# Service difficulty reports: N490DA, cancelled Feb 16, 2001

A list on [N490DA, cancelled Feb 16, 2001](https://openairdocs.org/deregistered/N490DA-2001-02-16.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 · 79 reports

- [SDR DL72S002229](https://openairdocs.org/sdr/DL72S002229.md): Battery Pack · discharged · Nov 14, 2000 · N490DA · Boeing 727232 · Emergency Lighting
  > AFT CABIN O/H EMERGENCY LIGHT BETWEEN LAVS INOP. REPLACED BATTERY PACK.
- [SDR DL72S000758](https://openairdocs.org/sdr/DL72S000758.md): Actuator · leaking · Apr 19, 2000 · N490DA · Boeing 727232 · Drag Control Actuator
  > LOSS OF SYSTEM A HYDRAULIC IN FLIGHT. INITIAL 0 QTY INDICATION WITH NO OTHER ABNORMALS. THEN SYS A ENG 1 AND 2 PUMPS FLICKERED AND RECOVERED SEVERAL TIMES. POM PROCEDURES FOR LOSS OF SYS A COMPLIED WITH. LANDED JFKL AND TOWED TO GATE. ZERO QTY INDICATION
- [SDR DL72S000693](https://openairdocs.org/sdr/DL72S000693.md): Rib · cracked · Apr 11, 2000 · N490DA · Boeing 727232 · Leading Edge Devices
  > RIB NUMBER 7 CRACKED MANUFACTURED DOUBLER. INSTALLED DOUBLER PER 57-54-0 FIG 814 MM.
- [SDR DL72S992700](https://openairdocs.org/sdr/DL72S992700.md): Shear Clip · cracked · Dec 9, 1999 · N490DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > THE SHEAR CLIP FOR THE FS 1263 FRAME BETWEEN STRINGERS 13L AND 14L WAS FOUND WITH A 1 INCH CRACK IN THE SKIN FLANGE RADIUS. THE SKIN FLANGE WAS TRIMMED OFF TO REMOVE THE CRACK. THE SHEAR CLIP WAS RESTORED BY INSTALLING AN ALUMINUM REPAIR ANGLE PER ER/A 3689
- [SDR DL72S992683](https://openairdocs.org/sdr/DL72S992683.md): Bracket · cracked · Dec 8, 1999 · N490DA · Boeing 727232 · Leading Edge Slat Actuator
  > NR 1 LEADING EDGE SLAT I/B AND O/B ACTUATOR MOUNT BRACKETS CRACKED. REPAIRED PER MM 57-20-21.
- [SDR DL72S992682](https://openairdocs.org/sdr/DL72S992682.md): Skin · cracked · Dec 8, 1999 · N490DA · Boeing 727232 · Leading Edge Devices
  > A.5 INCH CRACK AT FWD LWR SIDE OF NR 2 MIDFLAP AT I/B AFT FLAP ACTUATING ROD CUTOUT. REPAIRED PER MM 57-52-0 AND ERA 368899-14.
- [SDR DL72S992680](https://openairdocs.org/sdr/DL72S992680.md): Beam · cracked · Dec 8, 1999 · N490DA · Boeing 727232 · Cargo/Baggage Doors
  > C-2 DOOR HORIZONTAL BEAM WEB DAMAGED AT LIGHTNING HOLE AT DOOR HANDLE SNUBBER SRM 52-30-2D FIG 802D.
- [SDR DL72S992679](https://openairdocs.org/sdr/DL72S992679.md): Stiffener · cracked · Dec 8, 1999 · N490DA · Boeing 727232 · Leading Edge Devices
  > VERTICAL SPAR STIFFENER CRACKED NR 7 SLAT O/B SIDE OF I/B TRACK. REPLACED SPAR STIFFENER PER MM 57-20-21.
- [SDR DL72S992678](https://openairdocs.org/sdr/DL72S992678.md): Angle · cracked · Dec 8, 1999 · N490DA · Boeing 727232 · Leading Edge Devices
  > COVE SKIN ANGLE CRACKED 15 INCHES O/B OF NR 7 SLAT ACTUATOR ROD. REPAIRED PER MM 57-54-0.
