# Service difficulty reports: N917UP, cancelled Aug 23, 2006

A list on [N917UP, cancelled Aug 23, 2006](https://openairdocs.org/deregistered/N917UP-2006-08-23.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 · 59 reports

- [SDR UPS02238231](https://openairdocs.org/sdr/UPS02238231.md): Battery · discharged · May 14, 2002 · N917UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:AS-E BATTERIES IN THE COCKPIT EMERGENCY EXIT LIGHT ASSY ARE WEAK. UPON REPLACEMENT OF BATTERIES, THE BATTERY TRAY END TAB BROKE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSY IN THE COCKPIT AS PER M/M 33-50-67. OP'S CHECKS GOOD. OK FO
- [SDR UPS02237610](https://openairdocs.org/sdr/UPS02237610.md): Switch · out of adjust · Feb 12, 2002 · N917UP · Boeing 72730C · Door Warning System
  > INSPECTION TYPE:N/A UPON LEVELING AT FLT LEVEL 280 AMBER MAIN CARGO DOOR LIGHT ILLUMINATED, FOLLOWED APPROPRIATE EMERGENCY PROCEDURES. DESCENDED TO AIRCRAFT ALTITUDE 17,000, CABIN ALTITUDE 7,000. MAIN CARGO DOOR LIGHT WENT OUT. ADJ AFT MAIN CARGO DOOR MICRO
- [SDR UPS01237190](https://openairdocs.org/sdr/UPS01237190.md): Support · cracked · Oct 26, 2001 · N917UP · Boeing 72730C · Spoilers
  > INSPECTION TYPE:IN RT WING INBOARD GROUND SPOILER ACTUATOR FITTING ASSY LT AND RT PANEL SUPPORT BRACKETS CRACKED. REMOVED AND REPLACED INBOARD AND OUTBOARD GROUND SPOILER PANEL SUPPORT BRACKETS REF IPC 57-40-00 FIG 4A ITEM 186 & 188.
- [SDR UPS01235327](https://openairdocs.org/sdr/UPS01235327.md): Oxygen Mask · failed · Mar 21, 2001 · N917UP · Boeing 72730C · Crew Oxygen System
  > D-SECOND OBSEVERS. O2 MASK INOP M-211583. R & R 02 MASK & CLEANED AUDIO JACK. CHECKS GOOD THIS CLEARS DFRL.
- [SDR UPS00233393](https://openairdocs.org/sdr/UPS00233393.md): Unknown · odor · Jul 20, 2000 · N917UP · Boeing 72730C · Air Distribution System
  > INSPECTION TYPE:N/A, BRIEF ACRID SMELL DURING CLIMB. RAN ALL ENGS AND OPERATED PACKS. LOADED ELECTRICAL SYSTEM INCLUDING INTERIOR LIGHTING. COULD NOT FIND ANY ABNORMAL SMELL/ODOR.
- [SDR UPS00233384](https://openairdocs.org/sdr/UPS00233384.md): Stringer · cracked · Jun 17, 2000 · N917UP · Boeing 72730C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, IN FORWARD LWR CARGO COMPARTMENT STA 670, STR 22R, THE STRINGER HAS A CORROSION CRACK. CUT OUT DAMAGED STRINGER SECTION AND INSTALLED REPAIR IAW SRM 53-10-3 FIG 1. MATERIAL USED (P/N BAC1498-142), DOUBLER 20 INCHES.
- [SDR UPS00233388](https://openairdocs.org/sdr/UPS00233388.md): Fitting · corroded · Jun 12, 2000 · N917UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, EVIDENCE OF CORROSION IN PREVIOUS BLEND OUTS AT RIGHT SIDE BOTTLE PIN FITTING REAR LUG IN BUSHING BORE (FOUND AFTER BUSHING REMOVED). ACCOMPLISHED REPAIR IAW UPS ENGINEERING ORDER B727-5310-3056 AND BOEING DWG 65C23231, SH 1, 2 & 3.
