# Service difficulty reports: N219FE, cancelled Sep 23, 2009

A list on [N219FE, cancelled Sep 23, 2009](https://openairdocs.org/deregistered/N219FE-2009-09-23.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 · 77 reports

- [SDR FDEA200901090104](https://openairdocs.org/sdr/FDEA200901090104.md): Indication Sys · inoperative · Jan 9, 2009 · N219FE · Boeing 727233 · Central Warning
  > DURING CLIMB-OUT, NR 1 CSD "RISE" OUT OF LIMITS. QRH DIRECTED US TO DISCONNECT NR 1 CSD. REPLACED TEMP BULB. NO HELP TRIED NEW OUT TEMP BULB NO HELP. SWAPPED IND CONN & PROBLEM FOLLOWED. DURING NR 1 ENG RUN, RISE 10 DEG & NR 2 AND 3 WERE AT 1 DEG. NR 1 R
- [SDR 07FDEA00191](https://openairdocs.org/sdr/07FDEA00191.md): Floor Support · corroded · Jan 27, 2007 · N219FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT PIT ALONG LEFT SIDE OF S-29L FROM STA 950F-970 HAS SURFACE CORROSION REMOVED FLOOR SUPPORT FOR ACCESS IAW SRM 51-30-2. REMOVED CORROSION IAW SRM 51-10-6. AREA FOUND WITHIN LIMITS FOR STRAP REPAIR IAW SRM 27-53-023. FABBED STRAP IAW SR 27-53-023, MATERIA
- [SDR 07FDEA00155](https://openairdocs.org/sdr/07FDEA00155.md): Stringer · corroded · Jan 24, 2007 · N219FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > FWD PIT 3" FWD OF STA 600, STR 27L EXFOLIATED REPAIRED STR 27L AT STA 600 IAW SRM 53-10-3 PG4 FIG1 SHEET 2,TABLE I.
- [SDR 05FDEA03831](https://openairdocs.org/sdr/05FDEA03831.md): Cargo · leaking · Nov 15, 2005 · N219FE · Boeing 727233 · Cargo Compartments
  > FUMES IN COCKPIT STRONG ODOR, EMERGENCY EVACUATED ON TAXIWAY. DEPLOYED SLIDE. HAZMAT TEAM DETERMINED THE FUMES AND ODOR WERE COMING FROM THE HAZMAT CAN. HAZMAT TEAM DOWNLOADED HAZMAT CAN AND FOUND ONE DRUM LEAKING UN1993 (TERDODECIL MERCAPTANO). CLEANED UP
- [SDR 05FDEA03508](https://openairdocs.org/sdr/05FDEA03508.md): Warning Horn · activated · Oct 26, 2005 · N219FE · Boeing 727233 · Cabin Pressure Control System
  > PASSING THRU FL250 CABIN ALTITUDE WARNING HORN CAME ON AND CABIN WAS AT 10,000FT. BOTH PACKS ON, ENGINE BLEED NR 1 AND NR 3 OPEN. NO OTHER ABNORMAL INDICATIONS (OUTFLOW VALVE CLOSED AND ALL DOES CLOSED). EMERGENY DECLARED AND NO FUEL DUMP REQUIRED.
- [SDR 05FDEA03427](https://openairdocs.org/sdr/05FDEA03427.md): Clamp · loose · Oct 13, 2005 · N219FE · Boeing 727233 · Engine Bleed Air System
  > CRUISE POWER SETTING, NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. RAN QRH AND LIGHT WENT OUT GOOD SYST TEST, RETURNED TO KMIA. INSPECTED ALL DUCTS, CLAMPS AND SENSE LINES. FOUND NUMEROUS CLAMPS LOOSE AT NR 1 PRECOOLER AND NR 1 BLEED VALVE. TIGHTEN CLAMPS
- [SDR 04FDEA03002](https://openairdocs.org/sdr/04FDEA03002.md): Actuator · malfunctioned · Oct 30, 2004 · N219FE · Boeing 727200 · Leading Edge Slat Actuator
  > NR 1 SLAT LED FAILED TO RETRACT AND INDICATING AMBER ON FLAP RETRACTION TO FLAPS 2 IN FLIGHT. REMOVED AND REPLACED NR 1 SLAT ACTUATOR AS PER M/M 27-81-03-4, OP CKS NORM.
