# Service difficulty reports: N7640U, cancelled Mar 14, 2007

A list on [N7640U, cancelled Mar 14, 2007](https://openairdocs.org/deregistered/N7640U-2007-03-14.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 65 reports

- [SDR C7WA200600007](https://openairdocs.org/sdr/C7WA200600007.md): Control Box · false indication · Mar 22, 2006 · N7640U · Boeing 727222 · Fire Detection
  > NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED SHUTDOWN ENGINE AND RETURNED TO DEPARTURE. REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTION CONTROL BOX OPS CHECK GOOD IAW MM. (K)
- [SDR C7WA200600008](https://openairdocs.org/sdr/C7WA200600008.md): Clamp · loose · Mar 22, 2006 · N7640U · Boeing 727222 · Engine Bleed Air System
  > NR 1 ENGINE FIRE WARNING LIGHT AND BELL ILLUMINATED IN FLIGHT. PERFORMED ENGINE SHUTDOWN AND RETURNED TO DEPARTURE. INSPECTED ENGINE FOR LEAKS AND DAMAGE. TIGHTENED CLAMPS ON BLEED AIR DUCTS AND REPOSITIONED FIRE LOOP IN PYLON. RAN ENGINE OPERATIONAL CHECK
- [SDR C7WA200600003](https://openairdocs.org/sdr/C7WA200600003.md): Engine · fod · Feb 22, 2006 · N7640U · Boeing 727222 · Engine (Turbine/Turboprop)
  > IN FLIGHT, AT FL 28.0, NR 2 ENGINE COMPRESSOR STALLED. ENGINE WAS IN STABLE OPERATION, NO BLEED AT 1.80 EPR. EPR DROPPED TO 1.4 EGT RUNS 80 TO 100 HOTTER THAN ENGINES 1 AND 3 IN ALL PARAMETERS OF FLIGHT. INSPECTION ON NR 2 ENGINE REVEALED HEAVY FOD DAMAGE.
- [SDR C7WA200500110](https://openairdocs.org/sdr/C7WA200500110.md): Overheat Loop · grounded · Jul 23, 2005 · N7640U · Boeing 727222 · Overheat Detection
  > LOWER AFT BODY OVERHEAT LIGHT ON. COMPLETED EMERGENCY PROCEDURE, FOUND IT TO BE NR 2 ENGINE. INSPECTED NUMBER 2 ENGINE FOUND LOOP TOUCHING BLEED AIR DUCT. REPOSITIONED LOOP OPERATIONAL CHECKS GOOD PER MM 26-14-0. (M)
- [SDR C7WA200300077](https://openairdocs.org/sdr/C7WA200300077.md): Connector · dirty · Jan 15, 2005 · N7640U · Boeing 727222 · Leading Edge Slat Control System
  > AIR RETURN, UPON FLAP RETRACTION ON CLIMB-OUT, NR 1 SLAT FAILED TO RETRACT. CLEANED CONNECTOR IAW 20-80-01, OPS CHECKED FLAPS AND SLATS PER MM 27-80-0. ALL INDICATIONS NORMAL. OK FOR CONTINUED SERVICE. (M)
- [SDR C7WA200400041](https://openairdocs.org/sdr/C7WA200400041.md): Transmitter · frozen · Sep 7, 2004 · N7640U · Boeing 727222 · Trailing Flap Position Indicating System
  > EXPERIENCED FLAP PROBLEM ON EXTENSION, PERFORMED CHECK LIST. LANDED WITHOUT INCIDENT. FOUND LT IB FLAP POSITION TRANSMITTER FROZEN. REMOVED AND REPLACED TRANSMITTER AND REPAIRED WIRES AT D224 IB FLAP INDICATOR CONNECTOR OPERATIONAL CHECK GOOD IAW MM.
