# Service difficulty reports: Boeing 727-243

A list on [Boeing 727-243](https://openairdocs.org/model/boeing-727-243.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 11 · 534 reports

- [SDR CA141224004](https://openairdocs.org/sdr/CA141224004.md): Pcu · failed · Dec 22, 2014 · Boeing 727243 · Elevator Tab Control System
  > (CAN) SHORTLY AFTER TAKEOFF, THE HYDRAULIC SYSTEM A LOW PRESSURE LIGHTS ILLUMINATED. THE FLIGHT CREW DETERMINED THAT A LEAK HAD DEPLETED THE HYDRAULIC SYSTEM A FLUID, COMPLETED THE APPROPRIATE CHECKLIST AND A RETURN TO BASE WAS CONDUCTED. THE A/C LANDED SAFELY
- [SDR CA141027012](https://openairdocs.org/sdr/CA141027012.md): Wheel Half · cracked · Aug 20, 2014 · Boeing 727243 · Wheel/Ski/Float
  > (CAN) INNER WHEEL HALF FOUND TO BE CRACKED AT KEY BOSS DURING O/H.
- [SDR CA140425004](https://openairdocs.org/sdr/CA140425004.md): Switch · failed · Apr 22, 2014 · Boeing 727243 · Leading Edge Slat Control System
  > (CAN) MISSED APPROACH CARRIED OUT DUE NR 5 SLAT INDICATION FAILED TO INDICATE EXTENDED. CHECKLIST CARRIED OUT AND RETURNED FOR LANDING. SWITCH REPLACED AND ACFT RETURNED TO SERVICE.
- [SDR CA131204007](https://openairdocs.org/sdr/CA131204007.md): Duct · cracked · Nov 30, 2013 · Boeing 727243 · Engine (Turbine/Turboprop)
  > (CAN) ON ARRIVAL, MAINTENANCE DISCOVERED THE UPPER COWLING BLOWOUT PANEL MISSING ON THE NR 1 ENGINE. FURTHER INVESTIGATION FOUND THE 6TH STAGE DUCT RUPTURED. THE 6TH STAGE DUCT AND BLOWOUT PANEL WERE REPLACED. ACFT WAS RETURNED TO SERVICE.
- [SDR CA131120011](https://openairdocs.org/sdr/CA131120011.md): Tube · cracked · Nov 19, 2013 · Boeing 727243 · Air Intake Anti/De-Ice System
  > (CAN) DURING POST FLIGHT INSPECTION THE BLOW OUT PANEL WAS FOUND MISSING FROM THE UPPER COWL ON THE NR 3 ENGINE. FURTHER INSPECTION FOUND THE RT INLET ANTI-ICE DUCT CRACKED. THE DUCT AND UPPER COWL WERE REPLACED AND THE ACFT WAS RETURNED TO SERVICE.
- [SDR CA130803011](https://openairdocs.org/sdr/CA130803011.md): Manifold · cracked · Jul 31, 2013 · Boeing 727243 · Hydraulic System, Main
  > (CAN) GROUND CREWS NOTICED HYDRAULIC FLUID COMING FROM THE MAIN CARGO DOOR. MAINTENANCE DISCOVERED A CHECK VALVE HAD SHEARED IN TWO AND SUBSEQUENTLY REPLACED THE MAIN CARGO DOOR NR 6 HYDRAULIC MANIFOLD.
