# Service difficulty reports: N278US, cancelled Dec 9, 2011

A list on [N278US, cancelled Dec 9, 2011](https://openairdocs.org/deregistered/N278US-2011-12-09.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 · 81 reports

- [SDR GAIA05034OP](https://openairdocs.org/sdr/GAIA05034OP.md): Engine · leaking · Nov 29, 2005 · N278US · Boeing 727251 · Engine (Turbine/Turboprop)
  > DURING TAKEOFF ROLL THE COCKPIT FILLED WITH SMOKE. TAKEOFF WAS ABORTED AND THE AIRCRAFT TAXIED TO THE RAMP. INVESTIGATION FOUND OIL IN THE NR1 ENGINE BLEED SADDLE DUCTS. ENGINE REMOVED, AIRCRAFT PARKED. (K)
- [SDR GAIA05025](https://openairdocs.org/sdr/GAIA05025.md): Light · inoperative · Oct 5, 2005 · N278US · Boeing 727251 · Emergency Lighting
  > DURING POST FLIGHT, FOUND COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT ASSY, CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (K)
- [SDR GAIA05018OP](https://openairdocs.org/sdr/GAIA05018OP.md): Smoke Detector · dirty · Mar 30, 2005 · N278US · Boeing 727251 · Smoke Detection
  > DURING CRUISE, MAIN CARGO SMOKE WARNING ILLUMINATED IN FLIGHT. VISUAL INSPECTION REVEALED NO SMOKE IN CARGO AREA. FLIGHT CONTINUED TO DESTINATION, WHERE A LANDING WAS MADE WITHOUT INCIDENT. CLEANED SMOKE DETECTORS FROM NR1 TO NR 6. ON NR 1 REPLACED BOTH LI
- [SDR GAIA04086OP](https://openairdocs.org/sdr/GAIA04086OP.md): Bulb · inoperative · Jul 10, 2004 · N278US · Boeing 727251 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOPERATIVE. RELAMPED AND CLEANED BATTERY CONTACTS, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR GAIA04082OP](https://openairdocs.org/sdr/GAIA04082OP.md): Duct · blown · Jun 16, 2004 · N278US · Boeing 727251 · Cabin Cooling System
  > DURING CRUISE,UNABLE TO MAINTAIN CABIN ALTITUDE AT FLIGHT LEVEL 310, DIVERTED TO MSP. LANDED AIRCRAFT AT 169000 LBS, LANDING WAS UNEVENTFUL. FOUND BLOWN DUCT ON RIGHT PACK FROM FORWARD HEAT EXCHANGER TO COMPRESSOR DISCHARGE PORT OF ACM. REMOVED AND REPLACED
- [SDR GAIA04029OP](https://openairdocs.org/sdr/GAIA04029OP.md): Computer · malfunctioned · Feb 18, 2004 · N278US · Boeing 727251 · Autopilot Computer
  > DURING CRUISE THE AIRPLANE OCCASIONALLY TURNS RIGHT AND WILL NOT RESPOND BACK TO THE LEFT WITH FULL AUTOPILOT HEADING DEFLECTION TO THE LEFT. FLIGHT CONTINUED AND AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED THE AUTO PILOT ROLL CHANNEL COMPUTER. SYS
- [SDR GAIA04027OP](https://openairdocs.org/sdr/GAIA04027OP.md): Autopilot Sys · malfunctioned · Feb 6, 2004 · N278US · Boeing 727251 · Autopilot System
  > FLT 278 - SFO-FWA - DUIRNG CRUISE HAD TO KEEP AUTO PILOT TURN KNOB ALL THE WAY TO THE LEFT TO HAVE AIRPLANE FLY STRAIGHT AND LEVEL. FLIGHT CONTINUED AND AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE PERFORMED AUTOPILOT SYSTEM OPS CHECKS ON GROUND. COULD NOT D
- [SDR GAIA04005OP](https://openairdocs.org/sdr/GAIA04005OP.md): Battery · weak · Jan 22, 2004 · N278US · Boeing 727251 · Smoke Detection
  > FLT 874 - LAX-FWA - DURING CRUISE, THE FLIGHT CREW NOTICED THAT ONE AFT CARGO SMOKE DETECTOR LIGHT ILLUMINATED. REMOVED AND REPLACED BATTERIES IN THE SMOKE DETECTOR AND THE SYSTEM OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA04006OP](https://openairdocs.org/sdr/GAIA04006OP.md): Autopilot Sys · intermittent · Jan 22, 2004 · N278US · Boeing 727251 · Auto Flight System
