# Service difficulty reports: Boeing 727-270

A list on [Boeing 727-270](https://openairdocs.org/model/boeing-727-270.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 112 reports

- [SDR C1HA200797003](https://openairdocs.org/sdr/C1HA200797003.md): Indicator · malfunctioned · Jul 10, 2007 · N697CA · Boeing 727270 · Airspeed/Mach Indicator
  > DURING CLIMB-OUT CAPTAINS AIRSPEED INDICATOR.95 ON CAPTAINS SIDE/COPILOTS MACH INDICATOR.76 MACH AIRSPEED CLACKER SOUNDED UNCONTROLLABLE COMPLIED WITH COM 2.31.8 LANDED AT DFW CONFIRMED FAULT OF NR 1 MACH IND. REMOVED AND REPLACED IND SYSTEM CHECK GOOD IAW
- [SDR C1HA200797002](https://openairdocs.org/sdr/C1HA200797002.md): Indicator · inaccurate · Jul 8, 2007 · N697CA · Boeing 727270 · Airspeed/Mach Indicator
  > ON CLIMB-OUT, CAPTAIN'S AIRSPEED INDICATOR INDICATED ERRONEOUS AIRSPEED AND MACH. COMPLIED WITH COM 2.31.8.9.10.11.12 "FLIGHT WITH UNRELIABLE AIRSPEED/MACH" IVSI INDICATED INTERMITTENTLY VERTICAL SPEED INFORMATION ONLY. CLIMB STOPPED AT FL 280. ALL CIRCUIT
- [SDR C1HA200697021](https://openairdocs.org/sdr/C1HA200697021.md): Switch · failed · Nov 25, 2006 · N697CA · Boeing 727270 · Central Warning
  > AFTER TAKEOFF DURING FLAP RETRACTION STEADY HORN SOUNDED WITH NORMAL FLAP AND GEAR INDICATIONS. PULLED CB TO SILENCE HORN. RESET CB DURING CRUISE. DURING FLAP EXTENSION STEADY HORN SOUNDED AND STAYED ON UNTIL LANDING GEAR EXTENDED. ALL NORMAL INDICATIONS F
- [SDR C1HA200697018](https://openairdocs.org/sdr/C1HA200697018.md): Floorbeam · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage Main, Floor Beam
  > CORROSION AT FLOORBEAM 360 RBL 5. REMOVED FABRICATED NEW BACL 505-100617 AND INSTALLED AT LBL 8- RBL 14 IAW SRM 53-10-8 FIG 3 AND 51-30-2.
- [SDR C1HA200697009](https://openairdocs.org/sdr/C1HA200697009.md): Floorbeam · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage Main, Floor Beam
  > CORROSION ON CABIN FLOOR BEAM BS 440 LBL 45 TO RBL 24. REPAIRED FLOORBEAM AT BS 440 IAW SRM 53-10-8 FIG 3.
- [SDR C1HA200697017](https://openairdocs.org/sdr/C1HA200697017.md): Floorbeam · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage Main, Floor Beam
  > CORROSION OF FLOORBEAM BS 1110 LBL 65 TO RBL 65. REPAIRED DAMAGED AREA ON FLOORBEAM BS 1110 FROM LBL 66 TO RBL 15 IAW SRM 53-10-2 AND 53-10-8.
- [SDR C1HA200697015](https://openairdocs.org/sdr/C1HA200697015.md): Bulkhead · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage Main, Bulkhead
  > AFT SIDE OF COCKPIT BULKHEAD CORRODED BS 303 LBL 15-45. REMOVED AND REPLACED LOWER WEB SECTION OF AFT SIDE OF COCKPIT BULKHEAD IAW SRM 53-10-2 AND 51-20-4.