- [SDR UPS00233383](https://openairdocs.org/sdr/UPS00233383.md): Stringer · cracked · Jun 12, 2000 · N917UP · Boeing 72730C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, STRINGER 16 RIGHT CRACKED AT BS 480 AND BS 500. INSTALLED REPAIR AT STR 16R, BS 480 & BS 500 IAW SRM 53-10-3 FIG 1. MATERIAL USED (P/N BAC1498-140), SPLICE (P/N BAC1498-132).
- [SDR UPS00233387](https://openairdocs.org/sdr/UPS00233387.md): Angle · missing · Jun 10, 2000 · N917UP · Boeing 72730C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:N/A, VIEW FROM LEFT WHEEL WELL INSIDE KEEL BEAM, THE CENTER CHORD ANGLE HAS TWO AREAS OF MATERIAL MISSING. INSTALLED NEW CHORD ANGLE IAW BOEING DRAWING 65-18636 AND SRM 51-30- 2. MATERIAL USED 2024T3511, 50 INCHES.
- [SDR UPS00233385](https://openairdocs.org/sdr/UPS00233385.md): Pin · corroded · Jun 10, 2000 · N917UP · Boeing 72730C · Wing, Attach Fittings
  > INSPECTION TYPE:C, RIGHT WING FRONT SPAR WING-TO-BODY FITTING BOTTLE PIN CORRODED. RIGHT WING FRONT SPAR WING-TO-BODY FITTING BOTTLE PIN REPLACED IAW B727 MM 57-41-01.
- [SDR UPS00233382](https://openairdocs.org/sdr/UPS00233382.md): Seat Track · worn · Jun 10, 2000 · N917UP · Boeing 72730C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C, SEAT TRACK WORN BETWEEN BS 500 AND BS 520 AT RBL 24.75. REPLACED SECTION OF SEAT TRACK FROM STA 500 TO STA 520 AT RBL 24.75 IAW SRM 53-10-5 FIG 7. MATERIAL USED (P/N BAC1520-1432).
- [SDR UPS00233381](https://openairdocs.org/sdr/UPS00233381.md): Seat Track · damaged · Jun 10, 2000 · N917UP · Boeing 72730C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C, SEAT TRACK DAMAGED AT FRAME STA 500 AND BL RIGHT 0.5. REPLACED SEAT TRACK FROM BS 500 TO BS 550, RBL 0.5 IAW SRM 53-10-5 FIG 7. MATERIAL USED (P/N BAC1520-1331).
- [SDR UPS00233380](https://openairdocs.org/sdr/UPS00233380.md): Seat Track · worn · Jun 10, 2000 · N917UP · Boeing 72730C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C, SEAT TRACK WORN AT BS 1130 AND LBL 45.5. REPLACED SEAT TRACK FROM BS 1110 - 1130, LBL 45.5. MATERIAL USED (P/N BAC1520251) IAW B727 SRM 53-10-5 PG 5.
- [SDR UPS00233386](https://openairdocs.org/sdr/UPS00233386.md): Skin · corroded · Jun 7, 2000 · N917UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C AT FS 680, STR 19L HAS BULGE AREA ON SKIN. PERFORMED LFEC, SKIN LOSS 30 PERCENT. INSTALLED REPAIR DOUBLER IAW SRM 53-3 0-3 & DRAWING 69-61590 SHEET 12. MATERIAL USED 2024-T3, 0.063, 6 INCHES X 12 INCHES.
- [SDR UPS99228689](https://openairdocs.org/sdr/UPS99228689.md): Stringer · cracked · Jan 30, 1999 · N917UP · Boeing 72730C · Wing, Longeron/Stringer
  > INSPECTION TYPE:C RT WING STA 629 STR 13 FWD LUG CRACKED. REPAIR CARRIED OUT IAW UPS EO B727-5710-0314.
