# Service difficulty reports: Boeing 727-231

A list on [Boeing 727-231](https://openairdocs.org/model/boeing-727-231.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 17 · 840 reports

- [SDR FDEA2019041630790](https://openairdocs.org/sdr/FDEA2019041630790.md): Door · binding · Apr 13, 2019 · N986FD · Boeing 727231 · Passenger/Crew Doors
  > L1 DOOR WILL NOT CLOSE FROM INSIDE OF A/C, BUT WILL CLOSE FROM OUTSIDE OF A/C.
- [SDR PCSA2013122601](https://openairdocs.org/sdr/PCSA2013122601.md): Accessory Unit · faulty · Dec 24, 2013 · N905AJ · Boeing 727231 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF THE LG LEVER WOULD NOT GO PAST OFF TO UP POSITION. GEAR WOULD NOT COME UP.
- [SDR PCSA2013050602](https://openairdocs.org/sdr/PCSA2013050602.md): Bypass Valve · faulty · May 3, 2013 · N905AJ · Boeing 727231 · Trailing Edge Flap Control System
  > UPON RETRACTION, INBOARD FLAPS REMAINED AT 20°. AFTER LANDING FLAPS RETRACTED NORMALLY. MAINTENANCE REPLACED THE FLAP BYPASS VALVE, THE INBD FLAP ASYMMETRIC RELAY R187 AND THE INBD FLAP INDICATOR PER THE AMM, ACCOMPLISHED THE FLAP OPERATIONAL CHECK PER THE A
- [SDR SPUY201304030032](https://openairdocs.org/sdr/SPUY201304030032.md): Floorbeam · corroded · Apr 3, 2013 · N905AJ · Boeing 727231 · Fuselage Main, Floor Beam
  > DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT- FLOORBEAM CORRODED BS 620 RBL 53 ML 208 REF N/R 0930.
- [SDR SPUY201304030031](https://openairdocs.org/sdr/SPUY201304030031.md): Beam · corroded · Apr 3, 2013 · N905AJ · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT- SKIN AND BEAM FLANGE LWR SKIN CORRODED, STA 910.000 LBL-27 REF N/R 0922.
- [SDR SPUY201304030030](https://openairdocs.org/sdr/SPUY201304030030.md): Beam · corroded · Apr 3, 2013 · N905AJ · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT- BEAM FLANGE AND SKIN CORRODED, STA 910 REF N/R 0836.
- [SDR SPUY201304030029](https://openairdocs.org/sdr/SPUY201304030029.md): Beam · corroded · Apr 3, 2013 · N905AJ · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT- BEAM FLANGE AND SKIN CORRODED STA 910 RBL 25 (LWR PART) REF N/R 0835.
- [SDR SPUY201304030028](https://openairdocs.org/sdr/SPUY201304030028.md): Structure · corroded · Apr 3, 2013 · N905AJ · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING ROUTINE C CHECK INSPECTION, AFTER CARGO COMPT- CORRODED, S-29R, STA 1110 STA 1130. REF N/R 0703.
- [SDR SPUY201304030027](https://openairdocs.org/sdr/SPUY201304030027.md): Skin · corroded · Apr 3, 2013 · N905AJ · Boeing 727231 · Wing, Plate/Skin
  > DURING ROUTINE C CHECK INSPECTION, RIGHT WING LEADING EDGE UPPER SKIN CORRODED, WBL 92.8. REF N/R 0178.
- [SDR CA120817008](https://openairdocs.org/sdr/CA120817008.md): Sliding Window · cracked · Aug 14, 2012 · Boeing 727231 · Flight Compartment Windows
  > (CAN) IN CRUISE NOTICED ARCHING ON R2 WINDOW AND DISCOVERED OUTER PANE WAS CRACKED. WINDOW REPLACED.
- [SDR PCSA2011090601](https://openairdocs.org/sdr/PCSA2011090601.md): Oil System · overtemp · Sep 6, 2011 · N905AJ · Boeing 727231 · Engine Oil Temperature
  > NUMBER 3 ENGINE SHUT DOWN DUE TO HIGH OIL TEMPERATURE.