  > FLT 874 - LAX-FWA - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE AUTOPILOT HEADING SELECT INTERMITTENT. (M)
- [SDR GAIA04004OP](https://openairdocs.org/sdr/GAIA04004OP.md): Control Panel · intermittent · Jan 21, 2004 · N278US · Boeing 727251 · Auto Flight System
  > FLT 851 - SEA-FWA - DURING CRUISE, THE FILGHT CREW NOTICED THAT THE AUTOPILOT IN A MODE WITH THE HEADING SELECTOR ON OR OFF INTERMITTENTLY LOCKS UP. REMOVED AND REPLACED THE AUTOPILOT CONTROL PANEL. OPERATIONAL CHECKS ON THE GROUND FOUND NORMAL. THE AIRCRAF
- [SDR GAIA02164OP](https://openairdocs.org/sdr/GAIA02164OP.md): Switch · intermittent · Dec 6, 2002 · N278US · Boeing 727251 · Landing Gear Position and Warning
  > FLT 272 - LAX-FWA - DURING LANDING APPROACH TO FWA, WHEN LANDING GEAR SELECTOR LEVER WAS MOVED TO THE DOWN POSITION, THE NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. THE GEAR WAS RECYCLED AND A VISUAL CHECK WAS MADE THROUGH THE NOSE GEAR VIEW PORT
- [SDR GAIA02163OP](https://openairdocs.org/sdr/GAIA02163OP.md): Connector · loose · Dec 4, 2002 · N278US · Boeing 727251 · Landing Gear Position and Warning
  > FLT 715 - ELP-FWA - ON APPROACH TO FWA, WHEN LANDING GEAR SELECTOR LEVER WAS MOVED TO THE DOWN POSITION THE NLG RED UNSAFE LIGHT REMAINED ILLUMINATED. THE GEAR WAS RE-CYCLED AND ALL THREE DOWN AND LOCKED LIGHTS ILLUMINATED. THE AIRCRAFT LANDED WITHOUT FURTHE
- [SDR GAIA02162OP](https://openairdocs.org/sdr/GAIA02162OP.md): Accessory Unit · intermittent · Dec 3, 2002 · N278US · Boeing 727251 · Landing Gear Position and Warning
  > FLT 715 - ELP-FWA - ON APPROACH TO FW, WHEN LANDING GEAR SELECTOR LEVER WAS MOVED TO THE DOWN POSITION. THE NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH NO NOSE GREEN LIGHT AT ALL. THE GEAR WAS RE-CYCLED AND THE RED LIGHT REMAINED ON. FIVE MINUTES
- [SDR GAIA02159OP](https://openairdocs.org/sdr/GAIA02159OP.md): Sign · inoperative · Nov 20, 2002 · N278US · Boeing 727251 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA02157OP](https://openairdocs.org/sdr/GAIA02157OP.md): Connector · loose · Nov 20, 2002 · N278US · Boeing 727251 · Landing Gear Position and Warning
  > FLT 516 - FWA-ELP, ON APPROACH WHEN LANDING GEAR SELECTOR LEVER WAS MOVED TO THE DOWN POSITION. THE NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH NO NOSE GREEN LIGHT AT ALL. THE GEAR WAS RECYCLED AND THE RED LIGHT EXTINGUISHED. THE AIRCRAFT LANDED W
- [SDR GAIA02158OP](https://openairdocs.org/sdr/GAIA02158OP.md): Accessory Unit · malfunctioned · Nov 19, 2002 · N278US · Boeing 727251 · Landing Gear Position and Warning
  > FLT - 215 - DEN-FWA - ON APPROACH TO FWA, WHEN LANDING GEAR SELECTOR LEVER WAS MOVED TO THE DOWN POSITION THE NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED. THE GEAR WAS RECYCLED AND THE RED LIGHT EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT
- [SDR GAIA02096ST](https://openairdocs.org/sdr/GAIA02096ST.md): Skin · gouged · Aug 27, 2002 · N278US · Boeing 727251 · Fuselage Main, Plate/Skin