- [SDR UPS99228622](https://openairdocs.org/sdr/UPS99228622.md): Fitting · corroded · Jan 29, 1999 · N917UP · Boeing 72730C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C SEAT TRACK ATTACH FITTING CORRODED AT BS 740 RBL 45. FITTING AT BS 740 RBL 45 REPLACED PER DWR NR 65C13724.
- [SDR UPS99228621](https://openairdocs.org/sdr/UPS99228621.md): Cap Assy · cracked · Jan 29, 1999 · N917UP · Boeing 72730C · APU Core Engine
  > INSPECTION TYPE:C APU COMBUSTION UNIT HAS CRACK ON CAP ASSY. COMBUSTION UNIT LINER ASSY REPLACED IAW MM CHP 49-30-22.
- [SDR UPS99228686](https://openairdocs.org/sdr/UPS99228686.md): Skin · damaged · Jan 27, 1999 · N917UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, RT BS 740 SKIN (STRINGERS 17 TO 22 INCLUSIVE AREA) HOLES ARE 2ND OVERSIZE. REPAIR CARRIED OUT IAW EO 99-03-001, UPS ENGINEERING FILE NR 5310-2098.
- [SDR UPS99228808](https://openairdocs.org/sdr/UPS99228808.md): Skin · corroded · Jan 26, 1999 · N917UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE-C, ON CORROSION REMOVAL, PER NRC 811973 & 812094 & EO B727-5330-0509Q, FROM LAP STR 4L AND STR 4R, BS 1120, CORROSION AND DISBOND FOUND ON CROWN SKIN AND DOUBLERS, BS 1090 TO 1130 RT AND BS 1100 TO 1130 LT STR 4. CORROSION OUT OF LIMITS. CROW
- [SDR UPS99228636](https://openairdocs.org/sdr/UPS99228636.md): Seat Track · corroded · Jan 26, 1999 · N917UP · Boeing 72730C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-C, TO FACILITATE REPAIR OF FRAME 848.95 SEAT TRACK BETWEEN BS 760-870 L BL 62.5 HAD TO BE REMOVED ON REMOVAL OF THIS SEAT TRACK SECTION IT WAS FOUND TO BE CORRODED. SEAT TRACK SECTION REPLACED IAW SRM 53-10-5 FIG 1 AND SRM 51-30-2.
- [SDR UPS99228809](https://openairdocs.org/sdr/UPS99228809.md): Spacer · cracked · Jan 25, 1999 · N917UP · Boeing 72730C · Trailing Edge Flaps
  > INSPECTION TYPE-C, NR 1 FLAP TRACK FWD ATTACH FITTING OUTBD AFT SPACER CRACKED. BOLT REMOVED AND NEW SPACER, BOLT, WASHER AND LOCKNUT INSTALLED IAW SRM 51-30-2 AND MM 20-80-01.
- [SDR UPS99228688](https://openairdocs.org/sdr/UPS99228688.md): Mount · corroded · Jan 25, 1999 · N917UP · Boeing 72730C · Engine Mount Section
  > INSPECTION TYPE:C ENGINE NR 1 PITTING CORROSION ON BIG MOUNT HOLES, SMALL HOLES OK. CORROSION ON MOUNT HOLES REMOVED IAW SMRO EO 99-03-002 REV 1 UPS ENGINEERING FILE NR 727-71-0078, BUSHINGS INSTALLED IAW SMRO EO 99-03-005 REV 1 UPS ENGINEERING FILE NR 727-71
- [SDR UPS99228687](https://openairdocs.org/sdr/UPS99228687.md): Mount · corroded · Jan 25, 1999 · N917UP · Boeing 72730C · Engine Mount Section
  > INSPECTION TYPE:C ENGINE NR 3 PITTING CORROSION ON MOUNT HOLES, FWD O/B, AFT I/B. CORROSION IN MOUNT HOLES REMOVED IAW SMRO EO 99-03-003 UPS ENGINEERING FILE NR 727-71-0077.
