# Service difficulty reports: Boeing 727-290

A list on [Boeing 727-290](https://openairdocs.org/model/boeing-727-290.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 257 reports

- [SDR CIHA200759026](https://openairdocs.org/sdr/CIHA200759026.md): Support Angle · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Miscellaneous Structure
  > STRINGER 26L TO FRAME SUPPORT ANGLE CORRODED BS 950F. REMOVED SUPPORT ANGLE, FABRICATED AND INSTALLED NEW SUPPORT ANGLE IAW B727 SRM 51-10-3 FIG 2 & 51-30-2 FIG 1.
- [SDR C1HA200795011](https://openairdocs.org/sdr/C1HA200795011.md): Support · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Miscellaneous Structure
  > SURFACE CORROSION ON MAIN CABIN FWD LAV AFT WALL SUPPORT BS 344 RBL 15 - RBL 65. REPLACED LAV SUPPORT BS 344 RBL 15 TO 65 IAW B727 SRM 53-10-2.
- [SDR C1HA200795006](https://openairdocs.org/sdr/C1HA200795006.md): Frame · cracked · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Frame
  > COCKPIT FRAME AT STA 277 AND STR 16RT IS CRACKED APPROX 1 INCH LONG, VERIFED BY HFEC (BEHIND FE CONSOLE). REPAIRED COCKPIT FRAME AT STA 277, STR 16RT IAW B727 SRM 53-10-2 AND 51-40-2.
- [SDR C1HA200795008](https://openairdocs.org/sdr/C1HA200795008.md): Seat Track · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BS 420-480 RBL 55. REPLACED SEAT TRACK FROM BS 420 TO 480 RBL 55 IAW B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 7.
- [SDR CIHA200795010](https://openairdocs.org/sdr/CIHA200795010.md): Seat Track · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BS 344 - 380 RBL 45. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 53-10-2 AND 53-10-5 FIG 7.
- [SDR C1HA200795004](https://openairdocs.org/sdr/C1HA200795004.md): Support Angle · cracked · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Miscellaneous Structure
  > LEFT VENTRAL STAIRWELL LT TORQUE BOX SUPPORT ANGLE IS CRACKED AT STA 1253 BELOW BAZOOKA TUBES. FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 1253 LEFT TORQUE BOX SUPPORT ANGLE MATERIAL USE 7075-T6.050, DIM 8 X 3, IAW B727 SRM 51-40-3 FIG 1 & 53-10-2 FIG 6.
- [SDR C1HA200795001](https://openairdocs.org/sdr/C1HA200795001.md): Angle · cracked · May 4, 2007 · N295AS · Boeing 727290 · Wing Miscellaneous Structure
  > RIGHT WING L/E STA 130.7 INTERNAL ANGLE AT FRONT SPAR LWR CRACKED. FABRICATED AND INSTALLED REPAIR PART IAW B727 M/M 57-20-21 PG 801 AND SEALED AS REQUIRED IAW B727 M/M 51-30-11.
- [SDR C1HA200795021](https://openairdocs.org/sdr/C1HA200795021.md): Angle · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Miscellaneous Structure
  > ANGLE CORRODED RIGHT CUSP ANGLE TO FRAME SPLICE ATTACHED AFT SIDE OF STA 740 RIB AT FLOOR LEVEL STA 740-743 RBL 61. CORROSION FOUND OUT OF LIMITS. REPLACED ANGLE IAW B727 SRM 53-10-2 AND 51-30-2.
- [SDR C1HA200795020](https://openairdocs.org/sdr/C1HA200795020.md): Stringer · cracked · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 15R CRACKED AT BS 720B. REPAIRED STR 15R AT BS 720B IAW B727 SRM 53-10-3 FIG 5.
