# Service difficulty reports: Boeing 727

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

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 156 reports

- [SDR K11A2021092700077](https://openairdocs.org/sdr/K11A2021092700077.md): Gauge · failed · Sep 25, 2021 · N726CK · Boeing 727* · Engine Indicating System
  > R AND R #2 EGT GAUGE. PERFORMED OPS CHECK IAW B727 AMM 77-21-00 AND 77-21-51.
- [SDR CA110810008](https://openairdocs.org/sdr/CA110810008.md): Flap System · malfunctioned · Aug 8, 2011 · Boeing 727* · Trailing Edge Flap Control System
  > AFTER TAKEOFF WHEN MOVING FLAPS FROM 5 TO 2,THE INBD FLAPS REMAINED AT 5. SUPP PROCEDURE COMPLETED USING ALT FLAPS, AND RETURNED. SYS WAS INSPECTED & FUNCTION CHECKED FOR CORRECT OPERATION, ALL OK IAW AMM 27-51-00 PRIOR TO LUBING THE INBD & OTBD FLAP JACKSCR
- [SDR FOTR2111712446](https://openairdocs.org/sdr/FOTR2111712446.md): Structure · cracked · Jul 13, 2011 · N899AA · Boeing 727 · Vertical Stabilizer
  > VERTICAL STAB, L/E HAS CRACKED DOUBLER TOP OF FWD SPAR CHORD CENTER, JUST AFT OF ELEVATOR CONTROL CABLE QUADRANT. REPAIRED ON FASI WO 21117, NR 12446.
- [SDR CA100216017](https://openairdocs.org/sdr/CA100216017.md): Frame · cracked · Aug 21, 2009 · Boeing 727* · Fuselage, Landing Gear Attach Fittings
  > (CAN) DVI OF NLG BAY APPROX BS 328 FOUND RT TRUNNION SUPPORT FITTING A FRAME CRACKED ABOUT 3 INCHES LONG IN THE UPPER PORTION OF THE A FRAME. REPAIR WAS COMPLIED IAW SRM. (TC 20100216017)
- [SDR 2009FA0000003](https://openairdocs.org/sdr/2009FA0000003.md): Brake Assy · damaged · Jan 5, 2009 · Boeing 727* · Landing Gear Brake System
  > BRAKE, WHEEL, AND TIRE CAME INTO THE SHOP WITH SEVERE DAMAGE THAT OCCURRED WHILE INSTALLED ON THE ACFT. ACCORDING TO THE PRELIMINARY INSP PERFORMED IN THE SHOP, THE BRAKE'S, NR5 ROTOR LINK BROKE, CAUSING THE ROTOR TO SPREAD AND CAUSE DAMAGE NOT ONLY TO THE BRA
- [SDR DU4R2008189](https://openairdocs.org/sdr/DU4R2008189.md): Frame · dented · Jan 21, 2008 · N289MT · Boeing 727 · Fuselage Main, Frame
  > S/O 304002 N/R 26446 DEEP DENT AT FLANGE AREA BS 720A S24 - 25L IN FWD PIT LT SIDE. REPAIRED BY CUTTING OUT DENT, FABRICATED FRAME REPAIR 8.5 INCH X 3 INCH X 1 INCH FROM 7075-T6.063 INCH IAW SRM 51-40-3 FIG. 1, 51-30-2 AND 51-10-2 PARA. 2.
