# Service difficulty reports: N825BX, cancelled May 1, 2014

A list on [N825BX, cancelled May 1, 2014](https://openairdocs.org/deregistered/N825BX-2014-05-01.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 5 · 249 reports

- [SDR IXX2008F00098](https://openairdocs.org/sdr/IXX2008F00098.md): Hydraulic System · low · Sep 23, 2008 · N825BX · Doug DC871F · Hydraulic System, Main
  > DURING CRUISE FROM KSJC TO KRFD, FLT ENGINEER NOTICED HYDRAULIC QUANTITY INDICATOR WAS AT THE BOTTOM OF NORMAL QUANTITY, DID NOT DROP ANY FURTHER DURING THE REST OF THE FLT. THE CREW LANDED IN KTOL WITHOUT FURTHER INCIDENT. MX SERVICED HYDRAULIC SYS, OPS CHE
- [SDR IXX2008F00091](https://openairdocs.org/sdr/IXX2008F00091.md): Hose · leaking · Aug 29, 2008 · N825BX · Doug DC871F · Hydraulic System, Main
  > AT TOP OF DECENT, THE ACFT LOST HYDRAULIC FLUID DOWN TO THE STAND PIPE. MAINT INSPECTED AND FOUND NR 3 ENGINE HYDRAULIC PUMP HOSE LEAKING, REPLACED NR 3 ENGINE HYDRAULIC PUMP HOSE. OPS CHECK GOOD IAW MM 29-16. AC WAS RETURNED TO SERVICE. (K)
- [SDR IXX2008F00090](https://openairdocs.org/sdr/IXX2008F00090.md): Hydraulic System · failed · Aug 28, 2008 · N825BX · Doug DC871F · Hydraulic System, Main
  > AT TOP OF DECENT, THE ACFT LOST HYDRAULIC FLUID DOWN TO THE STAND PIPE. OPEN. (K)
- [SDR IXX2008F00009](https://openairdocs.org/sdr/IXX2008F00009.md): Switch · broken · Jun 26, 2008 · N825BX · Doug DC871F · Electrical Power System
  > DURING CLIMB-OUT, OVER RIDE TOGGLE SWITCH BROKE OFF. AIRCRAFT RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED OVER RIDE SWITCH; OPS CHECK GOOD IAW UAL MM 74-20-36. (K)
- [SDR IXXA06SMN329S](https://openairdocs.org/sdr/IXXA06SMN329S.md): Skin · misrepaired · Oct 6, 2006 · N825BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER SKIN HAS NON STANDARD REPAIR AT STATION XW104.000. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN (AL 2024 T3 0.040”). CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERN
- [SDR IXXA06SMN320S](https://openairdocs.org/sdr/IXXA06SMN320S.md): Skin · cracked · Sep 25, 2006 · N825BX · Doug DC871F · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND NR 4 ALTERNATE TANK CRACKED AT STATION XW485.000, CONFIRMED WITH NDT. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR PARTS. CLEANED TREATED AND P
- [SDR IXXA06SMN321S](https://openairdocs.org/sdr/IXXA06SMN321S.md): Fitting · cracked · Sep 25, 2006 · N825BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C-CHECK INSPECTION FOUND FITTING CRACKED AT STA 1212.000 LONGERON 29 RT. REPLACED FITTING AT STA 1212.000 LONGERON 29 RT. IAW SRM 51-1-20D.
