# Service difficulty reports: Boeing 727-223

A list on [Boeing 727-223](https://openairdocs.org/model/boeing-727-223.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 107 · 5,313 reports

- [SDR Y2PA2024042324011](https://openairdocs.org/sdr/Y2PA2024042324011.md): Rib · cracked · Apr 23, 2024 · N727US · Boeing 727223 · Wing, Rib/Bulkhead
  > WHILE AT C- CHECK IN KBQK, DURING A HFEC INSPECTION OF THE RH RIB CHORD AT STATION BL 70.5 PER AD 14-04-09 S/B 57-0112 R5,A CRACK WAS FOUND IN HOLE MARKED ON THE RH SIDE AT STATION BL 70.5. STOP DRILLED CRACK, PERFORMED A HFEC INSPECTION OF ALL EXISTING HOL
- [SDR Y2PA2024042324010](https://openairdocs.org/sdr/Y2PA2024042324010.md): Beam · corroded · Apr 23, 2024 · N727US · Boeing 727223 · Horizontal Stabilizer Structure
  > WHILE AT C-CHECK IN KBQK, FOUND THE LT HORIZONTAL STABILIZER, UPPER SURFACE, OUTBOARD TRAILING EDGE BEAM TO BE CORRODED ABOVE THE #6 ELEVATOR HINGE. CUT OUT THE DAMAGED SECTION OF THE LH BEAM BETWEEN STATIONS 136.50-173.21, THEY FABRICATED A NEW BEAM SECTI
- [SDR Y2PA2023060523029](https://openairdocs.org/sdr/Y2PA2023060523029.md): Keelbeam · corroded · Jun 5, 2023 · N726US · Boeing 727223 · Fuselage Main, Keel
  > DISCREPANCY: DURING C-CHECK AT BQK, STAMBAUGH AVIATION FOUND CORROSION ON THE LH KEEL BEAM IN THE AFT LOWER CARGO PIT BETWEEN FUSELAGE STATIONS 950-1010.CORRECTIVE ACTION: STAMBAUGH AVIATION IN BQK, REMOVED AND REPLACED THE LH KEEL BEAM BETWEEN STATIONS 950-1
- [SDR Y2PA2021030121015](https://openairdocs.org/sdr/Y2PA2021030121015.md): Frame · damaged · Mar 1, 2021 · N727US · Boeing 727223 · Fuselage Main, Frame
  > DISCREPANCY WHILE AT C-CHECK AT COMMERCIAL JET IN KDHN THE FOLLOWING DAMAGE WAS FOUND AT STATION 783 WL 213RBL AND LBL63 HAVE PILOT HOLES WITH NO PITCH FROM EXISTING HOLES, CHAFE DAMAGE AND A DRILL STRIKE ON THE INBOARD FREE FLANGE OF THE FRAME. CORRECTIVE AC
- [SDR Y2PA2020102920032](https://openairdocs.org/sdr/Y2PA2020102920032.md): Engine · fod · Oct 28, 2020 · N727US · Boeing 727223 · Engine (Turbine/Turboprop)
  > DISCREPANCY: CREW REPORTED THAT AFTER DEPARTURE FROM KLRD AND CLIMBING THROUGH 10000 FEET, THE NR 3 ENGINE FAILED WITH ASSOCIATED VIBRATIONS. THEY DECLARED AN EMERGENCY AND PERFORMED THE ENGINE FIRE, SEVERE DAMAGE OR SEPARATION CHECKLIST AND LANDED AT THE DEP
- [SDR Y2PA2020030920007](https://openairdocs.org/sdr/Y2PA2020030920007.md): Angle · cracked · Mar 9, 2020 · N727US · Boeing 727223 · Fuselage Main, Frame
  > DISCREPANCY: DURING MAINTENANCE INSPECTION PER AEI SUPPLEMENT SID# 50-601 REV F, TASK AEI-FC-5-3, A CRACK WAS FOUND ON FAILSAFE ANGLE OF THE FRAME LOCATED AT STA. 480. THE CRACK STARTED ON THE FASTENER THAT ATTACH THE ANGLE TO FRAME S-17L. CORRECTIVE ACTION: U
- [SDR Y2PA2019041800020](https://openairdocs.org/sdr/Y2PA2019041800020.md): Skin · corroded · Apr 18, 2019 · N726US · Boeing 727223 · Horizontal Stabilizer, Plate/Skin
  > DURING ROUTINE MAINTENANCE AT KYIP CORROSION WAS FOUND ON R/H HORIZONTAL STAB TRAILING EDGE BEAM AT STATIONS 88.9, 166.5, AND 182.1. REPAIR STATION FABRICATED AND INSTALLED 3 EACH REPAIR STRAPS IAW FVCI, REPAIR DWG. 55-19103-1, -2, AND -3. AND 8110-3’S 1910
- [SDR I5PA2019030800000](https://openairdocs.org/sdr/I5PA2019030800000.md): Smoke Detector · activated · Mar 8, 2019 · N705AA · Boeing 727223 · Smoke Detection
  > MAIN CARGO SMOKE DETECTOR GOES ON IN FLIGHT.
