N990CF, cancelled May 15, 2002

Service difficulty reports · 27

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 = 'N990CF' AND deregistration_id = 'N990CF-2002-05-15'
  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 RRXA003162Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE SPLICE FITTING IN THE FWD LWR CARGO COMPT BETWEEN STA''S 600 AND 620 AND L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Aug 9, 2000 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA003161Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE SPLICE FITTING IN THE AFT ACCESSORY COMPT AT STA 1340 AND 1360 AND L29R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Aug 9, 2000 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA003168Strap · tornDURING A MAINTENANCE VISIT FOUND A TEAR TO THE STRAP BETWEEN STRINGERS AT STA 902 AND 9 - 10 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW PD08-53-049.May 25, 2000 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA003163Strap · tornDURING A MAINTENANCE VISIT FOUND A TEAR TO THE STRAP BETWEEN STRINGERS AT STA 902 STRINGER 9-10 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW PD 08-53-049.May 25, 2000 · N990CF · Doug DC862 · Fuselage Main, StructureSDR RRXA003172Skin · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE NR 2 ENGINE PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED PART IAW DC-8 SRM 51-1-20D.May 8, 2000 · N990CF · Doug DC862 · Nacelle/Pylon, Plate/SkinSDR RRXA003171Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LONGERON END FITTING AT FS 902 AND L10L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW SRM 51-1-20D, EA PD08-53-048 AND DWG 364585May 8, 2000 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA003170Doubler · damagedDURING A MAINTENANCE VISIT FOUND A TEMP REPAIR ON FUSELAGE AT STA 879 TO 946 AND L5L TO L11L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EA PD08-53-047.May 8, 2000 · N990CF · Doug DC862 · Fuselage Main, Plate/SkinSDR RRXA003169Longeron · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LONGERON AT FS 935 AND L9L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 1D, 51-1-24 AND 51-1-8 FIG 10.May 8, 2000 · N990CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR RRXA003167Skin · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE NR 2 ENGINE PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D.May 8, 2000 · N990CF · Doug DC862 · Nacelle/Pylon, Plate/SkinSDR RRXA003166Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE END FITTING ON THE LONGERON AT FS 902 AND L10L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, EA PD08-53-048 AND DWG 3645859.May 8, 2000 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA003165Doubler · damagedDURING A MAINTENANCE VISIT FOUND A TEMP REPAIR ON FUSELAGE AT STA 879 TO 946 AND L5L TO L11L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW EA PD08-53-047.May 8, 2000 · N990CF · Doug DC862 · Fuselage Main, Plate/SkinSDR RRXA003164Longeron · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LONGERON 9L AT FS 935, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 1D AND 51-1-24.May 8, 2000 · N990CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR RRXA000001Bullet · damagedNR 3 ENG COMP STALLED VIOLENTLY AND REPEATEDLY ON CLIMB-OUT. NR 1 ENG COMP STALLED REPEATEDLY ON CLIMB-OUT. INSP NR 3 EMG INLET AND EXH FOR DAMAGE. NONE NOTED ENG RUNUP. PERFORMED MANIFOLD DECAY, INTERSTAGE BLEED SCHEDULE, HIGH STAGE BLEED AND REG CHKS. IJan 12, 2000 · N990CF · Doug DC862 · Turbine Engine Compressor SectionSDR RRXA991174Plate · damagedREPAIR MAIN CARGO DOOR UPPER JAMB HANGER PLATE PER COTNEY ENG DRW. REPAIRED MAIN CARGO DOOR UPPER JAMBHEADER PLATE PER COTNEY ENG'G DWG EAH 70-1, EMERY DWG NR 70-R01, STC1802SD.Jul 23, 1999 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA99004Rod End · failedUPON LANDING GEAR EXTENSION THE RIGHT MAIN LANDING GEAR FREE FELL INTO THE DOWN AND LOCKED POSITION. AFTER LANDING THE GEAR WAS PINNED AS A PRECAUTION, TAXIED TO