# Service difficulty reports: Boeing 727-227

A list on [Boeing 727-227](https://openairdocs.org/model/boeing-727-227.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 102 · 5,082 reports

- [SDR 2026FA0000477](https://openairdocs.org/sdr/2026FA0000477.md): Generator · failed · Jun 5, 2026 · Boeing 727227 · AC Generator-Alternator
  > IN V1 IF PRESENT LOSS OF ALL GENERATOR WAS PERFORMED EMERGENCY CHECK LIST WITH UNSATISFACTORY STATE. COME BACK AIRPORT OF BOGOTÁ. ACCOMPLISHED CHECKOUT ANALYSIS OF ELECTRICAL GENERATOR SYSTEM IAW 727 AMM 24-20-00 / 101-113. FOREIGN REGISTRATION: HK-5216
- [SDR FXGA07312024001](https://openairdocs.org/sdr/FXGA07312024001.md): Hose · leaking · Jul 27, 2024 · N794AJ · Boeing 727227 · Hydraulic System, Main
  > ON DESCENT "A" SYSTEM HYDRAULIC QUANTITY FLUID STARTED DECREASING. FOUND LEAK FROM HOSE FITTING ON #2 SPOILER ACTUATOR. REPLACED ORING ON FITTING
- [SDR FXGA2022121400512](https://openairdocs.org/sdr/FXGA2022121400512.md): Battery · discharged · Dec 12, 2022 · N794AJ · Boeing 727227 · Smoke Detection
  > CREW RECEIVED A LOWER AFT CARGO FIRE WARNING AT FL360 ON ARRIVAL INTO EFD. CREW IMMEDIATELY INITIATED THE EMERGENCY PROCEDURE AND BEGAN AN EMERGENCY DECENT AND DIVERTED TO CWF, WHICH WAS JUST SOUTH OF POSITION. THE FIRE CREW SWEPT AIRCRAFT UPON LANDING AND NO
- [SDR FXGA20211129001](https://openairdocs.org/sdr/FXGA20211129001.md): Duct · cracked · Nov 27, 2021 · N794AJ · Boeing 727227 · Engine Bleed Air System
  > ON CLIMB APPROXIMATELY 1500' #3 ENGINE HAD FIRE WARNING. ACCOMPLISHED CHECKLIST. LIGHT EXTINGUISHED DID NOT FIRE BOTTLE. RETURNED TO KFLL. ON VISUAL INSPECTION OF ENGINE IT WAS FOUND THAT THE BLEED AIR DUCT HAD RUPTURED/CRACKED.
- [SDR FXGA202103182103](https://openairdocs.org/sdr/FXGA202103182103.md): Stiffener · cracked · Mar 18, 2021 · N794AJ · Boeing 727227 · Wing Miscellaneous Structure
  > L/H WING FRONT SPAR VERTICAL STIFFENER CRACKED AT W/STA 255L. TO REPLACE A CRACKED VERTICAL STIFFENER ON THE LEFT WING FRONT SPAR WEB AT W/STA 254. REPLACE VERTICAL STIFFENER PER EA 20-2021-008. OBTAIN DTA WITHIN 12 MONTHS.
