# Service difficulty reports: N279US, cancelled Jan 17, 2018

A list on [N279US, cancelled Jan 17, 2018](https://openairdocs.org/deregistered/N279US-2018-01-17.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 3 · 121 reports

- [SDR GAIA07007](https://openairdocs.org/sdr/GAIA07007.md): Light · inoperative · Jul 12, 2007 · N279US · Boeing 727251 · Emergency Lighting
  > NO FLIGHT: THE COCKPIT DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED EMERGENCY COCKPIT LIGHT. OPS CHECK NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (K)
- [SDR GAIA06032OP](https://openairdocs.org/sdr/GAIA06032OP.md): Accessory Unit · intermittent · Oct 24, 2006 · N279US · Boeing 727251 · Landing Gear Retraction/Extension System
  > FLIGHT 714 - FWA-MIA - DURING APPROACH UPON GEAR EXTENSION THE FLIGHT CREW OBSERVED THREE GREEN AND THREE RED LIGHTS ON THE LANDING GEAR POSITION INDICATOR. THE GEAR WAS RECYCLED SEVERAL TIMES WITH THE SAME INDICATION ALSO THE TAIL SKID LIGHT INDICATED UNSAFE
- [SDR GAIA06031P](https://openairdocs.org/sdr/GAIA06031P.md): Indication Sys · malfunctioned · Oct 20, 2006 · N279US · Boeing 727251 · Landing Gear Position and Warning
  > FLIGHT 714 - FWA-MIA - DURING APPROACH UPON GEAR EXTENSION THE FLIGHT CREW OBSERVED THREE GREEN AND THREE RED LIGHTS ON THE LANDING GEAR POSITION INDICATOR. THE GEAR WAS RECYCLED WITH THE SAME INDICATION. THE CREW FOLLOWED KITTY HAWK AOM PROCEDURES AND WENT
- [SDR GAIA06021OP](https://openairdocs.org/sdr/GAIA06021OP.md): Indicator · fluctuates · May 23, 2006 · N279US · Boeing 727251 · Trailing Flap Position Indicating System
  > DURING APPROACH TO LANDING, THE IB FLAPS LOCKED OUT AT 2 DEGREES ASYMMETRICAL. THE FLIGHT CREW DECLARED AN EMERGENCY AND CONTINUED WITH THE LANDING APPROACH. AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED THE FLAP POSITION INDICATOR. THE FLAPS OPS C
- [SDR GAIA05038OP](https://openairdocs.org/sdr/GAIA05038OP.md): Pin · missing · Dec 14, 2005 · N279US · Boeing 727251 · Nose/Tail Landing Gear
  > EXCESSIVE NOSE WHEEL SHIMMY ON LANDING. THE AIRCRAFT WAS TOWED OFF THE RUNWAY. INSPECTION REVEALED THAT THE NOSE GEAR TORQUE LINK QUICK DISCONNECT WAS MISSING. THE AIRCRAFT WAS INSPECTED FOR DAMAGE AND THE TORQUE LINK PIN WAS REPLACED. AIRCRAFT WAS RETURNE
- [SDR GAIA05004OP](https://openairdocs.org/sdr/GAIA05004OP.md): Light · intermittent · Feb 12, 2005 · N279US · Boeing 727251 · Emergency Lighting
  > DURING MAINTENANCE, THE CREW ENTRY DOOR EMERGENCY EXIT LIGHT WAS FOUND INTERMITTENT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA04177OP](https://openairdocs.org/sdr/GAIA04177OP.md): Clamp · broken · Dec 7, 2004 · N279US · Boeing 727251 · Pneumatic Distribution System
  > DURING CLIMB, NR 2 ENGINE FIRE WARNING AFTER TAKEOFF. SHUT DOWN NR 2 ENGINE. RETURNED TO AIRPORT. DECLARED EMERGENCY. LANDING WAS MADE WITHOUT INCIDENT. FOUND BROKEN CLAMP ON 8TH STAGE SADDLE DUCT AT THE ANTI-ICE CONNECTION. REPLACED CLAMP. LEAK CHECKED
- [SDR GAIA04088OP](https://openairdocs.org/sdr/GAIA04088OP.md): Light · inoperative · Jul 17, 2004 · N279US · Boeing 727251 · Emergency Lighting
  > L1 EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT ILGHT. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR GAIA04083AOP](https://openairdocs.org/sdr/GAIA04083AOP.md): Engine · malfunctioned · Jun 23, 2004 · N279US · Boeing 727251 · Engine (Turbine/Turboprop)
  > SHUTDOWN NR 3 DUE TO HIGH OIL PRESSURE AND RISING OIL TEMP. OIL PRESSURE WAS 53 PSI, OIL TEMP WAS 130 UNTIL POWER REDUCED, THEN OIL TEMP SPIKED OFF SCALE. DUMPED 20,000 POUNDS FUEL. OIL TEMP GAUGE REMAINED OFF SCALE. (AN EMERGENCY WAS DECLARED AND THE CREW
- [SDR GAIA04083OP](https://openairdocs.org/sdr/GAIA04083OP.md): Engine · malfunctioned · Jun 19, 2004 · N279US · Boeing 727251 · Engine (Turbine/Turboprop)
