# Service difficulty reports: N616AW, cancelled Oct 29, 2014

A list on [N616AW, cancelled Oct 29, 2014](https://openairdocs.org/deregistered/N616AW-2014-10-29.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 3 · 106 reports

- [SDR A6WA200460066](https://openairdocs.org/sdr/A6WA200460066.md): Acm · odor · Dec 30, 2004 · N616AW · Bag BAE146300A · Cabin Cooling System
  > NR 2 PACK WAS INADVERTENTLY SWITCHED ON FOR APPROX 10 MINUTES ENROUTE. PILOTS NOTICED ODOR IN COCKPIT, PACK SWITCHED OFF AND A PUFF OF WHITE SMOKE CAME OUT OF VENT IN COCKPIT THEN SMOKE ODOR DISSIPATED. MAINTENANCE REMOVED AND REPLACED RIGHT HAND AIR CYCLE M
- [SDR A6WA200460052](https://openairdocs.org/sdr/A6WA200460052.md): Oxygen Mask · misinstalled · Nov 11, 2004 · N616AW · Bac 146300A · Passenger Oxygen System
  > DURING INSPECTION, ALL PASSENGER O2 DROP DOWN MASKS WERE FOUND STOWED INCORRECTLY. MAINTENANCE RESTOWED ALL PASSENGER O2 DROP DOWN MASKS, CORRECTLY IAW AMM 35-20-45.
- [SDR A6WA200460032](https://openairdocs.org/sdr/A6WA200460032.md): Wire · shorted · Aug 27, 2004 · N616AW · Bac 146300A · Communications System
  > SHORTLY AFTER TAKEOFF, LOST ALL RADIO COMMUNICATION. RETURNED TO RDU, LANDED UNDER LANDING WEIGHT. MAINTENANCE REPAIRED SHORTED KEY WIRE TO YOKE MIC JACK SYSTEM. OPS CHECK GOOD. (M)
- [SDR A6WA200360005](https://openairdocs.org/sdr/A6WA200360005.md): Cable · unserviceable · Apr 10, 2003 · N616AW · Bac 146300A · Power Lever
  > NR 2 THRUST LEVER WILL NOT MOVE BELOW CRUISE AT 31K (31,000 FEET), OK AFTER 14K (14,000 FEET). REMOVED AND REPLACED UPPER PYLON TELEFLEX CABLE. ON INSPECTION OF THE UNSERVICEABLE TELEFLEX CABLE. CONFIRMED THAT A CRIMP ALONG THE LENGTH OF THE CABLE CAUSED IT
- [SDR A6WA200260078](https://openairdocs.org/sdr/A6WA200260078.md): Bleed Band · out of tolerance · Dec 23, 2002 · N616AW · Bac 146300A · Compressor Bleed Control
  > UPON APPLICATION OF TAKEOFF POWER, NR 2 ENGINE DID NOT RESPOND WHILE TGT WENT TO 950 DEGREES FOR AN ESTIMATED 5 SECONDS BEFORE SECURING. MAINTENANCE FOUND NR 2 ENGINE BLEED BAND OUT OF TOLERANCE. ADJUSTED AS REQUIRED AND PERFORMED 4 POINT RUN. ALL RUNS WITH
- [SDR A6WA200260005](https://openairdocs.org/sdr/A6WA200260005.md): Cage · cracked · May 22, 2002 · N616AW · Bac 146300A · Cargo/Baggage Doors
  > REAR CARGO DOOR UPPER AFT INNER SEAL RETAINER CAGE IS CRACKED APPROX 2 INCHES IN LENGTH. REPLACED UPPER AFT INNER CAGE IAW SRM 51-42-00. REPAIRS CARRIED OUT PER BARA/AVR/5007/00. (M)
- [SDR A6WA200260010](https://openairdocs.org/sdr/A6WA200260010.md): Frame · chafed · May 22, 2002 · N616AW · Bac 146300A · Engine Cowling System
  > NR 3 ENGINE FORWARD INBOARD COWL DOOR HAS CHAFE MARKS ON FORWARD MOST FRAME. REPAIRED IAW BAE RIL HC711H9089. (M)
- [SDR A6WA200260007](https://openairdocs.org/sdr/A6WA200260007.md): Door · cracked · May 22, 2002 · N616AW · Bac 146300A · Engine Cowling System
  > NR 4 ENGINE INBOARD AFT COWL DOOR HAS A CRACK NEXT TO DRAIN TUBE. REPAIRED CRACK IAW BAE PROCEDURE REF NR NWH/RJ/0726-02 AND RIL HC7IIH9012. (M)