- [SDR C1HA200697002](https://openairdocs.org/sdr/C1HA200697002.md): Frame · cracked · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage Main, Frame
  > BS 1303 FRAME FIN WL (O) HAS WEB CRACK LT SIDE BOTTOM. STOP DRILLED CRACK AT FIN WL (0) IAW EO CA0909-06 REV N/C. VERIFIED CRACK STOPPED IAW NDTM PT 6 51-00-00 FIG 23.
- [SDR CIHA200697003](https://openairdocs.org/sdr/CIHA200697003.md): Frame · cracked · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage Main, Frame
  > BS 1303 FRAME FIN WL (6) HAS WEB CRACKED LT SIDE +6 INCHES FROM BOTTOM. STOP DRILLED CRACK AT WL 6 IAW EO CA 0909-06 REV N/C. VERIFIED CRACK STOPPED IAW NDTM PT 6 51-00-00 FIG 23.
- [SDR C1HA200697014](https://openairdocs.org/sdr/C1HA200697014.md): Floorbeam · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage Main, Floor Beam
  > CORROSION ON CABIN FLOORBEAM BS 340 LBL 65 - RBL 65 UPPER AND LOWER SURFACE. REPAIRED CORRODED AREA AT BS 340 FROM BL 0 TO RBL 28 IAW B727 SRM 53-10-2 AND 53-10-8 FIG 3.
- [SDR C1HA200697006](https://openairdocs.org/sdr/C1HA200697006.md): Seat Track · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER CABIN SEAT TRACK CORRODED 1110 - 1145 LBL 24. REMOVED AND REPLACED SEAT TRACK FROM BS 990 - 1145 LBL 45 IAW B727 SRM 53-10-5 FIG 7 AND 51-30-2 FIG 1 & 11.
- [SDR C1HA200697011](https://openairdocs.org/sdr/C1HA200697011.md): Support · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage Miscellaneous Structure
  > CORROSSION ON FWD LAV AFT WALL SUPPORT BS 340 RBL 10-55. FABRICATED AND INSTALLED NEW WALL SUPPORT IAW B727 SRM 53-10-2 FIG 7 AND 51-30-2 FIG 1.
- [SDR C1HA200697010](https://openairdocs.org/sdr/C1HA200697010.md): Floorbeam · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM (CABIN) BS 400 LBL 45- RBL 24 (UPPER T-SECTION). REMOVED UPPER T-SECTION OF FLOORBEAM FROM LBL 14 - RBL 17 IAW B727 SRM 53-10-8 FIG 3. FAB NEW SECTION P/N BAC1505100617 IAW B727 SRM 53-10-8 FIG 3. INSTALLED REPAIR PART IAW B727 SRM 51
- [SDR C1HA200697016](https://openairdocs.org/sdr/C1HA200697016.md): Seat Track · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage, Seat/Cargo Attach Fittings
  > SURFACE CORROSION ON SEAT TRACK RBL 45 BS 990-1130. REMOVED AND REPLACED SECTION OF SEAT TRACK FOUND WITH CORROSION OUT OF LIMITS AT BS 970-1080 RBL 45 IAW B727 SRM 53-10-2 AND 53-10-5.
- [SDR C1HA200697013](https://openairdocs.org/sdr/C1HA200697013.md): Support · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage Miscellaneous Structure
  > CORROSION IN CABIN AT FWD LAV WALL SUPPORT BS 303-340 RBL 20. FABRICATED AND INSTALLED NEW WALL SUPPORT IAW B727 SRM 53-10-2 FIG 7 AND 51-30-2 FIG 1.
- [SDR C1HA200697012](https://openairdocs.org/sdr/C1HA200697012.md): Seat Track · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON SEAT TRACK BS 340-480 RBL 24. REPLACED SEAT TRACK AT BS 340-480 RBL 24 AS PER B727 SRM 51-30-2, B727 SRM 53-10-2 FIG 7.