- [SDR CA110505004](https://openairdocs.org/sdr/CA110505004.md): Rib · cracked · May 5, 2011 · Boeing 727231 · Spoilers
  > (CAN) DURING CLIMB OUT FLIGHT CREW HAD TO INPUT A CONTROL WHEEL DISPLACEMENT OF 25 DEGREES TO THE RIGHT OF CENTER TO MAINTAIN LEVEL FLIGHT. 1 DEGREE OF SPEED BRAKE LEVER WAS INPUT AND THIS CAUSED A REDUCTION OF CONTROL WHEEL DISPLACEMENT TO 10 - 15 DEGREES. IN
- [SDR PCSA2011041501](https://openairdocs.org/sdr/PCSA2011041501.md): Start Valve · malfunctioned · Apr 14, 2011 · N905AJ · Boeing 727231 · Engine Start Valves/Controls
  > AT FL270 ENGINE NR 3 START VALVE ILLUMINATED. ACCOMPLISHED SUPPLEMENTAL PROCEDURES. SHUT DOWN NR 3 ENGINE. ACCOMPLISHED ABNORMAL ENGINE SHUTDOWN CHECKLIST ON GENERATOR INOP CHECKLIST AND ONE ENGINE INOP LANDING CHECKLIST AND WINDMILLED ENGINE SUPPLEMENTAL P
- [SDR PCSA2011011302](https://openairdocs.org/sdr/PCSA2011011302.md): Switch · shorted · Jan 13, 2011 · N905AJ · Boeing 727231 · Fire Detection
  > DURING APPROACH INTO SAL WHEEL WELL FIRE AND BELL WERE ACTIVATED. AFTER LANDING MAINTENANCE T/S SYSTEM AND FOUND SHORT IN THE TEST SWITCH AND CORRECTED IT. NO PARTS NECESSSARY.
- [SDR PCSA2011011301](https://openairdocs.org/sdr/PCSA2011011301.md): Control Unit · defective · Jan 13, 2011 · N905AJ · Boeing 727231 · Fire Detection
  > DURING TAXI OUT WHEEL WELL FIRE LIGHT AND BELL WENT ON INTERMITTENTLY.
- [SDR PCSA2010031801](https://openairdocs.org/sdr/PCSA2010031801.md): Smoke Detector · false activation · Mar 18, 2010 · N905AJ · Boeing 727231 · Smoke Detection
  > SMOKE DETECTOR NR 3 LIGHT CAME ON INTERMITTENTLY IN FLIGHT. VERIFIED NO SMOKE IN CARGO COMPARTMENT. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE SMOKE DETECTION SYSTEM. NO DEFECTS WERE FOUND AND THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR PCSA2010031502](https://openairdocs.org/sdr/PCSA2010031502.md): Detector · defective · Mar 12, 2010 · N905AJ · Boeing 727231 · Smoke Detection
  > CREW LOG ITEM " NR 3 SMOKE DETECTOR LIGHT ILLUMIMATED AT TOP OF DESCENT. INSPECTED AREA. FALSE INDICATION". MAINTENANCE REPLACED THE NR 3 SMOKE DETECTOR AND RETURNED THE AIRCRAFT TO SERVICE.
- [SDR PCSA2010031501](https://openairdocs.org/sdr/PCSA2010031501.md): Smoke Detector · defective · Mar 11, 2010 · N905AJ · Boeing 727231 · Smoke Detection
  > CREW LOG ITEM "SMOKE DETECTION SYSTEM NR 3 LIGHT ILLUMINATED IN FLIGHT". MAINTENANCE REPLACED THE NR 3 SMOKE DETECTOR AND RETURNED THE AIRCRAFT TO SERVICE.
