# Service difficulty reports: Boeing 727-2Q6

A list on [Boeing 727-2Q6](https://openairdocs.org/model/boeing-727-2q6.md).

Newest first. General aviation reporting is voluntary.

- [SDR CA081016008](https://openairdocs.org/sdr/CA081016008.md): Switch · inoperative · Oct 3, 2008 · Boeing 7272Q6 · Engine Thrust Reverser
  > (CAN) ON CLIMB OUT, NR 3 ENGINE THRUST REVERSER OPERATING LIGHT ILLUMINATED THROUGH 5000 FT. THE ACFT RETURNED TO THE AIRPORT. THE NR3 ENG THRUST REVERSER WAS DEACTIVATED AND MEL APPLIED. UPON REACHING THE DESTINATION, THE NR3 ENGINE THRUST REVERSER SWITCH WAS
- [SDR C7WA200700001](https://openairdocs.org/sdr/C7WA200700001.md): Controller · smoke · Apr 29, 2007 · N1279E · Boeing 7272Q6 · Cargo/Baggage Doors
  > ON CLIMBOUT FROM SJU FLIGHT ENGINEER SMELLED SMOKE AND TRIED TO ID SOURCE. ACCOMPLISHED AOM PROCEDURE AND REMOVED POWER FROM CARGO DOOR CONTROL. SMOKE STOPPED AND RETURNED FOR INSPECTION. [06-21-07] INSPECTION OF CARGO DOOR CONTROL AREA REVEALED THE HYDR
- [SDR C7WA200600017](https://openairdocs.org/sdr/C7WA200600017.md): Wire · broken · Nov 30, 2006 · N1279E · Boeing 7272Q6 · Door System Wiring
  > AIR RETURN: AT LIFT OFF, HEARD A LOUD BANG AND AIRCRAFT WOULD NOT PRESSURIZE. NO DOOR LIGHTS OBSERVED. RETURNED TO DEPARTURE. SECURED E&E BAY DOOR. PRESSURIZED AIRCRAFT OPERATIONAL CHECKS GOOD. E&E DOOR WARNING LIGHT INDICATION INOPERATIVE. REPAIRED BRO
- [SDR C7WA200600005](https://openairdocs.org/sdr/C7WA200600005.md): Actuator · inoperative · Feb 24, 2006 · N1279E · Boeing 7272Q6 · Leading Edge Slat Actuator
  > NR 3 LEADING EDGE FLAP WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED LEADING EDGE FLAP ACTUATOR IAW MM, OPERATIONAL CHECKS GOOD. (K)
- [SDR C7WA200400071](https://openairdocs.org/sdr/C7WA200400071.md): Actuator · leaking · Dec 10, 2004 · N1279E · Boeing 7272Q6 · Leading Edge Slat Actuator
  > AIR RETURN; AFTER TAKEOFF AND FLAP RETRACTION SYSTEM (A) HYDRAULIC QUANTITY WAS DROPPING RAPIDLY. ACCOMPLISHED ABNORMAL PROCEDURE FOR LOSS OF SYSTEM (A) QUANTITY. FOUND NR 1 SLAT ACTUATOR LEAKING. REMOVED AND REPLACED SLAT ACTUATOR IAW MM. (K)
- [SDR C7WA200400009](https://openairdocs.org/sdr/C7WA200400009.md): Strap · cracked · Apr 12, 2004 · N1279E · Boeing 7272Q6 · Passenger/Crew Doors
  > FOUND FORWARD ENTRANCE DOOR AFT LOWER STRAP CRACKED. REPAIRED STRAP IAW B727 SRM 51-40-4. (M)
- [SDR C7WA200400010](https://openairdocs.org/sdr/C7WA200400010.md): Door Frame · cracked · Apr 12, 2004 · N1279E · Boeing 7272Q6 · Cargo/Baggage Doors
  > FOUND MAIN CARGO DOOR FORWARD UPPER FRAME CRACKED. REPAIRED FRAME IAW AERONAUTICAL ENGINEERS INC EO NR 1434. (M)
- [SDR C7WA200400011](https://openairdocs.org/sdr/C7WA200400011.md): Door Frame · cracked · Apr 12, 2004 · N1279E · Boeing 7272Q6 · Fuselage Main, Structure
  > FOUND MAIN CARGO DOOR FORWARD UPPER FRAME CRACKED. REPAIRED FRAME IAW AERONAUTICAL ENGINEERS INC EO NR 1434. (M)
- [SDR C7WA200400013](https://openairdocs.org/sdr/C7WA200400013.md): Frame · cracked · Apr 12, 2004 · N1279E · Boeing 7272Q6 · Fuselage Main, Frame
  > FOUND FUSELAGE FRAME CRACKED FS 680 WL 208. REPAIRED FUSELAGE FRAME IAW B727 MM 51-40-3. (M)
- [SDR C7WA200400012](https://openairdocs.org/sdr/C7WA200400012.md): Hinge · cracked · Apr 12, 2004 · N1279E · Boeing 7272Q6 · Cargo/Baggage Doors