RAMP. ACFT FERRIED TO KMCN FOR REMOVAL AND REPLACEMENT OF RT MLG BOSS PIN IAW DC-8 SB 32-102 PG Jan 14, 1999 · N990CF · Doug DC862 · Landing Gear Retraction/Extension SystemSDR RRXA98280Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND LONGERON 24 RIGHT FITTING CORRODED BEYOND LIMITS IAW DC-8 SRM, AT STA 940. REMOVED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-1-0, PAGE 1.May 21, 1998 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA98279Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND LONGERON 24 RIGHT FITTING CORRODED BEYOND DC-8 SRM LIMITS, AT STA 920. REMOVED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW 53-1-0, PAGE 1.May 21, 1998 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA98278Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND LONGERON 24 RIGHT FITTING CORRODED BEYOND DC-8 LIMITS, AT STA 960. REMOVED DAMAGED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-1-20D.May 20, 1998 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA98282Skin · corrodedDURING A MAINTENANCE VISIT, FOUND HORIZONTAL STABILIZER LEADING EDGE RIGHT SIDE WITH EXFOLIATION CORROSION BEYOND DC-8 SRM LIMITS, AT STA XFS 178 TO STA XFS 200. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLMay 16, 1998 · N990CF · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR RRXA98281Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND LONGERON 24 RIGHT CORRODED BEYOND LIMITS IAW DC-8 SRM, AT STA 1480 TO 1500. REMOVED LONGERON 24 RIGHT, TREATED AREA IAW DC-8 SRM. FABRICATED AND INSTALLED NEW SECTION OF LONGERON IAW DC-8 SRM 53-2-2, FIGURE 10.May 11, 1998 · N990CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR RRXA98219Fitting · corrosionDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME FITTING AT STA 270 AND LONGERON 33 RIGHT. REMOVED DAMAGED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E54-R02.May 4, 1998 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA98218Skin · corrosionDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FUSELAGE SKIN AT STA 487 TO STA 490 AND LONGERON 29 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCHMay 4, 1998 · N990CF · Doug DC862 · Fuselage Main, Plate/SkinSDR RRXA98076Pin · brokenDOORS AND LANDING GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER GEAR HANDLE WAS PLACED IN THE UP POSITION. TOWER REPORTED LEFT MAIN LANDING GEAR DOWN. HYDRAULIC PRESSURE AND QUANTITY GOOD, THREE GEAR PINS ON BOARD. AIRCRAFT GEAR CYCLED ONCE TOWER REPORTED GApr 9, 1998 · N990CF · Doug DC862 · Landing Gear Retraction/Extension SystemSDR RRXA97223Mechanism · lack of lubeAT 0357Z ON TAKEOFF, AIRCRAFT MAIN CARGO DOOR LIGHT CAME ON. WOULD NOT PRESSURIZE PROPERLY WITH ALL T/C'S ON. RETURNED TO KCLT. SERVICED MAIN CARGO DOOR, LUBED DOOR LOCKS AND PINS, PERFORMED OPERATIONS CHECK MANUALLY AND ELECTRICALLY. NO DEFECTS NOTED.Aug 20, 1997 · N990CF · Doug DC862 · Cargo/Baggage DoorsSDR RRXA96163Fluorescent Bulb · failedON TAXI IN, SMOKE WAS SEEN FROM UNDER THE GLARESHIELD. MAINTENANCE FOUND THE CAPTAIN'S FLUORESCENT BULB SMOKED. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S FLUORESCENT BULB. NO OTHER DEFECTS NOTED.Nov 5, 1996 · N990CF · Doug DC862 · Flight Compartment LightingSDR 95ZZZX6630Uplatch Mech · lack of lubeKDAY/KCLT - FLT 004 - AFTER TAKEOFF DURING THE UPLATCH CHECK, THE LANDING GEAR UNSAFE LIGHT ILLUMINATED AND THE NOSE GEAR APPEARED TO FALL OUT OF THE NOSE WELL. THIS OCCURRED AFTER SEVERAL CYCLES OF THE LANDING GEAR. MAINTENANCE LUBED THE NOSE GEAR UPLATCH MNov 16, 1995 · N990CF · Doug DC862 · Landing Gear Retraction/Extension SystemSDR 95ZZZX4248Retract Pin · shearedKEWR/KBWI - FLT 118 - AFTER TAKEOFF OUT OF KEWR, THE DOORS, LIGHT, AND LANDING GEAR UNSAFE LIGHT STAYED ILLUMINATED. FOLLOWED ABNORMAL PROCEDURE AND LIGHTS STAYED ILLUMINATED. HYDRAULIC PRESSURE AND QTY NORMAL. NORMAL LANDING MADE AT KBWI. MAINTENANCE FOUNJul 21, 1995 · N990CF · Doug DC862 · Landing Gear Retraction/Extension System
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