- [SDR 02FDEA00407](https://openairdocs.org/sdr/02FDEA00407.md): Oil Cooler · faulty · Jun 15, 2002 · N219FE · Boeing 727200 · Alternator-Generator Drive
  > DURING CLIMBOUT NR 1 CSD AND NR 3 CSD OVERHEATED (NR 1 REPEAT), NR 1 WAS 130C & NR 3 125C WITH NR 2 105C (IN LIMITS). IAW QRH NR 1 GEN BREAKER WAS TRIPPED AND WAS STILL OVER 120C AFTER 3 MIN. DISCONNECTED NR 1 CSD. NR 3 GEN WAS TRIPPED AND WAS OVER 120C AFT
- [SDR 01FDEA00636](https://openairdocs.org/sdr/01FDEA00636.md): Motor · leaking · Aug 3, 2001 · N219FE · Boeing 727233 · Trailing Edge Flap Actuator
  > INBOARD FLAP DRIVE HYD MOTOR LEAKING IN LT WHEEL WELL. REMOVED AND REPLACED MOTOR PER 727 200 MM 27-51-062-4. LEAK CHECK GOOD.
- [SDR 01FDEA00352](https://openairdocs.org/sdr/01FDEA00352.md): Radar · faulty · May 15, 2001 · N219FE · Boeing 727233 · Weather Radar System
  > AT 14000 MSL WITH A/C STRAIGHT AND LEVEL RADAR TILT AT +2.5 DEG.R&R RADAR ANTENNA DRIVE UNIT PER AMM 34-41-021-4. R&R RADAR T/R PER AMM 34-41-041-4. TEST NORM.
- [SDR 01FDEA00297](https://openairdocs.org/sdr/01FDEA00297.md): Frame · cracked · Apr 6, 2001 · N219FE · Boeing 727233 · Fuselage Main, Frame
  > LWR CARGO COMPT PERF HFEC INSP FOUND 1 CRACK APPROX 1.5 INCH AT BS 600 JUST ABOVE S-20L AT I/B RADIUS SUB FRAME UNDER CARGO DOOR SPOOL FITTING. ** S/D ** R&R & FAB PER FDW DWG 53FX1349. PER SRM 51-10-01 & FDX DFWG 53FX1371.
- [SDR 00FDEA00606](https://openairdocs.org/sdr/00FDEA00606.md): Frame · corroded · Aug 28, 2000 · N219FE · Boeing 727233 · Fuselage Main, Frame
  > ON THE AFT AUX FUEL TANK THE LOWER, AFT STRAP CORRODED IN MULTIPLE PLACES THE LENGTH OF STRAP ON LOWER FACE. *S/D* REMOVED AND REPLACED PER IAW DRAWING 65-80689 & FEDEX SRM 51-30-2, 51-30-5.
- [SDR 00FDEA00517](https://openairdocs.org/sdr/00FDEA00517.md): Floorbeam · corroded · Aug 3, 2000 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (C53-111-01,3) AROUND NUT PLATE HOLE, LWR CHORD OF BS 1148 FLOORBEAM, RBL 22, WL 201. *S/D* REMOVED AND REPLACED FEDEX EA 7-5310-52128 & SRM 53-10-8.
- [SDR 00FDEA00513](https://openairdocs.org/sdr/00FDEA00513.md): Stringer · cracked · Aug 2, 2000 · N219FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > TWO INCH CRACK IN STRINGER, BS 740, STR 24R, UNDER I/B HAT. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 53-10-3.