  > FOUND MAIN CARGO DOOR FORWARD HINGE HAS A CRACKED LOBE. REPLACED FORWARD HING HALF IAW AERONAUTICAL ENGINEERS INC SERVICE BULLETIN AE101-01. (M)
- [SDR COOSDR020174](https://openairdocs.org/sdr/COOSDR020174.md): Support Fitting · corroded · Jul 1, 2002 · N1279E · Boeing 7272Q6 · Trailing Edge Flaps
  > LEFT AND RIGHT WING, INBOARD FLAP, INBOARD TRACK FORWARD SUPPORT FITTING WITH BORE CORRODED.
- [SDR COOSDR020173](https://openairdocs.org/sdr/COOSDR020173.md): Flap Track · corroded · Jul 1, 2002 · N1279E · Boeing 7272Q6 · Trailing Edge Flaps
  > RIGHT WING, FLAP TRACK NR 6, AFT PAD CORRODED.
- [SDR COOSDR020172](https://openairdocs.org/sdr/COOSDR020172.md): Skin · delaminated · Jun 1, 2002 · N1279E · Boeing 7272Q6 · Aileron Tabs
  > LEFT WING OUTBOARD AILERON TAB UPPER, LOWER SKIN DELAMINATED AND HONEYCOMB CORE SECTION CORRODED.
- [SDR COOSDR020171](https://openairdocs.org/sdr/COOSDR020171.md): Skin · delaminated · Jun 1, 2002 · N1279E · Boeing 7272Q6 · Spoilers
  > LEFT WING SPOILER NR 3 UPPER SKIN DELAMINATED AND HONEYCOMB CORE SECTION CORRODED.
- [SDR COOSDR020170](https://openairdocs.org/sdr/COOSDR020170.md): Skin · delaminated · Jun 1, 2002 · N1279E · Boeing 7272Q6 · Spoilers
  > RIGHT WING SPOILER NR 14 UPPER AND LOWER SKIN DELAMINATED AND HONEYCOMB CORE CORRODED.
- [SDR COOSDR020169](https://openairdocs.org/sdr/COOSDR020169.md): Aileron · delaminated · Jun 1, 2002 · N1279E · Boeing 7272Q6 · Ailerons
  > LEFT WING OUTBOARD AILERON TRAILING EDGE UPPER AND LOWER SKIN DELAMINATED AND HONEYCOMB CORE CORRODED.
- [SDR COOSDR020168](https://openairdocs.org/sdr/COOSDR020168.md): Panel · delaminated · Jun 1, 2002 · N1279E · Boeing 7272Q6 · Wing, Plate/Skin
  > RIGHT WING TRAILING EDGE LOWER FIX PANEL OUTER SKIN DELAMINATED AND HONEYCOMB CORE CORRODED.
- [SDR COOSDR020167](https://openairdocs.org/sdr/COOSDR020167.md): Aileron · delaminated · Jun 1, 2002 · N1279E · Boeing 7272Q6 · Ailerons
  > RIGHT WING OUTBOARD AILERON TRAILING EDGE UPPER AND LOWER SKIN DELAMINATED AND HONEYCOMB CORE CORRODED.
- [SDR COOSDR020166](https://openairdocs.org/sdr/COOSDR020166.md): Spoiler · delaminated · Jun 1, 2002 · N1279E · Boeing 7272Q6 · Spoilers
  > LEFT WING SPOILER NR 6 UPPER AND LOWER SKIN, DELAMINATED AND HONEYCOMB CORE CORRODED.
- [SDR COOSDR020165](https://openairdocs.org/sdr/COOSDR020165.md): Shear Tie · corroded · Jun 1, 2002 · N1279E · Boeing 7272Q6 · Fuselage Main, Structure
  > AFT CARGO COMP. BS 950A SHEAR TIE CORRODED BETWEEN STR 28R AND STR 29R.
- [SDR COOSDR020164](https://openairdocs.org/sdr/COOSDR020164.md): Skin · cracked · Jun 1, 2002 · N1279E · Boeing 7272Q6 · Fuselage Main, Plate/Skin
  > SECTION 46-RIGHT FUSELAGE SKIN CRACKED AND CORRODED BETWEEN BS 1164.5 AND BS 1179 BETWEEN STR 26R AND STR 25R.
- [SDR COOSDR020163](https://openairdocs.org/sdr/COOSDR020163.md): Rib · corroded · Jun 1, 2002 · N1279E · Boeing 7272Q6 · Wing, Rib/Bulkhead
  > RIB UPPER CHORD CORRODED, BETWEEN BS 836.95 AND BS 848.95, AT LEFT WING, BUTTOCK LINE 70.5.
- [SDR COOSDR020162](https://openairdocs.org/sdr/COOSDR020162.md): Rib · corroded · Jun 1, 2002 · N1279E · Boeing 7272Q6 · Wing, Rib/Bulkhead
