# Service difficulty reports: N217US, cancelled Jul 20, 2000 A list on [N217US, cancelled Jul 20, 2000](https://openairdocs.org/deregistered/N217US-2000-07-20.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR F3LA99109](https://openairdocs.org/sdr/F3LA99109.md): Mask · did not deploy · Aug 10, 1999 · N217US · Boeing 737201 · Passenger Oxygen System > DEN - DURING DEMONSTRATION, FLIGHT CREW REPORTED OXYGEN MASKS DID NOT DEPLOY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE PASSENGER OXYGEN SYSTEM MANUAL ACTIVATION PER MM 35-21-00A AND CHECKED OKAY. TC: 88,247. (X) - [SDR F3LA99045](https://openairdocs.org/sdr/F3LA99045.md): Valve · failed · Jun 4, 1999 · N217US · Boeing 737201 · Cabin Pressure Control System > DEN - FLT 546 - FLIGHT CREW REPORTED CABIN ALTITUDE HORN SOUNDED AT 10,000 FEET. CLOSED OUTFLOW VALVE USING MANUAL DC AT 32,500 FEET. CABIN CONTINUED TO CLIMB AT 1,000 FPM AND A RAPID DESCENT WAS MADE TO 14,000 FEET. OXYGEN MASKS WERE AUTOMATICALLY DEPLOYED - [SDR F3LA99033](https://openairdocs.org/sdr/F3LA99033.md): Bolt · cracked · Apr 23, 1999 · N217US · Boeing 737201 · Engine Mount Section > DEN - FLT 857 - DURING SERVICE CHECK, EO 71-20-737-002 WAS ACCOMPLISHED WHICH FOUND THE NR 2 ENGINE OUTBOARD LUG BEARING LOOSE AND DISPLACED. AN ULTRA SOUND INSPECTION REVEALED THE FORWARD ENGINE MOUNT BOLT CRACKED. MAINTENANCE REPLACED NR 2 ENGINE MOUNT ASS - [SDR F3LA99002](https://openairdocs.org/sdr/F3LA99002.md): Web · cracked · Jan 13, 1999 · N217US · Boeing 737201 · Fuselage Miscellaneous Structure > PHX - DURING SERVICE CEHCK, MAINTENANCE REPORTED.5 INCH CRACK ON WEB OF LEFT NLG WHEEL WELL STATION 285. ONE RIVET BORKEN AND EVIDENCE OF INTERGRANULAR CORROSION ON VERTICAL CHORD INSIDE NLG WHEEL WELL AT LEFT AFT ACCESS PANEL. MAINTENANCE REPLACED NLG WHEE - [SDR 99ZZZM189](https://openairdocs.org/sdr/99ZZZM189.md): Web · cracked · Jan 11, 1999 · N217US · Boeing 737201 · Fuselage Miscellaneous Structure > LEFT NLG W/W STATIN 285,.5 INCH CRACK ON WEB, ONE RIVET BROKEN AND EVIDENCE OF INTERGRANULAR CORROSION ON VERTICAL CHORD INSIDE NLG W/W AT LEFT AFT ACCESS PANEL. CORROSION ON VERTICAL CHORD INSIDE NLG W/W AT LEFT AFT ACCESS PANEL. - [SDR 99ZZZM187](https://openairdocs.org/sdr/99ZZZM187.md): Web · cracked · Jan 11, 1999 · N217US · Boeing 737201 · Fuselage Miscellaneous Structure > LEFT NLG W/W STATION 285 HAS.5 INCH CRACK ON WEB, ONE RIVET BROKEN AND EVIDENCE OF INTERGRANULAR CORROSION ON VERTICAL CHORD INSIDE NLG W/W AT LEFT AFT ACCESS PANEL. (M) - [SDR F3LA98197](https://openairdocs.org/sdr/F3LA98197.md): Battery · discharged · Dec 9, 1998 · N217US · Boeing 737201 · Emergency Lighting > DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FORWARD ENTRY DOOR EMERGENCY EXIT LIGHTED SIGN, PORTABLE TYPE (M186, REF WDM 33.51.01) FAILED TO ILLUMINATE BRIGHT DURING TESTING. MAINTENANCE REPLACED 2 RECHARGEABLE CD BATTERY CELLS AND CHECKED OK. (M) - [SDR F3LA98196](https://openairdocs.org/sdr/F3LA98196.md): Battery · discharged · Dec 9, 1998 · N217US · Boeing 737201 · Emergency Lighting > DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED CONTROL CABIN ENTRY DOOR EMERGENCY EXIT LIGHTED SIGN, PORTABLE TYPE (M185, REF WDM 33.51.01) FAILED TO ILLUMINATE DURING TESTING. MAINTENANCE REPLACED 2 RECHARGEABLE CD BATTERY CELLS AND CHECKED OK. (M) - [SDR F3LA98194](https://openairdocs.org/sdr/F3LA98194.md): Line · leaking · Nov 19, 1998 · N217US · Boeing 737201 · Hydraulic System, Main > DEN - UPON ARRIVAL, FLIGHT CREW REPORTED NR 2 ENGINE 'A' SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. SHUT DOWN NR 2 ENGINE HYDRAULIC PUMP AND DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC LINE AT NR 2 ENGINE PY - [SDR F3LA98193](https://openairdocs.org/sdr/F3LA98193.md): Fan · malfunctioned · Nov 13, 1998 · N217US · Boeing 737201 · Air Distribution Fan > SAN - UPON DESCENT INTO SAN, FLIGHT CREW REPORTED SULFUR/ELECTRICAL ODOR FROM AIR VENTS AT ROW 5 AND 6 ON LEFT SIDE OF AIRCRAFT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PLACARDED GASPER FAN PER MEL 21-24. UPON ARRIVAL IN DEN, GASPER FAN WAS REPLACED A - [SDR F3LA98171](https://openairdocs.org/sdr/F3LA98171.md): Solenoid · failed · Oct 13, 1998 · N217US · Boeing 737201 · Engine Start Valves/Controls > FLT 658 - DEN - AIR TURN BACK, UPON CLIMB-OUT FROM DEN, FLIGHT CREW REPORTED NR 1 ENGINE START VALVE 'OPEN' LIGHT ILLUMINATED. NR 1 ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO DEN WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE START VALVE SOLENOID AND - [SDR F3LA98075](https://openairdocs.org/sdr/F3LA98075.md): Skin · corroded · May 27, 1998 · N217US · Boeing 737201 · Fuselage Main, Plate/Skin > PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON SKIN AND DOUBLER AT BS 980-1012, STRINGER 27R. MAINTENANCE REMOVED CORROSION, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND ER 98-0478. (M) - [SDR F3LA98074](https://openairdocs.org/sdr/F3LA98074.md): Stringer · corroded · May 27, 1998 · N217US · Boeing 737201 · Fuselage Main, Longeron/Stringer > PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO BAY STRINGER 27R, RBL 5, BS 912-947. MAINTENANCE REMOVED CORROSION, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, 51-30-5, 53-10-1 AND 53-10-3. (M) - [SDR F3LA98073](https://openairdocs.org/sdr/F3LA98073.md): Frame · cracked · May 27, 1998 · N217US · Boeing 737201 · Fuselage Miscellaneous Structure > PAE - DURING C-CHECK, INSPECTION REPORTED A 1.25 INCH CRACK IN FORWARD GALLEY DOOR AFT FRAME, 4 INCHES DOWN FROM TOP CORNER OUTBOARD RADIUS. MAINTENANCE REMOVED DAMAGED AREA AND REPAIRED PER DRAWING 69-69887-3-4-5 AND SB 737-52-1070. (M) - [SDR F3LA98072](https://openairdocs.org/sdr/F3LA98072.md): Skin · cracked · May 27, 1998 · N217US · Boeing 737201 · Fuselage Main, Plate/Skin > PAE - DURING C-CHECK, INSPECTION REPORTED CRACKS ON UPPER SKIN SURFACE AT RIGHT WING, BL 103.5, TWO INCHES FORWARD OF AFT SPAR. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SB 737-57-1144. (M) - [SDR F3LA98071](https://openairdocs.org/sdr/F3LA98071.md): Doubler · cracked · May 27, 1998 · N217US · Boeing 737201 · Wing Miscellaneous Structure > PAE - DURING C-CHECK, INSPECTION REPORTED LEFT WING FIXED LEADING EDGE SKIN DOUBLER CRACKED AT NR 3 SLAT OUTBOARD AUXILLIARY TRACK CUTOUT. MAINTENANCE REMOVED DAMAGED DOUBLER AND REPAIRED PER ER 98-0483 AND SRM 51-30-2. (M) - [SDR F3LA98069](https://openairdocs.org/sdr/F3LA98069.md): Stringer · corroded · May 27, 1998 · N217US · Boeing 737201 · Fuselage Main, Longeron/Stringer > PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 26R, BS 907 PLUS 15, RBL 13, WL 169. MAINTENANCE REMOVED DAMAGED AREA (1.5 INCH BY 1 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2, 51-30-2, 53-10-1 AND 53-10-3. (M) - [SDR F3LA98068](https://openairdocs.org/sdr/F3LA98068.md): Bulkhead · cracked · May 27, 1998 · N217US · Boeing 737201 · Fuselage Main, Bulkhead > PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD, LBL 4.7, WL 192.5 TO 193.5. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-10-11. (M) - [SDR F3LA98067](https://openairdocs.org/sdr/F3LA98067.md): Bulkhead · cracked · May 27, 1998 · N217US · Boeing 737201 · Fuselage Main, Bulkhead > PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD INTERCOSTAL RIGHT CHORD, WL 196. MAINTENANCE REMOVED DAMAGED AREA 12 INCHES. FABRICATED REPLACEMENT PARTS AND REPAIRED PER ER 98-0426 AND SRM 51-30-2. (M) - [SDR F3LA98066](https://openairdocs.org/sdr/F3LA98066.md): Bulkhead · cracked · May 27, 1998 · N217US · Boeing 737201 · Fuselage Main, Bulkhead > PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD INTERCOSTAL LEFT CHORD, WL 196. MAINTENANCE REMOVED DAMAGED AREA, 12 INCHES. FABRICATED REPLACEMENT PARTS AND REPAIRED PER ER 98-0426 AND SRM 51-30-2. (M) - [SDR F3LA98065](https://openairdocs.org/sdr/F3LA98065.md): Shear Tie · corroded · May 27, 1998 · N217US · Boeing 737201 · Fuselage Miscellaneous Structure > PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON SHEAR TIE AT BS 1006, LBL 4 THROUGH RBL 4, WL 178. MAINTENANCE REMOVED CORRODED AREA, 1.5 INCH BY 2.5 INCH. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2 AND 51-30-2. (M) - [SDR F3LA98064](https://openairdocs.org/sdr/F3LA98064.md): Intercostal · cracked · May 27, 1998 · N217US · Boeing 737201 · Fuselage Miscellaneous Structure > PAE - DURING C-CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT BS 178, LBL 25, WL 195. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER ER 98-0426 AND SRM 51-30-2. (M) - [SDR F3LA98063](https://openairdocs.org/sdr/F3LA98063.md): Intercostal · cracked · May 27, 1998 · N217US · Boeing 737201 · Fuselage Miscellaneous Structure > PAE - DURING C-CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT BS 178, RBL 25, WL 195. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER ER 98-0476 AND SRM 51-30-2. (M) - [SDR F3LA98061](https://openairdocs.org/sdr/F3LA98061.md): Bulkhead · cracked · May 27, 1998 · N217US · Boeing 737201 · Fuselage Main, Bulkhead > PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD, RBL 4.7, WL 212-213. MAINTENANCE REMOVED CRACKED AREA (2 INCH BY 3.5 INCH), FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2. (M) - [SDR F3LA98060](https://openairdocs.org/sdr/F3LA98060.md): Stringer · corroded · May 27, 1998 · N217US · Boeing 737201 · Fuselage Main, Longeron/Stringer > PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 26L, BS 888-892, LBL 13, WL 163. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2, 51-30-2 AND 53-10-3. (M) - [SDR F3LA98059](https://openairdocs.org/sdr/F3LA98059.md): Stringer · corroded · May 27, 1998 · N217US · Boeing 737201 · Fuselage Main, Longeron/Stringer > PAE - DURNIG C-CHECK, INSPECTION REPORTED CORROSION AND CRACK ON STRINGER 26R, BS 1006-1014. MAINTENANCE FABRICATED REPLACEMENT STRINGER AND REPAIR PARTS AND REPAIRED PER SRM 51-20-1, 53-10-1 AND 53-10-2. (M) - [SDR F3LA98057](https://openairdocs.org/sdr/F3LA98057.md): Bulkhead Web · cracked · May 17, 1998 · N217US · Boeing 737201 · Fuselage Main, Bulkhead > PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BULKHEAD WEB AT BS 178, LBL 6.7, WL 212-213. MAINTENANCE STOP DRILLED CRACK, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-11, PATE 2, DETAIL III AND PAGE 6, FIG 1. (M) - [SDR F3LA98056](https://openairdocs.org/sdr/F3LA98056.md): Bulkhead Web · cracked · May 17, 1998 · N217US · Boeing 737201 · Fuselage Main, Bulkhead > PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BULKHEAD WEB AT BS 178, RBL 4.7, WL 190-191.5. MAINTENANCE REMOVED DAMAGED AREA (1 INCH BY 1 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-11, FIG 1, DETAIL IV AND SRM 51-30-2. (M) - [SDR F3LA98055](https://openairdocs.org/sdr/F3LA98055.md): Stringer · corroded · May 17, 1998 · N217US · Boeing 737201 · Fuselage Main, Longeron/Stringer > PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON SHEAR TIE AT BS 440, BL0, WL 148. MAINTENANCE REMOVED DAMAGED AREA (4.6 INCH BY 1.1 INCH). FABRICATED REPAIR DOUBLER AND REPAIRED PER SRM 51-30-2 AND 53-10-4. (M) - [SDR F3LA98054](https://openairdocs.org/sdr/F3LA98054.md): Stringer · corroded · May 17, 1998 · N217US · Boeing 737201 · Fuselage Main, Longeron/Stringer > PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION AND CRACK ON SHEAR TIE AT BS 727A, WL 149, RBL 13. MAINTENANCE FABRICATED REPLACEMENT SHEARTIE AND REPAIRED PER SRM 53-10-1, 51-30-2 AND 53-10-4. (M) - [SDR F3LA98014](https://openairdocs.org/sdr/F3LA98014.md): Skin · corroded · Apr 9, 1998 · N217US · Boeing 737201 · Fuselage Main, Plate/Skin > DEN - FLT 43 - DURING CIRCUMFERENTIAL SPLICE INSPECTION, WORK CARD 7-0126 (AD92-25-09), INSPECTION REPORTED BULGING OF SKIN (CORROSION) AT STATION 901, S23R AND S24R, AND STATION 895, STRINGER 25R. MAINTENANCE REPAIRED CORRODED AREAS PER SRM 53-30-1, PAGE 3 ( - [SDR F3LA98013](https://openairdocs.org/sdr/F3LA98013.md): Skin · cracked · Apr 9, 1998 · N217US · Boeing 737201 · Fuselage Main, Plate/Skin > DEN - DURING CIRCUMFERENTIAL SPLICE INSPECTION, WORK CARD 7-0126 (AD 92-25-09, INSPECTION REPORTED.625 INCH CRACK SIX INCHES FORWARD OF L-1 DOOR IN FUSELAGE SKIN AT STRINGER 7. MAINTENANCE REPAIRED CRACK PER SRM 53-30-3, PAGES 7 AND 8. (M) - [SDR F3LA97143](https://openairdocs.org/sdr/F3LA97143.md): Gearbox · failed · Sep 1, 1997 · N217US · Boeing 737201 · Turbine Engine