- [SDR CA100205001](https://openairdocs.org/sdr/CA100205001.md): Spring · broken · Feb 4, 2010 · Boeing 727231 · Rudder Control System
  > (CAN) ACFT YAWED ABRUPTLY TO THE LT ON TAKEOFF, RUDDER PEDALS FELT ABNORMALLY LOOSE, NO RESISTANCE/FRICTION. ACFT CONTINUED SHORT FLIGHT AND LANDED WITHOUT INCIDENT. MX FOUND INBD RUDDER CONTROL SPRING BROKEN. SPRING REPLACED. (TC 20100205001)
- [SDR PCSA2010012001](https://openairdocs.org/sdr/PCSA2010012001.md): Duct · cracked · Jan 19, 2010 · N905AJ · Boeing 727231 · Pneumatic Distribution System
  > CLIMBING THROUGH 9000FT THE NR 2 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED AND A 20 PSI SPLIT IN THE PRESSURE MANIFOLD. PERFORMED THE PROCEDURES, THE LIGHT EXTINGUISHED. OPERATED THE REMAINDER OF THE FLIGHT ON NR 2 BLEED. MAINTENANCE FOUND THE NR 3 ENGINE BLE
- [SDR PCSA2009110601](https://openairdocs.org/sdr/PCSA2009110601.md): Clamp · loose · Nov 6, 2009 · N905AJ · Boeing 727231 · Pneumatic Distribution System
  > DURING INITIAL CLIMB, ENGINE 3 STRUT OVERHEAT LIGHT ILLUMINATED. MAINTENANCE REPLACED THE AFT CLAMP ON 3 ENGINE BLEED AIR SHUTOFF VALVE. THE CLAMP WAS REPLACED AND LEAK CHECKED GOOD IN AN ENGINE OPERATIONAL CHECK.
- [SDR PCSA2009102101](https://openairdocs.org/sdr/PCSA2009102101.md): Clamp · loose · Oct 21, 2009 · N905AJ · Boeing 727231 · Pneumatic Distribution System
  > NUMBER 3 STRUT OVERHEAT LIGHT ILLUMINATED DURING CLIMBOUT. MAINTENANCE DISCOVERED A LOOSE CLAMP ON THE NUMBER 3 PRECOOLER. THE CLAMP WAS RETORQUED AND LEAK CHECKED GOOD IN AN ENGINE OPERATIONAL CHECK.
- [SDR PCSA2009072001](https://openairdocs.org/sdr/PCSA2009072001.md): Servo · malfunctioned · Jul 17, 2009 · N905AJ · Boeing 727231 · Autopilot Trim Servo
  > IN FLIGHT FROM SAP TO MIA "NOSE DOWN RUNAWAY TRIM" AND "JAM STABILIZER AFTER RUNAWAY TRIM". MAINTENANCE FOUND THE STABILIZER TRIM WHEEL MOVING IN THE SAME DIRECTION AT ALL TIMES REGARDLESS OF THE POSITION OF THE STABILIZER CRUISE TRIM SWITCH. THE AUTOPILOT S
- [SDR CA090416004](https://openairdocs.org/sdr/CA090416004.md): Manifold · chafed · Apr 8, 2009 · Boeing 727231 · Engine Fuel Distribution
  > (CAN) DURING MX RUN, FOUND SIGNIFIGANT FUEL LEAKING FROM NR 3 ENGINE "COLD STREAM" COWL. MX DETERMINED FUEL NOZZLE MANIFOLD CHAFED THROUGH ON HEAT SHROUD TO PRODUCE A PIN HOLE. MANIFOLD AND HEAT SHROUD REPLACED.
- [SDR PCSA2009021901](https://openairdocs.org/sdr/PCSA2009021901.md): Smoke Detector · false activation · Feb 19, 2009 · N905AJ · Boeing 727231 · Smoke Detection
  > LOWER CARGO FIRE DETECTION AMBER LIGHT ON IN FLIGHT (MX LIGHT). MAINTENANCE REPLACED AN AFT CARGO COMPARTMENT SMOKE DETECTOR.