  > DURING SEVERE WEATHER IN PHOENIX, THE FUSELAGE BELLY SKIN WAS GOUGED FROM STATION 950C TO 990 BETWEEN STRINGER 28L-29. MAINTENANCE REPAIRED THE GOUGE PER FLIGHT VEHICLES CONSULTING, INC DRAWING NR 53-02463-3 DATED 8/01/02. (M)
- [SDR GAIA02097ST](https://openairdocs.org/sdr/GAIA02097ST.md): Skin · damaged · Aug 27, 2002 · N278US · Boeing 727251 · Fuselage Main, Plate/Skin
  > DURING SEVERE WEATHER IN PHOENIX, THE FUSELAGE BELLY SKIN WAS DAMAGED FROM STATION 950C TO 990 BETWEEN STRINGER 26L-28L. MAINTENANCE REPAIRED THE DAMAGE PER FLIGHT VEHICLES CONSULTING, INC DRAWING NR 53-02463-1 DATED 8/01/02. (M)
- [SDR GAIA02098ST](https://openairdocs.org/sdr/GAIA02098ST.md): Skin · gouged · Aug 27, 2002 · N278US · Boeing 727251 · Fuselage Main, Plate/Skin
  > DURING SEVERE WEATHER IN PHOENIX, THE FUSELAGE BELLY SKIN WAS DENTED AND GOUGED FROM STATION 970C TO 1009 BETWEEN STRINGER 26L-29L. MAINTENANCE REPAIRED THE DAMAGE PER FLIGHT VEHICLES CONSULTING INC DRAWING NR 53-02463-2 DATED 8/01/02. (M)
- [SDR GAIA02072OP](https://openairdocs.org/sdr/GAIA02072OP.md): Hydraulic System · failed · Jul 20, 2002 · N278US · Boeing 727251 · Hydraulic System, Main
  > DURING CRUISE THE AIRCRAFT STARTED TO LOOSE BOTH A AND B SYSTEM HYDRAULIC SYSTEM FLUID. BOTH SYSTEMS WERE SECURED AND THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED, USING MINIMUM BRAKING AND REVERSE THRUST. THE AIRCRAFT WAS STOPPED ON THE RUNWAY, THE
- [SDR GAIA02039OP](https://openairdocs.org/sdr/GAIA02039OP.md): Bleed Valve · leaking · Apr 19, 2002 · N278US · Boeing 727251 · Compressor Bleed Valve
  > FLT 734- FWA-DFW - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THEN RN 3 BLEED, AND OPERATED AT REDUCED THRUST TO EXTINGUISH THE LIGHT. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT FWA WAS UNEVENTFUL. REPLACED CLAMPS ON NR 3
- [SDR GAIA02038OP](https://openairdocs.org/sdr/GAIA02038OP.md): Clamp · out of position · Apr 19, 2002 · N278US · Boeing 727251 · Pneumatic Distribution System
  > FLT 874 - LAX-FWA - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, AND OPERATED AT REDUCED THRUST TO EXTINGUISHED THE LIGHT. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT FWA WAS UNEVENTFUL. ADJUSTED SHIMS AND REP
- [SDR GAIA02036OP](https://openairdocs.org/sdr/GAIA02036OP.md): Clamp · out of position · Apr 18, 2002 · N278US · Boeing 727251 · Pneumatic Distribution System
  > FLIGHT 863 - EWR-FWA - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, AND OPERATED AT REDUCED THRUST. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT FWA WAS UNEVENTFUL. REPOSITIONED CLAMP ON HIGH PRESSURE BLEED DUC
- [SDR GAIA02037OP](https://openairdocs.org/sdr/GAIA02037OP.md): Clamp · out of position · Apr 18, 2002 · N278US · Boeing 727251 · Engine Bleed Air System
  > FLT 875 - FWA-LAX - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, AND OPERATED AT REDUCED THRUST TO EXTINGUISHED THE LIGHT. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT LAX WAS UNEVENTFUL. REPOSITIONED CLAMP ON
- [SDR GAIA02035OP](https://openairdocs.org/sdr/GAIA02035OP.md): Clamp · loose · Apr 17, 2002 · N278US · Boeing 727251 · Pneumatic Distribution System
