# Service difficulty reports: N822BX, cancelled May 1, 2014

A list on [N822BX, cancelled May 1, 2014](https://openairdocs.org/deregistered/N822BX-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 · 222 reports

- [SDR IXXA110044O](https://openairdocs.org/sdr/IXXA110044O.md): Striker · bent · Jun 4, 2011 · N822BX · Doug DC871F · Landing Gear Position and Warning
  > DURING CRUISE, THE MLG DOOR LIGHT REMAINED ON. THE CREW CYCLED THE MAIN LANDING GEAR AND LIGHT REMAINED ON. WHEN AIRSPEED INCREASED TO 210 IAS LIGHT WENT OUT. THEY LANDED WITHOUT FURTHER INCIDENT. MX TROUBLESHOT AND FOUND THE RT GEAR DOOR STRIKER BENT. TH
- [SDR IXXA110023O](https://openairdocs.org/sdr/IXXA110023O.md): Wire Harness · defective · Feb 18, 2011 · N822BX · Doug DC871F · Engine Indicating System Wiring
  > DURING CLIMBOUT FROM KTOL NR ONE EGT ANALOG AND DIGITAL READ OUTS DROPPED FROM 700 DEGREE TO 420 DEGREE WITH FLUCTUATION PLUS/ MINUS 5 DEGREE, N1 AND N2 SIMILAR TO THE OTHER 3 ENG. ALL 4 THROTTLES WERE ALIGNED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER
- [SDR IXXA100053S](https://openairdocs.org/sdr/IXXA100053S.md): Skin · corroded · Oct 11, 2010 · N822BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE B-CHECK, INSP FOUND CORROSION ON FUSELAGE SKIN AT STA 73 LONGERON 31 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REP
- [SDR IXXA100021O](https://openairdocs.org/sdr/IXXA100021O.md): Valve · leaking · Mar 5, 2010 · N822BX · Doug DC871F · Hydraulic System, Main
  > DURING CRUISE, THE RT HYD PRESSURE WAS AT ZERO AND THE LT HYD WAS FLUCTUATING. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX FOUND RESERVOIR DEPRESSURIZTION VALVE LEAKING. REPLACED RESERVOIR DEPRESSURIZATION VALVE. OPS CHECK GOOD IAW UAL MM29-13-
- [SDR IXXA100016O](https://openairdocs.org/sdr/IXXA100016O.md): Pump · cracked · Feb 18, 2010 · N822BX · Doug DC871F · Hydraulic Pump (Electric/Engine), Main
  > DURING CRUISE, THE AILERON AND RUDDER REVERSION LIGHT CAME ON, THE CREW ALSO NOTICED LOSS OF HYD PRESSURE AND QUANTITY. CREW ACCOMPLISHED PROCEDURES IAW QRH NR 27. DECLARED EMERGENCY LANDING WITHOUT FURTHER INCIDENT. MX FOUND CABIN AIR CHECK VALVE CLOGGED AN
- [SDR IXXA100006S](https://openairdocs.org/sdr/IXXA100006S.md): Skin · cracked · Dec 23, 2009 · N822BX · Doug DC871F · Wing, Plate/Skin
  > LT WING LOWER SKIN CRACKED AT STATION 428.0. REPAIRED SKIN IAW CASTLE SKETCH 20100104028.
- [SDR IXXA100004S](https://openairdocs.org/sdr/IXXA100004S.md): Stringer · cracked · Dec 23, 2009 · N822BX · Doug DC871F · Wing, Longeron/Stringer
  > LT WING STRINGER 62 CRACKED. REPAIRED STRINGER IAW SRM 57-2-1 AND CASTLE SKETCH 20100104018.
- [SDR IXXA100005S](https://openairdocs.org/sdr/IXXA100005S.md): Stringer · cracked · Dec 23, 2009 · N822BX · Doug DC871F · Wing, Longeron/Stringer
  > LT WING STRINGER 63 CRACKED. REPAIRED STRINGER 63 IAW SRM 57-2-1 AND CASTLE SKETCH 20100104018.