- [SDR DL72S992634](https://openairdocs.org/sdr/DL72S992634.md): Power Supply · failed · Dec 1, 1999 · N490DA · Boeing 727232 · Emergency Lighting
  > RT FWD EMERG EXIT HATCH EMERGENCY LT INOP. FOUND FUSE BROKEN OFF IN SOCKET OF PWR SUPPLY. REPLACED SAME.
- [SDR DL72S992365](https://openairdocs.org/sdr/DL72S992365.md): Battery Pack · discharged · Oct 24, 1999 · N490DA · Boeing 727232 · Emergency Lighting
  > ON L/O, FOUND L1 EMER EXIT LIGHT INOP. REPLACED BATTERY PACK, RACK AND REFLECTOR.
- [SDR DL72S992364](https://openairdocs.org/sdr/DL72S992364.md): Battery Pack · discharged · Oct 24, 1999 · N490DA · Boeing 727232 · Emergency Lighting
  > ON L/O, FOUND LT OVERWING EMER EXIT LIGHT INOP. REPLACED BATTERY PACK, CHECKS GOOD.
- [SDR DL72S991647](https://openairdocs.org/sdr/DL72S991647.md): Mount · corroded · Jul 14, 1999 · N490DA · Boeing 727232 · Engine Mount Section
  > ON HUSHKIT MOD, FOUND NR 2 AFT ENG MOUNT CORRODED. REPLACED MOUNT.
- [SDR DL72S991646](https://openairdocs.org/sdr/DL72S991646.md): Angle · corroded · Jul 12, 1999 · N490DA · Boeing 727232 · Engine Mount Section
  > ON HUSHKIT MODIFICATION, NR 2 ENG AFT MOUNT CHORD ANGLE CORRODED. REPLACED ANGLE WITH NEW MANUFACTURED PART LEFT SIDE.
- [SDR DL72S991053](https://openairdocs.org/sdr/DL72S991053.md): Rib · cracked · May 13, 1999 · N490DA · Boeing 727232 · Horizontal Stabilizer, Spar/Rib
  > LT ELEV HINGE SUPPORT RIB CRACKED BETWEEN NR 3 AND 4 BAL BOARDS AT LOWER END. REPAIRED PER MM 55-10-31.
- [SDR DL72S990743](https://openairdocs.org/sdr/DL72S990743.md): Skin · cracked · Apr 3, 1999 · N490DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A FEW CRACKS IN CONSECUTIVE SKIN FRAME BAYS. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT A
- [SDR DL72S990714](https://openairdocs.org/sdr/DL72S990714.md): Skin · cracked · Mar 30, 1999 · N490DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS IN THREE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND
- [SDR DL72S990713](https://openairdocs.org/sdr/DL72S990713.md): Skin · cracked · Mar 30, 1999 · N490DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 43 TOTAL CRACKS ALONG THE PANEL. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PANEL
- [SDR DL72S990712](https://openairdocs.org/sdr/DL72S990712.md): Skin · cracked · Mar 30, 1999 · N490DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 71 TOTAL CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WI
- [SDR DL72S990169](https://openairdocs.org/sdr/DL72S990169.md): Skin · corroded · Jan 26, 1999 · N490DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION AT FS 485 AND STRINGER 28R. THE CORROSION WAS REMOVED WITH A 7 X 3.5 CUTOUT. THERE WERE THREE OTHER REPAIR DOUBLERS NEAR THIS AREA FOR REPAIRS OF SIMILAR CUTOUTS. THE REPAIRS WERE REMOVED RESULTING IN 4
- [SDR DL72S990159](https://openairdocs.org/sdr/DL72S990159.md): Angle · corroded · Jan 21, 1999 · N490DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING MV-1 CHECK, CORROSION ON SUPPORT ANGLE AT STA 740 STR 27 RT. REPLACED ANGLE PER M/M 53-11-0 FIG 826.
- [SDR DL72S990149](https://openairdocs.org/sdr/DL72S990149.md): Floorbeam · corroded · Jan 18, 1999 · N490DA · Boeing 727232 · Fuselage Main, Floor Beam
  > FOUND DURING MV-1 CORROSION VISIT NRC 46, CORROSION AT FLOORBEAM STA 344 RBL 5 TO LBL 60 UPPER AND LOWER SIDES. REPAIRED PER SRM 53-10-8 FIG 11.