- [SDR A6WA200260008](https://openairdocs.org/sdr/A6WA200260008.md): Retainer · damaged · May 22, 2002 · N616AW · Bac 146300A · Electrical/Electronic Compartment Doors
  > ELECTRICAL EQUIPMENT BAY DOOR RETAINING ANGLE ON FORWARD FRAME DAMAGED. ANGLE REPAIRED IAW BAE PROCEDURE REF NR CH/RJ/0734-02. (M)
- [SDR A6WA200260006](https://openairdocs.org/sdr/A6WA200260006.md): Structure · chafed · May 22, 2002 · N616AW · Bac 146300A · Entrance Stairs
  > FOUND LEFT AFT PAX DOOR AIRSTAIR HOOK CUTOUT HAS CHAFING FROM HOOK. REPAIRS CARRIED OUT IAW BAE PROCEDURE REF NR CH/RJ/0735/02. (M)
- [SDR A6WA200260004](https://openairdocs.org/sdr/A6WA200260004.md): Skin · dented · May 22, 2002 · N616AW · Bac 146300A · Fuselage Main, Plate/Skin
  > DENT IN A VERTICAL DIRECTION AT STRINGER 26L BETWEEN FRAME 12 AND 13. FABRICATED A REPAIR PATCH. PERFORMED A DETAILED VISUAL INSPECTION TO ENSURE SOUND CRACK FREE STRUCTURE REMAINS.
- [SDR A6WA200260011](https://openairdocs.org/sdr/A6WA200260011.md): Panel · dented · May 22, 2002 · N616AW · Bac 146300A · Wing, Plate/Skin
  > DENTS FOUND IN LEFT AND RIGHT WINGS TRAILING EDGE PANELS BETWEEN RIB 14A AND 15B. INSPECTION CARRIED OUT IAW MFG MM.
- [SDR A6WA200260013](https://openairdocs.org/sdr/A6WA200260013.md): Trim Tab · dented · May 22, 2002 · N616AW · Bac 146300A · Aileron Tabs
  > DENTS FOUND IN LEFT AILERON TRIM TAB. INSPECTION CARRIED OUT IAW MM.
- [SDR A6WA200260012](https://openairdocs.org/sdr/A6WA200260012.md): Bracket · cracked · May 22, 2002 · N616AW · Bac 146300A · Spoilers
  > LEFT INBOARD SPOILER OUTBOARD END BRACKET CRACKED AT FORWARD TOP EDGE. CARRIED OUT IAW MFG NWH/RJ/0723-02.
- [SDR A6WA200260009](https://openairdocs.org/sdr/A6WA200260009.md): Attach Angle · cracked · May 22, 2002 · N616AW · Bac 146300A · Fuselage Miscellaneous Structure
  > FLOOR BEAM TO CROSSMEMBER ATTACH ANGLE CRACKED AT STA 183.15 FORWARD SIDE AND LBL 47 OUTBOARD SIDE. CROSSMEMBER ATTACH ANGLE REPLACED IAW SRM.
- [SDR A6WA200000082](https://openairdocs.org/sdr/A6WA200000082.md): A/C Pack · odor · Jan 4, 2001 · N616AW · Bag BAE146300A · Cabin Cooling System
  > SMOKY SMELL IN CABIN AFTER TAKEOFF, CREW SHUT OFF APU AIR AND SWITCHED TO ENGINE AIR, OPERATED ON NR 2 PACK AND SMOKY SMELL DISSIPATED. MAINTENANCE PERFORMED DUCT CONTAMINATION CLEARING PROCEDURE COULD NOT DUPLICATE SMELL, SYSTEM OPERATES NORMALLY ON ALL ENGI
- [SDR 98ZZZM936](https://openairdocs.org/sdr/98ZZZM936.md): Door Warning · activated · Mar 19, 1998 · N616AW · Bag BAE146300A · Landing Gear Position and Warning
  > AFTER GEAR RETRACTION, LEFT MAIN GEAR INTRANSIT LIGHT 'RED' REMAINED ON AND RED LT IN GR HANDLE. COULD NOT DUPLICATE MEGGED AND UPLOCK HARNESSES. GEAR UPLOCK, 50M OHM EACH DOOR UPLOCK.5M OHM. REMOVED AND REPLACED HARNESS, FROZE SENSORS, CLEANED SENSORS, ON
- [SDR 98ZZZX1234](https://openairdocs.org/sdr/98ZZZX1234.md): Pan · broken · Dec 5, 1997 · N616AW · Bag BAE146300A · Flight Compartment Equipment
  > CAPTAIN'S SEAT ASSY SEAT PAN BROKEN AT FWD RT CORNER. PAN ALSO HAS SEVERAL OTHER CRACKS. MADE NEW SEAT PAN IAW PS1 DRAWING AW-25-10-9707-06 INSTALLED PER DRAWING ALSO.