- [SDR IXXA100003S](https://openairdocs.org/sdr/IXXA100003S.md): Stringer · cracked · Dec 23, 2009 · N822BX · Doug DC871F · Wing, Longeron/Stringer
  > RT WING FOUND STRINGER 62 CRACKED. REPAIRED STRINGER 62 IAW SRM 57-2-2.
- [SDR IXXA100002S](https://openairdocs.org/sdr/IXXA100002S.md): Skin · cracked · Dec 23, 2009 · N822BX · Doug DC871F · Wing, Plate/Skin
  > RT WING LOWER SKIN CRACKED BETWEEN FWD AND AFT OF STRINGER 62. REPAIRED SKIN IAW SRM 57-2-1.
- [SDR IXXA090074O](https://openairdocs.org/sdr/IXXA090074O.md): Adi · defective · Dec 15, 2009 · N822BX · Doug DC871F · Flight Environment Data
  > DURING CLIMB OUT, CAPTAIN’S FLIGHT DIRECTOR INDICATOR READ’S DIFFERENT FROM THE F/O FLIGHT DIRECTOR INDICATOR, ALSO READ’S DIFFERENT IN FLIGHT LEVEL AND DESCENT. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED CAPTAIN’S FLIGHT DIRECTOR IN
- [SDR IXXA090070O](https://openairdocs.org/sdr/IXXA090070O.md): Relief Valve · defective · Dec 11, 2009 · N822BX · Doug DC871F · Hydraulic Indicating System
  > DURING CLIMB OUT, HYD PRESSURE DROPPED TO ZERO, AILERON AND MANUAL REVERSION LIGHTS ILLUMINATED. THE CREW ACCOMPLISHED ALL PROCEDURES IAW QRH, NO LOSS OF HYD QUANTITY. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED AND REPLACED DUAL FILT
- [SDR IXXA090054O](https://openairdocs.org/sdr/IXXA090054O.md): Rmi · defective · Sep 30, 2009 · N822BX · Doug DC871F · Magnetic Compass
  > DURING CRUISE, THE COMPASS CARD ON NR 2 RADIO MAGNETIC INDICATOR FROZE IN POSITION. AFTER SEVERAL MINUTES THE COMPASS CARD STARTED MOVING BUT IS 180 DEGREE OFF OF AIRCRAFT HEADING. THE CREW RETURNED TO KLRD WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 R
- [SDR IXXA090046O](https://openairdocs.org/sdr/IXXA090046O.md): Fire Loop · defective · Sep 1, 2009 · N822BX · Doug DC871F · Fire Detection
  > DURING CLIMB OUT, NR 4 FIRE WARNING HORN SOUNDED, THEN SILENCED AND SOUNDED AGAIN. THE CREW DISCHARGED BOTH BOTTLES AND SHUTDOWN NR 4 ENGINE. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED CORE FIRE LOOP, CORE LOOP CONNECTORS AND BOTH FIRE
- [SDR IXXA090045O](https://openairdocs.org/sdr/IXXA090045O.md): Radio · defective · Aug 31, 2009 · N822BX · Doug DC871F · VHF Communications System
  > DURING CLIMB OUT, NR 2 VHF RADIO WILL NOT TRANSMIT FROM ANY POSITION. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX REPLACED FIRST OBSERVERS AUDIO SELECT PANEL AND VHF/FM COMM TRANSCEIVER. OPS CHECK GOOD IAW MM 23-20-1, AND 23-50-1. ACFT WAS
- [SDR IXXA090014O](https://openairdocs.org/sdr/IXXA090014O.md): Wire · defective · Apr 1, 2009 · N822BX · Doug DC871F · Hydraulic Power System Wiring
  > DURING CRUISE FROM KPHL, BOTH AILERON AND RUDDER MANUAL LIGHTS CAME ON, HYDRAULIC SYSTEM PRESSURE INDICATED ZERO, HYDRAULIC QUANTITY SHOWS FULL. THE CREW ACCOMPLISHED LOSS OF HYDRAULICS CHECKLIST IN DC-8 QRH. THE CREW LANDED IN KTOL WITHOUT FURTHER INCIDENT.
