# Service difficulty reports: Boeing 727-2J4

A list on [Boeing 727-2J4](https://openairdocs.org/model/boeing-727-2j4.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 15 · 741 reports

- [SDR C1HA200796013](https://openairdocs.org/sdr/C1HA200796013.md): Flap System · malfunctioned · Oct 21, 2007 · N696CA · Boeing 7272J4 · Trailing Edge Flap Control System
  > UPON FLAP RETRACTION LE FLAP NR 6 DID NOT RETRACT. DISPATCH AND MC NOTIFIED. RETURN TO STL, REMOVED AND REPLACED NR 6 FLAP ACT IAW 27-81-22. OPS AND LEAK CK NORMAL.
- [SDR C1HA200796012](https://openairdocs.org/sdr/C1HA200796012.md): Wheel · fractured · Jul 22, 2007 · N696CA · Boeing 7272J4 · Wheel/Ski/Float
  > WHILE PERFORMING MX TAXI I/B ANTISKID LIGHT ILLUMINATED A/C TAXIED DIFFICULT STOPPED A/C AND FOUND NR 1, 2, 4 TIRES FLAT NR 3 TIRE MISSING AC REMOVED FROM SERVICE FOR REPAIRS, STATUS REMAINS OPEN.
- [SDR C1HA200796007](https://openairdocs.org/sdr/C1HA200796007.md): Stringer · corroded · May 29, 2007 · N696CA · Boeing 7272J4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 26R TENSION FITTING AT 1183. REMOVED AND REPLACED BS 1183 STR 26L TENSION FITTING PN 65-24276-24 IAW B727 SRM 51-30-2.
- [SDR C1HA200796006](https://openairdocs.org/sdr/C1HA200796006.md): Stringer · corroded · May 29, 2007 · N696CA · Boeing 7272J4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 26L TENSION FITTING AT 1183. REMOVED AND REPLACED BS 1183 STR 26L TENSION FITTING PN 65-24276-24 PO NR 720764 IAW B727 SRM 51-30-2.
- [SDR C1HA200796002](https://openairdocs.org/sdr/C1HA200796002.md): Skin · corroded · May 29, 2007 · N696CA · Boeing 7272J4 · Wing, Plate/Skin
  > LT LOWER WING SURFACE APPROX BS 800 IN RAM AIR AREA IS CORRODED (PLENUM). BLENDED OUT DAMAGED AREA AND REPAIRED IAW EO-727-5710-04 REV IR.
- [SDR C1HA200796001](https://openairdocs.org/sdr/C1HA200796001.md): Attach Fitting · corroded · May 29, 2007 · N696CA · Boeing 7272J4 · Wing, Attach Fittings
  > LEFT WING NR 2 FLAP TRACK FWD ATTACH FITTING CORRODED AT LUG FACE. REMOVED L/W NR 2 FLAP TRACK FWD ATTACH FITTING AND MACHINED FITTING CORRODED FACE PER SOPM 20-10-02. TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED IAW B727 SRM 51-30-2 FIG 15.
- [SDR C1HA200796003](https://openairdocs.org/sdr/C1HA200796003.md): Pan · corroded · May 29, 2007 · N696CA · Boeing 7272J4 · Fuselage Miscellaneous Structure
  > AFT LAV SERVICE PAN AT RT BS 1170 IS DAMAGED AND CORRODED BEYOND LIMITS. DRILLED NEW PAN PN 65-25815-2 AND INSTALLED PAN IAW B727 MM 51-30-*2 FIG 1 AND 15. LEAKED CHECK OK PER B727 MM 38-32-11.
- [SDR C1HA200796011](https://openairdocs.org/sdr/C1HA200796011.md): Frame · corroded · May 29, 2007 · N696CA · Boeing 7272J4 · Fuselage Main, Frame
  > CORROSION STA 312 AT DOGHOUSE, RT. REPAIRED FRAME AS REQUIRED IAW B727 SRM 53-10-4 FIG 14.
- [SDR C1HA200796005](https://openairdocs.org/sdr/C1HA200796005.md): Stringer · corroded · May 29, 2007 · N696CA · Boeing 7272J4 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 27R AT STA 740. REPAIRED STRINGER 27R AT STA 740 IAW B727 SRM 53-10-3 FIG 7.
- [SDR C1HA200796010](https://openairdocs.org/sdr/C1HA200796010.md): Stringer · corroded · May 29, 2007 · N696CA · Boeing 7272J4 · Fuselage Main, Longeron/Stringer
  > CORROSION STA 312 ON STRINGER 21R. CUT OUT DAMAGED AREA OF STR 21R AND REPAIRED STRINGER 21R IAW B727 SRM 53-10-3 FIG 1.
