# Service difficulty reports: N17402, cancelled Apr 27, 2001

A list on [N17402, cancelled Apr 27, 2001](https://openairdocs.org/deregistered/N17402-2001-04-27.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 · 67 reports

- [SDR CALA9901738](https://openairdocs.org/sdr/CALA9901738.md): Battery Pack · discharged · Dec 29, 1999 · N17402 · Boeing 727243 · Emergency Lighting
  > INSPECTION FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE IN CABIN AND AT OVERWING EXITS, BOTH SIDES. MAINTENANCE REPLACED A BAD FUSE. THE BATTERY PACKS WERE REMOVED, RECHARGED, AND REINSTALLED. OPERATIONAL CHECKS WERE GOOD IAW MM 33-50-01, PAGE 201.
- [SDR CALA9900418](https://openairdocs.org/sdr/CALA9900418.md): Skin · corroded · Apr 15, 1999 · N17402 · Boeing 727243 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND AFT LAV SERVICE PANEL AFT LOWER SKIN CORRODED. THE PANEL WAS REMOVED AND THE CORRODED INNER SKIN WAS REMOVED. A NEW SKIN AND INTERNAL AND OUTER DOUBLER WERE INSTALLED AND THE PANEL WAS REINSTALLED IAW SRM 51-10-2, PAGE 1, 51-30-2, PAGE 1 AND
- [SDR CALA9900417](https://openairdocs.org/sdr/CALA9900417.md): Stringer · cracked · Apr 15, 1999 · N17402 · Boeing 727243 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 4 INCH CRACK IN STRINGER 23L BETWEEN STA 1183 AND 1161, JUST BELOW LAV SERVICE PANEL INSIDE AFT CARGO COMPARTMENT. THE CRACKED SECTION OF STRINGER WAS CUT OUT, A NEW STRINGER, DOUBLER AND FILLER COVER PLATE WERE INSTALLED IAW SRM 51-10-2 AN
- [SDR CALA9900407](https://openairdocs.org/sdr/CALA9900407.md): Skin · cracked · Apr 14, 1999 · N17402 · Boeing 727243 · Ailerons
  > INSPECTION FOUND A.5 AND.375 INCH CRACK IN LT O/B AILERON LOWER SKIN WITH A BEND AT I/B EDGE. THE AILERON WAS REMOVED AND REPLACED IAW MM 27-10-31.
- [SDR CALA9900401](https://openairdocs.org/sdr/CALA9900401.md): Wire · broken · Apr 13, 1999 · N17402 · Boeing 727243 · Light System Wiring
  > THE RT FORWARD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE. THE WIRE WAS REPAIRED IAW WPM 20-10-13, PAGE 1. OPERATION OF THE EXIT LIGHT CHECKED GOOD.
- [SDR CALA9900400](https://openairdocs.org/sdr/CALA9900400.md): Angle · cracked · Apr 13, 1999 · N17402 · Boeing 727243 · Wing Miscellaneous Structure
  > INSPECTION FOUND A 2.75 INCH CRACK IN LT WING REAR SPAR O/B SUPPORT ANGLE WHERE NR 2 SPOILER ACTUATOR AND FLAP DRIVE CASTING MOUNTS. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.
- [SDR CALA9900398](https://openairdocs.org/sdr/CALA9900398.md): Bracket · cracked · Apr 13, 1999 · N17402 · Boeing 727243 · Leading Edge Slat Actuator
  > INSPECTION FOUND A.125 INCH CRACK AT UPPER END OF OUTBOARD BRACKET AT RT WING LEADING EDGE WHERE NR 5 L/E FLAP ACTUATOR MOUNTS. THE FASTENERS AND SUPPORT BRACKET WERE REMOVED IAW SRM 51-20-2. A NEW SUPPORT BRACKET WAS INSTALLED IAW SRM 51-10-1, PARAGRAPH 4
- [SDR CALA9900397](https://openairdocs.org/sdr/CALA9900397.md): Skin · debonded · Apr 13, 1999 · N17402 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND LT WING I/B MIDFLAP I/B END OF TRAILING EDGE SKIN DEBONDED. THE DEBONDED AREA WAS CUT OUT, A SKIN AND DOUBLER HOT BOND REPAIR WAS PERFORMED IAW SRM 51-40-6.