- [SDR UPS99228654](https://openairdocs.org/sdr/UPS99228654.md): Skin · corroded · Jan 25, 1999 · N917UP · Boeing 72730C · Horizontal Stabilizer, Plate/Skin
  > INSPECTION TYPE-C, CORROSION ON UPPER SKIN OF RT HORIZONTAL STABILIZER STAB STA 68. REMOVED CORROSION IAW SRM 51-10-6. REPAIRED AREA IAW SMRO EO 99-03-008 UPS ENGINEERING FILE NR 727-55-0383.
- [SDR UPS99228637](https://openairdocs.org/sdr/UPS99228637.md): Hinge · cracked · Jan 25, 1999 · N917UP · Boeing 72730C · Galley Doors
  > INSPECTION TYPE-C, CRACK (5MM) FOUND IN MID GALLEY DOOR HINGE FWD LOWER CUTOUT. REPAIR CARRIED OUT IAW EO B727-5330-1063 APPENDIX B.
- [SDR UPS99228624](https://openairdocs.org/sdr/UPS99228624.md): Bracket · cracked · Jan 25, 1999 · N917UP · Boeing 72730C · Engine Thrust Reverser
  > INSPECTION TYPE:C ENGINE NR 1 THRUST REV OUTER FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW MM 78-30-00.
- [SDR UPS99228623](https://openairdocs.org/sdr/UPS99228623.md): Bracket · cracked · Jan 25, 1999 · N917UP · Boeing 72730C · Engine Thrust Reverser
  > INSPECTION TYPE:C ENGINE NR 3 THRUST REV OUTER FAIRING MID AND AFT SUPPORT BRACKETS CRACKED. REPLACED BRACKETS IAW MM 78-30-00.
- [SDR UPS99228655](https://openairdocs.org/sdr/UPS99228655.md): Frame · cracked · Jan 23, 1999 · N917UP · Boeing 72730C · Fuselage Main, Frame
  > INSPECTION TYPE-C, CRACK AT FRAME STA 848.95 LT EMINATING FROM 4TH FASTENER HOLE ABOVE FLOOR. REPAIR CARRIED OUT TO FRAME AT STA 848.95 LT IAW SMRO EO 99-03-010 AND UPS EO B727-5310-5474 UPS ENGINEERING FILE NR 5310-2095.
- [SDR UPS99228740](https://openairdocs.org/sdr/UPS99228740.md): Skin · corroded · Jan 22, 1999 · N917UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE-C, CORROSION BETWEEN SKIN AND STIFFENER BS 1323 TO 1342, STRINGER 9L AND STRINGER 8L. REPAIRED IAW SMRO ENGINEERING ORDER 99-03-009, REF UPS ENGINEERING FILE NUMBER 727-53-2100.
- [SDR UPS99228639](https://openairdocs.org/sdr/UPS99228639.md): Rib · cracked · Jan 22, 1999 · N917UP · Boeing 72730C · Leading Edge Devices
  > INSPECTION TYPE-C, NR 6 L/E SLAT CRACK IN RIB 6 O/B OF FLAP ACTUATOR. AREA REPAIRED IAW SRM 57-50-03 FIG 9.
- [SDR UPS99228638](https://openairdocs.org/sdr/UPS99228638.md): Web · cracked · Jan 22, 1999 · N917UP · Boeing 72730C · Cargo/Baggage Doors
  > INSPECTION TYPE-C, DURING INSPECTION OF AFT CARGO DOOR STOP FITTINGS SUSPECT CRACK FOUND IN WEB, FWD OF AFT DOOR HINGE INSIDE DOOR WEB. REPLACED IAW SRM 51-30-02.
- [SDR UPS99228625](https://openairdocs.org/sdr/UPS99228625.md): Skin · cracked · Jan 22, 1999 · N917UP · Boeing 72730C · Leading Edge Devices
  > INSPECTION TYPE:C NR 3 LE KRUEGER FLAP HAS CRACK ON ANTI-ICE SKIN. CRACK STOP DRILLED IAW SRM 51-10-1.