- [SDR FXGA202103182110](https://openairdocs.org/sdr/FXGA202103182110.md): Skin · corroded · Mar 18, 2021 · N794AJ · Boeing 727227 · Elevator, Plate/Skin
  > CORROSION ON L/H ELEVATOR OUTBOARD TRAILING EDGE. TO REPAIR CORRODED ELEVATOR SKIN AT THE TRAILING EDGE IN THE STATIC WICKS AREA. PERFORM REPAIR OF ELEVATOR TRAILING EDGE PER STS ENGINEERING AUTHORIZATION 80-2021-016 AND 80-2021-015. OBTAIN DTA WITHIN 12 MONT
- [SDR FXGA202103042114](https://openairdocs.org/sdr/FXGA202103042114.md): Web · damaged · Mar 4, 2021 · N794AJ · Boeing 727227 · Ailerons
  > DAMAGE WEB AT L/H AILERON TAB HINGE ASSEMBLY. TO PREFORM SPLICE ON A DAMAGED WEB SUPPORTING THE L/H OUTBOARD AILERON TRIM ROD HINGE ASSEMBLY.REMOVE AILERON TRIM ROD HINGE ASSEMBLY. REPAIRE DAMAGE WEB PER B727 SRM 51-40-02 TYPICAL WEB REPAIR. INSTALL AILERON TR
- [SDR FXGA202102022111](https://openairdocs.org/sdr/FXGA202102022111.md): Skin · delaminated · Feb 2, 2021 · N794AJ · Boeing 727227 · Ailerons
  > DELAM ON LH AILERON COMPOSITE TRAILING EDGE. TO REPAIR DELAMINATION ON AILERON TRAILING EDGE. REPAIR AILERON TRAILING EDGE PER B727 SRM 51-40-20 GENERAL REPAIR - ALUMINUM HONEYCOMB REPAIRS - 250 DEGREE FAHRENHEIT (121 DEGREE CELSIUS) CURE.
- [SDR FXGA202102012109](https://openairdocs.org/sdr/FXGA202102012109.md): Stringer · corroded · Feb 1, 2021 · N794AJ · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CORRODED FUSELAGE STRINGER AT F/STA 443, STRINGER 11R. TO REPAIR A CORRODED FUSELAGE STRINGER AT F/STA 443, 11 RIGHT. CUT OUT DAMAGED AREA AND PERFORM REPAIR PER DC-6A&B OVERHAUL MANUAL FIGURE 12-2.
- [SDR FXGA202101062102](https://openairdocs.org/sdr/FXGA202101062102.md): Hinge Fitting · corroded · Jan 6, 2021 · N794AJ · Boeing 727227 · Leading Edge Devices
  > OUTBOARD HINGE FITTING CORRODED FOR L/H WING #2 LEADING EDGE FLAP AT W/STA 269L. TO REMOVE AND REPLACE A CORRODED FITTING ON #2 LEADING EDGE FLAP (W/STA 269L). REMOVED CORRODED FITTING. MANUFACTURE NEW FITTING PER DRAWINGS NUMBER 65-16271 AND BAC1508-128. INST
- [SDR FXGA202101062101](https://openairdocs.org/sdr/FXGA202101062101.md): Hinge Fitting · corroded · Jan 6, 2021 · N794AJ · Boeing 727227 · Leading Edge Slat Control System
  > CORRODED HINGE FITTING FOR L/H WING #1 LEADING EDGE FLAP AT W/STA 283L. TO REMOVE AND REPLACE A CORRODED FITTING ON #1 LEADING EDGE FLAP (W/STA 283L). REMOVE CORRODED FITTING. MANUFACTURE NEW FITTING PER DRAWINGS NUMBER 65-16273 AND BAC 1508-128. INSTALL NEW F
- [SDR FXGA202101062106](https://openairdocs.org/sdr/FXGA202101062106.md): Stringer Clip · corroded · Jan 6, 2021 · N794AJ · Boeing 727227 · Fuselage Main, Attach Fittings
  > CORRODED CLIP AT STRINGER 19L, F/STA 1186 BULKHEAD. TO REPLACE A CORRODED CLIP AT FUSELAGE STRINGER 19L, F/STA 1186. REMOVE AND REPLACE CORRODED STRINGER CLIP.
- [SDR FXGA202101062104](https://openairdocs.org/sdr/FXGA202101062104.md): Stringer Clip · corroded · Jan 6, 2021 · N794AJ · Boeing 727227 · Fuselage Main, Attach Fittings
  > CORRODED CLIP AT STRINGER 17L, F/STA 1186 BULKHEAD. TO REPLACE A CORRODED CLIP AT FUESLAGE STRINGER 17L, F/STA 1186. REMOVE AND REPLACE CORRODED STRINGER CLIP.