- [SDR 7IWB20190302001](https://openairdocs.org/sdr/7IWB20190302001.md): Not Reported · leaking · Mar 2, 2019 · N209TR · Boeing 727223 · Pneumatic Distribution System
  > AFTER TAKEOFF AND DURING CLIMBOUT FROM KMFE, THE FLIGHT CREW EXPERIENCED A NR 1 ENGINE FIRE WARNING. THEY PULLED THE THROTTLE BACK TO IDLE AND THE WARNING WENT OUT. THEY DUMPED APPROX 5,000 OF FUEL AND LANDED SAFELY BACK AT KMFE. TROUBLESHOOTING ON 3/3/2019 RE
- [SDR 7IWB20181221002](https://openairdocs.org/sdr/7IWB20181221002.md): Fire Warning · illuminated · Dec 21, 2018 · N209TR · Boeing 727223 · Fire Detection
  > DURING CLIMB OUT OF KELP, #1 ENGINE FIRE WARNING WENT OFF WITH A SPIKE IN OIL TEMP AND PRESSURE. THE A/C DID AN AIR TURN-BACK AND LANDED SAFELY BACK IN KELP. TO DATE, THERE'S NO CLEAR FAULT FOR WHAT CAUSED THE PROBLEM AND THE AIRCRAFT REMAINS IN KELP.
- [SDR 7IWB2018122018001](https://openairdocs.org/sdr/7IWB2018122018001.md): Fan · damaged · Nov 24, 2018 · N209TR · Boeing 727223 · Engine (Turbine/Turboprop)
  > DURING A ROUTINE SERVICE CHECK, IJW MX FOUND FOD DAMAGE TO THE #1 ENGINE FAN.
- [SDR I5PA2018110470501](https://openairdocs.org/sdr/I5PA2018110470501.md): Smoke Detector · unserviceable · Nov 4, 2018 · N705AA · Boeing 727223 · Smoke Detection
  > MAIN CARGO FIRE LIGHT AND BELL CAME ON IN FLIGHT. REPLACED FAULTY SMOKE DETECTOR UNIT.
- [SDR Y2PA201809250033](https://openairdocs.org/sdr/Y2PA201809250033.md): Channel · corroded · Sep 25, 2018 · N727US · Boeing 727223 · Fuselage Miscellaneous Structure
  > DISCREPANCY: DURING INSPECTION AT KYIP MAINTENANCE FOUND PRESSURE SEAL ZEE CHANNEL CORRODED AT STA 870, LBL 43. CORRECTIVE ACTION: AIRCRAFT FERRIED TO KSFB FOR REPAIR. MAINTENANCE AT KSFB REMOVED AND REPLACED CORRODED ZEE CHANNEL WITH NEW I/A/W B727 SRM 51-1
- [SDR Y2PA2018092200029](https://openairdocs.org/sdr/Y2PA2018092200029.md): Bearing · failed · Sep 22, 2018 · N726US · Boeing 727223 · Turbine Engine Compressor Section
  > CREW REPORTED – EXPERIENCED SEVERAL ABNORMAL AIRCRAFT VIBRATIONS. DISCUSSED WITH CREW. DECLARED AN EMERGENCY. LANDED AT NEAREST SUITABLE AIRPORT USING NORMAL PROCEDURES. USA JET MAINTENANCE WAS SENT TO KAFW TO TROUBLESHOOT PROBLEM. UPON INSPECTION OF THE #
- [SDR Y2PA2018052200019](https://openairdocs.org/sdr/Y2PA2018052200019.md): Spring · failed · May 20, 2018 · N727US · Boeing 727223 · Cabin Pressure Control System
  > CREW REPORTED DURING CRUISE, AT FL200, CABIN PRESSURE BEGAN TO INCREASE RAPIDLY. CABIN ALTITUDE WARNING HORN SOUNDED. RECALL ACTION ITEMS COMPLETED, AND EMERGENCY PROCEDURES CHECKLIST FOLLOWED. EMERGENCY DECLARED AND RAPID DESCENT TO 10,000 FEET COMPLETED.