- [SDR IXXA06SMN323S](https://openairdocs.org/sdr/IXXA06SMN323S.md): Skin · misrepaired · Sep 25, 2006 · N825BX · Doug DC871F · Elevator, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR UPPER SKIN HAS NON STANDARD REPAIR FROM STATION XE116.000 TO STATION XE79.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED BOTH PARTS WITH HYSOL IAW D
- [SDR IXXA06SMN325S](https://openairdocs.org/sdr/IXXA06SMN325S.md): Skin · misrepaired · Sep 25, 2006 · N825BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD FLAP LEADING EDGE UPPER SKIN WITH NON STANDARD REPAIR AT STATION XF211.000. REMOVED SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN. CLEANED TREATED AND PRIMED AREA AND NEW SKIN INTERNAL SURFAC
- [SDR IXXA06SMN326S](https://openairdocs.org/sdr/IXXA06SMN326S.md): Skin · misrepaired · Sep 25, 2006 · N825BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION FOUND RIGHT WING OUTBOARD FLAP UPPER SKIN WITH NON STANDARD REPAIR AT STATION XF445.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND P
- [SDR IXXA06SMN327S](https://openairdocs.org/sdr/IXXA06SMN327S.md): Skin · misrepaired · Sep 25, 2006 · N825BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD FLAP UPPER SKIN WITH NON STANDARD REPAIR AT STATION XF360.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN, AND DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND
- [SDR IXXA06SMN319S](https://openairdocs.org/sdr/IXXA06SMN319S.md): Skin · cracked · Sep 25, 2006 · N825BX · Doug DC871F · Aileron Control System
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD AILERON LEADING EDGE SKIN CRACKED AT STATION XD525.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNAL SURFACE. APPLIED SEALANT TO FAYING SURFACE
- [SDR IXXA06SMN328S](https://openairdocs.org/sdr/IXXA06SMN328S.md): Skin · misrepaired · Sep 25, 2006 · N825BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD FLAP UPPER SKIN HAS NON STANDARD REPAIR AT STATION XW105.000. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN (AL 2024 T3 0.050”), AND DOUBLER (AL 2024 T3 0.032”). BONDED SKIN AND DO
- [SDR IXXA06SMN318S](https://openairdocs.org/sdr/IXXA06SMN318S.md): Skin · misrepaired · Sep 25, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND EXISTING DOUBLER IMPROPER AT STATION 600.000 LONGERON 30 RIGHT. REMOVED EXISTING DOUBLER. TRIMMED OUT DAMAGED AREA. FABRICATED EXTERNAL REPAIR DOUBLER (AL 7075 T6 0.125), INTERNAL FINGER DOUBLER (AL 7075 T6 0.050”),
- [SDR IXXA06SMN317S](https://openairdocs.org/sdr/IXXA06SMN317S.md): Longeron · corroded · Sep 21, 2006 · N825BX · Doug DC871F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C-CHECK, INSPECTION FOUND LONGERON 32 LT CORRODED AT STA 610.000. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED FASTENERS AND REMOVED DAMAGED SECTION. FABRICATED NEW REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA. APPLIED SEALANT TO FAYING
- [SDR IXXA06SMN316S](https://openairdocs.org/sdr/IXXA06SMN316S.md): Longeron · corroded · Sep 21, 2006 · N825BX · Doug DC871F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C CHECK INSPECTION, FOUND LONGERON 34 RIGHT CORRODED BETWEEN STATION 1566.000 AND STATION 1766.000. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED FASTENERS AND REMOVED DAMAGED SECTION. FABRICATED NEW REPAIR PARTS. CLEANED, TREATED AND PRIM
- [SDR IXXA06SMN315S](https://openairdocs.org/sdr/IXXA06SMN315S.md): Frame · corroded · Sep 21, 2006 · N825BX · Doug DC871F · Fuselage Main, Frame
  > DURING ROUTINE C-CHECK INSPECTION, FOUND EXISTING FRAME REPAIR CORRODED AT STA 600 BETWEEN LONGERON 36 AND LONGERON 35 RT. REMOVED EXISTING REPAIR. FABRICATED NEW REPAIR DOUBLER. INTERNAL FINGER DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPA
- [SDR IXXA06SMN313S](https://openairdocs.org/sdr/IXXA06SMN313S.md): Skin · misrepaired · Sep 21, 2006 · N825BX · Doug DC871F · Nacelle/Pylon, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND A NON STANDARD REPAIR ON NUMBER 2 PYLON AT STATION XAR0.000. REMOVED EXISTING NON STANDARD REPAIR FROM STATION XAR0.000 TO STATION XE60.000. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. BONDED PARTS WITH HYSOL.