- [SDR FXGA202101062105](https://openairdocs.org/sdr/FXGA202101062105.md): Stringer Clip · corroded · Jan 6, 2021 · N794AJ · Boeing 727227 · Fuselage Main, Attach Fittings
  > CORRODED CLIP AT STRINGER 18L, F/STA 1186 BULKHEAD. TO REPLACE A CORRODED CLIP AT FUSELAGE STRINGER 18L, F/STA 1186. REMOVE AND REPLACE CORRODED STRINGER CLIP.
- [SDR FXGA2020011392002](https://openairdocs.org/sdr/FXGA2020011392002.md): Support Bracket · cracked · Jan 9, 2020 · N794AJ · Boeing 727227 · Spoilers
  > LEFT WING #3 FLIGHT SPOILER ACTUATOR SUPPORT BRACKETS CRACKED, INBRD AND OUTBRD. REPALACED LEFT WING #3 SPOILER ACTUATOR BRACKETS (BOTH). REMOVED AND REPLACE LEFT WING #3 SPOILER ACTUATOR BRACKETS P/N 65-24608-17 OUTBOARD BRACKET, AND P/N 65-24608-19 INBOARD
- [SDR FXGA201906261920](https://openairdocs.org/sdr/FXGA201906261920.md): Spar · corroded · Jun 26, 2019 · N794AJ · Boeing 727227 · Wing Spar
  > CORROSION ON AFT WING SPAR LOWER CHORD BETWEEN LBBL 19.2 AND WS 210L. CORROSION WAS FOUND ON THE AFT WING SPAR LOWER CHORD CENTER SECTION AND LT SECTION. SPLICES WILL BE PERFORMED AT LBBL 19.2 ON THE CENTER WING SECTION AND AT WS 210 ON THE LT WING SECTION.
- [SDR FXGA201906181949](https://openairdocs.org/sdr/FXGA201906181949.md): Mount · corroded · Jun 18, 2019 · N794AJ · Boeing 727227 · Engine Mount Section
  > REPLACEMENT OF CORODED #2 ENGINE MOUNT FITTING. TO REPLACE CORRODED AFT ENGINE MOUNT FITTING AND TEE CHORDS AT #2 ENGINE POSITION. REMOVE AND REPLACE #2 ENGINE SUPPORT FITTING P/N 65-18670-1, CHORDS P/N 65-31281-3, 65-31281-4, 65-22913-5, 65-22913-6, AND WEB
- [SDR FXGA201906111946](https://openairdocs.org/sdr/FXGA201906111946.md): Door Frame · corroded · Jun 11, 2019 · N794AJ · Boeing 727227 · Fuselage Main, Structure
  > MAIN CARGO DOOR JAMB INNER SKIN REPLACEMENT. TO REPLACE THE MAIN CARGO DOOR JAMB INNER SKIN (FORWARD LOWER SECTION AT F/STA 520) FOR CORROSION DAMAGE. REMOVE AND REPLACE CORRODED SECTIO OF DOOR JAMB PER B727 SRM 51-30-2.
- [SDR FXGA201905241945](https://openairdocs.org/sdr/FXGA201905241945.md): Spar · damaged · May 24, 2019 · N794AJ · Boeing 727227 · Wing Spar
  > CENTER WING SPAR TEMPORARY REPAIR FOR FERRY FLIGHT. TEMPORARY REPAIR FOR DAMAGE TO CENTER WING AFT SPAR LOWER CAP FOR FERRY FLIGHT TO INSTALL PERMANENT REPAIR. 727-227 LEFT HAND WING REPAIR TEMPORARY. S/N 21243.
- [SDR FXGA201905231944](https://openairdocs.org/sdr/FXGA201905231944.md): Skin · corroded · May 23, 2019 · N794AJ · Boeing 727227 · Fuselage Main, Plate/Skin
  > FUESLEAGE SKIN REPLACEMENT BETWEEN F/STA 259.5 AND 360 STRINGER 19L AND 26L. TO REPLACE A CORRODED SKIN BETWEEN F/STA 259.5 AND 360, FROM STRINGER 20L AND 25L. REMOVE AND REPLACE CORRODED SKIN PER SRM.
