# Service difficulty reports: N721RW, cancelled Aug 15, 2007

A list on [N721RW, cancelled Aug 15, 2007](https://openairdocs.org/deregistered/N721RW-2007-08-15.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 C7WA200500117](https://openairdocs.org/sdr/C7WA200500117.md): Transponder · inoperative · Aug 9, 2005 · N721RW · Boeing 7272M7 · ATC Transponder System
  > FLIGHT RETURN, NR 2 TRANSPONDER FAILED DURING FLIGHT. RETURNED TO KDAY PER ATC REQUEST. REMOVED AND REPLACED TRANSPONDER OPERATIONAL CHECKS GOOD PER B727 MM 34-43-10. (M)
- [SDR C7WA200400067](https://openairdocs.org/sdr/C7WA200400067.md): Line · loose · Nov 11, 2004 · N721RW · Boeing 7272M7 · Turbine Engine Oil System
  > ON CLIMB OUT THROUGH 16,000, NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE WAS 35 PSI AND DECREASING. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN IAW AOM. FOUND NR 3 ENGINE LOW OIL PRESSURE SWITCH OIL LINE LEAKING. REMOVED AND REINSTALLED LINE OPERA
- [SDR C7WA200400003](https://openairdocs.org/sdr/C7WA200400003.md): Warning Light · illuminated · Mar 1, 2004 · N721RW · Boeing 7272M7 · Fire Detection
  > LWR AFT CARGO FIRE LIGHT CAME ON AFTER TAKEOFF AND THEN EXTINGUISHED ON FINAL APPROACH BACK. ADDITIONALLY THE DUCT OVERHEAT LIGHT ON PILOTS OVERHEAD PANEL CAME ON AND REMAINED ON DURING FINAL APPROACH. TEMP PEGGED AT 250 DEGREES OR GREATER. OPS CHECK OF LOW
- [SDR C7WA200400001](https://openairdocs.org/sdr/C7WA200400001.md): Gyro · inoperative · Jan 27, 2004 · N721RW · Boeing 7272M7 · Directional Gyro and Indicating System
  > ABORTED TAKEOFF AT APPROX 80 KTS DUE TO FAILURE OF F/O DIRECTIONAL GYRO. REMOVED AND REPLACED VIRTICAL GYRO IAW MM.
- [SDR EISA20010150](https://openairdocs.org/sdr/EISA20010150.md): Accessory Unit · inoperative · Dec 23, 2001 · N721RW · Boeing 7272M7 · Landing Gear Position and Warning
  > AFTER T/O, GEAR HANDLE RAISED, ALL 3 GEAR UNSAFE RED LIGHTS REMAIN ILLUMINATED ON FNT PANEL & TAILSKID LIGHT ON F/E PANEL. PERFORMED ABNORMAL CHECKLIST WITH SAME RESULT. RETURN TO IND. FOR UNEVENTFUL LANDING. DOWN & LOCK INDICATIONS ALL NORMAL & BELOW MAX L
- [SDR EISA20010126](https://openairdocs.org/sdr/EISA20010126.md): Receptacle · dirty · Oct 16, 2001 · N721RW · Boeing 7272M7 · Landing Gear Position and Warning
  > GEAR RETRACTED ALL RED LIGHTS ILLUMINATED (GEAR LIGHTS)-TAIL SKID LIGHT ILLUMINATED ALSO.CORRECTIVE ACTION: REMOVED LANDING GEAR ACCESSORY UNIT. CLEANED AND INSP. RACK RECEPTICAL. REINSTALLED LANDING GEAR ACCESSORY UNIT. SYS OP CKS OK IAW 727 MM CH 32-09-121
- [SDR EISA20010116](https://openairdocs.org/sdr/EISA20010116.md): Web · cracked · Aug 20, 2001 · N721RW · Boeing 7272M7 · Drag Control Actuator
  > R/H SPOILER R/H ACTUATOR ATTACH WEB CRACKED 2 PLACES.CORRECTIVE ACTION:REMOVED DAMAGED SECTION OF WEB BY CUT-OUT IAW B727 SRM 51-10-1. VERIFIED DAMAGED AREA REMOVED BY NDT IAW B727 NDT MANUAL PART 6. FABRICATED WEB REPAIR IAW B727 SRM 51-40-2. TREATED, PRIMED
- [SDR EISA20010115](https://openairdocs.org/sdr/EISA20010115.md): Fitting · cracked · Aug 20, 2001 · N721RW · Boeing 7272M7 · Drag Control Actuator
  > #9 SPOILER R/H ACTUATOR SUPPORT FITTING CRACKED SEVERAL PLACES.FOUND DURING 'B' CHECK.CORRECTIVE ACTION:R/R #9 ACTUATOR SUPPORT FITTING IAW B727 SRM 51-30-1, 51-30-2 & 51-30-5.