- [SDR C1HA200697020](https://openairdocs.org/sdr/C1HA200697020.md): Beam · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage Miscellaneous Structure
  > NOSE SECTION, WALKWAY BEAM LEFTSIDE INTERNAL CHANNEL ANGLE HAS CORROSION BS 304, FROM LEFT TRUNNION ACCESS WINDOW. INSTALLED REPAIR AS REQUIRED IAW EO CA 0910-06, REV N/C.
- [SDR C1HA200697005](https://openairdocs.org/sdr/C1HA200697005.md): Shear Tie · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Vertical Stabilizer, Plate/Skin
  > VERT STAB NR 3 TENSION TIE MOUNT HOLE PITTED. REAMED HOLE TO REMOVE PITTING IAW B727 CHAMPION AIR M/M 55-30-61 FIG 604 AND INSTALLED A FASTENER HOLE REPAIR IAW EO- 727- 5531-02.
- [SDR C1HA200697008](https://openairdocs.org/sdr/C1HA200697008.md): Floorbeam · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage Main, Floor Beam
  > FOUND FLOORBEAM CORRODED BS 460 RBL 24-65. REPAIRED FLOORBEAM BS 460 FROM RBL 33 TO RBL 36 IAW B727 SRM 53-10-2 AND 53-10-8.
- [SDR C1HA200697007](https://openairdocs.org/sdr/C1HA200697007.md): Seat Track · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND PASSENGER CABIN SEAT TRACK CORRODED 1110-1145 LBL-55. REMOVED CORRODED SEAT TRACK FROM FS 1110-1145 LBL 55 IAW B727 SRM 51-30-2. FAB NEW SEAT TRACK (5'10") FROM BAC 1520-795 7178-T6511, IAW B727 SRM 53-10-5 FIG 7 SHEET 1. INSTALLED SEAT TRACK AT FS 11
- [SDR C1HA200697019](https://openairdocs.org/sdr/C1HA200697019.md): Seat Track · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND SEAT TRACK AT STA 950F RBL 45 HAS CORROSION. REPAIRED SEAT TRACK AS REQUIRED IAW B727 SRM 53-10-5 FIG 7.
- [SDR C1HA200697004](https://openairdocs.org/sdr/C1HA200697004.md): Tension Tie · corroded · Sep 25, 2006 · N697CA · Boeing 727270 · Vertical Stabilizer, Plate/Skin
  > VERT STAB TENSION TIE AFT END CORRODED. REMOVED AND REPLACED VERT STAB TENSION TIE IAW B727 MM 55-10-01 AND MM 55-30-51.
- [SDR C1HA200697001](https://openairdocs.org/sdr/C1HA200697001.md): Indicator · sticking · Jun 14, 2006 · N697CA · Boeing 727270 · Trailing Flap Position Indicating System
  > ON FINAL APPROACH NOTICED A SPLIT FLAP INDICATION, WENT AROUND PERFORMED COM PROCEDURES 2.27.28 AND 2.274. FLAPS OPERATED NORMALLY WITH THE ALTERNATE SYSTEM. CONTACTED DISPATCH AND LANDED NORMALLY. FOUND OUTBOARD POSITION IND STICKING. REMOVED AND REPLACED
- [SDR C1HA200597002](https://openairdocs.org/sdr/C1HA200597002.md): Transmission · inoperative · Aug 14, 2005 · N697CA · Boeing 727270 · Trailing Edge Flap Control System
  > AFTER LANDING FLAP INDICATOR FLAPS STUCK ON 8 DEG (INBOARD) C/B`S CLOSED. PERFORMED ADJUSTMENT, FOUND SHEERED PIN ON OUTPUT DRIVE GEAR OF NR 5 FLAP TRANSMISSION R@RED NR 5 FLAP TRANSMISSION PER MM 27-51-41.