- [SDR C7WA2004000AA](https://openairdocs.org/sdr/C7WA2004000AA.md): Switch · inoperative · Aug 25, 2004 · N7640U · Boeing 727222 · Engine Start Valves/Controls
  > ENGINE SHUTDOWN: IN CRUISE NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED AT THE SAME TIME THE RT DUCT OVERHEAT LIGHT CAME ON. ACCOMPLISHED ASSOCIATED EMERGENCY PROCEDURE IAW AOM. LIGHTS STAYED ON UNTIL ENGINE SHUTDOWN ON THE GROUND. REMOVED AND REPLACED N
- [SDR 2004F00172](https://openairdocs.org/sdr/2004F00172.md): Accessory Unit · faulty · Feb 4, 2004 · N7640U · Boeing 727222 · Landing Gear Retraction/Extension System
  > ON APPROACH INTO DAY, UNSAFE RIGHT MAIN LANDING GEAR INDICATION. RED LIGHT WAS ILLUMINATED. GEAR WS VISUALLY VERIFIED DOWN BY THE TOWER. ACCOMPLISHED APPROPRIATE CHECKLIST FOR UNSAFE GEAR. RECYCLED GEAR SECOND TIME AND ALL INDICATIONS WERE NORMAL. AIRCRAF
- [SDR 2004F00167](https://openairdocs.org/sdr/2004F00167.md): Duct · cracked · Feb 2, 2004 · N7640U · Boeing 727222 · Engine Bleed Air System
  > ON TAKEOFF ROLL OUT OF ICT, NR 3 ENGINE FIRE WARNING CAME ON. SHUTDOWN NR 3 ENGINE IAW RYAN PROCEDURES AND RETURNED ICT. AIRCRAFT LANDED ICT WITHOUT INCIDENT. REMOVED AND REPLCED NR 3 ENGINE 13 STAGE SADDLE DUCT. GROUND OPERATIONAL CHECK NORMAL. (M)
- [SDR 2004F00110](https://openairdocs.org/sdr/2004F00110.md): Generator · failed · Dec 11, 2003 · N7640U · Boeing 727222 · AC Generation System
  > DURING TAKEOFF FROM BNA, AIRCRAFT LOST NR 3 GENERATOR, EPR WENT TO 1.6 AND OIL PRESSURE FELL TO REDLINE. PERFORMED ENGINE SHUTDOWN PROCEDURES AND DECLARED EMERGENCY. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. DURING GROUND RUN OF ENGINES, FOUND N
- [SDR 2004F00072](https://openairdocs.org/sdr/2004F00072.md): Hinge · cracked · Sep 30, 2003 · N7640U · Boeing 727222 · Cargo/Baggage Doors
  > AT B-CHECK, FOUND AFT SECTION OF MAIN CARGO DOOR HINGE CRACKED AT AFT END AIRFRAME SIDE. REMOVED CRACKED SECTION OF MAIN CARGO DOOR HINGE. FABRICATE, TREAT, PRIME AND INSTALLED NEW HINGE SEGMENT. MAIN CARGO DOOR OPERATIONAL CHECKED NORMAL. (M)
- [SDR 2004F00057](https://openairdocs.org/sdr/2004F00057.md): Angle · cracked · Sep 30, 2003 · N7640U · Boeing 727222 · Wing, Attach Fittings
  > AT B-CHECK, FOUND NR 2 SPOILER ACTUATOR IB MOUNT BRACKET CRACKED. REMOVED AND REPLACED NR 2 SPOILER ACTUATOR IB MOUNT BRACKET. RIGG AND LEAK CHECKED NORMAL. (M)
- [SDR RYN2004F00027](https://openairdocs.org/sdr/RYN2004F00027.md): Module · failed · Sep 16, 2003 · N7640U · Boeing 727222 · Hydraulic System, Main
  > AFTER TAKEOFF, RETRACTED FLAPS AND RECEIVED AN A-HYDRAULIC LOW PRESSURE INDICATION AT FLIGHT ENGINEER PANEL AND PILOTS FWD PANEL. FOLLOWED HYDRAULIC LOSS PROCEDURES. AIRCRAFT RETURNED TO DEPARTURE AIRPORT WITHOUT INCIDENT. REMOVED AND REPLACED (A) SYSTEM HY
- [SDR 2003F00420](https://openairdocs.org/sdr/2003F00420.md): Floor Support · dented · Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous Structure
  > AT C-CHECK, FOUND DENT ON AFT CARGO FLOOR SUPPORT, STATION 950F, RBL 17. FABRICATE REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED DOUBLER AND FILLER AT AFT CARGO FLOOR SUPPORT RBL 17 STATION 950F PLUS 2 INCHES. (M)
- [SDR 2003F00419](https://openairdocs.org/sdr/2003F00419.md): Frame · cracked · Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Main, Frame