- [SDR EISA20010114](https://openairdocs.org/sdr/EISA20010114.md): Angle · cracked · Aug 20, 2001 · N721RW · Boeing 7272M7 · Drag Control Actuator
  > LT. WING SPOILER #4 ACTUATOR MOUNT O/B LWR. MOUNT LOBE IS BROKENFOUND DURING 'B' CHECK.CORRECTIVE ACTION:R/R #4 SPOILER ACTUATOR MOUNT BRACKET IAW B727 SRM 51-30-2.
- [SDR EISA20010107](https://openairdocs.org/sdr/EISA20010107.md): Ground Wire · loose · Jul 19, 2001 · N721RW · Boeing 7272M7 · Cabin Pressure Control System
  > A/C WOULD NOT PRESSURIZE (ALL MODES). RESECURED GROUND TO FLOW CONTROL VALVES (SHARD GRND FOR BOTH). A/C PRESSURIZATION AND PNEUMATIC SYSTEMS, OPS OK.
- [SDR EISA20010069](https://openairdocs.org/sdr/EISA20010069.md): Outflow Valve · stuck · Mar 16, 2001 · N721RW · Boeing 7272M7 · Pressure Regulator/Outflow Valve
  > AIRCRAFT WOULD NOT PRESSURIZE IN ANY MODE, DURING CLIMB. AIR TURNBACK. REMOVED AND REPLACED OUTFLOW VALVE AND PRESSURE CONTROLLER. OPS CHECK NORMAL.
- [SDR EISA20000213](https://openairdocs.org/sdr/EISA20000213.md): Flow Valve · inoperative · Dec 2, 2000 · N721RW · Boeing 7272M7 · Cabin Pressure Control System
  > AUTO PRESSURIZATION FAIL LIGHT CAME ON IN CLIMB UNABLE TO PRESSURIZE IN STANDBY OR MANUAL. REMOVED AND REPLACED FLOW CONTROL VALVE PER M/M 21-00, OPS CHECK NORMAL.
- [SDR EISA20000151](https://openairdocs.org/sdr/EISA20000151.md): Catcher · stalled · Sep 22, 2000 · N721RW · Boeing 7272M7 · Turbine Engine Compressor Section
  > COMPRESSOR STALL NR 2 ENGINE AIR TURNBACK TO (AUS). DRAINED MOISTURE TRAP IAW 73-33. RAN ENGINE, OPS CHECK GOOD PER M/M 71-00.
- [SDR EISA20000128](https://openairdocs.org/sdr/EISA20000128.md): Clamp · loose · Aug 16, 2000 · N721RW · Boeing 7272M7 · Pneumatic Distribution System
  > NR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON AFTER 10 MINUTES OF FLIGHT ON CLIMBOUT. PULLED NR 3 THROTTLE BACK AND LIGHT WENT OUT. WENT THROUGH PROCEDURES AND LIGHT DID NOT COME ON. CHECKED STRUT AREA FOR LEAKS, REPLACED 1 CLAMP ON 13TH STAGE DUCT PER M/M 36-00
- [SDR EISA2000027](https://openairdocs.org/sdr/EISA2000027.md): Seat Track · cracked · Feb 27, 2000 · N721RW · Boeing 7272M7 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND MAIN CABIN SEAT TRACK CRACKED AT FS 1090 RBL 45.5. REMOVED DAMAGED SEAT TRACK FROM FS 1070 TO FS 1100. FABRICATED NEW SECTION PER SAMPLE FROM BAC 1520-792 EXTRUSION. INSTALLED NEW SECTION PER SRM 5
- [SDR EISA2000020](https://openairdocs.org/sdr/EISA2000020.md): Skin · cracked · Jan 18, 2000 · N721RW · Boeing 7272M7 · Trailing Edge Flaps
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK, WORKCARD FOUND CRACK IN RIGHT WING OUTBOARD AFT FLAP AT NR 2 ROLLER. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-4 FIG 5 MATERIAL IO 2024-53.050. (M)
- [SDR EISA2000021](https://openairdocs.org/sdr/EISA2000021.md): Skin · cracked · Jan 18, 2000 · N721RW · Boeing 7272M7 · Trailing Edge Flaps
