# Service difficulty reports: N495DA, cancelled Feb 16, 2001

A list on [N495DA, cancelled Feb 16, 2001](https://openairdocs.org/deregistered/N495DA-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 · 57 reports

- [SDR DL72K001416](https://openairdocs.org/sdr/DL72K001416.md): Mount · cracked · Jul 25, 2000 · N495DA · Boeing 727232 · Engine Mount Section
  > WHILE ACCOMPLISHING INSPECTIONS OF THE FWD ENGINE MOUNT SUPPORT FITTING ON THE NR 3 PYLON PER AD 97-05-08 AND BAC S/B 727-54A0010, A CRACK INDICATION WAS NOTED IN HOLE ''B''. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK AND AN ADDITIONAL.0312 INCH OVERSIZE FOR
- [SDR DL72K001403](https://openairdocs.org/sdr/DL72K001403.md): Lap Joint · cracked · Jul 23, 2000 · N495DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING AN LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 480 A CRACK INDICATION WAS NOTED. INTERNAL MFEC INSPECTION OF THE ENTIRE LAP JOINT. CONFIRMED A SINGLE CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN BETWEEN FS 420
- [SDR DL72K001392](https://openairdocs.org/sdr/DL72K001392.md): Light · malfunctioned · Jul 20, 2000 · N495DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHT BETWEEN L1 AND R1 DOORS FAILED TO TURN OFF. REPLACED EMERGENCY LIGHT RACK. CHECKS GOOD.
- [SDR DL72K001062](https://openairdocs.org/sdr/DL72K001062.md): Battery Pack · inoperative · May 30, 2000 · N495DA · Boeing 727232 · Emergency Lighting
  > ON LAYOVER, FOUND CENTER AISLE OVERWING EMERGENCY EXIT OVERWING SIGN INOP. REPLACED BATTERY PACK.
- [SDR DL72K000945](https://openairdocs.org/sdr/DL72K000945.md): Light · inoperative · May 12, 2000 · N495DA · Boeing 727232 · Emergency Lighting
  > FOUND DURING L/O, EXT EMERGENCY EXIT SLIDE LIGHT ON MID CARGO DOOR RIGHT SIDE INOP. REPLACED BATTERY PACK RACK ASSY, CKS NORMAL PER M/M.
- [SDR DL72K000545](https://openairdocs.org/sdr/DL72K000545.md): Accessory Unit · failed · Mar 19, 2000 · N495DA · Boeing 727232 · Landing Gear Retraction/Extension System
  > AFTER NORMAL T/O AT LGA, THE LDG HANDLE WOULD NOT RAISE ABOVE THE OFF POSITION. RETURNED TO BLOCK. REPLACED LANDING GEAR ACCESSORY UNIT.
- [SDR DL72K000346](https://openairdocs.org/sdr/DL72K000346.md): Battery Pack · discharged · Feb 21, 2000 · N495DA · Boeing 727232 · Emergency Lighting
  > RIGHT HAND OVERWING AFT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72K992754](https://openairdocs.org/sdr/DL72K992754.md): Battery Pack · discharged · Dec 15, 1999 · N495DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHTS ON AFT CARGO DID NOT ILLUMINATE DURING TEST. REPLACED BATTERY PACK.
- [SDR DL72K992633](https://openairdocs.org/sdr/DL72K992633.md): Light · inoperative · Dec 1, 1999 · N495DA · Boeing 727232 · Emergency Lighting
  > AFT CARGO DOOR EMERG LIGHT INOP. REPLACED BATTERY AT RACK M957, CHECKS GOOD.
- [SDR DL72S992592](https://openairdocs.org/sdr/DL72S992592.md): Light · failed · Nov 21, 1999 · N495DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY EXIT SIGN TOO DIM TO SEE ON EMERGENCY PWR TEST. REPLACED LIGHT ASSY.
- [SDR DL72S992505](https://openairdocs.org/sdr/DL72S992505.md): Rib · cracked · Nov 12, 1999 · N495DA · Boeing 727232 · Leading Edge Devices
  > OUTBOARD RIB CRACKED. REPAIRED PER M/M 57-54-0 FIG 814.
- [SDR DL72S992504](https://openairdocs.org/sdr/DL72S992504.md): Rib · cracked · Nov 12, 1999 · N495DA · Boeing 727232 · Leading Edge Devices
  > NR 11 RIB CRACKED. REPAIRED RIB PER M/M 57-54-0.