- [SDR CA060119004](https://openairdocs.org/sdr/CA060119004.md): Actuator · frozen · Jan 17, 2006 · Boeing 727231 · Landing Gear Actuator
  > (CAN) ON APPROACH, NLG FAILED TO EXTEND NORMALLY. SUSPECT POSSIBLE FREEZING IN UPLOCK MECHANISM AND/OR BUNGEE LINK. MANUAL EXTENSION USED. NLG EXTENDED AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION BY MAINTENANCE SUSPECTED BUNGEE ACTUATOR FROZE
- [SDR CA060119003](https://openairdocs.org/sdr/CA060119003.md): Actuator · leaking · Jan 17, 2006 · Boeing 727231 · Landing Gear Actuator
  > (CAN) ON APPROACH, NLG FAILED TO EXTEND NORMALLY. SUSPECT POSSIBLE FREEZING IN UPLOCK MECHANISM AND/OR BUNGEE LINK. MANUAL EXTENSION USED, NLG EXTENDED AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION BY MAINTENANCE SUSPECTED ACTUATOR BYPASSING IN
- [SDR PCSA12140501](https://openairdocs.org/sdr/PCSA12140501.md): Door · open · Dec 14, 2005 · N905AJ · Boeing 727231 · Electrical/Electronic Compartment Doors
  > FLIGHT 8313 DEPARTED AND DURING CLIMB OUT CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE, CREW DUMPED FUEL AND RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LOWER 43 ELECTRONICS COMPARTMENT DOOR OPEN, ALSO THE COCKPIT DOOR WARNING INDICATION
- [SDR FX7A200500009](https://openairdocs.org/sdr/FX7A200500009.md): Line · leaking · Oct 15, 2005 · N54348 · Boeing 727231 · Hydraulic System, Main
  > AFTER TAKEOFF, DURING FLAP RETRACTION FROM 15 DEGREES TO 5 DEGREES LOST ALL OF THE SYSTEM A HYDRAULICS. TROUBLESHOT AND FOUND A FLEX LINE AT THE LEFT PCU ELEVATOR LEAKING, REMOVED AND REPLACED HYDRAULIC LINE, IAW MM REF 27-30-81, OP CHECK AND LEAK CHECK NORMA
- [SDR P9RA20050095](https://openairdocs.org/sdr/P9RA20050095.md): Flap System · out of adjust · Jul 18, 2005 · N54344 · Boeing 727231 · Trailing Edge Flap Control System
  > DURING DESCENT BACK INTO SFB, CREW NOTED VIBRATION IN AIRCRAFT ABOVE 270KIAS. LOW FREQUENCY VIBRATION. SUSPECT RIGHT FLAP AREA. MAINTENANCE ADJUSTED RIGHT INBD. FLAP IAW M/M. OPS CHECKED GOOD. NOTE. NO FURTHER VIBRATION NOTED AS OF 7/28/2005.
- [SDR P9RA20050091](https://openairdocs.org/sdr/P9RA20050091.md): Light · deteriorated · Jun 15, 2005 · N54344 · Boeing 727231 · Emergency Lighting
  > FLOOR TRACK LIGHTING IN FORWARD CABIN AREA DETERIORATED AND LOSING LIGHTING EFFECT. REMOVED AND REPLACED 12 LINEAR FEET OF FLOOR TRACK LIGHTING IAW SAFTGLO M/M.
- [SDR P9RA20050075](https://openairdocs.org/sdr/P9RA20050075.md): Window · cracked · Mar 26, 2005 · N54344 · Boeing 727231 · Passenger Compartment Windows
  > CRUISE FLT 270, ATL-SFB. F/A CALLED FORWARD AND ADVISED A PASSENGER CABIN WINDOW AT 18A HAD CRACKED. F/E RAISED CABIN DIFFERENTIAL TO 0 PSID. CREW REQUESTED NORMAL DESCENT TO 10,000 FEET. FLIGHT CONTINUED NORMALLY TO SFB. NO PRIORITY OR EMERGENCY HANDLING
- [SDR FX7A200500002](https://openairdocs.org/sdr/FX7A200500002.md): Indicator · inoperative · Feb 12, 2005 · N54348 · Boeing 727231 · Integrated Flight System
  > CAPTAINS ADI INOPERATIVE.
- [SDR FX7A200500001](https://openairdocs.org/sdr/FX7A200500001.md): Actuator · leaking · Feb 9, 2005 · N54348 · Boeing 727231 · Leading Edge Slat Actuator
  > DURING TAXI HYDRAULIC QUANTITY DROPS TO ZERO.