- [SDR CALA9900396](https://openairdocs.org/sdr/CALA9900396.md): Control Tab · dented · Apr 13, 1999 · N17402 · Boeing 727243 · Elevator, Tab Structure
  > INSPECTION FOUND THE RT ELEVATOR CONTROL TAB UPPER O/B TRAILING EDGE SKIN DENTED. THE ELEVATOR TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.
- [SDR CALA9900387](https://openairdocs.org/sdr/CALA9900387.md): Skin · cracked · Apr 12, 1999 · N17402 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND A.5 INCH CRACK IN LT O/B FOREFLAP I/B END CASTING AT LEADING EDGE AND TRAILING EDGE. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-11.
- [SDR CALA9900386](https://openairdocs.org/sdr/CALA9900386.md): Skin · debonded · Apr 12, 1999 · N17402 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND LT I/B FOREFLAP UPPER SURFACE DEBONDED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-14.
- [SDR CALA9900385](https://openairdocs.org/sdr/CALA9900385.md): Skin · debonded · Apr 12, 1999 · N17402 · Boeing 727243 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING UPPER AND LOWER SKIN DEBONDED O/B AND AFT OF APU EXHAUST AREA. THE SKIN PANEL WAS REPAIRED IAW SRM 51-30-08 PAGE 1.
- [SDR CALA9900384](https://openairdocs.org/sdr/CALA9900384.md): Skin · cracked · Apr 12, 1999 · N17402 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND A.3125 INCH CRACK IN RT INBOARD AFT FLAP LOWER LEADING EDGE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-02.
- [SDR CALA9900372](https://openairdocs.org/sdr/CALA9900372.md): Wedge · debonded · Apr 7, 1999 · N17402 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING O/B MID FLAP T/E WEDGE DEBONDED. THE TRAILING WAS REMOVED AND REPLACED IAW SRM 51-30-2, PAGE 1.
- [SDR CALA9900371](https://openairdocs.org/sdr/CALA9900371.md): Tab · dented · Apr 7, 1999 · N17402 · Boeing 727243 · Elevator, Tab Structure
  > INSPECTION FOUND LEFT ELEVATOR CONTROL TAB LOWER O/B LEADING EDGE SKIN DENTED. THE LEFT ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.
- [SDR CALA9900370](https://openairdocs.org/sdr/CALA9900370.md): Bulkhead Angle · cracked · Apr 7, 1999 · N17402 · Boeing 727243 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A.75 INCH CRACK IN FWD BULK VERT ANGLE AT RT WHEEL WELL BS 870 KEEL BEAM. THE FWD BULK VERT ANGLE WAS REPLACED IAW SRM 51-10-1, PAGE 4 AND 51-30-5, PAGE 1.
- [SDR CALA9900369](https://openairdocs.org/sdr/CALA9900369.md): Pressure Deck · cracked · Apr 7, 1999 · N17402 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3.5 INCH CRACK IN NOSE WHEEL WELL PRESSURE DECK AT FS 270, LBL 14. THE CRACKED AREA WAS CUT OUT, A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-40-2.
- [SDR CALA9900368](https://openairdocs.org/sdr/CALA9900368.md): Chord · cracked · Apr 7, 1999 · N17402 · Boeing 727243 · Leading Edge Devices
  > INSPECTION FOUND A.375 INCH AND.125 INCH CRACK AT LT WING NR 2 SLAT LOWER CHORD BELOW TELESCOPING ANT-ICE TUBE. THREE ACCESS PANELS WERE REMOVED PER SRM 51-30-2 AND THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1, PAGE 6B. AN ANGLE REPAIR DOUBLER WAS INSTALLE
- [SDR CALA9900367](https://openairdocs.org/sdr/CALA9900367.md): Chord · cracked · Apr 7, 1999 · N17402 · Boeing 727243 · Leading Edge Devices
  > INSPECTION FOUND A.3125 INCH CRACK AT LT WING NR 1 SLAT LOWER CHORD AT CUTOUT BELOW TELESCOPING ANTI-ICE TUBE. THE CRACK WAS STOP DRILLED AND AN ANGLE REPAIR WAS INSTALLED IAW SRM 57-30-2.