- [SDR DL72S992503](https://openairdocs.org/sdr/DL72S992503.md): Rib · cracked · Nov 12, 1999 · N495DA · Boeing 727232 · Leading Edge Devices
  > NR 8 RIB CRACKED IN CORNER OF RADIUS. REPAIRED RIB PER M/M 57-54-0, FIG 814.
- [SDR DL72S992502](https://openairdocs.org/sdr/DL72S992502.md): Skin · cracked · Nov 12, 1999 · N495DA · Boeing 727232 · Leading Edge Devices
  > SKIN CRACKED AT CORNER OF T DUCT HOLE. REPAIRED SKIN PER M/M 57-54-0, FIG 802A.
- [SDR DL72S992464](https://openairdocs.org/sdr/DL72S992464.md): Stiffener · cracked · Nov 1, 1999 · N495DA · Boeing 727232 · Wing Miscellaneous Structure
  > FOUND DURING D1 LETTER CHECK/SHUTTLE MOD NRC 69, NR 3 L/E SLAT SPAR STIFFENER CRACKED APPROX 1.5 INCH AT INBD TRACK OUTBD STIFFENER. REPLACED SPAR STIFFENER PER M/M 57-20-21 P 813.
- [SDR DL72S992426](https://openairdocs.org/sdr/DL72S992426.md): Web · cracked · Nov 1, 1999 · N495DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A.25 INCH CRACK AT LIGHTENING HOLE IN TORQUE BOX OF 48 SEC, STA 1323 LEFT SIDE. ROUTED OUT DAMAGED AREA PER M/M 53-11-0, DYE CHECK OK.
- [SDR DL72S992328](https://openairdocs.org/sdr/DL72S992328.md): Switch · failed · Oct 22, 1999 · N495DA · Boeing 727232 · Trailing Edge Flap Control System
  > RUDDER LIMITER WITH FLAPS EXT. REPLACED FLAP UP LIMIT SWITCH.
- [SDR DL72S992291](https://openairdocs.org/sdr/DL72S992291.md): Transmitter · failed · Oct 17, 1999 · N495DA · Boeing 727232 · Trailing Flap Position Indicating System
  > OUTBOARD FLAPS LOCKED OUT AT 2 DEGREES ON FLAP EXTENSION INBOUND TO ORF ON FLT 1220/17. DIVERTED TO RIC. MTC FOUND THE RT POSITION TRANSMITTER TO BE AT FAULT. REPLACED THE RT OUTBOARD POSITION TRANSMITTER, OPS CHECK NORM.
- [SDR DL72S990912](https://openairdocs.org/sdr/DL72S990912.md): Web · cracked · Apr 26, 1999 · N495DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON C2 LETTER CK, RT VERTICAL TORQUE BOX WEB CRACKED.375 INCH AT STA 1289. REPAIRED PER MM 53-11-0.
- [SDR DL72S990911](https://openairdocs.org/sdr/DL72S990911.md): Frame · cracked · Apr 26, 1999 · N495DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND AT C-2 LETTER CK, LEFT AFT ENTRY WAY DOOR FRAME HAS.375 IN VISIBLE CRACK AT UPPER CUTOUT. REPAIRED PER SRM 53-10-9.
- [SDR DL72S990357](https://openairdocs.org/sdr/DL72S990357.md): Actuator · failed · Feb 23, 1999 · N495DA · Boeing 727232 · Leading Edge Slat Actuator
  > SLC- AFTER T/O, LOST -A- SYSTEM HYDRAULIC SYSTEM. FOUND NR 2 L/E FLAP ACTUATOR LEAKING AND ACTUATOR BRACKET BROKEN. REPLACED SAME.
