# Service difficulty reports: N899US, cancelled Oct 16, 2003 A list on [N899US, cancelled Oct 16, 2003](https://openairdocs.org/deregistered/N899US-2003-10-16.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAF01032](https://openairdocs.org/sdr/USAAF01032.md): Battery Pack · faulty · Jun 6, 2001 · N899US · Fokker F28MK0100 · Emergency Lighting > RIC - FOUND NR 6 CEILING AND LAVATORY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE NR 8 BATTERY PACK. OPERATIONALLY CHECKED OK. (M) - [SDR USAA010410](https://openairdocs.org/sdr/USAA010410.md): Stringer · cracked · Mar 21, 2001 · N899US · Fokker F28MK0100 · Fuselage Main, Longeron/Stringer > PIT - FOUND STRINGER CRACKED.75 INCH, STRINGER 69, STATION 3850. REPAIRED PER SRM 51-70-06 DOUBLER. (M) - [SDR USAAF00065](https://openairdocs.org/sdr/USAAF00065.md): Slide · malfunctioned · Aug 22, 2000 · N899US · Fokker F28MK0100 · Escape Slide > PIT - THE FORWARD ENTRY L1 DOOR WAS OPENED WITH THE SLIDE IN THE ARMED POSITION. THE SLIDE FELL FROM THE BUSTLE, BUT DID NOT DEPLOY. MAINTENANCE REPLACED THE L1 DOOR ESCAPE SLIDE. OK FOR SERVICE. (M) - [SDR USAAF00028](https://openairdocs.org/sdr/USAAF00028.md): Slide · inoperative · Mar 28, 2000 · N899US · Fokker F28MK0100 · Escape Slide > ALB - THE FORWARD SERVICE DOOR WAS INADVERTENTLY DEPLOYED, BUT THE SLIDE DID NOT INFLATE. MAINTENANCE REPLACED THE FORWARD SERVICE DOOR SLIDE. (M) - [SDR USAAF00019](https://openairdocs.org/sdr/USAAF00019.md): Sensor · damaged · Feb 26, 2000 · N899US · Fokker F28MK0100 · Landing Gear Position and Warning > CLT-ILM - FLT 704 - AFTER TAKEOFF, THE LANDING GEAR HANDLE WAS JAMMED. THE LANDING GEAR OVERRIDE WAS PRESSED AND THE GEAR BEGAN TO RETRACT. AT THAT THE TIME THE ANNUNCIATOR INDICATED BRD/FLT CNTL. THE LANDING GEAR WAS LOWERED AND THE AIRCRAFT RETURNED TO TH - [SDR USAAF00010](https://openairdocs.org/sdr/USAAF00010.md): Bracket · broken · Feb 2, 2000 · N899US · Fokker F28MK0100 · Landing Gear Position and Warning > RIC-CLT - FLT 1093 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT AND THE AIR GROUND FAULT DISPLAYED ON THE MFDU. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR PROX SWITCH MOUNT BRACKET AND INBOARD PROX SWITCH. (M) - [SDR USAAF99001](https://openairdocs.org/sdr/USAAF99001.md): Coffee Maker · leaking · Jan 5, 1999 · N899US · Fokker F28MK0100 · Buffet/Galleys > CLT - FLT 575 - AFTER DEPARTING CLT EN ROUTE TO TRI, THE FLIGHT ATTENDANT REPORTED A LARGE WATER LEAK IN THE FORWARD GALLEY AREA. THE FLIGHT ATTENDANT SHUT OFF THE WATER SUPPLY AND THE LEAK STOPPED. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. - [SDR USAA980676](https://openairdocs.org/sdr/USAA980676.md): Fitting · corroded · Dec 24, 1998 · N899US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND 2 INCHES BY 2 INCHES CORROSION AT PAX DOOR STATION 3820-4610 FITTING. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR 1156519. (M) - [SDR USAA980675](https://openairdocs.org/sdr/USAA980675.md): Fitting · corroded · Dec 24, 1998 · N899US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND 2 INCH BY 2 INCH CORROSION AT FORWARD PAX DOOR GIRT BAR MOUNT FITTING. REPLACED BRACKET PER SRM 53-12-10, 51-22-01, 51-40-02. (M) - [SDR USAA980674](https://openairdocs.org/sdr/USAA980674.md): Beam · corroded · Dec 24, 1998 · N899US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND 1,000 MM BY 2 INCH CORROSION ON BEAM AT BL 600R STATION 