- [SDR I5PA2017121170501](https://openairdocs.org/sdr/I5PA2017121170501.md): Indicator · inoperative · Dec 10, 2017 · N705AA · Boeing 727223 · Airspeed/Mach Indicator
  > DISCREPANCY: F/O AIRSPEED INDICATOR INOP. CORRECTIVE ACTION: FOUND FOREIGN OBJECT IN AUXILIARY AND F/O PITOT PROBE. FLUSHED PER AMM 34-11-00. OPS CHECK GOOD
- [SDR AALA20170421007](https://openairdocs.org/sdr/AALA20170421007.md): Battery Pack · no test · Apr 21, 2017 · N185AN · Boeing 727223 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS BETWEEN BS 700 AND 720 WERE DIM. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD.
- [SDR AALA201704079019](https://openairdocs.org/sdr/AALA201704079019.md): Light · not seated · Apr 5, 2017 · N183AN · Boeing 727223 · Emergency Lighting
  > SEAT MOUNTED EMERGENCY LIGHT AT SEAT 35D IS INOPERATIVE. SEATED THE LIGHT ASSEMBLY IAW AMM 33-51-11. OPERATIONAL CHECKED GOOD.
- [SDR AALA20170405006](https://openairdocs.org/sdr/AALA20170405006.md): Fitting · corroded · Apr 4, 2017 · N173AN · Boeing 727223 · Fuselage Main, Attach Fittings
  > AFT GALLEY FLOOR BEAM MOUNT FITTING CORRODED AT BS 1687, RBL 52. REMOVED AND REPLACED THE FITTING ASSEMBLY IAW SRM 51-40-02.
- [SDR FOTR20160817001](https://openairdocs.org/sdr/FOTR20160817001.md): Skin · gouged · Aug 17, 2016 · N209TR · Boeing 727223 · Leading Edge Devices
  > TRAILING EDGE FLAP SKIN GOUGED WBL 95 RIGHT SIDE.
- [SDR FOTR20160813001](https://openairdocs.org/sdr/FOTR20160813001.md): Skin · corroded · Aug 13, 2016 · N209TR · Boeing 727223 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN AT BS 328 STRINGER 19R JUST AFT OF FWD LAV SERVICE PANEL.
- [SDR FOTR20160812001](https://openairdocs.org/sdr/FOTR20160812001.md): Panel · corroded · Aug 12, 2016 · N209TR · Boeing 727223 · Rudder Miscellaneous Structure
  > LOWER RUDDER LT SIDE HAS A SPOT OF CORROSION 2.5" IN LENGHT.
- [SDR FOTR20160802078](https://openairdocs.org/sdr/FOTR20160802078.md): Structure · gouged · Aug 2, 2016 · N209TR · Boeing 727223 · Trailing Edge Flaps
  > RT WING INBD FOREFLAP INBD END GOUGED. REPAIRED IAW FAS NR 85781 W/O N209TR-02-01.
- [SDR FOTR20160801077](https://openairdocs.org/sdr/FOTR20160801077.md): Skin · delaminated · Aug 1, 2016 · N209TR · Boeing 727223 · Ailerons
  > RIGHT WING T/E O/B AILERON UPPER SURFACE O/B SIDE T/E DELAMINATED. REPAIRED IAW FAS NR 85831 W/O N209TR-02-01.
- [SDR FOTR20160728001](https://openairdocs.org/sdr/FOTR20160728001.md): Skin · gouged · Jul 28, 2016 · N209TR · Boeing 727223 · Trailing Edge Flaps
  > RIGHT WING O/B FORE FLAP O/B END HAS SEVERAL GOUGES ON LEADING EDGE.
- [SDR FOTR20160727002](https://openairdocs.org/sdr/FOTR20160727002.md): Stiffener · cracked · Jul 27, 2016 · N209TR · Boeing 727223 · Elevator, Spar/Rib
  > PERFORMED DVI INSPECTION OF LT AND RT ELEVATOR REAR SPARS AND FOUND TWO STIFFENERS CRACKED AT ELEVATOR STATION 63.3
- [SDR FOTR20160727001](https://openairdocs.org/sdr/FOTR20160727001.md): Stiffener · corroded · Jul 27, 2016 · N209TR · Boeing 727223 · Wing Miscellaneous Structure
  > RIGHT WING FIXED T/E STA WBL 92.8 STIFFENER LOWER END IS COORODED.