- [SDR IXXA06SMN314S](https://openairdocs.org/sdr/IXXA06SMN314S.md): Skin · cracked · Sep 21, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION FOUND EXTERNAL SKIN CRACKED AT STATION 405.000, LONGERON 12 RIGHT. CORRECTIVE ACTION: REMOVED FASTENERS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND. CLEANED, TREATED A
- [SDR IXXA06SMN312S](https://openairdocs.org/sdr/IXXA06SMN312S.md): Clamp · improper · Sep 21, 2006 · N825BX · Doug DC871F · Nacelle/Pylon, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND ON NUMBER 2 PYLON ACCESS DOOR NUMBER 297, GENERATOR FEEDER CABLES ATTACH CLAMP IMPROPER. REMOVED FASTENERS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, (AL 2024 T3 0.016). BONDED BOTH PARTS WITH HYSOL. CLEANED,
- [SDR IXXA06SMN308S](https://openairdocs.org/sdr/IXXA06SMN308S.md): Fitting · cracked · Sep 18, 2006 · N825BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C-CHECK INSPECTION, FOUND FITTING CRACKED STA 1220.000 BETWEEN LONGERON 27 RT AND LONGERON 29 RT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. HEAT TREATED NEW FITTING. PERFORMED NDT INSPECTION, NO CRACKS FOUND. CLEANED, TREATED AND PRI
- [SDR IXXA06SMN310S](https://openairdocs.org/sdr/IXXA06SMN310S.md): Fitting · cracked · Sep 18, 2006 · N825BX · Doug DC871F · Fuselage, Landing Gear Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT MAIN LANDING GEAR LEFT TRAPEZOIDAL FITTING WEB CRACKED AT STATION 902.000. REMOVED CRACKED TRAPEZOIDAL FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW TRAPEZOIDAL FITTING AND REINSTALLED INBOARD AND OUT
- [SDR IXXA06SMN309S](https://openairdocs.org/sdr/IXXA06SMN309S.md): Fitting · cracked · Sep 18, 2006 · N825BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND FRAME FITTING CRACKED AT STATION FS 1160.000 LONGERON 27 RIGHT RBL 44. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. HEAT TREATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. CLEANED, TR
- [SDR IXXA06SMN307S](https://openairdocs.org/sdr/IXXA06SMN307S.md): Fitting · cracked · Sep 18, 2006 · N825BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C-CHECK INSPECTION FOUND A CRACKED FITTING AT STATION 1260.000 LONGERON 35 RIGHT. REMOVED CRACKED FITTING. FABRICATED FITTING (AL PLATE 7075 T6 51). PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA, AND FITTING. INSTALLED FITTING. IAW
- [SDR IXXA06SMN311S](https://openairdocs.org/sdr/IXXA06SMN311S.md): Skin · misrepaired · Sep 18, 2006 · N825BX · Doug DC871F · Rudder, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION FOUND NON STANDARD REPAIR ON THE LEFT HAND SIDE OF THE RUDDER FROM STATION ZR 178.000 TO STATION ZR 188.781. REMOVED SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN (AL 2024 T3 0.040). CLEANED, TREATED, AND PRIMED AREA,
- [SDR IXXA06SMN306S](https://openairdocs.org/sdr/IXXA06SMN306S.md): Fitting · cracked · Sep 15, 2006 · N825BX · Doug DC871F · Fuselage, Landing Gear Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR RIGHT HAND TRAPEZOIDAL FITTING OUTBOARD FLANGE CRACKED, AT STATION 902.000. REMOVED CRACKED TRAPEZOIDAL FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW TRAPEZOIDAL FITTING AND OUTBOAR
- [SDR IXXA06SMN300S](https://openairdocs.org/sdr/IXXA06SMN300S.md): Skin · cracked · Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION FOUND EXTERNAL SKIN CRACKED AT STATION -12 LONGERON 27 LEFT. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND
- [SDR IXXA06SMN305S](https://openairdocs.org/sdr/IXXA06SMN305S.md): Fitting · cracked · Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C-CHECK INSPECTION FOUND A CRACKED FITTING AT STATION 240.000 LONGERON 36. REMOVED CRACKED FITTING. FABRICATED FITTING (AL PLATE 7075 T6 51). PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA, AND FITTING.