Accessory Drive > DEN - FLT 780 - FLIGHT CREW REPORTED NR 1 ENGINE WAS SHUT DOWN DUE TO LOW OIL QTY AND AN EMERGENCY WAS DECLARED. MAINTENANCE REPLACED O-RING ON FUEL CARBON SEAL IN STL. DURING FLT NR 217 STL TO DEN, NR 1 ENGINE OIL QTY DECREASED AND AIRCRAFT DIVERTED TO MCI - [SDR F3LA97095](https://openairdocs.org/sdr/F3LA97095.md): Rib · cracked · Feb 18, 1997 · N217US · Boeing 737201 · Fuselage Main, Frame > CLT - ONE INCH CRACK IN RIB AROUND RIVET HOLES BS 800, S19R TO S27R. INSTALLED NEW FRAME AND WEBS PER BOEING DRAWINGS 65-C35243 AND 69-42945, AND EA 59494. (M) - [SDR F3LA97094](https://openairdocs.org/sdr/F3LA97094.md): Skin · cracked · Feb 3, 1997 · N217US · Boeing 737201 · Nacelle/Pylon, Plate/Skin > CLT - FOUND CRACK IN THE NR 2 ENGINE PYLON SCREW HOLE. INSTALLED NEW ANGLE, DOUBLERS AND FILLERS PER EA 57446, EA 57462, SRM 51-40-01 AND SRM 54-10-3. (M) - [SDR F3LA97045](https://openairdocs.org/sdr/F3LA97045.md): Seat Track · corroded · Jan 27, 1997 · N217US · Boeing 737201 · Fuselage, Seat/Cargo Attach Fittings > CLT - FOUND SURFACE CORROSION AT SEAT TRACK MOUNT AT STATION 294, RBL 45.5. REMOVED SURFACE CORROSION ALODINED AND PRIMED. (M) - [SDR F3LA97044](https://openairdocs.org/sdr/F3LA97044.md): Floor Beam · corroded · Jan 23, 1997 · N217US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - FOUND CORROSION AROUND SCREW HOLE BS 947, RBL 40. REMOVED SURFACE CORROSION ON FLOOR BEAM PER SRM 51-10-06. (M) - [SDR F3LA97043](https://openairdocs.org/sdr/F3LA97043.md): Floor Beam · corroded · Jan 23, 1997 · N217US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - FOUND CORROSION AROUND SCREW HOLES AND ADJACENT AREAS, BS 947, RBL 3 THROUGH RBL 22 ON FLOOR BEAM. REMOVED SURFACE CORROSION BY BURNISHING THE TOP SURFACE. (M) - [SDR F3LA97042](https://openairdocs.org/sdr/F3LA97042.md): Floor Beam · corroded · Jan 23, 1997 · N217US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - FOUND CORROSION (C53-107-02) ON FLOOR BEAM AT STATION 987, LBL 5. REMOVED SURFACE CORROSION AND ALODINED AND PRIMED THE AREA PER SRM 51-10-0. (M) - [SDR F3LA97041](https://openairdocs.org/sdr/F3LA97041.md): Floor Beam · corroded · Jan 23, 1997 · N217US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - FOUND CORROSION (C53-107-02) ON FLOOR BEAM AT STATION 967, RBL 42. REMOVED SURFACE CORROSION AND ALODINED AND PRIMED THE AREA PER SRM 51-10-6. (M) - [SDR F3LA97040](https://openairdocs.org/sdr/F3LA97040.md): Seat Track · corroded · Jan 23, 1997 · N217US · Boeing 737201 · Fuselage, Seat/Cargo Attach Fittings > CLT - FOUND CORROSION (C53-107-02) ON AFT GALLEY SEAT TRACK AT STATION 986-1016, RBL 20. REMOVED CORROSION PER SRM 51-10-6 AND ALODINED AND PRIMED THE AREA. (M) - [SDR F3LA97039](https://openairdocs.org/sdr/F3LA97039.md): Support · corroded · Jan 23, 1997 · N217US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND CORROSION (C53-107-02) ON AFT LAV FLOOR SUPPORT, STATION 1006-966, LBL 10-10. REMOVED NUT PLATES ON THE FLOOR BEAM SUPPORT, REMOVED LIGHT CORROSION BY BURNISHING PER SRM 51-10-6. (M) - [SDR F3LA97038](https://openairdocs.org/sdr/F3LA97038.md): Floor