- [SDR CALA9900366](https://openairdocs.org/sdr/CALA9900366.md): Chord · cracked · Apr 7, 1999 · N17402 · Boeing 727243 · Leading Edge Devices
  > INSPECTION FOUND A 3 INCH AND.375 INCH CRACK AT RT WING NR 7 SLAT LOWER CHORD. THE LOWER SLAT PANEL WAS REMOVED FOR ACCESS AND REMOVED ANGLE IAW SRM 51-30-2, PAGE 1. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-20 AND 51-30-2. REINSTALLED ACCESS PANEL IAW SRM 5
- [SDR CALA9900365](https://openairdocs.org/sdr/CALA9900365.md): Floorbeam Web · cracked · Apr 7, 1999 · N17402 · Boeing 727243 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A 3 INCH CRACK IN FLOORBEAM WEB AT FS 294, RBL 48. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-40-2 FIGURE 1, SHEET 6.
- [SDR CALA9900364](https://openairdocs.org/sdr/CALA9900364.md): Skin · debonded · Apr 7, 1999 · N17402 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND RT O/B FLAP AFT SEGMENT DEBONDED AT TRAILING EDGE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-11.
- [SDR CALA9900363](https://openairdocs.org/sdr/CALA9900363.md): Skin · dented · Apr 7, 1999 · N17402 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND LT O/B FLAP AFT SEGMENT UPPER SURFACE DENTED AND DEBONDED. THE FLAP WAS REPAIRED IAW SRM 51-40-6.
- [SDR CALA9900362](https://openairdocs.org/sdr/CALA9900362.md): Skin · debonded · Apr 7, 1999 · N17402 · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND LT INBOARD AFT FLAP LOWER SURFACE DEBONDED. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-2.
- [SDR CALA9801915](https://openairdocs.org/sdr/CALA9801915.md): Battery · discharged · Oct 1, 1998 · N17402 · Boeing 727243 · Emergency Lighting
  > INSPECTION FOUND RT AFT CARGO DOOR EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REPLACED AND LIGHT WAS RELAMPED.
- [SDR CALA9801234](https://openairdocs.org/sdr/CALA9801234.md): Gear Handle · lack of lube · Jul 11, 1998 · N17402 · Boeing 727243 · Landing Gear Selector
  > WHEN GEAR WAS EXTENDED ON APPROACH, CREW RECEIVED THREE GREEN AND THREE RED GEAR INDICATION LIGHTS. THE GEAR WAS CYCLED AND CREW GOT THREE GREEN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEAR HANDLE STICKING WHEN PULLED OUT. THE
- [SDR CALA9800202](https://openairdocs.org/sdr/CALA9800202.md): Door Frame · cracked · Feb 9, 1998 · N17402 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 5 INCH CRACK IN UPPER AFT SECTION OF R-1 DOOR FRAME AT BS 410. THE CRACKED SECTION OF DOOR FRAME WAS CUTOUT IAW BOEING DRAWING 69-69978. A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-11.
- [SDR CALA9800198](https://openairdocs.org/sdr/CALA9800198.md): Web · cracked · Feb 7, 1998 · N17402 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.125 CRACK IN RT MLG WHEEL WELL PRESSURE WEB AT BS 872.5, RBL 52.25. A PRESSURE WEB REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03671.
- [SDR CALA9800191](https://openairdocs.org/sdr/CALA9800191.md): Support · cracked · Feb 4, 1998 · N17402 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT WEB CRACKED.125 BEYOND STOP DRILL HOLE AT STA 303.9, LBL 45. THE FLOOR SUPPORT WEB WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, AND 51-30-1.
- [SDR CALA9800190](https://openairdocs.org/sdr/CALA9800190.md): Stringer · corroded · Feb 4, 1998 · N17402 · Boeing 727243 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 27R CORRODED IN AFT CARGO COMPARTMENT BETWEEN STA 720 AND 720A. THE CORRODED SECTION OF STRINGER AND SKIN WERE REMOVED. A STRINGER REPAIR, REPAIR SPLICES, AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-3, FIGURE 1, 53-30-3,
- [SDR CALA9800183](https://openairdocs.org/sdr/CALA9800183.md): Skin · dented · Feb 4, 1998 · N17402 · Boeing 727243 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 279, STRINGER 22L. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-1, FIGURE 1, 53-30-3, FIGURE 13, 51-10-2, 51-30-2, AND MM 51-20-11.
- [SDR CALA9800182](https://openairdocs.org/sdr/CALA9800182.md): Floorbeam · corroded · Feb 4, 1998 · N17402 · Boeing 727243 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT CLIP NUTS, STA 380 BETWEEN RBL 24 AND 45. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-8.