- [SDR C1HA200796009](https://openairdocs.org/sdr/C1HA200796009.md): Tension Tie · corroded · May 29, 2007 · N696CA · Boeing 7272J4 · Fuselage Internal Mounting Structure
  > AFT CARGO AT BS 1186 TENSION TIE FITTING AT STR 22L IS CORRODED. REMOVED DAMAGED FITTING AND INSTALLED NEW TENSION TIE FITTING PN 65-24276-26, IAW B727 SRM 51-30-2 FIG 15.
- [SDR C1HA200796008](https://openairdocs.org/sdr/C1HA200796008.md): Stringer · corroded · May 29, 2007 · N696CA · Boeing 7272J4 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STR 22L AT BS 1183 IS CORRODED. CUT OUT DAMAGED SECTION OF STRINGER 22L AND REPAIRED IAW B727 SRM 53-10-3 FIG 1.
- [SDR C1HA200796004](https://openairdocs.org/sdr/C1HA200796004.md): Support Bracket · cracked · May 29, 2007 · N696CA · Boeing 7272J4 · Entrance Stairs
  > AFT AIRSTAIR AREA STA 1263 RT ANGLE SUPPORT BRACKET IS CRACK APPROX 1/2 INCH LONG INSIDE LIGHTNING HOLE. REMOVED CRACKED SUPPORT ANGLE ON AFT AIRSTAIR STA 1263 RT AND REPLACED WITH NEW IAW B727 SRM 51-30-5 FIG 1 AND 51-30-2.
- [SDR AU510001528](https://openairdocs.org/sdr/AU510001528.md): Bear Strap · corroded · Dec 12, 2005 · Boeing 7272J4 · Fuselage Main, Plate/Skin
  > NR 3 CARGO DOOR BEAR STRAP INNER SURFACE CORRODED.
- [SDR AU510001527](https://openairdocs.org/sdr/AU510001527.md): Pressure Panel · corroded · Dec 12, 2005 · Boeing 7272J4 · Fuselage Main, Bulkhead
  > FUSELAGE STRUCTURE PRESSURE WEB CORRODED. WEB IS LOCATED AT FS 46 IN THE MAIN LANDING GEAR WHEEL WELL.
- [SDR AU510001492](https://openairdocs.org/sdr/AU510001492.md): Skin · corroded · Dec 12, 2005 · Boeing 7272J4 · Fuselage Main, Plate/Skin
  > CABIN WING CENTER SECTION UPPER SKIN PANEL CORRODED. PANEL IS LOCATED AT FS 822 RBL12.
- [SDR AU510001744](https://openairdocs.org/sdr/AU510001744.md): Bearing · collapsed · Oct 8, 2005 · Boeing 7272J4 · Drag Control System
  > GROUND SPOILER QUADRANT UPPER AND LOWER BEARINGS COLLAPSED. SPOILER DIFFERENTIAL MIXER P/N 10-60841-8 ROUGH IN OPERATION.
- [SDR C1HA200596010](https://openairdocs.org/sdr/C1HA200596010.md): Shear Tie · corroded · May 6, 2005 · N696CA · Boeing 7272J4 · Fuselage Internal Mounting Structure
  > STA 304 LOWER LT FRAME SHEAR TIE HAS CORROSION. REPAIRED SHEAR TIE PER SRM 53-10-4.
- [SDR C1HA200596011](https://openairdocs.org/sdr/C1HA200596011.md): Longeron · corroded · Apr 27, 2005 · N696CA · Boeing 7272J4 · Fuselage Main, Longeron/Stringer
  > E&E COMPT STA 440 LONGERON 26R, CORRODED. CENTER AND BOTTOM OF LONGERON UNDER FRAME REPLACED STRINGER FROM STA 429 TO 431 IAW SRM 53-10-2 FIG 1.
- [SDR C1HA200596009](https://openairdocs.org/sdr/C1HA200596009.md): Frame · corroded · Apr 26, 2005 · N696CA · Boeing 7272J4 · Fuselage Main, Frame
  > FUSELAGE INTERIOR STA 312 LOWER LT HORIZONTAL WALKBEAM, AND FRAME CORRODED (GENERATING ITEM C53-111-03-02) FUSELAGE INTERIOR STA 304 - LOWER LT FRAME HAS CORROSION. REPAIRED CHORD PER CAEO 727-5316-02 AND SRM 53-10-4 FIG 7.
