# Service difficulty reports: N499DA, cancelled Aug 15, 2013

A list on [N499DA, cancelled Aug 15, 2013](https://openairdocs.org/deregistered/N499DA-2013-08-15.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 · 56 reports

- [SDR DL72S001856](https://openairdocs.org/sdr/DL72S001856.md): Bulb · failed · Sep 21, 2000 · N499DA · Boeing 727232 · Exterior Lighting
  > R-1 DOOR AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED R-1 AFT EXTERIOR LIGHT, OPS CKS GOOD.
- [SDR DL72S001068](https://openairdocs.org/sdr/DL72S001068.md): Coalescer Bag · dirty · May 31, 2000 · N499DA · Boeing 727232 · Humidity Control System
  > SMOKE SMELL IN COCKPIT AND CABIN. CHANGED COALESCER BAGS. CHECKED SYSTEM. SUSPECT FOREST FIRE.
- [SDR DL72S000326](https://openairdocs.org/sdr/DL72S000326.md): Mount · cracked · Feb 17, 2000 · N499DA · Boeing 727232 · Engine Mount Section
  > CRACKED HOLE WHILE ACCOMPLISHING REPETITIVE INSPECTIONS OF THE FWD ENGINE MOUNT BOLT HOLES ON THE NR 3 ENGINE PYLON PER AD 97-05-08, A CRACK INDICATION WAS FOUND IN ONE HOLE (REF HOLE F OF BAC S/B 727-54A0010). THE HOLE WAS OVERSIZED TO REMOVE THE CRACK AND
- [SDR DL72S992376](https://openairdocs.org/sdr/DL72S992376.md): Angle · corroded · Oct 27, 1999 · N499DA · Boeing 727232 · Engine Mount Section
  > NR 2 ENG AFT MOUNT LOWER CHORD WAS CORRODED. REPLACED CHORD.
- [SDR DL72S992375](https://openairdocs.org/sdr/DL72S992375.md): Angle · corroded · Oct 27, 1999 · N499DA · Boeing 727232 · Engine Mount Section
  > NR 2 ENG AFT MOUNT SUPPORT ANGLE LEFT HAND WAS CORRODED. REPLACED ANGLE.
- [SDR DL72S992462](https://openairdocs.org/sdr/DL72S992462.md): Wire · split · Oct 25, 1999 · N499DA · Boeing 727232 · Electrical Power System Wiring
  > ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL P/N 012210733 PER BOEING SER- VICE LETTER 727-SL
- [SDR DL72S990832](https://openairdocs.org/sdr/DL72S990832.md): Oil Filter · contaminated · Apr 13, 1999 · N499DA · Boeing 727232 · Turbine Engine Oil System
  > NR 3 OIL FILTER BYPASS LIGHT CAME ON AT 17K FT. OIL PRESS TEMP AND QTY ARE GOOD POM PROCEDURES COMPLIED WITH. LIGHT REMAINED ON AND NR 3 ENGINE WAS SHUT DOWN IAW POM PROCEDURES. REMOVED FILTER, FOUND CARBON BUILDUP. INSTALLED NEW FILTER AND RAN ENG PER MM.