- [SDR C1HA200795003](https://openairdocs.org/sdr/C1HA200795003.md): Skin · cracked · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Plate/Skin
  > FOUND FUSE BS 1098 RBL 1 HAS 1/2" CRACK IN FASTENER HOLE. CUT OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B727 SB 727-53A0204 REV 3 FIG 2 AND AD 94-05-04-06.2
- [SDR C1HA200795014](https://openairdocs.org/sdr/C1HA200795014.md): Bracket · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Miscellaneous Structure
  > FOUND CORROSION EMANATING FROM BENEATH ANGLE BRACKET O/B OF AFT LAV FITTINGS AT STA 1165 RBL 45. REPLACED BRACKET ANGLE IAW B727 SRM 51-40-3 AND 53-10-2 AND REPAIRED SHEAR WEB IAW B727 SRM 53-10-2 AND 51-40-2.
- [SDR C1HA200795012](https://openairdocs.org/sdr/C1HA200795012.md): Angle · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON WEB ANGLE IN SEVERAL MARKED AREAS BETWEEN STA 1148-1165 RBL 60. REPLACED ANGLE BETWEEN STA 1148 TO 1165 RBL 60 IAW B727 SRM 53-10-2 AND 51-40-3.
- [SDR C1HA200795016](https://openairdocs.org/sdr/C1HA200795016.md): Seat Track · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND SEAT TRACK CORRODED IN SEVERAL MARKED AREAS STA 999-1110 LBL 25. REMOVED AND REPLACED SEAT TRACK ON STA 1010-1130 LBL 25 IAW B727 SRM 51-30-2 AND 53-10-5 FIG 7.
- [SDR C1HA200795033](https://openairdocs.org/sdr/C1HA200795033.md): Stringer Splice · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Longeron/Stringer
  > FOUND FWD CARGO COMPARTMENT AT BS 540 STR 26R HAS HEAVY CORROSION AT SPLICE. REMOVED AND REPLACED FWD CARGO BS 540 STR 26R SPLICE ANGLE IAW B727 SRM 53-10-2 AND 53-40-3.
- [SDR C1HA200795032](https://openairdocs.org/sdr/C1HA200795032.md): Stringer · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION IN E/E BAY AT BS 475 STR 27L. REPAIRED STR 27L AT BS 475 IAW B727 SRM 53-10-2 FIG 9 AND 53-10-3 FIG 1.
- [SDR C1HA200795031](https://openairdocs.org/sdr/C1HA200795031.md): Stringer Splice · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION IN E/E BAY AT BS 475 STR 26L. REMOVED EXISTING MANUFACTURE SPLICE, FABRICATED AND INSTALLED NEW SPLICE IAW B727 SRM 53-10-3 FIG 1.
- [SDR C1HA200795022](https://openairdocs.org/sdr/C1HA200795022.md): Seat Track · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CABIN SEAT TRACK AT BS 740-760 LBL 24 IS CORRODED BEYOND LIMITS. REPLACED MAIN CABIN SEAT TRACK AT BS 740-760 LBL 24 IAW B727 SRM 53-10-2 AND 53-10-5.
- [SDR C1HA200795019](https://openairdocs.org/sdr/C1HA200795019.md): Stringer · cracked · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Longeron/Stringer
  > FOUND STR 15L CRACKED AT BS 720C. REPAIR STR 15L AT BS 720C IAW B727 SRM 53-10-3 FIG 5.
- [SDR C1HA200795024](https://openairdocs.org/sdr/C1HA200795024.md): Floorbeam · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Floor Beam
  > BS 1130 FLOORBEAM AT LOWER FORWARD FLANGE HAS CORROSION (RBL-10). FOUND CORROSION OUT LIMITS, CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLERS, ANGLE, RADIUS FILLER AND STRAP REPAIRS TREATED AND PRIMED IAW B727 SRM 51-10-2, 53-10-1, 53-10-8 AND 51-30-2 FIG 1.
- [SDR C1HA200795027](https://openairdocs.org/sdr/C1HA200795027.md): Stringer · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON FRAME STA 420 BL 0 TO STR 28R. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED AND INSTALLED NEW SECTION FROM BS 400-420 STR 28R IAW B727 SRM 53-10-3 FIG 1.