- [SDR 00FDEA00514](https://openairdocs.org/sdr/00FDEA00514.md): Floorbeam · misdrilled · Aug 2, 2000 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > WHILE INSP NRC 0901 (INT 194) FINAL BAY OFF FOUND DOUBLE DRILLED HOLE AT BS 360, LBL 23, WL 208. *S/D* DAMAGE OUT OF LIMITS IAW FEDEX SRM 53-10-1 AND REPAIRED PER IAW FEDEX SRM 57-10-8 FIG 8.
- [SDR 00FDEA00512](https://openairdocs.org/sdr/00FDEA00512.md): Shear Tie · corroded · Aug 1, 2000 · N219FE · Boeing 727233 · Fuselage Main, Structure
  > CORROSION (C53-111-01) ON BS 950E, STR 26L SHEAR TIE AND TWO FASTENERS RUSTED OFF. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51-10-6 PG 5, 51-20-5.
- [SDR 00FDEA00496](https://openairdocs.org/sdr/00FDEA00496.md): Door Frame · corroded · Jul 28, 2000 · N219FE · Boeing 727233 · Fuselage Main, Structure
  > CORROSION (C53-111-02, 2) NR 3 CARGO DOORWAY FWD FRAME AT BS 1090, RBL 33, WL 150. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-10-6, 53-10-1, EA 7-5310-52146.
- [SDR 00FDEA00499](https://openairdocs.org/sdr/00FDEA00499.md): Floorbeam · corroded · Jul 28, 2000 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (C53-111-01, 3) ON LOWER CHORD BS 1148 FLOORBEAM LBL 1 - 3, 10, 21, 29, WL 200. *S/D* ACCOMPLISHED PER FEDEX EA 7-5310-52128. OUT OF LIMITS PER FEDEX 53-10-1.
- [SDR 00FDEA00497](https://openairdocs.org/sdr/00FDEA00497.md): Floorbeam · corroded · Jul 28, 2000 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01,3) AROUND NUT PLATE HOLES UPPER CHORD, BS 1030 FLOORBEAM, RBL 21, RBL 28, RBL 35, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-8.
- [SDR 00FDEA00498](https://openairdocs.org/sdr/00FDEA00498.md): Floorbeam · corroded · Jul 28, 2000 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (C53-111-01, 3) ON LOWER CHORD BS 1130 FLOORBEAM, LBL 43 - RBL 50, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX 51-30-2, 51-20-4.
- [SDR 00FDEA00494](https://openairdocs.org/sdr/00FDEA00494.md): Floorbeam · corroded · Jul 28, 2000 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01,1) ON FLOORBEAM BS 344, LBL 38, WL 208. *S/D* REMOVED AND REPLACED CORROSION PER IAW FEDEX SRM 53-10-4, 51-30-2 & SR 27-53-007.
- [SDR 00FDEA00495](https://openairdocs.org/sdr/00FDEA00495.md): Floorbeam · corroded · Jul 28, 2000 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR SUPPORT UPPER FLANGE LOWER FWD, AND AFT SIDE AT BS 720A, LBL 10, WL 208. *S/D* REMOVED AND REPLACED CORROSION PER IAW FEDEX SRM 51-10-6, 53-10-1. ALODINED, PRIMED, INSTALLED PARTS AND SEAT TRACK PER IAW FEDEX SRM 53-10-9, 51-20-021, 51-20
- [SDR 00FDEA00491](https://openairdocs.org/sdr/00FDEA00491.md): Floorbeam · corroded · Jul 26, 2000 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01, 1) ON FLOORBEAM AT BS 328, LBL 44, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX DRAWING SR 27-53-017.
- [SDR 00FDEA00490](https://openairdocs.org/sdr/00FDEA00490.md): Keelbeam · cracked · Jul 25, 2000 · N219FE · Boeing 727233 · Fuselage Main, Keel
  > LT KEEL BEAM IS CRACKED AT BS 873 ON UPPER FLANGE UNDER APU I/B. *S/D* REPAIRED PER FEDEX EA NR 7-5310-52126.
- [SDR 00FDEA00489](https://openairdocs.org/sdr/00FDEA00489.md): Keelbeam · cracked · Jul 25, 2000 · N219FE · Boeing 727233 · Fuselage Main, Keel
  > RT KEEL BEAM IS CRACKED AT BS 873 ON UPPER FLANGE UNDER APU I/B. *S/D* REPAIRED PER FEDEX EA NR 7-5310-52126.