- [SDR DL72S990772](https://openairdocs.org/sdr/DL72S990772.md): Controller · failed · Apr 8, 1999 · N499DA · Boeing 727232 · Cabin Pressure Controller
  > DURING CLIMB-OUT, CABIN ALT BEGAN TO CLIMB AT 1000 FT, BOTH PACKS APPEARED TO OP. NORMAL CABIN CLIMBED TO AN ALT OF 12,000 AND DESCENT BEGAN. POM PREC FOLLOWED STBY AND DC HAD NEG EFFECT TO CLOSE OUTFLOW FURTHER CARGO V. CLOSED LIGHT ILLUMINATED ENTIRE TIME
- [SDR DL72S990568](https://openairdocs.org/sdr/DL72S990568.md): Skin · cracked · Mar 11, 1999 · N499DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT ALONG ITS ENTIRE LENGTH A
- [SDR DL72S990541](https://openairdocs.org/sdr/DL72S990541.md): Skin · cracked · Mar 11, 1999 · N499DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 36 CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE LENGTH OF THE PANEL AND REPAIRED W
- [SDR DL72S990540](https://openairdocs.org/sdr/DL72S990540.md): Skin · cracked · Mar 11, 1999 · N499DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC CONFIRMED 69 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUTOUT ALONG THE ENTIRE LENGTH OF THE PA
- [SDR DL72S990411](https://openairdocs.org/sdr/DL72S990411.md): Oil Filter · dirty · Feb 26, 1999 · N499DA · Boeing 727232 · Turbine Engine Oil System
  > NR 3 ENGINE OIL FILTER INDICATED BYPASS IN CRUISE FL280. PRECAUTIONARY, SHUTDOWN PROCEDURE ACCOMPLISHED. REPLACED OIL FILTER, LOP SWITCH, FILTER BYPASS SWITCH, DRAINED OIL RES, PERFORMED OIL BREATHER PRESS CK TEST 'Z' PER PFHB AND OPN OK. REPLACED OIL FILTE
- [SDR DL72S982454](https://openairdocs.org/sdr/DL72S982454.md): Filter · clogged · Nov 29, 1998 · N499DA · Boeing 727232 · Turbine Engine Oil System
  > NR 3 ENGINE OIL FILTER BYPASS ILLUMINATED IN FLIGHT. THE LIGHT EXTINGUISHED AT 45 TO 50 PERCENT N1 ALL ON SHORT FINAL. LIGHT RE-ILLUMINATED AT IDLE. PER T/S CHART REPLACED FILTER, PERFORMED BREATHER PRESS CK, CKS GOOD. REPLACED FILTER, OK FOR SERVICE.
- [SDR DL72S981959](https://openairdocs.org/sdr/DL72S981959.md): Skin · cracked · Sep 18, 1998 · N499DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE R1 DOOR SURROUND SKIN ASSY WAS FOUND WITH A 2.25 INCH TYPICAL CRACK IN THE BEAR STRAP AT THE UPPER HINGE CUTOUT. THE CRACK WAS REPAIRED PER BAC S/B 727-53-0136, REV 3. THE REPAIR WAS DOCUMENTED PER ER/A 365667-14. NOTE: THE BEAR STRAP HAD THE S/B 53-01
- [SDR DL72S981049](https://openairdocs.org/sdr/DL72S981049.md): Bulb · failed · May 17, 1998 · N499DA · Boeing 727232 · Exterior Lighting
  > EMERGENCY LIGHT OUT AT RIGHT WING ROOT FAIRING. RELAMPED.
- [SDR DL72S980368](https://openairdocs.org/sdr/DL72S980368.md): Battery Pack · discharged · Feb 11, 1998 · N499DA · Boeing 727232 · Emergency Lighting
  > ON LAYOVER CK, FOUND LT OVERWING EMERGENCY EXIT SIGN NOT ILLUMINATING. REPLACED BATTERY PACK.
- [SDR DL72S980317](https://openairdocs.org/sdr/DL72S980317.md): Controller · malfunctioned · Feb 5, 1998 · N499DA · Boeing 727232 · Cabin Cooling System
  > AT FL 2500 WITH ONE PACK RUNNING, CABIN STARTED TO CLIMB, DIVERTED INTO DFW. MAINTENANCE IN PROGRESS. RT PACK ON PREVIOUS MCO. RT PACK REPLACED ACM. CKS GOOD. LT PACK REPLACED 35 DEGREE SENSOR AND 35 DEGREE CONTROLLER. PRESSURIZED A/C USING BOTH PAC
- [SDR DL72S972713](https://openairdocs.org/sdr/DL72S972713.md): Web · cracked · Dec 23, 1997 · N499DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A 1 INCH CRACK IN LIGHTENING HOLE TORQUE BOX WEB RT SIDE STA 1223. REPAIRED PER MM 53-11-0 PG 828.
- [SDR DL72S972250](https://openairdocs.org/sdr/DL72S972250.md): Light · inoperative · Nov 4, 1997 · N499DA · Boeing 727232 · Emergency Lighting
  > DURING SVC CHK AD9 FOUND L1 AND L2 DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSYS. OPS NML.
- [SDR DL72S971715](https://openairdocs.org/sdr/DL72S971715.md): Relay · inoperative · Sep 1, 1997 · N499DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY EXIT LTS AND EMERG PATH LTS CAME ON DURING CLIMB-OUT. COCKPIT SW IN ARMED POS AND CABIN SW IN NORM. REPLACED R70 CHARGING RELAY.