  > FLT 864 - FWA-EWR - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, THE LIGHT EXTINGUISHED AND REMAINED EXTINGUISHED. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT EWR WAS UNEVENTFUL. FOUND AIR LEAK AT THE NR 3 BLE
- [SDR GAIA02034OP](https://openairdocs.org/sdr/GAIA02034OP.md): Clamp · loose · Apr 16, 2002 · N278US · Boeing 727251 · Pneumatic Distribution System
  > FLT 879 - FWA-SJC - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THE NR 3 BLEED, THE LIGHT EXTINGUISHED AND REMAINED EXTINGUISHED. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT SJC WAS UNEVENTFUL. FOUND SEVERAL LOOSE CLAMPS AND
- [SDR GAIA01310OP](https://openairdocs.org/sdr/GAIA01310OP.md): Engine · failed · Sep 27, 2001 · N278US · Boeing 727251 · Turbine Section
  > DURING CLIMBOUT THROUGH 22,500 FEET, NR 1 ENGINE EPR DROPPED TO APPROXIMATELY 1.6 PROCEEDED BY A LOAD THUMP. ENGINE WAS SHUT DOWN AND EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO AIRPORT AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. INSPECTED THE AIRCRAF
- [SDR GAIA01304OP](https://openairdocs.org/sdr/GAIA01304OP.md): Smoke Detector · malfunctioned · Aug 29, 2001 · N278US · Boeing 727251 · Smoke Detection
  > FLT 1278 - DFW-FWA - AFTER TAKEOFF, THE UPPER CARGO COMPARTMENT SMOKE DETECTOR ILLUMINATED. VISUAL INSPECTION DID NOT DETECT ANY SMOKE IN CARGO AREA. THE FLIGHT CREW ELECTED TO RETURN TO DFW. AN UNEVENTFUL LANDING WAS MADE AT DFW. INSPECTION FOUND THE NR 3
- [SDR GAIA01303OP](https://openairdocs.org/sdr/GAIA01303OP.md): Smoke Detector · malfunctioned · Aug 28, 2001 · N278US · Boeing 727251 · Smoke Detection
  > KHA - FLT 278 - PHX-DFW - DURING CRUISE, THE UPPER CARGO COMPARTMENT SMOKE DETECTOR ILLUMINATED. VISUAL INSPECTION DID NOT DETECT ANY SMOKE IN CARGO AREA. AN UNEVENTFUL LANDING WAS MADE AT DFW. INSPECTION FOUND THE NR 6 SMOKE DETETECTOR FAILED TO TEST. THE
- [SDR GAIA01259ST](https://openairdocs.org/sdr/GAIA01259ST.md): Skin · dented · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Main, Plate/Skin
  > DURING AN LTC INSPECTION, IT WAS DISCOVERED A DENT ON FUSELAGE SKIN ABOVE NR 3 ENGINE AT BS 1263, STRINGER 7R. ACCOMPLISHED FUSELAGE SKIN REPAIR AT BS 1263, STRINGER 7R, IAW B727 SRM 53-03-3 FIG 3. (M)
- [SDR GAIA01260ST](https://openairdocs.org/sdr/GAIA01260ST.md): Elevator · corroded · Aug 6, 2001 · N278US · Boeing 727251 · Empennage Structure
  > DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED RIGHT ELEVATOR HAD CORROSION, BOTTOM SIDE, ELEVATOR STATION 66, AREA IS MARKED. ACCOMPLISHED ELEVATOR SKIN REPAIR IAW B727 SRM 55-20-3, FIG 1. (M)
- [SDR GAIA01261ST](https://openairdocs.org/sdr/GAIA01261ST.md): Door Frame · cracked · Aug 6, 2001 · N278US · Boeing 727251 · Electrical/Electronic Compartment Doors
  > DURING AN LTC INSPECTION, DISCOVERED E/E COMPARTMENT DOOR FRAME LEFT AFT SIDE AFT SIDE OF FRAME LOWER CORNER CRACKED. ACCOMPLISHED BS 420 FRAME REPAIR IAW B727 SRM 51-40-3, FIG 1. (M)
- [SDR GAIA01262ST](https://openairdocs.org/sdr/GAIA01262ST.md): Web · cracked · Aug 6, 2001 · N278US · Boeing 727251 · Doors
  > DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED E/E COMPARTMENT DOOR, RIGHT WEB HAS TWO CRACKS EMANATING FROM PUNCTURE. ACCOMPLISHED WEB REPAIR BS 420 IAW B727 SRM 51-40-2, FIG 1. (M)
- [SDR GAIA01263ST](https://openairdocs.org/sdr/GAIA01263ST.md): Fitting · cracked · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Structure (General)
  > DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED CARGO TIE DOWN FITTING CRACKED BS 720A, LBL 24, LBL 24, WL 156, FORWARD CARGO PIT. ACCOMPLISHED CARGO TIE DOWN FITTING REPLACEMENT IAW B727 SRM 51-30-2. (M)
- [SDR GAIA01264ST](https://openairdocs.org/sdr/GAIA01264ST.md): Angle · cracked · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Structure (General)
  > DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED FLOOR SUPPORT ATTACH ANGLE CRACKED AT BS 304-312, LBL 20 PLUS 30. ACCOMPLISHED FLOOR SUPPORT ATTACH ANGLE REPLACEMENT IAW B727 SRM 51-20-1 AND 51-20-2. (M)
- [SDR GAIA01265ST](https://openairdocs.org/sdr/GAIA01265ST.md): Angle · cracked · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED FLOOR SUPPORT ATTACH ANGLE CRACKED AT BS 312, LBL 12 IS CRACKED. ACCOMPLISHED FLOOR SUPPORT ATTACH ANGLE REPLACEMENT IAW B727 SRM 53-10-2, FIG 7, 51-20-1, FIG 7 AND 51-30-2. (M)
- [SDR GAIA01266ST](https://openairdocs.org/sdr/GAIA01266ST.md): Intercostal · cracked · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED INTERCOSAL UPPER FLANGE CRACKED AT BS 298, RBL 12 ABOVE PULLEY BRACKET. ACCOMPLISHED INTERCOSTAL REPLACEMENT IAW B727 SRM 53-10-2, FIG 7 AND 51-30-2. (M)
- [SDR GAIA01267ST](https://openairdocs.org/sdr/GAIA01267ST.md): Strap · cracked · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING AN LTC INSPECTION, IT WAS DISCOVERED FLOORBEAM LOWER CHORD STABILIZATION STRAP IS CRACKED AT BS 328, RBL 25. ACCOMPLISHED FLOORBEAM LOWER CHORD STABILIZATION STRAP REPAIR IAW B727 SRM 53-10-8, FIG 6. (M)
- [SDR GAIA01268ST](https://openairdocs.org/sdr/GAIA01268ST.md): Strap · cracked · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Miscellaneous Structure
  > DURING AN LTC INSPECTION, IT WAS DISCOVERED FLOORBEAM LOWER CHORD STABILIZATION STRAP IS CRACKED/BROKEN AT BS 360, LBL 25. ACCOMPLISHED FLOORBEAM LOWER CHORD STABILIZATION STRAP REPAIR IAW B727 SRM 53-10-8, FIG 6. (M)
- [SDR GAIA01269ST](https://openairdocs.org/sdr/GAIA01269ST.md): Frame · cracked · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Structure (General)
  > DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 400 FRAME CRACKED AND DENTED BETWEEN STRINGER 7-8R. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 53-10-4, FIG 1. (M)
- [SDR GAIA01270ST](https://openairdocs.org/sdr/GAIA01270ST.md): Frame · dented · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Structure (General)
  > DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 380 FRAME DENTED BETWEEN STRINGER 5-6I. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 53-10-4, FIG 2. (M)
- [SDR GAIA01271ST](https://openairdocs.org/sdr/GAIA01271ST.md): Floorbeam · corroded · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Main, Floor Beam
  > DURING AN LTC INSPECTION, IT WAS DISCOVERED LONGITUDINAL FLOOR BEAM UPPER CHORD EXFOLIATED BS 760-780 AND 800-820, INBOARD LEG, RBL 45.5. ACCOMPLISHED FLOOR BEAM UPPER CHORD REPLACEMENT IAW B727 SRM 53-10-2 AND 51-30-5. (M)