- [SDR DL72S990150](https://openairdocs.org/sdr/DL72S990150.md): Skin · cracked · Jan 21, 1999 · N495DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING SPECIAL HFEC INSPECTION, THE STRINGER 4R SKIN LAP SPLICE WAS FOUND WITH 4 CRACK INDICATIONS IN THE LOWER ROW OF FASTENERS OF THE INNER SKIN PANEL. THE ENTIRE LAP SPLICE WAS CUT (UPPER AND LOWER SKIN) AND REMOVED FOR FURTHER EVALUATION. THE CUT SKIN L
- [SDR DL72S990151](https://openairdocs.org/sdr/DL72S990151.md): Skin · cracked · Jan 20, 1999 · N495DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF SPECIAL HFEC AND LFEC INSPECTIONS, 82 CRACK INDICATIONS WERE FOUND IN THE LOWER ROW OF THE LOWER SKIN OF STRINGER 4R LAP SPLICE BETWEEN FS 480 TO 681. THE SKIN LAP AREA WAS CUT AWAY AND REMOVED. THE SPLICE WAS RESTORED WITH AND EXTER
- [SDR DL72S982636](https://openairdocs.org/sdr/DL72S982636.md): Skin · cracked · Dec 28, 1998 · N495DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE LT SIDE LWR FUSE SKIN AT S26L LAP SPLICE WAS FOUND WITH AN APPROX 19 INCH LONG CRACK BETWEEN BS 536 AND BS 564. THE CRACK IS LOCATED IN THE LWR OVERLAPPED SKIN, EXTENDING NEARLY HORIZ BETWEEN 20 FASTENERS IN THE LWR ROW OF THE TRIPLE ROW ATTACH PATTERN.
- [SDR DL72S981912](https://openairdocs.org/sdr/DL72S981912.md): Web · cracked · Sep 14, 1998 · N495DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > REF A/C 495 TPA LTR CHECK C-1, VERTICAL WEB CRACKED.5 INCH LT SIDE LWR LIGHTENING HOLE STA 1228. REPAIRED PER MM 53-11-0.
- [SDR DL72S971842](https://openairdocs.org/sdr/DL72S971842.md): Batteries · discharged · Sep 21, 1997 · N495DA · Boeing 727232 · Emergency Lighting
  > FWD Y/C CENTER AISLE LIGHTS VERY DIM. REPLACED BATTERIES, CHECKS GOOD.
- [SDR DL72S971841](https://openairdocs.org/sdr/DL72S971841.md): Lights · inoperative · Sep 21, 1997 · N495DA · Boeing 727232 · Emergency Lighting
  > OVERWING EMERGENCY EXIT SIGN LIGHTS INOP. REPLACED LIGHT CARTRIDGE, CHECKS NORMAL.
- [SDR DL72S971840](https://openairdocs.org/sdr/DL72S971840.md): Light · inoperative · Sep 21, 1997 · N495DA · Boeing 727232 · Emergency Lighting
  > LT OVERWING EMERGENCY EXIT SIGN LIGHTS ARE INOP. REPLACED LIGHT CARTRIDGE, CHECKS NORMAL.
- [SDR DL72S971839](https://openairdocs.org/sdr/DL72S971839.md): Rack · inoperative · Sep 21, 1997 · N495DA · Boeing 727232 · Emergency Lighting
  > LT OVERWING EMERGENCY EXIT SIGN LIGHTS INOP. REPLACED LIGHT RACK, CHECKS NORMAL.
- [SDR DL72S971774](https://openairdocs.org/sdr/DL72S971774.md): Door · damaged · Sep 8, 1997 · N495DA · Boeing 727232 · Landing Gear Doors
  > UPON LANDING, 2 MAIN TIRES BLEW CAUSING DAMAGE TO RT MAIN GEAR FLYING DOOR, RT I/B FLAP TRACK FAIRING, RT I/B TRAILING EDGE FLAP. REPLACED FLYING DOOR, REPLACED RT I/B TRAILING EDGE FLAP. REPAIRED RT I/B FLAP FAIRING.
- [SDR DL72S971251](https://openairdocs.org/sdr/DL72S971251.md): Frame · cracked · Jun 27, 1997 · N495DA · Boeing 727232 · Fuselage Main, Frame
  > A 3 INCH CRACK IN FS 930 FRAME AT STR 14R. TRIMMED UPPER FRAME PER SRM 53-10-4 FIG 25. DYE CHECKED PER SRM 53-10-4, NO CRACKS FOUND. FORMED REPAIR ANGLE FROM 071. 7075-0 SENT TO HEAT TREAT PER SRM 53-10-4. COMPLETED REPAIR PER SRM 53-10-4.