- [SDR DL72S961018](https://openairdocs.org/sdr/DL72S961018.md): Tank Plate · leaking · Apr 29, 1996 · N499DA · Boeing 727232 · Fuel Storage
  > FUEL LEAK LEFT WING, IN-FLIGHT. REPORTED BY PASSENGER. DIVERTED ATL. FOUND FIFTH TANK PLATE FROM LT WING TIP LEAKING FUEL. SECURED TANK PLATE. NO LEAKS NOTED.
- [SDR DL72S960634](https://openairdocs.org/sdr/DL72S960634.md): Angle · cracked · Mar 21, 1996 · N499DA · Boeing 727232 · Leading Edge Devices
  > DURING LETTER CHECK, NR 5 L/E SLAT AFT ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0 PAR 12.
- [SDR DL72S960631](https://openairdocs.org/sdr/DL72S960631.md): Angle · cracked · Mar 21, 1996 · N499DA · Boeing 727232 · Leading Edge Devices
  > FOUND DURING A-1 LETTER CHECK, NR 7 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0 PAR 12.
- [SDR DL72S960630](https://openairdocs.org/sdr/DL72S960630.md): Angle · cracked · Mar 21, 1996 · N499DA · Boeing 727232 · Leading Edge Devices
  > FOUND DURING A-1 LETTER CHECK, NR 5 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0 PAR 12.
- [SDR DL72S960629](https://openairdocs.org/sdr/DL72S960629.md): Angle · cracked · Mar 21, 1996 · N499DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND DURING A-1 LETTER CHECK,.75 INCH CRACK NR 4 KRUEGER FLAP ACTUATOR MOUNT BOX AT UPPER I/B FWD CORNER. REPAIRED PER M/M 57-20-21.
- [SDR DL72S960178](https://openairdocs.org/sdr/DL72S960178.md): Cable · broken · Jan 23, 1996 · N499DA · Boeing 727232 · Escape Slide
  > LEFT SERVICE DOOR EVACUATION SLIDE FAILED TO DEPLOY AND PULL HANDLE CAME OFF WHEN PULLED. CABLE ON PULL HANDLE BROKE. REPLACED DOOR SLIDE PER M/M 25-60-15.
- [SDR DL72S953903](https://openairdocs.org/sdr/DL72S953903.md): Spar · cracked · Sep 25, 1995 · N499DA · Boeing 727232 · Trailing Edge Flaps
  > AFT SPAR CHORD WAS FOUND CRACKED 33, 54 AND 61 FROM IB END OF NR 3 MIDFLAP. THE DAMAGED SECTION WAS REPLACED AND SPLICED IN PER MM 57-50-00.
- [SDR DL72S953636](https://openairdocs.org/sdr/DL72S953636.md): Angle · cracked · Sep 7, 1995 · N499DA · Boeing 727232 · Leading Edge Devices
  > NR 6 SLAT,.25 INCH CRACK AT FASTENER HOLE IN ATTACH ANGLE AFT OF RIB, 6 INCHES O/B OF TAI DUCT. REPAIRED PER MM 57-54-0 FIG 805A.
- [SDR DL72S953669](https://openairdocs.org/sdr/DL72S953669.md): Rib · cracked · Sep 6, 1995 · N499DA · Boeing 727232 · Leading Edge Devices
  > NR 1 SLAT I/B TRACK I/B RIB CRACKED. DRILLED DOUBLER AND INSTALLED PER M/M 57-54-0 PG 806 AND 807.
- [SDR DL72S953633](https://openairdocs.org/sdr/DL72S953633.md): Rib · cracked · Sep 6, 1995 · N499DA · Boeing 727232 · Leading Edge Devices
  > DURING HMV, FOUND NR 1 SLAT WITH CRACKED RIB AT TRACK ATTACH AREA. REPAIRED PER MM 57-40-0 PG 806 AND 807.
- [SDR DL72S953602](https://openairdocs.org/sdr/DL72S953602.md): Skin · cracked · Sep 3, 1995 · N499DA · Boeing 727232 · Leading Edge Devices
  > DURING HMV, NR 2 SLAT LOWER SKIN ATTACH ANGLE CRACKED UNDER I/B STOP PAD. REPAIRED PER MM 57-54-0 PG 816.