  > AT C-CHECK, FOUND CRACK ON FORWARD CARGO FRAME AT BS 660, STRINGER 23R/24R. FABRICATE REPAIR ANGLE. TREATED, PRIMED AND INSTALLED REPAIR ANGLE ON FORWARD CARGO FRAME STATION 660 STRINGER 23R AND 24R. (M)
- [SDR 2003F00417](https://openairdocs.org/sdr/2003F00417.md): Frame · cracked · Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Main, Frame
  > AT C-CHECK, FOUND CRACK ON FORWARD CARGO FRAME AT BS 680, STRINGER 23R/24R. FABRICATED REPAIR. TREATED, PRIMED AND INSTALLED REPAIR ON FORWARD CARGO FRAME STATION 680 STRINGER 23R THROUGH 24R. (M)
- [SDR 2003F00413](https://openairdocs.org/sdr/2003F00413.md): Floor Support · dented · Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous Structure
  > AT C-CHECK, FOUND DENT ON AFT CARGO FLOOR SUPPORT, STATION 950F, RBL 13. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED REPAIR AT AFT CARGO FLOOR SUPPORT RBL 13 STATION 950F. (M)
- [SDR 2003F00412](https://openairdocs.org/sdr/2003F00412.md): Floor Support · dented · Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous Structure
  > AT C-CHECK, FOUND DENT ON AFT CARGO FLOOR SUPPORT, STATION 950F, RBL 9. FABRICATE REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED DOUBLER AND FILLER AT AFT CARGO FLOOR SUPPORT RBL 9 STATION 950F. (M)
- [SDR 2003F00410](https://openairdocs.org/sdr/2003F00410.md): Access Panel · cracked · Mar 14, 2003 · N7640U · Boeing 727222 · Wing, Plate/Skin
  > AT C-CHECK, FOUND CRACK ON RIGHT WING, NR 6 SLAT LOWER ACCESS PANEL NR 6589. FABRICATED NEW PANEL. ALODINED, PRIMED AND INSTALLED NEW ACCESS PANEL AT RIGHT LOWER NR 6 SLAT. (M)
- [SDR 2003F00409](https://openairdocs.org/sdr/2003F00409.md): Bracket · broken · Mar 14, 2003 · N7640U · Boeing 727222 · Leading Edge Devices
  > AT C-CHECK, FOUND NR 6 SLAT INBOARD FIXED LEADING EDGE CAVITY STOP BRACKET BROKEN. REPLACD NR 6 SLAT INBOARD FIXED LEADING EDGE CAVITY STOP BOLT BRACKET. (M)
- [SDR 2003F00405](https://openairdocs.org/sdr/2003F00405.md): Frame · cracked · Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Main, Frame
  > AT C-CHECK, FOUND DENT ON FORWARD CARGO FRAME AT BS 720A, STRINGER 24L. FABRICATED REPAIR ANGLE. TREATED, PRIMED AND INSTALLED REPAIR ANGLE ON FORWARD CARGO FRAME STATION 720A STRINGER 24L. (M)
- [SDR 2003F00404](https://openairdocs.org/sdr/2003F00404.md): Frame · cracked · Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Main, Frame
  > AT C-CHECK, FOUND DENTS ON FORWARD CARGO FRAME AT BS 700, STRINGER 24L/25L. FABRICATED REPAIR. TREATED, PRIMED AND INSTALLED REPAIR ON FORWARD CARGO FRAME STATION 700 STRINGER 24L AND 25L. (M)
- [SDR 2003F00403](https://openairdocs.org/sdr/2003F00403.md): Floor Support · dented · Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous Structure
  > AT C-CHECK, FOUND DENT ON AFT CARGO COMPARTMENT FLOOR SUPPORT, STATION 950E, LBL 10. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED PARTS ON AFT CARGO FLOOR SUPPORT LBL 10 STATION 950E. (M)
- [SDR 2003F00401](https://openairdocs.org/sdr/2003F00401.md): Panel · cracked · Mar 14, 2003 · N7640U · Boeing 727222 · Wing, Plate/Skin
