# Service difficulty reports: N294AS, cancelled May 19, 2015 A list on [N294AS, cancelled May 19, 2015](https://openairdocs.org/deregistered/N294AS-2015-05-19.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 2 · 99 reports - [SDR C1HA200694002](https://openairdocs.org/sdr/C1HA200694002.md): Hydraulic Line · blown · Dec 24, 2006 · N294AS · Boeing 727290 · Hydraulic System, Main > ON GEAR RETRACTION LOST ALL SYSTEM QUANTITY AND PRESSURE. FOLLOWED COM RED BORDER AND AMPLIFIED 2.29.2 HYDRAULIC SYSTEM LOSS AND 2.28.4 FUEL DUMPING CHECKLIST RETURNED FOR LANDING IN ISO AT 155,000 LBS. T/S FOUND MLG ACT RETURN LINE BLOWN REMOVED AND INSTALLE - [SDR C1HA200694001](https://openairdocs.org/sdr/C1HA200694001.md): Display · defective · Mar 19, 2006 · N294AS · Boeing 727290 · Weather Radar System > RADAR DISPLAYS MAGENTA AND PURPLE COLORS ONLY, AND INTERMITTENTLY INOP. T/S IAW TIB-018 FOUND INDICATOR PAINTS RED/MAGENTA. REMOVED AND REPLACED INDICATOR IAW M/M 34-41-34. OPERATIONAL CHECK NORMAL IAW M/M 34-41-34. - [SDR C1HA200594012](https://openairdocs.org/sdr/C1HA200594012.md): Actuator · malfunctioned · Dec 23, 2005 · N294AS · Boeing 727290 · Landing Gear Actuator > LEFT MAIN GEAR DID NOT RETRACT ON TAKEOFF, BOTH GREEN LIGHT DOWN AND LOCK LIGHTS AND RED DOOR LIGHTS REMAIN ILLUMINATED, RED DISAGREE LIGHT WAS ALSO ILLUMINATED. REMOVED AND REPLACED LT MLG LOCK MECHANISM PER JOB STATUS MM REF 32-32-51, ALL OPS CHECKS NORMAL - [SDR C1HA200594011](https://openairdocs.org/sdr/C1HA200594011.md): Cap · loose · Nov 25, 2005 · N294AS · Boeing 727290 · Turbine Engine Oil System > DURING CLIMB-OUT DFW, NR 1 ENGINE OIL QUANTITY INDICATED CONSTANT DECREASE OIL. LANDED WITH 1.0 GALLONS OIL RETURNED DIRECT, UPON LANDING WITNESSED OIL LEAKING FROM COWLING. FOUND OIL CAP NOT ENGAGED. SERVICED ENGINE INSTALLED NEW OIL CAP REF 12-13-01. - [SDR C1HA200594010](https://openairdocs.org/sdr/C1HA200594010.md): Support · broken · Oct 17, 2005 · N294AS · Boeing 727290 · Wing, Attach Fittings > NR 12 SPOILER ACTUATOR OUTBOARD SUPPORT IS BROKEN WS 510. REMOVED AND REPLACED NR 12 SPOILER ACTUATOR O/B SUPPORT IAW B727 MM 27-61-0 AND SRM 51-30-2 NR 12 SPOILER ACTUATOR, OP CHECK GOOD IAW B727 MM 27-61-0. - [SDR C1HA200594009](https://openairdocs.org/sdr/C1HA200594009.md): Stiffener · cracked · Oct 17, 2005 · N294AS · Boeing 727290 · Fuselage Miscellaneous Structure > RIGHT MLG WHEEL WELL 870 BULKHEAD VERTICAL STIFFENER CRACKED AT KEELBEAM APU CUTOUT. REMOVED AND REPLACED VERTICAL STIFFENER BS 870 RIGHT WHEEL WELL P/N 65-18636-378 IAW 727 SRM 51-30-2. PERFORMED AT KEELBEAM AREA PNEUMATIC LEAK CHECK, NO LEAKS NOTED IAW B72 - [SDR C1HA200594008](https://openairdocs.org/sdr/C1HA200594008.md): Shear Tie · cracked · Oct 17, 2005 · N294AS · Boeing 727290 · Fuselage Internal Mounting Structure > RT SIDE OF THE NOSE WHEEL WELL DOGHOUSE FRAME AT STA 312 IS CRACKED. CUT OUT DAMAGED FRAME TO SKIN ATTACHMENT ANGLE FABBED & INSTALLED REPAIR SHEAR TIE IAW 727 SRM 53-10-4 FIG 15. - [SDR C1HA200594007](https://openairdocs.org/sdr/C1HA200594007.md): Frame · dented · Oct 17, 2005 · N294AS · Boeing 727290 · Fuselage Main, Frame > AFT CARGO COMPT FRAME AT STA 950F IS DENTED BETWEEN STR 25L - 026L. FOUND DENT OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. CUT OUT DAMAGE AREA IAW B727 SRM 51-10-1. FABRICATED ANGLE REPAIR IAW B727 SRM 53-10-2 FIG 3 AND 51-20-1. TREATED AND PRIMED PORT AND A - [SDR C1HA200594006](https://openairdocs.org/sdr/C1HA200594006.md): Skin · bulged · Oct 17, 2005 · N294AS · Boeing 727290 · Fuselage Main, Plate/Skin > RT FUSE SKIN BULGED AT NOSE WHEEL WELL LWR CHORD BS 350. REMOVED AND REPLACED DAMAGED NOSE WHEEL WELL RT LWR CHORD P/N 65-19861-8, IAW 727 SRM 51-30-2. - [SDR C1HA200594004](https://openairdocs.org/sdr/C1HA200594004.md): Skin · punctured · Oct 17, 2005 · N294AS · Boeing 727290 · Electrical/Electronic Compartment Doors > E&E BAY COMPARTMENT HATCH INTERIOR SKIN HAS SEVERAL GOUGES & A LARGE PUNCTURE HOLE. CUT OUT DAMAGED AREA, FABBED AND INSTALLED REPAIR FILLER & DOUBLER (7075 T6.050 PO 9002126, DIM 5.375 X 5.125 INCHES IAW SRM 51-40-2 FIG 1. - [SDR C1HA200594005](https://openairdocs.org/sdr/C1HA200594005.md): Channel · cracked · Oct 17, 2005 · N294AS · Boeing 727290 · Fuselage Main, Attach Fittings > NLG LOCK ACTUATOR SUPPORT CHANNEL HAS CRACK INDICATION AT UPPER OUTBOARD HOLE. REMOVED & REPLACED NLG LOCK ACTUATOR SUPPORT CHANNEL IAW B727 SRM 51-30-2, P/N 69-19122-2. - [SDR C1HA200594003](https://openairdocs.org/sdr/C1HA200594003.md): Skin · cracked · Oct 14, 2005 · N294AS · Boeing 727290 · Fuselage Main, Plate/Skin > L1 DOOR LOWER HINGE CUTOUT ON FUSE SKIN IS CRACKED. CUT OUT DAMAGED AREA, FABBED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SB 727-53A0198 REV 2 FIG 3 & 5. - [SDR C1HA200594002](https://openairdocs.org/sdr/C1HA200594002.md): Carriage · vibration · Jun 1, 2005 · N294AS · Boeing 727290 · Trailing Edge Flaps > DURING CLIMB-OUT AT APPROX FL 190, VIBRATION FELT THROUGHOUT A/C. VISUAL INSP FOUND LT TE FLAP VIBRATING AS BEFORE (LOG PAGE 3059). VIBRATION PERSISTED FROM 310 KIAS TO 250 KIAS. FUEL DUMPED (APPROX 4000 LBS) AND AIR RETURN TO MMUN. REF LP C03060 ITEM 3. - [SDR C1HA200594001](https://openairdocs.org/sdr/C1HA200594001.md): Roller · out of adjust · Jun 1, 2005 · N294AS · Boeing 727290 · Trailing Edge Flaps > ON CLIMBOUT APPROX 200, CREW BEGAN TO FEEL VIBRATION. ALL ENGINE INDICATIONS NORMAL. BEGAN TROUBLESHOOTING AND UPON VISUAL INSP FOUND LT INBOARD T/E FLAPS FLUTTERING APPROX 4 TO 5 INCHES AT SPEEDS ABOVE APPROX 290 KIAS. DECISION MADE TO AIR RETURN TO MMUN M - [SDR C1HA200494003](https://openairdocs.org/sdr/C1HA200494003.md): Accessory Unit · malfunctioned · May 13, 2004 · N294AS · Boeing 727290 · Landing Gear Retraction/Extension System > ON TAKEOFF FROM STL AFTER GEAR RETRACTION, THE RED NOSE GEAR LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED LDG ACC UNIT IAW 32-04-121 & NLG POS SW IAW32-61-71, PERFORMED ADJ/TEST, OP'S CHECK SATISFACTORY. - [SDR C1HA200494002](https://openairdocs.org/sdr/C1HA200494002.md): Accessory Unit · damaged · May 9, 2004 · N294AS · Boeing 727290 · Landing Gear Retraction/Extension System > ON DEPARTURE MBJ, GEAR LEVER FAILED TO MOVE TO UP COM 2.32.23 FOLLOWED. CONFIRMED LEVER LATCH FAILURE. R/R LANDING GEAR ACCESSORY UNIT MM 32-09-121 OPS CHECKS OF SYSTEM OK. - [SDR C1HA200494001](https://openairdocs.org/sdr/C1HA200494001.md): Latch · failed · May 8, 2004 · N294AS · Boeing 727290 · Landing Gear Retraction/Extension System > GEAR LEVER FAILED TO MOVE UP AT DEPARTURE AT CANCUN COM 2.32.23 RUN CONFIRMED FAILURE OF MECHANIC LATCH. PERFORMED LEVER LOCK TEST MM 32-31-11 OPS CHECKS GOOD - [SDR C1HA200394046](https://openairdocs.org/sdr/C1HA200394046.md): Battery Pack · inoperative · Nov 30, 2003 · N294AS · Boeing 727290 · Emergency Lighting > OVERHEAD EMERGENCY LIGHT INOPERATIVE AT ROW 4. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-22 ALL OPS NORMAL. - [SDR C1HA200394047](https://openairdocs.org/sdr/C1HA200394047.md): Battery Pack · inoperative · Nov 28, 2003 · N294AS · Boeing 727290 · Emergency Lighting > EXTERIOR EMERGENCY LIGHT ON C2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR C2 DOOR LIGHT OPS NORMAL IAW 727 MM 33-50-22. - [SDR C1HA200394044](https://openairdocs.org/sdr/C1HA200394044.md): Fitting · corroded · Nov 14, 2003 · N294AS · Boeing 727290 · Fuselage Main, Attach Fittings > RIGHT AFT LAV GUITAR FITTING BS 1140 HAS CORROSION. - [SDR C1HA200394043](https://openairdocs.org/sdr/C1HA200394043.md): Channel · corroded · Nov 14, 2003 · N294AS · Boeing 727290 · Fuselage Miscellaneous Structure > RIGHT AFT LAV HAT CHANNEL AT BS 1140 RBL 45.5 HAS CORROSION. - [SDR C1HA200394045](https://openairdocs.org/sdr/C1HA200394045.md): Seat Track · corroded · Nov 14, 2003 · N294AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK BS 959 - 1140 RBL 24 HAS BARE METAL AND CORROSION. - [SDR C1HA200394040](https://openairdocs.org/sdr/C1HA200394040.md): Seat Track · corroded · Nov 8, 2003 · N294AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK BS 1010 - 1148 LBL 45.5 HAS HEAVY CORROSION. - [SDR C1HA200394039](https://openairdocs.org/sdr/C1HA200394039.md): Seat Track · corroded · Nov 8, 2003 · N294AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK BS 344 - 480 LBL 45.5 HAS LIGHT CORROSION AND WORN AREAS. - [SDR C1HA200394038](https://openairdocs.org/sdr/C1HA200394038.md): Seat Track · corroded · Nov 8, 2003 · N294AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK BS 868 - 950+9 LBL 24.75 HAS LIGHT CORROSION AND WORN AREAS. - [SDR C1HA200394037](https://openairdocs.org/sdr/C1HA200394037.md): Seat Track · corroded · Nov 8, 2003 · N294AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK BS 344 - 480 LBL 24.75 HAS CORROSION AND WORN AREAS. - [SDR C1HA200394036](https://openairdocs.org/sdr/C1HA200394036.md): Seat Track · corroded · Nov 8, 2003 · N294AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK BS 480 - 689.45 LBL 45.5 HAS CORROSION AND WORN AREAS. - [SDR C1HA200394035](https://openairdocs.org/sdr/C1HA200394035.md): Seat Track · corroded · Nov 8, 2003 · N294AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK BS 480 - 689.45 LBL 24.75 HAS CORROSION AND WORN AREAS. - [SDR