- [SDR DL72S953586](https://openairdocs.org/sdr/DL72S953586.md): Stringer · cracked · Aug 29, 1995 · N499DA · Boeing 727232 · Wing, Longeron/Stringer
  > WING UPPER STRINGER TO RIB WS 686.5 STRINGER NR 5 IS CRACKED. STOP DRILLED CRACK PER M/M 57-13-0 PG 802. FABRICATED REPAIR PARTS AND INSTALLED PER M/M 57-13-00 PG 802.
- [SDR DL72S953666](https://openairdocs.org/sdr/DL72S953666.md): Attach Lug · broken · Aug 22, 1995 · N499DA · Boeing 727232 · Passenger/Crew Doors
  > AT HMV, FWD ENTRY DOOR UPPER GATE STOP ROD ATTACH LUG FOUND BROKEN. REPAIRED PER 52-10-2 FIG 10.
- [SDR DL72S953578](https://openairdocs.org/sdr/DL72S953578.md): Act Attach · cracked · Aug 22, 1995 · N499DA · Boeing 727232 · Wing Miscellaneous Structure
  > NR 6 L/E FLAP ACTUATOR ATTACH STRUCTURE CRACKED AT LOWER I/B CORNER. REPAIRED PER M/M 57-20-21 PG 811.
- [SDR DL72S953855](https://openairdocs.org/sdr/DL72S953855.md): Spar · cracked · Aug 21, 1995 · N499DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, NR 2 MIDFLAP HAS A CRACKED AFT SPAR CHORD 22 FT AND 53 FROM I/B END OF FLAP AND A CRACK AT I/B ACTUATOR CUTOUT. SPLICED IN NEW SECTIONS OF AFT SPAR CHORD AND INSTALLED DOUBLERS, PER MM 57-52-00 PG 807.
- [SDR DL72S953639](https://openairdocs.org/sdr/DL72S953639.md): Skin · cracked · Aug 21, 1995 · N499DA · Boeing 727232 · Leading Edge Devices
  > NR 5 SLAT SKIN WORN ON UPPER SURFACE AT FENCE ATTACHMENT. BURNISHED WORN AREA AND DYE PENETRANT INSP SHOWS CRACKS AT 3 FENCE ATTACH HOLES. ROUTED DAMAGE AT ATTACH HOLES, FABRICATED AND DRILLED DOUBLER PER M/M 57-54-0.
- [SDR DL72S953577](https://openairdocs.org/sdr/DL72S953577.md): Act Attach · cracked · Aug 21, 1995 · N499DA · Boeing 727232 · Wing Miscellaneous Structure
  > NR 5 L/E FLAP ACTUATOR ATTACH STRUCTURE CRACKED AT LWR O/B CORNER. REPAIRED PER M/M 57-20-21 PG 811. CRACK WAS FOUND AT HMV.
- [SDR DL72S953668](https://openairdocs.org/sdr/DL72S953668.md): Rib · cracked · Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge Devices
  > DURING HMV, FOUND NR 7 SLAT RIB CRACKED AT FASTENER HOLE, I/B OF I/B STOP PAD. FABRICATED REPAIR PER M/M 57-54-0 PG 807 AND INSTALLED REPAIR PER MM 57-54-0 PG 807.
- [SDR DL72S953649](https://openairdocs.org/sdr/DL72S953649.md): Web · cracked · Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge Devices
  > DURING HMV, FOUND WEB CRACKED NR 5 SLAT. REPAIRED WEB PER MM 57-54-0 FIG 805.
- [SDR DL72S953637](https://openairdocs.org/sdr/DL72S953637.md): Skin · worn · Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge Devices
  > NR 6 SLAT SKIN WORN AND CHAFED INBD OF INBD TRACK FAIRING AND BELOW SLAT ACTUATOR ON LWR TRAILING EDGE. TRIMMED AWAY DAMAGED PORTION OF TAB AND FABRICATED DOUBLER AND FILLER PER MM 57-54-0 PG 820.
- [SDR DL72S953632](https://openairdocs.org/sdr/DL72S953632.md): Angle · cracked · Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge Devices
  > UPON HMV, FOUND.25 INCH CRACK AT FASTENER HOLE IN ATTACH ANGLE AFT OF RIB 6 OUTBD OF T.A.I. DUCT. REPAIRED PER M/M 51-54-0, FIG 805A.
- [SDR DL72S953610](https://openairdocs.org/sdr/DL72S953610.md): Rib · cracked · Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge Devices
  > DURING HMV, FOUND NR 4 SLAT RIB CRACKED.5 INCH, ON O/B SIDE OF O/B TRACK FITTING. REPAIRED RIB PER MM 57-45-0 FIG 814.