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK, WORKCARD FOUND CRACK IN RIGHT WING OUTBOARD AFT FLAP AT NR 1 ROLLER. FABRICATED AND INSTALLED DOUBLER PE SRM 57-50-4 FIG 5 MATERIAL IO 2024-T3.050. (M)
- [SDR EISA2000023](https://openairdocs.org/sdr/EISA2000023.md): Floorbeam · corroded · Jan 18, 2000 · N721RW · Boeing 7272M7 · Fuselage Main, Floor Beam
  > DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK, WORKCARD OF FLOORBEAM T-CAP DAMAGED AT FS 344 LBL 53 TO RBL 46. REMOVED DAMAGED FLOORBEAM UPPER T-CAP. FABRICATED REPAIR ANGLE PER SRM 53-10-8. INSTALLED PER SRM 53-10-8 MATERIAL ID BAC 1505-2922 7075-T6.(M)
- [SDR EISA2000024](https://openairdocs.org/sdr/EISA2000024.md): Skin · gouged · Jan 18, 2000 · N721RW · Boeing 7272M7 · Rudder, Plate/Skin
  > DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND GOUGE IN SKIN OF LOWER RUDDER RIGHT SIDE TRAILING EDGE. BURNISHED GOUGE. MATERIAL LOSS OUT OF LIMITS. FABRICATED EXTERNAL DOUBLER AND INSTALLED PER SRM 55-40-2 FIG 1. (M)
- [SDR EISA2000025](https://openairdocs.org/sdr/EISA2000025.md): Tie Clip · cracked · Jan 18, 2000 · N721RW · Boeing 7272M7 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND TIE CLIP CRACKED AT FS 680 STRINGER 27L. REMOVED TIE CLIP. FABRICATED NEW CLIP PER SAMPLER AND INSTALLED PER SRM 51-30-2. (M)
- [SDR EISA2000026](https://openairdocs.org/sdr/EISA2000026.md): Frame · cracked · Jan 18, 2000 · N721RW · Boeing 7272M7 · Nacelle/Pylon, Frame/Spar/Rib
  > DURING ACCOMPLISHMENT OF A NON-ROUTINE WORK CARD, FOUND NR 3 ENGINE PYLON UPPER FORWARD MOUNT AFT T-CAP CRACKED FROM FASTENER HOLE. REMOVED AND REPLACED T-CAP ANGLE ON NR 3 PYLON PER SRM 51-10-1 AND 51-30-2. (M)
- [SDR EISA99295](https://openairdocs.org/sdr/EISA99295.md): Smoke Detector · activated · Oct 6, 1999 · N721RW · Boeing 7272M7 · Smoke Detection
  > NR 4 CARGO COMPARTMENT SMOKE SENSOR ILLUMINATED ON DESCENT. FOUND GAP BETWEEN AFT ENTRY DOOR AND CEILING PANELS. SECURED PANELS AND RE-TAPED IT. SYSTEM OPS CHECK PER MM 26-13-0. (M)
- [SDR EISA99172](https://openairdocs.org/sdr/EISA99172.md): Smoke Detector · failed · Sep 24, 1999 · N721RW · Boeing 7272M7 · Smoke Detection
  > ONCE DURING CLIMB AND ONCE DURING DESCENT, NR 4 SMOKE DETECTOR LIGHT ILLUMINATED BRIEFLY, NO SMOKE OBSERVED. REMOVED AND REPLACED NR 4 SMOKE DETECTOR. OPS CHECK NORMAL IAW MM 26-17-1. (M)
- [SDR EISA99153](https://openairdocs.org/sdr/EISA99153.md): Detector · illuminated · Aug 8, 1999 · N721RW · Boeing 7272M7 · Smoke Detection
  > SMOKE DETECTOR ILLUMINATES IN FLIGHT. REMOVED AND REPLACED NR 4 SMOKE DETECTOR IAW MM CHAPTER 26-10. NO DEFECTS NOTED. (M)
- [SDR EISA99152](https://openairdocs.org/sdr/EISA99152.md): Detector · malfunctioned · Aug 6, 1999 · N721RW · Boeing 7272M7 · Smoke Detection
  > SMOKE DETECTOR ILLUMINATES ON APPROACH, CHECKED CABIN NO SIGN OF SMOKE. CLEARED MOISTURE OUT OF VACUUM TUBE AND TESTED SYSTEM IAW MM CHAPTER 26-17. OPS CHECK GOD. (M)