  > AT C-CHECK, FOUND CRACK ON RIGHT WING, OUTBOARD TRAILING EDGE WING FIXED PANEL INBOARD ATTACH BRACKET. FABRICATED BRACKET. TREATED, PRIMED AND INSTALLED BRACKET ON RIGHT WING OUTBOARD TRAILING EDGE WING FIXED PANEL INBOARD. (M)
- [SDR 2003F00397](https://openairdocs.org/sdr/2003F00397.md): Floorbeam · cracked · Mar 14, 2003 · N7640U · Boeing 727222 · Fuselage Main, Floor Beam
  > AT C-CHECK, FOUND CRACK ON AFT CARGO FLOORBEAM AT STATION 950B, BL 0. FABRICATE NEW ANGLE. TREATED, PRIMED AND INSTALLED NEW ANGLE AT STATION 950B BL 0. (M)
- [SDR 2003F00418](https://openairdocs.org/sdr/2003F00418.md): Stringer Clip · cracked · Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous Structure
  > AT C-CHECK, FOUND CRACKED STRINGER CLIP AT STAITON 540, STRINGER 5R. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP AT STATION 540 STRINGER 5R. (M)
- [SDR 2003F00416](https://openairdocs.org/sdr/2003F00416.md): Frame · cracked · Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Main, Frame
  > AT C-CHECK, OFUND CRACK ON LOWER LEFT PANEL MOUNT FRAME AT LOWER END, BS 720. FABRICATE REPAIR ANGLE. ALODINED, PRIMED AND INSTALLED NEW ANGLE AT LOWER LEFT PANEL MOUTN FRAME STATION 720. (M)
- [SDR 2003F00415](https://openairdocs.org/sdr/2003F00415.md): Skin · cracked · Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Main, Plate/Skin
  > AT C-CHECK, FOUND CRACK ON OUTER SKIN OF CO-PILOT WINDOW POST AT BS 203. FABRICATE DOUBLER REPAIR. ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER ON OUTER SKIN OF CO-PILOT WINDOW POST AT BS 203. (M)
- [SDR 2003F00414](https://openairdocs.org/sdr/2003F00414.md): Fairing · cracked · Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous Structure
  > AT C-CHECK, FOUND CRACK ON LEFT AIR CONDITIONING BAY FAIRING BELOW TAXI LIGHT. CUT OUT CRACKED SECTION AND INSTALLED DOUBLER AT LEFT AIR CONDITIONING BAY FAIRING BELOW TAXI LIGHT. (M)
- [SDR 2003F00402](https://openairdocs.org/sdr/2003F00402.md): Clip · cracked · Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous Structure
  > AT C-CHECK, FOUND CRACKED STRINGER FRAME ATTACH CLIP AT STATION 570, STRINGER 5R. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW ATTACH CLIP AT STATION 560 STRINGER 5R. (M)
- [SDR 2003F00400](https://openairdocs.org/sdr/2003F00400.md): Clip · cracked · Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous Structure
  > AT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720, STRINGER 3L. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP AT STATION 720 STRINGER 3L. (M)
- [SDR 2003F00399](https://openairdocs.org/sdr/2003F00399.md): Clip · cracked · Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous Structure
  > AT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720C, STRINGER 5R. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP AT STATION 720C STRINGER 5R. (M)
- [SDR 2003F00398](https://openairdocs.org/sdr/2003F00398.md): Clip · cracked · Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous Structure
  > AT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720A, STRINGER 5L. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW ATTACH CLIP AT STATION 720A STRINGER 5L. (M)
- [SDR 2003F00422](https://openairdocs.org/sdr/2003F00422.md): Stringer Clip · cracked · Mar 13, 2003 · N7640U · Boeing 727222 · Fuselage Miscellaneous Structure