- [SDR C1HA200795005](https://openairdocs.org/sdr/C1HA200795005.md): Plenum · corroded · May 4, 2007 · N295AS · Boeing 727290 · Wing Miscellaneous Structure
  > A/C RAM AIR PLENUM HAS SURFACE CORROSION ON NR 2 TANK LWR SKIN ABOVE LT PRIMARY HEAT EXCHANGER. BLENDED OUT CORROSION DAMAGE, MAT LOSS.050, ORIGINAL THK.225. FLUORESCENT DYE PENETRANT AREA, NO DEFECTS NOTED. TREATED AND PRIMED AREA IAW B727 SRM 51-10-2.
- [SDR C1HA200795023](https://openairdocs.org/sdr/C1HA200795023.md): Shear Web · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Miscellaneous Structure
  > AFT CABIN LT SHEAR WEB BS 1166 LBL 35 HAS HEAVY PITTED CORROSION. REPAIRED AFT CABIN LT SHEAR WEB AT BS 1166 LBL 35 IAW B727 SRM 53-10-2 AND 51-40-2.
- [SDR C1HA200795009](https://openairdocs.org/sdr/C1HA200795009.md): Seat Track · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON SEAT TRACK BS 380 - 460 RBL 45. REPLACED SEAT TRACK AT BS 380 TO 460 RBL 45 IAW B727 SRM 53-10-2 AND 53-10-5 FIG 7.
- [SDR C1HA200795002](https://openairdocs.org/sdr/C1HA200795002.md): Skin · cracked · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Plate/Skin
  > EXT FUSE BS 303 AT L-1 DOOR LOWER HINGE HAS REPAIR DOUBLER CRACKED IN FWD CUTOUT. REMOVED EXISTING REPAIR DOUBLER, HFEC INSP AND FOUND SKIN AND INNER DOUBLER CRACKED, CRACK APPROX 2 1/4" LONG. CUTOUT DAMAGED AREA IAW B727 SRM 51-10-1. REPAIRED AREA IAW CA E
- [SDR C1HA200795025](https://openairdocs.org/sdr/C1HA200795025.md): Stringer · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION AT STA 740. CUT OUT DAMAGED AREA FROM STR 27L AT STA 740, FAB`D STR REPAIR AND SPLICE. TREATED AND PRIMED. REMOVED AND REPLACED DAMAGED FITTING AT LT STA 740 AT STR 27L. INSTALLED ALL PARTS IAW B727 SRM 53-10-3 FIG 1 AND 51-30-2.
- [SDR C1HA200795029](https://openairdocs.org/sdr/C1HA200795029.md): Frame · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Frame
  > FOUND CORROSION STA 351.2 FRAME AT 28R. REMOVED EXISTING TEE CHORD FRAME, FABRICATED AND INSTALLED NEW TEE CHORD IAW B727 SRM 53-10-2 FIG 1.
- [SDR C1HA200795017](https://openairdocs.org/sdr/C1HA200795017.md): Seat Track · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND MAIN CABIN STA 880 TO 950 LBL 24 SEAT TRACK HAS CORROSION ON TOP SURFACE. FABRICATED AND INSTALLED NEW SEAT TRACK P/N BAC1520-792 (91") IAW B727 SRM 53-10-5 FIG 1.
- [SDR C1HA200795007](https://openairdocs.org/sdr/C1HA200795007.md): Seat Track · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON SEAT TRACK AT AFT CUTOUT AND MOUNT POINT STA 1130 LBL 25. REPLACED SEAT TRACK AT BS 1110-1130 LBL 25, P/N BAC1520-792 IAW B727 SRM 53-10-5 FIG 7.
- [SDR C1HA200795028](https://openairdocs.org/sdr/C1HA200795028.md): Stringer · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION STR 28L AT STA 410. REPAIRED STRINGER AT BS 410 28L IAW B727 SRM 53-10-2 AND 53-10-3 FIG 1.