- [SDR DL72S971239](https://openairdocs.org/sdr/DL72S971239.md): Stringer · corroded · Jun 23, 1997 · N495DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > STRINGER 28R WAS CUT AT STA 980 IN ORDER TO REMOVE CORROSION. THE AFT SECTION OF THE STRINGER, TO STA 1010 WAS REPLACED AND A NEW STRINGER SECTION WAS SPLICED IN. THE STRINGER WAS TOO THICK TO BE REPAIRED PER THE SRM. THE REPAIR WILL CONSIST OF SPLICING IN
- [SDR DL72S971688](https://openairdocs.org/sdr/DL72S971688.md): Chord · cracked · Jun 19, 1997 · N495DA · Boeing 727232 · Trailing Edge Flaps
  > THE NR 2 MIDFLAP BN242 WAS FOUND WITH A CRACK IN THE AFT CHORD 41 FROM OB END OF FLAP DURING SHOP INSPECTION. THIS CONDITION WAS REPAIRED BY STOP DRILLING CRACK AND INSTALLING A DOUBLER PER 727 MM 57-52-0.
- [SDR DL72S971590](https://openairdocs.org/sdr/DL72S971590.md): Flap · damaged · Jun 19, 1997 · N495DA · Boeing 727232 · Trailing Edge Flaps
  > NR 2 MID FLAP BN242 AFT SPAR CRACKED 32 FROM I/B END OF SPAR REPAIRED PER M/M 57-52-0 FIG 802.
- [SDR DL72S971236](https://openairdocs.org/sdr/DL72S971236.md): Skin · separated · Jun 17, 1997 · N495DA · Boeing 727232 · Elevator, Plate/Skin
  > AT HMV, THE T/E OF RT ELEV WAS FOUND TO BE SEPARATED IN THREE DIFFERENT AREAS. THIS WAS REPAIRED PER MM 55-20-0 PG 801.
- [SDR DL72S971237](https://openairdocs.org/sdr/DL72S971237.md): Skin · cracked · Jun 16, 1997 · N495DA · Boeing 727232 · Leading Edge Devices
  > AT HMV, A CRACK WAS FOUND AT NR 3 SLAT AT RIB 4. THIS WAS REPAIRED PER MM 57-54-0 PG 801.
- [SDR DL72S971223](https://openairdocs.org/sdr/DL72S971223.md): Spar Web · cracked · May 30, 1997 · N495DA · Boeing 727232 · Trailing Edge Flaps
  > THE CENTER SPAR WEB WAS FOUND CRACKED IN TWO PLACES. THE FIRST LOCATION IS APPROX.75 INCH LONG LOCATED APPROX 25 INCHES FROM I/B END AT THE FOREFLAP CUTOUT NEAR THE UPPER I/B CORNER. THE OTHER CRACK WAS 51 INCHES FROM THE I/B END AT THE I/B CARRIAGE SUPPORT
- [SDR DL72S961742](https://openairdocs.org/sdr/DL72S961742.md): Batteries · discharged · Jul 20, 1996 · N495DA · Boeing 727232 · Emergency Lighting
  > ON PREFLIGHT, FOUND 1 EMERGENCY FLASHLIGHT AT 1L DOOR LED NOT FLASHING. REPLACED BATTERY AND BULB, NOW OPN NORM.
- [SDR DL72S961166](https://openairdocs.org/sdr/DL72S961166.md): Frame · corroded · May 16, 1996 · N495DA · Boeing 727232 · Cargo/Baggage Doors
  > LOWER FWD FRAME SECTION CORRODED BEYOND ALLOWABLE LIMITS. REPLACED FRAME SECTION PER CMM 65-56927-1.
- [SDR DL72S961165](https://openairdocs.org/sdr/DL72S961165.md): Angle · corroded · May 16, 1996 · N495DA · Boeing 727232 · Cargo/Baggage Doors
  > LOWER AFT T-ANGLE CORRODED BEYOND NEGLIGABLE DAMAGE LIMITS. REPLACED ANGLE PER CMM 65-56927-1.
- [SDR DL72S960431](https://openairdocs.org/sdr/DL72S960431.md): P/D Valve · leaking · Feb 24, 1996 · N495DA · Boeing 727232 · Fuel Controlling System
  > DESCENDING INTO ROC, NR 2 ENG FAILED/FLAME-OUT. ATTEMPTED RESTART NOT SUCCESSFUL. PRIOR TO DESCENT NR 2 FUEL FLOW 1,000 LBS HIGHER THAN OTHERS AND IT USED 1,000 LBS MORE DURING FLT. FOUND FUEL LEAK AT P AND D VLV. REPLACED PACKING, RAN ENGINE AND LEAK CHEC
- [SDR DL72S960290](https://openairdocs.org/sdr/DL72S960290.md): Skin · cracked · Feb 7, 1996 · N495DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > A.375 INCH CRACK AT F/O EYEBROW WINDOW LOWER FWD CORNER CUTOUT. FOUND DURING F-2 LTR CHECK TPAMM. REPAIRED PER SRM 53-30-3.