- [SDR IXXA06SMN304S](https://openairdocs.org/sdr/IXXA06SMN304S.md): Fitting · corroded · Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, FOUND FITTING CORRODED AT STATION 75.000, LONGERON 29 LEFT. REMOVED CORROSION. FOUND OUT ALLOWABLE LIMITS. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-21, DC-8 SRM 5
- [SDR IXXA06SMN301S](https://openairdocs.org/sdr/IXXA06SMN301S.md): Frame · misrepaired · Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Main, Frame
  > DURING ROUTINE C-CHECK INSPECTION FOUND FRAME WITH NON STANDARD REPAIR AT STATION 1580.000 BETWEEN LONGERON 20 LT AND LONGERON 21 LT. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, AFTER DAMAGE REMOVED, NO CRACKS OR CORROSION FOUND. FABRIC
- [SDR IXXA06SMN303S](https://openairdocs.org/sdr/IXXA06SMN303S.md): Longeron · cracked · Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C-CHECK INSPECTION FOUND CRACKED LONGERON AT STATION 1770.000 LONGERON 17 LEFT. REMOVED DAMAGED LONGERON. CLEANED, TREATED, AND PRIMED AREA, AND NEW LONGERON. INSTALLED LONGERON (EXTRUSION P/N S1616757) IAW DC8 SRM 53-1-0, DC-8 SRM 51-1-20D,
- [SDR IXXA06SMN302S](https://openairdocs.org/sdr/IXXA06SMN302S.md): Longeron · cracked · Sep 15, 2006 · N825BX · Doug DC871F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C-CHECK INSPECTION FOUND A CRACKED LONGERON AT STATION 1776.000 LONGERON 17 RIGHT. REMOVED CRACKED LONGERON. CLEANED, TREATED AND PRIMED AREA, AND NEW LONGERON. INSTALLED NEW LONGERON (EXTRUSION P/N S1616757) IAW DC8 SRM 53-5-1 FIG 7 SHEET 1
- [SDR IXXA06SMN293S](https://openairdocs.org/sdr/IXXA06SMN293S.md): Skin · misrepaired · Sep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION FOUND EXISTING REPAIR AT STATION FS 29 LONGERON 9.75 LT, DOES NOT MEET CURRENT SRM CRITERIA. REMOVED EXISTING REPAIR. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR PARTS. CLEANED TREATED AND PRIMED
- [SDR IXXA06SMN299S](https://openairdocs.org/sdr/IXXA06SMN299S.md): Skin · cracked · Sep 12, 2006 · N825BX · Doug DC871F · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE UPPER SKIN CRACKED AT STATION XFS360.000. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PARTS. APPLIED SEALAN
- [SDR IXXA06SMN286S](https://openairdocs.org/sdr/IXXA06SMN286S.md): Skin · misrepaired · Sep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND EXISTING REPAIR AT STATION 370 LONGERON 30.5 RIGHT DOES NOT MEET DTA REQUIREMENTS OF MDC 91K0262 REPORT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. TREATED AND PRIMED AREA AND REPAIR PAR
- [SDR IXXA06SMN292S](https://openairdocs.org/sdr/IXXA06SMN292S.md): Skin · misrepaired · Sep 12, 2006 · N825BX · Doug DC871F · Passenger/Crew Doors
  > DURING ROUTINE C CHECK INSPECTION, FOUND PASSENGER DOOR UPPER AFT CORNER. REPAIR FALLS INTO GROUP 2 PER SERVICE BULLETIN DC 8 53.075, AND AD 2000-20-08 GROUP 2. WITHIN 2,000 LANDINGS OR 3 YEARS AFTER THE EFFECTIVE DATE ACCOMPLISH THE PREVENTATIVE MODIFICATION
- [SDR IXXA06SMN296S](https://openairdocs.org/sdr/IXXA06SMN296S.md): Skin · misrepaired · Sep 12, 2006 · N825BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP EXISTING UPPER SKIN DOUBLER IMPROPER AT STATION, XW38.000. REMOVED EXISTING SKIN WITH EXISTING IMPROPER REPAIR. FABRICATED NEW SKIN WITH AL 2024 T3 0.025” AND BONDED DOUBLER AL 2024 T3 0.020”. BOND
- [SDR IXXA06SMN295S](https://openairdocs.org/sdr/IXXA06SMN295S.md): Skin · misrepaired · Sep 12, 2006 · N825BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C-CHECK INSPECTION, FOUND LT WING IB FLAP EXISTING LOWER. SKIN DOUBLER IMPROPER FROM STATION XW2.000 TO XW91.000. REMOVED EXISTING SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND PRIMED ARE
- [SDR IXXA06SMN289S](https://openairdocs.org/sdr/IXXA06SMN289S.md): Skin · misrepaired · Sep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, FOUND EXISTING REPAIR AT STATION 1430 LONGERON 36 IN CLOSE PROXIMITY TO ANOTHER EXISTING REPAIR AT THE LOWER SIDE OF (D) PIT DOOR. INCORPORATED BOTH REPAIRS INTO ONE REPAIR. (D) PIT DOOR CORNER REPAIR. REMOVED EXISTING RE