- [SDR C1HA200795030](https://openairdocs.org/sdr/C1HA200795030.md): Stringer · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION STR 26R STA 470. FABRICATED AND INSTALLED REPAIR PARTS FOR STRINGER 26R BS 450 - 490 IAW B727 SRM 53-10-3 FIG 1.
- [SDR C1HA200795015](https://openairdocs.org/sdr/C1HA200795015.md): Floorbeam · corroded · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Floor Beam
  > FOUND FLOORBEAM CORRODED AT STA 1110 LBL 25-45. REPAIRED FLOORBEAM STA 1110 FROM RBL 20 TO LBL 65 IAW B727 SRM 53-10-8 FIG 3.
- [SDR C1HA200795018](https://openairdocs.org/sdr/C1HA200795018.md): Stringer · cracked · May 4, 2007 · N295AS · Boeing 727290 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 15L CRACKED AT BS 720B. REPAIRED STRINGER 15L AT BS 720B IAW B727 SRM 53-10-3 FIG 5.
- [SDR C1HA200694002](https://openairdocs.org/sdr/C1HA200694002.md): Hydraulic Line · blown · Dec 24, 2006 · N294AS · Boeing 727290 · Hydraulic System, Main
  > ON GEAR RETRACTION LOST ALL SYSTEM QUANTITY AND PRESSURE. FOLLOWED COM RED BORDER AND AMPLIFIED 2.29.2 HYDRAULIC SYSTEM LOSS AND 2.28.4 FUEL DUMPING CHECKLIST RETURNED FOR LANDING IN ISO AT 155,000 LBS. T/S FOUND MLG ACT RETURN LINE BLOWN REMOVED AND INSTALLE
- [SDR C1HA200695003](https://openairdocs.org/sdr/C1HA200695003.md): Valve · stuck · Nov 25, 2006 · N295AS · Boeing 727290 · Compressor Bleed Control
  > NR 1 ENGINE WAS SHUT DOWN ON START-EGT 550 DEG AND IT APPEARED THAT IT WOULD NOT STABILIZE AT OR BELOW 550 DEG. RAN COM 2-72.9 FOUND NR 1 ENG 13 TH STAGE BLEED VALVES STUCK PER CMM 75-30-00 PAGE 603 LUBED 1 ENG. 13 TH STAGE VALVES WITH WC-393. OPS CHECKED N
- [SDR C1HA200695002](https://openairdocs.org/sdr/C1HA200695002.md): Unknown · malfunctioned · Jun 12, 2006 · N295AS · Boeing 727290 · Cabin Pressure Control System
  > AFTER TAKEOFF AC FAILED TO PRESSURIZE, RAN COM PROCEDURE 2.21.5. ON DESCENT EQUIP ENTRY LIGHT FLICKERD, RAN COM PROCEDURE 2.52.3. RETURNED TO DEN. INSPECTED BOTH E+E DOORS, FOUND TO BE SECURED AND INSPECTED E+E SWITCHES, NO DEFECTS NOTED. INSPECTED DUCTING
- [SDR C1HA200695001](https://openairdocs.org/sdr/C1HA200695001.md): Seal · damaged · May 13, 2006 · N295AS · Boeing 727290 · Rudder Miscellaneous Structure
  > ON TAXI INTO DEN, UPPER RUDDER INDICATOR DIDN'T MOVE FULLY TO THE LIMIT LINE WHEN RIGHT RUDDER WAS FULLY APPLIED. LEFT RUDDER OPERATED NORMALLY FOUND FIN FAIRING DAMAGED AT NR 6 SPOT ON RT SIDE. REMOVED AND REPLACED FAIRING AND REMOVED DAMAGED RUDDER BLADE S
- [SDR C1HA200694001](https://openairdocs.org/sdr/C1HA200694001.md): Display · defective · Mar 19, 2006 · N294AS · Boeing 727290 · Weather Radar System
  > RADAR DISPLAYS MAGENTA AND PURPLE COLORS ONLY, AND INTERMITTENTLY INOP. T/S IAW TIB-018 FOUND INDICATOR PAINTS RED/MAGENTA. REMOVED AND REPLACED INDICATOR IAW M/M 34-41-34. OPERATIONAL CHECK NORMAL IAW M/M 34-41-34.