- [SDR CA130726018](https://openairdocs.org/sdr/CA130726018.md): Module · bypassing · Jul 19, 2013 · Boeing 727243 · Hydraulic System, Main
  > (CAN) ON TAXI OUT, CREW EXPERIENCED AN EXCESSIVE DROP IN HYDRAULIC PRESSURE WHILE OPERATING THE FLAPS. THE ACFT RETURNED TO THE RAMP WHERE MAINTENANCE DISCOVERED THE ELEVATOR HYDRAULIC MODULE BYPASSING INTERNALLY. THE MODULE WAS REPLACED AND THE ACFT RETURNE
- [SDR CA121122007](https://openairdocs.org/sdr/CA121122007.md): Mount · broken · Nov 20, 2012 · Boeing 727243 · Leading Edge Devices
  > (CAN) UPON SELECTING FLAPS DOWN ON APPROACH, CREW NOTICED A HYDRAULIC SYS LOW PRESSURE LIGHT AND CORRESPONDING LOSS OF QTY. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED THE NR 2 SLAT ACTUATOR HAD BROKEN IT`S UPPER MOUNTS AND
- [SDR CA120511009](https://openairdocs.org/sdr/CA120511009.md): Strut · cracked · May 8, 2012 · Boeing 727243 · Main Landing Gear Strut/Axle/Truck
  > (CAN) DURING CLIMBOUT, CREW DISCOVERED THE RT MLG WOULD NOT RETRACT. CREW SELECTED GEAR DOWN AND LANDED UNEVENTFULLY. MAINTENANCE DISCOVERED THE RT MAIN UPPER SIDE STRUT CRACKED. THE DAMAGED PIECES WERE REPLACED AND THE ACFT RETURNED TO SERVICE.
- [SDR CA120125020](https://openairdocs.org/sdr/CA120125020.md): Wheel · failed · Jan 25, 2012 · Boeing 727243 · Wheel/Ski/Float
  > (CAN) UPON TOUCHDOWN AND WITH FULL REVERSE APPLIED,THE AIRCRAFT STARTED TO VEER OFF THE RUNWAY CENTERLINE,NORMAL CORRECTIVE PROCEDURES WERE APPLIED TO MAINTAIN DIRECTION CONTROL. MAINTENANCE FOUND THE FOLLOWING, ALL MAIN WHEEL TIRES FOUND TO BE BADLY SCUFFED
- [SDR CA120116013](https://openairdocs.org/sdr/CA120116013.md): Window · failed · Jan 12, 2012 · Boeing 727243 · Flight Compartment Windows
  > (CAN) WHILE INBOUND, THE FLIGHT CREW RADIOED AHEAD TO INFORM MAINTENANCE THAT THE L5 WINDOW WAS CRACKED. UPON INSPECTION IT WAS FOUND THAT THE L5 WINDOW INNER PANE WAS CRACKED. A NEW WINDOW WAS SHIPPED. L5 WINDOW WAS REPLACED AND ACFT DEPARTED.
- [SDR CA110902007](https://openairdocs.org/sdr/CA110902007.md): Flap System · lack of lube · Aug 26, 2011 · Boeing 727243 · Trailing Edge Flap Control System
  > (CAN) ON APPROACH, CREW DISCOVERED THE OTBD FLAPS WOULD NOT EXTEND TO LANDING POSITION AND ELECTED TO GO AROUND. CREW USED ALTERNATE (ELECTRIC) SYS TO EXTEND THE FLAPS AND LANDED UNEVENTFULLY. THE FLAP SYS WAS LUBED IAW THE MM AND TESTED SERVICEABLE, AND WAS
- [SDR CA110209017](https://openairdocs.org/sdr/CA110209017.md): Module · failed · Feb 8, 2011 · Boeing 727243 · Landing Gear Retraction/Extension System
  > DURING APPROACH, WITH THE GEAR DOWN, THE NOSE GEAR INDICATION GREEN LIGHT DID NOT ILLUMINATE. MAINT REPLACED THE LANDING GEAR INDICATION MODULE AND CHECKED IT SERVICEABLE.
- [SDR CA110209012](https://openairdocs.org/sdr/CA110209012.md): Module · failed · Feb 8, 2011 · Boeing 727243 · Landing Gear Retraction/Extension System
  > NOSE GEAR DOWN LOCK GREEN LIGHT WOULD NOT ILLUMINATE, REPLACED LANDING GEAR MODULE.