- [SDR 1HA200597001](https://openairdocs.org/sdr/1HA200597001.md): Position Switch · out of adjust · Jan 28, 2005 · N697CA · Boeing 727270 · Leading Edge Slat Position Indicating System
  > L/E FLAPS [AMBER] LIGHT REMAINED ILLUMINATED UPON CLIMB AT/FLAP RETRACTION. NR 5 L/E FLAP ALSO ILLUMINATED ON F/E'S AUX PANEL. ADJUSTED NR 5 L/E FLAP POSITION SWITCH ACTUATOR ARM IAW 727 MM 27-82-11. ALL OPS & INDICATIONS NORMAL, OK FOR CONTINUED SERVICE.
- [SDR C1HA200497015](https://openairdocs.org/sdr/C1HA200497015.md): Skin · cracked · Sep 25, 2004 · N697CA · Boeing 727270 · Leading Edge Devices
  > NR 4 SLAT EXTERNAL SKIN IS CRACKED 2 (EA) PLACES AT AERODYNAMIC FENCE MOUNTING AREA, (MARKED). REPAIRED 2 (EA) CRACKS IN NR 4 SLAT EXTERNAL SKIN IAW B727 SRM 57-50-3 FIG 1 TRANSFERRED TO LOG PAGE B 20238 ITEM 3 DUE TO RII INSPECTION RII ACCOMPLISHED.
- [SDR C1HA200497016](https://openairdocs.org/sdr/C1HA200497016.md): Skin · cracked · Sep 25, 2004 · N697CA · Boeing 727270 · Leading Edge Devices
  > NR 4 SLAT EXTERNAL SKIN IS CRACKED 2 PLACES AT AERODYNAMIC FENCE MOUNTING AREA (MARKED). REPAIRED 2 CRACKS IN NR 4 SLAT EXTERNAL SKIN IAW B727 SRM 57-50-3 FIG 1. TRANSFERRED TO LOG PAGE B 20238 ITEM 3 DUE TO RII INSPECTION RII ACCOMPLISHED.
- [SDR C1HA200497010](https://openairdocs.org/sdr/C1HA200497010.md): Rib · cracked · Sep 20, 2004 · N697CA · Boeing 727270 · Leading Edge Devices
  > NR 3 SLAT O/B CAP END SKIN IS CRACKED. CRACK=8 INCHES. REPLACED RIB.
- [SDR C1HA200497014](https://openairdocs.org/sdr/C1HA200497014.md): Skin · cracked · Sep 13, 2004 · N697CA · Boeing 727270 · Leading Edge Devices
  > NR 4 SLAT LEADING EDGE LOWER SKIN IS CRACKED AT AERODYNAMIC FENCE AFT LOWER MOUNT AREA (MARKED). REPAIRED PER SRM.
- [SDR C1HA200497011](https://openairdocs.org/sdr/C1HA200497011.md): Floorbeam · corroded · Sep 13, 2004 · N697CA · Boeing 727270 · Fuselage Main, Floor Beam
  > FLOORBEAM STA 1230 LBL 15 - RBL 24 IS CORRODED AROUND FASTENER HOLES. REPAIRED FLOORBEAM LBL 15 TO RBL 24.
- [SDR C1HA200497007](https://openairdocs.org/sdr/C1HA200497007.md): Floorbeam · corroded · Sep 13, 2004 · N697CA · Boeing 727270 · Fuselage Main, Floor Beam
  > FLOORBEAM STA 1230 LBL 15 - RBL 24 IS CORRODED AROUND FASTENER HOLES. REPAIRED FLOORBEAM LBL 15 TO RBL 24.
- [SDR C1HA200497002](https://openairdocs.org/sdr/C1HA200497002.md): Rib · gouged · Sep 13, 2004 · N697CA · Boeing 727270 · Leading Edge Devices
  > NR 4 SLAT O/B SIDE CHAFED & GOUGED. REPLACED RIB.
