# Service difficulty reports: N17410, cancelled Jul 22, 2004

A list on [N17410, cancelled Jul 22, 2004](https://openairdocs.org/deregistered/N17410-2004-07-22.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 · 60 reports

- [SDR EISA20010151](https://openairdocs.org/sdr/EISA20010151.md): Skin · torn · Dec 27, 2001 · N17410 · Boeing 727243 · Fuselage Main, Structure
  > ACCOMPLISHED SHEET METAL REPAIR AREA FORWARD OF RT OUT FLOW VALVE, STA 1166, STR. 24R.CORRECTIVE ACTION:CUT OUT DAMAGED AREA. FABRICATED DOUBLER.071 2024-T3 8" X 12" IAW B727 SRM 53-30-3, FIG. 3. TREATED & PRIMED AND INSTALLED DOUBLER IAW B727 SRM 51-10-2 &
- [SDR EISA20010119](https://openairdocs.org/sdr/EISA20010119.md): Structure · cracked · Aug 29, 2001 · N17410 · Boeing 727243 · Horizontal Stabilizer Structure
  > RT HORIZONTAL STAB O/B T/E CORNER IS CRACKED, TOP SIDE. FOUND DURING B-CHECK. ROUTED OUT CRACK IAW B727 SRM 55-10-1. NDT VERIFIED CRACK BEING REMOVED. FABRICATED DOUBLER AND FILLER PER EO NR 01-236. INSTALLED REPAIR PER EO 01-236 & B727 SRM 57-30-2 WITH APPR
- [SDR EISA20000196](https://openairdocs.org/sdr/EISA20000196.md): Plate · misaligned · Oct 28, 2000 · N17410 · Boeing 727243 · Rudder Control System
  > PACK FAN REMAINED ON AFTER FLAPS UP. RUDDER LOAD LIMITER LIGHT REMAINED ON FOR 4 MINUTES AFTER FLAPS UP. REMOVED AND REPLACED RIVETS ON STRIKER ON INBOARD FLAP CONTROL VALVE FOLLOW UP PULLEY. OPS CHECKED INBOARD FLAP FOLLOW UP CABLES, RUDDER LOAD LIMITER IN
- [SDR EISA2000001](https://openairdocs.org/sdr/EISA2000001.md): Receiver · shorted · Dec 29, 1999 · N17410 · Boeing 727243 · Attitude and Direction Data System
  > NR 1 NAV RECEIVER INOPERATIVE. INSTALLED SERVICEABLE NAV RECEIVER. (M)
- [SDR CALA9800863](https://openairdocs.org/sdr/CALA9800863.md): Fuel Pump · failed · May 14, 1998 · N17410 · Boeing 727243 · Engine Fuel Pump
  > NUMBER 2 ENGINE FAILED AT ROTATION. FOUND FUEL PUMP SHAFT SHEARED. REPLACED NUMBER 2 ENGINE FUEL PUMP AND FUEL CONTROL PER MM 71-00-67.
- [SDR CALA9800856](https://openairdocs.org/sdr/CALA9800856.md): Battery · discharged · May 14, 1998 · N17410 · Boeing 727243 · Emergency Lighting
  > EMERGENCY EXIT LIGHT OVER COCKPIT DOOR INOP. REPLACED BATTERY PACK.
- [SDR CALA9800469](https://openairdocs.org/sdr/CALA9800469.md): Stiffener · cracked · Mar 17, 1998 · N17410 · Boeing 727243 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.1562 INCH CRACK THROUGH FASTENER HOLE AT BOTTOM OF STIFFENER AT INBOARD SIDE OF LT WING LEADING EDGE RIB, WBL 92.0, ACCESS CUTOUT 6303. A REPAIR WAS INSTALLED IAW SRM 51-14-1.
- [SDR CALA9800468](https://openairdocs.org/sdr/CALA9800468.md): Floor Track · corroded · Mar 16, 1998 · N17410 · Boeing 727243 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND FLOOR TRACK CORRODED AT STA 380 TO 420, RBL 25. THE TRACK WAS REMOVED AND A NEW TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-05-01 AND 51-10-01.