- [SDR DL72S960202](https://openairdocs.org/sdr/DL72S960202.md): Deck · cracked · Jan 25, 1996 · N495DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > DURING MIDVISIT, TWO 1 INCH CRACKS WERE FOUND IN THE LT MAIN LANDING GEAR WHEEL WELL PRESSURE DECK BETWEEN STATIONS 940 AND 950, BETWEEN LBL 50 AND 60. MODIFICATION INSTALLED IN ACCORDANCE WITH BOEING SERVICE BULLETIN 727-53-0149, REVISION 4.
- [SDR DL72S960118](https://openairdocs.org/sdr/DL72S960118.md): Hinges · corroded · Jan 6, 1996 · N495DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FROM MV2 ATL ITEM, CORROSION BEHIND HINGES ON ACCESS DOOR 3448R, LOC RT A/C COMP. REMOVED ACCESS DOOR 3448R, DAMAGE SECTION OFF ANGLE AND INSTALLED REPAIR PER MM 53-30-1 PG 807.
- [SDR DL72S960172](https://openairdocs.org/sdr/DL72S960172.md): Angle · cracked · Jan 5, 1996 · N495DA · Boeing 727232 · Leading Edge Devices
  > CRACK FOUND IN LWR AFT ATTACH ANGLE. REPAIRED PER M/M 57-54-00 FOR NR 4 L/E SLAT.
- [SDR DL72S960171](https://openairdocs.org/sdr/DL72S960171.md): Skin · cracked · Jan 5, 1996 · N495DA · Boeing 727232 · Leading Edge Devices
  > DURING INSP, THE FOLLOWING DAMAGE WAS FOUND REQUIRING MRR'S N/R 0058 CRACKS FOUND IN NR 9 AND NR 18 RIB. REPAIRED PER M/M 57-54-0 FIG 805. N/R 0059 CRACKS FOUND IN REPAIR DOUBLERS ON NR 11 AND 12 RIBS. REPAIRED PER M/M 57-54-00. N/R 0062 CRACK FOUND IN UPP
- [SDR DL72S960068](https://openairdocs.org/sdr/DL72S960068.md): Frame · cracked · Jan 5, 1996 · N495DA · Boeing 727232 · Fuselage Main, Frame
  > AT MID VISIT 2, FOUND FRAME CRACKED AT STA 1110 ABOVE STR 27L. REMOVED LT FIXED FLOOR PNL FROM 1070 TO 1130 FOR ACCESS. CUT OUT DAMAGE PER SRM 53-10-4 FIG 27 AND INSTALLED REPAIR PER SRM 53-10-4 FIG 27.
- [SDR DL72S960044](https://openairdocs.org/sdr/DL72S960044.md): Mount Bolts · loose · Jan 4, 1996 · N495DA · Boeing 727232 · Drag Control System
  > NR 2 SPOILER POWER PACK BOTTOM MOUNT BOLTS ARE LOOSE. REMOVED SPOILER ACTUATOR ATTACH FITTING. REMOVED AND REPLACED ANGLE PER MM 57-42-0 PG 804. INSTALLED POWER PACK, ACTUATOR AND MOUNT FITTING.
- [SDR DL72S954811](https://openairdocs.org/sdr/DL72S954811.md): Power Supply · inoperative · Dec 31, 1995 · N495DA · Boeing 727232 · Emergency Lighting
  > RT AFT OVER DOOR EMERGENCY LIGHT OUT. REPLACED M1093 RACK AND OPERATIONAL CHECKS GOOD.
- [SDR DL72S953494](https://openairdocs.org/sdr/DL72S953494.md): Ribs · cracked · Aug 24, 1995 · N495DA · Boeing 727232 · Leading Edge Devices
  > DURING SHOP INSPECTION, NR 7 L/E SLAT WAS FOUND WITH NR 2 L/E RIB CRACKED IN LOWER AFT CORNER. REPAIRED PER MM 57-54-0 FIG 814.

Next page: https://openairdocs.org/deregistered/N495DA-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 = 'N495DA' AND deregistration_id = 'N495DA-2001-02-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N495DA-2001-02-16/reports

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