- [SDR IXXA090009O](https://openairdocs.org/sdr/IXXA090009O.md): Fire Loop · false activation · Mar 10, 2009 · N822BX · Doug DC871F · Fire Detection
  > DURING CLIMB FROM MGUM NR 4 ENGINE SHORT CIRCUIT LIGHT ILLUMINATED, FIRE WARNING WOULD NOT TEST. THE CREW SHUTDOWN NUMBER FOUR ENGINE PER COM PROCEDURES. WIND MILLING OIL PRESSURE WAS 3PSI. THE CREW LANDED IN KNGU WITHOUT FURTHER INCIDENT. MAINTENANCE REPL
- [SDR G412008F00000](https://openairdocs.org/sdr/G412008F00000.md): Ground Wire · broken · Jun 6, 2008 · N822BX · Doug DC871F · Fire Protection System Wiring
  > AFTER TAKEOFF FROM KIAH, NR 1 ENGINE FIRE WARNING SOUNDED, FIRE HANDLE LIGHT, AND MASTER FIRE WARNING LIGHT ILLUMINATED. WARNING HORN COULD BE SILENCED BUT CAME BACK ON THREE TIMES. ENGINE FIRE HANDLE SUBSEQUENTLY PLACED IN SELECT AGENT POSITION; LIGHT AND H
- [SDR IXXA08SMN090S](https://openairdocs.org/sdr/IXXA08SMN090S.md): Fitting · cracked · Feb 26, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 5 TRACK NUT BARRIER FITTING CRACKED AT STATION 70.000. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED MAGNETIC PARTICLE INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TR
- [SDR IXXA08SMN081S](https://openairdocs.org/sdr/IXXA08SMN081S.md): Fitting · cracked · Feb 15, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 857.000 LONGERON 1. REMOVED CRACKED FITTING. FABRICATED FITTING PERFORMED LIQUID PENETRANT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA
- [SDR IXXA08SMN088S](https://openairdocs.org/sdr/IXXA08SMN088S.md): Skin · dented · Feb 15, 2008 · N822BX · Doug DC871F · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP LOWER FORWARD PANEL PLATING DENTED AT STATION XW 2.000 - STA XW 91.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND BONDED DOUBLER. BONDED PARTS AS
- [SDR IXXA08SMN087S](https://openairdocs.org/sdr/IXXA08SMN087S.md): Skin · cracked · Feb 15, 2008 · N822BX · Doug DC871F · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER INNER SKIN INBOARD SPLICE CRACKED AT STATION XFS 341.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION.
- [SDR IXXA08SMN085S](https://openairdocs.org/sdr/IXXA08SMN085S.md): Skin · dented · Feb 15, 2008 · N822BX · Doug DC871F · Elevator, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR LOWER SKIN DENTED AT STATION XE 246.875. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AN
- [SDR IXXA08SMN084S](https://openairdocs.org/sdr/IXXA08SMN084S.md): Skin · misrepaired · Feb 15, 2008 · N822BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK, FOUND AT EXTERNAL DOUBLER AFT LOWER FUSELAGE BELLY TAIL SKID FAIRING HAS IMPROPER REPAIR AT STATION FS 1745 LONGERON 35.5 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED SKIN. FABRICATED
- [SDR IXXA08SMN082S](https://openairdocs.org/sdr/IXXA08SMN082S.md): Fitting · cracked · Feb 15, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FRAME FITTING CRACKED AT STATION 879.000 LONGERON 18 RIGHT TO LONGERON-19 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED FITTING. PERFORMED NDT INSPECTION. NO CRACK NO CORROSION FOU
- [SDR IXXA08SMN089S](https://openairdocs.org/sdr/IXXA08SMN089S.md): Skin · misrepaired · Feb 15, 2008 · N822BX · Doug DC871F · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING LEADING CENTER LEADING EDGE OUTER SKIN LOWER SHOWS IMPROPER REPAIR AT STATION XFS 385.200. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPE
- [SDR IXXA08SMN086S](https://openairdocs.org/sdr/IXXA08SMN086S.md): Skin · cracked · Feb 15, 2008 · N822BX · Doug DC871F · Fuselage Main, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT FUSELAGE TAIL SECTION PLATING CRACKED AT STATION FS 1766.000 TO STATION 1781.000 LONGERON10 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR
- [SDR IXXA08SMN080S](https://openairdocs.org/sdr/IXXA08SMN080S.md): Support Fitting · cracked · Feb 15, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TAIL SKID SUPPORT FITTING CRACKED AT STATION 1734.000 LONGERON36. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-3-1, DC8 SRM 51-1-20D, DC8 SRM 51-1-8B.