- [SDR 98ZZZX1205](https://openairdocs.org/sdr/98ZZZX1205.md): Hinge · cracked · Nov 28, 1997 · N616AW · Bag BAE146300A · Trailing Edge Flaps
  > DURING ADJUSTMENT/CHECK OF RT NR 2 CARRIAGE FLAP CANOE, FOUND HINGE ASSY CRACKED AT TOP FORWARD TRANSVERSE BEAD. DRESSED OUT CRACKED AREA (JM/RJ085-97). C/W FLUORSCENT DYE PENETRANT AND EDDY CURRENT INSPECTIONS. INSPECTED ENTIRE HINGE ASSY FOR CRACKS, NO DE
- [SDR 98ZZZX1208](https://openairdocs.org/sdr/98ZZZX1208.md): Bracket · cracked · Nov 25, 1997 · N616AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > PSU RAIL RT OTBD, STAND-OFF BRACKET AT FRAMES 39-40 CRACKED AND RIVETS LOOSE. REPLACED BRACKET.
- [SDR 98ZZZX1209](https://openairdocs.org/sdr/98ZZZX1209.md): Bulkhead Frame · chafed · Nov 24, 1997 · N616AW · Bag BAE146300A · Fuselage Main, Bulkhead
  > THERE IS AN L-SHAPED CHAFE MARK ON FRAME 32 PRESSURE BULKHEAD, NEAR CENTERLINE BEHIND RT MLG DOOR UPLOCK ASSY. NEEDS INVESTIGATION. BLENDED ABOVE AREA IAW BAE FAX JM/FJ0844-97. REPROTECTED, PRIMED AND PAINTED.
- [SDR 98ZZZX1201](https://openairdocs.org/sdr/98ZZZX1201.md): Bracket · cracked · Nov 22, 1997 · N616AW · Bag BAE146300A · Passenger/Crew Doors
  > FORWARD PASSENGER DOOR - DOOR HANDLE SUPPORT BRACKET CRACKED. CHECKED WITH ET CRACK DEFECT NOTED. ITEM MARKED WITH TAG. MFG ABOVE BRACKET PER BAE DRAWING AND PS1 PN AW524H970206-000. INSTALLED PER SRM AND BAE FAX DJR/RJ0318-97 2 EACH UNF BOLTS.
- [SDR 98ZZZX1229](https://openairdocs.org/sdr/98ZZZX1229.md): Rib · cracked · Nov 21, 1997 · N616AW · Bag BAE146300A · Wing, Rib/Bulkhead
  > ATW - LT WING TIP REMOVEABLE RIB PANEL HAS A FEW CRACKS IN IT. PATCHED SAID CRACKS IAW BAE STD PRACTICES AND AIR WISC MM PSI REF: AW-57-20-9412-06.
- [SDR 98ZZZX1199](https://openairdocs.org/sdr/98ZZZX1199.md): Intercostal · cracked · Nov 21, 1997 · N616AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > REAR FUSELAGE AREA - CENTER FLOOR SUPPORT INTERCOSTAL CRACKED UNDER GUSSET PLATE BETWEEN FRAMES 41 AND 43. MARKED WITH GREEN DOT. REPAIRED INTERCOSTAL IAW BAE FAX REF DJR/RJ0839-97.