- [SDR C1HA200594012](https://openairdocs.org/sdr/C1HA200594012.md): Actuator · malfunctioned · Dec 23, 2005 · N294AS · Boeing 727290 · Landing Gear Actuator
  > LEFT MAIN GEAR DID NOT RETRACT ON TAKEOFF, BOTH GREEN LIGHT DOWN AND LOCK LIGHTS AND RED DOOR LIGHTS REMAIN ILLUMINATED, RED DISAGREE LIGHT WAS ALSO ILLUMINATED. REMOVED AND REPLACED LT MLG LOCK MECHANISM PER JOB STATUS MM REF 32-32-51, ALL OPS CHECKS NORMAL
- [SDR C1HA200594011](https://openairdocs.org/sdr/C1HA200594011.md): Cap · loose · Nov 25, 2005 · N294AS · Boeing 727290 · Turbine Engine Oil System
  > DURING CLIMB-OUT DFW, NR 1 ENGINE OIL QUANTITY INDICATED CONSTANT DECREASE OIL. LANDED WITH 1.0 GALLONS OIL RETURNED DIRECT, UPON LANDING WITNESSED OIL LEAKING FROM COWLING. FOUND OIL CAP NOT ENGAGED. SERVICED ENGINE INSTALLED NEW OIL CAP REF 12-13-01.
- [SDR C1HA200594010](https://openairdocs.org/sdr/C1HA200594010.md): Support · broken · Oct 17, 2005 · N294AS · Boeing 727290 · Wing, Attach Fittings
  > NR 12 SPOILER ACTUATOR OUTBOARD SUPPORT IS BROKEN WS 510. REMOVED AND REPLACED NR 12 SPOILER ACTUATOR O/B SUPPORT IAW B727 MM 27-61-0 AND SRM 51-30-2 NR 12 SPOILER ACTUATOR, OP CHECK GOOD IAW B727 MM 27-61-0.
- [SDR C1HA200594009](https://openairdocs.org/sdr/C1HA200594009.md): Stiffener · cracked · Oct 17, 2005 · N294AS · Boeing 727290 · Fuselage Miscellaneous Structure
  > RIGHT MLG WHEEL WELL 870 BULKHEAD VERTICAL STIFFENER CRACKED AT KEELBEAM APU CUTOUT. REMOVED AND REPLACED VERTICAL STIFFENER BS 870 RIGHT WHEEL WELL P/N 65-18636-378 IAW 727 SRM 51-30-2. PERFORMED AT KEELBEAM AREA PNEUMATIC LEAK CHECK, NO LEAKS NOTED IAW B72
- [SDR C1HA200594008](https://openairdocs.org/sdr/C1HA200594008.md): Shear Tie · cracked · Oct 17, 2005 · N294AS · Boeing 727290 · Fuselage Internal Mounting Structure
  > RT SIDE OF THE NOSE WHEEL WELL DOGHOUSE FRAME AT STA 312 IS CRACKED. CUT OUT DAMAGED FRAME TO SKIN ATTACHMENT ANGLE FABBED & INSTALLED REPAIR SHEAR TIE IAW 727 SRM 53-10-4 FIG 15.
- [SDR C1HA200594007](https://openairdocs.org/sdr/C1HA200594007.md): Frame · dented · Oct 17, 2005 · N294AS · Boeing 727290 · Fuselage Main, Frame
  > AFT CARGO COMPT FRAME AT STA 950F IS DENTED BETWEEN STR 25L - 026L. FOUND DENT OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. CUT OUT DAMAGE AREA IAW B727 SRM 51-10-1. FABRICATED ANGLE REPAIR IAW B727 SRM 53-10-2 FIG 3 AND 51-20-1. TREATED AND PRIMED PORT AND A
- [SDR C1HA200594006](https://openairdocs.org/sdr/C1HA200594006.md): Skin · bulged · Oct 17, 2005 · N294AS · Boeing 727290 · Fuselage Main, Plate/Skin
  > RT FUSE SKIN BULGED AT NOSE WHEEL WELL LWR CHORD BS 350. REMOVED AND REPLACED DAMAGED NOSE WHEEL WELL RT LWR CHORD P/N 65-19861-8, IAW 727 SRM 51-30-2.