- [SDR C1HA200497012](https://openairdocs.org/sdr/C1HA200497012.md): Spar · cracked · Sep 12, 2004 · N697CA · Boeing 727270 · Leading Edge Devices
  > NR 3 SLAT FWD SPAR CRACKED AT SLAT STA 177 FWD OF ACTUATOR CONNECTION. INSTALLED REPAIR DOUBLERS.
- [SDR C1HA200497006](https://openairdocs.org/sdr/C1HA200497006.md): Rib · cracked · Sep 12, 2004 · N697CA · Boeing 727270 · Leading Edge Devices
  > NR 3 SLAT LEADING EDGE INTERNAL RIB IS CRACKED FWD OF ACTUATOR PISTON ROB END MOUNTING NUT (MARKED) WS 519. CRACK = 1 INCH. REPLACED RIB.
- [SDR C1HA200497005](https://openairdocs.org/sdr/C1HA200497005.md): Rib · cracked · Sep 12, 2004 · N697CA · Boeing 727270 · Leading Edge Devices
  > NR 3 SLAT LEADING EDGE INTERNAL RIB IS CRACKED IMMEDIATE I/B OF ACTUATOR PISTON ROD END AT WS 515 (MARKED). REPAIRED RIB.
- [SDR C1HA200497004](https://openairdocs.org/sdr/C1HA200497004.md): Rib · cracked · Sep 12, 2004 · N697CA · Boeing 727270 · Leading Edge Devices
  > NR 4 SLAT LEADING EDGE INTERNAL RIB IS CRACKED FWD OF SLAT ACTUATOR PISTON ROD END MOUNTING BOLT WS 410. CRACK = 0.500. REPLACED RIB.
- [SDR C1HA200497003](https://openairdocs.org/sdr/C1HA200497003.md): Rib · cracked · Sep 12, 2004 · N697CA · Boeing 727270 · Leading Edge Devices
  > NR 4 SLAT LEADING EDGE INTERNAL RIB IS CRACKED IMMEDIATE I/B OF SLAT ACTUATOR PISTON ROD END WS 408 (MARKED) CRACK = 0.490. REPLACED RIB.
- [SDR C1HA200497009](https://openairdocs.org/sdr/C1HA200497009.md): Rib · cracked · Sep 11, 2004 · N697CA · Boeing 727270 · Leading Edge Devices
  > RT WING NR 7 SLAT ACTUATOR ROD END ATTACH POINT AREA, INTERNAL RIBS CRACKED AT 2 EA PLACES ON THE RT AND 1 EA ON THE LEFT AS MARKED. REPLACED RIB.
- [SDR C1HA200497008](https://openairdocs.org/sdr/C1HA200497008.md): Rib · cracked · Sep 11, 2004 · N697CA · Boeing 727270 · Leading Edge Devices
  > RT WING NR 5 SLAT ACTUATOR ROD END ATTACH POINT AREA, INTERNAL RIBS CRACKED AT 2 EA PLACES ON THE RT AND 2 EA ON THE LEFT AS MARKED (5 EA CRACKS TOTAL 1 EA PREVIOUSLY STOP DRILLED). REPLACED RIB.
- [SDR C1HA200497013](https://openairdocs.org/sdr/C1HA200497013.md): Skin · corroded · Sep 8, 2004 · N697CA · Boeing 727270 · Fuselage Main, Plate/Skin
  > WING CENTER BOX LWR SKIN EXFOLIATED AT S-4C LBL 24 STA 825.95. INSTALLED REPAIR DOUBLER.