- [SDR EISA99151](https://openairdocs.org/sdr/EISA99151.md): Oil Line · chafed · Aug 6, 1999 · N721RW · Boeing 7272M7 · Engine Oil Pressure
  > NR 2 ENGINE LOW OIL PRESSURE, LIGHT CAME ON. OIL QTY INDICATION DROPPING. SHUT DOWN ENGINE IN FLIGHT. RIGHT ENGINE OIL PRESSURE TRANSMITTER LINE CHAFFED. INSTALLED UNION. RAN ENGINE LEAK CHECKS GOOD. NO DEFECTS NOTED. (M)
- [SDR EISA99002](https://openairdocs.org/sdr/EISA99002.md): Valve · malfunctioned · Jan 12, 1999 · N721RW · Boeing 7272M7 · Cabin Pressure Control System
  > CLIMBING THROUGH FL 27 RED CARGO DOOR LIGHT ILLUMINATED. RED DOOR WARNING LIGHT AND AMBER HOOKS UNLOCKED LIGHT ILLUMINATED ON POWER MASTER CONTROL. LOUD BANG HEARD BEFORE RED CARGO DOOR ILLUMINATED. HIGH CABIN DIFFERENTIAL PRESURE (8) HAD TO CLOSE CABIN HEA
- [SDR EISA99001](https://openairdocs.org/sdr/EISA99001.md): Control Box · malfunctioned · Dec 29, 1998 · N721RW · Boeing 7272M7 · Cargo/Baggage Doors
  > RED CARGO LIGH TON FLIGHT ENGINEERS PANEL ILLUMINATED, CHECK MASTER CONTROL OF CARGO DOOR AND HOOKS UNLOCKED LIGHT ILLUMINATED. CHECKLIST (ABNORMAL) COMPLETED NR 4 AMBER LIGHT ON CARGO DOOR MASTER CONTROL BOX WAS ILLUMINATED. CLIMBING THROUGH 17,000 FEET, A
- [SDR EISA98244](https://openairdocs.org/sdr/EISA98244.md): Actuator · failed · Sep 30, 1998 · N721RW · Boeing 7272M7 · Trailing Edge Flap Control System
  > AFTER TAKEOFF FROM ORB WHILE RETRACTING FLAPS FROM 5 DEGREES TO 2 DEGREES NR 4 LEADING EDGE DEVICE FAILED TO RETRACT. ACCOMPLISHED APPROPRIATE CHECKLIST, CONTACTED EXPRESS ONE DISPATCH AND WAS DIRECTED TO CPH. GENERATED FROM PILOT REPORT. REMOVED AND REPLAC
- [SDR 98ZZZM797](https://openairdocs.org/sdr/98ZZZM797.md): Switch · failed · Sep 30, 1998 · N721RW · Boeing 7272M7 · Leading Edge Slat Position Indicating System
  > AFTER TAKEOFF FROM ORB WHILE RETRACTING FLAPS FROM 5 DEGREES TO 2 DEGREES NR 4 LEADING EDGE DEVICE FAILED TO RETRACT. ACCOMPLISHED APPROPRIATE CHECKLIST, CONTACTED EXPRESS ONE DISPATCH AND WAS DIRECTED TO CPH. GENERATED FROM PILOT REPORT. REMOVED AND REPLAC
- [SDR EISA98220](https://openairdocs.org/sdr/EISA98220.md): Annunciator · malfunctioned · Sep 19, 1998 · N721RW · Boeing 7272M7 · Trailing Edge Flap Control System
  > AFTER TAKEOFF NR 2 LEADING EDGE FLAP LIGHT ON THE F/E ANNUNCIATOR PANEL WAS NOT ILLUMINATED, ALONG WITH THE LEADING EDGE FLAP AMBER LIGHT ON THE PILOTS FO RWARD PANEL. AIR TURN BACK TO ATH. GENERATED FROM PILOT REPORT. CYCLED FLAP THROUGH RANGES. OPS CHECK
- [SDR EISA98084](https://openairdocs.org/sdr/EISA98084.md): Bulb · failed · Apr 5, 1998 · N721RW · Boeing 7272M7 · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHT BULB INOPERATIVE. GENERATED BY PILOT REPORT. RELAMPED AS REQUIRED PER MM 30-00, CHECK GOOD. (M)
- [SDR EISA98073](https://openairdocs.org/sdr/EISA98073.md): Strip · loose · Apr 4, 1998 · N721RW · Boeing 7272M7 · Emergency Lighting
