA003227.md): Strap · broken · Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND A BROKEN T/E STRAP ON FRAME AT STA 360 AND L13R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003226](https://openairdocs.org/sdr/RRXA003226.md): Frame · cracked · Oct 19, 2000 · N500MH · Doug DC871F · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FRAME AT STA 360 ABOVE LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003247](https://openairdocs.org/sdr/RRXA003247.md): Stringer Clip · corroded · Oct 18, 2000 · N500MH · Doug DC871F · Wing Miscellaneous Structure
  > DURING 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.
- [SDR RRXA003246](https://openairdocs.org/sdr/RRXA003246.md): Stringer Clip · corroded · Oct 18, 2000 · N500MH · Doug DC871F · Wing Miscellaneous Structure
  > DURING 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.
- [SDR RRXA003245](https://openairdocs.org/sdr/RRXA003245.md): Stringer Clip · corroded · Oct 18, 2000 · N500MH · Doug DC871F · Wing Miscellaneous Structure
  > DURING 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.
- [SDR RRXA003244](https://openairdocs.org/sdr/RRXA003244.md): Intercostal · cracked · Oct 18, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR RRXA003243](https://openairdocs.org/sdr/RRXA003243.md): Intercostal · cracked · Oct 18, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A CRACKED INTERCOSTAL STRAP BELOW 3RD FROM O/B TRACK AT STA 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003242](https://openairdocs.org/sdr/RRXA003242.md): Seat Track · damaged · Oct 18, 2000 · N500MH · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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.
- [SDR RRXA003241](https://openairdocs.org/sdr/RRXA003241.md): Seat Track · damaged · Oct 18, 2000 · N500MH · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND DAMAGE TO THE CENTER SEAT TRACK FRAME AT STA 70, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003240](https://openairdocs.org/sdr/RRXA003240.md): Fitting · cracked · Oct 18, 2000 · N500MH · Doug DC871F · Fuselage Main, Bulkhead
  > DURING 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.
- [SDR RRXA003838](https://openairdocs.org/sdr/RRXA003838.md): Plate · cracked · Oct 17, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR RRXA003836](https://openairdocs.org/sdr/RRXA003836.md): Clip · cracked · Oct 17, 2000 · N500MH · Doug DC871F · Wing, Plate/Skin
  > DURING 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
- [SDR RRXA003255](https://openairdocs.org/sdr/RRXA003255.md): Intercostal · cracked · Oct 17, 2000 · N500MH · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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 51-1
- [SDR RRXA003254](https://openairdocs.org/sdr/RRXA003254.md): Intercostal · cracked · Oct 17, 2000 · N500MH · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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-
- [SDR RRXA003253](https://openairdocs.org/sdr/RRXA003253.md): Intercostal · cracked · Oct 17, 2000 · N500MH · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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-
- [SDR RRXA003257](https://openairdocs.org/sdr/RRXA003257.md): Panel · torn · Oct 17, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND A TEAR TO THE RT CUSP LINE AT STA 182 - 202, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003256](https://openairdocs.org/sdr/RRXA003256.md): Panel · cracked · Oct 17, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND A BROKEN CUST LINE PANEL AT STA 1340 - 1400, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003252](https://openairdocs.org/sdr/RRXA003252.md): Intercostal · cracked · Oct 17, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING 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.

Next page: https://openairdocs.org/deregistered/N500MH-2006-05-16/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 = 'N500MH' AND deregistration_id = 'N500MH-2006-05-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N500MH-2006-05-16/reports

---
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