- [SDR DU4R2008190](https://openairdocs.org/sdr/DU4R2008190.md): Skin · damaged · Jan 11, 2008 · N289MT · Boeing 727 · Fuselage Main, Plate/Skin
  > S/O 304002 N/R 26068 DEEP TOOL MARKS (5 EA) IN EXT. FUSELAGE SKIN AT BS 1123 FWD OF OUTFLOW VALVE RT SIDE. REPAIRED 5 EA TOOL MARKS BY CUTTING OUT AREA, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER 11 INCH X 10-3/4 INCH FROM 2024-T3.071 INCH AND 2024-T3
- [SDR AMTA200600523](https://openairdocs.org/sdr/AMTA200600523.md): Battery · discharged · Aug 17, 2006 · N403TZ · Boeing 727* · Emergency Equipment
  > FWD CABIN EMERGENCY FLASHLIGHT (TEST) RED LIGHTS NOT FLASHING. REMOVED AND REPLACED BOTH FWD FLASHLIGHT BATTERY AND SEAL IAW AMM, BOTH FWD FLASHLIGHTS TEST GOOD. (K)
- [SDR 05FDEA04183](https://openairdocs.org/sdr/05FDEA04183.md): Floorbeam · corroded · Dec 8, 2005 · N486FE · Boeing 727* · Fuselage Main, Floor Beam
  > AFT PIT MAIN DECK FLOORBEAM HAS CORROSION STA BS 1130 LBL67.0 REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-10-6 AND 53-10-1. FABRICATED REPAIR PARTS IAW B727 SRM 53-10-8 FIGURE 10. ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2.IN
- [SDR 05FDEA04176](https://openairdocs.org/sdr/05FDEA04176.md): Floorbeam · corroded · Dec 8, 2005 · N486FE · Boeing 727 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM HAS CORROSION AT FASTENER HOLES AT STA BS1130 BETWEEN RBL14 AND RBL40. REPAIRED OUT OF LIMTS SECTION OF STA BS 1130 FLOORBEAM IAW SRM 53-10-8 FIGURE 10. ALODINED AND PRIMED BARE METAL AREAS IAW SRM 51-10-2. INSTALLED REPAIR WITH WET
- [SDR 05FDEA04175](https://openairdocs.org/sdr/05FDEA04175.md): Floorbeam · corroded · Dec 8, 2005 · N486FE · Boeing 727 · Fuselage Main, Floor Beam
  > FORWARD CARGO COMPARTMENT STA BS 620 BOTTOM SURFACE OF FLOORBEAM UPPER TEE CAP HAS CORROSION AROUND SCREW HOLES LBL50 TO RBL50. REMOVED DAMAGED SECTION OF TEE CAP AT STA BS 620 BETWEEN LBL45 AND RT CUSP. FABRICATED NEW TEE CAP, SPLICES, SHIMS: ALODINED AND
- [SDR 05FDEA04174](https://openairdocs.org/sdr/05FDEA04174.md): Floorbeam · corroded · Dec 8, 2005 · N486FE · Boeing 727* · Fuselage Main, Floor Beam
  > AFT PIT MAIN DECK FLOORBEAM HAS CORROSION AT FASTENER CLIP AT STA, BS 950F, LBL21.0. REMOVED CORROSION IAW SRM 51-10-6 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIGURE 4. REMOVED AND REPLACED FLOORBEAM UPPER TEE CAP SECTION FROM LBL8 TO LBL70 IAW STAND
- [SDR 05FDEA04147](https://openairdocs.org/sdr/05FDEA04147.md): Structure · damaged · Dec 5, 2005 · N486FE · Boeing 727* · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR, LOWER CHORD, UPPER TEE CAP AT STA BS 950D TO BS 950E, ABOVE STRINGER 27-R HAS SEVERAL HOLES WITH NO EDGE DISTANCE AND MINIMUM SPACING. REPAIRED DAMAGED CHORD IAW B727 SRM 51-40-4 FIGURE 1. REMOVED AND REINSTALLED 4 EACH CHORD FITTINGS, FI