- [SDR 98ZZZX1194](https://openairdocs.org/sdr/98ZZZX1194.md): Frame · cracked · Nov 21, 1997 · N616AW · Bag BAE146300A · Fuselage Main, Frame
  > ATW - RIGHT SIDE OF ECS BAY AT FRAME NR 47 HAS A CRACK IN THE SHEAR ANGLE AT STR 9 THAT IS APPROX.25 INCH LONG IN THE BEND RADIUS. NOTE: VERIFIED WITH EDDY CURRENT. REPAIR SHEAR ANGLE IAW BAE REPAIR INSTRUCTIONS HC539H9014.
- [SDR 98ZZZX1207](https://openairdocs.org/sdr/98ZZZX1207.md): Angle · cracked · Nov 20, 1997 · N616AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > REAR CARGO BAY FLOOR SUPPORT ANGLE CRACKED AT SCREW HOLE FRAME 34. SPLICED 8 INCH SECTION TO SUPPORT ANGLE PER SRM 51-71-11, DAMAGED AREA REMOVED.
- [SDR 98ZZZX1221](https://openairdocs.org/sdr/98ZZZX1221.md): Stiffener · cracked · Nov 19, 1997 · N616AW · Bag BAE146300A · Wing Miscellaneous Structure
  > ATW - RIGHT WING TOP T/E SKIN STIFFENER CRACKED AT FWD END JUST INBD OF RIB NR 8. REPAIRED STIFFENER, REF FAX JM/RJ0317/97, AND JM/RJ0818-97.
- [SDR 98ZZZX1219](https://openairdocs.org/sdr/98ZZZX1219.md): Intercostal · broken · Nov 19, 1997 · N616AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > ATW - FORWARD CARGO INTERCOSTAL BROKEN BETWEEN FRAMES 23 AND 23 LT SIDE. REPAIRED INTERCOSTAL IAW BAE 146 SRM AND REINSTALLED IAW BAE 146 SCM. REF: 51-71-11. REPAIRED, OK FOR SERVICE.
- [SDR 98ZZZM372](https://openairdocs.org/sdr/98ZZZM372.md): Stiffener · cracked · Nov 19, 1997 · N616AW · Bag BAE146300A · Wing Miscellaneous Structure
  > RT WING TOP TE SKIN STIFFENER CRACKED AT FWD END BETWEEN RIBS 8/9, JUST OUTBOARD OF RIB 8. REPAIRED CRACKED STIFFENER IAW FAX NR'S JM/RJO317/97 AND NR JM/RJO818-97. (M)
- [SDR 98ZZZM369](https://openairdocs.org/sdr/98ZZZM369.md): Stiffener · cracked · Nov 19, 1997 · N616AW · Bag BAE146300A · Wing Miscellaneous Structure
  > LT WING, TRAILING EDGE AND SHROUD UPPER SKIN STIFFENER IS CRACKED AT FORWARD END IN AREA BETWEEN WING RIBS 7 AND 8. REPAIRED STIFFENER REF FAX JM/RJ0818-97. (M)
- [SDR 98ZZZM365](https://openairdocs.org/sdr/98ZZZM365.md): Stiffener · cracked · Nov 19, 1997 · N616AW · Bag BAE146300A · Wing Miscellaneous Structure
  > RT WING TOP TE SKIN STIFFENER CRACKED AT FWD END AT RIB NR 9, JUST INBOARD OF RIB 9. REPAIRED CRACKED STIFFENER IAW FAX NR'S JM/RJ0317/97 AND NR JM/RJO317/97 AND NR JM/RJO818-97. (M)
- [SDR 98ZZZX1195](https://openairdocs.org/sdr/98ZZZX1195.md): Frame · cracked · Nov 18, 1997 · N616AW · Bag BAE146300A · Fuselage Main, Frame
  > ATW - RIGHT SIDE OF STRUCTURE AFT OF FR 50 HAS A FRAME THAT IS CRACKED LOCATED ABOVE UPPER HINGE BLADE FOR AIRBRAKE BACKSIDE OF FR 50. CRACK IS UNDER OUTER CORNER OF GUSSET PLATE ACROSS THAT RIVET HOLE AND GOES INWARD TO INNER AND EDGE OF FRAME. REPLACED UPP
- [SDR 98ZZZM366](https://openairdocs.org/sdr/98ZZZM366.md): Frame · cracked · Nov 18, 1997 · N616AW · Bag BAE146300A · Fuselage Main, Frame