- [SDR CA100728005](https://openairdocs.org/sdr/CA100728005.md): Switch · failed · Jul 16, 2010 · Boeing 727243 · Pneumatic Distribution System
  > DURING CLIMB OUT FROM, THE LT AFT BODY O/H LIGHT ILLUMINATED. CHECKLIST- AFT BODY OVERHEAT CARRIED OUT. NR 1 BLEED AND LT PACK TURNED OFF, LIGHT EXTINGUISHED. LT PACK UTILIZED USING NR 2 BLEED, AFTER 3 MIN, NR 2 BLEED AIR HIGH TEMP LIGHT ILLUMINATED. CREW
- [SDR CA100705001](https://openairdocs.org/sdr/CA100705001.md): Turbine · damaged · Jun 30, 2010 · Boeing 727243 · Turbine Section
  > ACFT DEPARTED, ON CLIMB AT APROX 11,000FT CREW HAD A VIBRATION ON NR 1 ENG. FLT CREW CARRIED OUT SHUTDOWN PROCEDURES AND RETURNED. THE ENGINE WAS FOUND TO HAVE LOW PRESSURE TURBINE DAMAGE. ACFT FERRIED FOR ENGINE CHANGE.
- [SDR CA100223006](https://openairdocs.org/sdr/CA100223006.md): Pressure Switch · faulty · Feb 19, 2010 · Boeing 727243 · Engine Oil Indicating System
  > (CAN) CREW EXPERIENCED A LOW OIL PRESS/FILTER BYPASS LIGHT ILLUMINATE FOR THE NR 3 ENG. THE NR 3 ENGINE WAS SHUTDOWN IAW THE CHECKLIST. A FAULTY FILTER BYPASS SWITCH WAS REPLACED AND THE ACFT RETURNED TO SERVICE. (TC 20100223006)
- [SDR CA090520004](https://openairdocs.org/sdr/CA090520004.md): Controller · arced · May 19, 2009 · Boeing 727243 · Windshield/Door Rain/Ice Removal
  > (CAN) ON CLIMB OUT, CREW NOTICED ARCING FROM THE R2 WINDOW. ACFT DIVERTED TO A MX BASE WHERE THE WINDOW AND TEMP CONTROLLER WERE REPLACED AND THE ACFT RETURNED TO SERVICE.
- [SDR CA080728003](https://openairdocs.org/sdr/CA080728003.md): Pcu · failed · Jul 25, 2008 · Boeing 727243 · Aileron Control System
  > (CAN) ENROUTE, CREW NOTICED HYD SYS (A) QUANTITY DECREASING RAPIDLY. SYS (A) HYDR WERE SHUTOFF AND EMERGENCY DECLARED. UPON ARRIVAL AT DESTINATION, A/C REQUIRED TOWING TO RAMP WHERE MAINT DISCOVERED THE AILERON PCU HAD FAILED. THE AILERON PCU WAS REPLACED AND
- [SDR CA080716008](https://openairdocs.org/sdr/CA080716008.md): Position Switch · malfunctioned · Jul 14, 2008 · Boeing 727243 · Leading Edge Slat Position Indicating System
  > (CAN) ON APPROACH AN IN-TRANSIT INDICATION WAS ILLUMINATED ON THE NR 6 L/E SLAT. THE CREW ELECTED TO RETURN TO VANCOUVER WHERE THEY LANDED WITHOUT INCIDENT. INSPECTION REVEALED THAT THE NR 6 L/E SLAT WAS FUNCTIONING CORRECTLY BUT THE L/E SLAT POSITION SWITCH W
- [SDR CA070727004](https://openairdocs.org/sdr/CA070727004.md): Fitting · damaged · Jul 25, 2007 · Boeing 727243 · Engine Oil Distribution (Airframe Furnished)
  > (CAN) TOP OF DESCENT, THE NR 1 LOW OIL PRESSURE LIGHT ILLUMINATED, QTY AT ZERO. PRECAUTIONARY ENGINE SHUTDOWN CARRIED OUT. GEARBOX FITTING (OIL PRESSURE DIFFERENTIAL SWITCH) THREAD REPAIRED AND FITTING REPLACED. ENGINE INSPECTEED IAW MM AND RETURNED TO SERV