- [SDR FOTR20160723001](https://openairdocs.org/sdr/FOTR20160723001.md): Skin · corroded · Jul 23, 2016 · N209TR · Boeing 727223 · Fuselage Main, Plate/Skin
  > NR 1 ATC ANTENNA MOUNT ON THE LOWER FUSELAGE SKIN HAS CORROSION ALONG THE MATING SURFACE OF SKIN.
- [SDR FOTR20160714001](https://openairdocs.org/sdr/FOTR20160714001.md): Structure · cracked · Jul 14, 2016 · N209TR · Boeing 727223 · Leading Edge Devices
  > LEFT WING NR 4 SLAT AFT SIDE, LIGHTING HOLE HAS A CRACK ALONG THE BOTTOM EDGE, CRACK LENGTH IS 1/8".
- [SDR 7IWB2016020800003](https://openairdocs.org/sdr/7IWB2016020800003.md): Pressure Switch · failed · Dec 20, 2015 · N209TR · Boeing 727223 · Engine Oil Indicating System
  > DURING A RECENT FLIGHT, AT A POINT APPROXIMATELY 100 NM SW OF DESTINATION AND AT AN ALTITUDE OF 28,000 FT, THE NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. THE CREW REDUCED THRUST TO ABOUT 70 PERCENT N1 AND THE LIGHT BENT OUT. THE NR 2 OIL FILTER BYPASS
- [SDR 2015FA0000458](https://openairdocs.org/sdr/2015FA0000458.md): Unknown · multiple fail · Sep 20, 2015 · N209TR · Boeing 727223 · Navigation System
  > SHORTLY AFTER TAKEOFF, ACFT EXPERIENCED A LOSS OF CAPTAIN'S AIRSPEED INDICATOR, ALTIMETER, IVSI, TAWS, NR 1 TRANSPONDER FOLLOWED BY A CARGO SMOKE DETECTOR ILLUMINATION, FOLLOWED BY RT AFT NR 2 FUEL BOOST PUMP CIRCUIT BREAKER POPPED FOLLOWED BY BOTH CAPTAIN'S A
- [SDR Y2PA2015051400025](https://openairdocs.org/sdr/Y2PA2015051400025.md): Floorbeam · corroded · May 13, 2015 · N727US · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING C-CHECK DISCOVERED CORROSION ON THE FLOORBEAM AT STATION 1030, RBL55 LOWER SURFACE UNDER TOP CAP. COMPLETED FLOORBEAM REPAIR AT STATION 1030, RBL 50-55 IAW SRM 53-10-8 FIGURE 3 PAGES 18 - 23.
- [SDR Y2PA2015051400024](https://openairdocs.org/sdr/Y2PA2015051400024.md): Fitting · corroded · May 13, 2015 · N727US · Boeing 727223 · Wing, Attach Fittings
  > DURING C-CHECK DISCOVERED CORROSION ON THE LT AFT BOTTLE PIN FITTING & BUSHING. COMPLETED REPAIR OF LT AFT BOTTLE PIN FITTING BY INCREASING THE COUNTER BORE & REPLACING THE BUSHING IAW SERVICE BULLETIN 727-57-0175 R3 PAGE 20 PART III STEP “E” FIGURE 9.
- [SDR Y2PA2015051400023](https://openairdocs.org/sdr/Y2PA2015051400023.md): Skin Panel · corroded · May 13, 2015 · N727US · Boeing 727223 · Wing, Plate/Skin
  > DURING C-CHECK DISCOVERED CORROSION ON THE RT UPPER SURFACE SKIN OF WING AT WING STATION 727.5 TOWARD THE LE. CORROSION REMOVED ON UPPER SURFACE OF RT WING WITHIN LIMITS IAW SRM 57-30-01 PAGE 2 FIGURE 1 SHEET 2. INSTALLED REPAIR DOUBLER IAW SRM 51-10-2 & DWG
- [SDR Y2PA2015051400022](https://openairdocs.org/sdr/Y2PA2015051400022.md): Skin · cracked · May 13, 2015 · N727US · Boeing 727223 · Fuselage Main, Plate/Skin
  > DURING C-CHECK DISCOVERED A CRACK ON THE BELLY SKIN & A CORRODED FLOORBEAM AT STATION 729. REPAIRED CORRODED FLOORBEAM & BELLY SKIN IAW SRM 53-30-3 FIGURE 6 SHEET 1 53-30-3 FIGURE 3 SHEET 4 & 51-30-2 PAGE 2-3 PARAGRAPH 4.