  > FLT 2878 - DURING CLIMB, SFO-FWA - SHUTDOWN NR 3 DUE TO HIGH OIL PRESSURE AND RISING OIL TEMP. OIL PRESSURE WAS 53 PSI, OIL TEMP WAS 130 UNTIL POWER REDUCED, THEN OIL TEMP SPIKED OFF SCALE. DUMPED 20,000 LBS FUEL. OIL TEMP GAUGE REMAINED OFF SCALE. AN EMERG
- [SDR GAIA04081OP](https://openairdocs.org/sdr/GAIA04081OP.md): Indicator · inoperative · Jun 16, 2004 · N279US · Boeing 727251 · Trailing Flap Position Indicating System
  > ON CLIMB-OUT INBOARD FLAPS WOULD NOT RETRACT PAS 2 DEGREES. CREW RETURNED TO FWA WHERE A LANDING WAS MADE WITHOUT INCIDENT, LANDED AT 167600 LBS. REMOVED AND REPLACED INBOARD FLAP POSITION INDICATOR AND LUBED FLAP QUADRANT ASSEMBLIES. RAN FLAPS SEVERAL TIME
- [SDR GAIA04068OP](https://openairdocs.org/sdr/GAIA04068OP.md): Skin Panel · missing · Apr 1, 2004 · N279US · Boeing 727251 · Ailerons
  > ON POST FLIGHT INSPECTION FOUND RT OB AILERON DAMAGE AT IB LOWER SURFACE EDGE IB PANEL MISSING FROM AILERON. AIRCRAFT LANDED WITHOUT INCIDENT. INSTALLED MISSING PANEL AT IB HINGE LEADING EDGE. REPAIRED DAMAGED IB LOWER SURFACE EDGE IAW SRM, SHEET (5) PG 169
- [SDR GAIA04053OP](https://openairdocs.org/sdr/GAIA04053OP.md): Fire Loop · shorted · Mar 18, 2004 · N279US · Boeing 727251 · Fire Detection
  > FLT 602 - TOL-FWA - DURING CRUISE, NR 3 ENGINE FIRE PROTECTION GROUND FAULT LIGHT ILLUMINATED. FOUND SAFETY WIRE GROUNDING ON LOOP, REPOSTIIONED WIRE. NR 3 GROUND FAULT LIGHT EXTINGUISHED. AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA04035BOP](https://openairdocs.org/sdr/GAIA04035BOP.md): Fire Loop · out of adjust · Feb 25, 2004 · N279US · Boeing 727251 · Fire Detection
  > FLT 875 - FWA-LAX - DURING PREFLIGHT, ENGINE NR 3 FIRE PROTECTION GROUND FAULT LIGHT REMAINS ILLUMINATED. ADJUSTED NR 3 ENGINE FIRE LOOP. CLOSED NR 3 COWL. NR 3 GROUND FAULT LIGHT EXTINGUISHED. AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA04035AOP](https://openairdocs.org/sdr/GAIA04035AOP.md): Fire Loop · malfunctioned · Feb 24, 2004 · N279US · Boeing 727251 · Fire Detection
  > FLT 875 - FWA-LAX - DURING PREFLIGHT, ENGINE NR 3 FIRE PROTECTION GROUND FAULT LIGHT REMAINS ILLUMINATED. (M)
- [SDR GAIA03159OP](https://openairdocs.org/sdr/GAIA03159OP.md): Brake Assy · separated · Oct 30, 2003 · N279US · Boeing 727251 · Landing Gear Brake System
  > DURING TAXI TO DEPARTURE THE CAPTAIN NOTICED THAT THE LEFT BRAKES WERE DRAGGING. THE AIRCRAFT TAXIED BACK TO THE RAMP. THE NR 2 BRAKE DISK WAS FOUND SEPARATED AND JAMBED. THE NR 2 BRAKE AND DEBOOSTER VALVE WERE REPLACED. OPERATIONALLY CHECKED GOOD. THE AI
- [SDR GAIA03004OP](https://openairdocs.org/sdr/GAIA03004OP.md): Light · inoperative · Feb 5, 2003 · N279US · Boeing 727251 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT AND FORWARD ENTRY EXIT LIGHT WERE DIM. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLIES. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02128ST](https://openairdocs.org/sdr/GAIA02128ST.md): Seat Track · corroded · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE SEAT TRACK AT BS 520, RBL 25 WAS CORRODED OUT OF LIMITS. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 51-30-5, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02127ST](https://openairdocs.org/sdr/GAIA02127ST.md): Stringer · cracked · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, Longeron/Stringer
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT STRINGER S15L WAS CRACKED AT BS 730. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-3, FIGURE 5. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02126ST](https://openairdocs.org/sdr/GAIA02126ST.md): Stringer · cracked · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, Longeron/Stringer