- [SDR FXGA2019040941932](https://openairdocs.org/sdr/FXGA2019040941932.md): Stringer · corroded · Apr 4, 2019 · N794AJ · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CORRODED FUSELAGE LONGERON #27R F/STA 950. TO REPAIR A CORRODED STRINGER. REMOVE CORROSION AND INSTALL REPAIR PER B727 SRM 51-40-4.
- [SDR FXGA201903081922](https://openairdocs.org/sdr/FXGA201903081922.md): Beam · corroded · Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION ON LT HORIZONTAL STABILIZER LOWER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. CUT DAMAGED BEAM AT STA 78.29 AND SPLICE IN NEW OUTBOARD SECTION PER SRM 55-10-6 FIGURE 1 HORIZONTAL STABILIZER T.E. BEAM REPAIR.
- [SDR FXGA201903081923](https://openairdocs.org/sdr/FXGA201903081923.md): Beam · corroded · Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION ON LT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. CUT DAMAGED BEAM AT STA 82.5 AND SPLICE IN NEW OUTBOARD SECTION PER SRM 55-10-6 FIGURE 1 HORIZONTAL STABILIZER T.E. BEAM REPAIR.
- [SDR FXGA201903081924](https://openairdocs.org/sdr/FXGA201903081924.md): Beam · corroded · Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION ON RT HORIZONTAL STABILIZER LOWER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. CUT DAMAGED BEAM AT STA 88.29 AND SPLICE IN NEW OUTBOARD SECTION PER SRM 55-10-6 FIGURE 1 HORIZONTAL STABILIZER T.E. BEAM REPAIR.
- [SDR FXGA201903081925](https://openairdocs.org/sdr/FXGA201903081925.md): Beam · corroded · Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION ON RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. REMOVE AND REPLACE CORRODED BEAM WITH NEW PER SRM 51-30-2 FASTENER REMOVAL AND INSTALLATION.
- [SDR FXGA201902081912](https://openairdocs.org/sdr/FXGA201902081912.md): Crossbeam · cracked · Feb 8, 2019 · N794AJ · Boeing 727227 · Fuselage Miscellaneous Structure
  > CRACK ON CROSS BEAM STA 856-850 @ LBL 45.50. TO REPAIR A CRACKED WEB ON A FLOOR CROSS BEAM. THE CRACK IS LOCATED BETWEEN F/SAT 850 AND 856 AT LBL 45.50. PERFORM REPAIR OF CRACKED WEB PER REPAIR DRAWING #E2499-001. DTA MUST BE OBTAINED WITHIN 12 MONTHS.
- [SDR FXGA201902041918](https://openairdocs.org/sdr/FXGA201902041918.md): Skin · corroded · Feb 4, 2019 · N794AJ · Boeing 727227 · Fuselage Main, Plate/Skin
  > CORROSION AT RT WING ILLUMINATION LIGHT. TO REPAIR A CORRODED SKIN BETWEEN F/STA 720B AND 720C AND LONGERON S-14R AND S-16R. REPAIR CORRODED SKIN PER SRM 53-30-3 FIGURE 22. SEE PAGE 2 FOR RE-INSPECTION REQUIREMENTS.
- [SDR FXGA201901081901](https://openairdocs.org/sdr/FXGA201901081901.md): Floorbeam · corroded · Jan 8, 2019 · N794AJ · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION ON O/B END STA 880 FLOORBEAM LOWER CHORD @ RBL 68. CORROSION ON OUTBOARD END OF STA 880 FLOORBEAM LOWER CHORD AT RBL 68. CUT OUT AND REMOVE DAMAGE, REPAIR PER SRM 53-10-08 FIGURE 8. RE-INSPECTION REQUIREMENTS: HFEC REQUIRED. INITIAL: 55,000 CYCLES
- [SDR FXGA20160226001](https://openairdocs.org/sdr/FXGA20160226001.md): Controller · failed · Feb 25, 2016 · N794AJ · Boeing 727227 · Cabin Pressure Controller
  > AIRCRAFT DEPRESSURIZED IN THE MIDDLE OF A PARABOLA. DESCENT WAS INITIATED AT FIRST INDICATION OF DEPRESSURIZATION. MAXIMUM ALTITUDE REACHED WAS FLIGHT LEVEL 310. FOUND THAT THE CABIN PRESS CONTROLLER HAD FAILED.