- [SDR C1HA200594004](https://openairdocs.org/sdr/C1HA200594004.md): Skin · punctured · Oct 17, 2005 · N294AS · Boeing 727290 · Electrical/Electronic Compartment Doors
  > E&E BAY COMPARTMENT HATCH INTERIOR SKIN HAS SEVERAL GOUGES & A LARGE PUNCTURE HOLE. CUT OUT DAMAGED AREA, FABBED AND INSTALLED REPAIR FILLER & DOUBLER (7075 T6.050 PO 9002126, DIM 5.375 X 5.125 INCHES IAW SRM 51-40-2 FIG 1.
- [SDR C1HA200594005](https://openairdocs.org/sdr/C1HA200594005.md): Channel · cracked · Oct 17, 2005 · N294AS · Boeing 727290 · Fuselage Main, Attach Fittings
  > NLG LOCK ACTUATOR SUPPORT CHANNEL HAS CRACK INDICATION AT UPPER OUTBOARD HOLE. REMOVED & REPLACED NLG LOCK ACTUATOR SUPPORT CHANNEL IAW B727 SRM 51-30-2, P/N 69-19122-2.
- [SDR C1HA200594003](https://openairdocs.org/sdr/C1HA200594003.md): Skin · cracked · Oct 14, 2005 · N294AS · Boeing 727290 · Fuselage Main, Plate/Skin
  > L1 DOOR LOWER HINGE CUTOUT ON FUSE SKIN IS CRACKED. CUT OUT DAMAGED AREA, FABBED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SB 727-53A0198 REV 2 FIG 3 & 5.
- [SDR C1HA200594002](https://openairdocs.org/sdr/C1HA200594002.md): Carriage · vibration · Jun 1, 2005 · N294AS · Boeing 727290 · Trailing Edge Flaps
  > DURING CLIMB-OUT AT APPROX FL 190, VIBRATION FELT THROUGHOUT A/C. VISUAL INSP FOUND LT TE FLAP VIBRATING AS BEFORE (LOG PAGE 3059). VIBRATION PERSISTED FROM 310 KIAS TO 250 KIAS. FUEL DUMPED (APPROX 4000 LBS) AND AIR RETURN TO MMUN. REF LP C03060 ITEM 3.
- [SDR C1HA200594001](https://openairdocs.org/sdr/C1HA200594001.md): Roller · out of adjust · Jun 1, 2005 · N294AS · Boeing 727290 · Trailing Edge Flaps
  > ON CLIMBOUT APPROX 200, CREW BEGAN TO FEEL VIBRATION. ALL ENGINE INDICATIONS NORMAL. BEGAN TROUBLESHOOTING AND UPON VISUAL INSP FOUND LT INBOARD T/E FLAPS FLUTTERING APPROX 4 TO 5 INCHES AT SPEEDS ABOVE APPROX 290 KIAS. DECISION MADE TO AIR RETURN TO MMUN M
- [SDR C1HA200595007](https://openairdocs.org/sdr/C1HA200595007.md): Connector · loose · May 5, 2005 · N295AS · Boeing 727290 · Engine Pressure Ratio (EPR)
  > UPON APPLICATION OF T/O THRUST (FULL), NR 1 ENGINE WOULD NOT MAKE FULL EPR OF 2.14 ONLY 2.05. ALL OTHER PARAMETERS IN YELLOW ARC + POWER LEVER AT FORWARD STOP. ENGINES 2 + 3 POWER LEVERS APPROX 1 1/2 KNOBS BEHIND NR 1 POWER LEVER. (TEMP 31DEG C) ADJUSTED NR

Next page: https://openairdocs.org/model/boeing-727-290/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 = '727290'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-290/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.