  > LEFT SIDE OF STRUCTURE AFT OF FRAME 50 HAS A FRAME ABOVE THE UPPER HINGE BLADE FOR SPEED BRAKE THAT HAS A CRACK ACROSS THE 3RD RIVET HOLE DOWN ON OUTER FLANGE THAT ATTACHES TO SKIN. VERIFIED WITH EDDY CURRENT. REPLACED LEFT UPPER WEB DIAPHRAM. (M)
- [SDR 98ZZZM364](https://openairdocs.org/sdr/98ZZZM364.md): Web · cracked · Nov 18, 1997 · N616AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > RT SIDE OF STRUCTURE AFT OF FRAME NR 50 HAS A WEB THAT RUNS VERTICALLY FROM THE REAR FLANGE OF FRAME NR 50 DOWN TO THE LOWER BLADE OF THE SPEED BRAKE HINGE THAT HAS A SMALL CRACK ACROSS THE UPPER TOP RIVET HOLE AT OUTER FLANGE. CRACK VERIFIED WITH EDDY CURREN
- [SDR 98ZZZX1202](https://openairdocs.org/sdr/98ZZZX1202.md): Inserts · corroded · Nov 17, 1997 · N616AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > FORWARD LAV MODULE, METAL INSERTS IN FLOOR CORRODED. REPLACED AS NEEDED. INSTALLED PERMACEL AFTER REPLACMENT OF INSERTS. REPLACED INSERTS AS NEEDED AND INSTALLED NEW PERMACEL ON UNDER SIDE OF FORWARD LAV MODULE.
- [SDR 98ZZZX1236](https://openairdocs.org/sdr/98ZZZX1236.md): Bracket · cracked · Nov 14, 1997 · N616AW · Bag BAE146300A · Engine Cowling System
  > NR 2 ENGINE SHOULDER COWL TERMINAL BOARD FWD BRACKET CRACKED. REPLACED NR 2 ENG SHOULDER COWL TERMINAL BOARD FWD BRACKET.
- [SDR 98ZZZX1233](https://openairdocs.org/sdr/98ZZZX1233.md): Bracket · broken · Nov 13, 1997 · N616AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > FWD CLOSET WALL BEHIND FO'S SEAT, LOWER CORNER ATTACH BRACKET BROKEN. FABRICATED AND REPLACED FWD CLOSET WALL BRACKET BEHIND FO'S SEAT (LOWER ATTACH BRACKET).
- [SDR 98ZZZX1227](https://openairdocs.org/sdr/98ZZZX1227.md): Sill · corroded · Nov 13, 1997 · N616AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > AFT VESTIBULE SILL PLATE FOR SERVICE DOOR SIDE HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED AFT VESTIBULE SERVICE DOOR SILL PLATE.
- [SDR 98ZZZX1224](https://openairdocs.org/sdr/98ZZZX1224.md): Angle · cracked · Nov 13, 1997 · N616AW · Bag BAE146300A · Wing Miscellaneous Structure
  > ATW - RT WING T/E LOWER SKIN STIFFENER AFT TAG ANGLE CRACKED BETWEEN RIBS 3 AND 4. REPLACED ANGLE.
- [SDR 98ZZZX1223](https://openairdocs.org/sdr/98ZZZX1223.md): Angle · cracked · Nov 13, 1997 · N616AW · Bag BAE146300A · Wing Miscellaneous Structure
  > RT WING T/E LOWER SKIN STIFFENER AFT TAG ANGLE CRACKED AT RIB NR 4. REPLACED ANGLE.
- [SDR 98ZZZX1222](https://openairdocs.org/sdr/98ZZZX1222.md): Angle · cracked · Nov 13, 1997 · N616AW · Bag BAE146300A · Wing Miscellaneous Structure
  > ATW - RT WING T/E LOWER SKIN STIFFENERS AFT TAG ANGLE CRACKED BETWEEN RIBS 5 AND 6. REPLACED ANGLE.
- [SDR 98ZZZX1206](https://openairdocs.org/sdr/98ZZZX1206.md): Seal Cage · cracked · Nov 13, 1997 · N616AW · Bag BAE146300A · Cargo/Baggage Doors
  > REAR CARGO DOOR LOWER AFT SEAL CAGE CRACKED. REPLACED LOWER AFT SEAL CAGE.