- [SDR C1HA200596007](https://openairdocs.org/sdr/C1HA200596007.md): Floorbeam · corroded · Apr 25, 2005 · N696CA · Boeing 7272J4 · Fuselage Main, Floor Beam
  > MAIN PASSENGER CABIN STA 344 LBL 19 TO 57 FLOORBEAM TOP CORRODED.
- [SDR C1HA200596006](https://openairdocs.org/sdr/C1HA200596006.md): Floor Support · corroded · Apr 23, 2005 · N696CA · Boeing 7272J4 · Fuselage Miscellaneous Structure
  > MAIN PASSENGER CABIN B/L 15L STA 1137 FLOOR SUPPORT CORRODED.
- [SDR C1HA200596005](https://openairdocs.org/sdr/C1HA200596005.md): Floorbeam · corroded · Apr 22, 2005 · N696CA · Boeing 7272J4 · Fuselage Main, Floor Beam
  > MAIN PASSENGER CABIN STA 1030 LBL 24 TO RBL 24 TOP OF FLOORBEAM CORRODED.
- [SDR C1HA200596004](https://openairdocs.org/sdr/C1HA200596004.md): Floorbeam · corroded · Apr 22, 2005 · N696CA · Boeing 7272J4 · Fuselage Main, Floor Beam
  > MAIN PASSENGER CABIN STA 1130 LBL 26 TO 46 TOP OF FLOORBEAM CORRODED.
- [SDR C1HA200596003](https://openairdocs.org/sdr/C1HA200596003.md): Intercostal · corroded · Apr 22, 2005 · N696CA · Boeing 7272J4 · Fuselage Miscellaneous Structure
  > MAIN PASSENGER CABIN STA 304 TO 312 RBL 45, UNDER CONTROL CABIN BULKHEAD BOTTOM ANGLE, INTERCOSTAL CORRODED FWD END.
- [SDR C1HA200596002](https://openairdocs.org/sdr/C1HA200596002.md): Intercostal · corroded · Apr 22, 2005 · N696CA · Boeing 7272J4 · Fuselage Miscellaneous Structure
  > MAIN PASSENGER CABIN STA 304 TO 312 RBL 55, UNDER CONTROL CABIN BULKHEAD BOTTOM ANGLE, INTERCOSTAL CORRODED FWD END.
- [SDR C1HA200596008](https://openairdocs.org/sdr/C1HA200596008.md): Skin · bulged · Apr 21, 2005 · N696CA · Boeing 7272J4 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE BULGE IN SKIN FWD EDGE OF NOSE JACK PAD FOUND CORROSION ON THE INTERNAL DOUBLER. REMOVED AND REPLACED INTERNAL DOUBLER AT THE NOSE JACK PAD SRM 53-30-3 FIG 3.
- [SDR C1HA200596012](https://openairdocs.org/sdr/C1HA200596012.md): Stringer · corroded · Apr 13, 2005 · N696CA · Boeing 7272J4 · Fuselage Main, Longeron/Stringer
  > FWD ASSY COMP STA 312, STRINGER 27L IS CORRODED UNDER FRAME (C53-111-03-02) STRINGER SPLICE REPAIR IAW SRM 53-10-3 FIG 3.
- [SDR CIHA200596001](https://openairdocs.org/sdr/CIHA200596001.md): Indicator · malfunctioned · Feb 24, 2005 · N696CA · Boeing 7272J4 · Integrated Flight System
  > CAPTAINS ADI SHOWED A 5 DEG BANK TURN TO THE LEFT WITH AIRCRAFT NOT IN A TURN ATTITUDE FLAG IN VIEW, WHEN DUMP VALVES WERE OPENED TANK NR 2 RT FWD AND LF AFT BOOST PUMP C/B'S POPPED, TANK NR 3 DUMP VALVE INTRANSIT LIGHT DID NOT ILLUMINATE WHEN THE VALVE SWITCH
- [SDR AUS20040048](https://openairdocs.org/sdr/AUS20040048.md): Door Frame · cracked · Jan 29, 2004 · Boeing 7272J4 · Fuselage Main, Structure
  > (AUS) AFT CARGO DOOR CUTOUT FRAME LOCATED AT BS 1090 RIB BL28 CRACKED. CRACK LENGTH 8.255MM (0.325IN).
- [SDR P9RA20040001](https://openairdocs.org/sdr/P9RA20040001.md): Light · inoperative · Jan 12, 2004 · N288SC · Boeing 7272J4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. IN FLIGHT COMPARTMENT IAW BMM 33-50-01.