- [SDR CALA9800467](https://openairdocs.org/sdr/CALA9800467.md): Skin · worn · Mar 16, 1998 · N17410 · Boeing 727243 · Spoilers
  > INSPECTION FOUND A GROOVE WORN ON BOTTOM OF LT WING NR 7 SPOILER. THE NR 7 SPOILER WAS REMOVED AND REPLACED.
- [SDR CALA9800466](https://openairdocs.org/sdr/CALA9800466.md): Window · delaminated · Mar 16, 1998 · N17410 · Boeing 727243 · Flight Compartment Windows
  > INSPECTION FOUND A BURNED SPOT AND A DELAMINATION BUBBLE IN R-1 WINDOW UPPER EDGE. THE R-1 WINDOW WAS REMOVED AND REPLACED IAW MM 56-11-11.
- [SDR CALA9800465](https://openairdocs.org/sdr/CALA9800465.md): Beam · cracked · Mar 16, 1998 · N17410 · Boeing 727243 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN J-BEAM ABOVE AND INBOARD OF NR 7 SPOILER ACTUATOR. THE J-BEAM WAS REPAIRED IAW ECRA 5750-02193 AND EA 26865-5075.
- [SDR CALA9800464](https://openairdocs.org/sdr/CALA9800464.md): Foreflap · damaged · Mar 16, 1998 · N17410 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND LT INBOARD FOREFLAP CRUSHED (4 AREA) AT INBOARD END. THE FOREFLAP WAS REMOVED AND REPLACED.
- [SDR CALA9800463](https://openairdocs.org/sdr/CALA9800463.md): Skin · cracked · Mar 16, 1998 · N17410 · Boeing 727243 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 2 INCH CRACK IN R-1 DOOR CUTOUT AT FS 417. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5307-01141.
- [SDR CALA9800442](https://openairdocs.org/sdr/CALA9800442.md): Skin · dented · Mar 13, 1998 · N17410 · Boeing 727243 · Ailerons
  > INSPECTION FOUND LT OUTBOARD AILERON OUTBOARD UPPER TRAILING EDGE HAD A PREVIOUSLY FILLED SMALL DENT WITH FILLER BREAKING OUT. THE DENTED AREA WAS CUT OUT AND A HOT BONDED REPAIR WAS INSTALLED IAW SRM 51-40-6.
- [SDR CALA9800441](https://openairdocs.org/sdr/CALA9800441.md): Skin · cracked · Mar 13, 1998 · N17410 · Boeing 727243 · Wing, Plate/Skin
  > INSPECTION FOUND A.375 INCH CRACK IN LT WING FIXED LEADING EDGE CUTOUT ABOVE NR 3 SLAT OUTBOARD TRACK AREA. A SKIN FLUSH REPAIR WAS INSTALLED IAW SRM 57-30-4.
- [SDR CALA9800440](https://openairdocs.org/sdr/CALA9800440.md): Skin · dented · Mar 13, 1998 · N17410 · Boeing 727243 · Leading Edge Devices
  > INSPECTION FOUND A DENT 19.5 INCHES FROM OUTBOARD END IN LT WING NR 2 LEADING EDGE SLAT UPPER SKIN. A REPAIR WAS INSTALLED IAW SRM 57-50-3.
- [SDR CALA9800439](https://openairdocs.org/sdr/CALA9800439.md): Splice · cracked · Mar 13, 1998 · N17410 · Boeing 727243 · Wing Miscellaneous Structure
  > INSPECTION FOUND A 3 INCH CRACK AT SPLICE PLATE ON LOWER SURFACE OF LT WING UPPER LEADING EDGE SKIN DIRECTLY ABOVE NR 2 LEADING EDGE FLAP ACTUATOR, FSS 224. THE SPLICE PLATE WAS CUT OUT, A NEW PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-2.
- [SDR CALA9800438](https://openairdocs.org/sdr/CALA9800438.md): Bracket · cracked · Mar 13, 1998 · N17410 · Boeing 727243 · Wing Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN BRACKET AT AFT FACE OF LT GEAR BEAM WHERE HYDRAULIC LINES PASS THROUGH ACCESS DOOR 8405. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-0, 51-10-2, AND 51-30-2.