- [SDR 05FDEA02575](https://openairdocs.org/sdr/05FDEA02575.md): Skin · damaged · Aug 19, 2005 · N479 · Boeing 727 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN DAMAGED AFT OF SECTION 41 AROUND STRINGER 19 LT, REMOVED DAMAGE FABRICATED REPAIR DOUBLER FILLER AND INSTALLED IAW SRM 53-30-3 FIG 24. PREP AND PAINTED AREA I.A.W. M/M 51-20-151-7. THIS IS A CLASS B REPAIR WITH AN INSPECTION THRESHOL
- [SDR 2005FA0001040](https://openairdocs.org/sdr/2005FA0001040.md): Piston · broken · Jun 23, 2005 · Boeing 727* · Leading Edge Slat Actuator
  > PISTON BROKE AT THE KEY GROVE, FATIGUE. (196962/FXS) (K)
- [SDR 2005FA0000911](https://openairdocs.org/sdr/2005FA0000911.md): Cap · cracked · May 25, 2005 · Boeing 727* · Landing Gear Door Actuator
  > CAP IS CRACKED IN BOTTOM OF PORT C. CAP IS TOO WEAK. MAKE CAP STRONGER. (K) (REF: 195902/FXS)
- [SDR 2005FA0000804](https://openairdocs.org/sdr/2005FA0000804.md): Seat · damaged · May 23, 2005 · Boeing 727* · Fire Bottle, Fixed
  > RECEIVED APU FIRE EXTINGUISHER FOR OVERHAUL AFTER FIRING. DURING THE DISASSEMBLY, IT WAS DISCOVERED THAT THE PYROTECHNIC CARTRIDGE MELTED THE STAINLESS STEEL BOTTLE’S SEAT RENDERING THE PRESSURE VESSEL SCRAP. THIS TYPE OF DAMAGE IS CONSISTENT WITH PREVIOUSLY
- [SDR 2005FA0000910](https://openairdocs.org/sdr/2005FA0000910.md): Housing · broken · Apr 20, 2005 · Boeing 727* · Leading Edge Slat Actuator
  > AIRCRAFT RETURNED FROM A FLIGHT WITH HYDRAULIC FLUID LEAKING FROM ACTUATOR. FLIGHT ENGINEER WALK AROUND, FOUND BODY END BROKE OFF AT RETAINER END. UNKNOWN, THIS IS A NEW AND IMPROVED POST SB BODY. (K) (REF: 194950/LEB)
- [SDR 05FDEA00631](https://openairdocs.org/sdr/05FDEA00631.md): Lamp · malfunctioned · Mar 24, 2005 · N258FE · Boeing 727* · Fire Detection
  > LOWER CARGO SMOKE LIGHT ILLUMINATED ON T/O AT 90 KTS, RTO- NO OTHER INDICATION ON CARGO PANEL OR BELL. BOTH FWD AFT COMPARTMENTS CHECK CLEAR. RELAMPED INDICATOR OPS TEST NORMAL IAW MM 26-17-012-2 OK FOR SERVICE.
- [SDR 2005FA0000078](https://openairdocs.org/sdr/2005FA0000078.md): Housing · cracked · Jan 10, 2005 · Boeing 727* · Landing Gear Retraction/Extension System
  > CRACKED THROUGH THREADS IN CYL 1 PORT. FATIGUE, STRONGER BODY. MECHANIC JW2, JOB NR 191405. (K)
- [SDR 2005FA0000077](https://openairdocs.org/sdr/2005FA0000077.md): Cylinder · cracked · Jan 10, 2005 · Boeing 727* · Landing Gear Retraction/Extension System
  > CRACKED THROUGH THREADS IN CYL 1 PORT. FATIGUE, STRONGER BODY. MECHANIC JW2, JOB NR 191407. (K)
- [SDR 2005FA0000076](https://openairdocs.org/sdr/2005FA0000076.md): Cylinder · cracked · Jan 10, 2005 · Boeing 727* · Landing Gear Retraction/Extension System
  > CRACKED THROUGH THREADS IN CYL 1 PORT. FATIGUE, STRONGER BODY. MECHANIC JW2, JOB NR 191413. (K)
- [SDR C1HA200476004](https://openairdocs.org/sdr/C1HA200476004.md): Floorbeam · corroded · Aug 4, 2004 · N676MG · Boeing 727* · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM STA 1010 LBL 0 - 15 LBL. CLEAN, TREAT & INSTALLED REPAIR DOUBLER.