- [SDR C1HA200497001](https://openairdocs.org/sdr/C1HA200497001.md): Striker · out of adjust · Jun 10, 2004 · N697CA · Boeing 727270 · Entrance Stairs
  > AFT AIRSTAIR AMBER LIGHT CAME ON IN FLIGHT. RAN COM 2.25.2. RETURNED TO LAS. DAYLIGHT WAS VISABLE FROM INSIDE THE AIRCRAFT. INSPECTED & RESCHEDULED PER MEL 52-6-C CAT -C- CONTROL C06208. PLACARDS INSTALLED & MX CONTROL NOTIFIED. NO DDG REQUIRED. STAIRS V
- [SDR C1HA20039701](https://openairdocs.org/sdr/C1HA20039701.md): Charger · failed · Nov 12, 2003 · N697CA · Boeing 727270 · Emergency Lighting
  > EMERGENCY LIGHTS OUT BETWEEN ROW 11 TO ROW 20. REMOVED & REPLACED BATTERY CHARGER PER M/M 33-50-01. OPS CHECK GOOD. P/N 11-0049
- [SDR C1HA200397016](https://openairdocs.org/sdr/C1HA200397016.md): Battery · inoperative · Oct 21, 2003 · N697CA · Boeing 727270 · Emergency Lighting
  > AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERIES, OPS CHECK NORMAL IAW MM 33-50-61.
- [SDR C1HA200397015](https://openairdocs.org/sdr/C1HA200397015.md): Battery Pack · inoperative · Oct 19, 2003 · N697CA · Boeing 727270 · Emergency Lighting
  > RIGHT FWD EXTERIOR WING LIGHT INOP. REMOVED & REPLACED BATTERY PACK AT STA 835. REF M/M CH 33-50-23, OPS OK.
- [SDR C1HA200397014](https://openairdocs.org/sdr/C1HA200397014.md): Power Supply · inoperative · Oct 19, 2003 · N697CA · Boeing 727270 · Emergency Lighting
  > FOUND EMERGENCY EXIT LIGHT (FLOOR TRACK) INOP FROM ROWS 12 TO 20. REMOVED & REPLACED POWER SUPPLY AT STATION 440. REF MM CH 33-50-23, OPS OK.
- [SDR C1HA200397013](https://openairdocs.org/sdr/C1HA200397013.md): Battery Pack · inoperative · Oct 13, 2003 · N697CA · Boeing 727270 · Emergency Lighting
  > MID CABIN FLOOR EMERGENCY PATH LIGHTING INOP. REMOVED AND REPLACED FORWARD FLOOR POWER SUPPLY AND BATTERY PACK IAW 727 MM 33-50-23. FLOOR EMERGENCY PATH LIGHTING OPS. CHECKS NORMAL.
- [SDR C1HA200397012](https://openairdocs.org/sdr/C1HA200397012.md): Hydraulic System · leaking · Jun 6, 2003 · N697CA · Boeing 727270 · Hydraulic Power System
  > AFTER 1 HR IN FLIGHT SYSTEM A-HYDRAULIC QUANTITY STARTED TO DECREASE, QUANTITY FELL TO 2.3 GALLONS.
- [SDR CH1A200397011](https://openairdocs.org/sdr/CH1A200397011.md): Flap Track · corroded · Apr 18, 2003 · N697CA · Boeing 727270 · Trailing Edge Flaps
  > NR 7 FLAP TRACK CENTER FAIRING AFT FITTING HAS SOME CORROSION.
- [SDR C1HA200397008](https://openairdocs.org/sdr/C1HA200397008.md): Battery · corroded · Feb 22, 2003 · N697CA · Boeing 727270 · Emergency Lighting
  > AFT AIRSTAIR EMERGENCY AREA LIGHT IS INOPERATIVE. CLEANED/REMOVED CORROSION FROM BATTERY CONTACTS & OPS CHECK WAS GOOD. REF: 727 MM 33-50-01.
- [SDR C1HA200397007](https://openairdocs.org/sdr/C1HA200397007.md): Connector · loose · Feb 22, 2003 · N697CA · Boeing 727270 · Light System Wiring
  > RT STA 940 EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. SECURED LOOSE CONNECTOR AT BATTERY PACK IAW 727 MM 33-50-22. OPS CHECK WAS GOOD.

Next page: https://openairdocs.org/model/boeing-727-270/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 = '727270'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-270/reports

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