- [SDR GAIA0706OP](https://openairdocs.org/sdr/GAIA0706OP.md): Wire · broken · May 26, 2007 · N1269Y · Boeing 727243 · Landing Gear System Wiring
  > ON TAKEOFF THE LANDING GEAR LEVER WOULD NOT GO PAST THE OFF POSITION FOR GEAR UP. THE CREW LEFT THE GEAR HANDLE IN THE DODWN POSITION AND RETURNED TO DEPARTURE. AN UNEVENTFUL LANDING WAS MADE. THE GEAR HANDLE LOCK SOLENOID AND THE GEAR GROUND MODE PROXIMITY
- [SDR CA070404006](https://openairdocs.org/sdr/CA070404006.md): Switch · malfunctioned · Mar 29, 2007 · Boeing 727243 · Leading Edge Slat Position Indicating System
  > (CAN) ON FLAP RETRACTION THE CREW NOTICED THE NR 3 KRUGER FLAP INDICATED (IN TRANSIT). CREW RETURNED TO BASE. NR 3 KRUGER FLAP RETRACT SWITCH WAS REPLACED AND A/C RETURNED TO SERVICE. (TC NR 20070404006)
- [SDR CA080211016](https://openairdocs.org/sdr/CA080211016.md): Downlock Switch · failed · Feb 24, 2007 · Boeing 727243 · Landing Gear Position and Warning
  > (CAN) DURING APPROACH INTO AIRPORT, THE LANDING GEAR WAS EXTENDED AT WHICH TIME THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AND THE DOWN AND LOCKED LIGHT REMAINED EXTINGUISHED. THE GEAR WAS RECYCLED WITH THE SAME RESULT AND SOON AFTERWARD, THE UNSAFE LIGHT
- [SDR CA070125006](https://openairdocs.org/sdr/CA070125006.md): Engine · leaking · Jan 23, 2007 · Boeing 727243 · Turbine Engine Oil System
  > (CAN) ENROUTE, NR 3 ENGINE OIL LOSS, AIRCRAFT DIVERTED. INSPECTED AND FERRIED AIRCRAFT. ENGINE REPLACED (TC NR 20070125006)
- [SDR CA061216003](https://openairdocs.org/sdr/CA061216003.md): Line · leaking · Dec 12, 2006 · Boeing 727243 · Hydraulic System, Main
  > (CAN) AFTER T/O DURING CLIMB (B) PUMP LOW PX LITE ILLUMINATED WITH FLUID QTY DROP. RETURNED TO DEPARTURE, HYD LINE REPLACED IN B COMPT. (TC NR 20061216003)
- [SDR CA061014001](https://openairdocs.org/sdr/CA061014001.md): Valve · failed · Oct 11, 2006 · Boeing 727243 · Cabin Cooling System
  > (CAN) AFTER DEPARTURE, CREW DISCOVERED THAT THE A/C WOULD NOT PRESSURIZE. A/C RETURNED TO BASE WHERE A PACK VALVE WAS FOUND FAILED IN THE CLOSED POSITION. VALVE WAS REPLACED AND A/C RETURNED TO SERVICE. (TC NR 20061014001)
- [SDR CA060706004](https://openairdocs.org/sdr/CA060706004.md): Tru · smoke · Jul 2, 2006 · Boeing 727243 · DC Rectifier/Converter
  > (CAN) WHILE AIRCRAFT WAITING ON THE GATE TO BOARD PASSENGERS FOR DEPARTURE, SMOKE WAS OBSERVED IN THE COCKPIT. CAUSE OF SMOKE WAS DETERMINED TO BE THE NR 2 TRANSFORMER RECTIFIER. UNIT REPLACED WITH NO FURTHER DEFECTS. (TC# 20060706004)
- [SDR CA050617005](https://openairdocs.org/sdr/CA050617005.md): Valve · stuck · Jun 11, 2005 · Boeing 727243 · Fuel Heater