  > ESCAPE PATH LIGHTING STRIP LOOSE BEHIND SEAT 22D, STRIP IS CAUSING PASSENGERS TO TRIP. GENERATED BY PILOT REPORT. SECURED AS REQUIRED, GOOD FOR SERVICE MM 33-00. (M)
- [SDR EISA98072](https://openairdocs.org/sdr/EISA98072.md): Bulb · failed · Apr 4, 1998 · N721RW · Boeing 7272M7 · Emergency Lighting
  > L-1 DOOR EMERGENCY EXIT LIGHT BULB INOPERATIVE. GENERATED BY PILOT REPORT. RELAMPED AS REQUIRED IAW MM 33-00. (M)
- [SDR EISA98060](https://openairdocs.org/sdr/EISA98060.md): Cover · loose · Mar 25, 1998 · N721RW · Boeing 7272M7 · Emergency Lighting
  > FOUND R2 EMERGENCY LIGHT COVER IS LOOSE DURING CREW MEMBER WALKAROUND (PILOT REPORT P-49). RESECURED R2 EMERGENCY LIGHT COVER AS REQUIRED. (M)
- [SDR EISA98061](https://openairdocs.org/sdr/EISA98061.md): Lights · loose · Mar 22, 1998 · N721RW · Boeing 7272M7 · Emergency Lighting
  > FOUND FLOOR LIGHTING ON ROW 32D LOOSE DURING CREW MEMBER WALKAROUND (PILOT REPORT P-25). RESECURED AS REQUIRED. OK FOR SERVICE. (M)
- [SDR EISA98059](https://openairdocs.org/sdr/EISA98059.md): Light · inoperative · Mar 21, 1998 · N721RW · Boeing 7272M7 · Emergency Lighting
  > DURING SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOPERATIVE OVER MAIN ENTRY DOOR. REMOVED AND REPLACED EMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR MM 33-00. (M)
- [SDR EISA98068](https://openairdocs.org/sdr/EISA98068.md): Bulb · failed · Mar 11, 1998 · N721RW · Boeing 7272M7 · Emergency Lighting
  > LIGHT BULB INOPERATIVE IN EXIT SIGN ROW 20. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED LIGHT BULBS ON OVERWING EXIT SIGN. (M)
- [SDR EISA97157](https://openairdocs.org/sdr/EISA97157.md): Hyd Tube · cracked · Jul 9, 1997 · N721RW · Boeing 7272M7 · Hydraulic System, Main
  > DURING C-CHECK, FOUND 'A' SYSTEM SUPPLY LINE AT STATION 1148 LEAKING AT CRACK. REPLACED LINE PER STANDARD PRACTICES AND 20-12-5. (M)
- [SDR EISA97163](https://openairdocs.org/sdr/EISA97163.md): Battery Pack · discharged · Jul 6, 1997 · N721RW · Boeing 7272M7 · Emergency Lighting
  > DURING C-CHECK, L-2 OVERHEAD EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT BATTERY PACK IAW B727 MM 33-50-71, OPS CHECK GOOD IAW B727 MM 33-50-01. (M)
- [SDR EISA97162](https://openairdocs.org/sdr/EISA97162.md): Hinge Fairing · cracked · Jul 6, 1997 · N721RW · Boeing 7272M7 · Landing Gear Doors
  > DURING C-CHECK, FOUND RIGHT WING DOOR, FORWARD UPPER OUTBOARD FAIRING HINGES HALD IS BROKEN AT FORWARD END. REPLACED RIGHT WING DOOR FORWARD UPPER OUTBOARD HINGE IAW SRM B727 51-10-1. INSTALLED PER B727 51-30-02 SRM, PERFORMED GEAR SWING OPS NORMAL. (M)
- [SDR EISA97161](https://openairdocs.org/sdr/EISA97161.md): Carriage · cracked · Jul 6, 1997 · N721RW · Boeing 7272M7 · Trailing Edge Flaps
  > DURING C-CHECK, FOUND LEFT WING OUTBOARD FLAP INBOARD TRACK SEQUENCE CARRIAGE CRACKED. REMOVED AND INSTALLED LEFT FLAP SEQUENCE CARRIAGE IAW B727 MM 27-51-01. (M)