- [SDR C7WA200400063](https://openairdocs.org/sdr/C7WA200400063.md): Seal Plate · damaged · Oct 25, 2004 · N24343 · Boeing 727231 · Elevator Control System
  > LOSS OF SYSTEM A HYDRAULIC PRESSURE AND QUANITY IN FLIGHT. FOUND DAMAGED PLATE SEAL AT LT ELEVATOR POWER PACKAGE. REMOVED AND REPLACED SEAL PLATE.
- [SDR P9RA20040026](https://openairdocs.org/sdr/P9RA20040026.md): Gate · open · Jul 31, 2004 · N54344 · Boeing 727231 · Service Doors
  > UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKE OFF. FUEL DUMPED. NO EMERGENCY DECLARED. FOUND R1 DOOR PARTIALLY OPEN. PROPERLY SECURED DOOR AND GROUND PRESSURIZED THE AIRCRAFT. NO FURTHER DISCREPANCIES NOTED.NOTE. MAINTENANCE REPORTED GATE ASSEMBLY PARTIALLY
- [SDR C7WA200400016](https://openairdocs.org/sdr/C7WA200400016.md): Pump · exploded · May 10, 2004 · N54354 · Boeing 727231 · Hydraulic Pump (Electric/Engine), Main
  > NR 1 SYSTEM A-HYD PUMP LOW PRESSURE LIGHT ILLUMINATED, QUANTITY DECREASED TO 1.2 GALLONS. PERFORMED ASSOCIATED CHECK LIST. NR 2 ENGINE HYDRAULIC PUMP HAD A CATASTROPHIC FAILURE. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP. (M)
- [SDR C7WA200400006](https://openairdocs.org/sdr/C7WA200400006.md): Skin · corroded · Mar 9, 2004 · N54354 · Boeing 727231 · Fuselage Main, Plate/Skin
  > FOUND LOWER FUSELAGE SKIN CORRODED AT STRINGER 30 RT BETWEEN FS 1050 AND 1062. CUT OUT DAMAGE, SKIN REPAIRED IAW 727 SRM 53-30-3, FIG 3. (M)
- [SDR C7WA200400007](https://openairdocs.org/sdr/C7WA200400007.md): Skin · corroded · Mar 9, 2004 · N54354 · Boeing 727231 · Fuselage Main, Plate/Skin
  > FOUND LOWER FUSELAGE SKIN CORROSION AT STRINGER 28 RIGHT BETWEEN FS 1046 AND 1072, AFT EDGE OF EXISTING REPAIR. REMOVED EXISTING REPAIR. CUT OUT DAMAGE, SKIN REPAIRED IAW 727 SRM 53-30-3, FIG 3. (M)
- [SDR C7WA200400008](https://openairdocs.org/sdr/C7WA200400008.md): Frame · corroded · Mar 9, 2004 · N54354 · Boeing 727231 · Fuselage Main, Frame
  > FOUND LOWER FUSELAGE FRAME AND SKIN CORRODED FS 1140 STRINGER 29 RT. REMOVED CORROSION, SKIN CORROSION REMOVED WITHIN ALLOWABLE DAMAGE LIMITS PER 727 SRM 53-30-1 FIG 2. REPAIRED FRAME IAW 727 SRM 53-10-4 FIG 12. (M)
- [SDR P9RA20040002](https://openairdocs.org/sdr/P9RA20040002.md): Position Switch · dirty · Jan 15, 2004 · N54344 · Boeing 727231 · Landing Gear Position and Warning
  > RIGHT GEAR DOOR LIGHT ON FLIGHT ENGINEERS PANEL DOES NOT ILLUMINATE DURING GEAR RETRACTION OR EXTENSION. CLEANED RIGHT HAND GEAR DOOR POSITION SWITCH AND CHECKED SWITCH ADJUSTMENT. OPS CHECK OF DOOR INDICATION SYSTEM GOOD IAW MM 32-62-11.