  > (CAN) DURING CLIMB OUT, THE CREW NOTICED THAT NR 2 ENGINE OIL TEMPERATURE WAS INCREASING. TEMP CONTINUED TO INCREASE DURING CLIMB AND ENGINE WAS SHUT DOWN. AIRCRAFT RETURNED TO BASE. INVESTIGATION FOUND THAT THE NR 2 ENGINE FUEL HEAT VALVE WAS STUCK IN THE OP
- [SDR CA050614010](https://openairdocs.org/sdr/CA050614010.md): Engine · failed · Jun 10, 2005 · Boeing 727243 · Engine (Turbine/Turboprop)
  > DURING CLIMB AND AFTER DEPARTURE, NR 2 ENGINE HIGH OIL TEMP WAS EXPERIENCED. HIGH OIL TEMP SUP PROCEDURES ACCOMPLISHED, FOLLOWED BY THE ENGINE FAILURE/SHUTDOWN CHECKLIST. A/C RETURNED TO BASE. MAINTENANCE TROUBLESHOOTING FOUND 2 SNAGS. FUEL ANT-ICE VALVE P/N
- [SDR CA050620002](https://openairdocs.org/sdr/CA050620002.md): Bolt · loose · May 31, 2005 · Boeing 727243 · Landing Gear Position and Warning
  > (CAN) ON TAKEOFF, LANDING GEAR WOULD NOT RETRACT. MAINTENANCE FOUND AIR/GND PROX TARGET LEVER BOLT LOOSE. BOLT/NUT- P/N NAS 1303-8/BACN10JC3.
- [SDR GAIA05014ST](https://openairdocs.org/sdr/GAIA05014ST.md): Skin · delaminated · Mar 19, 2005 · N1269Y · Boeing 727243 · Trailing Edge Flaps
  > DURING A-CHECK, NO FLIGHT, FWA: FOUND LT IB MID-FLAP OB T/E MISSING 6 INCHES OF SKIN. REMOVED AND REPLACED LT IB MID-FLAP AND AFT FLAPS ASSY. OPS CHECKED NORMAL IAW MM 27-51. AIRCRAFT WAS RETURNED TO SERVICE. (SW07200506017) (K)
- [SDR CA050211005](https://openairdocs.org/sdr/CA050211005.md): Bearing · broken · Feb 6, 2005 · Boeing 727243 · Drag Control System
  > (CAN) THE PILOT REPORTED THE RT SPOILERS WERE NOT DEPLOYING PROPERLY AND 50 DEGREES RT AILERON WAS REQUIRED TO KEEP WINGS LEVEL AT FULL SPOILER DEFLECTION. UPON INSPECTION OF THE SPOILER RATIO CHANGER AND MIXER, THE RT AFT LOWER SPOILER CABLE ROD END BEARING
- [SDR CA040812001](https://openairdocs.org/sdr/CA040812001.md): B-Nut · cracked · Jul 29, 2004 · Boeing 727243 · Hydraulic System, Main
  > (CAN) CREW REPORTED 'A' SYSTEM HYDRAULIC FLUID LOSS IN FLIGHT. MAINTENANCE FOUND LEAK AT B-NUT END FITTING AT 'A' SYSTEM MODULE. LINE REPLACED.
- [SDR GAIA04084SD](https://openairdocs.org/sdr/GAIA04084SD.md): Tru · overheated · Jun 11, 2004 · N1269Y · Boeing 727243 · DC Rectifier/Converter
  > FIRE WAS REPORTED FROM NR 1 TRANSFORMER RECTIFIER UNIT (TRU), LOCATED IN FORWARD EE BAY. PWR HAD BEEN ON AC APPROX 1HOUR AND 30 MINUTES. FIRE WAS EXTINGUISHED AND TRU WAS REMOVED FROM AC. FIRE WAS CONTAINED WITHIN TRU WITH HEAT DAMAGE TO DRIP SHIELD LOCATED
- [SDR CA040521008](https://openairdocs.org/sdr/CA040521008.md): Sequence Valve · cracked · May 21, 2004 · Boeing 727243 · Landing Gear Door Retract Section
  > AFTER T/O AND GEAR RETRACTION, CREW NOTICED HYDRAULIC QUANTITY LOW. CREW MONITORED HYDRAULIC LEVEL FOR DURATION OF FLIGHT WITH NO CHANGE. UPON GEAR EXTENSION, HYDRAULIC QUANTITY DROPPED FURTHER, REQUIRING THE A/C TO BE TOWED TO RAMP FROM THE ACTIVE TAXIWAY.