- [SDR DL72S990148](https://openairdocs.org/sdr/DL72S990148.md): Frame · cracked · Jan 18, 1999 · N490DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING MV-1 CORROSION VISIT NRC 16,.25 INCH CRACK VISIBLE AT AFT ENTRY DOOR FRAME UPPER LT LOCATION. REPAIRED PER SRM 53-10-9 FIG 11.
- [SDR DL72S982596](https://openairdocs.org/sdr/DL72S982596.md): Battery Pack · discharged · Dec 21, 1998 · N490DA · Boeing 727232 · Emergency Lighting
  > LT MID WING SLIDE EMERGENCY LIGHT INOP. REPLACED BATTERY RACK M954, OPS CHKS GOOD.
- [SDR DL72S982595](https://openairdocs.org/sdr/DL72S982595.md): Battery · discharged · Dec 21, 1998 · N490DA · Boeing 727232 · Emergency Lighting
  > BOTH FWD EXIT SLIDE EMERGENCY LIGHTS INOP. REPLACED BATTERY ON RACK M982, OPS CHKS GOOD.
- [SDR DL72S981409](https://openairdocs.org/sdr/DL72S981409.md): Battery · discharged · Jul 5, 1998 · N490DA · Boeing 727232 · Emergency Lighting
  > FLASHLIGHT NOT BLINKING. REPLACED FLASHLIGHT BATTERY, BULB, AND PLAC. OPS CKS GOOD.
- [SDR DL72S980816](https://openairdocs.org/sdr/DL72S980816.md): Power Supply · inoperative · Apr 16, 1998 · N490DA · Boeing 727232 · Emergency Lighting
  > FOUND EMERGENCY LIGHT SECTION IN CABIN INOP. REPLACED PWR SUPPLY, SYSTEM CHECKS NORMAL.
- [SDR DL72S980526](https://openairdocs.org/sdr/DL72S980526.md): Spar · cracked · Mar 6, 1998 · N490DA · Boeing 727232 · Elevator, Spar/Rib
  > THE LT ELEVATOR REAR SPAR WAS FOUND WITH A TYPICAL CRACK AT THE SECOND FROM THE OUTBD END HINGE. THE CRACK WAS STOP DRILLED PER THE REQUIREMENTS OF BOEING S/B 727-55-0089 AND IS BEING TRACKED PER ER/A 364195-14AD. THE PERMANENT REPAIR WILL MODIFY THE SPAR PE
- [SDR DL72S980527](https://openairdocs.org/sdr/DL72S980527.md): Channel · cracked · Mar 5, 1998 · N490DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > THE FS 1263 UPPER CHANNEL ON THE LT AFT VENTRAL STAIRWELL TORQUE BOX WAS FOUND WITH A 1.5 INCH CRACK IN THE TYPICAL LOCATION PER S/B 727-53-0129. THE DAMAGED CHANNEL WAS REPLACED PER THE S/B AND DOCUMENTED PER ER/A 364193-14AD.
- [SDR DL72S972515](https://openairdocs.org/sdr/DL72S972515.md): Battery · discharged · Dec 2, 1997 · N490DA · Boeing 727232 · Emergency Lighting
  > ON PREFLIGHT, FWD EMERGENCY FLASHLIGHT WOULD NOT TEST. REPLACED BATT.
- [SDR DL72S972318](https://openairdocs.org/sdr/DL72S972318.md): Ballast · failed · Nov 10, 1997 · N490DA · Boeing 727232 · Passenger Compartment Lighting
  > SMOKE IN AFT 48 SECTION. REPLACED AFT LAV LIGHT BALLAST M276.
- [SDR DL72S971509](https://openairdocs.org/sdr/DL72S971509.md): Stiffener · cracked · Jul 30, 1997 · N490DA · Boeing 727232 · Wing Miscellaneous Structure
  > WING L/E SPAR STIFFENER CRACKED NR 4 SLAT INBD TRACK INBD SIDE. REPLACED ANGLE PER M/M 57-20-21.