Beam · corroded · Jan 23, 1997 · N217US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - FOUND CORROSION (C53-107-02) ON FLOOR BEAM AT STATION 986, RBL 50 THROUGH LBL 21. REMOVED SURFACE CORROSION PER SRM 51-10-6. ALODINED AND PRIMED THE AREA. (M) - [SDR 97ZZZX313](https://openairdocs.org/sdr/97ZZZX313.md): Wire · failed · Jan 3, 1997 · N217US · Boeing 737201 · Light System Wiring > ELP - DURING SERVICE CHECK, MAINTENANCE REPORTED EMERGENCY AISLE PATH LIGHTING AT ROW 9 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OKAY. - [SDR F3LA96008](https://openairdocs.org/sdr/F3LA96008.md): Warning Horn · sounded · Feb 14, 1996 · N217US · Boeing 737201 · Landing Gear Position and Warning > FLT NR 546 - DEN - UPON ARRIVAL, FLIGHT CREW REPORTED THE LANDING GEAR WARNING HORN SOUNDED WITH THROTTLES RETARDED TO IDLE AND FLAPS UP. WARNING HORN DID NOT SOUND AT FLAP SETTINGS 1 OR 5 WITH THROTTLES RETARDED TO IDLE. LANDING GEAR WAS UP IN BOTH CASES. - [SDR F3LA95019](https://openairdocs.org/sdr/F3LA95019.md): Pcu · malfunctioned · Dec 14, 1995 · N217US · Boeing 737201 · Rudder Control System > FLT NR 465 - DEN -UPON ARRIVAL, FLIGHT CREW REPORTED RUDDER TRIM REQUIRED ONE FULL UNIT OF RIGHT RUDDER ADJUSTMENT TO ESTABLISH ZERO DEGREE DRIFT. MAINTENANCE REPLACED THE RUDDER POWER CONTROL UNIT AND SYSTEM CHECKED OK. (M) - [SDR F3LA95015](https://openairdocs.org/sdr/F3LA95015.md): Anti-Skid Contl · failed · Jul 31, 1995 · N217US · Boeing 737201 · Brake Anti-Skid Section > BZN - UPON LANDING, FLIGHT CREW REPORTED LOSS OF LEFT MAIN LANDING GEAR BRAKES. MAINTENANCE INSPECTED AND BLED THE BRAKE SYSTEM AND PERFORMED AN OPERATIONAL CHECK. SYSTEM CHECKED OK. A FAULT WAS FOUND ON THE ANTI-SKID MODULE TEST AND THE LEFT OUTBOARD ANTI- - [SDR F3LA95003](https://openairdocs.org/sdr/F3LA95003.md): Eel Connector · broken · Jan 30, 1995 · N217US · Boeing 737201 · Emergency Lighting > FAR - PRIOR TO DEPARTURE, MAINTENANCE REPORTED THE RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. PLACARDED PER MEL 33-14. UPON ARRIVAL IN DEN, MAINTENANCE REPAIRED CANNON PLUG AND CHECKED OKAY. (X) - [SDR F3LA95002](https://openairdocs.org/sdr/F3LA95002.md): Eel Battery Pack · inoperative · Jan 25, 1995 · N217US · Boeing 737201 · Emergency Lighting > OMA - DURING AN FAA RAMP AUDIT, FAA REPORTED RT WING INTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BOTH LAMPS, BATTERY PACK AND BATTERY CHARGER AND CHECKED OKAY. REFERENCE CONTROL NR 95ZZZX785. (X) - [SDR 95ZZZX785](https://openairdocs.org/sdr/95ZZZX785.md): Eel Batt Charger · inoperative · Jan 25, 1995 · N217US · Boeing 737201 · Emergency Lighting > OMA - DURING AN FAA RAMP AUDIT, FAA REPORTED RT WING INTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BOTH LAMPS, BATTERY PACK AND BATTERY CHARGER AND CHECKED OKAY. REFERENCE CONTROL NR F3LA95002. ## 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 = 'N217US' AND deregistration_id = 'N217US-2000-07-20' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N217US-2000-07-20/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.