# Service difficulty reports: N990CF, cancelled May 15, 2002 A list on [N990CF, cancelled May 15, 2002](https://openairdocs.org/deregistered/N990CF-2002-05-15.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR RRXA003162](https://openairdocs.org/sdr/RRXA003162.md): Fitting · cracked · Aug 9, 2000 · N990CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING 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. - [SDR RRXA003161](https://openairdocs.org/sdr/RRXA003161.md): Fitting · cracked · Aug 9, 2000 · N990CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING 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. - [SDR RRXA003168](https://openairdocs.org/sdr/RRXA003168.md): Strap · torn · May 25, 2000 · N990CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING 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. - [SDR RRXA003163](https://openairdocs.org/sdr/RRXA003163.md): Strap · torn · May 25, 2000 · N990CF · Doug DC862 · Fuselage Main, Structure > DURING 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. - [SDR RRXA003172](https://openairdocs.org/sdr/RRXA003172.md): Skin · damaged · May 8, 2000 · N990CF · Doug DC862 · Nacelle/Pylon, Plate/Skin > DURING 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. - [SDR RRXA003171](https://openairdocs.org/sdr/RRXA003171.md): Fitting · cracked · May 8, 2000 · N990CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING 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 364585 - [SDR RRXA003170](https://openairdocs.org/sdr/RRXA003170.md): Doubler · damaged · May 8, 2000 · N990CF · Doug DC862 · Fuselage Main, Plate/Skin > DURING 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. - [SDR RRXA003169](https://openairdocs.org/sdr/RRXA003169.md): Longeron · cracked · May 8, 2000 · N990CF · Doug DC862 · Fuselage Main, Longeron/Stringer > DURING 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. - [SDR RRXA003167](https://openairdocs.org/sdr/RRXA003167.md): Skin · damaged · May 8, 2000 · N990CF · Doug DC862 · Nacelle/Pylon, Plate/Skin > DURING 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. - [SDR RRXA003166](https://openairdocs.org/sdr/RRXA003166.md): Fitting · cracked · May 8, 2000 · N990CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING 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. - [SDR RRXA003165](https://openairdocs.org/sdr/RRXA003165.md): Doubler · damaged · May 8, 2000 · N990CF · Doug DC862 · Fuselage Main, Plate/Skin > DURING 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. - [SDR RRXA003164](https://openairdocs.org/sdr/RRXA003164.md): Longeron · cracked · May 8, 2000 · N990CF · Doug DC862 · Fuselage Main, Longeron/Stringer > DURING 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. - [SDR RRXA000001](https://openairdocs.org/sdr/RRXA000001.md): Bullet · damaged · Jan 12, 2000 · N990CF · Doug DC862 · Turbine Engine Compressor Section > NR 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. I - [SDR RRXA991174](https://openairdocs.org/sdr/RRXA991174.md): Plate · damaged · Jul 23, 1999 · N990CF · Doug DC862 · Fuselage Miscellaneous Structure > REPAIR 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. - [SDR RRXA99004](https://openairdocs.org/sdr/RRXA99004.md): Rod End · failed · Jan 14, 1999 · N990CF · Doug DC862 · Landing Gear Retraction/Extension System > UPON 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 - [SDR RRXA98280](https://openairdocs.org/sdr/RRXA98280.md): Fitting · corroded · May 21, 1998 · N990CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING 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. - [SDR RRXA98279](https://openairdocs.org/sdr/RRXA98279.md): Fitting · corroded · May 21, 1998 · N990CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING 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. - [SDR RRXA98278](https://openairdocs.org/sdr/RRXA98278.md): Fitting · corroded · May 20, 1998 · N990CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING 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. - [SDR RRXA98282](https://openairdocs.org/sdr/RRXA98282.md): Skin · corroded · May 16, 1998 · N990CF · Doug DC862 · Horizontal Stabilizer, Plate/Skin > DURING 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 DOUBL - [SDR RRXA98281](https://openairdocs.org/sdr/RRXA98281.md): Longeron · corroded · May 11, 1998 · N990CF · Doug DC862 · Fuselage Main, Longeron/Stringer > DURING 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. - [SDR RRXA98219](https://openairdocs.org/sdr/RRXA98219.md): Fitting · corrosion · May 4, 1998 · N990CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING 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. - [SDR RRXA98218](https://openairdocs.org/sdr/RRXA98218.md): Skin · corrosion · May 4, 1998 · N990CF · Doug DC862 · Fuselage Main, Plate/Skin > DURING 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 SKETCH - [SDR RRXA98076](https://openairdocs.org/sdr/RRXA98076.md): Pin · broken · Apr 9, 1998 · N990CF · Doug DC862 · Landing Gear Retraction/Extension System > DOORS 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 G - [SDR RRXA97223](https://openairdocs.org/sdr/RRXA97223.md): Mechanism · lack of lube · Aug 20, 1997 · N990CF · Doug DC862 · Cargo/Baggage Doors > AT 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. - [SDR RRXA96163](https://openairdocs.org/sdr/RRXA96163.md): Fluorescent Bulb · failed · Nov 5, 1996 · N990CF · Doug DC862 · Flight Compartment Lighting > ON 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. - [SDR 95ZZZX6630](https://openairdocs.org/sdr/95ZZZX6630.md): Uplatch Mech · lack of lube · Nov 16, 1995 · N990CF · Doug DC862 · Landing Gear Retraction/Extension System > KDAY/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 M - [SDR 95ZZZX4248](https://openairdocs.org/sdr/95ZZZX4248.md): Retract Pin · sheared · Jul 21, 1995 · N990CF · Doug DC862 · Landing Gear Retraction/Extension System > KEWR/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 FOUN ## 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 = 'N990CF' AND deregistration_id = 'N990CF-2002-05-15' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N990CF-2002-05-15/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.