- [SDR DL72S953591](https://openairdocs.org/sdr/DL72S953591.md): Rib · cracked · Aug 20, 1995 · N499DA · Boeing 727232 · Leading Edge Devices
  > DURING HMV, NR 8 L/E SLAT WAS FOUND WITH CRACKED INTERNAL SUPPORT RIB. REPAIRED PER MM 57-54-0 PG 814.
- [SDR DL72S953587](https://openairdocs.org/sdr/DL72S953587.md): Stringer · cracked · Aug 20, 1995 · N499DA · Boeing 727232 · Wing, Longeron/Stringer
  > LEFT WING UPPER STRINGER TO RIB WS 629 STRINGER NR 3 CRACKED. FABRICATED AND INSTALLED PARTS PER M/M 57-13-00 FIG 804. CRACK WAS FOUND AT HMV.
- [SDR DL72S953497](https://openairdocs.org/sdr/DL72S953497.md): Seat Track · corroded · Aug 20, 1995 · N499DA · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AFT CABIN CORRODED RT SIDE OB TRACK STA 1090. REMOVED CORROSION PER SRM 51-10-6, OUT OF LIMITS PER SRM 53-10-1 FIG 1. REMOVED CORROSION BETWEEN STA 1090 TO 1110 WITHIN LIMITS PER SRM 53-10-1 FIG 1. REMOVED PIGTAIL STA 1110 TO 1130, BEGAN REPLACEM
- [SDR DL72S953496](https://openairdocs.org/sdr/DL72S953496.md): Seat Track · corroded · Aug 20, 1995 · N499DA · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN SEAT TRACK, RT SIDE STA 400 OB, AND 470 OB, REMOVED CORR PER SRM 51-10-6. STA 470 WITHIN LIMITS PER SRM 53-10-1 FIG 3, STA 400 OUT OF LIMITS PER SRM 53-10-1 FIG 3. ALSO, FS 400 SHOWS EVIDENCE OF PREVIOUS CORROSION REMOVAL. PREPARED NEW SEAT TRACK
- [SDR DL72S953640](https://openairdocs.org/sdr/DL72S953640.md): Blkhd Bolts · worn · Aug 19, 1995 · N499DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > DURING HMV, FOUND MOUNT BOLTS WORN FWD CARGO BULKHEAD AT FS 720D VERTICAL SUPPORT BEAMS ATTACH POINT AT STR 26L AND 26R. REPAIRED PER SRM 53-10-9 FIG 9.
- [SDR DL72S953638](https://openairdocs.org/sdr/DL72S953638.md): Skin · cracked · Aug 19, 1995 · N499DA · Boeing 727232 · Leading Edge Devices
  > DURING HMV, FOUND NR 5 SLAT RIVET MISSING IN LWR T/E SKIN O/B OF O/B TRACK. SKIN WORN AT FENCE ATTACHMENT AND WORN THIN AT BOLT HOLE ON LWR T/E SKIN. REF NR CARD 1148, BURNISHED WORN AREA. DIE PENETRANT INSP SHOWS CRACK AT 3 FENCE ATTACH HOLES. FABRICATED
- [SDR DL72S953658](https://openairdocs.org/sdr/DL72S953658.md): Fitting · loose · Aug 18, 1995 · N499DA · Boeing 727232 · Wing, Control Surface Attach Fittings
  > THE NR 2 SPOILER ACTUATOR SUPPORT FITTING LOWER TWO ATTACH BOLTS, AT REAR SPAR ARE VERY LOOSE IN MOUNT LUGS. REPAIRED PER MM 57-42-00 PG 804 STEP D.
- [SDR DL72S953550](https://openairdocs.org/sdr/DL72S953550.md): Actuator · loose · Aug 18, 1995 · N499DA · Boeing 727232 · Drag Control Actuator
  > ITEM: SPOILER ACTUATOR SUPPORT FITTING LOOSE INBD LOWER BOLT AT NR 13 SPOILER. REPAIRED FITTING PER MM 57-42-0 REV D.

Next page: https://openairdocs.org/deregistered/N499DA-2013-08-15/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 = 'N499DA' AND deregistration_id = 'N499DA-2013-08-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N499DA-2013-08-15/reports

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