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT STRINGER S15R WAS CRACKED AT BS 730. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-3, FIGURE 5. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02125ST](https://openairdocs.org/sdr/GAIA02125ST.md): Frame · dented · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, Frame
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE PREVIOUS REPAIR AT FRAME BS 600, STRINGER S17R. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-4, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02124ST](https://openairdocs.org/sdr/GAIA02124ST.md): Frame · dented · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, Frame
  > DURING LTC INSPECTION, IT WAS DISCOVERED THAT THE FRAME AT BS 560, STRINGER S7R IS DENTED. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-4, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02123ST](https://openairdocs.org/sdr/GAIA02123ST.md): Frame · dented · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, Frame
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT A PREVIOUS REPAIR TO A FRAME AT BS 540, STRINGER S17R HAD BEEN DENTED. ACCOMPLISHED REPAIR TO FRAME IAW 727 SRM 53-10-4, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02122ST](https://openairdocs.org/sdr/GAIA02122ST.md): Frame · dented · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, Frame
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE FRAME AT BS 540, STRINGER S9R WAS DENTED. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-4, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02121ST](https://openairdocs.org/sdr/GAIA02121ST.md): Skin · dented · Sep 19, 2002 · N279US · Boeing 727251 · Aileron Tabs
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE RIGHT WING OUTBOARD AILERON TAB HAS A SHARP DENT. REMOVED AND REPLACED THE RIGHT OUTBOARD AILERON TAB IAW BOEING MM 27-10-41. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02120ST](https://openairdocs.org/sdr/GAIA02120ST.md): Frame · dented · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, Frame
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THE THE FUSELAGE FRAME AT BS 400, STRINGER S6R WAS DENTED. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-4, FIGURE 2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02119ST](https://openairdocs.org/sdr/GAIA02119ST.md): Frame · dented · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, Frame
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE FRAME AT BS 380 WAS DENTED AT STRINGER S5L. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-4, FIGURE 2. THIS AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02118ST](https://openairdocs.org/sdr/GAIA02118ST.md): Skin · cracked · Sep 19, 2002 · N279US · Boeing 727251 · Cargo/Baggage Doors
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE MAIN CARGO DOOR INNER SKIN IS CRACKED AROUND NR 3 LATCH HOOK ASSEMBLY FROM AFT CENTER ATTACH BOLT. ACCOMPLISHED REPAIR IAW COTNEY EDR03-1, 8110-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02117ST](https://openairdocs.org/sdr/GAIA02117ST.md): Seat Track · corroded · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE SEAT TRACK AT BS 520, RBL 45.5 IS CORRODED. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-5, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02116ST](https://openairdocs.org/sdr/GAIA02116ST.md): Frame · cracked · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, Frame
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT A FRAME AT BS 344, STRINGER S2L WAS CRACKED. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-2, FIGURE 3 AND 53-10-4, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02115ST](https://openairdocs.org/sdr/GAIA02115ST.md): Beam · cracked · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE AFT PRESSURE BULKHEAD VERTICAL BEAM AT BS 1183, WL 240, RBL 36 IS CRACKED AT THE INBOARD CHORD. ACCOMPLISHED REPAIR IAW BOEING SERVICE BULLETIN 727-53-0192, REV 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02114ST](https://openairdocs.org/sdr/GAIA02114ST.md): Floorbeam · corroded · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, Floor Beam