- [SDR GAIA01272ST](https://openairdocs.org/sdr/GAIA01272ST.md): Web · cracked · Aug 6, 2001 · N278US · Boeing 727251 · Vertical Stabilizer
  > DURING AN LTC INSPECTION, IT WAS DISCOVERED STATION 1300 LEFT AND RIGHT CORNERS ON WEB HAVE.5 INCH CRACK. ACCOMPLISHED UPPER TORQUE BOX WEB REPAIR IAW B727 SRM 55-30-2, FIG 2 AND 51-40-2, FIG 1. (M)
- [SDR GAIA01273ST](https://openairdocs.org/sdr/GAIA01273ST.md): Frame · dented · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Structure (General)
  > DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 580 FRAME DENTED BETWEEN STRINGER 15 AND 16. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3, FIG 1 AND 53-10-2, FIG 3. (M)
- [SDR GAIA01274ST](https://openairdocs.org/sdr/GAIA01274ST.md): Frame · cracked · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Structure (General)
  > DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 640 IS CRACKED AND ENTERED BETWEEN STRINGER 16 AND 17R. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3, FIG 1 AND 53-10-2, FIG 3. (M)
- [SDR GAIA01275ST](https://openairdocs.org/sdr/GAIA01275ST.md): Stringer · cracked · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Structure (General)
  > DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15 RIGHT IS CRACKED AT BS 720B PLUS 15. ACCOMPLISHED STRINGER REPAIR IAW B727 SRM 53-10-3, FIG 5. (M)
- [SDR GAIA01276ST](https://openairdocs.org/sdr/GAIA01276ST.md): Stringer · cracked · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Structure (General)
  > DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15 LEFT IS CRACKED AT BS 720B PLUS 15. ACCOMPLISHED STRINGER REPAIR IAW B727 SRM 53-10-3, FIG 5. (M)
- [SDR GAIA01277ST](https://openairdocs.org/sdr/GAIA01277ST.md): Frame · dented · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Structure (General)
  > DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN LOWER AFT CARGO, FRAME BS 950C HAS A DENT AT STRINER 26L. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2, FIG 5. (M)
- [SDR GAIA01278ST](https://openairdocs.org/sdr/GAIA01278ST.md): Frame · dented · Aug 6, 2001 · N278US · Boeing 727251 · Fuselage Structure (General)
  > DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN LOWER AFT CARGO, FRAME BS 1110 HAS A DENT IN THE RADIUS ABOVE STRINGER 26L. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3, FIG 1 AND 53-10-2 FIG 5. (M)
- [SDR GAIA01279ST](https://openairdocs.org/sdr/GAIA01279ST.md): Web · cracked · Aug 6, 2001 · N278US · Boeing 727251 · Doors
  > DURING AN LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN AFT CARGO C-3 DOOR LOWER FORWARD WEB AND STRAP IS DENTED AND CRACKED AT STRINGER 26R. ACCOMPLISHED WEB AND STRAP REPAIR IAW B727 SRM 52-30-1, FIG 6 AND 51-40-2 FIG 1. (M)

Next page: https://openairdocs.org/deregistered/N278US-2011-12-09/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 = 'N278US' AND deregistration_id = 'N278US-2011-12-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N278US-2011-12-09/reports

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