- [SDR CA040521001](https://openairdocs.org/sdr/CA040521001.md): Module · failed · May 19, 2004 · Boeing 727243 · Landing Gear Actuator
  > (CAN) ON CLIMB OUT, CREW NOTICED NOSE (GEAR UNSAFE) LIGHT DID NOT EXTINGUISH. AFTER DUMPING FUEL, CREW RETURNED TO MAINTENANCE FACILLITY WHERE THE LANDING GEAR ACCY UNIT WAS REPLACED AND GEAR SWINGS PERFORMED. A/C RETURNED TO SERVICE.
- [SDR GAIA04052OP](https://openairdocs.org/sdr/GAIA04052OP.md): Connector · dirty · Mar 18, 2004 · N1269Y · Boeing 727243 · Flight Control System Wiring
  > ON TAKEOFF ROLL, AFTER FLAP RETRACTION THE NR 4 LEADING EDGE DEVICE INDICATED IN TRANSIT. NO ROLL WAS NOTED, THE AIRCARFT CONTINUED FLIGHT. CLEANED THE NR 4 LEADING EDGE FLAP SWITCH. RAN FLAPS SYSTEM OPS CHECKED NORMAL, THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR GAIA04054OP](https://openairdocs.org/sdr/GAIA04054OP.md): Switch · inoperative · Mar 17, 2004 · N579PE · Boeing 727243 · Trailing Flap Position Indicating System
  > FLT 753 - CLT-FWA - DURING TAXI, THE FLIGHT CREW NOTICED THAT THE NR 5 LEADING EDGE DEVICE WOULD NOT EXTEND. REMOVED AND REPLACED THE NR 5 LEADING EDGE FLAP POSTION SWITCH. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR CA040315002](https://openairdocs.org/sdr/CA040315002.md): Start Valve · cracked · Mar 13, 2004 · Boeing 727243 · Engine Starter
  > (CAN) DURING DEPARTURE CREW WAS UNABLE TO START NR 1 ENGINE. MAINTENANCE CALLED TO PERFORM A MANUAL START. FOUND THE BOTTOM OF THE START VALVE CRACKED AT THE ADJUSTMENT SCREW. VALVE REPLACED AND A/C DEPARTED.
- [SDR GAIA04022OP](https://openairdocs.org/sdr/GAIA04022OP.md): Computer · malfunctioned · Feb 6, 2004 · N1269Y · Boeing 727243 · Autopilot Computer
  > DURING CRUISE, THE AUTOPILOT OVER CORRECTS ON LOCALIZER. REMOVED AND REPLACED THE ROLL CHANNEL COMPUTER. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M)
- [SDR GAIA04025OP](https://openairdocs.org/sdr/GAIA04025OP.md): Connector · dirty · Feb 5, 2004 · N1269Y · Boeing 727243 · Flight Control System Wiring
  > DURING CRUISE, THE NR 4 LEADING EDGE FLAP SHOWS EXTENDED WITH THE FLAPS RETRACTED. CLEANED AND RESEATED THE CONNECTOR ON THE NR 4 LEADING EDGE FLAP SWITCH. OPS CHECK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M)
- [SDR GAIA04026OP](https://openairdocs.org/sdr/GAIA04026OP.md): Warning Light · illuminated · Feb 5, 2004 · N579PE · Boeing 727243 · Landing Gear System
  > AFTER TAKEOFF, THE TAIL SKID LIGHT REMAINED ILLUMINATED. RECYCLED THE LANDING GEAR AND THE LIGHT WENT OUT. PERFORMED OPERATIONAL CHECK AND TEST OF THE TAIL SKID SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M)
- [SDR GAIA04001OP](https://openairdocs.org/sdr/GAIA04001OP.md): Rib · corroded · Jan 17, 2004 · N1269Y · Boeing 727243 · Wing, Rib/Bulkhead