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT A FLOORBEAM AT BS 783, LBL 45.5 HAS CORROSION AT UPPER T-CAP. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-8, FIGURE 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02112ST](https://openairdocs.org/sdr/GAIA02112ST.md): Seat Track · cracked · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE SEAT TRACK WAS CRACKED AT BS 720D, RBL 45.5. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-5, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA0211ST](https://openairdocs.org/sdr/GAIA0211ST.md): Floorbeam · damaged · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Main, Floor Beam
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE FLOORBEAM AT BS 560, LBL 3 HAVE NUMEROUS HOLES THROUGH THE UPPER FLANGE AND RADIUS. ACCOMPLISHED A REPAIR IAW BOEING 727 SRM 51-40-4, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02110ST](https://openairdocs.org/sdr/GAIA02110ST.md): Torque Box · cracked · Sep 19, 2002 · N279US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE VENTRAL STAIRS RIGHT LOWER TORQUE BOX HAS A CRACKED REPAIR CHANNEL AT BS 1263. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 53-10-2, FIGURE 6. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02130ST](https://openairdocs.org/sdr/GAIA02130ST.md): Stiffener · cracked · Sep 19, 2002 · N279US · Boeing 727251 · Wing Miscellaneous Structure
  > DURING A LTC INSPECTION, IN WAS DISCOVERED THAT THE LEFT WING LEADING EDGE AT WS 62.4 HAS A BOTTOM STIFFENER CRACKED. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 57-10-2, FIGURE 3 AND 51-40-4, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA020129ST](https://openairdocs.org/sdr/GAIA020129ST.md): Rib · cracked · Sep 19, 2002 · N279US · Boeing 727251 · Wing, Rib/Bulkhead
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE RIB CHORD AT FUSELAGE BS 760.95 LEFT WAS CRACKED AT THE FIRST TWO FORWARD HOLES. ACCOMPLISHED REPAIR IAW BOEING 727 SERVICE BULLETIN 727-57-0112, REV 4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02028OP](https://openairdocs.org/sdr/GAIA02028OP.md): Light · inoperative · Mar 21, 2002 · N279US · Boeing 727251 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY IN THE COCKPIT. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA01079OP](https://openairdocs.org/sdr/GAIA01079OP.md): Warning Light · activated · Mar 2, 2001 · N279US · Boeing 727251 · Overheat Detection
  > FLT 723 - ROC-TOL, LOSER AFT BODY OVERHEAT MOMENTARY ILLUMINATION. ISOLATED BY LOWER AFT BODY OVERHEAT ILLUMINATION CHECKLIST. COULD NOT GET LIGHT TO RE-ILLUMINATE. AIRCRAFT MADE AN UNEVENTFUL LANDING IN TOL. INSPECTED AIR CONDITIONING AND ANTI-ICE DUCTS F
- [SDR GAIA01088OP](https://openairdocs.org/sdr/GAIA01088OP.md): Accessory Unit · malfunctioned · Jan 10, 2001 · N279US · Boeing 727251 · Landing Gear Retraction/Extension System
  > FLT 708 - OKC-PHX - DURING APPROACH TO PHX, THE CREW NOTED ON GEAR EXTENSION THREE RED LIGHTS AND THREE GREEN LIGHTS ILLUMINATED. THE LANDING GEAR WAS RECYCLED AND ONLY THE GREEN LIGHTS ILLUMINATED. THE AIRCRAFT CONTINUED ITS APPROACH AND LANDED SAFELY AT PH
- [SDR GAIA01002OP](https://openairdocs.org/sdr/GAIA01002OP.md): Socket · corroded · Jan 4, 2001 · N279US · Boeing 727251 · Emergency Lighting
  > DURING NON-ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE L1 DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. CLEANED CORROSION FROM LIGHT SOCKET PINS AND CLEANED SOCKET RECEPTACLE. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00717](https://openairdocs.org/sdr/GAIA00717.md): Connector · dirty · Nov 27, 2000 · N279US · Boeing 727251 · Landing Gear Position and Warning