- [SDR CA150505007](https://openairdocs.org/sdr/CA150505007.md): Cable · broken · Apr 22, 2015 · Boeing 727223 · Trailing Edge Flap Control System
  > (CAN) BOTH MID FLAP EXTENSION CABLES,, WERE FOUND BROKEN DURING A DAILY INSPECTION WHEN THE FLAPS WOULD NOT RETRACT. BOTH CABLES WERE REPLACED AND FLAPS WERE CYCLED REPEATEDLY WITH NO FURTHER PROBLEM. ACFT WAS RETURNED TO SERVICE.
- [SDR R34R2015040220150](https://openairdocs.org/sdr/R34R2015040220150.md): Garlock Seal · leaking · Mar 26, 2015 · N289MT · Boeing 727223 · Turbine Engine Oil System
  > THE ACFT WAS BEING FLOWN ON A POST-MAINTENACE ACCEPTANCE CHECK FLIGHT. SHORTLY AFTER TAKEOFF, THE FLIGHT ENGINEER NOTED A NOTICABLE DROP IN THE OIL QUANITY ON THE NR1 ENGINE. THE OIL QUANITY WAS BELOW 2 QUARTS. 15 MINUTES AFTER LEVEL OFF OIL QUANITY DROPPED T
- [SDR CA150114008](https://openairdocs.org/sdr/CA150114008.md): Duct · ruptured · Jan 13, 2015 · Boeing 727223 · Pneumatic Distribution System
  > (CAN) DURING CLIMB OUT NR 3 ENGINE FIRE INDICATION APPEARED, AFTER FOLLOWING CHECKLIST PROCEDURE NR 3 ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO EWR AIRPORT. FIRE INDICATION WENT AWAY AS THROTTLE WAS RETARDED TO IDLE AS PART OF ENGINE SHUT-DOWN PROCEDURE. M
- [SDR CA141104012](https://openairdocs.org/sdr/CA141104012.md): Wire · failed · Oct 31, 2014 · Boeing 727223 · Powerplant System Wiring
  > (CAN) NR 3 ENGINE OIL TEMP INDICATION PEGGED PAST RED BAND. SUPPLEMENTAL CHECK LIST COMPLIED WITH AND ENGINE SHUTDOWN. MAINTENANCE INSPECTED ENGINE AND ISOLATED FAULT TO GROUND WIRE ON NR 3 ENGINE. GROUND WIRE INSTALLED IAW SWPM 20-10-13. ACFT RETURNED TO S
- [SDR CA140627004](https://openairdocs.org/sdr/CA140627004.md): Line · burst · Jun 24, 2014 · Boeing 727223 · Hydraulic System, Main
  > (CAN) CREW REPORTED UPON GEAR RETRACTION AFTER TAKEOFF THEY HAD A SYSTEM A HYDRAULIC FAILURE. MAINTENANCE FOUND THE RT MAIN GEAR ACTUATOR "UP" LINE BURST APPROXIMATELY 1" FROM B-NUT FITTING. LINE REPLACED.
- [SDR CA140225024](https://openairdocs.org/sdr/CA140225024.md): Rod · sheared · Feb 6, 2014 · Boeing 727223 · Nose/Tail Landing Gear
  > (CAN) NLG SAFETY SWITCH PUSH/PULL TUBE FOUND SHEARED WHILE PREPARING ACFT FOR DEPARTURE. ROD ASSY REPLACED AND SAFETY SWITCH TESTED IAW 32-09-22.