  > DURING ROUTINE MAINTENANCE, FOUND CORROSION ON THE RIGHT WING LEADING EDGE SUPPORT RIB AT WING STATION 240. REPAIRED WING RIB IAW BOEING SRM CH 51-40-4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR CA031212004](https://openairdocs.org/sdr/CA031212004.md): Control Cable · out of adjust · Dec 9, 2003 · Boeing 727243 · Aileron Control System
  > (CAN) CONTROL WHEEL VERY STIFF WHEN DEFLECTED LT AND SLOW TO RETURN ON RT DEFLECTION. LOST MOTION CABLES ADJUSTED IAW MM 27-10-0 AILERON INPUT PUSHROD ADJUSTED IAW MM 27-10-0CENTERING PUSHROD ADJUSTED A PER MM 27-10-0 SPOILER MIXER CONTROL ROD ADJUSTED MM 27-6
- [SDR CA031126011](https://openairdocs.org/sdr/CA031126011.md): Skin · cracked · Nov 20, 2003 · Boeing 727243 · Trailing Edge Flaps
  > (CAN) WHILE PERFORMING A (C CHECK), CORROSION WAS FOUND ON THE LT IB FLAP AT WBL 124. AFTER PAINT REMOVING IT WAS DISCOVERED THAT A CRACK OF.5000 INCH LONG WAS BENEATH THE PAINT. CRACK REPAIR IAW SRM.
- [SDR CA031117004](https://openairdocs.org/sdr/CA031117004.md): Skin · cracked · Nov 13, 2003 · Boeing 727243 · Fuselage Main, Plate/Skin
  > (CAN) THE AIRCRAFT WAS ON A (C CHECK. UPON INSPECTION OF THE FUSELAGE, A QUESTIONABLE SCRATCH WAS FOUND AT STATION BS 700 STRINGER NR 1. PAINT WAS STRIPPED AND NDT INSPECTION CARRIED OUT. A CRACK OF HALF INCH LONG WAS DISCOVERED. THE FUSELAGE WAS REPAIRED IAW
- [SDR CA031126012](https://openairdocs.org/sdr/CA031126012.md): Skin · lightning strike · Nov 12, 2003 · Boeing 727243 · Fuselage Main, Plate/Skin
  > (CAN) WHILE PERFORMING A (C CHECK) IT WAS FOUND THAT THE AIRPLANE HAD BEEN HIT BY LIGHTING. POINT OF ENTRY WAS AT NOSE DOOR AND EXIT POINT AT RT ELEVATOR TAB. REPAIR HAD TO BE CARRIED OUT BETWEEN BS 196 TO 203, BS 219 TO 235, FORWARD OF NOSE LDG FS 188, NOSE
- [SDR GAIA03158ST](https://openairdocs.org/sdr/GAIA03158ST.md): Restraint · worn · Oct 24, 2003 · N1269Y · Boeing 727243 · Cargo Compartments
  > DURNG C-CHECK INSPECTION FOUND MAIN CARGO PALLET SIDE RESTRAINTS WORN. REF FASI N/R NR 61123, REMOVED AND REPLACED SIDE RESTRAINTS BS 348 TO 1168 IAW KHA EA-B7-53-113, RESTRAINT P/N 2956 PO NR 34817. (M)
- [SDR GAIA03144ST](https://openairdocs.org/sdr/GAIA03144ST.md): Seat Track · corroded · Oct 24, 2003 · N1269Y · Boeing 727243 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK INSPECTION FOUND MAIN CABIN SEAT TRACK LBL 45.5 CORRODED BS 760 TO 850. REF FASI N/R NR 61760, REPLACED SEAT TRACK BS 760 TO 850 LBL 45.5 PER B727 SRM 53-10-5 FIG 7 AND 53-10-2 FIG 7. (M)

Next page: https://openairdocs.org/model/boeing-727-243/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 aircraft_model_key = '727243'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-243/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.