  > RIB UPPER CHORD CORRODED, BETWEEN BS 836.95 AND BS 848.95 AT LEFT WING, BUTTOCK LINE 70.5.
- [SDR COOSDR020161](https://openairdocs.org/sdr/COOSDR020161.md): Skin · worn · Jun 1, 2002 · N1279E · Boeing 7272Q6 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN - RIGHT SIDE BODY STATION 720D+11 INCHES, STRINGER 19R - SKIN WITH WEAR.
- [SDR C8GA200000006](https://openairdocs.org/sdr/C8GA200000006.md): Connector · dirty · Jul 7, 2000 · N1279 · Boeing 7272Q6 · Central Warning
  > FLIGHT 205 FROM IND TO DFW. IN TAKE OFF CONFIGURATION, WHEN THROTTLES ADVANCED, THE TAKE OFF WARNING HORN SOUNDED. THE AIRCRAFT TAXIED FROM RUNWAY AND RETURNED TO GATE.FOUND TAKE OFF WARNING SWITCH CONNECTOR DIRTY. CLEANED CONNECTOR. PERFORMED TAKE OFF WARN
- [SDR 20000619AP001](https://openairdocs.org/sdr/20000619AP001.md): Hydraulic Line · leaking · Feb 9, 2000 · N782AT · Boeing 7272Q6 · Hydraulic System, Main
  > INBOUND TO MDW A/C WAS DIVERTED TO ORD DUE TO THE NR 2 B SYSTEM PUMP LOW PRESSURE LIGHT CAME ON AND THE B SYSTEM QTY DROPPED. THE NR 1 B SYSTEM PUMP LOW PRESSURE LIGHT CAME ON AND THE PILOT LOST ALL THE B SYSTEM PRESSURE. A/C WAS TOWED TO GATE AFTER LANDING.
- [SDR 99ZZZM633](https://openairdocs.org/sdr/99ZZZM633.md): Connector · damaged · Jul 15, 1999 · N782AT · Boeing 7272Q6 · Fire Detection
  > NR 1 ENGINE FIRE WARNING ANNUNCIATOR CAME ON AT 230. ACCOMPLISHED ENGINE FIRE SHUTDOWN PROCEDURE, FIRE HANDLE PULLED AND FIRED BOTH BOTTLES AND LIGHT REMAINED ON UNTIL AT APPROXIMATELY 3,000 FT. AFTER EXTENSIVE TROUBLESHOOTING CONNECTOR D400 WAS FOUND WITH A
- [SDR 99ZZZM779](https://openairdocs.org/sdr/99ZZZM779.md): Tube · inoperative · Jul 12, 1999 · N782AT · Boeing 7272Q6 · Engine Anti-Icing System
  > DURING LEVEL CRUISE AT 310, THE NR 1 ENGINE FIRE WARNING ANNUNCIATOR CAME ON. ACCOMPLISHED ENGINE FIRE SHUTDOWN PROCEDURE, FIRE HANDLE PULLED, LIGHT IMMEDIATELY EXTINGUISHED. REPLACED LEFT FRONT ANTI-ICING TUBE AS REQUIRED. NO LEAKS NOTED AT THIS TIME, OK F
- [SDR 99ZZZX2831](https://openairdocs.org/sdr/99ZZZX2831.md): Engine · failed · Jun 26, 1999 · N1279E · Boeing 7272Q6 · Engine (Turbine/Turboprop)
  > KDAY/KJAX - FLT 326 - IN CRUISE, THE NR 2 ENGINE OIL PRESSURE LOW LIGHT ILLUMINATED ON FORWARD CONTROL PANEL. A CORRESPONDING DROP IN OIL PRESSURE WAS NOTED. OIL QUANTITY INDICATION WAS NORMAL. PRESSURE CONTINUED TO DROP. FLIGHT CREW SECURED THE NR 2 ENGIN
- [SDR 98ZZZX4544](https://openairdocs.org/sdr/98ZZZX4544.md): Battery · discharged · Jul 2, 1998 · N782AT · Boeing 7272Q6 · Emergency Lighting
  > IND - RIGHT SIDE AFT OVERWING EXPRESS (ABOVE FLAP) LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK.
- [SDR C8GA973204](https://openairdocs.org/sdr/C8GA973204.md): Retract Mech · malfunctioned · Sep 18, 1997 · N1279E · Boeing 7272Q6 · Landing Gear Retraction/Extension System
  > KTPA/KATL - FLT 103/18 - LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. PERFORMED LANDING GEAR EXTENSION AND RETRACTION CHECK PER MM 32-31-0 WITH AIRCRAFT ON JACKS. NO FAULTS NOTED. CYCLED GEAR MANY TIMES. GEAR AND INDICATION SYSTEM OPS CK OK. VERIFIED A-SYST

## 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 = '7272Q6'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-2q6/reports

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