- [SDR C1HA200396020](https://openairdocs.org/sdr/C1HA200396020.md): Engine · leaking · Dec 5, 2003 · N696CA · Boeing 7272J4 · Turbine Engine Oil System
  > OIL QUANTITY DECREASED TO.1 GALLONS IN FLIGHT. OIL TEMP 112 AT POWER PRESSURE 49. AIRCRAFT DIVERTED INTO DFW. MAINTENANCE FOUND OIL COMING OUT OF THE COMBUSTION DRAIN, ENGINE CHANGE IN PROGRESS.
- [SDR 2003F00646](https://openairdocs.org/sdr/2003F00646.md): Power Supply · inoperative · Nov 14, 2003 · N288SC · Boeing 7272J4 · Emergency Lighting
  > MAIN CABIN DOOR, SERVICE DOOR AND FORWARD, BULKHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. (M)
- [SDR AUS20031137](https://openairdocs.org/sdr/AUS20031137.md): Switch · faulty · Nov 11, 2003 · Boeing 7272J4 · Leading Edge Slat Position Indicating System
  > (AUS) NR 5 LEADING EDGE KRUEGER FLAP POSITION SWITCH FAULTY.
- [SDR C1HA200396019](https://openairdocs.org/sdr/C1HA200396019.md): Door · not closed · Oct 26, 2003 · N696CA · Boeing 7272J4 · Service Doors
  > SHORTLY AFTER TAKEOFF A LOUD NOISE FROM AIRCRAFT FORWARD WAS HEARD. THE AIRCRAFT WAS NOT PRESSURIZING. THE 1R DOOR APPEARED NOT TO BE PROPERLY SEALED. NO DOOR LIGHTS WHERE ILLUMINATED ON THE F/E'S PANEL. AN EMERGENCY WAS DECLARED. FUEL WAS DUMPED, LANDING
- [SDR AUS20031072](https://openairdocs.org/sdr/AUS20031072.md): Circuit Breaker · failed · Oct 23, 2003 · Boeing 7272J4 · AC Power Distribution System
  > (AUS) PACK COOLING FAN CIRCUIT BREAKER (C) PHASE TERMINAL OVERHEATED.
- [SDR AUS20031033](https://openairdocs.org/sdr/AUS20031033.md): Sealant · deteriorated · Oct 4, 2003 · Boeing 7272J4 · Fuel Storage
  > (AUS) NR 2 FUEL TANK LEAKING. INVESTIGATION FOUND TANK WING TO CENTERBOX LOWER ATTACHMENT FITTING INBOARD FASTENER SEALANT LIFTING. REMOVED SEALANT FOUND TO HAVE INCLUSIONS AND VOIDS RESULTING FROM IMPROPER CLEANING AT PREVIOUS SEALANT APPLICATION.
- [SDR C1HA200396018](https://openairdocs.org/sdr/C1HA200396018.md): Module · malfunctioned · Aug 29, 2003 · N696CA · Boeing 7272J4 · Landing Gear Position and Warning
  > ON DEP NOSEGEAR UNSAFE LT REMAINED ILLUM ON GEAR RETRACT. CYCLED GEAR, THEN TO OFF POSITION, NO CHANGE. VISUALLY VERIFIED NOSEGEAR DOOR CLOSED. THROUGH TELE CONFERANCE, CONFIRMED THAT IT IS RED NOSE GEAR LIGHT THAT ILLUMINATED. NOT NOSE GEAR DOOR LT. INPECT W
- [SDR C1HA200396017](https://openairdocs.org/sdr/C1HA200396017.md): Accessory Unit · malfunctioned · Aug 28, 2003 · N696CA · Boeing 7272J4 · Landing Gear Position and Warning
  > ON GEAR RETRACTION AT STL, RED NOSE GEAR LIGHT REMAINED ILLUMINATED. CYCLED GEAR HANDLE UP - LIGHT REMAINED ON (CONT) ON ARRIVAL AT LAS. RED LIGHT EXTINGUSHIED WITH GEAR EXTENTION. RED NOSE GEAR LIGHT FLICKERED ON & OFF DURING TAXI INSPECTED NOSE GEAR WIRING
- [SDR C1HA200396016](https://openairdocs.org/sdr/C1HA200396016.md): Wire · chafed · Aug 28, 2003 · N696CA · Boeing 7272J4 · Light System Wiring
  > RED (NOSE GEAR) DISAGREEMENT LIGHT REMAINED ILLUMINATED AFTER RETRACTION IN MDJ. LIGHT EXTINGUISHED WHEN GEAR LEVER WAS PLACED TO OFF FOUND CHAFFED WIRE COMING FROM LOCK SWITCH, WIRE WAS RUBBING ON AFT WALL OF WHEEL WELL, REPAIRED AND SECURED WIRE. SYS CHECK G
- [SDR C1HA200396015](https://openairdocs.org/sdr/C1HA200396015.md): Switch · contaminated · Aug 28, 2003 · N696CA · Boeing 7272J4 · Landing Gear Position and Warning
  > BOTH RED (NOSE GEAR) DISAGREEMENT LIGHT AND GREEN (NOSE GEAR) DOWN/LOCKED LIGHT ILLUMINATED. NOSE GEAR LOCK AND POS SWITCHES ADJUSTMENT TEST DONE AFTER FOUND SW CONTAMINATED AND SAME CLEANED. IND NORMAL.MM 32-61-71.