- [SDR CALA9800181](https://openairdocs.org/sdr/CALA9800181.md): Skin · corroded · Feb 4, 1998 · N17402 · Boeing 727243 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN TEAR STRAP CORRODED IN FORWARD CARGO COMPARTMENT AT BS 68, STRINGER 28R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-4, 51-30-8, 51-30-3, FIGURE 12, AND 51-10-2.
- [SDR CALA9800180](https://openairdocs.org/sdr/CALA9800180.md): Support · cracked · Feb 3, 1998 · N17402 · Boeing 727243 · Elevator Structure
  > INSPECTION FOUND A 1.25 INCH CRACK IN LT ELEVATOR SUPPORT AT TRAILING EDGE OF ELEVATOR OUTBOARD OF INBOARD TRIM TAB HINGE BEARING. A 1.25 INCH CRACK WAS FOUND IN RT ELEVATOR OUTBOARD SUPPORT FOR ELEVATOR TRAILING EDGE AT TRIM TAB MOUNT AREA. THE SUPPORTS WER
- [SDR CALA9800179](https://openairdocs.org/sdr/CALA9800179.md): Stringer · corroded · Feb 3, 1998 · N17402 · Boeing 727243 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 28R IN FORWARD CARGO COMPARTMENT CORRODED BETWEEN STA 680 AND 700. THE STRINGER SPLICE WAS REMOVED AND A STRINGER SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-30-02, 51-10-2, AND MM 51-20-11.
- [SDR CALA9800178](https://openairdocs.org/sdr/CALA9800178.md): Skin · cracked · Feb 3, 1998 · N17402 · Boeing 727243 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 5.25 INCH CRACK IN FUSELAGE SKIN AT STA 510 BETWEEN STRINGER 25 AND 26R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. THE DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-8 AND 51-30-3.
- [SDR CALA9800177](https://openairdocs.org/sdr/CALA9800177.md): Support · cracked · Feb 3, 1998 · N17402 · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.5 INCH CRACK ON UPPER FLANGE OF CABIN FLOOR SUPPORT THREE INCHES AFT OF FLOORBEAM AT STA 294.5, RBL 45. THE FLOOR SUPPORT WAS REMOVED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, FIGURE 1, 51-10-1, 51-40-3, FIGURE 3, AN
- [SDR CALA9700977](https://openairdocs.org/sdr/CALA9700977.md): Sequence Valve · leaking · Jun 29, 1997 · N17402 · Boeing 727243 · Landing Gear Retraction/Extension System
  > THE SYSTEM-A HYDRAULIC FAILURE LIGHTS ILLUMINATED ON CO-PILOT PANEL AFTER GEAR RETRACTION. ALSO, THE A-SYSTEM HYDRAULIC LOW PRESSURE LIGHTS ON SECOND OFFICER'S PANEL ILLUMINATED WITH THE ELEVATOR LOW PRESSURE LIGHT ILLUMINATING MOMENTARILY. THE GEAR WAS LOWE
- [SDR CALA9700796](https://openairdocs.org/sdr/CALA9700796.md): Hyd Module · cracked · Jun 1, 1997 · N17402 · Boeing 727243 · Hydraulic System, Main
  > THE AIRCRAFT WAS DIVERTED TO PHX, AFTER LOSING THE A-HYDRAULIC SYSTEM FLUID QUANTITY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM HYDRAULIC MODULE FITTING CRACKED. THE A-SYSTEM HYDRAULIC MODULE WAS REMOVED AND REPLACED. IN ADDITION
- [SDR CAL960373](https://openairdocs.org/sdr/CAL960373.md): Flex Hose · leaking · Mar 20, 1996 · N17402 · Boeing 727243 · Hydraulic System, Main
  > FLT NR 477 - TPA - A/C LOST THE 'B' SYS HYD FLUID IN FLT. THE LOSS WAS ACCOMPANIED BY FLICKERING 'B' SYS HYD LOW PRESS LIGHTS. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MX FOUND THE HYD PRESS FLEX HOSE FROM THE NR 2 E
- [SDR CAL960251](https://openairdocs.org/sdr/CAL960251.md): Angle · corroded · Feb 2, 1996 · N17402 · Boeing 727243 · Fuselage Miscellaneous Structure
  > STATION 31J - INSPECTION FOUND CORROSION AT BOTTOM OF FLOOR BEAM AT GILL SUPPORT FRAME ANGLE IN AFT CARGO PIT AT BS 1168, RBL 55. THE CORRODED AREA OF ANGLE WAS CUT OUT. A NEW ANGLE AND DOUBLER ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-20-2, AN