C1HA200394029](https://openairdocs.org/sdr/C1HA200394029.md): Intercostal · broken · Nov 7, 2003 · N294AS · Boeing 727290 · Fuselage Miscellaneous Structure > INTERCOSTAL BETWEEN BS 970 - 990, BL-0 ATTACH ANGLE BROKEN IN SEVERAL PLACES. - [SDR C1HA200394028](https://openairdocs.org/sdr/C1HA200394028.md): Seat Track · corroded · Nov 7, 2003 · N294AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK BS 689 - 741, LBL 24.75 HAS AREAS OF CORROSION AND WORN AREAS. - [SDR C1HA200394027](https://openairdocs.org/sdr/C1HA200394027.md): Floorbeam · corroded · Nov 7, 2003 · N294AS · Boeing 727290 · Fuselage Main, Floor Beam > FLOORBEAM CORRODED BS 1110 RBL 12. - [SDR C1HA200394025](https://openairdocs.org/sdr/C1HA200394025.md): Seat Track · corroded · Nov 7, 2003 · N294AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK BS 480-690, RBL 24 HAS BARE METAL & CORROSION AS MARKED. - [SDR C1HA200394024](https://openairdocs.org/sdr/C1HA200394024.md): Seat Track · corroded · Nov 7, 2003 · N294AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK BS 852 - 868, LBL-45.5 HAS LIGHT CORROSION AS MARKED. - [SDR C1HA200394034](https://openairdocs.org/sdr/C1HA200394034.md): Seat Track · corroded · Nov 7, 2003 · N294AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK AT BS 689.5 - 741 LBL 24.75 HAS CORROSION AND WORN AREAS. - [SDR C1HA200394033](https://openairdocs.org/sdr/C1HA200394033.md): Seat Track · corroded · Nov 7, 2003 · N294AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK BS 741 - 757 LBL 45.5 HAS BARE METAL, CORROSION AND WORN AREAS. - [SDR C1HA200394032](https://openairdocs.org/sdr/C1HA200394032.md): Seat Track · corroded · Nov 7, 2003 · N294AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK AT BS 344 - 380 RBL 56 HAS BARE METAL AND CORROSION. - [SDR C1HA200394031](https://openairdocs.org/sdr/C1HA200394031.md): Seat Track · corroded · Nov 7, 2003 · N294AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK AT BS 344 - 480 RBL 45 HAS BARE METAL AND CORROSION. - [SDR C1HA200394030](https://openairdocs.org/sdr/C1HA200394030.md): Seat Track · corroded · Nov 7, 2003 · N294AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK AT BS 480 - 580 RBL 45 HAS BARE METAL AND CORROSION. - [SDR C1HA200394023](https://openairdocs.org/sdr/C1HA200394023.md): Battery Pack · inoperative · Oct 13, 2003 · N294AS · Boeing 727290 · Emergency Lighting > LEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ASSY IAW 727 MM 33-50-22, ALL OPS NORMAL. - [SDR C1HA200394022](https://openairdocs.org/sdr/C1HA200394022.md): Battery · inoperative · Oct 13, 2003 · N294AS · Boeing 727290 · Emergency Lighting > OVERHEAD EMERGENCY LIGHT IN AFT AIRSTAIRS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY AND BATTERIES IAW 727 MM 33-50-61. ALL OPS NORMAL. - [SDR C1HA200394021](https://openairdocs.org/sdr/C1HA200394021.md): Battery Pack · discharged · Oct 9, 2003 · N294AS · Boeing 727290 · Emergency Lighting > EMERGENCY LIGHT EXIT OVER LEFT OVERWING EXITS INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-00, OPS CHECK GOOD. - [SDR