- [SDR CA141103034](https://openairdocs.org/sdr/CA141103034.md): Rod End · failed · Oct 31, 2014 · Boeing 727227 · Drag Control System
  > (CAN) DURING THE DAILY INSPECTION, MAINTENANCE IDENTIFIED THAT SPOILERS 10, 11 & 12 WERE EXTENDED WITHOUT CONTROL HANDLE INPUT. INVESTIGATION REVEALED A BROKEN ROD END ON SPOILER CABLE RT AT THE SPOILER MIXER RATIO CHANGER. MAINTENANCE REPLACED THE ROD END A
- [SDR CA141011001](https://openairdocs.org/sdr/CA141011001.md): Cable · failed · Oct 8, 2014 · Boeing 727227 · Drag Control System
  > (CAN) PILOTS REPORTED THAT, IN FLIGHT, AIRCRAFT ROLLS TO THE LEFT WHEN SPEEDBRAKES ARE DEPLOYED. MAINTENANCE INVESTIGATION DISCOVERED THE WSA-1 SEGMENT P SPOILER CABLE FAILED AT A PULLEY CONTACT. THE CABLE WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE.
- [SDR CA141014014](https://openairdocs.org/sdr/CA141014014.md): Wheel · cracked · Oct 6, 2014 · Boeing 727227 · Wheel/Ski/Float
  > (CAN) DURING THE A/C WALK AROUND, MAINTENANCE NOTICED THE NR 4 TIRE WAS FLAT. THE WHEEL/TIRE ASSY WAS REMOVED AND UPON INVESTIGATION, A CRACK WAS IDENTIFIED IN THE RADIUS AREA WERE THE BRAKE DRIVE KEYS MOUNT IN THE WHEEL ASSY. THE FAULTY NR 4 WHEEL ASSY WAS RE
- [SDR E4EB2014073112892](https://openairdocs.org/sdr/E4EB2014073112892.md): Flap System · unknown · Jul 27, 2014 · N17773 · Boeing 727227 · Trailing Edge Flap Control System
  > NR 1 L/E FLAP INDICATION GREEN LIGHTS DO NOT ILLUMINATE WHEN FLAPS SELECTED TO FULL DOWN.
- [SDR E4EB2014073112891](https://openairdocs.org/sdr/E4EB2014073112891.md): Battery Pack · inoperative · Jul 27, 2014 · N17773 · Boeing 727227 · Emergency Lighting
  > FORWARD CENTER AISLE OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK.
- [SDR CA140623025](https://openairdocs.org/sdr/CA140623025.md): Accessory Unit · failed · Jun 18, 2014 · Boeing 727227 · Landing Gear Actuator
  > (CAN) DURING CRUISE, THE LT MAIN GEAR INDICATION RED UNSAFE LIGHT ILLUMINATED. THE CREW PERFORMED THE GEAR LIGHT ILLUMINATED CHECK LIST FOLLOWED BY A MANUAL GEAR EXTENSION CHECKLIST. AFTER MANUAL EXTENSION WAS COMPLETED, THE LT MAIN GEAR DOWN AND LOCKED INDIC
- [SDR R5KB2014012556936](https://openairdocs.org/sdr/R5KB2014012556936.md): Shear Tie · corroded · Jan 25, 2014 · N422BN · Boeing 727227 · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED AT BS 1010 BETWEEN STRINGERS 29-30L.
- [SDR R5KB2014012556902](https://openairdocs.org/sdr/R5KB2014012556902.md): Floor Support · corroded · Jan 25, 2014 · N422BN · Boeing 727227 · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SUPPORT AT BS 1177, RBL 3, HAS AREA OF CORROSION.