- [SDR 2004F00095](https://openairdocs.org/sdr/2004F00095.md): Wheel · cracked · Mar 25, 2004 · N495 · Boeing 727 · Wheel/Ski/Float
  > RETURNED, TO REPAIR SHOP, WHEEL/ TIRE ASSY REMOVED FOR LOSS OF TIRE PRESSURE,CAUSED BY SEVERE CRACK TO OUTBOARD WHEEL HALF.(REURNING FRACTURED PART TO MFG. FOR ANALYSIS)
- [SDR GAIA03025SP](https://openairdocs.org/sdr/GAIA03025SP.md): Stringer · cracked · Jul 19, 2003 · N281KH · Boeing 727* · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND MAIN CABIN FORWARD STATION 720C, STRINGER 15L IS CRACKED AFT OF WING LIGHT. CUT OUT CRACK FROM STRINGER 15L, IAW SRM 53-10-3 FIG 5, FABRICATED REPAIR PARTS ONE CHANNEL.040 7075-T6 DIM 5.2 INCH BY 3.2 INCH, TWO FILLERS.100 7075-T6 5.2 B
- [SDR GAIA03029SP](https://openairdocs.org/sdr/GAIA03029SP.md): Frame · dented · Jul 19, 2003 · N281KH · Boeing 727* · Fuselage Main, Frame
  > DURING C-CHECK, FOUND MAIN CABIN FRAME BS 520 HAS A DENT INTO THE RADIUS AT STRINGER 16R FASN/R 35745. CUT OUT DAMAGED AREA, FABRICATED FILLER FROM MATERIAL 7075-T6.050 PO NR 991420, DIM 2.5 INCH BY 3 INCH, DOUBLER FROM MATERIAL 7075-T6.063, PO NR 9912495 D
- [SDR GAIA03028SP](https://openairdocs.org/sdr/GAIA03028SP.md): Frame · dented · Jul 19, 2003 · N281KH · Boeing 727* · Fuselage Main, Frame
  > DURING C-CHECK, FOUND MAIN CABIN FRAME BS 540 HAS DENT INTO THE RADIUS AT STRINGER 16 RT, FASI N/N 35744. CUT OUT DAMAGED AREA, FABRICATED SECTION OF FRAME MATERIAL USED 7075-T6.063 P/O NR 991245 DIM 12 INCHES BY 3.5 INCHES, DOUBLER 7075-T6.071 P/O NR 99120
- [SDR GAIA03038SP](https://openairdocs.org/sdr/GAIA03038SP.md): Splice · cracked · Jul 19, 2003 · N281KH · Boeing 727* · Fuselage Main, Floor Beam
  > DURING C-CHECK, FOUND MAIN CARGO DOOR DECK BS 640, FLOORBEAM SPLICE PLATE CRACKED FROM SLOT RADIUS FASI N/R 35932. REMOVED AND REPLACED FLOORBEAM SPLICE PLATE P/N AE727-1-42-11, PO NR 319397 IAW STC AE179850 DTD 4-7-93. (M)
- [SDR GAIA03037SP](https://openairdocs.org/sdr/GAIA03037SP.md): Splice · cracked · Jul 19, 2003 · N281KH · Boeing 727* · Fuselage Main, Floor Beam
  > DURING C-CHECK, FOUND MAIN CARGO DECK BS 600, FLOORBEAM SPLICE PLATE CRACKED AT SLOT RADIUS FASI N/R 35931. REMOVED AND REPLACED FLOORBEAM SPLICE PLATE P/N AE727-1-42-11, PO NR 319397 IAW STC AE 179850 DTD 4-7-93. (M)
- [SDR GAIA03036SP](https://openairdocs.org/sdr/GAIA03036SP.md): Floorbeam · cracked · Jul 19, 2003 · N281KH · Boeing 727* · Fuselage Main, Floor Beam
  > DURING C-CHECK, FOUND MAIN CARGO DECK BS 580, FLOORBEAM SPLICE PLATE CRACKED AT SLOT RADIUS, FASI N/R 35930. REMOVED AND REPLACED SPLICE PLATE P/N AE 727-1-42-11, PO NR 319397 IAW STC AE 179850-DTD 4-7-93. (M)
- [SDR GAIA03034SP](https://openairdocs.org/sdr/GAIA03034SP.md): Frame · dented · Jul 19, 2003 · N281KH · Boeing 727* · Fuselage Main, Frame
  > DURING C-CHECK, FOUND MAIN CABIN FRAME BS 560 HAVE DENTS INTO THE RADIUS AT STRINGER 16R AND STRINGER 8R FASI N/R 35743. CUT OUT DAMAGED AREAS, FABRICATED DOUBLERS FROM MAT 7075-T6.063 PO NR 9912495, DIM 7 INCH BY 4.5 INCH AND 10 INCH BY 3 INCH. INSTALLED D