- [SDR DL72S971508](https://openairdocs.org/sdr/DL72S971508.md): Angle · cracked · Jul 30, 1997 · N490DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON B1 LETTER CK,.5 INCH CRACK FWD LOWER RT INBD VERTICAL KEEL BEAM ANGLE AT STA 870. REPAIRED PER SRM 53-10-9.
- [SDR DL72S971173](https://openairdocs.org/sdr/DL72S971173.md): Water Heater · overheated · Jun 17, 1997 · N490DA · Boeing 727232 · Lavatories
  > SMOKE REPORTED IN AFT CABIN BY F/A, CONFIRMED BY SECOND OFFICER. BOTH AFT LAV SMOKE DETECTORS ALARMED, DID SMOKE CLEARANCE CHECKLIST. REPLACED AFT LAV WATER HEATER, CHECKS NORMAL.
- [SDR DL72S970162](https://openairdocs.org/sdr/DL72S970162.md): Power Contl Unit · leaking · Jan 27, 1997 · N490DA · Boeing 727232 · Elevator Control System
  > ATB - DUE TO HYDRAULIC FLUID LOSS FROM THE LEFT ELEVATOR, POWER CONTROL UNIT LEAKS.
- [SDR DL72S962058](https://openairdocs.org/sdr/DL72S962058.md): Batteries · discharged · Sep 5, 1996 · N490DA · Boeing 727232 · Emergency Lighting
  > CENTER AISLE EMERGENCY EXIT LIGHT BETWEEN AFT LAVS DID NOT COME ON DURING TEST. REPLACED BATTERIES AND BULBS OPS NORMAL.
- [SDR DL72S962057](https://openairdocs.org/sdr/DL72S962057.md): Light · inoperative · Sep 5, 1996 · N490DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ABOVE L-2 DOOR DID NOT COME ON DURING TEST. REPLACED LIGHT ASSY, OPS NORMAL.
- [SDR DL72S961273](https://openairdocs.org/sdr/DL72S961273.md): Angle · cracked · May 24, 1996 · N490DA · Boeing 727232 · Leading Edge Devices
  > COVE SKIN ATTACH ANGLE CRACKED 1 INCH AT ANTI-ICE TUBE CUTOUT, NR 2 SLAT. REPAIRED PER M/M 57-54-0.
- [SDR DL72S961287](https://openairdocs.org/sdr/DL72S961287.md): Skin · damaged · May 22, 1996 · N490DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > AIRCRAFT STRUCK BY A GROUND SERVICE TRUCK, DAMAGE CONSISTED OF A DENTED SKIN, A BROKEN STRINGER AND A CRACKED SHEAR CLIP. THE DENT WAS REMOVED WITH A CUTOUT AT STA 1080, THE STRINGER HAS BEEN CUT AND WILL BE SPLICED IN THE BAYS FWD AND AFT OF THE DAMAGE. ALS
- [SDR DL72S961249](https://openairdocs.org/sdr/DL72S961249.md): Skin · dented · May 21, 1996 · N490DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FROM AC LOG 759101001, FUSELAGE SKIN DENTED FS 1080 THROUGH 1100 STR 23L. STR 23L AND SKIN REPAIRED PER ERA 303624-14.
- [SDR DL72S954494](https://openairdocs.org/sdr/DL72S954494.md): Doubler · cracked · Nov 14, 1995 · N490DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, NR 4 MIDFLAP WAS FOUND WITH CRACKED DOUBLER AT AFT CLOSE OUT RIB LOWER AFT CORNER. REPAIRED PER MM 57-52-0.
- [SDR DL72S954729](https://openairdocs.org/sdr/DL72S954729.md): Le Skin · worn · Nov 9, 1995 · N490DA · Boeing 727232 · Trailing Edge Flaps
  > L/E EDGE SKIN WORN AT I/B END OF NR 1 MIDFLAP. REPAIRED PER MM 57-53-00.