- [SDR 00FDEA00485](https://openairdocs.org/sdr/00FDEA00485.md): Floorbeam · corroded · Jul 25, 2000 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (C53-111-01, 3) ON LOWER CHORD BS 1030 FLOORBEAM LBL 10 - 12, 18, 40 RBL 34, WL 200. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-1, 53-10-8.
- [SDR 00FDEA00487](https://openairdocs.org/sdr/00FDEA00487.md): Floorbeam · corroded · Jul 25, 2000 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01, 3) AROUND NUT PLATE HOLES UPPER CHORD BS 1110 FLOORBEAM, RBL 15, LBL 15, LBL 21, LBL 41 - 44, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-1, 53-10-8 & FEDEX EA NR 7-5310-52116.
- [SDR 00FDEA00484](https://openairdocs.org/sdr/00FDEA00484.md): Skin · gouged · Jul 25, 2000 · N219FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > NUMEROUS NICKS AND GOUGES IN SKIN FROM BS 480 - 520 BETWEEN STR 27L AND 26R. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-30-3 FIG 3.
- [SDR 00FDEA00488](https://openairdocs.org/sdr/00FDEA00488.md): Floorbeam · corroded · Jul 25, 2000 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01, 3) ON UPPER CHORD BS 950D FLOORBEAM RBL 10, 2, LBL 10, 21, WL 208. *S/D* BLENDED CORROSION IAW FEDEX SRM 51-10-6. REMOVED AND REPLACED RBL 10 PER FEDEX SRM 53-10-8.
- [SDR 00FDEA00486](https://openairdocs.org/sdr/00FDEA00486.md): Floorbeam · corroded · Jul 25, 2000 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (C53-111-01, 3) ON LOWER CHORD BS 1070 FLOORBEAM LBL 27 - 43, RBL 40, WL 200. *S/D* REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED NEW REPAIR ANGLES AND FILLERS PER IAW FEDEX SRM 53-10-1 FIG 4 AND FEDEX SRM 53-10-8 FIG 8.
- [SDR 00FDEA00476](https://openairdocs.org/sdr/00FDEA00476.md): Stringer · cracked · Jul 19, 2000 · N219FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > STRINGER 4 LT IS CRACKED AT BS 640. *S/D* REPAIRED PER FEDEX SRM 53-10-3.
- [SDR 00FDEA00299](https://openairdocs.org/sdr/00FDEA00299.md): Warning Light · illuminated · Apr 26, 2000 · N219FE · Boeing 727233 · Attitude Gyro and Indicating System
  > HDG COMPARATOR LIGHT REPEATEDLY ILLUM. *S/D* REPLACED SPLICES AS PER MM 20-30-12, REPAIRED WIRES AS PER SMP & REPLACED NR 1 & 2 COMPASS RACKS & DIRECTIAL GYROS AS PER MM 34-21-071-4.
- [SDR 00FDEA00298](https://openairdocs.org/sdr/00FDEA00298.md): Amplifier · inoperative · Apr 26, 2000 · N219FE · Boeing 727233 · Attitude Gyro and Indicating System
  > DURING CLIMBOUT INOP HEADING FLAGS WERE OBSERVED ON CAPT RMI & FOS HSI. HDG INSTRUMENT COMPARATOR LIGHT ALSO ILLUM. REMOVED AND REPLACED NR 1 COMPASS AMP RACK AS PER SMP AND NR 1 DG AS PER MM 34-21-071-4. PERFORMED OPER TEST OK.
- [SDR 99FDEA00492](https://openairdocs.org/sdr/99FDEA00492.md): Accessory Unit · malfunctioned · Dec 1, 1999 · N219FE · Boeing 727233 · Landing Gear Position and Warning
  > WHEN LANDING GEAR EXTENDED, BOTH GROUND AND RED IND LIGHTS WERE PRESENT ON FRONT IND. REMOVED AND REPLACED LANDING GEAR ASSY UNIT AND CLEANED ELECTRICAL CONNECTORS ON THE RACK WITH CONTACT CLEANER MM 32-01-122, TEST OK ON GROUND.