5305, 6305. BLENDED OUT CORROSION PER EA 51234. (M) - [SDR USAA980673](https://openairdocs.org/sdr/USAA980673.md): Beam · corroded · Dec 24, 1998 · N899US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND CORROSION 2 INCHES BY 7 INCHES BL 0 T-CAP STATION 5305 BEAM. REPLACED T-CAP SECTION 1710037 2024T3 STOCK PER SRM 53-12-10, 51-40-02, 51-22-01, 51-30-02. (M) - [SDR USAA980672](https://openairdocs.org/sdr/USAA980672.md): T-Cap · corroded · Dec 24, 1998 · N899US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND 2 INCH SECTION OF UNDERSIDE OF T-CAP CORROSION AT FS NR 3845 ( 2 INCHES FORWARD) AT BL NR 0 T-CAP. REPLACED T-CAP STRIP SECTION WITH 1710037 2024T3 STOCK PER SRM 53-12-10, 51-22-01, 51-40-02, 51-30-02. (M) - [SDR USAA980671](https://openairdocs.org/sdr/USAA980671.md): Beam · corroded · Dec 24, 1998 · N899US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND CORROSION 6 INCHES LONG 100 PERCENT CORRODED THROUGH AT FS 3845 AT BL NR 0 BEAM TOP SURFACE. REPLACED T-CAP SECTION USING 1710037 2024T3 STOCK PER SRM 53-12-10, 51-22-01, 51-40-02, 51-30-02. (M) - [SDR USAA980670](https://openairdocs.org/sdr/USAA980670.md): Beam · corroded · Dec 24, 1998 · N899US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND 28 INCH APPROX SURFACE CORROSION ON BEAM BL 0 FS 5305-5805 T-CAP. REPLACED T-CAP SECTION USING 1710038 2024T3 STOCK PER SRM 53-12-10, 51-22-01, 51-40-02, 51-30-02. (M) - [SDR USAA980669](https://openairdocs.org/sdr/USAA980669.md): Beam · corroded · Dec 24, 1998 · N899US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND 2 INCH AREA TOP SURFACE CORRODED FS NR 3845 AT BL 914R BEAM. REPAIRED PER EA 51235. (M) - [SDR USAA980668](https://openairdocs.org/sdr/USAA980668.md): T-Cap · corroded · Dec 24, 1998 · N899US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND CORROSION TOP SURFACE ENTIRE LENGTH 10 INCH T-CAP FS 3845-4850 AT BL 600R. REPLACED TOP CAP STRIP WITH LOCALLY FABRICATED PART OF 2024T3 PER SRM 53-12-10, 51-22-01, 51-40-02. (M) - [SDR USAA980667](https://openairdocs.org/sdr/USAA980667.md): T-Cap · corroded · Dec 24, 1998 · N899US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND CORROSION TOP SURFACE 100MM LONGERON FS 3845-4850 T-CAP ENTIRE LENGTH BL NR 1127R. REPLACED TOP CAP STRIP WITH PART OF LOCAL FABRICATION 2024T3 PER SRM 52-12-10, 51-22-01, 51-40-02. (M) - [SDR USAA980666](https://openairdocs.org/sdr/USAA980666.md): Beam · corroded · Dec 24, 1998 · N899US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND 28 INCH APPROXIMATELY BY 2 INCH CORROSION ON BEAM AT BL 1127L STATION 3845-4850. TOP CAP STRIP REPLACED (LOCALLY FABRICATED) 2024-T3 PER SRM 53-12-10, 51-22-01, 51-40-02. (M) - [SDR USAA980665](https://openairdocs.org/sdr/USAA980665.md): Beam · corroded · Dec 24, 1998 · N899US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND 20 INCH APPROXIMATELY BY 2 INCH CORROSION ON BEAM AT BL 221R STATION 5805-6305. REPAIRED WITH MODIFIED 1155009 BEAM PER SRM 51-70-06, 53-12-10, 51-22-01, 51-40-01. (M) - [SDR USAA980664](https://openairdocs.org/sdr/USAA980664.md): T-Cap · corroded · Dec 24, 1998 · N899US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND CORROSION AT SCREW HOLES TOP SURFACE FS NR 3845 AT 1127R T-CAP. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR 115-4834 PER SRM 53-12-10, 51-22-01, 51-40-02. (M) - [SDR USAA980663](https://openairdocs.org/sdr/USAA980663.md): Fitting · corroded · Dec 24, 1998 · N899US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND SURFACE CORROSION ENTIRE AREA FORWARD S/E DOOR GIRT BAR MOUNT FITTING 3845 OUTBOARD 1127R. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR 115-3459 PER SRM 53-12-10, 51-22-01, 51-40-02. (M) - [SDR USAA980662](https://openairdocs.org/sdr/USAA980662.md): Fitting · corroded · Dec 24, 1998 · N899US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND CORROSION AT S/E DOOR SILL PLATE MOUNT FITTINGS 3845-4850 BL NR 1127R. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR 1154982 PER SRM 53-12-10, 51-22-01, 51-40-02. (M) - [SDR USAAF98028](https://openairdocs.org/sdr/USAAF98028.md): Selector Valve · failed · Mar 12, 1998 · N899US · Fokker F28MK0100 · Landing Gear Selector > FLT 743 - PWM - ON APPROACH TO PWM THE LANDING GEAR SELECTOR HANDLE WOULD NOT MOVE FROM THE 'UP' POSITION. CREW PERFORMED A GO AROUND AND LOWERED THE LANDING GEAR WITH THE ALTERNATE PROCEDURE. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND WAS TOWED TO THE GATE. - [SDR USAAF97103](https://openairdocs.org/sdr/USAAF97103.md): Flow Regulator · failed · Dec 23, 1997 · N899US · Fokker F28MK0100 · Fuel Controlling System > CLT - FLT 668 - ON APPROACH TO CLT, AT 1000 FT AGL, CAPTAIN TRIED TO IDLE BACK ON THROTTLE FROM 80 PERCENT. NR 2 ENGINE WOULD NOT SET BACK AND HUNG AT 80 PERCENT. THERE WAS NO RESPONSE CUTTING BACK THE POWER. AFTER GO AROUND AND HAVING CONTINUED POWER PROBL - [SDR USAAF97091](https://openairdocs.org/sdr/USAAF97091.md): Battery Pack · discharged · Nov 6, 1997 · N899US · Fokker F28MK0100 · Emergency Lighting > IND - MAINTENANCE FOUND THE FORWARD ENTRY DOOR OVERHEAD EMERGENCY LIGHTS DIM. REPLACED THE BATTERY PACK. (M) - [SDR USAAF97030](https://openairdocs.org/sdr/USAAF97030.md): Relay · failed · Mar 15, 1997 · N899US · Fokker F28MK0100 · Emergency Lighting > PHL - FL 723 - CABIN EMERGENCY LIGHTS DID NOT ILLUMINATED WHEN TESTED. MAINTENANCE REPLACED THE D-3982A RELAY. (M) - [SDR USAAF96042](https://openairdocs.org/sdr/USAAF96042.md): Dnlock Sensor · failed · May 13, 1996 · N899US · Fokker F28MK0100 · Landing Gear Position and Warning > PIT - FL 8076 - ON DESCENT INTO PIT, CREW LOWERED GEAR AND RECEIVED THREE GREEN LIGHTS WHILE BLUE LIGHTS IN GEAR HANDLE REMAINED ON AND A MFDU MESSAGE THAT READ 'LEFT LG DOWNLOCK SWITCH'. AT 400 FEET THE THE AURAL WARNING FOR THE GEAR CAME ON. CREW RECYCLED - [SDR USAAF96041](https://openairdocs.org/sdr/USAAF96041.md): Door Sensor · out of adjust · May 12, 1996 · N899US · Fokker F28MK0100 · Landing Gear Position and Warning > DCA - FL 2286 - ON DESCENT INTO DCA, LEFT LANDING GEAR DOOR SWITCH CAME ON MFDU AFTER THE GEAR WAS LOWERED. CREW HAD THREE GREEN LIGHTS FOR GEAR BUT AS THEY DESCENED BELOW 900 FEET, THE LANDING GEAR AURAL WARNING CAME ON. CREW RECYCLED GEAR AND LIGHT WENT OU - [SDR USAA950750](https://openairdocs.org/sdr/USAA950750.md): Eel Pack · failed · Jul 8, 1995 · N899US · Fokker F28MK0100 · Cabin Cooling System > CLT - FLT 166 - AT APPROX FL 301, THE LT PACK WENT OUT MAKING A LOUD NOISE. CREW DECIDED TO DIVERTED TO CLT. MAINTENANCE REPLACED THE LT PACK ASSEMBLY, OPERATIONS CHECKED GOOD. (W) ## 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 = 'N899US' AND deregistration_id = 'N899US-2003-10-16' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N899US-2003-10-16/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.