- [SDR IXXA08SMN079S](https://openairdocs.org/sdr/IXXA08SMN079S.md): Skin · dented · Feb 15, 2008 · N822BX · Doug DC871F · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD AFT LOWER FLAP SKIN SHOWS DENTS AT STATION XE 2.000 TO STA XE 91.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS AS NEEDED WI
- [SDR IXXA08SMN078S](https://openairdocs.org/sdr/IXXA08SMN078S.md): Skin · dented · Feb 15, 2008 · N822BX · Doug DC871F · Ailerons
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD AILERON UPPER SKIN HAS DENT AND NO STANDARD REPAIR AT STATION XA 580.000 TO XA 610.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PART
- [SDR IXXA08SMN077S](https://openairdocs.org/sdr/IXXA08SMN077S.md): Frame · cracked · Feb 14, 2008 · N822BX · Doug DC871F · Fuselage Main, Frame
  > DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT FRAME LOWER FLANGE CRACKED AT STATION 480.000 LONGERON 34 RIGHT. REMOVED DAMAGED AREA. FABRICATED NEW FRAME SEGMENT, SPLICES, ANGLES. HEAT TREATED EXTRUSION FRAME SEGMENT. CLEANED, TREATED,
- [SDR IXXA08SMN076S](https://openairdocs.org/sdr/IXXA08SMN076S.md): Skin · dented · Feb 14, 2008 · N822BX · Doug DC871F · Elevator, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND ELEVATOR LEFT UPPER SKIN SHOWS DENTS AND CORROSION AT DIFFERENT POINTS AT STATION XE 146.000 AND XE 270.000. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAG
- [SDR IXXA08SMN075S](https://openairdocs.org/sdr/IXXA08SMN075S.md): Skin · misrepaired · Feb 14, 2008 · N822BX · Doug DC871F · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER OUTER SKIN SHOWS IMPROPER REPAIR AT STATION XOLDI 6.2246. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION.
- [SDR IXXA08SMN074S](https://openairdocs.org/sdr/IXXA08SMN074S.md): Skin · misrepaired · Feb 14, 2008 · N822BX · Doug DC871F · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER OUTER SKIN SHOWS IMPROPER REPAIR AT STATION XFS 304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRA
- [SDR IXXA08SMN072S](https://openairdocs.org/sdr/IXXA08SMN072S.md): Skin · scratched · Feb 14, 2008 · N822BX · Doug DC871F · Elevator, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN SHOWS SCRATCHES AT STATION XE 273.000 TO STATION XE 283.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED
- [SDR IXXA08SMN073S](https://openairdocs.org/sdr/IXXA08SMN073S.md): Flap · dented · Feb 14, 2008 · N822BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBD FLAP UPPER PART SHOWS DENTS AT STATION XF 375.000 TO STA XF 404.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL.