- [SDR 98ZZZX1226](https://openairdocs.org/sdr/98ZZZX1226.md): Bolts · loose · Nov 12, 1997 · N616AW · Bag BAE146300A · Wing Miscellaneous Structure
  > ATW - AIR WISC EO E92/083/657 RECC ATTACH BOLTS AND NUTS ON RT SIDE, A, B, C, D ARE LOOSE ON THE REAR SPAR ROOT ATTACHMENT FITTING AT WING RIB 2. REPLACED FASTENERS IAW BAE REPAIR INSTRUCTIONS HC53H9043. BOLTS A, C, D ORIG SIZE. BOLT B FIRST OVERSIZE, RESEA
- [SDR 98ZZZX1225](https://openairdocs.org/sdr/98ZZZX1225.md): Mounting · cracked · Nov 11, 1997 · N616AW · Bag BAE146300A · Drag Control System
  > ATW - RT LIFT SPOILER VALVE MOUNTING PLATE CRACKED. REMOVED AND REPLACED RT SPOILER VALVE MOUNTING PLATE. NO DISCONNECTING OF VALVE REQUIRED.
- [SDR 98ZZZX1237](https://openairdocs.org/sdr/98ZZZX1237.md): Cowl · chafed · Nov 7, 1997 · N616AW · Bag BAE146300A · Engine Cowling System
  > NR 2 ENGINE LT FWD COWL DOOR AFT FRAME CHAFED AT LATCH AREA AND AT MID-AREA DUE TO CONTACT WITH HYDRAULIC LINE. REPLACED CAP STRIP ON NR 2 ENG LT FWD COWL DOOR AFT FRAME.
- [SDR 98ZZZX1216](https://openairdocs.org/sdr/98ZZZX1216.md): Floor · buckled · Nov 7, 1997 · N616AW · Bag BAE146300A · Fuselage Floor Panel
  > REF FAX LM/115-97, LM/116-97, JM/RJ0096-97, AND DJR/RJ0098-97. MLG PRESS FLOOR BETWEEN FRAMES 29 AND 32 OTBD SEAT RAILS 19 INCHES, 20 INCHES OTBD CENTERLINE HV BUCKLE APPROX.125 INCH DEEP. DV DUE EA 500 CYC. REPORT FINDINGS AI (R) REMOVE FLOOR STS. CUR 230
- [SDR 98ZZZX1231](https://openairdocs.org/sdr/98ZZZX1231.md): Bracket · cracked · Nov 6, 1997 · N616AW · Bag BAE146300A · Wing Miscellaneous Structure
  > ATW - LT WING BRACKET FOR HYD LINES THAT PASS THROUGH THE AFT END OF THE SPOILER HINGE RIB AT WING RIB NR 5 IS CRACKED. REPLACED BRACKET.
- [SDR 98ZZZX1220](https://openairdocs.org/sdr/98ZZZX1220.md): Angle · cracked · Nov 6, 1997 · N616AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > FREIGHT ANGLE AT FRAME 19D CRACKED CENTER SECTION. REPLACED FREIGHT ANGLE AT FRAME 19D IAW BAE 146 SRM.
- [SDR 98ZZZX1213](https://openairdocs.org/sdr/98ZZZX1213.md): Jobolts · damaged · Nov 6, 1997 · N616AW · Bag BAE146300A · Wing Miscellaneous Structure
  > REPLACED JOBOLTS ON RT WING CENTER TANK RIB 2 INBOARD PER RIL HC571H9033. PERFORMED RIL HC571H9033 TO RIB 2 INBD CENTER TANK. REPLACED JOBOLTS WITH MRL FASTENERS.
- [SDR 98ZZZX1203](https://openairdocs.org/sdr/98ZZZX1203.md): Support · cracked · Nov 6, 1997 · N616AW · Bag BAE146300A · Fuselage Miscellaneous Structure
  > FRONT CARGO BAY CENTER CARGO FLOOR SUPPORT AT 19C CORRODED AND CRACKED. AREA MARKED. REPLACED FREIGHT ANGLE AT FR 19C IAW BAE 146 SRM.

Next page: https://openairdocs.org/deregistered/N616AW-2014-10-29/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 = 'N616AW' AND deregistration_id = 'N616AW-2014-10-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N616AW-2014-10-29/reports

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