- [SDR CAL960266](https://openairdocs.org/sdr/CAL960266.md): Floor Pan · corroded · Jan 27, 1996 · N17402 · Boeing 727243 · Fuselage Floor Panel
  > INSPECTION FOUND CENTER OF LT AFT LAV FLOOR PAN CORRODED AT BS 1140 TO BS 1176. THE CORROSION WAS REMOVED FROM THE FLOOR PAN. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 51-20-4. (X)
- [SDR CAL960272](https://openairdocs.org/sdr/CAL960272.md): Channel Support · corroded · Jan 26, 1996 · N17402 · Boeing 727243 · Fuselage Miscellaneous Structure
  > STATION 31J - INSPECTION FOUND CORROSION ON CHANNEL SUPPORT AT BS 803, BL 0. THE CORROSION WAS REMOVED AND A 'T' ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4. (M)
- [SDR CAL960271](https://openairdocs.org/sdr/CAL960271.md): Panel Support · corroded · Jan 25, 1996 · N17402 · Boeing 727243 · Fuselage Miscellaneous Structure
  > STATION 31J - INSPECTION FOUND LOWER FUSELAGE PANEL SUPPORT CORRODED AT BS 880, LBL 9 AND RBL 9. THE CORRODED AREA WAS CUT OUT. REPAIR ANGLES AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3. (M)
- [SDR CAL960274](https://openairdocs.org/sdr/CAL960274.md): Flap Track · corroded · Jan 24, 1996 · N17402 · Boeing 727243 · Trailing Edge Flaps
  > STATION 31J - INSPECTION FOUND CORROSION AT RIGHT MLG BEAM INBOARD FLAP INBOARD TRACK ATTACH POINT. THE AREA WAS REPAIRED IAW ECRA 5750-02438. (M)
- [SDR CAL960273](https://openairdocs.org/sdr/CAL960273.md): Beam · corroded · Jan 24, 1996 · N17402 · Boeing 727243 · Wing Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON LT MLG BEAM LOWER FLANGE AT INBOARD FLAP INBOARD TRACK ATTACH POINT. A REPAIR WAS PERFORMED IAW ECRA 5750-02437 AND SRM 51-10-6 AD SRM 51-10-2. (X)
- [SDR CAL960269](https://openairdocs.org/sdr/CAL960269.md): Floor Beam · corroded · Jan 24, 1996 · N17402 · Boeing 727243 · Fuselage Main, Floor Beam
  > STATION 31J - INSPECTION FOUND ELONGATED HOLES AND PITTING CORROSION IN FLOOR BEAM AND SEAT TRACK AT BS 1010, RBL 55. THE AREA OF ELONGATED HOLES WAS CUT OUT. REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, FIGURE 1. (M)
- [SDR CAL960265](https://openairdocs.org/sdr/CAL960265.md): Floor Beam · corroded · Jan 21, 1996 · N17402 · Boeing 727243 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 1110, RBL 26 TO RBL 44. THE CORRODED SECTION OF FLOOR BEAM UPPER CHORD WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, SRM 51-10-2, AND MM 51-20-151. (X)
- [SDR CAL960258](https://openairdocs.org/sdr/CAL960258.md): Support · corroded · Jan 21, 1996 · N17402 · Boeing 727243 · Fuselage Miscellaneous Structure
  > STATION 31J - INSPECTION FOUND FUSELAGE PANEL SUPPORT CORRODED BELOW ANCHOR NUT AT BS 813, RBL 9 BETWEEN HEAT EXCHANGERS. THE CORRODED AREA WAS CUT OUT, TWO 'L' ANGLES AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-0
- [SDR CAL960257](https://openairdocs.org/sdr/CAL960257.md): Support · corroded · Jan 21, 1996 · N17402 · Boeing 727243 · Fuselage Miscellaneous Structure
  > STATION 31J - INSPECTION FOUND FUSELAGE PANEL SUPPORT CORRODED BELOW ANCHOR NUT AT BS 813, LBL 9 BETWEEN LEFT AND RIGHT HEAT EXCHANGER. THE CORROSION WAS REMOVED IAW SRM 51-10-2, AN 'L' ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20

Next page: https://openairdocs.org/deregistered/N17402-2001-04-27/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 = 'N17402' AND deregistration_id = 'N17402-2001-04-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N17402-2001-04-27/reports

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