- [SDR CA140113003](https://openairdocs.org/sdr/CA140113003.md): Coupling · failed · Jan 6, 2014 · Boeing 727223 · Pneumatic Distribution System
  > (CAN) AFTER TAKEOFF, ON CLIMB-OUT, THE FLIGHT CREW RECEIVED A NR 1 STRUT OVERHEAT INDICATION. THE ACFT RETURNED TO THE DEPARTURE AIRPORT FOR AN UNEVENTFUL, UNSCHEDULED LANDING. UPON INSPECTION BY MAINTENANCE, A DUCT LEAK WAS FOUND AT THE NR 1 ENGINE STRUT HEA
- [SDR C8GA20120427006](https://openairdocs.org/sdr/C8GA20120427006.md): Actuator · damaged · Apr 24, 2012 · N713AA · Boeing 727223 · Air Distribution System
  > RT RAM AIR DOOR AND LOWER ACTUATOR ROD MISSING ON POST FLIGHT INSPECTION. NO DAMAGE TO FUSELAGE NOTED. R & R RIGHT RAM AIR DOOR ACTUATOR, INSTALLED RAM AIR DOOR OPS CHECKED GOOD.
- [SDR C8GA20120208003](https://openairdocs.org/sdr/C8GA20120208003.md): Gyro · inaccurate · Feb 8, 2012 · N715AA · Boeing 727223 · Attitude Gyro and Indicating System
  > DURING CRUISE, BOTH CAPTAIN'S AND FIRST OFFICER'S ADI SHOWED A 10 DEGREE LT TURN. AN EMERGENCY WAS DECLARED AND THE ACFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. R & R THE NR 1 AND NR 2 GYRO, PERFORM OPERATION CHECKS WITH NO DEFECTS.
- [SDR C8GA2011000028](https://openairdocs.org/sdr/C8GA2011000028.md): Proximity Switch · faulted · Dec 8, 2011 · N708AA · Boeing 727223 · Landing Gear Position and Warning
  > DURING CLIMB, ON GEAR RETRACTION THE RED NOSE GEAR LIGHT REMAINED ILLUMINATED. THE GEAR LEVER WAS CYCLED TO THE OFF POSITION, RED NOSE LIGHT REMAINED ILLUMINATED WITH THE GREEN NOSE GEAR DOWN LOCK LIGHT ILLUMINATED. THE ACFT RETURNED TO DEPARTURE AND LANDED WI
- [SDR C8GA2011000027](https://openairdocs.org/sdr/C8GA2011000027.md): Warning Horn · false activation · Nov 18, 2011 · N715AA · Boeing 727223 · Stall Warning System
  > DURING TAKEOFF ROLL AT APPROX 60 KNOTS THE TAKEOFF WARNING HORN SOUNDED. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED AND OPS CHECK OF THE TAKEOFF WARNING SYS WAS CONDUCTED NOTING NO DEFECT
- [SDR C8GA201111150025](https://openairdocs.org/sdr/C8GA201111150025.md): Transceiver · failed · Nov 15, 2011 · N708AA · Boeing 727223 · Weather Radar System
  > DURING CRUISE, THE WEATHER RADAR SCREEN WENT BLANK. THE ACFT RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED NOTING THAT THE RADAR TRANSCEIVER TO BE AT FAULT. R & R THE RADAR TRANSCEIVER AND PERFORMED OPS CHECKS WITHOUT DE
- [SDR C8GA2011000020](https://openairdocs.org/sdr/C8GA2011000020.md): Actuator · sticking · Sep 9, 2011 · N715AA · Boeing 727223 · Leading Edge Slat Position Indicating System
  > AFTER TAKEOFF AND DURING CLIMB, THE NR 8 L/E SLAT IN TRANSIT LIGHT STAYED ON DURING FLAP RETRACTION AND ACFT ROLLED TO THE LT. THE ACFT RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED, R & R THE NR 8 L/E ACTUATOR AND PER
- [SDR C8GA2011000018](https://openairdocs.org/sdr/C8GA2011000018.md): Relief Valve · leaking · Aug 19, 2011 · N715AA · Boeing 727223 · Rudder Control System
  > WHILE EN-ROUTE, THE CREW NOTED THAT THE B-SYSTEM HYD QUANTITY WAS DECREASING AND THE LOW LIGHT ILLUMINATED. ACFT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED, NOTING THAT THE UPPER RUDDER LOAD LIMIT RELIEF VALUE WAS
- [SDR FOTR2111712809](https://openairdocs.org/sdr/FOTR2111712809.md): Skin · debonded · Aug 1, 2011 · N899AA · Boeing 727223 · Trailing Edge Flaps
  > LT INBD FOREFLAP T/E HAS AREA OF DEBONDED JUST INBD OF PREVIOUS REPAIR WBL 135.0. REPAIRED ON FASI WO 21117, NR 12809.

Next page: https://openairdocs.org/model/boeing-727-223/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 = '727223'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-223/reports

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