- [SDR CALA9800437](https://openairdocs.org/sdr/CALA9800437.md): Angle · cracked · Mar 13, 1998 · N17410 · Boeing 727243 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK THROUGH AFT FASTENER HOLE AT REPAIR ANGLE INSIDE LT WING LEADING EDGE RIB, WS 330, AFT OF NR 4 SLAT, INBOARD END. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-6.
- [SDR CALA9800436](https://openairdocs.org/sdr/CALA9800436.md): Bracket · cracked · Mar 13, 1998 · N17410 · Boeing 727243 · Leading Edge Devices
  > INSPECTION FOUND A 1 INCH CRACK IN LT WING NR 1 SLAT LOWER LEADING EDGE SKIN TO INBOARD TRACK ATTACH BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-1.
- [SDR CALA9800435](https://openairdocs.org/sdr/CALA9800435.md): Skin · disbonded · Mar 13, 1998 · N17410 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND RT TRAILING EDGE INBOARD FOREFLAP DISBONDED IN TWO AREAS. THE FOREFLAP WAS REMOVED AND REPLACED.
- [SDR CALA9800434](https://openairdocs.org/sdr/CALA9800434.md): Angle · cracked · Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.6 INCH CRACK AT BOTTOM OF LEFT CURVED SIDEWALL SUPPORT ANGLE MOUNTED TO FORWARD SIDE OF CIRCUMFERENTIAL STA 950D. A NEW SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-40-3.
- [SDR CALA9800433](https://openairdocs.org/sdr/CALA9800433.md): Skin · corroded · Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND CORROSION IN SKIN ATTACH LEG AT FORWARD SIDE OF CIRCUMFERENTIAL, BS 1148, STRINGER 28L AND 29L. THE CORROSION WAS CUT OUT IAW SRM 51-10-6. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-10-6.
- [SDR CALA9800432](https://openairdocs.org/sdr/CALA9800432.md): Angle · cracked · Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL UPPER SUPPORT ANGLE BETWEEN FLOORBEAM SUPPORT, STA 720 AND 720A. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.
- [SDR CALA9800431](https://openairdocs.org/sdr/CALA9800431.md): Skin · cracked · Mar 13, 1998 · N17410 · Boeing 727243 · Spoilers
  > INSPECTION FOUND A.0937 INCH CRACK AT LT WING UPPER SKIN CUTOUT FOR NR 2 SPOILER. THE FASTENERS WERE REMOVED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-4, 51-10-2, AND 57-30-2.
- [SDR CALA9800430](https://openairdocs.org/sdr/CALA9800430.md): Angle · cracked · Mar 13, 1998 · N17410 · Boeing 727243 · Spoilers
  > INSPECTION FOUND A.5 INCH CRACK IN FALSE SPAR LOWER ANGLE BELOW AND INBOARD OF NR 7 SPOILER ACTUATOR INBOARD COVE AREA. REPAIRED FALSE SPAR LOWER ANGLE IAW EA NR 26865-5182 AND REINSTALLED ADJACENT STRUCTURE IAW SRM 51-30-2.
- [SDR CALA9800429](https://openairdocs.org/sdr/CALA9800429.md): Hinge · cracked · Mar 13, 1998 · N17410 · Boeing 727243 · Elevator Structure
  > INSPECTION FOUND A.5 INCH CRACK IN RT ELEVATOR BALANCE PANEL NR 9214 FORWARD HINGE. THE HINGE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.
- [SDR CALA9800428](https://openairdocs.org/sdr/CALA9800428.md): Stringer · cracked · Mar 13, 1998 · N17410 · Boeing 727243 · Vertical Stabilizer
  > INSPECTION FOUND VERTICAL STABILIZER INTERNAL COMPARTMENT NR 9 RT NR 3 STRINGER CRACKED 1 BEHIND ATTACH BOLT. REMOVED FASTENERS IAW SRM 51-30-2. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-2, AND 51-40-5.
- [SDR CALA9800427](https://openairdocs.org/sdr/CALA9800427.md): Stringers · cracked · Mar 13, 1998 · N17410 · Boeing 727243 · Vertical Stabilizer
  > INSPECTION FOUND VERTICAL STABILIZER INTERNAL COMPARTMENT NR 6 RT NR 3 STRINGER AND NR 5 STRINGER CRACKED 1 BEHIND ATTACH BOLT. REMOVED FASTENERS IAW SRM 51-30-2. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-2, AND 51-40-5.