- [SDR UPS99228429](https://openairdocs.org/sdr/UPS99228429.md): Frame · cracked · Jan 11, 1999 · N917UP · Boeing 72730C · Fuselage Main, Frame
  > INSPECTION TYPE-C, CRACK AT BS 930 LT FRAME. CRACK REPAIRED IAW DRAWING 65-80107 AND EO B727-5310-2611.
- [SDR UPS99228431](https://openairdocs.org/sdr/UPS99228431.md): Web · cracked · Jan 8, 1999 · N917UP · Boeing 72730C · Wing Miscellaneous Structure
  > INSPECTION TYPE-C, LT WING NR 4 LE SLAT AND O/B ACTUATOR WEB CRACKED. CRACK STOP DRILLED IAW SRM 51-10-1 AND REPAIRED IAW SRM 57-50-3.
- [SDR UPS99228640](https://openairdocs.org/sdr/UPS99228640.md): Bulkhead Fitting · cracked · Jan 7, 1999 · N917UP · Boeing 72730C · Fuselage Main, Bulkhead
  > INSPECTION TYPE-C, BS 740 FITTING CRACKED RIGHT HAND SIDE BS 740 RT BULKHEAD FORGING. REPLACED PER EO B727-5310-7477-D.
- [SDR UPS99228436](https://openairdocs.org/sdr/UPS99228436.md): Fitting · cracked · Jan 7, 1999 · N917UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CRACK EMANATING FROM FASTENER HOLE IN BS 870 LT FITTING AT FWD OUTBOARD FLANGE ABOVE STRINGER 9. REPAIR CARRIED OUT IAW APPENDIX C OF B727-5310-3057 AND DRAWING 65C3 5277.
- [SDR UPS99228435](https://openairdocs.org/sdr/UPS99228435.md): Fitting · cracked · Jan 7, 1999 · N917UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CRACK EMANATING FROM FASTENER HOLE IN BS 870 RT FITTING AT AFT O/B FLANGE ABOVE STRINGER 9. REPAIR CARRIED OUT IAW B727-5310-3057 AND DRAWING 65C35277.
- [SDR UPS99228434](https://openairdocs.org/sdr/UPS99228434.md): Web · cracked · Jan 6, 1999 · N917UP · Boeing 72730C · Nacelle/Pylon Structure
  > INSPECTION TYPE-C, CENTER ENGINE SUPPORT STRUCTURE SUSPECT CRACK ON WEB AT BS 1376 RT APPROX. NEW WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555.
- [SDR UPS99228433](https://openairdocs.org/sdr/UPS99228433.md): Web · cracked · Jan 6, 1999 · N917UP · Boeing 72730C · Nacelle/Pylon Structure
  > INSPECTION TYPE-C, CENTER ENGINE SUPPORT STRUCTURE SUSPECT CRACK ON WEB AT BS 1376 LT APPROX. NEW WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555.
- [SDR UPS99228432](https://openairdocs.org/sdr/UPS99228432.md): Skin · delaminated · Jan 5, 1999 · N917UP · Boeing 72730C · Spoilers
  > INSPECTION TYPE-C, NR 9 SPOILER PANEL LOWER SKIN DELAMINATED. REPAIRED IAW SRM 57-50-6 FIG 5.
- [SDR UPS97225364](https://openairdocs.org/sdr/UPS97225364.md): Light · loose · Dec 26, 1997 · N917UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE-N/A, UPON LANDING EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR FLICKERED NUMEROUS TIMES. FOUND EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY, OPS CHECK GOOD.
- [SDR UPS97223766](https://openairdocs.org/sdr/UPS97223766.md): Skin · cracked · Jul 3, 1997 · N917UP · Boeing 72730C · Wing, Plate/Skin
  > INSPECTION TYPE:C, RT WING L/E SKIN CRACKED ABOVE REFUELING PANEL SLAT STN 128 APROX. REPAIR CARRIED OUT I.A.W. SRM 57-30-4 FIG 4.