C1HA200394020](https://openairdocs.org/sdr/C1HA200394020.md): Power Supply · inoperative · Oct 9, 2003 · N294AS · Boeing 727290 · Emergency Lighting > OVERWING EMERGENCY EXIT LIGHT (UPPER) INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW CHAMPION AMM 33-51-00; OPS CHECK GOOD. - [SDR C1HA200394018](https://openairdocs.org/sdr/C1HA200394018.md): Switch · malfunctioned · Sep 26, 2003 · N294AS · Boeing 727290 · Landing Gear Selector > ON DEPARTURE RETRACTED THE GEAR AND HAD THREE RED GEAR LIGHTS ILLUMINATED AT REMAINED ILLUMINATED. CLEANED GEAR HANDLE POSITION POSITION SWITCH S92 IAW B727MM32-60-0 OPS CK GOOD IAW B727MM32-60-0. - [SDR C1HA200394015](https://openairdocs.org/sdr/C1HA200394015.md): Light · inoperative · Jul 17, 2003 · N294AS · Boeing 727290 · Emergency Lighting > RIGHT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. - [SDR C1HA200394016](https://openairdocs.org/sdr/C1HA200394016.md): Warning Light · illuminated · Jul 17, 2003 · N294AS · Boeing 727290 · Landing Gear Position and Warning > ON GEAR EXTENSION ALL DOOR LIGHTS ILLUMINATED ALONG WITH TAIL SKID LIGHT. GO AROUND INITAITED. ON SECOND GEAR EXTENSION ALL LIGHTS AND INDICATIONS NORMAL - COULD NOT DUPLICATE. - [SDR C1HA200394017](https://openairdocs.org/sdr/C1HA200394017.md): Warning Horn · false activation · Jul 17, 2003 · N294AS · Boeing 727290 · Central Warning > DURING TAKE-OFF, WHEN POWER ADVANCED PAST 1.4 EPR THE T/O WARNING SOUNDED - ALL SETTINGS NORMAL TRIM IN GREEN FLAPS 15 DEG SPEED BRAKE FORWARD - ACCOMPLISHED SYSTEM TEST NO TROUBLE FOUND. - [SDR C1HA200394014](https://openairdocs.org/sdr/C1HA200394014.md): Wire · damaged · Jul 11, 2003 · N294AS · Boeing 727290 · Fire Protection System Wiring > LOWER AFTER BODY OVERHEAT LIGHT CAME ON DURING TAXI BACK TO GATE. REPAIRED DAMAGED WIRE ABOVE ROW 3DEF W298-122-16+ W298-012-16 IAW WIRING PRACTICES CH 20. REMOVED AND REPLACED FIRE AND OVERHEAT ACCY UNIT, OPS CHECK NORMAL IAW MM 26-14-11. - [SDR C1HA200394011](https://openairdocs.org/sdr/C1HA200394011.md): Slide · dislodged · Jun 29, 2003 · N294AS · Boeing 727290 · Escape Slide > SLIDE FELL OUT OF R-1 DOOR. - [SDR C1HA200394012](https://openairdocs.org/sdr/C1HA200394012.md): Bleed Valve · failed · Jun 28, 2003 · N294AS · Boeing 727290 · Compressor Bleed Control > NR 2 ENGINE COMPRESSOR STALL ON FINAL AS POWER ADDED. ON GROUND COMPRESSOR STALL WHILE TAXIING. - [SDR C1HA200394010](https://openairdocs.org/sdr/C1HA200394010.md): Switch · malfunctioned · Jun 3, 2003 · N294AS · Boeing 727290 · Trailing Flap Position Indicating System > TAKEOFF ROLL GOT T/O WARNING HORN. ABORTED T/O, BEFORE RETURNING TO GATE CYCLED THE FLAPS AND RAN POWER UP, T/O WARNING HORN WENT AWAY. AFTER RETURNING TO GATE CYCLED FLAPS, NO TROUBLE FOUND. THE 5 DEG FLAP SWITCH CHANGED PRECAUTIONARY. Next page: https://openairdocs.org/deregistered/N294AS-2015-05-19/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 = 'N294AS' AND deregistration_id = 'N294AS-2015-05-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N294AS-2015-05-19/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.