- [SDR DL72S954453](https://openairdocs.org/sdr/DL72S954453.md): Rib · cracked · Nov 6, 1995 · N490DA · Boeing 727232 · Wing, Rib/Bulkhead
  > DURING ACCOMPLISHMENT OF EO 4-58560-3AD, A CRACK WAS DISCOVERED IN THE VERTICAL FLANGE OF THE LBL 70.5 WING RIB CHORD. THE CRACK RAN FROM ONE OF THE UPPER FASTENERS IN THE VERTICAL FLANGE AT STA 760.95 DOWN TO THE HORIZONTAL FLANGE. THIS CRACK REQUIRES AN ALT
- [SDR DL72S960426](https://openairdocs.org/sdr/DL72S960426.md): Frame · cracked · Nov 3, 1995 · N490DA · Boeing 727232 · Service Doors
  > DURING INSPECTION, A 2 INCH CRACK WAS FOUND EMANATING FROM THE CORNER OF THE UPPER HINGE CUTOUT ON THE FWD FRAME OF THE LT AFT SERVICE DOOR. IN ACCORDANCE WITH B727 SRM 52-40-2 FIG 4, A DOUBLER WAS INSTALLED AROUND THE DAMAGE.
- [SDR DL72S954493](https://openairdocs.org/sdr/DL72S954493.md): Doubler · cracked · Nov 1, 1995 · N490DA · Boeing 727232 · Trailing Edge Flaps
  > NR 2 MIDFLAP WAS FOUND TO HAVE CRACKED DOUBLER AT AFT LOWER SPAR ANGLE REPAIR AT I/B QUADRANT CUTOUT. REPAIR WAS PERFORMED PER M/M 57-52-0 FIG 802. FOUND DURING SHOP MTC VISIT.
- [SDR DL72S954145](https://openairdocs.org/sdr/DL72S954145.md): Stringer · cracked · Oct 30, 1995 · N490DA · Boeing 727232 · Wing, Longeron/Stringer
  > FOUND DURING HMV, RT OUTER WING UPPER STRINGER TO RIB SHOWS CRACK INDICATION ON FASTENER HOLE AT W.S. 656.5, STRINGER 10. MANUFACTURED REPAIR DOUBLER PER M/M 57-13-0 AND INSTALLED DOUBLER PER M/M 57-13-0, PG. 801.
- [SDR DL72S954143](https://openairdocs.org/sdr/DL72S954143.md): Rib · cracked · Oct 30, 1995 · N490DA · Boeing 727232 · Wing, Rib/Bulkhead
  > FOUND ON HMV, RIGHT WING STRINGER TO RIB FASTENER HOLE HAS CRACK INDICATION AT STA. 629, 3RD STRINGER FWD FROM AFT SPAR. STOP DRILLED CRACK PER M/M 57-13-0.
- [SDR DL72S954134](https://openairdocs.org/sdr/DL72S954134.md): Skin · punctured · Oct 30, 1995 · N490DA · Boeing 727232 · Cargo/Baggage Doors
  > DURING INSPECTION, C-3 CARGO DOOR WAS FOUND WITH INNER SKIN PUNCTURED, REPAIRED PER SRM 52-00-3.
- [SDR DL72S954129](https://openairdocs.org/sdr/DL72S954129.md): Skin · dented · Oct 29, 1995 · N490DA · Boeing 727232 · Ailerons
  > DURING INSPECTION, FOUND LEFT OUTBOARD AILERON WITH DENTS IN UPPER SKIN. ACCOMPLISHED REPAIRS PER SRM 57-50 -5.
- [SDR DL72S954495](https://openairdocs.org/sdr/DL72S954495.md): Doubler · disbonded · Oct 28, 1995 · N490DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FUSELAGE SKIN REPAIR AT AFT LAVATORY SERVICE PANEL CUTOUT, FS 1158 TO FS 1183, BETWEEN S-20L AND S-24L. DURING ACCOMPLISHMENT OF EO 4-69078-3AD, THE INTERNAL BONDED DOUBLER WAS FOUND DISBONDED IN SEVERAL LOCATIONS AROUND THE AFT LAVATORY SERVICE PANEL. AFFEC

Next page: https://openairdocs.org/deregistered/N490DA-2001-02-16/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 = 'N490DA' AND deregistration_id = 'N490DA-2001-02-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N490DA-2001-02-16/reports

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