- [SDR CALA9800426](https://openairdocs.org/sdr/CALA9800426.md): Gusset · cracked · Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 CRACK IN GUSSET ON FORWARD SIDE OF RT FUSELAGE FRAME AT STA 825, RBL 70. THE GUSSET WAS REMOVED AND A NEW ONE WAS INSTALLED IAW EA SA012-5310-01870.
- [SDR CALA9800425](https://openairdocs.org/sdr/CALA9800425.md): Web · cracked · Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 7 CRACK JUST BELOW DRAIN CHUTE IN LT AFT LAV FLOOR WEB AT BS 1176, LBL 50. THE CRACKED SECTION OF WEB WAS REMOVED. A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-20-01.
- [SDR CALA9800424](https://openairdocs.org/sdr/CALA9800424.md): Skin · bulged · Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT FUSELAGE SKIN BULGED JUST AFT AND BELOW FORWARD LAV SERVICE PANEL. THE BULGED AREA WAS REMOVED. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-10-2.
- [SDR CALA9800423](https://openairdocs.org/sdr/CALA9800423.md): Floor Track · corroded · Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CABIN FLOOR TRACK CORRODED AT STA 1050 TO 1130, BL 25R. THE CORRODED SECTION OF FLOOR TRACK WAS REPLACED IAW SRM 53-10-5 AND 51-10-1.
- [SDR CALA9800422](https://openairdocs.org/sdr/CALA9800422.md): Floor Track · corroded · Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CABIN FLOOR TRACK CORRODED AT STA 1100, BL 45R. THE CORRODED SECTION OF FLOOR TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-5.
- [SDR CALA9800718](https://openairdocs.org/sdr/CALA9800718.md): Battery Pack · discharged · Mar 12, 1998 · N17410 · Boeing 727243 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN IVER COCKPIT DOOR FELL OUT AND WAS FOUND INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK AND LENSE ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.
- [SDR CALA9800421](https://openairdocs.org/sdr/CALA9800421.md): Intercostal · cracked · Mar 12, 1998 · N17410 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.25 CRACK IN SUPPORT INTERCOSTAL AT AFT BAGGAGE COMPARTMENT BETWEEN BS 1030 AND 1050 ABOVE STRINGER 25L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.
- [SDR CALA9800143](https://openairdocs.org/sdr/CALA9800143.md): Light · inoperative · Jan 31, 1998 · N17410 · Boeing 727243 · Emergency Lighting
  > INSPECTION FOUND EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. THE EXIT LIGHT WAS REMOVED AND REPLACED.
- [SDR CALA9700787](https://openairdocs.org/sdr/CALA9700787.md): Brake Housing · cracked · May 26, 1997 · N17410 · Boeing 727243 · Brake
  > ACFT RETURNED TO THE GATE AFTER DRAGGING THE NR 3 BRAKE DURING TAXI. THE NR 3 TIRE CAUGHT ON FIRE, FOAM WAS USED TO EXTINGUISH THE FIRE. THE NR 3 AND 4 MAIN TIRE/WHEEL ASSEMBLIES AND BRAKES WERE REMOVED AND REPLACED. THE NR 3 BRAKE DEBOOST VALVE WAS ALSO RE
- [SDR CALA9700516](https://openairdocs.org/sdr/CALA9700516.md): Skin · corroded · Mar 27, 1997 · N17410 · Boeing 727243 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND AFT CARGO COMPARTMENT INTERIOR SKIN CORRODED AT ANTENNA, STA 1030 TO 1050, STRINGER 29R TO 30. THE AREA WAS REPAIRED IAW SRM 51-40-3.
- [SDR CALA9700581](https://openairdocs.org/sdr/CALA9700581.md): Angle · cracked · Mar 26, 1997 · N17410 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN VENTRAL STAIRWELL TORQUE BOX ANGLE AT STAIR ACTUATOR FITTING, STA 1272, RBL 22. A REPAIR WAS INSTALLED IAW BOEING DRAWING 65C27136.