  > AT C-CHECK, FOUND CRACKED STRINGER CLIP AT STATION 720E, STRINGER 5L. FABRICATE NEW ATTACH CLIP. TREATED, PRIMED AND INSTALLED NEW STRINGER TO FRAME ATTACH CLIP AT STATION 720E, STRINGER 5L. (M)
- [SDR 2003F00421](https://openairdocs.org/sdr/2003F00421.md): Duct · cracked · Mar 13, 2003 · N7640U · Boeing 727222 · Air Distribution System
  > AT C-CHECK, FOUND CRACK ON HEATING AND AIR CONDITIONING DUCT AT BS 720E/D, STRINGER 12/13. STOP DRILLED CRACKS. FABRICATED DOUBLER. ALODINED, PRIMED AND INSTALLED DOUBLER AT FUSELAGE HEATING AND AIR CONDITIONING DUCT, RIGHT SIDE OF CABIN, BETWEEN STATION 72
- [SDR 2003F00441](https://openairdocs.org/sdr/2003F00441.md): Frame · cracked · Mar 12, 2003 · N7640U · Boeing 727222 · Fuselage Main, Frame
  > AT C-CHECK, FOUND INDICATION OF CRACK AT TERMINAL HOLE FITTING, BS 870. STOP DRILLED CRACK AT SECOND FASTENER ROW, SECOND FASTENER DOWN FROM STRINGER 9R ON BS 870 TERMINAL FITTING. FABRICATED AN EXTERNAL DOUBLER REPAIR. TREATED AND PRIMED DOUBLER AND AREA O
- [SDR 2003F00440](https://openairdocs.org/sdr/2003F00440.md): Skin · cracked · Mar 12, 2003 · N7640U · Boeing 727222 · Fuselage Main, Plate/Skin
  > AT C-CHECK, FOUND FORWARD GALLEY DOOR CUTOUT, LOWER AFT CORNER SKIN CRACKED. STOPPED DRILLED CRACKS ON RIGHT FORWARD GALLEY DOOR CUTOUT, LOWER AFT CORNER SKIN. FABRICATED DOUBLER. TREATED, PRIMED AND INSTALLED DOUBLER ON RIGHT FORWARD GALLEY DOOR LOWER AFT,
- [SDR 2003F00439](https://openairdocs.org/sdr/2003F00439.md): Frame · cracked · Mar 12, 2003 · N7640U · Boeing 727222 · Fuselage Main, Frame
  > AT C-CHECK, FOUND TIE FRAME TO FUSELAGE CRACKED AT STATION 680, STRINGER 17L. FABRICATED ANGLE REPAIR. ALODINED, PRIMED AND INSTALLED ANGEL REPAIR ON BS 680, STRINGER 17L, LOWER SILL BEAM TIE FRAME. (M)
- [SDR 2003F00429](https://openairdocs.org/sdr/2003F00429.md): Skin · cracked · Mar 12, 2003 · N7640U · Boeing 727222 · Fuselage Main, Plate/Skin
  > AT C-CHECK, FOUND FORWARD GALLEY DOOR CUTOUT LOWER FORWARD CORNER SKIN CRACKED. STOP DRILLED CRACK ON RIGHT FORWARD GALLEY DOOR CUTOUT, FORWARD, LOWER CORNER SKIN. FABRICATED DOUBLER AND TRIPLER. TREATED, PRIMED AND INSTALLED DOUBLER AND TRIPLER ON FORWARD
- [SDR 2003F00493](https://openairdocs.org/sdr/2003F00493.md): Skin · cracked · Mar 10, 2003 · N7640U · Boeing 727222 · Wing, Plate/Skin
  > AT C-CHECK, FOUND CRACK ON LEADING EDGE WING SKIN AT NR 5 OUTBOARD SLAT TRACK. STOP DRILLED CRACK. FABRICATED DOUBLER. ALODINED AND PRIMED AREA REPAIR DOUBLER. INSTALLED AT RIGHT WING NR 5 OUTBOARD SLAT TRAKC LEADING EDGE CUT OUT. (M)
- [SDR 2003F00458](https://openairdocs.org/sdr/2003F00458.md): Skin · cracked · Mar 10, 2003 · N7640U · Boeing 727222 · Leading Edge Devices
  > AT C-CHECK, FOUND CRACK AT RT WING LEADING EDGE ABOVE NR 5 INBOARD SLAT TRACK LEADING EDGE CUTOUT UPPER RADIUS. STOP DRILLED CRACK AT RIGHT WING LEADING EDGE NR 5 SLAT TRACK CUT OUT, AT WING STATION 383. FABRICATED REPARI DOUBLER. ALODINED, PRIMED AND INSTA
- [SDR 2003F00457](https://openairdocs.org/sdr/2003F00457.md): Panel · cracked · Mar 10, 2003 · N7640U · Boeing 727222 · Elevator, Plate/Skin
  > AT C-CHECK, FOUND CRACK AT LEFT ELEVATOR BALANCE BAY PANEL 9720. ROUTED CRACKED AREA ON LT ELEVATOR BALANCE PANEL NR 9720. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER. (M)