- [SDR C1HA200396010](https://openairdocs.org/sdr/C1HA200396010.md): Seat Track · corroded · May 20, 2003 · N696CA · Boeing 7272J4 · Fuselage, Seat/Cargo Attach Fittings
  > PITTING CORROSION AND GOUGING ON NR 3 SEAT TRACK AT RBL 22 BETWEEN BS 690 & 740.
- [SDR C1HA200396009](https://openairdocs.org/sdr/C1HA200396009.md): Seat Track · corroded · May 20, 2003 · N696CA · Boeing 7272J4 · Fuselage, Seat/Cargo Attach Fittings
  > PITTING CORROSION AND GOUGING ON NR 2 SEAT TRACK AT LBL 22 BETWEEN BS 480 & 620.
- [SDR C1HA200396008](https://openairdocs.org/sdr/C1HA200396008.md): Seat Track · corroded · May 20, 2003 · N696CA · Boeing 7272J4 · Fuselage, Seat/Cargo Attach Fittings
  > PITTING CORROSION AND GOUGING ON NR 1 SEAT TRACK AT LBL 44 BETWEEN BS 380 & 480.
- [SDR C1HA200396007](https://openairdocs.org/sdr/C1HA200396007.md): Seat Track · gouged · May 20, 2003 · N696CA · Boeing 7272J4 · Fuselage, Seat/Cargo Attach Fittings
  > GOUGING ON NR 1 SEAT TRACK AT LBL 44 BETWEEN BS 344 & 380.
- [SDR C1HA200396011](https://openairdocs.org/sdr/C1HA200396011.md): Seat Track · corroded · May 20, 2003 · N696CA · Boeing 7272J4 · Fuselage, Seat/Cargo Attach Fittings
  > PITTING CORROSION AND GOUGING ON NR 4 SEAT TRACK AT RBL 44 BETWEEN BS 690 & 740
- [SDR C1HA200396012](https://openairdocs.org/sdr/C1HA200396012.md): Seat Track · corroded · May 20, 2003 · N696CA · Boeing 7272J4 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN SEAT TRACK RBL 45 HAS NUMEROUS AREAS OF PITTING CORROSION BETWEEN BS 955F AND 1070
- [SDR C1HA200396005](https://openairdocs.org/sdr/C1HA200396005.md): Seat Track · corroded · May 19, 2003 · N696CA · Boeing 7272J4 · Fuselage, Seat/Cargo Attach Fittings
  > PITTING CORROSION AND GOUGING ON NR 2 SEAT TRACK AT LBL22, BETWEEN BS 480 & 620.
- [SDR AUS20030312](https://openairdocs.org/sdr/AUS20030312.md): Drive Shaft · failed · Feb 27, 2003 · Boeing 7272J4 · Turbine Engine Accessory Drive
  > (AUS) NR 1 ENGINE TOWER DRIVE SHAFT FAILED.
- [SDR C1HA200396003](https://openairdocs.org/sdr/C1HA200396003.md): Switch · malfunctioned · Feb 27, 2003 · N696CA · Boeing 7272J4 · Landing Gear Door Retract Section
  > DURING TAXI IN LAS NOSE GEAR DOOR LIGHT ILLUMINATED. OPENED NOSE GEAR DOORS AND INSPECTED DOOR LOCK SWITCH. ADJUSTED NOSE GEAR DOOR ADJ. STRUT & OPS CHECKED DOORS IN REF. TO M/M CH 32-22-01 OPS NORMAL

Next page: https://openairdocs.org/model/boeing-727-2j4/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 = '7272J4'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-2j4/reports

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