  > FLT 728 - BOS-TOL - ON APPROACH TO TOL, WITH THE GEAR HANDLE DOWN, THE AIRCRAFT INDICATED THE RED NOSE GEAR LIGHT AN NO GEAR DOWN AND LOCKED LIGHT. THE AIRCRAFT LANDED SAFELY, WITHOUT ANY FURTHER DIFFICULTIES. CLEANED AND SECURED CANNON PLUGS ON NOSE GEAR PO
- [SDR GAIA00477](https://openairdocs.org/sdr/GAIA00477.md): Shear Tie · corroded · Aug 11, 2000 · N279US · Boeing 727251 · Fuselage Main, Structure
  > DISCREPANCY: NO FLIGHT: FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT TIMCO/OSC MAINTENANCE FACILITY. FOUND SHEAR TIE CORRODED AT BS 950B FRAME, OUTBOARD OF STRINGER S29L. REF 20626. CORRECTIVE ACTION: REPAIRED SHEAR TIE IAW B727 SRM 53-10-1 AND 53-10-4. A/C
- [SDR GAIA00495](https://openairdocs.org/sdr/GAIA00495.md): Fitting · cracked · Aug 7, 2000 · N279US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DISCREPANCY: NO FLIGHT: FOUND DURING ROUTINE SCHEDULED MAINTENANCE. FOUND BS 370 STRINGER S-5R FITTING CRACKED. REF 20823. CORRECTIVE ACTION: REMOVED AND REPLACED FITTING IAW 727 SRM 51-30-2. A/C WAS RETURNED TO SERVICE.
- [SDR GAIA00500](https://openairdocs.org/sdr/GAIA00500.md): Stringer Clip · damaged · Aug 7, 2000 · N279US · Boeing 727251 · Fuselage Miscellaneous Structure
  > FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT TIMCO/OSC, IMPROPER BLEND OUT ON STRINGER CLIP AT BS 680, S7L, REF NR 20619. REMOVED AND REPLACED STRINGER CLIP IAW B727 SRM 51-20-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00498](https://openairdocs.org/sdr/GAIA00498.md): Rib · damaged · Aug 7, 2000 · N279US · Boeing 727251 · Vertical Stabilizer
  > FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT TIMCO/OSC, VERTICAL STAB CLOSURE REQUIRES SPOT FACING IAW S/B 727-55-071, REF NR 20880. REWORKED STAB CLOSURE RIB IAW B727 S/B 55-0071. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00497](https://openairdocs.org/sdr/GAIA00497.md): Clip · damaged · Aug 7, 2000 · N279US · Boeing 727251 · Fuselage Miscellaneous Structure
  > FOUND DURNIG ROUTINE SCHEDULED MAINTENANCE AT TIMCO/OSC, FOUND STRINGER CLIP GROUND OUT OF LIMITS AT BS 700, S3L, REF NR 20788. REMOVED AND REPLACED CLIP IAW B72 SRM 51-20-1 AND 53-10-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00496](https://openairdocs.org/sdr/GAIA00496.md): Angle · cracked · Aug 7, 2000 · N279US · Boeing 727251 · Fuselage Miscellaneous Structure
  > FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT TIMCO/OSC, FOUND FRAME ATTACH ANGLE CRACKED BS 620, AFT SIDE OF CUSP, REF NR 20854. REMOVED AND REPLACED CRACKED CUSP TO FRAME ATTACH ANGLE IAW B727 SRM 51-20-1 AND 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR GAIA00494](https://openairdocs.org/sdr/GAIA00494.md): Frame · damaged · Aug 7, 2000 · N279US · Boeing 727251 · Fuselage Main, Frame
  > FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT TIMCO/OSC, FOUND FRAME DENT BETWEEN STRINGER 5R AND STRINGER 6R AT BS 380, REF 20822. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER, AND INSTALLED DOUBLER IAW B727 SRM 53-10-4, FIGURE 2. THE AIRCRAFT WAS RETURN
- [SDR GAIA00493](https://openairdocs.org/sdr/GAIA00493.md): Lamp · inoperative · Aug 7, 2000 · N279US · Boeing 727251 · Emergency Lighting
  > FOUND DURING SCHEDULED MAINTENANCE AT TIMCO/OSC, EMERGENCY EXIT LIGHT AT L-1 DOOR HAS ONE LAMP INOPERATIVE. CLEANED LAMP HOLDER CONTACT AND SECURED LAMP. SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Next page: https://openairdocs.org/deregistered/N279US-2018-01-17/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 = 'N279US' AND deregistration_id = 'N279US-2018-01-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N279US-2018-01-17/reports

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