- [SDR GAIA03031SP](https://openairdocs.org/sdr/GAIA03031SP.md): Frame · cracked · Jul 19, 2003 · N281KH · Boeing 727* · Fuselage Main, Frame
  > DURING C-CHECK, FOUND MAIN CABIN FRAME BS 360 HAS A DENT AND CRACK BETWEEN STRINGERS 7R AND 8R FASI N/R 35751. CUT OUT DAMAGED AREA, FABRICATED DOUBLER REPAIR FROM 7075-T6.050, PO NR 9911488 DIM 11 INCH BY 5.5 INCH. INSTALLED REPAIR IAW B727 SRM 51-30-2 AND
- [SDR GAIA03030SP](https://openairdocs.org/sdr/GAIA03030SP.md): Frame · damaged · Jul 19, 2003 · N281KH · Boeing 727* · Fuselage Main, Frame
  > DURING C-CHECK, FOUND MAIN CABIN FRAME BS 460 HAS A TOOLING HOLE INTO THE RADIUS AT STRINGER 17R FASI N/R 35747. CUT OUT DAMAGE AREA, FABRICATED DOUBLER FROM 7075-T6.063 PO NR 9912495 DIM 3.5 INCH BY 7.75 INCH, INSTALLED REPAIR IAW B727 SRM 51-30-2. (M)
- [SDR GAIA03042SP](https://openairdocs.org/sdr/GAIA03042SP.md): Seat Track · corroded · Jul 19, 2003 · N281KH · Boeing 727* · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK, FOUND MAIN CABIN SEAT TRACK CORRODED LBL 45 BS 720D FASI N/R 36068. REPLACED DAMAGED PARTS 90 INCHES LONG P/N BAC1520-792 AND BAS 1593-100122 IAW B-727 SRM 53-10-5 FIG 1. (M)
- [SDR GAIA03044SP](https://openairdocs.org/sdr/GAIA03044SP.md): Skin · chafed · Jul 19, 2003 · N281KH · Boeing 727 · Rudder, Plate/Skin
  > DURING C-CHECK, FOUND LOWER RUDDER LOWER L/E CLOSE OUT WEB CHAFED THROUGH FASI N/R 36010. REPLACED WEB P/N 65-16830-4 IAW B-727 SRM 51-30-2. (M)
- [SDR DHL2003741501](https://openairdocs.org/sdr/DHL2003741501.md): Skin · cracked · Mar 23, 2003 · N741DH · Boeing 727* · Fuselage Main, Plate/Skin
  > DISCREPANCY DURING C CHECK, FUSELAGE UPPER LOBE INTERIOR BS 680 AND CARGO DOOR LWR. SILL BEAM FRAME CRACKED FWD. AND AFT. ALSO MISSING FASTENERS (8 EACH). REMOVED FASTENERS IAW B-727 SRM 51-30-2. CUT-OUT DAMAGED AREA AND FABRICATED ANGLE IAW B-727 SRM.
- [SDR C1HA200396001](https://openairdocs.org/sdr/C1HA200396001.md): Warning Light · illuminated · Jan 5, 2003 · N696CA · Boeing 727* · Landing Gear Position and Warning
  > AFTER GEAR RETRACTION, THE FWD DOOR LIGHT AND F/E'S RT GEAR DOOR LIGHT REMAINED ILLUMINATED. PERFORMED COM PROCEDURE 2.32.29 AND BOTH LIGHTS EXTINGUISHED. INSTALLED 3 PINS LANDING GEAR AND CYCLED FOR 2 TIMES, DOORS LANDING GEAR LIGHTS WORKING GOOD IAW MM 32-
- [SDR 2002FA0000614](https://openairdocs.org/sdr/2002FA0000614.md): Nut · fractured · Mar 27, 2002 · Boeing 727* · Fuel Boost Pump
  > NUT FRACTURED INTO THREE PIECES UNDER NORMAL TORQUE OF (75-80 IN-LBS).
- [SDR 2002FA0000609](https://openairdocs.org/sdr/2002FA0000609.md): Cap · eroded · Feb 11, 2002 · Boeing 727* · Landing Gear Retraction/Extension System
  > ACTUATOR CAP PORT (C) HAS EROSION INTERNALLY.
- [SDR 2002FA0000608](https://openairdocs.org/sdr/2002FA0000608.md): Cap · eroded · Feb 11, 2002 · Boeing 727* · Landing Gear Retraction/Extension System
  > ACTUATOR CAP PORT HAS EROSION INTERNALLY.
- [SDR 2001FA0000676](https://openairdocs.org/sdr/2001FA0000676.md): Cap · corroded · Nov 12, 2001 · Boeing 727 · Elevator Control System
  > CAP ASSEMBLY HAS SEVERE CORROSION IN THE PACKING GROOVE, THE INTERIOR AND EXTERIOR SURFACES. DISSIMILAR METAL CORROSION.