- [SDR CALA9700519](https://openairdocs.org/sdr/CALA9700519.md): Skin · disbonded · Mar 26, 1997 · N17410 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND LT INBOARD MIDFLAP UPPER SURFACE OF TRAILING EDGE WEDGE DISBONDED 24 INCHES FROM INBOARD END. THE DISBONDED AREA WAS CUT OUT, CORE AND DOUBLERS WERE FABRICATED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6.
- [SDR CALA9700515](https://openairdocs.org/sdr/CALA9700515.md): Skin · corroded · Mar 26, 1997 · N17410 · Boeing 727243 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT FUSELAGE SKIN CORRODED AT STA 1130. THE CORRODED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1.
- [SDR CALA9700512](https://openairdocs.org/sdr/CALA9700512.md): Spar Web · cracked · Mar 26, 1997 · N17410 · Boeing 727243 · Wing Spar
  > INSPECTION FOUND A.75 CRACK IN WEB AT FRONT SPAR JUST OUTBOARD OF LT FORWARD TERMINAL PIN FITTING. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-40-2.
- [SDR CALA9700511](https://openairdocs.org/sdr/CALA9700511.md): Skin · cracked · Mar 26, 1997 · N17410 · Boeing 727224 · Wing, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK AT AFT OUTBOARD END OF CUTOUT FOR NR 6 SLAT OUTBOARD HOOK OF RT WING FIXED LEADING EDGE. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 57-30-4.
- [SDR CALA9700580](https://openairdocs.org/sdr/CALA9700580.md): Skin · cracked · Mar 25, 1997 · N17410 · Boeing 727243 · Wing, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN RT WING FIXED LEADING EDGE SKIN AT NR 6 SLAT OUTBOARD TRACK CUTOUT, STA 216. THE CRACK WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5730-01489.
- [SDR CALA9700518](https://openairdocs.org/sdr/CALA9700518.md): Skin · delaminated · Mar 25, 1997 · N17410 · Boeing 727243 · Aileron Tabs
  > INSPECTION FOUND OUTBOARD END OF LT OUTBOARD AILERON TAB DELAMINATED. THE TAB WAS REMOVED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. THE TAB WAS REINSTALLED.
- [SDR CALA9700514](https://openairdocs.org/sdr/CALA9700514.md): Skin · disbonded · Mar 25, 1997 · N17410 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND LEFT OUTBOARD FOREFLAP DISBONDING AT INBOARD END. THE END CAP WAS REMOVED, THE DISBONDED AREA WAS CUT OUT, A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6 AND THE END CAP WAS REINSTALLED.
- [SDR CALA9700513](https://openairdocs.org/sdr/CALA9700513.md): Rib · cracked · Mar 25, 1997 · N17410 · Boeing 727243 · Wing, Rib/Bulkhead
  > INSPECTION FOUND A 1 INCH CRACK BETWEEN TWO AFT UPPER BOLTS OF LT WING LEADING EDGE RIB AT SLAT STA 0. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.
- [SDR CAL960427](https://openairdocs.org/sdr/CAL960427.md): Frame · cracked · Feb 27, 1996 · N17410 · Boeing 727243 · Fuselage Main, Frame
  > INSPECTION FOUND A 1.5 INCH CRACK IN AFT BAG PIT FLOOR LEVEL FRAME AT BS 1166, RBL 24. THE CRACKED AREA WAS CUT OUT. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2, AND 51-30-2. (M)
- [SDR CAL960431](https://openairdocs.org/sdr/CAL960431.md): Floorbeam · oversized hole · Feb 25, 1996 · N17410 · Boeing 727243 · Fuselage Main, Floor Beam
  > INSPECTION FOUND OVERSIZED HOLE ON MAIN CABIN INTERIOR FLOORBEAM AT BS 350, RBL 40. THE EFFECTED SECTION WAS REMOVED. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-1, 51-10-2, 51-30-8 AND MM 51-20-2. (M)

Next page: https://openairdocs.org/deregistered/N17410-2004-07-22/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 = 'N17410' AND deregistration_id = 'N17410-2004-07-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N17410-2004-07-22/reports

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