- [SDR IXXA06SMN287S](https://openairdocs.org/sdr/IXXA06SMN287S.md): Skin · misrepaired · Sep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE, C-CHECK INSPECTION FOUND EXISTING REPAIR AT STATION 1384 LONGERON 35.5 RT DOES NOT MEET THE DTA REQUIREMENTS OF MDC 91K0262. REMOVED EXISTING REPAIR. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO
- [SDR IXXA06SMN285S](https://openairdocs.org/sdr/IXXA06SMN285S.md): Skin · misrepaired · Sep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER EXISTING REPAIR AT STATION 370 LONGERON 25.5 RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIME
- [SDR IXXA06SMN284S](https://openairdocs.org/sdr/IXXA06SMN284S.md): Skin · misrepaired · Sep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION 248, LONGERON 26 RIGHT. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA
- [SDR IXXA06SMN282S](https://openairdocs.org/sdr/IXXA06SMN282S.md): Skin · misrepaired · Sep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION FOUND EXISTING REPAIR AT STATION 8 LONGERON 28.5 RIGHT DOES NOT MEET THE DTA REQUIREMENTS OD MDC 91K0262. REMOVED EXISTING REPAIR DOUBLER. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEA
- [SDR IXXA06SMN294S](https://openairdocs.org/sdr/IXXA06SMN294S.md): Skin · damaged · Sep 12, 2006 · N825BX · Doug DC871F · Leading Edge Devices
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SLOT VANE SKIN HOLES ELONGATED AT STATION XS 250.000. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION AFTER DAMAGE REMOVED, NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR DOUBLER, INTERN
- [SDR IXXA06SMN288S](https://openairdocs.org/sdr/IXXA06SMN288S.md): Skin · misrepaired · Sep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK, MODIFY CARGO DOOR JAMB CORNERS AT STATION 1420 LONGERON 34.5 RIGHT IAW AD 2004-06-06. REMOVED EXISTING REPAIR. FABRICATED REPAIR PARTS. CLEANED TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED
- [SDR IXXA06SMN283S](https://openairdocs.org/sdr/IXXA06SMN283S.md): Skin · misrepaired · Sep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND EXISTING REPAIR DOES NOT MEET DTA REQUIREMENTS OF MDC 941K0262, AT STATION 8 LONGERON 32.5 LEFT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, NO CRACKS OR CORROSION FOUND. FABRICATED REPA
- [SDR IXXA06SMN291S](https://openairdocs.org/sdr/IXXA06SMN291S.md): Skin · misrepaired · Sep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION FOUND EXISTING DOUBLER AT STATION 1761 LONGERON 16.5 LT FAILED DTA REQUIREMENTS OF MDC 91K0262 REPORT. REMOVED EXISTING REPAIR DOUBLER. FABRICATED REPAIR DOUBLER, INTERNAL FINGER DOUBLER, AND FILLER. CLEANED, TREATED AND PRIM
- [SDR IXXA06SMN290S](https://openairdocs.org/sdr/IXXA06SMN290S.md): Skin · misrepaired · Sep 12, 2006 · N825BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION FOUND IMPROPER REPAIR DOUBLER AT BS 1752 LONGERON 16.5 LT. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, INTERNAL FINGER DOUBLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PA
- [SDR IXXA060457O](https://openairdocs.org/sdr/IXXA060457O.md): Transmitter · failed · Jul 15, 2006 · N825BX · Doug DC871F · Hydraulic Pressure Indicator
  > DURING CRUISE FROM KTOL TO CYJT, CREW NOTICED THE HYDRAULIC PRESSURE DROPPED TO 2000 POUNDS OF PRESSURE. THE CREW ELECTED TO RETURN TO KTOL AND SAFELY LANDED. MAINTENANCE REPLACED THE HYDRAULIC PRESSURE TRANSMITTER. THE HYDRAULIC SYSTEM OPERATIONAL CHECK WA
- [SDR IXXA060451O](https://openairdocs.org/sdr/IXXA060451O.md): Adi · faulty · Jun 21, 2006 · N825BX · Doug DC871F · Integrated Flight System
  > DURING CRUISE FROM KMIA THE CAPTAINS ADI DISPLAYED BOTH FLIGHT DIRECTOR AND GYRO FLAGS, FLAGS STAYED IN VIEW FOR APPROXIMATELY 1-2 MINUTES THEN WENT AWAY FOR APPROXIMATELY 5 MINUTES, THEN INTERMITTENTLY DISPLAYED AFTER THAT. THE CREW RETURNED TO KMIA AND LAND

Next page: https://openairdocs.org/deregistered/N825BX-2014-05-01/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 = 'N825BX' AND deregistration_id = 'N825BX-2014-05-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N825BX-2014-05-01/reports

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