- [SDR IXXA08SMN070S](https://openairdocs.org/sdr/IXXA08SMN070S.md): Fitting · cracked · Feb 14, 2008 · N822BX · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO INTERCOSTAL END CLIP CRACKED AT STATION 857.000 LONGERON 18 RIGHT. REMOVED CRACKED INTERCOSTAL END CLIP. FABRICATED INTERCOSTAL END CLIP. PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND INT
- [SDR IXXA08SMN047S](https://openairdocs.org/sdr/IXXA08SMN047S.md): Fitting · cracked · Feb 14, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND AFT ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 1690.000 LONGERON 28 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-3-1, SRM 51-1-20D, AND SRM 51-
- [SDR IXXA08SMN071S](https://openairdocs.org/sdr/IXXA08SMN071S.md): Skin · dented · Feb 14, 2008 · N822BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD FLAP LOWER AFT SKIN HAS DENTS AT STATION XF 434.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED,
- [SDR IXXA08SMN065S](https://openairdocs.org/sdr/IXXA08SMN065S.md): Skin · dented · Feb 8, 2008 · N822BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN FORWARD SHOWS DENTS BETWEEN STATION XF 160.000 - XF 213.000. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK NO CORROSION FOUND. PERFORMED MEASUREMENT DIA 2.00 BY 0.008" DEPTH WITHIN PERM
- [SDR IXXA08SMN067S](https://openairdocs.org/sdr/IXXA08SMN067S.md): Fitting · cracked · Feb 8, 2008 · N822BX · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 847.000 LONGERON1. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-1-8-B, DC8 SRM 51-1-2
- [SDR IXXA08SMN63S](https://openairdocs.org/sdr/IXXA08SMN63S.md): Skin · dented · Feb 8, 2008 · N822BX · Doug DC871F · Trailing Edge Flaps
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN SHOWS DENTS AT STATION XF 434.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED TREA
- [SDR IXXA08SMN062S](https://openairdocs.org/sdr/IXXA08SMN062S.md): Fitting · cracked · Feb 8, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FITTING CRACKED AT STATION 680.000 LONGERON 11 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-0, DC8 SRM 51-1-21, AND DC8 SRM 51-
- [SDR IXXA08SMN061S](https://openairdocs.org/sdr/IXXA08SMN061S.md): Fitting · corroded · Feb 8, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CORRODED AT STATION 960.000 TO STATION 980.000 LEFT BUTTOCKS LINE 45. REMOVED CORRODED FITING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3
- [SDR IXXA08SMN066S](https://openairdocs.org/sdr/IXXA08SMN066S.md): Fitting · cracked · Feb 8, 2008 · N822BX · Doug DC871F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 690.000 LONGERON 1. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, AND DC8 SRM 51-1-8B.
- [SDR IXXA08SMN064S](https://openairdocs.org/sdr/IXXA08SMN064S.md): Skin · dented · Feb 8, 2008 · N822BX · Doug DC871F · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN DENTS AT STATION XF 169.000 - XF 213.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEAN
- [SDR IXXA08SMN054S](https://openairdocs.org/sdr/IXXA08SMN054S.md): Skin · scratched · Feb 7, 2008 · N822BX · Doug DC871F · Ailerons
  > DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD AILERON LOWER SKIN SCRATCHED BETWEEN STATION XA 737.000 AND XA 763.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH
- [SDR IXXA08SMN053S](https://openairdocs.org/sdr/IXXA08SMN053S.md): Support Angle · cracked · Feb 7, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FORMER CRACKED AT STATION 1766.000 LONGERON1. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP HOLE ON END CRACK. FABRICATED ANGLE DOUBLER. PERFORMED HEAT TREATMENT CLEANED, TREATED AND PRIME
- [SDR IXXA08SMN052S](https://openairdocs.org/sdr/IXXA08SMN052S.md): Fitting · cracked · Feb 7, 2008 · N822BX · Doug DC871F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FITTING CRACKED AT STATION 680.000 LONGERON 20 RT. REMOVE CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-3-1, SRM 51-1-20D, AND SRM 51-1-8B.
- [SDR IXXA08SMN058S](https://openairdocs.org/sdr/IXXA08SMN058S.md): Skin · dented · Feb 7, 2008 · N822BX · Doug DC871F · Rudder, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, FOUND RUDDER RIGHT SKIN SIDE DENTED AT STATION ZR 276.531 TO ZR 267.218. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE PANEL PLATING. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CL

Next page: https://openairdocs.org/deregistered/N822BX-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 = 'N822BX' AND deregistration_id = 'N822BX-2014-05-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N822BX-2014-05-01/reports

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