- [SDR EISA97160](https://openairdocs.org/sdr/EISA97160.md): Battery Charger · inoperative · Jul 6, 1997 · N721RW · Boeing 7272M7 · Emergency Lighting
  > DURING C-CHECK, FOUND CENTER AISLE OVERWING EMERGENCY LIGHT BATTERY CHARGER INOP. CLEANED AND RESEATED C/B ON CHARGER, OPS CHECK NORMAL. (M)
- [SDR EISA97159](https://openairdocs.org/sdr/EISA97159.md): Fitting · cracked · Jul 6, 1997 · N721RW · Boeing 7272M7 · Trailing Edge Flaps
  > DURING C-CHECK, FOUND T-FITTING ON RIGHT ELEPHANT EAR AT ATTACH POINT CRACKED. REMOVED AND REPLACED T-FITTING RIGHT ELEPHANT EAR IAW B727 SRM 51-10-1, OPS CHECK SEQ 23. (M)
- [SDR EISA97158](https://openairdocs.org/sdr/EISA97158.md): Carriage · corroded · Jul 6, 1997 · N721RW · Boeing 7272M7 · Trailing Edge Flaps
  > DURING C-CHECK, FOUND NR 2 FLAP CARRIAGE HAS MOD LEVEL CORROSION UNDER HAT BUSHING ON SPINDLE. REPLACED NR 2 FLAP CARRIAGE IAW 27-51-13 SEQ 23 FOR OPS CHECK RII. (M)
- [SDR EISA97154](https://openairdocs.org/sdr/EISA97154.md): Sliding Window · out of adjust · Jun 26, 1997 · N721RW · Boeing 7272M7 · Flight Compartment Windows
  > DURING C-CHECK, EXTERIOR EMERGENCY HANDLE FOR THE COCKPIT F/O SLIDING WINDOW INOP. WILL NOT OPEN WINDOW WHEN OPERATIONAL. ADJUSTED EMERGENCY HANDLE F/O SLIDING WINDOW IAW 727 MM 56-12-01, OPS CHECK NORMAL. (M)
- [SDR EISA97149](https://openairdocs.org/sdr/EISA97149.md): Rib · cracked · Jun 24, 1997 · N721RW · Boeing 7272M7 · Trailing Edge Flaps
  > DURING C-CHECK, 1.5 INCH CRACK ON TOP INBOARD INTERNAL RIB AT LEFT OUTBOARD FLAP. REPAIRED CRACK PER B727 SRM 57-50-4. (M)
- [SDR EISA97148](https://openairdocs.org/sdr/EISA97148.md): Structure · corroded · Jun 24, 1997 · N721RW · Boeing 7272M7 · Trailing Edge Flaps
  > DURING C-CHECK, RIGHT INBOARD FLAP NR 5 BEARING (FOR CARRIAGE) OUTBOARD ATTACH STRUCTURE CORRODED. REMOVED RT INBOARD FLAP NR 5 ATTACH STRUCTURE. REMOVED FASTENERS BECAUSE OF CORROSION. INSTALLED NEW FASTENERS AND ATTACH STRUCTURE IAW B727 SRM 51-30-02. (M
- [SDR EISA97147](https://openairdocs.org/sdr/EISA97147.md): Skin · dented · Jun 24, 1997 · N721RW · Boeing 7272M7 · Trailing Edge Flaps
  > DURING C-CHECK, RIGHT WING, INBOARD FOREFLAP HAS A 2.5 INCH CRACK AND 1.5 INCH NARROW DENT ON UPPER SURFACE OUTBOARD IN INBOARD END. REPAIRED CORE AND INSTALLED FIBERGLASS OVERLAY IAW SRM IAW SRM 51-40-06. (M)
- [SDR EISA97146](https://openairdocs.org/sdr/EISA97146.md): Support · cracked · Jun 24, 1997 · N721RW · Boeing 7272M7 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FORWARD CARGO COMPARTMENT LEFT SIDE CARGO FLOOR SUPPORT, HAS CRACK ABOVE STRINGER 26 STATION 540-560. REPAIRED CRACK IAW SRM 51-20-1. (M)

Next page: https://openairdocs.org/deregistered/N721RW-2007-08-15/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 = 'N721RW' AND deregistration_id = 'N721RW-2007-08-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N721RW-2007-08-15/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.