- [SDR 2004F00250](https://openairdocs.org/sdr/2004F00250.md): Pin · backed out · Jan 5, 2004 · N54348 · Boeing 727231 · Landing Gear Steering System
  > LOSS OF STEERING DURING LINING UP FOR TAKEOFF RETURNED TO GATE. FOUND APEX PIN BACKED OUT OF STEERING KNUCKLE. INSTALLED APEX PIN AND OPS CHECK SYSTEM PER 32-51. INSPECTED AREA AND FOUND NO FURTHER DAMAGE A/C RETURNED TO SERVICE. (M)
- [SDR CA040104002](https://openairdocs.org/sdr/CA040104002.md): Flange · cracked · Jan 1, 2004 · Boeing 727231 · Accessory Gearboxes
  > (CAN) SCHEDULED MAINTENANCE WAS CARRIED OUT TO REPLACE THE FCU/FUEL PUMP QUAD RING. THE RUN OUT TORQUE INSPECTION WAS CARRIED OUT AND THE CLEARANCE FAILED. DISASSEMBLY OF THE AREA DETERMINED THAT THE QUAD RING NUT ATTACHMENT FLANGE WAS CRACKED. THE UNSERVICEA
- [SDR 2003F00604](https://openairdocs.org/sdr/2003F00604.md): Skid · malfunctioned · Aug 10, 2003 · N64346 · Boeing 727231 · Nose/Tail Landing Gear
  > AFTER TAKEOFF WITH THE LANDING GEAR RETRACTED THE TAIL SKID REMAINED EXTENDED, RETURNED TO MIAMI DUMPED 15000 LBS OF FUEL AND LANDED WITHOUT INCIDENT. CHECKED TAIL SKIN OPERATION AFTER CHECKING AREA AROUND TAIL SKIN FOR OBSTRUCTION PER MM 32-30-0 AND 32-00-11
- [SDR CA030627008](https://openairdocs.org/sdr/CA030627008.md): Connector · shorted · Jun 18, 2003 · Boeing 727231 · Engine Starting System Wiring
  > (CAN) ON DESCENT THROUGH 3,000 FT, IT WAS OBSERVED THAT THE NR 2 ENGINE START VALVE OPEN LIGHT WAS FLICKERING AND THEN REMAINED STEADY. NR 2 ENGINE IN FLT SHUTDOWN WAS CARRIED OUT AND AIRCRAFT LANDED WITHOUT INCIDENT. DURING INVESTIGATION, IT WAS OBSERVED
- [SDR HOC2003F00013](https://openairdocs.org/sdr/HOC2003F00013.md): Floorbeam · corroded · Apr 29, 2003 · N54348 · Boeing 727231 · Fuselage Main, Floor Beam
  > DURING A (C) CHECK CORROSION WAS NOTED ON LOWER FLANGE. COMMON TO FLOORBEAM STRAP AND INTERCOSTAL. STA 1130, LBL24.
- [SDR HOC2003F00010](https://openairdocs.org/sdr/HOC2003F00010.md): Support Bracket · corroded · Apr 28, 2003 · N54348 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING A (C) CHECK CORROSION WAS NOTED ON LEFT, OUTBOARD DITCHING PAN SUPPORT BRACKET. STA 1176-1183.
- [SDR HOC2003F00003](https://openairdocs.org/sdr/HOC2003F00003.md): Floorbeam · corroded · Apr 25, 2003 · N54348 · Boeing 727231 · Fuselage Main, Floor Beam
  > DURING A (C) CHECK CORROSION WAS NOTED ON FLOORBEAM TOP SURFACE STA 440, 12 LBL-12 RBL.
- [SDR HOC2003F00002](https://openairdocs.org/sdr/HOC2003F00002.md): Intercostal · corroded · Apr 25, 2003 · N54348 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING A (C) CHECK CORROSION WAS NOTED ON OUTBOARD LWR INTERCOSTAL, STA 1070-STGR30, RBL 2.0.
- [SDR HOC2003F00005](https://openairdocs.org/sdr/HOC2003F00005.md): Splice · corroded · Apr 20, 2003 · N54348 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING A (C) CHECK CORROSION WAS NOTED ON TENSION TIE FITTING AND SPLICE ANGLE AT STA 1183, STR 17R.

Next page: https://openairdocs.org/model/boeing-727-231/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 = '727231'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-231/reports

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