- [SDR 99FDEA00490](https://openairdocs.org/sdr/99FDEA00490.md): Accessory Unit · inop · Nov 29, 1999 · N219FE · Boeing 727233 · Landing Gear Position and Warning
  > DURING GEAR EXT, 3 GRN LIGHT+3 RED GEAR LIGHT+TAILSKID LIGHT WERE ILLUMINATED. REMOVED AND REPLACED L/G ACCESSORY UNIT PER MM 32-09-122 & TEST OK.
- [SDR 99FDEA00295](https://openairdocs.org/sdr/99FDEA00295.md): Accessory Unit · failed · Jul 27, 1999 · N219FE · Boeing 727233 · Landing Gear Retraction/Extension System
  > 99-180 - LAND GEAR LEVER UNABLE TO RAISE AFT T/O. LAND GEAR LEVER LATCH LIGHTS CIRCUIT BREAKER WAS CK IN. NO CHG. FLAPS RAISED TO 2 AND NO WARN HORN. WING ANTI-ICE TEST AND DID NOT OPEN. NOSE GEAR STEER HANDLE ALIGNMENT MARKS WERE ALIGNED. REMOVED AND RE
- [SDR 99FDEA00286](https://openairdocs.org/sdr/99FDEA00286.md): Relay · inop · Jul 27, 1999 · N219FE · Boeing 727233 · Landing Gear Retraction/Extension System
  > 99-172 LANDING GEAR LEVER FAILED TO RAISE AFTER TAKEOFF. WING ANTI-ICE WAS TESTED AND DID NOT OPEN. REMOVED AND REPLACED R-92 RELAY, OPER CK WAS NORM PER MM 32-31-011-1 THROUGH 5. CLEANED PROXIMITY SWITCHES.
- [SDR 99FDEA00030](https://openairdocs.org/sdr/99FDEA00030.md): Air Dist · odor · Jan 28, 1999 · N219FE · Boeing 727233 · Air Distribution System
  > AN ODOR WAS NOTICED IN THE ENTRYWAY. INSPECTED UPPER DECK AREA, E & E COMP, LWR CARGO AREAS AND AFT AIRSTAIR AREA, RUN ENGINES AND OPERATED PACKS PER JET RUN HANDBOOK. COULD NOT DUPLICATE ODOR. OK TO CONTINUE.
- [SDR 98FDEA00664](https://openairdocs.org/sdr/98FDEA00664.md): Floorbeam · corroded · Oct 20, 1998 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION ON TOP FLANGE AND BOTTOM OF TOP FLANGE ON FLOORBEAM BS 1110, LBL 65. REPAIRED FLOORBEAM AT BS 1110, LBL 65 PER SRM 53-10-8 AND EA 7-5310-29647.
- [SDR 98FDEA00642](https://openairdocs.org/sdr/98FDEA00642.md): Bellframe · bent · Oct 9, 1998 · N219FE · Boeing 727233 · Fuselage Main, Frame
  > NR 1755 UPR LOBE BENT BELLFRAME AT BS 560, RBL 65 5 APPROX ABOVE FLOORBEAM. CUT OUT DAMAGE AREA FAB DOUBLER, ALODINED, PRIMED & INSTALLED DOUBLER PER SRM 51-40-3.
- [SDR 98FDEA00643](https://openairdocs.org/sdr/98FDEA00643.md): Seat Track · corroded · Oct 8, 1998 · N219FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > NR 975 CORROSION ON SEAT TRACK & FLOORBEAM AT BS 1050 AT LBL 25 FROM C/L. SEAT/TRACK CORROSION REMOVED & NOW OUT OF LIMITS. INSTALL FLOORBEAM UPPER CHORD BY ACCORD WITH SRM 53-10-8 FIG 1 & EA 7-5310-29647 DATED 9/30/98.