- [SDR 2001FA0000675](https://openairdocs.org/sdr/2001FA0000675.md): Cap · corroded · Nov 12, 2001 · Boeing 727* · Elevator Control System
  > CAP ASSEMBLY HAS SEVERE CORROSION IN THE PACKING GROOVE, THE INTERIOR AND EXTERIOR SURFACES. DISSIMILAR METAL CORROSION.
- [SDR 2001FA0000674](https://openairdocs.org/sdr/2001FA0000674.md): Housing · corroded · Nov 12, 2001 · Boeing 727* · Elevator Control System
  > ELBOW HOUSING HAS SEVERE CORROSION IN THE BOLT HOLES, CHECK VALVE PORT, PACKING LANDS AND ON THE SEALING SURFACE. DISSIMILAR METAL CORROSION.
- [SDR 2001FA0000678](https://openairdocs.org/sdr/2001FA0000678.md): Coil · shorted · Nov 8, 2001 · Boeing 727* · Nose/Tail Landing Gear
  > BRAKE COILS ARE SHORTED AND BURNED. UNDER NORMAL OPERATION THE VIBRATION INCURRED HAS BEEN FOUND TO CAUSE ABRADING BETWEEN THE BRAKE COILS AND STUDS WHICH RESULTS IN A SHORT AND ARCING OF THE BRAKE COILS. REDUCE THE SIZE OF THE COIL WINDINGS OR DIAMETER OF T
- [SDR 2001FA0000677](https://openairdocs.org/sdr/2001FA0000677.md): Coil · shorted · Nov 8, 2001 · Boeing 727* · Nose/Tail Landing Gear
  > BRAKE COILS ARE SHORTED AND BURNED. UNDER NORMAL OPERATION THE VIBRATION INCURRED HAS BEEN FOUND TO CAUSE ABRADING BETWEEN THE BRAKE COILS AND STUDS WHICH RESULTS IN A SHORT AND ARCING OF THE BRAKE COILS. REDUCE THE SIZE OF THE COIL WINDINGS OR DIAMETER OF T
- [SDR 2001FA0000673](https://openairdocs.org/sdr/2001FA0000673.md): Housing · corroded · Nov 8, 2001 · Boeing 727* · Elevator Control System
  > HOUSING ASSEMBLY HAS HEAVY PITTING AND CORROSION IN THE BOLT HOLES, PORTS, CAP ASSEMBLIES AND ON THE SEALING SURFACES. DISSIMILAR METAL CORROSION.
- [SDR IU62001F00012](https://openairdocs.org/sdr/IU62001F00012.md): Actuator · flaking · Oct 31, 2001 · Boeing 727* · Leading Edge Slat Actuator
  > CHROME PLATING IS FLAKING OFF INSIDE THE BORE.
- [SDR 01FDEA00899](https://openairdocs.org/sdr/01FDEA00899.md): Switch · failed · Oct 21, 2001 · N205FE · Boeing 727 · Leading Edge Slat Control System
  > 01-344 #6 L/E FLAP INDICATING IN TRANSIT AFTER RETRACTION. AIR RETURN. ** S/D ** COMING
- [SDR DHL2001741017](https://openairdocs.org/sdr/DHL2001741017.md): Controller · lack of lube · Sep 8, 2001 · N741DH · Boeing 727 · Trailing Flap Position Indicating System
  > 1) DURING FLAP EXTENSION LEFT INBOARD FLAP WOULD NOT EXTEND TO FLAPS 30. APPROX. 1 NEEDLE WIDTH OUT OF BOX DURING APPROACH AND 2ND ATTEMPT WAS MADE AFTER LANDING. 2) LUBRICATED FLAP MECHANISM AND ADJUSTED LEFT INBOARD FLAP TRANSMITER CHECK OPS. IS GOOD P
- [SDR 2001FA0000423](https://openairdocs.org/sdr/2001FA0000423.md): Housing · cracked · Aug 21, 2001 · Boeing 727 · Drag Control Actuator
  > HOUSING IS CRACKED ALONG FIRST SHOULDER ON SAME SIDE AS PORTS.

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

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

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