- [SDR R5KB2014012557598](https://openairdocs.org/sdr/R5KB2014012557598.md): Stringer · corroded · Jan 25, 2014 · N422BN · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > STRINGER 24L HAS CORROSION AT BS 735.
- [SDR R5KB2014012557633](https://openairdocs.org/sdr/R5KB2014012557633.md): Stringer · cracked · Jan 25, 2014 · N422BN · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > STRINGER 29R AT BS 1000 UPPER FLANGE CRACKED.
- [SDR R5KB2014012557653](https://openairdocs.org/sdr/R5KB2014012557653.md): Attach Angle · corroded · Jan 25, 2014 · N422BN · Boeing 727227 · Fuselage Main, Attach Fittings
  > HORIZONTAL WEB INBD ATTACH ANGLE AT BS 299, LBL 16 CORRODED.
- [SDR R5KB2014012556944](https://openairdocs.org/sdr/R5KB2014012556944.md): Shear Tie · corroded · Jan 25, 2014 · N422BN · Boeing 727227 · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED AT BS 985 STUB FRAME BETWEEN STRINGER 28-29R.
- [SDR R5KB2014012556941](https://openairdocs.org/sdr/R5KB2014012556941.md): Stringer · corroded · Jan 25, 2014 · N422BN · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > STRINGER 29L HAS AREAS OF CORROSION BETWEEN BS 970 AND 990.
- [SDR R5KB2014012556904](https://openairdocs.org/sdr/R5KB2014012556904.md): Skin · corroded · Jan 25, 2014 · N422BN · Boeing 727227 · Fuselage Main, Plate/Skin
  > EVIDENCE OF CORROSION AT SKIN DOUBLER AT STRINGER 26L BETWEEN BS 1160 AND 1180.
- [SDR R5KB2014012556952](https://openairdocs.org/sdr/R5KB2014012556952.md): Stringer · corroded · Jan 25, 2014 · N422BN · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > STRINGER 29L HAS AREAS OF CORROSION BETWEEN BS 950E AND 950F.
- [SDR R5KB2014012556955](https://openairdocs.org/sdr/R5KB2014012556955.md): Stringer · corroded · Jan 25, 2014 · N422BN · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > STRINGER 29L HAS CORROSION BETWEEN BS 950D AND 950E.
- [SDR R5KB2014012556956](https://openairdocs.org/sdr/R5KB2014012556956.md): Stringer · corroded · Jan 25, 2014 · N422BN · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > STRINGER 29R HAS CORROSION BETWEEN BS 950D AND 950E.
- [SDR R5KB2014012556960](https://openairdocs.org/sdr/R5KB2014012556960.md): Stringer · corroded · Jan 25, 2014 · N422BN · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > STRINGER 30L HAS AREAS OF CORROSION BETWEEN BS 950A AND 950C.
- [SDR R5KB2014012556938](https://openairdocs.org/sdr/R5KB2014012556938.md): Stringer · corroded · Jan 25, 2014 · N422BN · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > STRINGER 29R CORRODED AT BS 1000.
- [SDR R5K20140125B56992](https://openairdocs.org/sdr/R5K20140125B56992.md): Intake Duct · corroded · Jan 25, 2014 · N422BN · Boeing 727227 · Engine Air Intake System
  > NR 2 ENGINE S-DUCT INTERNAL SKIN BULGING AT RIB 22 AT 6 O'CLOCK POSITION.
- [SDR R5KB2014012557643](https://openairdocs.org/sdr/R5KB2014012557643.md): Intake Duct · damaged · Jan 25, 2014 · N422BN · Boeing 727227 · Engine Air Intake System
  > AT PRODUCTION BREAK SPLICE IN S-DUCT AT BS 1243 BOTTOM SIDE BETWEEN RIB 16 AND 17 SPLICE REPAIR DAMAGED.

Next page: https://openairdocs.org/model/boeing-727-227/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 = '727227'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-227/reports

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