- [SDR 98FDEA00636](https://openairdocs.org/sdr/98FDEA00636.md): Floorbeam · corroded · Oct 6, 1998 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION BETWEEN FLOORBEAM AND SEAT TRACK BS 1050, RBL 25. REMOVED CORROSION AND CUT OUT DAMAGE. INSTALLED REPAIR DOUBLERS PER SRM 53-10-8.
- [SDR 98FDEA00635](https://openairdocs.org/sdr/98FDEA00635.md): Floorbeam · corroded · Oct 6, 1998 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > BS 950D RBL 25 TO LBL 25, 8 FLOORBOARD FASTENER HOLES CORRODED AT FLOORBEAM. REMOVED CORROSION AREA AT RBL 10, BS 950D OUT OF LIMITS. INSTALLED FLOORBEAM REPAIR PER AARD 53-10-07-2 IAW EA 7-5310-29647.
- [SDR 98FDEA00634](https://openairdocs.org/sdr/98FDEA00634.md): Floorbeam · damaged · Oct 6, 1998 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > ACCOMPLISH REPAIR TO BS 950D, BL 0 AS PER SRM 53-10-8 FIG 8 PG 44 REF AARD 51-20-1-05. INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8 FIG 8 AND EA 7-5310-29647.
- [SDR 98FDEA00633](https://openairdocs.org/sdr/98FDEA00633.md): Fitting · corroded · Oct 6, 1998 · N219FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > BS 870 FLOORBEAM FITTING AT CENTER EXPANSION TRACK BELOW FLOOR LWR FITTING HAS CORROSION BOTH SIDES. REMOVED AND REPLACED CORROSION PER EA 7-5310-29647 AND REINSTALLED EXPANSION TRACK.
- [SDR 98FDEA00632](https://openairdocs.org/sdr/98FDEA00632.md): Floorbeam · corroded · Oct 6, 1998 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > BS 870 FLOORBEAM AT BL 0 TO RBL 25 CORROSION ON FLOORBEAM AND IN FASTENER HOLES. REMOVED CORROSION AND INSTALLED FREEZE PLUG PER EA 7-5310-2964.
- [SDR 98FDEA00631](https://openairdocs.org/sdr/98FDEA00631.md): Floorbeam · corroded · Oct 6, 1998 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM BS 1130, LBL 35 AND LBL 42. REPAIRED IAW EA NR 7-5310-29637B.
- [SDR 98FDEA00630](https://openairdocs.org/sdr/98FDEA00630.md): Floorbeam · damaged · Oct 6, 1998 · N219FE · Boeing 727233 · Fuselage Main, Floor Beam
  > BS 1030 BL 0, FLOORBEAM REPAIR NOT PER SRM ON I/B AIRCRAFT. REMOVED PREVIOUS REPAIR AND INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8, FIG 3.
- [SDR 98FDEA00629](https://openairdocs.org/sdr/98FDEA00629.md): Bell Frame · crushed · Oct 6, 1998 · N219FE · Boeing 727233 · Fuselage Main, Frame
  > LWR FWD CARGO COMP BS 580 BELL FRAME CRUSHED IN SEVERAL AREAS BETWEEN STR 26 AND 23 LEFT. REPAIRED BELL FRAME AT BS 580 BETWEEN STR 26L AND 23L PER SRM 51-40-3.
- [SDR 98FDEA00628](https://openairdocs.org/sdr/98FDEA00628.md): Beltframe · damaged · Oct 6, 1998 · N219FE · Boeing 727233 · Fuselage Main, Frame
  > BELTFRAME DAMAGED BS 520, RT SIDE 6 INCHES ABOVE FLOORBEAM. TRIMMED OUT DAMAGE. INSTALLED TYPICAL FORMED SECTION REPAIR PER SRM 51-40-3.

Next page: https://openairdocs.org/deregistered/N219FE-2009-09-23/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 = 'N219FE' AND deregistration_id = 'N219FE-2009-09-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N219FE-2009-09-23/reports

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