- [SDR UPS97223773](https://openairdocs.org/sdr/UPS97223773.md): Skin · delaminated · Jun 27, 1997 · N917UP · Boeing 72730C · Spoilers
  > INSPECTION TYPE:C, NR 7 SPOILER PANEL LWR SKIN IS DELAMINATED AT I/B AND IN AREA OF SMALL DOUBLER. NR 7 SPOILER REPAIRED I.A.W. EO C-5100-7322.
- [SDR UPS97223771](https://openairdocs.org/sdr/UPS97223771.md): Skin · delaminated · Jun 27, 1997 · N917UP · Boeing 72730C · Trailing Edge Flaps
  > INSPECTION TYPE:C, LT O/B MIDFLAP T/E IS DELAMINATED IN 3 AREAS ON UPPER AFT SKIN WEDGE. 3 AREAS OF THE LT O/B MIDFLAP T/E WERE REPAIRED I.A.W. EO C-5100-7 322.
- [SDR UPS97223769](https://openairdocs.org/sdr/UPS97223769.md): Web · cracked · Jun 27, 1997 · N917UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, CRACK AT FWD WALL OF LT WHEELWELL AT BS 870 LBL 56 AT RIVET. REPAIRED I.A.W. SRM 53-10-9 FIG 4.
- [SDR UPS97223768](https://openairdocs.org/sdr/UPS97223768.md): Stringer · damaged · Jun 27, 1997 · N917UP · Boeing 72730C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C TO AID IN REMOVAL OF STR 8 R END FITTING AT BS 1183. CUT STRINGER BETWEEN BS 1148 AND 1166. STRINGER REPAIRED I.A.W. SRM 53-10-3 FIG 3.
- [SDR UPS97223794](https://openairdocs.org/sdr/UPS97223794.md): Seat Track · corroded · Jun 26, 1997 · N917UP · Boeing 72730C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C, EVIDENCE OF CORROSION BETWEEN TRACK AND HORIZONTAL MEMBER BS 680 RBL 14. CORRODED BEYOND LIMITS I.A.W. SRM 53-10-1. TRACK REPAIRED IAW SRM 53-10-5 FIG 5.
- [SDR UPS97223779](https://openairdocs.org/sdr/UPS97223779.md): Ramp Skin · worn · Jun 26, 1997 · N917UP · Boeing 72730C · Engine Thrust Reverser
  > INSPECTION TYPE:C, NR 3 ENG THRUST REV LOWER DOOR RAMP SKIN WORN DUE TO CHAFFING OF SEAL REPAIRED I.A.W. EFIS AND RE ENGINE SUPP SRM 54-10-03 FIG 203.
- [SDR UPS97223776](https://openairdocs.org/sdr/UPS97223776.md): Ramp Skin · worn · Jun 26, 1997 · N917UP · Boeing 72730C · Engine Thrust Reverser
  > INSPECTION TYPE:C, NR 1 ENG T.REV LOWER DOOR INNER RAMP SKIN WORN DUE TO CHAFFING OF SEAL. REPAIR CARRIED OUT I.A.W. EFIS AND RE ENGINE SUPPLEMENT SRM 54-10-0 3 FIG 203.
- [SDR UPS97223775](https://openairdocs.org/sdr/UPS97223775.md): Skin · delaminated · Jun 26, 1997 · N917UP · Boeing 72730C · Spoilers
  > INSPECTION TYPE:C, NR 5 SPOILER PANEL HAS TWO SMALL AREAS OF DELAMINATION ON LWR SKIN AT O/B FWD END AND I/B MIDLE AT EDGE. NR 5 SPOILER PANEL REPAIRED I.A.W. EO C-5100-7322.

Next page: https://openairdocs.org/deregistered/N917UP-2006-08-23/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 = 'N917UP' AND deregistration_id = 'N917UP-2006-08-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N917UP-2006-08-23/reports

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