- [SDR 2003F00449](https://openairdocs.org/sdr/2003F00449.md): Retainer · cracked · Mar 10, 2003 · N7640U · Boeing 727222 · Leading Edge Devices
  > AT C-CHECK, FOUND CRACK AT RIGHT WING NR 5 SLAT OUTBOARD SEAL RETAINER. REMOVED AND REPLACED RIGHT WING NR 5 SLAT, OUTBOARD HOOK SEAL, UPPER LEADING EDGE WING, OUTBOARD SEAL RETAINER TRIM. (M)
- [SDR 2003F00448](https://openairdocs.org/sdr/2003F00448.md): Plate · cracked · Mar 10, 2003 · N7640U · Boeing 727222 · Leading Edge Devices
  > AT C-CHECK, FOUND CRACK AT NR 6 SLAT LOWER BACKSIDE ACTUATOR ROD END ACCESS CUTOUT SUPPORT PLATE. REMOVED DAMAGED PLATE FROM RIGHT WING NR 6 SLATE LOWER BACKSIDE SLAT ACTUATOR ROD END ACCESS CUT OUT. FABRICATED PLATE. TREATED AND PRIMED PART AND AREA. INST
- [SDR 2003F00436](https://openairdocs.org/sdr/2003F00436.md): Retainer · cracked · Mar 10, 2003 · N7640U · Boeing 727222 · Leading Edge Devices
  > AT C-CHECK, FOUND CRACK AT NR 5 SLAT, INBOARD HOOK SEAL CUTOUT, OUTBOARD SEAL RETAINER. REMOVED AND REPLACED NR 5 SLAT INBOARD HOOK SEAL, UPPER LEADING EDGE, OUTBOARD SEAL RETAINER TRIM. (M)
- [SDR 2003F00435](https://openairdocs.org/sdr/2003F00435.md): Bracket · cracked · Mar 10, 2003 · N7640U · Boeing 727222 · Leading Edge Devices
  > AT C-CHECK, FOUND CRACK AT NR 6 SLATE ACTUATOR SUPPORT BRACKET. ACCOMPLISHED AN HFEC INSPECTION ON RIGHT WING NR 6 SLAT ACTUATOR OUTBOARD MOUNT BRACKET. NO CRACKS NOTED. (M)
- [SDR 2003F00430](https://openairdocs.org/sdr/2003F00430.md): Angle · cracked · Mar 10, 2003 · N7640U · Boeing 727222 · Wing Miscellaneous Structure
  > AT C-CHECK, FOUND STRUCTURE CRACKED, NOSE WHEEL WELL AT BS 294.5, LBL 12 RT, WL 177. STOP DRILLED CRACKS. FABRICATED FORMED ANGLE REPAIRS AND STRAPS. TREATED, PRIMED AND INSTALLED ANGLES AND STRAPS IN NOSE WHEEL WELL RIGHT SUPPORT AT STATION 294.5. (M)
- [SDR 2003F00433](https://openairdocs.org/sdr/2003F00433.md): Skin · burned · Mar 9, 2003 · N7640U · Boeing 727222 · Elevator, Plate/Skin
  > AT C-CHECK, FOUND STATIC DISCHARGE BURN, RIGHT ELEVATOR OUTBOARD TRAILING EDGE CORNER. CUT OUT DAMAGED AREA ON RIGHT ELEVATOR OUTBOARD TRAILING EDGE CORNER. FABRICATED DOUBLERS AND FILLER. TREATED AND PRIMED PARTS. INSTALLED REPAIR PARTS. (M)
- [SDR 2003F00427](https://openairdocs.org/sdr/2003F00427.md): Frame · cracked · Mar 9, 2003 · N7640U · Boeing 727222 · Fuselage Main, Frame
  > AT C-CHECK, FOUND TIE FRAME CRACKED AT BS 480, STRINGER 17L. FABRICATED REPAIR ANGLES. TREATED AND PRIMED FABRICATED REPAIR ANGLES. INSTALLED AT STATION 480, STRINGER 17L. (M)
- [SDR 2003F00446](https://openairdocs.org/sdr/2003F00446.md): Bracket · cracked · Mar 8, 2003 · N7640U · Boeing 727222 · Wing Miscellaneous Structure
  > AT C-CHECK, FOUND CRACK AT LT WING LOWER TRAILING EDGE PANEL SUPPORT BRACKET, OUTBOARD OF NR 2 SPOILER ACTUATOR. REMOVED AND REPLACED BRACKET ON LEFT WING LOWER TRAILING EDGE PANEL SUPPORT BRACKET AT NR 2 SPOILER, OUTBOARD OF ACTUATOR. (M)

Next page: https://openairdocs.org/deregistered/N7640U-2007-03-14/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 n_number = 'N7640U' AND deregistration_id = 'N7640U-2007-03-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N7640U-2007-03-14/reports

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